# N9744C: 1959 Lockheed 188A, registration cancelled 2002-08-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 28, 2002
- Exported to: United Kingdom
- Status when cancelled: Triennial form not returned
- Airframe: [Lockheed 188A](https://openairdocs.org/model/lockheed-188a) (registry code 5262602)
- Engine: [Allison 501-D13 series](https://openairdocs.org/engine/allison-501-d13-series) (registry code 03004)
- Data sheets: [TCDS 4A22](https://openairdocs.org/tcds/4A22), [TCDS E-282](https://openairdocs.org/tcds/E-282) (OpenAirDocs)
- Serial number: 188A1140
- Year built: 1959
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: September 20, 1993
- Certificate issued: November 9, 1970
- Last registry action: April 18, 2000
- Mode S code: AD9568
- Owner when cancelled: [Reeve Aleutian Airways Inc](https://openairdocs.org/faa-owner/REEVE%20ALEUTIAN%20AIRWAYS%20INC)
- Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)
- Owner type: Corporation
- Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N9744C
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9744C
- Page: https://openairdocs.org/deregistered/N9744C-2002-08-28

From the FAA registry file of October 29, 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 188A: https://openairdocs.org/model/lockheed-188a.md

## Service difficulty reports (170, newest 50)

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

- [SDR RAAA01E406](https://openairdocs.org/sdr/RAAA01E406), Apr 11, 2001: FRAME. BENT. DURING SCHEDULED #4 MAINTENANCE CHECK, FOUND FORMER BENT IN BETWEEN STR 36 & 39. REPAIRED FORMER PER L-188 SRM 53-2-3.
- [SDR RAAA01E405](https://openairdocs.org/sdr/RAAA01E405), Apr 11, 2001: FRAME. BENT. DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND FORMER BENT IN BETWEEN STR 34 & 36. REPAIRED FORMER PER SRM 53-2-3.
- [SDR RAAAO1E404](https://openairdocs.org/sdr/RAAAO1E404), Apr 11, 2001: SKIN. TORN. DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND FWD BAGGAGE PIT DOOR SKIN TORN AT LOWER AFT EDGE. REPAIRED PER L-188 SRM 53-2-1 FIG 2. M-54 # 162
- [SDR RAAA01E403](https://openairdocs.org/sdr/RAAA01E403), Apr 11, 2001: FRAME. CORRODED. DURING SCHEDULED NR 4 MAINTENANCE CHECK FOUND CORROSION ON FORMER BETWEEN PREVIOUS REPAIR AND FORMER. REPAIRED PER LKHEED DRAWING 841811.
- [SDR RAAA01E402](https://openairdocs.org/sdr/RAAA01E402), Apr 11, 2001: SKIN. CRACKED. DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND RT WING LOWER NR 2 PLANK CRACKED AT MOUNTING SCREW HOLE NR 3 TANK OVERFLOW VALVE WS 128. REPAIRED IAW LDS DWG 188
- [SDR RAAA01E401](https://openairdocs.org/sdr/RAAA01E401), Apr 11, 2001: SKIN. CORRODED. DURING SCHEDULED NR 4 MAINTENANCE CHECK, FOUND CORROSION IN NR 1 UPPER WING PLANK NUT PLATE HOLES FOR WING TO FUSELAGE FILLET. REPAIRED PLANK PER LUNDBY DESIGN 
- [SDR RAAA00E4009](https://openairdocs.org/sdr/RAAA00E4009), Mar 27, 2000: GENERATOR. DEFECTIVE. NR 3 GEN MECH FAILURE CAME ON AT GATE. DEFERED PER L-188 OPS MANUAL 41.50.31
- [SDR RAAA00E4008](https://openairdocs.org/sdr/RAAA00E4008), Mar 27, 2000: SWITCH. DEFECTIVE. RIGHT EDC LOW PRESSURE LIGHT ILLUMINATED ON ENGINE START. REPLACED LOW OIL PRESSURE SWITCH IAW L-188 M/M 21-1-1, OPS OK.
- [SDR RAAA00E4007](https://openairdocs.org/sdr/RAAA00E4007), Feb 17, 2000: DOOR SEAL. FAILED. RAPID LOSS OF PRESSURIZATION EXPERIENCED AT FL190. EMERGENCY DESCENT ACCOMPLISHED. OVERWEIGHT LANDING ACCOMPLISHED AT 101800 LBS. INSPECTED MCD AREA SEAL RETAIN
