# Service difficulty reports: N964AX, cancelled Jan 4, 2010

A list on [N964AX, cancelled Jan 4, 2010](https://openairdocs.org/deregistered/N964AX-2010-01-04.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 · 63 reports

- [SDR ABXA070283](https://openairdocs.org/sdr/ABXA070283.md): Pan · cracked · Sep 11, 2007 · N964AX · Doug DC941 · Cargo/Baggage Doors
  > WHILE COMPLYING WITH NEA 52300001-001, FOUND INNER DOOR PAN CRACKED. REPAIRED PAN IAW DC9 SRM 52-05, FIGURE 26A.
- [SDR ABXA070282](https://openairdocs.org/sdr/ABXA070282.md): Pan · cracked · Sep 11, 2007 · N964AX · Doug DC941 · Cargo/Baggage Doors
  > DURING INSPECTION OF DOOR NEA 52300001-001, FOUND INNER DOOR PAN CRACKED. REPAIRED PAN IAW DC9 SRM 52-05, FIGURE 26A.
- [SDR ABXA070281](https://openairdocs.org/sdr/ABXA070281.md): Angle · cracked · Sep 8, 2007 · N964AX · Doug DC941 · Fuselage, Stabilizer Attach Fittings
  > DURING ROUTINE SERVICE BULLETIN INSPECTION OF LEFT DORSAL FIN ATTACH ANGLE, FOUND ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA060294](https://openairdocs.org/sdr/ABXA060294.md): Door Frame · cracked · Oct 31, 2006 · N964AX · Doug DC941 · Fuselage Main, Structure
  > LEFT AND RIGHT UPPER DOOR JAMBS ON AFT P-DOME WERE CRACKED. REPAIRED AREA IAW REA D953-54944.
- [SDR ABXA060243](https://openairdocs.org/sdr/ABXA060243.md): Battery · discharged · Aug 15, 2006 · N964AX · Doug DC941 · Emergency Lighting
  > FOUND EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001.
- [SDR ABXA060058](https://openairdocs.org/sdr/ABXA060058.md): Battery · discharged · Jan 23, 2006 · N964AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53. OPS CHECK GOOD.
- [SDR ABXA050357](https://openairdocs.org/sdr/ABXA050357.md): Coalescer Bag · unknown · Dec 13, 2005 · N964AX · Doug DC941 · Humidity Control System
  > EN ROUTE RIGHT AC PACK MAINTAINED 13 PSI, AC PRESSURIZATION CONTROLLER WENT TO STBY/LOCKOUT AT TOP OF DESCENT, CABIN PRESSURE CONTROLLER FAILED, PERFORMED EMERGENCY DESCENT. PERFORMED BITE CHECK ON BOTH CABIN PRESSURE CONTROLLERS. NO FAULTS FOUND. SWAPPED N
- [SDR ABXA050285](https://openairdocs.org/sdr/ABXA050285.md): Controller · defective · Nov 5, 2005 · N964AX · Doug DC941 · Cabin Pressure Control System
  > CABIN PRESSURIZATION LOSS AT TOP OF DESCENT. CABIN PRESSURE EMERGENCY LIGHT ILLUMINATED, EMERGENCY PROCEDURE COMPLETED. NO FURTHER INCIDENT. PERFORMED BITE TEST PROCEDURES AND THE FOWARD CABIN PRESSURE CONTROLLER FAILED TEST. REPLACED FORWARD CABIN PRESSU
- [SDR ABXA050243](https://openairdocs.org/sdr/ABXA050243.md): Fitting · leaking · Oct 7, 2005 · N964AX · Doug DC941 · Crew Oxygen System
  > AT FLIGHT LEVEL 350, NOTICED CREW 02 BOTTLE WAS LOSING PRESSURE. DESCENDED TO LOWER ALTITUDE (170). REMAINDER OF FLIGHT, PRESSURE REMAINED AT 1000 PSI. SERVICED CREW 02 BOTTLE TO 1800 (WAS 1000) PSI. FOUND LINE FROM BOTTLE TO VALVE FITTING ON BULKHEAD LEAK
- [SDR ABXA050208](https://openairdocs.org/sdr/ABXA050208.md): Duct · loose · Aug 31, 2005 · N964AX · Doug DC941 · Air Distribution System
  > AT FL 350 LOST CABIN PRESSURE. LT PACK WAS NOT PROVIDING PRESSURIZATION BUT WAS IN AUTO AND INDICATED 160 PSI. ONLY ABLE TO MAINTAIN FL 210 WITH RIGHT PAC AT 260 PSI. BOTH PAC TEMPS NORMAL. FOUND RIGHT ACM DISCHARGE DUCT LOOSE AND RESECURED. REMOVED AND REPLAC
- [SDR ABXA040391](https://openairdocs.org/sdr/ABXA040391.md): Shear Tie · cracked · Nov 30, 2004 · N964AX · Doug DC941 · Fuselage Main, Structure
  > UPPER END OF SHEAR TIE CRACKED AT LONGERON 14 RIGHT, AFT OF FRAME 1056. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5.
