# N250TR: 1981 Boeing 737-2K5, registration cancelled 2017-10-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 25, 2017 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 737-2K5](https://openairdocs.org/model/boeing-737-2k5) (registry code 138448X) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22597 - Year built: 1981 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 19, 2001 - Certificate issued: June 16, 2011 - Last registry action: June 16, 2011 - Mode S code: A25937 - Owner when cancelled: [Map Asset Preservation LLC](https://openairdocs.org/faa-owner/MAP%20ASSET%20PRESERVATION%20LLC) - Location: [Boca Raton, FL](https://openairdocs.org/faa-place/FL/Boca%20Raton) - Owner type: Corporation - Owner's area on the map: 26.3471° N, 80.1592° W: Placed by OpenAirDocs at the center of ZIP code 33433, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N250TR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=250TR - Page: https://openairdocs.org/deregistered/N250TR-2017-10-25 From the FAA registry file of November 5, 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 Boeing 737-2K5: https://openairdocs.org/model/boeing-737-2k5.md ## Service difficulty reports (105, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR PID2008F00012](https://openairdocs.org/sdr/PID2008F00012), Aug 8, 2008: BATTERY. INOPERATIVE. FOUND FWD F/A FLASHLIGHT NOT WORKING. REPLACED BATTERY IN FLASHLIGHT. OPS CHECK GOOD, AMM 25-69-0. (S) - [SDR PID2008F00006](https://openairdocs.org/sdr/PID2008F00006), Jul 13, 2008: SWITCH. DIRTY. OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN RT ENGINE IAW QRH. DIVERTED FLT, INSPECTED NR 2 MAIN ENGINE OIL FILTER AND CLEANED BYPASS CONNECTOR SWIT - [SDR PID2008F00001](https://openairdocs.org/sdr/PID2008F00001), Jul 13, 2008: BYPASS SWITCH. INOPERATIVE. OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN RT ENGINE IAW QRH. DIVERTED FLT. INSPECTED NR 2 MAIN ENGINE OIL FILTER AND CLEANED BYPASS CONNECTOR SWIT - [SDR PIDA07040](https://openairdocs.org/sdr/PIDA07040), Aug 11, 2007: BATTERY PACK. DISCHARGED. DURING MAINTENANCE, FOUND RIGHT OVERWING EMERGENCY DOOR LIGHT OUT. REPLACED BATTERY PACK AND OPS CHECKED OK. - [SDR PIDA07034](https://openairdocs.org/sdr/PIDA07034), May 21, 2007: FLOORBEAM. CORRODED. DURING MAINTENANCE, NOTED CORROSION ON UPPER FLANGE OF BS 947.5 FLOORBEAM. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-120. - [SDR PIDA07035](https://openairdocs.org/sdr/PIDA07035), May 19, 2007: FLOORBEAM. CORRODED. DURING MAINTENANCE, NOTED CORROSION ON UPPER FLANGE OF BS 986.5 FLOORBEAM. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-115. - [SDR PIDA07033](https://openairdocs.org/sdr/PIDA07033), May 19, 2007: FLOORBEAM. CORRODED. DURING MAINTENANCE, NOTED CORROSION ON UPPER FLANGE OF BS 967.5 FLOORBEAM. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-122. - [SDR PIDA07032](https://openairdocs.org/sdr/PIDA07032), May 8, 2007: SKIN. CRACKED. DURING MAINTENANCE, NOTED A CRACK IN THE AFT UPPER CORNER OF THE AFT CARGO DOOR SKIN AT THE HANDLE ACCESS CUTOUT. REPLACED DOOR SKIN PER DWG 65-47952 AND SRM 51 - [SDR PIDA07030](https://openairdocs.org/sdr/PIDA07030), May 1, 2007: STRUCTURE. CRACKED. DURING MAINTENANCE, NOTED FORWARD AND AFT CORNERS OF THE AFT CARGO DOOR LOWER -T- CORD ARE CRACKED. REPLACED -T- CORD IN ACCORDANCE WITH DRAWING 65C80735 AND SR - [SDR PIDA07031](https://openairdocs.org/sdr/PIDA07031), Apr 30, 2007: STRINGER. CRACKED. DURING MAINTENANCE, NOTED CRACK AT THE END OF STR 16RT AT BS 500B+2. REPAIRED PER SB 737-53-1145. - [SDR PIDA07028](https://openairdocs.org/sdr/PIDA07028), Apr 30, 2007: STRINGER CLIP. CRACKED. DURING MAINTENANCE, NOTED STRINGER 18LT TIE CLIP CRACKED AT BS 277. REPLACED TIE CLIP PER SRM 51-30-02 AND DRAWING 65-73744. - [SDR PIDA07027](https://openairdocs.org/sdr/PIDA07027), Apr 27, 2007: FLOORBEAM. CORRODED. DURING MAINTENANCE, NOTED CORROSION ON THE UPPER CORD OF THE BS 344 FLOORBEAM FROM LBL 50 TO RBL 16. INSTALLED REPLACEMENT SECTION OF -T- CAP PER SRM 53-10-09. - [SDR PIDA07029](https://openairdocs.org/sdr/PIDA07029), Apr 26, 2007: FLOORBEAM. CORRODED. DURING MAINTENANCE, NOTED CORROSION ON UPPER CORD OF BS 294 FLOORBEAM FROM BL 0 TO LBL 12. REPLACED SECTION OF FLOORBEAM -T- CAP FROM LBL 12 TO THE RIGHT SERVIC - [SDR PIDA07026](https://openairdocs.org/sdr/PIDA07026), Apr 25, 2007: FLOOR SUPPORT. CORRODED. DURING INSPECTION, NOTED CORROSION ON LOWER SURFACE OF THE OUTBOARD LONGITUDINAL FLOOR SUPPORT ANGLE IN THE AFT CARGO BIN AT BS 767 +6. REMOVED DAMAGED SECTION - [SDR PIDA07021](https://openairdocs.org/sdr/PIDA07021), Apr 21, 2007: FRAME. DAMAGED. DURING INSPECTION, NOTED FIGURE 8 HOLE IN BS 927 FRAME AT STR 6LT. REPAIRED FRAME PER SRM 51-40-02, 51-40-05 AND 51-30-00 AND REPLACED STRINGER CLIP PER SRM 51- - [SDR PIDA07025](https://openairdocs.org/sdr/PIDA07025), Apr 20, 2007: STRINGER CLIP. CRACKED. DURING MAINTENANCE, FOUND STR 2LT TIE CLIP CRACKED AT BS 947. REPLACED TIE CLIP PER SRM 51-30-0. - [SDR PIDA07020](https://openairdocs.org/sdr/PIDA07020), Apr 20, 2007: FLOORBEAM. CORRODED. DURING MAINTENANCE CHECK, NOTED CORROSION ON UPPER CHORD OF BS 312 FLOORBEAM FROM BL 0 TO LBL 12. REPLACED SECTION OF TEE CAP PER SRM 53-10-9 FIGURE 5. - [SDR PIDA07024](https://openairdocs.org/sdr/PIDA07024), Apr 