# Service difficulty reports: N942AX, cancelled Sep 26, 2013

A list on [N942AX, cancelled Sep 26, 2013](https://openairdocs.org/deregistered/N942AX-2013-09-26.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 · 90 reports

- [SDR ABXA050286](https://openairdocs.org/sdr/ABXA050286.md): Battery · weak · Nov 22, 2005 · N942AX · Doug DC931 · Emergency Lighting
  > EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERIES. OPS CHECK GOOD, IAW AMM 33-53-00-0-0001.
- [SDR ABXA040369](https://openairdocs.org/sdr/ABXA040369.md): Frame · cracked · Oct 27, 2004 · N942AX · Doug DC931 · Fuselage Main, Frame
  > FORWARD LEFT MAIN FRAME, STA 699 WAS CRACKED WITHIN REPAIRABLE LIMITS. REPAIRED MAIN FRAME, STA 699 LT IAW DC-9 SERVICE REWORK DRAWING 5933650 AND JOB CARD EA 63400110-001-1.
- [SDR ABXA040371](https://openairdocs.org/sdr/ABXA040371.md): Frame · cracked · Oct 27, 2004 · N942AX · Doug DC931 · Fuselage Main, Frame
  > AFT LEFT MAIN FRAME, STA 737, REQUIRED REPLACEMENT DUE TO CRACKS. REMOVED AND REPLACED AFT LEFT MAIN FRAME STA 737 IAW JOB CARD EA 53400325-001-4.
- [SDR ABXA040370](https://openairdocs.org/sdr/ABXA040370.md): Frame · cracked · Oct 27, 2004 · N942AX · Doug DC931 · Fuselage Main, Frame
  > FORWARD RIGHT MAIN FRAME, STA 699, REQUIRED REPLACEMENT. CRACKED BEYOND LIMITS OF REPAIR. REMOVED AND REPLACED RIGHT MAIN FRAME, STA 699 IAW JOB CARD EA 53400322-001-4.
- [SDR ABXA040030](https://openairdocs.org/sdr/ABXA040030.md): Charger · defective · Jan 15, 2004 · N942AX · Doug DC931 · Battery/Charger System
  > IN FLIGHT, BATTERY CHARGER WAS CHARGING BATTERY CONTINUALLY AT 20 AMPS, THE BATTERY WAS AT 38 TO 39 VOLTS. REMOVED AND REPLACED BOTH MAIN BATTERIES, BATTERY CHARGER, AND BATTERY SENSOR IAW DC-9 AMM 24-30-01-4-0001 AND 24-30-02-2-001. OPS CHECKED GOOD.
- [SDR ABXA030164](https://openairdocs.org/sdr/ABXA030164.md): Spar Cap · corroded · Apr 15, 2003 · N942AX · Doug DC931 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER REAR UPPER SPAR CORRODED JUST INBOARD OF XHS 68. REPAIRED AREA IAW REA D955-47165 AND DC-9 SRM.
- [SDR ABXA030169](https://openairdocs.org/sdr/ABXA030169.md): Skin · corroded · Apr 15, 2003 · N942AX · Doug DC931 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAD BULGE AT APPROXIMATELY STA 589, LONGERON 18 RIGHT. REPAIRED AREA IAW REA D958-47172MR AND DC-9 SRM 51-10-3.
- [SDR ABXA030168](https://openairdocs.org/sdr/ABXA030168.md): Longeron · corroded · Apr 15, 2003 · N942AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 30, DEEPLY PITTED AT FS 756. REPAIRED LONGERON 30 IAW DC-9 SRM 53-02.
- [SDR ABXA030166](https://openairdocs.org/sdr/ABXA030166.md): Door Frame · corroded · Apr 15, 2003 · N942AX · Doug DC931 · Fuselage Main, Structure
  > EVIDENCE OF CORROSION DETECTED AROUND FORWARD LOWER CARGO DOOR JAMB LOWER SET SCREW FITTINGS, BETWEEN SKIN LAYERS. REPAIRED AREA IAW REA D953-47181MR AND DC-9 SRM 53-05.
- [SDR ABXA030165](https://openairdocs.org/sdr/ABXA030165.md): Floorbeam · corroded · Apr 14, 2003 · N942AX · Doug DC931 · Fuselage Main, Floor Beam
  > FLOORBEAM WAS EXFOLIATED AT FS 408 DIRECTLY ABOVE FORWARD LOWER CARGO DOOR CUTOUT AND OUTBOARD OF RIGHT BUTT LINE 54. REPAIRED AREA IAW REA D953-47171 AND DC-9 SRM.
