N945F, cancelled May 4, 2015
Service difficulty reports · 70
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 = 'N945F' AND deregistration_id = 'N945F-2015-05-04' 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 = 'N945F' AND deregistration_id = 'N945F-2015-05-04' 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 EIA2002019Battery · inoperativeDURING CRUISE AT FL 330, AT APPROX 2015Z, THE NR 1 NAV FAILED. SHORTLY AFTER THAT, THE CAPTAINS ADI TUMBLED THEN THE TRANSMITT FUNCTION OF THE RADIOS FAILED. REPLIES WERE MADE BY THE IDENT ON THE TRANSPONDER. ALL LIGHTS IN THE COCKPIT OTHER THAN THE MASTER SDR 20000620SH020Web · corrodedDURING C-CHECK FOUND CORROSION ON CUSP WEB BS 937 TO BS 965, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000619SH016Web · crackedDURING C-CHECK, FOUND CRACKS AND CORROSION ON CUSP WEB BS 775 TO BS 897, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000619SH015Floorbeam · misdrilledDURING MAINTENANCE, THE FLOORBEAM AT BS 756, RBL 45, AND BS 737, RBL 45, WERE FOUND MISDRILLED. (X)SDR 20000619SH013Bulkhead · crackedDURING C-CHECK, FOUND CRACK IN DOUBLER ON THE AFT PRESSURE BULKHEAD BS 996. CAUSE UNKNOWN. (X)SDR 20000619SH012Skin · dentedDURING C-CHECK, FOUND MULTIPLE DENTS IN FUSELAGE SKIN BS 351 TO BS 362, LONGERON 23R TO LONGERON 26R. CAUSE UNKNOWN. (X)SDR 20000619SH011Web · crackedDURING C-CHECK, TWO CRACKS WERE FOUND IN RHS CUSP WEB A BS 605 TO BS 617, RBL 44.5 TO RBL 60. CAUSE UNKNOWN. (INT)SDR 20000619SH009Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES, CRACKS, AND CORROSION ON CUSP WEB AT BS 737 TO BS 756, RBL 44.5 AND RBL 60. (X)SDR 20000619SH010Web · corrodedDURING C-CHECK, FOUND ELONGATED HOLES, CRACKS, AND CORROSION ON CUSP WEB AT BS 737 TO BS 756, RBL 44.5 AND RBL 60. (X)SDR 20000615SH013Web · crackedDURING C-CHECK, FOUND CRACK IN CUSP WEB, BS 598, LBL 44.5. CAUSE UNKNOWN. (X)SDR 20000619SH017Beam · crackedDURING C-CHECK, FOUND CRACK IN FORWARD CARGO DOOR HORIZONTAL BEAM, PN 9957663-13. CAUSED BY FASTENER TOOL. (X)SDR 20000619SH014Seat Track · crackedDURING C-CHECK, FOUND CRACK ON THE HORIZONTAL FLANGE OF SEAT TRACK, MAIN CABIN FLOOR. CAUSE UNKNOWN. (X)SDR 20000619SH008Structure · misdrilledDURING C-CHECK, FOUND MISLOCATED HOLES COMMON TO CUSP TEE AT BS 775, LBL 60. CAUSE UNKNOWN. (X)SDR 20000615SH040Floorboard · crackedDURING C-CHECK, FOUND FLOOR PANEL DENTED AND CRACKED IN TWO PLACES FROM BS 447 TO BS 452.5, BL ZERO. CAUSE UNKNOWN. (X)SDR 20000615SH039Structure · misdrilledDURING C-CHECK, FOUND MISLOCATED HOLES COMMON TO CUSP TEE AT BS 794, LBL 60. CAUSE UNKNOWN. (X)SDR 20000615SH038Floorboard · puncturedDURING C-CHECK, FOUND PUNCTURE IN FLOOR PANEL AT RT BS 516.5, RBL 10-26. CAUSE UNKNOWN. (X)SDR 20000615SH037Pan · damagedDURING C-CHECK, FOUND OVERSIZED FASTENER HOLE IN THE FORWARD ENTRANCE DOOR PAN AT LEFT BS 197.75 NEAR BEAM NR 1. CAUSE UNKNOWN. (X)SDR 20000615SH036Longeron · misdrilledDURING C-CHECK, FOUND DOUBLE