20, 2007: STRINGER CLIP. CRACKED. DURING MAINTENANCE, FOUND STR 7RT TIE CLIP CRACKED AT BS 747. REPLACED TIE CLIP PER SRM 51-10-1. - [SDR PIDA07023](https://openairdocs.org/sdr/PIDA07023), Apr 20, 2007: STRINGER CLIP. CRACKED. DURING MAINTENANCE, FOUND STR 8LT TIE CLIP CRACKED AT BS 727A. REPLACED TIE CLIP PER SRM 51-10-1. - [SDR PIDA07022](https://openairdocs.org/sdr/PIDA07022), Apr 20, 2007: STRINGER CLIP. CRACKED. DURING MAINTENANCE, FOUND STR 11LT TIE CLIP CRACKED AT BS 663.17. REPLACED TIE CLIP PER SRM 51-30-0. - [SDR TSAA0732014](https://openairdocs.org/sdr/TSAA0732014), Feb 26, 2007: TIRE. FLAT. FLIGHT 210 LIH-HNL - ON LANDING, ATC OBSERVED SMOKE FROM THE LEFT MAIN LANDING GEAR. CREW FOUND NORMAL BRAKING AND NO LOSS OF CONTROL. CREW REQUESTED THE AIRPOR - [SDR TSAA0626078](https://openairdocs.org/sdr/TSAA0626078), Sep 21, 2006: CONTROL PANEL. FAILED. NON-ETOPS FLT 206 HNL-OGG: AS THE AIRCRAFT WAS TAXIING PRIOR TO TAKEOFF, THE (OVHT/DET) LIGHT ILLUMINATED ON THE MASTER CAUTION ANNUNCIATOR PANEL ALONG WITH THE - [SDR TSAA0626074](https://openairdocs.org/sdr/TSAA0626074), Sep 15, 2006: WIRE. CHAFED. NON-ETOPS FLT 242 HNL-ITO: DURING ENGINE START ON PUSH BACK, THE (OVHT/DET) LIGHT ILLUMINATED ON THE MASTER CAUTION ANNUNCIATOR PANEL ALONG WITH THE FIRE WARNIN - [SDR TSAA0626073](https://openairdocs.org/sdr/TSAA0626073), Aug 26, 2006: ELECTRONIC UNIT. MALFUNCTIONED. DURING PUSH BACK, THE OVHT/DET LIGHT ILLUMINATED ON THE MASTER CAUTION ANNUNCIATOR PANEL ALONG WITH THE FORWARD CARGO FAULT LIGHT. THE CREW FOLLOWED QRH PROCEDU - [SDR TSAA0626067](https://openairdocs.org/sdr/TSAA0626067), Aug 18, 2006: SMOKE DETECTOR. MALFUNCTIONED. NON-ETOPS FLT 281 KOA-HNL: AFTER ENGINE START, (OVHT/DET) ANNUNCIATOR LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. CREW WAS UNABLE TO RESET LIGHT AND RETURNED TO - [SDR TSAA0626062](https://openairdocs.org/sdr/TSAA0626062), Aug 6, 2006: CONTROL PANEL. FAILED. NON-ETOPS FLT 34 HNL-ITO: AFTER ENGINE START, (OVHT/DET) ANNUNCIATOR LIGHT ILLUMINATED WITH NO CORRELATED SYSTEM OVERHEAT INDICATION DURING RECALL CHECK. CREW W - [SDR TSAA0626063](https://openairdocs.org/sdr/TSAA0626063), Aug 6, 2006: CONTROL PANEL. FAILED. NON-ETOPS FLT 72 LIH-HNL: AFTER ENGINE START, ( OVHT/DET) ANNUNCIATOR LIGHT ILLUMINATED WITH NO CORRELATED SYSTEM OVERHEAT INDICATION DURING RECALL CHECK. CREW - [SDR TSAA0626064](https://openairdocs.org/sdr/TSAA0626064), Aug 6, 2006: WARNING LIGHT. FALSE INDICATION. NON-ETOPS FLT 34 HNL-ITO: AFTER ENGINE START, OVHT/DET ANNUNCIATOR LIGHT ILLUMINATED WITH NO CORRELATED SYSTEM OVERHEAT INDICATION DURING RECALL CHECK. CREW WAS - [SDR