# Service difficulty reports: N951AX, cancelled Jul 11, 2013

A list on [N951AX, cancelled Jul 11, 2013](https://openairdocs.org/deregistered/N951AX-2013-07-11.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 · 83 reports

- [SDR ABXA080231](https://openairdocs.org/sdr/ABXA080231.md): Circuit Board · shorted · Aug 8, 2008 · N951AX · Doug DC941 · Ground Proximity System
  > GPWS FAIL LIGHT AND TERR INOP LIGHT ON TAWS CIRCUIT BRAKE TRIPPED. NR 1 ADC AND NR 1 GS C/B TRIPPED. DEFERRED 61397 FOUND TAWS COMPUTER INOP. CAPPED AND STOWED WIRES TW9020 FROM S30-6 (55) TW9056A FROM S30-16 (32) AND TW9014A22 FROM S30-6 (52) IAW REA D934-576
- [SDR ABXA080187](https://openairdocs.org/sdr/ABXA080187.md): Battery · discharged · Jul 6, 2008 · N951AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-0. (A)
- [SDR ABX2008F00000](https://openairdocs.org/sdr/ABX2008F00000.md): Power Supply · defective · Jul 6, 2008 · N951AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW DC9 AMM 33-53-00. (K)
- [SDR ABXA080178](https://openairdocs.org/sdr/ABXA080178.md): Wire · burned · Jun 7, 2008 · N951AX · Doug DC941 · Light System Wiring
  > WHILE TROUBLE SHOOTING THE INOP LT INBO TAIL LIGHT AND THIS LT AFT WING TIP LIGHT FOUND WIRE L 26AH20N BURNT FROM R5-1051D TO GROUND STUD 713 IAW WDM 33-42-02. (A)
- [SDR ABXA080124](https://openairdocs.org/sdr/ABXA080124.md): Bungee Cylinder · leaking · Apr 16, 2008 · N951AX · Doug DC941 · Main Landing Gear Strut/Axle/Truck
  > RIGHT HYDRAULIC QUANTITY LOSS TO ZERO. FOUND LEFT MAIN LANDING GEAR HYDRAULIC BUNGEE CYLINDER LEAKING. REPLACED LEFT BUNGEE CYLINDER IAW DC9 AMM 32-32-03-2.
- [SDR ABXA070167](https://openairdocs.org/sdr/ABXA070167.md): Intercostal · cracked · May 10, 2007 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FRAME BETWEEN STA 427 AND 446 CRACKED AT APPROXIMATELY 435. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM.
- [SDR ABXA070166](https://openairdocs.org/sdr/ABXA070166.md): Floor Support · cracked · May 10, 2007 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > LEFT FLOOR TRACK END FITTING/CLIP CRACKED AND ATTACHING INTERCOSTAL WAS CORRODED UNDER NUT PLATES, STA 1056 - 1072, LONGERON 27 - 28 LEFT. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1.
- [SDR ABXA070165](https://openairdocs.org/sdr/ABXA070165.md): Angle · cracked · May 8, 2007 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > THE TEE ANGLE CRACKED, FORWARD DOOR JAMB, INBOARD MOUNT. REMOVED AND REPLACED TEE ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA070091](https://openairdocs.org/sdr/ABXA070091.md): Power Supply · defective · Apr 9, 2007 · N951AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-53-02-4.
- [SDR ABXA070026](https://openairdocs.org/sdr/ABXA070026.md): Skin · cracked · Jan 29, 2007 · N951AX · Doug DC941 · Fuselage Main, Plate/Skin
  > DURING INSPECTION OF FUSELAGE SKIN AT LONGERON 22, FOUND SKIN CRACKED AT LOWER AFT CORNER OF AIR STAIR DOOR, STA 200. REPAIRED CRACK IAW ABX EA 5300001-003-2.
- [SDR ABXA050112](https://openairdocs.org/sdr/ABXA050112.md): Cusp Web · cracked · May 4, 2005 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CRACKED AT EXISTING REPAIR, STA 1021 - 1041, RIGHT BUTT LINE 50. REMOVED AND REPLACED CUSP AT STA 1021 - 1041 IAW DC-9 SRM 53-03 AND 51-30-4.
