# Service difficulty reports: N929AX, cancelled Jul 20, 2017

A list on [N929AX, cancelled Jul 20, 2017](https://openairdocs.org/deregistered/N929AX-2017-07-20.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 · 71 reports

- [SDR ABXA060308](https://openairdocs.org/sdr/ABXA060308.md): Floorbeam · corroded · Nov 14, 2006 · N929AX · Doug DC931 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA 446 APPROXIMATELY 12 INCHES INBOARD FROM RIGHT SIDE SKIN WAS CORRODED. REPAIRED AREA IAW REA D953-55057 MR.
- [SDR ABXA060307](https://openairdocs.org/sdr/ABXA060307.md): Finger Doubler · corroded · Nov 9, 2006 · N929AX · Doug DC931 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS BULGING AT FS 237, 294, AND 306 TO 332 LONGERON 18 RIGHT. REMOVED AND REPLACED FINGER DOUBLER FS 201 - 351 AT LONGERON 18 RIGHT IAW DC9 SRM.
- [SDR ABXA050290](https://openairdocs.org/sdr/ABXA050290.md): Battery Pack · discharged · Nov 25, 2005 · N929AX · Doug DC931 · Emergency Lighting
  > EMERGENCY EVACUATION LIGHTS WERE INOP. REPLACED BATTERY PACK IAW DC9 MM 3-53-02. OPS CHECKED GOOD.
- [SDR ABXA050158](https://openairdocs.org/sdr/ABXA050158.md): Relay · malfunctioned · Jun 23, 2005 · N929AX · Doug DC931 · Landing Gear Position and Warning
  > NOSE LANDING GEAR LIGHTS DID NOT ILLUMINATE. UNSAFE LIGHT WAS OUT. CYCLED GEAR WITH THE SAME RESULT. WIGGLED GEAR HANDLE AND NOSE LIGHT ILLUMINATED NORMAL. REMOVED AND REPLACED RELAY R2-28. SWUNG GEAR IAW DC-9 ADJ/TEST 32-60-00-2-0201. OPS CHECKED GOOD.
- [SDR ABXA050022](https://openairdocs.org/sdr/ABXA050022.md): Warning Switch · defective · Jan 22, 2005 · N929AX · Doug DC931 · Landing Gear Position and Warning
  > NOSE GEAR UNSAFE RED WARNING LIGHT ILLUMINATED DURING UPLATCH CHECK (APPROX 10,000 FT MSL), COMPLIED WITH ABNORMAL. RECYCLED LANDING GEAR AND GOT GOOD DOWN AND LOCK (GREEN INDICATORS) WHEN THE LANDING GEAR WAS RETRACTED, THE NOSE GEAR UNSAFE LIGHT CAME ON AGA
- [SDR ABXA050012](https://openairdocs.org/sdr/ABXA050012.md): Skin · cracked · Jan 5, 2005 · N929AX · Doug DC931 · Fuselage Main, Plate/Skin
  > RIGHT NOSE SKIN CRACKED AT 2 RIVETS AT FS 76.5 FORWARD OF FIRST OFFICER'S WINDSHIELD WIPER MOTOR. REPAIRED AREA IAW DC-9 JOB CARD EA 53100074-003-1.
- [SDR ABXA050014](https://openairdocs.org/sdr/ABXA050014.md): Fitting · cracked · Jan 5, 2005 · N929AX · Doug DC931 · Fuselage Main, Attach Fittings
  > FLOORBEAM SUPPORT UPPER END FITTING CRACKED AT BOTH BOLT HOLES FS 965 AT LEFT BUTTLINE 32. REMOVED AND REPLACED FLOORBEAM SUPPORT UPPER END FITTING IAW DC-9 SRM 51-30-1 AND DC-9 SRM 51-30-5.
- [SDR ABXA050013](https://openairdocs.org/sdr/ABXA050013.md): Skin · cracked · Jan 5, 2005 · N929AX · Doug DC931 · Fuselage Main, Plate/Skin
  > LEFT NOSE SKIN AT STA 69.5 FORWARD OF CAPTAIN'S WINDSHIELD WIPER MOTOR NEEDED STRIPPED AT AREA MARKED. REPAIRED AREA IAW DC-9 JOB CARD EA 53100075-003-2.
