# Service difficulty reports: N949AX, cancelled Sep 26, 2013

A list on [N949AX, cancelled Sep 26, 2013](https://openairdocs.org/deregistered/N949AX-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 · 78 reports

- [SDR ABXA080149](https://openairdocs.org/sdr/ABXA080149.md): Skin · cracked · Apr 30, 2008 · N949AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING LINE MAINTENANCE WHILE CHANGING THE LEFT STATIC PORT PLATE, FOUND THE SKIN UNDER THE STATIC PORT PLATE CRACKED APPROXIMATELY 1/2 INCH LONG BETWEEN LONGERONS 23 LEFT - 24 LEFT. REPAIRED AREA IAW DC9 SRM 53-04, FIGURE 12C.
- [SDR ABXA080088](https://openairdocs.org/sdr/ABXA080088.md): Battery · discharged · Mar 3, 2008 · N949AX · Doug DC931 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT ILLUMINATE WITH SWITCH IN THE 'ON' POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8.
- [SDR ABXA070084](https://openairdocs.org/sdr/ABXA070084.md): Doubler · corroded · Mar 7, 2007 · N949AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DOUBLER ATTACHED TO FUSELAGE SKIN AT FUEL SHROUD WAS CORRODED, LONGERON 20 AREA. REMOVED AND INSTALLED NEW DOUBLER IAW DC9 SRM.
- [SDR ABXA070083](https://openairdocs.org/sdr/ABXA070083.md): Longeron · corroded · Mar 7, 2007 · N949AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 20 INBOARD AT LEFT WHEEL WELL CORRODED AT STA 718. REMOVED LONGERON 20. DRILLED LONGERON 20 P/N 5914259-501AX, IAW DOUGLAS DWG 5914579 AND DC9 SRM 51-10-4. REINSTALLED LONGERON 20 IAW DWG 5914579, DC9 SRM 51-30-5 AND 51-30-1.
- [SDR ABXA070112](https://openairdocs.org/sdr/ABXA070112.md): Pressure Panel · corroded · Mar 6, 2007 · N949AX · Doug DC931 · Fuselage Main, Bulkhead
  > WHEEL WELL PRESSURE PANEL WAS BULGED AND CRACKED AT APPROXIMATELY FS 708, BUTT LINE 0. REPAIRED WHEEL WELL PRESSURE PANEL APPROXIMATELY FS 708 IAW DC9 REA D953-55487.
- [SDR ABXA070082](https://openairdocs.org/sdr/ABXA070082.md): Seat Track · corroded · Mar 2, 2007 · N949AX · Doug DC931 · Fuselage, Seat/Cargo Attach Fittings
  > LOWER LEG OF SEAT TRACK CORRODED AT STA 699, RIGHT BUTT LINE 10. BLENDED OUT OF LIMITS. REMOVED SEAT TRACK FROM STA 663 - 763 AND FLOOR PANEL 8F. REINSTALLED NEW SEAT TRACK IAW DC9 SRM DWG K05482. RE-INSTALLED FLOOR PANEL 8F IAW DC9 SRM 51-30-1.
- [SDR ABXA070081](https://openairdocs.org/sdr/ABXA070081.md): Intercostal · corroded · Mar 2, 2007 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > CORROSION AT AND AROUND INTERCOSTAL STA 737 - 756, LEFT BUTT LINE 22. INSTALLED INTERCOSTAL IAW DC9 SRM 51-30-5.
- [SDR ABXA070111](https://openairdocs.org/sdr/ABXA070111.md): Frame · corroded · Feb 28, 2007 · N949AX · Doug DC931 · Fuselage Main, Frame
  > CRACK WITH EXFOLIATION ABOVE RADIUS ON FORWARD SIDE OF FRAME AT STA 718, APPEARED TO BE IN THE WEB AREA. REPLACED FRAME ON EA 53400323-001-2.
- [SDR ABXA070080](https://openairdocs.org/sdr/ABXA070080.md): Intercostal · corroded · Feb 28, 2007 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT LONGERON 29 RIGHT CORRODED BETWEEN LONGERON 29 RIGHT AND INTERCOSTAL FROM STA 965 - 980, BULGED ON INBOARD LEGS. REMOVED AND REPLACED INTERCOSTAL LONGERON 29 RIGHT, FS 965 TO 980 IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA070079](https://openairdocs.org/sdr/ABXA070079.md): Frame · corroded · Feb 28, 2007 · N949AX · Doug DC931 · Fuselage Main, Frame
  > FORWARD LOWER CARGO FRAME CORRODED AT FS 465 BETWEEN LONGERON 28 LEFT AND LONGERON 28 RIGHT. REMOVED CORROSION AND REPLACED SECTION OF FRAME IAW DC9 SRM 53-03.
- [SDR ABXA050073](https://openairdocs.org/sdr/ABXA050073.md): Web · cracked · Mar 8, 2005 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > STA 1038 BULKHEAD AT LONGERON 13 LEFT WAS CRACKED AT LIGHTENING HOLE. REPAIRED IAW DC-9 SRM 53-01.
- [SDR ABXA050072](https://openairdocs.org/sdr/ABXA050072.md): Frame · cracked · Mar 7, 2005 · N949AX · Doug DC931 · Fuselage Main, Frame
  > FRAME CRACKED FS 889 AT LONGERON 29 LEFT. REPAIRED CRACKED FRAME FLANGE IAW DC-9 SRM DWG K05159.
- [SDR ABXA030325](https://openairdocs.org/sdr/ABXA030325.md): Intercostal · cracked · Jul 30, 2003 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED AT FORWARD CONDUIT HOLE, STA 155, 43 INCHES UP FROM FLOOR RIGHT SIDE. REPAIRED AREA IAW DC-9 SRM 53, 51-30-2 AND 51-30-5.
- [SDR ABXA030324](https://openairdocs.org/sdr/ABXA030324.md): Stop Fitting · cracked · Jul 21, 2003 · N949AX · Doug DC931 · Cargo/Baggage Doors
  > UPPER AFT DOOR STOP FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1.
- [SDR ABXA010682](https://openairdocs.org/sdr/ABXA010682.md): Skin · cracked · Jan 24, 2002 · N949AX · Doug DC931 · Fuselage Structure (General)
  > DURING LINE MAINTENANCE VISIT, FUSELAGE SKIN WAS CRACKED AT THE FORWARD ENTRY DOOR, UPPER AFT CORNER, STATION 218, LONGERON 7 LEFT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM.
- [SDR ABXA010622](https://openairdocs.org/sdr/ABXA010622.md): Web · cracked · Nov 27, 2001 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED AT SEAT TRACK HOLE RIGHT BUTT LINE 54, STATION 795. REPAIRED CUSP WEB IAW DC-9 SRM 51-00.
- [SDR ABXA010621](https://openairdocs.org/sdr/ABXA010621.md): Longeron · cracked · Nov 26, 2001 · N949AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > LONGERON 17 LEFT WAS CRACKED ON UPPER AND LOWER FLANGE AT STATION 945 FRAME. REPAIRED AREA IAW DC-9 SRM 53-02.
- [SDR ABXA010620](https://openairdocs.org/sdr/ABXA010620.md): Former · cracked · Nov 26, 2001 · N949AX · Doug DC931 · Horizontal Stabilizer, Spar/Rib
  > SHEARTIE AT STATION 980 WAS CRACKED AT LONGERON 14 LEFT. REPLACED SHEARTIE IAW DC-9 SRM 51-30-5.
- [SDR ABXA010423](https://openairdocs.org/sdr/ABXA010423.md): Acm · malfunctioned · Aug 2, 2001 · N949AX · Doug DC931 · Cabin Cooling System
  > TOP OF DESCENT SAW AND SMELLED ELECTRIC SMOKE IN COCKPIT. SMOKE CLEARED THEN RECURRED. REQUESTED PRIORITY LANDING. LANDING NORMAL. NO ABNORMAL ELECTRICAL INDICATIONS. CHECKED ELECTRICAL SYSTEM FOR BURNING, NOTHING FOUND. RAN ENGINES AND APU PRESSURE A/C
- [SDR ABXA9800817](https://openairdocs.org/sdr/ABXA9800817.md): Longeron · cracked · Sep 8, 1998 · N949AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 17L CRACKED FS 965. REPLACED SECTION OF LONGERON 17L FS 965 IAW DC9 SRM 53-02.