- [SDR ABXA030326](https://openairdocs.org/sdr/ABXA030326.md): Radome · out of tolerance · Aug 12, 2003 · N964AX · Doug DC941 · Weather Radar System
  > RADAR PAINTS STREAK OF GROUND RETURNS AT 60 DEGREES RIGHT OF NOSE ON COUNTER CLOCKWISE SWEEP. SOUNDS LIKE RADAR HITS DOME ON CLOCKWISE SWEEP. FOUND RADAR DRIVE PLATE BINDING AGAINST RADOME STATIC DISCHARGE STRIP PLASTIC NUT PLATES. REPLACED THE RADOME ASSEMBLY
- [SDR ABXA030183](https://openairdocs.org/sdr/ABXA030183.md): Attach Angle · cracked · May 14, 2003 · N964AX · Doug DC941 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED, LEFT SIDE OF VERTICAL AFT END. REPAIRED ANGLE IAW DC-9 SRM 53-05.
- [SDR ABXA030083](https://openairdocs.org/sdr/ABXA030083.md): Sensor · failed · Feb 25, 2003 · N964AX · Doug DC941 · Landing Gear Position and Warning
  > AFTER LANDING GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ON. AFTER CYCLING GEAR, THE LIGHT REMAINED ON FOR ONE MINUTE, THEN WENT OUT. REMOVED AND REPLACED THE NOSE LANDING GEAR LOCK SENSOR IAW DC-9 MM 32-60-01-2.
- [SDR ABXA020059](https://openairdocs.org/sdr/ABXA020059.md): Fuel Control · malfunctioned · Jul 19, 2002 · N964AX · Doug DC941 · Fuel Controlling System
  > NR 1 ENGINE WOULD NOT DECELERATE FROM FULL POWER TO IDLE, WOULD NOT RESPOND AFTER THE THROTTLE WAS RETARDED. IN-FLIGHT SHUTDOWN AND DID AN AIR TURN BACK. REPLACED THE FUEL CONTROL AND MAIN FUEL PUMP IAW DC-9 MM 73-20-01-2.
- [SDR ABXA010567](https://openairdocs.org/sdr/ABXA010567.md): Packing · defective · Nov 1, 2001 · N964AX · Doug DC941 · Engine Oil Pressure
  > RIGHT ENGINE LOST OIL PRESSURE ON CLIMBOUT, FOR DURATION OF 9 MINUTES ENGINE WINDMILLED. OIL PRESSURE DECREASED AS OIL QUANTITY DECREASED. IN FLIGHT SHUT-DOWN. REPLACED THE MAIN OIL FILTER HOUSING CAP O-RING AND INSPECTED THE MAIN OIL FILTER, NO METAL FOUND, I
- [SDR ABXA010521](https://openairdocs.org/sdr/ABXA010521.md): Doubler · corroded · Sep 18, 2001 · N964AX · Doug DC941 · Fuselage Main, Plate/Skin
  > CORROSION SPOTS WERE NOTED BELOW FRAME AT FUSELAGE STATION 617L AND LONGERON 29L. MAINTENANCE REPLACED THE INTERNAL DOUBLER IAW DC-9 SRM 51-30-5 AND 51-30-1.
- [SDR ABXA000490](https://openairdocs.org/sdr/ABXA000490.md): Light · inoperative · Nov 6, 2000 · N964AX · Doug DC941 · Emergency Lighting
  > OVERHEAD EVACUATION LIGHTS INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED THE EVACUATION LIGHT BATTERY CONTACTS, IAW DC-9 MAINTENANCE MANUAL. OPERATIONAL CHECKED GOOD.
