N69735, cancelled Jul 29, 2011
Service difficulty reports · 78
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 = 'N69735' AND deregistration_id = 'N69735-2011-07-29' 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 = 'N69735' AND deregistration_id = 'N69735-2011-07-29' 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 GAIA07013OPLight · inoperativeNO FLIGHT: DURING A CHECK, FOUND L-1 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK NORMAL. AC WAS RETURNED TO SERVICE. (K)SDR GAIA0709Servo · inoperativeON DOWN WIND LEG TO LANDING WITH THE AUTO PILOT ON THE FLIGHT CREW TURNED THE YOKE LEFT AND RIGHT WITH NO MOVEMENT OF THE AIRCRAFT. A RATCHETING SOUND WAS OBSERVED. THE AUTO PILOT WAS TURNED OFF AND THE CONDITION CONTINUED FOR 1 MINUTE THEN NORMAL OPERATION SDR GAIA06023STFrame · dentedNO FLIGHT: DURING INSPECTION THE FRAME AT STATION 380 WAS FOUND DENTED BETWEEN STRINGERS S5L AND S6L. REPAIRED FRAME WITH DOUBLER REPAIR IAW SRM. AIRCRAFT RETURNED TO SERVICE. (K)SDR GAIA06024STFrame · dentedNO FLIGHT: DURING INSPECTIO THE FRAME AT STATION 400 WAS FOUND DENTED BETWEEN STRINGERS S6L AND S7L. REPAIRED FRAME WITH DOUBLER REPAIR SRM. AIRCRAFT RETURNED TO SERVICE. (K)SDR GAIA06025STFrame · dentedNO FLIGHT: DURING INSPECTION THE FRAME AT STATION 560 WAS FOUND DENTED BETWEEN STRINGERS S5R AND S6R. REPAIRED FRAME WITH DOUBLER REPAIR IAW SRM. AIRCRAFT RETRUNED TO SERVICE. (K)SDR GAIA06026STFrame · dentedNO FLIGHT: DURING INSPECTION THE FRAME AT STATION 600 WAS FOUND DENTED BETWEEN STRINGERS S6R AND S7R. REPAIRED FRAME WITH DOUBLER REPAIR SRM. AIRCRAFT RETURNED TO SERVICE. (K)SDR GAIA06005Turbine · failedDURING TAKEOFF AFTER V- THE FLIGHT CREW FELT A DULL THUD ON AN ENGINE THE NR 1 ENGINE THEN FAILED. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED TURBINE BLADE DAMAGE ON THE NR 1 ENGINE. SDR GAIA05040OPOil Filter · bypassingDURING CRUISE, DURING FLIGHT VIBRATION AND NOISE FOLLOWED BY OIL FILTER BYPASS LIGHT ON NR 3 ENGINE. NR 3 EINGINE SHUTDOWN AND ENGINE WINDMILLING PROCEDURE FOLLOWED (OIL FILTER BYPASS LIGHT WENT OUT BELOW 25 PERCENT, N2) NOTE: ENGINE WINDMILLED FOR 38 MIN AT SDR GAIA05039OPFilter · bypassingDURING CLIMB, OIL FILTER BYPASS LIGHT ILLUMINATED. RETARDING THROTTLE DID NOT EXTINGUISH. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW ABNORMAL PORCEDURES. NOTE: THE ENGINE WAS WINDMILLING FOR ABOUT 15-20 MIN AND OIL PRESSURE WAS ABOUT 20-25 PSI. FLIGHT RETSDR GAIA05033OPSwitch · out of adjustDURING CLIMB FROM 14,000 FEET THE (MAIN CARGO DOOR NOT CLOSED) LIGHT ILLUMINATED. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. ON DECENT THE LIGHT WENT OFF AT 12,000 FEET. AN UNEVENTFUL LANDING WAS MADE AT DEPARTURE. THE MAIN CARGO DOORSDR GAIA04079OPTube · brokenFLT 6007 - SEA-KTN - DURING DEPARTURE, ENGINE NR 2 N2 AT 102 PERCENT AND EGT AT RED LINE ON CLIMB-OUT, EPR AT 1.89. AIRCRAFT RETURNED. LANDING WEIGHT 142000, NORMAL LANDING AND BRAKING. LANDING WAS MADE WITHOUT INCIDENT. INSPECTED NR 2 ENGINE AND FOND BROKSDR GAIA04076AOPIndicator · smokeBOS - AFTER PUSH-BACK, FLIGHT CREW INDICATED SMOKE COMING FROM RADAR INDICATOR. REMOVED AND REPLACED RADAR INDICATOR. OPS CHECK AND SELF TEST GOOD ON GROUND. THIS CLEARS DMI NR 1855. PLACARD REMOVED. