N934AX, cancelled Apr 18, 2011

Service difficulty reports · 82

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 = 'N934AX' AND deregistration_id = 'N934AX-2011-04-18'
  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 ABXR201009250052Control Cable · corrodedDURING FERRY FLIGHT PREP FOUND CABLE 51C CORRODED FWD OF APB. R & R CABLE 51C IAW AMM.Sep 25, 2010 · N934AX · Doug DC933F · Engine Thrust ReverserSDR ABXR201009250051Control Cable · brokenDURING FERRY FLIGHT PREP FOUND NR 1 ENGINE FWD TELESCOPING BRAIDED CABLE RUSTED, WORN, AND BROKEN STRANDS. R & R NR1 ENGINE FWD TELESCOPING GRAIDED CABLE IAW AMM.Sep 25, 2010 · N934AX · Doug DC933F · Power LeverSDR ABXR201009250050Control Cable · brokenDURING FERRY FLIGHT PREP FOUND CABLE RUN 52C FOR RT THRUST REVERSER CORRODED AND BROKEN STRANDS. R & R CABLE 52C IAW AMM.Sep 25, 2010 · N934AX · Doug DC933F · Engine Thrust ReverserSDR ABXR201009250049Control Cable · brokenDURING FERRY FLIGHT PREP FOUND THRUST REVERSER CONTROL CABLE 48C BROKEN. R & R CABLE 48C IAW AMM.Sep 25, 2010 · N934AX · Doug DC933F · Engine Thrust ReverserSDR ABXR201009250048Control Cable · brokenDURING FERRY FLIGHT PREP FOUND NR 1 T/R SECTOR ON AFT 'P' DOME DOESN'T MOVE WITH T/R HANDLE MOVEMENT. REPLACED CABLE 47C IAW AMM.Sep 25, 2010 · N934AX · Doug DC933F · Engine Thrust ReverserSDR ABXR201009250047Push-Pull Cable · damagedDURING FERRY FLIGHT PREP FOUND NR 2 ENGINE THROTTLE DOES NOT MOVE FROM THROTTLE LEVER. R & R NR 2 ENGINE THROTTLE PUSH PULL CABLE IAW MM.Sep 25, 2010 · N934AX · Doug DC933F · Power LeverSDR ABXR201009250046Yoke · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 ENGING FWD. YOKE CORRODED. R & R NR 2 ENG FWD YOKE IAW AMM.Sep 25, 2010 · N934AX · Doug DC933F · Nacelle/Pylon, Main FrameSDR ABXR201009250045Fitting · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD. UPPER SPLICE FITTING CORRODED. R & R NR2 PYLON FWD UPPER SPLICE FITTING IAW AMM.Sep 25, 2010 · N934AX · Doug DC933F · Nacelle/Pylon Miscellaneous StructureSDR ABXR201009250044Fitting · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD LOWER SPLICE FITTING CORRODED. R & R SPLICE FITTING IAW SRM.Sep 25, 2010 · N934AX · Doug DC933F · Nacelle/Pylon Miscellaneous StructureSDR ABXR201009250043Mount · corrodedDURING FERRY FLIGHT PREP FOUND NR2 PYLON AFT ENGINE MOUNT CORRODED. R AND R AFT MOUNT ASSY IAW MM.Sep 25, 2010 · N934AX · Doug DC933F · Engine Mount SectionSDR ABXR201009250042Isolator · corrodedDURING FERRY FLIGHT PREP FOUND NR1 PYLON UPPER VIBRATION ISOLATOR RUSTED AND PITTED. R & R NR1 PYLON UPPER VIBRATION ISOLATOR IAW MM.Sep 25, 2010 · N934AX · Doug DC933F · Engine Mount SectionSDR ABXR201009250041Isolator · corrodedDURING FERRY FLIGHT PREP FOUND NR 1 PYLON YOKE LOWER ISOLATION ABSORBER RUSTED AND PITTED. R & R LOWER ISOLATION ABSORBER IAW MM.Sep 25, 2010 · N934AX · Doug DC933F · Engine Mount SectionSDR ABXR201009250040Mount · corrodedDURING FERRY FLIGHT FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT RECEIVER RUSTED AND PITTED. R & R NR1 PYLON AFT MOUNT IAW MM.Sep 25, 2010 · N934AX · Doug DC933F · Engine Mount