Boeing 747-4H6
Service difficulty reports · 524
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 = '7474H6' 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 = '7474H6' 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 KCSA111159Light · inoperativeAPPROX STA 630, UPPER DECK EMERGENCY EXIT LIGHT INOP.SDR KCSA111158Sign · inoperativeRT UPPER DECK EMERGENCY DOOR EXIT SIGNS BOTH INOP.SDR KCSA111157Sign · inoperativeLT UPPER DECK EMERGENCY DOOR, UPPER EXIT SIGN INOP.SDR KCSA111155Stringer · corrodedSTR 42R AT STA 2160 HAS CORROSION ON UPPER SIDE WEB FLANGE OF STRINGER.SDR KCSA111154Web · corrodedSTA 2160 - 2180 STR 40R HAS SMALL AREA OF CORROSION ON SIDE WEB FLANGE.SDR KCSA111153Stringer · corrodedSTA 2160 - 2180 STR 41R CORROSION THROUGH STRINGER SIDE WEB FLANGE.SDR WRLA20110512485Reveal · crackedCRACKED SKIN AT DOOR REVEAL POS: L/1 FWD LOWER SIZE OF 1 INCH. REPAIRED IAW FRR WOA-744-001 PER KAL-WLD-11-0003-02B DATED 10 MAY 2011.SDR WRLA20110510481Stringer · debondedDISBONDED STRINGER 10R AND 10AR BETWEEN STA 360 - STA 380 RT STRINGER 10. COMPLIED WITH WOA EO 10-53000-101 R1, PERFORMED TERMINATING ACTION PER SB 747-53A2409 REV 5, THIS COMPLIES WITH AD 2006-20-02.SDR WRLA20110510480Attach Bolt · wornNR 2 PYLON ATTACH FITTING SEALANT MISSING ON FWD SIDE AND PARTIALLY MISSING ON AFT SIDE DIAGONAL SIDE BRACE (BEARING ROTATION). SUP - COMPLIED WITH WOA EO 09-5400-56R2 TERMINATING ACTION. SERVICE BULLETIN 747-54A2218R3 (PARTS 3 AND 4).SDR WRLA20110510483Doubler · crackedMANUFACTURED DOUBLER BS 1220 RT SIDE SHEAR TENSION TIE UPPER AREA FRAME WEB 2 INCH CRACK. TRIM OUT CRACK STA 1220 IAW SRM 53-40-07 HFEC AREA NO CRACKS FOUND IAW SRM 51-00-00 FIG 3 PG 6. FABRICATED PARTS IAW SRM 53-40-07 FIG 201. INSTALLED PER SRM 53-40-07 FSDR WRLA20110510482Frame · crackedCRACK RT BS 1160 FRAME 1 EA HOLE ( AFTER 0.313 OVERSIZE REAMING) CRACK STILL PROGRESSING. TRIMMED OUT CRACK AT FRAME BS1160 IAW SRM 53-40-07. HFEC AREA NO CRACKS FOUND IAW SRM 51-00-00 FIG 3 PG 6. FABRICATED PARTS IAW SRM 53-40-07 FIG 201. INSTALLED PER SRSDR WRLA20110303473Fire Warning · activatedCREW REPORTED A NR 4 FIRE INDICATION INFLT AND SHUT THE ENGINE DOWN. THE NR 4 ENG A-LOOP IS CURRENTLY ON DMI FOR BEING INTERMITTENT. MX IS OPENING THE ENGINE TO CHECK THE WIRING AND FIRE DETECTORS.SDR KCSA111058Battery Pack · failedUPPER DECK LT DOOR EMERGENCY OPENING SYSTEM FAILED BATTERY PACK CHECK.SDR KCSA111057Light · inoperativeEMERGENCY LIGHT IN FORWARD SECTION OF UPPER DECK IS INOP.SDR KCSA111056Light · inoperativeEMERGENCY LIGHT IN STAIR WELL TO