DRILLED HOLES ON FLANGE OF LONGERON L30 AT BS 340. CAUSE UNKNOWN. (X)SDR 20000615SH035Skin · misdrilledDURING C-CHECK,, FOUND MISLOCATED HOLES IN FUSELAGE SKIN AT BS 951.8 TO BS 959.6, LONGERON L24. CAUSE UNKNOWN. (X)SDR 20000615SH034Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES, CRACKS AND CORROSION ON CUSP WEB AT BS 775 TO BS 832, LBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH033Bulkhead · misdrilledDURING C-CHECK, FOUND NUMEROUS HOLES MISLOCATED IN THE WEB AT RT BS 965 BETWEEN L7 AND L15. CAUSE UNKNOWN. (X)SDR 20000615SH032Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES, CRACKS, AND CORROSION ON CUSP WEB AT BS 832 TO BS 897, LBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH031Longeron · corrodedDURING C-CHECK, CORROSION DAMAGE WAS FOUND ON L29L AND L30. CAUSE UNKNOWN.SDR 20000615SH030Web · crackedDURING C-CHECK, FOUND NUMEROUS CRACKS AND ELONGATED HOLES IN CUSP WEB AT BS 218 TO BS 237, LBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH029Web · crackedDURING C-CHECK, FOUND NUMEROUS CRACKS AND ELONGATED HOLES IN CUSP WEB AT BS 237 TO BS 313. CAUSE UNKNOWN. (X)SDR 20000615SH028Seat Track · misdrilledDURING C-CHECK, FOUND MISLOCATED HOLES IN SEAT TRACK AT BS 266 TO BS 455, LBL 54.0. CAUSE UNKNOWN. (X)SDR 20000615SH027Floorboard · damagedDURING C-CHECK, FOUND ELONGATED HOLES IN CABIN FLOOR PANEL NR 14, PN 5922429-37. CAUSE UNKNOWN. (X)SDR 20000615SH026Floorbeam · misdrilledDURING C-CHECK, FOUND MIS-DRILLED HOLE IN UPPER CAP OF FUSELAGE FLOORBEAM AT BS 427, LBL 37. (X)SDR 20000615SH025Floorboard · crackedDURING C-CHECK, FOUND ELONGATED FASTENER HOLES AND CRACKS IN CAPTAIN''S FLOOR PANEL, PN 9910078-3. CAUSE UNKNOWN. (X)SDR 20000615SH024Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES AND CRACKS IN CUSP WEB BS 756 TO BS 775, LBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH023Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES, CORROSION, AND CRACKS IN CUSP WEB AT BS 756 TO BS 775, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH022Web · damagedDURING C-CHECK, FOUND ELONGATED HOLES IN CUSP WEB AT BS 503 TO BS 598,RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH021Floorbeam · corrodedDURING C-CHECK, FOUND CORROSION ON FLOORBEAM, PN 9958212-25 AT BS 756, APPROXIMATELY LBL 14.5. CAUSE UNKNOWN. (X)SDR 20000615SH020Web · damagedDURING C-CHECK, FOUND ELONGATED HOLES IN CUSP WEB AT BS 313 TO BS 389, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH019Web · damagedDURING C-CHECK, FOUND ELONGATED HOLES IN CUSP WEB AT BS 389 TO BS 503, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH018Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES AND CRACKS IN CUSP WEB BS 218 TO BS 237, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH017Web · crackedDURING C-CHECK, FOUND ELONGATED HOLES AND CRACKS IN CUSP WEB AT BS 237 TO BS 313, RBL 44.5. CAUSE UNKNOWN. (X)SDR 20000615SH016Floorbeam · gougedDURING C-CHECK, FOUND