# Service difficulty reports: N900AX, cancelled Sep 24, 2013

A list on [N900AX, cancelled Sep 24, 2013](https://openairdocs.org/deregistered/N900AX-2013-09-24.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 3 · 117 reports

- [SDR ABXA200811070261](https://openairdocs.org/sdr/ABXA200811070261.md): Battery · discharged · Nov 4, 2008 · N900AX · Doug DC932 · Emergency Lighting
  > DURING PREDEPARTURE FOUND EMERGENCY LIGHTING SYSTEM INOP. DEFERRED: 62393 REMOVED AND REPLACED EMERGENCY BATTERIES IAW DC9 AMM 33-03-00-8; DEFERRED PER DC9 AMM 33-53-00-3 AND GMM 07.04 FOR TRACKING MBCB 3 FLYT DAYS. CODE 2 CLEARED DI 62393 REMOVED & REPLACE
- [SDR ABXA080233](https://openairdocs.org/sdr/ABXA080233.md): Vertical Gyro · defective · Aug 21, 2008 · N900AX · Doug DC932 · Attitude Gyro and Indicating System
  > A COUPLE OF MINUTES AFTER GYRO FLAG, THERE WAS A STRONG ELECTRICAL HOT SMELL IN THE COCKPIT. REPLACED NR 2 VERTICAL GYRO IAW DC9 MM 34-27-00-2. INSPECTED WIRING AND CANNON PLUGS. NO EVIDENCE OF OVERHEAT CONDITION. RAN V.G. FOR 2 MINUTES WITH NO EVIDENCE OF
- [SDR ABXA080119](https://openairdocs.org/sdr/ABXA080119.md): Transformer · defective · Apr 5, 2008 · N900AX · Doug DC932 · DC Rectifier/Converter
  > ELECTRICAL SMELL IN COCKPIT, WORSE WITH EMERGENCY POWER SELECTED ON. FOUND SMELL TO BE WORSE IN FORWARD ACCESSORY COMPARTMENT. NO SIGNS OF OVERHEATED OR BURNING EQUIPMENT WITH POWER ON. DETERMINED ODOR TO BE RESIDUAL FROM RIGHT TRANSFORMER RECTIFIER THAT WA
- [SDR ABXA070340](https://openairdocs.org/sdr/ABXA070340.md): Skin · corroded · Sep 27, 2007 · N900AX · Doug DC932 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CORRODED AT AFT LOWER CARGO DOOR STOP ADJUSTMENT SCREW MAT. REPAIRED AREA IAW DC9 SRM.
- [SDR ABXA070339](https://openairdocs.org/sdr/ABXA070339.md): Pan · cracked · Sep 24, 2007 · N900AX · Doug DC932 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR OUTER PAN CRACKED AT BARREL NUT HOLE AT FORWARD END OF BEAM NR 3. REPAIRED AREA IAW DC9 SRM 52-03, FIGURE 9.
- [SDR ABXA070337](https://openairdocs.org/sdr/ABXA070337.md): Structure · corroded · Sep 18, 2007 · N900AX · Doug DC932 · Fuselage Miscellaneous Structure
  > STA 200 LEFT BUTT LINE 50 CORRODED ON SUBFLOOR. REMOVED CORROSION AND REPAIRED IAW DC9 SRM 53-01.
- [SDR ABXA070338](https://openairdocs.org/sdr/ABXA070338.md): Bracket · cracked · Sep 18, 2007 · N900AX · Doug DC932 · Passenger/Crew Doors
  > AFT ENTRY DOOR LOWER LEFT LOCK MECHANISM BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW DC9 SRM.
- [SDR ABXA070336](https://openairdocs.org/sdr/ABXA070336.md): Seat Track · corroded · Sep 18, 2007 · N900AX · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT BUTT LINE 44 STA 220 TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK LEFT BUTT LINE 44, STA 160 - 230 IAW DC9 SRM 51-30-1.
