# Service difficulty reports: N953AX, cancelled May 26, 2017

A list on [N953AX, cancelled May 26, 2017](https://openairdocs.org/deregistered/N953AX-2017-05-26.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 · 97 reports

- [SDR ABXA200812190271](https://openairdocs.org/sdr/ABXA200812190271.md): Battery Pack · discharged · Dec 15, 2008 · N953AX · Doug DC941 · Emergency Lighting
  > DURING PRE-DEPARTURE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.
- [SDR ABXA080060](https://openairdocs.org/sdr/ABXA080060.md): Window Frame · cracked · Feb 6, 2008 · N953AX · Doug DC941 · Fuselage Main, Structure
  > DURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND CENTER FRAME WITH MULTIPLE CRACKS. REPLACED CENTER FRAME SEGMENT IAW DC9 SRM 51-30-2 PER WO 600283624.
- [SDR ABXA080058](https://openairdocs.org/sdr/ABXA080058.md): Window Frame · cracked · Feb 6, 2008 · N953AX · Doug DC941 · Fuselage Main, Structure
  > DURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND RIGHT SIDE FRAME CRACKED LESS THAN 2.50 INCHES. REPAIRED IAW DC9 SRM 53-03, FIG 34 PER WO 600283624.
- [SDR ABXA080057](https://openairdocs.org/sdr/ABXA080057.md): Intercostal · cracked · Feb 6, 2008 · N953AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND FORWARD INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-10-4 PER WO 600283624.
- [SDR ABXA080059](https://openairdocs.org/sdr/ABXA080059.md): Window Frame · cracked · Feb 6, 2008 · N953AX · Doug DC941 · Fuselage Main, Structure
  > DURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND LEFT SIDE FRAME CRACKED LESS THAN 2.50 INCHES. REPAIRED IAW DC9 SRM 53-05, FIG 34 PER WO 600283624.
- [SDR ABXA070362](https://openairdocs.org/sdr/ABXA070362.md): Intercostal · corroded · Oct 25, 2007 · N953AX · Doug DC941 · Fuselage Miscellaneous Structure
  > INTERCOSTAL BETWEEN STA 1056 - 1072 AT LONGERON 27 - 28 LEFT CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA070363](https://openairdocs.org/sdr/ABXA070363.md): Seat Track · cracked · Oct 24, 2007 · N953AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT BUTT LINE 44.5 SEAT TRACK UPPER FLANGE CRACKED AT STA 240. REPLACED SEAT TRACK SECTION IAW DC9 SRM 51-30-01.
- [SDR ABXA070378](https://openairdocs.org/sdr/ABXA070378.md): Frame · cracked · Oct 23, 2007 · N953AX · Doug DC941 · Fuselage Main, Frame
  > LEFT AFT MAIN FRAME STA 775, HAD A CRACK IN THE FORWARD FLANGE AT POINT J. REPAIRED MAIN FRAME IAW DC9 SRM.
- [SDR ABXA070361](https://openairdocs.org/sdr/ABXA070361.md): Strap · cracked · Oct 23, 2007 · N953AX · Doug DC941 · Fuselage Main, Floor Beam
  > FS 775, LEFT BUTT LINE 12, FLOORBEAM ATTACH STRAP CRACKED. REMOVED AND REPLACED ATTACH STRAP FS 775, LEFT BUTT LINE 12 IAW DC9 SRM.
- [SDR ABXA070360](https://openairdocs.org/sdr/ABXA070360.md): Floor Support · corroded · Oct 23, 2007 · N953AX · Doug DC941 · Fuselage Miscellaneous Structure
  > EXFOLIATED FLOOR SUPPORT FROM FS 993 TO 1072 LEFT. REMOVED AND REPLACED TRACK SUPPORT FLOOR IAW DC9 SRM 53-05, FIG 4G, SHEET 1.
- [SDR ABXA070359](https://openairdocs.org/sdr/ABXA070359.md): Intercostal · cracked · Oct 22, 2007 · N953AX · Doug DC941 · Fuselage Miscellaneous Structure
  > SUPPORT INTERCOSTAL BETWEEN FRAMES 427 - 446 AT LONGERON 29 LEFT WAS CRACKED. REPAIRED INTERCOSTAL IAW DC9 SRM.
- [SDR ABXA070176](https://openairdocs.org/sdr/ABXA070176.md): Power Supply · defective · May 30, 2007 · N953AX · Doug DC941 · Emergency Lighting
  > DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC9 AMM 33-50-00.
