# Service difficulty reports: N905AX, cancelled Apr 27, 2012

A list on [N905AX, cancelled Apr 27, 2012](https://openairdocs.org/deregistered/N905AX-2012-04-27.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 · 91 reports

- [SDR ABXA070424](https://openairdocs.org/sdr/ABXA070424.md): Battery · discharged · Dec 8, 2007 · N905AX · Doug DC932F · Emergency Lighting
  > CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.
- [SDR ABXA070154](https://openairdocs.org/sdr/ABXA070154.md): Bulkhead · cracked · Apr 23, 2007 · N905AX · Doug DC932F · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD SKIN CRACKED AT 4:00 POSITION ADJACANT TO DOOR PIN ALIGNMENT RECEPTACLE. REPAIRED CRACK IN SKIN IAW DWG 5934886-502 AND REA D953-55733.
- [SDR ABXA070155](https://openairdocs.org/sdr/ABXA070155.md): Cusp Web · cracked · Apr 23, 2007 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED AT STA 598 TO 617 AT BUTT LINE 58 LEFT. REPAIRED AREA OF WEB IAW DC9 SRM 53-01.
- [SDR ABXA070153](https://openairdocs.org/sdr/ABXA070153.md): Skin · cracked · Apr 20, 2007 · N905AX · Doug DC932F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED 2 PLACES FS 1087 LONGERON 3 - LONGERON 4 RIGHT. REPAIRED FUSELAGE SKIN AT STA 1095, LONGERON 3 - 4 RIGHT IAW DC9 SRM 53-04.
- [SDR ABXA070041](https://openairdocs.org/sdr/ABXA070041.md): Jackscrew · obstructed · Feb 9, 2007 · N905AX · Doug DC932F · Stabilizer Control System
  > HORIZONTAL STABILIZER JACKSCREW FOUND TO BE HITTING MECHANICAL STOPS DURING OPERATION. REMOVED AND REPLACED JACKSCREW IAW DC9 MM, REF WORK ORDER 600265725.
- [SDR ABXA060272](https://openairdocs.org/sdr/ABXA060272.md): Battery · discharged · Sep 23, 2006 · N905AX · Doug DC932F · Emergency Lighting
  > EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.
- [SDR ABXA050104](https://openairdocs.org/sdr/ABXA050104.md): Skin · corroded · Apr 18, 2005 · N905AX · Doug DC932F · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION EMITTING FROM FINGER DOUBLER JUST FORWARD OF FS 332 TO 351, LONGERON 26 RT OUTBOARD AND INBOARD SIDES. REPAIRED CORRODED SKIN IAW DC-9 SRM 53-04.
- [SDR ABXA050103](https://openairdocs.org/sdr/ABXA050103.md): Panel · cracked · Apr 15, 2005 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > RIGHT BUTT LINE '0' ANGLE FITTING COMMON TO KEEL WEB AND RIGHT SLANT PANEL CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-5.
- [SDR ABXA050101](https://openairdocs.org/sdr/ABXA050101.md): Skin · corroded · Apr 14, 2005 · N905AX · Doug DC932F · Fuselage Main, Plate/Skin
  > SKIN BULGING AND RIVET HEAD POPPED AT STA 949, LONGERON 24 LEFT. REPLACED LONGERON 24 LEFT, FS 927-996 IAW DC-9 SRM 51-30-2, 51-30-5 AND 53-02.
- [SDR ABXA050102](https://openairdocs.org/sdr/ABXA050102.md): Longeron · corroded · Apr 14, 2005 · N905AX · Doug DC932F · Fuselage Main, Longeron/Stringer
  > SKIN BULGING, RIVETS CUPPED AT STA 342, LONGERON 29 RIGHT AND LONGERON 28 RIGHT. REMOVED FASTENERS, EVALUATED. SPLICED LONGERON IAW DC-9 SRM.
- [SDR ABXA040403](https://openairdocs.org/sdr/ABXA040403.md): Relay · failed · Dec 26, 2004 · N905AX · Doug DC932F · Stabilizer Control System
  > DURING INITIAL CLIMB, PRIMARY TRIM C/B 0A TRIPPED, ALTERNATE TRIM WORKED FINE. ELECTED TO PULL PRIMARY TRIM C/B'S 0B AND 0C. CONTINUED FLIGHT USING AUTOPILOT. WHEN REMOVING CREW BAGS, NOTICED STRONG ELECTRICAL SMELL (BURNT ODOR) IN BELLY'S 1 AND 2. FOUND U
- [SDR ABXA040327](https://openairdocs.org/sdr/ABXA040327.md): Wire · broken · Sep 15, 2004 · N905AX · Doug DC932F · Ice/Rain Protection System Wiring
  > IN CLIMB, BOTH MASTER CAUTIONS ILLUMINATED, DIVERTED TO SGF. INSTALLED NEW LEFT THERMAL CONTROL AMPLIFIER, BITE TEST SHOWED PROBLEM IN SENSOR ON CIRCUIT. FOUND WIRES ON LEFT ICE PROTECT TEMP HIGH SENSOR BROKEN, SPLICED WIRES IAW DC-9 MM 20-50-1. OPS CHECKED
- [SDR ABXA040138](https://openairdocs.org/sdr/ABXA040138.md): Channel · damaged · Apr 3, 2004 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > FOUND BOLT PULLED OUT OF C-CHANNEL AT NR 11 9G NET ARM AT STA 207. DAMAGE WAS AT PREVIOUSLY REPAIRED AREA. REPAIRED DAMAGED AREA IAW REA D953-49568MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0.
- [SDR ABXA040171](https://openairdocs.org/sdr/ABXA040171.md): Support · failed · Apr 2, 2004 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > ON POST FLIGHT INSPECTION, MAINTENANCE DISCOVERED 1 9G NET SUPPORT PULLED FROM FUSELAGE MOUNT. REPAIRED DAMAGED AREA IAW REA D953-49569MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0.
- [SDR ABXA030360](https://openairdocs.org/sdr/ABXA030360.md): Structure · corroded · Aug 21, 2003 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > COCKPIT SUBFLOOR HAD AREAS OF LEVEL II CORROSION, STA 160 RPL 32 TO 54. REPAIRED AREA IAW DC-9 SRM.
- [SDR ABXA030359](https://openairdocs.org/sdr/ABXA030359.md): Pressure Panel · cracked · Aug 19, 2003 · N905AX · Doug DC932F · Fuselage Main, Bulkhead
  > PRESSURE PANEL LEFT WHEEL WELL AT FS 718 LEFT BUTT LINE 36 APPROXIMATELY, CRACKED. REPAIRED RPESSURE PANEL IAW REA D953-48107.
- [SDR ABXA030350](https://openairdocs.org/sdr/ABXA030350.md): Floor Support · cracked · Aug 18, 2003 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT STRUT END FITTING STA 313 CRACKED AT LONGERON 23 RIGHT. REPLACED FLOOR SUPPORT STRUT IAW DC-9 SRM.
- [SDR ABXA030357](https://openairdocs.org/sdr/ABXA030357.md): Skin · corroded · Aug 18, 2003 · N905AX · Doug DC932F · Fuselage Main, Plate/Skin
  > CORROSION BETWEEN LONGERON 26 RIGHT AND SKIN, BETWEEN STA 794 AND 813. REPAIRED AREA IAW DC-9 SRM 53-04.
- [SDR ABXA030356](https://openairdocs.org/sdr/ABXA030356.md): Floor Support · cracked · Aug 18, 2003 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT FITTING FS 434 LONGERON 18 LEFT CRACKED AT UPPER HORIZONTAL FLANGE BETWEEN FASTENERS AND HAD LEVEL I CORROSION ON AFT SIDE. REPLACED FITTING AND REPAIRED AREA IAW DC-9 SRM 51-10-3.
