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 UIEA2011020800071Rib · crackedCRACKED RIB AND LOWER CLIP HORIZONTAL STAB STA 441: FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI NO T2011A55B-283 REV 00 AND REV 01.SDR UIEA2011020800070Rib · crackedCRACKED RIB AND LOWER CLIP HORIZONTAL STAB STA 407: FIXED L/E NOSE CAVITY. REPAIRED DAMAGE AREA IAW EI NO T2011A55B-303 REV 00 AND REV 01.SDR UIEA2011020800069Rib · crackedCRACKED RIB AND LOWER CLIP STAB STA 399: LT HORIZONTAL STAB FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI NO T2011A55B-302 REV 00 AND REV 01.SDR UIEA2011020800068Rib · crackedCRACKED RIB AND UPPER CLIP L/E STA 159: LT HORIZONTAL STAB FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI NO T2011A55B-301 REV 00 AND REV 01.SDR UIEA2011020800067Rib · crackedCRACK - RIB AND UPPER CLIP L/E STA 151: LT HORIZONTAL STAB FIXED L/E NOSE CAVITY. REPAIRED DAMAGE AREA IAW EI T2011A55B-300 REV 00 AND REV 01.SDR UIEA2011020800066Rib · crackedCRACK - RIB AND UPPER CLIP L/E STA 145 LT HOR STAB FIXED L/E NOSE CAVITY. REPAIRED DAMAGE AREA IAW EI T2011A55B-299 REV 00 AND REV 01.SDR UIEA2011020700057Skin · wornFOUND WEAR ON FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2517 THROUGH 2628 LT SIDE. REMOVED DAMAGED AREA AND CHECKED REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.SDR UIEA2011020700056Skin · wornFWD WEAR ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2280 THROUGH 2416 RT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.SDR UIEA2011020700055Skin · wornWEAR FOUND ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FORM BS 2280 THROUGH 2416 LT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.SDR UIEA2011020700054Skin · wornFOUND WEAR ON THE FUSELAGE SKIN AND VERTICAL F/N SEAL INTERFACE FROM BS 2517 THRU 2628 RT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA CORD IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.SDR UIEA2011020400045Fire Detector · false activationDURING CLIMB OUT LWR FWD CARGO FIRE WARNING BELL- NO EICAS MESSAGE BUT WARNING LIGHT IN FWD LWR CARGO FIRE SWITCH. QRH PROCEDURES ACCOMPLISHED. LOWER CARGO CHECKED AND NO EVIDENCE OF FIRE, SENSORS CHECKED AND CLEANED . FIRE TEST ACCOMPLISHED; AND OK. LOWER FWSDR P5CA2011020300001Flap · damagedBIRD STRIKE INSPECTION REVEALED DAMAGE ON THE LEFT WING, INBOARD, MID FLAP, LEADING EDGE AT WBL 291.5. