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Steven F. Udvar-Hazy Center: South hangar panorama, including Vought OS2U-3 Kingfisher seaplane, B-29 Enola Gay

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Steven F. Udvar-Hazy Center: South hangar panorama, including Vought OS2U-3 Kingfisher seaplane, B-29 Enola Gay
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Image by Chris Devers
Quoting Smithsonian National Air and Space Museum | Vought OS2U-3 Kingfisher:

The Kingfisher was the U.S. Navy’s primary ship-based, scout and observation aircraft during World War II. Revolutionary spot welding techniques gave it a smooth, non-buckling fuselage structure. Deflector plate flaps that hung from the wing’s trailing edge and spoiler-augmented ailerons functioned like extra flaps to allow slower landing speeds. Most OS2Us operated in the Pacific, where they rescued many downed airmen, including World War I ace Eddie Rickenbacker and the crew of his B-17 Flying Fortress.

In March 1942, this airplane was assigned to the battleship USS Indiana. It later underwent a six-month overhaul in California, returned to Pearl Harbor, and rejoined the Indiana in March 1944. Lt. j.g. Rollin M. Batten Jr. was awarded the Navy Cross for making a daring rescue in this airplane under heavy enemy fire on July 4, 1944.

Transferred from the United States Navy.

Manufacturer:
Vought-Sikorsky Aircraft Division

Date:
1937

Country of Origin:
United States of America

Dimensions:
Overall: 15ft 1 1/8in. x 33ft 9 1/2in., 4122.6lb., 36ft 1 1/16in. (460 x 1030cm, 1870kg, 1100cm)

Materials:
Wings covered with fabric aft of the main spar

Physical Description:
Two-seat monoplane, deflector plate flaps hung from the trailing edge of the wing, ailerons drooped at low airspeeds to function like extra flaps, spoilers.

• • • • •

Quoting Smithsonian National Air and Space Museum | Boeing B-29 Superfortress "Enola Gay":

Boeing’s B-29 Superfortress was the most sophisticated propeller-driven bomber of World War II and the first bomber to house its crew in pressurized compartments. Although designed to fight in the European theater, the B-29 found its niche on the other side of the globe. In the Pacific, B-29s delivered a variety of aerial weapons: conventional bombs, incendiary bombs, mines, and two nuclear weapons.

On August 6, 1945, this Martin-built B-29-45-MO dropped the first atomic weapon used in combat on Hiroshima, Japan. Three days later, Bockscar (on display at the U.S. Air Force Museum near Dayton, Ohio) dropped a second atomic bomb on Nagasaki, Japan. Enola Gay flew as the advance weather reconnaissance aircraft that day. A third B-29, The Great Artiste, flew as an observation aircraft on both missions.

Transferred from the United States Air Force.

Manufacturer:
Boeing Aircraft Co.
Martin Co., Omaha, Nebr.

Date:
1945

Country of Origin:
United States of America

Dimensions:
Overall: 900 x 3020cm, 32580kg, 4300cm (29ft 6 5/16in. x 99ft 1in., 71825.9lb., 141ft 15/16in.)

Materials:
Polished overall aluminum finish

Physical Description:
Four-engine heavy bomber with semi-monoqoque fuselage and high-aspect ratio wings. Polished aluminum finish overall, standard late-World War II Army Air Forces insignia on wings and aft fuselage and serial number on vertical fin; 509th Composite Group markings painted in black; "Enola Gay" in black, block letters on lower left nose.

Nile Crocodile
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Image by wallygrom
These crocodiles were living in an enclosed lagoon at the Kaleta Reserve near Amboasary in southern Madagascar.

From Wikipedia –

The Nile Crocodile (Crocodylus niloticus) is an African crocodile which is common in Somalia, Ethiopia, Uganda, Kenya, Egypt, Zambia and Zimbabwe.

In antiquity, Nile crocodiles occurred in the Nile delta and the Zarqa River (Jordan), and they are recorded by Herodotus to have inhabited Lake Moeris. They are thought to have become extinct in the Seychelles in the early 19th century. It is known from fossil remains that they once inhabited Lake Edward. The Nile crocodile’s current range of distribution extends from the Senegal River, Lake Chad, Wadai and the Sudan to the Cunene and the Okavango Delta.

In Madagascar, crocodiles occur in the western and southern parts from Sembirano to Port Dauphin. They have occasionally been spotted in Zanzibar and the Comoros. Until recently, many permanent waters in the Sahara still housed relict populations.

In West Africa, Nile crocodiles are found most frequently in coastal lagoons, estuaries, and in the rivers bordering the equatorial forest belt. In East Africa, they are found mostly in rivers, lakes, marshes, and dams. They have been known to enter the sea in some areas, with one specimen having been seen 11 km off St Lucia Bay in 1917. In Madagascar, they have adapted to living in caves.

Nile Crocodiles have a dark bronze colouration above, with black spots on the back and a dirty purple on the belly. The flanks, which are yellowish green in colour, have dark patches arranged in oblique stripes. There is some variation relative to environment; specimens from swift flowing waters tend to be lighter in colour than those dwelling in lakes or swamps. They have green eyes.

Like all crocodiles, they are quadrupeds with four short, splayed legs; long, powerful tails; a scaly hide with rows of ossified scutes running down their back and tail; and powerful jaws. They have nictitating membranes to protect their eyes and have lachrymal glands, and can cleanse their eyes with tears.

Nostrils, eyes, and ears are situated on the tops of their head, so the rest of the body can remain concealed underwater. Their coloration also helps them hide: Juveniles are grey, multicoloured, or brown; with darker cross-bands on their tail and body. As they mature they become darker and the cross-bands fade, especially those on the body. The underbelly is yellowish, and makes high-quality leather.

They normally crawl along on their bellies, but they can also "high walk" with their trunks raised above the ground. Smaller specimens can gallop, and even larger crocodiles are capable of surprising bursts of speeds, briefly reaching up to 12 to 14 km/h (7.5 to 8.5 mi/h). They can swim much faster by moving their body and tail in a sinuous fashion, and they can sustain this form of movement much longer at about 30 to 35 km/h (18 to 22 mi/h).

They have a three-chambered heart which is often mistaken as four-chambered due to an elongated cardiac septum, which is physiologically similar to the four chambered heart of a bird, which is especially efficient at oxygenating their blood. They normally dive for only a couple of minutes, but will stay underwater for up to 30 minutes if threatened, and if they remain inactive they can hold their breath for up to 2 hours. They have an ectothermic metabolism, so they can survive a long time between meals — though when they do eat, they can eat up to half their body weight at a time.

They have a rich vocal range, and good hearing. Their skin has a number of poorly-understood integumentary sense organs (ISOs), that may react to changes in water pressure.

The bite force exerted by an adult Nile crocodile has been shown by Dr Brady Barr to measure 5,000 lbf (22 kN). However, the muscles responsible for opening the mouth are exceptionally weak, allowing a man to easily hold them shut with a small amount of force. Their mouths are filled with a total of 64 to 68 cone-shaped teeth. On each side of the mouth, there are 5 teeth in the front of the upper jaw (the premaxilla), 13 or 14 in the rest of the upper jaw (the maxilla), and 14 or 15 on either side of the lower jaw (the mandible). Hatchlings quickly lose a hardened piece of skin on the top of their mouth called the egg tooth, which they use to break through their egg’s shell at birth.

Outside water crocodiles can meet concurrence with other dominant Savanna predators, notably felines such as lions and leopards. Occasionally, both will hunt and prey on each other, depending on size, if regular food becomes scarce.

From the 1940s to the 1960s, the Nile crocodile was hunted, primarily for high-quality leather, though also for meat and purported curative properties. The population was severely depleted, and the species faced extinction. National laws, and international trade regulations have resulted in a resurgence in many areas, and the species as a whole is no longer threatened with extinction. Crocodile ‘protection programs’ are artificial environments where crocodiles exist safely and without the threat of extermination from hunters.

There are an estimated 250,000 to 500,000 individuals in the wild. The Nile crocodile is also widely distributed, with strong, documented populations in many countries in east and southern Africa, including Somalia, Ethiopia, Kenya, Zambia and Zimbabwe. Successful sustainable-yield programs focused on ranching crocodiles for their skins have been successfully implemented in this area, and even countries with quotas are moving toward ranching. In 1993, 80,000 Nile crocodile skins were produced, the majority from ranches in Zimbabwe and South Africa.

The situation is more grim in central and west Africa, which make up about two-thirds of the Nile crocodile’s habitat. The crocodile population in this area is much more sparse, and has not been adequately surveyed. While the natural population of Nile crocodiles in these areas may be lower due to a less-than-ideal environment and competition with sympatric slender-snouted and dwarf crocodiles, extirpation may be a serious threat in some of these areas. Additional factors are a loss of wetland habitats, and hunting in the 1970s. Additional ecological surveys and establishing management programs are necessary to resolve this.

The Nile crocodile is the top predator in its environment, and is responsible for checking the population of species like the barbel catfish, a predator that can overeat fish populations that other species, like birds, depend on. The Nile crocodile also consumes dead animals that would otherwise pollute the waters. The primary threat to Nile crocodiles, in turn, are humans. While illegal poaching is no longer a problem, they are threatened by pollution, hunting, and accidental entanglement in fishing nets.

Much of the hunting stems from their reputation as a man-eater, which is not entirely unjustified. Unlike other "man-eating" crocodiles, like the salties, the Nile crocodile lives in close proximity to human populations, so contact is more frequent. While there are no solid numbers, the Nile crocodile probably kills a couple of hundred people a year, which is more than all the other crocodiles combined. Some estimates put the number of annual victims in the thousands.

The Conservation Status of the Nile crocodile under the 1996 World Conservation Union (IUCN) Red List is "Lower Risk" (Lrlc). The Convention on International Trade in Endangered Species of Wild Fauna and Flora (CITES) lists the Nile crocodile under Appendix I (threatened with extinction) in most of its range; and under Appendix II (not threatened, but trade must be controlled) in the remainder, which either allows ranching or sets an annual quota of skins taken from the wild.