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA04076OPIndicator · malfunctionedAFTER PUSH-BACK, FLIGHT CREW INDICATED SMOKE COMING FROM RADAR INDICATOR. INSPECTED RADAR SYSTEM, FOUND BAD RADAR INDICATOR, TRANSFERRED TO DMI NR 1855 IAW MEL 34-21, CAT (C) DUE.SDR GAIA02011OPSkin · crackedDURING B-CHECK INSPECTION MAINTENANCE, FOUND A 2.5 INCH CRACK TO THE NR 3 ENGINE NOSE COWL SKIN LOCATED AT NAC STATION 77.5. MAINTENANCE REMOVED AND REPLACED THE NR 3 ENGINE NOSE COWL. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)SDR GAIA01317OPHydraulic Line · puncturedFLT 1925 - FWA-BNA - DURING CLIMB-OUT, THE CREW NOTICED THAT SYSTEM 'A' WAS LOSING HYDRAULIC FLUID. THE CREW RETURNED TO FWA, AND DECLARED AN EMERGENCY. AN UNEVENTFUL LANDING WAS MADE AT FWA. THE AIRPLANE REQUIRED TOW BACK TO THE MAINTENANCE RAMP. MAINTENASDR GAIA01240OPSwitch · dirtyFLT 2011 - PDX-MHR - DURING APPROACH, THE GEAR WAS SELECTED TO THE DOWN POSITION. ALL THREE GREEN LIGHTS ILLUMINATED AND THE NOSE GEAR LIGHT WENT OUT AND DID NOT COME BACK ON. THE FLIGHT CREW DECLARED EMERGENCY, VERIFIED NOSE GEAR POSITION THROUGH THE VIEWINSDR GAIA00590Warning System · activatedFLT 3771 - FWA-MCI - DURING CRUISE, THE APU FIRE BELL AND LIGHT CAME ON. PERFORMED CHECKLIST, DECLARED AN EMERGENCY, AND DIVERTED TO MLI. THE AIRCRAFT LANDED AT MLI WITHOUT ANY FURTHER DIFFICULTIES. DEFERRED THE APU FIRE DETECTION SYSTEM PER KHA B727 MEL. SDR GAIA00436Light · will not testFOUND DURING PREFLIGHT, EMERGENCY EXIT LIGHT DOES NOT TEST AT ENTRY WAY DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. PERFORMED A SATISFACTORY OPERATIONAL CHECK PER B-727-224 AMM. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA00046Fire Detector · malfunctionedMHR/LAX - FLT 2031 - DURING CRUISE, THE APU FIRE WARNING LIGHT ILLUMINATED. THE CREW PERFORMED ABNORMAL CHECK LIST AND DECLARED AN EMERGENCY AND RETURNED TO MHR. THE AIRCRAFT LANDED SAFELY WITHOUT ANY INCIDENT. VISUALLY INSPECTED APU AND SHROUD FOR EVIDENCESDR GAIA99212Sense Line · disconnectedFLT 2027 - DEN-MHR - DURING TAKEOFF, THE NR 2 ENGINE FAILED AFTER TAKEOFF. THE CREW PERFORMED ABNORMAL CHECKLIST AND RETURNED TO DEN DECLARING AN EMERGENCY LANDING. THE AIRCRAFT LANDED SAFELY WITHOUT ANY INCIDENT. MAINTENANCE FOUND THE SENSE LINE TO THE FUESDR CALA9801979Fitting · corrodedINSPECTION FOUND NR 4 FLAP TRACK ATTACH FITTING CORRODED. THE ATTACH FITTING WAS REMOVED AND REPLACED IAW ECRA 5740-01862 AND MM 32-11-51.SDR CALA9801952Fitting · wornRIGHT WING FORWARD SIDE OF MLG BEAM WING T/E PANEL TO BEAM ATTACH LINK FITTING HAS ELONGATED BOLT HOLES. REMOVED AND REPLACED FITTING PER SRM 51-30-1.SDR CALA9801951Fitting · corrodedNLG TRUNNION CORRODED AND PITTED IN BORES LT AND RT. REMOVED CORROSION AND PITTING, FABRICATED AND INSTALLED NEW BUSHINGS PER SRM 53-40-1.SDR CALA9801947Fairing · crackedNR 6 FLAP TRACK MID FAIRING IS CRACKED .5 INCH LONG AT SKIN AFT EDGE. STOP DRILLED CRACK, HFEC INSP, FABRICATED TYPICAL REPAIR, DRILLED, DEBURRED, COUNTERSUNK, INSTALLED REPAIR. REMOVED AN INSTALLED TRACK GUIDE, TREATED, PRIMED PER SRM 51-10-1, 51-40-2, 51-3SDR CALA9801938Housing · corrodedLEFT SIDE AFT TRUNNION BEARING HOUSING IS PITTED. REMOVED AND REPLACED LT AFT BEARING HOUSING PER MM 32-11-0.SDR CALA9801937Fairing · crackedNR 4 FLAP TRACK FAIRING AFT INBOARD ANGLE IS CRACKED .5 LONG. STOP DRILLED CRACK ON NR 4 FLAP TRACK FAIRING. FABRICATED REPAIR FROM 7075 T6 .050. LOCATED, DRILLED, DEBURRED, ALODINED, PRIMED PER SRM 51-40-3, 51-10-2, MM 51-20-12 AND INSTALLED PER SRM 51-30-SDR CALA9801936Angle · crackedRT WING NR 5 FLAP FWD INBOARD FAIRING BRACKET CRACKED IN RADIUS .25 INCH LONG. FABRICATED ANGLE FROM 7075 T6 .063. LOCATED, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED PER SRM 51-40-3.SDR CALA9801935Panel · crackedRT WING 35 FLAP TRACK AFT INBD PANEL LEADING EDGE OF PANEL IS BENT AND TORN. BLEND OUT TORN AREA PER SRM 53-10 FIG 1 MAT LOSS .001.SDR CALA9801923Fairing · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING NR 4 FLAP TRACK FAIRING AT WS 124. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, 51-10-2, MM 51-20-11.SDR CALA9801922Fairing · crackedINSPECTION FOUND A .25 INCH CRACK AT BOLT HOLE OF NR 5 FLAP TRACK CENTER FAIRING. A REPAIR WAS INSTALLED IAW SRM 51-40-2, 51-10-2, 51-40-2, 51-30-2, AND MM 51-20-11.SDR CALA9801417Anti-Ice Duct · blownTHE FIRE WARNING BELL SOUNDED FOLLOWED BY ILLUMINATION OF THE NR 3 ENGINE FIRE WARNING LIGHT ON CLIMB-OUT OF IAH AT ABOUT 900 FEET. THE NR 3 ENGINE POWER WAS REDUCED AND THE FIRE WARNINGS CEASED. A VALID FIRE TEST WAS RUN. THE LIGHT AND BELL CAME ON AGAIN WSDR CALA9801377Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT LEFT SIDE OF FUSELAGE AT CUTOUT FOR L-1 DOOR UPPER HINGE ARM. THE CRACKED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5330-02675, SRM 51-10-2 AND SRM 51-30-2, AND SERVICE BULLETIN 727-53-0198.SDR CALA9801281Skin · crackedINSPECTION FOUND A 2.75 INCH CRACK IN FUSELAGE SKIN AT L-1 DOOR LOWER HINGE CUTOUT. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-20-4.SDR CALA9801280Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME ATTACH ANGLE INSIDE LT SIDE OF VERTICAL STABILIZER AT STRINGER 5L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.SDR CALA9801302Skin · crackedINSPECTION FOUND A 2.75 INCH CRACK IN LOWER AFT FUSELAGE SKIN CUTOUT AT R-1 DOOR. THE CRACK WAS STOP DRILLED, A DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW ECRA 5307-01141.SDR CALA9801300Panel · crackedINSPECTION FOUND CRACKS IN THE NLG WHEEL WELL TOP LEFT AND TOP RIGHT SKIN PANELS. THE CRACKS WERE .75 TO 1 INCH LONG. THE SKIN WAS REMOVED IAW SRM 51-10-1. WEB SKIN WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.SDR CALA9801299Skin · crackedINSPECTION FOUND A .75 INCH CRACK THROUGH FASTENER HOLE OF SKIN AT LT SIDE OF VERTICAL STABILIZER AROUND ACCESS PANEL 9523 ABOVE BS 1215. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-0, 55-30-3, 51-10-2, 51-30-2, AND 51-00-SDR CALA9801298Stringer · crackedINSPECTION FOUND A 1.375 INCH CRACK IN RT WING VENT BOX STRINGER 19 AT WS 171.5, NR 2 TANK. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER, FILLER, AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 57-10-4, 51-10-2, 51-30-2, 51-10-6, AND 51-20-4.SDR CALA9801317Support · crackedINSPECTION FOUND A 1 CRACK IN FLOORBEAM SUPPORT AT STA 400-420, BL 0. A 2 CRACK WAS FOUND IN FLOORBEAM SUPPORT AT STA 760, BL 0. THE FLOOR SUPPORT AT STA 400-420 WAS REMOVED IAW SRM 51-30-2. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, SDR CALA9801315Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 380 TO 400, RBL 16 AND STA 1150, RBL 18. THE FLOOR SUPPORTS WERE REMOVED, NEW FLOOR SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-10-1.SDR CALA9801314Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 303 TO 344, LBL 28. THE CORROSION WAS REMOVED IAW SRM 51-10-8. ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-8.SDR CALA9801313Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 380 BETWEEN RBL 32 AND RBL 42. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT IAW SRM 53-10-8. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, AND 51-40-4.SDR CALA9801312Sidewall · crackedTHE NLG WHEEL WELL RIGHT SIDEWALL AND TOP CENTER PANEL HAD CRACKS MEASURING .5 TO 1 INCH LONG. THE CRACKED AREAS WERE CUT OUT, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.SDR CALA9801311Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 400 AND 420, RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED IAW SRM 51-30-2. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-30-2, AND 51-10-2.SDR CALA9801310Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO COMPARTMENT FRAME AT BS 680 BETWEEN STRINGER 23L AND 24L. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-2.SDR CALA9801309Skin · corrodedINSPECTION FOUND FUSELAGE BELLY SKIN CORRODED AT BS 720 TO 720A, BL 0. A DOUBLER AND SHEAR TIE WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 53-30-4, AND 53-10-4.SDR CALA9801308Stringer · crackedINSPECTION FOUND A 1.25 INCH CRACK IN STRINGER 15R AND A 2 INCH CRACK IN STRINGER 15L AT STA 720B. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, 53-10-3, AND 51-10-2.SDR CALA9801307Housing · crackedINSPECTION FOUND A 1.5 INCH CRACK IN R-2 DOOR CUTOUT UPPER HINGE HOUSING. THE HINGE HOUSING WAS REMOVED IAW SRM 51-10-1. A NEW HOUSING WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9801306Floorbeam · corrodedINSPECTION FOUND FORWARD LAV FLOORBEAM AT STA 344, RBL 24 CORRODED. THE CORRODED AREA OF FLOORBEAM WAS REMOVED, A NEW FLOORBEAM SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.SDR CALA9801305Web · crackedINSPECTION FOUND STA 700 SUPPORT WEBS CRACKED AT S22L, S23L, S23R, AND S25R. THE CRACKS WERE 1 TO 1.5 INCH LONG. THE CRACKED AREAS WERE CUT OUT. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3.
Back to N69735, cancelled Jul 29, 2011