N286F1960 Lockheed 188C
Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply41 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Rockland Aerospace INC
- Owner type
- Corporation
- City, state
- Crofton, MD
- Certificate issued
- Sep 29, 2009
- Expires
- Sep 30, 2028
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jan 11, 1961
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Lockheed
- Model
- 188C
- Year
- 1960
- Serial number
- 1146
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 102
- Engines
- 4
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A2E4C2
Engine
- Make and model
- Allison 501-D13 Ser
- Type
- Turbo-prop
- Power
- 3750 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2009 – nowRockland Aerospace INCCrofton, MD · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (2)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2006-25-12 | Rolls-Royce Corporation 501-D Series Turboprop Engines | Jan 23, 2007 | Engine (501-D13 SER) |
| 2000-23-10 | Lockheed Model 188A and 188C Series Airplanes | Dec 27, 2000 | Airframe (188C) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (41)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuselage · floor support · corrodedDec 8, 2003
YIP - 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. REMOVED AND REPLACED CORRODED FLOOR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · door frame · crackedSep 20, 2002
YIP - 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. REINSTALLED REPAIR DOUBLERS IAW L-188 SRM…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · corrodedNov 27, 2001
YIP - 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 CORROSION CLEAN OUT BTW WS 67.25 AND 75.23.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · frame · crackedSep 6, 2001
YIP - FOUND FUSELAGE FRAME CRACKED AT FS 388 BETWEEN STRINGERS 72-1. REPAIRED FRAME AT STRINGER 72-1 PER LOCKHEED S/B 706 DWG 842354. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedSep 6, 2001
FOUND FUSELAGE FRAME CRACKED AT FS 407 BETWEEN STRINGERS 1-2. REPAIRED FRAME AT STRINGER 1-2 PER L188 SRM 53-2-3, FIG 2. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floorbeam · corrodedSep 6, 2001
YIP - FOUND FLOORBEAM AT FS 200 RIGHT SIDE NEAR PORTA POTTY AREA CORRODED. REMVOED CORRODED SECTION OF FLOORBEAM AND REPAIRED FS 200 FLOORBEAM PER L-188 SRM 53-2-4, FIG 2 SHEET 1. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedSep 6, 2001
FOUND FUSELAGE FRAME CRACKED AT FS 426 AT STRINGER 1. REPAIRED FRAME AT FS 426 FROM STRINGER 68-4 IAW L-188 SRM 53-2-3. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedSep 6, 2001
YIP - FOUND FUSELAGE FRAME CRACKED AT FS 426 AT STRINGER 71. REPAIRED FRAME AT FS 426 FROM STRINGER 68-4 IAW L-188 SRM 53-2-3. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedSep 6, 2001
YIP - FOUND FUSELAGE FRAME CRACKED AT FS 464 AT STRINGER 70-71. REPAIRED FRAME AT STRINGER 70-71 IAW L-188 SRM 53-2-3, FIG 2. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · corrodedSep 6, 2001
FOUND LIGHT CORROSION ON FRAME AT FS 540 STRINGER 69. REMOVED CORROSION AND REPAIRED FRAME PER L-188 SRM 53-2-3, FIG 2. PLUGGED NEGLIBIBLE HOLES PER L-188 SRM 51-3-6, FIG 1. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 41 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026