- [SDR ABXA050108](https://openairdocs.org/sdr/ABXA050108.md): Attach Angle · cracked · May 3, 2005 · N951AX · Doug DC941 · Nacelle/Pylon, Attach Fittings
  > UPPER PYLON ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED AREA IAW DC-9 SRM 54-04.
- [SDR ABXA050111](https://openairdocs.org/sdr/ABXA050111.md): Stop Fitting · cracked · May 3, 2005 · N951AX · Doug DC941 · Cargo/Baggage Doors
  > FORWARD UPPER STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA050110](https://openairdocs.org/sdr/ABXA050110.md): Stiffener · cracked · May 3, 2005 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > AFT PRESSURE BULKHEAD RIGHT SIDE DOOR JAMB STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA050109](https://openairdocs.org/sdr/ABXA050109.md): Floor Support · corroded · May 2, 2005 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT STA 1072 WAS CORRODED TOP AND BOTTOM SIDE LONGERON 28 LEFT - LONGERON 28 RIGHT. REMOVED AND REPLACED FLOOR SUPPORT SECTIONS IAW DC-9 SRM 51-30-2, 51-30-5, AND SSRM DRAWING K05159.
- [SDR ABXA040270](https://openairdocs.org/sdr/ABXA040270.md): Engine · defective · Jul 25, 2004 · N951AX · Doug DC941 · Engine (Turbine/Turboprop)
  > LEFT ENGINE LOW OIL QUANTITY 0, LOW OIL PRESSURE 35 PSI, OIL PRESSURE LIGHT ON, SHUT DOWN LEFT ENGINE. FROM PDX, MADE DIVERSION TO YAK. REMOVED AND REPLACED LEFT ENGINE IAW DC-9 JOB CARD 9090010 ON WP 600204098. OPS CHECKED GOOD IAW DC-9 MM.
- [SDR ABXA030458](https://openairdocs.org/sdr/ABXA030458.md): Light · shorted · Dec 4, 2003 · N951AX · Doug DC941 · Flight Compartment Lighting
  > ODOR OF WIRES BURNING FOLLOWED BY MAP AND BRIEFCASE CIRCUIT BREAKER TRIPPED, AND LOSS OF THOSE LIGHTS. ODOR WENT AWAY. CAPTAIN'S MAP LIGHT LENS ASSEMBLY SHORTED ON MOUNTING PLATE. REPOSITIONED AND SECURED LENS ASSEMBLY. OPS CHECKED GOOD IAW DC-9 MM.
- [SDR ABXA030372](https://openairdocs.org/sdr/ABXA030372.md): Channel · cracked · Sep 12, 2003 · N951AX · Doug DC941 · Landing Gear Doors
  > LEFT MAIN LANDING GEAR INBOARD DOOR CRACKED AT FORWARD HINGE. REPLACED PAN SECTION AND REPAIRED AREA, REINSTALLED DOOR IAW DC-9 MM 32-12-01-2 AND SRM 52-05, 53-05, AND 51-30-1.
- [SDR ABXA030373](https://openairdocs.org/sdr/ABXA030373.md): Beam · cracked · Sep 9, 2003 · N951AX · Doug DC941 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR BEAM NR 2 END FITTING CRACKED ON AFT SIDE. REPLACED AFT LOWER CARGO DOOR BEAM NR 2 END FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA030374](https://openairdocs.org/sdr/ABXA030374.md): Shear Tie · cracked · Sep 9, 2003 · N951AX · Doug DC941 · Fuselage Main, Structure
  > SHEAR TIE CRACKED, FS 1021 AT LONGERON 14 RIGHT. REPLACED SECTION OF SHEAR TIE IAW DC-9 SRM.
