- Registered owner
- Northrop Grumman Systems Corp
- Location
- El Segundo, CA
- Owner type
- Corporation
- Serial number
- BB-291
- Year built
- 1977
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 30, 2013
- Certificate issued
- October 8, 2015
- Expires
- October 31, 2028
- Mode S code
- A2FA77
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 59
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 | 3 |
| 1976 | 5 |
| 1977 | 4 |
| 1978 | 3 |
| 1979 | 1 |
| 1980 | 3 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 4 |
| 1998 | 4 |
| 2003 | 3 |
| 2004 | 3 |
| 2005 | 5 |
| 2006 | 1 |
| 2008 | 3 |
| 2012 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2025 | 1 |
See all 61 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N291PAMatched 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 Beech 200 aircraft
FAA incident reports
No FAA accident or incident reports matched to N291PAMatched 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 Beech 200 aircraft
Service difficulty reports · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
STCs that may be installed · 422
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 200
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA4175NMInstallation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft.STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.