# N188AT: 1974 Lockheed L-1011-385-1, registration cancelled 2006-04-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 25, 2006
- Status when cancelled: Triennial form not returned
- Airframe: [Lockheed L-1011-385-1](https://openairdocs.org/model/lockheed-l-1011-385-1) (registry code 5265010)
- Engine: [Rolls-Royce RB-211-22 series](https://openairdocs.org/engine/rolls-royce-rb-211-22-series) (registry code 54554)
- Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE), [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (OpenAirDocs)
- Serial number: 193C-1078
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard
- Certificate issued: June 9, 1989
- Last registry action: April 18, 2006
- Mode S code: A15E76
- Owner when cancelled: [Ata Airlines Inc](https://openairdocs.org/faa-owner/ATA%20AIRLINES%20INC)
- Location: [Indianapolis, IN](https://openairdocs.org/faa-place/IN/Indianapolis)
- Owner type: Corporation
- Owner's area on the map: 39.7235° N, 86.3306° W: Placed by OpenAirDocs at the center of ZIP code 46231, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N188AT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=188AT
- Page: https://openairdocs.org/deregistered/N188AT-2006-04-25

From the FAA registry file of October 31, 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-1011-385-1: https://openairdocs.org/model/lockheed-l-1011-385-1.md

## Service difficulty reports (46)

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

- [SDR AMTA200400526](https://openairdocs.org/sdr/AMTA200400526), May 5, 2004: ENGINE. VIBRATION. NR 2 ENGINE EXPERIENCED A SUDDEN INCREASE IN VIBRATION FROM .8 TO 2.5 WITH A SELECTED. WARNING LIGHT WAS ON. SELECTED B DID NOT HELP SHUTDOWN ENGINE AT 1350Z EN
- [SDR AMTA200301515](https://openairdocs.org/sdr/AMTA200301515), Dec 23, 2003: LIGHT. DAMAGED. FOUND EGRESS TRACK DAMAGED AFT OF 39H. REPAIRED DAMAGED EGRESS TRACK AS REQUIRED. (M)
- [SDR AMTA200301175](https://openairdocs.org/sdr/AMTA200301175), Sep 15, 2003: CHARGER. INOPERATIVE. L3 DOOR EXTERIOR EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED L3 DOOR EGRESS LIGHTING POWER PA CHECK IAW MM 33-51-03, OPS. CHECK NORMAL.
- [SDR AMTA200301125](https://openairdocs.org/sdr/AMTA200301125), Sep 3, 2003: SKIN. CORRODED. AFT FUSELAGE SKIN CORRODED. REPAIRED DAMAGED AREA PER ER/A L10-53R-5272. (M)
- [SDR AMTA200301276](https://openairdocs.org/sdr/AMTA200301276), Aug 27, 2003: SKIN. DENTED. FOUND 5R SLAT L/E SKIN DENTED AT MID SECTION. REPAIRED SLAT L/E SKIN IAW SRM 57-51-00, FIG 807. (M)
- [SDR AMTA200301274](https://openairdocs.org/sdr/AMTA200301274), Aug 25, 2003: ATTACH FITTING. BROKEN. LT OUTBOARD AILERON OUTBOARD ACTUATOR WING SIDE ATTACH POINT ANTI-ROTATION TAB BROKEN. REPLACED AILERON ACTUATOR ATTACH FITTING IAW SRM 51-10-01 AND SRM 51-40-0
