# Service difficulty reports: N955AX, cancelled Nov 10, 2011

A list on [N955AX, cancelled Nov 10, 2011](https://openairdocs.org/deregistered/N955AX-2011-11-10.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 · 72 reports

- [SDR ABXA070426](https://openairdocs.org/sdr/ABXA070426.md): Battery · discharged · Dec 11, 2007 · N955AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTING WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8.
- [SDR ABXA070364](https://openairdocs.org/sdr/ABXA070364.md): Unknown · smoke · Nov 5, 2007 · N955AX · Doug DC941 · Air Distribution System
  > AIRCRAFT HAD FUMES/SMOKE IN COCKPIT. GROUND RAN APU A/C PACKS, NR 1 & 2 ENGINES, POWERED UP COCKPIT ELECTRICAL SYSTEMS, NO FUMES OR SMOKE NOTICED. INSPECTED TAIL COMPARTMENT, BAG BINS, E & E COMPARTMENT AND NOSE COMPARTMENT. NO EVIDENCE OF OVERHEATING NOTED
- [SDR ABXA070332](https://openairdocs.org/sdr/ABXA070332.md): Skin · corroded · Sep 28, 2007 · N955AX · Doug DC941 · Fuselage Main, Plate/Skin
  > LEFT STATIC PORT SKIN WAS CORRODED ON INSIDE OF FORWARD LOWER CARGO BETWEEN FS 332 AND 351, LONGERON 27 AND 26 LEFT. INSTALLED REPAIR IAW DC9 SRM 53-04, FIGURE 12C.
- [SDR ABXA070331](https://openairdocs.org/sdr/ABXA070331.md): Skin · corroded · Sep 28, 2007 · N955AX · Doug DC941 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER UPPER SURFACE WAS CORRODED APPROXIMATELY 30 INCHES OUTBOARD OF THE VERTICAL CAP. REPAIRED AREA IAW DC9 SRM 55-01 FIGURE 2, SHEET 2.
- [SDR ABXA070330](https://openairdocs.org/sdr/ABXA070330.md): Attach Fitting · cracked · Sep 21, 2007 · N955AX · Doug DC941 · Emergency Exits
  > RIGHT FORWARD EMERGENCY EXIT DOOR LOWER BEAM AFT END ATTACH CLIP WAS CRACKED. REMOVED AND REPLACED CLIP IAW DC9 SRM.
- [SDR ABXA070329](https://openairdocs.org/sdr/ABXA070329.md): Longeron · cracked · Sep 20, 2007 · N955AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 4 LEFT CRACKED AT STA 160 AT OUTBOARD FASTENER. REPLACED SECTION OF LONGERON 4 IAW DC9 SRM 53-02 FIGURE 18.
- [SDR ABXA070327](https://openairdocs.org/sdr/ABXA070327.md): Beam · cracked · Sep 19, 2007 · N955AX · Doug DC941 · Service Doors
  > SERVICE DOOR UPPER BEAM AFT END WAS CRACKED. REPAIRED AREA IAW DC9 SRM 52-05, FIGURE 25.
- [SDR ABXA070326](https://openairdocs.org/sdr/ABXA070326.md): Seat Track · cracked · Sep 19, 2007 · N955AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO SEAT TRACK CRACKED STA 160 - 200 LEFT BUTT LINE 44. REMOVED AND REPLACED SEAT TRACK FS 160 - 228 LEFT BUTT LINE 44.
- [SDR ABXA070328](https://openairdocs.org/sdr/ABXA070328.md): Intercostal · cracked · Sep 19, 2007 · N955AX · Doug DC941 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT LONGERON 29 LEFT, CRACKED AND BENT FROM STA 351 TO STA 370. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.
- [SDR ABXA070035](https://openairdocs.org/sdr/ABXA070035.md): Engine · damaged · Feb 3, 2007 · N955AX · Doug DC941 · Engine (Turbine/Turboprop)
  > FLIGHT 509, ILN - JAX, AT CRUISE POWER SETTING, LEFT EPR HAD SUDDEN DROP OF.4 EPR. LOUD POPPING SOUND. MODERATE VIBRATION, THROTTLED BACK, VIBRATION WORSENED. SHUT LEFT ENGINE DOWN. AIRCRAFT LANDED WITHOUT INCIDENT AT JAX. FOUND TURBINE DAMAGED. REMOVED
- [SDR ABXA050248](https://openairdocs.org/sdr/ABXA050248.md): Frame · cracked · Sep 29, 2005 · N955AX · Doug DC941 · Fuselage Main, Frame
  > FRAME 1152 CRACKED LONGERON 2 RIGHT. REPLACED CRACKED FRAME SECTION FS 1152 IAW DC-9 SRM 53-03.
- [SDR ABXA050247](https://openairdocs.org/sdr/ABXA050247.md): Strut · corroded · Sep 29, 2005 · N955AX · Doug DC941 · Main Landing Gear Strut/Axle/Truck
  > NOSE LANDING GEAR STRUT BARREL HAD PITTING IN FIRST BEVEL OF BARREL HOUSING. REMOVED AND REPLACED STRUT BARREL IAW DC-9 SRM.
- [SDR ABXA050246](https://openairdocs.org/sdr/ABXA050246.md): Skin · cracked · Sep 27, 2005 · N955AX · Doug DC941 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACKED AT STA 1135 LONGERON 4 LEFT. REPAIRED AREA IAW DC-9 SRM.
- [SDR ABXA040390](https://openairdocs.org/sdr/ABXA040390.md): Downlock Switch · malfunctioned · Dec 6, 2004 · N955AX · Doug DC941 · Landing Gear Position and Warning
  > EN ROUTE, NOSE GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR, LIGHT REMAINED ON. REPLACED NOSE GEAR DOWNLOCK SWITCH IAW DC9 MM 32-60-01.
- [SDR ABXA040320](https://openairdocs.org/sdr/ABXA040320.md): Computer · malfunctioned · Aug 31, 2004 · N955AX · Doug DC941 · Autopilot System
  > AIRCRAFT INITITATED DUTCH ROLL DURING CLIMBOUT AND PROGRESSIVELY GOT WORSE WITH THE HIGHER CLIMB. ROLL TOOK PLACE WITH OR WITHOUT AUTO PILOT ON AND OFF, WITH YAW DAMPER SWITCH ON OR OFF. ACCOMPLISHED RUDDER CONTROL TAB INSP/TEST IAW DC9 MM 27-20-02-04. NO D
- [SDR ABXA040296](https://openairdocs.org/sdr/ABXA040296.md): Control Box · malfunctioned · Aug 17, 2004 · N955AX · Doug DC941 · Landing Gear Position and Warning
  > AFTER SELECTING GEAR DOWN, NOTED A RT GEAR UNSAFE LIGHT. THE LIGHT CHANGED FROM GREEN TO RED 3 TIMES. MISSED APPROACH AND CYCLED GEAR, UNLOCK REMAINED GREEN. (NOTE: INBOUND PROBLEM ON FLIGHT 194 8/16 OPS) PERFORMED SEVERAL GEAR SWINGS IAW AMM 32-60-00-2 WITH N
- [SDR ABXA040046](https://openairdocs.org/sdr/ABXA040046.md): Hinge · cracked · Jan 13, 2004 · N955AX · Doug DC941 · Doors
  > FITTING ABOVE UPPER HINGE ON AFT PRESSURE BULKHEAD DOOR WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA040045](https://openairdocs.org/sdr/ABXA040045.md): Bulkhead · cracked · Jan 13, 2004 · N955AX · Doug DC941 · Fuselage Main, Bulkhead
  > FITTING BELOW UPPER HINGE INSIDE AFT PRESSURE BULKHEAD DOOR WAS CRACKED. REPLACED DOOR FITTING IAW DC-9 SRM.
- [SDR ABXA040044](https://openairdocs.org/sdr/ABXA040044.md): Skin · corroded · Jan 13, 2004 · N955AX · Doug DC941 · Trailing Edge Flaps
  > LEFT FLAP INBOARD UPPER SKIN SURFACE CORRODED BEYOND LIMITS. REPLACED SKIN ON LEFT FLAP INBOARD UPPER SKIN SURFACE IAW DC-9 SRM.
