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 UIEA2013041200192Door Frame · crackedCRACK ON L5 MAIN ENTRY DOOR FWD FRAME. REPAIRED IAW EI NR T2013A53B-671, REV O. CONDITION CHECKED NORMAL.SDR P5CA2013041000190Pump · leakingSTATUS MESSAGE HYD OVERHEAT SYSTEM 1 ACCOMPANIED BY HYD PRESS ENG 1. FOUND HYD EDP LEAKED AT OUTLET PORT. REMOVED AND REPLACED NR 1 HYD EDP PER AMM 29-11-05. SERVICED NR 1 HYDRAULIC SYSTEM PER AMM 12-12-01. OPS AND LEAK CHECK GOOD. MESSAGE CLEARED.SDR UIEA2013040900188Transmitter · failedEICAS FLAPS DRIVE, DURING RETRACTION FROM 20 TO 10. OTBD T/E FLAPS STOPPED. SEEMED LT T/E FLAP REMAINED LOWER THAN RT. EXPANDED VIEW AND STATUS T/E FLAPS INDICATED. APPROX 50-55 MIN INTO FLT. EXPANDED VIEW EXTINGUISHED AND SYS APPEARED NORMAL. DURING HOLDSDR UIEA2013040400171Computer · failedUNABLE TO ENGAGE ANY OF THE THREE AUTOPILOTS, CMC SHOWS AILERON SERVO C/FCC- C /FCC FAIL. R & R CENTER AND LEFT FCC IAW AMM 22-11-01-004-026. PERFORMED CMC TEST ON CENTER AND LT FCC PASSED REF 22-11-01 ALSO PERFORMED AUTOLAND UNIQUE TEST PASSED.SDR UIEA2013040100159Pdu · malfunctionedEICAS MESSAGE FLAPS DRIVE. CMC MESSAGE 27685 L/E L3 DRIVE FAIL IAW FIM 27-88, TASK 809, R & R L/E FLAP PDU L3 IAW AMM 27-81-03. OPS CHECK SATISFACTORY. OK TO CONTINUE SERVICE. SERVICEABLE UNIT INSTALLED.SDR UIEA2013032200145Filter · failedENGINE 4 FUEL FILTER EICAS MESSAGE AT APPROX 2000 FT, ENG 1 FUEL FILTER EICAS MESSAGE & RETURNED TO AIRPORT QRH PROCEDURES. DUMPED 40.0 KG FUEL. REPLACED NR 4 AND NR 1 ENGINE FUEL FILTERS AND LEAK CHECK, OPS CHECKS OK IAW MM.SDR UIEA2013040100160Fitting · crackedLEFT OTBD ELEVATOR MOST OTBD HINGE FITTING BS 406.8 OTBD SIDE CORNER CRACKED AT SIDE OF T/E BEAM AREA. FITTING REPLACED IAW R1-55-20-10168 REV A.SDR UIEA2013032800156Cargo Track · damagedDURING C4/A3 CHECK, CHAFE WAS FOUND ON CARGO TRACK IN SECTION 42 AT BS 885, RBL 24.75 IN FWD CARGO BAY. CARGO TRACK WAS REPAIRED IAW SRM 53-00-52-2R-10, REPAIR 10.SDR UIEA2013031800133Warning Light · illuminatedON TAKEOFF ROLL AT 60 KNOTS EICAS ANNUNCIATED BLEED 3. ABORTED TAKEOFF. MESSAGE WENT OUT AT IDLE THRUST AND BLEED HP ENG 3 MESSAGE DISPLAYED.SDR UIEA2013031500129Smoke Detector · false activationCAPTAIN`S SIDE CREW REST DETECTOR ACTIVATED WITHOUT PRESENCE OF SMOKE. SYS WAS RESET.SDR UIEA2013031200127Seat Track · damagedFOUND DAMAGE TO THE MAIN DECK SEAT TRACK BETWEEN BS 1509 AND 1521 RBL 11.33. DAMAGE FOUND TO BE BEYOND THE SRM 53-00-52, FIG 101, PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-00-52, REPAIR 12.SDR UIEA2013031000122Frame · gougedFRAME CRACKED AND GOUGED ON THE LT FRAME IN APU BAY AT BS 2664, WL 305. REPAIRED IAW NR T2013A53B-431, REV 