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 06FDEA1921Bracket · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-99639, WINGS LH OUTBOARD TRAILING EDGE FLAP INBD BRACKET ATTACHMENT BORE, CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GSDR 06FDEA1920Bracket · corrodedFOUND LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD FORWARD HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, FORWARD FITTING INBOARD FORWARD HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-99639, TITLE: WINGS LEFTSDR SWAA061654Skin · debondedDURING SCHEDULED 10Y CHECK, FOUND RT WING T/E INBOARD FORE FLAP DISBONDED. REPAIRED FORE FLAP PER SRM.SDR SWAA061648Wedge · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING T/E MID FLAP T/E WEDGE CRACKED. REMOVED AND REPLACED T/E WEDGE PER MM AND SRM.SDR ASAA0680589Vane · gougedLEFT WING OUTBOARD FLAP INBOARD VANE IS GOUGED ON LEADING EDGE. REMOVED DAMAGED AREA. INSTALLED A SKIN FILLER AND INTERNAL DOUBLER PER SRM 51 70 2.SDR DHL2006754511Skin · dentedLEFT SIDE L/E AFT FLAP DENT O/B HINGE. EVALUATED DENT A/Y= 4/.40= .10 FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-50-1 FIG 1. REMOVED LEFT I/B AFT FLAP ASSY IAW B727 MM 27-51-03, CUT OUT DAMAGED AREA DIM 23.5 X 14.25 INCHES IAW B727 SRM 57-50-4 FIG 11, FAB FILSDR QXEA200601287Skin · chafedYYC - C4 RIGHT OUTBOARD FLAP UPPER SKIN HAS CHAF MARK FROM TRAILING EDGE. REPAIRED IAW RD8-57-3376 AND EA 2-57-365.SDR QXEA200601286Skin · chafedYYC - C4 RIGHT FLAP UPPER SKIN OUTBOARD END HAS CHAF MARK FROM TRAILING EDGE. REPAIRED IAW RD8-57-3376 AND EA 2-57-365.SDR 06FDEA1911Attach Fitting · corrodedNR 2 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REMOVED, REPAIRED AND REINSTALLED NR 2 FLAP TRACK FWD ATTACH FITTING IAW OHM 20-50-01 ANS FED EX EA 7-5710-96623.SDR SWAA061618Structure · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING T/E FLAPS INBOARD FORE FLAP CRACKED. REPAIRED FORE FLAP PER SRM.SDR 06FDEA1876None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE RT OUTBD FLAP T/E WEDGE UPPER SURFACE OUTBD OF NUMBER THREE FLAP TRACK, WS 871-893. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR .NEW REPAIR ACCOMPLISHESDR 06FDEA1875None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE RT OUTBD FLAP T/E WEDGE UPPER SURFACE INBD OF NUMBER THREE FLAP TRACK, WS 713-728. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING REPAIR OF SRM 57-53-12 FIG. 2SDR 06FDEA1874Wedge · damagedPREVIOUS REPAIR FOUND LOCATED ON THE LT OUTBD FLAP T/E WEDGE UPPER SURFACE OUTBD OF NUMBER FIVE FLAP TRACK, WS 1468-1484. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 57-53-12 FIG. 208 REPAIR EVALUATED SDR IXXA06SMN127SSkin · misrepairedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP UPPER PANEL HAS NON STANDARD REPAIR BETWEEN STATIONS XW 104.000 AND XW 115.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED PANEL PLATING WITH NON STANDARD REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, SDR IXXA06SMN122SSkin · misrepairedDURING ROUTINE C CHECK FOUND LEFT HAND WING INBOARD FLAP HAS NON STANDARD REPAIR AND DENTS FROM STATIONS XW 3.000 TO XW 92.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW DC-8 SRM 57-1-0, DC-8 SRM 51-1-21. FABRICATED NSDR IXXA06SMN124SSkin · misrepairedDURING ROUTINE C CHECK FOUND LEFT HAND WING INBOARD FLAP PLATING HAS NON STANDARD REPAIR BETWEEN STATIONS XW 104.000 AND XW 122.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED EXISTING PLATING WITH NON-STANDARD REPAIR IAW DC-8 SRM 57-1-0 PAGE SDR IXXA06SMN123SSkin · misrepairedDURING ROUTINE C CHECK FOUND LEFT HAND WING INBOARD FLAP PLATING HAS NON STANDARD REPAIR FROM STATIONS XW 122.000 TO XW 125.