# Service difficulty reports: N251TR, cancelled Apr 1, 2013

A list on [N251TR, cancelled Apr 1, 2013](https://openairdocs.org/deregistered/N251TR-2013-04-01.md).

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

Page 1 of 2 · 92 reports

- [SDR KNNA251092010KACY](https://openairdocs.org/sdr/KNNA251092010KACY.md): Wire · broken · Sep 20, 2010 · N251TR · Boeing 737228 · Fuel System Wiring
  > AFTER PUSHBACK / DURING ENGING START NR 2 ENGINE STARTED / WHILE STARTING NR 1 ENGINE - NR 2 ENGINE FLAMED OUT. TROUBLESHOT TO A BROKEN WIRE (WDM: 28-21-01 WIRE NR: 388-010-20) ON THE ENGINE FUEL SHUTOFF VALVE AT CANNON PLUG (D790 - PIN: A) REPAIRED REF: (BO
- [SDR PIDA09006](https://openairdocs.org/sdr/PIDA09006.md): Battery Pack · discharged · May 19, 2009 · N251TR · Boeing 737228 · Emergency Lighting
  > L-1 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. TROUBLESHOT TO BATTERY. REMOVED AND REPLACED L-1 DOOR EMERGENCY ESCAPE SLIDE LIGHT BATTERY PACK. OPS CHECKS GOOD PER MM 33-51-02.
- [SDR PIDA08033](https://openairdocs.org/sdr/PIDA08033.md): Battery · discharged · Oct 6, 2008 · N251TR · Boeing 737228 · Emergency Equipment
  > EMERGENCY FLASHLIGHT AT L-1 DOOR INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00. OPS CHECK GOOD. (K)
- [SDR PID2008F00003](https://openairdocs.org/sdr/PID2008F00003.md): Sensor · failed · Jul 10, 2008 · N251TR · Boeing 737228 · Landing Gear Position and Warning
  > GEAR WOULD NOT RETRACT. OVER RIDE TRIGGER USED TO RETRACT GEAR. AC RETURNED TO FIELD. PERFORMED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-291. AC IS SAFE FOR INTENDED FERRY FLIGHT.. 7/11/2008: FOUND AIR SAFETY SENSOR BAD. REPLACED AIR SAFELY SENSOR AND O
- [SDR PID2008F00005](https://openairdocs.org/sdr/PID2008F00005.md): Battery Pack · inoperative · Jul 1, 2008 · N251TR · Boeing 737228 · Emergency Lighting
  > AFT EMERGENCY EXIT LIGHTS NOT WORKING. REMOVED AND REPLACED AFT BATTERY PACK IAW MM 33-51-57. LIGHTS WORKING NORMAL. (K)
- [SDR PIDA08008](https://openairdocs.org/sdr/PIDA08008.md): Battery Pack · inoperative · Feb 4, 2008 · N251TR · Boeing 737228 · Emergency Lighting
  > AFT EMERGENCY EXIT LIGHTS OUT. REPLACED LEFT EMERGENCY EXIT BATTERY PACK. OPS CHECK GOOD PER MM 33-51-31.
- [SDR PIDA08007](https://openairdocs.org/sdr/PIDA08007.md): Battery Pack · discharged · Jan 30, 2008 · N251TR · Boeing 737228 · Emergency Lighting
  > EMERGENCY LIGHTS INOP AT RIGHT OVERWING AND NR 9 OVERHEAD BIN. REPLACED BATTERY PACK AT RIGHT OVERHEAD MID-CABIN. EMERGENCY LIGHTS OPS GOOD PER MM 33-51-31.
- [SDR PIDA07059](https://openairdocs.org/sdr/PIDA07059.md): Skin · damaged · Dec 21, 2007 · N251TR · Boeing 737228 · Rudder, Plate/Skin
  > DURING MAINTENANCE CHECK, DAMAGE NOTED ON THE TRAILING OF THE RUDDER APPROXIMATELY 10 INCHES BELOW THE TOP. REPAIRED DAMAGE PER SRM 51-40-14.