- [SDR ABXA9800816](https://openairdocs.org/sdr/ABXA9800816.md): Frame · cracked · Sep 8, 1998 · N949AX · Doug DC931 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND LEFT MAIN FRAME FS 718 CRACKED. REPAIRED LEFT FUSELAGE MAIN FRAME FS 718 IAW ABX REA D953- 24732-SB.
- [SDR ABXA9800815](https://openairdocs.org/sdr/ABXA9800815.md): Skin · corroded · Sep 8, 1998 · N949AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED FS 946-950 LONGERON 27R - LONGERON 29R. REPLACED DOUBLERS FS 945-980 LONGERON 27R TO LONGERON 29R, IAW DC9 MM 51-30-2.
- [SDR ABXA9800814](https://openairdocs.org/sdr/ABXA9800814.md): Skin · corroded · Sep 8, 1998 · N949AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND CORROSION ON LONGERON 30 AND ADJACENT FUSELAGE SKIN LONGERON 29R TO LONGERON 30R, FS 756-760. REPAIRED FUSELAGE SKIN IAW ABX REA D953 24724.
- [SDR ABXA9800813](https://openairdocs.org/sdr/ABXA9800813.md): Web · corroded · Sep 8, 1998 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND CUSP WEB CORRODED FS 945, LBL 50-54. REPLACED SECTION OF LEFT CUSP WEB 945L IAW ABX REA 953 24 702 MR.
- [SDR ABXA9800812](https://openairdocs.org/sdr/ABXA9800812.md): Longeron · cracked · Sep 8, 1998 · N949AX · Doug DC931 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 4 LEFT AT FS 160 CRACKED. REPLACED NEW SECTION OF LONGERON IAW DC9 SRM 53-02.
- [SDR ABXA900811](https://openairdocs.org/sdr/ABXA900811.md): Frame · corroded · Sep 8, 1998 · N949AX · Doug DC931 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND CORROSION ON FRAME 917 AT LONGERON 29L-LONGERON 29R. REPAIRED IAW DC9 SRM 53-03.
- [SDR ABXA9702000](https://openairdocs.org/sdr/ABXA9702000.md): Window · binding · Dec 22, 1997 · N949AX · Doug DC931 · Flight Compartment Windows
  > CAPTAIN'S SIDE WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED WINDOW TRIM AND LUBRICATED UPPER SLIDE TRACK.
- [SDR ABXA9701979](https://openairdocs.org/sdr/ABXA9701979.md): Window · binding · Dec 15, 1997 · N949AX · Doug DC931 · Flight Compartment Windows
  > CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED LOCKBAR, CHECKED RIGGING AND OPERATION OF WINDOW. OPS CHECKED GOOD.,
- [SDR ABXA9701416](https://openairdocs.org/sdr/ABXA9701416.md): Battery · discharged · Aug 20, 1997 · N949AX · Doug DC931 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKED GOOD.
- [SDR ABXA9701396](https://openairdocs.org/sdr/ABXA9701396.md): Window Lock · stuck · Aug 12, 1997 · N949AX · Doug DC931 · Flight Compartment Windows
  > CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. FREED THE TOP LOCK ON WINDOW, OPS CHECKED GOOD.
- [SDR ABXA9700597](https://openairdocs.org/sdr/ABXA9700597.md): Bulkhead Tee Cap · corroded · Feb 17, 1997 · N949AX · Doug DC931 · Fuselage Main, Bulkhead
  > DURING C-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD TEE CAP CORRODED FROM LONGERON 27 RIGHT TO LONGERON 30. REPAIRED AFT PRESSURE BULKHEAD T-CAP IAW DC-9 SRM CHAPTER 53-03 FIGURE 37.
