Boeing 747-46NF
Service difficulty reports · 1,079
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '74746NF' 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 aircraft_model_key = '74746NF' 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 P5CA2010080201650Fairing · delaminatedRIGHT I/B FORE FLAP L/E FAIRING HAS DELAMINATION AT SEVERAL AREAS AND PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.SDR P5CA2010080201648Fairing · delaminatedLEFT WING OUTBOARD FORE FLAP INBOARD L/E FAIRING HAS DELAMINATION IN ONE AREA AND PERMANENT REPAIR WAS ACCOMPLISHED AS PER E/O 4457A279.SDR P5CA2010072201645Door · delaminatedRT WING LANDING GEAR FIXED LOWER STRUT DOOR DELAMINATED. PART ONE TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4452A082, WITH FAA 8110-3 DATED 18 JULY 2010. DVI EVERY 15 FLIGHT CYCLES WITH PERMANENT REPAIR PRIOR TO 1000 FLIGHT HOURS AFTER PART ONE SDR P5CA2010070101644Thrust Reverser · damagedLOWER BALLSCREW REMOVED FROM LEFT SLEEVE OF THE NR 2 THRUST REVERSER. TIME LIMITED REPAIR ACCOMPLISHED PER AMM 78-31-00-& NBSP; EO 4478A133 AND FAA 8110-3 DATED 27 JUNE 2010. NOTE: DETAILED VISUAL INSPECTION IS DUE EVERY FLIGHT CYCLE UNTIL PERMANENT REPAIR SDR P5CA2010060801640Structure · damagedNUMBER 4 ENGINE LT & RT CORE COWLS DAMAGED AT FORWARD EDGE AT 6 O'CLOCK POSITION. TIME LIMITED REPAIR PART ONE ACCOMPLISHED PER ENGINEERING ORDER 4471A057, WITH FAA 8110-3 DATED 08 JUN 2010. DVI EVERY 15 FLIGHT CYCLES AND PERMANENT REPAIR PRIOR TO 50 FLIGHT CSDR P5CA2010052901639Floor Panel · delaminatedMAIN DECK BS 1600 TO 1720 FLOOR PANEL DELAMINATED. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4453A366, WITH FAA 8110-3 DATED 29 MAY 2010. REPEAT DVI EVERY 25 FLIGHT CYCLES. PERMANENT REPAIR WITHIN 1000 FLIGHT HOURS.SDR P5CA2010050701636Wedge · damagedFOUND LEFT I/B AFT FLAP T/E WEDGE WITH TEAR / GROUND DAMAGE WITH A DIMENSION OF 7 X 11 X 1.5 INCHES. FLAP TIME LIMITED REPAIR PER EO 4457A248 WITH FAA 8110-3 DATED 07 MAY 2010. INSTALLED EXTERNAL DOUBLER WITH REPEAT INSPECTION AT EVERY 10 FC AND PERMANENT RESDR P5CA2010050601635Compressor · damagedMEMO MESSAGE "VVVVVV" DISPLAYED AT 1515Z AT FL 360, ENGINE 3 N2 VIBRATION AT 5.0. ALL OTHER PARAMETERS WERE NORMAL AND MONITORED. AT APPROXIMATELY 12,000 FT, NR 3 ENGINE FAILED. QRH PROCEDURES ACCOMPLISHED. INSPECTION OF TAILPIPE REVEALED NO METAL. BOROSCSDR P5CA2010042801634Switch · dirtyDURING TAKEOFF ROLL RECEIVED STATUS MESSAGE - UPPER DECK ESCAPE HATCH OPEN. UPPER DECK HATCH LINER REMOVED FOR DVI, DOOR FRAME, SKIN, SEAL, AND MECHANISM CHECKED WITH NO DEFECTS FOUND. LINER RE-INSTALLED. DOOR OPEN AND CLOSE WITH MICRO-SWITCH CLEANED AND OPSDR P5CA2010041801633Roller · damagedFIRST OFFICER SEAT, LEFT FORWARD TRACK ROLLER ASSEMBLY DAMAGED. ACCOMPLISHED ENGINEERING ORDER 4425A155, WITH FAA 8110-3 DATED 25 APR 2010 PART 1, TIME-LIMITED REPAIR TO INSTALL TEMP BOLT. DVI REQUIRED AT EVERY FLIGHT CYCLE AND PERMANENT REPAIR PRIOR TO 10 FSDR P5CA2010041801631Skin · damagedON WALK AROUND FOUND DAMAGE TO NR 4 ENGINE RIGHT CORE COWLING OUTER SKIN AT FORWARD EDGE 6 O'CLOCK POSITION. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4471A054 WITH FAA 8110-3 DATED 18 APR 2010 TO TRIM DAMAGE AND APPLY SPEED TAPE. DVI TO BE PERFSDR P5CA2010041801630Skin · crackedFOUND ON WALK AROUND 1-.5 INCH CRACK ON NR 4 ENGINE RIGHT CORE COWLING OUTER SKIN. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4471A053 WITH FAA 8110-3 DATED 18 APR 2010. DVI TO BE PREFORMED EVERY 3 FLIGHT CYCLES WITH PERMANENT REPAIR AT NEXT A-CHSDR P5CA2010041601629Skin · crackedFOUND ON WALK AROUND A 3.5 INCH CRACK ON NR 2 ENGINE RIGHT CORE COWLING OUTER SKIN. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4471A052 WITH FAA 8110-3 DATED 16 APR 2010. DVI TO BE PERFORMED EVERY 3 FLIGHT CYCLES WITH PERMANENT REPAIR AT NEXT A-CSDR P5CA2010041301628Skin · dentedLOWER AFT CARGO DOOR LOWER AFT CORNER SKIN DENT REPAIR AT BS 1920. DURING C-CHECK AT TPE ACCOMPLISHED PART 2 INTERIM REPAIR IAW ENGINEERING ORDER 44452A072 REV A.SDR P5CA2010040601626Flange · damagedENGINEERING ORDER 4457A139 REVISION "A" WITH FAA 8110-3 DATED 30 MARCH 2010 FOR ACCOMPLISHMENT OF PERMANENT REPAIR TO THE FIXED LEADING EDGE LOWER CHORD FLANGE AT ILES 817.51. THIS EO IS CLASSIFIED AS MAJOR.SDR P5CA2010032901625Sleeve · damagedSUSPECT LIGHTNING STRIKE DAMAGE FOUND ON NR 2 ENGINE OUTBOARD REVERSER SLEEVE AT TRAILING EDGE AT THE 3 O'CLOCK POSITION. TEMPORARY REPAIR ACCOMPLISHED PER EO 4478A126 WITH CHAPTER 5 LIGHTNING STRIKE INSPECTION.SDR P5CA2010031001624Winglet · damagedDURING PARKING OPERATION OF N452PA, THE LEFT WINGLET OF N450PA AND DAMAGED IT. THE LEFT WINGLET WAS REMOVED IAW CDL 57-28-1 AND AMM 57-28-01. NO FURTHER DAMAGED WAS NOTED.SDR P5CA2010031001623Winglet · damagedDURING PARKING OPERATION THE LEFT WINGLET MADE CONTACT WITH THE LEFT WINGLET OF AIRCRAFT N450PA. THE LEFT WINGLET WAS REMOVED IAW CDL 57-28-1 AND AMM 57-28-01. NO FURTHER DAMAGE WAS NOTED.SDR P5CA2010030901622Seat Track · damagedMAIN DECK SEAT TRACK FROM BS 1518 THROUGH 1530 LBL 11.33 WAS FOUND DAMAGED. TIME LIMITED REPAIR ACCOMPLISHED PER PART 1 OF EO 4453A341 AND 8110-3 DATED 08MAR10. DVI REQUIRED EVERY 5 FLIGHT CYCLES WITH A PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO THE 25TH CSDR P5CA2010030101621Nozzle · crackedENGINE 3 EXHAUST NOZZLE HAS A CRACK AT THE 12 O'CLOCK POSITION APPROXIMATELY 24 INCHES LONG RUNNING FROM 10 O'CLOCK TO 1 O'CLOCK POSITION, 13 INCHES FROM EDGE OF NOZZLE. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4478A121 AND FAA 8110-3 DATED 25 FEB 2010. DVI RSDR P5CA1001618Nozzle · crackedNUMBER TWO EXHAUST NOZZLE HAS TWO CRACKS. ENGINEERING ORDER 4478A114 ACCOMPLISHED STOP DRILL AS INTERIM REPAIR AND 3 CYCLE REINSPECTION. NOZZLE MUST BE REPLACED BEFORE NEXT A CHECK. THIS EO APPROVED BY FAA 8110-3 DATED 11 JAN 2010.SDR P5CA1001617Flap · delaminatedDURING AIRCRAFT C-CHECK INSPECTION DENT/DELAMINATION WAS FOUND ON THE LT & RT TRAILING EDGE FLAPS AND THE LT INBOARD AILERON. PERMANENT REPAIR WAS ACCOMPLISHED PER SRM 57-53-01 FIGURE 201 REPAIR 1 TABLE 1, SRM 51-70-17 FIGURE 5 AND SRM 57-60-01 FIGURE 201 AS SDR P5CA1001616Skin · damagedDAMAGE WAS FOUND TO THE RT UPPER RUDDER EXTERNAL SURFACE MID-AREA WITH DENT 1.0 INCHES IN DIAMETER. PERMANENT REPAIR WAS ACCOMPLISHED BY ENGINEERING ORDER 4455A033. THIS EO IS CLASSIFIED AS "MAJOR" AS DEFINED IN FAR 43 APPENDIX A.SDR P5CA1001615Skin · damagedDAMAGE WAS FOUND TO THE FUSELAGE SKIN RIGHT BS 2655. INTERIM REPAIR WAS PERFORMED AS PER SRM 53-00-00 AND REPEAT INSPECTION EVERY 6,000 FLIGHT CYCLES PER ENGINEERING ORDER 4453A316. THIS REPAIR IS CLASSIFIED AS "MAJOR" AS DEFINED IN FAR 43 APPENDIX A.SDR P5CA1001614Door · damagedDAMAGE WAS FOUND ON LEFT APU COMPARTMENT DOOR, A "MAJOR REPAIR" WAS PERFORMED BY ENGINEERING ORDER 4452A075 AS PER SRM 52-00-00 FIGURE 201.SDR P5CA1001620Skin · damagedDURING DEICING OPERATIONS NR 2 ENGINE INLET COWL SUSTAINED DAMAGE CONSISTING OF SCRATCHES ON THE EXTERNAL SKIN AT APPROXIMATELY 10 O'CLOCK POSITION. DAMAGE IS OUT OF ALLOWABLE DAMAGE SRM 54-15-01 LIMITS. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDERSDR P5CA2010012201627Panel · crackedDURING WALK AROUND CHECK THE LEFT LOWER LEADING EDGE PANEL IN FRONT OF THE FUELING PANEL DOOR WAS FOUND CRACKED. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4457A227 AND FAA 8110-3 DATED 22JAN10. DVI REQUIRED EVERY A-CHECK WITH PERMANENT REPAIR TO BE ACCOMPLISHESDR P5CA1001619Nozzle · crackedNUMBER TWO EXHAUST NOZZLE HAS A CRACK. ENGINEERING ORDER 4478A115 & FAA 8110-3 DATED 19 JAN 2010. ACCOMPLISHED TO STOP DRILL CRACK AS INTERIM REPAIR & DVI EVERY 3 FLIGHT CYCLES. NOZZLE MUST BE REPLACED BEFORE NEXT A-CHECK.SDR P5CA2009111501612Depressor · damagedDURING WALK AROUND CHECK THE MAIN DECK, SIDE CARGO DOOR SEAL DEPRESSOR ON THE FORWARD AND AFT SIDES WERE FOUND TO BE DAMAGED AT THE TOP CORNERS. TIME LIMITED ACCOMPLISHED IAW EO 4453A308. FAA 8110-3 ISSUED 15 NOV 2009. DVI REQUIRED EVERY FLIGHT CYCLE WITH PSDR P5CA2009111201611Depressor · damagedDURING WALK AROUND FOUND DEPRESSOR SEAL DAMAGE ON MAIN DECK SIDE CARGO DOOR FWD SIDE APPROX 1.5 IN X 0.5 IN. TIME LIMITED REPAIR