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4457A334 AND FAA 8110-3 DATED 30JAN11. DETAILED VISUAL INSPECTION REQUIRED EVERY 25 FLIGHT CYCLES WITH A PERMANENT SDR UIEA2011013100053Support · crackedTHE SUPPORT AND SKIN PANEL OF LT: LWR FUSELAGE LONGERON BOX FAIRING SUPPORT STRUCTURE CRACKED, S35L. STA 1372. REPAIRED IAW SRM 51-70-07, REV 58 REPAIR DAMAGE AREA.SDR UIEA2011013100052Support · crackedTHE SUPPORT AND SKIN PANEL OF RT LWR FUSELAGE LONGERON BOX FAIRING SUPPORT STRUCTURE CRACKED S35R, STA 1372 IAW SRM 51-70-07, REV 58 REPAIR DAMAGE AREA.SDR UIEA2011012500008Support Fitting · damagedDURING D-CHECK INSP OF DATUM ACFT, DAMAGE (WORN HOLE) WAS FOUND ON SUPPORT FITTING OF APU LT SUPPORT LINK FWD SIDE AT STA 2658 (REFER TO FIG 1 FOR DAMAGE LOCATION). (THE REPAIR (FIG 2) WAS PERFORMED IAW EGA-TLS-11-0009 AND WAS APPROVED IAW SR 1-1777633064 ANDSDR UIEA2011012400026Support · chafedCHAFING DAMAGE ON THE SEAL SUPPORT OF LT WING FIXED T/E SPOIL SUPPORT RIB AT WX 863.73. REPAIR IAW EI NR T201157B-154. REV 00.SDR UIEA2011012400022Frame · damagedHEAT DAMAGE ON THE FRAME INNER CHORD AT STA 2638, WL 285 LT SIDE. REPAIRED IAW EI NR T2011 A53B-139 REV EO 00, 01,02 AND 03.SDR UIEA2011012300018Intercostal · crackedCRACK ON BULK CARGO FLOOR INTERCOSTALS AT STA 2020, RBL 0.25 AND STA 2080, RBL 0.25". (REPAIRD IAW EI 2011A53B-122 REV 00 AND 01.)SDR UIEA2011012300016Skin · dentedCREASE AND DENT DAMAGE ON RT FUSELAGE SKIN AT STA 2600 S-42R LWR AFT TAIL JACK PAD AREA. (REPAIRED IAW EI NO T2011 A53B-093REV.00. AND REV 01.)SDR UIEA2011012300012Stiffener · damagedDURING THE D02 PLUS C03, GENERAL DAMAGE WAS DETECTED ON STIFFENER, DEFORMED DAMAGE WAS DETECTED ON 65B04925-47 STIFFENER, AND IMPACT CRACK DAMAGE WAS DETECTED ON THE 65B04925-84 STIFFENERS (2 PLACES).( REPAIR OF GENERAL DAMAGE ON 65B04325-42 STIFFENER AT BS 17SDR UIEA2011012300009Structure · deformedDURING D-CHECK INSP OF DATUM ACFT, DAMAGE (DEFORMATION) WAS FOUND ON AFT CARGO SEAT TRACK AT BS 1826, RBL25. (THE DAMAGE AREA WAS REPAIRED IAW SRM 53-00-52, REPAIR 10.)SDR UIEA2011012200035Web · brokenBROKEN WEB AFT LWR CARGO STRUCTURE AT STA 1760 BETWEEN STRINGER S43R TO S44R (REPAIR DAMAGE AREA IAW SRM 51-70-13, REV 58)SDR UIEA2011012100019Panel · damagedDAMAGE WAS FOUND ON M/D CARGO COMPARTMENT DADO PANEL (P/N 453U7023-33). AT STA 1720(REPAIR IAW EI NO T2011A53B-131 REV 00)SDR UIEA2011012100029Rib · crackedCRACKS ON LT HST L/E RIB AND CLIP AT L/E STA 1318 ( REPLACED CLIP IAW EO NO T2011P55B-188, REV 00. 2. REPAIRED CRACK RIB IAW EI NO T2011A55B-184 REV 00.)SDR UIEA2011012100020Panel · brokenDAMAGE WAS FOUND ON M/D CARGO COMPARTMENT DADO PANEL (P/N 453U7023-33). AT STA 1720(REPAIR IAW EI NO T2011A53B-131 REV 00)SDR UIEA2011012100017Frame · crackedREPAIR NR 4 ENG RT FAN REVERSER TORQUE BOX FWD FRAME CRACK. (REPAIR IAW EI NO T2011 A78B-208 REV 00)SDR UIEA2011012100014Structure · damagedPERFORM AFT CARGO LWR CHORD STRUCTURE AT STA 1640 BETWEEN STRINGER S49R TO S47R. (REPAIR DAMAGE AREA IAW SRM 51-70-13. REV 58)SDR UIEA2011012100013Skin · gougedDURING D02 PLUS C03 CHECK OF DATUM ACFT, GOUGE DAMAGE (1 IN LONG AND 0.003 IN WIDE) WAS FOUND ON THE FUSELAGE SKIN BETWEEN BS 1920-BS 1940 AND S-33L - S-34L.