- Owner type
- LLC
- Serial number
- 11298
- Year built
- 1975
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard
- Certificate issued
- May 6, 2021
- Expires
- May 31, 2028
- Mode S code
- A92B6B
Rockwell International 690ATCDS 2A4Airframe · Rockwell International 690AEngine modelAiResearch TPE331-5&6SER
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 26
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1975 | 4 |
| 1977 | 2 |
| 1978 | 1 |
| 1979 | 1 |
| 1984 | 1 |
| 1988 | 1 |
| 1994 | 3 |
| 1995 | 2 |
| 1996 | 1 |
| 1998 | 5 |
| 1999 | 1 |
| 2000 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2010 | 1 |
| 2013 | 1 |
Airframe · Rockwell International 690A
AD 2013-09-05FuselageAD 2009-25-02Upper wing skinsAD 2006-15-01Inboard and center aileron hinge fittingsInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Rockwell International 690A
SAIB 2023-14Landing Gear Retract/Extend SystemNTSB investigations
No NTSB investigations matched to N690HFMatched 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 Rockwell International 690A aircraft
FAA incident reports
No FAA accident or incident reports matched to N690HFMatched 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 Rockwell International 690A aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 96ZZZX848Stator · defectiveDURING C/W WITH AD 95-16-08, FOUND HOT SECTION 3RD STATOR WAS IMPROPER DUE TO NOT BEING STAMPED OR SIGNED AND SERIAL NUMBER OF PART NOT ENTERED.SDR 95ZZZX6459Line · defectiveDURING C/W SL 327, NOTED AFT FLARE ON BLEED LINE HAD ALMOST COMPLETELY WORN AWAY. PART WAS VERY CLOSE TO FAILURE WHICH WOULD HAVE RESULTED IN LARGE BLEED AIR LEAK IN AFT AVIONICS BAY. SUBMITTER RECOMMENDS SB 327 BE C/W ON ALL AFFECTED AIRCRAFT.
STCs that may be installed · 169
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Rockwell International 690A
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller