JASC 5753
Service difficulty reports · 31,513
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 A6WA2018100146092Skin · gougedLEFT HAND, OUT BOARD FLAP VANE, O/B END OF VANE HAS A GOUGE. REPLACED LT, O/B FLAP VANE LEADING EDGE SKIN IAW SRM 57-53-00, 51-42-13, 51-24-36, TR-51-42.SDR SWAA2018092825606Flap Track · looseRT WING OUTBOARD AFT FLAP OUTBOARD TRACK LOOSE AT ATTACH POINT. R&R TRACK PER AMM.SDR U2RA201809250009Skin Panel · corrodedRIGHT HAND WING TRAILING EDGE OUTBOARD FORE FLAP HAS 2 EACH AREAS OF CORROSION ON LOWER SKIN PANEL. CORROSION CLEANUP OUTSIDE OF STRUCTURAL REPAIR MANUAL LIMITS. REPLACED RIGHT HAND WING TRAILING EDGE OUTBOARD FORE FLAP PER AIRCRAFT MAINTENANCE MANUAL 27-51-0SDR FDEA201809252684Hinge Bracket · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) LOWER MOUNT OUTBD HOLE BORE FOUND CORROSION. LH WING O/B FLAP I/B HINGE ( WING SIDE) LOWER MOUNT O/B HOLE BORE( #7 HOLE) CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM57-44-08. NEW OVERSIZED BUSHSDR FDEA201809252683Hinge · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) LOWER MOUNT INBD HOLE BORE FOUND CORROSION LH WING O/B FLAP I/B HINGE ( WING SIDE) LOWER MOUNT I/B HOLE BORE (#7 HOLE) CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM57-44-08. NEW OVERSIZED BUSHINSDR FDEA201809252682Hinge · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) BARREL NUT HOLE SURFACE FOUND CORROSION LH WING O/B FLAP I/B HINGE ( WING SIDE) BARREL NUT HOLE SURFACE CORROSION REWORKED AS PER MD1 CMM57-44-08. NEW REPAIR SHIM FABRICATED AND INSTALLED PER MD11 CMM57-4SDR FDEA201809252681Hinge · corrodedLEFT WING - OUTBD FLAP INBD HINGE ( WING SIDE ) PIVOT HOLE BORE FOUND CORROSION. LH WING ( WING SIDE ) O/B FLAP I/B HINGE PIVOT HOLE BORE #4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER MD11 CMM 57-44-08. NEW OVERSIZED BUSHING FABRICATED BY MACHINING ASDR FDEA201809252722Skin · crackedRT WING INBD FLAP UPPER SURFACE APPROX XIFH 207, TWO CRACKS AROUND FASTENERS. CONFIRMED USING NDT HFEC. DOUBLER REPAIRED PER SRM 57-10-00 FIG 85 SHEET 3 VOL 1. REF EA 8-5700-T0342609.SDR FDEA201809252706Skin · puncturedRIGHT WING INBD FLAP VANE LOWER SURFACE FOUND PUNCTURED AT XIFH 193.875. SKIN REPAIR CARRIED OUT METAL BONDED WITH FILLER AND DOUBLER AS PER SRM 51-71-00 PARAGRAPH 20 AN EA 1-5750-T0342536 PART 1. REPAIR ON RT INBD FLAP VANE ARC2557-54 LOWER SKIN. REPAIR CLASSSDR DALA2018092505740Flap · puncturedINBD RIGHT TRAILING EDGE FLAP PUNCTURE/HOLE. INSTALLED PERM REPAIR PER ERA 571754-14 REV ORIGINAL SECTION III.SDR AALA2018092549011Strut · corrodedLEFT FLAP INTERCONNECT STRUT HAD CORROSION ON THE SHAFT. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLAP INTERCONNECT STRUT IAW AMM 27-51-44. OPS CHECKED GOOD.SDR FDEA201809202643Flap · gougedFOUND DAMAGE ON LEADING EDGE OF OUTBOARD FLAP ADJACENT TO NR 12 SPOILER ACTUATOR. REF WRI 29-02/8711 LEADING EDGE FLAP GOUGE IS OUT OF LIMITS REF SRM 57-53-01-1A. COMPLIED WITH EA G-2750-T0342462 PART1. REPAIRED RT WING OUTBOARD FLAP LEADING EDGE PER SRM 51-70SDR LR7A2018092101446Skin · dentedDURING SCHEDULED C-3 CHECK, FOUND THE LT OUTBOARD FLAP LOWER SKIN DENTED AT OWFS16L. REPAIRED IAW SRM, FIG 51-140-12.SDR A6WA2018092146080Skin · chafedRIGHT FLAP VANE SKIN CHAFED AT I/B BUMPER. REPLACED FLAP VANE SKIN IAW SRM 51-42-13.SDR AALA2018092109004Attach Fitting · corrodedCORROSION FOUND