# Service difficulty reports: N971AX, cancelled Nov 18, 2009

A list on [N971AX, cancelled Nov 18, 2009](https://openairdocs.org/deregistered/N971AX-2009-11-18.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 · 83 reports

- [SDR ABXA080238](https://openairdocs.org/sdr/ABXA080238.md): Battery · defective · Sep 5, 2008 · N971AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8.
- [SDR ABXA080140](https://openairdocs.org/sdr/ABXA080140.md): Battery · discharged · Apr 28, 2008 · N971AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8.
- [SDR ABXA070024](https://openairdocs.org/sdr/ABXA070024.md): Seat Track · corroded · Jan 17, 2007 · N971AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT BUTT LINE 54, STA 225, SEAT TRACK HAD EXFOLIATION CORROSION. REMOVED & REPLACED SEAT TRACK SECTION IAW DC9 SRM 51-10-4 AND 51-30-1.
- [SDR ABXA070023](https://openairdocs.org/sdr/ABXA070023.md): Threshold · cracked · Jan 15, 2007 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO DOOR THRESHOLD WEB HAD IMPROPERLY INSTALLED RIVET THAT HAD CRACKED THE WEB BETWEEN STA 389 - 408. REMOVED AND INSTALLED NEW INTERCOSTAL AND REPAIRED AREA IAW REA D953-55-335MR.
- [SDR ABXA070022](https://openairdocs.org/sdr/ABXA070022.md): Rivet · sheared · Jan 12, 2007 · N971AX · Doug DC941 · Fuselage, Stabilizer Attach Fittings
  > LEFT VERTICAL STAB ATTACH ANGLE CHECKED AND HAD 2 SHEARED RIVETS. REPAIRED LEFT VERTICAL STAB ATTACH ANGLE IAW DC9 SRM 53-05, FIG 23.
- [SDR ABXA070021](https://openairdocs.org/sdr/ABXA070021.md): Skin · corroded · Jan 12, 2007 · N971AX · Doug DC941 · Wing, Plate/Skin
  > RIGHT WING UPPER SKIN BULGED AT REMOVEABLE TRAILING EDGE AND PANEL NR 1252. REPAIRED RIGHT WING UPPER SKIN BULGE ON TRAILING EDGE PANEL IAW DC9 SRM 51-10-4.
- [SDR ABXA070020](https://openairdocs.org/sdr/ABXA070020.md): Spar Cap · corroded · Jan 12, 2007 · N971AX · Doug DC941 · Wing Spar
  > LEFT WING LOWER OUTBOARD SPAR CAP CORRODED, RIVETS POPPED, CUPPED AND SKIN BULGING AT XRS 509. REPAIRED LEFT WING LOWER OUTBOARD SPAR CAP IAW REA D957-55323MR.
- [SDR ABXA060282](https://openairdocs.org/sdr/ABXA060282.md): Battery · discharged · Oct 23, 2006 · N971AX · Doug DC941 · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00.
- [SDR ABXA050028](https://openairdocs.org/sdr/ABXA050028.md): Floorbeam · corroded · Jan 31, 2005 · N971AX · Doug DC941 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED ON LOWER FLANGE STA 1013 AT CARGO DOOR UPLATCH BRACKET. REPAIRED IAW DC-9 SSRM K07411.
- [SDR ABXA050027](https://openairdocs.org/sdr/ABXA050027.md): Attach Angle · cracked · Jan 20, 2005 · N971AX · Doug DC941 · Nacelle/Pylon, Main Frame
  > LOWER LEFT PYLON ATTACH ANGLE WAS CRACKED INBOARD OF PYLON ACCESS PANEL 8101. REPAIRED AREA IAW DC-9 SRM 54-04.
- [SDR ABXA050026](https://openairdocs.org/sdr/ABXA050026.md): Cusp Web · cracked · Jan 17, 2005 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED AT FS 984, 1010, 1030 - 1040, LEFT BUTT LINE 54, UNDER SEAT TRACK. REPLACED CUSP WEB IAW DC-9 SRM 51-30-1 AND 51-30-2.
