Boeing 747-47UF
Service difficulty reports · 3,116
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 = '74747UF' 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 = '74747UF' 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 UIEA2023013100070Skin · crackedTWO CRACKS FOUND AND 1EA CORROSION FOUND ON LT FUSELAGE SKIN BETWEEN BS 1680 AND 1700, STR 43L. FUSELAGE SKIN CORROSION AND CRACK AREA REPAIRED IAW RI-53-00-16037 REV A.SDR UIEA2023013140071Lamp · inoperativeDOOR 1 EMERGENCY LIGHT EQUIPMENT NO. L1854 FIND INOP. DOOR #1 EMERGENCY LIGHT NO.L1854 REPLACED AND "OP" TEST "NORMAL" IAW AMM 33-51-05 REV 106, 15 NOV 2022SDR UIEA2023012300073Skin · dentedRH I/B FORE O/B UPPER PNL FOUND DENT(<P>PERFORMED METAL HOT BOND REPAIR AS PER SRM 51-70-10 REPAIR 4 </P>)SDR UIEA2023012400074Frame · crackedFUS - LH STA 1000 BULKHEAD CHORD BETWEEN S-38 AND S-39 FOUND 1EA CRACKED.(<P>FUS - STA 1000 BULKHEAD CHORD BETWEEN STR 38L AND STR 39L CRACK AREA MODIFICATED IAW EO 4453A506 PART 3.</P>)SDR UIEA2023013140075Skin · delaminatedRHW I/B MID FLAP LOWER SURFACE FOUND DELAMINATION (O/B OF #5 FLAP TRACK)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023013140076Skin · delaminatedRHW I/B MID FLAP L/E MOST I/B AREA FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023013140078Skin · delaminatedLHW O/B FORE FLAP I/B L/E FOUND 1EA DELAMINATION (39" TO I/B EDGE)(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023012400079Skin · delaminatedLHW I/B MID FLAP I/B L/E FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2023013170051Seat Track · corrodedM/D STA 1658 TO 1680 LBL 11.33 SEAT TRACK BOTH SIDE FLANGE CORRODED.(<P>M/D STA 1650.45 TO STA 1690.45 LBL 11.33 SEAT TRACK REPAIRED IAW SRM 53-00-52-2R-12 REPAIR 12.</P>)SDR UIEA2023013170053Web · crackedLH STA 1480 WEB FOUND CRACK AFTER REMOVE LONGERON EXTENSION FTG.(<P>FX STA 1480 LH WEB CRACK AREA REPAIRED AND MODIFICATION IAW EO 4453A818 PART 7 AND SB 747-53A2860 R3 FIG 14 AND FIG 15.</P>)SDR UIEA2023013180054Skin · corroded1EA CORROSION FOUND ON STA 1720 STR 43L.(<P>FX - STA 1720 STR 43L FUS SKIN CORROSION AREA REPAIRED IAW RI-53-00-16035 REV.A</P>)SDR UIEA2023012000068Structure · crackedLH - BS 2231 STR 17L, 1EA HOLE FOUND CRACK ON AFT INNER CHORD.(<P>MED - L5 DOOR CUTOUT STA 2231 STR 17L AFT INNER CHORD CRACK AREA REPAIRED IAW RI-53-00-16036 REV A.</P>)SDR UIEA2023013120069Structure · cracked1EA CRACK FOUND ON AFT UPR CORNER OF MAIN ENTER DOOR 5L CUTOUT, CRACK FOUND ON SECOND LAYER RUNNING TO FORWARD.(<P>FX - MAIN ENTER DOOR 5L CUTOUT AFT UPPER CORNER BEAR STRAP AND SKIN CRACK AREA REPAIRED AND MODIFICATION IAW EO 4453A804 PART 3.</P>)SDR UIEA2023013170052Fitting · crackedLH STA 1480 TO 1540 STR 32-33 LONGERON EXTENSION FITTING FOUND 1EA CRACKED.(<P>FX STA 1480 TO STA 1540 STR 32L-33L LONGERON EXTENSION FTG CRACK AREA TRIMMED OFF REPAIRED IAW SB 747-53A2860R3 FIG 13 AND FIG 14 AND EO 4453A818 PART 7.</P>)SDR UIEA2023013140040Support · crackedCOCKPIT - LH RUDDER PEDAL CAVITIES I/B VERTICAL METAL PANEL CORNER FOUND CRACK.