# Service difficulty reports: N967AX, cancelled May 24, 2017

A list on [N967AX, cancelled May 24, 2017](https://openairdocs.org/deregistered/N967AX-2017-05-24.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 · 92 reports

- [SDR ABXA200811120263](https://openairdocs.org/sdr/ABXA200811120263.md): Battery Pack · discharged · Nov 6, 2008 · N967AX · Doug DC941 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHTS DIM. DEFERRED: 62445 REMOVED AND REPLACED 1.2 VDC BATTERIES IAW 33-53-02-4. OPS CHECK GOOD. BATTERY PACK NEED REPLACED WITHIN 3 FLT DAYS. DEFERRED FOR TRACKING PER AMM 33-53-00-8 & GMM 07.04. MPCW. PLACARD INSTALLED. CODE 2. C
- [SDR ABX2008F00001](https://openairdocs.org/sdr/ABX2008F00001.md): Rod · detached · Jul 19, 2008 · N967AX · Doug DC941 · Flight Compartment Windows
  > F/O WINDOW WOULD NOT OPEN. FOUND LOWER AFT LINKAGE ROD NOT ATTACHED AT THE AFT LOCK BAR. SECURED ROD (ATTACHED) TO AFT LOCK BAR IAW AMM CHAPTER 56. (K)
- [SDR ABXA070325](https://openairdocs.org/sdr/ABXA070325.md): Angle · cracked · Sep 22, 2007 · N967AX · Doug DC941 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON STRUCTURE CRACKED FORWARD OF CONNECTOR. REPAIRED NR 1 PYLON STRUCTURE FORWARD OF CONNECTOR IAW DC9 SSRM DWG K05159.
- [SDR ABXA070046](https://openairdocs.org/sdr/ABXA070046.md): Seal · leaking · Feb 7, 2007 · N967AX · Doug DC941 · Nose/Tail Landing Gear Strut/Axle
  > LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. COMPLIED WITH ABNORMALS. FOUND NLG STRUT SERVICING 50 PSI LOW. STRUT DID NOT EXTEND SMOOTHLY. REPLACED NLG STRUT SEALS IAW DC9 MM 32-21-02-8-0001.
- [SDR ABXA060060](https://openairdocs.org/sdr/ABXA060060.md): Switch · out of position · Jan 27, 2006 · N967AX · Doug DC941 · Cabin Pressure Control System
  > AIRCRAFT DEPRESSURIZED WHILE AT 6000 FEET, OUTFLOW VALVE WAS FULL CLOSED. THE AIR CONDITIONING SUPPLY SWITCHES WERE ON AND PRESSURIZATION WAS SET FOR LANDING. PRESSURIZED AIRCRAFT TO MAXIMUM DIFFERENTIAL PRESSURE WITH NO PROBLEMS NOTED. INSPECTED LINKAGE TO
- [SDR ABXA050254](https://openairdocs.org/sdr/ABXA050254.md): Frame · cracked · Oct 7, 2005 · N967AX · Doug DC941 · Fuselage Main, Frame
  > ADDITIONAL CRACK FOUND IN LEFT AFT MAIN FRAME FORWARD FLANGE. FRAME IS OUT OF REPAIR LIMITS IAW ES00916 DUE TO CRACKS IN BOTH FLANGES. REPLACED MAIN FRAME ON EA 53400325-001-5.
- [SDR ABXA050253](https://openairdocs.org/sdr/ABXA050253.md): Support Fitting · cracked · Oct 6, 2005 · N967AX · Doug DC941 · Fuselage Main, Attach Fittings
  > LEFT SUPPORT FITTING CRACKED CANTED BULKHEAD 1219, LT OF RUDDER TORQUE TUBE MECHANISM. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-2.
- [SDR ABXA050252](https://openairdocs.org/sdr/ABXA050252.md): Seat Track · cracked · Oct 6, 2005 · N967AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WAS CRACKED 2 PLACES BETWEEN FS 160 AND 200 AT LEFT BUTT LINE 41.5. REPAIRED DAMAGED AREAS (2 EA) IAW DC-9 SSRM DWG K05159.