- [SDR ABXA040386](https://openairdocs.org/sdr/ABXA040386.md): Structure · vibration · Nov 24, 2004 · N971AX · Doug DC841 · Fuselage Main, Structure
  > IN DESCENT THROUGH APPROX 16,000 FEET AND AROUND 300 KTS, THERE WAS A NOTICABLE AIRFRAME VIBRATION THAT LASTED UNTIL WE SLOWED THROUGH ABOUT 270 KTS. ENGINE/POWER CHANGES HAD NOT NOTICABLE EFFECT ON THE VIBRATION. NO INDICATION OF ANY ENGINES PROBLEMS WERE N
- [SDR ABXA040376](https://openairdocs.org/sdr/ABXA040376.md): Structure · vibration · Nov 7, 2004 · N971AX · Doug DC941 · Aircraft Structures
  > IN DESCENT, LEVELED OFF AT 300 KIAS, INCURRED VIBRATION, SLOWED TO 290 KIAS, VIBRATION WENT AWAY THEN CAME BACK AGAIN WHEN ACCELERATING THROUGH 295 KIAS. INSPECTED FOR GENERAL CONDITION & SECURITY OF THE FOLLOWING ITEMS: NOSE GEAR AREA, FUSELAGE, FLAPS, SLATS
- [SDR ABXA040375](https://openairdocs.org/sdr/ABXA040375.md): Vane · damaged · Nov 5, 2004 · N971AX · Doug DC941 · Trailing Edge Flaps
  > AIRFRAME RUMBLE/VIBRATION AT 285 KTS WITH AIRCRAFT CLEAN, VIBRATION CAN BE FELT THROUGH FLOOR AND RUDDER PEDALS. REPLACED RT FLAP FORWARD MOVABLE VANE IAW DC9 MM 27-51-02-4-0001. REPLACED BUSHING IN EYEBOLT ON RT WING T/E UPPER I/B PANEL SUPPORT. REPLACED S
- [SDR ABXA030291](https://openairdocs.org/sdr/ABXA030291.md): Support Fitting · cracked · Jul 4, 2003 · N971AX · Doug DC941 · Wing, Attach Fittings
  > LEFT INBOARD SPOILER TORSION BAR SUPPORT FITTING CRACKED AT UPPER END. REPLACED FITTING IAW DC-9 SRM 51-30-1, 51-30-2, AND 51-30-5.
- [SDR ABXA030290](https://openairdocs.org/sdr/ABXA030290.md): Support Bracket · cracked · Jul 4, 2003 · N971AX · Doug DC941 · Spoilers
  > LEFT INBOARD SPOILER TORSION BAR SUPPORT BRACKET CRACKED AT UPPER END. REPLACED SUPPORT IAW SRM 51-30-1 AND 51-30-5.
- [SDR ABXA030289](https://openairdocs.org/sdr/ABXA030289.md): Support Bracket · cracked · Jul 2, 2003 · N971AX · Doug DC941 · Spoilers
  > LEFT OUTBOARD SPOILER TORSION BAR OUTBOARD SUPPORT BRACKET CRACKED AT UPPER END. REPLACED SUPPORT BRACKET FOR LEFT OUTBOARD SPOILER TORSION BAR IAW DC-9 SRM.
- [SDR ABXA010154](https://openairdocs.org/sdr/ABXA010154.md): Downlock Switch · stuck · Apr 17, 2001 · N971AX · Doug DC941 · Landing Gear Position and Warning
  > DURING CLIMBOUT A RED GEAR UNSAFE LIGHT ILLUMINATED FOR THE RIGHT MAIN LANDING GEAR. THE CREW COMPLIED WITH THE ABNORMAL CHECKLIST AND CONTINUED OPERATIONS. MAINTENANCE INSPECTED AND FOUND THE RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH TO BE STICKING. MAINTENA
- [SDR ABXA000473](https://openairdocs.org/sdr/ABXA000473.md): Screw · corroded · Oct 20, 2000 · N971AX · Doug DC941 · Empennage Structure
  > JACKSCREW ASSY CORRODED AND GALLED, NUT WORN AND CORRODED AND WASHER CORRODED.REPLACED ASSY IAW DC9 OHM 27-41-1.
- [SDR ABXA000134](https://openairdocs.org/sdr/ABXA000134.md): Frame · corroded · Feb 24, 2000 · N971AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND FUSELAGE FRAME AT STA 889 AND LONGERON 30 CORRODED BEYOND LIMITS. REPLACED FRAME IAW DC9 SRM 51-30-2.
- [SDR ABXA000120](https://openairdocs.org/sdr/ABXA000120.md): Skin · cracked · Feb 22, 2000 · N971AX · Doug DC941 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS CRACKED AROUND THE NOSE LANDING GEAR LEFT AFT DOOR HINGE CUTOUT. REPAIRED SKIN IAW DC9 SRM 53-05, FIGURE 62.
- [SDR ABXA000119](https://openairdocs.org/sdr/ABXA000119.md): Panel · delaminated · Feb 21, 2000 · N971AX · Doug DC941 · Wing, Plate/Skin
  > PANEL 1246A WAS DELAMINATED AND SEPARATED. REPLACED PANEL IAW DC9 SRM 51-10-4.
- [SDR ABXA000118](https://openairdocs.org/sdr/ABXA000118.md): Frame · corroded · Feb 17, 2000 · N971AX · Doug DC941 · Fuselage Main, Frame
  > FRAME IN KEEL AREA AT STA 660 AND LONGERON 29L WAS CORRODED BEYOND LIMITS. REPLACED FRAME IAW DC9 SRM 51-30-5.
