# Service difficulty reports: N954AX, cancelled Apr 22, 2013

A list on [N954AX, cancelled Apr 22, 2013](https://openairdocs.org/deregistered/N954AX-2013-04-22.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 ABXA080240](https://openairdocs.org/sdr/ABXA080240.md): Current Limiter · failed · Sep 12, 2008 · N954AX · Doug DC941 · AC Power Distribution System
  > CREW REPORTED SMOKE COMING FROM CIRCUIT BREAKER PANEL BEHIND CAPTAINS SEAT WHEN GROUND POWER WAS CONNECTED TO ACFT. FOUND GROUND SERVICE BUS CONTROL AND A & C PHASE GROUND SERVICE BUSS BREAKERS TRIPPED. REPLACED BLOWN CURRENT LIMITERS FOR CROSS TIE RELAY T2.
- [SDR ABXA080118](https://openairdocs.org/sdr/ABXA080118.md): Light · out of position · Apr 4, 2008 · N954AX · Doug DC941 · Flight Compartment Lighting
  > MAP & BRIEFCASE CIRCUIT BREAKER TRIPPED, SMOKE EXITING FROM FIRST OFFICER'S MAP LIGHT ON FIRST OFFICER'S CONTROL COLUMN. REPOSITIONED LIGHT ASSEMBLY. SYSTEM CHECKS GOOD IAW DC9 AMM 33-13-00.
- [SDR ABXA080026](https://openairdocs.org/sdr/ABXA080026.md): Window Frame · cracked · Jan 7, 2008 · N954AX · Doug DC941 · Fuselage Main, Structure
  > CENTER AND SIDE WINDSHIELD RIGHT ZEE P/N: 5912360-68 CRACKED. REPLACED RIGHT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014.
- [SDR ABXA080025](https://openairdocs.org/sdr/ABXA080025.md): Structure · cracked · Jan 7, 2008 · N954AX · Doug DC941 · Fuselage Main, Structure
  > CENTER AND SIDE WINDSHIELD LEFT ZEE P/N: 5912360-67 CRACKED. REPLACED LEFT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014.
- [SDR ABXA080024](https://openairdocs.org/sdr/ABXA080024.md): Angle · cracked · Jan 7, 2008 · N954AX · Doug DC941 · Fuselage Main, Structure
  > COCKPIT WINDOW SILL LEFT ANGLE CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA080023](https://openairdocs.org/sdr/ABXA080023.md): Angle · cracked · Jan 7, 2008 · N954AX · Doug DC941 · Fuselage Main, Structure
  > COCKPIT WINDOW SILL RIGHT ANGLE CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA08026](https://openairdocs.org/sdr/ABXA08026.md): Angle · cracked · Jan 7, 2008 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CENTER AND SIDE WINDSHIELD RIGHT ZEE P/N: 5912360-68 CRACKED. REPLACED RIGHT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014.
- [SDR ABXA08025](https://openairdocs.org/sdr/ABXA08025.md): Angle · cracked · Jan 7, 2008 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CENTER AND SIDE WINDSHIELD LEFT ZEE P/N: 5912360-67 CRACKED. REPLACED LEFT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014.
- [SDR ABXA08024](https://openairdocs.org/sdr/ABXA08024.md): Angle · cracked · Jan 7, 2008 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > COCKPIT WINDOW SILL LEFT ANGLE P/N: 9957860-7 CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA08023](https://openairdocs.org/sdr/ABXA08023.md): Angle · cracked · Jan 7, 2008 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > COCKPIT WINDOW SILL RIGHT ANGLE P/N: 9957860-8 CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA070417](https://openairdocs.org/sdr/ABXA070417.md): Skin · corroded · Nov 22, 2007 · N954AX · Doug DC941 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN FS 813 AT LONGERON 29 RIGHT TO LONGERON 28 LEFT. REPAIRED BLENDED AREA IN ACCORDANCE WITH DC9 SRM 53-04, FIGURE 38.