TSAA0621058](https://openairdocs.org/sdr/TSAA0621058), Jul 18, 2006: FAN. ODOR. NON-ETOPS FLT 269 KOA-HNL: SHORTLY AFTER LANDING, THE CREW AND FLIGHT MECHANIC NOTICED A BURNING SMELL COMING FROM THE GASPERS. THE CREW SWITCHED OFF THE GASPER - [SDR PIDA06047](https://openairdocs.org/sdr/PIDA06047), Jun 22, 2006: PANEL. CORRODED. DURING B-CHECK, INSPECTION NOTED FORWARD LAVATORY SERVICE PANEL CORRODED ON INBOARD SIDE. REMOVED MINOR SURFACE CORROSION FROM LAVATORY PAN PER SRM 51-10-6 AND - [SDR PIDA06041](https://openairdocs.org/sdr/PIDA06041), May 13, 2006: CONTROL UNIT. MALFUNCTIONED. TAKEOFF ABORTED DUE TO NR 1 GENERATOR TRIPPED OFF LINE. CHECKED NR 1 CSD OIL LEVEL, DP INDICATOR, FOUND NORMAL. CHECKED APU OIL QUANTITY. DISCONNECTED NR 1 CSD - [SDR PIDA06028](https://openairdocs.org/sdr/PIDA06028), Mar 1, 2006: POWER SUPPLY. INOPERATIVE. FORWARD AND AFT SECTIONS OF SEAT MOUNTED EMERGENCY LIGHTS INOP. REPLACED FWD AND AFT POWER SUPPLIES PER MM 33-50. - [SDR PIDA06029](https://openairdocs.org/sdr/PIDA06029), Feb 28, 2006: CONTROL UNIT. OUT OF ADJUST. AUTO THROTTLE ADVANCES THRUST LEVERS UNCOMMANDED. ADJUSTED RIGHT ENGINE LVDT PER MM 22-31-81. - [SDR PIDA06026](https://openairdocs.org/sdr/PIDA06026), Feb 21, 2006: CONNECTOR. CORRODED. RIGHT WING EGRESS LIGHTS OUT. CLEANED SLIGHT CORROSION FROM BULB CONNECTOR. OPS CHECKS GOOD. - [SDR PIDA06006](https://openairdocs.org/sdr/PIDA06006), Jan 12, 2006: CONTROL UNIT. MALFUNCTIONED. YAW DAMPER WILL NOT ENGAGE. PLACED ON MEL 22-3-B. 01/16/2006: REPLACED YAW DAMPER CONTROL UNIT. SYSTEM TESTS OK PER MM 22-12-01. - [SDR PIDA20050202](https://openairdocs.org/sdr/PIDA20050202), Dec 24, 2005: BATTERY PACK. INOPERATIVE. OVERHEAD EMERGENCY LIGHT INOP AT ROW 2. REPLACED BATTERY PACK. OPS CHECKS GOOD PER MM 25-60-10. - [SDR PIDA20050183](https://openairdocs.org/sdr/PIDA20050183), Nov 2, 2005: CONTROL PANEL. MALFUNCTIONED. MODE CONTROL PANEL INOP. REPLACED MODE CONTROL PANEL PER MM 22-11-01. - [SDR PIDA20050179](https://openairdocs.org/sdr/PIDA20050179), Oct 21, 2005: YAW DAMPER. MALFUNCTIONED. YAW DAMPER TRIPS OFF ON GROUND ONLY WHEN WIDE TURNS ARE MADE WITH TILLER OR RUDDER. PLACED ON MEL 22-3-1B. - [SDR PIDA20050173](https://openairdocs.org/sdr/PIDA20050173), Oct 9, 2005: YAW DAMPER. FAILED. YAW DAMPER WILL NOT ENGAGE. PLACED YAW DAMPER ON MEL 22-3-18. - [SDR PIDA20050172](https://openairdocs.org/sdr/PIDA20050172), Oct 7, 2005: TRANSFORMER. FAILED. AUTO THROTTLES WON'T ENGAGE. LOSS OF VALID AIR DATA SPEED SIGNAL PREVENTED AUTO THROTTLE ENGAGEMENT. REPLACED T98 TRANSFORMER IN J4 BOX PER WDM SPM CHAPTER 20 D - [SDR PIDA20050171](https://openairdocs.org/sdr/PIDA20050171), Oct 