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                             AIRCRAFT GENERAL SPECIFICATIONS

 

  •     VH-WHA

    • 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

     

     

        VH-LSM

    • 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

     

     

     

        VH-LSF

    • 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

     

     

        VH-HSM

    • 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

     

     

        VH-DPH

    • Cessna 182Q Skylane II

    • High wing, 4 seat, utility aircraft with fixed tricycle undercarriage

           Dimensions:

    • Wing span       11.0m              (36ft)

    • Length             8.8m                (29ft)

    • Height             2.8m                (9ft 4in)

           Powerplant:

    • One Continental O-470 (6 cylinder, horizontally opposed, 470 cubic inch displacement) developing 230 bhp @ 2400 rpm driving a 2 blade constant speed propeller

           Fuel:

    • AVGAS

    • Total usable fuel          284 L

    • Fuel flow                        50 L/hour

           Weights (normal operation):

    • Basic Empty Weight                  815 Kg          1830 lb

    • Maximum Take-off Weight    1338 Kg          2950 lb

    • Maximum Landing Weight    1338 Kg          2950 lb

           Operating speeds:

    • Never exceed speed                          Vne                              179 kts

    • Maximum structural cruise             Vno                              143 kts

    • Maneuvering                                    Va        2950 lb            111 kts

    •                                                                        2450 lb            100 kts

    •                                                                        1950 lb              89 kts

    • Maximum flap extension speed     Vfe        10°                   140 kts

    •                                                                         Full                   95 kts

           Avionics:

    • Dual VHF (Cessna 300 RT 385A /Garmin SL 40)

    • Single NAV (Cessna 300 RT 385A)

    • Single ADF (Cessna 300 R 546E)

    • Single Transponder (Cessna 300)

    • Single HF SSB (Barrett F 24)

    • Trimble 1000DC GPS

    • NVFR rated

     

     

        VH-IWL

    • 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

     

     

        VH-CBP

    • Piper PA-23-250 Aztec C

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

           Dimensions:

    • Wing span       10.67m            (37 ft)

    • Length             7.25m              (30ft 2.4in)

    • Height             3.15m              (10ft 4in)

           Powerplants:

    • Two Lycoming IO-540 (6 cylinder, fuel injected, horizontally opposed, 540 cubic inch displacement) developing 250 bhp @ 2575 rpm driving a 2 blade constant speed full feathering propeller

           Fuel:

    • AVGAS

    • Total usable fuel          530 L

    • Fuel flow                      109 L/hour

           Weights (normal operation):

    • Basic Empty Weight                  1457 Kg          3211 lb

    • Maximum Take-off Weight      2359 Kg          5200 lb

    • Maximum Landing Weight      2241 Kg          4940 lb

           Operating speeds:

    • Never exceed speed                              Vne                                221 kts

    • Maximum structural cruise speed       Vno                               175 kts

    • Maneuvering speed                              Va        2325 lb             131 kts

    • Maximum gear extension speed          Vle                                132 kts

    • Maximum flap extension speed           Vfe                                141 kts

           Avionics:

    • Dual VHF/NAV (King KX 175B)

    • Dual ADF (King KR 85)

    • Single Transponder (King KT 76A)

    • Single HF SSB (Barrett F 24)

    • II Morrow Apollo 820 Flybuddy GPS

    • Piper Altimatic IIIC autopilot

    • IFR rated

     

     

        VH-LTU

    • Piper PA-31-350 Navajo Chieftain

    • Low wing, 10 seat, transport aircraft with retractable tricycle undercarriage

           Dimensions:

    • Wing span       10.67m            (40ft 8in)

    • Length             7.25m              (34ft 7.6in)

    • Height             2.23m              (13ft)

           Powerplants:

    • Two Lycoming TIO-540 (6 cylinder, turbocharged, fuel injected, horizontally opposed, 540 cubic inch displacement) developing 350 bhp @ 2575 rpm driving a 3 blade constant speed full feathering propeller

           Fuel:

    • AVGAS

    • Total usable fuel          690 L

    • Fuel flow                      145 L/hour

           Weights (normal operation):

    • Basic Empty Weight                 2124 Kg          4683 lb

    • Maximum Take-off Weight      3342 Kg          7368 lb

    • Maximum Landing Weight     3175 Kg          7000 lb

           Operating speeds:

    • Never exceed speed                            Vne                              236 kts

    • Maximum structural cruise speed     Vno                             185 kts

    • Maneuvering speed                             Va         3342 kg        159 kts

    • Maximum gear extension speed         Vle                             153 kts

    • Maximum flap extension speed          Vfe                             154 kts

           Avionics:

    • Dual VHF (Narco COM 111)

    • Dual NAV (Narco NAV 112/ Narco Nav 122)

    • Dual ADF (King KR 85/Bendix T12D)

    • Single DME (King KN 62A)

    • Single Transponder (King KT 76A)

    • Single HF SSB (Sunair ASB-125)

    • Trimble TNL2000A Approach GPS

    • Piper Altimatic IIIB autopilot

    • IFR rated

     

     

        VH-MZM

    • Piper PA-31-350 Chieftain

    • Low wing, 10 seat, transport aircraft with retractable tricycle undercarriage

           Dimensions:

    • Wing span       10.67m           (40ft 8in)

    • Length             7.25m             (34ft 7.6in)

    • Height             2.23m              (13ft) 

           Powerplants:

    • Two Lycoming TIO-540 (6 cylinder, turbocharged, fuel injected, horizontally opposed, 540 cubic inch displacement) developing 350 bhp @ 2575 rpm driving a 3 blade constant speed full feathering propeller

           Fuel:

    • AVGAS

    • Total usable fuel          690 L

    • Fuel flow                      145 L/hour

           Weights (normal operation):

    • Basic Empty Weight                 2191 Kg          4831 lb

    • Maximum Take-off Weight      3342 Kg          7368 lb

    • Maximum Landing Weight     3175 Kg          7000 lb

           Operating speeds:

    • Never exceed speed                            Vne                                236 kts

    • Maximum structural cruise speed     Vno                               185 kts

    • Maneuvering speed                            Va          3342 kg          159 kts

    • Maximum gear extension speed        Vle                                153 kts

    • Maximum flap extension speed         Vfe                                162 kts

           Avionics:

    • Dual VHF (King KN 196)

    • Dual NAV (Collins VIR 351)

    • Dual ADF (King KR 87/Collins ADF-650A)

    • Single DME (Collins TCR-451)

    • Dual Transponder (King KT 76A)

    • Single HF SSB (Codan HF 2000)

    • King KLN90B GPS                                      

    • King KFC 200 autopilot

    • King RDR-160 weather radar

    • IFR rated

     
 
   
 

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Contact Us

Postal:            R.S.D. 4 Victa Road, Bendigo MC,

                       Victoria 3539 Australia

Airport:          Victa Road, Bendigo Victoria Australia

Phone/fax:       Ph: 03 5443 1030    Fax: 03 5443 1030

Email:             enquiries@bendigoaviation.com.au

 

 
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                                                                                                                                                                                  A division of Gobel Aviation Pty Ltd
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