- [SDR ABXA050288](https://openairdocs.org/sdr/ABXA050288.md): Longeron · cracked · Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 28 RIGHT, STA 642 AND 660, CRACKED AND EXFOLIATED. REMOVED AND REPLACED LONGERON AND FRAME IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA050287](https://openairdocs.org/sdr/ABXA050287.md): Fitting · cracked · Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Miscellaneous Structure
  > LONGERON END FITTING CRACKED AT FS 642, LONGERON 29 RIGHT. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA050284](https://openairdocs.org/sdr/ABXA050284.md): Frame · cracked · Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Main, Frame
  > RIGHT AFT OVER WHEEL WELL FRAME FS 775 FORWARD FLANGE CRACKED AT P & G. REPAIRED FRAME IAW JOB CARD EA 53400320-001-2.
- [SDR ABXA050283](https://openairdocs.org/sdr/ABXA050283.md): Support Fitting · cracked · Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FRAME SUPPORT FITTING HAD CRACK INDICATIONS ON INBOARD SIDE FS 675 AT LONGERON 29 LEFT. REMOVED AND REPLACED SUPPORT FITTING FS 675, LONGERON 29 LEFT IAW DC-9 SRM 51-30-5.
- [SDR ABXA050282](https://openairdocs.org/sdr/ABXA050282.md): Fitting · cracked · Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Miscellaneous Structure
  > LONGERON END CRACKED FS 642 AT LONGERON 26 LEFT. REMOVED AND REPLACED LONGERON END FITTING FS 642, LONGERON 26 LEFT IAW DC-9 SRM 51-30-5.
- [SDR ABXA050281](https://openairdocs.org/sdr/ABXA050281.md): Clip · cracked · Nov 14, 2005 · N953AX · Doug DC941 · Wing, Attach Fittings
  > FRAME SUPPORT FITTING HAD CRACK INDICATIONS ON INBOARD SIDE. REMOVED AND REPLACED SUPPORT FITTING FS 675, LONGERON 29 LEFT IAW DC9 SRM 51-30-5.
- [SDR ABXA040209](https://openairdocs.org/sdr/ABXA040209.md): Landing Gear · malfunctioned · Jun 15, 2004 · N953AX · Doug DC941 · Landing Gear Retraction/Extension System
  > OVERSHOT UPLATCH CHECK DETENT. RIGHT & LEFT RED GEAR UNSAFE & YELLOW GEAR DOOR OPEN LIGHT ILLUMINATED. PER ABNORMAL, RECYCLED GEAR & NORMAL OPERATION FOLLOWED. NOTED BY MAINTENANCE, PERFORMED VISUAL INSPECTION OF GEAR UPLOCKS. NO DEFECTS NOTED.
- [SDR ABXA040108](https://openairdocs.org/sdr/ABXA040108.md): Fitting · cracked · Mar 5, 2004 · N953AX · Doug DC941 · Fuselage, Landing Gear Attach Fittings
  > FITTING CRACKED ON UPPER END OF KEEL VERTICAL SUPPORT, INBOARD OF BRAKE CONTROL VALVES. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA020187](https://openairdocs.org/sdr/ABXA020187.md): Clip · cracked · Aug 7, 2002 · N953AX · Doug DC941 · Nacelle/Pylon Structure
  > LOWER BOLT HOLE WAS CRACKED AT #2 ENGINE AFT MOUNT. REPLACED ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA020186](https://openairdocs.org/sdr/ABXA020186.md): Pan · cracked · Aug 6, 2002 · N953AX · Doug DC941 · Doors
  > CRACK IN FORWARD ENTRY DOOR ABOVE FORWARD LOWER STOP PAD. REPLACED DOOR IAW DC-9 MM.
- [SDR ABXA020185](https://openairdocs.org/sdr/ABXA020185.md): Splice · cracked · Aug 4, 2002 · N953AX · Doug DC941 · Fuselage Main, Bulkhead
  > PYLON BULKHEAD ATTACH FITTING AT STA. 1041, LEFT BUTT LINE 30, WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA020184](https://openairdocs.org/sdr/ABXA020184.md): Skin · cracked · Aug 2, 2002 · N953AX · Doug DC941 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED ON RIGHT SIDE OF VENTRAL DOORWAY APPROXIMATELY 36" UP FROM FLOOR. REPAIRED AREA IAW DC-9 SRM 53-05.
