N905AX, cancelled Apr 27, 2012
Service difficulty reports · 91
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 = 'N905AX' AND deregistration_id = 'N905AX-2012-04-27' 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.
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 = 'N905AX' AND deregistration_id = 'N905AX-2012-04-27' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ABXA070424Battery · dischargedCABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.SDR ABXA070154Bulkhead · crackedAFT PRESSURE BULKHEAD SKIN CRACKED AT 4:00 POSITION ADJACANT TO DOOR PIN ALIGNMENT RECEPTACLE. REPAIRED CRACK IN SKIN IAW DWG 5934886-502 AND REA D953-55733.SDR ABXA070155Cusp Web · crackedCUSP WEB CRACKED AT STA 598 TO 617 AT BUTT LINE 58 LEFT. REPAIRED AREA OF WEB IAW DC9 SRM 53-01.SDR ABXA070153Skin · crackedFUSELAGE SKIN CRACKED 2 PLACES FS 1087 LONGERON 3 - LONGERON 4 RIGHT. REPAIRED FUSELAGE SKIN AT STA 1095, LONGERON 3 - 4 RIGHT IAW DC9 SRM 53-04.SDR ABXA070041Jackscrew · obstructedHORIZONTAL STABILIZER JACKSCREW FOUND TO BE HITTING MECHANICAL STOPS DURING OPERATION. REMOVED AND REPLACED JACKSCREW IAW DC9 MM, REF WORK ORDER 600265725.SDR ABXA060272Battery · dischargedEMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.SDR ABXA050104Skin · corrodedEVIDENCE OF CORROSION EMITTING FROM FINGER DOUBLER JUST FORWARD OF FS 332 TO 351, LONGERON 26 RT OUTBOARD AND INBOARD SIDES. REPAIRED CORRODED SKIN IAW DC-9 SRM 53-04.SDR ABXA050103Panel · crackedRIGHT BUTT LINE '0' ANGLE FITTING COMMON TO KEEL WEB AND RIGHT SLANT PANEL CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-5.SDR ABXA050101Skin · corrodedSKIN BULGING AND RIVET HEAD POPPED AT STA 949, LONGERON 24 LEFT. REPLACED LONGERON 24 LEFT, FS 927-996 IAW DC-9 SRM 51-30-2, 51-30-5 AND 53-02.SDR ABXA050102Longeron · corrodedSKIN BULGING, RIVETS CUPPED AT STA 342, LONGERON 29 RIGHT AND LONGERON 28 RIGHT. REMOVED FASTENERS, EVALUATED. SPLICED LONGERON IAW DC-9 SRM.SDR ABXA040403Relay · failedDURING INITIAL CLIMB, PRIMARY TRIM C/B 0A TRIPPED, ALTERNATE TRIM WORKED FINE. ELECTED TO PULL PRIMARY TRIM C/B'S 0B AND 0C. CONTINUED FLIGHT USING AUTOPILOT. WHEN REMOVING CREW BAGS, NOTICED STRONG ELECTRICAL SMELL (BURNT ODOR) IN BELLY'S 1 AND 2. FOUND USDR ABXA040327Wire · brokenIN CLIMB, BOTH MASTER CAUTIONS ILLUMINATED, DIVERTED TO SGF. INSTALLED NEW LEFT THERMAL CONTROL AMPLIFIER, BITE TEST SHOWED PROBLEM IN SENSOR ON CIRCUIT. FOUND WIRES ON LEFT ICE PROTECT TEMP HIGH SENSOR BROKEN, SPLICED WIRES IAW DC-9 MM 20-50-1. OPS CHECKEDSDR ABXA040138Channel · damagedFOUND BOLT PULLED OUT OF C-CHANNEL AT NR 11 9G NET ARM AT STA 207. DAMAGE WAS AT PREVIOUSLY REPAIRED AREA. REPAIRED DAMAGED AREA IAW REA D953-49568MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0.SDR ABXA040171Support · failedON POST FLIGHT INSPECTION, MAINTENANCE DISCOVERED 1 9G NET SUPPORT PULLED FROM FUSELAGE MOUNT. REPAIRED DAMAGED AREA IAW REA D953-49569MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0.SDR