- [SDR ABXA050251](https://openairdocs.org/sdr/ABXA050251.md): Fitting · cracked · Oct 6, 2005 · N967AX · Doug DC941 · Spoilers
  > LEFT INBOARD SPOILER HAD AN APPROXIMATE.1562 INCH CRACK IN THE CENTER DOUBLER ABOVE THE CENTER DRIVE FITTING. BLENDED CRACK IAW REA D957-52510.
- [SDR ABXA050250](https://openairdocs.org/sdr/ABXA050250.md): Skin · corroded · Oct 4, 2005 · N967AX · Doug DC941 · Fuselage Main, Plate/Skin
  > AREA OF BULGING AND DISHED RIVETS - FS 626 AT LONGERON 26 LEFT. EXFOLIATED DOUBLER ON THE INSIDE, ABOVE HAT CHANNEL. REPAIRED AREA IAW REA D953-52507.
- [SDR ABXA040076](https://openairdocs.org/sdr/ABXA040076.md): Longeron · cracked · Feb 10, 2004 · N967AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > STA. 1040 LONGERON 17 LT CRACKED. SPLICED IN NEW SECTION OF LONGERON IAW DC-9 SRM 53-02.
- [SDR ABXA040075](https://openairdocs.org/sdr/ABXA040075.md): Bulkhead · cracked · Feb 9, 2004 · N967AX · Doug DC941 · Nacelle/Pylon, Bulkhead/Firewall
  > LT FORWARD PYLON BULKHEAD WAS CRACKED AT BOTTOM AT LT BUTT LINE 44.0. REPAIRED LT FORWARD PYLON BULKHEAD IAW DC-9 SRM 53-03.
- [SDR ABXA040074](https://openairdocs.org/sdr/ABXA040074.md): Frame · cracked · Feb 6, 2004 · N967AX · Doug DC941 · Fuselage Main, Frame
  > STA 775 AFT OVERWHEEL WELL FRAME WAS CRACKED BETWEEN POINTS E AND E IN AFT OB POCKET AND CRACKED BETWEEN POINTS H AND I IN AFT IB POCKET AND CRACKED IN FORWARD IB POCKET BETWEEN FASTENERS THAT ARE LOCATED BETWEEN POINTS H AND I. FORWARD IB POCKET CRACK EMINA
- [SDR ABXA040072](https://openairdocs.org/sdr/ABXA040072.md): Frame · cracked · Feb 6, 2004 · N967AX · Doug DC941 · Fuselage Main, Frame
  > EDDY CURRENT INDICATED LT MAIN FRAME AT FS 737 CRACKED AT AFT SIDE AT POINT J TO POINT G. REPAIRED IAW J.C. EA 53400110-001-2.
- [SDR ABXA040070](https://openairdocs.org/sdr/ABXA040070.md): Fitting · corroded · Feb 6, 2004 · N967AX · Doug DC941 · Fuselage Main, Attach Fittings
  > LONGERON 23 RT END CAP EXFOLIATED AT FS 1065. REPLACED LONGERON 23 RT END CAP USING P/N 3914590-1N IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA040071](https://openairdocs.org/sdr/ABXA040071.md): Web · cracked · Feb 6, 2004 · N967AX · Doug DC941 · Fuselage Miscellaneous Structure
  > CUSP WEB CRACKED FROM F.S. 1025-1039 APPROXIMATELY LT BUTT LINE 56. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.
- [SDR ABXA040066](https://openairdocs.org/sdr/ABXA040066.md): Rib · cracked · Feb 5, 2004 · N967AX · Doug DC941 · Wing, Rib/Bulkhead
  > RT WING LE HAD CRACKED RIB AT LOWER NUTPLATES FOR NR 2 IB SLAT TRACK RIB. FOUND 4 CRACKS, REPAIRED IAW REA D957-49005 AND INSTALLED NUTPLATES IAW DC-9 SRM 51-30-2.
- [SDR ABXA040073](https://openairdocs.org/sdr/ABXA040073.md): Support · cracked · Feb 5, 2004 · N967AX · Doug DC941 · Fuselage Miscellaneous Structure
  > VERTICAL SUPPORT NR 7 CRACKED FORWARD SIDE OF FORWARD AUX TANK. REPLACED VERTICAL SUPPORT NR 7 IAW DC-9 SRM 51-30-1.