- [SDR ABXA020183](https://openairdocs.org/sdr/ABXA020183.md): Fitting · corroded · Aug 1, 2002 · N953AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FRAME FOOT AT STA 617 LEFT HAD HEAVY EXFOLIATION CORROSION. REPLACED FRAME FOOT AT STA 617 LEFT AND FASTENERS IAW DC-9 SRM 51-30-1 AND 51-30-2.
- [SDR ABXA020182](https://openairdocs.org/sdr/ABXA020182.md): Splice · cracked · Aug 1, 2002 · N953AX · Doug DC941 · Fuselage Main, Bulkhead
  > LEFT SIDE F.S. 1041 BULKHEAD FITTING WAS CRACKED. REPLACED FITTINGS IAW DC-9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA020181](https://openairdocs.org/sdr/ABXA020181.md): Web · cracked · Aug 1, 2002 · N953AX · Doug DC941 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CRACKED BEWTEEN F.S. 1021 AND 1041. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.
- [SDR ABXA020180](https://openairdocs.org/sdr/ABXA020180.md): Skin Panel · delaminated · Jul 31, 2002 · N953AX · Doug DC941 · Wing, Plate/Skin
  > DELAMINATION AREA ON OUTBOARD TRAILING EDGE BONDED PANEL LOCATED ON WING UPPER SURFACE AND FORWARD OF AILERON. REPLACED OUTBOARD TRAILING EDGE BONDED PANEL IAW DC-9 SRM 51-30-2 AND 51-30-1.
- [SDR ABXA020179](https://openairdocs.org/sdr/ABXA020179.md): Clip · cracked · Jul 31, 2002 · N953AX · Doug DC941 · Cargo/Baggage Doors
  > BEAM #5 TEE FITTING AT FORWARD END WAS CRACKED. REPLACED THE #5 TEE IAW DC-9 SRM 51-30-5 AND 51-30-4.
- [SDR ABXA020033](https://openairdocs.org/sdr/ABXA020033.md): Battery · discharged · Jul 8, 2002 · N953AX · Doug DC941 · Emergency Lighting
  > MAINTENANCE FOUND EMERGENCY EXIT LIGHTS DIM. REPLACED BOTH BATTERIES FOR EMERGENCY EXIT LIGHT AND CHECKED BATTERY PACK FOR CHARGING. OPS CHECKED GOOD IAW DC-9 MM.
- [SDR ABXA010302](https://openairdocs.org/sdr/ABXA010302.md): Separator · contaminated · Jun 6, 2001 · N953AX · Doug DC941 · Humidity Control System
  > ON TAKEOFF ROLL, AT ILN AND FLL, CREW IDENTIFIED AN UNKNOWN ODOR IN THE COCKPIT. ODOR SEEMED TO BE PNEUMATIC IN NATURE, NOT ELECTRICAL. IT STARTED HALFWAY THROUGH EACH TAKEOFF ROLL AND DISSIPATED WITHIN 15 MINUTES IN THE CLIMB. ODOR WAS OBVIOUS AND CLEARLY
- [SDR ABXA010208](https://openairdocs.org/sdr/ABXA010208.md): Power Supply · discharged · Apr 26, 2001 · N953AX · Doug DC941 · Emergency Lighting
  > THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING THE CREW PREFLIGHT INSPECTION. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY, IAW DC-9 MM 33-53-02.
- [SDR ABXA010137](https://openairdocs.org/sdr/ABXA010137.md): Computer · faulty · Apr 12, 2001 · N953AX · Doug DC941 · Stall Warning System
  > DURING ROTATION AT SJU THE CREW NOTED A STALL WARNING WITH STICK SHAKER ACTIVATION. THE CREW FOLLOWED ABNORMAL PROCEDURES, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AT SJU. MAINTENANCE INSPECTED AND REPLACED THE LT STALL WARNING COMPUTER.
- [SDR ABXA010049](https://openairdocs.org/sdr/ABXA010049.md): Electrical Box · odor · Feb 7, 2001 · N953AX · Doug DC941 · Flight Compartment Lighting
  > A HOT ELECTRICAL ODOR WAS NOTED COMING FROM THE FORWARD CENTER CONSOLE AREA. WHEN THE FORWARD CONSOLE CIRCUIT BREAKER WAS PULLED, THE ODOR SUBSIDED. MAINTENANCE INSPECTED THE PEDESTAL LIGHTS SWITCH BOX AND CONSOLE AREA WIRING. NO DEFECTS WERE NOTED. MAINTE
- [SDR ABXA010033](https://openairdocs.org/sdr/ABXA010033.md): Longeron · cracked · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 30 AT FUSELAGE STATION 617 - 642 WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.
