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 2005FA0001546Support Bracket · brokenDURING APPROACH TO LANDING LT FLAP RETRACTED WHILE RT FLAP REMAINED EXTENDED. AN ASYMMETRICAL FLAP LANDING WAS MADE WITH MUCH DIFFICULTY BUT WITHOUT INCIDENT. INVESTIGATION REVEALED THAT A FLAP SUPPORT BRACKET PN 0523231-24 LOCATED WITHIN THE WING HAD FAILEDSDR AWXA200501592Skin · debondedMCN - DURING C20 CHECK DISCOVERED DISBOND AREA ON THE OUTBOARD END OF THE LT INBOARD MID-FLAP WEDGE PANEL, UPPER SURFACE. MAINTENANCE REMOVED DISBONDED SKIN IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 201. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 51-SDR AWXA200501591Wedge · debondedMCN - DURING C20 CHECK DISCOVERED DISBOND AREA AT THE AFT EDGE OF THE LT OUTBOARD FORE FLAP, APPROXIMATELY 8" FROM THE INBOARD END. MAINTENANCE REMOVED DISBONDED SKIN ON THE LT OTBD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R4. FABRICATED REPAIR FILLER AND SDR AWXA200501590Skin · delaminatedMCN - DURING C20 CHECK DISCOVERED SEVERAL AREAS OF DELAMINATIONS ON THE RT WING OUTBOARD FORE FLAP FROM WBL 202.69R TO WBL 281.0R. MAINTENANCE REMOVED AND REPLACED THE RT WING OUTBOARD FORE FLAP.SDR 05FDEA03779Repair · undamagedFOUND REPAIR ON LT OUTBD FORE FLAP INBD LEADING EDGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION, AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT OUTBD FORE FLAP I/B L/E WAS DETERMINED TO BE IAW SRM 5SDR 05FDEA03778Repair · undamagedFOUND REPAIR ON LT INBD FORE FLAP LEADING EDGE, 36 INCHES FROM OUTBD END. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT I/B FORE FLAP WAS DETERMINED TO BE IWSDR 05FDEA03762Hinge Fitting · corrodedFOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90057.SDR 05FDEA03760Hinge Fitting · corrodedFOUND LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90056.SDR 05FDEA03759Hinge Fitting · corrodedFOUND LEFT WING OUTBOARD FLAP INBOARD HINGE FITTING MOST AFT BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90059.SDR 05FDEA03756Repair · undamagedFOUND REPAIR RT INBD FORE FLAP. LEADING EDGE REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION, AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA, PREVIOUSLY INSTALLED REPAIR AT RT INBD FORE FLAP WAS DETERMINED TO BE IAW SRM 57-50-4 FIG 1. SDR 05FDEA03754Repair · damagedFOUND REPAIR LT I/B FORE FLAP, L/E REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT LT I/B, FORE FLAP WAS DETERMINED TO BE IAW SRM 57-50-4 FIG 1. BASED ON AN ESDR 05FDEA03761Hinge Fitting · corrodedFOUND RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING MOST AFT BOLT HOLE FOUND CORROSION. CORROSION REMOVED & REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-90058.SDR LR7A05189Spar · corrodedDURING C-7 CHECK PER HC5712, FOUND CORROSION ON LWR RT OB FLAP SPAR BEYOND LIMITS, FLAP STA 163-208. REPAIRED FLAP SPAR CAP IAW DRG R05-28-07, MEA 