Decommissioned PAF Aircrafts (Support)

C-47 | O-46A | PT-26 | U6A | HU-16 | BAC-1-11 | YS-11A | L-4J | J3C | PT-17 | PT-1 | O-1 | BT-1 | SR-7B | L-5B | Rotary Wing

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Douglas Aircraft Company C-47 'Dakota/Skytrain'
Type: Tactical Transport Aircraft
Origin: USA
Similar aircraft: C-46 Commando
Wings: Low-wing monoplane.
Fuselage:
Tail unit:
Landing gear: Retractable tricycle type.
Accommodation: Crew of three and provision for up to 33 troops or 2,700 kg (6,000 lb) of cargo.
Powerplant: Two 1,200 hp (895 kW) Pratt & Whitney R-1830-92 Twin Wasp 14-cylinder radial piston engines, driving a three-blade propeller.
Systems:
Avionics and equipment:
Dimensions, External
Wing span: 29.11 m (95' 6")
Length, overall: 19.65 m (64' 5 ½")
Height, overall: 5.17 m (16' 11 ½")
Areas
Wings, gross: 91.70 m² (987 ft²)
Weights and loadings
Weight, empty: 7,666 kg (16,865 lb)
Typical mission weights
Max T-O weight: 11,545 kg (25,200 lb)
Wing loading: 129 kg/m² (26.3 lb/ft²)
Power/mass ratio: 150 W/kg (0.092 hp/lb)
Performance
Max speed: 434 kph (270 mph)
Max cruising speed: 333 kph (207 mph)
Stalling speed:
Rate of climb: 5.75 m/sec (1,130 ft/min)
Service ceiling: 7,073 m (23,200')
T-O run:
Landing run:
Combat radius:
Range: 2,816 km (1,750 mi)
Weapon systems: None
Program:

Douglas Aircraft Company O-46A
Type:
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

Douglas Aircraft Company PT-26 'Cornell'
Type:
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

de Havilland Canada L-20/U6A 'Beaver'
Type: Utility Aircraft
Origin:
Similar aircraft:
Wings: High-wing monoplane.
Fuselage:
Tail unit:
Landing gear: Non-retractable tricycle type.
Accommodation:
Powerplant: One 450 hp Pratt & Whitney R-985-AN Wasp Junior radial piston engine.
Systems:
Avionics and equipment:
Dimensions, External
Wing span: 13.1 m (43')
Length, overall: 9.25 m (30' 4")
Height, overall: 2.74 m (9')
Areas
Wings, gross:
Weights and loadings
Weight, empty: 1,295 kg (2,850 lb)
Typical mission weights
Max T-O weight: 2,318 kg (5,100 lb)
Performance
Max speed: 225 kph (140 mph)
Max cruising speed: 177 kph (110 mph)
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range: 1,239 km (770 mi)
Weapon systems: Generally none, though some units were utilized as light bombers.
Program:

Grumman Aircraft Corporation SA-16/ HU-16 'Albatross'
Type: Twin-engined Utility Seaplane
Origin: USA
Similar aircraft:
Wings: High-wing monoplane.
Fuselage:
Tail unit:
Landing gear:
Accommodation: Crew of four. Capacity for 10 passengers or 5,000 lb or cargo
Powerplant: Two 1,425 hp (1,063 kW) Curtiss-Wright R-1820-76A/76B Cyclone radial piston engine, driving a three-blade propeller. Fuel capacity 4,000 liters (1,075 US gallons) and provision for two 1,100 liters (300 US gallons) drop tanks. Additional lift utilizing two or four JATO 15KS1000 units, 15 second solid propellant, 1,000 lb thrust.
Systems:
Avionics and equipment:
Dimensions, External
Wing span: 29.47 m (96' 8")
Length, overall: 18.67 m (61' 3")
Height, overall: 7.88 m (25' 10")
Areas
Wings, gross:
Weights and loadings
Weight, empty: 10,401 kg (22,883 lb)
Typical mission weights
Max T-O weight: 16,227 kg (35,700 lb)
Performance
Max speed: 380 kph (236 mph)
Max cruising speed: 241 kph (150 mph)
Stalling speed:
Rate of climb:
Service ceiling: 6,555 m (21,500')
T-O run:
Landing run:
Combat radius:
Range with max int fuel and ext fuel tanks: 4,586 km (2,850 mi)
Weapon systems: Generally none. Provision for outboard hardpoints for external fuel tanks.
Program:

