N903AX, cancelled Jul 20, 2017
Service difficulty reports · 125
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 = 'N903AX' AND deregistration_id = 'N903AX-2017-07-20' 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 = 'N903AX' AND deregistration_id = 'N903AX-2017-07-20' 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 ABXA070218Battery · dischargedEMERGENCY LIGHTS WOULD NOT TURN ON WITH THE EMERGENCY LIGHT SWITCH IN ON POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-02-4.SDR ABXA070148Seat Track · corrodedSEAT TRACK CORRODED LOWER FLANGE AND UNDERSIDE OF TRACK AT STA 560 TO 600 LEFT BUTT LINE 12. REMOVED AND REPLACED SEAT TRACK FS 49 L - 606 LEFT BUTT LINE 1L IAW DC9 SRM 53-05.SDR ABXA070147Angle · crackedANGLE CRACKED - PYLON AFT SPAR, AFT SIDE, LOWER STRAP, OUTBOARD END - JUST INBOARD OF AFT ENGINE MOUNT. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5.SDR ABXA070146Floor Support · corrodedFLOOR SUPPORT CHANNEL EXFOLIATED IN 3 PLACES - FS 365 TO 380, LONGERON 28 LEFT. REPAIRED AREA IAW DC9 SRM.SDR ABXA070145Longeron · crackedLONGERON 30 CRACKED ON BOTH SIDES - FS 439 TO 446. REMOVED AND REPLACED LONGERON 30, STA 439 TO 446 IAW DC9 SRM.SDR ABXA070144Skin · cracked1.125" LFEC CRACK INDICATION BETWEEN FASTENERS AT LOWER FORWARD CORNER. FASTENERS ARE AT EDGE OF CUTOUT AND COMMON TO DOOR SEAL DEPRESSOR. REPAIRED AFT LOWER CARGO LOWER FORWARD CORNER IAW DC9 SRM.SDR ABXA070139Seat Track · corrodedSEAT TRACK SECTION BUTT LINE 0, STA 570 - 785 CORRODED AT STA 785 - 765, 737, 710 - 699, 680 - 670 AND 636 - 617. REMOVED AND REPLACED SEAT TRACK STA 160 - 784 IAW DC9 SRM 51-30-1 AND 51-10-4.SDR ABXA070143Retainer · crackedCRACK IN UPPER FORWARD CORNER OF WINDOW RETAINER JUST AFT OF STA 699 FRAME. REPAIRED AREA IAW REA D956-55634-MR.SDR ABXA070142Spar Cap · crackedLEFT HORIZONTAL STABILIZER LOWER SPAR OUTBOARD END CRACKED JUST ABOVE DRAINS, TRAVELS INBOARD UNDER HINGE. REPAIRED LEFT HORIZONTAL STABILIZER LOWER SPAR CAP IAW DC9 SRM 55-02.SDR ABXA070141Door Frame · crackedLEFT AFT OVERWING EXIT DOOR HAD CRACKED DOOR OUTER FRAME IN 3 PLACES AT SEAL SUPPORT FITTINGS. REPAIRED AREA IAW DC9 SRM.SDR ABXA070140Door Frame · crackedRIGHT FORWARD OVERWING EXIT DOOR HAD CRACKED DOOR OUTER FRAME IN 1 PLACE AT SEAL SUPPORT FITTING. REPAIRED CRACK IAW DC9 SRM.SDR ABXA070138Seat Track · corrodedFOUND SEAT TRACK RIGHT BUTT LINE 44 CORRODED AT STA 718. REMOVED AND REPLACED SEAT TRACK STA 570 TO 748 IAW DC9 SRM 51-30-1. REINSTALLED FLOOR PANELS IAW DC9 SRM 51-30-1.SDR ABXA070133Structure · crackedUPPER CARGO SUBFLOOR CRACKED AT RIGHT BUTT LINE 28, FS 180. REPAIRED SUBFLOOR RIGHT BUTT LINE 28 AT STA 180 IAW DC9 SRM 53-01.SDR ABXA070137Seat Track · corrodedFOUND SEAT TRACK AT RIGHT BUTT LINE 11 CORRODED ON BOTH SIDES OF SPLICE AT STA 493. REMOVED AND REPLACED SEAT TRACK IAW DC9 SRM 53-05.SDR ABXA070136Longeron Splice · crackedFOUND LONGERON 30 SPLICE FS 794 - 813 CRACKED. REMOVED AND REPLACED LONGERON 30 STA 794 - 813 IAW DC9 SRM 53-11-3.SDR ABXA070135Seat Track · corrodedUPPER CARGO SEAT TRACK CORRODED AT RIGHT BUTT LINE 9, FS 160. REMOVED AND REPLACED SEAT TRACK IAW DC9 SRM 51-10-3 AND 51-30-1.SDR ABXA070134Structure · crackedUPPER CARGO SUBFLOOR CRACKED AT LEFT BUTT LINE 50, FS 180. REPAIRED SUBFLOOR LEFT BUTT LINE 