# Service difficulty reports: N962AX, cancelled May 13, 2015

A list on [N962AX, cancelled May 13, 2015](https://openairdocs.org/deregistered/N962AX-2015-05-13.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 · 60 reports

- [SDR ABXA070358](https://openairdocs.org/sdr/ABXA070358.md): Door Frame · gouged · Oct 8, 2007 · N962AX · Doug DC941 · Fuselage Main, Structure
  > DOOR JAMB STA 200, LONGERON 15 RIGHT GOUGED. REPAIRED DOOR JAMB IAW DC9 SRM.
- [SDR ABXA070356](https://openairdocs.org/sdr/ABXA070356.md): Repair · cracked · Oct 8, 2007 · N962AX · Doug DC941 · Passenger/Crew Doors
  > MAIN ENTRY DOOR FORWARD LOWER CORNER REPAIR CRACKED. REMOVED AND REPLACED REPAIR IAW DC9 SRM 52-01 FIG 4.
- [SDR ABXA070357](https://openairdocs.org/sdr/ABXA070357.md): Angle · cracked · Oct 8, 2007 · N962AX · Doug DC941 · Passenger/Crew Doors
  > MAIN ENTRY DOOR UPPER AFT CORNER, ANGLE CRACKED INSIDE LIGHTENING HOLE. REPAIRED MAIN ENTRY DOOR UPPER AFT ANGLE IAW DC9 SRM.
- [SDR ABXA070355](https://openairdocs.org/sdr/ABXA070355.md): Fitting · cracked · Oct 6, 2007 · N962AX · Doug DC941 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR BEAM END FITTING WAS CRACKED AFT END OF NR 2 BEAM. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.
- [SDR ABXA070354](https://openairdocs.org/sdr/ABXA070354.md): Cusp Web · cracked · Oct 5, 2007 · N962AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED ON LEFT SIDE AT STA 980. REPAIRED CRACKED WEB IAW REA E-43520.
- [SDR ABXA070353](https://openairdocs.org/sdr/ABXA070353.md): Cusp Web · cracked · Oct 5, 2007 · N962AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED AT STA 1022 - 1036. REPLACED CUSP WEB AS REQUIRED IAW DC9 SRM.
- [SDR ABXA070324](https://openairdocs.org/sdr/ABXA070324.md): Wheel · separated · Sep 28, 2007 · N962AX · Doug DC941 · Wheel/Ski/Float
  > AIRCRAFT BLOCKED IN WITH NR 4 MAIN TIRE FLAT. FOUND NR 4 WHEEL RIM SEPARATED. REPLACED NR 4 MAIN WHEEL ASSEMBLY, NR 4 BRAKE AND THE RIGHT MAIN LANDING GEAR PISTON AND AXLE ASSEMBLY IAW DC9 MM CHAPTER 32.
- [SDR ABXA060024](https://openairdocs.org/sdr/ABXA060024.md): Torque Tube · damaged · Jan 12, 2006 · N962AX · Doug DC941 · Landing Gear Door Retract Section
  > LANDING GEAR MALFUNCTION, GEAR DOOR OPEN LIGHT ILLUMINATED WITH GEAR HANDLE DOWN & 3 GREEN WHILE IN FLIGHT. LANDING GEAR WAS RECYCLED. REPLACED GEAR DOOR, TORQUE TUBE AND DOOR SEQUENCE DRIVE ARM IAW DC9 MM 32-11-03-2-02-1.
- [SDR ABXA050258](https://openairdocs.org/sdr/ABXA050258.md): Cargo Track · corroded · Oct 12, 2005 · N962AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD LOWER CARGO LEFT TRACK HAD EXFOLIATED CORROSION AT TWO ATTACH FASTENERS BETWEEN STA 218 AND 237. REPLACED BAD SECTION OF TRACK IAW DC-9 SSRM K05159 DRAWING.
