JASC 5753
Service difficulty reports · 31,521
Reports filed under 5753 · Trailing Edge Flaps, newest first.
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 jasc_code = '5753' 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 jasc_code = '5753' 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 USAA050052Skin · chafedPIT - FOUND FLAP SKIN LEADING EDGE WITH CHAFE MARK .020 BY 4.25 INCH LONG BY .5 INCH WIDE, RT OUTBOARD MID FLAP ADJACENT TO OUTBOARD FLAP TRACK. (M)SDR SWAA050006Structure · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING T/E OUTBOARD AFT FLAP, DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR DHL2004809513Skin · damagedRT WING OUTBOARD FLAP FWD UPPER PLATING HAS INTERIM REPAIR, XF 211.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 12-28-04, DWG X32-R03 REV IR DATE 12-21-04. REMOVED PLATING WITH INTERIM REPAIR AND EXISTING INTERNAL SPLICE IAW DWG X32-R03, SRSDR SWAA043732Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD T/E FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FORE FLAP PER MM.SDR DHL2004809506Structure · wornRIGHT WING OUTBOARD FLAP UPPER AFT PLATING WORN, XF 227.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED WORN PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING (AL2024T3 0.063) IAW SRM 57-7-1 FIG 4 TR 57-94. CLEANED, TREATED AND PSDR SWAA043723Skin · puncturedDURING SCHEDULED MV1 CHECK, FOUND LT WING T/E INBD AFT FLAP SKIN PUNCTURED NEAR INBOARD END. REPAIRED AFT FLAP PER SWA EA.SDR AWXA200401432Wedge · separatedON DESCENT A PASSENGER REPORTED THAT A 3FT X 6FT SECTION OF RT WING INBOARD TRAILING EDGE FLAP HAD BROKEN OFF AND SEPARATED FROM THE AIRCRAFT, A ROLL WAS FELT WITH FLAPS AT 25, SELECTED FLAPS 20 AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE EVALUATED DAMAGE ASDR AWXA200500150Skin · delaminatedMCN - MAJOR REPAIR - DURING C-17 CHECK, FOUND THE LT INBOARD FLAP DELAMINATED AT THE AFT OUTBOARD CORNER. MAINTENANCE REMOVED AND REPLACED THE LT INBOARD FLAP IAW T/C R3M27007.SDR AWXA200500036Skin · delaminatedMCN - MAJOR REPAIR - DURING C-17 CHECK THE UPPER SURFACE OF LT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 10 INCHES FROM INBOARD END, WBL 208.69 - 210.69 LT. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON UPPER SURFACE OF LT OUTBOARD FORE FLAP; FABRICATED A HONEYCSDR AWXA200500026Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-17 CHECK THE LT INBOARD MID FLAP WEDGE WAS FOUND DELAMINATED ON LOWER SURFACE 36 INCHES FROM THE INBOARD END BEWTEEN WBL 104 AND WBL 115. MAINTENANCE CUT OUT DAMAGE IN LT INBOARD MID FLAP WEDGE ON LOWER SURFACE 36 INCHES FROM INBSDR A6WA200440226Skin · dentedFLAP LOWER SKIN DENTED AT WS NEAR T/E. DENT MEASURES 2 INCHES ROUND BY .085 INCH DEEP. INSTALLED EXTERNAL REPAIR TO LT IB FLAP LOWER SKIN AT WS 106, 5 INCHES FROM T/E IAW REO.SDR SWAA043662Structure · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT OUTBOARD AFT FLAP PER MM.SDR ASAA0480607Vane · wornOKC - HV-CHECK, RIGHT WING FLAP OUTBOARD VANE INBOARD T/E IS WORN. REMOVED WORN AREA. INSTALLED FILLER AND REPAIR DOUBLER. (M)SDR ASAA0480605Joint · damagedOKC - DURING HV-CHECK, LT WING FLAP FLEX JOINT UPPER BAR 6TH HOLE FROM T/E DAMAGED. REPAIRED WITH WASHER PER EA 5750-02019. (M)SDR ASAA0480606Vane · chafedOKC - HV-CHECK, RIGHT WING OUTBOARD FLAP INBOARD VANE PREVIOUS L/E REPAIR IS CHAFED. REPLACED DAMAGED REPAIR DOUBLER. (M)SDR ASAA0480608Bracket · corrodedOKC - HV-CHECK, LEFT WING INBOARD FLAP TRACK MOUNTING BRACKET BOLT HOLES ARE PITTED. REAMED HOLES AND INSERTED BUSHINGS PER EA 5750-01160. (M)SDR SWAA043651Skin · separatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP, SKIN SEPARATED. REPAIRED FLAP PER SRM.SDR ASA0440340Skin · dentedOKC - FOUND LEFT OUTBOARD FLAP HAS A DENT ON THE LOWER SURFACE SKIN, A=.5, Y=.55, AY=9. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (M)SDR SWAA043641Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA043636Structure · warpedDURING SCHEDULED D-CHECK, FOUND RT WING OUTBOARD T/E FORE FLAP, WARPED. REMOVED AND REPLACED RT WING OUTBOARD T/E FORE FLAP PER MM.SDR ASA0440320Skin · delaminatedOKC - FOUND RIGHT OUTBOARD FLAP INBOARD CORNER IS DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM. (M)SDR A6WA200440209Vane · wornLT OB FLAP - VANE FITTING AT WS 296.073 IS WORN BEYOND LIMITS. COMPLY WITH MFG REO.SDR SWIA200414253Flap Track · malfunctionedON TAKE OFF AFTER SELECTING FLAPS UP, RECEIVED "FLAP" AND "ADVANCED SWS" LIGHTS ON THE MAP. REMOVED AND REPLACED ALL MOVEABLE AND STATIONARY FLAP TRACKS, GUIDES AND ROLLER WITH SERVICEABLE UNITS IAW MM 57-53-04 AND 57-53-06. OPERATIONAL CHECK GOOD.SDR SWAA043595Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD T/E AFT FLAP PER MM.SDR IXXA0500112SVane · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING EXTENDED LEADING EDGE OUTBOARD VANE FORWARD PLATING A