# N287F: Lockheed 188C, registration cancelled 2001-09-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 13, 2001 - Status when cancelled: Sale reported - Airframe: [Lockheed 188C](https://openairdocs.org/model/lockheed-188c) (registry code 5262604) - Data sheets: [TCDS 4A22](https://openairdocs.org/tcds/4A22) (OpenAirDocs) - Serial number: 1148 - Type of aircraft: Fixed wing multi engine - Last registry action: September 13, 2001 - Mode S code: A2E879 - Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage) - Owner type: Individual - 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/N287F - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=287F - Page: https://openairdocs.org/deregistered/N287F-2001-09-13 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 188C: https://openairdocs.org/model/lockheed-188c.md ## Service difficulty reports (16) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR LR7A9730](https://openairdocs.org/sdr/LR7A9730), Nov 21, 1997: NTS VALVE. FAILED. NR 2 ENG SHUTDOWN DUE TO RPM FOLLOWING POWER LEVER POSITION. REMOVED AND REPLACED NTS VALVE IAW N ITEM CARD N61-13 AND ALSO, REMOVED AND REPLACED PITCHLOCK VALV - [SDR LR7A9729](https://openairdocs.org/sdr/LR7A9729), Nov 18, 1997: GOVERNOR. ERRATIC. NR 2 ENGINE SHUTDOWN AT 2150Z DUE TO RPM FOLLOWING POWER LEVER POSITION. ERRATIC GOVERNOR VALVE OPERATION. REPLACED NR 1 PROP GOVERNOR PER M/M CARD N61-13. OPS - [SDR LR7A9723](https://openairdocs.org/sdr/LR7A9723), Oct 14, 1997: ENGINE. FAILED. SHUTDOWN NR 1 ENG DUE TO ENG LOW OIL PRESSURE LIGHT ILLUMINATION AND LESS THAN 130 PSI REDUCTION GEAR IN FLIGHT AT 0715Z. REPLACED NR 1 ENGINE PER ONE120. - [SDR LR7A97020](https://openairdocs.org/sdr/LR7A97020), Sep 11, 1997: WINDSHIELD. CRACKED. CO-PILOTS WINDSHIELD OUTER PANE CRACKED. REPLACED CO-PILOTS WINDSHIELD. - [SDR 97ZZZX3953](https://openairdocs.org/sdr/97ZZZX3953), Aug 12, 1997: STIFFENER. CRACKED. DURING SERVICE CHECK AT ANC, THE PRESSURE DECK STIFFENER WAS DISCOVERED CRACKED AT FS 129 WHERE IT ATTACHES TO THE FUSELAGE CIRCUMFERENTIAL. REPLACED ZEE-ANGLE - [SDR 97ZZZX3951](https://openairdocs.org/sdr/97ZZZX3951), Aug 12, 1997: STIFFENER. CRACKED. DURING A SERVICE CHECK AT ANC, NOSE GEAR PRESSURE DECK STIFFENER WAS DISCOVERED CRACKED A FS 150R WHERE THE STIFFENER ATTACHES TO THE FUSELAGE CIRCUMFERENTIAL, - [SDR 97ZZZX3959](https://openairdocs.org/sdr/97ZZZX3959), Aug 4, 1997: SKIN. CRACKED. DURING SERVICE CHECK AT ANC LEFT WING NR 1 PLANK WAS CRACKED AT WS 248. THE CRACK RUNS FORWARD .125 INCH FROM FASTENER HOLE TOWARD FORWARD EDGE OF PLANK. VERIFI - [SDR 97ZZZX3956](https://openairdocs.org/sdr/97ZZZX3956), Aug 4, 1997: DOUBLER. CRACKED. DURING SERVICE CHECK AT ANC, RT WING NR 6 PLANK LEAP DOUBLER WAS DISCOVERED CRACKED AT RWS 257. CRACK RAN BETWEEN FASTENERS. VERIFIED RACK DID NOT CONTINUE BY B - [SDR 97ZZZX3955](https://openairdocs.org/sdr/97ZZZX3955), Aug 