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 UIEA2011030900214Rib · crackedCRACK ON 65B23604-26, RIB OF RT HST L/E FAIRING LWR SIDE AT STA 518.646. (REPAIR IAW T2011A55B-608 REV 00; 01)SDR UIEA2011030900213Rib · crackedCRACK ON 65B23604-24 RIB OF RT HST L/E FAIRING LWR SIDE AT 510.103. (REPAIR IAW T2011A55B607, REV 00; 01)SDR UIEA2011030900212Rib · crackedCRACK - CRACK ON 65B23604-22 RIB OF RT HST L/E FAIRING LWR SIDE AT STA 501.559. (REPAIR IAW T2011A55B-605, REV 00; 01)SDR UIEA2011030900204Rib · crackedCRACK - CRACK ON 65B23604-14 RIB OF RT HST L/E FAIRING LWR SIDE AT STA 467.384. (REPAIR IAW T2011A55B-604, REV 00; 01)SDR UIEA2011030900200Rib · crackedCRACK ON 65B23604-12 RIB OF RT HST L/E FAIRING LWR SIDE AT STA 458.841. (REPAIR IAW T2011A55B-603, REV 00 ; 01)SDR UIEA2011030900198Rib · crackedCRACK ON 65B23604-10 RIB OF RT HST L/E FAIRING LWR SIDE AT STA 450.297. (REPAIR IAW T2011A55B-602, REV 00; 01)SDR UIEA2011030900197Rib · crackedCRACK ON 65B23604-8 RIB OF RT HST 4E FAIRING LWR SIDE AT STA 441.753. (REPAIR - IAW T2011A55B-601, REV 00 ; 01)SDR UIEA2011030900189Skin · dentedFOUND BULK CARGO DOOR OUTER SKIN HAD DENT AT STA 1994 L X W X D = 1" X 0.6" X 0.031" (REPAIR - IAW SRM 52-00-01-2R-9, REV 58.)SDR UIEA2011030900182Skin · crackedCRACK ON THE FOLDING NOSE SKIN OF LT WING NR 10 VC FLAP OTBD EDGE AT ILES 779.50.SDR UIEA2011030900153Skin · dentedDENT - FWD BULK CARGO DOOR OUTER SKIN HAD DENT AT STA 1994 L-1", W-0.6", D-0.031". (IN PROCESS).SDR UIEA2011030900152Skin · dentedDENT- FWD EXTERNAL SKIN HAD A DENT AT AFT AND LOWER SIDE, STA 1917 TO 1918 (IN PROCESS).SDR UIEA2011030800235Skin · dentedFOUND EXTERNAL SKIN HAD DENT AT AFT CARGO DOOR FWD; LWR SIDE, STA 1812 TO STA 1815. (REPAIR - IAW EI T2011A52B-564, REV 00 ; REV 01)SDR UIEA2011030800187Skin · dentedFOUND EXTERNAL SKIN DENTED AT FWD CGO DOOR AFT; LWR STA 670. (REPAIR IAW SRM 52-30-01-2R-2, REV 58).SDR UIEA2011030800147Skin · dentedFWD EXTERNAL SKIN DENTED AT FWD CARGO DOOR AFT AND LOWER SIDE STA 670. REPAIRED FWD CARGO DOOR SKIN IAW SRM 52-30-01 REPAIR 2 FIGURE 201 SHEET 10 REV 58.SDR UIEA2011030800146Skin · dentedDENT FWD EXTERNAL SKIN HAD DENT AT AFT CGO DOOR FWD AND LOWER SIDE. STA 1812 TO STA 1815 (OPEN)SDR UIEA2011030800148Slide · no testDURING U/D SERVICE DOOR SLIDE DEPLOYMENT TEST FOUND SLIDE AUTOMATIC AND MANUAL DEPLOY FUNCITONAL FAIL. (OPEN)SDR UIEA2011030700192Structure · chafedCHAFING DAMAGE ON THE NR 1 ENG NACELLE STRUT INBD AFT SIDE OF FR ACCESS DOOR ASSY. (REPAIR IAW EI T2011A54B-536, REV 00)SDR UIEA2011030600144Sleeve · crackedDURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 8" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OFSDR UIEA2011030200137Lens · damagedDURING WALK-AROUND INSP AT PVG, MX FOUND THE LT OTBD LANDING LIGHT - LENS COVER ASSY DAMAGED. (DISPOSITION WAS MADE TO ACCOMPLISH TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSP EVERY 1 FC AND PERMANENT REPAIR BY REPLACING TSDR UIEA2011030200138Skin · damagedEGAT FOUND DAMAGE ON EXISTING REPAIR OF AFT CARGO DOOR (P/N 65B04250-17, S/N 001244) OUTER SKIN AT FOWARD LOWER SIDE AND SEAL RETAINERS (P/N 65B04712-5) IN FEBRUARY 2011.