- [SDR ABXA000091](https://openairdocs.org/sdr/ABXA000091.md): Frame · corroded · Jan 28, 2000 · N964AX · Doug DC941 · Fuselage Main, Frame
  > FUSELAGE FRAME AT STA 1041 CORRODED BETWEN LONGERON 28 LEFT SIDE TO 28 RIGHT SIDE IN AFT BAG BIN. REPAIRED FRAME IAW DC9 SRM 53-03 FIGURE 2A.
- [SDR ABXA000087](https://openairdocs.org/sdr/ABXA000087.md): Pan · cracked · Jan 25, 2000 · N964AX · Doug DC941 · Emergency Exits
  > LEFT MAIN ENTRY DOOR PAN CRACKED AT TOP HINGE CUT OUT. FABRICATED DOOR REPAIR ANGLE IAW DC9 SRM 52-05 FIGURE 47. INSTALLED DOOR REPAIR ANGLE IAW DC9 SRM 51-30-5 AND 51-30-1 AND 52-05 FIGURE 4.
- [SDR ABXA000086](https://openairdocs.org/sdr/ABXA000086.md): Support · cracked · Jan 21, 2000 · N964AX · Doug DC941 · Wing Miscellaneous Structure
  > RIGHT WING INBOARD SPOILER OUTBOARD SPOILER SUPPORT CRACKED. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-1.
- [SDR ABXA000085](https://openairdocs.org/sdr/ABXA000085.md): Bracket · cracked · Jan 20, 2000 · N964AX · Doug DC941 · Wing Miscellaneous Structure
  > RIGHT WING OUTBOARD SPOILER OUTBOARD SUPPORT CRACKED. REPLACED OUTBOARD SPOILER SUPPORT BRACKET IAW 51-30-2 AND 51-30-5.
- [SDR ABXA000080](https://openairdocs.org/sdr/ABXA000080.md): Pan · cracked · Jan 2, 2000 · N964AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO DOOR INNER PAN CRACKED IN TWO AREAS JUST ABOVE BEAM NR 1 FORWARD SIDE OF DOOR. REPAIRED EXTERNAL CRACK IAW DC9 SRM 52-05 PAGE 110A. MATERIAL 2024-T3-.063. EDDY CURRENT INTERNAL MARKED AREA. NO CRACK FOUND.
- [SDR ABXA9801183](https://openairdocs.org/sdr/ABXA9801183.md): Battery Pack · discharged · Dec 14, 1998 · N964AX · Doug DC941 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPS CHECKED GOOD.
- [SDR ABXA9800639](https://openairdocs.org/sdr/ABXA9800639.md): Prox Control · malfunction · Jul 24, 1998 · N964AX · Doug DC941 · Landing Gear Position and Warning
  > AFTER LANDING GEAR RETRACTION, RIGH GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR, LIGHT REMAINED ON. REPLACED PROX CONTROL BOX, OPS CHECKED GOOD IAW DC9 MM 32-60-00.
- [SDR ABXA9800568](https://openairdocs.org/sdr/ABXA9800568.md): Floorbeam · cracked · Jun 20, 1998 · N964AX · Doug DC941 · Fuselage Main, Floor Beam
  > WHILE COMPLYING WITH C-INSPECTION, FOUND A FLOORBEAM AT FS 718 CRACKED AT RBL 48. REPLACED FLOORBEAM IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA9800569](https://openairdocs.org/sdr/ABXA9800569.md): Shear Tie · cracked · Jun 19, 1998 · N964AX · Doug DC941 · Nacelle/Pylon Structure
  > WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT ENGINE PYLON SHEAR-TIE CRACKED AT LONGERON 14 LEFT AND FS 1041. REPLACED SHEAR-TIE IAW DOUGLAS DC9 SRM CHAPTERS 53-12-3, 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA9800567](https://openairdocs.org/sdr/ABXA9800567.md): Longeron · cracked · Jun 19, 1998 · N964AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > WHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 LEFT CRACKED AT PYLON ATTACH BOLT AT FS 1041. REPAIRED LONGERON IAW DC9 SRM CHAPTER 53-02.
- [SDR ABXA9800566](https://openairdocs.org/sdr/ABXA9800566.md): Longeron · cracked · Jun 19, 1998 · N964AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > WHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 RIGHT CRACKED AT UPPER FASTENER HOLE ATTACHING IT TO BULKHEAD AT FS 1052. REPLACED LONGERON SECTION IAW DC9 SRM CHAPTER 53-02.
- [SDR ABXA9800565](https://openairdocs.org/sdr/ABXA9800565.md): Longeron · cracked · Jun 19, 1998 · N964AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > WHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 16 LEFT CRACKED AT PYLON UPPER ATTACH BOLT AT FS 1041. REPAIRED LONGERON IAW DC9 SRM CHAPTER 53-02.
