N908AX, cancelled Mar 31, 2016

Service difficulty reports · 110

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 = 'N908AX' AND deregistration_id = 'N908AX-2016-03-31'
  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 ABXA060072Intercostal · crackedINTERCOSTAL AT BS 996 LONGERON 12 RIGHT FOUND CRACKED. REPAIRED AREA IAW DC9 SRM 53-01.Jan 30, 2006 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA060071Fitting · crackedAFT PRESSURE BULKHEAD DOOR JAMB HAD BOTH LEFT AND RIGHT UPPER ATTACH ANGLES CRACKED. REMOVED AND REPLACED UPPER ATTACH ANGLES IAW DC9 SRM 51-30-5 AND 51-30-2.Jan 19, 2006 · N908AX · Doug DC931 · Fuselage Main, Attach FittingsSDR ABXA060068Splice · corrodedFOUND LONGERON 23 LEFT AT P DOME SPLICE HAD CORROSION ON OUTBOARD FLANGE. REMOVED AND REPLACED LONGERON SECTION IAW DC9 SRM 53-02.Jan 18, 2006 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA060069Skin · corrodedFUSELAGE SKIN INTERIOR SURFACE HAD SURFACE CORROSION FROM LONGERON 26 RIGHT TO 26 LEFT AT AFT PRESSURE BULKHEAD TEE CAP AREA. REPAIRED SKIN IAW DC9 SRM.Jan 18, 2006 · N908AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA060067Bulkhead · corrodedAFT LOWER CARGO BULKHEAD WEB, STA 996 LEFT, CORRODED AT NUMEROUS AREAS. REMOVED AND REPLACED WEB IAW DC9 SRM 53-11-3.Jan 18, 2006 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA060070Bulkhead · corrodedAFT PRESSURE BULKHEAD LOWER WEB HAD SURFACE CORROSION ON FORWARD AND AFT SIDE LONGERON 23 RIGHT TO 23 LEFT IN TEE CAP AREA. REPAIRED AFT PRESSURE BULKHEAD WEB IAW DC9 SRM 53-05.Jan 18, 2006 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA060066Bulkhead · crackedFORMER ON AFT PRESSURE BULKHEAD STA. Z74 RIGHT CRACKED. REMOVED AND REPLACED FORMER IAW DC9 SRM 51-30-2.Jan 17, 2006 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA060065Structure · gougedAFT PRESSURE BULKHEAD 'T' CAP WAS GOUGED ABOUT 3/8" BELOW SKIN JUST TO THE RIGHT OF CENTER AT BOTTOM. NR 4 TEE CAP REMOVED AND REPLACED ON JC EA 53120035-006.Jan 13, 2006 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA060063Repair · crackedAFT PRESSURE BULKHEAD LEFT UPPER CORNER 5910130-13 DOUBLER (ORIGINAL OEM) CRACKED FROM LEFT EOP. REPAIRED CORNER IAW REA D953-53106-MR.Jan 12, 2006 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA060061Repair · crackedAFT PRESSURE BULKHEAD LEFT DOOR JAMB CORNER REPAIR DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER IAW DC9 SRM.Jan 12, 2006 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA060064Frame · crackedLEFT FORWARD MAIN FRAME FS 699, FORWARD FLANGE CRACKED AT PT J AND AFT FLANGE CRACKED PTS H-I. REMOVED AND REPLACED MAIN FRAME AT FS 699 LEFT IAW JC EA 53400321-001-2.Jan 12, 2006 · N908AX · Doug DC931 · Fuselage Main, FrameSDR ABXA060062Longeron · crackedFOUND LONGERON 4 FEET AT STA 200 CRACKED. REMOVED AND REPLACED LONGERON 4 LEFT, STA 160.230 IAW DC9 SRM 51-30-2 AND 51-30-5.Jan 12, 2006 · N908AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA050151Wire · brokenRT MAIN GEAR DOWN INDICATION "GREEN LIGHT" INTERMITTENT. CHECKED WITH ALT MAIN GEAR INDICATION. SHOWED GEAR DOWN. DID A MISSED APPROACH AND DECLARED AN EMERGENCY. VERIFIED NO RIGHT GEAR INDICATION, ALT SYS GOOD, FOUND CORROSION ON SWITCH S1-184 AND CONNECTJun 10, 2005 · N908AX · Doug DC931 · Landing Gear System WiringSDR ABXA040142Latch · jammedCOCKPIT DOOR LATCH JAMMED. DISASSEMBLED COCKPIT DOOR LATCH ASSEMBLY, FOUND HANDLE JAMMED. FREED JAM AND REASSEMBLED. OPS CHECKED GOOD IAW DC-9 MM.Apr 21, 2004 · N908AX · Doug DC931 · Fixed Inner DoorsSDR ABXA040084Structure · crackedRIVET ROW FOUND CRACKED AT STA 76.550 UNDER CO-PILOT'S WINDSHIELD WIPER BETWEEN APPROXIMATELY LONGERON 3 AND 4 RIGHT. REPAIRED AREA IAW EA 53100075-003-2.Feb 18, 2004 · N908AX · Doug DC931 · Fuselage Main, StructureSDR ABXA040082Fitting · crackedSLANT PANEL INBOARD ANGLE FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-10-4, AND 51-30-1.Feb 17, 2004 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA040080Angle · crackedLEFT PYLON UPPER ATTACH ANGLE WAS CRACKED AT STA 1019. REPAIRED AREA IAW DC-9 SRM 54-04.Feb 17, 2004 · N908AX · Doug DC931 · Nacelle/Pylon Miscellaneous StructureSDR ABXA040083Actuator · crackedFITTING FORWARD OF DOOR ACTUATOR CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.Feb 17, 2004 · N908AX · Doug DC931 · Landing Gear Door ActuatorSDR ABXA040081Longeron · crackedLONGERON 17 RIGHT HAD 2 CRACKS AT EACH LOCATION, FS 389, FS 408 AND FS 427. REPAIRED LONGERON 17 RIGHT FROM STA 388 TO 446 IAW DC-9 SRM 53-02.Feb 17, 2004 · N908AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA040029Amplifier · failedCARGO SMOKE LIGHT ON IN FLT. COULD NOT DUPLICATE. INSPECTED WIRING, TAPPED ON DETECTORS & AMPLIFIER, LIGHT REMAINED OUT. FOR PRECAUTION, R & R BOTH SMOKE DETECTORS & SMOKE DETECTOR AMP. PERFORMED CHECK USING LIQUID SMOKE. SYSTEM OPS CHECKED GOOD IAW DC-9 Jan 15, 2004 · N908AX · Doug DC931 · Smoke DetectionSDR ABXA030371Uplock · out of adjustCYCLED MAIN LANDING GEAR AT 210 KNOTS, 3000 FT, CLEAN UPON RETRACT. RIGHT MAIN LANDING GEAR UNSAFE LIGHT STAYED ON. ADJUSTED RIGHT MAIN LANDING GEAR DOOR UPLATCH IAW DC-9 MM AND WORK ACCOMPLISHED ON W.O. NR 2003908. OPS CHECKED GOOD.Sep 30, 2003 · N908AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA030055Control Panel · defectiveAIRCRAFT SHOOK VIOLENTLY WHEN AUTO PILOT TURNED ON. TURNED OFF AND TRIED AGAIN. SAME RESULTS. TURNED OFF AUTO PILOT, NOTICED NO YOKE MOVEMENT. REMOVED AND REPLACED AUTO PILOT CONTROLLER. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 22-10-00-5.Jan 30, 2003 · N908AX · Doug DC931 · Autopilot SystemSDR ABXA020342Elevator · jammedELEVATOR JAMMED, WOULD NOT PULL BACK WHILE PERFORMING CONTROL CHECK. INSPECTED ELEVATOR TABS, CONTROL VALVES, FOLLOW UP MECHANISMS, LOAD FEEL AND CENTERING SPRING, VISIBLE PORTIONS OF CABLE RUNS IN TAIL COMPARTMENT AND E/E COMPARTMENT. NO DEFECTS FOUND. CONTRONov 26, 2002 · N908AX · Doug DC931 · Elevator Control