(A PERMANENT REPAIR WAS ACCOMPLISHED PER NRC 346 AND EGAT EL NO. T2011A52B-332. BOEING APPSDR UIEA2011022800134Skin · damagedDURING D2-CHECK, A DENT AND A GOUGE WERE FOUND ON RT FUSELAGE SKIN AT BS 2586, S-50R TO S-51R.THE DENT AND GOUGE WERE LOCATED CLOSE TO AN EXISTING EXTERNAL SKIN REPAIR AND THE DENT AND GOUGE WERE BEYOND THE ALLOWABLE LIMIT PER SRM 53-00-01 FIG.101. REPLACED THSDR UIEA2011022800133Shutoff Valve · stuckFIRE INDICATION, WARNING AND FIRE BELL DURING CLIMB. PERFORMED "FIRE ENGINE 4" CHECKLIST PER QRH. FIRE EXTINGUISHED IMMEDIATELY AFTER DISCHARGE OF ONE BOTTLE(FOUND NR 4 PRSOV STUCK OPEN. REPLACED PRSOV AND PERFORMED PNEUMATIC HEALTH CHECK. ALL PNEUMATIC CHECKSSDR UIEA2011022400122Warning Message · illuminatedCONFIGURATION GEAR CENTER, TAKEOFF WARNING AT APPROX 20 KTS. REJECTED TAKEOFF(BODY GEAR STEERING INDICAITON SYSTEM DEACTIVATED AND DEFERRED. BODY GEAR SYSTEM CONFIRMED DEACTIVATED)SDR UIEA2011022300132Skin · dentedDENT DAMAGE IN 65B23701-5 SKIN WAS DETECTED AT BS 529 BETWEEN S23L TO S24L. DEPTH OF DENT WAS .046 INCHES, WIDTH WAS 1.1 INCHES, & LENGTH WAS 1.9 INCHES AS RECORDED PER EGAT NRC 035. TO RESTORE THE TRIMMED OUT AREAS OF 65B23701-5 SKIN TO ITS ORIGINAL STRENGTH SDR UIEA2011021800090Skin · delaminatedMAJOR REPAIR. DURING WALK-AROUND INSP. MX FOUND THE NR 4 RT THRUST REVERSER TRANSLATING COWL WITH DELAMINATION DAMAGE TO THE OUTER SKIN, LOCATED APPROX AT THE 3 O'CLOCK POSITION (REF FIG 1 AND 2). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESSDR UIEA2011021600140Bolt · wrong partFWD NR 1, NR 8 BOLT TOO SHORT REF EGAT EI NR T2011A27B-349, REV 00. REPLACED NEW BOLT.SDR UIEA2011021600089Stiffener · damagedDURING LOADING OPERATIONS AT ACC THROUGH THE NOSE CARGO DOOR, LOADER DROPPED CAUSING DAMAGE TO BS260, WL195.8 - CANTED BULKHEAD STIFFENERS (2 EA), CONSISTING IN EDGE CRACKS MEASURING 1.5 INCHES LONG (REF FIG 1). DAMAGE TO THE STIFFENERS EXCEEDS THE SRM 53-10-SDR UIEA2011021500063Fairing · crackedEO 4452A115: DURING WALKAROUND INSP, MX FOUND THE LT WING GEAR DOOR FAIRING - LOWER EDGE CRACKED, MEASURING 3.0 IN. X 1.5 IN. (REF FIG 1). TIME LIMITED REPAIR HAS BEEN ACCOMPLISHED AFTER PART 1 IAW SRM 51-70-17 & SRM 51-70-07.SDR UIEA2011021400139Access Door · wornWORN ON NR 1 PYLON RT ACCESS DOOR ASSY. REPAIRED DAMAGE AREA IAW T2011A54B-34, REV 00.SDR UIEA2011021100060Compressor · smokeDURING OFFLOAD, LOADMASTER NOTED SMOKE COMING OUT OF THE RT SIDE VENT AT STA 850. ISOLATED SMOKE TO POTABLE WATER COMPRESSOR, INSPECTED GENERAL AREA AND NO ABNORMALITIES FOUND. POTABLE WATER COMPRESSOR INOPERATIVE AND POTABLE WATER SYS DEACTIVATED.SDR UIEA2011021100050Control Cable · frayedFWD LT WING SPOILER CTRL CABLE WS1A-3 BROKEN STAND. REPAIRED IAW AMM 27-61-00, REV 70 ADJUSTMENT / TEST.SDR UIEA2011021100049Control Cable · wornFWD LT AILERON CONTROL CABLE AS-3 WORN