- [SDR ABXA9800570](https://openairdocs.org/sdr/ABXA9800570.md): Spar Cap · corroded · Jun 18, 1998 · N964AX · Doug DC941 · Wing Spar
  > WHILE COMPLYING WITH C-INSPECTION, FOUND LEVEL 2 CORROSION ON THE LEFT WING REAR SPAR UPPER T-CAP AT STATION XRS 160. REPAIRED LEFT WING REAR SPAR UPPER CAP IAW ABX REA D957-23974 MR.
- [SDR ABXA9701326](https://openairdocs.org/sdr/ABXA9701326.md): Uplatch Assy · out of adjust · Jul 30, 1997 · N964AX · Doug DC941 · Landing Gear Position and Warning
  > RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTED. RECYCLED GEAR, LIGHT REMAINED ON. ADJUSTED DOOR UPLATCH ASSY AND ROLLER. OPS CHECKED GOOD IAW DC9 MM 32-31-4.
- [SDR ABXA9701157](https://openairdocs.org/sdr/ABXA9701157.md): Uplimit Switch · worn hardware · Jun 19, 1997 · N964AX · Doug DC941 · Landing Gear Position and Warning
  > RIGHT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKE OFF AND DURING FLIGHT. GEAR UPLATCH CHECKED GOOD. REPLACED WORN HARDWARE ON RIGHT MAIN LANDING GEAR UP-LIMIT SWITCH. PERFORMED ADJUSTMENT AND TEST IAW DC9 MM 32-60-00. OPS CHECKED GOOD.
- [SDR ABXA9701021](https://openairdocs.org/sdr/ABXA9701021.md): Skin · corroded · Dec 4, 1996 · N964AX · Doug DC941 · Trailing Edge Flaps
  > FOUND LEFT FLAP UPPER AND LOWER SKINS CORRODED. REPLACED SKINS (P/N 9957578-15, 995757-503) IAW DC9 SRM 51-30-1.
- [SDR ABXA9701022](https://openairdocs.org/sdr/ABXA9701022.md): Rib · cracked · Nov 18, 1996 · N964AX · Doug DC941 · Trailing Edge Flaps
  > FOUND RIGHT FLAP OUTBOARD HINGE INBOARD AND OUTBOARD RIBS CRACKED. REPLACED FITTINGS (P/N 9957600-7, 9957600-15) IAW DC9 SRM 51-30-2.
- [SDR ABXA9700701](https://openairdocs.org/sdr/ABXA9700701.md): Angle · cracked · Oct 29, 1996 · N964AX · Doug DC941 · Nacelle/Pylon Structure
  > DURING ACCEPTANCE INSPECTION FOUND THE LEFT ENGINE PYLON TO FUSELAGE ATTACH ANGLE CRACKED IN TWO PLACES. REPAIRED LEFT PYLON ATTACH ANGLE IAW ABX REA D954-16868-MR.
- [SDR ABXA9700696](https://openairdocs.org/sdr/ABXA9700696.md): Bulkhead Clip · cracked · Oct 29, 1996 · N964AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING ACCEPTANCE INSPECTION FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 16L. REMOVED AND REPLACED END CLIPS AT LONGERON 16L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.
- [SDR ABXA9700711](https://openairdocs.org/sdr/ABXA9700711.md): Spar Cap · corroded · Oct 22, 1996 · N964AX · Doug DC941 · Vertical Stabilizer, Spar/Rib
  > DURING ACCEPTANCE INSPECTION, FOUND THE VERTICAL STABILIZER REAR SPAR CAPS CORRODED AT STATIONS ZRS 4, 8 AND 10. REPAIRED VERTICAL STAB REAR SPAR CAPS IAW ABX REA D957-16873-MR.
- [SDR ABXA9700699](https://openairdocs.org/sdr/ABXA9700699.md): Angle · cracked · Oct 22, 1996 · N964AX · Doug DC941 · Nacelle/Pylon Structure
  > DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT ENGINE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED. REPLACED THE RT UPPER PYLON TO FUSELAGE ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-2 AND 51-30-5 AND REPAIRED ONE CRACK IAW ABX REA D954-16695-MR.