- [SDR ABXA030319](https://openairdocs.org/sdr/ABXA030319.md): Pivot Assy · lack of lube · Aug 1, 2003 · N951AX · Doug DC941 · Landing Gear Retraction/Extension System
  > RIGHT MAIN LANDING GEAR CAME OUT ON UPLATCH CHECK. RECYCLED LANDING GEAR AND RECEIVED NORMAL INDICATION. FOUND UPLOCK PIVOT BOLT BOUND UP TO HOOK AND STRUCTURE IMPEDING MOVEMENT OF HOOK. PULLED, CLEANED AND LUBRICATED PIVOT BOLT AND BOSS. INSTALLED REMOTE
- [SDR ABXA030287](https://openairdocs.org/sdr/ABXA030287.md): Uplock Switch · failed · Jul 18, 2003 · N951AX · Doug DC941 · Landing Gear Position and Warning
  > RT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. ALL INDICATIONS WERE NORMAL. REPLACED RIGHT GEAR UPLOCK SWITCH IAW MM 32-60-01-2. ALSO FOUND CANNON PLUG P1-1150 VERY CORRODED, REPLACED PLUG. OPS CHECKE
- [SDR ABXA030284](https://openairdocs.org/sdr/ABXA030284.md): Pin · bent · Jul 15, 2003 · N951AX · Doug DC941 · Landing Gear Position and Warning
  > AFTER TAKEOFF, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER INITIAL RETRACTION. THERE WAS NO ASSOCIATED YAW OR NOISE. AFTER RECYCLING GEAR, ALL INDICATIONS WERE NROMAL. FOUND PIN A BENT ON R5-1150. STRAIGHTENED PIN. OPS CHECKED GOOD IAW DC-9 AMM 32-60-0
- [SDR ABXA030076](https://openairdocs.org/sdr/ABXA030076.md): Drain · frozen · Feb 18, 2003 · N951AX · Doug DC941 · Drag Control System
  > DEPLOYING SPOILERS CREATED A LT ROLL OF 5 DEGREES PER SECOND. AILERONS BINDED DURING APPROACH, AILERONS HEAVY DURING APPROACH. FOUND SLAT PANEL DRAINS BLOCKED BY ICE, WATER LEAKED OUT OF SLANT PANEL AND DOWN ONTO AILERON AND SPOILER CABLES, FREEZING THEM UP. T
- [SDR ABXA010674](https://openairdocs.org/sdr/ABXA010674.md): Panel · corroded · Jan 4, 2002 · N951AX · Doug DC941 · Fuselage Main, Structure
  > RIGHT SLANT PANEL HAD CORROSION AROUND NUT PLATES, LOWER EDGE FROM INBOARD TO OUTBOARD. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-2, 51-10-4, 51-30-1 AND 51-20-6.
- [SDR ABXA010673](https://openairdocs.org/sdr/ABXA010673.md): Panel · corroded · Jan 3, 2002 · N951AX · Doug DC941 · Fuselage Structure (General)
  > LEFT SLANT PANEL CORRODED AROUND NUTPLATES. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-1.
- [SDR ABXA010672](https://openairdocs.org/sdr/ABXA010672.md): Attach Angle · corroded · Jan 3, 2002 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > LEFT WHEEL WELL OUTBOARD SLANT PANEL ATTACH ANGLE EXFOLIATED AT LOWER FASTENER. LOCATED AND DRILLED SLANT PANEL ATTACH ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA010671](https://openairdocs.org/sdr/ABXA010671.md): Angle · cracked · Jan 3, 2002 · N951AX · Doug DC941 · Fuselage Main, Structure
  > LEFT WHEEL WELL ATTACH ANGLE CRACKED IN RADIUS, JUST OUTBOARD OF THE TRAP PANEL, ABOVE THE HYDRAULIC SERVICE ACCESS. REPLACED ANGLE IAW DC-9 SRM.
