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AIRCRAFT SPECIFICATIONS

 

 

 

VH-WHAwha


Piper PA-28-161 Warrior II

Low wing, 4 seat, basic trainer with fixed tricycle undercarriage


Dimensions:

Wing span 10.67m (35ft)

Length 7.25m (23ft 9.5in)

Height 2.23m (7ft 3.8in)


Powerplant:

One Lycoming O-320 (4 cylinder, horizontally opposed, 320 cubic inch displacement) developing 160 bhp @ 2700 rpm driving a 2 blade fixed pitch propeller


Fuel:

AVGAS

Total usable fuel 181 L

Fuel flow 36 L/hour


Weights (normal operation):

Basic Empty Weight 660 Kg 1455 lb

Maximum Take-off Weight 1100 Kg 2425 lb

Maximum Landing Weight 1100 Kg 2425 lb


Operating speeds:

Never exceed speed Vne 160 kts

Maximum structural cruise speed Vno 126 kts

Maneuvering speed Va 2325 lb 111 kts, 1531 lb 88 kts

Maximum flap extension speed Vfe 103 kts


Avionics:

Dual VHF (King KX 155 / King KY 97A)

Dual NAV (King KX 155 / Narco NAV 824)

Single ADF (King KR 86)

Single Transponder (Narco AT 150)

NVFR rated

riv

 

 

 

VH-LSMlsm


Piper PA-28-161 Warrior II

Low wing, 4 seat, basic trainer with fixed tricycle undercarriage


Dimensions:

Wing span 10.67m (35ft)

Length 7.25m (23ft 9.5in)

Height 2.23m (7ft 3.8in)


Powerplant:

One Lycoming O-320 (4 cylinder, horizontally opposed, 320 cubic inch displacement) developing 160 bhp @ 2700 rpm driving a 2 blade fixed pitch propeller


Fuel:

AVGAS

Total usable fuel 181 L

Fuel flow 36 L/hour


Weights (normal operation):

Basic Empty Weight 676 Kg 1489 lb

Maximum Take-off Weight 1055 Kg 2325 lb

Maximum Landing Weight 1055 Kg 2325 lb


Operating speeds:

Never exceed speed Vne 160 kts

Maximum structural cruise speed Vno 126 kts

Manoeuvring speed Va 2325 lb 111 kts, 1531 lb 88 kts

Maximum flap extension speed Vfe 103 kts


Avionics:

Dual VHF/ NAV (KX 170B)

Single ADF (Bendix BX 2000)

Single Transponder (King KT 76A)

NVFR rated

riv

 

 

 

VH-LSFlsf


Piper PA-28-161 Warrior II

Low wing, 4 seat, basic trainer with fixed tricycle undercarriage


Dimensions:

Wing span 10.67m (35ft)

Length 7.25m (23ft 9.5in)

Height 2.23m (7ft 3.8in)


Powerplant:

One Lycoming O-320 (4 cylinder, horizontally opposed, 320 cubic inch displacement) developing 160 bhp @ 2700 rpm driving a 2 blade fixed pitch propeller


Fuel:

AVGAS

Total usable fuel 181 L

Fuel flow 36 L/hour


Weights (normal operation):

Basic Empty Weight 701 Kg 1544 lb

Maximum Take-off Weight 1100 Kg 2425 lb

Maximum Landing Weight 1100 Kg 2425 lb


Operating speeds:

Never exceed speed Vne 160 kts

Maximum structural cruise speed Vno 126 kts

Maneuvering speed Va 2325 lb 111 kts, 531 lb 88 kts

Maximum flap extension speed Vfe 103 kts


Avionics:

Dual VHF/ NAV (King KX 165)

Single ADF (King KR 87)

Single DME (King KN 62A)

Single Transponder (King KT)

IFR rated

riv

 

 

 

VH-HSMhsm


Cessna R172K Hawk XP II

High wing, 4 seat, advanced trainer with fixed tricycle undercarriage


Dimensions:

Wing span 11.0m (36ft 1in)

Length 8.3m (27ft 2in)

Height 2.7m (8ft 11in)


Powerplant:

One Continental IO-360 (6 cylinder, fuel injected, horizontally opposed, 360 cubic inch displacement) developing 195 bhp @ 2600 rpm driving a 2 blade constant speed propeller


Fuel:

AVGAS

Total usable fuel 185 L

Fuel flow 40 L/hour


Weights (normal operation):

Basic Empty Weight 740 Kg 1632 lb

Maximum Take-off Weight 1157 Kg 2550 lb

Maximum Landing Weight 1157 Kg 2550 lb


Operating speeds:

Never exceed speed Vne 163 kts

Maximum structural cruise Vno 129 kts

Maneuvering Va 2550 lb 105 kts, 2150 lb 96 kts, 1750 lb 87 kts

Maximum flap extension speed Vfe 10° 110 kts Full 85 kts


Avionics:

Dual VHF/ NAV (Cessna 300 RT 385A)

Single ADF (Cessna 300 R 546E)

Single DME (Narco DME 190)

Single Transponder (King KT 76A)

Single HF SSB (Barrett F 24)

II Morrow Apollo 820 Flybuddy GPS

S-Tec System 50 two axis autopilot

IFR rated

riv

 

 

 

VH-IWLiwl


Piper PA-32R-300 Lance II

Low wing, 6 seat, transport aircraft with retractable tricycle undercarriage


Dimensions:

Wing span 10.00m (32ft 9.8in)

Length 8.44m (27ft 8.2in)

Height 2.74m (9ft)


Powerplant:

One Lycoming IO-540 (6 cylinder, fuel injected, horizontally opposed, 540 cubic inch displacement) developing 300 bhp @ 2700 rpm driving a 3 blade constant speed propeller


Fuel:

AVGAS

Total usable fuel 355 L

Fuel flow 60 L/hour


Weights (normal operation):

Basic Empty Weight 975 Kg 2149 lb

Maximum Take-off Weight 1633 Kg 3600 lb

Maximum Landing Weight 1633 Kg 3600 lb


Operating speeds:

Never exceed speed Vne 191 kts

Maximum structural cruise Vno 148 kts

Maneuvering Va 3600 lb 132 kts, 2170 lb 106 kts

Maximum gear extension speed Vle 129 kts

Maximum gear operation speed Vlo 106 kts

Maximum flap extension speed Vfe 106 kts


Avionics:

Dual VHF (Collins VHF 251)

Dual NAV (Collins VIR 351)

Single ADF (Collins ADF-650)

Single DME (King KN 64)

Single Transponder (Collins TDR-950)

II Morrow Apollo 820 Flybuddy GPS

Piper Altimatic IIIC autopilot

NVFR rated