- [SDR ABXA030355](https://openairdocs.org/sdr/ABXA030355.md): Doubler · corroded · Aug 18, 2003 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > LEVEL II CORROSION BUTT LINE '0' F.S. 180 AT SHACKLE BOX. REPLACED SUBFLOOR DOUBLER WITH NEW FABRICATED DOUBLER AND INSTALLED IAW DC-9 SRM 53-01, 53-10-4, 53-10-3, 51-30-1, AND 51-30-2.
- [SDR ABXA030354](https://openairdocs.org/sdr/ABXA030354.md): Structure · corroded · Aug 18, 2003 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > LEVEL II CORROSION ON SUBFLOOR AT RIGHT BUTT LINE 44 F.S. 180 SHACKLE BOX. REPAIRED AREA IAW DC-9 SRM 53-01.
- [SDR ABXA030353](https://openairdocs.org/sdr/ABXA030353.md): Floor Support · cracked · Aug 18, 2003 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT STRUT TO FRAME ATTACH FITTING CRACKED STA. 237 BETWEEN LONGERON 24 LEFT AND 25 LEFT. REPLACED SUPPORT IAW DC-9 SRM.
- [SDR ABXA030352](https://openairdocs.org/sdr/ABXA030352.md): Floor Support · cracked · Aug 18, 2003 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT STRUT TO FRAME ATTACH BRACKET CRACKED AT STA. 275, BETWEEN LONGERON 24 LEFT AND 25 LEFT. REPLACED LEFT FLOOR SUPPORT STRAP TO FRAME ATTACH BRACKET IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA030351](https://openairdocs.org/sdr/ABXA030351.md): Fitting · cracked · Aug 18, 2003 · N905AX · Doug DC932F · Fuselage Main, Attach Fittings
  > LT FRAME 294 ENG. FITTING CRACKED AT CARGO FLOOR ATTACH POINT. REPLACED FITTING IAW DC-9 SRM 51-10-4, 51-30-5 AND 51-30-1.
- [SDR ABXA030358](https://openairdocs.org/sdr/ABXA030358.md): Skin · corroded · Aug 18, 2003 · N905AX · Doug DC932F · Fuselage Main, Plate/Skin
  > CORROSION BETWEEN LONGERON 26 LT AND SKIN BETWEEN STA. 775 AND 813. REPAIRED AREA IAW DC-9 SRM.
- [SDR ABXA030349](https://openairdocs.org/sdr/ABXA030349.md): Pressure Panel · corroded · Aug 15, 2003 · N905AX · Doug DC932F · Fuselage Main, Bulkhead
  > PRESSURE PANEL DOUBLER WAS BULGING LEFT BUTT LINE 8 TO LEFT BUTT LINE 16, FS 756. REPLACED LOWER T-ANGLE OF FLOORBEAM FS 756, BUTT LINE 56 RIGHT TO BUTT LINE 54 IAW DC-9 SRM 51-30-2, 51-30-5 AND REA D953-48132.
- [SDR ABXA030348](https://openairdocs.org/sdr/ABXA030348.md): Skin · corroded · Aug 15, 2003 · N905AX · Doug DC932F · Fuselage Main, Plate/Skin
  > BULGE IN FUSELAGE SKIN, CUPPED OR BROKEN FASTENERS, FS 332, LONGERON 30. REPLACED DAMAGED AREA IAW DC-9 SRM.
- [SDR ABXA030347](https://openairdocs.org/sdr/ABXA030347.md): Structure · corroded · Aug 14, 2003 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > LEFT WHEEL WELL STA 712, BUTT LINE 53 RETAINER CORRODED AND RIVETS POPPED. REPLACED RETAINER FROM FS 699 AND 756 LEFT BUTT LINE 30 TO LEFT BUTT LINE 56 IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA030346](https://openairdocs.org/sdr/ABXA030346.md): Structure · corroded · Aug 14, 2003 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > RIGHT WHEEL WELL UPPER AFT CORNER STA. 756, BUTT LINE '0' - BUTT LINE '4', CORROSION ON KEEL ANGLE AND BULGES UNDER RETAINER. REPAIRED AREA IAW REA D953-48136MR. REMOVED PREVIOUS REPAIR FROM AFT UPPER KEEL ANGLE, REPAIRED IAW DC-9 SRM 53-05.
