- Registered owner
- Zangeneh Aeronautics Consulting Inc
- Location
- Irvine, CA
- Owner type
- Corporation
- Serial number
- 19261
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Airworthiness
- Standard, transport
- Airworthiness date
- June 16, 1967
- Certificate issued
- March 6, 2025
- Expires
- March 31, 2032
- Mode S code
- A9BD95
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 33
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1970 | 4 |
|---|---|
| 1971 | 2 |
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 4 |
| 1978 | 1 |
| 1980 | 1 |
| 1986 | 2 |
| 1992 | 1 |
| 1995 | 4 |
| 1996 | 1 |
| 1997 | 3 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2003 | 2 |
| 2005 | 1 |
| 2006 | 1 |
See all 33 ADs
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N727AHMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 727-21 aircraft
FAA incident reports
No FAA accident or incident reports matched to N727AHMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 727-21 aircraft
Service difficulty reports
No reports matched to N727AHGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Boeing 727-21 aircraft
STCs that may be installed · 17
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · Pratt & Whitney JT8D-1
STC SE01588ATInstallation of McClain International JT8D first stage turbine airseal as documented.STC SE2930SOInstallation of an alternate gearbox cover seal utilizing an aluminum retainer .040-inch thick with a molded-in-place elastomeric seal contoured to fit the main housing/cover flange interface.STC SE497NEInstallation of oil tank filler neck check valve assembly.