ON THE RIGHT WING OTBD FLAP TRACK SPHERICAL BEARING ATTACH FITTING. REPLACED THE FLAP IAW TC 26L00027009.SDR SWIA2018101645147Cap · chafedCHAFED ON LT INBD FLAP, OUTBOARD CENTER FLAP VANE CAP. (C-CHECK) RO: 10/14/2018 INSTALLED NEW LT INBD FLAP, OUTBOARD CENTER FLAP VANE CAP IAW SRM.SDR FDEA201809182574Hinge · corrodedLEFT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT OUTBD LUG HOLE FOUND CORROSION. HOLE A AND B REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-73337 D PART 4 STEP 2A AND 2B. REPAIR CLASSIFIED AS MSDR FDEA201809182573Hinge · corrodedLEFT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT INBD LUG HOLE FOUND CORROSION. CORROSION (HOLE F AND G) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-73337 D PART 4 STEP 2A AND 2B. REPAIR CLASSIFSDR FDEA201809182572Hinge · corrodedRIGHT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT ATTACHED OUTBD LUG HOLE FOUND CORROSION. CORROSION (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0326166 B PART 4 STEP 2A AND 2BSDR FDEA201809182571Hinge · corrodedRIGHT WING INBD FLAP OUTBD HINGE (FLAP SIDE) PIVOT ATTACHED INBD LUG HOLE FOUND CORROSION. CORROSION (HOLE F AND G) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0326166 B PART 4 STEP 2A AND 2B. RSDR AALA2018092199013Strut · corrodedCORROSION FOUND ON THE LEFT WING INTERCONNECTING STRUT. REPLACED LEFT WING INTERCONNECTING STRUT.SDR AALA2018092199012Strut · corrodedCORROSION FOUND ON THE RIGHT WING INTERCONNECTING STRUT. REPLACED RIGHT WING INTERCONNECTING STRUT.SDR DALA2018092000219Cover Plate · missingFLAP TRACK FAIRING COVER MISSING ON LEFT WING LOCATION 531AB, FIRST FAIRING. REPLACED COVER PLATE.SDR ASOA2018092065213Skin · dentedSEVERAL DENT FOUND ON THE LT OUTBOARD FLAP UPPER SKIN. PERFORMED A MAJOR REPAIR TO LT OUTBOARD FLAP UPPER SKIN IAW EC/TC SNIEO 601R14535 S02.SDR AALA201809179031Skin · corrodedCORROSION FOUND ON THE LEFT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE. THE AIRCRAFT WAS GROUNDED. REPAIRED THE FLAP IAW EA 284911.SDR DALA2018091805648Support · corrodedCORROSION ON AFT FAIRING FLAP SUPPORT STA WS 315 AT RT WING INBD MAIN FLAP. LEVEL CORROSION 2, SUPPORT ON FAIRING FLAP WAS REPLACED WHERE ORIG THICKNESS 0.266" REMAINING THICKNESS 0.252" PER SRM 51-40-02 PAR 9 AND B DRAWING 113N2383 REV D.SDR Q5QA2018122809Spar · crackedINSPECTION DISCLOSED LEFT FLAP SPAR WAS CRACKED ALONG UPPER FLANGE CORNER AT OUTBOARD FLAP TRACK BRACKETRY.SDR FDEA201809142546Fitting · corrodedRT O/B FLAP VANE HORN FITTING "F" FOUND HOLE BORE CORROSION. RT O/B FLAP VANE HORN FITTING 'F' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0342271 PART 1 STEP 1B. REPAIR CSDR FDEA201809142545Fitting · corrodedRT O/B FLAP VANE HORN FITTING "E" FOUND HOLE BORE CORROSION. RT O/B FLAP VANE HORN FITTING 'E' HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0342271 PART 1 STSDR IPXA2018092434321Rib · chafedLEFT WING INBD FLAP, INBD TRACK FAIRING RIB WAS CHAFED. REMOVED AND REPLACED THE RIB IAW SRM 51-33-01, AND 51-35-01. MINOR.SDR IPXA2018092104202Tee Fitting · crackedLEFT WING, OTBD FLAP, INBD FWD HINGE FAIRING, OTBD FWD LOWER PANEL SUPPORT TEE FITTING WAS CRACKED. REMOVED AND REPLACED THE TEE IAW SRM 51-33-01. MINOR.SDR FDEA2018091432497Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132149 C PART 5 STSDR FDEA2018091432496Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132149 