UPPER DECK IS INOP.SDR KCSA111055Light · inoperativeCOCKPIT EMERGENCY LIGHT INOP.SDR KCSA101110Skin · damagedEXTERNAL FUSELAGE SKIN IS DAMAGED AT BS 215 BETWEEN STR 42AR AND 43R.SDR KCSA101109Skin · damagedEXTERNAL FUSELAGE SKIN IS DAMAGED AT BS 210 BETWEEN STR 43R AND 45R.SDR KCSA101108Skin · damagedEXTERNAL FUSELAGE SKIN IS DAMAGED AT BS 190 BETWEEN STR 42AR AND 43R.SDR KCSA101107Skin · damagedEXTERNAL FUSELAGE SKIN IS DAMAGED AT BS 150 BETWEEN STR 42AR AND 45R.SDR UIEA2010071200107Skin · crackedAN INSP IN THE UPPER FWD CORNER SKIN OF THE AFT CARGO DOOR CUTOUT REVEALED A CRACK (REPAIRED IAW SB 747-53A2448, REV 1 AND SRM 53-60-01, FIG 201, REPAIR 3 WITH A REVISED FASTENER PATTERN AND (2) FASTENERS OVERSIZED BEYOND THE SRM LIMITATIONS, SEE FIGURE 1. THSDR UIEA2010070900096Skin · corrodedCORROSION WAS FOUND ON THE RT INBD MID FLAP UPPER SKIN AT WBL 315 AND 388. LEVEL 1 CORROSION. (THE CORROSION WAS BLENDED OUT TO A MINIMUM THICKNESS OF 0.070 INCH, NDI INSPECTED, THE SURFACE FINISH WAS RESTORED AND A BONDED FILLER AND REPAIR DOUBLER WAS INSTALLSDR UIEA2010070800112Skin · corrodedDURING THE D-03 CHECK, CORROSION FOUND ON RT WING T/E, LOWER SKIN 112U4502-2 WHICH MATING WITH FIXED PANEL 112U4710-38 AT WBL 1144. LEVEL 1 CORROSION. (CORROSION WAS COMPLETELY REMOVED AND THE BLENDED SKIN AREA AND FASTENER HOLES ARE DET/HFEC INSPECTED TO CONSDR UIEA2010070700095Strut · gougedDURING THE LCF MODIFICATION IN TPE AND INSP IAW SB 747-54A2218 (AD 2005-19-09), A GOUGE WAS FOUND IN THE NR 4 STRUT LT SIDE & NBSP; LINK & NBSP; DO NOT SCHEDULE; THIS EO DOCUMENTS AN INTERIM REPAIR ACCOMPLISHED AT TPE DURING THE SEPTEMBER 2008 LCF MODIFICATIONSDR UIEA2010063000055Skin Panel · damagedDURING THE LCF MODIFICATION IN TPE, THE SKIN PANEL FROM BS 340 TO 520, S-6L TO -14L WAS REPLACED IAW EGAT EI B2008A53M-048 AND NRC U09082. DURING THE PANEL REPLACEMENT, SHORT EDGE MARGINS WERE FOUND IN THE STRAPS AND DOUBLERS IN THE SKIN PANEL. (THE SEM WAS RSDR WRLA20100620394Angle · crackedCRACK - CRACK WAS FOUND ON ANGLE OF LT SEAL RETAINER SUPPORT BEAM NR 2 FLAP TRACK MOVABLE FAIRING. FABRICATE AND INSTALL NEW STIFFENER PER DWG 314T4210.SDR WRLA20100616404Skin · dentedDENT - DENT DAMAGE ON EXISTING REPAIR DOUBLER OF LT BODY LANDING GEAR DOOR OUTER SKIN (P/N 65B10919-7) AT STA 1428. REMOVE DAMAGE DOUBLER AND PFM NDT MEASURE FREE OF CRACK. FABRICATE AND INSTALL REPAIR DOUBLER & FILLER.SDR WRLA20100616392Skin · crackedCRACK - CRACK DAMAGE WAS FOUND ON RT FUSELAGE SKIN (P/N 65B02781-4) AT STA 2701. CUT OUT THE DAMAGE SKIN AND PFM NDT MEASURE FREE