- [SDR ABXA030163](https://openairdocs.org/sdr/ABXA030163.md): Skin · corroded · Apr 14, 2003 · N942AX · Doug DC931 · Trailing Edge Flaps
  > BULGE IN FLAP SKIN AND CUPPED HEAD FASTENERS UPPER SURF AT INBOARD EXPANSION JOINT. REPLACED SKIN AND REINSTALLED INBOARD FLAP SECTION IAW DC-9 SRM.
- [SDR ABXA030167](https://openairdocs.org/sdr/ABXA030167.md): Pressure Panel · corroded · Apr 14, 2003 · N942AX · Doug DC931 · Fuselage Main, Bulkhead
  > ONE SHEARED FASTENER AND SKIN BULGED AT DOUBLER RIGHT WHEEL WELL UPPER PRESSURE PANEL, STA 716, RIGHT BUTT LINE 56. REPAIRED AREA IAW REA D953-47174.
- [SDR ABXA010478](https://openairdocs.org/sdr/ABXA010478.md): Fitting · cracked · Sep 6, 2001 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > A CRACK WAS INDICATED ON THE AFT PRESSURE BULKHEAD TEE FITTING NR 6, L14L. MAINTENANCE INSPECTED AND REPLACED THE TEE FITTING IAW ABX EA 53120037-006.
- [SDR ABXA010479](https://openairdocs.org/sdr/ABXA010479.md): Frame · cracked · Sep 5, 2001 · N942AX · Doug DC931 · Fuselage Main, Frame
  > FUSELAGE FRAME AT STATION 1076 WAS FOUND TO HAVE THREE CRACKS AT FASTENERS L13L AND L14L. MAINTENANCE INSPECTED AND REPLACED THE AFFECTED SECTION OF THE FRAME FROM LONGERON 10L TO 17L IAW DC-9 SRM 53-03.
- [SDR ABXA010480](https://openairdocs.org/sdr/ABXA010480.md): Support · corroded · Sep 1, 2001 · N942AX · Doug DC931 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT AT FUSELAGE STATION 945 WAS FOUND TO BE CORRODED ABOVE LONGERON 30. MAINTENANCE MANUFACTURED AND INSTALLED A SUPPORT SPLICE IAW DRAWING 99577 AND DC-9 SRM.
- [SDR ABXA010482](https://openairdocs.org/sdr/ABXA010482.md): Stiffener · cracked · Sep 1, 2001 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > RADIAL 5A ON AFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED. REPAIRED THE RADIAL IAW SERVICE BULLETIN 53-166-W.
- [SDR ABXA010477](https://openairdocs.org/sdr/ABXA010477.md): Track · corroded · Aug 30, 2001 · N942AX · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > THE CENTER SEAT TRACK AT STATION 237-275 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW DC-9 SRM.
- [SDR ABXA010481](https://openairdocs.org/sdr/ABXA010481.md): Angle · cracked · Aug 30, 2001 · N942AX · Doug DC931 · Fuselage Main, Bulkhead
  > UPPER OUTBOARD ATTACH ANGLE ON RADIAL 5A, FWD SIDE, WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE ATTACH ANGLE IAW ABX EA 53120037-006.
- [SDR ABXA010087](https://openairdocs.org/sdr/ABXA010087.md): Skin · damaged · Mar 8, 2001 · N942AX · Doug DC931 · Fuselage Main, Plate/Skin
  > A FIVE INCH CREASE WAS NOTED ON THE FUSELAGE OUTER SKIN, APPROX 24 INCHES AFT AND 24 INCHES BELOW MAIN ENTRY DOOR. MAINTENANCE REPAIRED AREA IAW DC-9 SRM 53-04 FIG 12B.
- [SDR ABXA000533](https://openairdocs.org/sdr/ABXA000533.md): Power Supply · discharged · Dec 26, 2000 · N942AX · Doug DC931 · Emergency Lighting
  > EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHTING POWER PACK ASSEMBLY, IAW DC-9 MM CHAPTER 33. OPS CHECKED GOOD.
- [SDR ABXA000068](https://openairdocs.org/sdr/ABXA000068.md): Support · cracked · Jan 13, 2000 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FLOORBEAM SUPPORT CRACKED STATION 658, RBL 22. REPLACED FLOORBEAM SUPPORT IAW DC9 SRM 51-30-2.
- [SDR ABXA000047](https://openairdocs.org/sdr/ABXA000047.md): Pan · cracked · Jan 13, 2000 · N942AX · Doug DC931 · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN AND SKIN CRACKED. REPAIRED IAW REA D95235065 AND SRM 52-05 FIGURE 50 SHEET 2.