- [SDR ABXA030477](https://openairdocs.org/sdr/ABXA030477.md): Power Supply · discharged · Dec 16, 2003 · N955AX · Doug DC941 · Emergency Lighting
  > FOUND COCKPIT EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PACK POWER SUPPLY IAW DC9 MM 33-53-02-4-0001. OPS CHECK GOOD.
- [SDR ABXA010899](https://openairdocs.org/sdr/ABXA010899.md): Shear Tie · cracked · May 20, 2002 · N955AX · Doug DC941 · Fuselage Main, Structure
  > SHEAR TIE CRACKED AT FS 1171, VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE. REPLACED SHEAR TIE IAW DC-9 SRM.
- [SDR ABXA010898](https://openairdocs.org/sdr/ABXA010898.md): Pan · corroded · May 17, 2002 · N955AX · Doug DC941 · Fuselage Miscellaneous Structure
  > BULGING STRUCTURE AND SEVERAL POPPED FASTENERS ALONG BOTTOM OF FORWARD LOWER CARGO COMPARTMENT DOOR CUTOUT. INSTALLED NEW PAN AND REPAIRED AREA IAW DC-9 SRM 53-05.
- [SDR ABXA000470](https://openairdocs.org/sdr/ABXA000470.md): Fitting · cracked · Oct 11, 2000 · N955AX · Doug DC941 · Leading Edge Devices
  > RIGHT WING LEADING EDGE FITTING CRACKED INBOARD OF NR 2 SLAT TRACK AT LOWER POCKET. REPAIRED FITTING IAW ABX REA D957-38812-MR.
- [SDR ABXA000469](https://openairdocs.org/sdr/ABXA000469.md): Frame · cracked · Sep 29, 2000 · N955AX · Doug DC941 · Trailing Edge Flaps
  > RIGHT FLAP FRAME CRACKED AT PANEL NR 1634A AND STATION 267. REPLACED FRAME IAW DC9 SRM.
- [SDR ABXA000381](https://openairdocs.org/sdr/ABXA000381.md): Proximity Switch · out of adj · Aug 10, 2000 · N955AX · Doug DC941 · Landing Gear Position and Warning
  > DURING CLIMB AT 280 KNOTS, THE GEAR DOOR OPEN LIGHT ILLUMINATED. RECYCLED THE LANDING GEAR AND THE LIGHT EXTINGUISHED. ADJUSTED THE RIGHT MAIN LANDING GEAR DOOR PROXIMITYSWITCH.
- [SDR ABXA000365](https://openairdocs.org/sdr/ABXA000365.md): Warning Light · false indication · Aug 7, 2000 · N955AX · Doug DC941 · Landing Gear Position and Warning
  > RIGHT GEAR UNSAFE LIGHT WAS ON AFTER GEAR RETRACTION, WITH GEAR HANDLE IN THE UP POSITION. RECYCLED GEAR. LIGHT REMAINED ON BUT EXTINGUISHED ON APPROACH INTO DEN. PERFORMED BITECHECK. ADJUSTED AND TESTED THE GEAR DOOR MECHANISM. NO DEFECTS FOUND.
- [SDR ABXA000077](https://openairdocs.org/sdr/ABXA000077.md): Warning Light · illuminated · Jan 28, 2000 · N955AX · Doug DC941 · Landing Gear Position and Warning
  > LEFT GEAR UNSAFE LIGHT ILLUMINATED WITH THE HANDLE UP. CREW REPORTED GEAR CYCLED SEVERAL TIMES, NO HELP.
