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 IXXA0400034SSkin · damagedDURING ROUTINE C-CHECK INSPECTION RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR BETWEEN STA XF 415.000 TO XF 440.00. REPAIR IS ACCOMPLISHED BY REPLACEMENT WAS ACCOMPLISHED IN ACCORDANCE WITH DC8 SRM CHAPTERS 57-1-0 PG 1, 57-7-1 FIG 4 TR 57-94, 51SDR IXXA0400032SSkin · damagedDURING ROUTINE INSPECTION RT OUTBOARD FLAP HAS INTERIM REPAIR ON UPPER PANEL (STA SF 415.000-440.000) MAJOR REPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-4 FIG 4. REMOVED UPPER SKIN WITH INTERIM REPAIR ON ISDR IXXA0400030SHinge Fitting · crackedDURING ROUTINE C-CHECK INSPECTION RT WING INBD FLAP HINGE SUPPORT FITTING CRACKED 4 INCHES STA XW 97-906. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REAIR IAW DC8 SRM 57-1-0 PAGE 1. REMOVED CRACKED FITTING IAW DC8 SRM 51-3-0 PAGE 1. CLEANED, TREATED AND PSDR 04FDEA00545Support · crackedRT WING OUTBOARD FLAP INBOARD HINGE BRACKET SUPPORT RIB (INTERIOR) FOUND CRACKED. RT WING O/B FLAP ASSY REMOVED & REPLACED AS PER AMM 27-50-30, OPERATION TEST & ADJUSTMENT CARRIED OUT FOUND SATIS AS PER AMM 27-50-00. COMPLIED WITH EA 1-5750-7529.1 TE FLAPS O/BSDR AWXA200400297Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-15 CHECK FOUND LOWER SURFACE OF LT INBOARD MID FLAP WEDGE DELAMINATED 13.75 INCHES FROM OUTBOARD END. MAINTENANCE CUT OUT DAMAGED SKIN AND CORE ON LOWER SURFACE OF LT INBOARD MID FLAP WEDGE; FABRICATED REPAIR CORE AND DOUBLER; INSDR AWXA200400341Doubler · debondedMCN - MAJOR REPAIR - DURING C-15 CHECK FOUND EXISTING REPAIR ON UPPER SURFACE OF LT INBOARD FORE FLAP DISBONDED 36 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED DISBONDED REPAIR ON UPPER SURFACE OF LT INBOARD FORE FLAP; FABRICATED REPAIR DOUBLERS; INSTALLED RSDR ASAA0480129Skin · dentedOKC - DURING HV6 CHECK, FOUND STRIP, ANTI-ABRASION COATING AT OUTBOARD LOWER END OF LEFT INBOARD FLAP WEDGE AND EVALUATE 3 DENTS. REMOVED DAMAGED SKIN SECTION, FABRICATED AND INSTALLED REPAIR SKIN IAW MD80 SRM 51-70-4. (M)SDR ASAA0480124Vane · wornOKC - DURING HV6 CHECK, FOUND RIGHT WING OUTBOARD FLAP VANE INBOARD AFT EDGE IS WORN. BLENDED OUTBOARD FLAP TRAILING EDGE. FOUND TO BE IN LIMITS IAW ASA EA 5750-01923, AND AAR EA 10283. (M)SDR DHL2004720002Skin · corrodedLEFT-HAND INBOARD MID FLAP LOWER SURFACE 2 AREAS OF SURFACE CORROSION. REMOVED CORROSION, TREATED AND PRIMED IAW B-727 SRM 51-10-2.SDR UPS04541961Skin · crackedRIGHT O/B TRAILING EDGE FLAP HAS A 3 INCH CRACK. DEFERRED AS PER EO 757-5750-8002 D INITIAL REPAIR IS C/W. COMPLY W/FINAL REPAIR AT OR BEFORE NEXT C CHECK. D276705 ASSIGNED. C/W REPLACEMENT OF PANEL PER BOEING DRAWING 113N3600 AND EO #B757-5720-20123-ASDR SWAA040639Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD AFT FLAP PER MM.SDR SWAA040638Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER MM.SDR 2004UALA00173Skin · delaminatedTRAILING EDGE FLAPS SKIN HAS DAMAGE AND IS DELAMINATED. REPLACED THE TRAILING EDGE WEDGE.SDR GLBA20030574Rib · crackedCRACK ON RIB LINK ALONG CENTER RIB ON LT NAC FLAP, REMOVED AND REPLACED RLB LINK PN 120-34222-009 ON NACCLLE FLAP.SDR MASA200400114Flap · contaminatedAFTER TAKE-OFF THE FLAPS WOULD NOT RETRACT, THE LANDING GEAR WOULD NOT RETRACT PROPERLY AND SEVERAL WING ANTI-ICE MSGS APPEARED. THE A/C RETURNED TO THE FIELD WERE MX FOUND ICE FOULING THE FLAPS AND LANDING GEAR. AFTER RESETTING THE FLAPS AND CLEARING THE ICE SDR IXXA0400031SSkin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND RT WING INBD FLAP UPPER PANEL HAS INTERM REPAIR, STA XW 28.000-XW 86.000 MAJOR REPAIR. REPAIRS ARE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 2 PAGE 2. REMOVED INTERM REPAIR ISDR SWAA040580Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT T/E. REMOVED AND REPLACED FOREFLAP PER MM.SDR 04FDEA00517Hinge · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE FOUND CORRODED. RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LT AND RT INBOARD TRAILING EDGE FLAP - HSDR CALA0400163Flap · delaminatedINSPECTION FOUND LEFT WING NR 1 AFT FLAP INBOARD T/E DELAMINATED. REPAIRED IAW SRM 51-70-10.SDR ASAA0480108Vane · chafedOKC - DURING HVC CHECK, FOUND LEFT WING OUTBOARD FLAP VANE INBOARD CAM AND VANE LEADING EDGE ARE CHAFED. REMOVED DAMAGED SECTION. INSTALLED FILLER AND DOUBLER PER SRM 51-70-2 AND 57-03. (M)SDR 04FDEA00516Hinge · corrodedRT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE FOUND