- [SDR ABXA050261](https://openairdocs.org/sdr/ABXA050261.md): Bulkhead · cracked · Oct 11, 2005 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD DOOR UPPER LT CORNER 13 DOUBLER HAD RADIAL CRACK EXTENDING FROM STOP DRILL. CRACK EXCEEDED APPLICABILITY AND CRACK REPAIR LIMITS FOR PREVIOUS J060088-1 ANGLE REPAIR. STOP DRILLED CRACKS AND REPAIRED IAW SRM.
- [SDR ABXA050257](https://openairdocs.org/sdr/ABXA050257.md): Intercostal · cracked · Oct 11, 2005 · N962AX · Doug DC941 · Fuselage Miscellaneous Structure
  > AFT ASSY COMPARTMENT INTERCOSTAL BETWEEN FS 1114 AND FS 1133, LONGERON 17 RIGHT AND LONGERON 16 RIGHT HAD A CRACK ON BOTTOM FORWARD SIDE. FABRICATED AND INSTALLED REPAIR ANGLE AS REQUIRED IAW DC-9 SRM K05159 DRAWING.
- [SDR ABXA050260](https://openairdocs.org/sdr/ABXA050260.md): Skin · corroded · Oct 10, 2005 · N962AX · Doug DC941 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BULGED AT STA 579, LONERON 30, EVIDENCE OF CORROSION INTERNAL. REMOVED INTERNAL CORRODED DOUBLER / INSTALLED NEW DOUBLER IAW SRM.
- [SDR ABXA050256](https://openairdocs.org/sdr/ABXA050256.md): Skin · cracked · Oct 10, 2005 · N962AX · Doug DC941 · Fuselage Main, Plate/Skin
  > FUSELAGE CRACK AT STA. 1087, LONGERON 2 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA040377](https://openairdocs.org/sdr/ABXA040377.md): Pressure Panel · leaking · Nov 12, 2004 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > DESCENDING, PASSING FL 180, AUTOPILOT WITH HEADING MODE ENGAGED, NOTICED A/C DRIFTED 20 DEGREES LT OF COURSE WITH NOSE DOWN, SWITCHED TO TURN KNOB, A/C WOULD NOT RESPOND. DISENGAGED AUTOPILOT, YOKE STILL IN LT/FWD POSITION. WENT TO ROLL WINGS LEVEL BUT YOKE JA
- [SDR ABXA040183](https://openairdocs.org/sdr/ABXA040183.md): Link · damaged · May 11, 2004 · N962AX · Doug DC941 · Aerodynamic Fairings
  > AIRCRAFT VIBRATES AT 320 KTS AT LOW ALTITUDE CLIMB AND CRUISE REGARDLESS OF POWER SETTINGS. REPLACED RT WING TO STRUCTURE TRAILING LINKS AND HARDWARE DUE TO EXCESSIVE MOVEMENT IAW MM 20-10, 20-15 & 20-16.
- [SDR ABXA040059](https://openairdocs.org/sdr/ABXA040059.md): Stiffener · cracked · Jan 28, 2004 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FORWARD RIGHT STIFFENER, 4TH FROM TOP, WAS CRACKED AT TEE. REPAIRED AREA IAW DC-9 SSRM K05159.
- [SDR ABXA020353](https://openairdocs.org/sdr/ABXA020353.md): Link · cracked · Dec 6, 2002 · N962AX · Doug DC941 · Engine Thrust Reverser
  > NR 1 ENGINE UPPER RIGHT LINK THRUST REVERSER CRACKED. REPLACED IAW MM.
- [SDR ABXA020036](https://openairdocs.org/sdr/ABXA020036.md): Stringer · cracked · Jun 5, 2002 · N962AX · Doug DC941 · Horizontal Stabilizer, Spar/Rib
  > RIGHT STAB. INTERIOR #2 UPPER STRINGER, WAS CRACKED AT XHS 204.1, APPROXIMATELY 1.5" INBOARD TO OUTBOARD OF RIB. REPAIRED #2 STRINGER IAW DC-9 SRM 55-02.