- [SDR ABXA070416](https://openairdocs.org/sdr/ABXA070416.md): Floorbeam · cracked · Nov 22, 2007 · N954AX · Doug DC941 · Fuselage Main, Floor Beam
  > FLOORBEAM CRACKED ON BOTH SIDES OF INTERCOSTAL AT STATION 180, LEFT BUTT LINE 20-23. REPAIRED FLOORBEAM IN ACCORDANCE WITH DC9 SRM.
- [SDR ABXA070422](https://openairdocs.org/sdr/ABXA070422.md): Attach Fitting · cracked · Nov 14, 2007 · N954AX · Doug DC941 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR BEAM NR 3 AFT FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH DC9 SRM 51-30-5.
- [SDR ABXA070420](https://openairdocs.org/sdr/ABXA070420.md): Bulkhead · cracked · Nov 14, 2007 · N954AX · Doug DC941 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD TEE NR 2 WAS CRACKED APPROXIMATELY.75 INCHES LONG AT LONGERON 14 RIGHT. REMOVED AND REPLACED TEE CAP IN ACCORDANCE WITH DC9 SRM.
- [SDR ABXA070421](https://openairdocs.org/sdr/ABXA070421.md): Skin · gouged · Nov 14, 2007 · N954AX · Doug DC941 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR SKIN WAS GOUGED FORWARD LOWER CORNER. REPLACED SKIN IN ACCORDANCE WITH DC9 SRM 51-10-4.
- [SDR ABXA070419](https://openairdocs.org/sdr/ABXA070419.md): Attach Fitting · cracked · Nov 14, 2007 · N954AX · Doug DC941 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR BEAM NR 2 AFT FITTING WAS CRACKED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH DC9 SRM 51-30-5.
- [SDR ABXA070418](https://openairdocs.org/sdr/ABXA070418.md): Cusp Web · cracked · Nov 13, 2007 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > LEFT CUSP WEB CRACKED TWO (2) PLACES BETWEEN FS 636-655. REPAIRED CRACKS IN ACCORDANCE WITH DC9 SRM 53-01, FIGURE 2.
- [SDR ABXA070415](https://openairdocs.org/sdr/ABXA070415.md): Skin · cracked · Nov 9, 2007 · N954AX · Doug DC941 · Fuselage Main, Plate/Skin
  > MAIN ENTRY DOOR CUTOUT UPPER AFT CORNER WAS DAMAGED AND CRACKED. REPAIRED UPPER AFT CORNER IN ACCORDANCE WITH DC9 SRM 53-05, FIGURE 114 AND 117.
- [SDR ABXA070044](https://openairdocs.org/sdr/ABXA070044.md): Battery · discharged · Feb 2, 2007 · N954AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00.
- [SDR ABXA060200](https://openairdocs.org/sdr/ABXA060200.md): Door · unlatched · Jul 11, 2006 · N954AX · Doug DC941 · Landing Gear Door Retract Section
  > ON GEAR RETRACTION, SHUDDER WAS FELT AT THE NOSE GEAR AREA. SUSPECT DOORS NOT RETRACTED PROPERLY. CYCLED GEAR TO VERIFY, NO CHANGE, ALL LIGHTS FOR GEAR SYSTEM NORMAL. FOUND THE RIGHT NOSE GEAR DOOR UNLATCHED. SECURED RIGHT NOSE GEAR DOOR.
- [SDR ABXA060040](https://openairdocs.org/sdr/ABXA060040.md): Battery · discharged · Jan 17, 2006 · N954AX · Doug DC941 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED CABIN EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8-0002.
