JASC 5753
Service difficulty reports · 31,515
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 AWXA200600068Wedge · debondedMCN - DURING C15 CHECK DISCOVERED THE RT INBOARD MID-FLAP TRAILING EDGE WEDGE HAD DISBOND ON THE UPPER SURFACE, 58" FROM THE INBOARD END. MAINTENANCE REMOVED THE DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED FILLER AND DOUBLER IAW BOEING 737SDR QXEA200600058Flap Track · corrodedPDX - LEFT NR 4 FLAP TRACK WEB VERTICAL ROLLER TRACK IS RUSTY AND PITTED. REPAIRED IAW RD 8-57-988.SDR IXXA05SMN293SSkin · damagedDURING ROUTINE C-CHECK INSPECTION, RT OB FLAP HAS A NON STANDARD REPAIR ON UPPER SKIN, STA XF 210.000PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4, TR NR 57-94, EO SEMAN NR 20051460 DATED 12-16-05. REMOVED DAMAGED PLATING IAW SRM 57-1-0, SRM 51-1-21. FABRICATED SDR IXXA05SMN296SVane · damagedC-CHECK INSPECTION, LT WING INBD FLAP VANE HOLES ELONGATED, XILD 42. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED DAMAGED SECTION. PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER (AL7075T60.070) & FILLER (AL7075T60.063) & INTERNAL DOUBLER (AL7075SDR IXXA05SMN294SSkin · wornDURING ROUTINE C-CHECK INSPECTION, RT OB FLAP UPPER SKIN WORN, STA XF 224.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 2Q. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG. 2Q. FABRICATED EXTERNAL REPAIR DOUBLER (ALCLAD 2024 TSDR IXXA05SMN295SVane · damagedDURING INSPECT, LT WING OUTBD VANE FWD HOLES ELONGATED, XOLDO 66.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05586 DATE 12-28-05, SEMAN DWG NR ED 4121 DATE 12-23-05 AND EO SEMAN NR 20051452 DATE 12-28-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVEDSDR IXXA05SMN285SRepair · improperDURING INSP, RT INBD FLAP FWD UPPER SURFACE HAS NO STANDARD REPAIR (STA XW 37.000-48.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05580 DATE 12-21-05, SEMAN DWG NR ED 4129 DATE 12-20-05, EO SEMAN 20051444 DATE 12-21-05. REMOVED REPAIR IAW DC-8 SRM 51-SDR SWAA054169Skin · delaminatedDURING SCHEDULED RON CHECK, FOUND LT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR SWAA054124Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR SWAA054122Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA054121Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ABXA060013Panel · corrodedRIGHT FLAP SEGMENT FROM OUTBOARD EDGE LOWER SURFACE ATTACH POINTS WERE SEPARATING AND CORRODED BETWEEN SKINS. REPLACED SKIN AND DOUBLER IAW DC9 REA C057-52966.SDR 05FDEA04408Flap Track · corrodedN0108, CORROSION ON UPPER SURFACE OF NR 6 FLAP TRACK AROUND BOTH AFT MOUNT BOLT HOLES AND CNT OB MOUNT BOLT HOLE. COMING REPLACED NR 6 FLAP TRACK IAW WC27X5708-03SDR CA051222008Bolt · migratedDURING GROUND INSPECTION IT WAS DISCOVERED THAT AFT ATTACHMENT BOLT OF THE NR 3 FLAP FAIRING HAD MIGRATED INBOARD AND PUNCTURED A HOLE THROUGH THE COMPOSITE FAIRING. THE AIRCRAFT WAS REMOVED FROM SERVICE FOR REPAIRS. UPON FURTHER INVESTIGATION, THREE(3) OF TSDR SWAA054084Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR UPS05645891Flap · delaminatedINSPECTION TYPE: N/A LT WING OB T/E FLAP DELAMINATED. A/C FERRIED TO HEAVY MX FACILITY FOR REPAIR. RMVD LW OB FLAP IAW 27-51-20-4. RMVD LW OB FLAP OB TE DEFLECTION CNTRL CARRIAGE FR DMGD FLAP & INSTLLD RPLCMNT FLAP IAW MM 27-51-24-4. RMVD LW OB