N6827, cancelled Sep 26, 2011
Service difficulty reports · 61
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 = 'N6827' AND deregistration_id = 'N6827-2011-09-26' 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 = 'N6827' AND deregistration_id = 'N6827-2011-09-26' 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 GAIA05036OPLight · inoperativeDURING MAINTENANCE THE CREW ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AC WAS RETURNED TO SERVICE. (K)SDR GAIA05023Engine · failedDURING CRUISE, NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON BRIGHT, NOTICED NR 2 OIL PRESSURE DROPPED RAPIDLY TO ZERO. OIL TEMPS AND QUANTITY REMAINED NORMAL. ENGINE FAILURE CHECKLIST WAS PERFORMED. N1S WIND MILLED FOR APPROXIMATELY 25 MINUTES. EMERGENCY WAS SDR GAIA04075OPLight · inoperativeL-1 EMERGENCY EXIT LIGHT DIM, COCKPIT EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED (L-1 AND COCKPIT) EMERGENCY LIGHTS. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR GAIA04048OPSmoke Detector · inoperativeLOWER CARGO FIRE WARNING ILLUMINATED SHORTLY AFTER TAKEOFF, RETURNED TO FWA. LIGHT WENT OUT BEFORE LANDING. BITE TEST CARRIED OUT. FOUND THREE SMOKE DETECTORS WEAK IN THE AFT CARGO. REMOVED AND REPLACED THREE WEAK SMOKE DETECTORS, RESET THE SYSTEM. OPS CHSDR GAIA01305OPActuator · failedFLT - 1843 - PHL-FWA - ON APPROACH TO FWA, THE FLIGHT CREW NOTICED THAT THE NR 8 SLAT DID NOT INDICATE EXTENDED WHEN THE FLAP HANDLE WAS MOVED FROM 2 DEGREES TO THE 5 DEGREE POSITION. AN EMERGENCY WAS DECLARED AND A UNEVENTFUL LANDING WAS MADE AT FWA. REMOVESDR GAIA01291OPCoalescer Bag · dirtyFLT 2031 - RNO-DEN - AFTER TAKEOFF, THERE WAS A STRONG ODOR OF JET FUEL IN THE COCKPIT. THIS AIRCRAFT MADE AN UNEVENTFUL RETURN TO RNO. REMOVED AND REPLACED BOTH CONDENSER BAGS. INSPECTED AND CHECKED FOR LEAKS. RAN APU AND ENGINES WITH NO LEAKS OR SMELL NOSDR GAIA01257STFrameDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 380 FRAME HAS SEVERAL HOLES IN THE INBOARD RADIUS BETWEEN STRINGER 4-7L. ACCOMPLISHED BS 380 FRAME REPAIR STRINGER 4-7. IAW B727 SRM 53-10-4 FIG 1. FASI NON ROUTINE 08343. (M)SDR GAIA01256STSkin · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT WING UPPER SURFACE LEADING EDGE SKIN CRACKED IN 2 PLACES AT AFT END OF NR 6 SLAT OUTBOARD HOOK SEAL CUTOUT. (M)SDR GAIA01255STSkin · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN, POPPED FASTENER HEADS, CORROSION ALONG STRINGER 24L, BS 294-310. ACCOMPLISHED FUSELAGE SKIN LAP REPAIR AT BS 294-310, STRINGER 24L IAW B727 SRM 53-30-3 FIG 5. (M)SDR GAIA01253STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD CRACKED AT RBL 2, WL 198, ALSO STIFFENERS (HORIZONTAL) ABOVE WL 200 AND BELOW WL 196 ARE CRACKED AT RBL 5. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AND STIFFENERS REPLACEMENT WL 196-200, SDR GAIA01252STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT TORQUE BOX LIGHTNING HOLE AT STATION 1225 HAS A CRACK 1 INCH LONG. ACCOMPLISHED RIGHT TORQUE BOX WEB REPAIR AT BS 1225 IAW B727 SRM 51-40-2 AND SRM 53-10-2 FIG 6. (M)SDR GAIA01251STFrame · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 CARGO DOOR CUT OUT FORWARD OUTBOARD CHORD IS CRACKED 1.5 INCH BS 1090, STRINGER 24R. ACCOMPLISHED BS 1090 FRAME REPAIR AT STRINGER 24R IAW B727 SRM 53-10-2 FIG 5 AND SRM 51-40-3 FIG 1. (M)SDR GAIA01250STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 178 BULKHEAD WEB IS CRACKED AT APPROXIMATELY WL 218, LBL 12 (POSITION 1L PER W/C 2210). ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AT LBL 12, WL 218 (POSITION 1L) PER KHA W/C 2210. (M)SDR GAIA01249STAngle · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-2 DOOR CUT OUT FORWARD FRAME LOWER STANCHION ADAPTER ATTACH ANGLE BROKEN AT BS 950E, STRINGER 26R. ACCOMPLISHED STANCHION ADAPTER ATTACH ANGLE REPLACEMENT BS 950E, STRINGER 26R IAW B727 SRM 53-10-2 FISDR GAIA01248STSkin · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BULGING SKIN AND DISHED FASTENER HEADS AT BS 215, STRINGER 24R. ACCOMPLISHED FUSELAGE SKIN LONGITUDINAL LAP SPLICE REPAIR IAW B727 SRM 53-30-3 FIG 14. (M)SDR GAIA01247STSkin · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED L1 DOOR AFT UPPER CORNER FRAME IS CRACKED 1.5 INCH BS 344, STRINGER 5L-6L. ACCOMPLISHED FORWARD ENTRY DOOR UPPER CUT OUT SKIN/FRAME REPAIR IAW S/B 727-53-0186 (ACTUAL CRACK WAS IN DOOR CUTOUT SKIN/DOUBLSDR GAIA01246STSeat TrackDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED SEAT TRACK AT BS 520-540, LBL 45.5 HAS ELONGATED HOLES. ACCOMPLISHED SEAT TRACK REPLACEMENT AT BS 480-550, LBL 45.5 IAW B727 SRM 53-10-5 FIG 1. (M)SDR GAIA01237STWeb · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED WEB AT BS 328 LBL 45 CORRODED, FLIGHTSTAR AIRCRAFT SERVICES, INC. ACCOMPLISHED FLOORWEB REPLACEMENT BS 295-351, LBL 15-45 IAW B727 SRM 51-40-2 AND SRM 53-10-2 FIG 2. (M)SDR GAIA01236STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 620 FRAME FORWARD WEB CRACKED THROUGH SEAL RETAINER FASTENER HOLES ABOVE STRINGER 25 RT. ACCOMPLISHED BS 620 FRAME WEB REPAIR AT STRINGER 2R IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 3. (M)SDR GAIA01235STAngle · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN THE AFT AIRSTAIR, THE LOWER TORQUE BOX TO BS 1342 LOWER SPANWISE CHORD STIFFENER ATTACH ANGLE IS CRACKED AT BS 1338, RBL 20, WL 200. ACCOMPLISHED STIFFENER ATTACH ANGLE REPLACEMENT BS 1338, RBL 20, WSDR GAIA01234STStringer · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRACKED AT FORWARD END OF LEFT WING SCANNING LIGHT BS 720B PLUS 5. ACCOMPLISHED STRINGER 15L REPAIR AT BS 720B PLUS 5 IAW B727 SRM 53-10-3 FIG 5. (M)SDR GAIA01233STStringer · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15L CRAKED AT AFT END OF LEFT WING SCANNING LIGHT BS 720B PLUS 15. ACCOMPLISHED STRINGER 15L REPAIR AT BS 720B PLUS 15 IAW B727 SRM 53-10-3 FIG 5. (M)SDR GAIA01232STFrame · dentedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED BS 720 FRAME DENTED IN RADIUS BETWEEN STRINER 16-17 LEFT. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINER 16-17L IAW B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. (M)SDR GAIA01231STStringer · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED STRINGER 15R CRACKED AT FORWARD END OF WING SCANNING LIGHT CUT OUT BS 720B PLUS 5. ACCOMPLISHED STRINGER 15R REPAIR AT BS 720B PLUS 5 IAW B727 SRM 53-10-2 FIG 5. (M)SDR GAIA01230STFrame · dentedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN AFT CARGO FRAME BS 1110 HAS A DENT AT STRINGER 26L. ACCOMPLISHED BS 1110 FRAME REPAIR AT STRINGER 26L IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-40-2 FIG 5. (M)SDR GAIA01229STFrame · dentedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAD A DENT BELOW STRINGER 25R. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINGER 25R IAW B27 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. (M)SDR GAIA01228STFrame · dentedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 720 HAS 2 DENTS AT STRINGER 25L. ACCOMPLISHED BS 720 FRAME REPAIR AT STRINGER 25L IAW B727 SRM 51-40-3 FIG 1 AND SRM 53-10-2 FIG 3. (M)SDR GAIA01227STFrame · dentedDURING A LTC INSPECTION, IT WAS DISCOVERED IN FORWARD CARGO FRAME BS 700 HAS 2 DENTS AT STRINGER 25L AND 24L. ACCOMPLISHED BS 700 FRAME REPAIR AT STRINGER 25L AND 24L IAW B727 SRM 51-40-4 FIG 1 AND SRM 53-10-2 FIG 3. (M)SDR GAIA01226STFloorbeam · corrodedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED IN DOG HOUSE AREA, FLOORBEAM T-CAP IS CORRODED AT BS 312 LBL 3. ACCOMPLISHED BS 312 FLOORBEAM UPPER CHORD REPAIR AT LBL 3 IAW B727 SRM 53-10-2 FIG 7 AND SRM 51-40-3 FIG 1. (M)SDR GAIA01225STBulkhead · crackedDURING A LTC INSPECTION , IT WAS DISCOVERED IN 2 CRACKS AT FASTENER LOCATIONS BS 178, RBL 10, WL 235. ACCOMPLISHED BS 178 BULKHEAD WEB REPAIR AT RBL 10, WL 235 IAW B727 SRM 53-10-9 FIG 4. (M)SDR GAIA01224STSkin · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT WING LEADING EDGE CAVITY LOWER SKIN CRACKED. ACCOMPLISHED RIGHT WING LEADING EDGE LOWER SKIN REPAIR AT WS 474 IAW B727 SRM 57-30-4 FIG 1. (M)SDR GAIA01223STAngle · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED RIGHT WING LEADING EDGE CAVITY UPPER ATTACH ANGLE CRACKED AT SLAT STATION .260, WL 343. ACCOMPLISHED RIGHT WING LEADING EDGE CAVITY UPPER ATTACH ANGLE REPLACEMENT WS 343, SLAT STATION .260 IAW B727 SRM SDR GAIA01222STSkin · crackedDURING A LTC INSPECTION ,IT WAS DISCOVERED LEFT WING INBOARD INTERNAL LEADING EDGE SKIN, ACCESS THROUGH PANEL 6301, L/E STATION 130.5 IS CRACKED AROUND SEVERAL FASTENERS. ACCOMPLISHED LEFT WING INBOARD INTERNAL LEADING EDGE SKIN CRACK REPAIR AT WS 130.5 IAW BSDR GAIA01221STPressure Panel · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED LEFT MAIN WHEEL WELL PRESSURE WEB IS CRACKED AT BS 948, LBL 65, WL 200. ACCOMPLISHED LEFT MAIN WHEEL WELL PRESSURE DECK CRACK REPAIR AT BS 948, LBL 65, WL 200 IAW BOEING DRAWING 65-89360. (M)SDR GAIA01220STPressure Panel · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED RIGHT MAIN WHEEL WELL PRESSURE WEB IS CRACKED AT BS 948, RBL 65, WL 200. ACCOMPLISHED RIGHT MAIN WHEEL WELL PRESSURE DECK CRACK REPAIR AT BS 948, RBL 65, WL 200 IAW BOEING DRAWING 65-89360. (M)SDR GAIA01219STPressure Panel · crackedDURING A LTC INSPECTION ,DISCOVERED 2 CRACKS IN NWW CEILING RECESSED WEB AT BS 285, RBL 4-8 AND BS 290, BL 0. ACCOMPLISHED NOSE WHEEL WELL RECESSED CEILING WEB CRACK REPAIR AT BS 285-290, BL 0 RBL 8 IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 2. (M)SDR GAIA01218STPressure Panel · crackedDURING A LTC INSPECTION , IT WAS DISCOVERED THAT THE NLG WW LEFT WEB IS CRACKED HORIZONTALLY AT BS 240-250, WL 180. ACCOMPLISHED LEFT NOSE WHEEL WELL WEB CRACK REPAIR AT BS 240-250, WL 180 IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 2. (M)SDR GAIA01217STSkin · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED C-3 DOOR SKIN CRACKED AT OUTER HANDLE COVER PLATE BS 1125 BETWEEN STRINGER 23-24 RIGHT, FILGHT STAR AIRCRAFT