- [SDR ABXA010584](https://openairdocs.org/sdr/ABXA010584.md): Relay · malfunctioned · Nov 13, 2001 · N951AX · Doug DC941 · Stabilizer Control System
  > DURING DESCENT, ALTERNATE LONGITUDINAL TRIM RAN AWAY. AUTOPILOT AND ALTERNATE TRIM CIRCUIT BREAKERS PULLED. COULD NOT DUPLICATE ON GROUND. REPLACED ALTERNATE TRIM BRAKE RELAY R20-14 AND UP AND DOWN RELAYS R20-12 AND R20-13 AS A PRECAUTION. OPS CHECKED GOOD
- [SDR ABXA010235](https://openairdocs.org/sdr/ABXA010235.md): Lock · disconnected · May 15, 2001 · N951AX · Doug DC941 · Flight Compartment Windows
  > THE PILOTS CLEARVIEW WINDOW AFT LOCK WAS DISCONNECTED. MAINTENANCE INSPECTED AND RECONNECTED THE AFT LOCK AS REQUIRED.
- [SDR ABXA010063](https://openairdocs.org/sdr/ABXA010063.md): Battery Pack · dirty · Feb 24, 2001 · N951AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND CLEANED EMERGENCY LIGHT BATTERY PACK AT FSD AND RETURNED THE A/C TO SERVICE. UPON ARRIVAL AT ILN, MAINTENANCE REPLACED EMERGENCY LIGHT PACK AS A RELIABILITY PRECAUTION IAW DC9 MM 33-02-4.
- [SDR ABXA0100016](https://openairdocs.org/sdr/ABXA0100016.md): Battery · discharged · Jan 21, 2001 · N951AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-02-4-0001.
- [SDR ABXA000482](https://openairdocs.org/sdr/ABXA000482.md): Wheel · jammed · Oct 30, 2000 · N951AX · Doug DC941 · Cabin Pressure Control System
  > TOP OF DESCENT UPON SETTING LANDING ELEVATION, CABIN CLIMB INDICATOR SHOWED 1500 FPM CLIMB, WENT ON OXYGEN, WENT TO MANUAL. COULD NOT CONTROL. PRESSURIZATION WHEEL JAMMED. OPS CHECKED AUTO AND MANUAL PRESSURIZATION. AIRCRAFT PRESSURIZED TO 7.5 PSI. NO LEA
- [SDR ABXA000275](https://openairdocs.org/sdr/ABXA000275.md): Skin · corroded · May 11, 2000 · N951AX · Doug DC941 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED UNDER LEFT STATIC PORT PLATE. REPAIRED SKIN IAW DC9 SRM 53-04.
- [SDR ABXA000274](https://openairdocs.org/sdr/ABXA000274.md): Skin · corroded · May 11, 2000 · N951AX · Doug DC941 · Fuselage Main, Plate/Skin
  > CENTER KEEL FUSELAGE SKIN EXTERIOR BETWEEN MAIN LANDING GEAR INBOARD WHEEL WELL DOORS CORRODED. REPLACED SKIN IAW DC9 SRM 51-30-2.
- [SDR ABXA000253](https://openairdocs.org/sdr/ABXA000253.md): Angle · cracked · May 10, 2000 · N951AX · Doug DC941 · Passenger/Crew Doors
  > ATTACH ANGLE CRACKED INSIDE AFT PRESSURE DOME DOOR AT UPPER DOOR HINGE. REPLACED ANGLE (P/N 9915565-157) IAW DC9 SRM 51-30-2.
- [SDR ABXA000257](https://openairdocs.org/sdr/ABXA000257.md): Panel · delaminated · May 10, 2000 · N951AX · Doug DC941 · Wing, Plate/Skin
  > TRAILING EDGE PANEL FORWARD OF OUTBOARD END OF LEFT AILERON DELAMINATED. REPLACED TRAILING EDGE PANEL IAW DC9 SRM 51-30-1.
- [SDR ABXA000256](https://openairdocs.org/sdr/ABXA000256.md): Angle · cracked · May 10, 2000 · N951AX · Doug DC941 · Vertical Stabilizer
  > RIGHT DORSAL FIN ATTACH ANGLE CRACKED FORWARD OF AFT END OF ANGLE, 12 INCHES LONG. REPAIRED ANGLE IAW DC9 SRM 53-05, FIGURE 23.
