# Service difficulty reports: N960AX, cancelled May 15, 2017

A list on [N960AX, cancelled May 15, 2017](https://openairdocs.org/deregistered/N960AX-2017-05-15.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 · 73 reports

- [SDR ABXA080179](https://openairdocs.org/sdr/ABXA080179.md): Target · defective · Jun 20, 2008 · N960AX · Doug DC941 · Landing Gear Position and Warning
  > RIGHT GEAR UNSAFE LIGHT ON AFTER TAKE OFF, RECYCLED GEAR STILL ON. REPLACED STIKER/TARGET ASSEMBLY IAW DC9 MM. (A)
- [SDR ABXA070302](https://openairdocs.org/sdr/ABXA070302.md): Floor Support · cracked · Sep 12, 2007 · N960AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT STA 351 LEFT HAD A 10 INCH CRACK ON UPPER FLANGE. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA070301](https://openairdocs.org/sdr/ABXA070301.md): Bulkhead · cracked · Sep 4, 2007 · N960AX · Doug DC941 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CUTOUT UPPER RIGHT CORNER HAD APPROXIMATELY 1.20 INCH LONG CRACK IN DOUBLER WITH NO PREVIOUS REPAIR CONFIG INSTALLED. NOTE: UPPER LEFT CORNER PREVIOUS J060088-1 CONFIG REPAIRED DOOR CORNERS IAW DC9 SRM.
- [SDR ABXA070300](https://openairdocs.org/sdr/ABXA070300.md): Fitting · cracked · Aug 31, 2007 · N960AX · Doug DC941 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR NR 2 AFT BEAM END FITTING CRACKED. REMOVED AND REPLACED AFT LOWER CARGO DOOR NR 2 AFT BEAM END FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA070284](https://openairdocs.org/sdr/ABXA070284.md): Angle · cracked · Aug 30, 2007 · N960AX · Doug DC941 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON WEB ANGLE ABOVE FORWARD EDGE OF PANEL 8206A INSIDE PYLON CRACKED. REPAIRED ANGLE IAW DC9 SSRM K05159. PO 421513435. INSTALLED WITH HI-LOKS IAW DC9 SRM 51-30-5.
- [SDR ABXA060305](https://openairdocs.org/sdr/ABXA060305.md): Battery · discharged · Nov 20, 2006 · N960AX · Doug DC932F · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001.
- [SDR ABXA060187](https://openairdocs.org/sdr/ABXA060187.md): Access Door · missing · Jun 13, 2006 · N960AX · Doug DC941 · Accessory Compartment Doors
  > PANEL 7503A FOR LEFT ENGINE THRUST REVERSER CONTROL VALVE WAS FOUND MISSING FROM AIRCRAFT. INSTALLED NEW PANEL IAW DC9 AMM.
- [SDR ABXA050235](https://openairdocs.org/sdr/ABXA050235.md): Engine · defective · Sep 22, 2005 · N960AX · Doug DC941 · Engine (Turbine/Turboprop)
  > LEFT ENGINE WOULD NOT SPOOL UP DURING APPROACH. WHEN THROTTLE WAS ADVANCED, ENGINE WOULD NOT START, COMPRESSOR STALLED. EMERGENCY DECLARED. LANDED WITH ENGINE AT IDLE POWER. SERVICED FUEL CONTROL UNIT WITH 6 ML OF SILICON OIL IAW P&W JT8D-11 MM 73-21-01.
- [SDR ABXA050213](https://openairdocs.org/sdr/ABXA050213.md): Floor Support · cracked · Aug 21, 2005 · N960AX · Doug DC941 · Fuselage Miscellaneous Structure
  > LEFT VERTICAL FLOOR SUPPORT CRACKED AT FS 718, LEFT BUTT LINE 44. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-1.
- [SDR ABXA030470](https://openairdocs.org/sdr/ABXA030470.md): Door Frame · cracked · Dec 2, 2003 · N960AX · Doug DC941 · Fuselage Main, Structure
  > CRACKS EMANATING FROM OPEN HOLE ON LEFT AFT EMERGENCY DOOR JAMB LOWER WEB AT FS 711 BETWEEN LONGERONS 16 AND 17 LEFT. INSTALLED DOUBLER REPAIR IAW DC-9 SRM 51-30-2 AND REPAIRED AREA IAW DC-9 53-01.
- [SDR ABXA030472](https://openairdocs.org/sdr/ABXA030472.md): Fitting · cracked · Dec 2, 2003 · N960AX · Doug DC941 · Fuselage Main, Attach Fittings
  > FITTING WAS CRACKED AT STA 366 LONGERON 29 RT. REMOVED AND REPLACED FITTING AT STA 366 LONGERON 29 RIGHT IAW DC-9 SRM 51-30-5.
- [SDR ABXA030471](https://openairdocs.org/sdr/ABXA030471.md): Shear Tie · cracked · Dec 2, 2003 · N960AX · Doug DC941 · Fuselage Main, Structure
  > SHEAR TIE FS 1056 LONGERON 14 RT CRACKED. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA030469](https://openairdocs.org/sdr/ABXA030469.md): Rib · cracked · Nov 30, 2003 · N960AX · Doug DC941 · Wing, Rib/Bulkhead
  > CRACK IN LT WING RIB UPPER CLIP AT X0S 447. REPLACED CLIP IAW DC-9 SRM 51-30.
- [SDR ABXA000421](https://openairdocs.org/sdr/ABXA000421.md): Power Supply · discharged · Sep 15, 2000 · N960AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS CAME ON WHEN POWER WAS SELECTED OFF AND THE SWITCH WAS IN THE OFF POSITION. REPLACED THE EMERGENCY LIGHT POWER SUPPLY.
- [SDR ABXA000297](https://openairdocs.org/sdr/ABXA000297.md): Receptacle · burned · Jun 13, 2000 · N960AX · Doug DC941 · External Power System
  > DURING LINE OPERATION WHILE CONNECTING GROUND EXTERNAL POWER, CREW REPORTED SPARKS AND SMOKE COMING FROM EXTERNAL POWER RECEPTACLE WHEN GROUND POWER CART WAS CONNECTED AND POWER APPLIED. REPLACED EXTERNAL POWER RECEPTACLE.
- [SDR ABXA9900560](https://openairdocs.org/sdr/ABXA9900560.md): Fuse · defective · Jun 29, 1999 · N960AX · Doug DC941 · Hydraulic System, Main
  > DURING TAXI-OUT, RIGHT BRAKE WAS GRABBING. TIRE APPEARED TO BE FLAT-SPOTTED. WHILE TAXIING BACK TO BLOCKS, RIGHT BRAKE PEDAL WENT ALL THE WAY TO THE FLOOR. PUMPING THE BRAKES BROUGHT THE PEDAL BACK UP. REPLACED NR 3 AND NR 4 MAIN TIRE AND WHEEL ASSEMBLIES
- [SDR ABXA9900545](https://openairdocs.org/sdr/ABXA9900545.md): Window · stuck · Jun 25, 1999 · N960AX · Doug DC941 · Flight Compartment Windows
  > FIRST OFFICER'S CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED FIRST OFFICER'S WINDOW MECHANISM, OPS CHECKED GOOD.
- [SDR ABXA9900101](https://openairdocs.org/sdr/ABXA9900101.md): Longeron · cracked · Feb 1, 1999 · N960AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 16 RIGHT CRACKED AT STATION 1041. REPLACED LONGERON SECTION 16 RIGHT IAW DC9 SRM 53-02.
- [SDR ABXA9900100](https://openairdocs.org/sdr/ABXA9900100.md): Longeron · cracked · Feb 1, 1999 · N960AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 1041. REPLACED LONGERON 17 LEFT IAW DC9 SRM 53-02.
- [SDR ABXA9701830](https://openairdocs.org/sdr/ABXA9701830.md): Tab · delaminated · Nov 6, 1997 · N960AX · Doug DC941 · Aileron Tabs
  > DURING INSPECTION, FOUND RT WING AILERON CONTROL TAB HAD 6 DELAMINATED AREA BELOW MIDDLE HINGE ON LOWER SURFACE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.
