# N162AT: Lockheed L-1011-385-3, registration cancelled 2016-01-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 12, 2016
- Exported to: Panama
- Status when cancelled: Valid registration
- Airframe: [Lockheed L-1011-385-3](https://openairdocs.org/model/lockheed-l-1011-385-3) (registry code 5265020)
- Engine: [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series) (registry code 54555)
- Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE) (OpenAirDocs)
- Serial number: 1220
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 19, 1999
- Certificate issued: December 2, 2015
- Last registry action: December 2, 2015
- Mode S code: A0F92E
- Owner when cancelled: [Barq Aviation Inc](https://openairdocs.org/faa-owner/BARQ%20AVIATION%20INC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.7635° N, 80.3127° W: Placed by OpenAirDocs at the center of ZIP code 33144, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N162AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=162AT
- Page: https://openairdocs.org/deregistered/N162AT-2016-01-12

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Lockheed L-1011-385-3: https://openairdocs.org/model/lockheed-l-1011-385-3.md

## Service difficulty reports (73, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR AMTA200800031](https://openairdocs.org/sdr/AMTA200800031), Jan 23, 2008: CHARGER. INOPERATIVE. EMERGENCY POWERPACK AT R2 DOOR, INOPERATIVE. REPLACED EMERGENCY POWERPACK WITH SERVICEABLE UNIT. OPS CHECKS GOOD REF AMM 33-51-03. (K)
- [SDR AMTA200800010](https://openairdocs.org/sdr/AMTA200800010), Jan 7, 2008: WIRE. SHORTED. EMERGENCY LIGHT PATHWAY LIGHT AT FWD GALLEY AND RT FWD CABIN INOPERATIVE. DRIED OUT WET WIRES AND PLUGS BY A2 LAVATORY. OPS CHECK GOOD. (K)
- [SDR AMTA200700506](https://openairdocs.org/sdr/AMTA200700506), Oct 15, 2007: COMPUTER. UNSERVICEABLE. RUDDER HYDR LIMITER ANNUNCIATION LIGHT ON. RUDDER LIMITER PANEL HYDR PUSH LT OFF. REMOVED AND REPLACED NR 2, CADC IAW MM 34-14-01, OPS CHECK GOOD. (K)
- [SDR AMTA200700478](https://openairdocs.org/sdr/AMTA200700478), Oct 4, 2007: UNKNOWN. UNKNOWN. REJECTED T/O, SPEED 70 KTS, WEIGHT 380.0 LBS. PERFORMED CLAPPER LUB IAW MM 72-31-05. INSPECTED MASTER GB CHIP DETECTOR, NO DEBRIS DETECTED. NO EVIDENCE OF ENG F
- [SDR AMTA200700248](https://openairdocs.org/sdr/AMTA200700248), May 24, 2007: CONNECTOR. CONTAMINATED. FWD GALLEY AND FIRST SECTION OF ESCAPE PATH LIGHTING RT SIDE INOPERATIVE. SYS WAS SHORTED BY WATER. DRIED CONNECTORS AND INSULATED THEM. OPS CHECK NORMAL. (K)
- [SDR AMTA200700126](https://openairdocs.org/sdr/AMTA200700126), Mar 1, 2007: LIGHT. INOPERATIVE. AFT GALLEY EGRESS STRIP INOPERATIVE. REMOVED AND REPLACED AFT GALLEY EGRESS STRIP OPS CHECKS NORMAL. (K)
- [SDR AMTA200700037](https://openairdocs.org/sdr/AMTA200700037), Jan 25, 2007: BEAM. CRACKED. RIGHT WING TE BAT STRUCTURE AREA UPPER LATERAL BEAM FOUND CRACKED AT TWO LOCATIONS, ONE CRACK 2 INCHES AND ONE CRACK .5 INCHES. RIGHT WING TE BAT STRUCTURE CAP 
