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 SWAA050975Skin · peelingRIGHT WING INBOARD T/E FOREFLAP PREVIOUS REPAIR PEELING. TEMP REPAIRED PER SWA EA, THEN LATER AT PHX, REMOVED AND REPLACED FOREFLAP PER MM.SDR 05FDEA00763Structure · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR AND MINOR CLASSIFICATION. RT WING RT I/B T/E LOWER SURFACE AFT OF NR 2 FLAP TRACK BEAM. COMPLIED WITH EA 6-5750-87747 PART 1. NO DEFECTS NOTED PER NTM 51-10-08. REPAIR IS CLASSIFIED AS A MINOR REPAISDR 05FDEA00756Wedge · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION, LT WING COMPOSITE REPAIR LOWER SURFACE INBD T/E FLAP WEDGE 5 INCH FWD OF AFT EDGE AND 28 INCH O/B OF I/B EDGE. COMPLIED WITH EA6-5750-87746 PT1 NO ANOMALIES NOTED AS PER FEDEX GMSDR 05FDEA00708Hinge · corrodedLEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT OUTBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01. ALODINED AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED AND INSTALLED FINAL HONED NEW OVERSIZED BUSHING TO 0.99SDR 05FDEA00707Hinge · corrodedLEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION FROM BORE IAW DAC CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC19-10 SRM 51-21-01 VOL 2. FABRICATED AND INSTALLED AND FINAL HONED NEW OVERSIZED BUSHING TO 0.SDR 05FDEA00706Skin · damagedRIGHT WING INBOARD FLAP, INCORRECT REPAIR ON UPPER SKIN, INBOARD WEDGE. REMOVED DOUBLER, FABRICATED NEW SKIN, FINGER DOUBLERS AND DOUBLER AND BONDED IAW FEDEX EA 8- 5710-84001 AND TPS 1001 REV E AND DC10 SRM 51-21-01 VOL 2 AND DC10 SRM 51-31-01 VOL 2. REFESDR DHL2005740514Skin · delaminatedCUT OUT DAMAGED AREA LWR SKIN APPROX 5 X 1.5 INCH IAW B727 SRM 51-40-20 FIG 31. FABRICATED ONE FILLER APPROX 5 X 1.5 INCH AND ONE DOUBLER APPROX 8 X 3 INCHES USING .016 2024-T3 PO 9001660 IAW B727 SRM 57-50-2 FIG 4. CLEANED, PREPPED, APPLIED ADHESIVE PRIMERSDR DHL2005740513Skin · debondedRT WING TE OB AFT FLAP LOWER SKIN DISBONDED AT TE CENTER. CUT OUT DAMAGED AREA LWR SKIN APPROX 5 INCHES BY 1 1/2 INCHES IAW B727 SRM 54-40-20 FIG 31. FABRICATED ONE FILLER APPROX 5 INCHES BY 1 1/2 INCHES AND ONE DOUBLER APPROX 8 INCHES BY 3 INCHES USING .01SDR DHL2005740505Skin · delaminatedRT WING OUTBD AFT-FLAP TRAILING EDGE INBD CORNER IS DELAMINATED LOWER SURFACE. CUTOUT DAMAGED LWR SURFACE APPROX 3 INCH BY 5 INCH BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 32. REMOVAL AND REPLACED HONEYCOMB CORE APPROX 3 INCH BY 4 INCH USING DUR-SDR SWAA050938Skin · delaminatedRIGHT WING INBOARD T/E FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR QXEA200500537Skin · chafedPDX - LEFT WING OUTBOARD FLAP, UPPER SURFACE IS CHAFED BETWEEN YW222 AND YW285. REPAIRED IAW HORIZON AIR EA 6-57-325.SDR 05FDEA00644Flap Track · corrodedNR 1 FLAP TRACK FWD I/B ATTACH LUG CORRODED. REPLACED PER FED EX W/C 27X5707-03.SDR 05FDEA00643Flap Track · corrodedNR 3 FLAP TRACK AFT MOUNTING