# Service difficulty reports: N947AX, cancelled Dec 3, 2009

A list on [N947AX, cancelled Dec 3, 2009](https://openairdocs.org/deregistered/N947AX-2009-12-03.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 ABXA070287](https://openairdocs.org/sdr/ABXA070287.md): Bracket · cracked · Aug 13, 2007 · N947AX · Doug DC931 · Spoilers
  > LEFT WING TRAILING EDGE OUTBOARD SPOILERS INBOARD TORSION BAR BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW DC9 SRM 51-30-1 AND 51-30-2.
- [SDR ABXA070089](https://openairdocs.org/sdr/ABXA070089.md): Downlock Switch · malfunctioned · Apr 4, 2007 · N947AX · Doug DC931 · Landing Gear Position and Warning
  > ON 1ST GEAR EXTENSION, GOT GEAR ABNORMAL INDICATION. NO RIGHT MAIN GEAR GREEN LIGHT (ALSO NO UNSAFE LIGHT). ON 2ND GEAR EXTENSION, ALL GEAR INDICATION WAS NORMAL. REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH (INTERMITTENT) IAW DC9 MM 32-60-01-2-0101.
- [SDR ABXA060077](https://openairdocs.org/sdr/ABXA060077.md): Actuator · broken · Jan 20, 2006 · N947AX · Doug DC931 · Leading Edge Slat Actuator
  > DURING MAINTENANCE INSPECTION AT RDU, ON RIGHT WING, FOUND SLAT ACTUATOR ASSEMBLY BROKEN. REMOVED AND REPLACED SLAT ACTUATOR CYLINDER ASSEMBLY IAW DC9 MM. OPS CHECKED GOOD. WORK ACCOMPLISHED ON WO 600240033.
- [SDR ABXA060038](https://openairdocs.org/sdr/ABXA060038.md): Fitting · cracked · Jan 13, 2006 · N947AX · Doug DC931 · Fuselage Main, Attach Fittings
  > LEFT WHEEL WELL (KEEL AREA) LONGERON ATTACH END FITTING AT STA 750, LEFT BUTT LINE 8 (BELOW HYD RESERVOIR) HAD A 6 - 8 INCH CRACK ON VERTICAL LEG. REMOVED AND REPLACED ATTACH END FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA050317](https://openairdocs.org/sdr/ABXA050317.md): Indication Sys · malfunctioned · Dec 1, 2005 · N947AX · Doug DC931 · Landing Gear Position and Warning
  > ON FINAL APPROACH, GEAR DOOR OPEN LIGHT REMAINED ON WITH 3 GREEN INDICATIONS. WENT AROUND ON APPROACH, RECYCLED GEAR, GEAR DOOR OPEN LIGHT EXTINGUISHED. JACKED AIRCRAFT, CYCLED LANDING GEAR SEVERAL TIMES, NO DEFECTS NOTED. OPS CHECKED GOOD, REF AMM 32-60
- [SDR ABXA050149](https://openairdocs.org/sdr/ABXA050149.md): Bulkhead · cracked · Jun 1, 2005 · N947AX · Doug DC931 · Fuselage Main, Bulkhead
  > LEFT BULKHEAD SPAR STUB (HORIZONTAL WEB) AT FS 1039 APPROX LONGERON 15 LEFT CRACKED ON BOTTOM COMING FROM INBOARD FORWARD BOLT HOLE. STOP DRILLED/REPAIRED IAW DC-9 SRM 53-01.
- [SDR ABXA050153](https://openairdocs.org/sdr/ABXA050153.md): Pan · cracked · May 31, 2005 · N947AX · Doug DC931 · Fuselage Miscellaneous Structure
  > PASSENGER ENTRY DOOR PAN CRACKED IN 3 LOCATIONS ON FORWARD SIDE, 2 EACH 5 INCH CRACKS, 1 EACH 2 INCH CRACK. REMOVED AND REPLACED MAIN ENTRY DOOR IAW DC-9 MM 52-11-00-5-001.
- [SDR ABXA050150](https://openairdocs.org/sdr/ABXA050150.md): Pan · cracked · May 31, 2005 · N947AX · Doug DC931 · Passenger/Crew Doors
  > PASSENGER ENTRY DOOR PAN CRACKED IN 3 LOCATIONS ON FORWARD SIDE. REMOVED AND REPLACED MAIN ENTRY DOOR IAW DC-9 MM 52-11-00-5-001. WORK ACCOMPLISHED ON NON ROUTINE 0311. (2 EACH - 5 INCH CRACKS, 1 EACH - 2 INCH CRACKS).