SystemSDR ABXA020169Skin · corrodedDURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN, LOCATED AT THE LOWER CARGO DOOR JAMB, FORWARD LOWER CORNER. THE DAMAGE TO THE SKIN WAS TRIMMED OUT AND A NEW SECTION OF SKIN WAS SPLICED IN, IAW DC-9 SRM 53-04, FIG. Sep 4, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)SDR ABXA020168Doubler · corrodedDURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN RESULTING IN THE DISCOVERY OF CORROSION ON THE INTERNAL DOUBLER P/N 5910158-24. THE DAMAGE TO THE INTERNAL DOUBLER WAS TRIMMED OUT AND A NEW SECTION SPLICED IN IAW DC-Sep 4, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)SDR ABXA020152Latch · out of adjustRIGHT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. UPLATCH CHECK FAILED (GEAR DOOR OPEN LIGHT CAME ON AND GEAR EXTENDED). WHEN THE GEAR HANDLE WAS PLACED IN UP POSITION, RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT WENT OUT. RIGHT GEAR RETRACTEDAug 30, 2002 · N908AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA020146Bracket · out of adjustAFTER TAKEOFF WITH GEAR HANDLE UP, THE RIGHT GEAR RED UNSAFE LIGHT ILLUMINATED. RECYCLED THE GEAR WITH NO CHANGE. THE GEAR UPLATCH CHECK ALSO FAILED. ADJUSTED THE TENSION ON THE RIGHT MAIN GEAR DOOR ROLLER BRACKET AND SPRING ASSEMBLY IAW DC-9 MM 32-31-04-2-Aug 28, 2002 · N908AX · Doug DC931 · Landing Gear Retraction/Extension SystemSDR ABXA020155Doubler · crackedCRACK IN FUSELAGE SKIN AT STATION 994, LONGERON 12 RIGHT, BETWEEN 2 RIVETS AND EXTENDING 1/4" PAST BOTH RIVETS. REPAIRED CRACK IAW DC-9 DWG SR09530151 AND E.A. 5311005-034.Jul 8, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)SDR ABXA020160Cap · crackedLONGERON END CAP CRACKED NR 11 RIGHT. INSTALLED NEW END CAP NR 11 RIGHT IAW DC-9 SRM 51-30-2 AND 51-30-5.Jul 6, 2002 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA020159Bulkhead · damagedAFT PRESSURE BULKHEAD SIDE SKIN SPLICED AT Z 14.00. SPLICE NOT IAW DOUGLAS AFT PRESSURE BULKHEAD RE-WORK. SPLICED NEW SECTION (LOWER) OF RIGHT AFT PRESSURE BULKHEAD WEB IAW REA D953-44534-MR AND DOUGLAS DWG J060088.Jun 25, 2002 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA020158Doubler · crackedANGLED DOUBLER COMMON TO #7 SLAT TRACK RIB INBOARD AND FRONT SPAR CRACKED. REPAIRED AREA IAW DC-9 SRM 57-09.Jun 24, 2002 · N908AX · Doug DC931 · Wing StructureSDR ABXA020157Rib · crackedNR 8 SLAT TRACK INBOARD LEADING EDGE RIB ANGLE COMMON TO ROLLERS CRACKED AT AFT LOWER VERTICAL LEG. REPLACED RIB IAW DC-9 SRM 51-30-2 AND 51-30-5.Jun 24, 2002 · N908AX · Doug DC931 · Wing, Rib/BulkheadSDR ABXA020156Doubler · cracked5" CRACK TOP OF FUSELAGE AT #1 LONGERON IN AFT PRESSURE BULKHEAD AREA. REPAIRED CRACK IAW DC-9 DWG SR0953151 AND E.A. 5311005-034.Jun 21, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)SDR ABXA010783Power Supply · dischargedDURING PREFLIGHT CHECK, FOUND THE EMERGENCY CABIN LIGHTS INOPERATIVE. REPLACED THE BATTERY POWER SUPPLY IAW DC-9 MM. OPS CHECKED GOOD.Mar 25, 2002 · N908AX · Doug DC931 · Emergency LightingSDR ABXA010566Battery · dischargedAFT COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 AMM 33-53-02-4-0001. OPS CHECKED GOOD.Oct 29, 2001 · N908AX · Doug DC931 · Emergency LightingSDR ABXA000495Beam · crackedAFT VENTRAL DOOR BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED VENTRAL DOOR BEAM IAW DC-9 MM.Nov 15, 2000 · N908AX · Doug DC931 · Passenger/Crew DoorsSDR ABXA000510Gusset · crackedINTERCOSTAL GUSSET CRACKED AT FS 465. MAINTENANCE REPLACED THE GUSSET IAW DC-9 SRM.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000509Splice · crackedAFT PRESSURE BULKHEAD TEE CAP SPLICE CRACKED. MAINTENANCE REPLACED THE SPLICE IAW DC-9 SRM 51-30-5.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000508Frame · crackedFUSELAGE FRAME CRACKED AT FS 680. MAINTENANCE REPLACED FRAME IAW ABX REA 953-38971-MR.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Main, FrameSDR ABXA000507Web · crackedCUSP WEB CRACKED AT FS 218. MAINTENANCE REPLACED THE CUSP WEB IAW DC-9 SRM 51-30-1.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000506Floorbeam · crackedFLOORBEAM SUPPORT CRACKED AT FS 560. MAINTENANCE REPAIRED THE SUPPORT IAW DC-9 SRM DRAWING K05159.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA000505Floorbeam · crackedFLOORBEAM SUPPORT CRACKED AT LOWER INBOARD FASTENER. MAINTENANCE REPAIRED IAW DC-9 SRM DRAWING K05159.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA000504Fitting · crackedAFT LOWER CARGO DOOR BEAM NR 2 END FITTING CRACKED. MAINTENANCE REPLACED THE END FITTING IAW SRM 51-30-5.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000503Fitting · crackedAFT LOWER CARGO DOOR NR 1 BEAM FITTING CRACKED. MAINTENANCE REPLACED THE NR 1 BEAM END FITTING IAW DC-9 SRM.Nov 15, 2000 · N908AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA000502Intercostal · corrodedINTERCOSTAL AT FS 579 - 598 HAD LEVEL ONE CORROSION. MAINTENANCE REPLACED THE INTERCOSTAL IAW DC-9 SRM 51-30-2.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000501Doubler · crackedAFT PRESSURE BULKHEAD DOOR FRAME HAS A CRACKED DOUBLER. REPAIRED DOUBLER IAW ABX REA D953-38986.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000500Stiffener · crackedAFT LOWER CARGO DOOR FORWARD STIFFENER CRACKED. MAINTENANCE REPLACED THE STIFFENER IAW DRAWING 5913304-11.Nov 15, 2000 · N908AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA000499Intercostal · crackedUPPER CARGO FLOOR INTERCOSTAL CRACKED. MAINTENANCE REPLACED THE INTERCOSTAL END CLIPS IAW DC-9 MM.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000498Tee Chord · crackedAFT PRESSURE BULKHEAD NR 2 TEE CRACKED. MAINTENANCE REPLACED THE TEE IAW ABX EA 53120033-006.Nov 15, 2000 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA000497Panel · delaminatedLEFT WING TRAILING EDGE PANEL DELAMINATED. MAINTENANCE REPLACED PANEL IAW DC-9 MM.Nov 15, 2000 · N908AX · Doug DC931 · Wing, Plate/Skin
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