- [SDR ABXA9701045](https://openairdocs.org/sdr/ABXA9701045.md): Panel · delaminated · May 18, 1997 · N960AX · Doug DC941 · Spoilers
  > DURING D-INSPECTION, FOUND THE LEFT WING OUTBOARD SPOILER PANEL DELAMINATED. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS.
- [SDR ABXA9701043](https://openairdocs.org/sdr/ABXA9701043.md): Panel · delaminated · May 18, 1997 · N960AX · Doug DC941 · Spoilers
  > DURING D-INSPECTION, FOUND THE LEFT WING INBOARD SPOILER PANEL DELAMINATED. *S/D* REPAIRED UNIT COMPLETE.
- [SDR ABXA9701046](https://openairdocs.org/sdr/ABXA9701046.md): Door Assy · cracked · May 12, 1997 · N960AX · Doug DC941 · Landing Gear Doors
  > DURING D-INSPECTION, FOUND THE RIGHT MAIN LANDING GEAR DOOR PAN CRACKED AT FORWARD SIDE OF ACTUATOR ATTACH BRACKET. REMOVED AND REPLACED RIGHT MLG DOOR IAW DC9 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 32-12-01.
- [SDR ABXA9701044](https://openairdocs.org/sdr/ABXA9701044.md): Door · cracked · May 12, 1997 · N960AX · Doug DC941 · Landing Gear Doors
  > DURING D-INSPECTION, FOUND THE LEFT MAIN LANDING GEAR WHEEL WELL DOOR CRACKED AT FORWARD UPPER CORNER OF ACTUATOR ATTACH FITTING. REPLACED LEFT MLG W/WELL DOOR IAW DC-9 SMM 32-12-01.
- [SDR ABXA9701053](https://openairdocs.org/sdr/ABXA9701053.md): Keel Frame · cracked · May 7, 1997 · N960AX · Doug DC941 · Fuselage Main, Keel
  > DURING D-INSPECTION, FOUND THE RIGHT LOWER KEEL FRAME CRACKED AT FS 675 IN CANTED KEEL AREA. REPLACED FRAME AND CLIP IAW DC9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9701058](https://openairdocs.org/sdr/ABXA9701058.md): Fitting · corroded · May 6, 1997 · N960AX · Doug DC941 · Leading Edge Devices
  > DURING D-INSPECTION, FOUND THE RIGHT WING NR 3 SLAT CENTER ATTACH FITTING CORRODED. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.
- [SDR ABXA9701057](https://openairdocs.org/sdr/ABXA9701057.md): Slat · corroded · May 6, 1997 · N960AX · Doug DC941 · Leading Edge Devices
  > DURING D-INSPECTION, FOUND THE RIGHT WING NR 4 SLAT CORRODED INBOARD OF CENTER ATTACH FITTING. *S/D* REPAIRED UNIT COMPLETE.
- [SDR ABXA9701056](https://openairdocs.org/sdr/ABXA9701056.md): Fitting · chafed · May 6, 1997 · N960AX · Doug DC941 · Leading Edge Devices
  > DURING D-INSPECTION, FOUND THE RIGHT WING NR 5 SLAT OUTBOARD FITTING CHAFED BEYOND LIMITS. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.
- [SDR ABXA9701055](https://openairdocs.org/sdr/ABXA9701055.md): Fitting · corroded · May 6, 1997 · N960AX · Doug DC941 · Leading Edge Devices
  > DURING D-INSPECTION, FOUND THE RIGHT WING NR 1 SLAT CENTER ATTACH FITTING CORRODED. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.
- [SDR ABXA9701054](https://openairdocs.org/sdr/ABXA9701054.md): Fitting · corroded · May 6, 1997 · N960AX · Doug DC941 · Leading Edge Devices
  > DURING D-INSPECTION, FOUND THE RIGHT WING NR 2 SLAT CENTER ATTACH FITTING CORRODED. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.