- [SDR ABXA070335](https://openairdocs.org/sdr/ABXA070335.md): Seat Track · corroded · Sep 18, 2007 · N900AX · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT BUTT LINE 44 STA 170 TRACK CRACKED. REMOVED AND REPLACED SEAT TRACK LEFT BUTT LINE 44, STA 160 - 230 IAW DC9 SRM 51-30-1.
- [SDR ABXA070334](https://openairdocs.org/sdr/ABXA070334.md): Seat Track · corroded · Sep 18, 2007 · N900AX · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT BUTT LINE 44 STA 218 TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK STA 160 - 230, LEFT BUTT LINE 44 IAW DC9 SRM 51-30-1.
- [SDR ABXA070333](https://openairdocs.org/sdr/ABXA070333.md): Bulkhead · cracked · Sep 17, 2007 · N900AX · Doug DC932 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CUTOUT LOWER LEFT UNMODIFIED CORNER HAD CRACK OF UNKNOWN LENGTH IN LOWER INBOARD SKIN TAB PORTION OF SKIN. REPAIRED AFT PRESSURE BULKHEAD ON LEFT AND RIGHT LOWER CORNERS IAW DC9 SRM.
- [SDR ABXA070043](https://openairdocs.org/sdr/ABXA070043.md): Battery · discharged · Feb 2, 2007 · N900AX · Doug DC932 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00.
- [SDR ABXA070008](https://openairdocs.org/sdr/ABXA070008.md): Coalescer Bag · defective · Jan 12, 2007 · N900AX · Doug DC932 · Humidity Control System
  > PILOT REPORTED OIL ODOR FROM AIR CONDITIONING SYSTEM. REPLACED LEFT AND RIGHT WATER SEPARATOR BAGS IAW DC9 MM 21-20-02.
- [SDR ABXA060269](https://openairdocs.org/sdr/ABXA060269.md): Switch · obstructed · Sep 25, 2006 · N900AX · Doug DC932 · Landing Gear Position and Warning
  > NO NOSE GEAR INDICATION ON GEAR, RED OR GREEN. CREW EXCHANGED BULBS. NO INDICATION AND NO LIGHTS OR TEST. RECYCLED GEAR. NO INDICATION. COULD NOT SEE MARK ON VISUAL CHECK. MIRROR WAS DIRTY OR OUT OF ALIGNMENT. TRIED TO RECYCLE GEAR AGAIN AND RECEIVED TH
- [SDR ABXA060268](https://openairdocs.org/sdr/ABXA060268.md): Hose · blown · Sep 22, 2006 · N900AX · Doug DC932 · Air Distribution System
  > CLIMBING THROUGH 9000 MSL, TAIL COMP TEMP HIGH LIGHT CAME ON. AFTER COMPLETION OF EMERGENCY CHECKLIST, WAS UNABLE TO KEEP THE TEMP HIGH LIGHT OUT. AIR TURN BACK. FOUND GROUND AIR COND CHECK VALVE UPPER CONNECTOR DUCT BLOWN. REPLACED BLOWN CONNECTOR DUCTS. OPE
- [SDR ABXA060199](https://openairdocs.org/sdr/ABXA060199.md): Plug · unlocked · Jul 11, 2006 · N900AX · Doug DC932 · Landing Gear Position and Warning
  > ON APPROACH, NO GREEN NOSE GEAR LIGHT. PUT GEAR DOWN AGAIN AND LIGHT CAME ON AFTER RECYCLE.FOUND NOSE GEAR DOWN LOCK SWITCH DEUTSCH PLUG NOT IN THE LOCKED POSITION AND DIRTY FROM GREASE. CLEANED DEUTSCH PLUG AND RECONNECTED TO THE LOCKED POSITION.
- [SDR ABXA050221](https://openairdocs.org/sdr/ABXA050221.md): Spar Cap · cracked · Sep 2, 2005 · N900AX · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR TEE CAP MOST OUTBOARD END CRACKED. REPAIRED HORIZONTAL REAR SPAR CAP IAW DC-9 SRM 55-02.
