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 P5CA2011051100043Access Panel · damagedNUMBER 1 ENGINE STRUT FAIRING ACCESS PANEL 452EL HAS FASTENER HOLE ELONGATED. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1025.SDR P5CA2011051000026Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE FAIRING RIB AT STATION 501.559 IS CRACKED ON THE LOWER SIDE. PERMANENT REPAIR ACCOMPLISHED IAW EI T2011A55B-1059.SDR P5CA2011051000020Blowout Door · wornNR 3 ENGINE, RIGHT THRUST REVERSER FORWARD AND AFT EDGES OF BLOW OUT DOOR SHOWS WEAR. PERMANENT REPAIR ACCOMPLISHED IAW T2011A78B-1028.SDR P5CA2011051000034Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 441.753 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000042Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 527.190 HAS CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000040Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 159.109 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000039Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 131.946 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000038Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 510.103 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000037Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 501.559 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000035Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 467.384 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000032Rib · crackedLEFT HORIZONTAL STABILIZER LEADING RIB AT STATION 407.579 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000030Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 159.109 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000029Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 151.543 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000028Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 145.011 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000027Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE FAIRING RIB AT STATION 501.103 HAS CRACK ON THE LOWER SIDE. PERMANENT REPAIR ACCOMPLISHED IAW EI T2011A55B-1059.SDR P5CA2011051000018Blowout Door · wornNR 1 ENGINE, RIGHT THRUST REVERSER FORWARD AND AFT EDGES OF BLOW OUT DOOR SHOWS SIGNS OF WEAR. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A78B-1026.SDR P5CA2011051000033Rib · crackedLEFT HORIZONTAL STABILIZER LEADING EDGE RIB AT STATION 450.297 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A55B-1059.SDR P5CA2011051000025Door Frame · crackedCRACK ON NR 1 PYLON, RIGHT SIDE, FWD PRESSURE RELIEF DOOR FRAME OF AFT FAIRING. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1110.SDR P5CA2011051000024Skin · crackedBOTTOM OF AFT CARGO DOOR, OUTER SKIN AT STATION 1770 HAS A CRACK. ACCOMPLISHED PERMAMENT REPAIR IAW SRM 52-30-01, REPAIR 2, DETAIL IV, FIGURE 201, SHEET 9.SDR P5CA2011051000023Skin · damagedTHE EDGE OF THE FUSELAGE SKIN AT STATION 2598, S-42R IS DAMAGED. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A53B-1054.SDR P5CA2011051000022Panel · damagedDADO PANEL AT STATION 1720 OF THE LEFT SIDE OF THE MAIN DECK IS DAMAGED. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A25B-1053.SDR P5CA2011051000019Blowout Door · wornNR 2 ENGINE RIGHT THRUST REVERSER FORWARD AND AFT EDGES OF BLOW OUT DOOR SHOWS WEAR. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A78B-1028.SDR P5CA2011051000017Frame · crackedCRACK FOUND ON THE AFT HAT FRAME OF NR 2 ENGINE, LEFT CORE COWL. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A71B-990.SDR P5CA2011051000016Access Panel · damagedCHAFING DAMAGE ON NR 1 ENGINE NACELLE STRUT, INBOARD AFT SIDE OF ACCESS PLATE 452FR. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-958.SDR P5CA2011051000015Panel · damagedWEAR DAMAGE FOUND ON FASTENER HOLE OF NUMBER 4 ENGINE STRUT FAIRING PANEL 482EL. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1001 DATED 22APRIL11.SDR P5CA2011051000014Skin · dentedFUSELAGE SKIN AT BS 2601.5 BETWEEN S-46R AND S-49R HAS A DENT. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-01, REPAIR 15, DETAIL I, REV 59.SDR P5CA2011051000013Skin · activatedFORWARD CARGO DOOR OUTER SKIN AT THE LOWER AFT SIDE HAS CREASE AT STATION 667.5 TO STATION 678. ACCOMPLISHED PERMANENT REPAIR IAW SRM 52-30-01, DETAIL III, REV 59.SDR P5CA2011050600012Seat Track · crackedCRACK ON MAIN DECK SEAT TRACK AT STATION 995 RBL 75.92, .8 INCH LONG. PERMANENT REPAIR ACCOMPLISHED IAW 747-400F SRM 53-00-52, REPAIR 13, REV 59.SDR P5CA2011050600010Seat Track · crackedCRACK ON MAIN DECK SEAT TRACK AT STATION 995 LBL 75.92 ABOUT.8 INCH LONG. PERMANENT REPAIR ACCOMPLISHED IAW 747-400F SRM 53-00-52, REPAIR 13, REV 59.SDR P5CA2011050300009Fairing · damagedLEFT WING GEAR DOOR FAIRING DAMAGE. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4452A121.SDR P5CA2011030400007Cowling · damagedDURING THE REPEAT DETAILED VISUAL INSPECTION OF PART 2 OF EO4471A069 IT WAS FOUND THAT THERE WAS ADDITIONAL DAMAGE FOUND TO THE RIGHT CORE COWL. A TIME LIMITED REPAIR WAS ACCOMPLISHED ACCORDING TO REVISION A OF THIS SAME EO & FAA 8110-3 DATED 28FEB11. REPEATSDR P5CA2011030300006Light · inoperativeEMERGENCY LIGHT LOCATED ON THE MAIN DECK, ZONE A, WAS FOUND TO BE INOPERATIVE. BOTH LAMPS IN THE ASSEMBLY WERE REPLACED IAW AMM 33-51-07 AND OPERATION WAS & NBSP; NORMAL THEREAFTER.SDR P5CA2011030300005Light · inoperativeL1 DOOR SILL EMERGENCY LIGHT ASSEMBLY HAS THE AFT BULB OUT. THE AFT BULB WAS REPLACED IAW AMM 33-51-05. LIGHT TEST WAS NORMAL.SDR P5CA2011020900004Unknown · odorDURING LOADING OPERATIONS THERE WAS A NOTICEABLE ELECTRICAL SMELL IN COCKPIT. ACCOMPLISHED VISUAL INSPECTION OF ALL IDS, COCKPIT LIGHTING, FMS SYSTEM AND ALL CB PANELS. THERE WERE NO DEFECTS NOTED. EQUIPMENT COOLING TEST WAS ACCOMPLISHED PER AMM 51-58-00 ANSDR P5CA2011020700003Thrust Reverser · damagedNUMBER 4 ENGINE THRUST REVERSER TRAILING EDGE DAMAGED AT 6 O'CLOCK POSITION. (TIME LIMITED REPAIR ACCOMPLISHED IAW PART 1 OF EO 4478A160, WITH FAA 8110-3 DATED 01FEB2011. A DETAILED VISUAL INSPECTION IS REQUIRED EVERY 1000 FLIGHT HOURS AND A PERMANENT REPAIRSDR P5CA2011020700002Cowling · damagedNUMBER 4 ENGINE LOWER CORE COWL DAMAGED AT 6 O'CLOCK POSITION. TIME LIMITED REPAIR ACCOMPLISHED IAW PART 1 OF EO 4471A069, WITH 8110-3 DATED 07FEB2011. DVI