00 AND REV 01.SDR UIEA2013030500114Exhaust Stack · crackedDURING MX WALK AROUND, FOUND A CRACK ON ENGINE NR 3 PRIMARY EXHAUST NOZZLE LOCATED AT 9 O'CLOCK POSITION AFT EDGE. THE CRACK DIMENSION RUNS 4.7500" LONG CIRCUMFERENTIAL AND LOCATED .7500" FROM THE NOZZLE AFT END. THE CRACK IS DETERMINED TO BE OUTSIDE ALLOWASDR UIEA2013030400112Seat Track · damagedDAMAGE TO THE MAIN DECK SEAT TRACK WAS FOUND CRACKED, MEASURING 11.5" LONG. DAMAGE FOUND TO BE BEYOND THE SRM 53-00-52, FIG 101, ALLOWABLE DAMAGE 1 -SEAT TRACKS LIMITS. PERFORMED A TIME LIMITED REPAIR IAW EO 4453A829.SDR UIEA2013030500113Seat Track · crackedDURING WALK-AROUND INSPECTION, DAMAGE TO THE MAIN DECK BS 1509 - 1521, LBL 11.33 - SEAT TRACK, CRACKED & DAMAGED, CRACK MEASURING 11.5 INCHES LONG. DAMAGE FOUND TO BE BEYOND THE SRM 53-00-52, FIG 101, ALLOWABLE DAMAGE 1 SEAT TRACKS LIMITS. PERFORMED A TIME LSDR UIEA2013021900093Stiffener · damagedDURING WALKAROUND INSPECTION, MX FOUND DAMAGE ON BS 260, LBL10.75 RBL10.75, WL195.8 TWO CANTED BULKHEAD STIFFENERS, CONSISTING EDGE CRACKS MEASURING 1.00 AND 0.5" LONG (REF FIG 1). DAMAGE TO THE STIFFENERS EXCEEDS THE SRM 53-10-08-1A-2 ALLOWABLE DAMAGE LIMISDR UIEA2013020700075Skin · damagedON WALK AROUND FOUND LIGHTNING STRIKE BURN MARK ON RT WINGLET T/E AT STA 121.637; WLT BL 62.836, MEASURING 2.5" X 1.0". (THE DAMAGE EXCEEDS THE SRM 57-30-01-1A-2 ALLOWABLE DAMAGE 2 - WINGLET SKIN LIMITS. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR SDR UIEA2013021900100Structure · chafedRT WING L/E NR 18 VC FLAP LOWER EDGE FOUND CHAFING. REPAIRED IAW R1 NR 57-40-10152, REV A.SDR UIEA2013021900101Support Channel · crackedNR 4 PYLON CASE DRAIN MODULE SUPPORT CHANNEL, S/E SIDE FOUND CRACKED.NR 4 PYLON CORE DRAIN MODULE SUPPORT CHANNEL FABRICATED IAW BS NO R1-94-00-10147 AND REPLACED IAW SRM 51-10-02SDR UIEA2013021900099Stop · looseNR 1 PYLON AFT BULKHEAD OTBD STOP PAD FOUND LOOSE. (NR 1 PYLON AFT BULKHEAD SIDE LOAD FITTING WORN FASTENER HOLES REPAIRED IAW R1 NO R1-5400-10146 REV B.)SDR UIEA2013021900098Skin · damagedVERT FIN L/E FAIRING 321H M/D AREA SKIN FOUND DENT AND DAMAGED. (VERT FIN L/E FAIRING 321H, PN 174U11 MID AREA SKIN DENT AREAS REPAIRED IAW R8. R1-55-33-10148).SDR UIEA2013021900097Frame · chafedNR 2 ENG RT CORE COWL INNER FACE NR 2 FRAME FOUND CHAFED. (NR 2 ENG RT CORE COWL INNER FACE NR 2 FRAME CHAFING MARK AREA REPAIRED IAW CN13-0428).SDR UIEA2013021900096Frame · chafedNR 1 ENGINE LT CORE COWL NR 2 INTERIOR FRAME FOUND CHAFING MARK. (NR 1 ENG LT CORE COWL NR 2 INTERIOR FRAME CHAFING MARK AREA REPAIRED IAW SRM 54-45-02-2R1, REP 1, FIG 201.)SDR UIEA2013020500070Access Panel · damagedDURING C3 