ABXA030360Structure · corrodedCOCKPIT SUBFLOOR HAD AREAS OF LEVEL II CORROSION, STA 160 RPL 32 TO 54. REPAIRED AREA IAW DC-9 SRM.SDR ABXA030359Pressure Panel · crackedPRESSURE PANEL LEFT WHEEL WELL AT FS 718 LEFT BUTT LINE 36 APPROXIMATELY, CRACKED. REPAIRED RPESSURE PANEL IAW REA D953-48107.SDR ABXA030350Floor Support · crackedRIGHT FLOOR SUPPORT STRUT END FITTING STA 313 CRACKED AT LONGERON 23 RIGHT. REPLACED FLOOR SUPPORT STRUT IAW DC-9 SRM.SDR ABXA030357Skin · corrodedCORROSION BETWEEN LONGERON 26 RIGHT AND SKIN, BETWEEN STA 794 AND 813. REPAIRED AREA IAW DC-9 SRM 53-04.SDR ABXA030356Floor Support · crackedCABIN FLOOR SUPPORT FITTING FS 434 LONGERON 18 LEFT CRACKED AT UPPER HORIZONTAL FLANGE BETWEEN FASTENERS AND HAD LEVEL I CORROSION ON AFT SIDE. REPLACED FITTING AND REPAIRED AREA IAW DC-9 SRM 51-10-3.SDR ABXA030355Doubler · corrodedLEVEL II CORROSION BUTT LINE '0' F.S. 180 AT SHACKLE BOX. REPLACED SUBFLOOR DOUBLER WITH NEW FABRICATED DOUBLER AND INSTALLED IAW DC-9 SRM 53-01, 53-10-4, 53-10-3, 51-30-1, AND 51-30-2.SDR ABXA030354Structure · corrodedLEVEL II CORROSION ON SUBFLOOR AT RIGHT BUTT LINE 44 F.S. 180 SHACKLE BOX. REPAIRED AREA IAW DC-9 SRM 53-01.SDR ABXA030353Floor Support · crackedLEFT FLOOR SUPPORT STRUT TO FRAME ATTACH FITTING CRACKED STA. 237 BETWEEN LONGERON 24 LEFT AND 25 LEFT. REPLACED SUPPORT IAW DC-9 SRM.SDR ABXA030352Floor Support · crackedLEFT FLOOR SUPPORT STRUT TO FRAME ATTACH BRACKET CRACKED AT STA. 275, BETWEEN LONGERON 24 LEFT AND 25 LEFT. REPLACED LEFT FLOOR SUPPORT STRAP TO FRAME ATTACH BRACKET IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.SDR ABXA030351Fitting · crackedLT FRAME 294 ENG. FITTING CRACKED AT CARGO FLOOR ATTACH POINT. REPLACED FITTING IAW DC-9 SRM 51-10-4, 51-30-5 AND 51-30-1.SDR ABXA030358Skin · corrodedCORROSION BETWEEN LONGERON 26 LT AND SKIN BETWEEN STA. 775 AND 813. REPAIRED AREA IAW DC-9 SRM.SDR ABXA030349Pressure Panel · corrodedPRESSURE PANEL DOUBLER WAS BULGING LEFT BUTT LINE 8 TO LEFT BUTT LINE 16, FS 756. REPLACED LOWER T-ANGLE OF FLOORBEAM FS 756, BUTT LINE 56 RIGHT TO BUTT LINE 54 IAW DC-9 SRM 51-30-2, 51-30-5 AND REA D953-48132.SDR ABXA030348Skin · corrodedBULGE IN FUSELAGE SKIN, CUPPED OR BROKEN FASTENERS, FS 332, LONGERON 30. REPLACED DAMAGED AREA IAW DC-9 SRM.SDR ABXA030347Structure · corrodedLEFT WHEEL WELL STA 712, BUTT LINE 53 RETAINER CORRODED AND RIVETS POPPED. REPLACED RETAINER FROM FS 699 AND 756 LEFT BUTT LINE 30 TO LEFT BUTT LINE 56 IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA030346Structure · corrodedRIGHT WHEEL WELL UPPER AFT CORNER STA. 756, BUTT LINE '0' - BUTT LINE '4', CORROSION ON KEEL ANGLE AND BULGES UNDER RETAINER. REPAIRED AREA IAW REA D953-48136MR. REMOVED PREVIOUS REPAIR FROM AFT UPPER KEEL ANGLE, REPAIRED IAW DC-9 SRM 53-05.SDR ABXA010779Spar · crackedLEFT WHEEL WELL, JUST OUTBOARD OF STATION ZERO, CENTER TANK ON REAR SPAR, UPPER INBOARD CORNER, HAD A CRACK. REPAIRED