# N249TR: 1981 Boeing 737-2K5, registration cancelled 2012-05-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 30, 2012
- Status when cancelled: Sale reported
- 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: 22598
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 6, 2001
- Last registry action: May 30, 2012
- Mode S code: A25327
- Location: [Hamilton, OH](https://openairdocs.org/faa-place/OH/Hamilton)
- Owner type: Individual
- Owner's area on the map: 39.3741° N, 84.5627° W: Placed by OpenAirDocs at the center of ZIP code 45015, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N249TR
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=249TR
- Page: https://openairdocs.org/deregistered/N249TR-2012-05-30

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 Boeing 737-2K5: https://openairdocs.org/model/boeing-737-2k5.md

## Service difficulty reports (143, newest 50)

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

- [SDR KNNA20112492](https://openairdocs.org/sdr/KNNA20112492), Mar 27, 2011: SKIN. DENTED. DURING WALKAROUND NOTICED LT WING NR 2 L/E SLAT BIRD STRIKE. REMOVED LT NR 2 L/E SLAT IAW ACO 052775. CKD OK.
- [SDR KNNA20112491](https://openairdocs.org/sdr/KNNA20112491), Feb 3, 2011: LINE. BROKEN. DISCREPANCY- IN FLIGHT BOTH "A" PUMPS LOW PRESSURE MASTER CAUTION. SYS A QUANTITY 0. FOUND BROKEN FLEX LINE AT SYS A LT WHEEL WELL. R & R LINE IAW AMM 20-10-51.
- [SDR KNNA20100040](https://openairdocs.org/sdr/KNNA20100040), Sep 30, 2010: TIE CLIP. CRACKED. DURING C-CHECK ACCOMPLISHMENT OF AD 1993-08-04 NDT REVEALED A CRACKED TIE CLIP AT FS 559, STRINGER 3R.
- [SDR KNNA2497232010CMH](https://openairdocs.org/sdr/KNNA2497232010CMH), Jul 23, 2010: PUMP. FAILED. FAR 91 MX FERRY KACY-KSLC-KMER FOR C-CHECK, AT FL360 NR 2 RIGHT ENGINE SHUTDOWN, FUEL FLOW 0 N1, N2, & OIL PRESS NORMAL. DIVERTED TO KCMH.
- [SDR PIDA09001](https://openairdocs.org/sdr/PIDA09001), Mar 6, 2009: BATTERY PACK. DEFECTIVE. FWD EMERGENCY EXIT LIGHT BATTERY PACK WILL NOT HOLD A CHARGE. REMOVED AND REPLACED BATTERY PACK, CHARGED PACK, ALL LIGHTS WORK FINE.
- [SDR PIDA08034](https://openairdocs.org/sdr/PIDA08034), Oct 30, 2008: BATTERY PACK. DISCHARGED. EXTERNAL EMERGENCY LIGHTS INOP AT THE L2 AND R2 DOORS. REPLACED BATTERY PACK IN THE RIGHT AFT CARGO COMPARTMENT AND OPS CHECKED LIGHTS PER MM 33-51-51.
- [SDR PID2008F00004](https://openairdocs.org/sdr/PID2008F00004), Jun 6, 2008: BATTERY PACK. INOPERATIVE. MID CABIN CEILING - EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS AT MID CABIN CEILING. OPS CHECK, EMERGENCY EXIT LIGHTS GOOD, IAW MM33-
- [SDR PIDA08017](https://openairdocs.org/sdr/PIDA08017), Mar 30, 2008: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT ABOVE R2 DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ABOVE R2 DOOR IAW 737-200 MM 33-51-101.
- [SDR PIDA08011](https://openairdocs.org/sdr/PIDA08011), Mar 7, 2008: BATTERY PACK. DISCHARGED. AT THE COMPLETION OF MAINTENANCE CHECK, NOTED SEAT MOUNTED EMERGENCY EXIT LIGHTING AND OVERHEAD "BULL NOSE" EMERGENCY LIGHT INOP. REPLACED BATTERY PACKS AND OPS
- [SDR PIDA08012](https://openairdocs.org/sdr/PIDA08012), Feb 7, 2008: STRINGER. CORRODED. DURING MAINTENANCE CHECK, NOTED CORROSION AT STRINGER 22LT BETWEEN ATTACH ANGLE AND STRINGER AT BS 727A. REPAIRED DAMAGED AREA PER SRM AND EA 53-017A.