- [SDR ABXA020035](https://openairdocs.org/sdr/ABXA020035.md): Stringer · cracked · Jun 5, 2002 · N962AX · Doug DC941 · Horizontal Stabilizer, Spar/Rib
  > RIGHT STAB. INTERIOR, #3 UPPER STRINGER, WAS CRACKED AT XHS 158, 1" INBOARD TO OUTBOARD OF RIB. REPAIRED #3 STRINGER IAW DC-9 SRM 55-02.
- [SDR ABXA000298](https://openairdocs.org/sdr/ABXA000298.md): Control Box · failed · Jun 12, 2000 · N962AX · Doug DC941 · Landing Gear Position and Warning
  > ON TAKEOFF, THE GREEN NOSE LANDING GEAR LIGHT WAS OUT WITH THE GEAR IN THE DOWN POSITION. THE RED NOSE GEAR UNSAFE LIGHT WAS ILLUMINATED WITH THE GEAR HANDLE UP. RECYCLED THE GEAR AND ACCOMPLISHED ABNORMAL PROCEDURES. THE UNSAFE LIGHT EXTINGUISHED. REPLACE
- [SDR ABXA000112](https://openairdocs.org/sdr/ABXA000112.md): Control · failed · Feb 18, 2000 · N962AX · Doug DC941 · Landing Gear Position and Warning
  > LEFT MAIN GEAR INDICATED UNSAFE POSITION ON GEAR EXTENSION. MAIN GEAR DOWNLOCK SWITCH INDICATES GREEN. GEAR WARNING HORN COULD NOT BE SILENCED. PULLED P26 AND SILENCED HORN. LANDING UNEVENTFUL. CREW RECYCLED GEAR. RERACKED PROX CONTROL BOX. OPS CHECKED
- [SDR ABXA9900830](https://openairdocs.org/sdr/ABXA9900830.md): Power Supply · discharged · Dec 6, 1999 · N962AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE INTERMITTENTLY. REPLACED EMERGENCY LIGHT POWER SUPPLY.
- [SDR ABXA9701363](https://openairdocs.org/sdr/ABXA9701363.md): Skin · corroded · Jul 31, 1997 · N962AX · Doug DC941 · Wing, Plate/Skin
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE CENTER WING TANK LOWER KEEL DOUBLER HAD NUMEROUS CORROSION BLENDOUTS BEYOND SRM LIMITS. REPAIRED CENTER WING LOWER KEEL DOUBLER IAW ABX REA D957-19608-MR.
- [SDR ABXA9701362](https://openairdocs.org/sdr/ABXA9701362.md): Longeron · corroded · Jul 31, 1997 · N962AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND LONGERON 25 LEFT TEE ANGLE CORRODED AT FS 1152. REPAIRED LONGERON 25 IAW ABX REA D953-20348-MR.
- [SDR ABXA9701392](https://openairdocs.org/sdr/ABXA9701392.md): Fitting · cracked · Jul 10, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND KEEL FITTING AT FS 737 CRACKED. REPLACED KEEL FITTING AT FS 737 IAW DC-9 SRM CHAPTER 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA9701385](https://openairdocs.org/sdr/ABXA9701385.md): Bracket · corroded · Jul 9, 1997 · N962AX · Doug DC941 · Leading Edge Slat Control System
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE SLAT CONTROL VALVE PULLEY BRACKET CORRODED AT FS 675. REPLACED SLAT CABLE PULLEY BRACKET AND RIGGED SLAT CONTROL SYSTEM IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-80-2.
- [SDR ABXA9701383](https://openairdocs.org/sdr/ABXA9701383.md): Jamb · cracked · Jul 9, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT MAIN LANDING GEAR DOOR FORWARD JAMB CRACKED AT UPLOCK SWITCH. REPAIRED DOOR JAMB IAW ABX REA D953-20150.