AREA IAW DC-9 SRM 51-30-5 AND 57-09.SDR ABXA010778Support · crackedVERTICAL SUPPORT FOR SLAT MECHANISM MOUNT HAD A CRACK AT LOWER INBOARD MOUNT BOLT. REPLACED VERTICAL SUPORT IAW DC-9 SRM 51-30-5.SDR ABXA000351Skin · corrodedFUSELAGE SKIN BUBBLED AT LONGERON 30 BETWEEN STATION 445 AND 465. REPAIRED IAW DC9 SRM 53-04.SDR ABXA000353Longeron · crackedLONGERON 29 LEFT CRACKED BELOW SPLICE BETWEEN STATION 408 AND 427. REPLACED LONGERON SECTION.SDR ABXA000352Longeron · crackedLONGERON 30 CRACKED BELOW SPLICE BETWEEN STATION 408 AND 427. REPLACED LONGERON 30BETWEEN STATION 408 AND 427.SDR ABXA000357Structure · crackedCRACK ON PRESSURE DOME RADIAL NR 1. REPLACED RADIAL IAW DC9 SRM 51-30-2.SDR ABXA000356Shear Tie · crackedSHEAR TIE CRACKED AT STATION 945 BELOW LONGERON 14 LEFT. REPAIRED SHEAR TIE IAW DC9 SRM.SDR ABXA000355Longeron · crackedLONGERON 17 RIGHT CRACKED AT STATION 945. REPLACED LONGERON IAW DC9 SRM.SDR ABXA000358Door · delaminatedLEFT BUTE DOOR NR 1502 WAS DELAMINATED. REPLACED BUTE DOOR.SDR ABXA000350Panel · delaminatedRIGHT WING LOWER INBOARD BONDED PANEL HAS 4 INCH DELAMINATION. REPLACED PANEL IAW DC9 SRM51-30-2.SDR ABXA9801188Pan · corrodedDURING C-CHECK, FOUND LEFT WHEEL WELL PRESSURE PANEL RETAINER PAN AT STATION 718 CORRODED. REPAIRED IAW ABX REA D953-25980MR.SDR ABXA9801187Keel Beam · crackedDURING C-CHECK, FOUND KEEL BEAM CORRODED AND CRACKED IN THE RIGHT WHEEL WELL, AFT UPPER CORNER AT STATION 737. REPAIRED IAW ABX REA D953-25903MR.SDR ABXA9800487Battery · dischargedCOCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED POWER SUPPLY BATTERIES.SDR ABXA9800289Seat · lack of lubeFIRST OFFICER'S SEAT WAS DIFFICULT TO LOCK IN FULL FORWARD POSITION. SEAT SLID BACK ON INITIATION OF TAKEOFF ROLL. SEAT UNLOCKED ON FINAL APPROACH INTO ILN WITH FIRST OFFICER FLYING AIRCRAFT. LUBRICATED FIRST OFFICER'S SEAT LINKAGE. SEAT OPERATES NORMALLY.SDR ABXA9700752Fitting · crackedDURING C-CHECK, THE FLOORBEAM SUPPORT STRUT FITTING AT STA 937 LONG 24 LT WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM.SDR ABXA9700753Vane · delaminatedDURING C-CHECK, THE INBOARD FIXED VANE WAS FOUND DELAMINATED. THE VANE WAS REPLACED IAW DC9 MM.SDR ABXA9700754Fitting · crackedDURING C-CHECK, THE FITTING JUST BELOW THE PYLON BULKHEAD LBL 44 AT STA 965 WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM.SDR ABXA9701184Skin · delaminatedFOUND LEFT WING SPOILER UPPER AND LOWER SKIN DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.SDR ABXA9701131Skin · delaminatedLEFT INBOARD FLAP VANE OUTER SKIN 40 PERCENT DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.SDR ABXA9700760Hinge · corrodedDURING C-CHECK, THE CENTER FLAP FORWARD HINGE AND ATTACH STUDS WERE FOUND CORRODED. THE HINGE WAS REPLACED IAW DC9 MM.SDR ABXA9700759Hinge · corrodedDURING C-CHECK, THE INBOARD FLAP FORWARD HINGE AND ATTACH STUDS WERE FOUND CORRODED. THE HINGE WAS REPLACED IAW DC9 MM.
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