AISA I-115

Airplanes

Length

7.35 m

Flat Wing Span

9.54 m

Height

2.1 m

Flat Wing Area

14 m²

Cruise Speed

204 km/h

Max Speed

240 km/h

Max Ceiling

4400 m

Number of Engines

Aircraft Engine

First Flight

1952-06-20

Entry Into service

1956-01-01

Number Built

200

Total Fuel Capacity

135

Pictures

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Aircraft	Total Fuel Capacity
AISA I-115	135

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
American Eagle A-251 Phaeton	Wright R-540 Whirlwind	7.3152	9.4488		Compare
Blackburn Turcock		7.42	9.49		Compare
Airmak J4		7.4	9.44		Compare
Aviamilano Nibbio		7.25	9.5	3	Compare
Arado Ar 76		7.2	9.5		Compare
Blériot-SPAD S.27		7.3	9.72	2	Compare

All data (26 fields)

Name: AISA I-115
Manufacturer: Aeronáutica Industrial S.A.
Description: The AISA I-115 is a low-wing single-engined military primary trainer with tandem seating, which went into service with the Spanish Air Force in 1956.
ICAO Code: I115
First Flight: 1952-06-20
Entry Into service: 1956-01-01
Service End: 1976-01-01
Designer: Aeronáutica Industrial S.A.
Length (m): 7.35
Height (m): 2.1
Cockpit Crew: 2
Max Speed (km/h): 240
Cruise Speed (km/h): 204
Max Ceiling (m): 4400
Rate of Climb (m/s): 3.4849
Endurance (h): 3.5
National Origin: Spain
Number Built: 200
Powerplant Description: 1 × ENMA Tigre G-IV-B four-cylinder inverted air-cooled, 112 kW (150 hp) each
Primary Users: Spanish Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/AISA_I-115
Flat Wing Span (m): 9.54
Flat Wing Area (m²): 14
Wake Category: L
Aircraft Engine: Elizalde Tigre IV
Number of Engines: 1