SERVICES, INC. ACCOMPLISHED NR 3 CARGO DOOR SKIN REPAIR AT BS 1125, STRINGER 23-24R IAW B727 SDR GAIA01254STWeb · crackedDURING A LTC INSPECTION AT FLIGHTSTAR, IT WS DISCOVERED VERTICAL CRACK NOSE WHEEL WELL LEFT WEB BS 260, WL 160. ACCOMPLISHED WEB REPAIR BS 260, WL 160 IN LEFT NWW IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 2. (M)SDR GAIA01239STFloorbeam · corrodedDURING A ROUTINE MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE FLOORBEAM AT BS 1030, RBL 34.5 WAS CORRODED OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 1030, RBL 34.5 IAW BOEING 727 SRM 53-10-8, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA01110OPGcu · faultyFLT 2019 - ABQ-PHX, NO CLIMB-OUT, SHORTLY AFTER FLAP RETRACTION, EXPERIENCED DIFFERENTIAL FAULT IN NR 2 SYSTEM IN COMBINATION WITH ESSENTIAL POWER LOSS AND OVER EXCITATION IN SYSTEMS 1 AND 3, WHICH RESULTED IN THE LOSS OF THE SYNCHRONIZING BUS. AIRCRAFT MADE SDR GAIA01108OPGenerator · malfunctionedFLT 2071 - GEG-PHX - AFTER TAKEOFF, LOSS OF ALL GENERATORS OCCURRED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN GEG. RAN ENGINES AND GENERATORS. LOADED GENERATORS UP ELECTRICALLY, HYDRAULICALLY AND PNEUMATICALLY. RAN FOR 15 MINUTES WITH NO DEFECTS NOTED, PER BSDR GAIA01075OPClamp · leakingFLT 2507 - GEG-IND - AT 1000 FEET AGL, ENGINE AND WING HEAT OPENED. ONE MINUTE LATER NR 1 STRUT OVER HEAT LIGHT ILLUMINATED AS A/C CLIMBED THROUGH CLOUDS INTO CLEAR. ALL ANTI-ICE SYSTEMS CLOSED AND STRUT OVER HEAT LIGHT EXTINGUISHED. NORMAL CONDITIONS THROUSDR GAIA01014Light · intermittentFLT 1777 - BOS-FWA - LOWER AFT BODY HEAT LIGHT INTERMITTENT TEST. PTT WORKS GOOD. AIRCRAFT MADE AN UNEVENTFUL LANDING IN FWA. REPLACED AFT BODY OVERHEAT LAMP. OPS CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA00793Light · inoperativeMAINTENANCE ONLY, MHR, EMERGENCY EXIT LIGHT IN COCKPIT DOES NOT ILLUMINATE.REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT. SYSTEM OPERATIONALLY CKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR GAIA00721Handle · stuckFLT 8106 - SEA-ANC - ON APPROACH, FLAP HANDLE WOULDN'T MOVE. AIRCRAFT MADE AN UNEVENTFUL ZERO FLAP LANDING IN ANC. CANNOT DUPLICATE PROBLEM ON GROUND. FLAP SYSTEM CHECK GOOD PER BAC B727 MM, 27-51-0, THROUGH NUMEROUS CYCLES. LUBED CABLES AND FLAP CONTROL VSDR GAIA9931Bulb · failedEN ROUTE FROM YIP TO HUF, THE CARGO SMOKE LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED EMERGENCY CHECKLIST PROCEDURES. THERE WAS NO SMOKE OR SMELL INTHE COCKPIT OR THE CARGO COMPARTMENT. LIGHT EXTINGUISHED 15 MINUTES LATER. ALL TEST WERE GOOD. THE AIRCRAFT SDR GAIA9857ASeal · wornDFW - AFTER DEPARTING, NR 2 ENGINE OIL PRESSURE LOW, (LOSS OF PRESSURE). ENGINE SHUT DOWN. AIRCRAFT MADE AN UNEVENTFUL RETURN TO DFW. INSPECTED ENGINE WITH NO DEFECTS NOTED. NO DEFECTS NOTED IN OIL SCREEN. GARLOCK SEAL FOR STARTER REPLACED FOR OIL QUANTITSDR GAIA9838Light · inoperativeDURING MAINTENANCE AT OKC, FOUND EMERGENCY LIGHT ABOVE L-1 DOOR FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATIONALLY CHECKS GOOD. (M)SDR GAIA9809Light · inoperativeUPON ARRIVAL TOL, CREW REPORTS EMERGENCY EXIT LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED EXIT LIGHT IAW MM ATA 33-50. SYSTEM CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M)
Back to N6827, cancelled Sep 26, 2011