382-27-05-096, NR 0606.SDR LR7A05188Spar · corrodedDURING C-7 CHECK PER HC571, FOUND CORROSION ON LWR TH IB FLAP SPAR BEYOND LIMITS, FLAP STA 177-213. REPAIRED FLAP SPAR CAP IAW DRG R05-28-05, MEA 382-27-05-094, NR 0580.SDR LR7A05187Spar Cap · corrodedDURING C-7 CHECK PER HC5712, FOUND CORROSION ON LWR RT IB FLAP SPAR CAP BEYOND LIMITS, FLAP STA 177-213. REPAIRED FLAP SPAR CAP IAW DRG R05-28-06, MEA 382-27-05-095, NR 0566.SDR LR7A05186Spar Cap · corrodedDURING C-7 CHECK PER HC571, FOUND CORROSION ON LOWER LT OB FLAP SPAR CAP BEYOND LIMITS, FLAP STA 180. REPAIRED FLAP SPAR CAP IAW SMP 583 57-70-09, NR 0565.SDR LR7A05175Skin · crackedDURING C-7 CHECK PER HC5711, FOUND LT OB FLAP LE SKIN CRACKED 0.35 INCH ADJACENT TO FLAP CARRIAGE AT FLAP STA 28.1 AND 173.1. FS 600, WL270. REPAIRED SKIN AT FLAP STA 28.1 IAW DRG R05-028-02, MEA 382-57-05-088 AND SKIN AT FLAP STA 173.1 IAW SMP 583 FIG 51-140SDR 05FDEA03734Flap Track · corrodedNR 6 FLAP TRACK, AFT MOUNTING SURFACE IS CORRODED. RECEIVED NR 6 FLAP TRACK INSTALLED ON FED EX WC 27X5708-03.SDR 05FDEA03733Flap Track · corrodedNR 6 FLAP TRACK, FWD MOUNT BUSHINGS ARE CORRODED. NR 6 FLAP TRACK REPLACED ON FED EX WC 27X5708-03.SDR 05FDEA03728Skin · dentedLEFT WING OUTBOARD FLAP HAS DENTS 4 PLACES. DENTS AT XOF657, 639, AND 611 FOUND TO BE WITHIN LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL I. REPAIRED DENT AT XOF 516 IAW DC10 SRM 57-10-00 FIG 85 VOL I. SEE FEDEX NONROUTINE NR N00229 OF WORK ORDER 0030375.SDR C2XA05SH130Bushing · gougedSHV - DURING C-CHECK, MAINTENANCE FOUND LT I/B FLAP O/B BUSHING GOUGED (ON FLAP). MAINTENANCE REMOVED AND REPLACED LT I/B FLAP O/B BUSHING (ON FLAP) IAW EMB 145 EC5710-01096. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 05FDEA03717Skin · dentedLEFT WING INBD FLAP LOWER SKIN HAS SMALL DENTS. CHECKED DENT LIMITS IAW DC10 SRM 57-10-00 FIG 48 VOL I. FOUND TWO DENTS OUT OF LIMITS. REPAIRED DENTS AT XIFH 230-231 AND XIFH 278-280 IAW DC10 SRM 57-10-00 FIG 85 VOLI.SDR 05FDEA03670Doubler · unknownFOUND EXTERNAL DOUBLER REPAIR AT LEFT WING INBOARD FLAP, INBOARD TRAILING EDGE AREA BETWEEN WING STATION XIF187 AND XIF189. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST FOUND IN COMPLIANCE WITH SRM 57-00-01 FIG 4 SHT 2 VOL 1.SDR USAA051341Skin · gougedWEDGE SKIN 13.5 INCH FROM THE OUTBOARD END GOUGED. REMOVED SKIN AND DAMAGED CORE, INSTALLED CORE, FILLER AND DOUBLER IAW SRM 57-50-15 REV A. DEFECT SIZE: 4.3 X .5 INCH.SDR QXEA200501528Flap Track · damagedPDX: RIGHT INBOARD FLAP INBOARD UPPER FLAP TRACK INNER CHANNEL IS GALLED FROM THE MIDPOINT FWD BY THE AFT FLAP ROLLER SHAFT. MAINTENANCE REPAIRED IAW QX EA 6-57-393, NDTM PART 6, 51-00-02 AND RD 8/4-57-575.SDR USAA051328Skin · wornINBOARD LEADING EDGE. FABRICATED DOUBLER AND INSTALLED IAW SRM 57-53-01. DEFECT SIZE: 1 X 8 INCH DEEP WEAR AREA ON LEADING EDGE.SDR 05FDEA03613Skin · dentedRIGHT