- [SDR ABXA050381](https://openairdocs.org/sdr/ABXA050381.md): Cable · broken · Dec 21, 2005 · N954AX · Doug DC941 · Landing Gear Door Retract Section
  > AFTER TAKEOFF AT GEAR RETRACTION, LOUD NOISE AND SEVERE VIBRATION FROM THE NOSE GEAR AREA WAS FELT. RECYCLED THE LANDING GEAR AND A LOUD BANG WAS HEARD. RETURNED TO THE AIRPORT AND MADE A NORMAL LANDING WITH ALL THE CORRECT INDICATIONS. FOUND THE NOSE GEAR DO
- [SDR ABXA050334](https://openairdocs.org/sdr/ABXA050334.md): Clip · cracked · Dec 3, 2005 · N954AX · Doug DC941 · Nacelle/Pylon, Main Frame
  > RIGHT FORWARD PYLON HAD A CRACKED ATTACH BRACKET INBOARD AND AFT SIDE RIGHT BUTT LINE 30 APPROXIMATELY AT FLOOR SURFACE. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA050333](https://openairdocs.org/sdr/ABXA050333.md): Fitting · cracked · Nov 30, 2005 · N954AX · Doug DC941 · Wing, Center Box
  > FOUND CRACKED END FITTING AFT SIDE OF PRESSURE BULKHEAD AT LONGERON 29 RIGHT. REPLACED END FITTING IAW DC9 SRM.
- [SDR ABXA050332](https://openairdocs.org/sdr/ABXA050332.md): Skin · cracked · Nov 30, 2005 · N954AX · Doug DC941 · Wing, Plate/Skin
  > FOUND SKIN, FORWARD OF PANEL 1601, HAD A CRACK COMPLETELY ACROSS THE SKIN. MANUFACTURED NEW SKIN AND INSTALLED IAW DC9 51-30-5 AND 51-30-1.
- [SDR ABXA050331](https://openairdocs.org/sdr/ABXA050331.md): Skin · corroded · Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Plate/Skin
  > BROKEN FASTENER HEADS AND BULGE IN FUSELAGE SKIN FS 617, LONGERON 30 - LONGERON 29 RIGHT. REPAIRED AREA IAW DC9 SRM 53-04.
- [SDR ABXA050330](https://openairdocs.org/sdr/ABXA050330.md): Fitting · corroded · Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Attach Fittings
  > BROKEN FASTENER HEAD AND BULGE IN FUSELAGE SKIN FS 1072. REMOVED AND REPLACED FITTING AT HING 23H, FS 1072 IAW DC9 SRM.
- [SDR ABXA050329](https://openairdocs.org/sdr/ABXA050329.md): Fitting · cracked · Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Attach Fittings
  > RIGHT KEEL FS 675 LONGERON 29 RIGHT CRACKED FITTING. REMOVED AND REPLACED FITTING IAW DC9 SRM.
- [SDR ABXA050328](https://openairdocs.org/sdr/ABXA050328.md): Fitting · corroded · Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CORROSION RIGHT KEEL AFT OF PRESSURE BULKHEAD LONGERON 26 RIGHT END CAP. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA050327](https://openairdocs.org/sdr/ABXA050327.md): Bulkhead · corroded · Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Bulkhead
  > FORWARD LOWER CARGO STA 644 BULKHEAD SKIN WAS BULGED FROM LONGERON 30 TO LONGERON 29 LEFT, NUMEROUS RIVETS SHEARED. REMOVED AND REPLACED FINGER DOUBLER IAW DC9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA050326](https://openairdocs.org/sdr/ABXA050326.md): Longeron · corroded · Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION LONGERON 30 END CAP AFT OF PRESSURE BULKHEAD TO FS 648 APPROXIMATELY LEFT KEEL AREA. REMOVED AND REPLACED END CAPS IAW DC9 SRM.
- [SDR ABXA050325](https://openairdocs.org/sdr/ABXA050325.md): Bulkhead · corroded · Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Bulkhead
  > FOUND CORROSION LONGERON 29 LEFT AND ADJACENT LONGERON PRESSURE BULKHEAD TO FS 675 LEFT KEEL AREA. REPAIRED AREA IAW DC9 SRM 53-01.