OF CRACK. FABRICATE AND INSTALL REPAIR DOUBLER & FILLER.SDR WRLA20100615405Fitting · chafedCHAFING - FOUND PYLON-4 MID SPAR UNDER WING FITTING BUSHING OUTSIDE AROUND CHAFING (LT FITTING RT SIDE, RT FITTING RT SIDE). ACCOMPLISHED PYLON 4 MID SPAR UNDER WING FITTING REPAIRED REFERENCE JOB CARD ATTACHING SHEET 025857, 025858. CONDITION CHECK SATISFACSDR WRLA20100612399Flap Track · corrodedCORROSION - NR 4 FLAP TRACK FORWARD END CLEVIS BUSHING HOLE AND OUTSIDE SURFACE CORROSION. BLEND OUT THE CORROSION. SPOT FACE THE FWD END CLEVIS. OVERSIZE THE BUSHING HOLE. NDT MEASURE NO DAMAGE WAS FOUND. FLAP PEEN EACH CLEVIS LUG. FABRICATE AT INSTALL SDR WRLA20100607390Angle · crackedCRACK - CRACK WAS FOUND ON ANGLE (P/N 69B13824-5) OF RT WING T/E RIB INSTALLATION AT STA WBL 432.65. FABRICATE & INSTALL NEW ANGLE PER DWG 69B13824. NOTE: THIS SDR IS A DUPLICATE OF SDR WRLA20100604387.SDR WRLA20100607388Attach Angle · crackedCRACK - FOUND NR 3 ENG LEFT T/R TORQUE BOX ATTACH BRACKET CRACK AT 8 O'CLOCK POSITION. REMOVED THE CRACK BRACKET IAW 747-400 SRM 51-40-02 REV 76. PERFORMED E/I W2010P78B-1235 REV 00 FABRICATION - BRACKET (P/N: 315T3633-39) OF NR 3 ENGINE LEFT T/R TORQUE BOXSDR WRLA20100607393Stiffener · wornNR 1 ENG RT CORE COWL HAS ANGLE WEAR NEAR SUPPORT ROD END. REMOVED DAMAGE PARTS AND FABRICATE NEW PARTS IAW EI W2010P548-1283 REV 00. RE-INSTALLED NEW PARTS IAW SRM 51-40-02 REV 76. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR WRLA20100607364Door Frame · crackedCRACK - LEFT NR 5 ENTRY DOOR FWD CENTER FRAME CRACK. NRC U05069 ISSUED. TRIM OUT THE DAMAGE FRAME AND KEEP 0.5 INCH RADIUS PER NDT MANUAL PART 6 51-00-00, FIG 23 ENSURE THE TRIM OUT AREA FREE OF CRACK.SDR WRLA20100604389Attach Bracket · crackedCRACK - BRACKET, LANDING GEAR SUPPORT BEAM FRONT SPAR, WBL 130, RIGHT WING. REPLACED THE BRACKET, LANDING GEAR SUPPORT BEAM FRONT SPAR WBL 130 RIGHT WING IAW SRM 51-40-02 REV 76. JOB COMPLETED AND COND CHECK NORMAL.SDR WRLA20100604387Bracket · crackedCRACK - BRACKET, RIB-ASSY - INBOARD T/E COMPARTMENT WBL 432.65 RT WING. REMOVED THE ANGLE IAW SRM 51-40-02 REV 76. PERFORMED E/I W20/OP57B-1231 REV 00 INSTALLATION AT STA WBL 432.65. INSTALLED THE ANGLE IAW SRM 51-40-02 REV 76. CONDITION CHECK NORMAL AND SDR WRLA20100601403Bearing · wornWORN - FOUND PYLON -4 DIAGONAL BRACE FWD FITTING BEARING WORN. PER SRM 54-50-90 REPAIR 1 REV 76 REPAIRED PYLON -4 LOWER SPAR FITTING BEARING.SDR WRLA20100601402Bushing · corrodedCORROSION - FOUND PYLON -4 DIAGONAL BRACE AFT BUSHING CORROSION. PER OHM 54-00-01 REV 54, REPLACED