- [SDR ABXA9701384](https://openairdocs.org/sdr/ABXA9701384.md): Fitting · corroded · Jul 8, 1997 · N962AX · Doug DC941 · Nacelle/Pylon, Attach Fittings
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT ENGINE PYLON UPPER BEAVERTAIL FITTING CORRODED. REMOVED AND REPLACED LEFT BEAVERTAIL FITTING AND REPAIRED AREA IAW ABX REA D954-20135-MR AND DC-9 SRM CHAPTER 51-30-5.
- [SDR ABXA9701387](https://openairdocs.org/sdr/ABXA9701387.md): Fitting · corroded · Jul 1, 1997 · N962AX · Doug DC941 · Nacelle/Pylon, Attach Fittings
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT ENGINE PYLON LOWER BEAVERTAIL FITTING CORRODED. REPAIRED LEFT LOWER BEAVERTAIL IAW ABX REA D954-20074 AND DC-9 SRM CHAPTER 53-04, FIGURE 13.
- [SDR ABXA9701386](https://openairdocs.org/sdr/ABXA9701386.md): Fitting · corroded · Jul 1, 1997 · N962AX · Doug DC941 · Nacelle/Pylon, Attach Fittings
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT ENGINE PYLON LOWER BEAVERTAIL FITTING CORRODED. REPAIRED RIGHT PYLON LOWER BEAVERTAIL IAW ABX REA D954-19607-MR.
- [SDR ABXA9701388](https://openairdocs.org/sdr/ABXA9701388.md): Bracket · cracked · Jun 27, 1997 · N962AX · Doug DC941 · Aileron Control System
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT LATERAL CONTROL MIXER BRACKET CRACKED AND CORRODED. REPLACED LEFT LATERAL CONTROL MIXER BRACKET IAW DC-9 MAINTENANCE MANUAL CHAPTERS 20-16-0 AND 27-61-4.
- [SDR ABXA9701361](https://openairdocs.org/sdr/ABXA9701361.md): Fitting · corroded · Jun 27, 1997 · N962AX · Doug DC941 · Nacelle/Pylon Structure
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT PYLON UPPER BEAVERTAIL EXCESSIVELY CORRODED. REPAIRED RIGHT UPPER BEAVERTAIL IAW ABX REA D954-19607-MR.
- [SDR ABXA9701389](https://openairdocs.org/sdr/ABXA9701389.md): Rib · cracked · Jun 24, 1997 · N962AX · Doug DC941 · Wing, Rib/Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT WING NR 2 SLAT TRACK INBOARD RIB CRACKED AT AFT LOWER FLANGE. REPLACED NR 2 RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9701376](https://openairdocs.org/sdr/ABXA9701376.md): Skin · cracked · Jun 23, 1997 · N962AX · Doug DC941 · Fuselage Main, Plate/Skin
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND TWO FUSELAGE SKIN CRACKS AT RIVETS AT FS58 ON LEFT HAND SIDE. REPAIRED IAW DC-9 SRM CHAPTER 53-01.
- [SDR ABXA9701391](https://openairdocs.org/sdr/ABXA9701391.md): Rib · cracked · Jun 19, 1997 · N962AX · Doug DC941 · Wing, Rib/Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT WING LEADING EDGE RIB AT STATION XIS 136 CORRODED. REPLACED WING LEADING EDGE RIB AT XIS 136 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9701390](https://openairdocs.org/sdr/ABXA9701390.md): Bulkhead Jamb · cracked · Jun 18, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH VISUAL INSPECTION OF THE AFT PRESSURE BULKHEAD IAW AD 85-01-02 PER SB 53-137, FOUND THE BULKHEAD DOOR JAMB CRACKED JUST BELOW THE UPPER LEFT CORNER OF DOOR CUTOUT. REPLACED CRACKED DOUBLER IAW DC-9 SRM CHAPTER 51-30-5.