C PART 5 STSDR FDEA2018091432495Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132148 C PART 5 STSDR FDEA2018091432494Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1- 5750-132148 C PART 5 SSDR FDEA2018091432511Skin · wornRT MAIN FLAP TOP SURFACE HAS 2 WEAR MARKS OPPOSITE NR 10 SPOILER ACTUATOR. REPLACED DAMAGED REPAIR PLATE ON RT MAIN FLAP TOP SURFACE IAW SRM 57-53-01-2R REPAIR 2 FIG 201 REV 124SDR FDEA2018091432491Bracket · crackedRT OB FLAP OB TOP TO LWR SKIN AFT BRACKET CRACKED. FABRICATED AND INSTALLED NEW BRACKET IAW GMM 7-00-1001 REV 150 AND DRAWING 113N3370 SHEET 2 REV C AND SRM 51-30-01 AND 51-40-02 REV 124.SDR AALA201809149010Trunnion · corrodedTHE LEFT WING OUTER TRUNNION HAS CORROSION ON THE SPLINE. THE AIRCRAFT WAS GROUNDED. REPLACED THE TRUNNION IAW TC 26L00027003.SDR R61A201809111011Bolt · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. LEVEL 2 CORROSION WAS FOUND AT RT WING NR 2 FLAP TRACK SUPPORT ACTUATOR FITTING FASTENERS . FASTENERS WERE REMOVED AND REPLACED IAW AMM 57-54-21-000-801A. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPSDR AALA201809149012Skin · damagedTHE RIGHT WING OUTBOARD TRAILING EDGE FLAP HAS MOISTURE INGRESS. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLAP IAW AMM 27-51-22.SDR AALA201809149011Skin · damagedTHE LEFT WING OUTBOARD TRAILING EDGE FLAP HAS MOISTURE INGRESS. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLAP IAW AMM 27-51-22.SDR AALA201809129016Strut · corrodedCORROSION WAS FOUND ON THE RIGHT WING INBOARD FLAP INTERCONNECTING STRUT. REPLACED IAW TC 26C67057001.SDR AALA201809129015Strut · corrodedCORROSION WAS FOUND ON THE LEFT WING INBOARD FLAP INTERCONNECTING STRUT. REPLACED IAW TC 26C57057001.SDR IPXA2018091133876Skin · damagedINSPECTION TYPE:SEG3, RT IB MAIN FLAP LOWER SURFACE DAMAGE APPROX 1 FOOT OB OF FLAP CANOE FAIRING. REPAIRED LWR SURFACE PANRL PN 113N2402 IAW SRM 51-70-10-2R.SDR K2ZA2018091200001Bracket · damagedAFTER LANDING, DURING FLAP RETRACTION, A LOUD POP WAS HEARD BY BOTH PEOPLE ABOARD. DURING POST FLIGHT IT WAS FOUND RT FLAP HAD BOUND ON BRACKET PN 0523231-5 DURING RETRACTION CAUSING DAMAGE TO FLAP, BRACKET, AND FLAP TRACK BRACKET. CRACKS FOUND IN THE LOWER ELSDR DALA2018091005526Fairing · damagedRT WING INBD TRUNNION FAIRING DAMAGED. RMVD RT WING INBD AFT FLAP FAIRING PER AMM 27-51. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 57-51-70 SANDED, CLEANED AND PAINTED REPAIR AS REQUIRED PER SRM 57-51-70. REINSTALLED FAIRING PER AMM 27-51.SDR ASOA2018091885200Skin · dentedRIGHT INBOARD FLAP LOWER SKIN AT LOCATION K WAS DENTED APPROX .739 INCHES BY .070 INCHES DEEP. PERFORMED A MAJOR REPAIR TO RIGHT INBOARD FLAP LOWER SKIN IAW SRM 57-52-00.SDR IPXA2018091033747Fairing · damagedINSPECTION TYPE:SEG4, RT WING I/B FLAP LOWER SIDE AT CANOE FAIRING HAVE TWO DINGS. REMOVED PANEL REPAIRED IAW SRM 51-70-10-2R REINSTALLED PANEL.SDR A6WA2018091046046Skin · gougedRIGHT I/B FLAP, LOWER SKIN HAS GOUGE AND DENT. REPAIRED RIGHT I/B FLAP LOWER SKIN IAW REO 601R-57-52-1544 REV-.SDR FDEA2018091172417Fitting · corrodedLT O/B FLAP VANE HORN FITTING 'F' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHEET 1. EXISTING SLOT HOLE: LENGTH 0.852", WIDTH 0.600", FINAL SLOT HOLE: LENGTH 0.960", WIDTH 0.708". REPAIR LIMIT - LENGTH 0.940", WIDTH
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