- [SDR ABXA050010](https://openairdocs.org/sdr/ABXA050010.md): Pan · cracked · Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR PAN CRACKED BETWEEN LATCH AND STOP FROM GOUGE. REPAIRED FORWARD LOWER CARGO DOOR PAN IAW DC-9 SRM 52-05.
- [SDR ABXA050011](https://openairdocs.org/sdr/ABXA050011.md): Support Fitting · cracked · Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR STOP SUPPORT FITTING CRACKED AFT OF FORWARD HINGE INSIDE LIGHTING HOLE. REMOVED AND REPLACED FITTING ON FORWARD LOWER CORNER DOOR AFT OF FORWARD HINGE IAW DC-9 SRM 51-30-5.
- [SDR ABXA050009](https://openairdocs.org/sdr/ABXA050009.md): Support Fitting · cracked · Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR SUPPORT FITTING CRACKED AT STOP BOLT HOLE. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.
- [SDR ABXA050008](https://openairdocs.org/sdr/ABXA050008.md): Pan · cracked · Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage Doors
  > TWO CRACKS EMINATING FROM HILOC HOLE AT AFT LOWER DOOR STOP ON FORWARD LOWER CARGO DOOR. REPAIRED AREA AND REMOVED AND REPLACED BRACKET IAW DC-9 SRM 52-03, 51-30-2, 51-20-5, AND 51-30-1.
- [SDR ABXA050007](https://openairdocs.org/sdr/ABXA050007.md): Pan · cracked · Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage Doors
  > TWO CRACKS EMINATING FROM HILOC HOLE AT UPPER FORWARD DOOR STOP ON FORWARD LOWER CARGO DOOR. REPAIRED AREA IAW DC-9 SRM 52-03.
- [SDR ABXA050006](https://openairdocs.org/sdr/ABXA050006.md): Fitting · corroded · Jan 4, 2005 · N929AX · Doug DC931 · Fuselage Main, Attach Fittings
  > CORRODED BATHTUB FITTING LONGERON 29 LEFT STA 996. REMOVED AND REPLACED FITTING AT LONGERON 29 LEFT IAW DC-9 SRM 51-30-5.
- [SDR ABXA030415](https://openairdocs.org/sdr/ABXA030415.md): Battery Pack · discharged · Nov 6, 2003 · N929AX · Doug DC931 · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER PACK IAW DC-9 MM 32-53-02.
- [SDR ABXA030181](https://openairdocs.org/sdr/ABXA030181.md): Floorbeam · corroded · May 20, 2003 · N929AX · Doug DC931 · Fuselage Main, Floor Beam
  > EXFOLIATED FLOORBEAM IN FORWARD LOWER CARGO, FS 313 AT RIGHT BUTT LINE 6. REPAIRED CORRODED FLOORBEAM IAW DC-9 SRM 53-05.
- [SDR ABXA030180](https://openairdocs.org/sdr/ABXA030180.md): Bulkhead · cracked · May 19, 2003 · N929AX · Doug DC931 · Nacelle/Pylon, Bulkhead/Firewall
  > LEFT FORWARD PYLON BULKHEAD WEB HAD CRACK AT ATTACH FASTENER 20 INCHES FROM FLOOR, LEFT BUTT LINE 54. REPAIRED IAW DC-9 SRM 53-01.
- [SDR ABXA030179](https://openairdocs.org/sdr/ABXA030179.md): Longeron · cracked · May 14, 2003 · N929AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 17 RIGHT CRACKED BEHIND SPLICE SECTION AT FS 965 BEHIND FORWARD PYLON BULKHEAD. REPAIRED AREA IAW DC-9 SRM 53-02.
- [SDR ABXA030178](https://openairdocs.org/sdr/ABXA030178.md): Web · corroded · May 13, 2003 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > LEFT CUSP WEB EXFOLIATED BETWEEN FS 256-275. REPLACED CUSP WEB AT STA 237 TO 296 IAW DC-9 SRM 51-30-1 AND 51-30-2.
- [SDR ABXA030177](https://openairdocs.org/sdr/ABXA030177.md): Beam · cracked · May 12, 2003 · N929AX · Doug DC931 · Fuselage Main, Structure
  > MAIN ENTRY DOOR HORIZONTAL BEAM ABOVE UPPER HINGE ATTACH POINT WAS CRACKED. REPAIRED MAIN ENTRY DOOR BEAM PLANE NR 5 IAW DC-9 SRM 52-05.