- [SDR ABXA050220](https://openairdocs.org/sdr/ABXA050220.md): Frame · cracked · Sep 1, 2005 · N900AX · Doug DC932 · Fuselage Main, Frame
  > RIGHT FORWARD MAIN FRAME, STA 699, CRACKED AT POINTS G AND J, AFT FLANGE REQUIRED 5935650 REPAIR INSTALLED. REPAIRED MAIN FRAME AT FS 699 IAW EA 53400120-001-1.
- [SDR ABXA050219](https://openairdocs.org/sdr/ABXA050219.md): Frame · cracked · Sep 1, 2005 · N900AX · Doug DC932 · Fuselage Main, Frame
  > RIGHT MAIN FRAME STA 718 HAD CRACK IN S/B SECTION. CRACK HAD GROWN INTO ATTACHMENT HOLES FOR REPAIR. FRAME REQUIRED REPLACEMENT PER S/B 53-100. FRAME WAS REMOVED AND REPLACED ON EA 53400324-0021-2.
- [SDR ABXA050218](https://openairdocs.org/sdr/ABXA050218.md): Frame · cracked · Sep 1, 2005 · N900AX · Doug DC932 · Fuselage Main, Frame
  > PREVIOUSLY REPAIRED LEFT WHEEL WELL MAIN FRAME 718 HAD SEPARATION IN PREVIOUS CRACKS WITH CORROSION INSIDE CRACKS. ALSO HAD CORROSION AROUND MAIN FRAME BOTTOM BOLT IN FORWARD FLANGE. REMOVED AND REPLACED MAIN FRAME STA 718 LEFT ON JOB CARD EA 53400323-001-2.
- [SDR ABXA050152](https://openairdocs.org/sdr/ABXA050152.md): Outflow Valve · frozen · Jun 15, 2005 · N900AX · Doug DC932 · Pressure Regulator/Outflow Valve
  > AT 35,000 FEET, RED CABIN PRESS LIGHT ILLUMINATED AND OUTFLOW VALVE WAS FROZEN IN PLACE. ONCE DESCENDED TO FL 190, PRESSURIZATION WORKED OKAY IN MANUAL AND AUTO. OPS CHECKED CABIN PRESS SWITCH IAW DC-9 MM 21-30-00-0-0202. OPS NORMAL, NO DEFECTS NOTED. THIS
- [SDR ABXA040085](https://openairdocs.org/sdr/ABXA040085.md): Pump · inoperative · Feb 27, 2004 · N900AX · Doug DC932 · Hydraulic Pump (Electric/Engine), Main
  > LEFT ENGINE HYDRAULIC PUMP FAILED IN FLIGHT INTO BTV. REPLACED LEFT ENGINE HYDRAULIC PUMP ON LEFT ENGINE IAW DC-9 AMM 29-10-05-2-0001. OPS AND LEAK CHECKED GOOD. ALSO INSPECTED FLUID IN PUMP, ALL CLEAN, '0' CONTAMINANTS. REPLACED LEFT ENGINE CASE DRAIN FIL
- [SDR ABXA040061](https://openairdocs.org/sdr/ABXA040061.md): Connector · damaged · Feb 12, 2004 · N900AX · Doug DC932 · Landing Gear Position and Warning
  > ABORTED APPROACH AND CYCLED THE GEAR ON A GO-AROUND. WHEN GEAR WAS EXTENDED, RIGHT MAIN GEAR UNSAFE LIGHT DID NOT COME ON. RIGHT LANDING GEAR GREEN LIGHT DID NOT COME ON. PROX INDICATION WAS NORMAL. PROBLEM VERIFIED. FOUND NR 5 PIN ON RIGHT MAIN LANDING G
- [SDR ABXA040037](https://openairdocs.org/sdr/ABXA040037.md): Inverter · defective · Jan 19, 2004 · N900AX · Doug DC932 · AC Inverter
  > DURING PRE-FLIGHT, TURNED EMERGENCY POWER SWITCH ON AND AC EMERGENCY BUS OFF LIGHT CAME ON. REMOVED AND REPLACED EMERGENCY AC POWER INVERTER IAW DC-9 MM. OPS CHECKED GOOD.
