- Registered owner
- Rockland Aerospace Inc
- Location
- Crofton, MD
- Owner type
- Corporation
- Serial number
- 1146
- Year built
- 1960
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- January 11, 1961
- Certificate issued
- September 29, 2009
- Expires
- September 30, 2028
- Mode S code
- A2E4C2
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Allison 501-D13 model are included below.
On this page
Airworthiness directives that may apply · 77
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1960 | 6 |
|---|---|
| 1961 | 3 |
| 1962 | 1 |
| 1963 | 3 |
| 1964 | 2 |
| 1965 | 6 |
| 1966 | 3 |
| 1967 | 3 |
| 1968 | 1 |
| 1969 | 3 |
| 1970 | 1 |
| 1974 | 1 |
| 1975 | 3 |
| 1976 | 1 |
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 3 |
| 1981 | 2 |
| 1982 | 1 |
| 1986 | 1 |
| 1987 | 2 |
| 1989 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 2000 | 2 |
| 2003 | 1 |
| 2004 | 1 |
| 2007 | 1 |
| 2015 | 3 |
| 2018 | 1 |
| 2023 | 1 |
| 2026 | 1 |
See all 79 ADs
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N286FMatched 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 Lockheed 188C aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 41
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ZIAA04059Floor Support · corrodedYIP - FOUND RIGHT WING CENTER SECTION RBL 40 AT NR 1 PLANK UPPER SURFACE CORROSION AT FLOOR SUPPORT BRACKET. REMOVED CORROSION AND TREATED AREA PER L-188 SRM 51-2-14. MATERIAL REMOVED IS PAST NEGLIGIBLE LIMITS. REPAIRED AREA PER L-188 SRM 57-2-1, PAGE 19. RSDR ZIAA04058Door Frame · crackedYIP - INVESTIGATE X-RAY INDICATIONS AT 2 RIVETS MARKED IN RED ON OUTER SURFACE OF AFT LOWER CARGO DOOR, LOWER FORWARD CORNER. REMOVED REPAIR DOUBLERS TO INVESTIGATE FUSELAGE SKIN. FOUND EXISTING CRACK WAS STOP DRILLED PER L-188 SRM 53-2-1, FIG 2, SHEET 6. RSDR ZIAA04057Skin · corrodedYIP - REMOVE REPAIR INSTALLATION AT RT WING UPPER SURFACE, WS 70, 7/8 PLANK SEAM FOR CO CONVENIENCE. CONFIRM THE EXTENT OF DAMAGE AT THIS LOCATION. INSTALL REPAIR PER ZANTOP DWG A72-R03. REMOVED EXTERNAL DOUBLERS ON PLANK 7/8 SEAM AT WS 65-83. CONFIRM CORR
See all 41 reportsSTCs that may be installed · 89
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 89 STCs