- [SDR ABXA050148](https://openairdocs.org/sdr/ABXA050148.md): Pan · cracked · May 31, 2005 · N947AX · Doug DC931 · Fuselage Miscellaneous Structure
  > PASSENGER ENTRY DOOR PAN CRACKED ABOVE UPPER DOOR HINGE MOUNT APPROX 3 INCHES EMANATING FROM PREVIOUS REPAIR. REPLACED DOOR ON NON ROUTINE 0311 AND IAW DC-9 MM.
- [SDR ABXA050147](https://openairdocs.org/sdr/ABXA050147.md): Floor Support · corroded · May 27, 2005 · N947AX · Doug DC931 · Fuselage Miscellaneous Structure
  > STA 218 FLOOR SUPPORT HAD INTERGRANULAR CORROSION ON LOWER SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-30-5.
- [SDR ABXA050146](https://openairdocs.org/sdr/ABXA050146.md): Door · cracked · May 27, 2005 · N947AX · Doug DC931 · Passenger/Crew Doors
  > LT MAIN ENTRY DOOR FORWARD UPPER CORNER APPEARED TO BE CRACKED. DOOR REPLACED ON NON ROUTINE 0311, IAW DC-9 MM.
- [SDR ABXA050038](https://openairdocs.org/sdr/ABXA050038.md): Warning System · malfunctioned · Mar 2, 2005 · N947AX · Doug DC931 · Landing Gear Position and Warning
  > GEAR DOOR OPEN LIGHT DID NOT GO OUT AFTER EXTENDING ON APPROACH TO ILN, WENT ON MISSED APPROACH. RECYCLED GEAR AND LIGHT WENT OUT. CYCLED GEAR DOORS SEVERAL TIMES, LIGHT OPS CHECKED GOOD IAW DC-9 MM 32-30-00.
- [SDR ABXA040156](https://openairdocs.org/sdr/ABXA040156.md): Proximity Switch · malfunctioned · Apr 29, 2004 · N947AX · Doug DC931 · Landing Gear Position and Warning
  > GO AROUND-MISSED APPROACH-GEAR RECYCLE. UPON PLACING MLG HANDLE IN THE DOWN POSITION FOR LANDING, MLG DOWN LIGHT FAILED TO ILLUMINATE. AFTER RUNNING ABNORMALS, DISCOVERED THE MLG WARNING CIRCUIT BREAKER WAS OUT. RESET CIRCUIT BREAKER AND EXTENDED MLG. AFTER SE
- [SDR ABXA030404](https://openairdocs.org/sdr/ABXA030404.md): Fitting · cracked · Oct 10, 2003 · N947AX · Doug DC931 · Fuselage Miscellaneous Structure
  > FITTING IN LEFT WHEEL WELL STA 699, LEFT BUTT LINE '10' CRACKED. REPLACED FITTING IAW DC-9 SRM.
- [SDR ABXA030403](https://openairdocs.org/sdr/ABXA030403.md): Skin · cracked · Oct 9, 2003 · N947AX · Doug DC931 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT MAIN ENTRY DOOR UPPER/AFT STOP. REPAIRED AREA IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA030402](https://openairdocs.org/sdr/ABXA030402.md): Web · cracked · Oct 9, 2003 · N947AX · Doug DC931 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED AT RIGHT BUTT LINE 54 BETWEEN FS 945 - 965. REPAIRED CRACK IAW DC-9 53-01.
- [SDR ABXA030400](https://openairdocs.org/sdr/ABXA030400.md): Door · cracked · Oct 8, 2003 · N947AX · Doug DC931 · Doors
  > AFT PRESSURE BULKHEAD DOOR CRACKED AT LOWER HINGE. REPLACED AREA NOTED IAW DC-9 SRM 52-05, 51-30-5 AND 51-30-1.
- [SDR ABXA030399](https://openairdocs.org/sdr/ABXA030399.md): Skin · cracked · Oct 8, 2003 · N947AX · Doug DC931 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAD 1.5 INCH TEAR/CRACK IN SKIN FORWARD ENTRANCE DOOR CUTOUT FORWARD SIDE BETWEEN STOP F4 AND F5. REPAIRED AREA IAW REA D953-48357MR.