(<P>COCKPIT LH FWD PANEL SUPPORT WEB CRACK AREAS REPAIRED IAW RI-53-00-16024 REV.A</P>)SDR UIEA2023011400041Support · crackedCOCKPIT - RH RUDDER PEDAL CAVITIES I/B VERTICAL METAL PANEL CORNER FOUND CRACK.(<P>COCKPIT RH FWD PANEL SUPPORT WEB CRACK AREAS REPAIRED IAW RI-53-00-16024 REV.A</P>)SDR UIEA2023013160044Seat Track · damagedM/D STA 880 AND STA 920 RBL 11.33 SEAT TRACK SLOT HOLE ELONGATED(<P>M/D STA 830.45 TO STA 950.45 RBL 11.33 SEAT TRACK REPAIRED IAW SRM 53-00-52-2R-12 REPAIR 12</P>)SDR UIEA2023011600045Intercostal · crackedRH STA 1000 FRONT SPAR INTERCOSTAL LUG FTG FOUND CRACK(<P>M/D STA 1000 RBL 11.33" FRONT SPAR INTERCOSTAL LUG FTG P/N: 69B14592-10 REPLACED AND INSTALLED IAW EO 4453C024 PART 7 AND SB 747-53A2904 FIG 18</P>)SDR UIEA2023011600050Intercostal · crackedLEFT BS 1000 FRONT SPAR INTERCOSTAL LUG FTG FOUND CRACK M/D BS 1000 LBL 11.33" FRONT SPAR INTERCOSTAL LUG FTG P/N: 69B14592-9 REPLACED AND INSTALLED IAW EO 4453C024 PART 3 AND SB 747-53A2904 FIG 5.</P>)SDR UIEA2023011200015Landing Gear · handler errorGEAR DOOR DISAGREE MSG IN FLIGHT. SHORTLY AFTER T/O, RETURNED TO STATION. REMOVED LT WING GEAR PIN, FOUND STILL INSTALLED IAW AMM 32-09-03.SDR UIEA2022120701206Engine · stalledNR 2 ENGINE N2 VIBRATION 5.0 AND NR 2 COMPRESSOR STALLED ON CLIMB OUT. R & R NR 2 ENGINE IAW WORD CARD 71-099-02-01. OPS CHECK GOOD</P>)SDR UIEA2022081800872Door · warning lightL1 DOOR NOT FULLY CLOSED OR DOOR LOCK MECHANISM NOT FULLY ENGAGED BEFORE TAKE OFF(<P>RETURNED TO AIRPORT, INSPECTED FOR DEFECTS, FOUND NONE. CLOSED DOOR, ENSURED DOOR MECHANISM WAS FULLY ENGAGED AND PRESSURIZED AIRCRAFT. NO DEFECTS NOTED, AND NO SOUNDS INDICATSDR UIEA2022080500815Pressure System · low pressureAFTER T/O "HYD QTY 1" EICAS MSG, SHORTLY AFTER "HYD SYS 1"(<P>FOUND #1 ADP PRESSURE HOSE LEAKING. R/R #1 ADP PRESSURE HOSE PER AMM 20-11-18. PERFORMED LEAK CHECK, NO LEAKS NOTED PER AMM 29-11-17. SERVICED HYD SYS #1 PER AMM 12-12-01.</P>)SDR UIEA2022072500771Pressure Switch · faultyEICAS CAUTION MSG CAME ON FOR "XFEED CONFIG," "FUEL TANK TO ENGINE," & "FUEL XFEED 4" DURING CRUISE FLIGHT. AIRCRAFT RETURNED TO ANC.(<P>2 DEFERRALS HAD BEEN PLACED ON THE A/C IN THE ANC BEFORE DEPARTURE. #4 FUEL CROSS FEED VALVE INOP ON MEL 28-22-05-01 & #3 MSDR UIEA2022071500765Antenna · fault messageTCAS STATUS MESSAGE (REMOVED AND REPLACED TCAS COMPUTER AND TCAS LOWER ANTENNA IAW AMM 34-45-01 AND 34-45-02 BOTH OPS CHECKED& GOOD</P>)SDR UIEA2022062400661Floorbeam · corrodedCORROSION ON M/D FLOORBEAM UPPER CAP AT STA 2280 LBL 73 REMOVE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02 REV 94. 2) PERFORM FLOORBEAM REPAIR IAW SRM 53-40-51-2R-3 REPAIR 3 REV 94 AND EI T2022A53M-1725 REV 2. 3) INSTALL FASTENERS IAW SRM 51-40-02 REV 94SDR UIEA2022062400668Wedge · debondedDISBOND - AILERON, RH WING INBD AILERON OUTBD WEDGE PERFORM RH WING INBD AILERON OUTBD EDGE T/E WEDGE SKIN REPAIR. REFER TO J/C ATTACHING SHEET 0307588. 2) CONDITION CHECK IS SATISFACTORY</P>)SDR UIEA2022062400669Skin · crackedLH INBD AILERON, OUTBD EDGE T/E SKIN CRACK AND CHAFING WORN PERFOM LH WING INBD AILERON OUTBD EDGE T/E WEDGE SKIN REPAIR. REFER O J/C ATTACHING SHEET 0307587. 