Latin American Military - Argentina - Policía de la Provincia de Buenos Aires (PBA) - Stinson 108 Voyager

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Revised: October 14, 2007
Copyright © 1997-2010 by Jean Charles Barroux - jbarroux@LAMilitary.org

Some five Stinson 108 Voyager, LQ-XXG (C/N 108-403), LQ-XYW (C/N 108-483), LQ-ZDW (C/N 108-1507), LQ-ZDU (C/N 108-3722) and LQ-YSF (C/N 108-2606), were acquired in 1937 and some served until 1959. They were used mostly for liaison, patrol, highway search, transport and MEDEVAC functions.

Stinson 108 Voyager

Stinson 108-1 Voyager light utility

Designation: Stinson 108-1 Voyager
Manufacturer: The Stinson Aircraft Division of the Aviation Manufacturing
   Corp., U.S.A.
Crew: 1+1
Passengers: None.
Construction: High-wing cabin monoplane.
Engine: 1 x Lycoming O-435-1
Engine Type: Piston
Engine Thrust: 135 kW (--- hp)
Propeller: --- x --- bladed constant speed
Length: --- m
Height: --- m
Wing Span: --- m
Wing Area: --- m2
Empty Weight: --- kg
Max. Weight: --- kg
Max. Speed: 210 km/h
Stall Speed: --- km/h
Max. Speed at Sea Level: --- km/h
Max. Cruising Speed: --- km/h
Normal Cruising Speed: --- km/h
Initial Rate of Climb: --- ft./min
Ceiling: --- ft. (4,810 mts)
Fuel Capacity: --- lts
Range on Internal Fuel: 805 km
Range with Max. Fuel: 805 km
Range with Max. Payload: --- km
Endurance: --- Hrs
Useful Load: --- kg
Take-off Distance: --- m
Landing Distance: --- m
Radar: None.
EW: None.
Avionics: ---
Weapons: None.
Format: 1.0
Notes: 

S/N       C/N        Unit          Built       Bought      Disposition         Notes
LQ-XXG    108-403    DOAPBA        --/---/---- --/---/1937 wfu --/---/1959
LQ-XYW    108-483    DOAPBA        --/---/---- --/---/1937 wfu --/---/1959
LQ-ZDW    108-1507   DOAPBA        --/---/---- --/---/1937 wfu --/---/1959

Stinson 108-2 Voyager light utility

Designation: Stinson 108-2 Voyager
Manufacturer: The Stinson Aircraft Division of the Aviation Manufacturing
   Corp., U.S.A.
Crew: 1+1
Passengers: None.
Construction: High-wing cabin monoplane.
Engine: 1 x Lycoming O-435-1
Engine Type: Piston
Engine Thrust: 135 kW (--- hp)
Propeller: --- x --- bladed constant speed
Length: --- m
Height: --- m
Wing Span: --- m
Wing Area: --- m2
Empty Weight: --- kg
Max. Weight: --- kg
Max. Speed: 210 km/h
Stall Speed: --- km/h
Max. Speed at Sea Level: --- km/h
Max. Cruising Speed: --- km/h
Normal Cruising Speed: --- km/h
Initial Rate of Climb: --- ft./min
Ceiling: --- ft. (4,810 mts)
Fuel Capacity: --- lts
Range on Internal Fuel: 805 km
Range with Max. Fuel: 805 km
Range with Max. Payload: --- km
Endurance: --- Hrs
Useful Load: --- kg
Take-off Distance: --- m
Landing Distance: --- m
Radar: None.
EW: None.
Avionics: ---
Weapons: None.
Format: 1.0
Notes: 

S/N       C/N        Unit          Built       Bought      Disposition         Notes
LQ-ZDU    108-3722   DOAPBA        --/---/---- --/---/1937 wfu --/---/1959
LQ-YSF    108-2606   DOAPBA        --/---/---- --/---/1937 wfu --/---/1959

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