- [SDR ABXA040069](https://openairdocs.org/sdr/ABXA040069.md): Nose Cowl · cracked · Feb 5, 2004 · N967AX · Doug DC941 · Engine Cowling System
  > NOSE COWL CRACKED 3 PLACES 6:00 POSITION AT NOSE COWL ANTI-ICE DUCT. INSTALLED ANTI-ICE DUCT IAW DC-9 MM 71-10-01-2-0001, REPLACED DOUBLER IAW DOUGLAS DWG 5959155.
- [SDR ABXA040068](https://openairdocs.org/sdr/ABXA040068.md): Skin · damaged · Feb 5, 2004 · N967AX · Doug DC941 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR'S EXTERIOR SKIN WAS DAMAGED AT LOWER EDGE 3 PLACES. REPAIRED AREA IAW REA D952-49012.
- [SDR ABXA040067](https://openairdocs.org/sdr/ABXA040067.md): Intercostal · cracked · Feb 5, 2004 · N967AX · Doug DC941 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR HAD CRACKED INTERCOSTAL AT AFT HINGE. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR ABXA020045](https://openairdocs.org/sdr/ABXA020045.md): Bulkhead · cracked · Jun 19, 2002 · N967AX · Doug DC941 · Fuselage Main, Bulkhead
  > CRACK IN LEFT BULKHEAD WEB, FS 1041 AT LONGERON 17L, INBOARD END. REPAIRED BULKHEAD IAW DC-9 SRM 53-01.
- [SDR ABXA020044](https://openairdocs.org/sdr/ABXA020044.md): Floorbeam · cracked · Jun 19, 2002 · N967AX · Doug DC941 · Fuselage Main, Floor Beam
  > FLOORBEAM SUPPORT CRACKED AT LOWER END, FS 617 AND LONGERON 23L. REPAIRED FLOOR BEAM SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5.
- [SDR ABXA020043](https://openairdocs.org/sdr/ABXA020043.md): Longeron · cracked · Jun 18, 2002 · N967AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 17, STATION 408, WAS CRACKED APPROXIMATELY.5-.75 INCH. REPAIRED LONGERON 17 IAW DC-9 SRM 53-02.
- [SDR ABXA020042](https://openairdocs.org/sdr/ABXA020042.md): Longeron · cracked · Jun 18, 2002 · N967AX · Doug DC941 · Fuselage Main, Longeron/Stringer
  > LONGERON 17, STATION 389, WAS CRACKED APPROXIMATELY 3/4 INCH. REPAIRED LONGERON 17 IAW DC-9 SRM 53-02.
- [SDR ABXA020041](https://openairdocs.org/sdr/ABXA020041.md): Pan · cracked · Jun 18, 2002 · N967AX · Doug DC941 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR INNER PAN, WAS CRACKED IN RADIUS BELOW AFT LATCH. REPAIRED AREA IAW DC-9 SRM 52-05.
- [SDR ABXA010720](https://openairdocs.org/sdr/ABXA010720.md): Clip · defective · Feb 13, 2002 · N967AX · Doug DC941 · Flight Compartment Lighting
  > SMOKE FROM FIRST OFFICER'S YOKE CLIPBOARD LIGHT. TRIPPED MAP AND BRIEFCASE LIGHT CIRCUIT BREAKER. REMOVED METAL CLIP FROM FIRST OFFICER'S CLIPBOARD IAW DC-9 MM 33-10-00.
- [SDR ABXA010719](https://openairdocs.org/sdr/ABXA010719.md): Rheostat · malfunctioned · Feb 12, 2002 · N967AX · Doug DC941 · Flight Compartment Lighting
  > BURNING SMELL FROM FIRST OFFICER'S YOKE FOLLOWED BY MAP AND BRIEFCASE CIRCUIT BREAKER TRIPPING. REPLACED FIRST OFFICER'S BRIEFCASE RHEOSTAT IAW DC-9 AMM 33-10-00-2.