- [SDR ABXA000255](https://openairdocs.org/sdr/ABXA000255.md): Pan · cracked · May 10, 2000 · N951AX · Doug DC941 · Electrical/Electronic Compartment Doors
  > ELECTRONIC COMPARTMENT DOOR PAN IS CRACKED AT ALL FOUR CORNERS. REPLACED ELECTRONIC COMPARTMENT DOOR.
- [SDR ABXA000254](https://openairdocs.org/sdr/ABXA000254.md): Attach Fitting · cracked · May 10, 2000 · N951AX · Doug DC941 · Fuselage Main, Attach Fittings
  > AFT ENTRY DOOR LEFT LOWER STOP FITTING CRACKED AT FORWARD ATTACH POINT, 19 INCHES ABOVE FLOOR LEVEL. REPLACED FITTING IAW DC9 SRM 51-30-2.
- [SDR ABXA000260](https://openairdocs.org/sdr/ABXA000260.md): Hinge · cracked · May 9, 2000 · N951AX · Doug DC941 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR DOOR HINGE CRACKED AT LOBE. REPLACED HINGE IAW DC9 SRM 51-30-1.
- [SDR ABXA000259](https://openairdocs.org/sdr/ABXA000259.md): Skin · cracked · May 9, 2000 · N951AX · Doug DC941 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR EXTERIOR SKIN CRACKED AT CENTER BEAM FORWARD ATTACH FITTING. REPAIRED IAW ABX REA D952-36797.
- [SDR ABXA000258](https://openairdocs.org/sdr/ABXA000258.md): Attach Fitting · cracked · May 5, 2000 · N951AX · Doug DC941 · Fuselage Main, Attach Fittings
  > SEAT TRACK ATTACH FITTING CRACKED AT STA 370. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA000236](https://openairdocs.org/sdr/ABXA000236.md): Angle · cracked · May 5, 2000 · N951AX · Doug DC941 · Service Doors
  > FORWARD SERVICE DOOR ATTACH ANGLE CRACKED INSIDE LIGHTENING HOLE, FORWARD UPPER CORNER OF DOOR AT UPPER BEAM TO DOOR PAN. REPLACED ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA000235](https://openairdocs.org/sdr/ABXA000235.md): Attach Fitting · cracked · May 5, 2000 · N951AX · Doug DC941 · Fuselage Main, Attach Fittings
  > RIGHT FLOORBEAM TO KEEL ATTACH FITTING AT STATION 737 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA000234](https://openairdocs.org/sdr/ABXA000234.md): Intercostal · cracked · May 5, 2000 · N951AX · Doug DC941 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO COMPARTMENT DOOR INTERCOSTAL WEB CRACKED AT UPPER AFT DOOR STOP. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.
- [SDR ABXA000233](https://openairdocs.org/sdr/ABXA000233.md): Web · cracked · May 5, 2000 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > RIGHT CUSP WEB CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-01.
- [SDR ABXA000232](https://openairdocs.org/sdr/ABXA000232.md): Skin · cracked · May 5, 2000 · N951AX · Doug DC941 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STATION 1152 AND LONGERON 14 LEFT. REPAIRED SKIN IAW DC9SRM 53-04.
- [SDR ABXA000231](https://openairdocs.org/sdr/ABXA000231.md): Web · cracked · May 5, 2000 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FORWARD SUB FLOOR CRACKED AT STATION 203 AND RBL 22. REPAIRED SUB FLOOR IAW DC9 SRM53-0.
- [SDR ABXA000230](https://openairdocs.org/sdr/ABXA000230.md): Fitting · cracked · May 1, 2000 · N951AX · Doug DC941 · Fuselage Miscellaneous Structure
  > AFT ENTRY DOOR FRAME LEFT SIDE STOP FITTING CRACKED AT FORWARD END, 36 INCHES ABOVE FLOOR LEVEL. REPLACED FITTING IAW DC9 SRM 51-30-2.

Next page: https://openairdocs.org/deregistered/N951AX-2013-07-11/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 = 'N951AX' AND deregistration_id = 'N951AX-2013-07-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N951AX-2013-07-11/reports

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