- [SDR ABXA010779](https://openairdocs.org/sdr/ABXA010779.md): Spar · cracked · Mar 6, 2002 · N905AX · Doug DC932F · Wing Spar
  > LEFT WHEEL WELL, JUST OUTBOARD OF STATION ZERO, CENTER TANK ON REAR SPAR, UPPER INBOARD CORNER, HAD A CRACK. REPAIRED AREA IAW DC-9 SRM 51-30-5 AND 57-09.
- [SDR ABXA010778](https://openairdocs.org/sdr/ABXA010778.md): Support · cracked · Feb 27, 2002 · N905AX · Doug DC932F · Wing Structure
  > VERTICAL SUPPORT FOR SLAT MECHANISM MOUNT HAD A CRACK AT LOWER INBOARD MOUNT BOLT. REPLACED VERTICAL SUPORT IAW DC-9 SRM 51-30-5.
- [SDR ABXA000351](https://openairdocs.org/sdr/ABXA000351.md): Skin · corroded · Jul 18, 2000 · N905AX · Doug DC932F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BUBBLED AT LONGERON 30 BETWEEN STATION 445 AND 465. REPAIRED IAW DC9 SRM 53-04.
- [SDR ABXA000353](https://openairdocs.org/sdr/ABXA000353.md): Longeron · cracked · Jul 13, 2000 · N905AX · Doug DC932F · Fuselage Main, Longeron/Stringer
  > LONGERON 29 LEFT CRACKED BELOW SPLICE BETWEEN STATION 408 AND 427. REPLACED LONGERON SECTION.
- [SDR ABXA000352](https://openairdocs.org/sdr/ABXA000352.md): Longeron · cracked · Jul 13, 2000 · N905AX · Doug DC932F · Fuselage Main, Longeron/Stringer
  > LONGERON 30 CRACKED BELOW SPLICE BETWEEN STATION 408 AND 427. REPLACED LONGERON 30BETWEEN STATION 408 AND 427.
- [SDR ABXA000357](https://openairdocs.org/sdr/ABXA000357.md): Structure · cracked · Jul 8, 2000 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > CRACK ON PRESSURE DOME RADIAL NR 1. REPLACED RADIAL IAW DC9 SRM 51-30-2.
- [SDR ABXA000356](https://openairdocs.org/sdr/ABXA000356.md): Shear Tie · cracked · Jun 30, 2000 · N905AX · Doug DC932F · Fuselage Main, Structure
  > SHEAR TIE CRACKED AT STATION 945 BELOW LONGERON 14 LEFT. REPAIRED SHEAR TIE IAW DC9 SRM.
- [SDR ABXA000355](https://openairdocs.org/sdr/ABXA000355.md): Longeron · cracked · Jun 30, 2000 · N905AX · Doug DC932F · Fuselage Main, Longeron/Stringer
  > LONGERON 17 RIGHT CRACKED AT STATION 945. REPLACED LONGERON IAW DC9 SRM.
- [SDR ABXA000358](https://openairdocs.org/sdr/ABXA000358.md): Door · delaminated · Jun 28, 2000 · N905AX · Doug DC932F · Wing Miscellaneous Structure
  > LEFT BUTE DOOR NR 1502 WAS DELAMINATED. REPLACED BUTE DOOR.
- [SDR ABXA000350](https://openairdocs.org/sdr/ABXA000350.md): Panel · delaminated · Jun 28, 2000 · N905AX · Doug DC932F · Wing, Plate/Skin
  > RIGHT WING LOWER INBOARD BONDED PANEL HAS 4 INCH DELAMINATION. REPLACED PANEL IAW DC9 SRM51-30-2.