- [SDR ABXA9700598](https://openairdocs.org/sdr/ABXA9700598.md): Skin · corroded · Feb 15, 1997 · N949AX · Doug DC931 · Fuselage Main, Plate/Skin
  > DURING C-INSPECTION, FOUND THE FUSELAGE SKIN BULGING AROUND FASTNERS AT FS 604 AT LONG 30. REPLACED TEE CAP AND DOUBLERS IAW ABX REA D953-18329MR AND D953-18288MR.
- [SDR ABXA9700601](https://openairdocs.org/sdr/ABXA9700601.md): Floorbeam · corroded · Feb 14, 1997 · N949AX · Doug DC931 · Fuselage Main, Floor Beam
  > DURING C-INSPECTION, FOUND LEVEL 2 CORROSION ON FLOORBEAM AT FS 937 LOWER FLANGE RBL 10 TO RBL 18. REPAIRED FLOORBEAM IAW ABX REA D953-18328MR AND DC-9 SRM CHAPTER 53-05, FIGURE 65.
- [SDR ABXA9700600](https://openairdocs.org/sdr/ABXA9700600.md): Floorbeam · corroded · Feb 14, 1997 · N949AX · Doug DC931 · Fuselage Main, Floor Beam
  > DURING C-INSPECTION, FOUND THE LOWER CHANNEL ON FLOORBEAM AT FS 939 CORRODED AT NUT PLATES FROM LONGERON 18 RIGHT TO LONGERON 18 LEFT. REPLACED FLOORBEAM SUPPORT CHANNELS IAW DC-9 SRM CHAPTER 51-30-2.
- [SDR ABXA9700606](https://openairdocs.org/sdr/ABXA9700606.md): Web · cracked · Feb 11, 1997 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-INSPECTION, FOUND THE RIGHT CUSP WEB IN MAIN CARGO COMPARTMENT CRACKED AT FS 617 AND RBL 56. REPLACED CUSP PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.
- [SDR ABXA9700602](https://openairdocs.org/sdr/ABXA9700602.md): Clip · cracked · Feb 11, 1997 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-INSPECTION, FOUND SHEAR TIE CLIP CRACKED AT FS 980 BELOW LONGERON 14 RIGHT. REPLACED SHEAR TIE CLIP AT FS 980 FROM LONGERON 13 RIGHT TO 17 RIGHT IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9700605](https://openairdocs.org/sdr/ABXA9700605.md): Spar Cap · corroded · Feb 10, 1997 · N949AX · Doug DC931 · Horizontal Stabilizer, Spar/Rib
  > DURING C-INSPECTION, FOUND THE RIGHT HORIZONTAL STAB FORWARD FACE OF THE UPPER REAR SPAR HAS LEVEL 2 CORROSION AT APPROXIMATE STATION XHS 140. REPAIRED RT HORIZONTAL UPPER REAR SPAR CAP IAW ABX REA D955-18175MR.
- [SDR ABXA9700588](https://openairdocs.org/sdr/ABXA9700588.md): Vane · delaminated · Feb 9, 1997 · N949AX · Doug DC931 · Trailing Edge Flaps
  > DURING C-INSPECTION, FOUND THE RIGHT FLAP INBOARD FIXED VANE DELAMINATED. REPLACED RT INBOARD FIXED VANE IAW DC-9 MAINTENANCE MANUAL, CHAPTER 27-51-3.
- [SDR ABXA9700876](https://openairdocs.org/sdr/ABXA9700876.md): Vane · delaminated · Feb 6, 1997 · N949AX · Doug DC931 · Trailing Edge Flaps
  > THE RIGHT WING INBOARD FIXED FLAP VANE HAD DELAMINATION ON THE UPPER SURFACE BETWEEN RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN IAW DC-9 SRM.
- [SDR ABXA9700290](https://openairdocs.org/sdr/ABXA9700290.md): Vane · delaminated · Feb 6, 1997 · N949AX · Doug DC931 · Trailing Edge Flaps
  > LEFT WING INBOARD VANE DELAMINATED. REPLACED HONEYCOMB CORE, DOUBLERS AND SKIN.
- [SDR ABXA9700897](https://openairdocs.org/sdr/ABXA9700897.md): Vane · corroded · Feb 5, 1997 · N949AX · Doug DC931 · Trailing Edge Flaps
  > LEFT INBOARD FIXED VANE CHAFFED AND CORRODED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.
