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About: dbkwik:resource/eq-UmE9__zVTMu3H_UmhfQ==

PropertyValue
rdf:type
rdfs:label
  • AISA I-115
rdfs:comment
  • 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. After retirement in 1976 many were sold to civil operators.
owl:sameAs
empty weight kg
  • 612
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
ceiling ft
  • 14430
climb rate ftmin
  • 686
met or eng?
  • met
eng1 type
  • ENMA Tigre G-IV-B four cylinder inverted aircooled
endurance h
  • at 70% power 3
gross weight kg
  • 900
length in
  • 1
endurance min
  • 30
Introduced
  • 1956
primary user
Type
  • Basic trainer
eng1 kW
  • 112
wing area sqft
  • 150.600000
height m
  • 2.100000
Height in
  • 10
span m
  • 9.540000
climb rate ms
  • 3.750000
Manufacturer
  • AISA
max speed kmh
  • 240
empty weight lb
  • 1346
ceiling m
  • 4400
cruise speed kmh
  • 204
length m
  • 7.350000
max speed mph
  • 149
National Origin
  • Spain
length ft
  • 24
Developed From
Height ft
  • 6
First Flight
  • 1952-06-20
span ft
  • 31
cruise speed mph
  • 127
gross weight lb
  • 1980
span in
  • 3
wing area sqm
  • 14
Retired
  • 1976
Crew
  • 2
Number Built
  • c.200
eng1 hp
  • 150
eng1 number
  • 1
abstract
  • 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. After retirement in 1976 many were sold to civil operators.