WING INBOARD FLAP HAS SPEED TAPE (LINE REPAIR) AFT OF NR 7 TIRE. REMOVED TEMP REPAIR AND REPAIRED SKIN IAW DC10 SRM 57-10-00 VOL I AND FEDEX EA 8-5750-91110 PART 3. P3 MOD TYPE T MOD REV NO A PS P3. EA IS ATTACHED TO WORK CARD 57501429, WORK ORDER 000SDR DHL2005749020Skin · delaminatedLT WING IB FOREFLAP DELAMINATED AT UPPER SURFACE IB EDGE. REMOVED UPPER SURFACE S/S RUBSTRIP AND DELAMINATED UPPER SKIN APPROX 14" BY 4" CUTOUT DAMAGED CORE APPROX 3 1/4" BY 6" FAB`D SEPTUM APPROX 3 1/4" BY 5 3/4" FROM 2024T3 .012 PO 900534 AND REPAIR CORE APSDR USAA051324Clip · crackedNR 3 FLAP TRACK STRUCTURE IB SIDE, AFT END. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-10-02 DEFECT SIZE: 1 INCH.SDR CA051102007Skin · cracked(CAN) OPENED LEADING EDGE OF RT FLAP SKIN FOR REPAIR. VISUALLY NOTICED CRACKED CENTER LEADING EDGE RIB AT BOLT HOLE FOR FLAP ACUATING PUSH ROD BRACKET ATTACHMENT. OUTER LEADING EDGE SKIN NOT DAMAGED AT THIS LOCATION.SDR AWXA200501471Skin · debondedMAJOR REPAIR - DURING C19 CHECK DISCOVERED DEBONDED AREA ON THE UPPER SURFACE OF THE LT OB FORE FLAP AT REPAIR DOUBLER, 88 INCHES FROM THE IB END. MAINTENANCE REMOVED DEBONDED AREA AT REPAIR DOUBLER AND DAMAGED HONEYCOMB CORE ON THE LT OB FORE FLAP IAW SRM 51SDR AWXA200501470Skin · debondedMAJOR REPAIR - DURING C19 CHECK DISCOVERED DEBOND AREA ON THE UPPER SURFACE OF THE RT OB FORE FLAP FROM WBL 306.61R TO WBL 308.61R. MAINTENANCE REMOVED DEBOND AREA ON THE UPPER SURFACE OF THE RT OB FORE FLAP IAW SRM 51-70-10-2R4. FABRICATED REPAIR DOUBLERS ISDR AWXA200501469Skin · debondedMAJOR REPAIR - DURING C19 CHECK DISCOVERED SKIN SEPARATED AT AFT IB CORNER OF THE RT OB AFT FLAP ASSEMBLY, UPPER AND LOWER SURFACE, FROM WBL 230.28R TO WBL 232.38R. MAINTENANCE REMOVED DISBONDED SKIN FROM UPPER AND LOWER SURFACE IAW SRM 51-70-10-2R4 FIG 203. SDR AWXA200501468Skin · debondedMAJOR REPAIR - DURING C19 CHECK DISCOVERED DEBONDED AREA ON THE UPPER AND LOWER SURFACE OF THE LT OB AFT FLAP FROM WBL 230.68L TO WBL 234.68L, IB END. MAINTENANCE REMOVED AREA OF DEBOND IAW SRM 51-70-10-2R4 FIG 203. FABRICATED CORE AND REPAIR DOUBLER IAW SRMSDR QXEA200501619Skin · damagedYYC - DURING C3 CHECK, RIGHT INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. MAINTENANCE BLENDED DAMAGE AREA IAW CRJ-700 SRM 57-01-101-001-A01, RESTORED FINISH.SDR QXEA200501617Skin · chafedYYC - DURING C3 CHECK, RIGHT WING INBOARD FLAP LOWER SKIN CHAFFED TRACK UNDER HINGE FAIRING 683BB. MAINTENANCE BLENDED DAMAGE IAW CRJ-700 57-52-01-101-001-A01. NO CRACKS FOUND. RESTORED FINISH.SDR QXEA200501616Skin · chafedYYC - DURING C3 CHECK, RIGHT WING INBOARD FLAP VANE UPPER SKIN HAS CHAFED DAMAGE AT TRAILING EDGE. REPAIRED IAW CRJ-700 SRM 51-12-00-001-001-A01. TREATED AND PRIMED AND PAINTED AREA.SDR DHL2005749009Skin · dentedFOUND LT WING I/B AFT FLAP DENTED AT LWR SURFACE. CUT OUT DENTED AREA APPROX 3 INCHES. DIA AT LT INB AFT FLAP