ACCOMPLISHED AS PER EO 4453A307. FAA 8110-3 ISSUED 12 NOV 09. DVI REQUIRED EVERY FLIGHT CYCLE WITH PERMANENT REPAIR TO BE ACCOMPSDR P5CA2009111001610Depressor · damagedDURING WALK AROUND CHECK THE MAIN DECK, SIDE CARGO DOOR SEAL DEPRESSOR ON THE FORWARD SIDE APPROXIMATELY 1 INCH DOWN FROM TOP WAS FOUND TO BE DAMAGED. TIME LIMITED REPAIR ACCOMPLISHED IAW EO4453A306. FAA 8110-3 WAS ISSUED 10 NOV 09. VISUAL INSPECTION REQUIRSDR P5CA2009100201608Window · delaminatedDURING CRUISE FLIGHT R1 WINDOW ARCED AND THE OUTER LAYER OF WINDOW DELAMINATED. WINDOW AND WINDOW HEAT CONTROLLER REPLACED IAW AMM 56-11-01.SDR P5CA2009090401607Seal Depressor · damagedAFT LOWER CARGO SEAL DEPRESSOR DAMAGED AT UPPER AFT CORNER. ACCOMPLISHED PART 1 OF EO 4453A275 SINCE REPAIR DEVIATES FROM SRM EO WAS APPROVED VIA FAA FORM 8110-3 ISSUED 30 AUG 2009. A VISUAL INSPECTION IS REQUIRED EVERY FLIGHT CYCLES UNTIL PERMANENT REPAIR CSDR P5CA2009090101606Sleeve · crackedCRACK FOUND ON NR 2 ENGINE EXHAUST SLEEVE FROM 12 O'CLOCK TO THE 1 O'CLOCK POSITION. NO OTHER DAMAGE FOUND. INTERIM REPAIR ACCOMPLISHED IAW EO 4478A097/FAA 8110-3 DATED 29 AUG09. DETAIL VISUAL INSPECTION DUE EVERY 3 FLIGHT CYCLES AND PERMANENT REPAIR DUE ATSDR P5CA2009082801605Sleeve · crackedCRACK FOUND ON THE NR 2 ENGINE EXHAUST SLEEVE AT THE 12 O'CLOCK POSITION DURING WALK AROUND INSPECTION. INTERIM REPAIR ACCOMPLISHED IAW EO 4478A096 ISSUED PER FAA 8110-3 DATED 27 AUG 09. DETAILED VISUAL INSPECTION DUE EVERY 3 FLIGHT CYCLES UNTIL NEXT A-CHECKSDR P5CA0901604Tire · separatedAIR TURNBACK DUE TO GEAR MONITOR AND GEAR TILT EICAS MESSAGE CAUSED BY NUMBER 12 TIRE CAP SEPARATION. REPAIRS ACCOMPLISHED PER AMM, WDM, SRM. TIRE REPLACED PER AMM 32-45-01.SDR P5CA2009071301602Structure · damagedDURING WALK AROUND INSPECTION FOUND BIRD STRIKE DAMAGED TO THE LE OF THE LEFT WING GEAR DOOR. "TEMP. REPAIR PER EO 4452A093 AS PER SRM 51-70-07 WITH DVI INSP AT EVERY 5 FLT CYCLES AND PERMANENT REPAIRS AT THE NEXT A- CHECK."SDR P5CA2009071301603Skin · damagedON POST FLIGHT WALKAROUND FOUND LEFT INBOARD FLAP MISSING PIECE OF SKIN. "DAMAGE FOUND TO BE WITHIN LIMITS AS PER SRM 51-70-02. PERFORMED TIME LIMITED REPAIR IAW SRM 57-53-01/51-70-17. REQUIRED DIVE CYCLES WITH PERMANENT REPAIR NEXT "A" CHECK."SDR P5CA2009061601600Structure · dentedON WALK AROUND CHECK, FOUND NR 26 VARIABLE CHAMBER FLAP FOLDING NOSE HAS A DENT 3 INCH BY 1/3 INCH WITH A DEPTH OF 1/4 INCH. TIME LIMITED REPAIR ACCOMPLISHED PER EO 4457A194 PART 1. SEALANT AND ALUMINUM FOIL TAPE APPLIED.SDR P5CA2009061101599Blades · damagedCREW REPORTED VIBRATION FROM NR 1 ENGINE ON CLIMB. CREW DUMPED FUEL AND RETURNED TO LAX. FOUND EVIDENCE OF BIRD STRIKE IN NR 1 ENGINE INLET. ACCOMPLISHED BIRD STRIKE