- [SDR ABXA000046](https://openairdocs.org/sdr/ABXA000046.md): Frame · cracked · Jan 13, 2000 · N942AX · Doug DC931 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND STATION 737 RT MAIN FRAME CRACKED. REPAIRED CRACK IAW REA D95335059 MR.
- [SDR ABXA9900375](https://openairdocs.org/sdr/ABXA9900375.md): Wire · loose · May 19, 1999 · N942AX · Doug DC931 · Light System Wiring
  > EMERGENCY LIGHTS WERE DIM AND INTERMITTENT. FOUND GROUND WIRE AT EMERGENCY BATTERY PACK LOOSE AND CORRODED. CLEANED AND REINSTALLED GROUND WIRE, OPS CHECKED GOOD.
- [SDR ABXA9900007](https://openairdocs.org/sdr/ABXA9900007.md): Battery · discharged · Jan 10, 1999 · N942AX · Doug DC931 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK.
- [SDR ABXA9800480](https://openairdocs.org/sdr/ABXA9800480.md): Intercostal · cracked · Jun 2, 1998 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND INTERCOSTAL CRACKED AT STATION 180 TO 200 LONGERON 30. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA9800476](https://openairdocs.org/sdr/ABXA9800476.md): Angle · cracked · Jun 1, 1998 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FORWARD LOWER INBOARD CORNER ATTACH ANGLE CRACKED AT EDGE OF RIGHT WHEEL WELL STRUCTURE. REPLACED ANGLE IAW DC9 SRM 51-30-1.
- [SDR ABXA9800474](https://openairdocs.org/sdr/ABXA9800474.md): Sub Floor · cracked · May 31, 1998 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND SUB FLOOR CRACKED AT STATION 205 AND LBL 22 AND STATION 200 AT BL 0. REPAIRED SUB FLOOR IAW DC9 SRM 53-01.
- [SDR ABXA9800468](https://openairdocs.org/sdr/ABXA9800468.md): Web · cracked · May 25, 1998 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CUSP WEB STATION 260 RIGHT SIDE CRACKED. REPAIRED CUSP WEB IAW ABX REA D953-23794-MR AND REA 953-23777MR.
- [SDR ABXA9800467](https://openairdocs.org/sdr/ABXA9800467.md): Bulkhead Angle · cracked · May 25, 1998 · N942AX · Doug DC931 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD, FORWARD RIGHT SIDE 3RD STIFFENER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DC9 SB 53-166 AND CACO DWG 941558.
- [SDR ABXA9800466](https://openairdocs.org/sdr/ABXA9800466.md): Frame · corroded · May 25, 1998 · N942AX · Doug DC931 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND FRAME AT STATION 446 AND LONGERON 28L TO 29R CORRODED. REPAIRED FRAME IAW DC9 SRM 53-03.
- [SDR ABXA9701194](https://openairdocs.org/sdr/ABXA9701194.md): Battery · discharged · Jul 5, 1997 · N942AX · Doug DC931 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT SHUT OFF. REPLACED EMERGENCY LIGHTS POWER SUPPLY, OPS CHECKED GOOD IAW DC-9 MM.
- [SDR ABXA9700050](https://openairdocs.org/sdr/ABXA9700050.md): Seat · defective · Mar 5, 1997 · N942AX · Doug DC931 · Flight Compartment Equipment
  > CAPTAIN'S SEAT SLIPS DOWN DURING TAKEOFF. REPLACED CAPTAIN'S SEAT IAW DC-9 MM.
- [SDR ABXA9700632](https://openairdocs.org/sdr/ABXA9700632.md): Skin · gouged · Oct 12, 1996 · N942AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND SKIN GOUGED AFT OF FLC DOOR. REPAIRED IAW ABX REA D953-16631-MR.
- [SDR ABXA9700633](https://openairdocs.org/sdr/ABXA9700633.md): Frame · corroded · Oct 9, 1996 · N942AX · Doug DC931 · Fuselage Main, Frame
  > DURING C-CHECK, CANTED FRAME WEB AT FS 1089 CORRODED. REPAIRED IAW ABX REA D953-16618-MR.
- [SDR ABXA9700647](https://openairdocs.org/sdr/ABXA9700647.md): Fitting · cracked · Oct 8, 1996 · N942AX · Doug DC931 · Drag Control System
  > DURING C-CHECK, FOUND RIGHT WING INBOARD SPOILER TORQUE TUBE CENTER SUPPORT FITTING CRACKED. REPLACED IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5.
- [SDR ABXA9700631](https://openairdocs.org/sdr/ABXA9700631.md): Skin · dented · Oct 8, 1996 · N942AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND 2 DENTS IN FUSELAGE SKIN AND WINDOW BELT DOUBLER AT FS 334. REPAIRED IAW ABX REA D953-16639-MR.