LWR SURFACE FABBED FILLER APPROX 3" DIA AND DOUBLER APPROX 6" DIA FROM .016" 2024-T3 PO NR 9002556 BONDED FILLER AND DOUBLER SEALED AND PRIMED IAW BSDR SWAA053398Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING INBD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR 05FDEA03536Skin · crackedLEFT WING OUTBD FLAP UPPER SURFACE FOUND 2 EA CRACKS 0.25" LONG ON SKIN AT STA XOF 787. TRIMMED OUT DAMAGE SKIN INSTALLED DOUBLER AND FILLER IAW SRM 57-10-00 FIG 85 COLD BOND IAW SRM 51-71-00 PAR 16C VOL 2 AND SRM 51-35-02 PAGE 3/9. FABRICATED PARTS IAW DETASDR 05FDEA03535Skin · crackedLEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 EA CRACK 0.50" LONG ON SKIN AT STA XOF 563. TRIMMED OUT DAMAGE SKIN FABRICATED FILLER DOUBLER AND INSTALLED PER SRM 57-10-00 FIG 85 COLD BOND PER SRM 51-71-00 PAR 16C VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER SDR 05FDEA03533Skin · crackedLEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 EA CRACK 3" LONG ON SKIN AT STA XOF 557. TRIMMED OUT DAMAGE SKIN INSTALLED FILLER DOUBLER PER SRM 57-10-00 FIG 85 AND SRM 51-35-01 PAGE 1-13 COLD BOND PER SRM 51-71-00 PAR 16C VOL 2. FABRICATED PART IAW DETAIL PART SDR 05FDEA03520Skin · crackedLEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 CRACK 1" LONG ON SKIN AT STA XOF 575. TRIMMED OUT DAMAGED SKIN INSTALLED FILLER AND DOUBLER IAW SRM 57-10-00 FIG 85 AND COLD BOND SRM 51-71-00 PAR 16C VOL2 AND SRM 51-35-02 PAGE 3-9. FABRICATED PARTS IAW DETAIL PARTSDR 05FDEA03518Skin · nickedLT WING OUTBD FLAP UPPER SURFACE FOUND DEEP DENT AND NICK ON SKIN AT STA XOF 467. TRIMMED OUT DAMAGE SKIN INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 85 SHT 1 AND SRM 51-35-02 PAGE 3/9 VOL 2. COLD BOND PER SRM 51-71-00 PAR 16C VOL 2 FABRICATED PARTS IAW DESDR 05FDEA03514Flap Track · corrodedNR 3 FLAP TRACK AFT MOUNT PAD HAS HEAVY CORROSION. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4.SDR 05FDEA03513Flap Track · corrodedNR 6 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4.SDR 05FDEA03512Flap Track · corrodedNR 6 FLAP TRACK HAS CORROSION ON AFT MOUNT PAD. REPLACED FLAP TRACK WITH SERVICEABLE FLAP TRACK IAW MM 27-51-031-4.SDR SWAA053356Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR AWXA200501430Skin · debondedMCN - DURING C13 CHECK DISCOVERED DISBOND AREA AT THE OUTBOARD END OF THE RT INBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE CUTOUT DISBOND AREA ON THE UPPER AND LOWER SURFACES IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 203. FABRICATED REPLACEMENT CORE AND DOSDR AWXA200501415Wedge · debondedMCN - DURING C13 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE RT INBOARD FOREFLAP, 45" FROM INBOARD END. MAINTENANCE REMOVED DISBOND AREA ON THE RT INBOARD FOREFLAP IAW BOEING 737-300 SRM 51-70-10-2R REPAIR 4 FIG 201. FABRICATED FILLER AND DOUBL
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