- [SDR ABXA020299](https://openairdocs.org/sdr/ABXA020299.md): Door Frame · cracked · Nov 10, 2002 · N929AX · Doug DC931 · Passenger/Crew Doors
  > WHILE COMPLYING WITH AD 80-02-16, FOUND CRACK IN OUTER PLUG DOOR FRAME. REPAIRED AREA IAW REA D952-45160-MR.
- [SDR ABXA020258](https://openairdocs.org/sdr/ABXA020258.md): Battery · discharged · Oct 23, 2002 · N929AX · Doug DC931 · Emergency Lighting
  > EMERGENCY LIGHTS NOT ARMED WAS NOT ILLUMINATED ON OVERHEAD PANEL. REPLACED 2 EACH, 1.2 VDC BATTERIES IAW DC-9 MM 33-53-00-8. OPS CHECKED GOOD.
- [SDR ABXA010677](https://openairdocs.org/sdr/ABXA010677.md): Battery · discharged · Jan 17, 2002 · N929AX · Doug DC931 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS TEST VERY DIM, OVERHEAD PANEL IN COCKPIT. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-00-8-0001.
- [SDR ABXA010571](https://openairdocs.org/sdr/ABXA010571.md): Control Valve · defective · Nov 4, 2001 · N929AX · Doug DC931 · Cabin Temperature Control System
  > SLOW BUT STEADY LOSS OF CABIN PRESSURIZATION AT FLIGHT LEVEL 350, FOLLOWED BY ODOR OF HEAT FILLING THE COCKPIT. EMERGENCY DECLARED. SELECTED HIGH PRESSURE BLEED OFF. ODOR PERSISTED. BELOW 10,000 FEET, VENTED AIRCRAFT, ODOR GONE. INSPECTED TAIL COMPARTMENT
- [SDR ABXA010523](https://openairdocs.org/sdr/ABXA010523.md): Frame · cracked · Sep 20, 2001 · N929AX · Doug DC931 · Fuselage Main, Frame
  > MULTIPULE CRACKS WERE FOUND ON FRAME 718 AFT INBOARD FLANGE. THE FIRST CRACK IS LOCATED IN THE MACHINED RADIOUS AND EXTENDS SIX INCHES FROM THE BASE. THE SECOND CRACK IS 2.5 INCHES LONG AND ORIGINATES AT THE LOWER THROUGH BOLT, EXTENDING TOWARD THE AFT EDGE OF
- [SDR ABXA000283](https://openairdocs.org/sdr/ABXA000283.md): Wire · broken · May 24, 2000 · N929AX · Doug DC931 · Landing Gear System Wiring
  > ON GEAR EXTENSION AT LBB, RIGHT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE. RECYCLED GEAR AND PERFORMED ABNORMAL PROCEDURES. LANDING WITHOUT INCIDENT. REPAIRED BROKEN WIRE NR 2G205C20 AT CANNON PLUG FOR RIGHT GEAR DOWN LIMIT SWITCH. OPS CHECKED GOOD.
- [SDR ABXA000104](https://openairdocs.org/sdr/ABXA000104.md): Shear Tie · cracked · Feb 9, 2000 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > SHEAR-TIE AT STA 996 AND LONGERON 18L IS CRACKED.. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-5 AND 51-30-2.
- [SDR ABXA000099](https://openairdocs.org/sdr/ABXA000099.md): Finger Doubler · cracked · Feb 2, 2000 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > FINGER DOUBLER IS CRACKED AT STATION 239 JUST BELOW LONGERON 18 LEFT INSIDE FORWARD LOWER CARGO COMPARTMENT. REPAIRED FINGER DOUBLER IAW ABX REA D953-35352.
- [SDR ABXA000098](https://openairdocs.org/sdr/ABXA000098.md): Angle · corroded · Jan 31, 2000 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR FORWARD HINGE LOWER FUSELAGE SUPPORT BRACKET ATTACH ANGLE EXFOLIATED. REPLACED ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA000097](https://openairdocs.org/sdr/ABXA000097.md): Web · cracked · Jan 31, 2000 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND THE LEFT FORWARD EMERGENCY EXIT DOOR INTERIOR WEB CRACKED. REPAIRED WEB IAW DC9 SRM 52-01, FIGURE 2, SHEET 3.