(THE SURFACE FINISH OF THE BLENDED AREA WAS INSPECTED AND VERIFIED TO BE 125 MICROINCHES OR BETTER. THESDR UIEA2011012100010Skin · damagedDURING D02 PLUS C03 CHECK OF DATUM ACFT, CREASE DAMAGE AND A DENT LOCATED ON THE RT FUSELAGE SKIN AT BS 2060 AND S-42R (LOWER AFT SIDE OF TAIL JACK'S LOCATION) WERE SCHEDULED FOR A PERMANENT REPAIR. THE DAMAGED AREAS WERE PREVIOUSLY REPORTED IAW SR 1-18269954SDR UIEA2011012000034Frame · wornWORN NR 4 ENG LT CORE COWL INNER FRAME WORN AT 7:00 POS. (REPAIR IAW 747-400 SRM 54-45-02. REPAIR 1. REV 58)SDR UIEA2011012000006Structure · dentedDURING WALK-AROUND INSP, DAMAGE WAS FOUND TO THE LOWER LOBE - BS 1820, WL 188 - LOWER AFT CARGO DOOR CONSISTING OF A DENT. LENGTH: 10 IN. WIDTH: 2.0 IN. DEPTH:0.175 (REF. FIG 1). THE DAMAGE IS OUT OF THE SRM 52-30-01, FIG 101, ALLOWABLE DAMAGE 1, DETAILS XI ASDR UIEA2011011900033Frame · wornWORN NR 4 ENG LT CORE COWL INNER FRAME WORN AT 7:00 POS. (REPAIR IAW 747-400 SRM 54-45-02. REPAIR 1. REV 58)SDR UIEA2011011900025Skin · dentedREPAIR 2 EA DENTS ON LOWER SIDE WALL FLOW PATH SKIN OF NR1 ENG; RT FAN REVERSER (REPAIR IAW EI NO. T2011A38B-155 REV 00.)SDR UIEA2011011900024Support · crackedREPAIR CRACK ON THE CHORD OF THE LT WING FIXED T/E LWR SUPPORT STRUCTURE AT WS 1293. (REPAIR IAW T2011A57B-157, REV 00.)SDR UIEA2011011900015Cowling · chafedCHAFING FOUND NR 1 ENG LT CORE COWL HAD CHAFING ON INTERIOR FRAME AREA AT ABOUT 3:00. (REPAIR DAMAGE AREA IAW SRM 54-45, FIG 201, REPAIR 1. REV 58.)SDR UIEA2011011900007Skin · dentedDURING WALK-AROUND INSPECTION, DAMAGE WAS FOUND TO THE FUSELAGE SKIN BS 2596 BELOW STR - 46R (TAIL JACK AREA) CONSISTING OF 2 DENTS. THE DAMAGE IS OUT OF THE SRM 53-00-01, FIGURE 101 ALLOWABLE DAMAGE 1, DETAIL III.SDR UIEA2011011700005Fairing · crackedDURING WALKAROUND INSP, MX REPORTED CRACK DAMAGE FOUND ON THE RT OTBD WBL1241 - L/E FIXED FAIRING. THE CRACK MEASURES 0.375 IN. LONG (REF FIG 1). THE CRACK EXCEEDS THE SRM 57-41-01, FIG 101, ALLOWABLE DAMAGE LIMITS. (DISPOSITION WAS MADE TO PERFORM TIME LIMSDR UIEA2011011500002Solenoid · inoperativeGEAR LEVER WOULD NOT RETRACT. ACCOMPLISHED QRH PROCEDURES. AIR TURN BACK. (TROUBLESHOT TO BAD SOLENOID IN LANDING GEAR CONTROL PANEL. ITEM DEFERRED DDG 32-31-1)SDR UIEA2011011400023Shim · migratedSHIM MIGRATION UNDER FIN TO BODY SUPPORT FITITNG AT STA 2517 LBL/RBL 25 (IAW EO T2011A53B-135, REV 00) REPLACE NEW SHIM.SDR UIEA2011011000032Panel · crackedLT