- [SDR ABXA030401](https://openairdocs.org/sdr/ABXA030401.md): Channel · cracked · Oct 8, 2003 · N947AX · Doug DC931 · Passenger/Crew Doors
  > AFT PRESSURE BULKHEAD DOOR CRACKED AT UPPER HINGE. REPAIRED DOOR IAW DC-9 SRM 52-05.
- [SDR ABXA030398](https://openairdocs.org/sdr/ABXA030398.md): Intercostal · cracked · Oct 7, 2003 · N947AX · Doug DC931 · Emergency Exits
  > LEFT AFT OVERWING DOOR HAD CRACKED INTERCOSTAL AT LATCH HANDLE. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA030397](https://openairdocs.org/sdr/ABXA030397.md): Pan · cracked · Oct 7, 2003 · N947AX · Doug DC931 · Emergency Exits
  > LEFT AFT OVERWING DOOR HAD CRACKED DOOR PAN AT STOP NR 6. REPAIRED AREA IAW DC-9 SRM 52-05.
- [SDR ABXA030396](https://openairdocs.org/sdr/ABXA030396.md): Spar Cap · cracked · Oct 6, 2003 · N947AX · Doug DC931 · Wing Spar
  > CRACK ON UPPER SPAR CAP REAR SPAR XCW '0' TO XCW '10' RIGHT. REPAIRED AREA IAW DC-9 SRM.
- [SDR ABXA030135](https://openairdocs.org/sdr/ABXA030135.md): Window · misaligned · Apr 16, 2003 · N947AX · Doug DC931 · Flight Compartment Windows
  > FIRST OFFICER'S WINDOW WOULD NOT OPEN. FOUND SCREW IN UPPER FORWARD CORNER OF FIRST OFFICER'S WINDOW TO BE TO LONG AND MIS-ALIGNED WINDOW TRACK. REPLACED WITH SHORTER SCREW. WINDOW OPS CHECKED GOOD IAW DC-9 MM 56.
- [SDR ABXA030134](https://openairdocs.org/sdr/ABXA030134.md): Lock · sticking · Apr 15, 2003 · N947AX · Doug DC931 · Flight Compartment Windows
  > FIRST OFFICER'S CLEAR VIEW WINDOW WOULD NOT OPEN. FOUND UPPER WINDOW LOCK STICKING. CLEANED AND LUBRICATED LOCK. OPS CHECKED GOOD IAW DC-9 MM 56.
- [SDR ABXA030108](https://openairdocs.org/sdr/ABXA030108.md): Pushrod · disconnected · Mar 10, 2003 · N947AX · Doug DC931 · Landing Gear Retraction/Extension System
  > AFTER TAKE-OFF, UNABLE TO RAISE GEAR HANDLE. RAN CHECK LIST AND DETERMINED THAT AIRCRAFT FAILED TO GO INTO FLIGHT MODE (GROUND SHIFT IN GROUND MODE) - PULLED CIRCUIT BREAKERS AND DETERMINED THAT THE GROUND SHIFT WAS BAD. FOUND GROUND SHIFT MECHANISM PUSHROD DI
- [SDR ABXA010723](https://openairdocs.org/sdr/ABXA010723.md): Web · cracked · Jan 30, 2002 · N947AX · Doug DC931 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED BETWEEN FS 945 - 965, LONGERON 18 LEFT. REPAIRED AREA, DOUBLER INSTALLED ON CUSP WEB IAW DC-9 SRM 53-01.
- [SDR ABXA010722](https://openairdocs.org/sdr/ABXA010722.md): Skin · cracked · Jan 25, 2002 · N947AX · Doug DC931 · Fuselage Main, Plate/Skin
  > CRACK INDICATION IN SKIN BETWEEN 2 FASTENERS, BETWEEN LONGERON 5 RIGHT AND LONGERON 6 RIGHT AT FS 996. INSTALLED PERMANENT REPAIR IAW DC-9 EA 53110005.
- [SDR ABXA010443](https://openairdocs.org/sdr/ABXA010443.md): Battery Pack · discharged · Aug 10, 2001 · N947AX · Doug DC931 · Emergency Lighting
  > EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACK POWER SUPPLY IAW DC-9 MM. OPS CHECKED GOOD.