- [SDR PIDA07061](https://openairdocs.org/sdr/PIDA07061.md): Door · damaged · Dec 20, 2007 · N251TR · Boeing 737228 · Engine Thrust Reverser
  > DURING MAINTENANCE CHECK, DAMAGE NOTED ON THE LEFT ENGINE THRUST REVERSER LOWER DOOR FORWARD EDGE AT APPROXIMATELY 5 O'CLOCK POSITION. REPAIRED PER PACE AIRLINES REPAIR PROCEDURE REPORT EA NR 78-348 DATED 12/14/07 WITH FAA DER APPROVED 8110-3 DATED 12/14/2007
- [SDR PIDA07060](https://openairdocs.org/sdr/PIDA07060.md): Skin · damaged · Dec 20, 2007 · N251TR · Boeing 737228 · Rudder, Plate/Skin
  > DURING MAINTENANCE CHECK, DAMAGE NOTED ON THE LOWER FORWARD LEFT CORNER OF THE RUDDER. REPAIRED PER BOEING TELEX MESSAGE NOS 1-724910440-9 AND -10 WITH FAA DOA APPROVED 8100-9 DATED DEC 20, 2007.
- [SDR PIDA07058](https://openairdocs.org/sdr/PIDA07058.md): Skin · cracked · Dec 17, 2007 · N251TR · Boeing 737228 · Rudder, Plate/Skin
  > DURING MAINTENANCE CHECK, NOTED A CRACK IN THE LEADING EDGE OF THE RUDDER AT RUDDER STATION 58.6. REPAIRED PER BOEING TELEX 1-720703898-1 AND -3 WITH FAA DOA APPROVED 8100-9 DATED DEC 15, 2007. SUSPECT DAMAGE OCCURRED DURING RUDDER REMOVAL FROM VERTICAL FIN.
- [SDR PIDA07043](https://openairdocs.org/sdr/PIDA07043.md): Thrust Reverser · damaged · Sep 20, 2007 · N251TR · Boeing 737228 · Engine Thrust Reverser
  > DURING MAINTENANCE VISIT, NOTED DAMAGE TO LEFT ENGINE I/B THRUST REVERSER SKIN AND SUPPORT FRAME. REPAIRED PER PACE AIRLINES REPAIR PROCEDURE REPORT, EA 78-190.
- [SDR PIDA07019](https://openairdocs.org/sdr/PIDA07019.md): Wedge · damaged · Apr 19, 2007 · N251TR · Boeing 737228 · Rudder Structure
  > DURING MAINTENANCE, DISCOVERED A NICK IN THE TRAILING EDGE OF THE RUDDER APPROXIMATELY 86 INCHES FROM THE LOWER END. REPAIRED DAMAGE PER SRM 51-40-15 REPAIR 11 AND BOEING MESSAGES 1-317406998-1, -7, -8, -9, -10, AND -11 WITH FAA DOA APPROVED 8100-9 DATED APR
- [SDR PIDA06085](https://openairdocs.org/sdr/PIDA06085.md): Control Panel · inoperative · Aug 14, 2006 · N251TR · Boeing 737228 · Autopilot System
  > AUTOPILOT SWITCHES WILL NOT MOVE IF OPPOSING SYSTEM IS ENGAGED. REMOVED AND REPLACED MODE CONTROL PANEL IAW AMM 22-11-34 AND PERFORMED SATISFACTORY FUNCTIONAL CHECK.
- [SDR PIDA06084](https://openairdocs.org/sdr/PIDA06084.md): Pitot Tube · obstructed · Aug 11, 2006 · N251TR · Boeing 737228 · Pitot/Static System
  > RTO 90 KTS 86000 LBS, NO CAPTAIN'S AIRSPEED, NO STANDBY AIRSPEED, FIRST OFFICER AIRSPEED NORMAL. REMOVED OBSTRUCTION FROM CAPTAINS PITOT TUBE. OPS CHECK NORMAL IAW MM 34-11-0.
- [SDR PIDA06043](https://openairdocs.org/sdr/PIDA06043.md): Sensor · out of adjust · May 31, 2006 · N251TR · Boeing 737228 · Autopilot System
  > AUTO PILOT BUMPS CONTROL COLUMN UPON SELECTION OF EITHER A OR B CHANNEL. ADJUSTED ELEVATOR POSITION SENSOR PER MM 22-11-0. OPS NORMAL.
- [SDR PIDA06037](https://openairdocs.org/sdr/PIDA06037.md): Coupler · inoperative · Apr 4, 2006 · N251TR · Boeing 737228 · Speed-Attitude Correction System
  > MACH TRIM IS INOP. REPLACED MACH TRIM COUPLER AND OPS CHECKED PER MM 22-21-0.