- [SDR ABXA9701067](https://openairdocs.org/sdr/ABXA9701067.md): Panel · delaminated · Apr 23, 1997 · N960AX · Doug DC941 · Wing, Plate/Skin
  > DURING D-INSPECTION, FOUND THE RIGHT WING LOWER BONDED TRAILING EDGE PANEL INBOARD OF MLG ATTACH FITTING DELAMINATED. REPLACED BONDED PANEL IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA9701068](https://openairdocs.org/sdr/ABXA9701068.md): Arm · cracked · Apr 22, 1997 · N960AX · Doug DC941 · Rudder Control System
  > DURING D-INSPECTION, FOUND THE FIRST OFFICERS RIGHT RUDDER PEDAL ARM CRACKED AT OUTBOARD ATTACH HOLD. REPLACED RIGHT RUDDER PEDAL ARM IAW DC9 MAINTENANCE MANUAL CHAPTER 20-16-0.
- [SDR ABXA9701069](https://openairdocs.org/sdr/ABXA9701069.md): Jamb · corroded · Apr 14, 1997 · N960AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING D-INSPECTION, FOUND THE WEB AROUND THE AFT BAG BIN DOOR JAMB CORRODED. REMOVED AND REPLACED WEB IAW DC-9 SRM CHAPTER 51-30-2.
- [SDR ABXA9701072](https://openairdocs.org/sdr/ABXA9701072.md): Bracket · corroded · Apr 11, 1997 · N960AX · Doug DC941 · Wing Miscellaneous Structure
  > DURING D-INSPECTION, FOUND THE RIGHT WING TIP REAR SPAR ATTACH BRACKET CORRODED. REMOVED AND REPLACED WING TIP ATTACH BRACKET IAW DC-9 SRM 51-30-1.
- [SDR ABXA9701071](https://openairdocs.org/sdr/ABXA9701071.md): Bracket · corroded · Apr 11, 1997 · N960AX · Doug DC941 · Wing Miscellaneous Structure
  > DURING D-INSPECTION, FOUND THE LEFT WING TIP REAR SPAR ATTACH BRACKET CORRODED. REPLACED BRACKET IAW DC-9 SRM CHAPTER 51-30-5.
- [SDR ABXA9701070](https://openairdocs.org/sdr/ABXA9701070.md): Panel · delaminated · Apr 11, 1997 · N960AX · Doug DC941 · Wing, Plate/Skin
  > DURING D-INSPECTION, FOUND THE RIGHT WING UPPER TRAILING EDGE BONDED PANEL INBOARD OF THE MLG ATTACH FITTING DELAMINATED. REMOVED AND REPLACED PANEL ASSY IAW DC-9 SRM CHAPTER 51-30-2.
- [SDR ABXA9701051](https://openairdocs.org/sdr/ABXA9701051.md): Panel · corroded · Apr 11, 1997 · N960AX · Doug DC941 · Wing, Plate/Skin
  > DURING D-INSPECTION, FOUND THE LEFT WING UPPER TRAILING EDGE PANEL BETWEEN STATIONS XRS 69 AND XRS 111 CORRODED AND DELAMINATED. REMOVED AND REPLACED BONDED PANEL IAW DC9 SRM CHAPTERS 51-30-1.
- [SDR ABXA9701050](https://openairdocs.org/sdr/ABXA9701050.md): Fitting · corroded · Apr 10, 1997 · N960AX · Doug DC941 · Wing, Landing Gear Attach Fittings
  > DURING D-INSPECTION, FOUND THE RIGHT MAIN LANDING GEAR ATTACH FITTING CORRODED ON FORWARD AND AFT SIDES OF THE FIXED SIDE BRACE LUG. REPAIRED IAW ABX REA D932-18677-MR.
- [SDR ABXA9701049](https://openairdocs.org/sdr/ABXA9701049.md): Fitting · corroded · Apr 10, 1997 · N960AX · Doug DC941 · Main Landing Gear Attach Section
  > DURING D-INSPECTION, FOUND THE LEFT MAIN LANDING GEAR ATTACH FITTING CORRODED ON THE FORWARD AND AFT SIDES OF THE FIXED BRACE ATTACH LUG. REPAIRED IAW ABX REA D932-18677-MR.
- [SDR ABXA9701048](https://openairdocs.org/sdr/ABXA9701048.md): Fitting · corroded · Apr 10, 1997 · N960AX · Doug DC941 · Wing, Landing Gear Attach Fittings
  > DURING D-INSPECTION, FOUND LEFT MAIN LANDING GEAR ATTACH FITTING CORRODED IN POCKET AT INBOARD END OF AUX SPAR LOWER FITTING. REPAIRED IAW ABX REA D957-18899-MR.