- [SDR ABXA050324](https://openairdocs.org/sdr/ABXA050324.md): Hinge Bracket · cracked · Nov 28, 2005 · N954AX · Doug DC941 · Fuselage, Door Hinge
  > CRACK AT FORWARD BOTTOM EDGE OF FORWARD ENTRY DOOR BELOW BOTTOM HINGE BRACKET. REPAIRED CRACK PAN WITH REPAIR IAW DC9 SRM 52-05.
- [SDR ABXA050323](https://openairdocs.org/sdr/ABXA050323.md): Door Frame · cracked · Nov 23, 2005 · N954AX · Doug DC941 · Fuselage Main, Structure
  > AFT ENTRY DOOR JAMB CRACKED UNDER SEAL DEPRESSOR JUST BELOW UPPER RIGHT CORNER. REPAIRED AFT ENTRY DOOR JAMB UNDER SEAL DEPRESSOR BELOW UPPER RIGHT CORNER IAW DC9 SRM 53-01.
- [SDR ABXA050322](https://openairdocs.org/sdr/ABXA050322.md): Structure · cracked · Nov 22, 2005 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AND CRACK IN SUBFLOOR, UNDER FIRST OFFICER'S INBOARD SEAT TRACK. CUT OUT CRACK AND CORROSION IN SUBFLOOR, INSTALLED DOUBLER IAW DC9 SRM 53.
- [SDR ABXA030361](https://openairdocs.org/sdr/ABXA030361.md): Odor · detected · Sep 6, 2003 · N954AX · Doug DC941 · Air Distribution System
  > A FAINT BURNING ODOR DETECTED ON DESCENT. INSPECTED ELECTRONIC COMPARTMENT, ENGINE CONTROL UNITS FOR LOOSE CONNECTOR AND ACCESSORIES FOR SECURITY. NO DEFECTS NOTED.
- [SDR ABXA030047](https://openairdocs.org/sdr/ABXA030047.md): Proximity Sensor · dirty · Jan 27, 2003 · N954AX · Doug DC941 · Landing Gear Position and Warning
  > RT GEAR UNSAFE LIGHT CAME ON DURING UPLATCH CHECK AFTER TAKE-OFF. FOLLOWED ABNORMAL PROCEDURE AND RECYCLED GEAR. UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE UP AND RT HYDRAULIC SYSTEM IN 'HIGH', RT GEAR LIGHT REMAINED ILLUMINATED. ON DESCENT AT FL 250, RT GEAR
- [SDR ABXA020220](https://openairdocs.org/sdr/ABXA020220.md): Controller · malfunctioned · Oct 1, 2002 · N954AX · Doug DC941 · Cabin Pressure Controller
  > ON CLIMBOUT, AIRCRAFT DID NOT PRESSURIZE. PERFORMED ABNORMAL, AUTO CONTROLLER WAS INOPERATIVE. UNABLE TO CONTROL PRESSURE. INSPECTED ALL ACCESS DOORS, ALL CLOSED. INSPECTED AND LUBRICATED OUTFLOW BUTTERFLY VALVE LINKAGE AND OUTFLOW NOZZLE, NO DEFECTS FOUND
- [SDR ABXA020148](https://openairdocs.org/sdr/ABXA020148.md): Sensor · defective · Aug 29, 2002 · N954AX · Doug DC941 · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. RIGHT HYDRAULIC PUMPS ON HIGH. AT GEAR UPLATCH CHECK, THE LIGHT WENT OUT. GEAR RECYCLED ONE TIME BEFORE UPLATCH CHECK WITH THE LIGHT STILL ON. REPLACED THE LEFT GEAR DOWN SENSOR IAW DC-9 MM 32
- [SDR ABXA020211](https://openairdocs.org/sdr/ABXA020211.md): Web · cracked · Aug 16, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CUSP WEB WAS CRACKED AT STA 1041, LONGERON 18 LEFT. REPLACED CUSP WEB STRINGER IAW DC-9 SRM 53-01.