- [SDR ABXA9701382](https://openairdocs.org/sdr/ABXA9701382.md): Jamb · corroded · Jun 17, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT VENTRAL DOOR JAMB FRAME CORRODED FROM FS 1133 TO FS 1163. REPLACED THE UPPER JAMB CAP AND DOOR STOP FITTINGS IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9701381](https://openairdocs.org/sdr/ABXA9701381.md): Bulkhead Clip · cracked · Jun 17, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 9 LEFT. REMOVED AND REPLACED CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.
- [SDR ABXA9701379](https://openairdocs.org/sdr/ABXA9701379.md): Bulkhead Clip · cracked · Jun 16, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 9 RIGHT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1.
- [SDR ABXA9701378](https://openairdocs.org/sdr/ABXA9701378.md): Bulkhead Clip · cracked · Jun 16, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 7R. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.
- [SDR ABXA9701364](https://openairdocs.org/sdr/ABXA9701364.md): Former · cracked · Jun 16, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND A FRAME FITTING CRACKED AT FS 675 JUST INBOARD OF LEFT CANTED KEEL. REPAIRED FRAME FITTING IAW DC-9 SRM CHAPTER 53-03, FIGURE 12.
- [SDR ABXA9701380](https://openairdocs.org/sdr/ABXA9701380.md): Slat · corroded · Jun 13, 1997 · N962AX · Doug DC941 · Leading Edge Devices
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE NR 1 LEFT SLAT CORRODED AT CENTER ATTACH FITTING. REPLACED NR 1 LEFT SLAT IAW DC-9 MAINTENANCE MANUAL, CHAPTER 27-80-1.
- [SDR ABXA9701360](https://openairdocs.org/sdr/ABXA9701360.md): Keelbeam · corroded · Jun 13, 1997 · N962AX · Doug DC941 · Fuselage Main, Keel
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE KEEL BEAM HAD EXCESSIVE CORROSION BLENDOUTS AT FS665.0. REPAIRED KEEL BEAM IAW ABX REA D953-19727-MR.
- [SDR ABXA9701377](https://openairdocs.org/sdr/ABXA9701377.md): Bulkhead Skin · cracked · Jun 12, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB CRACKED ON RIGHT SIDE. REPAIRED DOOR JAMB IAW DC-9 SRM CHAPTER 53-05.
- [SDR ABXA9701374](https://openairdocs.org/sdr/ABXA9701374.md): Bracket · corroded · Jun 12, 1997 · N962AX · Doug DC941 · Vertical Stabilizer
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LOWER RUDDER HINGE BRACKET CORRODED. REPLACED HINGE BRACKET IAW DC-9 MM 20-16-0.
- [SDR ABXA9701373](https://openairdocs.org/sdr/ABXA9701373.md): Former · cracked · Jun 12, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND A FORMER CRACKED AT FS660 IN RIGHT CANTED KEEL AREA. REPLACED FORMER AND CLIP IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9701370](https://openairdocs.org/sdr/ABXA9701370.md): Bulkhead Clip · cracked · Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 12 RIGHT. REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.
- [SDR ABXA9701369](https://openairdocs.org/sdr/ABXA9701369.md): Bulkhead Clip · cracked · Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 14 RIGHT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.
- [SDR ABXA9701368](https://openairdocs.org/sdr/ABXA9701368.md): Bulkhead Clip · cracked · Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 14 LEFT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.
- [SDR ABXA9701367](https://openairdocs.org/sdr/ABXA9701367.md): Bulkhead Clip · cracked · Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 15 LEFT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.

Next page: https://openairdocs.org/deregistered/N962AX-2015-05-13/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 = 'N962AX' AND deregistration_id = 'N962AX-2015-05-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N962AX-2015-05-13/reports

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