- [SDR PIDA08010](https://openairdocs.org/sdr/PIDA08010), Feb 7, 2008: STRINGER. CORRODED. DURING MAINTENANCE CHECK, NOTED CORROSION BETWEEN STRINGER 22LT AND FUSELAGE ATTACH ANGLE AT BS 727A. REPLACED DAMAGED SECTION OF STRINGER AND INSTALLED NEW STR
- [SDR PIDA08005](https://openairdocs.org/sdr/PIDA08005), Jan 22, 2008: BULKHEAD. CORRODED. DURING MAINTENANCE CHECK, NOTED CORROSION ON THE AFT SIDE OF THE BS 1016 PRESSURE WEB AT THE FRAME ATTACHMENT BETWEEN STR 26LT AND 27LT. CUT ACCESS HOLE IN FUSE
- [SDR PIDA08004](https://openairdocs.org/sdr/PIDA08004), Jan 17, 2008: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE CHECK, NOTED CORROSION FROM BS 800 TO BS 827 ON THE FLOOR SUPPORT ANGLE AT RBL 17 IN THE AFT CARGO BIN. REPLACED FLOORBEAM FROM BS 787 TO BS 
- [SDR PIDA07036](https://openairdocs.org/sdr/PIDA07036), Jul 16, 2007: BATTERY PACK. DISCHARGED. OVERHEAD AISLE EMERGENCY EXIT LIGHT AT ROW 2 INOP. RELEASED FOR FLIGHT PER MEL 33-15-3 CONTROL NUMBER 0716003. CHARGED EMERGENCY BATTERY PACK. CLEARED MEL.
- [SDR PIDA07007](https://openairdocs.org/sdr/PIDA07007), Feb 2, 2007: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 747 AT STR 7LT. REPLACED TIE CLIP.
- [SDR PIDA07006](https://openairdocs.org/sdr/PIDA07006), Feb 2, 2007: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 727B AT STR 4LT. REPLACED TIE CLIP.
- [SDR PIDA07004](https://openairdocs.org/sdr/PIDA07004), Feb 2, 2007: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 787 AT STR 6LT. REPLACED TIE CLIP.
- [SDR PIDA07005](https://openairdocs.org/sdr/PIDA07005), Feb 2, 2007: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 767 AT STR 6 LT. REPLACED TIE CLIP.
- [SDR PIDA07003](https://openairdocs.org/sdr/PIDA07003), Jan 31, 2007: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 420 AT STR 5LT. REPLACED TIE CLIP.
- [SDR PIDA06119](https://openairdocs.org/sdr/PIDA06119), Oct 27, 2006: BATTERY PACK. INOPERATIVE. AFT BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT BULLNOSE ASILE LIGHT BATTERY PACK IAW AMM 33-51-81 OPPS GHECK GOOD.
- [SDR PIDA06117](https://openairdocs.org/sdr/PIDA06117), Oct 3, 2006: GASPER FAN. ODOR. CABIN AND COCKPIT HAD STRONG ELECTRICAL BURNING SMELL, COCKPIT FILLED UP WITH SMOKE 10 TO 15 PERCENT. DETERMINED THAT GASPER FAN BURNED UP. FOUND GASPER FAN TO 
- [SDR PIDA06116](https://openairdocs.org/sdr/PIDA06116), Sep 27, 2006: MODULE. MALFUNCTIONED. RIGHT MAIN GEAR UNSAFE LIGHT WITH GEAR RETRACTED, RETURNED TO FIELD. REMOVED AND REPLACED LANDING GEAR MODULE PER AMM 32-09-100.
- [SDR PIDA06113](https://openairdocs.org/sdr/PIDA06113), Sep 15, 2006: BATTERY PACK. INOPERATIVE. FWD EXTERIOR L1 & R1 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK FOR L1 & R1 DOORS IAW AMM 33-51-71, OPS CHECK GOOD.
- [SDR PIDA06094](https://openairdocs.org/sdr/PIDA06094), Aug 31, 2006: CONTROL PANEL. MALFUNCTIONED. MCP PANEL BLANKED OUT THREE TIMES IN FLT WOULD NOT ACCEPT VNAV OR LNAV INPUTS. PERFORMED RECONNECT OF MCP C/P & FCC, RERACKED A/T COMPUTER AND ACCY UNIT AND PER
- [SDR PIDA06046](https://openairdocs.org/sdr/PIDA06046), Jun 8, 2006: AUTOPILOT SYS. MALFUNCTIONED. LEFT AUTO PILOT TURNED HEADING FROM 050 TO 080. AUTO PILOT ROLLED INTO A 30 DEGREE RIGHT TURN (AS IT SHOULD) THEN PITCHED DOWN 5 DEGREES FOR NO REASON. DISCONNE
- [SDR PIDA06044](https://openairdocs.org/sdr/PIDA06044), May 30, 2006: COMPUTER. MALFUNCTIONED. WHEN AUTO PILOT -B- SYSTEM IS ENGAGED, PITCH MODE FLUCTUATES. REPLACED FCC -B- COMPUTER. OPS NORMAL PER MM 22-11-331.