- [SDR AMTA200700036](https://openairdocs.org/sdr/AMTA200700036), Jan 25, 2007: STRUCTURE. CRACKED. NOSE LANDING GEAR RT DOOR FOUND CRACKED ON UPPER EDGE BETWEEN MID AND AFT HINGE. NLG RT FWD DOOR REMOVED, ROUTED TO SHOP IAW AMM 32-22-01. NLG DOOR CRACK BEYOND
- [SDR AMTA200700035](https://openairdocs.org/sdr/AMTA200700035), Jan 25, 2007: BUSHING. MIGRATED. RT MAIN LANDING GEAR TRUNNION FITTING FORWARD AND AFT LANDING GEAR ATTACHING LUG BUSHINGS FOUND MIGRATED AT IWS 346. REPAIRED IAW EER 13226 WO 319386. REMOVED G
- [SDR AMTA200700020](https://openairdocs.org/sdr/AMTA200700020), Jan 21, 2007: SUPPORT ANGLE. CRACKED. CENTER SECTION LOWER AREA SUPPORT ATTACHMENT ANGLE FOUND CRACKED AT FS 1212, LBL 42.5. REPAIR CARRIED OUT ON CRACKED SUPPORT ANGLE AT FS 1212, LBL 42.5 CENTER S
- [SDR AMTA200600706](https://openairdocs.org/sdr/AMTA200600706), Dec 6, 2006: FEEDER CABLE. BROKEN. THE FORWARD RIGHT SECTION OF EGRESS FLOOR PATH LIGHTING IS INOPERATIVE. FOUND 1 LIGHT STRIP NOT WORKING AND TRACK CABLE ASSEMBLY BROKEN. REPLACED LIGHT STRIP AN
- [SDR AMTA200600690](https://openairdocs.org/sdr/AMTA200600690), Nov 29, 2006: LIGHT. INOPERATIVE. EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT FWD GALLEY. REMOVED AND REPLACED FWD GALLEY LIGHT STRIP, OPS CHECK NORMAL IAW MM. (K)
- [SDR AMTA200600335](https://openairdocs.org/sdr/AMTA200600335), May 15, 2006: LIGHT. INOPERATIVE. EGRESS LTS AT FWD GALLEY AND ROW 5 HJK INOPERATIVE. REPLACED FWD GALLEY LIGHT STRIP. OPS CHECK GOOD. MM REF 33. (K)
- [SDR AMTA200600303](https://openairdocs.org/sdr/AMTA200600303), May 1, 2006: FIXTURE. INOPERATIVE. EGRESS TRACK IN FRONT OF FWD GALLEY INOPERATIVE. REMOVED AND REPLACED EGRESS TRACK IN FRONT OF FWD GALLEY. OPS CHECK GOOD. (K)
- [SDR AMTA200600235](https://openairdocs.org/sdr/AMTA200600235), Mar 31, 2006: FLAP. CRACKED. AN EXISTING REPAIR ON THE L/E OF THE NR 3 LT FLAP OB FOUND TO BE CRACKED ADJACENT TO THE INSERT REPAIR. CRACK IS 1 INCH IN LENGTH AND STARTS AT THE LOWER EDGE O
- [SDR AMTA200600147](https://openairdocs.org/sdr/AMTA200600147), Feb 28, 2006: FLAP. GOUGED. DEEP GOUGE MARKS WERE FOUND ON LT FLAP NR 3 IB RIB ASSY. REPAIRED IAW RS L57-50-34. (K)
- [SDR AMTA200600146](https://openairdocs.org/sdr/AMTA200600146), Feb 28, 2006: SKIN. GOUGED. LT ELEVATOR IB TOP SKIN NEAR LEADING EDGE HAS GOUGES LOCATED JUST AFT OF FWD SPAR SKIN ATTACHMENT AND BETWEEN RIB ATTACHMENT AT ES 113.350 AND 140.349. DAMAGE R
- [SDR AMTA200600123](https://openairdocs.org/sdr/AMTA200600123), Feb 9, 2006: STRUCTURE. CRACKED. BOLT HOLE EDDY CURRENT INSPECTION ON L2 DOOR UPPER FORWARD CORNER DETECTED FOUR CRACKS. L2 DOOR UPPER FORWARD CORNER CRACK DETECTED, UNABLE TO STOP DRILL. NO RE
- [SDR AMTA200600107](https://openairdocs.org/sdr/AMTA200600107), Feb 2, 2006: INTERCOSTAL. CORRODED. CABIN FLOORBOARD SUPPORT INTERCOSTAL FOUND WITH CORROSION BETWEEN FS 313-328 AT APPROX RBL 64. CLEANED AND BLENDED AREA AND FOUND BEYOND NEGLIGIBLE DAMAGE LIMIT
- [SDR AMTA200600113](https://openairdocs.org/sdr/AMTA200600113), Feb 1, 2006: INLET. CORRODED. NR 2 RAM AIR INLET HAS SURFACE CORROSION AT SEVERAL PLACES. CORROSION AT THE NR 2 RAM AIR INLET WAS BLENDED OUT AND FOUND WITHIN LIMITS IAW SRM 51-50-02 FIG 01.