- [SDR ABXA9701077](https://openairdocs.org/sdr/ABXA9701077.md): Jamb · corroded · Apr 8, 1997 · N960AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING D-INSPECTION, FOUND THE LEFT SIDE OF THE VENTRAL STAIR JAMB HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED AFT JAMB WEB AND CAP IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA9701076](https://openairdocs.org/sdr/ABXA9701076.md): Angle · corroded · Apr 8, 1997 · N960AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING D-INSPECTION, FOUND THE LOWER KEEL ATTACH ANGLE CORRODED SEVERAL PLACES FROM FS 642 TO FS 729. REPLACED LOWER KEEL ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-5.
- [SDR ABXA9701075](https://openairdocs.org/sdr/ABXA9701075.md): Former · cracked · Apr 8, 1997 · N960AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING D-INSPECTION, FOUND THE FRAME CLIP AT FS 660 IN THE LEFT LOWER KEEL CRACKED AT CANTED KEEL. REPLACED FRAME AT FS 660 IAW DC-9 SRM CHAPTER 51-30-2.
- [SDR ABXA9701074](https://openairdocs.org/sdr/ABXA9701074.md): Bulkhead Fitting · cracked · Apr 8, 1997 · N960AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR FRAME ATTACH FITTING CRACKED JUST ABOVE STIFFENER AT Z14R BETWEEN LONGERONS 16 AND 17 RIGHT. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9701073](https://openairdocs.org/sdr/ABXA9701073.md): Bulkhead Fitting · cracked · Apr 8, 1997 · N960AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR FRAME ATTACH FITTING CRACKED JUST ABOVE STIFFENER Z34 RIGHT AT LONGERON 14 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-2.
- [SDR ABXA9701047](https://openairdocs.org/sdr/ABXA9701047.md): Bulkhead Web · cracked · Apr 7, 1997 · N960AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LEFT HAND DOUBLER HAD A BEND RADIUS CRACK. REPAIRED IAW ABX REA D953-18897-MR.
- [SDR ABXA9701052](https://openairdocs.org/sdr/ABXA9701052.md): Retainer · cracked · Apr 4, 1997 · N960AX · Doug DC941 · Flight Compartment Windows
  > WHILE COMPLYING WITH X-RAY INSPECTION OF THE FLIGHT COMPARTMENT OVERHEAD WINDOW RETAINERS IAW AD 90-18-03 AND SB 56-11, FOUND CRACK AT RIGHT SLIDING WINDOW UPPER AFT CORNER. REPLACED DOUBLER WITH NEW PART IAW DC9 SRM CHAPTER 51-30-2.
- [SDR ABXA9701118](https://openairdocs.org/sdr/ABXA9701118.md): Skin · corroded · Apr 3, 1997 · N960AX · Doug DC941 · Spoilers
  > DURING D-CHECK, FOUND RIGHT OUTBOARD SPOILER LEADING EDGE CORRODED AND.5 INCH HOLE IN UPPER SKIN. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.
- [SDR ABXA9701078](https://openairdocs.org/sdr/ABXA9701078.md): Bulkhead Jamb · cracked · Apr 3, 1997 · N960AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING D-INSPECTION, FOUND TWO CRACKS IN THE AFT PRESSURE BULKHEAD DOOR JAMB, RIGHT UPPER CORNER. REMOVED AND REPLACED CRACKED Y-DOUBLER IAW DC-9 SRM CHAPTER 51-30-5.
- [SDR ABXA9701079](https://openairdocs.org/sdr/ABXA9701079.md): Angle · corroded · Mar 31, 1997 · N960AX · Doug DC941 · Wing Miscellaneous Structure
  > DURING D-INSPECTION, FOUND THE LEFT WING INBOARD UPPER TRAILING EDGE PANEL, ATTACH ANGLE CORRODED AT LONGERON 20. REMOVED AND REPLACED ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-1.

Next page: https://openairdocs.org/deregistered/N960AX-2017-05-15/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 = 'N960AX' AND deregistration_id = 'N960AX-2017-05-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N960AX-2017-05-15/reports

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