- [SDR ABXA000117](https://openairdocs.org/sdr/ABXA000117.md): Frame · cracked · Feb 17, 2000 · N971AX · Doug DC941 · Fuselage Main, Frame
  > E&E COMPARTMENT FRAME ANGLE WAS CRACKED AT STA FS 148 AND LONGERON 27R. REPLACED ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA000116](https://openairdocs.org/sdr/ABXA000116.md): Skin · delaminated · Feb 17, 2000 · N971AX · Doug DC941 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR OUTBOARD DOOR WAS DELAMINATED BEYOND LIMITS. REPLACED DOOR IAW DC9 SRM 51-30-2 AND DC9 OHM 32-10-6.
- [SDR ABXA000115](https://openairdocs.org/sdr/ABXA000115.md): Panel · delaminated · Feb 17, 2000 · N971AX · Doug DC941 · Wing, Plate/Skin
  > PANEL 1142A WAS DELAMINATED AND SEPARATED. REPLACED PANEL IAW DC9 SRM.
- [SDR ABXA000114](https://openairdocs.org/sdr/ABXA000114.md): Angle · cracked · Feb 17, 2000 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ATTACH ANGLE AT STATION 617 AND LONGERON 19R WAS CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-5.
- [SDR ABXA000113](https://openairdocs.org/sdr/ABXA000113.md): Fitting · cracked · Feb 17, 2000 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > FITTING IN KEEL AREA AT STA 675 AND LONGERON 29L WAS CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-4.
- [SDR ABXA9900860](https://openairdocs.org/sdr/ABXA9900860.md): Battery Pack · discharged · Dec 27, 1999 · N971AX · Doug DC941 · Emergency Lighting
  > EMERGENCY LIGHTS WERE INOPERATIVE. REPAIRED SHORTED WIRE AT EMERGENCY BATTERY PACK AND REPLACED BATTERY POWER SUPPLY.
- [SDR ABXA9800585](https://openairdocs.org/sdr/ABXA9800585.md): Fitting · cracked · Jun 26, 1998 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FITTING (P/N 3925817-1) CRACKED LBL 44.5 STATION 718. REPLACED SEAT TRACK SUPPORT FITTING IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA9800584](https://openairdocs.org/sdr/ABXA9800584.md): Fitting · cracked · Jun 26, 1998 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FITTING (P/N 3925817-1) CRACKED LBL 22 STATION 677. REPLACED SEAT TRACK SUPPORT FITTING IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA9800583](https://openairdocs.org/sdr/ABXA9800583.md): Skin · corrosion · Jun 26, 1998 · N971AX · Doug DC941 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED STATION 185 TO 173 LONGERON 27 LEFT. REPLACED LONGERON IAW DC9 SRM 53-04-00 AND SRM 51-10-3.
- [SDR ABXA9800582](https://openairdocs.org/sdr/ABXA9800582.md): Longeron · cracked · Jun 26, 1998 · N971AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160. REPLACED LONGERON 4 LEFT IAW DC9 SRM 51-30-2, 51-30-1 AND 51-30-5.
- [SDR ABXA9800581](https://openairdocs.org/sdr/ABXA9800581.md): Skin · corrosion · Jun 26, 1998 · N971AX · Doug DC941 · Elevator, Plate/Skin
  > DURING C-CHECK, FOUND CORROSION ON RIGHT ELEVATOR SKIN AT STATION XE 49. REPLACED SKIN IAW DACO DWG 5910412.
- [SDR ABXA9800580](https://openairdocs.org/sdr/ABXA9800580.md): Fitting · cracked · Jun 26, 1998 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND FITTING AT LBL 44.5 STATION 696 CRACKED. REPLACED SEAT TRACK SUPPORT FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA9800525](https://openairdocs.org/sdr/ABXA9800525.md): Bracket · cracked · Jun 17, 1998 · N971AX · Doug DC941 · Vertical Stabilizer
  > DURING C-CHECK, FOUND THE SUPPORT BRACKET FOR THE RIGHT VOR ANTENNA IN THE VERTICAL STABILIZER LEADING EDGE ASSY CRACKED. REPLACED SUPPORT BRACKET IAW DC9 SRM 51-30-2.
- [SDR ABXA9800524](https://openairdocs.org/sdr/ABXA9800524.md): Frame · cracked · Jun 17, 1998 · N971AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND FRAME CRACKED AT FS 1056 AND LONGERON 16L. REPAIRED FRAME IAW DC9 SRM 53-03.
- [SDR ABXA9701798](https://openairdocs.org/sdr/ABXA9701798.md): Bulb · failed · Nov 3, 1997 · N971AX · Doug DC941 · Emergency Lighting
  > DURING PREFLIGHT INSPECTION, FOUND EMERGENCY LIGHT UNDER COCKPIT GLARESHIELD WAS INOPERATIVE. REPLACED LIGHT BULB FOR EMERGENCY LIGHT UNDER GLARESHIELD.