GOUGE IN FLOORBEAM WEB BS 100, RBL 10. CAUSE UNKNOWN. (X)SDR 20000615SH015Door Frame · damagedDURING C-CHECK, FOUND OVERSIZED HOLE IN AFT CARGO DOOR JAMB AT BS 937. CAUSE UNKNOWN. (X)SDR 20000615SH014Frame · tool damageDURING C-CHECK, FOUND HOLE AND DRILL MARKS IN FRAME BS 294 BETWEEN LONGERON L16 AND L18.SDR EIA990287Skin · crackedSEA - DURING PREFLIGHT, FOUND 11 INCH CRACK IN LEFT SIDE OF AIRCRAFT AT STATION 89, ALSO, FOUND FUSELAGE FRAME CRACKED AT STATION 83, LEFT SIDE. REPAIRED DAMAGED SKIN AREA PER SRM 51-10-03 AND SRM 51-30-02. REMOVED AND REPLACED DAMAGED FRAME WITH NEW PART PSDR 99ZZZM783Frame · crackedSEA - DURING PREFLIGHT, FOUND 11 INCH CRACK IN LEFT SIDE OF AIRCRAFT AT STATION 89, ALSO, FOUND FUSELAGE FRAME CRACKED AT STATION 83, LEFT SIDE. REPAIRED DAMAGED SKIN AREA PER SRM 51-10-03 AND SRM 51-30-02. REMOVED AND REPLACED DAMAGED FRAME WITH NEW PART PSDR EIA990188Pedal · bindingKSEA - ON FLIGHT 823, CRWE REPORTED THAT ON TAKEOFF ROLL AT ABOUT 100 KTS AIRCRAFT BEGAN PULLING TO THE RIGHT. CAPTAIN APPLIED HEAVY LEFT FOOT PRESSURE ON THE LEFT RUDDER AND HEARD AN AUDIBLE SNAP. CAPTAIN THEN RELEASED PRESSURE ON PEDAL AND AIRCRAFT IMMEDIASDR EIAA990186Seat · misinstalledMMV - DURING EVALUATION, FOUND COURIER SEAT INSTALLED PER STC SA2398S0 DID NOT C/W THE 9G FORWARD REQUIREMENT OF FAR 25.561. COURIER SEAT DEACTIVATED PER EO 25-DC9-955-99. SEAT INSTALLATION WILL BE MODIFIED PER EIA EO 25-DC9-805-91. REV C. EO APPROVED BY 811SDR EIA990187Drive Link · brokenAFTER LANDING AT PAJN, RIGHT ENGINE THRUST REVERSER WOULD NOT STOW. THRUST REVERSER DRIVE LINK P/N 5958782-503 FOUND BROKEN. (M)SDR EIAA990004Retract Mech · malfunctionedDEN - ON DEPARTURE FROM DEN, THE FLIGHT CREW, UPON ATTEMPTING TO RAISE THE LANDING GEAR, RECEIVED THE GEAR DOOR OPEN LIGHT ILLUMINATION AND THREE RED GEAR UNSAFE LIGHTS. AFTER RECYCLING THE GEAR HANDLE TO THE DOWN POSITION THE CREW RECEIVED THREE GREEN LANDINSDR EIA980361Strut · flatSEA - DURING POST FLIGHT WALK AROUND INSPECTION, THE RIGHT GEAR STRUT WAS FOUND COMPLETELY DEFLATED. DURING FURTHER INVESTIGATION IT WAS FOUND THAT THE GLAND NUT WAS COMPLETELY DISENGAGED FROM THE OUTER CYLINDER. (M)SDR EIA980350Retract Mech · dirtySEA - DURING APPROACH SET FLAPS INDICATED AS FOLLOWS 5 DEGREES, 9 DEGREES, 15, L 18 - R 16) 25 = 27.5, 40-45. CHECKED ADJUSTMENT OF CONTROL VALVE PUSHROD ARM PER MM 27-52-1, INSPECTED AND CLEANED DEBRIS (EXCESSIVE AND DIRTY LUBE) FROM FOLLOW-UP CABLES. (M)SDR EIA980349Valve · failedSEA - DURING APPROACH SET FLAPS TO 15 DEGREES (L FLAP 20R, R FLAP 15) FLAPS THEN BLEW BACK TO 10 DEGREE WHILE 15 SELECTED, SELECTED 25 GOT 30, SELECTED 40 GOT 45 INITIAL LANDED WITH 38 DEGREES. REPLACED FLAP CONTROL VALVE PER MM 27-51-1 SYSTEM CHECKED GOOD. SDR EIAA980337Skin · crackedMZJ - DURING C4 CHECK, LEFT FORWARD DOOR SKIN AT FED LOWER CORNER IS CRACKED AT TWO PLACES. REPAIRED PER SRM 52-05 FIG 32. (M)
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