DIAGONAL BRACE AFT BUSHING OF PYLON-4.SDR WRLA20100601401Bushing · damagedCHAFING - FOUND PYLON -4 FRONT SPAR UPPER LINK FITTING BUSHING DAMAGE (LT). PER SRM 57-20-90 REPAIR 1 REV 76, REPAIRED FRONT SPAR UPPER LINK LT SIDE BUSHING OF PYLON-4.SDR WRLA20100601400Bearing · wornWORN - FOUND PYLON -4 UPPER LINK AFT SIDE BEARING WORN. PER CMM 54-00-01 REV 54, REPLACED UPPER LINK AFT SIDE BEARING OF PYLON-4.SDR WRLA20100601363Skin Panel · crackedCRACK - NR 4 PYLON RIGHT SIDE ACCESS DOOR (482ER) SURROUND SKIN CRACK NRC U05004 ISSUED. REPAIRED CRACK AREA AT NR 4 PYLON STRUT NAC STA 227.27 NAC WL 155 IAW SRM 54-50-01 REPAIR 2 FIG 701 REV 76 AND REF JOB CARD ATTACHING SHEET 025021, 025824. COND CHECK NSDR WRLA20100601362Wedge · damagedPUNCH - LEFT OUTBOARD AILERON TRAILING EDGE WEDGE ON INBOARD SIDE WAS DAMAGE DURING CARGO UNLOADING IN AFGHANISTAN. NRC U07011 ISSUED. PER SRM 57-60-01 REPAIR 1 & SRM 51-70-07 FIG 6 TO REPAIR THE DAMAGE WEDGE. PER SRM 51-60-01 PFM OUTBOARD AILERON BALANCINGSDR WRLA20100305345Anti-Ice System · defectiveSMOKE IN COCKPIT FROM 3R WINDOW. DE-SELECTED WINDOW HEAT R SWITCH - SMOKE DISSIPATED. ISSUED MEL FOR 3R WINDOW HEAT PER MEL 30-41-03-01, DMI M30MR0510-165, CAT C DUE MARCH 15, 2010. MEL PROCEDURE C/W. MTC CNTL ADVISED DUE SMOKE DETECTED IN COCKPIT.SDR KCSA101004Strap · crackedFUSELAGE FRAME STABILIZATION STRAP IS CRACKED AT STA 2180 TO 2200, RBL 20.SDR KCSA101002Strap · crackedFUSELAGE FRAME STABILIZATION STRAP IS CRACKED AT STA 2180 TO 2200, LBL 20.SDR KCSA101003Strap · crackedFUSELAGE FRAME STABILIZATION STRAP IS CRACKED AT STA 2180 TO 2200, RBL 10.SDR KCSA101001Strap · crackedFUSELAGE FRAME STABILIZATION STRAP IS CRACKED AT STA 2180 TO 2200, LBL 10.SDR WRLA20090924252Support · corrodedEXFOLIATION - LOWER FUSELAGE FS 987.5, LBL 9 TO RBL 9 THE T-SUPPORT OF FAIRING EXFOLIATED. REPLACED THE EXFOLIATED FAIRING SUPPORT WITH NEW PARTS PER WOA 747-400 SRM 51-40-02 REV 73.SDR WRLA20090922244Beam · crackedCRACK - THE OUTBOARD BEAM OF RIGHT WING FIXED T/E STRUCTURE CRACK ABOUT 2 INCHES, WBL 249. REMOVED THE DAMAGE SUPPORT BEAM AT RT WING WBL 249 IAW 747-400 SRM 51-40-02 REV 73. FABRICATED THE NEW PART IAW EI NR W2009P57B-119 REV 00. INSTALLED NEW PART AT RT WSDR WRLA20090922243Beam · crackedCRACK - AT LEFT WING FIXED T/E STRUCTURE WBL 249 THE OUTBOARD BEAM CRACKED AS RADIATION FROM THE FASTENER HOLE AREA. REMOVED THE DAMAGE SUPPORT BEAM AT LT WING WBL 249 IAW 747-400 SRM 51-40-02 REV 73. FABRICATED THE NEW PART IAW EI W2009P57B-118 REV 00. INS
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