Fairchild AU-23 Peacemaker
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|Fairchild AU-23A Peacemaker in flight|
|Role||Armed gunship, counter-insurgency, utility transport|
|Primary users||United States Air Force
Royal Thai Air Force
|Developed from||Pilatus PC-6 Porter|
The Fairchild AU-23 Peacemaker was an American armed gunship, counter-insurgency, utility transport version of the Pilatus PC-6 Porter for the United States Air Force. A total of 15 were built under license in the United States by Fairchild Industries, for use during the Vietnam War in the early 1970s. All aircraft were later sold to the Royal Thai Air Force.
Design and development
In May 1971 the Aeronautical Systems Division at Wright-Patterson Air Force Base, Ohio, began work on a project to evaluate the potential use of armed light utility short takeoff and landing aircraft in Southeast Asia. The program, named Credible Chase, was designed to add mobility and firepower to the South Vietnamese Air Forces in a relatively short time. Two commercial aircraft were selected for testing: the Fairchild Porter and the Helio Stallion. Initial performance testing was conducted with leased aircraft at Eglin Air Force Base, Florida, and was successful enough to warrant a combat evaluation. The Porter, designated AU-23A, was fitted with a side-firing 20mm XM-197 Gatling cannon, four wing pylons and a center fuselage station for external ordnance. The 20mm cannon was essentially a three-barrel version of the M61 Vulcan 6-barrel 20mm cannon. The aircraft could carry a variety of ordnance including forward-firing gun pods, 500 and 250 pound bombs, napalm units, cluster bomb units, flares, rockets, smoke grenades and Airborne leaflet propaganda dispensers.
The combat evaluation, PAVE COIN, was done in June and July 1971. The AU-23A was tested for eight possible missions: armed escort of helicopters, close air support, hamlet defense, STOL airlift and resupply, armed reconnaissance, border surveillance, forward air control, and counter infiltration. USAF crews flew 73 missions (94 sorties) and RVNAF crews flew 68 missions (85 sorties). Several types of weapons were test dropped/fired including 2.75-inch rockets (explosive and smoke), cluster bomb units (CBU-14), MK 6 Mod 3 flares, and MK 81, 82 and 106 practice bombs. More than 8,000 rounds of 20mm ammunition was fired also—both high explosive incendiary and target practice tracer types. Several problems were discovered during the PAVE COIN program, the most serious was the extreme vulnerability of the aircraft to all but the lightest antiaircraft fire (below 12.7mm). Despite the problems, the USAF continued with the development program and ordered 15 AU-23As for further testing.
The 4400th Special Operations Squadron (Provisional) was created to complete the operational test and evaluation of the Credible Chase aircraft. The first AU-23A (72-1306) was delivered to the 4400th SOS on Jan. 2, 1972, followed by two more aircraft (72-1304 & 72-1305) at the end of the month. Testing continued until Feb. 4, when the three aircraft were grounded because of cracks in the rudder assemblies. The first three aircraft were returned to Fairchild for repair and delivery of new aircraft resumed in late April 1972. On May 10, 1972, an AU-23A (S/N 72-1309) crashed after an in-flight engine failure. The pilot was not hurt, but all AU-23As were grounded until May 22, during the accident investigation. The last AU-23A was delivered on June 7 and testing was completed on June 28.
The 4400th recommended the aircraft not be used in combat without a major upgrade program. Specific problems identified included a slow combat speed (135 knots), a low working altitude, no capability for "zoom" escapes after delivering ordnance and a complete lack of armor protection for the crew and vital aircraft systems. On June 30, 1972, the 4400th SOS ferried the AU-23As to Davis-Monthan Air Force Base, Arizona, for storage.
- Crew: 3 (pilot, co-pilot, gunner)
- Capacity: 5 troops or 6 passengers or 1 litter patient, 3 ambulatory patients with 1 medical attendant
- Length: 36 ft 10 in (11.23 m)
- Wingspan: 49 ft 8 in (15.14 m)
- Height: 14 ft 4 in (4.37 m)
- Gross weight: 6,100 lb (2,767 kg)
- Powerplant: 1 × Garrett TPE-331-1-101F turboprop engine, 650 hp (480 kW)
- Maximum speed: 148 kn (170 mph; 274 km/h) at take-off power, 5,000 ft (1,524 m)5,000 feet altitude, 6,000 lb (2,722 kg) gross weight
- Cruise speed: 77 kn; 88 mph (142 km/h) at maximum continuous power, 129 kn (239 km/h) combat cruise
- Range: 365 nmi; 676 km (420 mi)
- Combat range: 175 nmi; 323 km (201 mi)
- Endurance: 4.84
- Up to 1925 lbs. of external stores on five pylons
- XM197 20mm cannon, door-mounted
- XM93 7.62mm minigun
- XM59 .50-cal. machine gun and XMU-470 20mm fixed side-firing gun pods.
- SUU11 gun pods
- 2.75-inch rocket pods
- BDU33 with 25 lbs. bomblets
- MK81 250 lb bombs
- MK82 500 lb bombs
- BLU118 500 lb napalm canisters
- CBU55 500 lb cluster bomb units
- MK24 flares
- ADU272 canisters
- smoke grenades
- propaganda leaflet dispensers.
- Related development
- Aircraft of comparable role, configuration and era
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