- [SDR AMTA200301102](https://openairdocs.org/sdr/AMTA200301102), Aug 25, 2003: SHEAR TIE. CRACKED. FRAME, SHEAR TIE CRACKED AND CORRODED OUT OF LIMITS AT FS 1800 FROM STRINGER 33 TO STRINGER 36. REMOVED CRACKED AND CORRODED SECTION OF SHEAR TIE AND REPLACED W
- [SDR AMTA200301266](https://openairdocs.org/sdr/AMTA200301266), Aug 16, 2003: STRINGER. GOUGED. FOUND C2 PIT STRINGER GOUGED AND HAS ENLARGED HOLE. REPAIRED STRINGER IAW SRM 51-50-02 AND 51-21-02. (M)
- [SDR AMTA200301277](https://openairdocs.org/sdr/AMTA200301277), Aug 15, 2003: SKIN. DENTED. FOUND 7R SLAT SKIN DENTED AT OUTBOARD LEADING EDGE. REPAIRED SLAT SKIN IAW SRM 57-51-00, FIG 807. (M)
- [SDR AMTA200301100](https://openairdocs.org/sdr/AMTA200301100), Aug 13, 2003: LONGERON. CORRODED. FOUND LONGERON 30 CORRODED AT APPROX FS 1808 JUST FWD OF APB FRAME. REPAIRED STRINGER IAW SRM 53-13-00 SEE PARTAIL ACCOMPLISHED AND ATTACHED M12A. (M)
- [SDR AMTA200301267](https://openairdocs.org/sdr/AMTA200301267), Aug 12, 2003: WEB. CRACKED. C3 PIT WEB ABOVE STRINGER 29 IS CRACKED. REPAIRED WEB IAW SRM 53-23-00 AND 51-50-01, FIG 2. (M)
- [SDR AMTA200301099](https://openairdocs.org/sdr/AMTA200301099), Aug 12, 2003: FRAME. CORRODED. FOUND BULKHEAD FRAME, CORRODED BETWEEN STRINGER 33 AND STRINGER 39 AT FS 1809 APB. FRAME WAS REPAIRED PER SRM 53-11-00 FIG 848 REF M-12 1342M-12A 10591 ITEMS 5 
- [SDR AMTA200301101](https://openairdocs.org/sdr/AMTA200301101), Aug 11, 2003: STRINGER. CORRODED. FOUND STRINGER CORRODED NEAR APB. REMOVED CORRODED STRINGER SECTION AND REPAIRED IAW SRM 53-13-00. (M)
- [SDR AMTA200301086](https://openairdocs.org/sdr/AMTA200301086), Aug 11, 2003: STIFFENER. CORRODED. FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER AFT OF STRINGER 33, CORRODED AT FRAME ATTACH POINT. INSTALLED FASTENERS AND REPAIR PARTS PER SRM 53-11-00 FIG 8 59.
- [SDR AMTA200301265](https://openairdocs.org/sdr/AMTA200301265), Aug 8, 2003: SKIN. DENTED. FOUND FUSELAGE SKIN DENTED FORWARD OF LAV SERVICE DOOR. REPAIRED FUSELAGE SKIN IAW SRM 53-31-00, FIG 802. (M)
- [SDR AMTA200301278](https://openairdocs.org/sdr/AMTA200301278), Aug 7, 2003: SUPPORT. DAMAGED. INTERIM REPAIR OF CORROSION TO RIGHT MLG TRUNNION LOWER SUPPORT FLANGE REQUIRES PERMANENT REPAIR. APPLIED PERMANENT REPAIR TO BLENDOUTS PER ER/A L10-57R-4741. (
- [SDR AMTA200301279](https://openairdocs.org/sdr/AMTA200301279), Aug 6, 2003: SUPPORT. DAMAGED. INTERIM REPAIR OF LEFT MUG TRUNNION LOWER SUPPORT FLANGE REQUIRES PERMANENT REPAIR. APPLIED PERMANENT REPAIR TO BLENDOUTS PER ER/A L10-57R-4752. (M)
- [SDR AMTA200301094](https://openairdocs.org/sdr/AMTA200301094), Aug 6, 2003: STIFFENER. CORRODED. ON APB RIGHT RADIAL STIFFENER IN C3 CARGO COMP AT STRINGER 25 CORROSION AROUND DRAIN HOLE. REPAIRED APB RT RADIAL STIFFENER AT STRINGER 25 IAW SRM 53-11-00. SEE
