# N5512: 1958 Lockheed 188A, registration cancelled 2013-08-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 6, 2013
- Status when cancelled: Sale reported, canceled
- 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: 188A-1017
- Year built: 1958
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard
- Airworthiness date: January 3, 1959
- Last registry action: October 21, 2009
- Mode S code: A705C0
- Location: [Crofton, MD](https://openairdocs.org/faa-place/MD/Crofton)
- Owner type: Individual
- Owner's area on the map: 39.0097° N, 76.6839° W: Placed by OpenAirDocs at the center of ZIP code 21114, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N5512
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5512
- Page: https://openairdocs.org/deregistered/N5512-2013-08-06

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 (12)

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

- [SDR ZIAA03003](https://openairdocs.org/sdr/ZIAA03003), May 21, 2003: RELAY. OVERHEATED. LANDED IN TORONTO DUE TO ELECTRICAL SMOKE COMING FROM BEHIND COCKPIT CIRCUIT BREAKER PANEL. REMOVED AND REPLACED NR 2 MAIN DC BUS REVERSE CURRENT CUTOUT RELAY I
- [SDR ZIAA00010](https://openairdocs.org/sdr/ZIAA00010), Jul 27, 2000: PANEL. CRACKED. YIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION BETWEEN NR 45-46 RISERS AT LT WS 200, CRACK SIZE 1.25 BY .375. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAGE 2
- [SDR ZIAA00009](https://openairdocs.org/sdr/ZIAA00009), Jul 27, 2000: PANEL. CRACKED. YIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION COMING FROM UNDER FASTENER BETWEEN NR 19 AND 20 RISERS AT LT WS 170, CRACK SIZE 1.25 BY .5. CLEANED OUT CRAC
- [SDR ZIAA00008](https://openairdocs.org/sdr/ZIAA00008), Jul 27, 2000: PANEL. CRACKED. YIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION IN FORWARD RADIUS OF NR 19 RISER AT LT WS 170, CRACK SIZE 1X.375. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAG
- [SDR ZIAA00007](https://openairdocs.org/sdr/ZIAA00007), Jul 27, 2000: PANEL. CRACKED. YIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION COMING FROM UNDER FASTENER BETWEEN NR 17-18 RISERS AT LT WS 170, CRACK SIZE .75 INCH BY .375. CLEANED OUT CR
- [SDR ZIAA98040](https://openairdocs.org/sdr/ZIAA98040), Oct 23, 1998: FIRE LOOP. MALFUNCTIONED. MEM - SHUTDOWN NR 4 ENGINE DUE TO FIRE WARNING IN ZONES 2/3 AT 1811Z. FIRED BOTTLE AND LIGHTS WENT OUT. AT 1838Z FIRE WARNING IN ZONES 2/3, ENGINE NR 4 CAME ON 
- [SDR ZIAA98010](https://openairdocs.org/sdr/ZIAA98010), Aug 4, 1998: PANEL. CRACKED. YIP - RIGHT DRY BAY UPPER SURFACE CRACK AT WS 200 BETWEEN RISER 40-41 COMING FROM OUTBOARD SKATE ANGLE FASTENERS, ROUTED OUT CRACK. REPAIRED PER ZIA SKETCH NR F
- [SDR ZIAA98008](https://openairdocs.org/sdr/ZIAA98008), Apr 29, 1998: CONNECTOR. SHORTED. LRD - NR 4 ENGINE FIRE WARNING LIGHTS IN ZONES 2 AND 3 ON CONTINUOUSLY. CHECKED AND FOUND CONNECTOR SHORTED ON FIREWALL. REMOVED, CLEANED AND RESECURED CONNECTO
- [SDR ZIAA98006](https://openairdocs.org/sdr/ZIAA98006), Apr 25, 1998: FIRE LOOP. OUT OF POSITION. FIRE WARNING ON NR 3 ENGINE ZONE 1 LIGHT. SHUT DOWN NR 3 ENGINE. INSPECTED ZONE 1 AREA OF NR 3 ENGINE FIRE DETECTION SYSTEM. FOUND NR 3 SWIRL STRAIGHTENER COCKE
- [SDR ZIAA98002A](https://openairdocs.org/sdr/ZIAA98002A), Mar 4, 1998: FIRE LOOP. BROKEN. CAE - DURING DESCENT, NR 4 ENGINE FIRE WARING CAME ON AT 0403Z, SHUT DOWN ENGINE AND DISCHARGED HRD. REMOVED AND REPLACED BROKEN FIRE WARNING LOOP WIRE ON LEFT 
- [SDR ZIAA97040](https://openairdocs.org/sdr/ZIAA97040), Sep 3, 1997: GENERATOR. FAILED. EWR - DURING CLIMB, NR 1 GENERATOR MECHANICAL FAIL LIGHT CAME ON. SHUTDOWN THE ENGINE. REPLACED NR 1 GENERATOR. GROUND TEST NORMAL. (M)
- [SDR ZIAA97010](https://openairdocs.org/sdr/ZIAA97010), Jan 23, 1997: LINKAGE. LOOSE. HUF - DURING TAXI OUT, NR 1 POWER LEVER 1 INCH TO 1.5 INCH OF FREE TRAVEL. RETURNED TO THE RAMP. RETORQUED LINKAGE AT THE FUEL CONTROL. GROUND TEST NORMAL. (M)

## 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 20011119035109I](https://openairdocs.org/incident/20011119035109I), Nov 19, 2001: Lkheed 188A (N5512), Cleveland, OH. (-23) Takeoff aborted, auto feather #3 eng. Initial inspection shows compressor blade damage. Engine s/n 501393. Time remaining to hot section 4846.6
- [Incident 19870926067559I](https://openairdocs.org/incident/19870926067559I), Sep 26, 1987: Lkheed 188ALKHEED (N5512), Kansas City, MO. The right gear failed to indicate down and locked. Aircraft landed safely. Gear down microswitch was readjusted.

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