LONGERON BOX FAIRING & NBSP; PANEL CRACK (REPAIR IAW SRM 51-70-07, REV 58).SDR UIEA2010123100249Skin · dentedDURING WALKAROUND INSP, MX REPORTED DENT DAMAGE FOUND ON THE LT OTBD FORE FLAP - WBL745 UPPER EXTERNAL SKIN PANEL. MEASURING 5.0 IN LENGTH X 3.125 IN. WIDTH & AMP; 0.625 IN. (REF FIG 1). THE DAMAGED AREA EXCEEDS THE SRM 57-53-01, FIG 101, ALLOWABLE DAMAGE 1 SDR UIEA2010122200197Skin · damagedDURING WALK-AROUND INSP BEING PERFORMED, DAMAGE WAS FOUND TO THE FUSELAGE SKIN BS 2596 ABOVE STR- 46R (TAIL JACK AREA) CONSISTING OF DENT L:1.5 IN. W:0.750 IN. D:0.0625 (REF FIG 1). THE DAMAGE IS OUT OF THE SRM 53-00-01, FIG 101. ALLOWABLE DAMAGE 1, DETAIL ISDR UIEA2010121900196Skin · damagedDURING DEICING ON 19DEC2010, THE R STABILIZER FIXED T/E PANEL WAS STRUCK AT STABILIZER BL 418. THE DAMAGE MEASURES APPROX 1.375 INCH DEEP BY 1.500 INCH WIDE AS SHOWN IN FIG 1. (THE REPAIR IAW PART 1, THE REPETITIVE INSP IAW PART 2 ARE APPROVED BY DER ON THE 8SDR UIEA2010121900195Sleeve · crackedDURING MX WALKAROUND OF N408MC MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 16" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LSDR UIEA2010121600194Sleeve · crackedDURING MX WALKAROUND, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 12" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF THE SDR UIEA2010121100189Skin · damagedDURING WALKAROUND INSP, MX FOUND DAMAGE TO THE OTBD RT WS1585 - L/E NOSE EXTERNAL SKIN MEASURING 2.5 IN. L X 1.5 IN. W AND 0.125 IN. DEPTH (REF. FIG 1). DAMAGED AREA FOUND BEYOND THE SRM 57-41-01, FIG 101, DETAIL III ALLOWABLE DAMAGE (GENERAL) LIMITS. (DISPOSSDR UIEA2010120500186Winglet · damagedDURING TAXI, ENROUTE FOR TAKEOFF. ACFT CAME IN CONTACT WITH ANOTHER ACFT ON THE TAXI WAY. THE WINGLET WAS DAMAGED. (REMOVED WINGLET AND DISPATCHED IAW CDL 57-28-1).SDR UIEA2010120300184Torque Tube · shearedDURING WALKAROUND INSP, MX FOUND THE MED L1 - UPPER TORQUE TUBE ASSY SHEARED. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE REPEAT INSPECTIONS AT EVERY 5 FC (FLIGHT CYCLES) AND PERMANENT REPAIR PRIORSDR UIEA2010112500183Web · crackedDURING WALK AROUND INSP, DAMAGE TO THE LOWER AFT CARGO COMPARTMENT - BS1850, LBL45.5 FLOOR WEB - CRACK/DAMAGE WAS FOUND MEASURING 2.0 IN. X 4.450 IN. (REF FIGURE 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIOSDR UIEA2010112300180Skin · dentedDURING WALKAROUND INSP, MX FOUND THE LWR LOBE - LWR AFT CARGO DOOR AT BS1817, LWR FWD CORNER AREA WITH A DENT/DAMAGE, MEASURING 12.5 IN. LONG X 0.150 IN. (REF FIG 1). THE DENT EXCEEDS THE SRM 52-30-01, FIG 101, DETAIL XI ALLOWABLE LIMITS. (DISPOSITION WAS MAD
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