- [SDR ABXA010064](https://openairdocs.org/sdr/ABXA010064.md): Link · worn · Feb 24, 2001 · N947AX · Doug DC931 · Landing Gear Door Retract Section
  > THE MAIN LANDING GEAR FAILED GEAR UPLATCH CHECKS AFTER TAKEOFF. THE FLIGHT CREW COMPLIED WITH ABNORMAL CHECKLIST. MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN LANDING GEAR DOOR, LATCH TO DOOR JAMB LINK ASSY IAW DC-9 MM 32-31-04. MAINTENANCE INSPECTED AN
- [SDR ABXA000294](https://openairdocs.org/sdr/ABXA000294.md): Power Supply · defective · Jun 8, 2000 · N947AX · Doug DC931 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS REMAINED ON AFTER POWER WAS REMOVED AND THE SWITCH WAS OFF. REPLACED EMERGENCY LIGHT POWER SUPPLY.
- [SDR ABXA000286](https://openairdocs.org/sdr/ABXA000286.md): Angle · cracked · May 26, 2000 · N947AX · Doug DC931 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND THE LEFT FLAP OUTBOARD HINGE ATTACH ANGLE CRACKED. REPLACED ANGLEIAW DC9 SRM 51-30-2.
- [SDR ABXA000285](https://openairdocs.org/sdr/ABXA000285.md): Angle · cracked · May 26, 2000 · N947AX · Doug DC931 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA000284](https://openairdocs.org/sdr/ABXA000284.md): Fitting · corroded · May 26, 2000 · N947AX · Doug DC931 · Horizontal Stabilizer, Attach Fittings
  > DURING C-CHECK, FOUND HORIZONTAL CENTER SECTION HINGE BORE CORRODED. REPAIRED IAW ABX REA D955-37167MR.
- [SDR ABXA000282](https://openairdocs.org/sdr/ABXA000282.md): Hinge Fitting · corroded · May 26, 2000 · N947AX · Doug DC931 · Horizontal Stabilizer, Attach Fittings
  > DURING C-CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION HINGE BORE CORRODED. REPAIRED IAW ABX REA D955-37167MR.
- [SDR ABXA000281](https://openairdocs.org/sdr/ABXA000281.md): Angle · cracked · May 26, 2000 · N947AX · Doug DC931 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE, OUTBOARD SUPPORT ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1.
- [SDR ABXA000280](https://openairdocs.org/sdr/ABXA000280.md): Skin · cracked · May 26, 2000 · N947AX · Doug DC931 · Vertical Stabilizer, Plate/Skin
  > DURING C-CHECK, FOUND THE VERTICAL STABILIZER SKIN CRACKED UNDER PANEL NR 3804. REPLACED SKIN IAW DC9 SRM 51-30-1.
- [SDR ABXA000279](https://openairdocs.org/sdr/ABXA000279.md): Skin · cracked · May 26, 2000 · N947AX · Doug DC931 · Vertical Stabilizer, Plate/Skin
  > DURING C-CHECK, FOUND VERTICAL STABILIZER SKIN CRACKED AT PANEL NR 3703. REPLACED SKIN IAW DC9 SRM 51-30-1.
- [SDR ABXA000278](https://openairdocs.org/sdr/ABXA000278.md): Bulkhead · cracked · May 23, 2000 · N947AX · Doug DC931 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND SUPPORT ANGLE AFT SIDE OF STATION 37 BULKHEAD CRACKED IN 2 PLACES. REPLACED ANGLE IAW DC9 SRM 51-30-2.
- [SDR ABXA000277](https://openairdocs.org/sdr/ABXA000277.md): Angle · cracked · May 23, 2000 · N947AX · Doug DC931 · Trailing Edge Flaps
  > DURING C-CHECK, FOUND THE OUTBOARD FLAP HINGE AFT FITTING, INBOARD ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1.
- [SDR ABXA000276](https://openairdocs.org/sdr/ABXA000276.md): Attach Fitting · corroded · May 23, 2000 · N947AX · Doug DC931 · Horizontal Stabilizer, Attach Fittings
  > DURING C-CHECK, FOUND THE HORIZONTAL STABILIZER CENTER SECTION CENTER HINGE BOLT FITTING CORRODED INSIDE THE LEFT HINGE BOLT HOLE. REPLACED FITTING IAW DC9 SRM 51-30-1.