- [SDR ABXA9801188](https://openairdocs.org/sdr/ABXA9801188.md): Pan · corroded · Dec 21, 1998 · N905AX · Doug DC932F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND LEFT WHEEL WELL PRESSURE PANEL RETAINER PAN AT STATION 718 CORRODED. REPAIRED IAW ABX REA D953-25980MR.
- [SDR ABXA9801187](https://openairdocs.org/sdr/ABXA9801187.md): Keel Beam · cracked · Dec 20, 1998 · N905AX · Doug DC932F · Fuselage Main, Keel
  > DURING C-CHECK, FOUND KEEL BEAM CORRODED AND CRACKED IN THE RIGHT WHEEL WELL, AFT UPPER CORNER AT STATION 737. REPAIRED IAW ABX REA D953-25903MR.
- [SDR ABXA9800487](https://openairdocs.org/sdr/ABXA9800487.md): Battery · discharged · Jun 1, 1998 · N905AX · Doug DC932 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED POWER SUPPLY BATTERIES.
- [SDR ABXA9800289](https://openairdocs.org/sdr/ABXA9800289.md): Seat · lack of lube · Mar 31, 1998 · N905AX · Doug DC932 · Flight Compartment Equipment
  > FIRST OFFICER'S SEAT WAS DIFFICULT TO LOCK IN FULL FORWARD POSITION. SEAT SLID BACK ON INITIATION OF TAKEOFF ROLL. SEAT UNLOCKED ON FINAL APPROACH INTO ILN WITH FIRST OFFICER FLYING AIRCRAFT. LUBRICATED FIRST OFFICER'S SEAT LINKAGE. SEAT OPERATES NORMALLY.
- [SDR ABXA9700752](https://openairdocs.org/sdr/ABXA9700752.md): Fitting · cracked · Apr 14, 1997 · N905AX · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE FLOORBEAM SUPPORT STRUT FITTING AT STA 937 LONG 24 LT WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM.
- [SDR ABXA9700753](https://openairdocs.org/sdr/ABXA9700753.md): Vane · delaminated · Apr 12, 1997 · N905AX · Doug DC933F · Trailing Edge Flaps
  > DURING C-CHECK, THE INBOARD FIXED VANE WAS FOUND DELAMINATED. THE VANE WAS REPLACED IAW DC9 MM.
- [SDR ABXA9700754](https://openairdocs.org/sdr/ABXA9700754.md): Fitting · cracked · Apr 11, 1997 · N905AX · Doug DC933F · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE FITTING JUST BELOW THE PYLON BULKHEAD LBL 44 AT STA 965 WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM.
- [SDR ABXA9701184](https://openairdocs.org/sdr/ABXA9701184.md): Skin · delaminated · Apr 10, 1997 · N905AX · Doug DC932F · Spoilers
  > FOUND LEFT WING SPOILER UPPER AND LOWER SKIN DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.
- [SDR ABXA9701131](https://openairdocs.org/sdr/ABXA9701131.md): Skin · delaminated · Apr 10, 1997 · N905AX · Doug DC932F · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE OUTER SKIN 40 PERCENT DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.
- [SDR ABXA9700760](https://openairdocs.org/sdr/ABXA9700760.md): Hinge · corroded · Apr 9, 1997 · N905AX · Doug DC933F · Trailing Edge Flaps
  > DURING C-CHECK, THE CENTER FLAP FORWARD HINGE AND ATTACH STUDS WERE FOUND CORRODED. THE HINGE WAS REPLACED IAW DC9 MM.
- [SDR ABXA9700759](https://openairdocs.org/sdr/ABXA9700759.md): Hinge · corroded · Apr 9, 1997 · N905AX · Doug DC933F · Trailing Edge Flaps
  > DURING C-CHECK, THE INBOARD FLAP FORWARD HINGE AND ATTACH STUDS WERE FOUND CORRODED. THE HINGE WAS REPLACED IAW DC9 MM.

Next page: https://openairdocs.org/deregistered/N905AX-2012-04-27/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 = 'N905AX' AND deregistration_id = 'N905AX-2012-04-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N905AX-2012-04-27/reports

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