Hunting/British Aircraft Corporation/BAe BAC-1-11
Type: Short Range Jet Transport
Origin: UK
Similar aircraft: Sud Aviation Caravelle, Vickers Viscount
Wings: Cantilever low-wing monoplane.
Fuselage:
Tail unit:
Landing gear: Retractable
Accommodation: Two pilots, three flight attendants and about eighty nine passengers in charter layout
Powerplant: Two 47 kN (10,600 lb) Rolls-Royce RB.163 Spey Mk. 506 nonafterburning turbofans
Systems:
Avionics and equipment:
Dimensions, External
Wing span: 26.9 m (88' 6")
Length, overall: 28.2 m (92' 6")
Height, overall: 7.2 m (23' 9")
Areas
Wings, gross: 93.2 m² (1,003 ft²)
Weights and loadings
Weight, empty: 21,049 kg (46,405 lb)
Typical mission weights
Max T-O weight: 33,800 kg (74,500 lb)
Performance
Max speed: 870 kph (470 knts; 540 mph)
Cruising speed: 795 kph (430 knts; 495 mph)
Stalling speed:
Rate of climb:
Service ceiling: 10,700 m (35,000')
T-O run:
Landing run:
Combat radius:
Range: 2,320 km (1,440 mi)
Weapon systems: None
Program:

Nikkon Aeroplane Manufacturing Company YS-11A
Type: Twin-engined Medium Range Transport
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

Piper O-59/L-4J 'Cub'
Type: Liaison Aircraft
Origin: USA
Similar aircraft: Aeronca Champ, Kitfox Model 5, Taylorcraft BC-65
Wings: High-wing monoplane.
Fuselage:
Tail unit:
Landing gear: Non-retractable.
Accommodation: Tandem seats, seating one pilot and one passenger
Powerplant: One 65 hp (48 kW) Continental A-65-8 air-cooled flat-four piston engine
Systems:
Avionics and equipment:
Dimensions, External
Wing span: 10.73 m (35' 2 ½")
Length, overall: 6.78 m (22' 3")
Height, overall: 2.03 m (6' 8")
Areas
Wings, gross: 16.58 m² (178.5 ft²)
Weights and loadings
Weight, empty: 290.91 kg (640 lb)
Typical mission weights
Max T-O weight: 500 kg (1,100 lb)
Wing loading: 33.4 kg/m² (6.84 lb/ft²)
Power/mass ratio: 11.35 kg/kW (18.75 lb/hp)
Performance
Max speed: 140 kph (76 knts; 87 mph)
Cruising speed: 121 kph (65 knts; 75 mph)
Stalling speed:
Rate of climb: 2.3 m/sec (450 ft/min)
Service ceiling: 3,500 m (11,500')
T-O run:
Landing run:
Combat radius:
Range: 354 km (191 nm; 202 mi)
Weapon systems: None
Program:

Piper J3C 'Cub'
Type:
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

Stearman Aircraft Company/Boeing model 75 US Army Air Corps designation PT-13/PT-17 'Kaydet"
Type: Two-seat primary trainer
Origin: USA
Similar aircraft:
Wings: Biplane. Wood structure covered with fabric skin.
Fuselage: Welded steel structure with fabric skin.
Tail unit:
Landing gear: Non-retractable.
Accommodation: Two
Powerplant: One 220 hp Continental R-670-5 piston radial engine, driving a two-blade propeller.
Systems:
Avionics and equipment:
Dimensions, External
Wing span: 9.81 m (32' 2")
Length, overall: 7.39 m (24' 3")
Height, overall: 2.79 m (9' 2")
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Max speed: 200 kph (124 mph)
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling: 3,415 m (11,200')
T-O run:
Landing run:
Combat radius:
Range: 812 km (505 mi)
Weapon systems: None
Program:

Stearman Aircraft Company 73L3/ PT-1
Type:
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

Stearman Aircraft Company A73L3/ PT-1
Type:
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

Stearman Aircraft Company A75L3/ O-1
Type:
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

Stearman Aircraft Company 76D1/ BT-1
Type:
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

Stearman Aircraft Company 76D3/ BT-1
Type:
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

Stearman Aircraft Company SR-7B 'Reliant'
Type:
Origin:
Similar aircraft:
Wings:
Fuselage:
Tail unit:
Landing gear:
Accommodation:
Powerplant:
Systems:
Avionics and equipment:
Dimensions, External
Wing span:
Length, overall:
Height, overall:
Areas
Wings, gross:
Weights and loadings
Weight, empty:
Typical mission weights
Max T-O weight:
Performance
Never exceed speed:
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling:
T-O run:
Landing run:
Combat radius:
Range:
Weapon systems:
Program:

Stinson/Vultee Aircraft O-62/U-19/L-5B 'Sentinel'
Type: Liaison Aircraft
Origin: USA
Similar aircraft:
Wings: High-wing monoplane.
Fuselage:
Tail unit:
Landing gear: Non-retractable.
Accommodation:
Powerplant: One 185 hp Lycoming O-435 flat-six piston engine, driving a two-blade propeller.
Systems:
Avionics and equipment:
Dimensions, External
Wing span: 10.37 m (34')
Length, overall: 7.34 m (24' 1")
Height, overall: 2.41 m (7' 11")
Areas
Wings, gross:
Weights and loadings
Weight, empty: 705 kg (1,550 lb)
Typical mission weights
Max T-O weight: 918 kg (2,020 lb)
Performance
Max speed: 209 kph (130 mph)
Max cruising speed:
Stalling speed:
Rate of climb:
Service ceiling: 4,817 m (15,800')
T-O run:
Landing run:
Combat radius:
Range: 579 km (360 mi)
Weapon systems: None
Program:


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