- [SDR ABXA000070](https://openairdocs.org/sdr/ABXA000070.md): Bushing · failed · Jan 20, 2000 · N955AX · Doug DC941 · Landing Gear Position and Warning
  > AFTER TAKEOFF, NOSE GEAR UNSAFE LIGHT BEGAN FLICKERING. RECYCLED GEAR THEN GOT STEADY RIGHT MAIN GEAR UNSAFE LIGHT. PERFORMED ABNORMAL PROCEDURES, FELT STRONG VIBRATION AT 210 KTS. RETURNED TO PNS. REPLACED BUSHING, TARGET SPRING AND ADJUSTED UPLATCH ROLLE
- [SDR ABXA000005](https://openairdocs.org/sdr/ABXA000005.md): Proximity Box · defective · Jan 3, 2000 · N955AX · Doug DC941 · Landing Gear Position and Warning
  > GEAR UPLATCH CHECK FAILED WHEN GEAR HANDLE WAS PLACED IN UPLATCH POSITION. NOSE GEAR UNSAFE LIGHT CAME ON. GEAR WAS RECYCLED TWICE. RIGHT GEAR UNSAFE LIGHT REMAINED ON. VERIFIED ALL CLEARANCES, CLEANED CANNON PLUG, REPLACED SENSOR CONTROL BOX AND OPS CHEC
- [SDR ABXA9900861](https://openairdocs.org/sdr/ABXA9900861.md): Battery · discharged · Dec 27, 1999 · N955AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERIES.
- [SDR ABXA9900677](https://openairdocs.org/sdr/ABXA9900677.md): Control Box · malfunctioned · Aug 29, 1999 · N955AX · Doug DC941 · Landing Gear Position and Warning
  > RIGHT MAIN LANDING GEAR LIGHT ILLUMINATED DURING FLIGHT. COMPLIED WITH ABNORMAL PROCEDURES. RECYCLED GEAR, LIGHT REMAINED ON. SPEED DECREASED TO LESS THAN 300 KNOTS FOR REMAINDER OF FLIGHT. ON DESCENT LIGHT EXTINGUISHED. REPLACED LANDING GEAR PROXIMITY CO
- [SDR ABXA9900323](https://openairdocs.org/sdr/ABXA9900323.md): Prox Box · defective · Apr 28, 1999 · N955AX · Doug DC941 · Landing Gear Position and Warning
  > AFTER TAKEOFF, RIGHT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR, NO CHANGE. REPLACED PROXIMITY SWITCH CONTROL BOX.
- [SDR ABXA9900145](https://openairdocs.org/sdr/ABXA9900145.md): Pan · cracked · Feb 19, 1999 · N955AX · Doug DC941 · Landing Gear Doors
  > DURING C-CHECK, FOUND LEFT MAIN LANDING GEAR DOOR PAN CRACKED ON FORWARD OUTBOARD EDGE. REPAIRED DOOR PAN IAW DC9 SRM 52-05.
- [SDR ABXA9900144](https://openairdocs.org/sdr/ABXA9900144.md): Floorbeam · cracked · Feb 19, 1999 · N955AX · Doug DC941 · Fuselage Main, Floor Beam
  > DURING C-CHECK, FOUND UPPER CARGO COMPARTMENT FLOORBEAM CRACKED AT STATION 237, LBL 6.0. REPAIRED FLOORBEAM IAW DC9 SRM SUPP DWG K05011.
- [SDR ABXA9900143](https://openairdocs.org/sdr/ABXA9900143.md): Longeron · cracked · Feb 19, 1999 · N955AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-02.
- [SDR ABXA9900142](https://openairdocs.org/sdr/ABXA9900142.md): Longeron · cracked · Feb 19, 1999 · N955AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 16 LEFT CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-02.
- [SDR ABXA9900184](https://openairdocs.org/sdr/ABXA9900184.md): Fitting · cracked · Feb 18, 1999 · N955AX · Doug DC941 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND AFT LOWER CARGO DOOR NR 2 BEAM END FITTING CRACKED AT NR 2 DOOR STOP. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA9900183](https://openairdocs.org/sdr/ABXA9900183.md): Fitting · cracked · Feb 18, 1999 · N955AX · Doug DC941 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND AFT LOWER CARGO DOOR NR 4 BEAM END FITTING CRACKED AT NR 4 DOOR STOP. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA9900178](https://openairdocs.org/sdr/ABXA9900178.md): Fitting · corroded · Feb 18, 1999 · N955AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND SEAT TRACK ATTACH FITTING EXFOLIATED AT STATION 794 AND LONGERON 3 LEFT. REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA9900177](https://openairdocs.org/sdr/ABXA9900177.md): Skin · cracked · Feb 18, 1999 · N955AX · Doug DC941 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND SKIN CRACKED BELOW LONGERON 14 RIGHT AT STATION 1072. REPAIRED SKIN IAW ABX REA D953-26826 MR.