- [SDR ABXA010220](https://openairdocs.org/sdr/ABXA010220.md): Structure · vibration · May 8, 2001 · N967AX · Doug DC941 · Fuselage Main, Structure
  > ON FINAL APPROACH WITH FLAPS EXTENDED TO 25 DEGREES, THE AIRCRAFT EXPERIENCED VIBRATIONS AND UNUSUAL NOISE. THE AIRCRAFT CONTINUED THE APPROACH AND LANDED WITH FLAPS AT 25 DEGREES. MAINTENANCE INSPECTED THE FLAPS, FAIRINGS BUTT DOORS, FIXED AND MOVABLE VANES
- [SDR ABXA010212](https://openairdocs.org/sdr/ABXA010212.md): Engine · failed · Apr 30, 2001 · N967AX · Doug DC941 · Engine (Turbine/Turboprop)
  > THE RIGHT ENGINE (NR 2) EXPERIENCED AN UNCOMMANDED SHUT DOWN DURING THE LANDING FLARE. MAINTENANCE COMPLETED VISUAL INSPECTIONS OF THE INTAKE AND EXHAUST. NO DEFECTS WERE NOTED. THE RIGHT ENGINE FUEL FILTER WAS REPLACED AS A PRECAUTION. NO DEFECTS WERE NOT
- [SDR ABXA0100005](https://openairdocs.org/sdr/ABXA0100005.md): Unknown · odor · Jan 15, 2001 · N967AX · Doug DC941 · Air Distribution System
  > FLIGHT CREW REPORTED AN ELECTRICAL ODOR WAS NOTED IN THE AIRCRAFT DURING CLIMB. THE RIGHT CSD TEMPERATURE WAS NOTED TO BE IN THE UPPER YELLOW SCALE. ABNORMAL CSD PROCEDURES WERE PERFORMED BY THE CREW. THE CSD TEMPERATURE THEN DECREASED TO BELOW CAUTION RANG
- [SDR ABXA0000001](https://openairdocs.org/sdr/ABXA0000001.md): Bulb · failed · Dec 30, 1999 · N967AX · Doug DC941 · Landing Gear Position and Warning
  > ON LANDING, WHEN GEAR WAS LOWERED, THE GEAR DOOR OPEN LIGHT WOULD NOT ILLUMINATE. PRESS TO TEST WAS OK. REPLACED GEAR DOOR OPEN LIGHT BULB.
- [SDR ABXA9900360](https://openairdocs.org/sdr/ABXA9900360.md): Bulkhead Jamb · cracked · May 10, 1999 · N967AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB, RIGHT UPPER CORNER CRACKED. REPAIRED IAW DC9 SRM 53-03.
- [SDR ABXA9900359](https://openairdocs.org/sdr/ABXA9900359.md): Bulkhead Jamb · cracked · May 10, 1999 · N967AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB UPPER CORNER CRACKED. REPAIRED CRACK IAW DC9 SRM 53-03.
- [SDR ABXA9900358](https://openairdocs.org/sdr/ABXA9900358.md): Spar Cap · cracked · May 10, 1999 · N967AX · Doug DC941 · Wing Spar
  > DURING C-CHECK, FOUND LEFT WING REAR SPAR CAP CRACKED AT NUMEROUS HOLES. REPAIRED IAW ABX REA D957-28455MR.
- [SDR ABXA9800589](https://openairdocs.org/sdr/ABXA9800589.md): Latch · loose · Jun 30, 1998 · N967AX · Doug DC941 · Fixed Inner Doors
  > COCKPIT DOOR LATCH LOOSE ON THE INSIDE, SOMETIMES WOULD BIND. REPLACED LATCH ASSY.
- [SDR ABXA9800588](https://openairdocs.org/sdr/ABXA9800588.md): Latch · inoperative · Jun 29, 1998 · N967AX · Doug DC941 · Fixed Inner Doors
  > COCKPIT DOOR INSIDE LATCH INOPERATIVE. CREW WAS UNABLE TO OPEN DOOR FROM COCKPIT. REPAIRED AS REQUIRED.
- [SDR ABXA9800446](https://openairdocs.org/sdr/ABXA9800446.md): Drive Link · cracked · May 11, 1998 · N967AX · Doug DC941 · Engine Thrust Reverser
  > DURING COMPLIANCE WITH AD 96-10-11 AND AD 75-14-06, FOUND NR 2 ENGINE THRUST REVERSER, UPPER, LEFT, DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 MM 78-31-5.
- [SDR ABXA9800036](https://openairdocs.org/sdr/ABXA9800036.md): Latch · out of adjust · Jan 22, 1998 · N967AX · Doug DC941 · Fixed Inner Doors
  > COCKPIT DOOR WOULD NOT OPEN. LUBRICATED AND ADJUSTED DOOR LATCH ASSEMBLY.
