N967AX, cancelled May 24, 2017

Service difficulty reports · 92

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ABXA200811120263Battery Pack · dischargedCOCKPIT 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. CNov 6, 2008 · N967AX · Doug DC941 · Emergency LightingSDR ABX2008F00001Rod · detachedF/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)Jul 19, 2008 · N967AX · Doug DC941 · Flight Compartment WindowsSDR ABXA070325Angle · crackedNR 1 PYLON STRUCTURE CRACKED FORWARD OF CONNECTOR. REPAIRED NR 1 PYLON STRUCTURE FORWARD OF CONNECTOR IAW DC9 SSRM DWG K05159.Sep 22, 2007 · N967AX · Doug DC941 · Nacelle/Pylon Miscellaneous StructureSDR ABXA070046Seal · leakingLANDING 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.Feb 7, 2007 · N967AX · Doug DC941 · Nose/Tail Landing Gear Strut/AxleSDR ABXA060060Switch · out of positionAIRCRAFT 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 TOJan 27, 2006 · N967AX · Doug DC941 · Cabin Pressure Control SystemSDR ABXA050254Frame · crackedADDITIONAL 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.Oct 7, 2005 · N967AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050253Support Fitting · crackedLEFT SUPPORT FITTING CRACKED CANTED BULKHEAD 1219, LT OF RUDDER TORQUE TUBE MECHANISM. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-2.Oct 6, 2005 · N967AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050252Seat Track · crackedSEAT 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.Oct 6, 2005 · N967AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA050251Fitting · crackedLEFT INBOARD SPOILER HAD AN APPROXIMATE .1562 INCH CRACK IN THE CENTER DOUBLER ABOVE THE CENTER DRIVE FITTING. BLENDED CRACK IAW REA D957-52510.Oct 6, 2005 · N967AX · Doug DC941 · SpoilersSDR ABXA050250Skin · corrodedAREA 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.Oct 4, 2005 · N967AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA040076Longeron · crackedSTA. 1040 LONGERON 17 LT CRACKED. SPLICED IN NEW SECTION OF LONGERON IAW DC-9 SRM 53-02.Feb 10, 2004 · N967AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA040075Bulkhead · crackedLT FORWARD PYLON BULKHEAD WAS CRACKED AT BOTTOM AT LT BUTT LINE 44.0. REPAIRED LT FORWARD PYLON BULKHEAD IAW DC-9 SRM 53-03.Feb 9, 2004 · N967AX · Doug DC941 · Nacelle/Pylon, Bulkhead/FirewallSDR ABXA040074Frame · crackedSTA 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 EMINAFeb 6, 2004 · N967AX · Doug DC941 · Fuselage Main, FrameSDR ABXA040072Frame · crackedEDDY 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.Feb 6, 2004 · N967AX · Doug DC941 · Fuselage Main, FrameSDR ABXA040070Fitting · corrodedLONGERON 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.Feb 6, 2004 · N967AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA040071Web · crackedCUSP WEB CRACKED FROM F.S. 1025-1039 APPROXIMATELY LT BUTT LINE 56. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.Feb 6, 2004 · N967AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040066Rib · crackedRT 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.Feb 5, 2004 · N967AX · Doug DC941 · Wing, Rib/BulkheadSDR ABXA040073Support · crackedVERTICAL SUPPORT NR 7 CRACKED FORWARD SIDE OF FORWARD AUX TANK. REPLACED VERTICAL SUPPORT NR 7 IAW DC-9 SRM 51-30-1.Feb 5, 2004 · N967AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040069Nose Cowl · crackedNOSE 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.Feb 5, 2004 · N967AX · Doug DC941 · Engine Cowling SystemSDR ABXA040068Skin · damagedFORWARD LOWER CARGO DOOR'S EXTERIOR SKIN WAS DAMAGED AT LOWER EDGE 3 PLACES. REPAIRED AREA IAW REA D952-49012.Feb 5, 2004 · N967AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA040067Intercostal · crackedFORWARD 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.Feb 5, 2004 · N967AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA020045Bulkhead · crackedCRACK IN LEFT BULKHEAD WEB, FS 1041 AT LONGERON 17L, INBOARD END. REPAIRED BULKHEAD IAW DC-9 SRM 53-01.Jun 19, 2002 · N967AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA020044Floorbeam · crackedFLOORBEAM 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.Jun 19, 2002 · N967AX · Doug DC941 · Fuselage Main, Floor BeamSDR ABXA020043Longeron · crackedLONGERON 17, STATION 408, WAS CRACKED APPROXIMATELY .5-.75 INCH. REPAIRED LONGERON 17 IAW DC-9 SRM 53-02.Jun 18, 2002 · N967AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA020042Longeron · crackedLONGERON 17, STATION 389, WAS CRACKED APPROXIMATELY 3/4 INCH. REPAIRED LONGERON 17 IAW DC-9 SRM 53-02.Jun 18, 2002 · N967AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA020041Pan · crackedAFT LOWER CARGO DOOR INNER PAN, WAS CRACKED IN RADIUS BELOW AFT LATCH. REPAIRED AREA IAW DC-9 SRM 52-05.Jun 18, 2002 · N967AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA010720Clip · defectiveSMOKE 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.Feb 13, 2002 · N967AX · Doug DC941 · Flight Compartment LightingSDR ABXA010719Rheostat · malfunctionedBURNING 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.Feb 12, 2002 · N967AX · Doug DC941 · Flight Compartment LightingSDR ABXA010220Structure · vibrationON 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 VANESMay 8, 2001 · N967AX · Doug DC941 · Fuselage Main, StructureSDR ABXA010212Engine · failedTHE 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 NOTApr 30, 2001 · N967AX · Doug DC941 · Engine (Turbine/Turboprop)SDR ABXA0100005Unknown · odorFLIGHT 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 RANGJan 15, 2001 · N967AX · Doug DC941 · Air Distribution SystemSDR ABXA0000001Bulb · failedON LANDING, WHEN GEAR WAS LOWERED, THE GEAR DOOR OPEN LIGHT WOULD NOT ILLUMINATE. PRESS TO TEST WAS OK. REPLACED GEAR DOOR OPEN LIGHT BULB.Dec 30, 1999 · N967AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA9900360Bulkhead Jamb · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB, RIGHT UPPER CORNER CRACKED. REPAIRED IAW DC9 SRM 53-03.May 10, 1999 · N967AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9900359Bulkhead Jamb · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB UPPER CORNER CRACKED. REPAIRED CRACK IAW DC9 SRM 53-03.May 10, 1999 · N967AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9900358Spar Cap · crackedDURING C-CHECK, FOUND LEFT WING REAR SPAR CAP CRACKED AT NUMEROUS HOLES. REPAIRED IAW ABX REA D957-28455MR.May 10, 1999 · N967AX · Doug DC941 · Wing SparSDR ABXA9800589Latch · looseCOCKPIT DOOR LATCH LOOSE ON THE INSIDE, SOMETIMES WOULD BIND. REPLACED LATCH ASSY.Jun 30, 1998 · N967AX · Doug DC941 · Fixed Inner DoorsSDR ABXA9800588Latch · inoperativeCOCKPIT DOOR INSIDE LATCH INOPERATIVE. CREW WAS UNABLE TO OPEN DOOR FROM COCKPIT. REPAIRED AS REQUIRED.Jun 29, 1998 · N967AX · Doug DC941 · Fixed Inner DoorsSDR ABXA9800446Drive Link · crackedDURING 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.May 11, 1998 · N967AX · Doug DC941 · Engine Thrust ReverserSDR ABXA9800036Latch · out of adjustCOCKPIT DOOR WOULD NOT OPEN. LUBRICATED AND ADJUSTED DOOR LATCH ASSEMBLY.Jan 22, 1998 · N967AX · Doug DC941 · Fixed Inner DoorsSDR ABXA9701681Latch Assy · defectiveDURING MAINTENANCE CHECK, FOUND COCKPIT DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. REINSTALLED TUMBLER MECHANISM INSIDE DOOR HANDLE.Oct 17, 1997 · N967AX · Doug DC941 · Fixed Inner DoorsSDR ABXA9701624Latch · wornCOCKPIT DOOR WOULD NOT OPEN FROM THE INSIDE. REPAIRED THE LATCH ASSEMBLY. OPS CHECKED GOOD.Oct 14, 1997 · N967AX · Doug DC941 · Fixed Inner DoorsSDR ABXA9701517Fitting · corrodedDURING 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.Sep 24, 1997 · N967AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701516Web · crackedDURING 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.Sep 24, 1997 · N967AX · Doug DC941 · Horizontal Stabilizer StructureSDR ABXA9701515Angle · crackedDURING C-CHECK, FOUND A CRACKED ANGLE AT STA 1041 AND LONGERON 18 LEFT, UNDER CUSP WEB. REPAIRED ANGLE IAW ABX REA D953-20903-MR.Sep 24, 1997 · N967AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701511Cusp Web · crackedDURING C-CHECK, FOUND LT CUSP WEB AT STA 1040 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.Sep 22, 1997 · N967AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701510Frame · crackedDURING 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.Sep 22, 1997 · N967AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9701512Blkhd Fitting · crackedDURING 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.Sep 19, 1997 · N967AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701504Cusp Web · crackedDURING 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.Sep 19, 1997 · N967AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701503Frame · crackedDURING C-CHECK, FOUND THE LT MAINFRAME AT STA 775 CENTER POCKET AFT LOWER FLANGE CRACKED. REPAIRED FRAME IAW ABX REA D953-20786-MR.Sep 19, 1997 · N967AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9701502Fixed Vane · delaminatedDURING C-CHECK, FOUND THE CENTER FIXED VANE TOP SIDE DELAMINATED. REPLACED VANE IAW DC9 MM 27-51-3.Sep 19, 1997 · N967AX · Doug DC941 · Wing Miscellaneous Structure
Back to N967AX, cancelled May 24, 2017