OUT. REPAIRED IAW AMM 27-11-00 REV 70. ADJUSTMENT TEST.SDR UIEA2011021100048Control Cable · wornFWD LT AILERON CONTROL CABLE AB-9 WORN OUT. (IAW AMM 27-11-00. ADJUSTMENT TEST.)SDR UIEA2011021100047Control Cable · frayedFWD RT WING SPOILER CONTROL CABLE WSIA-6: BROKEN STRAND (IAW AMM 20-11-03. REV 70. ADJUSTMENT/TEST).SDR UIEA2011020900136Skin · damagedDURING D-CHECK INSP OF DATUM ACFT, A SCRATCH AND DENT WERE REPORTED ON THE BULK CARGO DOOR (PN 65B01857-22, SN TLS11203) OUTER SKIN AT THE FWD LOWER CORNER. (THE DAMAGED AREA WAS REPAIRED IAW EGAT NRC 352 AND EGAT EI T2011A52B-363 BY TRIMMING OUT THE DAMAGE ASDR UIEA2011020800086Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 441. REPAIRED DAMAGE AREA IAW EI T2011A55B-289 REV 00 AND REV 01.SDR UIEA2011020800085Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 450. REPAIRED DAMAGE AREA IAW EI T2011A55B-290 REV 00 AND REV 01.SDR UIEA2011020800084Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 467. REPAIRED DAMAGE AREA IAW EI T2011A55B-292 REV 00 AND REV 01.SDR UIEA2011020800083Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 493. REPAIRED DAMAGE AREA IAW EI T2011A55B-294 REV 00 AND REV 01.SDR UIEA2011020800082Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 527. REPAIRED DAMAGE AREA IAW EI T2011A55B-298 REV 00 AND REV 01.SDR UIEA2011020800081Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORZ STAB STA 518. REPAIRED DAMAGE AREA IAW EI T2011A55B-297 REV 00 AND REV 01.SDR UIEA2011020800080Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 510. REPAIRED DAMAGE AREA IAW EI T2011A55B-296 REV 00 AND REV 01.SDR UIEA2011020800079Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 501. REPAIR DAMAGE AREA IAW EI NO T2011A55B-295 REV 00 AND REV 01.SDR UIEA2011020800078Rib · crackedCRACKED RIB AND LOWER CLIP IN THE FIXED L/E NOSE CAVITY RT HORIZONTAL STAB STA 484. REPAIRED DAMAGE AREA IAW EI T2011A55B-293 REV 00 AND REV 01.SDR UIEA2011020800077Rib · crackedCRACKED RIB AND LOWER CLIP IN THE FIXED L/E NOSE CAVITY RT HORIZONAL STAB STA 458. REPAIRED DAMAGE AREA IAW EI T2011A55B-291 REV 00 AND REV 01.SDR UIEA2011020800076Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, LT HORIZONTAL STAB STA 518. REPAIRED DAMAGE AREA IAW EI T2011A55B-291 REV 00 AND REV 01.SDR UIEA2011020800075Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, LT HORIZONTAL STAB STA 510. REPAIRED DAMAGE AREA IAW EI T2011A55B-287 REV.00 AND REV 01.SDR UIEA2011020800074Rib · crackedCRACKED RIB IN THE FIXED L/E NOSE CAVITY, LT HORIZONTAL STAB STA 501. REPAIRED DAMAGE AREA IAW EI T2011A55B-286 REV 00 AND REV 01.SDR UIEA2011020800073Rib · crackedCRACKED LOWER RIB AND CLIP IN THE FIXED L/E NOSE CAVITY HORIZONAL STAB 458. REPAIRED DAMAGE AREA IAW EI T2011A55B-285 REV 00 AND REV 01.SDR UIEA2011020800072Rib · crackedCRACK - RIB AND LOWER CLIP HORIZONTAL STAB STA 450. FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI T2011A55B-284 REV 00 AND REV 01.
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