- [SDR PIDA06035](https://openairdocs.org/sdr/PIDA06035.md): Transmitter · malfunctioned · Mar 22, 2006 · N251TR · Boeing 737228 · Auto Throttle System
  > AUTO THROTTLE SYSTEM IS INOP. DISCONNECTED IN FLIGHT, WOULD NOT RESET. PLACED ON MEL 22-7. REPLACED NR 1 ENGINE LVDT, THRUST LEVER TRANSMITTER, RIGGED AND OPS CHECKED PER MM 22-31-81.
- [SDR PIDA06032](https://openairdocs.org/sdr/PIDA06032.md): Computer · malfunctioned · Mar 17, 2006 · N251TR · Boeing 737228 · Autopilot Computer
  > AIRCRAFT WILL NOT DESCEND IN AUTO-PILOT USING VERTICAL SPEED; REVERTS TO LEVEL CHANGE MODE. FOUND FCC B-SYSTEM AT FAULT. PLACED ON MEL 22-1. 03/20/2006: REPLACED FCC -B- AND PERFORMED SATISFACTORY OPS CHECK PER MM 22-11-331.
- [SDR PIDA06022](https://openairdocs.org/sdr/PIDA06022.md): Computer · faulty · Feb 21, 2006 · N251TR · Boeing 737228 · Autopilot Computer
  > FIRST OFFICER'S FLIGHT DIRECTOR INOP. REPLACED AFCS COMPUTER NR 2. OPS NORMAL PER MM 22-11-331.
- [SDR PIDA20050199](https://openairdocs.org/sdr/PIDA20050199.md): Control Panel · inoperative · Dec 10, 2005 · N251TR · Boeing 737228 · Autopilot System
  > FIRST OFFICER'S COURSE WINDOW MIDDLE DIGIT SKIPS PAST THE NR 1 ON THE MODE CONTROL PANEL. REPLACED MODE CONTROL PANEL AND OPS NORMAL IAW MM 22-11-341.
- [SDR PIDA20050190](https://openairdocs.org/sdr/PIDA20050190.md): Door Frame · cracked · Nov 13, 2005 · N251TR · Boeing 737228 · Fuselage Main, Structure
  > CRACK BEHIND R1 DOOR FRAME UPPER FORWARD STOP FITTING. REPLACED FRAME WEB PER DWG 65-45807.
- [SDR PIDA20050178](https://openairdocs.org/sdr/PIDA20050178.md): Actuator · leaking · Oct 17, 2005 · N251TR · Boeing 737228 · Autopilot System
  > HYDRAULIC FLUID ON LINES AT AUTO PILOT ACTUATOR -B- IN LEFT WHEEL WELL. REPLACED -B- SYSTEM AUTO PILOT ACTUATOR PER MM 22-11-251.
- [SDR PIDA20050176](https://openairdocs.org/sdr/PIDA20050176.md): Floorbeam · corroded · Oct 10, 2005 · N251TR · Boeing 737228 · Fuselage Main, Floor Beam
  > BS 986 FLOORBEAM HAS CORROSION AT FLOORBOARD ATTACH LOCATIONS LBL 48 TO RBL 48. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-301.
- [SDR PIDA20050166](https://openairdocs.org/sdr/PIDA20050166.md): Intercostal · corroded · Oct 5, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > CORROSION AT CLIP NUT HOLES ON INTERCOSTAL AT RBL12 BETWEEN BS 344 AND BS 360. REPLACED INTERCOSTAL PER SRM 51-10-1.
- [SDR PIDA20050165](https://openairdocs.org/sdr/PIDA20050165.md): Pan · corroded · Oct 5, 2005 · N251TR · Boeing 737228 · Fuselage Floor Panel
  > AFT LAVATORY PAN HAS CORROSION ON LOWER SURFACE FROM BS 986+8 TO BS 1016 AT LBL 38. REPLACED PAN PER DWG 65-46812 AND SRM 51-10-1.
- [SDR PIDA20050169](https://openairdocs.org/sdr/PIDA20050169.md): Floorbeam · cracked · Oct 4, 2005 · N251TR · Boeing 737228 · Fuselage Main, Floor Beam
  > CRACK IN RADIUS OF RBL 24 FLOORBEAM AT BS 520. REPAIRED PER SB 737-53-1120.