CHECK, DAMAGE TO THE NR 4 PYLON, LT ACCESS PANEL NR 482IL WAS FOUND WITH A CRACK APPROX 6.0" IN LENGTH ON THE LOWER RADIUS AREA. ACCOMPLISHED AN INTERIM REPAIR.SDR UIEA2013020300065Fairing · damagedDURING THE CURRENT "A" CHECK, MX FOUND A DAMAGED RIVET HOLE ON THE NR 4 LT THRUST REVERSER AFT TAIL FAIRING. REMOVED AFT FAIRING, ACCOMPLISHED A REPAIR BY FABRICATING SPLICE PLATE AND AN EXTERNAL REPAIR DOUBLER, INSTALLED AFT FAIRING, SPLICE PLATE AND REPAISDR UIEA2013021900095Stringer · damagedEO1952A109 DOOR NLD RT STA 160-180 STR 14D, RT STRINGER FOUND DENT. DAMAGED STRINGER REPAIRED IAW R1 NR R1-53-11-10139 AND SRM 53-00-03 REPAIR 4.SDR UIEA2013020500069Skin · crackedDURING C3/A4 CHECK, WHILE UNDERGOING EO 4453A499 (SB 747-53A2444, REV 2/ AD 2001-22-04) INSPECTION, A CRACK WAS DETECTED IN THE FUSELAGE SKIN AT THE 11 AND 5 O'CLOCK POSITION OF A FASTENER HOLE COMMON TO S38L NEAR BS 980. PERMANENT REPAIR ACCOMPLISHED IAW SRSDR UIEA2013013100040Extinguisher · inoperativeUPPER DECK WATER FIRE EXTINGUISHER INOPERATIVE. R & R FIRE EXTINGUISHER IAW AMM 26-20-00.SDR UIEA2013021900094Skin · crackedFUSELAGE BS 933 STR 38R AT DRAG SPLICE FITTING AREA FOUND ONE FASTENER HOLE CRACKED AT FUSELAGE SKIN. REPAIRED IAW SRM 53-20-01-2R2 REPAIR 2, FIG 201.SDR UIEA2013013100039Extinguisher · inoperativeUPPER DECK LIQUID FIRE EXTINGUISHER INOPERATIVE. REPLACED FIRE EXTINGUISHER IAW AMM 26-20-00.SDR UIEA2013013100049Flap Track · damagedNR 12 FLAP TRACK DAMAGED RT OTBD MID FLAP. NEW TRACK INSTALLED WITH INSTALLATION OF SERVICE MID FLAP ASSY, REF ITEM NR 7 IAW AMM 27-51-04-401.SDR UIEA2013013100053Flap · damagedREMOVE RT OTBD MID FLAP DUE TO DAMAGE. REMOVED RT OTBD MID FLAP IAW AMM 27-51-04. INSTALLED SERVICEABLE RT OTBD MID FLAP IAW AMM 27-51-04. OPS CHECK NORMAL IAW MM 27-51-04.SDR UIEA2013013100058Carriage · lack of lubeRT WING OTBD FLAP, LUBE BOTH INBD AND OTBD MID FLAP CARRIAGES. (LUBED BOTH INBD AND OTBD CARRIAGES OF OTBD FLAP RT WING IAW AMM 12-21-20-643-001.)SDR UIEA2013013100059Lever · damagedRT WING OTBD FORE FLAP TRACK NR 12 ATTACH LEVER ASSY DAMAGED. REMOVED DAMAGED LEVER ASSY LOCATED AND INSTALLED NEW LEVER ASSY IAW COMPONENT MM 57-52-51.SDR UIEA2013012300020Bulkhead · crackedBS 1241 LT MLG WW PRESSURE BULKHEAD FOUND CRACKED AT LBL 75 AREA. REPAIRED IAW RS R1-53-48-10119)SDR UIEA2013012300022Cargo Track · corrodedCARGO TRACK HAS CORROSION AT BS 1920, BL L78. CORROSION REMOVED IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-52. APPLIED IAW AMM 51-24-11 CORROSION INHIBITOR COMPOUND APPLIED IAW AMM 51-24-13.SDR UIEA2013012300023Cargo Track · corrodedCARGO TRACK CORROSION AT BS 1900-1905, RBL 11. REPAIRED IAW SRM FIG 53-00-52-2R-12 