INSPECTION PER AMM 72-00-00 AND 05-51-14. REPLACED 7 DAMAGED FAN BLADES PER AMM 72-31-02.SDR P5CA2009060501598Fairing · damagedWHILE ATTEMPTING TO REPLACE THE MISSING LEFT OUTBOARD HORIZONTAL STABILIZER STATIC DISCHARGER, MAINTENANCE FOUND A PORTION OF THE STABILIZER TIP FAIRING DAMAGED. A REPLACEMENT WAS RECEIVED AND INSTALLED PER SRM 51-10-02.SDR P5CA2009052901597Exhaust Pipe · crackedDURING WALK AROUND CHECK, AN 8 INCH LONG CRACK WAS FOUND AT THE 12 O'CLOCK POSITION 13 INCHES FROM THE TRAILING EDGE OF THE NR 2 ENGINE EXHAUST NOZZLE. "AREA WAS INSPECTED IAW SRM 54-41-30 AND EO 4478A086 WAS ISSUED BY ENGINEERING WITH FAA 8110-3. THE AIRCRASDR P5CA2009052901596Exhaust Pipe · crackedDURING WALK AROUND CHECK, A 12 INCH LONG CRACK WAS FOUND AT THE 12 O'CLOCK POSITION 13 INCHES FROM THE TRAILING EDGE OF THE NR 3 ENGINE EXHAUST NOZZLE. "AREA WAS INSPECTED IAW SRM 54-41-30 AND EO 4478A085 WAS ISSUED BY ENGINEERING WITH FAA 8110-3. THE AIRCRASDR P5CA200904140194Warning Message · false activationEICAS MESSAGE BTL LOW ENGINE A APPEARED ON CLIMB-OUT AT 1000 FEET, ALSO BOTTLE A DISCHARGE LIGHT ON OVERHEAD ALSO ILLUMINATED. AT APPROX 20,000 FEET ALL LIGHTS EXTINGUISHED. "REMOVED BOTTLE, WEIGHED AND REINSTALLED. OPENED MEL 26-20-1. SQUIB TEST ACCOMPLISHSDR P5CA2009033001589Bleed Valve · malfunctionedCREW REPORTED VIA ACARS EXPERIENCED BLEED PROBLEMS. "ICN MAINTENANCE TROUBLESHOT TO THE NR 2 PRSOV. DEACTIVATED VALVE AND DEFERRED THE ITEM PER DDG 36-11-1."SDR P5CA2009031501588Sleeve · cracked2.5 IN CRACK FOUND ON NR 2 ENG EXHAUST NOZZLE OUTER SLEEVE AT THE TRAILING EDGE AT THE 10 O'CLOCK POSITION. "PER EO 4478A081, STOP DRILLED CRACK AND REPAIR WITHIN 10 FLIGHT CYCLES. FAA 8110-3 ISSUED 15 MAR 09".SDR P5CA2009022501587Chiller · defectiveGALLEY CHILLER MOTOR MAKES GRINDING SOUND AND COMPARTMENT HAS BURNED ELECTRICAL ODOR. REPLACED CHILLER.SDR P5CA2008020601585Access Door · missingNR 1 RT OUTBOARD STRUT ACCESS DOOR 454DR WAS FOUND TO BE MISSING DURING WALK AROUND INSPECTION. EO 4454A072 WAS ISSUED WITH A TIME LIMITED REPAIR AND A PERMANENT REPAIR TO BE DONE PRIOR TO 25 FLIGHT CYCLES.SDR P5CA2008010901586Rvdt · faultyDURING CLIMBOUT OF NRT, CREW EXPERIENCED SEVERE WIND SHEAR AND A FLAP ASYMMETRY PROBLEM. OUTBOARD TRAILING EDGE FLAPS WOULD NOT RETRACT PASSED 5 DEGREES. AIRCRAFT RETURNED TO NRT. CONDITIONAL INSPECTIONS FOR HIGH ENERGY STOP AND SEVERE TURBULENCE WERE ACCOMSDR P5CA2008121801584Panel · damagedDURING LOADING OF MAIN DECK DAMAGE WAS FOUND ON THE CEILING PANEL BETWEEN STA 620 AND 720 AT RBL 17.0. DAMAGE WAS FOUND TO BE OVER LIMIT EO 4425A100 WAS ISSUED CONSISITING OF A TEMPORARY REPAIR AND DVI EACH A-CHECK ACFT DEPARTED.
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