Latin American Military - Argentina - Policía de la Provincia de Buenos Aires (PBA) - Stinson SR-9D and SR-10ED Reliant

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

One Stinson SR-9D Reliant, LQ-XAE (C/N 5455), was acquired at the end of the 30s. Initially it was serialled as LV-IAC, then in 1943 as LV-XAE and, in 1953, as LQ-XAE. Also, another Stinson SR-10ED Reliant, LQ-YSG (C/N E5-5954), was acquired at the end of the 30s. They were used mostly for liaison, patrol, highway search, transport and MEDEVAC functions.

Stinson Reliant

Stinson SR-9D Reliant light transport and training

Designation: Stinson SR-9D Reliant
Manufacturer: The Stinson Aircraft Division of the Aviation Manufacturing
   Corp., U.S.A.
Crew: 1+1
Passengers: None
Construction: High wing single engine monoplane
Engine: 1 x  Wright R-760-E2
Engine Type: 7-cylinder radial engine
Engine Thrust: --- kW (285 hp)
Propeller: 1 x 2 bladed constant speed
Length: 8.39 m
Height: 2.59 m
Wing Span: 12.79 m
Wing Area: --- m2
Empty Weight: 1,114 kg
Max. Weight: 1,758 kg
Max. Speed: 235 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. (5,000 mts)
Fuel Capacity: --- lts
Range on Internal Fuel: 1,046 km
Range with Max. Fuel: --- km
Range with Max. Payload: --- km
Endurance: --- Hrs
Useful Load: --- kg
Take-off Distance: --- m
Landing Distance: --- m
Radar: N/A
EW: N/A
Avionics: ---
Weapons: None.
Format: 1.0
Notes: Also known as UC-81, C-81 and AT-19. Designed in 1937.

S/N       C/N        Unit          Built       Bought      Disposition         Notes
LQ-XAE    5455       DOAPBA        --/---/---- --/---/193? wfu --/---/----     Ex-LV-IAC, ex-LV-XAE

Stinson SR-10ED Reliant light transport and training

Designation: Stinson SR-10ED Reliant
Manufacturer: The Stinson Aircraft Division of the Aviation Manufacturing
   Corp., U.S.A.
Crew: 1+1
Passengers: None
Construction: High wing single engine monoplane
Engine: 1 x Wright R-760-E2
Engine Type: 7-cylinder radial engine
Engine Thrust: --- kW (320 hp)
Propeller: 1 x 2 bladed constant speed
Length: 8.39 m
Height: 2.59 m
Wing Span: 12.79 m
Wing Area: --- m2
Empty Weight: 1,114 kg
Max. Weight: 1,758 kg
Max. Speed: 235 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. (5,000 mts)
Fuel Capacity: --- lts
Range on Internal Fuel: 1,046 km
Range with Max. Fuel: --- km
Range with Max. Payload: --- km
Endurance: --- Hrs
Useful Load: --- kg
Take-off Distance: --- m
Landing Distance: --- m
Radar: N/A
EW: N/A-
Avionics: ---
Weapons: None.
Format: 1.0
Notes: Also known as UC-81, C-81 and AT-19. Designed in 1938.

S/N       C/N        Unit          Built       Bought      Disposition         Notes
LQ-YSG    E5-5954    DOAPBA        --/---/---- --/---/193? wfu --/---/----

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