Boeing 747-132
Service difficulty reports · 1,451
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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 = '747132' 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 = '747132' 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 P5CA9801193Panel · delaminatedLEFT WING UPPER SURFACE PANEL DELAMINATED INBD 2ND FROM ROOT AREA. REPAIRED PER SRM 51-40-15.SDR P5CA9801192Cowl · looseNR 2 ENGINE CORE COWL 3RD LATCH AREA HAS LOOSE FASTENERS. REPAIRED PER SRM 51-30-02.SDR P5CA9801191Cowl · looseNR 1 ENGINE OUTBOARD CORE COWL TOP AFT CORNER LOOSE FASTENERS. REPAIRED PER SRM 51-30-02.SDR P5CA9801190Hinge · corrosionRIGHT CENTER GEAR DOOR HINGE LIGHT SURFACE CORROSION. REPAIRED BY SRM 51-10-02 AND 51-10-06.SDR P5CA9801189Skin · delaminatedNR 4 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PANEL PER MM 27-61-02.SDR P5CA9801188Cowl · crackedNR 1 ENGINE OUTBD CORE COWL MOST AFT LATCH HOUSING CRACKED AND DAMAGED. REPAIRED PER SRM 51-30-02.SDR P5CA9801187Cowl · chafedNR 2 ENGINE INBD CORE COWL PREVIOUS REPAIR CHAFFED THROUGH. REPAIRED PER SRM 54-30-03.SDR P5CA9801186Panel · delaminatedRIGHT WING UPPER SURFACE FIXED TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-15.SDR P5CA9801185Skin · delaminatedLEFT WING GEAR DOOR CORNER DELAMINATED. REPAIRED PER SRM 51-40-09.SDR P5CA9801184Skin · delaminatedRIGHT WING GEAR DOOR 5 INCH DELAMINATED. REPAIRED PER SRM 51-40-09.SDR P5CA9801183Skin · delaminatedLEFT OUTBOARD TRAILING EDGE AFT FLAP LOWER SURFACE 4 FOOT DELAMINATION. REPAIRED PER SRM 51-40-07.SDR P5CA9801182Panel · delaminationLEFT WING UPPER SURFACE FWD INBOARD TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-09.SDR P5CA9801173Press Xmtr · inoperativeNR 4 HYD PRESS PEGGED AT 4,000 PSI, FOLLOWED BY A LOW QTY ANNUNCIATOR AND DECREASING HYD QTY. HYD TEMP REMAINED NORMAL PRIOR TO AND FOLLOWING ABNORMAL PROCEDURES IN AOM. REPLACED NR 4 HYD PRESS TRANSMITTER IAW MM 29-31-01. OPS AND LEAK CHECK NORMAL. SYSTEMSDR P5CA9801172Battery Pack · dischargedUPPER DECK EMERGENCY LIGHTS WILL NOT GO OUT WITH POWER OFF POSTION. REMOVED AND REPLACED UPPER DECK EMERGENCY LIGHTING BATTERY PACK PER MM 33-51-00.SDR CKSA98384Web · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION FUSELAGE LWR AREA, BS 1200, RBL 58, WEB CORRODED AT O/B FACE LWR AREA. REMOVED CORROSION IAW B747 SRM 51-10-01. FABRICATED REPAIR IAW B747 SRM 51-40-02. INSTALLED REPAIR IAW BOEING 747 SRM 51-40-02. COSDR CKSA98383Floorbeam · crackedDURING ROUTINE CPCP INSPECTION, FOUND FS 440 RBL 50 UPPER DECK FLOORBEAM WEB CRACKED. REMOVED DAMAGED WEB IAW B747 SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW SRM 53-10-07 FIG 11. INSTALLED REPAIR IAW SRM 53-10-07 FIG 11. CORROSION TASK CARD NUMBER C53-21SDR CKSA98382Intercostal · crackedDURING ROUTINE CPCP INSPECTION, FOUND FS 440 TO FS 460 RBL 50 INTERCOSTAL WEB CRACKED. REMOVED CRACKED WEB IAW B747 SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW B747 SRM 53-10-07 FIG 11. INSTALLED REPAIR IAW B747 SRM 53-10-07 FIG 11. CORROSION TASK CARD NUSDR CKSA98381Angle · crackedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS440 RBL50 UPPER DECK FLOORBEAM ATTACH ANGLE CRACKED ON AFT INBD SIDE. REMOVED AND REPLACED ATTACH ANGLE IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-03. NON-ROUTINE TASK CASDR CKSA98380Frame · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND BS 2020 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED AND A FLOOR SUPPORT. PERFORMED HFEC PER NDT MANUAL 51-00-00 PART 6. NO CRACKS NOTED. REPAIRED UPPER CHORD IAW AIA EDR NBR B4-05880. INSTALLED REPAIR IAW AIA EDR B4-0SDR CKSA98379Frame · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND BS 2000 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED UNDER FLOOR SUPPORT. REPAIRED UPPER CHORD IAW AIA EDR NBR B4-05879. INSTALLED