- [SDR ABXA9700604](https://openairdocs.org/sdr/ABXA9700604.md): Spar Cap · corroded · Feb 5, 1997 · N949AX · Doug DC931 · Horizontal Stabilizer, Spar/Rib
  > DURING C-INSPECTION, FOUND THE RIGHT HORIZONTAL STAB INTER SPAR BOX HAS A CORROSION BLEND OUT THAT WAS BLENDED BEYOND LIMITS AT XHS 130. REPAIRED RT HORIZONTAL UPPER REAR SPAR CAP IAW ABX REA D955-18175MR.
- [SDR ABXA9700603](https://openairdocs.org/sdr/ABXA9700603.md): Clip · cracked · Feb 5, 1997 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-INSPECTION, FOUND A SHEAR TIE CLIP CRACKED AT FS 945 BELOW LONGERONS 14 RIGHT AND 15 RIGHT. REPLACED SHEAR TIE CLIP AT FS 945 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9700594](https://openairdocs.org/sdr/ABXA9700594.md): Rib · cracked · Feb 5, 1997 · N949AX · Doug DC931 · Vertical Stabilizer, Spar/Rib
  > DURING C-INSPECTION, FOUND VERTICAL STAB LEADING EDGE 4TH RIB CRACKED RIGHT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.
- [SDR ABXA9700593](https://openairdocs.org/sdr/ABXA9700593.md): Rib · cracked · Feb 5, 1997 · N949AX · Doug DC931 · Vertical Stabilizer, Spar/Rib
  > DURING C-INSPECTION, FOUND VERTICAL STAB LEADING EDGE LOWER SECTION 5 RIB CRACKED, LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.
- [SDR ABXA9700595](https://openairdocs.org/sdr/ABXA9700595.md): Gusset · cracked · Feb 4, 1997 · N949AX · Doug DC931 · Fuselage Miscellaneous Structure
  > DURING C-INSPECTION, FOUND A GUSSET CRACKED ON THE FLOORBEAM AT FS 737 RIGHT BL 30. REPLACED GUSSET IAW DC-9 SRM CHAPTER 51-30-2.
- [SDR ABXA9700589](https://openairdocs.org/sdr/ABXA9700589.md): Spar Cap · corroded · Feb 4, 1997 · N949AX · Doug DC931 · Horizontal Stabilizer, Spar/Rib
  > DURING C-INSPECTION, FOUND LT HORIZONTAL STAB UPPER REAR SPAR CAP AT XHS 181.0 CORRODED. REPAIRED LT HORIZONTAL REAR SPAR CAP IAW ABX REA D955-18219MR.
- [SDR ABXA9700587](https://openairdocs.org/sdr/ABXA9700587.md): Doubler · cracked · Feb 3, 1997 · N949AX · Doug DC931 · Wing Miscellaneous Structure
  > DURING C-INSPECTION, FOUND THE RIGHT WING LEADING EDGE SKIN SEAM DOUBLER AND ATTACH ANGLE AT WS 267 CRACKED. REPLACED LEADING EDGE SEAM DOUBLER IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.
- [SDR ABXA9700596](https://openairdocs.org/sdr/ABXA9700596.md): Door · cracked · Jan 31, 1997 · N949AX · Doug DC931 · Landing Gear Doors
  > DURING C-INSPECTION, FOUND THE LOWER CORNER OF THE LEFT MLG OUTBOARD ARTICULATING DOOR CRACKED. REPLACED THE DOOR IAW DC-9 SRM CHAPTER 51-30-2.
- [SDR ABXA9700592](https://openairdocs.org/sdr/ABXA9700592.md): Rib · cracked · Jan 31, 1997 · N949AX · Doug DC931 · Vertical Stabilizer, Spar/Rib
  > DURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 3 RIB CRACKED LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.

Next page: https://openairdocs.org/deregistered/N949AX-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 = 'N949AX' AND deregistration_id = 'N949AX-2013-09-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N949AX-2013-09-26/reports

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