- [SDR AMTA200301137](https://openairdocs.org/sdr/AMTA200301137), Aug 6, 2003: THRESHOLD. CRACKED. C-2 CARGO THRESHOLD AFT TOP BEAM/TRACK CRACKED AT FASTENER HOLE WERE FLOOR PANEL AND THRESHOLD MEET. REMOVED AND REPLACED C-2 CARGO THRESHOLD AFT TOP BEAM WITH 
- [SDR AMTA200301135](https://openairdocs.org/sdr/AMTA200301135), Aug 2, 2003: KEELBEAM. CORRODED. TOP PORTION OF LOWER FLANGES OF BOTH KEELBEAMS CORRODED. AREA WAS REPAIRED PER E/R L10-53R-5281. (M)
- [SDR 200201206](https://openairdocs.org/sdr/200201206), Sep 18, 2002: ENGINE. BIRD INGESTION. NR 2 ENGINE SHUTDOWN FOR HIGH VIBS, 2.6 BOTH CHANNELS. OIL PRESSURE 19 PSI, ALL PARAMETERS NORMAL. INSPECTED INLET AND EXHAUST , REMOVED EVIDENCE OF BIRD STRIKE
- [SDR 2002F00812](https://openairdocs.org/sdr/2002F00812), Aug 15, 2002: FUEL FILTER. DIRTY. ON DESCENT NR 3 ENGINE FUEL PRESSURE LIGHT ON, THROTTLES AT IDLE, ENGINE FLAMED-OUT. PERFORMED EMERGENCY RESTART, OK. REMOVED AND REPLACED NR 3 ENGINE LP FUEL F
- [SDR 2002F00431](https://openairdocs.org/sdr/2002F00431), Mar 30, 2002: BULKHEAD. CORRODED. DURING SCHEDULED INSPECTION LEVEL 2 CORROSION DISCOVERED ON BULKHEAD LOWER WEB AT FS 315, LBL 18 TO RBL 18. MAINTENANCE REPLACED THE LOWER WEB IN ACCORDANCE WIT
- [SDR 2002F00433](https://openairdocs.org/sdr/2002F00433), Mar 24, 2002: CHANNEL. CORRODED. DURING SCHEDULED INSPECTION THE LEFT MAIN LANDING GEAR TORQUE BOX LOWER AFT BATHTUB FITTING CHANNEL WAS CORRODED (LEVEL 2). MAINTENANCE REMOVED AND REPLACED THE
- [SDR 2002F00432](https://openairdocs.org/sdr/2002F00432), Mar 19, 2002: DOUBLER. CRACKED. DURING SCHEDULED INSPECTION A 3 INCH CRACK WAS DISCOVERED AT FESC INTERNAL SKIN DOUBLER. MAINTENANCE REPAIRED THE DOUBLER IN ACCORDANCE WITH AMTA ER/A L10-53R-4
- [SDR 2002F00350](https://openairdocs.org/sdr/2002F00350), Mar 15, 2002: SUPPORT. CORRODED. DURING SCHEDULED INSPECTION CABIN FLOORBEAM SUPPORT AT FS 1523, WL 195, RBL 83 HAD LEVEL 2 CORROSION. MAINTEANCE COMPLIED WITH AMTA ERA L10-53R-4737 FS 1523 FLO
- [SDR 2002F00430](https://openairdocs.org/sdr/2002F00430), Mar 12, 2002: FLOORBEAM. CORRODED. DURING SCHEDULED INSPECTION LEVEL 2 CORROSION DISCOVERED ON CABIN FLOORBEAM UPPER CAP, FS 901, WL 200, LBL 115 TO RBL 14. MAINTENANCE REPAIRED THE FLOORBEAM IN 
- [SDR 2002F00323](https://openairdocs.org/sdr/2002F00323), Mar 5, 2002: STRINGER. CORRODED. FORWARD FUSELAGE SECTION, STRINGER 30, FS 235 TO 297, BL 24 HAS LEVEL 2 CORROSION. MAINTENANCE REMOVED AND REPLACED STRINGER 30 AT STATION 235 - 297 IN ACCORDAN
- [SDR 2002F00321](https://openairdocs.org/sdr/2002F00321), Mar 3, 2002: STIFFENER. CRACKED. MAIN FRAME VERTICAL STIFFENER ON FORWARD BULKHEAD OF LEFT ACM BAY IS CRACKED (LOWER STIFFENER) CRACK LENGTH 3.760 INCHES FS 315, BL 36L, WL 125. MAINTENANCE REP
- [SDR 2002F00346](https://openairdocs.org/sdr/2002F00346), Feb 27, 2002: SHEAR TIE. CORRODED. DURING SCHEDULED INSPECTION, FORWARD FUSELAGE SECTION, SHEAR TIE AT FS 297, RBL 8 TO 32 RIGHT WAS CORRODED, LEVEL 2 CORROSION. MAINTENANCE REMOVED AND REPLACED 