50 AT STA 180 IAW DC9 SRM 53-01.SDR ABXA070132Hinge Fitting · crackedAFT FLAP HINGE FITTING CRACKED AT ACTUATOR ATTACH EAR, STA 164. REMOVED AND REPLACED HINGE FITTING IAW DC9 SRM.SDR ABXA070131Rib · crackedLEFT LEADING EDGE RIB HAD CRACKED DOUBLER 2ND RIB INBOARD OF NR 11 TRACK. REPAIRED RIB IAW REA D957-55597.SDR ABXA060183Power Supply · dischargedEMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY SUPPLY IAW DC9 MM 33-53-02. EMERGENCY LIGHTS OPS CHECKED GOOD.SDR ABXA050087Cusp Web · corrodedCUSP WEB CORRODED AT FS 200, BETWEEN SEAT TRACKS, RBL 44.5 - RBL 54.5. CUT OUT CORRODED SECTION OF CUSP WEB AT FS 200 RBL 49. INSTALLED REPAIR DOUBLER IAW DC-9 SRM 53-01 AND 51-30-5.SDR ABXA050233Pan · corrodedSERVICE DOOR PAN CORRODED. REMOVED AND REPLACED LOWER SECTION OF SERVICE DOOR JAMB PAN IAW DC-9 SRM 53-05.SDR ABXA050232Cusp Web · corrodedCUSP WEB ANGLE AT SERVICE DOOR THRESHOLD CORRODED. REPAIRED CUSP WEB ANGLE IAW DC-9 SRM 53-05.SDR ABXA050231Skin · crackedFUSELAGE SKIN CRACKED AFT OF SERVICE DOOR CUTOUT, AT LOWER AFT CORNER. REPAIRED AFT LOWER CORNER OF DOOR IAW DC-9 SRM 53-05.SDR ABXA050230Skin · corrodedFUSELAGE SKIN FORWARD OF KIDNEY PANEL WAS BULGING AROUND FASTENERS FROM JUST ABOVE SKIN SPLICE AT LONGERON 26 LEFT TO SPLICE AT LONGERON 26 RIGHT. INNER SKIN CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED NEW SKIN AND LONGERON IAW DC-9 SRM 51-30-2 AND 51-SDR ABXA050229Frame · crackedCENTER OVER WHEEL WELL MAIN FRAME RIGHT SIDE IN WHEEL WELL, HAD CRACK EXTENDING INTO TWO EACH FASTENERS. MAIN FRAME NEEDED REPLACED PER SERVICE BULLETIN DC9-53-100. MAIN FRAME REPLACED ON EA 53400324-001-2.SDR ABXA050074Battery · dischargedEMERGENCY EXIT LIGHTS FAILED TO REMAIN ON WITH POWER, FAILURE. REMOVED AND REPLACED EMERGENCY LIGHTING POWER SUPPLY IAW DC-9 MM 24-30. OPS CHECKED GOOD.SDR ABXA040401Odor · detectedWHILE EN ROUTE TO FSD, FLIGHT 140 HAD A SLIGHT ODOR IN THE COCKPIT. ISOLATED TO AROUND FIRST OFFICER'S MAP LIGHT. PULLED MAP LIGHT CIRCUIT BREAKER, ODOR APPEARED TO GO AWAY. DURING DESCENT, AROUND 8000 FT, ODOR RE-APPEARED. NO OTHER INDICATIONS, (I.E. SMOKSDR ABXA030436Controller · malfunctionedAFTER TAKEOFF 3000 FT, BOTH AUTO TEMP CONTROLLERS WERE SELECTED FULL HOT. ABOUT 14000 FT, AIRFLOW STOPPED & CABIN CLIMBED UNCONTROLLABLY AT 1400 FT FPM. LEFT PRESSURE GAUGE INDICATED '0' PSI, RIGHT GAUGE INDICATED '30' PSI, LEFT AND RIGHT DUCTS TEMPS PEGGED HOSDR ABXA030331Longeron · crackedLONGERON 17 CRACKED ON AFT SIDE OF BULKHEAD FS 965. REPLACED LONGERON IAW DC-9 SRM.SDR ABXA030004Control Panel · defectiveAT CRUISE, SAW SMOKE COMING OUT AROUND CENTER INSTRUMENT AND PEDESTAL LIGHT PANEL. TURNED LIGHTS OFF. DECLARED EMERGENCY, RAN CHECKLIST AND RETURNED AIRPORT, AFTER SMOKE STOPPED. ISOLATED BURNING ODOR TO CENTER INSTRUMENT PANEL LIGHTING CONTROL PANEL. REPLACEDSDR ABXA010704Light · looseEMERGENCY EVACUATION LIGHTS FLICKER OCCASIONALLY DURING TAKEOFF ROLL AND LANDING ROLLOUT. FOUND THE CAPTAIN'S SIDE LAMP LOOSE. ADJUSTED/CLEANED THE CONTACTS AND REPLACED LAMPS.SDR ABXA010702Terminal · looseEMERGENCY EVACUATION PEANUT LIGHTS CAME ON AFTER ENGINE START AND ON AIRCRAFT POWER. NO ABNORMAL ANNUNCIATOR PANEL INDICATIONS. FOUND LOOSE TERMINAL AT EMERGENCY LIGHT CIRCUIT BREAKER. TIGHTENED TERMINAL. OPS CHECKED GOOD IAW DC-9 MM 33-50-00-00.SDR ABXA010406Control Rod · malfunctionedNR 1 THRUST REVERSER UNLOCKED BUT DID NOT DEPLOY. REPLACED THE NR 1 THRUST REVERSER UNLOCK CONTROL ROD ASSEMBLY. COMPLIED WITH ADJUSTMENT TEST OF NR 1 THRUST REVERSER SYSTEM IAW DC-9 MM. OPS CHECKED GOOD.SDR ABXA010106Control Unit · faultyA LOWER CARGO FIRE ANNUNCIATOR ILLUMINATED ON SHORT FINAL APPROACH. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND DEFERRED THE CARGO SMOKE DETECTION SYSTEM IAW DC-9 MEL. ON 03/25/01, MAINTENANCE REPLACESDR ABXA000530Bracket · bentAT FL 230, CABIN PRESSURE LIGHT ILLUMINATED. THE CREW PERFORMED EMERGENCY CHECKLIST AND DESCENDED TO 22,000 FT. AT 22,000 FT, CABIN PRESSURIZATION WAS MAINTAINED. MAINTENANCE INSPECTED AND FOUND THE FORWARD MAIN ENTRY DOOR LEAKING DURING PRESSURIZATION CHECKSDR ABXA000203Panel · delaminatedRIGHT WING LOWER INBOARD TRAILING EDGE BONDED PANEL DELAMINATED. REPLACED TRAILING EDGE PANEL IAW DC9 SRM 51-30-02.SDR ABXA000202Angle · crackedRIGHT WING INBOARD TRAILING EDGE BONDED PANEL INBOARD ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1.SDR ABXA000201Vane · delaminatedLEFT FLAP INBOARD FIXED VANE WAS DELAMINATED 2 SQUARE INCHES BETWEEN CENTER RUB STRIPS. REPLACED LEFT INBOARD FLAP FIXED VANE IAW DC9 MM 27-51-03.SDR ABXA000200Floorboard · corrodedCOCKPIT FLOOR PANEL WAS HEAVILY CORRODED AT STATION 158 AND RBL 16. REPLACEDFLOOR PANEL IAW DC9 SRM 51-30-01.SDR ABXA000199Longeron · crackedLONGERON 30 CRACKED AT LEFT FLANGE, STATION 231. REPAIRED IAW ABX REA D953-36554MR.SDR ABXA000198Longeron · crackedLONGERON 29 LEFT WAS CRACKED BETWEEN STATION 302 TO 306 UNDER SPLICE. REPAIREDIAW ABX REA D953-36554MR.SDR ABXA000196Fitting · crackedSUPPORT FITTING PN 59148657 AT STA. 598 AND LONGERON 24 LT IS CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2, AND 51-30-5.SDR ABXA000195Fitting · crackedSUPPORT FITTING PN 59148658 AT STA. 598 AND LONGERON 24 RT IS CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5, AND 51-30-2.SDR ABXA9900325Latch · looseCOCKPIT DOOR INITIALLY JAMMED IN THE CLOSED AND LOCKED POSITION. AFTER DOOR WAS OPENED, THE LOCK MECHANISM WOULD NOT LATCH IN THE CLOSED POSITION. TIGHTENED SCREWS ON LATCH MECHANISM AND LUBRICATED MECHANISM.SDR ABXA9800878Bulkhead · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT CANTED BULKHEAD AT FS 699 CORRODED BETWEEN LBL 22 AND LBL 54. FABRICATED NEW PANEL IAW DOUGLAS DRAWING NR 5956065 AND ABX REA D924-24804.SDR ABXA9800877Bulkhead · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT CANTED BULKHEAD AT FS 699 CORRODED BETWEEN RBL 22 AND RBL 44. FABRICATED NEW PANEL IAW DOUGLAS DRAWING NR 5956065 AND ABX REA D924-24804.SDR ABXA9800870Angle · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT WHEEL WELL SLANT PRESSURE PANEL LOWER ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE IAW DC9 SRM.SDR ABXA9800869Angle · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT WHEEL WELL SLANT PRESSURE PANEL LOWER ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE IAW DC9 SRM.SDR ABXA9800863Skin · corrodedWHILE COMPLYING WITH C-INSPECTION, FOUND THE UPPER SURFACE OF THE CENTER WING TANK CORRODED AT REAR SPAR AT STATION XCW20. REPAIRED UPPER SKIN SURFACE IAW ABX REA D957-24799MR.
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