PAD CORRODED. REPLACED NR 3 FLAP TRACK PER FED EX W/C 27X5705-03.SDR QXEA200500633Hinge · chafedYYC - RIGHTHAND INBOARD FLAP LOWER SURFACE INBOARD HINGE AREA HAS CHAFED MARKS FROM FAIRING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.SDR QXEA200500627Skin · damagedYYC - RIGHTHAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-12-00-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 57-52-01-101-001-A01.SDR UIEA200500038Spar · corrodedDURING SCHEDULE INSPECTION, CORROSION WAS FOUND ON THE REAR SPAR ATTACHMENT HOLES OF NR 5 TRAILING EDGE FLAP TRACK. OVERSIZED THE AFFECTED ATTACHMENT HOLES. MAGNETIC PARTICLE INSPECTED THE REWORKED AREA TO ENSURE CRACK AND DEFECT FREE CONDITION. THE REPAIRESDR UIEA200500039Skin · delaminatedDURING SCHEDULE INSPECTION, DELAMINATION WAS FOUND ON THE OUTBOARD TRAILING EDGE FLAP AFT FLAP LOWER SKIN PANEL. PANELS EXCEEDED 25 PERCENT DAMAGE OF THE TOTAL AREA. TRIMMED OUT THE DELAMINATED SKIN REGIONS. NDT INSPECTED TO ENSURE CRACK AND DEFECT FREE CONSDR QXEA200500553Skin · damagedYYC - LEFTHAND INBOARD FLAP LOWER SURFACE GRAVEL DAMAGED. REPAIRED IAW CRJ 700 SRM 51-25-01-001-A01.SDR SWAA050904Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBOARDD MIDFLAP OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.SDR DHL2005782561Skin · delaminatedLT WING OB AFT FLAP OB TE CORNER DELAMINATED. REMOVED PREVIOUS REPAIR AND CUT OUT DELAMINATED AREA OF LOWER SKIN APPROX 7" BY 5" AT O/B CORNER AND VACUUM BAGGED FOR MOISTURE REMOVAL IAW B727 SRM 51-40-20 FIG 31. FABRICATED REPLACEMENT SKIN APPROX 7" BY 5" ASDR SWAA050878Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD AFT FLAP T/E DELAMINATED. REPAIRED FLAP PER SRM.SDR UIEA200500030Link · migratedDURING SCHEDULE MAINTENANCE, NR 4 T/E FLAP TRACK FAIL/SAFE LINK TOP END BEARING ON THE 'T' CHORD FOUND MIGRATED. THE LEFT FIXED TRAILING EDGE UPPER CHORD HOLE HAS ELONGATED DAMAGED. OVERSIZED HOUSING BORE TO A MAXIMUM OF .8930 INCH DIAMTER. NDT INSPECTED THSDR DL757050179Spar · crackedDURING SHOP VISIT, IMPACT DAMAGE WAS FOUND ON THE RT INBOARD MAIN FLAP. THE IMPACT CAUSED DAMAGE TO THE REAR SPAR LOWER CHORD, WHICH WAS SPLICE REPAIRED BETWEEN STA 117 AND 127. REPAIRED PER DELTA ERA 097596-14.SDR ASAA0540193Wedge · chafedRT WING IB T/E MIF FLAP T/E WEDGE IS CHAFFED. REMOVED DAMAGED WEDGE, ORDERED AND REPLACED WITH A NEW WEDGE IAW SRM. (K)SDR UPS05844293Rib · damagedINSPECTION TYPE:C2 RIGHT STA 3 AFT LINK TO FLAP HINGE BOLT FROZEN & NUT PLATE BROKEN. REMOVED DAMAGED RIB, REMOVED AND REPLACED NUT PLATE, AND FABRICATED & INSTALLED REPLACEMENT RIB PER EO DC8-5750-16293-A AND DWG DC8-57-009.SDR GAIA05014STSkin · delaminatedDURING A-CHECK, NO FLIGHT, FWA: FOUND LT IB MID-FLAP OB T/E MISSING 6 INCHES OF SKIN. REMOVED AND REPLACED LT IB MID-FLAP AND AFT FLAPS ASSY. OPS CHECKED NORMAL IAW MM 27-51. AIRCRAFT WAS RETURNED TO SERVICE. (SW07200506017) (K)SDR