- [SDR ABXA000096](https://openairdocs.org/sdr/ABXA000096.md): Angle · cracked · Jan 31, 2000 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND STA 756 BULKHEAD CENTER VERTICAL SUPPORT ANGLE CRACKED. REPAIRED ANGLE IAW DC9 SRM DRAWING NR K05159.
- [SDR ABXA000095](https://openairdocs.org/sdr/ABXA000095.md): Beam · cracked · Jan 31, 2000 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND NR 5 HORIZONTAL BEAM IN FORWARD ENTRY DOOR CRACKED AT THE BOLT HOLE AT THE CENTER OF THE BEAM. REPAIRED BEAM IAW SRM DRAWING NR K05159.
- [SDR ABXA000094](https://openairdocs.org/sdr/ABXA000094.md): Rib · cracked · Jan 31, 2000 · N929AX · Doug DC931 · Wing, Rib/Bulkhead
  > DURING C CHECK, FOUND A RIGHT WING TRAILING EDGE RIB ABOVE THE INBOARD FIXED VANE CRACKED. REPAIRED RIB IAW ABX REA D957-35354.
- [SDR ABXA000093](https://openairdocs.org/sdr/ABXA000093.md): Rib · cracked · Jan 31, 2000 · N929AX · Doug DC931 · Wing, Rib/Bulkhead
  > DURING C CHECK, FOUND A RIGHT WING TRAILING EDGE RIB ABOVE THE INBOARD FIXED VANE CRACKED. REPLACED RIB IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA000092](https://openairdocs.org/sdr/ABXA000092.md): Pan · cracked · Jan 31, 2000 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND THE SERVICE DOOR PAN CRACKED IN TWO PLACES AT THE FORWARD UPPER CORNER. REPAIRED DOOR PAN IAW DC9 SRM 52-03 FIGURE 3.
- [SDR ABXA9900361](https://openairdocs.org/sdr/ABXA9900361.md): Wire · broken · Apr 26, 1999 · N929AX · Doug DC931 · Landing Gear System Wiring
  > NOSE GEAR UNSAFE LIGHT FAILED TO ILLUMINATE DURING GEAR RETRACTION. RECYCLED GEAR, UNSAFE LIGHT FAILED TO ILLUMINATE INTRANSIT. ALL OTHER INDICATIONS WERE NORMAL. REPAIRED BROKEN WIRE IN CONDUIT JUST AFT OF NOSE GEAR DEPLOYMENT SWITCH (P1-133).
- [SDR ABXA9800534](https://openairdocs.org/sdr/ABXA9800534.md): Angle · cracked · Jun 4, 1998 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > WHILE COMPLYING WITH C INSPECTION, FOUND THE RIGHT ENGINE PYLON TO FUSELAGE ATTACH ANGLE CRACKED AT FS 996. REPLACED ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-2.
- [SDR ABXA9800533](https://openairdocs.org/sdr/ABXA9800533.md): Skin · cracked · Jun 4, 1998 · N929AX · Doug DC931 · Fuselage Main, Plate/Skin
  > WHILE COMPLYING WITH C INSPECTION, FOUND THE RIGHT AFT FUSELAGE SKIN CRACKED AT FS 945 BETWEEN LONGERONS 15R AND 16R. REPAIRED IAW ABX REA D953-23860MR.
- [SDR ABXA9800486](https://openairdocs.org/sdr/ABXA9800486.md): Longeron · cracked · Jun 2, 1998 · N929AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 17L CRACKED AT STATION 980 FRAME ATTACH POINT. REPLACED LONGERON IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA9800485](https://openairdocs.org/sdr/ABXA9800485.md): Angle · cracked · Jun 2, 1998 · N929AX · Doug DC931 · Nacelle/Pylon Structure
  > DURING C-CHECK, FOUND NR 1 ENGINE PYLON TRAILING EDGE INTERIOR ANGLE CRACKED AT AFT OUTBOARD CORNER. REPLACED ANGLE IAW DC9 SRM 51-30-2, 51-30-5 AND DACO DWG 9915555.