REPAIR 12 FIG 201, RS RI-53-25-10116 CORROSION INHIBITOR COMPOUND APPLIED IAW SRM 51-20-01.SDR UIEA2013012300024Cargo Track · corrodedMAIN DECK BS 1953, RBL 11.33 CARGO TRACK HAS CORROSION. CARGO TRACK REPAIRED IAW SRM 53-00-53 REPAIR 12 FIG 201 AND R1 RI-53-25-10117 REV A.SDR UIEA2013012300025Skin · gougedGOUGE FOUND BY L1 DOOR, 3.80 X .125 DEEP. REPAIRED IAW EO 4453A127SDR UIEA2013012300026Ring · crackedNR 4 ENG RT 'C' DUCT AFT CASCADE SUPPORT RING FOUND CRACKED AT R8 CASCADE VANE NUT PLATE. REPAIRED AS PER EO 1978A067.SDR UIEA2013012300016Channel · crackedMAIN DECK RT STA 740, TENSION TIE AFT CHANNEL 1EA FASTENER HOLE FOUND CRACK APPROX 0.020". DETAIL IAW DWG. BS 740, RT TENSION TIE AFT CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1, FIG 201.SDR UIEA2013012300017Channel · crackedM/D BS720, RT TENSION TIE AFT CHANNEL ONE FASTENER HOLE FOUND CRACKED REFER TO NDT TEST REPORT. CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1, FIG 201.SDR UIEA2013012300018Channel · crackedMAIN DECK BS 760 RT TENSION TIE FWD CHANNEL TWO FASTENER HOLES FOUND CRACKED IAW NDT TEST REPORT. BS760 RT TENSION TIE FWD CHANNEL REPAIR IAW SRM 53-20-30-2R-1 REPAIR 1, FIG 201.SDR UIEA2013012300019Channel · crackedMAIN DECK BS 760 RT TENSION TIE AFT CHANNEL 1EA FASTENER HOLE FOUND CRACKED REFER TO NDT TEST REPORT. REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1 FIG 201)SDR UIEA2013012300021Web · crackedWEB FOUND CRACKED AT BS 2231, STR L22. REPAIRED IAW RI NR :RI-53-62-10120)SDR UIEA2013011800014Pdu · odorDURING CARGO LOADING, ELECTRICAL ODOR FROM MAIN DECK 8R PDU, DEACTIVATED PDU.SDR UIEA2013012000015Skin · damagedRT WING INBD AFT T/E FLAP DAMAGED AT WBL 178.46. PREPARED CLEANED AND REPAIRED AREA OF DAMAGE ON RT WING INBD AFT FLAP T/E AT STATION WBL 178.48 IAW SRM 57-51-01-2R1-1. REPAIR 1, FIG 201 SHEET 4 AND 8. IAW 250 DEGREE F; CORE. SRM 51-70-01.SDR UIEA2013010500012Pdu · inoperativePDU 17L INOPERATIVE DUE TO OVERHEATING. PULLED CIRCUIT BREAKER AND REMOVED PDU. REMOVED PDU 17L AND INSTALLED BLANKING PLATE. INSPECTED PDU WIRING AND FOUND OK.SDR UIEA2012122700565Actuator · inoperativeDURING ROUTINE INSPECTION OF NR 2 RT THRUST REVERSER, MX FOUND THE THRUST REVERSER NOT STOWING. AFTER INSPECTION FOUND UPPER BALLSCREW ACTUATOR AT FAULT. PERFORMED A DETAIL INSPECTION OF THE REVERSER HALF IN QUESTION INCLUDING REVERSER CONE BRAKE FUNCTIONAL SDR UIEA2012122400562Skin · damagedDURING POST FLIGHT WALK-AROUND INSPECTION, PUNCTURE DAMAGE APPROX 4.5" BY 2.5" WAS FOUND ON THE LOWER SURFACE OF THE L/E OF THE RIGHT WING INBD AFT FLAP. PERFORMED A TIME LIMITED REPAIR.
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