Acai berries will not help you lose weight
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Image by Jodiepedia
This image is probably being used to advertise a product containing acai berries for weight loss. Unfortunately the person who’s used this image is trying to sell you a product that doesn’t actually work, beyond making them some money. I wrote this description in the hope of highlighting this, see this page for more info brodiesnotes.blogspot.com/2011/07/update-on-skeptical-sne…

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KC-130 Aerial Refueling Tankers Practicing Touch and Goes At Davis-Monthan AFB in Tucson, AZ Feb 18, 2016 <<>> P1010591 – Version 2
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Image by Chic Bee
Lockheed C-130 Hercules
From Wikipedia, the free encyclopedia

en.wikipedia.org/wiki/Lockheed_C-130_Hercules

C-130 Hercules
Straight-wing, four-engine turboprop-driven aircraft overflying water
USAF C-130E
Role: Military transport aircraft
National origin: United States
ManufacturerLockheed
Lockheed Martin
First flight23 August 1954
Status: In service
Primary users:
United States Air Force
United States Marine Corps
Royal Air Force
Royal Canadian Air Force
Produced: 1954–present
Number built: Over 2,500 as of 2015[1]
Unit cost
C-130E .9 million[2]
C-130H .1 million[3]
Variants:
AC-130 Spectre/Spooky
Lockheed DC-130
Lockheed EC-130
Lockheed HC-130
Lockheed Martin KC-130
Lockheed LC-130
Lockheed MC-130
Lockheed WC-130
Lockheed L-100 Hercules
Developed into: Lockheed Martin C-130J Super Hercules

The Lockheed C-130 Hercules is a four-engine turboprop military transport aircraft designed and built originally by Lockheed, now Lockheed Martin.

Capable of using unprepared runways for takeoffs and landings, the C-130 was originally designed as a troop, medivac, and cargo transport aircraft. The versatile airframe has found uses in a variety of other roles, including as a gunship (AC-130),for
airborne assault,
search and rescue,
scientific research support,
weather reconnaissance,
aerial refueling,
maritime patrol, and
aerial firefighting.

It is now the main tactical airlifter for many military forces worldwide. Over forty models and variants of the Hercules, including a civilian one marketed as Lockheed L-100, operate in more than sixty nations.

The C-130 entered service with the U.S. in the 1950s, followed by Australia and others. During its years of service, the Hercules family has participated in numerous military, civilian and humanitarian aid operations. In 2007, the C-130 became the fifth aircraft—after the English Electric Canberra, B-52 Stratofortress, Tu-95, and KC-135 Stratotanker—to mark 50 years of continuous service with its original primary customer, in this case, the United States Air Force. The C-130 Hercules is the longest continuously produced military aircraft at over 60 years, with the updated C-130J Super Hercules being produced today.[4]

Contents [hide]
1Design and development
1.1Background and requirements
1.2Design phase
1.3Improved versions
1.4More improvements
1.5Later models
1.6Next generation
1.7Upgrades and changes
1.8Replacement
2Operational history
2.1Military
2.2Civilian
3Variants
4Operators
5Accidents
6Aircraft on display
6.1Australia
6.2Canada
6.3Colombia
6.4Indonesia
6.5Norway
6.6Saudi Arabia
6.7United Kingdom
6.8United States
7Specifications (C-130H)
8See also
9References
10External links
Design and development[edit]

This section needs additional citations for verification. Please help improve this article by adding citations to reliable sources. Unsourced material may be challenged and removed. (February 2014)
Background and requirements[edit]

The Korean War, which began in June 1950, showed that World War II-era piston-engine transports—Fairchild C-119 Flying Boxcars, Douglas C-47 Skytrains and Curtiss C-46 Commandos—were inadequate for modern warfare. Thus, on 2 February 1951, the United States Air Force issued a General Operating Requirement (GOR) for a new transport to Boeing, Douglas, Fairchild, Lockheed, Martin, Chase Aircraft, North American, Northrop, and Airlifts Inc. The new transport would have a capacity of 92 passengers, 72 combat troops or 64 paratroopers in a cargo compartment that was approximately 41 feet (12 m) long, 9 feet (2.7 m) high, and 10 feet (3.0 m) wide. Unlike transports derived from passenger airliners, it was to be designed from the ground-up as a combat transport with loading from a hinged loading ramp at the rear of the fuselage.

A key feature was the introduction of the Allison T56 turboprop powerplant, first developed specifically for the C-130. At the time, the turboprop was a new application of turbine engines that used exhaust gases to turn a propeller, which offered greater range at propeller-driven speeds compared to pure turbojets, which were faster but consumed more fuel. As was the case on helicopters of that era, such as the UH-1 Huey, turboshafts produced much more power for their weight than piston engines. Lockheed would subsequently use the same engines and technology in the Lockheed L-188 Electra. That aircraft failed financially in its civilian configuration but was successfully adapted into the Lockheed P-3 Orion maritime patrol and submarine attack aircraft where the efficiency and endurance of turboprops excelled.

Design phase[edit]
The Hercules resembled a larger four-engine brother to the C-123 Provider with a similar wing and cargo ramp layout that evolved from the Chase XCG-20 Avitruc, which in turn, was first designed and flown as a cargo glider in 1947.[5] The Boeing C-97 Stratofreighter also had a rear ramp, which made it possible to drive vehicles onto the plane (also possible with forward ramp on a C-124). The ramp on the Hercules was also used to airdrop cargo, which included low-altitude extraction for Sheridan tanks and even dropping large improvised "daisy cutter" bombs.

The new Lockheed cargo plane design possessed a range of 1,100 nmi (1,270 mi; 2,040 km), takeoff capability from short and unprepared strips, and the ability to fly with one engine shut down. Fairchild, North American, Martin, and Northrop declined to participate. The remaining five companies tendered a total of ten designs: Lockheed two, Boeing one, Chase three, Douglas three, and Airlifts Inc. one. The contest was a close affair between the lighter of the two Lockheed (preliminary project designation L-206) proposals and a four-turboprop Douglas design.

The Lockheed design team was led by Willis Hawkins, starting with a 130-page proposal for the Lockheed L-206.[6] Hall Hibbard, Lockheed vice president and chief engineer, saw the proposal and directed it to Kelly Johnson, who did not care for the low-speed, unarmed aircraft, and remarked, "If you sign that letter, you will destroy the Lockheed Company."[6] Both Hibbard and Johnson signed the proposal and the company won the contract for the now-designated Model 82 on 2 July 1951.[7]

The first flight of the YC-130 prototype was made on 23 August 1954 from the Lockheed plant in Burbank, California. The aircraft, serial number 53-3397, was the second prototype, but the first of the two to fly. The YC-130 was piloted by Stanley Beltz and Roy Wimmer on its 61-minute flight to Edwards Air Force Base; Jack Real and Dick Stanton served as flight engineers. Kelly Johnson flew chase in a Lockheed P2V Neptune.[8]

After the two prototypes were completed, production began in Marietta, Georgia, where over 2,300 C-130s have been built through 2009.[9]

The initial production model, the C-130A, was powered by Allison T56-A-9 turboprops with three-blade propellers and originally equipped with the blunt nose of the prototypes. Deliveries began in December 1956, continuing until the introduction of the C-130B model in 1959. Some A-models were equipped with skis and re-designated C-130D.

As the C-130A became operational with Tactical Air Command (TAC), the C-130’s lack of range became apparent and additional fuel capacity was added in the form of external pylon-mounted tanks at the end of the wings.

Improved versions[edit]

A Michigan Air National Guard C-130E dispatches its flares during a low-level training mission
The C-130B model was developed to complement the A-models that had previously been delivered, and incorporated new features, particularly increased fuel capacity in the form of auxiliary tanks built into the center wing section and an AC electrical system. Four-bladed Hamilton Standard propellers replaced the Aeroproducts three-blade propellers that distinguished the earlier A-models. The C-130B had ailerons with increased boost—3,000 psi (21 MPa) versus 2,050 psi (14 MPa)—as well as uprated engines and four-blade propellers that were standard until the J-model’s introduction.

An electronic reconnaissance variant of the C-130B was designated C-130B-II. A total of 13 aircraft were converted. The C-130B-II was distinguished by its false external wing fuel tanks, which were disguised signals intelligence (SIGINT) receiver antennas. These pods were slightly larger than the standard wing tanks found on other C-130Bs. Most aircraft featured a swept blade antenna on the upper fuselage, as well as extra wire antennas between the vertical fin and upper fuselage not found on other C-130s. Radio call numbers on the tail of these aircraft were regularly changed so as to confuse observers and disguise their true mission.

The extended-range C-130E model entered service in 1962 after it was developed as an interim long-range transport for the Military Air Transport Service. Essentially a B-model, the new designation was the result of the installation of 1,360 US gal (5,150 L) Sargent Fletcher external fuel tanks under each wing’s midsection and more powerful Allison T56-A-7A turboprops. The hydraulic boost pressure to the ailerons was reduced back to 2050 psi as a consequence of the external tanks’ weight in the middle of the wingspan. The E model also featured structural improvements, avionics upgrades and a higher gross weight. Australia took delivery of 12 C130E Hercules during 1966–67 to supplement the 12 C-130A models already in service with the RAAF. Sweden and Spain fly the TP-84T version of the C-130E fitted for aerial refueling capability.

The KC-130 tankers, originally C-130F procured for the US Marine Corps (USMC) in 1958 (under the designation GV-1) are equipped with a removable 3,600 US gal (13,626 L) stainless steel fuel tank carried inside the cargo compartment. The two wing-mounted hose and drogue aerial refueling pods each transfer up to 300 US gal per minute (19 L per second) to two aircraft simultaneously, allowing for rapid cycle times of multiple-receiver aircraft formations, (a typical tanker formation of four aircraft in less than 30 minutes). The US Navy’s C-130G has increased structural strength allowing higher gross weight operation.

More improvements[edit]

Royal Australian Air Force C-130H, 2007
The C-130H model has updated Allison T56-A-15 turboprops, a redesigned outer wing, updated avionics and other minor improvements. Later H models had a new, fatigue-life-improved, center wing that was retrofitted to many earlier H-models. For structural reasons, some models are required to land with certain amounts of fuel when carrying heavy cargo, reducing usable range.[10] The H model remains in widespread use with the United States Air Force (USAF) and many foreign air forces. Initial deliveries began in 1964 (to the RNZAF), remaining in production until 1996. An improved C-130H was introduced in 1974, with Australia purchasing 12 of type in 1978 to replace the original 12 C-130A models, which had first entered RAAF Service in 1958.

The United States Coast Guard employs the HC-130H for long-range search and rescue, drug interdiction, illegal migrant patrols, homeland security, and logistics.