- [SDR PIDA20050168](https://openairdocs.org/sdr/PIDA20050168.md): Floorbeam · cracked · Oct 4, 2005 · N251TR · Boeing 737228 · Fuselage Main, Floor Beam
  > CRACK IN RADIUS OF RBL 45.50 FLOORBEAM AT BS 520. REPAIRED PER SB 737-53-1120.
- [SDR PIDA20050167](https://openairdocs.org/sdr/PIDA20050167.md): Floorbeam · cracked · Oct 4, 2005 · N251TR · Boeing 737228 · Fuselage Main, Floor Beam
  > CRACK IN RADIUS OF LBL 45.50 FLOORBEAM AT BS 520. REPAIRED PER SB 737-53-1120.
- [SDR PIDA20050160](https://openairdocs.org/sdr/PIDA20050160.md): Intercostal · corroded · Oct 4, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 947 + 9 HAS CORROSION FROM LBL 18 TO LBL 42. REPLACED INTERCOSTAL SRM 51-10-1.
- [SDR PIDA20050157](https://openairdocs.org/sdr/PIDA20050157.md): Intercostal · cracked · Oct 4, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > INTERCOSTAL SHIM AT BS 540 IS CRACKED AT RBL1. REPLACED INTERCOSTAL PER DWG 65-46891 AND SRM 51-10-1.
- [SDR PIDA20050159](https://openairdocs.org/sdr/PIDA20050159.md): Intercostal · corroded · Oct 4, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 947 + 9 HAS CORROSION FROM LBL 8 TO LBL 18. REPLACED INTERCOSTAL PER DWG 65C10592.
- [SDR PIDA20050161](https://openairdocs.org/sdr/PIDA20050161.md): Intercostal · cracked · Oct 4, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BEHIND THE UPPER AFT STOP FITTING ON THE AFT SIDE OF THE R1 DOOR FRAME IS CRACKED UNDER THE RIVET HEADS. REPLACED INTERCOSTAL PER 737 SB 53A1108.
- [SDR PIDA20050158](https://openairdocs.org/sdr/PIDA20050158.md): Intercostal · cracked · Oct 4, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 540 IS CRACKED AT BL0. REPLACED INTERCOSTAL PER DWG 65-46891 AND SRM 51-10-1.
- [SDR PIDA20050162](https://openairdocs.org/sdr/PIDA20050162.md): Intercostal · cracked · Oct 3, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT BS 540 IS CRACKED AT THE AFT I/B EDGE AT RBL47. REPLACED INTERCOSTAL PER DWG 65-46891.
- [SDR PIDA20050177](https://openairdocs.org/sdr/PIDA20050177.md): Floorbeam · corroded · Sep 30, 2005 · N251TR · Boeing 737228 · Fuselage Main, Floor Beam
  > BS 967 FLOORBEAM HAS CORROSION FROM LBL 42 TO LBL 48. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-268.
- [SDR PIDA20050156](https://openairdocs.org/sdr/PIDA20050156.md): Floorbeam · cracked · Sep 30, 2005 · N251TR · Boeing 737228 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 520 IS CRACKED AT LBL24. REPAIRED FLOORBEAM PER 737 SB 53-1120.
- [SDR PIDA20050154](https://openairdocs.org/sdr/PIDA20050154.md): Support Channel · corroded · Sep 30, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > LOWER SUPPORT CHANNEL FOR AFT DRAIN MAST BETWEEN BS 986 AND BS 1006 BETWEEN STR 24 LT AND STR 25 LT HAS CORROSION. REPLACED HAT CHANNEL PER SRM 51-10-1 AND SRM 51-30-2.
- [SDR PIDA20050151](https://openairdocs.org/sdr/PIDA20050151.md): Intercostal · cracked · Sep 30, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > TOP FLANGE OF INTERCOSTAL BETWEEN BS 500B AND BS 520 AT BL 0 IS CRACKED. REPLACED INTERCOSTAL PER DWG 69-41680 AND SRM 51-10-1 AND SRM 51-30-0.
- [SDR PIDA20050148](https://openairdocs.org/sdr/PIDA20050148.md): Stringer · corroded · Sep 30, 2005 · N251TR · Boeing 737228 · Fuselage Main, Longeron/Stringer
  > FOUND STR 27 LT HAS CORROSION FROM BS 967 TO BS 1016. REPLACED DAMAGED SECTION OF STRINGER PER SRM 53-10-03 AND SRM 51-30-00.