- [SDR PIDA06034](https://openairdocs.org/sdr/PIDA06034), Mar 16, 2006: FLAP. LACK OF LUBE. DURING RETURN TO FIELD FOR STAB TRIM PROBLEM, AT 225 KIAS AT 6000 FT MSL WHEN FLAPS EXTENDED TO 5, FELT SHUDDER IN RUDDER PEDALS WHICH CONTINUED TO LANDING. MAD
- [SDR PIDA06033](https://openairdocs.org/sdr/PIDA06033), Mar 16, 2006: RELAY. FAILED. AFTER TAKEOFF, STABILIZER TRIM BECAME INOPERATIVE. STAB TRIM LIGHT ILLUMINATED BUT TRIM WOULD NOT MOVE. RETURNED TO FIELD; INSPECTED AIRCRAFT. FERRIED AIRCRAFT 
- [SDR PIDA2005O187](https://openairdocs.org/sdr/PIDA2005O187), Nov 5, 2005: ACTUATOR. INTERMITTENT. MACH TRIM INTERMITTENT. PLACED ON MEL 22-5. 11/07/2005: REPLACED MACH TRIM ACTUATOR PER MM 22-21-11. OPS CHECKS GOOD.
- [SDR PIDA2005O186](https://openairdocs.org/sdr/PIDA2005O186), Nov 4, 2005: SWITCH. MALFUNCTIONED. AUTO PILOT A & B DISENGAGES AT FLAP 1 POSITION. REPLACED FLAP UP SWITCH 25EN55-6 PER MM 27-51-291. SYSTEM OPS CHECKS GOOD.
- [SDR PIDA20050185](https://openairdocs.org/sdr/PIDA20050185), Oct 31, 2005: COMPUTER. MALFUNCTIONED. AUTO PILOT "A" CHANNEL DISENGAGES. REPLACED "A" SYSTEM FCC. OPERATION NORMAL PER MM 22-11-00.
- [SDR PIDA20050184](https://openairdocs.org/sdr/PIDA20050184), Oct 21, 2005: RECORDER. MALFUNCTIONED. AERO INSTRUMENTS & AVIONICS READOUT OF THE FDR INDICATE THAT THE LEADING EDGE SLAT DISCRETES NEVER CHANGE STATE DURING FLIGHT. ACCOMPLISHED EMTEQ ENGINEERING MO
- [SDR 249TR0105](https://openairdocs.org/sdr/249TR0105), Mar 24, 2005: INDICATOR. MALFUNCTIONED. RIGHT ENGINE N1 GAUGE WENT TO 80 PERCENT AND STOPPED. ABORTED TAKEOFF PRIOR TO 60 KNOTS. MINIMUM BREAKING APPLIED. REPLACED N1 TACH AND OPS CHECKED PER MM 77-12
- [SDR 249TR0103](https://openairdocs.org/sdr/249TR0103), Jan 3, 2005: GASPER FAN. BURNED OUT. GASPER FAN CREATES A SMELL OF SMOKE IN FORWARD SECTION OF CABIN. REPLACED GASPER FAN AND OPS CHECKED GOOD PER MM 21-24-21. NOTE: NO FURTHER WRITE UPS AS OF 01/1
- [SDR 249TR0104](https://openairdocs.org/sdr/249TR0104), Jan 3, 2005: CIRCUIT BREAKER. TRIPPED. AUTO PILOT WILL NOT FOLLOW COMMANDED INPUTS FROM PILOT AND FLIGHT DIRECTOR. RESET STABILIZER TRIM CIRCUIT BREAKER. SYSTEM TESTS GOOD PER MM 22-11-01.
- [SDR 249TR0102](https://openairdocs.org/sdr/249TR0102), Dec 22, 2004: SWITCH. INOPERATIVE. RIGHT TO/GA SWITCH IS INOP. REPLACED SWITCH S787B IN RIGHT THROTTLE PER MM 34-22-0 AND MM 22-31-01.
- [SDR 249TR0088](https://openairdocs.org/sdr/249TR0088), Dec 22, 2004: INTERCOSTAL. CORRODED. INTERCOSTAL AT RBL 8, BETWEEN BS 947.5 AND BS 927 IS CORRODED. REPLACED INTERCOSTAL PER SRM 51-30-0 AND 53-10-2.