DHL2005782559Skin · debondedLT I/B T/E FOREFLAP DISBONDED AT T/E. CUT OUT DISBONDED AREA AT TE APPROX 4 1/2" BY 1 3/4". REMOVED DAMAGED CORE APPROX 4 1/2" BY 1 3/4" AND VACUUM BAGGED FOR MOISTURE REMOVAL FABRICATED REPLACEMENT SKIN APPROX 4 1/2" BY 1 3/4" EXTERNAL DOUBLER APPROX 3 1/2"SDR DHL2005782500Skin · debondedLEFT INBOARD T/E FOREFLAP DISBONDED AT /TE. CUT OUT DISBONDED AREA AT T/E APPROX 4.5 X 1.75 INCH, REMOVED DAMAGED CORE APPROX 4.5 X 1.75 INCH AND VACUUM BAGGED FOR MOISTURE REMOVAL. FABRICATED REPLACEMENT SKIN APPROX 4.5 X 1.75 INCH EXTERNAL DOUBLER 3.5 X 7.SDR ASAA0540181Wedge · dentedOKC - FOUND LEFT INBOARD TRAILING EDGE FLAP HAS SEVERAL DENTS. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 51-70-10 PAGE 8. (M)SDR ASAA0540179Wedge · dentedOKC - FOUND RIGHT INBOARD TE MID FLAP WEDGE DENTED WITH A CRACK. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW B737 SRM 51-70-10. (M)SDR 05FDEA00579Pad · corrodedPITTING AND CORROSION ON AFT MOUNTING PAD ON RT WING FOR NR 6 FLAP TRACK. REMOVED CORROSION IAW SRM 51-10-6 PG 5 FIG 4, FOUND TO BE WITHIN LIMITS ORIGINAL DRWG SPECS IAW DWG 66-14734. TREATED & PRIMED IAW SRM 51-10-2, ORIGINAL MAT THICKNESS .600, REMOVED .00SDR 05FDEA00578Skin · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. RT WING RT INBOARD TRAILING EDGE FLAP LOWER SURFACE AFT AND INBOARD OF NR 2 TRACK BEAM, ITEM 43 OF LIST. RT WING RT INBOARD TRAILING EDGE FLAP LOWER SUFACE AFT AND I/B OF NR 2 FSDR 05FDEA00577Wedge · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. LT WING REPAIR LOWER SURFACE I/B TRAILING EDGE FLAP FWD OF THE TRAILING EDGE WEDGE AND AFT OF NR 2 FLAP TRACK BEAM, ITEM 57 OF LIST. LT WING I/B FLAP LOWER SURFACE, AND AFT OF NSDR 05FDEA00532Skin · misrepairedCOMPLY WITH AGING 9 - AGING INSPECTION, LT WING - REPAIR AT LT INBOARD FLAP TRAILING EDGE, UPPER SURFACE (PLEASE EVALUATE). REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHSDR 05FDEA00527Skin · misrepairedCOMPLY WITH AGING 9 - AGING INSPECTION, RT WING - REPAIR AT RT INBOARD FLAP LOWER TRAILING EDGE. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 57-52-12.SDR SWAA050795Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED ON OUTBOARD EDGE LOWER SKIN. REMOVED AND REPLACED FLAP ASSY PER MM.SDR DHL2005805635Plate · crackedLT INBD FLAP LWR PLATING (2EA) DENTS AND 0.250 CRACK (STA XF 30.000- 40.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 02-28-05 EO NR AST 050209 DATED 02-25-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED SKIN SEGMENT IAW SDR UIEA200500019Link · gougedDURING D-CHECK, DEEP GOUGE FOUND ON THE EDGE OF THE INBOARD LINK ON THE NR 18 VARIABLE CAMBER FLAP. BLENDED OUT DAMAGE FROM SURFACE OF LINK. NDT INSPECTED TO ENSURE CRACK AND DEFECT CONDITION. SHOP PREENED PER SOPM 20-10-03, INTENSITY .006A2. REFINISHED LISDR DHL2005782536Skin · chafedRT IB FOREFLAP LOWER OB END CHAFFED THROUGH