FLAP IB/OBSDR 05FDEA04398Flap Track · corrodedNR 2 FLAP TRACK HAS CORROSION AT BOLT HOLES. REPLACED NR 2 FLAP TRACK ON CUSTOMER CARD 27X5706-03.SDR USAA051599Skin · gougedFOUND 2.0"L BY 0.80"W BY .055"D AND 1.2"L BY 0.30"W BY .013"D. FAB'D OVERLAY REPAIR AND BONDED TO AREA PER SRM 51-70-17 AND EA 97150, DEFECT SIZE: 2.0"L BY .080"W BY .055"D AND 1.2"L BY .20"W BY .013"D.SDR AWXA200600139Skin · chafedMCN - MAJOR REPAIR - DURING C19 CHECK DISCOVERED LOWER SKIN CHAFED AT O/B END OF THE RT O/B FORE FLAP, RT WING. MAINTENANCE REPAIRED LOWER SKIN AREA BY REMOVING CHAFED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPLACEMENT DOUBSDR ABXA060007Skin · corrodedRIGHT FLAP SECOND FROM OUTBOARD TRAILING EDGE SEGMENT UPPER SURFACE HAD 3 AREAS THAT WERE BULGED. REMOVED SEGMENT, REMOVED AND REPLACED SKIN IAW DC9 SRM 51-30-2.SDR SWAA054022Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR UPS06M46293Angle · crackedINSPECTION TYPE:C AFTER I/B FLAP O/B SEGMENT REMOVAL, FOUND FWD O/B SEGMENT MOST O/B AFT END 01/EA ANGLE CRACKED. THE ABOVE MENTIONED CRACKED AREA ANGLE REMOVED PER SRM 51-35-01.V.2R.38. NEW T-FAB & MAT USED S2931361X7075T6511 PER EN1063-06. HFEC C/OUT FOUNSDR AWXA200501611Wedge · debondedMCN - MAJOR REPAIR - DURING C15 CHECK DISCOVERED DISBOND AREA UPPER SURFACE LT INBOARD MIDFLAP TRAILING WEDGE ASSEMBLY, FROM WBL 87.75 TO WBL 93.75. MAINTENANCE REMOVED DISBONDED AREA ON UPPER SURFACE OF THE LT INBOARD MID FLAP TRAILING EDGE WEDGE IAW BOEING SDR 05FDEA04367Skin · dentedRIGHT WING OUTBOARD FLAP LOWER SKIN, DENT AT XFS 651, 6 INCHES FROM AFT EDGE IS OUT OF LIMITS. REPAIRED IAW DC10 SRM 57-10-00 FIG 85 VOL I MECH. 2668 QC316 SEE FEDEX NON ROUTINE NR N00598 OF WORK ORDER 00031297.SDR 05FDEA04359Skin · dentedRIGHT WING FLAP LOWER SKIN DENT AT XFS 674, 22" FROM TRAILING EDGE IS OUT OF LIMITS. REPAIRED SKIN IAW DC-10 SRM 57-10-00 FIG 85 VOL I. SEE FEDEX NONROUTINE NR N00599 OF WORK ORDER 00031297.SDR 05FDEA04358Skin · dentedRIGHT WING FLAP LOWER SKIN, DENT AT XFS 535, 12" FROM TRAILING EDGE IS OUT OF LIMITS. REPAIRED SKIN IAW DC-10 SRM 57-10-00 FIG 85 VOL I. SEE FEDEX NONROUTINE NR N00597 OF WORK ORDER NR 00031297.SDR 05FDEA04357Skin · dentedLEFT WING INBOARD FLAP LOWER SKIN DENT FILLED WITH SEALANT AT XW234-238, 31" FWD OF TRAILING EDGE. FOUND DENT TO BE OUT OF LIMITS, REPAIRED SKIN IAW DC10 SRM 57-00-00 VOL I. SEE FEDEX NONROUTINE NR N00295 OF WORK ORDER 00031297.SDR QXEA200600272Fitting · damagedYYC - C2 RIGHT WING OUTBOARD FLAP ROLLER GUIDE FITTING HAS DAMAGE AT FLS168.98. REPAIRED IAW CRJ700 SRM 57-51-02-201-001-A01 AND SRM 51-25-16-001-001-A01.SDR QXEA200600264Skin · damagedYYC - RIGHT HAND INBOARD FLAP BOTTOM SKIN HAS GRAVEL DAMAGE. REPAIRED IAW CRJ 700 SRM 57-01-101-001-A01.SDR IXXA05SMN273SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, LT OB FLAP SKIN CRACKED .5, STA XF 212.000 PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 2Q, EO NR 20051445 DATED 12-15-051. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG. 2Q. FABRICATED EXTERNALSDR AWXA200600092Skin · debondedMCN - DURING C16 CHECK DISCOVERED LT OUTBOARD AFT FLAP DISBONDED 3" FROM THE INBOARD EDGE FROM WS 230.68L TO WS 232.68L. MAINTENANCE REMOVED DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-10-2RSDR AWXA200600069Wedge · debondedMCN - DURING C15 CHECK DISCOVERED THE RT INBOARD MID-FLAP TRAILING EDGE WEDGE HAD DISBOND ON THE UPPER SURFACE, 48.5" FROM THE INBOARD END. MAINTENANCE REMOVED THE DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED FILLER AND DOUBLER IAW BOEING 7SDR IXXA05SMN272SSkin · damagedDURING INSPECT, LT OB FLAP UPPER SURFACE HAS NO STANDARD REPAIR, STA XF 347.000. PERFORMED MAJOR REPAIR, DWG NR ED 4118 DATE 12-20-05, EO 20051446 DATE 12-21-05. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21. REMOVED DAMAGED SEGMENT IAW DWG ED-4118. PERFORMESDR SWAA053982Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR AU510002115Fitting · shearedLT INBOARD TRAILING EDGE FLAP OUTBOARD HINGE FITTING OUTBOARD LUG SHEARED. FOUND DURING INSPECTION IAW AD/B767/188 (EI 767-57-073).SDR AU510001787Rib · corroded(AUS) LT FLAP IB HINGE BRACKET ATTACHMENT RIB SEVERELY CORRODED. FOUND DURING INSPECTION IAW AD/23/43.(AD/SB DESC: AD/ 23/43 ) (CASA NR 510001787)SDR AU510001603Seal · failedLT WING LT INBOARD FLAP OUTBOARD UPPER SEAL SEPARATED DURING TAKEOFF.SDR AU510001481Nipple · missing(AUS) FLAP BALL NUT GREASE NIPPLE MISSING.(OTHER CAUSE: UNKNOWN ) (CASA# 510001481)SDR AU510001443Skin · cracked(AUS) LH AND RH WING FLAP SKINS CRACKED. WHEN THE SKINS WERE REMOVED FOR REPLACEMENT, INTERNAL CORROSION WAS ALSO FOUND.(OTHER CAUSE: AGE ) (CASA# 510001443)SDR ASAA0580557Vane · dentedC-CHECK, LT WING NR 1 FLAP VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K)SDR ASAA0580556Vane · puncturedC-CHECK, LT WING NR 1 FLAP VANE IS PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K)SDR ASAA0580555Vane · gougedC-CHECK, LT WING OB FLAP IB VANE IS GOUGED. BLENDED GOUGE. INSTALLED REPAIR DOUBLER. (K)SDR SROM200500017Spindle · crackedDURING ROUTINE NDT INSPECTION OF OB FLAP SPINDLE IAW AD 2003-24-08 AND SB 737-57A1277 FOUND A FLAP CARRIAGE SPINDLE CRACKED 40 PERCENT AT THE RADIUS OF THE YOKE TO THE FIRST BEARING LAND. FLAP CARRIAGE ASSEMBLY REPLACED WITH A NEW UNIT. RECORDS INDICATE 5221 SDR 05FDEA04245Skin · scratchedSCARATCHES TO UPPER SURFACE OF RT WING O/B FLAP BETWEEN NR 3 AND NR 4 CANOES NR 36 HURRICANE RITA REF N00086. REPAIRED 3 EA DENTS ON RT O/B FLAP IAW A310-200 SRM 57-53-12 REPAIR NR 11.SDR USAA051496Skin · debondedFOUND TRAILING EDGE WEDGE TOP SKIN DISBONDED INBOARD END NUMBER 3 SLAT. MAJOR REPAIR IAW SRM 51-70-10, DEFECT SIZE: 1".SDR USAA051507Wedge · delaminatedFOUND DELAMINATION INBOARD FOREFLAP TOP SKIN INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 3.5.SDR 05FDEA04237Mount · corrodedFOUND RIGHT WING, REFWERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE SIDE LOAD FITTING ATTACHMENT LOWER MOUNT BORE CORRODED. REPAIRED AS PER FEDEX EA 1-5750-94562.SDR 05FDEA04236Bushing · migratedFOUND RIGHT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE UPPER OUTBOARD MOUNT BUSHING MIGRATED.SDR 05FDEA04235Bushing · migratedRIGHT HAND WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE UPPER INBOARD MOUNT BUSHING MIGRATED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94562.SDR 05FDEA04234Mount · corrodedFOUND RIGHT WING, WITH REFERENCE TO EO 1-5750-7-5002, OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG BORE CORRODED. CORROSION REMOVED AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-94562.
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