- [SDR 249TR0101](https://openairdocs.org/sdr/249TR0101), Dec 22, 2004: COMPUTER. FAULTY. AUTO THROTTLE FAILS STEP A; SHOWS AF6 FAULT CODE. REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-101.
- [SDR 249TR0100](https://openairdocs.org/sdr/249TR0100), Dec 22, 2004: ACTUATOR. LEAKING. EVIDENCE OF FLUID LEAK FROM -A- SYSTEM AUTO PILOT ELEVATOR SERVO ACTUATOR. FOUND -B- SYSTEM AUTO PILOT ACTUATOR LEAKING DOWN ONTO -A- SYSTEM ACTUATOR. REPLACED 
- [SDR 249TR0099](https://openairdocs.org/sdr/249TR0099), Dec 22, 2004: STRINGER. MISREPAIRED. STRINGER REPAIRS NOT PER THE SRM AT STR 15LT. REPAIRED PER SRM 53-10-3.
- [SDR 249TR0098](https://openairdocs.org/sdr/249TR0098), Dec 22, 2004: SUPPORT ANGLE. CRACKED. LEFT INBOARD SUPPORT ANGLE CRACKED UNDER FORWARD WING TO BODY FAIRING. REPAIRED PER EA 53-341.
- [SDR 249TR0097](https://openairdocs.org/sdr/249TR0097), Dec 22, 2004: GALLEY TRACK. CORRODED. RIGHT OUTBOARD GALLEY TRACK CORRODED FOR G-2 GALLEY. REPLACED SECTION OF TRACK PER BOEING DRAWING 65-45834 AND SRM 53-10-2 AND 51-10-2.
- [SDR 249TR0096](https://openairdocs.org/sdr/249TR0096), Dec 22, 2004: INTERCOSTAL. CORRODED. EDGE OF INTERCOSTAL BETWEEN BS 328 AND BS 340 AT LBL 12 DAMAGED. REPLACED INTERCOSTAL PER SRM 51-10-1.
- [SDR 249TR0095](https://openairdocs.org/sdr/249TR0095), Dec 22, 2004: INTERCOSTAL. CORRODED. CORROSION ON TWO INTERCOSTALS AT BS 320 RBL 12 AND RBL 56. REPLACED INTERCOSTALS PER SRM 51-10-1.
- [SDR 249TR0094](https://openairdocs.org/sdr/249TR0094), Dec 22, 2004: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL BETWEEN BS 312 AND BS 328 AT RBL 12. REPLACED INTERCOSTAL PER SRM 51-10-1.
- [SDR 249TR0093](https://openairdocs.org/sdr/249TR0093), Dec 22, 2004: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL AT LAV DOOR FROM BS 294 TO BS 312. REPLACED INTERCOSTAL PER SRM 51-10-1 AND 51-30-2.
- [SDR 249TR0092](https://openairdocs.org/sdr/249TR0092), Dec 22, 2004: ATTACH ANGLE. CORRODED. CORROSION ON ATTACH ANGLE FOR AFT WALL OF FORWARD LAV. REPLACED HAT CHANNEL PER SRM 51-10-1.
- [SDR 249TR0091](https://openairdocs.org/sdr/249TR0091), Dec 22, 2004: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 38 HAS CORROSION AT BS 986 + 4. REPLACED SECTION OF TRACK PER SRM 51-10-1 AND 53-10-2.
- [SDR 249TR0090](https://openairdocs.org/sdr/249TR0090), Dec 22, 2004: INTERCOSTAL. CORRODED. INTERCOSTAL AT BS 947+14 FROM RBL 8 TO RBL 17 CORRODED. REPLACED INTERCOSTAL PER SRM 51-10-1.
- [SDR 249TR0089](https://openairdocs.org/sdr/249TR0089), Dec 22, 2004: INTERCOSTAL. CORRODED. INTERCOSTAL FROM BS 947 TO BS 967 AT RBL 8 CORRODED. REPLACED INTERCOSTAL PER BOEING DRAWING 65C10592 AND SRM 51-40-0.

All 143: https://openairdocs.org/deregistered/N249TR-2012-05-30/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 20090916018559I](https://openairdocs.org/incident/20090916018559I), Sep 16, 2009: Boeing 7372K5 (N249TR), Merced, CA, No damage. The aircraft was en-route from salem, NC to Castle Airport, Merced CA. Upon arrival at Castle Airport, the aircraft landed next to the temporary runway on an…
- [Incident 20061003021699I](https://openairdocs.org/incident/20061003021699I), Oct 3, 2006: Boeing 7372K5 (N249TR), Roanoke, VA. (-23) The aircraft diverted and landed on runway 33 due to smoke in the cockpit. The ARFF responded and observed no fire. The aircraft taxied to the ramp…

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