SectionSDR ABXR2010092400039Link · corrodedDURING FERRY FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT UPPER INBD "H" DOG BONE AND OTBD BOLT RUSTY. R & R BOLT AND MOUNT LINK IAW MM.Sep 24, 2010 · N934AX · Doug DC933F · Engine Mount SectionSDR ABXA070365Battery · dischargedEMERGENCY LIGHTS WILL ARM BUT WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW DC9 MM 33-53-00-8.Nov 5, 2007 · N934AX · Doug DC933F · Emergency LightingSDR ABXA070322Window · out of adjustCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEARVIEW WINDOW IAW DC9 MM 56-10-03-5.Sep 20, 2007 · N934AX · Doug DC933F · Flight Compartment WindowsSDR ABXA060287Linkage · lack of lubeCAPTAIN'S SLIDING WINDOW (EMERGENCY EXIT) WOULD NOT OPEN. LUBED CAPTAIN'S SLIDING WINDOW LINKAGE AS REQUIRED. OPERATIONAL CHECK GOOD IAW MM 56-10-03-5-0002.Nov 10, 2006 · N934AX · Doug DC933F · Flight Compartment WindowsSDR ABXA060293Frame · crackedLEFT WHEEL WELL, LEFT AFT CORNER ANGLE WAS CRACKED. REMOVED AND REPLACED MAIN FRAME AT FS 756 LEFT IAW DACO DC9 DWG 9919649.Oct 13, 2006 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA060284Angle · crackedLEFT WHEEL WELL AFT CORNER ANGLE WAS CRACKED. REMOVED AND REPLACED MAIN FRAME AT FS 756 LEFT IAW DACO DC9 DWG 9919649.Oct 13, 2006 · N934AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA060078Rod End · brokenUPON SLAT EXTENSION, AIRCRAFT ROLLED TO THE RIGHT AND SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE SLAT EXTEND LIGHT DID NOT ILLUMINATE AFTER RECYCLING SLATS, NORMAL INDICATIONS WERE OBTAINED. FOUND BROKEN ROD END ON LEFT WING INBOARD SLAT ACTUATOR. REMOVED AJan 25, 2006 · N934AX · Doug DC933F · Leading Edge Slat ActuatorSDR ABXA050039Contact · wornUPON LOWERING THE LANDING GEAR, NO NOSE GEAR SAFE LIGHT. TESTED IN BRIGHT AND DIM. AFTER INITIATING A GO-AROUND, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED (APPROXIMATELY 30 SECONDS). FOUND BULB CONTACTS TO BE WORN. RELAMPED, OPS CHECKED GOOD.Mar 2, 2005 · N934AX · Doug DC933F · Landing Gear Position and WarningSDR ABXA040387Window · stuckCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. OPENED WINDOW AND APPLIED LUBRICANT TO WINDOW MECHANISM, WINDOW OPERATES NORMAL.Dec 1, 2004 · N934AX · Doug DC933F · Flight Compartment WindowsSDR ABXA040399Bearing · crackedRIGHT HORIZONTAL STAB PIVOT BEARING FOUND CRACKED IN HALF. REPLACED BEARING ON NR 0131 IAW DC-9 SRM.Nov 16, 2004 · N934AX · Doug DC933F · Horizontal Stabilizer StructureSDR ABXA040398Frame · crackedRIGHT FORWARD MAIN FRAME FS 699 CRACKED AT FORWARD FLANGE POINTS F & E AND AFT FLANGE POINTS H & I. REMOVED AND REPLACED FRAME AT STA 699 IAW EA 53400322-001-3.Nov 12, 2004 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA040393Skin · crackedLOWER AFT CORNER OF FORWARD LOWER CARGO DOOR CUTOUT HAD 2 EACH CRACKS. REPAIRED IAW DC-9 SRM 53-05 AND REA D953-51052MR.Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA040392Skin · crackedMAIN ENTRY DOOR UPPER AFT STOP HAD CRACKED SURFACE SKIN. REPAIRED MAIN ENTRY DOOR UPPER AFT CORNER IAW JOB CARD EA 53100126-001, SERVICE REPAIR DRAWING SR09530252-7001 AND DC-9 SRM 53-05.Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA040397Frame · crackedAFT ASSY CANTED FRAME 1121 CRACKED BETWEEN LONGERON 16 LEFT AND LONGERON 17 LEFT. REPAIRED IAW DC-9 SSRM K05159.Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA040396Skin Panel · crackedTWO CRACKS IN FUSELAGE SKIN FS 1143, APPROXIMATELY LONGERON 14 RIGHT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM 53-01.Nov 11, 2004 · N934AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA040395Frame · crackedFRAME CRACKED FS 357 AT LONGERON 30. REPAIRED FRAME STA 357 AT LONGERON 30 IAW DC-9 SRM 53-03.Nov 10, 2004 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA040394Longeron · crackedLONGERON 30 CRACKED FORWARD AND AFT AT SPLICE FS 380. REMOVED AND REPLACED LONGERON 30 FROM STA 355 TO 415.Nov 10, 2004 · N934AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR ABXA040112Switch · malfunctionedAFTER GEAR HANDLE SELECTED DOWN, NOSE GEAR LIGHT DID NOT ILLUMINATE. RECYCLED GEAR WITH SAME RESULT. CHECKED GEAR DOWN VISUAL (PEEP HOLE) AND NOSE LIGHT ILLUMINATED AT 500 FT AGL ON FINAL. FOUND WIRING HARNESS KINKED BEHIND DOWNLOCK SWITCH CANNON PLUG. RE-Mar 23, 2004 · N934AX · Doug DC933F · Landing Gear Position and WarningSDR ABXA030162Skin · delaminatedLARGE AREA OF DELAMINATION ON UPPER AND LOWER SURFACE OF THE RIGHT WING INBOARD SPOILER PANEL. REPLACED SPOILER IAW DC-9 MM 27-61-01-4-0001.Apr 21, 2003 · N934AX · Doug DC933F · SpoilersSDR ABXA030041Outflow Valve · lack of lubeAIRCRAFT WOULD NOT AUTO PRESSURIZE ON CLIMBOUT. MANUAL PRESSURIZATION ATTEMPTED, BUT OUTFLOW CONTROL WHEEL WOULD NOT MOVE. INSPECTED AND CLEANED OUTFLOW VALVE AS REQUIRED. NO DEFECTS NOTED. REMOVED CIRCUIT BREAKER COLLARS FROM CABIN PRESS CONTROL. OPS CHEJan 17, 2003 · N934AX · Doug DC933F · Pressure Regulator/Outflow ValveSDR ABXA020276Actuator · failedRUDDER PEDALS WERE STIFF DURING CONTROL CHECK, ON CLIMB OUT OF ICT. CLIMBING TO FL 350, AIRCRAFT STARTED TO YAW AND DUTCH ROLL. DISCONNECTED AUTO PILOT. TURNING OFF YAW DAMPER AND GOING TO MANUAL RUDDER DID NOT STOP YAW/DUTCH ROLL. AIRCRAFT SLOWED AND DESCENDOct 29, 2002 · N934AX · Doug DC933F · Rudder Tab Control SystemSDR ABXA020188Control Cable · brokenON INITIAL CLIMB OUT, EXCESSIVE NOISE AND VIBRATION IN VICINITY OF NOSE GEAR. WHEN GEAR LOWERED, NOISE, VIBRATION STOPPED. FOUND RIGHT FORWARD NOSE GEAR DOOR OPEN, AND DOOR STOP CABLE BROKEN. REPLACED LEFT AND RIGHT NOSE GEAR DOOR STOP CABLES IAW DC-9 MM 32Sep 11, 2002 · N934AX · Doug DC933F · Landing Gear Door Retract SectionSDR ABXA010467Fitting · corrodedLEFT SLANT PANEL, OUTBOARD ATTACH FITTING WAS CORRODED. REPLACED FITTING IAW DC-9 SRM 51-30-5.Aug 16, 2001 · N934AX · Doug DC933F · Fuselage Structure (General)SDR ABXA010466Panel · corrodedLEFT SLANT PANEL WAS CORRODED AROUND THE LOWER NUTPLATES. LEVEL II CORROSION. INSTALLED NEW SLANT PANEL IAW DC-9 SRM 51-30-1.Aug 14, 2001 · N934AX · Doug DC933F · Fuselage Structure (General)SDR ABXA010465Panel · corrodedRIGHT SLANT PANEL WAS CORRODED AROUND NUTPLATES ON THE LOWER EDGE OF PANEL. LEVEL II CORROSION. INSTALLED