6, 2005: BATTERY PACK. INOPERATIVE. RIGHT SIDE EMERGENCY LIGHT FOR OVERWING EXIT NOT ILLUMINATING. REPLACED RIGHT SIDE OVERWING EXIT LIGHT BATTERY PACK. LIGHT OPS CHECKS GOOD. - [SDR PIDA20050164](https://openairdocs.org/sdr/PIDA20050164), Oct 5, 2005: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS AT REAR EXIT DOORS AND AT FORWARD EXIT DOORS ARE NOT ILLUMINATING. REPLACED BATTERY PACK FOR REAR DOOR LIGHTS AND FORWARD DOOR LIGHTS AND - [SDR PIDA200500016](https://openairdocs.org/sdr/PIDA200500016), Apr 21, 2005: COMPASS. MALFUNCTIONED. AFTER TAKEOFF, BOTH COMPASS HEADINGS ROLLED AWAY FROM RUNWAY HEADING. RETURNED TO FIELD. PERFORMED SYSTEM CHECKOUT PER MM 34-21-00. SYSTEM CHECKED NORMAL. PERFO - [SDR 250TR0060](https://openairdocs.org/sdr/250TR0060), Feb 28, 2005: WIRE. DAMAGED. IN PREPARATION TO TAXI, LEFT ENGINE UNCOMMANDED SHUT DOWN AFTER START. FOUND BROKEN WIRES W368-011 AND 010 UNDER CLAMP SIX INCHES BEFORE FUEL SHUTOFF VALVE CONN - [SDR 250TR0059](https://openairdocs.org/sdr/250TR0059), Dec 1, 2004: LAMP. INOPERATIVE. L-1, R-1, R-2 EXTERNAL EMERGENCY EXIT LIGHTS INOP. REPLACED LAMPS. OPS CHECKS GOOD PER MM 33-40-1. - [SDR 250TR0053](https://openairdocs.org/sdr/250TR0053), Oct 22, 2004: ATTACH ANGLE. CRACKED. INTERCOSTAL WEB ATTACH ANGLE CRACKED AFT SIDE OF FRAME AT BS 500 AT STR 28 RT IN FORWARD CARGO BIN. REPLACED ANGLE PER BOEING DWG 69-37261 AND SRM 51-30-2. - [SDR 250TR0058](https://openairdocs.org/sdr/250TR0058), Oct 22, 2004: STRINGER. CORRODED. CORROSION ON STR 26 LT BETWEEN BS 986 AND BS 1006. REPAIRED PER EA 53-292 AND SRM 53-10-1. - [SDR 250TR0048](https://openairdocs.org/sdr/250TR0048), Oct 22, 2004: INTERCOSTAL. CRACKED. FORWARD CARGO INTERCOSTAL WEB CRACKED UNDER THRESHOLD AT STR 26 RT AT BS 460+10. REPAIRED PER SRM 51-40-3 AND SRM 51-30-02. - [SDR 250TR0046](https://openairdocs.org/sdr/250TR0046), Oct 22, 2004: SCUFF PLATE. CRACKED. FORWARD CARGO THRESHOLD FWD AND AFT CORNER SCUFF PLATES CRACKED. REPAIRED PER BOEING SPEC BAC5975. - [SDR 250TR0057](https://openairdocs.org/sdr/250TR0057), Oct 22, 2004: SKIN. CRACKED. CRACK AT FORWARD END OF OXYGEN SERVICE PANEL CUTOUT. REPAIRED PER EA 53-288 AND SRM 53-30-3. All 105: https://openairdocs.org/deregistered/N250TR-2017-10-25/reports.md ## Other aircraft with N250TR - [Cancelled 1992-03-13](https://openairdocs.org/deregistered/N250TR-1992-03-13): Beech 200, S/N BB688. Exported to France. Owner: [Commuter Air Technology Inc](https://openairdocs.org/faa-owner/COMMUTER%20AIR%20TECHNOLOGY%20INC), [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale) --- 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.