EVERY 15 FLIGHT CYCLES WITH PERMANENT REPAIR DUE PRIOR TO 9000 FLIGHT HOURS AFTER PART 1 IS ACCOMPLISHSDR P5CA2010100901669Lens · damagedDURING WALK AROUND INSPECTION FOUND LT OUTBOARD LANDING LIGHT LENS COVER ASSEMBLY DAMAGED. TIME LIMITED REPAIR ACCOMPLISHED AS PER EO 4433AO25.SDR P5CA2010092901668Control Panel · malfunctionedLT EFIS CONTROL EICAS AND STATIS MESSAGE CIRCUT BREAKER POPPED WITH SMOKE AND FUMES FROM LT EFIS CONTROL. REMOVED AND REPLACED LT EFIS AS PER AMM 31-61-02 OPERATIONAL CHECK HAD STATIS MESSAGE #31460. ITEM DEFERRED ON LOG PAGE #435034.SDR P5CA2010092901667Control Panel · malfunctionedLT EFIS CONTROL EICAS AND STATIS MESSAGE CIRCUIT BREAKER POPPED WITH SMOKE AND FUMES FROM LT EFIS CONTROL. REMOVED AND REPLACED LT EFIS CONTROL AS PER AMM 31-61-02. OPERATIONAL CHECK RETURNED STATIS MESSAGE 31460 ITEM DEFERRED ON LOG PAGE 435034.SDR P5CA2010929001Control Unit · failedLEFT EICAS AND STATUS MESSAGE CIRCUIT BREAKER POPPED WITH SMOKE AND FUMES FROM LT EFIS CONTROL. REMOVED AND REPLACED LT EFIS CONTROL AS PER AMM 31-61-02. OPERATIONAL CHECK RETURNED STATUS MESSAGE NR 31460. ITEM DEFERRED ON LOG PAGE 435034.SDR P5CA20100922002Cowling · erodedNR 3 ENGINE RT FAN COWL LEADING EDGE HAS ERROSION DAMAGE -FOUND ON WALKAROUND BY MAINTENANCE.A TIME LIMITED REPAIR WAS ACCOMPLISHED IAW PART 1 OF EO 4471AO64 AND FAA FORM 8110-3 DATED 22 SEPT.2010 WITH DVI EVERY 5 FLIGHT CYCLES AND A PERMENANT REPAIR PRIOR TO SDR P5CA2010081101663Support · damagedBS 1920 MAIN DECK LEFT SIDEWALL SUPPORT STRUCTURE UPPER CORNER WAS FOUND DAMAGED. TIME LIMITED REPAIR WAS ACCOMPLISHED PER ENGINEERING ORDER 4425A173, WITH FAA 8110-3 DATED 30 JULY 2010. DVI REQUIRED EVERY FLIGHT CYCLE WITH PERMANENT REPAIR DUE PRIOR TO 1000SDR P5CA2010080201659Floor Support · deformedBULK CARGO COMPT AT STA 2020 TO STA 2060 LBL 37 HAS DEFORMED FLOOR SUPPORT WITH PERMANENT REPAIR AS PER ENGINEERING ORDER 4453A407.SDR P5CA2010080201658Floor Support · deformedBULK CARGO COMPT AT STATION 2000 LBL 37 HAS DEFORMED FLOOR SUPPORT WITH PERMANENT REPAIR AS PER ENGINEERING ORDER 4453A407.SDR P5CA2010080201657Frame · crackedNR 4 ENGINE RT CORE COWL HAS MOST AFT FRAME CRACKED. REMOVED AND REPLACED FRAME HAS PERMANENT REPAIR AS PER ENGINEERING ORDER 4471A061.SDR P5CA2010080201656Skin · delaminatedLEFT WING OUTBOARD AILERON LOWER SURFACE MID SECTION HAS 1 EA AREA OF DELAMINATION WITH PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A280.SDR P5CA2010080201655Skin · dentedRIGHT WING OUTBOARD AFT FLAP LOWER SURFACE MID AREA HAS DENT MARK WITH PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.SDR P5CA2010080201654Fastener · looseLEFT WING OUTBOARD MID FLAP T/E HAS NR 9 FINGER BRACKET AFT ATTACH MOUNT SCREW LOOSE AT MOST O/B END WITH PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.SDR P5CA2010080201653Fairing · erodedLT WING OUTBOARD FORE FLAP L/E FAIRING FOUND EROSION AND PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.SDR P5CA2010080201652Skin · delaminatedRT WING I/B MID-FLAP UPPER SURFACE O/B SECTION HAS ONE AREA OF DELAMINATION WITH PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.
Back to Boeing 747-46NF