- [SDR RAAA00E4006](https://openairdocs.org/sdr/RAAA00E4006), Feb 16, 2000: STRUT. DISCHARGED. LOUD BANG HEARD IN VICINITY OF NOSE WHEEL AREA, CLIMBING THROUGH FLIGHT LEVEL 18,000. ON FIRST LANDING GEAR EXTENSION WE HAD READ UNSAFE NOSE GEAR INDICATION. S
- [SDR RAAA00E4005](https://openairdocs.org/sdr/RAAA00E4005), Jan 7, 2000: LIGHT. INOPERATIVE. AFT EMERGENCY EXIT PULL DOWN LIGHT DOES NOT TEST. REPLACED PULL DOWN LIGHT. OPS CHECKED GOOD PER ECO NR 86-25.
- [SDR RAAA00E4004](https://openairdocs.org/sdr/RAAA00E4004), Jan 7, 2000: LIGHT. FAILED. ROW 15 AISLEWAY EGRESS LIGHT DOES NOT TEST. REPLACED LIGHT ASSY. OPS CHECKED GOOD PER RAA ECO NR 86-25.
- [SDR RAAA00E4003](https://openairdocs.org/sdr/RAAA00E4003), Jan 7, 2000: BATTERY. DISCHARGED. ROW 12L EMERGENCY EXIT ID DOES NOT TEST. REPLACED BATTERY OPS CHECKED PER RAA ECO NR 86-25.
- [SDR RAAA00E4002](https://openairdocs.org/sdr/RAAA00E4002), Jan 7, 2000: BATTERY. DISCHARGED. ROW 12 AISLEWAY EGRESS LIGHT DOES NOT TEST. REPLACED LIGHT ASSY. OPS CHECKED GOOD PER RAA ECO NR 86-25.
- [SDR RAAA00E4001](https://openairdocs.org/sdr/RAAA00E4001), Jan 7, 2000: BATTERY. DISCHARGED. ROW 10 AISLEWAY EGRESS LIGHT DOES NOT TEST. REPLACED BATTERY OPS CHECKED GOOD PER RAA ECO NR 86-25.
- [SDR RAAA99E4084](https://openairdocs.org/sdr/RAAA99E4084), Dec 17, 1999: LIGHT. WON'T TEST. MAIN CABIN DOOR EMERGENCY PULL DOWN LIGHT DOES NOT TEST. REPLACED PULL DOWN LIGHT, OPS CK GOOD PPER RAA ECO NR 86-24.
- [SDR RAAA99E4083](https://openairdocs.org/sdr/RAAA99E4083), Dec 17, 1999: LIGHT. WON'T TEST. AFT EMERGENCY EXIT PULL DOWN LIGHT DOES NOT TEST. REPLACED PULL DOWN LIGHT, OPS CHECK GOOD PER RAA ECO NR 86-24.
- [SDR RAAA99E4082](https://openairdocs.org/sdr/RAAA99E4082), Dec 13, 1999: BATTERY PACK. DISCHARGED. EMERGENCY AISLE LIGHT AT ROW 19 D, E INOP. REPLACED BATTERY PACK AND OPS CHECKED IAW RAA GMM.
- [SDR RAAA99E4081](https://openairdocs.org/sdr/RAAA99E4081), Dec 13, 1999: BATTERY PACK. DISCHARGED. EMERGENCY AISLE LIGHT AT ROW 14 C, D, E INOP. REPLACED BATTERY PACK AND OPS CHECKED IAW RAA GMM.
- [SDR RAAA99E4080](https://openairdocs.org/sdr/RAAA99E4080), Nov 5, 1999: MOUNT. STICKING. EMERGENCY EVACUATION SLIDE AT PAX ENTRY DOOR, STICKING IN FLOOR SLOT. LUBRICATED EVAC SLIDE MOUNTS, OPERATION CHECKED NORMAL.
- [SDR RAAA99E4076](https://openairdocs.org/sdr/RAAA99E4076), Oct 30, 1999: LIGHT. INOP. EMERGENCY PULL DOWN LIGHT AT FLIGHT STATION, DID NOT TEST. REPLACED LIGHT ASSEMBLY.
- [SDR RAAA99E4075](https://openairdocs.org/sdr/RAAA99E4075), Oct 30, 1999: LIGHT. INOP. EMERGENCY PULL DOWN LIGHT AT ROW 12 A & B, DID NOT TEST. REPLACED LIGHT ASSEMBLY.
- [SDR RAAA99E4039](https://openairdocs.org/sdr/RAAA99E4039), Oct 24, 1999: LIGHT. INOP. DURING SCHEDULED NR 1 CHECK, FOUND ROW 12 C, D, E EXIT IDENTIFIER LIGHT WILL NOT TEST. REPLACED LIGHT ASSY.
- [SDR RAAA99E4028](https://openairdocs.org/sdr/RAAA99E4028), Oct 5, 1999: SEAT TRACK. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK CORRODED AT BBL 0 FUS/STA 371-502. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 130.
- [SDR RAAA99E4027](https://openairdocs.org/sdr/RAAA99E4027), Oct 5, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND TRANSVERSE FLOORBEAM CORRODED AT FUS/STA 502 BBL 0 TO LBL 25. REPAIRED AS PER SRM 53-2-4, M-54 NR 129.