- [SDR AMTA200600118](https://openairdocs.org/sdr/AMTA200600118), Feb 1, 2006: SCOOP. CORRODED. NR 1 RAM AIR INLET SCOOP, INTERNAL AREA HAS SURFACE CORROSION. CLEANED UP CORROSION ON THE RAM AIR LEADING EDGE SCOOP DOUBLER AND FOUND BEYOND ALLOWABLE DAMAGE 
- [SDR AMTA200600110](https://openairdocs.org/sdr/AMTA200600110), Feb 1, 2006: SKIN. CRACKED. X-RAY CARRIED OUT ON R1 DOOR UPPER FORWARD CORNER AND DETECTED FIVE FASTENER HOLES CRACKED. FURTHER INSPECTION FURTHER REVEALED 3 ADDITIONAL HOLES CRACKED. EIGH
- [SDR AMTA200600109](https://openairdocs.org/sdr/AMTA200600109), Feb 1, 2006: SILL. CORRODED. L1 DOOR LOWER SILL BETWEEN FS 281-297 WL 200 FOUND WITH SURFACE CORROSION. L1 DOOR LWR SILL INBOARD TEE ANGLE CORROSION AT CLIP NUT HOLE FOUND BEYOND ALLOWABLE 
- [SDR AMTA200600112](https://openairdocs.org/sdr/AMTA200600112), Feb 1, 2006: SKIN. CORRODED. NOSE GEAR DOOR CUTOUT ALL FOUR CORNER DOUBLERS FOUND WITH RUST. RUST AND CORROSION CLEANED AND BLENDED IAW SRM 51-50-01 FIG 1. BLEND AREA WITHIN SRM 51-50-01 FI
- [SDR AMTA200600102](https://openairdocs.org/sdr/AMTA200600102), Jan 31, 2006: SUPPORT BRACKET. CORRODED. FORWARD CABIN AREA LONGITUDINAL SUPPORTING BRACKET FOUND CORRODED BETWEEN FS 281.5-297 RBL 40. BLENDED FLOOR SUPPORT IAW WITH SRM 51-21-02 AND FOUND WITHIN LIMI
- [SDR AMTA200600106](https://openairdocs.org/sdr/AMTA200600106), Jan 31, 2006: PRESSURE PANEL. CORRODED. NLG COMPT PRESS DECK FOUND WITH CORROSION BETWEEN FS 349-36 LBL 29-31. FORWARD PRESSURE DECK CORROSION DAMAGE BEYOND SRM 53-11-00 FIG 6 LIMITS. REPAIRED DAMAGED
- [SDR AMTA200600101](https://openairdocs.org/sdr/AMTA200600101), Jan 31, 2006: FLOORBEAM. CORRODED. AFT CABIN FLOOR STRUCTURE FLOORBEAM UPPER FLANGE FOUND WITH CORROSION AT FS 1763 LBL 39-55. FLOORBEAM WAS BLENDED AND FOUND BEYOND LIMITS PER SRM 53-21-00. CUTO
- [SDR AMTA200600099](https://openairdocs.org/sdr/AMTA200600099), Jan 31, 2006: STRUCTURE. CORRODED. NR 3 RAM AIR SCOOP UPPER AFT CORNER BETWEEN FS 315-398 AND BETWEEN STRINGER 21-22 FOUND WITH CORROSION INSIDE THE FESC. REMOVED BADLY DAMAGED FITTING P/N 154052
- [SDR AMTA200600095](https://openairdocs.org/sdr/AMTA200600095), Jan 30, 2006: INTERCOSTAL. CRACKED. MID CABIN FLOOR AT FS 1163 LEFT SIDE AT LBL 98 WL 200 INTERCOSTAL DOUBLER FOUND CRACKED. (M)
- [SDR AMTA200600096](https://openairdocs.org/sdr/AMTA200600096), Jan 30, 2006: SUPPORT FITTING. CORRODED. FORWARD WASTE TANK BALL VALVE SUPPORT FITTING CORRODED. SUPPORT FITTING REMOVED AND AREA CORROSION CLEANED IAW SRM 51-20-01. AREA CLEANED WAS FOUND BEYOND LIMIT