REPAIR PATCH. REMOVED FASTENERS AND PREVIOUS REPAIR FOR ACCESS IAW 727 SRM 51-30-2. HFEC INSPECTED AREA WITH NO CRACKS NOTED IAW B727 NDT MAN. PT. 6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER FROM 2024T3 .071 PO NSDR DHL2005782531Skin · delaminatedRT IB T/E FLAP IS DELAMINATED ON THE UPPER SURFACE OF THE AFT FLAP INBOARD EDGE CORRECTIVE ACTION: CUT OUT DELAM AREAS 3 APPROX 3 INCH DIAM, 2 INCH DIAM AND 2 INCH BY 4 1/4 AND CUT OUT PUNCTURED SKIN APPROX 2 INCH IAW B727 SRM 51-40-20 FIG 30. FABBED 2 FILLERSDR DHL2005782569Strip · missingLEFT I/B FORE FLAP WBL 70 UPPER SURFACE HAS CHAFE STRIP MISSING. REMOVED AND INSTALLED LEFT I/B FORE FLAP AFTER SHEET METAL REPAIR IAW B727 MM 27-51-1, OP CHECK GOOD IAW B727 27-51-0. CUT OUT DAMAGE SKIN, FABBED FILLER 3.5 X 2.5 INCH & DOUBLER 5 X 4 INCH FROSDR DHL2005782532Skin · debondedLT OB AFT FLAP IB UPPER SURFACE WBL 300 HAS DISBOND AT EDGE OF EXISTING REPAIR. FOUND 2 EACH DISBONDED AREA OF LOWER SKIN, ALSO REMOVED PREVIOUS REPAIR FROM LOWER SKIN AND CUTOUT DAMAGED AREA APPROX 48 SQ IN IAW B727 SRM 51-40-20 FIG 31. FABRICATED ON FILLERSDR DHL2005782526Skin · gougedLT OB FORE FLAP L/E IB AT WBL 314 HAS GOUGES IN REPAIR DOUBLER SURFACE. REMOVED DOUBLER IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER USING 2024T3 .063 PO# 9001978 DIM. 7 1/2" BY 3 1/2" IAW B727 SRM 57-50-2 FIG 3 AND 57-30-4 FIG 1. ALODINE AND PRIMED PART ANSDR DHL200578228Skin · gougedLT OB FORE FLAP L/E IB AT WBL 314 HAS 2 GOUGES IN REPAIR DOUBLER SURFACE. REMOVED DOUBLER IAW B727 SRM 51-30-2 FABRICATED NEW DOUBLER USING 2024T3 .063 PO NR 9001978 DIM 7 1/2" BY 3 1/2" IAW B727 SRM 57-50-2 FIG 3 AND 57-30-4 FIG 1. ALODINE AND PRIMED PART ASDR UPS05244172Fitting · corrodedINSPECTION TYPE:C NR 5 FLAP TRACK FWD SUPPORT FITTING P/N 65-21651 HAS PITTING CORROSION ON HOLE FOR SPECIAL STUD. REPAIR CARRIED OUT IAW AAAE EO 2005-021-003.SDR 05FDEA00484Support · corrodedCOMPLY WITH EA 8-5750-55451, RT OB FLAP FLAP VANE SUPPORT CORROSION REWORK. CLOSING ACTION ON 03/08/05. ON N/R S00013. COMPLIED WITH EA 8-5750-55451.SDR 05FDEA00460Vane · wornRIGHT HAND WING, INBOARD FLAP VANE, LEADING EDGE, ABOUT 25 INCHES (FROM OUTBOARD TO INBOARD). FOUND WITH CHAFFING DAMAGE OF 3 INCHES DIAMETER. REMOVED AND REPLACED PER AMM 27-50-22-02. ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-50-22-05.SDR 05FDEA00443Flap Track · corrodedRT WING FLAP O/B UPPER SURFACE AT NR 3 FLAP TRACK AND NR 4 FLAP TRACK HAS 2 EA AREAS OF NOTED CORROSION REF N00771. REMOVED CORR IAW SRM 51-74-10, FOUND IN LIMITS IAW SRM 57-53-12.SDR 05FDEA00442Skin · puncturedRT WING I/B FLAP UPPER SURFACE 3.9 IN FROM T/E AND 30 IN FROM I/B END SKIN PUNCTURED REF N00914. REPAIRED FLAP IAW SRM 57-52-12 FIG 4D.SDR ASAA0580172Vane · wornHV-CHECK - LT IB FLAP IB VANE IS WORN AT LEADING EDGE. INSTALLED REPAIR DOUBLER. (K)
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