REPAIR IAW AIA EDR NBR B4-05879. NON-ROUTINE TASK CARD NUMBER 26149.SDR CKSA98378Frame · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND BS 1980 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED UNDER FLOOR SUPPORT. REPAIRED UPPER CHORD IAW AIA EDR NBR B4-05878. INSTALLED REPAIR IAW AIA EDR B4-05878. NON-ROUTINE TASK CARD NUMBER 26148.SDR CKSA98377Longeron · corrodedDURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON UPPER SURFACE OF LEFT OVERWING LONGERON APPROX STA 1320. REMOVED CORROSION FROM ACCESSABLE AREA IAW SRM 51-10-01. CORROSION RUNNING UNDER LONGERON SPLICE RAISED EDR AS PER AIA ENGINEERING. REPAIRED LT OVERWSDR CKSA98376Keel Beam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION UPPER WEB OF KEEL BEAM BOX CORRODED AND CRACKED APPROX STA 1265 AT PREVIOUS REPAIR. REMOVED FASTENERS IAW B747 SRM 51-30-2. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SSDR CKSA98375Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND FS2240 RBL75 FLOORBEAM T CHORD HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 51-40-4 FIG 12 AND AIA EDR B4-05887. INSTASDR CKSA98374Spar · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LOWER FWD SPAR LWS1356 EXFOLIATED. REMOVED NR 2 PANEL RT SIDE. HFEC INSPECTED FASTENERS HOLES IN THE HORIZ FLANGE OF THE SPAR CHORD PER NDT MANUAL 51-00-00 PART 6. NO DEFECTS NOTED. PENETRANT INSPECTED CHORD PER STASDR CKSA98373Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS440 RBL50 UPPER DECK FLOORBEAM HAS CORROSION ON FWD SIDE. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. MANF REPAIR PARTS IAW EDR B4-05871. INSTALLED REPSDR CKSA98372Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, STA1940-1960 LBL11.33 LONGITUDINAL FLOORBEAM UPPER CHORD CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 53-10-05 SDR CKSA98371Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS1100 LBL70 SEAT TRACK UNDERSIDE HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR IAW B747 SRM 53-10-5 FIG 34. INSTALLED SEAT TRACSDR CKSA98370Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, STA 340 FWD SIDE LBL33 SEAT TRACK FLANGE HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 53-10-05 FIG 1A. INSTALLED SEAT SDR CKSA98369Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION AROUND 2 CLIP NUTS ON RBL 49 SEAT TRACK FWD OF BS 240. REMOVED CORROSION IAW 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED SEAT TRACK SECTION IAW B747 SRM 51-30-02. RESDR CKSA98368Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, CORROSION AROUND CLIP NUT ON UPPER CHORD OF BS680 FLOORBEAM LBL3. CUTOUT DAMAGE AREA IAW SRM 51-40-04 FIG 1. MADE REPAIR ANGLES AND DRILLED IAW SRM 51-40-04 FIG 1. INSTALLED REPAIR IAW B747 SRM 51-40-4SDR CKSA98367Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION STA760 FWD LBL44 FLOORBEAM HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUTOUT CORROSION AND FABRICATED REPAIR IAW B747 SRM 51-40-4 FIG 1. INSTALLED REPAIR IAW B747 SRM 51-40SDR CKSA98366Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STA760 FWD LBL72 FLOORBEAM HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUTOUT CORRODED SECTION OF UPPER CHORD AND FABRICATED REPAIR IAW SRM 51-40-4 FIG 1. ALSO AIA EDR NR BSDR CKSA98365Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STA 760 AFT, LBL 79 FLOORBEAM ANGLE HAS CORROSION. REMOVED FITTING IAW B747 SRM 51-30-2. REPLACED FITTING IAW 51-30-2 AND 51-10-1. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUTINE TASK CARD NUMBER 2SDR CKSA98364Floor · corrodedDURING ROUTINE CPCP INSPECTION, FOUND FLOOR HAS CORROSION BETWEEN STA 860 AND STA 880 RBL 98 BOTTOM SIDE. REMOVED FLOOR PANEL CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-20-00 FIG 2. MADE NEW FLOOR PANEL IAW B747 SRM 53-20-01. INSTALLED FLOOR PANEL SDR CKSA98363Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND 1 AREA OF CORROSION ON BOTTOM OF RBL11.33 SEAT TRACK FWD OF BS 520. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED SEAT TRACK IAW B747 SRM 51-30-02. INSTALLED NEW SEATSDR CKSA98362Floorbeam · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION 2 AREA OF CORROSION ON BS480 FLOOR BEAM FWD, UPPER, SIDE AT RBL-76. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 51-SDR CKSA98361Angle · crackedDURING ROUTINE CPCP INSPECTION, FOUND FS1000 LBL 30 FRONT SPAR FLOOR SUPPORT ATTACH ANGLE CRACKED. REMOVED FLOOR SUPPORT. REWORKED FITTINGS IAW EDR B4-05869 DTD 6-2-98. INSTALLED FITTINGS IAW B747 SRM 51-30-02 AND EDR B4-05885 DTD 6-9-98. CORROSION TASK CASDR CKSA98360Angle · crackedDURING ROUTINE CPCP INSPECTION, FOUND FS1080 LBL90 OUTBD SIDE WEB ATTACH ANGLE CRACKED. FAB NEW ATTACH ANGLE 7075-T6. INSTALLED ATTACH ANGLE IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-210-05. NON-ROUTINE TASK CARD NUMBER 25171.SDR CKSA98359Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION BS980, RBL50, PANEL SUPPORT FRAME CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REPAIR FRAME FLANGE IAW B747 SRM 53-50-04. INSTALLED REPAIR IAW B7SDR CKSA98358Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND BS920, FROM BOTTOM CENTERLINE TO BOTH RT AND LEFT BL50, PANEL SUPPORT FRAME CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REPAIR FRAME IAW B747 SRM 53-50-04 AND AIA SDR CKSA98357Angle · corrodedDURING ROUTINE CPCP INSPECTION, FOUND AT BS1060, FROM BOTTOM CENTERLINE TO LBL50, PANEL SUPPORT FRAME WITH CORROSION AROUND ANCHOR NUTS AND FASTENERS. REMOVED DAMAGED T-CHORD, FAB NEW PER SRM 51-10-01. FAB REPAIR ANGLES PER SRM 51-40-02. INSTALLED REPAIR ANSDR CKSA98356Skin · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: FS1200 RBL95 CNTR WING SKIN HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 57-10-01. INSTALLED REPAIR IAW AIA EA B4-57-051. C/W OPEN HOLE HFEC AND SURFSDR CKSA98355Skin · crackedDURING ROUTINE CPCP INSPECTION FOUND: C-2 DOOR OUTER SKIN IS DENTED AND HAS 2 EA 1 CRACKS AT BOTTOM EDGE BETWEEN BS 1840 AND BS 1860. DAMAGED FOUND TO BE OUT OF LIMITS IAW B747 SRM 52-00-2. REPAIR DOOR SKIN IAW B747 SRM 52-00-03 FIG 3. INSTALLED REPAIR IAW SDR CKSA98354Skin · gougedDURING ROUTINE C CHECK INSPECTION FOUND: SEVERAL GOUGES IN FUSELAGE SKIN AT AFT LOWER CORNER OF C-2 DOOR CUT-OUT BS1920. REMOVED FASTENERS AND BLENDED AREA IAW B747 SRM 51-30-2. C/W OPEN HOLE HFEC OF 3 FASTENER HOLE AND SURFACE PERIFERY OF BLEND-OUT AREA IASDR EIAA980218Engine · failedHNL - LOG PAGE: F40104 - DURING CLIMB-OUT APPROXIMATELY 20 MINUTES INTO FLIGHT, NR 4 ENGINE OIL QUANTITY SLOWLY DECREASED TO ZERO, ENGINE SHUT DOWN. PER EIA PROCEDURES, ENGINE WINDMILLED AT APPROXIMATELY 9 PSI OIL PRESSURE FOR 13 MINUTES, AND REDUCED TO 3 PSSDR EIAA980217Line · looseHNL - LOG PAGE: F40104 - DURING CLIMB-OUT, NR 4 ENGINE OIL QUANTITY SLOWLY DECREASED TO ZERO, ENGINE SHUT DOWN PER EIA PROCEDURES, ENGINE WINDMILLED AT APPROXIMATELY 20 PSI OIL PRESSURE FOR 35 MINUTES. SERVICED ENGINE OIL AND MOTORED, FOUND OIL DRAINING FROMSDR EIAA980209Switch · out of adjustMNL - LOG PAGE: F66950 - AT FL 390, MAIN DECK SIDE, CARGO DOOR WARNING LIGHT ILLUMINATED. DIVERTED TO MNL. NOTE: LIGHT FLASHED MOMENTARILY DURING TURBULENCE. ADJUSTED MAIN CARGO DECK CARGO DOOR WARNING SWITCH PER MM 52-32-00. CHECKED WIRING FROM PLUG D47SDR P5CA9800776Cowl · dentedNUMBER 2 ENGINE NOSE COWL SKIN DENTED AT 0630 POSITION. REPAIRED NOSE COWL PANEL AT 0630 POSITION PER SRM 51-40-07.SDR P5CA9800774Transmitter · inoperativeNR 2 ENGINE WOULD NOT MAKE TAKEOFF THRUST. TEMP 912 DEGREES 1:08 EPR. ABORTED TAKEOFF. REMOVED AND REPLACED EPR TRANSMITTER REF MM 77-11-00. REMOVED AND REPLACED T7 LINE AS PRECAUTION REF MM 77-12-00. REQ OPS CHECK. OPS CHECK SATISFACTORY PER MM 77-00-00.
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