N141WEDouglas DC-10-40F
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched26 service difficulty reports
Registration
FAA Aircraft Registry · Oct 19, 2026- Registered owner
- Omega Air INC
- Owner type
- Corporation
- City, state
- San Antonio, TX
- Certificate issued
- Dec 5, 2023
- Expires
- Dec 31, 2030
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
- Douglas
- Model
- DC-10-40F
- Serial number
- 46661
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 380
- Engines
- 3
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A0A860
Engine
- Type
- Turbo-jet
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2023 – nowOmega Air INCSan Antonio, TX · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (0)
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.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (26)
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.
- Engine indicating · indicator · inoperativeFeb 22, 2009
TAKEOFF ABORTED FROM MHLM AT 110 KTS. ON TAKEOFF ROLL ENGINE NR 2 EPR GAUGE FAILED AT 1.20 EPR. POINTER AND ANALOG DIGITS FAILED IN PLACED WITH NO FLAG IN VIEW. TRANSFERRED TO DMI 22467, PLACARD INSTALLED, PER MEL 77-3-2, PAGE 77-2. REMOVED AND REPLACED NR 2 EPR INDICATOR IAW MM 77-13-02.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · cowling · delaminatedDec 4, 2002
DURING SCHEDULED MAINTENANCE, NR 1 FAN COWL PREVIOUS REPAIR WAS FOUND DELAMINATED ON THE INBOARD LOWER CORNER. REPAIRED IAW AS11 DRAWING AS11476, DOUBLER REPAIR. AIRCRAFT RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · thrust reverser · debondedNov 3, 2002
DURING ROUTINE MAINTENANCE, THE NR 2 ENGINE THRUST REVERSER INNER SURFACE WAS FOUND DEBONDED. REMOVED DEBONDED AREA, FABRICATED DOUBLER REPAIR AND REPAIRED AREA IAW AS11 DRAWING AS11465, AND AN 8110-3 WAS ISSUED. RETURNED AIRCRAFT TO REVENUE SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Hydraulic power · hydraulic system · malfunctionedApr 27, 2002
FLT 558 - MSLP-KMIA - DURING CLIMB-OUT, LOST HYDRAULIC SYSTEMS ONE AND TWO. RETURNED TO MSLP AND A NORMAL LANDING WITHOUT INCIDENT WAS MADE. NR 1 TIRE MISSING A LARGE SECTION OF TREAD, NR 5 TIRE DAMAGED BY GROUND DEBRIS. BOTH NR 1 AND 5 WHEELS WERE INTACT. LEFT WING INBOARD FLAP WELL AREA HAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · thrust reverser · damagedDec 1, 2001
DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN AS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-GO8284 AND A 8110-3 WAS ISSUED. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedDec 1, 2001
DURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 47L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO-G08333. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · crackedDec 1, 2001
DURING C-CHECK, FOUND LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-G08321 REV IR AND FAA FORM 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · corrodedDec 1, 2001
DURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · thrust reverser · damagedDec 1, 2001
DURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284 AND A 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · corrodedDec 1, 2001
DURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO-G08333. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 26 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026