STA XOLDI 6.224. MAJOR REPAIR ACCOMPLISHED REMOVAL FASTENERS IAW DC8 SRM 51-1-21 PGG1, DC8 SRM 51-3-0 PG 1. REMOVED DAMAGED AREA IAW DSDR 04FDEA03399Hinge · corrodedLT WING INBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-07 PAGES 403- 404.SDR AWXA200401422Skin · corrodedDURING C-18 CHECK A DISBOND AREA WAS FOUND ON LOWER SURFACE OF RT OUTBOARD FORE FLAP AT WBL 220.00. MAINTENANCE REMOVED DISBONDED SKIN ON LOWER SURFACE OF RT OUTBOARD FORE FLAP FROM WBL 216 TO WBL 224; FABRICATED A NEW SECTION OF SKIN AND A DOUBLER; BONDED RESDR 04FDEA03398Hinge · corrodedRT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD HOLE SPOT FACE FOUND CORRODED. SPOT FACE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM57-52-03. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78057.SDR 04FDEA03397Hinge · corrodedRT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78057.SDR 04FDEA03396Hinge · corrodedRT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. BORE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-78057.SDR IXXA0500084SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN HAS INTERIM REPAIR BETWEEN STATION XW63.00-XW91.000. MAJOR REPAIR WAS ACCOMPLISHED BY REMOVED THE UPPER PLATING WITH INTERIM REPAIR. FABRICATED NEW PLATING PANEL, CLEANED, TREATED AND PRIMED SDR AWXA200401453Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP OUTBOARD GIMBLE, OUTBOARD BEARING SUPPORT AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP OUTBOARD GIMBLE, OUTBOARD BEARING SUPPORT IAW B737-300 SSDR AWXA200401452Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBLE SUPPORT AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBLE SUPPORT IAW B737-300 SOPM 20-50-01 FIG 1.SDR AWXA200401440Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON RT INBOARD MID FLAP INBOARD GIMBLE OUTER BEARING SUPPORT AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED RT INBOARD MID FLAP INBOARD GIMBLE OUTER BEARING SUPPORT ASSEMBLY IAW B737-300 SOSDR AWXA200401439Support · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTER GIMBLE INDEXING PLATE SUPPORT AT WBL 173.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTER GIMBLE INDEXING PLATE SUPPORT IAW B737-300 SOPM 20-50-0SDR AWXA200401438Retainer · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP INBOARD GIMBLE ASSEMBLY RETAINER AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP INBOARD GIMBLE ASSEMBLY RETAINER IAW B737-300 OHM 57-53-22 FIG 11SDR AWXA200401436Plate · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LT INBOARD MID FLAP OUTER INDEXING PLATE AT WBL 73.00. MAINTENANCE REMOVED AND REPLACED LT INBOARD MID FLAP OUTER INDEXING PLATE IAW B737-300 OHM 57-53-22 FIG 1101.SDR ASAA0480590Flap Track · corrodedCHECK-RT IB FLAP TRACK MOUNTING BRACKETS BOLT HOLES PITTED. REAMED PITTED HOLES AND INSTALLED BUSHINGS IAW EA. (K)SDR AWXA200500015Skin · debondedMCN - MAJOR REPAIR - DURING C-18 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF RT OUTBOARD FORE FLAP AFT OF A REPAIR AT INBOARD END BETWEEN WBL 212.5 LT AND WBL 217.5 LT. MAINTENANCE REMOVED DAMAGE ON UPPER SURFACE OF RT OUTBOARD FORE FLAP; FABRICATED A SDR SWAA043566Structure · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING INBOARD T/E AFT FLAP PER MM.SDR SWAA043565Structure · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING OUTBOARD T/E AFT FLAP PER MM.SDR SWAA043569Spindle · wornDURING SCHEDULED SERVICE CHECK, RT WING OUTBOARD T/E AFT MID FLAP SPINDLE HAS EXCESSIVE PLAY. REMOVED RT SPINDLE PER MM.SDR 04FDEA03380Hinge · corrodedLT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 PAGES 442-443.SDR 04FDEA03381Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER FEDEX EA1-5750-78058,SDR UPS04M43587Skin · delaminatedLEFT OUTBOARD FLAP DELAMINATED.SDR SWAA043545Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM.SDR 04FDEA03373Fairing · damagedREPAIR, NR 4 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49991 REV NO. POS P2 ENT BY: EMMD24 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 20OCT04 15:38:48:9 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:44:51:3 S=M. COMPLIESDR 04FDEA03372Fairing · damagedREPAIR, NR 2 FLAP TRACK MOVABLE FAIRING. COMPLY WITH EA 6-5720-49992 REV NO POS P2 ENT BY: EMMD24 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 20OCT04 15:38:56:3 BY:195875 S=M PLND: DATE:06NOV04 AT: LIS-VNMX ENT BY: 478289 ON: 31OCT04 20:45:04:9 S=M. COMPLIEDSDR 04FDEA03371Structure · damagedCOMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 24NOV04 16:00 MC1 R, DETACHED FROM WORK ORDER 00027509. INSPECTION COMPLIED WITH AT TAP; AWAITING FAA APPROVAL TO UPDATE THE OPS SPEC. ENT BY: 067708 LT WING, REPAIRS (2 EA) LT INBD FLAPSDR 04FDEA03362Skin · delaminatedLEFT INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX EA 1575079794.
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