# Service difficulty reports: N287F, cancelled Sep 13, 2001 A list on [N287F, cancelled Sep 13, 2001](https://openairdocs.org/deregistered/N287F-2001-09-13.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR LR7A9730](https://openairdocs.org/sdr/LR7A9730.md): Nts Valve · failed · Nov 21, 1997 · N287F · Lkheed 188C · Propeller Controlling System > 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 VALVE IAW N ITEM CARD N61-13. OPS AND LEAK CHECK NORMAL. - [SDR LR7A9729](https://openairdocs.org/sdr/LR7A9729.md): Governor · erratic · Nov 18, 1997 · N287F · Lkheed 188C · Propeller Governor > 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 CHECK NORMAL. - [SDR LR7A9723](https://openairdocs.org/sdr/LR7A9723.md): Engine · failed · Oct 14, 1997 · N287F · Lkheed 188C · Engine (Turbine/Turboprop) > 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.md): Windshield · cracked · Sep 11, 1997 · N287F · Lkheed 188C · Flight Compartment Windows > CO-PILOTS WINDSHIELD OUTER PANE CRACKED. REPLACED CO-PILOTS WINDSHIELD. - [SDR 97ZZZX3953](https://openairdocs.org/sdr/97ZZZX3953.md): Stiffener · cracked · Aug 12, 1997 · N287F · Lkheed 188C · Fuselage Miscellaneous Structure > 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 PRESSURE DECK STIFFENER PER LAC SRM CHAPTER 53-1-5 AND REPLACEMENT PER LAC SRM 51-1-9. - [SDR 97ZZZX3951](https://openairdocs.org/sdr/97ZZZX3951.md): Stiffener · cracked · Aug 12, 1997 · N287F · Lkheed 188C · Fuselage Miscellaneous Structure > 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, CRACK TERMINATED IN THE LOWER LEG OF ZEE STIFFENER. STIFFENER REPLACED PER LAC SRM 53-1-5 AND SRM 5 - [SDR 97ZZZX3959](https://openairdocs.org/sdr/97ZZZX3959.md): Skin · cracked · Aug 4, 1997 · N287F · Lkheed 188C · Wing, Plate/Skin > 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. VERIFIED DEFECTS RUNS FORWARD ONLY FROM FASTENER HOLE USING HIGH FREQUENCY EDDY CURRENT BOLT HOLE PROBE - [SDR 97ZZZX3956](https://openairdocs.org/sdr/97ZZZX3956.md): Doubler · cracked · Aug 4, 1997 · N287F · Lkheed 188C · Wing Miscellaneous Structure > 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 BOLT HOLE EDDY CURRENT AFTER FASTENER REMOVAL. REPAIRED BY PATCHING PER DRAWING NR C95-R02 AND SE - [SDR 97ZZZX3955](https://openairdocs.org/sdr/97ZZZX3955.md): Doubler · cracked · Aug 4, 1997 · N287F · Lkheed 188C · Wing Miscellaneous Structure > 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 CRACK PER LAC SRM 57-2-1, PAGE 41. DEFECT CONSIDERED NEGLIGIBLE DAMAGE AFTER CLEAN UP, SEALED ARE - [SDR 97ZZZX3954](https://openairdocs.org/sdr/97ZZZX3954.md): Doubler · cracked · Aug 4, 1997 · N287F · Lkheed 188C · Wing Miscellaneous Structure > 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 AUTHORIZATION TO CONTINUE SERVICE UNTIL PHASE CHECK NOT TO EXCEED 500 HOURS. RE-INSPECTED AREA OF - [SDR 97ZZZX3952](https://openairdocs.org/sdr/97ZZZX3952.md): Support · cracked · Aug 2, 1997 · N287F · Lkheed 188C · Fuselage Miscellaneous Structure > 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 CRACK, 6.5 INCHES, ONE CRACK 1.5 INCHES IN PRESSURE DECK EXTENDED INBOARD FROM STA 124. STA 130 WAS - [SDR 97ZZZX3950](https://openairdocs.org/sdr/97ZZZX3950.md): Doubler · cracked · Aug 1, 1997 · N287F · Lkheed 188C · Wing Miscellaneous Structure > 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 241.75,.50 INCH LENGTH. REPAIRED BY PATCHING PER LAC SRM CHAPTER 57-2-1, PAGE 43. SEALED AREA PER - [SDR 97ZZZM896](https://openairdocs.org/sdr/97ZZZM896.md): Oil Pressure · failed · Jul 26, 1997 · N287F · Lkheed 188C · Engine Oil Pressure > 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' NUT AT RGB PRESSURE TRANSMITTER. OPS CHECK NORMAL, NO LEAKS NOTED. (M) - [SDR LR7A9708R](https://openairdocs.org/sdr/LR7A9708R.md): Turbine · failed · Jul 17, 1997 · N287F · Lkheed 188C · Turbine Section > 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 FOUND IN TAIL PIPE. AIRCRAFT FERRIED TO ANC ON 7/18/97 DUE AKN RUNWAY CLOSURE. NR 4 ENGINE WAS CH - [SDR 97ZZZM894](https://openairdocs.org/sdr/97ZZZM894.md): Turbine · failed · Jul 17, 1997 · N287F · Lkheed 188C · Turbine Section > 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 TAIL PIPE. AIRCRAFT FERRIED TO ANC ON 7/18/97 DUE AKN RUNWAY CLOSURE. NR 4 ENGINE WAS CHANGED. E - [SDR 97ZZZM726](https://openairdocs.org/sdr/97ZZZM726.md): Brush Block · worn · May 23, 1997 · N287F · Lkheed 188C · Propeller/Rotor Anti-Ice/De-Ice System > AT TAKEOFF, NR 1 ENGINE HAD UNCONTROLLABLE FLUCTUATIONS OF PLUS/MINUS 500 RPM. SHUT DOWN ENGINE AND RETURNED TO MAKE LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED BRUSHBLOCK AND OPERATION THEN NORMAL. (M) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N287F' AND deregistration_id = 'N287F-2001-09-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N287F-2001-09-13/reports --- 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.