FAA · Type Certificate Data Sheet
TCDS A-787
Univair Aircraft Corporation
Special Airworthiness Information Bulletins (3)
Advisory bulletins on these airframes. Not mandatory like ADs — but operators tracking AD compliance often miss the SAIB on the same component.
- 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
Certification-time deviations: SCs add requirements where the design is novel; ELOS allows alternative compliance. Most modern types have both.
- 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
Engineering specs aggregated from the FAA Aircraft Registry — what every actually-flying tail under this TCDS reports. Median + 10th–90th-percentile range across the active fleet.
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
The TCDS PDF on drs.faa.gov is the authoritative document for design-as-certified weight limits, performance, equipment, AD compliance times, and operating limitations. Open on drs.faa.gov ↗ DRS frequently breaks — when it does, the fleet view above and the cross-links below are usually what you actually need.