C-130H models produced from 1992 to 1996 were designated as C-130H3 by the USAF. The "3" denoting the third variation in design for the H series. Improvements included ring laser gyros for the INUs, GPS receivers, a partial glass cockpit (ADI and HSI instruments), a more capable APN-241 color radar, night vision device compatible instrument lighting, and an integrated radar and missile warning system. The electrical system upgrade included Generator Control Units (GCU) and Bus Switching units (BSU)to provide stable power to the more sensitive upgraded components.[citation needed]

Royal Air Force C-130K (C.3)
The equivalent model for export to the UK is the C-130K, known by the Royal Air Force (RAF) as the Hercules C.1. The C-130H-30 (Hercules C.3 in RAF service) is a stretched version of the original Hercules, achieved by inserting a 100 in (2.54 m) plug aft of the cockpit and an 80 in (2.03 m) plug at the rear of the fuselage. A single C-130K was purchased by the Met Office for use by its Meteorological Research Flight, where it was classified as the Hercules W.2. This aircraft was heavily modified (with its most prominent feature being the long red and white striped atmospheric probe on the nose and the move of the weather radar into a pod above the forward fuselage). This aircraft, named Snoopy, was withdrawn in 2001 and was then modified by Marshall of Cambridge Aerospace as flight-testbed for the A400M turbine engine, the TP400. The C-130K is used by the RAF Falcons for parachute drops. Three C-130K (Hercules C Mk.1P) were upgraded and sold to the Austrian Air Force in 2002.[11]

Later models[edit]
The MC-130E Combat Talon was developed for the USAF during the Vietnam War to support special operations missions in Southeast Asia, and led to both the MC-130H Combat Talon II as well as a family of other special missions aircraft. 37 of the earliest models currently operating with the Air Force Special Operations Command (AFSOC) are scheduled to be replaced by new-production MC-130J versions. The EC-130 Commando Solo is another special missions variant within AFSOC, albeit operated solely by an AFSOC-gained wing in the Pennsylvania Air National Guard, and is a psychological operations/information operations (PSYOP/IO) platform equipped as an aerial radio station and television stations able to transmit messaging over commercial frequencies. Other versions of the EC-130, most notably the EC-130H Compass Call, are also special variants, but are assigned to the Air Combat Command (ACC). The AC-130 gunship was first developed during the Vietnam War to provide close air support and other ground-attack duties.

USAF HC-130P refuels a HH-60G Pavehawk helicopter
The HC-130 is a family of long-range search and rescue variants used by the USAF and the U.S. Coast Guard. Equipped for deep deployment of Pararescuemen (PJs), survival equipment, and (in the case of USAF versions) aerial refueling of combat rescue helicopters, HC-130s are usually the on-scene command aircraft for combat SAR missions (USAF only) and non-combat SAR (USAF and USCG). Early USAF versions were also equipped with the Fulton surface-to-air recovery system, designed to pull a person off the ground using a wire strung from a helium balloon. The John Wayne movie The Green Berets features its use. The Fulton system was later removed when aerial refueling of helicopters proved safer and more versatile. The movie The Perfect Storm depicts a real life SAR mission involving aerial refueling of a New York Air National Guard HH-60G by a New York Air National Guard HC-130P.

The C-130R and C-130T are U.S. Navy and USMC models, both equipped with underwing external fuel tanks. The USN C-130T is similar, but has additional avionics improvements. In both models, aircraft are equipped with Allison T56-A-16 engines. The USMC versions are designated KC-130R or KC-130T when equipped with underwing refueling pods and pylons and are fully night vision system compatible.

The RC-130 is a reconnaissance version. A single example is used by the Islamic Republic of Iran Air Force, the aircraft having originally been sold to the former Imperial Iranian Air Force.

The Lockheed L-100 (L-382) is a civilian variant, equivalent to a C-130E model without military equipment. The L-100 also has two stretched versions.

Next generation[edit]
Main article: Lockheed Martin C-130J Super Hercules
In the 1970s, Lockheed proposed a C-130 variant with turbofan engines rather than turboprops, but the U.S. Air Force preferred the takeoff performance of the existing aircraft. In the 1980s, the C-130 was intended to be replaced by the Advanced Medium STOL Transport project. The project was canceled and the C-130 has remained in production.

Building on lessons learned, Lockheed Martin modified a commercial variant of the C-130 into a High Technology Test Bed (HTTB). This test aircraft set numerous short takeoff and landing performance records and significantly expanded the database for future derivatives of the C-130.[12] Modifications made to the HTTB included extended chord ailerons, a long chord rudder, fast-acting double-slotted trailing edge flaps, a high-camber wing leading edge extension, a larger dorsal fin and dorsal fins, the addition of three spoiler panels to each wing upper surface, a long-stroke main and nose landing gear system, and changes to the flight controls and a change from direct mechanical linkages assisted by hydraulic boost, to fully powered controls, in which the mechanical linkages from the flight station controls operated only the hydraulic control valves of the appropriate boost unit.[13] The HTTB first flew on 19 June 1984, with civil registration of N130X. After demonstrating many new technologies, some of which were applied to the C-130J, the HTTB was lost in a fatal accident on 3 February 1993, at Dobbins Air Reserve Base, in Marietta, Georgia.[14] The crash was attributed to disengagement of the rudder fly-by-wire flight control system, resulting in a total loss of rudder control capability while conducting ground minimum control speed tests (Vmcg). The disengagement was a result of the inadequate design of the rudder’s integrated actuator package by its manufacturer; the operator’s insufficient system safety review failed to consider the consequences of the inadequate design to all operating regimes. A factor which contributed to the accident was the flight crew’s lack of engineering flight test training.[15]

In the 1990s, the improved C-130J Super Hercules was developed by Lockheed (later Lockheed Martin). This model is the newest version and the only model in production. Externally similar to the classic Hercules in general appearance, the J model has new turboprop engines, six-bladed propellers, digital avionics, and other new systems.[16]

Upgrades and changes[edit]
In 2000, Boeing was awarded a US.4 billion contract to develop an Avionics Modernization Program kit for the C-130. The program was beset with delays and cost overruns until project restructuring in 2007.[17] On 2 September 2009, Bloomberg news reported that the planned Avionics Modernization Program (AMP) upgrade to the older C-130s would be dropped to provide more funds for the F-35, CV-22 and airborne tanker replacement programs.[18] However, in June 2010, Department of Defense approved funding for the initial production of the AMP upgrade kits.[19][20] Under the terms of this agreement, the USAF has cleared Boeing to begin low-rate initial production (LRIP) for the C-130 AMP. A total of 198 aircraft are expected to feature the AMP upgrade. The current cost per aircraft is US million although Boeing expects that this price will drop to US million for the 69th aircraft.[17]

An engine enhancement program saving fuel and providing lower temperatures in the T56 engine has been approved, and the US Air Force expects to save billion and extend the fleet life.[21]

Replacement[edit]
In October 2010, the Air Force released a capabilities request for information (CRFI) for the development of a new airlifter to replace the C-130. The new aircraft is to carry a 190 percent greater payload and assume the mission of mounted vertical maneuver (MVM). The greater payload and mission would enable it to carry medium-weight armored vehicles and drop them off at locations without long runways. Various options are being considered, including new or upgraded fixed-wing designs, rotorcraft, tiltrotors, or even an airship. Development could start in 2014, and become operational by 2024. The C-130 fleet of around 450 planes would be replaced by only 250 aircraft.[22] The Air Force had attempted to replace the C-130 in the 1970s through the Advanced Medium STOL Transport project, which resulted in the C-17 Globemaster III that instead replaced the C-141 Starlifter.[23] The Air Force Research Laboratory funded Lockheed and Boeing demonstrators for the Speed Agile concept, which had the goal of making a STOL aircraft that can take off and land at speeds as low as 70 kn (130 km/h; 81 mph) on airfields less than 2,000 ft (610 m) long and cruise at Mach 0.8-plus. Boeing’s design used upper-surface blowing from embedded engines on the inboard wing and blown flaps for circulation control on the outboard wing. Lockheed’s design also used blown flaps outboard, but inboard used patented reversing ejector nozzles. Boeing’s design completed over 2,000 hours of windtunnel tests in late 2009. It was a 5 percent-scale model of a narrowbody design with a 55,000 lb (25,000 kg) payload. When the AFRL increased the payload requirement to 65,000 lb (29,000 kg), they tested a 5% scale model of a widebody design with a 303,000 lb (137,000 kg) take-off gross weight and an "A400M-size" 158 in (4.0 m) wide cargo box. It would be powered by four IAE V2533 turbofans.[24] In August 2011, the AFRL released pictures of the Lockheed Speed Agile concept demonstrator. A 23% scale model went through wind tunnel tests to demonstrate its hybrid powered lift, which combines a low drag airframe with simple mechanical assembly to reduce weight and better aerodynamics. The model had four engines, including two Williams FJ44 turbofans.[23][25] On 26 March 2013, Boeing was granted a patent for its swept-wing powered lift aircraft.[26]

As of January 2014, Air Mobility Command, Air Force Materiel Command and the Air Force Research Lab are in the early stages of defining requirements for the C-X next generation airlifter program to replace both the C-130 and C-17. An aircraft would be produced from the early 2030s to the 2040s. If requirements are decided for operating in contested airspace, Air Force procurement of C-130s would end by the end of the decade to not have them serviceable by the 2030s and operated when they can’t perform in that environment. Development of the airlifter depends heavily on the Army’s "tactical and operational maneuver" plans. Two different cargo planes could still be created to separately perform tactical and strategic missions, but which course to pursue is to be decided before C-17s need to be retired.[27]

Operational history[edit]

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Military[edit]

USMC KC-130F Hercules performing takeoffs and landings aboard the aircraft carrier Forrestal in 1963. The aircraft is now displayed at the National Museum of Naval Aviation.
The first production aircraft, C-130As were first delivered beginning in 1956 to the 463d Troop Carrier Wing at Ardmore AFB, Oklahoma and the 314th Troop Carrier Wing at Sewart AFB, Tennessee. Six additional squadrons were assigned to the 322d Air Division in Europe and the 315th Air Division in the Far East. Additional aircraft were modified for electronics intelligence work and assigned to Rhein-Main Air Base, Germany while modified RC-130As were assigned to the Military Air Transport Service (MATS) photo-mapping division.

In 1958, a U.S. reconnaissance C-130A-II of the 7406th Support Squadron was shot down over Armenia by MiG-17s.[28]

Australia became the first non-American force to operate the C-130A Hercules with 12 examples being delivered from late 1958. These aircraft were fitted with AeroProducts three-blade, 15-foot diameter propellers. The Royal Canadian Air Force became another early user with the delivery of four B-models (Canadian designation C-130 Mk I) in October / November 1960.[29]

In 1963, a Hercules achieved and still holds the record for the largest and heaviest aircraft to land on an aircraft carrier.[30] During October and November that year, a USMC KC-130F (BuNo 149798), loaned to the U.S. Naval Air Test Center, made 29 touch-and-go landings, 21 unarrested full-stop landings and 21 unassisted take-offs on Forrestal at a number of different weights.[31] The pilot, LT (later RADM) James H. Flatley III, USN, was awarded the Distinguished Flying Cross for his role in this test series. The tests were highly successful, but the idea was considered too risky for routine "Carrier Onboard Delivery" (COD) operations. Instead, the Grumman C-2 Greyhound was developed as a dedicated COD aircraft. The Hercules used in the test, most recently in service with Marine Aerial Refueler Squadron 352 (VMGR-352) until 2005, is now part of the collection of the National Museum of Naval Aviation at NAS Pensacola, Florida.