- [SDR ABXA9900857](https://openairdocs.org/sdr/ABXA9900857.md): Seat · worn · Dec 21, 1999 · N947AX · Doug DC931 · Flight Compartment Equipment
  > CAPTAIN'S SEAT VERTICAL MOVEMENT ADJUSTMENT RELEASES INADVERTENTLY. SEAT SLIDES TO FLOOR WITHOUT ACTUATION. REPLACED CAPTAIN'S SEAT.
- [SDR ABXA9900609](https://openairdocs.org/sdr/ABXA9900609.md): Seat · lack of lube · Jul 27, 1999 · N947AX · Doug DC931 · Flight Compartment Equipment
  > CAPTAIN'S SEAT MOVED AFT AND DOWN, UNCOMMANDED, ON TAKEOFF. LUBRICATED SEAT ADJUSTMENT MECHANISM AND CHECKED LOCKING PIN ENGAGEMENT. NO DEFECTS NOTED.
- [SDR ABXA9900014](https://openairdocs.org/sdr/ABXA9900014.md): Frame · cracked · Jan 7, 1999 · N947AX · Doug DC931 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND CRACK IN FUSELAGE FRAME AT STATION 980, LONGERON 16 LEFT. REPLACED FRAME SECTION IAW DC9 SRM 53-03.
- [SDR ABXA9900013](https://openairdocs.org/sdr/ABXA9900013.md): Longeron · cracked · Jan 7, 1999 · N947AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND CRACK IN LONGERON 16 RIGHT AT STATION 965. REPLACED SECTION OF LONGERON IAW DC9 SRM 53-02.
- [SDR ABXA00012](https://openairdocs.org/sdr/ABXA00012.md): Frame · corroded · Jan 7, 1999 · N947AX · Doug DC931 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND FRAME AT STATION 484, LONGERON 29 LEFT AND 29 RIGHT. REPLACED SECTION OF FRAME IAW DC9 SRM 53-03.
- [SDR ABXA9801159](https://openairdocs.org/sdr/ABXA9801159.md): Switch · malfunction · Dec 3, 1998 · N947AX · Doug DC931 · Landing Gear Position and Warning
  > GEAR UPLATCH CHECK NOT SATISFACTORY, THE LEFT MAIN GEAR INDICATION REMAINED GREEN. RECYCLED GEAR DOWN, ALL 3 GEAR HAD NO UNSAFE LIGHT. RAISED GEAR, LEFT GEAR GREEN LIGHT STAYED ON, NO GEAR DOOR OPEN LIGHT. REPLACED LEFT MAIN GEAR DOWNLOCK SWITCH, OPS CHECKE
- [SDR ABXA9800062](https://openairdocs.org/sdr/ABXA9800062.md): Battery · discharged · Feb 7, 1998 · N947AX · Doug DC931 · Emergency Lighting
  > EMERGENCY LIGHTS ILLUMINATED WITH POWER OFF AND LIGHT SWITCH IN THE OFF POSITION. REPLACED EMERGENCY LIGHT BATTERY PACK.
- [SDR ABXA9701774](https://openairdocs.org/sdr/ABXA9701774.md): Battery · discharged · Nov 4, 1997 · N947AX · Doug DC931 · Emergency Lighting
  > DURING SERVICE CHECK, WHEN ALL POWER WAS REMOVED FROM AIRCRAFT, EMERGENCY LIGHTS STAYED ON. REPLACED EMERGENCY LIGHT BATTERIES.
- [SDR ABXA9700526](https://openairdocs.org/sdr/ABXA9700526.md): Door · cracked · Mar 11, 1997 · N947AX · Doug DC931 · Cargo/Baggage Doors
  > DURING C-CHECK, THE FORWARD LOWER CARGO DOOR SKIN AND PAN WAS FOUND CRACKED. THE DOOR WAS REPLACED IAW DC9 MAINTANCE MANUAL 52-31-0.
- [SDR ABXA9700514](https://openairdocs.org/sdr/ABXA9700514.md): Skin · corroded · Mar 10, 1997 · N947AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, THE CENTER FUSELAGE SKIN UNDER THE NR 1 ADF LOOP ANTENNA WAS FOUND CORRODED. THE SKIN WAS REPAIRED IAW DC9 REA D953-18649-SB.

Next page: https://openairdocs.org/deregistered/N947AX-2009-12-03/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 = 'N947AX' AND deregistration_id = 'N947AX-2009-12-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N947AX-2009-12-03/reports

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