- [SDR ABXA9700627](https://openairdocs.org/sdr/ABXA9700627.md): Skin · gouged · Oct 8, 1996 · N942AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND FUSELAGE SKIN GOUGED FROM STATION 208 TO 223, BETWEEN LONGERON 24R TO 25R. REPAIRED IAW ABX REA D953-16659-MR.
- [SDR ABXA9700626](https://openairdocs.org/sdr/ABXA9700626.md): Skin · torn · Oct 7, 1996 · N942AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING C-CHECK FOUND ENTRY DOOR AFT JAMB INNER SKIN TORN AT FS 200. REPAIRED IAW ABX REA D953-16621-MR.
- [SDR ABXA9700623](https://openairdocs.org/sdr/ABXA9700623.md): Intercostal · cracked · Oct 7, 1996 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND CRACKED INTERCOSTAL BETWEEN FRAMES 699 TO 718 AT LONGERON 6L. FABRICATED NEW INTERCOSTAL IAW DC-9 DWG 9958242-3, INSTALLED IAW DC-9 SRM 51-30-2.
- [SDR ABXA9700609](https://openairdocs.org/sdr/ABXA9700609.md): Latch Cup · cracked · Oct 7, 1996 · N942AX · Doug DC931 · Passenger/Crew Doors
  > DURING C-CHECK, FOUND ENTRY DOOR HOLD OPEN LATCH CUP CRACKED. REPAIRED IAW ABX REA D952-16507.
- [SDR ABXA9700608](https://openairdocs.org/sdr/ABXA9700608.md): Door · cracked · Oct 7, 1996 · N942AX · Doug DC931 · Landing Gear Doors
  > DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND LEFT MLG INBOARD DOOR CRACKED AT FORWARD UPPER CORNER. REPLACED DOOR IAW DC-9 SUPPLEMENTAL M/M 32-12-01.
- [SDR ABXA9700628](https://openairdocs.org/sdr/ABXA9700628.md): Web · cracked · Oct 6, 1996 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CUSP WEB BETWEEN FS 237 TO 317 CRACKED AND CORRODED. REPAIRED IAW ABX REA D953-16630-MR.
- [SDR ABXA9700629](https://openairdocs.org/sdr/ABXA9700629.md): Bulkhead Web · gouged · Oct 5, 1996 · N942AX · Doug DC931 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND GOUGES ON APB WEB AT LONGERON 28L AT TEE CAP. REPAIRED IAW ABX REA D953-16658-MR.
- [SDR ABXA9700613](https://openairdocs.org/sdr/ABXA9700613.md): Seat Track · cracked · Oct 5, 1996 · N942AX · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SEAT TRACK CRACKED AT RBL 22 AT STA 690. REPAIRED IAW ABX EA NR FS-53-04023-MA.
- [SDR ABXA9700610](https://openairdocs.org/sdr/ABXA9700610.md): Seat Track · worn · Oct 5, 1996 · N942AX · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND RBL 22 SEAT TRACK WORN STA 220, 275. REPAIRED IAW ABX EA NR FS-53-04023-MA.
- [SDR ABXA9700646](https://openairdocs.org/sdr/ABXA9700646.md): Spar Cap · cracked · Oct 4, 1996 · N942AX · Doug DC931 · Horizontal Stabilizer, Spar/Rib
  > DURING C-CHECK FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR LOWER CAP CRACKED, AT XFS 180. REPAIRED IAW ABX REA D955-15489-MR.
- [SDR ABXA9700630](https://openairdocs.org/sdr/ABXA9700630.md): Shear Tie · cracked · Oct 4, 1996 · N942AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SHEAR TIE CRACKED AT FS 945. INSTALLED NEW SHEAR TIE IAW DC-9 SRM 51-30-2.
- [SDR ABXA9700641](https://openairdocs.org/sdr/ABXA9700641.md): Rib · cracked · Oct 3, 1996 · N942AX · Doug DC931 · Vertical Stabilizer, Spar/Rib
  > DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, UPPER RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.
- [SDR ABXA9700640](https://openairdocs.org/sdr/ABXA9700640.md): Rib · cracked · Oct 3, 1996 · N942AX · Doug DC931 · Vertical Stabilizer, Spar/Rib
  > DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, CANTED RIB RIGHT SIDE. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Next page: https://openairdocs.org/deregistered/N942AX-2013-09-26/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 = 'N942AX' AND deregistration_id = 'N942AX-2013-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N942AX-2013-09-26/reports

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