In 1964, C-130 crews from the 6315th Operations Group at Naha Air Base, Okinawa commenced forward air control (FAC; "Flare") missions over the Ho Chi Minh Trail in Laos supporting USAF strike aircraft. In April 1965 the mission was expanded to North Vietnam where C-130 crews led formations of B-57 bombers on night reconnaissance/strike missions against communist supply routes leading to South Vietnam. In early 1966 Project Blind Bat/Lamplighter was established at Ubon RTAFB, Thailand. After the move to Ubon the mission became a four-engine FAC mission with the C-130 crew searching for targets then calling in strike aircraft. Another little-known C-130 mission flown by Naha-based crews was Operation Commando Scarf, which involved the delivery of chemicals onto sections of the Ho Chi Minh Trail in Laos that were designed to produce mud and landslides in hopes of making the truck routes impassable.[citation needed]

In November 1964, on the other side of the globe, C-130Es from the 464th Troop Carrier Wing but loaned to 322d Air Division in France, flew one of the most dramatic missions in history in the former Belgian Congo. After communist Simba rebels took white residents of the city of Stanleyville hostage, the U.S. and Belgium developed a joint rescue mission that used the C-130s to airlift and then drop and air-land a force of Belgian paratroopers to rescue the hostages. Two missions were flown, one over Stanleyville and another over Paulis during Thanksgiving weeks.[32] The headline-making mission resulted in the first award of the prestigious MacKay Trophy to C-130 crews.

In the Indo-Pakistani War of 1965, as a desperate measure the transport No. 6 Squadron of the Pakistan Air Force modified its entire small fleet of C-130Bs for use as heavy bombers, capable of carrying up to 20,000 lb (9,072 kg) of bombs on pallets. These improvised bombers were used to hit Indian targets such as bridges, heavy artillery positions, tank formations and troop concentrations.[33][34] Some C-130s even flew with anti-aircraft guns fitted on their ramp, apparently shooting down some 17 aircraft and damaging 16 others.[35]

The C-130 Hercules were used in the Battle of Kham Duc in 1968, when the North Vietnamese Army forced U.S.-led forces to abandon the Kham Duc Special Forces Camp.
In October 1968, a C-130Bs from the 463rd Tactical Airlift Wing dropped a pair of M-121 10,000 pound bombs that had been developed for the massive B-36 bomber but had never been used. The U.S. Army and U.S. Air Force resurrected the huge weapons as a means of clearing landing zones for helicopters and in early 1969 the 463rd commenced Commando Vault missions. Although the stated purpose of COMMANDO VAULT was to clear LZs, they were also used on enemy base camps and other targets.[citation needed]

During the late 1960s, the U.S. was eager to get information on Chinese nuclear capabilities. After the failure of the Black Cat Squadron to plant operating sensor pods near the Lop Nur Nuclear Weapons Test Base using a Lockheed U-2, the CIA developed a plan, named Heavy Tea, to deploy two battery-powered sensor pallets near the base. To deploy the pallets, a Black Bat Squadron crew was trained in the U.S. to fly the C-130 Hercules. The crew of 12, led by Col Sun Pei Zhen, took off from Takhli Royal Thai Air Force Base in an unmarked U.S. Air Force C-130E on 17 May 1969. Flying for six and a half hours at low altitude in the dark, they arrived over the target and the sensor pallets were dropped by parachute near Anxi in Gansu province. After another six and a half hours of low altitude flight, they arrived back at Takhli. The sensors worked and uploaded data to a U.S. intelligence satellite for six months, before their batteries wore out. The Chinese conducted two nuclear tests, on 22 September 1969 and 29 September 1969, during the operating life of the sensor pallets. Another mission to the area was planned as Operation Golden Whip, but was called off in 1970.[36] It is most likely that the aircraft used on this mission was either C-130E serial number 64-0506 or 64-0507 (cn 382-3990 and 382-3991). These two aircraft were delivered to Air America in 1964.[37] After being returned to the U.S. Air Force sometime between 1966 and 1970, they were assigned the serial numbers of C-130s that had been destroyed in accidents. 64-0506 is now flying as 62-1843, a C-130E that crashed in Vietnam on 20 December 1965 and 64-0507 is now flying as 63-7785, a C-130E that had crashed in Vietnam on 17 June 1966.[38]

The A-model continued in service through the Vietnam War, where the aircraft assigned to the four squadrons at Naha AB, Okinawa and one at Tachikawa Air Base, Japan performed yeoman’s service, including operating highly classified special operations missions such as the BLIND BAT FAC/Flare mission and FACT SHEET leaflet mission over Laos and North Vietnam. The A-model was also provided to the South Vietnamese Air Force as part of the Vietnamization program at the end of the war, and equipped three squadrons based at Tan Son Nhut AFB. The last operator in the world is the Honduran Air Force, which is still flying one of five A model Hercules (FAH 558, c/n 3042) as of October 2009.[39] As the Vietnam War wound down, the 463rd Troop Carrier/Tactical Airlift Wing B-models and A-models of the 374th Tactical Airlift Wing were transferred back to the United States where most were assigned to Air Force Reserve and Air National Guard units.

U.S. Marines disembark from C-130 transports at the Da Nang Airbase on 8 March 1965
Another prominent role for the B model was with the United States Marine Corps, where Hercules initially designated as GV-1s replaced C-119s. After Air Force C-130Ds proved the type’s usefulness in Antarctica, the U.S. Navy purchased a number of B-models equipped with skis that were designated as LC-130s. C-130B-II electronic reconnaissance aircraft were operated under the SUN VALLEY program name primarily from Yokota Air Base, Japan. All reverted to standard C-130B cargo aircraft after their replacement in the reconnaissance role by other aircraft.

The C-130 was also used in the 1976 Entebbe raid in which Israeli commando forces carried a surprise assault to rescue 103 passengers of an airliner hijacked by Palestinian and German terrorists at Entebbe Airport, Uganda. The rescue force — 200 soldiers, jeeps, and a black Mercedes-Benz (intended to resemble Ugandan Dictator Idi Amin’s vehicle of state) — was flown over 2,200 nmi (4,074 km; 2,532 mi) almost entirely at an altitude of less than 100 ft (30 m) from Israel to Entebbe by four Israeli Air Force (IAF) Hercules aircraft without mid-air refueling (on the way back, the planes refueled in Nairobi, Kenya).

During the Falklands War (Spanish: Guerra de las Malvinas) of 1982, Argentine Air Force C-130s undertook highly dangerous, daily re-supply night flights as blockade runners to the Argentine garrison on the Falkland Islands. They also performed daylight maritime survey flights. One was lost during the war. Argentina also operated two KC-130 tankers during the war, and these refueled both the Douglas A-4 Skyhawks and Navy Dassault-Breguet Super Étendards; some C-130s were modified to operate as bombers with bomb-racks under their wings. The British also used RAF C-130s to support their logistical operations.

USMC C-130T Fat Albert performing a rocket-assisted takeoff (RATO)
During the Gulf War of 1991 (Operation Desert Storm), the C-130 Hercules was used operationally by the U.S. Air Force, U.S. Navy and U.S. Marine Corps, along with the air forces of Australia, New Zealand, Saudi Arabia, South Korea and the UK. The MC-130 Combat Talon variant also made the first attacks using the largest conventional bombs in the world, the BLU-82 "Daisy Cutter" and GBU-43/B "Massive Ordnance Air Blast" bomb, (MOAB). Daisy Cutters were used to clear landing zones and to eliminate mine fields. The weight and size of the weapons make it impossible or impractical to load them on conventional bombers. The GBU-43/B MOAB is a successor to the BLU-82 and can perform the same function, as well as perform strike functions against hardened targets in a low air threat environment.

Since 1992, two successive C-130 aircraft named Fat Albert have served as the support aircraft for the U.S. Navy Blue Angels flight demonstration team. Fat Albert I was a TC-130G (151891),[40] while Fat Albert II is a C-130T (164763).[41] Although Fat Albert supports a Navy squadron, it is operated by the U.S. Marine Corps (USMC) and its crew consists solely of USMC personnel. At some air shows featuring the team, Fat Albert takes part, performing flyovers. Until 2009, it also demonstrated its rocket-assisted takeoff (RATO) capabilities; these ended due to dwindling supplies of rockets.[42]

The AC-130 also holds the record for the longest sustained flight by a C-130. From 22 to 24 October 1997, two AC-130U gunships flew 36 hours nonstop from Hurlburt Field Florida to Taegu (Daegu), South Korea while being refueled seven times by KC-135 tanker aircraft. This record flight shattered the previous record longest flight by over 10 hours while the two gunships took on 410,000 lb (190,000 kg) of fuel. The gunship has been used in every major U.S. combat operation since Vietnam, except for Operation El Dorado Canyon, the 1986 attack on Libya.[43]

C-130 Hercules performs a tactical landing on a dirt strip
During the invasion of Afghanistan in 2001 and the ongoing support of the International Security Assistance Force (Operation Enduring Freedom), the C-130 Hercules has been used operationally by Australia, Belgium, Canada, Denmark, France, Italy, the Netherlands, New Zealand, Norway, Portugal, South Korea, Spain, the UK and the United States.

During the 2003 invasion of Iraq (Operation Iraqi Freedom), the C-130 Hercules was used operationally by Australia, the UK and the United States. After the initial invasion, C-130 operators as part of the Multinational force in Iraq used their C-130s to support their forces in Iraq.

Since 2004, the Pakistan Air Force has employed C-130s in the War in North-West Pakistan. Some variants had forward looking infrared (FLIR Systems Star Safire III EO/IR) sensor balls, to enable close tracking of Islamist militants.[44]

Civilian[edit]

A C-130E fitted with a MAFFS-1 dropping fire retardant
The U.S. Forest Service developed the Modular Airborne FireFighting System for the C-130 in the 1970s, which allows regular aircraft to be temporarily converted to an airtanker for fighting wildfires.[45] In the late 1980s, 22 retired USAF C-130As were removed from storage at Davis-Monthan Air Force Base and transferred to the U.S. Forest Service who then sold them to six private companies to be converted into air tankers (see U.S. Forest Service airtanker scandal). After one of these aircraft crashed due to wing separation in flight as a result of fatigue stress cracking, the entire fleet of C-130A air tankers was permanently grounded in 2004 (see 2002 airtanker crashes). C-130s have been used to spread chemical dispersants onto the massive oil slick in the Gulf Coast in 2010.[46]

A recent development of a C-130–based airtanker is the Retardant Aerial Delivery System developed by Coulson Aviation USA . The system consists of a C-130H/Q retrofitted with an in-floor discharge system, combined with a removable 3,500- or 4,000-gallon water tank. The combined system is FAA certified.[47]

Variants[edit]

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C-130H Hercules flight deck

A U.S. JC-130 aircraft retrieving a reconnaissance satellite film capsule under parachute.