- [SDR RAAA99E4026](https://openairdocs.org/sdr/RAAA99E4026), Oct 5, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND TRANSVERSE FLOORBEAM CORRODED AT FUS/STA 637 LBL 0-LBL 20. REPLACED FLOORBEAM AS PER SRM 51-2-9. INSTALLED FLOORBEAM AS PER S
- [SDR RAAA99E4025](https://openairdocs.org/sdr/RAAA99E4025), Oct 5, 1999: SEAT TRACK. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK CORRODED AT FUS/STA 371 TO 502 LBL 26. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 127.
- [SDR RAAA99E4024](https://openairdocs.org/sdr/RAAA99E4024), Oct 5, 1999: SEAT TRACK. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK FLANGE CORRODED AT FUS/STA 654 LBL55. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 126.
- [SDR RAAA99E4023](https://openairdocs.org/sdr/RAAA99E4023), Oct 5, 1999: SEAT TRACK. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND SEAT TRACK CORRODED AT FUS/STA 695 LBL 56. REPLACED SEAT TRACK AS PER ECO 99-05, M-54 NR 125.
- [SDR RAAA99E4073](https://openairdocs.org/sdr/RAAA99E4073), Jun 30, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM, TOP FLANGE AT FS 371 LBL 22 - LBL 58. REPLACED TRANVERSE FLOORBEAM AS PER SRM 51-2-1, M-54 
- [SDR RAAA99E4072](https://openairdocs.org/sdr/RAAA99E4072), Jun 30, 1999: FLOORBEAM. OUT OF LIMITS. DURING SCHEDULED NR 1 CHECK, FOUND TRANVERSE FLOORBEAM DRESSED OUT BEYOND LIMITS, FS 333 LBL 50. REPLACED TRANVERSE FLOORBEAM AS PER SRM 51-2-1, M-54 NR 261.
- [SDR RAAA99E4071](https://openairdocs.org/sdr/RAAA99E4071), Jun 30, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM FS 333 LBL 55, BETWEEN REPAIR AND TOP FLANGE. REPLACED FLOORBEAM AS PER SRM 51-2-1 M-54 NR 2
- [SDR RAAA99E4070](https://openairdocs.org/sdr/RAAA99E4070), Jun 30, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM AT TOP FLANGE FS 309 LBL 29 - LBL 50. REPLACED TRANVERSE FLOORBEAM PER SRM 51-2-1, M-54 NR 5
- [SDR RAAA99E4074](https://openairdocs.org/sdr/RAAA99E4074), Jun 29, 1999: FRAME. MISDRILLED. DURING SCHEDULED NR 1 CHECK, FS 695 FRAME INNER FLANGE HAS RANDOM HOLES DRILLED IN AFT VERTICAL FLANGE BETWEEN S-54 AND S-54A, L-H. REPAIRED AS PER LDS DRAWING 
- [SDR RAAA99E4069](https://openairdocs.org/sdr/RAAA99E4069), Jun 29, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM AT TOP FLANGE FS 293 LBL 22 - LBL 52. REPLACED TRANVERSE FLOORBEAM AS PER SRM 51-2-1 M-54 NR
- [SDR RAAA99E4068](https://openairdocs.org/sdr/RAAA99E4068), Jun 29, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM AT TOP FLANGE FS 275, LBL 22-LBL 52. REPLACED FLOORBEAM AS PER SRM 51-2-1, M-54 NR 256.
- [SDR RAAA99E4067](https://openairdocs.org/sdr/RAAA99E4067), Jun 29, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANSVERSE FLOORBEAM CAP AT FS 236 LBL 27 - LBL 60. REPLACED FLOORBEAM AS PER SRM 51-2-1 M-54 NR 251.
- [SDR RAAA99E4066](https://openairdocs.org/sdr/RAAA99E4066), Jun 29, 1999: INTERCOSTAL. CRACKED. DURING SCHEDULED NR 1 CHECK, FOUND INTERCOSTAL ATTACH ANGLE CRACKED AT FS 502 RBL 13. REPLACED INTERCOSTAL AS PER SRM 51-2-7 M-54 3 250.
- [SDR RAAA99E4065](https://openairdocs.org/sdr/RAAA99E4065), Jun 29, 1999: ANGLE. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON FLOORBOARD ATTACH PLATE AT FS 588-610 LBL 60. INSTALLED NEW ATTACH ANGLE AS PER SRM 51-2-7 M-54 NR 248.