- [SDR 2002F00371](https://openairdocs.org/sdr/2002F00371), Feb 25, 2002: FRAME. CRACKED. DURING SCHEDULED INSPECTION MAIN FRAME CHORD FS 315 WAS FOUND CRACKED AT RBL 22. CRACK WAS 1 INCH IN LENGTH. MAINTENANCE COMPLIED WITH ER/A L10-53R-4740, ER/A L
- [SDR 2002F00349](https://openairdocs.org/sdr/2002F00349), Feb 24, 2002: FRAME. CRACKED. DURING SCHEDULED INSPECTION MAIN FRAME, SPLICE ANGLE AND STRAP FOR FS 328 FRAMES WHERE FOUND TO BE CRACKED. 3 CRACKS WERE DISCOVERED AND EACH CRACK WAS 2.00 INC
- [SDR 2002F00385](https://openairdocs.org/sdr/2002F00385), Feb 18, 2002: FLOORBEAM. CORRODED. DURING SCHEDULED INSPECTION FOUND LEVEL 2 CORROSION AT CABIN FLOOR SUPPORT, FLOORBEAM AT FS 865, LBL 34, RBL 39 AS VIEWED FROM LOWER GALLEY. MAINTENANCE REPAIRE
- [SDR 2002F00384](https://openairdocs.org/sdr/2002F00384), Feb 18, 2002: TORQUE BOX. CRACKED. DURING SCHEDULED INSPECTION A 2 INCH CRACK WAS FOUND AT THE LEFT MAIN LANDING GEAR TORQUE BOX AFT WEB WALL, LOWER INBOARD CORNER. MAINTENANCE INSTALLED ANGLE AN
- [SDR 2002F00383](https://openairdocs.org/sdr/2002F00383), Feb 18, 2002: FLOOR SUPPORT. CORRODED. DURING SCHEDULED INSPECTION LEVEL 2 CORROSION WAS FOUND AT CABIN FLOOR SUPPORT, LOWER GALLEY, LOWER T-CAP ABOVE LEFT ELEVATOR DOOR FS 901, WL 190, RBL 55 TO LBL
- [SDR 2002F00382](https://openairdocs.org/sdr/2002F00382), Feb 15, 2002: SKIN. CORRODED. DURING SCHEDULED INSPECTION LEVEL 2 CORROSION FOUND ON LEFT ELEVATOR LOWER SURFACE FROM ES 180 TO ES 451. MAINTENANCE REMOVED AND REPLACED THE LEFT ELEVATOR IN 
- [SDR 2002F00395](https://openairdocs.org/sdr/2002F00395), Feb 14, 2002: FLOOR SUPPORT. CORRODED. DURING SCHEDULED INSPECTION THE CABIN FLOOR SUPPORT FS 1521, RBL 48.5-74.5 WAS FOUND TO HAVE LEVEL 2 CORROSION. MAINTENANCE REPAIRED THE FLOOR SUPPORT AT FS 152
- [SDR 2002F00381](https://openairdocs.org/sdr/2002F00381), Feb 14, 2002: SPLICE. CORRODED. DURING SCHEDULED INSPECTION LEVEL 2 CORROSION FOUND ON MOUNT PAD FOR NOSE LANDING GEAR RIGHT FORWARD GEAR DOOR FORWARD HINGE ATTACH BRACKET TO AIRFRAME, AFT SID
- [SDR 2002F00375](https://openairdocs.org/sdr/2002F00375), Feb 14, 2002: PRESSURE PANEL. CORRODED. DURING SCHEDULED INSPECTION LEVEL 2 CORROSION ON NOSE LANDING GEAR WHEEL WELL TOP PANEL AT FS 369, RBL 22, AFT RIGHT OUTBOARD CORNER OF FORWARD WHEEL WELL PANEL
- [SDR 2002F00322](https://openairdocs.org/sdr/2002F00322), Feb 14, 2002: STRINGER. CORRODED. MID FUSELAGE SECTION, MAIN EQUIPMENT SERVICE CENTER, STRINGER 30, FS 930 TO 983, BL 25 AFT SIDE OF BULKHEAD 943 LEVEL 2 CORROSION. MAINTENANCE REPAIRED IN ACCOR
- [SDR 2002FA0000382](https://openairdocs.org/sdr/2002FA0000382), Feb 13, 2002: STINGER. CORRODED. FORWARD FUSELAGE SECTION, FORWARD E/E, SURFACE CORROSION ON TOP OF STRINGER 38, FS 297 TO FS 312, BL 45. MAINTENANCE REPAIRED STRINGER AT FS 297 TO 312 IAW SB.