- [SDR ABXA020177](https://openairdocs.org/sdr/ABXA020177.md): Web · cracked · Aug 16, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CUSP WEB WAS CRACKED AT STATION 1041, LONGERON 18 LEFT. REPLACED CUSP WEB IAW DC-9 SRM 53-01.
- [SDR ABXA020210](https://openairdocs.org/sdr/ABXA020210.md): Intercostal · cracked · Aug 14, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > INTERCOSTAL JUST BELOW RIGHT RADOME HINGE WAS CRACKED AT CUTOUT. REPLACED INTERCOSTAL AND INSTALLED FASTENERS IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA020209](https://openairdocs.org/sdr/ABXA020209.md): Angle · corroded · Aug 14, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > EXFOLIATED ANGLE ON OUTBOARD END OF SLANT PANEL. REPLACED ANGLE IAW DC-9 SRM.
- [SDR ABXA020208](https://openairdocs.org/sdr/ABXA020208.md): Hinge · cracked · Aug 14, 2002 · N954AX · Doug DC941 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR INBOARD DOOR HINGE WAS CRACKED. REMOVED AND REINSTALLED THE RIGHT MAIN LANDING GEAR DOOR FOR HINGE CHANGE IAW DC-9 MM 32-12-01-2-02-01, SRM 51-30-1, 51-30-5 AND 52-05.
- [SDR ABXA020176](https://openairdocs.org/sdr/ABXA020176.md): Intercostal · cracked · Aug 14, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > INTERCOSTAL JUST BELOW RIGHT RADOME HINGE WAS CRACKED AT CUTOUT. REPLACED INTERCOSTAL AND INSTALLED FASTENERS IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA020175](https://openairdocs.org/sdr/ABXA020175.md): Angle · corroded · Aug 14, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > EXFOLIATED ANGLE ON OUTBOARD END OF SLANT PANEL. REPLACED ANGLE IAW DC-9 SRM.
- [SDR ABXA020174](https://openairdocs.org/sdr/ABXA020174.md): Hinge · cracked · Aug 14, 2002 · N954AX · Doug DC941 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR INBOARD DOOR HINGE WAS CRACKED. REMOVED AND REINSTALLED RIGHT MAIN LANDING GEAR DOOR FOR HINGE CHANGE IAW DC-9 MM 32-12-01-2-02-01 AND SRM 51-30-1, 51-30-5, AND 52-05.
- [SDR ABXA010757](https://openairdocs.org/sdr/ABXA010757.md): Battery · discharged · Mar 4, 2002 · N954AX · Doug DC941 · Emergency Lighting
  > COCKPIT OVERHEAD EMERGENCY LIGHTS WOULD NOT TEST. REPLACED NICAD BATTERIES IN EMERGENCY LIGHTING BATTERY PACK IAW DC-9 MM 33-53-00-8. OPS CHECKED GOOD.
- [SDR ABXA010061](https://openairdocs.org/sdr/ABXA010061.md): Door Frame · cracked · Feb 20, 2001 · N954AX · Doug DC941 · Fuselage Main, Structure
  > UPPER LEFT CORNER VENTRAL DOOR JAMB WAS CRACKED AND WAS PROPAGATING FROM STOP DRILL. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW ABX REA D953-39998-MR.
- [SDR ABXA010060](https://openairdocs.org/sdr/ABXA010060.md): Fitting · cracked · Feb 20, 2001 · N954AX · Doug DC941 · Fuselage Miscellaneous Structure
  > LOWER FRAME ATTACH FITTING AT FUSELAGE STATION 677R WAS CRACKED APPROX 3 INCHES. VERIFIED WITH DYE PEN AND EDDY CURRENT INSPECTION.

Next page: https://openairdocs.org/deregistered/N954AX-2013-04-22/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 = 'N954AX' AND deregistration_id = 'N954AX-2013-04-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N954AX-2013-04-22/reports

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