- [SDR ABXA040033](https://openairdocs.org/sdr/ABXA040033.md): Warning Light · illuminated · Jan 15, 2004 · N900AX · Doug DC932 · AC Power Distribution System
  > DURING PREFLIGHT, EMERGENCY POWER CHECK, A/C EMERGENCY BUSS POWER OFF LIGHT ILLUMINATED. RESET EMERGENCY BUS BREAKER B1-185 IAW DC-9 WD MANUAL 24-23-00. SYSTEM OPS CHECKED GOOD.
- [SDR ABXA040003](https://openairdocs.org/sdr/ABXA040003.md): Odor · detected · Jan 11, 2004 · N900AX · Doug DC932 · Air Distribution System
  > APPROXIMATELY 5 MINUTES AFTER TAKEOFF, NOTICED PRESSURIZATION BUMPS ON CLIMBOUT FOLLOWED BY LIGHT SMOKE AND ODOR IN COCKPIT. RETURNED TO ILN. INSPECTED AFT ACCESSORY COMPARTMENT DUCT WORK AND FLUID LINES. FOUND NO VISIBLE DAMAGE OR FLUID LEAKS AND FOUND NO
- [SDR ABXA040018](https://openairdocs.org/sdr/ABXA040018.md): Frame · corroded · Dec 23, 2003 · N900AX · Doug DC932 · Fuselage Main, Frame
  > FUSELAGE FRAME HAD LEVEL 2 CORROSION AT LONGERON 30, STA 813. REPAIRED AREA IAW DC-9 SRM 53-03.
- [SDR ABXA040021](https://openairdocs.org/sdr/ABXA040021.md): Angle · cracked · Dec 23, 2003 · N900AX · Doug DC932 · Fuselage Miscellaneous Structure
  > SUBFLOOR AND ANGLE CRACKED AT BUTTLINE 0, STA 160. REPAIRED SUBFLOOR IAW DC-9 SRM 53-01.
- [SDR ABXA040017](https://openairdocs.org/sdr/ABXA040017.md): Beam · cracked · Dec 23, 2003 · N900AX · Doug DC932 · Service Doors
  > FORWARD RIGHT SERVICE DOOR HAD A CRACK ON UPPER HORIZONTAL BEAM FORWARD END. REPAIRED UPPER BEAM OF SERVICE DOOR IAW DC-9 SRM 52-05.
- [SDR ABXA040020](https://openairdocs.org/sdr/ABXA040020.md): Shear Tie · cracked · Dec 23, 2003 · N900AX · Doug DC932 · Fuselage Main, Structure
  > SHEAR TIE CRACKED AT FS 947 BETWEEN LONGERON 15 AND 16 RT. REMOVED AND REPLACED SHEARTIE IAW DC-9 SRM.
- [SDR ABXA040019](https://openairdocs.org/sdr/ABXA040019.md): Shear Tie · cracked · Dec 23, 2003 · N900AX · Doug DC932 · Fuselage Main, Structure
  > SHEARTIE CRACKED AT FS 947, BETWEEN LONGERON 15 LT AND 16 LT. REMOVED AND REPLACED SHEAR TIE IAW SRM.
- [SDR ABXA040015](https://openairdocs.org/sdr/ABXA040015.md): Shear Tie · cracked · Dec 22, 2003 · N900AX · Doug DC932 · Fuselage Main, Structure
  > SHEAR TIE FS 622 WAS CRACKED, LONGERON 25 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA040016](https://openairdocs.org/sdr/ABXA040016.md): Keelbeam · cracked · Dec 22, 2003 · N900AX · Doug DC932 · Fuselage Main, Keel
  > KEELBEAM LONGERON 30 END CAP WAS CRACKED, LT SIDE FS 604. REPLACED KEELBEAM END CAP IAW DC-9 SRM.