- [SDR ABXA010032](https://openairdocs.org/sdr/ABXA010032.md): Longeron · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON AT STRINGER 29L WAS EXFOLIATED ON THE HORIZONTAL FLANGE AT APPROX FUSELAGE STATION 675. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30.
- [SDR ABXA010031](https://openairdocs.org/sdr/ABXA010031.md): Vane · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Trailing Edge Flaps
  > FIXED VANE ON LEFT WING WAS CORRODED INTERNALLY. MAINTENANCE INSPECTED AND REPLACED THE LEFT FIXED VANE IAW DC-9 MM.
- [SDR ABXA010030](https://openairdocs.org/sdr/ABXA010030.md): Longeron · cracked · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > FUSELAGE LONGERON 28L WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON AT 28L IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA010029](https://openairdocs.org/sdr/ABXA010029.md): Latch · cracked · Feb 2, 2001 · N953AX · Doug DC941 · Cargo/Baggage Doors
  > REPAIR NEAR THE AFT BAG BIN AFT LATCH WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE BAG BIN DOOR IAW DC-9 SRM AND ABX NEA52300001-005.
- [SDR ABXA010028](https://openairdocs.org/sdr/ABXA010028.md): Doubler · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Plate/Skin
  > INTERNAL FUSELAGE DOUBLER AT STA 642 L30 WAS CORRODED FORWARD OF THE KIDNEY PANEL. MAINTENANCE INSPECTED AND REPLACED THE DOUBLER IAW DC-9 SRM 51-30-1 AND DRAWING 9923434.
- [SDR ABXA010037](https://openairdocs.org/sdr/ABXA010037.md): Longeron · cracked · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 26R WAS CRACKED FROM FUSELAGE STATION 617 TO 642. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-2.
- [SDR ABXA010036](https://openairdocs.org/sdr/ABXA010036.md): Shear Tie · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Structure
  > FUSELAGE SHEAR TIE AT FRAME 675 WAS CORRODED ON LEFT SIDE AT KEEL AREA. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-9 SRM.
- [SDR ABXA010035](https://openairdocs.org/sdr/ABXA010035.md): Frame · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Frame
  > FUSELAGE FRAME AT STATION 560 LONGERON 29R WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW DC-9 SRM 53-03 PAGE 4E FIG 2A.
- [SDR ABXA010034](https://openairdocs.org/sdr/ABXA010034.md): Longeron · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON LONGERON 29L, FUSELAGE STATION 617 - 642. MAINTENANCE REPLACED THE LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.
- [SDR ABXA0100037](https://openairdocs.org/sdr/ABXA0100037.md): Longeron · cracked · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 26R WAS CRACKED FROM FUSELAGE STATION 617 TO 642. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-2.
- [SDR ABXA0100036](https://openairdocs.org/sdr/ABXA0100036.md): Shear Tie · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Structure
  > FUSELAGE SHEAR TIE AT FRAME 675 WAS CORRODED ON LEFT SIDE AT KEEL AREA. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-9 SRM.
- [SDR ABXA0100035](https://openairdocs.org/sdr/ABXA0100035.md): Frame · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Frame
  > FUSELAGE FRAME AT STATION 560 LONGERON 29R WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW DC-9 SRM 53-03 PAGE 4E FIG 2A.
- [SDR ABXA0100033](https://openairdocs.org/sdr/ABXA0100033.md): Longeron · cracked · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 30 AT FUSELAGE STATION 617 - 642 WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.
- [SDR ABXA0100032](https://openairdocs.org/sdr/ABXA0100032.md): Longeron · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON AT STRINGER 29L WAS EXFOLIATED ON THE HORIZONTAL FLANGE AT APPROX FUSELAGE STATION 675. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30.
- [SDR ABXA0100031](https://openairdocs.org/sdr/ABXA0100031.md): Vane · corroded · Feb 2, 2001 · N953AX · Doug DC941 · Trailing Edge Flaps
  > FIXED VANE ON LEFT WING WAS CORRODED INTERNALLY. MAINTENANCE INSPECTED AND REPLACED THE LEFT FIXED VANE IAW DC-9 MM.

Next page: https://openairdocs.org/deregistered/N953AX-2017-05-26/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 = 'N953AX' AND deregistration_id = 'N953AX-2017-05-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N953AX-2017-05-26/reports

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