- [SDR PIDA20050149](https://openairdocs.org/sdr/PIDA20050149.md): Stringer · corroded · Sep 30, 2005 · N251TR · Boeing 737228 · Fuselage Main, Longeron/Stringer
  > STR 25 LT HAS CORROSION UNDER FRAME AT BS 986. REPLACED DAMAGED SECTION OF STRINGER FROM BS 967 TO BS 1016 PER SRM 53-10-03 AND SRM 51-30-00.
- [SDR PIDA20050152](https://openairdocs.org/sdr/PIDA20050152.md): Strap · corroded · Sep 29, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > STRAP IN AFT LAVATORY AREA HAS CORROSION FROM BS 1006 TO BS 1016+12. REPLACED STRAP PER DWG 65-46812 AND SRM 51-10-1.
- [SDR PIDA20050153](https://openairdocs.org/sdr/PIDA20050153.md): Panel · corroded · Sep 29, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > CLOSE-OUT PANEL AT BS 1016 HAS CORROSION ON UPPER SURFACE AT RBL4. REPAIRED CLOSE-OUT PANEL PER SRM 51-40-1.
- [SDR PIDA20050155](https://openairdocs.org/sdr/PIDA20050155.md): Angle · cracked · Sep 28, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > ANGLE FORWARD OF R1 DOOR JUST BELOW STR 12RT IS CRACKED. REPLACED CRACKED ANGLE PER DWG 65-45807 AND SRM 51-10-1.
- [SDR PIDA20050150](https://openairdocs.org/sdr/PIDA20050150.md): Frame · cracked · Sep 28, 2005 · N251TR · Boeing 737228 · Fuselage Main, Frame
  > CRACK AT I/B CHORD LOWER FASTENER HOLE IN BS 616 FRAME LEFT. REPAIRED FRAME PER SB 737-53-1182.
- [SDR PIDA20050147](https://openairdocs.org/sdr/PIDA20050147.md): Channel · cracked · Sep 28, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > CRACK IN VHF ANTENNA MOUNT BRACKET AND HAT CHANNEL AT BS 506 AND BL 0. REPLACED MOUNT BRACKET AND HAT CHANNEL PER DWG 65-45783 AND SRM 51-10-1.
- [SDR PIDA20050146](https://openairdocs.org/sdr/PIDA20050146.md): Attach Angle · cracked · Sep 27, 2005 · N251TR · Boeing 737228 · Fuselage Main, Attach Fittings
  > CRACK IN THE WEB AND ATTACH ANGLE JUST FORWARD OF THE R1 DOOR AT BS 294 ABOVE STR 12RT. REPLACED WEB AND ANGLE PER DWG 65-45807 AND SRM 51-10-1.
- [SDR PIDA20050145](https://openairdocs.org/sdr/PIDA20050145.md): Stringer · corroded · Sep 26, 2005 · N251TR · Boeing 737228 · Fuselage Main, Longeron/Stringer
  > STR 26 RT HAS CORROSION FROM BS 1006 TO BS 1016. REPLACED STRINGER SECTION PER SRM 51-10-1.
- [SDR PIDA20050144](https://openairdocs.org/sdr/PIDA20050144.md): Frame · cracked · Sep 26, 2005 · N251TR · Boeing 737228 · Fuselage Main, Frame
  > RIGHT FORWARD DOOR FRAME (FUSELAGE FRAME) CRACKED AT FLOOR LEVEL BEHIND THE ZEE ANGLE. REPAIRED DAMAGE PER SRM 51-40-3 AND SRM 51-10-1.
- [SDR PIDA20050143](https://openairdocs.org/sdr/PIDA20050143.md): Angle · cracked · Sep 26, 2005 · N251TR · Boeing 737228 · Fuselage Miscellaneous Structure
  > ATTACH ANGLE FOR THE RIGHT FORWARD ZEE ANGLE JUST FORWARD OF THE R1 DOOR CUTOUT IS CRACKED. REPLACED ANGLE PER SRM 51-10-1.

Next page: https://openairdocs.org/deregistered/N251TR-2013-04-01/reports.md?page=2

## 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 = 'N251TR' AND deregistration_id = 'N251TR-2013-04-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N251TR-2013-04-01/reports

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