NEW SLANT PANEL IAW DC-9 SRM.Aug 14, 2001 · N934AX · Doug DC933F · Fuselage Structure (General)SDR ABXA010362Battery Pack · dischargedCOCKPIT EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE AT RFD. MAINTENANCE INSPECTED AND RE-SEATED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN ILN AS A PRECAUTION, MAINTENANCE INSPECTED ANJul 3, 2001 · N934AX · Doug DC933F · Emergency LightingSDR ABXA010219Switch · intermittentTHE EMERGENCY EVACUATION LIGHT SWITCH WAS REPORTED AS INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT EMERGENCY LIGHT CONTROL SWITCH, AND RELAMPED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVIMay 7, 2001 · N934AX · Doug DC933F · Emergency LightingSDR ABXA000432Battery · dischargedDURING PRE-DEPARTURE CHECK, NOTED COCKPIT EMERGENCY LIGHTS INOP. REPLACED COCKPIT EMERGENCY LIGHT BATTERIES IAW DC9 MM 33-51-0-2. OPS CHECKED GOOD.Sep 25, 2000 · N934AX · Doug DC933F · Emergency LightingSDR ABXA000418Light · inoperativeDURING PREFLIGHT INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. RESECURED WIRING TO OVERHEAD LIGHT SOCKET.Sep 14, 2000 · N934AX · Doug DC933F · Emergency LightingSDR ABXA000133Battery · dischargedDURING COCKPIT CHECK, EMERGENCY EVAC LIGHT FOUND NOT WORKING WHEN SWITCH WAS IN THE ON POSITION. REPLACED EMERGENCY LIGHT BATTERY SUPPLY IAW DC9 SMM 33-53-00. OPS CHECKED GOOD.Feb 23, 2000 · N934AX · Doug DC933F · Emergency LightingSDR ABXA000050Web · corrodedDURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT AFT BULKHEAD WEB EXFOLIATED AND RIVET HEADS POPPED JUST ABOVE LONGERON 30 ON BOTH SIDES OF BULKHEAD CENTER SUPPORT. REPLACED WEB IAW DC9 SRM 51-30-2 AND 51-30-5.Jan 6, 2000 · N934AX · Doug DC933F · Fuselage Main, BulkheadSDR ABXA000049Panel · crackedDURING C-CHECK, FOUND THE LEFT INBOARD SPOILER CRACKED AT THE UPPER SURFACE CUT-OUT. REPLACED SPOILER PANEL IAW DC9 SMM 27-61-01..Jan 6, 2000 · N934AX · Doug DC933F · SpoilersSDR ABXA000048Fitting · crackedDURING C-CHECK, FOUND THE FLOORBEAM FITTING AT STATION 579 JUST BELOW CUSP WEB RIGHT SIDE CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.Jan 6, 2000 · N934AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA000065Frame · crackedDURING C-CHECK, FOUND THE FUSELAGE FRAME FOOT FITTING AT STATION 579 RIGHT CRACKED AT BOLT HOLE. REPLACED FITTING IAW DC9 SRM 51-30-5.Jan 3, 2000 · N934AX · Doug DC933F · Fuselage Main, FrameSDR ABXA000064Web · corrodedDURING C-CHECK, FOUND THE CUSP WEB CORRODED AND CRACKED AT STATION 579 ON RIGHT SIDE. REPLACED CUSP WEB IAW DC9 SRM 53-01.Jan 3, 2000 · N934AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA000063Spar · corrodedDURING C-CHECK, FOUND THE FORWARD SIDE OF THE LOWER T-CAP OF THE FRONT SPAR CORRODED AT LBL 5 TO RBL 12 (CENTER WING). REPLACED FINGER DOUBLER IAW DC9 SRM 51-30-2.Jan 3, 2000 · N934AX · Doug DC933F · Wing SparSDR ABXA000054Floorbeam · corrodedDURING C-CHECK, FOUND FLOORBEAM AT STATION 965 AND RBL 8 CORRODED. REPAIRED FLOORBEAM IAW ABX REA D95334885 MR.Jan 3, 2000 · N934AX · Doug DC933F · Fuselage Main, Floor Beam
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