- [SDR ABXA9701193](https://openairdocs.org/sdr/ABXA9701193.md): Uplock Switch · worn · Jul 2, 1997 · N971AX · Doug DC941 · Landing Gear Position and Warning
  > AFTER TAKEOFF, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. LANDING WAS UNEVENTFUL. REPLACED LEFT MLG UPLOCK SWITCH, OPS CHECKED GOOD IAW DC9 MM 32-60-0.
- [SDR ABXA9701106](https://openairdocs.org/sdr/ABXA9701106.md): Fitting · corroded · May 31, 1997 · N971AX · Doug DC941 · Horizontal Stabilizer Structure
  > DURING COMPLIANCE WITH AD 82-06-02 AND 92-22-08, FOUND HORIZONTAL STABILIZER UPPER AFT FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-1.
- [SDR ABXA9701104](https://openairdocs.org/sdr/ABXA9701104.md): Frame · cracked · May 31, 1997 · N971AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND THE LEFT MAIN FRAME STATION 737, CRACKED ON FWD AND AFT UPPER FLANGES. REPLACED FRAME IAW DC9 S/B 53-131.
- [SDR ABXA9700172](https://openairdocs.org/sdr/ABXA9700172.md): Doubler · corroded · Dec 7, 1996 · N971AX · Doug DC941 · Wing Miscellaneous Structure
  > DURING C-CHECK, FOUND LEVEL 2 CORRSION ON LEFT MAIN LANDING GEAR DOUBLER. REPAIRED IAW DC-9 SRM 51-10-3, FIGURE 6.
- [SDR ABXA9700180](https://openairdocs.org/sdr/ABXA9700180.md): Fitting · gouged · Dec 4, 1996 · N971AX · Doug DC941 · Wing, Control Surface Attach Fittings
  > DURING C-CHECK, FOUND LEFT WING INBOARD SPOILER FITTING GOUGED. REPAIRED THE LEFT WING INBOARD FITTING IAW ABX REA D957-17399-MR.
- [SDR ABXA9700177](https://openairdocs.org/sdr/ABXA9700177.md): Frame · cracked · Dec 3, 1996 · N971AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND FS 737 LEFT MAIN FRAME CRACKED. REPAIRED LEFT MAIN FRAME AT FS 737 IAW ABX REA D953-17381.
- [SDR ABXA9700173](https://openairdocs.org/sdr/ABXA9700173.md): Angle · cracked · Dec 3, 1996 · N971AX · Doug DC941 · Nacelle/Pylon Structure
  > DURING C-CHECK, FOUND REPAIR ON UPPER PYLON ATTACH ANGLE CRACKED ON LEFT PYLON. REPAIRED IAW DC-9 SRM 54-04, FIGURE 10.
- [SDR ABXA9700178](https://openairdocs.org/sdr/ABXA9700178.md): Blkhd Stiffener · gouged · Dec 2, 1996 · N971AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND VERTICAL STIFFENER GOUGED ON FORWARD BULKHEAD IN ALC COMPARTMENT. REPAIRED VERTICAL STIFFENER IAW ABX REA D953-17379-MR.
- [SDR ABXA9700174](https://openairdocs.org/sdr/ABXA9700174.md): Clip · corroded · Dec 2, 1996 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND LEVEL 2 CORROSION ON CLIP AT BASE OF FRAME 168. FABRICATED CLIP IAW DAC DRAWING 9911516, INSTALLED IAW DC-9 SRM 51-30-2.
- [SDR ABXA9700188](https://openairdocs.org/sdr/ABXA9700188.md): Window Frame · cracked · Dec 1, 1996 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND WINDOW FRAME BETWEEN STATION 677-697 LEFT. REPAIRED WINDOW FRAME BETWEEN STATION 677-697 LEFT, IAW ABX REA D953-17346.
- [SDR ABXA9700184](https://openairdocs.org/sdr/ABXA9700184.md): Window Frame · cracked · Dec 1, 1996 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND WINDOW FRAME CRACKED AT STATION 617 RIGHT. REPAIRED WINDOW FRAME AT STATION 617 RIGHT IAW ABX REA D953-17346.
- [SDR ABXA9700179](https://openairdocs.org/sdr/ABXA9700179.md): Window Frame · cracked · Dec 1, 1996 · N971AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND WINDOW FRAME CRACKED BETWEEN STATION 718-737. REPAIRED THE WINDOW FRAME IAW ABX REA D953-17384.

Next page: https://openairdocs.org/deregistered/N971AX-2009-11-18/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 = 'N971AX' AND deregistration_id = 'N971AX-2009-11-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N971AX-2009-11-18/reports

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