- [SDR RAAA99E4063](https://openairdocs.org/sdr/RAAA99E4063), Jun 29, 1999: FRAME. DAMAGED. DURING SCHEDULED NR 1 CHECK, FOUND CIRCUMFERENTIAL FRAME BENT AND HOLE TORN AT FS 654, 5-50. REPLACED FRAME TIP AS PER SRM 51-2-12, M-54 NR 246.
- [SDR RAAA99E4062](https://openairdocs.org/sdr/RAAA99E4062), Jun 29, 1999: FRAME. CRACKED. DURING SCHEDULED NR 1 CHECK, FOUND CIRCUMFERENTIAL FRAME CRACKED AT FS 673 AT FLOORBEAM FLANGE RBL 60. REPLACED FRAME SECTION AT FACTORY SPLICE AS PER SRM 51-2-
- [SDR RAAA99E4061](https://openairdocs.org/sdr/RAAA99E4061), Jun 29, 1999: FRAME. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CIRCUMFERENTIAL FRAME CORRODED AT FS 654 AT FLOORBEAM RBL 60. REPLACED FRAME SECTION AT FACTORY SPLICE PER SRM 51-21-1 AND 51
- [SDR RAAA99E4060](https://openairdocs.org/sdr/RAAA99E4060), Jun 29, 1999: FRAME. CRACKED. DURING SCHEDULED NR 1 CHECK, FOUND CIRCUMFERENTIAL FRAME CRACKED AT FLOORBEAM FLANGE FS 597 RBL 60. REPLACED FRAME SECTION AT FACTORY SPLICE AS PER SRM 51-2-1 A
- [SDR RAAA99E4059](https://openairdocs.org/sdr/RAAA99E4059), Jun 25, 1999: SKIN. PUNCTURED. DURING SCHEDULED NR 1 CHECK, AIRCRAFT DAMAGED BY STAND, HOLE PUNCHED IN FUSELAGE SKIN AT FS 1130 STRINGER 42 DAMAGED. REPAIRED STRINGER AS PER SRM 53-3-2. REPAI
- [SDR RAAA99E4058](https://openairdocs.org/sdr/RAAA99E4058), Jun 14, 1999: FLOORBEAM. OUT OF LIMITS. DURING SCHEDULED #1 CHECK, FOUND FLOOR BEAM DRESSED OUT BEYOND LIMITS @ TRACK ATTACH FASTENER ON AFT FLANGE FUS/STA 654 LBL 55. REPLACED FLOOR BEAM AS PER SRM 5
- [SDR RAAA99E4057](https://openairdocs.org/sdr/RAAA99E4057), Jun 11, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANSVERSE FLOORBEAM, TOP CAP FS 920 BL 0. REPAIRED AS PER SRM 53-2-4, M-54 NR 232.
- [SDR RAAA99E4056](https://openairdocs.org/sdr/RAAA99E4056), Jun 11, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION AT TRANSVERSE FLOORBEAM TOP CAP FS 901 BL 0. REPAIRED AS PER SRM 53-2-4, M-54 NR 231.
- [SDR RAAA99E4055](https://openairdocs.org/sdr/RAAA99E4055), Jun 11, 1999: INTERCOSTAL. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON INTERCOSTAL FS 863-920 BL 0. REPLACED INTERCOSTAL AS PER SRM 51-2-12.
- [SDR RAAA99E4054](https://openairdocs.org/sdr/RAAA99E4054), Jun 10, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED # 1 CHECK, FOUND CORROSION ON TRANSVERSE FLOOR BEAM, UPPER FLANGE @ FUS/STA 274 LBL 54. REPLACED FLOOR BEAM AS PER SRM 51-2-1 M-54 # 229.
- [SDR RAAA99E4053](https://openairdocs.org/sdr/RAAA99E4053), Jun 10, 1999: FLOORBEAM. CORRODED. DURING SCHEDULED NR 1 CHECK, FOUND CORROSION ON TRANVERSE FLOORBEAM, UPPER FLANGE FS 293 LBL 40. REPLACED FLOORBEAM AS PER SRM 51-2-1 M-54 NR 228.

All 170: https://openairdocs.org/deregistered/N9744C-2002-08-28/reports.md

## FAA accident and incident reports (2)

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 19970502015819I](https://openairdocs.org/incident/19970502015819I), May 2, 1997: Lkheed 188A (N9744C), Bethel, AK. Narrative: #3 engine was shut down by the flight crew after a fire warning light illuminated on decent into st. paul island. Crew obtained clearance from…
- [Incident 19780807050449I](https://openairdocs.org/incident/19780807050449I), Aug 7, 1978: Lkheed 188LKHEED/ (N9744C), Anchorage, AK. Overhead life raft fell down and injured passenger.

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