- [SDR ABXA9700712](https://openairdocs.org/sdr/ABXA9700712.md): Skin · eroded · Oct 18, 1996 · N964AX · Doug DC941 · Horizontal Stabilizer, Plate/Skin
  > DURING ACCEPTANCE INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE SKINS ERODED. REPAIRED LEFT HORIZONTAL STAB LEADING EDGE SKINS IAW ABX REA D955-16859-MR.
- [SDR ABXA9700700](https://openairdocs.org/sdr/ABXA9700700.md): Angle · cracked · Oct 17, 1996 · N964AX · Doug DC941 · Nacelle/Pylon Structure
  > DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT ENGINE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED AT FS 1095. REPAIRED THE RIGHT PYLON UPPER ATTACH ANGLE IAW ABX REA NR D954-16695-MR.
- [SDR ABXA9700695](https://openairdocs.org/sdr/ABXA9700695.md): Bulkhead Clip · cracked · Oct 16, 1996 · N964AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 15L. REPLACED END CLIP AT LONGERON 15L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.
- [SDR ABXA9700710](https://openairdocs.org/sdr/ABXA9700710.md): Keel Beam · corroded · Oct 15, 1996 · N964AX · Doug DC941 · Fuselage Main, Keel
  > DURING ACCEPTANCE INSPECTION, FOUND THE BUTT LINE O KEEL BEAM UPPER CAP SEVERELY CORRODED AT FS 660. REPAIRED KEEL BEAM UPPER CAP IAW ABX REA D953-16673-MR.
- [SDR ABXA9700713](https://openairdocs.org/sdr/ABXA9700713.md): Rib · cracked · Oct 14, 1996 · N964AX · Doug DC941 · Wing, Rib/Bulkhead
  > DURING ACCEPTANCE INSPECTION, FOUND THE OUTBOARD LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 10 CRACKED. REMOVED AND REPLACED LEADING EDGE RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9700702](https://openairdocs.org/sdr/ABXA9700702.md): Panel · corroded · Oct 14, 1996 · N964AX · Doug DC941 · Wing, Plate/Skin
  > DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING LOWER TRAILING EDGE BONDED PANEL JUST INBOARD OF MLG CORRODED. REPLACED RIGHT WING LOWER INBOARD TRAILING EDGE PANEL IAW DC9 SRM 51-30-1.
- [SDR ABXA9700705](https://openairdocs.org/sdr/ABXA9700705.md): Jamb · cracked · Oct 11, 1996 · N964AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT MLG WHEEL WELL DOOR JAMB CRACKED INBOARD OF HYDRAULIC SUMP JAR. REPAIRED RIGHT MLG DOOR JAMB IAW ABX REA D953-16723.
- [SDR ABXA9700704](https://openairdocs.org/sdr/ABXA9700704.md): Panel · delaminated · Oct 10, 1996 · N964AX · Doug DC941 · Wing, Plate/Skin
  > DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING OUTBOARD TRAILING EDGE PANEL FORWARD OF AILERON DELAMINATED AND CORRODED. REPLACED RIGHT WING OUTBOARD TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.
- [SDR ABXA9700703](https://openairdocs.org/sdr/ABXA9700703.md): Panel · delaminated · Oct 10, 1996 · N964AX · Doug DC941 · Wing, Plate/Skin
  > WHILE COMPLYING WITH ACCEPTANCE INSPECTION, FOUND THE RIGHT WING UPPER TRAILING EDGE BONDED PANEL FORWARD OF AILERON DELAMINATED AND CORRODED. REMOVED AND REPLACED RIGHT WING TRAILING EDGE PANEL IAW DC-9 CHAPTERS 51-30-1 AND 51-30-2.
- [SDR ABXA9700884](https://openairdocs.org/sdr/ABXA9700884.md): Spoiler · corroded · Oct 9, 1996 · N964AX · Doug DC941 · Spoilers
  > THE RIGHT WING OUTBOARD SPOILER HAD SEVERAL AREAS OF CORROSION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.
- [SDR ABXA9700709](https://openairdocs.org/sdr/ABXA9700709.md): Spar Car · corroded · Oct 9, 1996 · N964AX · Doug DC941 · Wing Spar
  > DURING ACCEPTANCE INSPECTION, FOUND THE LEFT WING REAR TEE CAP DOUBLER CORRODED. REPAIRED LEFT WING REAR SPAR CAP IAW ABX REA D957-16504-MR.

Next page: https://openairdocs.org/deregistered/N964AX-2010-01-04/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 = 'N964AX' AND deregistration_id = 'N964AX-2010-01-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N964AX-2010-01-04/reports

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