- [SDR ABXA030132](https://openairdocs.org/sdr/ABXA030132.md): Switch · shorted · Apr 11, 2003 · N900AX · Doug DC932 · Windshield/Door Rain/Ice Removal
  > SAW SMOKE IN BEHIND CAPTAIN'S OVERHEAD MAP LIGHT AND SMELLED ELECTRICAL. DONNED OXYGEN AND JUMP SEATER CHECKED NO SMOKE/FIRE IN UPPER DECK. NO FIRE/SMOKE INDICATOR LIGHTS, ALL PANEL INDICATIONS NORMAL AND COULDN'T IDENTIFY SOURCE, SMOKE SUBSIDED, THEN LESS THA
- [SDR ABXA020367](https://openairdocs.org/sdr/ABXA020367.md): Duct · loose · Dec 19, 2002 · N900AX · Doug DC932 · Air Distribution System
  > DURING FINAL APPROACH, ODOR OF SYNTHETIC OIL IN THE COCKPIT. LT TEMP CONTROLLER IN MANUAL WITH LT DUCT TEMP PEAKED. TURNED IT OFF. ODOR WENT AWAY. ON THE GROUND, TURNED LT SUPPLY SWITCH BACK ON, WAS ABLE TO CONTROL TEMP MANUALLY. OPS CHECKED LT MANUAL TEMP CON
- [SDR ABXA020368](https://openairdocs.org/sdr/ABXA020368.md): Sensor · out of tolerance · Dec 17, 2002 · N900AX · Doug DC932 · Cabin Temperature Control System
  > COCKPIT TEMP VALVE IN AUTO WENT TO 80 PERCENT FULL HOT. LT DUCT TEMP PEGGED OUT HOT. SLIGHT SMOKE IN COCKPIT. MANUALLY DROVE VALVE FULL COLD. AC SMOKE CHECKLIST RUN. LT BLEED VALVE OFF FOR REST OF FLT. FOUND AUTO TEMP CONTROL TO COCKPIT TEMP SENSOR OUT OF TOL
- [SDR ABXA010887](https://openairdocs.org/sdr/ABXA010887.md): Light · loose · May 20, 2002 · N900AX · Doug DC932 · Landing Gear Position and Warning
  > WHEN LANDING GEAR EXTENDED, NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE RED INTRANSIT LIGHT WAS EXTINGUISHED ALONG WITH THE UNSAFE LIGHT. THE PROBLEM CORRECTED BY ITSELF. THE NOSE LANDING GEAR UNSAFE BULB WAS LOOSE IN THE SOCKET. REPLACED BULB AND PERFORMED A
- [SDR ABXA010885](https://openairdocs.org/sdr/ABXA010885.md): Panel · cracked · May 3, 2002 · N900AX · Doug DC932 · Flight Compartment Equipment
  > RIGHT EYEBROW PANEL FORWARD LOWER CORNER JAMB CRACKED. JAMB ON UPPER AFT CORNER OF CLEARVIEW. REPAIRED CRACKS IAW DACO, SERVICE REWORK DRAWING 5952965.
- [SDR ABXA010884](https://openairdocs.org/sdr/ABXA010884.md): Clip · cracked · Apr 23, 2002 · N900AX · Doug DC932 · Wing Structure
  > LEADING EDGE SPLICE ANGLE CRACKED JUST OUTBOARD OF #6 SLAT TRACK CUT-OUT. REPLACED SPLICE IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA010883](https://openairdocs.org/sdr/ABXA010883.md): Bracket · cracked · Apr 23, 2002 · N900AX · Doug DC932 · Drag Control System
  > LATERAL CONTROL MIXER, OUTBOARD SECTION, BRACKET CRACKED AT NUT PLATE ON THE BACK SIDE. REPLACED RIGHT LATERAL CONTROL MIXER IAW DC-9 MM 27-61-04-4-0007.
- [SDR ABXA010882](https://openairdocs.org/sdr/ABXA010882.md): Spar · cracked · Apr 22, 2002 · N900AX · Doug DC932 · Elevator, Spar/Rib
  > X-RAY OF RIGHT ELEVATOR FORWARD SPAR INDICATED A 2 INCH CRACK ON SPAR AT STA XET 90. REPAIRED CRACK AT STA XET 90 IAW DC-9 SRM 55-02.
- [SDR ABXA010881](https://openairdocs.org/sdr/ABXA010881.md): Trim Tab · delaminated · Apr 22, 2002 · N900AX · Doug DC932 · Rudder, Tab Structure
  > UPPER LEFT CORNER OF RUDDER TAB WAS DELAMINATED. REPLACED RUDDER TRIM TAB IAW DC-9 MM.