C-130s from the: U.S., Canada, Australia and Israel (foreground to background)

RAAF C-130J-30 at Point Cook, 2006

Brazilian Air Force C-130 (L-382)
For civilian versions, see Lockheed L-100 Hercules.
Significant military variants of the C-130 include:

C-130A/B/E/F/G/H/K/T
Tactical airlifter basic models
C-130A-II Dreamboat
Early version Electronic Intelligence/Signals Intelligence (ELINT/SIGINT) aircraft[48]
C-130J Super Hercules
Tactical airlifter, with new engines, avionics, and updated systems
C-130K
Designation for RAF Hercules C1/W2/C3 aircraft (C-130Js in RAF service are the Hercules C.4 and Hercules C.5)
AC-130A/E/H/J/U/W
Gunship variants
C-130D/D-6
Ski-equipped version for snow and ice operations United States Air Force / Air National Guard
CC-130E/H/J Hercules
Designation for Canadian Armed Forces / Royal Canadian Air Force Hercules aircraft. U.S. Air Force used the CC-130J designation to differentiate standard C-130Js from "stretched" C-130Js (Company designation C-130J-30s).
DC-130A/E/H
USAF and USN Drone control
EC-130
EC-130E/J Commando Solo – USAF / Air National Guard psychological operations version
EC-130E – Airborne Battlefield Command and Control Center (ABCCC)
EC-130E Rivet Rider – Airborne psychological warfare aircraft
EC-130H Compass Call – Electronic warfare and electronic attack.[49]
EC-130V – Airborne early warning and control (AEW&C) variant used by USCG for counter-narcotics missions[50]
GC-130
Permanently Grounded "Static Display"
HC-130
HC-130B/E/H – Early model combat search and rescue
HC-130P/N Combat King – USAF aerial refueling tanker and combat search and rescue
HC-130J Combat King II – Next generation combat search and rescue tanker
HC-130H/J – USCG long-range surveillance and search and rescue
JC-130
Temporary conversion for flight test operations
KC-130F/R/T/J
United States Marine Corps aerial refueling tanker and tactical airlifter
LC-130F/H/R
USAF / Air National Guard – Ski-equipped version for Arctic and Antarctic support operations; LC-130F previously operated by USN
MC-130
MC-130E/H Combat Talon I/II – Special operations infiltration/extraction variant
MC-130W Combat Spear/Dragon Spear – Special operations tanker/gunship[51]
MC-130P Combat Shadow – Special operations tanker
MC-130J Commando II (formerly Combat Shadow II) – Special operations tanker Air Force Special Operations Command[52]
YMC-130H – Modified aircraft under Operation Credible Sport for second Iran hostage crisis rescue attempt
NC-130
Permanent conversion for flight test operations
PC-130/C-130-MP
Maritime patrol
RC-130A/S
Surveillance aircraft for reconnaissance
SC-130J Sea Herc
Proposed maritime patrol version of the C-130J, designed for coastal surveillance and anti-submarine warfare.[53][54]
TC-130
Aircrew training
VC-130H
VIP transport
WC-130A/B/E/H/J
Weather reconnaissance ("Hurricane Hunter") version for USAF / Air Force Reserve Command’s 53d Weather Reconnaissance Squadron in support of the National Weather Service’s National Hurricane Center

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PACKARD 120 CONVERTIBLE COUPE (1939)
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Image by pedrosimoes7
Belem, Lisbon, Portugal

DESCRIPTION

Packard was an American luxury automobile marque built by the Packard Motor Car Company of Detroit, Michigan, United States.

The first Packard automobiles were produced in 1899, and the last Detroit-built Packard in 1956, when they built the Packard Predictor, their last concept car.

Packard bought Studebaker in 1953 and formed the Studebaker-Packard Corporation of South Bend, Indiana.

The 1957 and 1958 Packards were actually badge engineered Studebakers, built in South Bend.

HISTORY

1899–1905

Packard was founded by James Ward Packard, his brother William and their partner, George Lewis Weiss, in the city of Warren, Ohio, where 400 Packard automobiles were built at their factory on Dana Street Northeast, from 1899 to 1903.

A mechanical engineer, James Packard believed they could build a better horseless carriage than the Winton cars owned by Weiss, an important Winton stockholder, after Packard complained to Alexander Winton and offered suggestions for improvement, which were ignored.

Packard’s first car was built in Warren, Ohio, on November 6, 1899.

Henry Bourne Joy, a member of one of Detroit’s oldest and wealthiest families, bought a Packard. Impressed by its reliability, he visited the Packards and soon enlisted a group of investors—including Truman Handy Newberry and Russell A. Alger Jr.

On October 2, 1902, this group refinanced and renamed the New York and Ohio Automobile Company as the Packard Motor Car Company, with James Packard as president. Alger later served as vice president.

Packard moved operations to Detroit soon after, and Joy became general manager (and later chairman of the board). An original Packard, reputedly the first manufactured, was donated by a grateful James Packard to his alma mater, Lehigh University, and is preserved there in the Packard Laboratory.Another is on display at the Packard Museum in Warren, Ohio.

In the beginning, all Packards had a single-cylinder engine until 1903. Packard vehicles featured innovations, including the modern steering wheel and, years later, the first production 12-cylinder engine, adapted from developing the Liberty L-12, and air-conditioning in a passenger car. Packard produced its "Twin Six" model series of 12-cylinder cars from 1915 to 1923.

While the Black Motor Company’s Black went as low as 5, Western Tool Works’ Gale Model A roadster was 0, the high-volume Oldsmobile Runabout went for 0, and the Cole 30 and Cole Runabout were US,500,Packard concentrated on cars with prices starting at ,600.

The marque developed a following among wealthy purchasers both in the United States and abroad, competing with European marques like Rolls-Royce and Mercedes Benz.

The 3,500,000-square-foot (330,000 m2) Packard plant on East Grand Boulevard in Detroit was located on over 40 acres (16 ha) of land.

Designed by Albert Kahn Associates, it included an early use of reinforced concrete for an automotive factory when building #10 opened in early 1906.

Its skilled craftsmen practiced over 80 trades. The dilapidated plant still stands,despite repeated fires. The factory is in close proximity to the current General Motors Detroit/Hamtramck Assembly, which was the former site of the Dodge Vehicle factory from 1910 until 1980.

Architect Kahn also designed the Packard Proving Grounds in Shelby Township, Michigan.

1906–1930

From this beginning, through and beyond the 1930s, Packard-built vehicles were perceived as highly competitive among high-priced luxury American automobiles.

The company was commonly referred to as being one of the "Three Ps" of American motordom royalty, along with Pierce-Arrow of Buffalo, New York, and Peerless of Cleveland, Ohio.

For most of its history, Packard was guided by its President and General Manager James Alvan Macauley, who also served as President of the National Automobile Manufacturers Association.

Inducted into the Automobile Hall of Fame, Macauley made Packard the number one designer and producer of luxury automobiles in the United States. The marque was also highly competitive abroad, with markets in 61 countries. Gross income for the company was ,889,000 in 1928. Macauley was also responsible for the iconic Packard slogan, "Ask the Man Who Owns One".

In the 1920s, Packard exported more cars than any other in its price class, and in 1930, sold almost twice as many abroad as any other marque priced over 00.

In 1931, 10 Packards were owned by Japan’s royal family.

Between 1924 and 1930, Packard was also the top-selling luxury brand.

In addition to excellent luxury cars, Packard built trucks. A Packard truck carrying a three-ton load drove from New York City to San Francisco between 8 July and 24 August 1912. The same year, Packard had service depots in 104 cities.

The Packard Motor Corporation Building at Philadelphia, also designed by Albert Kahn, was built in 1910-1911. It was added to the National Register of Historic Places in 1980.

By 1931, Packards were also being produced in Canada.

1931–1936
Entering the 1930s, Packard attempted to beat the stock market crash and subsequent Great Depression by manufacturing ever more opulent and expensive cars than it had prior to October 1929.

While the Eight five-seater sedan had been the company’s top-seller for years, the Twin Six, designed by Vincent,[23] was introduced for 1932, with prices starting at ,650 (equal to 397 today) at the factory gate;] in 1933, it would be renamed the Packard Twelve, a name it retained for the remainder of its run (through 1939).

Also in 1931, Packard pioneered a system it called Ride Control, which made the hydraulic shock absorbers adjustable from within the car.

For one year only, 1932, Packard fielded an upper-medium-priced car, the Light Eight, at a base price of ,750, or 5 less than the standard Eight.

Rivals Cadillac and Lincoln benefited from the huge support structure of GM and Ford. Packard could not match the two automotive giants for resources, however the 1920s had proven extremely profitable for the company and it had assets of approximately million in 1932 while many luxury car manufacturers were almost broke.

Peerless ceased production in 1932, changing the Cleveland manufacturing plant from producing cars to brewing beer for Carling Black Label Beer. By 1938, Franklin, Marmon, Ruxton, Stearns-Knight, Stutz, Duesenberg, and Pierce-Arrow had all closed.

Packard also had one other advantage that some other luxury automakers did not: a single production line. By maintaining a single line and interchangeability between models, Packard was able to keep its costs down.

Packard did not change cars as often as other manufacturers did at the time. Rather than introducing new models annually, Packard began using its own "Series" formula for differentiating its model changeovers in 1923. New model series did not debut on a strictly annual basis, with some series lasting nearly two years, and others lasting as short a time as seven months. In the long run, though, Packard averaged around one new series per year.

By 1930, Packard automobiles were considered part of its Seventh Series. By 1942, Packard was in its Twentieth Series. The "Thirteenth Series" was omitted.

To address the Depression, Packard started producing more affordable cars in the medium price range.

This was a necessary step as the demand for hand-built luxury cars had diminished sharply and even people who could afford such vehicles were reluctant to be seen in them at a time when unemployment was higher than 20%.

In 1935, the company introduced its first car under 00, the 120. Sales more than tripled that year and doubled again in 1936.