- [SDR ABXA9701681](https://openairdocs.org/sdr/ABXA9701681.md): Latch Assy · defective · Oct 17, 1997 · N967AX · Doug DC941 · Fixed Inner Doors
  > DURING MAINTENANCE CHECK, FOUND COCKPIT DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. REINSTALLED TUMBLER MECHANISM INSIDE DOOR HANDLE.
- [SDR ABXA9701624](https://openairdocs.org/sdr/ABXA9701624.md): Latch · worn · Oct 14, 1997 · N967AX · Doug DC941 · Fixed Inner Doors
  > COCKPIT DOOR WOULD NOT OPEN FROM THE INSIDE. REPAIRED THE LATCH ASSEMBLY. OPS CHECKED GOOD.
- [SDR ABXA9701517](https://openairdocs.org/sdr/ABXA9701517.md): Fitting · corroded · Sep 24, 1997 · N967AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND THE SUPPORT FITTING ON TOP OF THE CENTER WING FUEL TANK AT STA 645 BELOW THE LT CUSP WEB EXFOLIATED. REPLACED FITTING IAW DC9 SRM 51-30-5 AND ABX REA D953-21067-DE.
- [SDR ABXA9701516](https://openairdocs.org/sdr/ABXA9701516.md): Web · cracked · Sep 24, 1997 · N967AX · Doug DC941 · Horizontal Stabilizer Structure
  > DURING C-CHECK, FOUND THE RIGHT HORIZONTAL STABILIZER LEADING EDGE WEB CRACKED BETWEEN STA XRS.83.624 AND 145.000. REPAIRED WEB IAW ABX REA D955-20896.
- [SDR ABXA9701515](https://openairdocs.org/sdr/ABXA9701515.md): Angle · cracked · Sep 24, 1997 · N967AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND A CRACKED ANGLE AT STA 1041 AND LONGERON 18 LEFT, UNDER CUSP WEB. REPAIRED ANGLE IAW ABX REA D953-20903-MR.
- [SDR ABXA9701511](https://openairdocs.org/sdr/ABXA9701511.md): Cusp Web · cracked · Sep 22, 1997 · N967AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND LT CUSP WEB AT STA 1040 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.
- [SDR ABXA9701510](https://openairdocs.org/sdr/ABXA9701510.md): Frame · cracked · Sep 22, 1997 · N967AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND THE MAINFRAME AT STA 655 LEFT CRACKED AT BASE OF FRAME JUST BELOW LONGERON 18L. REPAIRED FRAME IAW ABX REA D953-2092-MR AND DC9 SRM 53-03.
- [SDR ABXA9701512](https://openairdocs.org/sdr/ABXA9701512.md): Blkhd Fitting · cracked · Sep 19, 1997 · N967AX · Doug DC941 · Fuselage Main, Bulkhead
  > DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING AT THE LOWER RT STOP PAD ATTACH FASTENER HOLE CRACKED. REPLACED THE FITTING IAW DC9 SRM 51-30-5 AND 51-30-5.
- [SDR ABXA9701504](https://openairdocs.org/sdr/ABXA9701504.md): Cusp Web · cracked · Sep 19, 1997 · N967AX · Doug DC941 · Fuselage Miscellaneous Structure
  > DURING C-CHECK, FOUND RT CUSP WEB AT STA 665 TO 677 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.
- [SDR ABXA9701503](https://openairdocs.org/sdr/ABXA9701503.md): Frame · cracked · Sep 19, 1997 · N967AX · Doug DC941 · Fuselage Main, Frame
  > DURING C-CHECK, FOUND THE LT MAINFRAME AT STA 775 CENTER POCKET AFT LOWER FLANGE CRACKED. REPAIRED FRAME IAW ABX REA D953-20786-MR.
- [SDR ABXA9701502](https://openairdocs.org/sdr/ABXA9701502.md): Fixed Vane · delaminated · Sep 19, 1997 · N967AX · Doug DC941 · Wing Miscellaneous Structure
  > DURING C-CHECK, FOUND THE CENTER FIXED VANE TOP SIDE DELAMINATED. REPLACED VANE IAW DC9 MM 27-51-3.

Next page: https://openairdocs.org/deregistered/N967AX-2017-05-24/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 = 'N967AX' AND deregistration_id = 'N967AX-2017-05-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N967AX-2017-05-24/reports

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