- [SDR ABXA9900176](https://openairdocs.org/sdr/ABXA9900176.md): Blkhd Stiffener · cracked · Feb 18, 1999 · N955AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CRACKED AT LONGERON 15R. REPLACED CLIP IAW DC9 SRM 51-30-5.
- [SDR ABXA9900175](https://openairdocs.org/sdr/ABXA9900175.md): Clip · cracked · Feb 18, 1999 · N955AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER AT LONGERON 14 RIGHT CRACKED. REPLACED CLIP IAW DC9 SRM 51-30-5 AND DWG 9915558.
- [SDR ABXA9900174](https://openairdocs.org/sdr/ABXA9900174.md): Longeron · cracked · Feb 18, 1999 · N955AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 17R AT STATION 1041 CRACKED. REPAIRED LONGERON IAW DC9 SRM 53-02.
- [SDR ABXA9701139](https://openairdocs.org/sdr/ABXA9701139.md): Vane · delaminated · Jun 10, 1997 · N955AX · Doug DC941 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND THE LEFT FLAP CENTER FIXED VANE DELAMINATED OUT OF LIMITS AT THE LEADING EDGE. *S/D* REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN.
- [SDR ABXA9701138](https://openairdocs.org/sdr/ABXA9701138.md): Fitting · cracked · Jun 10, 1997 · N955AX · Doug DC941 · Spoilers
  > DURING C-CHECK, FOUND THE LT WING INBOARD SPOILER TORSION BAR SUPPORT FITTING IS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5.
- [SDR ABXA9701137](https://openairdocs.org/sdr/ABXA9701137.md): Skin · delaminated · Jun 10, 1997 · N955AX · Doug DC941 · Wing, Plate/Skin
  > DURING C-CHECK, FOUND THE LT WING LOWER SURFACE OF TRAILING EDGE PANEL FORWARD OF LT MLG DELAMINATED BEYOND LIMITS. REMOVED AND REPLACED BONDED PANEL (T/E) IAW DC-9 SRM 51-30-1.
- [SDR ABXA9701136](https://openairdocs.org/sdr/ABXA9701136.md): Spoiler · dented · Jun 10, 1997 · N955AX · Doug DC941 · Spoilers
  > DURING C-CHECK, FOUND THE RIGHT WING INBOARD SPOILER DENTED IN NUMEROUS PLACES ON UPPER SURFACE. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.
- [SDR ABXA9701114](https://openairdocs.org/sdr/ABXA9701114.md): Press Panel · corroded · Jun 6, 1997 · N955AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND THE LOWER SURFACE OF THE LEFT MLG WHELL WELL PRESSURE PANEL CORRODED AT STA 758 AND LBL 32. REPAIRED PRESSURE PANEL IAW DC9 SRM 53-04.
- [SDR ABXA9701113](https://openairdocs.org/sdr/ABXA9701113.md): Fitting · cracked · Jun 6, 1997 · N955AX · Doug DC941 · Nacelle/Pylon, Attach Fittings
  > DURING C-CHECK, FOUND THE RIGHT ENGINE PYLON REAR SPAR UPPER FITTING CRACKED AT THE FWD INBD CORNER. REPLACED FITTING IAW DC9 SRM.
- [SDR ABXA9701112](https://openairdocs.org/sdr/ABXA9701112.md): Fitting · corroded · Jun 6, 1997 · N955AX · Doug DC941 · Wing, Control Surface Attach Fittings
  > DURING C-CHECK, FOUND THE LEFT FLAP INBOARD FWD HINGE FITTING CORRODED. REPLACED THE FWD HINGE FITTING IAW DC9 MM 57-40-01.

Next page: https://openairdocs.org/deregistered/N955AX-2011-11-10/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 = 'N955AX' AND deregistration_id = 'N955AX-2011-11-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N955AX-2011-11-10/reports

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