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TCDS A-787

Historical · Aircraft · Small Airplane · Rev 32 (08/12/1994) · FAA TCDS database

Univair Aircraft Corporation drs.faa.gov ↗

The TCDS PDF on drs.faa.gov is authoritative for design-as-certified weight limits, performance, equipment and operating limitations.

Models covered (10)

Airworthiness directives (12) · mandatory: an aircraft out of compliance is not airworthy

  • 2012-27457 Airworthiness Directives; Univair Aircraft Corporation Airplanes 2012-11-13
  • 2012-21018 Airworthiness Directives; Univair Aircraft Corporation Airplanes 2012-08-29
  • 2011-9091 Airworthiness Directives; Univair Aircraft Corporation Models (ERCO) 415-C, 415-CD, 415-D, E, G; (Forney) F-1 and F-1A; (Alon) A-2 and A2-A; and (Mooney) M10 Airplanes 2011-04-14
  • 03-25699 Airworthiness Directives; Univair Aircraft Corporation Models Alon A-2 and A2-A; ERCO 415-C, 415-CD, 415-D, 415-E, and 415-G; Forney F-1 and F-1A; and Mooney M10 Airplanes 2003-10-14
  • 03-13511 Airworthiness Directives; Univair Aircraft Corporation Models Alon A-2 and A2-A; ERCO 415-C, 415-CD, 415-D, 415-E, and 415-G; Forney F-1 and F-1A; and Mooney M10 Airplanes 2003-05-30
  • 02-32885 Airworthiness Directives; Univair Aircraft Corporation Models Alon A-2 and A2-A; ERCO 415-C, 415-CD, 415-D, 415-E, and 415-G; Forney F-1 and F-1A; and Mooney M10 Airplanes 2003-01-02
  • 02-19874 Airworthiness Directives; Univair Aircraft Corporation Models (ERCO) 415-C, (ERCO) 415-CD, (ERCO) 415-D, (ERCO) 415-E, (ERCO) 415-G, (Forney) F-1, and (Forney) F-1A Airplanes 2002-08-12
  • 02-8989 Airworthiness Directives; Univair Aircraft Corporation Models (ERCO) 415-C, (ERCO) 415-CD, (ERCO) 415-D, (ERCO) 415-E, (ERCO) 415-G, (Forney) F-1, and (Forney) F-1A Airplanes 2002-04-15
  • 02-7996 Airworthiness Directives; Univair Aircraft Corporation Alon A-2 and A2-A, ERCO 415-C, 415-CD, 415-D, E, and G, Forney F-1 and F-1A, and Mooney M10 Airplanes 2002-04-03
  • 01-24782 Airworthiness Directives; Univair Aircraft Corporation Models (ERCO) 415-C, (ERCO) 415-CD, (ERCO) 415-D, (ERCO) 415-E, (ERCO) 415-G, (Forney) F-1, and (Forney) F-1A Airplanes 2001-10-04
  • 94-8681 Airworthiness Directives: Univair Aircraft Corporation Models Ercoupe 415-C, 415-CD, 415-D, 415-E, and 415-G, Forney F-1 and F-1A, Alon A-2 and A-2A, and Mooney M10 Airplanes 1994-04-12
  • 94-4837 Airworthiness Directives; Teledyne Continental Motors Models C75, C85, C90, C125, C145, O-200, O-300, and GO-300 Series Reciprocating Engines 1994-03-03

SAIBs (3)

  • CE-19-20 Flight Compartment Windows
  • NM-07-39R1 Powerplant System: Forward bearing fitting attach bolts
  • NM-07-48 Flight Controls Aileron Boost Bellcrank Lug

Special conditions + ELOS findings

  • ELOS ST17976LA-T-25.251 Equivalent Level of Safety (ELOS) Finding for Vibration/Buffeting Compliance Criteria for Externally Mounted Installations
  • ELOS ENV24021-25.251(b) Equivalent Level of Safety (ELOS) Finding for Vibration/Buffeting Criteria for Externally Mounted Installation
  • ELOS ST07784DE-T-25.251(b)-1 Equivalent Level of Safety (ELOS) Finding for Vibration/Buffeting Compliance Criteria for External Modifications
  • ELOS AT5177AT-T-S-29 Information: Equivalent Level of Safety Finding for Gulfstream Models GV-SP and GIV-X FAA Project Number Nos. AT5177AT-T and AT5080AT-T, respectively

Certification basis — 14 CFR

Former holders

  • Alon
  • Mooney
  • ERCO
  • Forney

Comments

CAR 3, effective December 15, 1946 with no amendments, no exemptions. Type Certificate No.787 issued June 13, 1947. Application for Type certificate dated February 6, 1947.

Fleet view · 277 registered tails · FAA registry, median and p10–p90

Seats
2
n=277
Horsepower
95
n=271
Cruise (kts)
93
90–93
Year of mfr
1966
1946–1970

Engines on the type, by tail count

  • CONT MOTOR C90 SERIES 255
  • CONT MOTOR C85 SERIES 10
  • LYCOMING 0-320 SERIES 1
  • CONT MOTOR C90-16F 1
  • LYCOMING 0-290 SERIES 1
  • CONT MOTOR C85-12 1
  • CONT MOTOR A&C75 SERIES 1
  • CONT MOTOR C85-12F 1
NTSB events
75
across all model variants
Applicable ADs
119
FAA airworthiness directives
Per-tail rate
0.27 events / tail · 0.43 ADs / tail