To produce the 120, Packard built and equipped an entirely separate factory. By 1936, Packard’s labor force was divided nearly evenly between the high-priced "Senior" lines (Twelve, Super Eight, and Eight) and the medium-priced "Junior" models, although more than 10 times more Juniors were produced than Seniors.

This was because the 120 models were built using thoroughly modern mass production techniques, while the senior Packards used a great deal more hand labor and traditional craftsmanship.

Although Packard almost certainly could not have survived the Depression without the highly successful Junior models, they did have the effect of diminishing the Senior models’ exclusive image among those few who could still afford an expensive luxury car. The 120 models were more modern in basic design than the Senior models; for example, the 1935 Packard 120 featured independent front suspension and hydraulic brakes, features that would not appear on the Senior Packards until 1937.

During this time, Packards were built in Windsor, Ontario by the Packard Motor Company of Canada Ltd.

Production started in 1931, with the best year being 1937, with just over 2,500 cars built.Parts manufactured in Canada included tires, upholstery, radiator cores, headlamps, springs, wheels, while the engines were locally assembled.

Production ended in 1939, although the company maintained an office in Windsor for many years.

1937–1941

1939 (17th series) Twelve
Packard was still the premier luxury automobile, even though the majority of cars being built were the 120 and Super Eight model ranges. Hoping to catch still more of the market, Packard decided to issue the Packard 115C in 1937, which was powered by Packard’s first six-cylinder engine since the Fifth Series cars in 1928. The decision to introduce the "Packard Six", priced at around 00, was in time for the 1938 recession. This model also tagged Packards as something less exclusive than they had been in the public’s mind and in the long run hurt Packard’s reputation of building some of America’s finest luxury cars.

The Six, redesignated 110 in 1940–41, continued for three years after the war.

In 1939, Packard introduced Econo-Drive, a kind of overdrive, claimed able to reduce engine speed 27.8%; it could be engaged at any speed over 30 mph (48 km/h). The same year, the company introduced a fifth, transverse shock absorber and made column shift (known as Handishift) available on the 120 and Six.

1941

A new body shape was introduced for the 1941 the Packard Clipper. It was available only as a four-door model on the 127 in (3,226 mm) wheelbase of the 160, but powered by 125 hp (93 kW; 127 PS) version of straight-8 engine used the 120.

1942–1945

In 1942, the Packard Motor Car Company converted to 100% war production.

During World War II, Packard again built airplane engines, licensing the Merlin engine from Rolls-Royce as the V-1650, which powered the famous P-51 Mustang fighter, ironically known as the "Cadillac of the Skies" by GIs in WWII.

Packard also built 1350-, 1400-, and 1500-hp V-12 marine engines for American PT boats (each boat used three) and some of Britain’s patrol boats. Packard ranked 18th among United States corporations in the value of wartime production contracts.

By the end of the war in Europe, Packard Motor Car Company had produced over 55,000 combat engines. Sales in 1944 were 5,118,600. By May 6, 1945, Packard had a backlog on war orders of 8,000,000.[37]

1946–1956

By the end of World War II, Packard was in excellent financial condition with assets of around million, but several management mistakes became ever more visible as time went on.

Like other US automobile companies, Packard resumed civilian car production in late 1945, labelling them as 1946 models by modestly updating their 1942 models. As only tooling for the Clipper was at hand, the Senior-series cars were not rescheduled. One version of the story is that the Senior dies were left out in the elements to rust and were no longer usable. Another long-rumored tale is that Roosevelt gave Stalin the dies to the Senior series, but the ZiS-110 state limousines were a separate design.[41]

1949 Packard convertible coupé

1950 Packard Eight Club Sedan
The Clipper became outdated as the new envelope bodies started appearing, led by Studebaker and Kaiser-Frazer. Had they been a European car maker, this would have meant nothing; they could have continued to offer the classic shape not so different from the later Rolls-Royce with its vertical grill. Although Packard was in solid financial shape as the war ended, they had not sold enough cars to pay the cost of tooling for the 1941 design. While most automakers were able to come out with new vehicles for 1948–49, Packard could not until 1951. They therefore updated by adding sheet metal to the existing body (which added 200 lb (91 kg) of curb weight).

Six-cylinder cars were dropped for the home market, and a convertible was added. These new designs hid their relationship to the Clipper. Even that name was dropped—for a while.

The design chosen was a "bathtub" type. While this was considered futuristic during the war and the concept was taken further with the 1949 Nash—and survived for decades in the Saab 92-96 in Europe—the 1948–1950 Packard styling was polarizing. To some it was sleek and blended classic with modern; others nicknamed it the "pregnant elephant". Test driver for Modern Mechanix, Tom McCahill, referred to the newly designed Packard as "a goat" and "a dowager in a Queen Mary hat". Packard sold 92,000 vehicles for 1948 and 116,000 of the 1949 models, however in the early post-WWII years, the demand for new cars was extremely high and nearly any vehicle would sell. Attempting to maintain strong sales beyond this point would prove far more problematic.

Cadillac’s new 1948 cars had sleek, aircraft-inspired styling that immediately made Packard’s "bathtub" styling seem old-fashioned. Moreover, Cadillac also debuted a brand-new OHV V8 engine in 1949 which gave their cars a reputation for performance that Packard’s dependable, but aging inline eight engine couldn’t match. The lack of a modern powerplant would prove an increasing liability for Packard as the 1950s unfolded.

Packard outsold Cadillac until about 1950; most sales were the midrange volume models. During this time, Cadillac was among the earliest U.S. makers to offer an automatic transmission (the Hydramatic in 1941), but Packard caught up with the Ultramatic,[42] offered on top models in 1949 and all models from 1950 onward.

Designed and built by Packard, the Ultramatic featured a lockup torque converter with two speeds. Early Ultramatics normally operated only in "high", with "low" having to be selected manually. Beginning in late 1954, it could be set to operate only in "high" or to start in "low" and automatically shift into "high". "High" was intended for normal driving and "Low" mainly for navigating hills.

The Ultramatic made Packard the only American automotive manufacturer other than GM to develop an automatic transmission completely in-house, as even Ford had chosen to outsource the design of theirs to Borg-Warner (Ford had initially attempted to purchase Ultramatics from Packard to install in Lincolns, but ended up buying Hydramatics until Lincoln got its own automatic transmission a few years later). However, Ultramatic did not compare to GM’s Hydramatic for smoothness of shifting, acceleration, or reliability. The resources spent on Ultramatic deprived Packard of the chance to develop a badly needed modern V8 engine. Also, when a new body style was added in addition to standard sedans, coupes, and convertibles, Packard introduced a station wagon instead of a two-door hardtop in response to Cadillac’s Coupe DeVille. The Station Sedan, a wagon-like body that was mostly steel, with good deal of decorative wood in the back; only 3864 were sold over its three years of production. Although the Packards of the late 1940s and early 1950s were built in its old tradition with craftsmanship and the best materials, all was not well. The combination of the lower priced Packards leading sales and impacting the prestige of their higher end brethren and some questionable marketing decisions, Packard’s crown as "king" of the luxury car market was at risk — and it would eventually be stolen by a rising Cadillac. In 1950, sales dropped to 42,000 cars for the model year. When Packard’s president George T. Christopher set course for an evolutionary styling approach with a facelift for 1951, others wanted a radical new design. In the end, Christopher resigned and Packard treasurer Hugh Ferry became president – he demanded a new direction. Ferry, who had spent his career at Packard in the accounting department, did not want the job and quickly made it clear that he was serving on a temporary basis until a permanent company president could be found.

The 1951 Packards were completely redesigned. Designer John Reinhart introduced a high-waisted, more squared-off profile fitting the contemporary styling trends — very different from the traditional flowing design of the immediate postwar era. New styling features included a one-piece windshield, a wrap-around rear window, small tailfins on the long-wheelbase models, a full-width grill (replacing the traditional Packard upright design), and blunt "guideline fenders" with the hood and front fenders at the same height. The 122-inch (3,099 mm) wheelbase supported low-end 200-series standard and Deluxe two- and four-doors, and 250-series Mayfair hardtop coupes (Packard’s first), and convertibles. Upmarket 300 and Patrician 400 models rode a 127-inch (3,226 mm) wheelbase. The 200-series models were again low-end models and now included a business coupe.

The 250, 300, and 400/Patricians were Packard’s flagship models and comprised the majority of production for that year. The Patrician was now the top-shelf Packard, replacing the Custom Eight line. Original plans were to equip it with a 356 cu in (5.8 L) engine, but the company decided that sales would probably not be high enough to justify producing the larger, more expensive power plant, and so the debored 327 cu in (5.4 L) (previously the middle engine) was used instead. While the smaller powerplant offered nearly equal performance in the new Packards to that of the 356, the move was seen by some as further denigrating Packard’s image as a luxury car.

Since 1951 was a quiet year with little new from the other auto manufacturers, Packard’s redesigned lineup sold nearly 101,000 cars. The 1951 Packards were a quirky mixture of the modern (the automatic transmissions) and aging (still using flathead inline eights when OHV V8 engines were rapidly becoming the norm). No domestic car lines had OHV V8s in 1948, but by 1955, every car line offered a version. The Packard inline eight, despite being an older design that lacked the power of Cadillac’s engines, was very smooth. When combined with an Ultramatic transmission, the drivetrain made for a nearly quiet and smooth experience on the road. However, it struggled to keep pace with the horsepower race, which was increasingly moving to high compression, short stroke engines capable of sustained driving at speeds greater than 55 MPH.

Packard’s image was increasingly seen as dowdy and old-fashioned, unappealing to younger customers. Surveys found that nearly 75% of Packard customers were repeats who had owned previous Packards and few new buyers were being attracted to the make. Compounding this problem was the company’s geriatric leadership. The Packard board of directors by the early 1950s had an average age of 67 and younger executives with a fresher approach to running the company were badly needed–in 1948, Alvin Macauley, born during the Grant Administration, had stepped down as chairman. Hugh Ferry therefore decided that there was no choice but to hire an outsider to take over as president. To that end, he recruited James Nance from appliance manufacturer Hotpoint. At 52, Nance was more than a decade younger than the youngest Packard executive.