- [SDR 99ZZZM48](https://openairdocs.org/sdr/99ZZZM48), Dec 31, 1998: SENSOR. FAILED. DTW - DURING CLIMB, THE LANDING GEAR TRUCK WARNING LIGHT CAME ON. AIRCRAFT WAS RETURNED TO BLOCK. LANDED SAFELY. THE LEFT MAIN LANDING GEAR TRUCK POSITIONER WAS
- [SDR 98ZZZM464](https://openairdocs.org/sdr/98ZZZM464), May 16, 1998: LIGHT. MALFUNCTIONED. DURING CRUISE, THE EMERGENCY EVACUATION LIGHTS CAME ON, HAD TO TURNOFF AT OVERHEAD PANEL. THE EMERGENCY SENSE C/B 'J6' POPPED, WOULD NOT RESET. CONTINUED FLT. T
- [SDR 98ZZZM408](https://openairdocs.org/sdr/98ZZZM408), Jan 2, 1998: LIGHT PANEL. FAILED. CLE - WHEN REMOVING POWER FROM AIRCRAFT ALL EMERGENCY LIGHTS (INSIDE AND OUT) CAME ON. WOULD NOT TURN OFF UNTIL POWER WAS REAPPLIED TO AIRCRAFT. INSTALLED NEW E
- [SDR 95ZZZX5190](https://openairdocs.org/sdr/95ZZZX5190), Jul 8, 1995: SHUT-OFF VALVE. INOPERATIVE. DTW - DURING CLIMB THROUGH 26,000 FEET, NR 3 ENGINE TANK VALVE FLOW BAR LIGHT WENT OUT WHICH WAS ASSOCIATED WITH NR 3 ENGINE FLAMING OUT. ENGINE WINDMILL FOR 20
- [SDR 95ZZZW680](https://openairdocs.org/sdr/95ZZZW680), Mar 28, 1995: TRIPLER. CRACKED. IND - DURING A 'C4' CHECK, THE L1 DOOR WAS FOUND WITH A CRACK AT THE LOWER AFT CORNER, APPROX 1.5 INCHES LONG. A VISUAL INSPECTION DETECTED THIS CRACK TO A TRIP

## FAA accident and incident reports (5)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20010305003899I](https://openairdocs.org/incident/20010305003899I), Mar 5, 2001: Lkheed 10113851 (N188AT), Honolulu, HI, Minor damage. (-23) At approx. 10,000 ft. no. 1 engine experienced an uncontained engine failure. Corrective action will be determined by the chdo.
- [Incident 19980625027709I](https://openairdocs.org/incident/19980625027709I), Jun 25, 1998: Lkheed L10113851 (N188AT), Los Angeles, CA, Minor damage. Capt. nevil, PIC of amta 744 used unsafe thrust management procedures while taxiing into gate 26 at lax. His actions caused a baggage container to become…
- [Incident 19970307006819I](https://openairdocs.org/incident/19970307006819I), Mar 7, 1997: Lkheed 10113851 (N188AT), Denver, CO. Narrative: at approximately 100NM east of the Denver VOR, the crew noticed that they were losing fuel. There was approximately 30,000 lb on board at that time.…
- [Incident 19890712042669I](https://openairdocs.org/incident/19890712042669I), Jul 12, 1989: Lkheed 10113851 (N188AT), Kansas City, MO, Minor damage. Shut down NR3 engine due to oil loss. Diverted to Kansas City. Found small fire in engines. No cockpit warning.
- [Incident 19860714059889I](https://openairdocs.org/incident/19860714059889I), Jul 14, 1986: Lkheed 10113851 (N188AT), Detroit, MI, Minor damage. During climbout left truck unlevel light came on briefly. At destination found fixed main gear door had separated.

## Other aircraft with N188AT

- [Cancelled 2012-10-02](https://openairdocs.org/deregistered/N188AT-2012-10-02): Ayres S-2R, S/N 2569R, built 1982. Exported to Canada. Owner: [Koehn Anthony A](https://openairdocs.org/faa-owner/KOEHN%20ANTHONY%20A), [Bakersfield, CA](https://openairdocs.org/faa-place/CA/Bakersfield)

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