CORRODED. RT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAPSDR CALA0400162Skin · puncturedINSPECTION FOUND RIGHT INBOARD T/E AFT FLAP PUNCTURED ON BOTTOM SIDE. THE FLAP WAS REPAIRED IAW SRM 51-70-10.SDR AWXA200400264Skin · debondedMCN - MAJOR REPAIR - DURING C-20 CHECK FOUND DISBOND AREA ON UPPER SURFACE OF LT OUTBOARD FORE FLAP, 104 INCHES FROM OUTBOARD END. MAINTENANCE CUT OUT DISBOND AREA ON UPPER SURFACE OF LT OUTBOARD FORE FLAP; FABRICATED A REPAIR CORE AND DOUBLER; INSTALLED REPASDR AWXA200400251Skin · debondedMCN - MAJOR REPAIR - DURING C-20 CHECK THE UPPER SURFACE OF LT WING INBOARD FORE FLAP WAS FOUND DISBONDED 34.75 INCHES FROM OUTBOARD END. MAINTENANCE CUT OUT DISBOND AREA OF LT WING INBOARD FORE FLAP; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW 51-SDR SWAA040560Spindle · crackedDURING SCHEDULED SPV, FOUND RT WING NR 8 T/E FLAP SPINDLE WITH CRACK INDICATION. REMOVED AND REPLACED NR 8 FLAP SPINDLE PER MM.SDR 04FDEA00512Hinge · corrodedLT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-74322 - WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP HINGE BRACKETS CORRODED.SDR 04FDEA00513Hinge · corrodedLT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE FOUND CORRODED. LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74322, WINGS - LEFT AND RIGHT INBOARD TRAILING EDGE FLAP HISDR SWAA040553Flap · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING RT OUTBOARD T/E FLAP DELAMINATED. REPAIRED T/E FLAP PER SRM.SDR AWXA200400266Skin · delaminatedMCN - MAJOR REPAIR - DURING C-20 CHECK FOUND THE LT WING TRAILING EDGE FORE FLAP DELAMINATED ON THE OUTBOARD LOWER SURFACE, APPROXIMATELY 2 INCHES FROM END. MAINTENANCE CUT OUT DELAMINATION ON LT WING TRAILING EDGE FORE FLAP; FABRICATED A REPAIR CORE AND DOUBSDR AWXA200400250Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-20 CHECK THE RT WING INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED ON LOWER SURFACE APPROXIMATELY 36 INCHES FROM INBOARD END. MAINTENANCE CUT OUT DELAMINATED AREA OF MID FLAP TRAILING EDGE WEDGE AND FOUND NO CORE DAMSDR SWAA040536Wedge · delaminatedDURING SCHEDULED 5Y CHECK, FOUND LT WING OUTBOARD AFT FLAP T/E WEDGE DELAMINATED. REPAIRED T/E WEDGE PER SRM.SDR CALA0400145Skin · gougedINSPECTION FOUND NR 3 MID FLAP OUTBOARD L/E SKIN GOUGED JUST FORWARD OF EXHAUST GATE. FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5752-01144.SDR SWAA040529Flap · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD T/E AFT FLAP PER MM.SDR 04FDEA00465Hinge · corrodedRT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00464Hinge · corrodedRIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00463Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00462Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00461Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00460Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00459Hinge · corrodedRIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00458Hinge · corrodedRIGHT WING - OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00455Hinge · corrodedRT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, TITLE SDR 04FDEA00454Hinge · corrodedRT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. RT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750- 74319, TISDR 04FDEA00453Hinge · corrodedRT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00452Hinge · corrodedRT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00451Hinge · corrodedRT WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74319 - WINGS - LT AND RT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00450Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE SPOT FACE CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, - LEFT AND RIGHT OUTBAORD FLAP INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00449Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE CORRODED. CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, WINGS - LEFT AND RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA00448Hinge · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORRODED. RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE CORROSION REMOVED AND REPAIRED AS PER EA 1-5750-74319, WINGS - LT AND RT OUTBOARD FLAP INBOARDSDR 04FDEA00447Hinge · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-74320 - WINGS - LT AND RT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.
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