4, 1997: DOUBLER. CRACKED. DURING SERVICE CHECK AT ANC, A CRACK WAS DISCOVERED IN LWS 248 DOUBLER AT NR 4 PLANK. CRACK RUNS FORWARD .20 INCH AND AFT .075 INCH FROM FASTENER HOLE. REMOVED - [SDR 97ZZZX3954](https://openairdocs.org/sdr/97ZZZX3954), Aug 4, 1997: DOUBLER. CRACKED. DURING SERVICE CHECK AT ANC, NR 6 LEFT WING PLANK LEAP DOUBLER WAS DISCOVERED CRACKED, LWS 237.30. LONG CRACKS EMANATED FROM FASTENER HOLES. RECEIVED LOCKHEED A - [SDR 97ZZZX3952](https://openairdocs.org/sdr/97ZZZX3952), Aug 2, 1997: SUPPORT. CRACKED. DURING SERVICE CHECK AT ANC, 2 CRACKS WERE DISCOVERED AT BL 40R FLOOR SUPPORT BEAM CAP STA 124. CRACKS EXTENDED FROM UNDER A PREVIOUS REPAIR. TOTAL LENGTH OF CR - [SDR 97ZZZX3950](https://openairdocs.org/sdr/97ZZZX3950), Aug 1, 1997: DOUBLER. CRACKED. DURING SERVICE CHECK INSPECTION AT ANC, A LEAP DOUBLER CRACK WAS DISCOVERED AT WS 240R. CRACK LENGTH WAS 1.3 INCHES; AN ADDITIONAL CRACK WAS DISCOVERED AT RWS 2 - [SDR 97ZZZM896](https://openairdocs.org/sdr/97ZZZM896), Jul 26, 1997: OIL PRESSURE. FAILED. NR 1 ENGINE SHUTDOWN DUE TO INDICATED LOSS OF OIL PRESSURE. NR 1 ENGINE SHUTDOWN AT 1637Z. REPLACED RGB OIL PRESSURE SWITCH (LIGHT STAYS ON), TIGHTENED LOOSE 'B - [SDR LR7A9708R](https://openairdocs.org/sdr/LR7A9708R), Jul 17, 1997: TURBINE. FAILED. NR 4 ENGINE WILL NOT SUSTAIN RPM ABOVE 7000 RPM. PREPARED AIRCRAFT FOR FERRY FLIGHT PER ZIA MAINTENANCE MANUAL GMM 04-07-01 BY INSTALLING FERRY KIT. FRAGMENTS F - [SDR 97ZZZM894](https://openairdocs.org/sdr/97ZZZM894), Jul 17, 1997: TURBINE. FAILED. NR 4 ENGINE WILL NOT SUSTAIN RPM ABOVE 7000 RPM. PREPARED AIRCRAFT FOR FERRY FLIGHT PER ZIAA MM GMM 04-07-01 BY INSTALLING FERRY KIT. BLADE FRAGMENTS FOUND IN T - [SDR 97ZZZM726](https://openairdocs.org/sdr/97ZZZM726), May 23, 1997: BRUSH BLOCK. WORN. AT TAKEOFF, NR 1 ENGINE HAD UNCONTROLLABLE FLUCTUATIONS OF PLUS/MINUS 500 RPM. SHUT DOWN ENGINE AND RETURNED TO MAKE LANDING WITHOUT INCIDENT. MAINTENANCE REPLA ## 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 19920617025219I](https://openairdocs.org/incident/19920617025219I), Jun 17, 1992: Lkheed 188C (N287F), Wichita, KS. NR1 hydraulic system quantity dropping on climb. Returned. Landed safely. Defective fitting on main supply line. - [Incident 19870101005699I](https://openairdocs.org/incident/19870101005699I), Jan 1, 1987: Lkheed 188ALKHEED (N287F), San Antonio, TX, Minor damage. Experienced an engine overspeed after takeoff. Returned and engine was replaced. ## Other aircraft with N287F - [Cancelled 2006-11-09](https://openairdocs.org/deregistered/N287F-2006-11-09): Dassault FALCON 2000EX, S/N 87, built 2006. Exported to Canada. Owner: [Dassault Falcon Jet Corp](https://openairdocs.org/faa-owner/DASSAULT%20FALCON%20JET%20CORP), [Little Ferry, NJ](https://openairdocs.org/faa-place/NJ/Little%20Ferry) --- 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.