One of the main reasons for the aged leadership of Packard was the company’s lack of a pension plan for executives (the rank-and-file workers had a pension plan per their UAW contract). As a result, Packard executives were reluctant to retire and be left with no source of income other than a Social Security payment, thus blocking younger men from coming to power in the company. One of James Nance’s first actions as president was creating a pension plan to induce Packard executives to retire. Nance worked to snag Korean War military contracts and turn around Packard’s badly diluted image. He declared that from now on, Packard would cease producing midpriced cars and build only luxury models to compete with Cadillac. As part of this strategy, Nance unveiled a low-production (only 750 made) glamor model for 1953, the Caribbean convertible. Competing directly with the other novelty ragtops of that year (Buick Skylark, Oldsmobile Fiesta, and Cadillac Eldorado), it was equally well received, and outsold its competition. However, overall sales declined in 1953. While the limited edition luxury models as the Caribbean convertible and the Patrician 400 Sedan, and the Derham custom formal sedan brought back some of the lost prestige from better days, the "high pocket" styling that had looked new two years earlier was no longer bringing people into the showrooms for the bread and butter Packards. Packard’s build quality, which had once been second-to-none, also began slipping during this period as employee morale decreased.

1953 Packard Caribbean convertible
While American independent manufacturers like Packard did well during the early postwar period, supply had caught up with demand and by the early 1950s they were increasingly challenged as the "Big Three"—General Motors, Ford, and Chrysler—battled intensely for sales in the economy, medium-priced, and luxury markets.[43] Those independents that remained alive in the early ’50s, merged. In 1953, Kaiser merged with Willys to become Kaiser-Willys. Nash and Hudson became American Motors Corporation (AMC). The strategy for these mergers included cutting costs and strengthening their sales organizations to meet the intense competition from the Big Three.[44]

In 1953–54, Ford and GM waged a brutal sales war, cutting prices and forcing cars on dealers. While this had little effect on either company, it gravely damaged the independent automakers. Nash president George W. Mason thus proposed that the four major independents (Nash, Hudson, Packard, and Studebaker) all merge into one large outfit to be named American Motors Corporation (AMC). Mason held informal discussions with Nance to outline his strategic vision, and an agreement was reached for AMC to buy Packard’s Ultramatic transmissions and V8 engines. They were used in 1955 Hudsons and Nashes.

Although Korean War defense contracts brought in badly-needed revenue, the war ended in 1953 and new Secretary of Defense Charles E. Wilson began cutting off defense contracts from all automotive manufacturers other than GM, which he had formerly been president of.

Chrysler and Ford during the early 1950s also waged a campaign of "stealing" Packard dealerships, consequently Packard’s dealer network became steadily smaller and more scattered.

Packard’s last major development was the Bill Allison–invented Torsion-Level suspension, an electronically controlled four-wheel torsion-bar suspension that balanced the car’s height front to rear and side to side, having electric motors to compensate each spring independently. Contemporary American competitors had serious difficulties with this suspension concept, trying to accomplish the same with air-bag springs before dropping the idea.

Studebaker-Packard Corporation[edit]
Main article: Studebaker-Packard Corporation
As of October 1, 1954 Packard Motor Car Company bought the failing Studebaker Corporation to form America’s fourth largest automobile company but without full knowledge of their circumstances or consideration of the financial implications.[45] However, SPC’s Nance refused to consider merging with AMC unless he could take the top command position (Mason and Nance were former competitors as heads of the Kelvinator and Hotpoint appliance companies, respectively), but Mason’s grand vision of a Big Four American auto industry ended on October 8, 1954 with his sudden death from acute pancreatitis and pneumonia.

A week after the death of Mason, the new president of AMC, George W. Romney, announced "there are no mergers under way either directly or indirectly".[46] Nevertheless, Romney continued with Mason’s commitment to buy components from SPC. Although Mason and Nance had previously agreed that SPC would purchase parts from AMC, it did not do so. Moreover, Packard’s engines and transmissions were comparatively expensive, so AMC began development of its own V8 engine, and replaced the outsourced unit by mid-1956.[47] Although Nash and Hudson merged along with Studebaker and Packard joining, The four-way merger Mason had hoped for, which would have joined Nash, Hudson, Studebaker and Packard, did not materialize. The S-P marriage (really a Packard buyout) proved to be a crippling mistake. Although Packard was still in fair financial shape, Studebaker was not, struggling with high overhead and production costs and needing the impossible figure of 250,000 cars a year to break even. Due diligence was placed behind "merger fever", and the deal was rushed. It became clear after the merger that Studebaker’s deteriorating financial situation put Packard’s survival at risk.

Nance had hoped for a total redesign in 1954, but the necessary time and money were lacking. Packard that year (total production 89,796) comprised the bread-and-butter Clipper line (the 250 series was dropped), Mayfair hardtop coupes and convertibles, and a new entry level long-wheelbase sedan named Cavalier. Among the Clippers was a novelty pillared coupe, the Sportster, styled to resemble a hardtop.

With time and money again lacking, 1954 styling was unchanged except for modified headlights and taillights, essentially trim items. A new hardtop named Pacific was added to the flagship Patrician series and all higher-end Packards sported a bored-out 359-cid engine. Air conditioning became available for the first time since 1942. Packard had introduced air conditioning in the 1930s. Clippers (which comprised over 80% of production) also got a hardtop model, Super Panama, but sales tanked, falling to only 31,000 cars.

1955 Packard Patrician
The revolutionary new model Nance hoped for was delayed until 1955, partially because of Packard’s merger with Studebaker. Packard stylist Richard A. Teague was called upon by Nance to design the 1955 line, and to Teague’s credit, the 1955 Packard was indeed a sensation when it appeared. Not only was the body completely updated and modernized, but the suspension also was totally new, with torsion bars front and rear, along with an electric control that kept the car level regardless of load or road conditions. Crowning this stunning new design was Packard’s brand new ultra-modern overhead-valve V8, displacing 352 cu in (5.8 l), replacing the old, heavy, cast-iron side-valve straight-eight that had been used for decades. In addition, Packard offered a variety of power, comfort, and convenience features, such as power steering and brakes as well as electric window lifts. But air conditioning was an anomaly. Although available on all makes by the mid-1950s, it was installed on only a handful of cars in 1955 and 1956 despite Packard’s status as a luxury car. Model year sales only climbed back to 55,000 units in 1955, including Clipper, in what was a very strong year across the industry.

As the 1955 models went into production, an old problem flared up. Back in 1941, Packard had outsourced its bodies to Briggs Manufacturing Company. Briggs founder Walter Briggs had died in early 1952 and his family decided to sell the company off to pay for estate taxes. Chrysler promptly purchased Briggs and notified Packard that they would cease supplying bodies after Packard’s contract with Briggs expired at the end of 1953. Packard was forced to move body production to an undersized plant on Connor Avenue in Detroit. The facility proved too small and caused endless tie-ups and quality problems.[citation needed] Bad quality control hurt the company’s image and caused sales to plummet for 1956, though the problems had largely been resolved by that point.[citation needed] Additionally, a "brain drain" of talent away from Packard was underway, most notably John Z. DeLorean.[citation needed]

1956 Packard Clipper
For 1956, the Clipper became a separate make, with Clipper Custom and Deluxe models available. Now the Packard-Clipper business model was a mirror to Lincoln-Mercury. "Senior" Packards were built in four body styles, each with a unique model name. Patrician was used for the four-door top of the line sedans, Four Hundred for the hardtop coupes, and Caribbean for the convertible and vinyl-roof two-door hardtop. In the spring of 1956, the Executive was introduced. Coming in a four-door sedan and a two-door hardtop, the Executive was aimed at the buyer who wanted a luxury car but could not justify Packard’s pricing. It was an intermediate model using the Packard name and the Senior models’ front end, but using the Clipper platform and rear fenders. This was to some confusing and went against what James Nance had been attempting for several years to accomplish, the separation of the Clipper line from Packard. However, as late as the cars’ introduction to the market, was there was reasoning for in 1957 this car was to be continued. It then became a baseline Packard on the all-new 1957 Senior shell. Clippers would share bodies with Studebaker from 1957.

Despite the new 1955/56 design, Cadillac continued to lead the luxury market, followed by Lincoln, Packard, and Imperial. Reliability problems with the automatic transmission and all electrical accessories further eroded the public’s opinion of Packard. Sales were good for 1955 compared to 1954. The year was also an industry banner year. Packard’s sales slid in 1956 due to the fit and finish of the 1955 models, and mechanical issues relating to the new engineering features. These defects cost Packard millions in recalls and tarnished a newly won image just in its infancy.

For 1956, Teague kept the basic 1955 design, and added more styling touches to the body such as then−fashionable three toning. Headlamps hooded in a more radical style in the front fenders and a slight shuffling of chrome distinguished the 1956 models. "Electronic Push-button Ultramatic", which located transmission push buttons on a stalk on the steering column, proved trouble-prone, adding to the car’s negative reputation, possibly soon to become an orphan. Model series remained the same, but the V8 was now enlarged to 374 cu in (6.1 L) for Senior series, the largest in the industry. In the top-of-the-line Caribbean, that engine produced 310 hp (230 kW). Clippers continued to use the 352 engine. There were plans for an all−new 1957 line of Senior Packards based on the showcar Predictor. Clippers and Studebakers would also share many inner and outer body panels. (A private presentation of this 1957 new-car program was made to Wall Street’s investment bankers at the Waldorf-Astoria Hotel in New York in January 1956.) These models were in many ways far advanced from what would be produced by any automaker other at the time, save Chrysler, which would soon feel public wrath for its own poor quality issues after rushing its all−new 1957 lines into production. Nance was dismissed and moved to Ford as the head of the new Mercury-Edsel-Lincoln division. Although Nance tried everything, the company failed to secure funding for new retooling, forcing Packard to share Studebaker platforms and body designs. With no funding to retool for the advanced new models envisioned, SPC’s fate was sealed; the large Packard was effectively dead in an executive decision to kill "the car we could not afford to lose". The last fully Packard-designed vehicle, a Patrician four-door sedan, rolled off the Conner Avenue assembly line on June 25, 1956.[48]

1957–1958[edit]

1958 Packard
In 1957, no more Packards were built in Detroit and the Clipper disappeared as a separate brand name. Instead, a Studebaker President–based car bearing the Packard Clipper nameplate appeared on the market, but sales were slow. Available in just two body styles, Town Sedan (four-door sedan) and Country Sedan (four-door station wagon), they were powered by Studebaker’s 289 cu in (4.7 l) V8 with a McCulloch supercharger, delivering the same 275 hp (205 kW) as the 1956 Clipper Custom, although at higher revolutions. Borrowing design cues from the 1956 Clipper (visual in the grille and dash), with wheel covers, tail lamps, and dials from 1956 along with the Packard cormorant hood mascot and trunk chrome trim from 1955 senior Packards, the 1957 Packard Clipper was more than a badge-engineered Studebaker—but also far from a Patrician. Had the company been able to invest more money to finish the transformation and position the car under a senior line of "true Packards", it might have been a successful Clipper. However, standing alone the cars sold in very limited numbers—and a number of Packard dealers dropped their franchises while customers stayed away, despite huge price discounts, fearful of buying a car that could soon be an orphaned make. With the market flooded by inexpensive cars, minor automakers struggled to sell vehicles at loss leader prices to keep up with Ford and GM.[49] Also, a general decline in demand for large cars heralded an industry switch to compact cars such as the Studebaker Lark.