- [SDR AMTA200600087](https://openairdocs.org/sdr/AMTA200600087), Jan 30, 2006: FLOOR SUPPORT. CORRODED. PAX CABIN AT FS 1794 LBL 48 DIAGONAL SUPPORT BEAM FOUND CORRODED. CLEANED AND BLENDED CORROSION AND FOUND BEYOND NEGLIGIBLE DAMAGE LIMITS IAW SRM 53-21-00 FIG 8
- [SDR AMTA200600089](https://openairdocs.org/sdr/AMTA200600089), Jan 30, 2006: FLOOR SUPPORT. CORRODED. PAX CABIN AT FS 1763 AT LBL 61 FLOOR SUPPORT FOUND WITH CORROSION. FOUND AREA TO HAVE BEEN PREVIOUSLY REPAIRED. BLENDED CORROSION AN FOUND BEYOND LIMITS OF SRM 
- [SDR AMTA200600086](https://openairdocs.org/sdr/AMTA200600086), Jan 30, 2006: FLOOR SUPPORT. CORRODED. FORWARD CABIN FLOOR SUPPORT STRUCTURE FOUND CORRODED BETWEEN FS 3690389 AND RBL 42-74. FORWARD CABIN FLOOR SUPPORT STRUCTURE CORRODED ON PREVIOUS REPAIR. REPAIR
- [SDR AMTA200600084](https://openairdocs.org/sdr/AMTA200600084), Jan 30, 2006: INTERCOSTAL. CORRODED. FORWARD CABIN FLOOR STRUCTURE BETWEEN FS 328-349 AND LBL 30-56 HAS CORROSION. CLEANED AND BLENDED CORROSION ON INTERCOSTAL AND FOUND BEYOND NEGLIGIBLE DAMAGE IA
- [SDR AMTA200600077](https://openairdocs.org/sdr/AMTA200600077), Jan 25, 2006: FLOOR SUPPORT. CORRODED. FORWARD CABIN FLOOR SUPPORT STRUCTURE FOUND CORRODED BETWEEN FS 313 TO 297 AND BETWEEN LBL 0-15. CLEAN AND BLENDED CORRODED FLOOR SUPPORT IAW SRM 51-21-01. BLEN
- [SDR AMTA200600049](https://openairdocs.org/sdr/AMTA200600049), Jan 20, 2006: ACCESS PANEL. CORRODED. LT UNDER WING SURFACE FUEL TANK 2L ACCESS CUTOUT HOLES FOUND WITH SURFACE CORROSION ON THE FOLLOWING PANELS, 532BB, 532DB, 532FB, 533BB, 533DB, 533FB, 533HB, 53
- [SDR AMTA200600048](https://openairdocs.org/sdr/AMTA200600048), Jan 20, 2006: ACCESS PANEL. CORRODED. LT OVERWING FUEL TANK ACCESS PANEL CUTOUT IS PITTED AND CORRODED AT OWS 452. LT WING UPPER SURFACE AT OWS 452 FUEL TANK ACCESS CUTOUT FLANGE SURFACE CORROSION C
- [SDR AMTA200600047](https://openairdocs.org/sdr/AMTA200600047), Jan 20, 2006: ACCESS PANEL. CORRODED. LEFT OVERWING FUEL TANK ACCESS CUTOUT FLANGE PITTED AND CORRODED AT OWS 70. LEFT WING UPPER SURFACE AT OWS 70 CORROSION CLEANED FROM FUEL TANK ACCESS CUTOUT IAW
- [SDR AMTA200600046](https://openairdocs.org/sdr/AMTA200600046), Jan 20, 2006: ACCESS PANEL. CORRODED. LT OVERWING IWS 412 FUEL TANK ACCESS CUTOUT FLANGES PITTING AND CORRODED. LEFT WING UPPER SURFACE AT IWS 412 CORROSION CLEANED FROM FUEL TANK ACCESS CUTOUT IAW 
- [SDR AMTA200600045](https://openairdocs.org/sdr/AMTA200600045), Jan 20, 2006: SPAR. CORRODED. LT WING OVERWING IWS 241.08 TO 372.64 TE REAR SPAR DOUBLER IS RUSTY. CLEANED MINOR RUST CORROSION IAW SRM 51-10-02. CORROSION CLEANED ARE FOUND WITHIN ALLOWABLE