- [SDR ABXA9800484](https://openairdocs.org/sdr/ABXA9800484.md): Web · canned · Jun 2, 1998 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CUSP WEB OIL CANNING AT STATION 945 TO 965, LEFT SIDE. REPAIRED CUSP WEB IAW ABX REA D953-23817-MR.
- [SDR ABXA9800527](https://openairdocs.org/sdr/ABXA9800527.md): Frame · cracked · Jun 1, 1998 · N929AX · Doug DC931 · Fuselage Main, Frame
  > WHILE COMPLYING WITH C-CHECK, FOUND FUSELAGE FRAME AT FS 980 CRACKED AT LONGERON 16R. REPLACED FUSELAGE FRAME SECTION FROM LONGERON 15R TO LONGERON 18R IAW DC-9 SRM CHAPTER 53-03.
- [SDR ABXA9800473](https://openairdocs.org/sdr/ABXA9800473.md): Beam · cracked · May 31, 1998 · N929AX · Doug DC931 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND FORWARD LOWER CARGO COMPARTMENT DOOR VERTICAL BEAM CRACKED AT BOTTOM FORWARD PRESSURE STOP. REPLACED VERTICAL BEAM IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA9800469](https://openairdocs.org/sdr/ABXA9800469.md): Angle · cracked · May 25, 1998 · N929AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND THE LEFT MAIN LANDING GEAR WHEEL WELL DOOR JAMB ANGLE CRACKED INBOARD OF HAND PUMP. REPLACED ANGLE IAW DACO DWG 9915518 AND DC9 SRM 51-30-2.
- [SDR ABXA9701906](https://openairdocs.org/sdr/ABXA9701906.md): Spar · cracked · Dec 3, 1997 · N929AX · Doug DC931 · Wing Spar
  > RIGHT WING REAR SPAR HAS CRACK ON WEB AT STATION 58. REPAIRED IAW ABX REA D957-21828.
- [SDR ABXA9701682](https://openairdocs.org/sdr/ABXA9701682.md): Rod Assy · out of adjust · Oct 21, 1997 · N929AX · Doug DC931 · Landing Gear Door Retract Section
  > DURING APPROACH UPON GEAR EXTENSION, THE GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. WHEN GEAR WAS RECYCLED, THE DOOR LIGHT WENT OUT AFTER A PERIOD OF TIME. CHECKED THE MAIN LANDING GEAR CONTROL VALVE AND ADJUSTED THE RIGHT HAND DOOR VALVE CRANK IAW DC-9 MM 3
- [SDR ABXA9700607](https://openairdocs.org/sdr/ABXA9700607.md): Door · delaminated · Feb 14, 1997 · N929AX · Doug DC931 · Landing Gear Doors
  > WHILE COMPLYING WITH AD 91-22-07, FOUND RIGHT MAIN LANDING OUTBOARD DOOR DELAMINATED. REPLACED RIGHT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 MM 32-12-01.
- [SDR ABXA9701011](https://openairdocs.org/sdr/ABXA9701011.md): Tab · corroded · Oct 28, 1996 · N929AX · Doug DC931 · Elevator, Tab Structure
  > FOUND ELEVATOR CONTROL TAB INBOARD NOSE CAP CORRODED. REPLACED NOSE CAP (P/N 591041311) IAW DC9 SRM 51-30-1.
- [SDR ABXA9700458](https://openairdocs.org/sdr/ABXA9700458.md): Angle · cracked · Oct 16, 1996 · N929AX · Doug DC931 · Nacelle/Pylon Structure
  > DURING C-CHECK, THE LEFT UPPER AFT PYLON ATTACH ANGLE WAS FOUND CRACKED NR WC-855. REPAIRED ATTACH ANGLE IAW DC9 SRM 51-30-1.
- [SDR ABXA9700457](https://openairdocs.org/sdr/ABXA9700457.md): Fitting · cracked · Oct 16, 1996 · N929AX · Doug DC931 · Trailing Edge Flaps
  > DURING C-CHECK, THE LEFT WING MOVEABLE VANE AFT ATTACH FITTING WAS FOUND CRACKED, NR WC-800. REPLACED ATTACH FITTING IAW DC9 OHM 27-50-2.

Next page: https://openairdocs.org/deregistered/N929AX-2017-07-20/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 = 'N929AX' AND deregistration_id = 'N929AX-2017-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N929AX-2017-07-20/reports

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