2) CONDITION CHECK IS SATISFACTORY</P>)SDR UIEA2022062400652Power Supply · inoperativeFOUND EMERGENCY LIGHT (L1853, L1854, L5735) INOP IAW AMM 33-51-04-002-009-001 & 33-51-04-402-012-001 REV 104. REPLACED M5170 EMERGENCY LIGHT POWER SUPPLY AND PERFORMED POWER SUPPLY INSTALLATION TEST, THE RESULT WAS SATISFACTORY</P>)SDR UIEA2022062400653Elt · failed inspFOUND FIXED ELT SELF-TEST FAIL IAW AMM AR 23-24-01/401 REV 104 REPLACED THE EMERGENCY LOCATOR TRANSMITTER. 2) IAW AMM AR 23-24-01/401 REV 104 PERFORMED ELT INSTALLATION TEST. THE RESULT WAS SATISFACTORY</P>)SDR UIEA2022062400654Web · corrodedCORROSION ON LOWER CHORD AND WEB OF WING TO BODY FAIRING FRAME ASSY (PN: 65B06749-50) AT STA 880 BETWEEN BL 0 LBL 40 REMOVED DAMAGE PARTS IAW SRM 51-40-02 REV 94. 2) REPAIRED DAMAGE AREA IAW SRM 53-00-71 REPAIR 2 REV 94 EI T2022A53M-1726 REV 1. 3) INSTALLED SDR UIEA2022062400655Frame · corrodedCORROSION - TEE LOWER FACE OF FWD LOWER FRAME STA 1239.25 LBL 30 - RBL 30 REMOVED DAMAGE PART IAW SRM 51-40-02 REV 94. 2) INSTALL THE NEW PART IAW SRM 51-40-02 REV 94 DWG 651310533 SH21 REV D; 65B10533 SH24 REV C; 65B10533 SH26 REV A; 65B10533 SH28 REV C; 6SDR UIEA2022062400656Cap · corrodedCORROSION ON CAP AT M/D FLOOR SUPPORT BEAM STA 2369.8 RBL 15.75 REMOVE DAMAGE PART IAW SRM 51-40-02 REV 94. 2) INSTALL NEW PART IAW SRM 51-40-02 REV 94 AND DWG 65B06154 SHEET 1 REV A 65B38754 SH8 REV A. 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2022062400657Floor Support · corrodedFOUND M/D FLOOR STRUCTURE SUPPORT CORROSION AT STA 2376 RBL 16 REMOVE DAMAGE PART IAW SRM 51-40-02 REV 94. 2) INSTALLED NEW PART IAW SRM 51-40-02 REV 94 AND DWG 65B38754 SHEET 8 REV A. 3) JOB COMPLETED</P>)SDR UIEA2022062400658Shear Tie · crackedCRACK - FOUND SHEAR TIE HAVE CRACK AT STA 1000 RBL 57.5 REMOVE DAMAGE SHEAR TIE IAW SRM 51-40-02 REV 94. 2) INSTALL NEW SHEAR TIE IAW EI T2022A53M-1601 REV 2 AND SRM 51-40-02 REV 94. 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2022062400660Web · crackedCRACK DAMAGE ON THE WEB OF LH SIDE HST CLOSURE RIB ON STAB BL 421.50. REMOVE DAMAGE PARTS IAW SRM 51-40-02 REV 94. 2) REPAIR WEB IAW SRM 55-10-09-2R-13 REV 94 AND EI T2022A55M-1751 REV 1. 3) INSTALL NEW PARTS IAW SRM 51-40-02 REV 94 AND DWG 65B03520 SH2 REV G.SDR UIEA2022062400659Shear Tie · crackedCRACK - FOUND SHEAR TIE HAVE CRACK AT STA 1000 RBL 33.99 REMOVE DAMAGE SHEAR TIE IAW SRM 51-40-02 REV 94. 2) INSTALL NEW SHEAR TIE IAW EI T2022A53M-1601 REV 2 AND SRM 51-40-02 REV 94. 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2022062400662Cap · corrodedCORROSION ON THE UPPER CAP (PN: 65B38075-3) OF M/D FLOOR STRUCTURE AT STA 1500, BETWEEN LBL 75.92 AND LBL 98.58 REMOVE AFFECTED FASTENERS IAW SRM 51-40-02 REV 94. 2) REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REPAIR 3 REV 94 AND EI T2022A53M-1662 REV 1. 3) INSTASDR UIEA2022062400663Floorbeam · noneDEVIATION FOR SB 747-53A2443 UPPER DECK FLOORBEAM INSPECTION AND MODIFICATION(<P>1) ACCOMPLISHED JOB IAW EI T2022A53M-1591 REV 1. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2022062400664Cap · corrodedCORROSION ON THE UPPER CAP (PN: 65B38075-3) OF MAIN DECK FLOOR STRUCTURE AT STA 1500, BETWEEN RBL 75.92 AND RBL 98.58 REMOVE AFFECTED FASTENER IAW SRM 51-40-02 REV 94. 2) REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REPAIR 3 REV 94 AND EI T2022A53M-1661 REV 1. 3SDR UIEA2022062400665Floorbeam · corrodedCORROSION DAMAGES ON MAIN DECK FLOORBEAM UPPER CAP AT STA 2140, NEAR LBL 61 AND 83.5(<P>1) REMOVE AFFECTED FASTENERS IAW SRM 51-40-02 REV 94. 2) REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REPAIR 3 REV 94 AND EI T2022A53M-1696 REV 1. 3) INSTALL REPAIR PARTS IAW SSDR UIEA2022062400666Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER CAP AT STA 2240 BETWEEN RBL 33.99 AND RBL 67.01 REMOVE AFFECTED FASTENERS IAW SRM 51-40-02 REV 94. 2) REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REPAIR 3 REV 94 AND EI T2022A53M-1653 REV 1. 3) INSTALL PARTS IAW SRM 53-00-51-2R-3 REPSDR UIEA2022062400667Seat Track · corrodedCORROSION DAMAGES ON THE MAIN DECK SEAT TRACK (PN: 65B38268-2) AT STA 2090, 2150 AND 2220, RBL 89.67(<P>1) REMOVE AFFECTED FASTENERS IAW SRM 51-40-02-REV 96. 2) REPAIR DAMAGE AREA IAW SRM 5-00-52-2R-6 REPAIR 6 REV 94 AND EI T2022A53M-1659 REV 2. 3) INSTALL REPSDR UIEA2022062200645Fire Detector · damagedPRIOR TO DEPARTURE, ENG 4 FIRE DET LOOP B WAS DEFERRED. SHORTLY AFTER TAKEOFF, LOOP A ON THE SAME ENGINE BEGAN FLAGGING IN AHM. QRH PROCEDURES FOR DUAL LOOP FAILURE INDICATES FIRE DETECTION AND OVERHEAT DETECTION MAY BE INOP FOR THAT ENGINE. DUE TO CLOSE PROXISDR UIEA2022060200568Indicator · fault messageENGINE #2 OIL QUANTITY INDICATED 19 PRIOR TO START, 14 AFTER START, 10 AT THE TOP OF THE CLIMB, AND DECREASED TO 7 BY LANDING AFTER 2:51 FLIGHT TIME. RETURNED TO RKSI WITH ENGINE #2 AT IDLE POWER. REMOVED AND REPLACED WITH NO.2 ENG AND THEN LEAK CHECK NORMAL SDR UIEA2022051700486Plate · migratedR/H W/W STA 1350 WING LANDING GEAR SUPPORT BEAM SPLICE LOWER PLATE AFT I/B CORNER SHIM MIGRATED. SHIM MIGRATION INSPECTION PER SRM 51-20-08, MOUNT BOLT TORQUE CHECK PERFORMED PER SRM 51-40-04-0G-0, EDGE SEALEANT APPLIED PER AMM 51-31-01.SDR UIEA2022052200493Attach Plate · corrodedR/H WLG W/W STA 1241 R/H CTR OJ PUMP BONDING ATT SURFACE FOUND CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITSSDR UIEA2022052200494Attach Plate · corrodedL/H WLG W/W STA 1241 L/H CTR OJ PUMP BONDING ATT SURFACE FOUND CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101 LIMITS.SDR UIEA2022052200495Attach Angle · crackedM/D RHS STA 960 S-7 FRAME FWD / CREASE BEAM LWR ATT ANGLE CRACKED. LOCAL FABRICATED ANGLE P/N: 65B38488-159 AS PER BOEING DWG: 65B38488 PL AND INSTALLED AS PER SRM 51-40-02 REV 94 DATE 20FEB2022</P>)SDR UIEA2022052200496Skin · cracked#4 ENG R/H CORE COWL LWR AREA OF AIR EXHAUST FOUND 2EA BOLT HOLE CRACKED SKIN 2EA BOLT HOLE CRACK AREA REPAIRED AS PER SRM 54-45-01-2R-4 REPAIR 4 FIG 201</P>)
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