- [SDR AMTA200600044](https://openairdocs.org/sdr/AMTA200600044), Jan 20, 2006: BRACKET. CRACKED. LEFT WHEEL WELL AT FS 1346 FRAME TO KEELBEAM LONGERON ATTACHMENT ANGLE BRACKET CRACKED. LEFT W/W AT FS 1349 FRAME TO KEELBEAM LONGERON ATTACHMENT FWD AND AFT SU
- [SDR AMTA200600043](https://openairdocs.org/sdr/AMTA200600043), Jan 20, 2006: ANGLE. CORRODED. LT NR 4 TORQUE BOX OWS 20.00 AREA INBOARD UPPER ANGLE CORRODED. LEFT NR 4 TORQUE BOX OWS 020.00 AREA INBOARD UPPER CAP MINOR SURFACE CORROSION CLEANED. CLEANED 
- [SDR AMTA200500514](https://openairdocs.org/sdr/AMTA200500514), Jun 12, 2005: COMPRESSOR. STALLED. NR 3 ENGINE COMPRESSOR STALLED ON CLIMB AT FL 27.0 TGT SPIKED AT 860 DEGREES FOR LESS THAN 2 SECONDS. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN WINDMILLED FOR 40 
- [SDR AMTA200401464](https://openairdocs.org/sdr/AMTA200401464), Dec 2, 2004: POWERPACK. DISCHARGED. R3 AND R4 EXTERIOR EMERGENCY LIGHT SHUT OFF WITHIN 2 MINUTES. REMOVED AND REPLACED EMERGENCY POWER PACK. IAW MM 33-51-03. OK FOR SERVICE.
- [SDR AMTA200401463](https://openairdocs.org/sdr/AMTA200401463), Dec 2, 2004: POWERPACK. DISCHARGED. DURING WALK AROUND, L3 AND L3A DOOR LIGHTS TURN OFF IN 2 MINUTES. REMOVED AND REPLACED EMERGENCY POWER PACK FOR L3 AND L3A DOOR LIGHTS (EXTERIOR). IAW MM 33-51-
- [SDR AMTA200301364](https://openairdocs.org/sdr/AMTA200301364), Nov 5, 2003: WARNING LIGHT. MALFUNCTIONED. NR 2 THRUST REVERSER PRESSURE LIGHT CAME ON INFLIGHT. NO INDICATION THRUST REVERSER DEPLOYED. LIGHT COMES ON AT 95 PERCENT N1.
- [SDR AMTA200301131](https://openairdocs.org/sdr/AMTA200301131), Sep 4, 2003: SLIDE. MALFUNCTIONED. R-1 DOOR WOULD NOT ARM BEFORE FLIGHT. REMOVED AND REPLACED R-1 DOOR SLIDE PER M-11-25-36. OPS CHECK GOOD. (M)
- [SDR AMTA200301126](https://openairdocs.org/sdr/AMTA200301126), Sep 2, 2003: ACTUATOR. INOPERATIVE. R-1 DOOR IS INOPERATIVE ELECTRICALLY. REMOVED AND REPLACED R-1 DOOR ELECT ACTUATOR IAW 52-12-01, OPS CHECKED OK. (M)
- [SDR AMTA200301097](https://openairdocs.org/sdr/AMTA200301097), Aug 27, 2003: MECHANISM. INOPERATIVE. R1 DOOR INOPERATIVE ELECTRICALLY. (M)
- [SDR AMTA200300903](https://openairdocs.org/sdr/AMTA200300903), Jun 21, 2003: ATTACH FITTING. CRACKED. RIGHT WING AFT SPAR OUTBOARD AILERON ATTACH FITTING CRACKED AT SECOND HINGE FROM OUTBOARD. REPLACED FITTING IAW SRM 51-10-01 AND ER/A L10-57R-5202. (M)

All 73: https://openairdocs.org/deregistered/N162AT-2016-01-12/reports.md

## Other aircraft with N162AT

- [Registered now](https://openairdocs.org/aircraft/N162AT): Diamond Aircraft Ind DA 40 NG, S/N 40.NC265, built 2023

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.