Predictably, many Packard devotees were disappointed by the marque’s perceived further loss of exclusivity and what they perceived as a reduction in quality. They joined competitors and media critics in christening the new models as "Packardbakers". The 1958 models were launched with no series name, simply as "Packard". New body styles were introduced, a two-door hardtop joined the four-door sedan. A new premier model appeared with a sporting profile: the Packard Hawk was based on the Studebaker Golden Hawk and featured a new nose and a fake spare wheel molded in the trunk lid reminiscent of the concurrent Imperial. The 1958 Packards were amongst the first in the industry to be "facelifted" with plastic parts. The housing for the new dual headlights and the complete fins were fiberglass parts grafted on Studebaker bodies. Very little chrome was on the lower front clip. Designer Duncan McRae managed to include the 1956 Clipper tail lights for one last time, this time in a fin, and under a canted fin, a wild—or to some bizarre—mixture. Added to the front of all but the Hawk were tacked on pods for dual headlights, in a desperate attempt to keep up with late-1950s styling cues. All Packards were given 14 in (36 cm) wheels to lower the profile. The public reaction was predictable and sales were almost nonexistent. The Studebaker factory was older than Packard’s Detroit plant, with higher production requirements, which added to dipping sales. A new compact car on which the company staked its survival, the Lark, was a year away, and failed to sell in sufficient numbers to keep the marque afloat. Several makes were discontinued around this time: Packard, Edsel, Hudson, Nash, DeSoto, and Kaiser. Not since the 1930s had so many makes disappeared, and it wouldn’t be until the automotive industry crisis of 2008–10 that so many makes would be dropped at the same time again.

CONCEPT PACKARDS

1956 Predictor concept, at the Studebaker National Museum
During the 1950s, a number of "dream cars" were built by Packard in an attempt to keep the marque alive in the imaginations of the American car-buying public. Included in this category are the 1952 Pan American that led to the production Caribbean and the Panther (also known as Daytona), based on a 1954 platform. Shortly after the introduction of the Caribbean, Packard showed a prototype hardtop called the Balboa.[50] It featured a reverse-slanted rear window that could be lowered for ventilation, a feature introduced in a production car by Mercury in 1957 and still in production in 1966.

The Request was based on the 1955 Four Hundred hardtop, but featured a classic upright Packard fluted grille reminiscent of the prewar models. In addition, the 1957 engineering mule "Black Bess" was built to test new features for a future car. This car had a resemblance to the 1958 Edsel. It featured Packard’s return to a vertical grill. This grill was very narrow with the familiar ox-yoke shape that was characteristic for Packard, and with front fenders with dual headlights resembling Chrysler products from that era. The engineering mule Black Bess was destroyed by the company shortly after the Packard plant was shuttered. Of the 10 Requests built, only four were sold off the showroom floor.

Richard A. Teague also designed the last Packard show car, the Predictor. This hardtop coupe’s design followed the lines of the planned 1957 cars. It had many unusual features, among them a roof section that opened either by opening a door or activating a switch, well ahead of later T-tops. The car had seats that rotated out, allowing the passenger easy access, a feature later used on some Chrysler and GM products. The Predictor also had the opera windows, or portholes, found on concurrent Thunderbirds. Other novel ideas were overhead switches—these were in the production Avanti—and a dash design that followed the hood profile, centering dials in the center console area. This feature has only recently been used on production cars. The Predictor survives and is on display at the Studebaker National Museum section of the Center for History in South Bend, Indiana.

Astral[edit]
One unusual prototype, the Studebaker-Packard Astral, was made in 1957 and first unveiled at the South Bend Art Centre on January 12, 1958, and then at the March 1958 Geneva Motor Show.[51] It had a single gyroscopic balanced wheel and the publicity data suggested it could be nuclear powered or have what the designers described as an ionic engine. No working prototype was ever made, nor was it likely that one was ever intended.[52][53]

The Astral was designed by Edward E. Herrmann, Studebaker-Packard’s director of interior design,[54] as a project to give his team experience in working with glass-reinforced plastic. It was put on show at various Studebaker dealerships before being put into storage. Rediscovered 30 years later, the car was restored and put on display by the Studebaker museum.

The end[edit]
Studebaker-Packard pulled the Packard nameplate from the marketplace in 1959. In 1962, "Packard" was dropped off the corporation’s name at a time when it was introducing the all new Avanti, and a less anachronistic image was being sought, thus finishing the story of the American Packard marque. The Packard name (as well as Pierce-Arrow) had been considered for the Avanti, but this wasn’t done.

In the late 1950s, Studebaker-Packard was approached by enthusiasts to rebadge the French car maker Facel-Vega’s Excellence four-door hardtop as a Packard for sale in North America, using stock Packard V8s and identifying trim including red hexagonal wheel covers, cormorant hood ornament, and classic vertical ox-yoke grille.[citation needed] The proposition was rejected when Daimler-Benz threatened to pull out of its 1957 marketing and distribution agreement, which would have cost Studebaker-Packard more in revenue than they could have made from the badge-engineered Packard. Daimler-Benz had little of its own dealer network at the time and used this agreement to enter and become more established in the American market through SPC’s dealer network, and felt this car was a threat to their models.

Aborted revival[edit]
In the late 1990s, Roy Gullickson revived the Packard nameplate by buying the trademark and developing a Packard Twelve for the 1999 model year. His goal was annual production of 2,000 cars, but lack of investment funds stalled that plan indefinitely. The only prototype Twelve made was sold at an auto auction in Plymouth, MI, in July 2014 for 3,000.[55]

Packard engines[edit]
Automobile[edit]
Packard’s engineering staff designed and built excellent, reliable engines. Packard offered a 12-cylinder engine—the "Twin Six"—as well as a low-compression straight-eight, but never a 16-cylinder engine. After WWII, Packard continued with their successful straight-eight-cylinder flathead engines. While as fast as the new GM and Chrysler OHV V8s, they were perceived as obsolete by buyers. By waiting until 1955, Packard was almost the last U.S. automaker to introduce a high-compression V8 engine. The design was physically large and entirely conventional, copying many of the first-generation Cadillac, Buick, Oldsmobile, Pontiac, and Studebaker Kettering features. It was produced in 320 cu in (5.2 L) and 352 cu in (5.8 L) displacements. The Caribbean version had two four-barrel carburetors and produced 275 hp (205 kW). For 1956, a 374 cu in (6.1 L) version was used in the Senior cars and the Caribbean two four-barrels produced 305 hp (227 kW).[clarification needed]

Other Packard engines[edit]

Gar Wood’s Miss America 2, winner of the 1921 Harmsworth Trophy, was powered by four Packard-built Liberty L-12 engines.

Later variants of the North American P-51 Mustang were powered by a Packard V-1650 Merlin, a license-built version of the Rolls-Royce Merlin.

PT boats were powered by a trio of Packard 4M-2500 engines, and later models featured the improved 5M-2500.
Packard also made large aeronautical and marine engines. Chief engineer Jesse G. Vincent developed a V12 airplane engine called the "Liberty engine" that was used widely in Entente air corps during World War I. After the war the Liberty was adapted for marine use, becoming a multiple world record setter under inventor and boating pioneer Gar Wood from the late 1910s through the 1930s.

In the interbellum, Packard built one of the world’s first diesel aviation engines, the 225-hp DR-980 radial. It powered the Stinson SM-8D, among others. It also powered a Bellanca CH-300 on a record endurance flight of over 84 hours, a mark that stood for more than 50 years. Other Packard-powered airplanes set several records during the 1920s.

During WWII, Packard license-built Rolls-Royce Merlin engines under the Packard V-1650 designation, used with great success in the famed P-51 Mustang fighter. A marine version of the successor to the V12 Liberty was adapted in three versions – M3-2500, M4-2500, and M5-2500 – to power the war’s iconic PT boats.

After WWII, Packard produced a new line of flathead design six (model 1M-245) and eight (model 1M-356) cylinder marine engines based on the automobile versions and the experience gained from the war production. Of the 1M-245 type engines, only 1,865 were produced between Spring 1947 and January 1951, with only a handful survivors.[56] Of the 1M-356 type engines, approximately 1,525 were produced between 1947 and 1950.[57] Even more rare is the experimental "R" type racing versions (1M-245 "R"), of which only 10 were produced with currently only one known survivor, a 1M-245 R six-cylinder engine powering today a 1936 Gar Wood Speedster.[58]

Packard also developed two turbine aircraft engines for the US Air Force, the XJ41 an XJ49. This was one reason for the Curtiss-Wright take-over in 1956: Packard wanted to sell their own jet.[59]

Packard automobile models[edit]

1907 Packard, The New York Times, November 6, 1907
Packard single-cylinder models:
Packard Model A (1899–1900)
Packard Model B (1900)
Packard Model C (1901)
Packard Model E (1901)
Packard Model F (1901–1903)
Packard Model M (1904)
Packard twin-cylinder model:
Packard Model G (1902)
Packard four-cylinder models:
Packard Model K (1903)
Packard Model K Gray Wolf (1903)
Packard Model L (1904)
Packard Model N (1905)
Packard Model 24 (Series S) (1906)
Packard Model 18 (Series NA-NC) (1905–1907)
Packard Model 30 (Series U) (1907–1912)
Packard six-cylinder models:
Packard Dominant Six (1912–1915)
Packard Single Six (1921–1924)
Packard Six (1925–1929)
Packard One-Ten
Packard 115 (1937)
Packard Six (1937–1949)
Packard Eight
Packard Single Eight & Eight (1924-)
Packard Custom Eight
Packard Light Eight
Packard One-Twenty (1935–1942)
Packard 160
Packard 180
Packard Super Eight
Packard V-12:
Packard Twin Six (1916–1923)
Packard 905 (1916–1923)
Packard Twin Six (1932)
Packard Twelve (1932–1939)
Postwar Packards (including Clipper)
Packard 400, see Packard Four Hundred
Packard Caribbean
Packard Cavalier
Packard Clipper
Packard Clipper Constellation
Packard 200
Packard 250, see Packard 200
Packard 300
Packard Executive
Packard Four Hundred
Packard Hawk (1958)
Packard Mayfair
Packard Pacific
Packard Patrician (including Patrician 400)
Packard Station Sedan (1949–1950)
Packard Super Panama
1957 and 1958 Packards

SOURCE: en.wikipedia.org/wiki/Packard