- [SDR ABXA010401](https://openairdocs.org/sdr/ABXA010401.md): Rod End · broken · Jul 17, 2001 · N900AX · Doug DC932 · Leading Edge Slat Actuator
  > RIGHT WING LEADING EDGE SLAT ACTUATOR ROD END BROKEN. REPLACED THE RIGHT WING LOWER SLAT ACTUATOR ROD END IAW DC-9 MM 27-80-05-2-10. OPS CHECKED GOOD.
- [SDR ABXA010384](https://openairdocs.org/sdr/ABXA010384.md): Switch · defective · Jul 12, 2001 · N900AX · Doug DC932 · Landing Gear Position and Warning
  > UPON GEAR RETRACTION, GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR WAS RECYCLED PER ABNORMALS AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED WITH THE GEAR EXTENDED ALSO. REPLACED THE RIGHT MAIN LANDING GEAR DOOR SWITCH IAW DC-9 MM 32-60
- [SDR ABXA000447](https://openairdocs.org/sdr/ABXA000447.md): Fitting · corroded · Sep 18, 2000 · N900AX · Doug DC932 · Fuselage Main, Attach Fittings
  > AFT ACCESSORY AUXILIARY LANDING GEAR SUPPORT FITTING HAD AREA OF EXFOLIATION ON FORWARD RIGHT SIDE. REPLACED AFT ACCESSORY AUXILIARY LANDING GEAR SUPPORT IAW DC9 MM.
- [SDR ABXA000449](https://openairdocs.org/sdr/ABXA000449.md): Fitting · corroded · Sep 17, 2000 · N900AX · Doug DC932 · Fuselage Main, Attach Fittings
  > AFT ACCESSORY AUXILIARY LANDING GEAR SUPPORT FITTING HAD AREA OF EXFOLIATION LEVEL 1 CORROSION ON FORWARD LEFT SIDE. REPLACED LEFT AUXILIARY LANDING GEAR SUPPORT IAW DC9 SRM 51-30-2 & 51-30-5.
- [SDR ABXA000446](https://openairdocs.org/sdr/ABXA000446.md): Floorbeam · corroded · Sep 13, 2000 · N900AX · Doug DC932 · Fuselage Main, Floor Beam
  > STATION 965 FLOORBEAM HAD CORROSION ON THE TOP FLANGE AT RIGHT BUTT LINE 30. REPAIRED FLOORBEAM IAW DC9 REA D953-38476.
- [SDR ABXA000450](https://openairdocs.org/sdr/ABXA000450.md): Floorbeam · corroded · Sep 13, 2000 · N900AX · Doug DC932 · Fuselage Main, Floor Beam
  > FLOORBEAM 965 UPPER CAP ANGLE HAD LEVEL 1 CORROSION AT RIGHT BUTT LINE 44.0. REPLACED ANGLE IAW DC9 SRM.
- [SDR ABXA000448](https://openairdocs.org/sdr/ABXA000448.md): Pan · cracked · Sep 11, 2000 · N900AX · Doug DC932 · Cargo/Baggage Doors
  > EDDY CURRENT INSPECTION INDICATED CRACK ON OUTER PAN AT FORWARD STOP AT NR 5 BEAM ON AFT LOWER CARGO DOOR S/N ABX 47380. REPLACED AFT LOWER CARGO DOOR IAW DC9 SRM 52-03.
- [SDR ABXA000445](https://openairdocs.org/sdr/ABXA000445.md): Fitting · cracked · Sep 8, 2000 · N900AX · Doug DC932 · Nacelle/Pylon, Attach Fittings
  > PYLON BULKHEAD SUPPORT UPPER FITTING WAS CRACKED AT FLOORBEAM 965, BUTT LINE 35 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Next page: https://openairdocs.org/deregistered/N900AX-2013-09-24/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 = 'N900AX' AND deregistration_id = 'N900AX-2013-09-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N900AX-2013-09-24/reports

---
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