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-7-1 FIG 1. REMOVED EXISTING PLATING WITH NON-STANDARD REPAIR IAW DC-8 SRM 57-1-0 PAGE 1, DSDR SROM200600012Carriage · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING CPCP 10 YEAR REQUIREMENTS TO THE TRAILING EDGE FLAP CARRIAGES FOUND THE NR 3 TRAILING EDGE FLAP CARRIAGE IB CARRIAGE HALF TO HAVE LEVEL 2 CORROSION. REMOVED AND REPLACED WITH NEW UNIT V/S REPAIR FOR COMPANY CONSDR SROM200600011Carriage · corrodedDURING HEAVY MAINTENANCE CHECK WHILE PERFORMING A 10 YEAR CPCP INSPECTION REQUIREMENTS OF THE TRAILING EDGE FLAP CARRIAGES FOUND LEVEL 2 CORROSION ON NR 3 CARRIAGE OB CARRIAGE HALF. REPLACED WITH NEW HALF V/S REPAIR FOR COMPANY CONVENIENCE.SDR SWAA061593Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING T/E OUTBOARD FLAP DELAMINATED. REMOVED AND REPLACED LT T/E FLAP PER MM.SDR SWAA061585Torque Tube · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING T/E MID FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED OUTBOARD TORQUE TUBE PER CMM AND SRM.SDR SWAA061584Torque Tube · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING T/E MID FLAP INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED INBOARD TORQUE TUBE PER CMM AND SRM.SDR SWAA061583Flap Track · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING T/E MID FLAP CETER FORE FLAP TRACK CORRODED. REMOVED AND REPLACED FORE FLAP TRACK PER CMM AND SRM.SDR SWAA061571Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING T/E INBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR 06FDEA1758Flap Track · corrodedNR 7 FLAP TRACK FORWARD SUPPORT FITTING HAS CORROSION PITTING ON INBOARD FACE. REMOVED FITTING, REPAIRED IAW FED EX DWG SR27-57-020 REV A AND SOPM 20-10-03 AND REINSTALLED FITTING IAW OHM 20-50-01.SDR SWAA061541Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD T/E FLAP DELAMINATED. REPAIRED T/E FLAP PER SRM.SDR 06FDEA1727Strut · corrodedLT WING OUTBD FLAP INBD HINGE FITTING AFT STRUT NR 2 BOLT HOLE FOUND WITH CORROSION. REPAIR CARRIED OUT AT LT WING OUTBD FLAP INBD HINGE FITTING AFT STRUT NR 2 BOLT HOLE AS PER FEDEX EA NR 1-5750-97750, TITLE: "WINGS - OUTBOARD TRAILING EDGE FLAP, LT I/B SUPPSDR 06FDEA1726Strut · corrodedLT WING OUTBD FLAP INBD HINGE FITTING AFT STRUT NR 1 BOLT HOLE FOUND WITH CORROSION. REPAIR CARRIED OUT AT LT WING OUTBD FLAP INBD HINGE FITTING AFT STRUT NR 1 BOLT HOLE AS PER FEDEX EA NR 1-5750-97750, TITLE: "WINGS, OUTBOARD TRAILING EDGE FLAP, LT I/B SUPPOSDR AWXA200600991Skin · debondedMCN - MAJOR REPAIR - NR 5868398 - DURING C19 CHECK DISCOVERED DISBOND AREA AT OUTBOARD END OF THE RT INBOARD MID FLAP TRAILING EDGE WEDGE, LOWER SURFACE FROM WBL 162R TO WBL 175R. MAINTENANCE REMOVED DAMAGED AREA ON THE RT INBD MID FLAP T/E WEDGE IAW BOEING 7SDR SWAA061508Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING AFT FLAP PER MM.SDR 06FDEA1703Skin · corrodedLT WING, I/B MID FLAP UPPER SKIN IS CORRODED, 4 INCHES FROM T/E AND 12 INCHES AND 58 INCHES FROM I/B END. *S/D* REMOVED & REPLACED FLAP PER FED EX MM 27-51-013.SDR UIEA200600112Spar · corrodedCORROSION DAMAGE FOUND IN SUBJECT SPAR AFT FLANGE AT WBL 770. INTERIM REPAIR TO OUTBOARD TRAILING EDGE MIDFLAP, NR 3 SPAR LOWER CHORD ACCOMPLISHED AS PER BOEING MESSAGE 1-177581561 AND FAA FORM 8100-9. DETAIL VISUAL INSPECTION THE EXPOSED AFFECTED AREA, FOR SDR QXEA200601250Vane · chafedPDX - C3 CHAFING ON FLAP MOVABLE VANE LEADING EDGE BETWEEN THE TWO MIDDLE VANE ACTUATORS. REPAIRED IAW SRM 57-52-02, SRM 51-25-16, AND SRM 51-42-10.SDR 06FDEA1697Flap Track · damagedNR 6 FLAP TRACK AFT ATTACH FITTING DAMAGED OB BARREL NUT HOLE. REMOVED AND REPLACED NR 6 FLAP TRACK AFT O/B ATTACH FITTING PER SRM 51-30-02 AND SRM 51-20-01.SDR CA060509001Flap Track · cracked(CAN) LT IB FLAP TRACK, FWD ANGLES, AGAINST SPAR FOUND CRACKED AT BEND RADIUS, LOWER END. (TC NR 20060509001)SDR XN0A1325Tab · departedFIRST TRAILING EDGE FLAP OUTBOARD OF THE ALL-SPEED AILERONS ON LEFT WING MISSING ON POST FLIGHT. MAINTENANCE IN PROCESS. INSTALLED CENTER INBD TAB I/A/W A300 AMM CHAPTER 27-51-52, NO DEFECT NOTED.(STATUS:SUPP/CLOSED)SDR C1HA200685006Angle · crackedRT WING I/B MID FLAP HAS CRACK AT EDGE OF CUTOUT BELOW THE I/B MECHANISM. CUT OUT DAMAGED SECTION OF CHORD (70 INCHES) IN LENGTH, FABRICATED NEW SECTION P/N BAC 1503 100046 (70 INCHES) & SPLICE ANGLE 7075 T6 .050 IAW B727 SRM 57-50-2 FIG 5 & 51-40-4 FIG 1, TRSDR 06FDEA1669Support Fitting · corrodedLEFT WING O/B FLAP I/B HINGE SUPPORT FITTING (P/N ARC4009) O/B NR 3 BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED WITH A NEW FLAP AS PER AMM 27-50-30-4. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR SWIA200617000Roller · corrodedRT OTBD BUTTE DOOR ROLLERS ARE CORRODED AND WORN (5 EA), DISCOVERED DURING C-CHECK INSPECTION. REPLACED RT OTBD FLAP BUTTE DOOR ROLLERS (5 EA) PER CRJ200 AMM 20-24-00-910-801.SDR SWIA200616999Roller · corrodedLT OTBD FLAP HAS ALL FIVE BUTTE DOOR ROLLERS CORRODED AND WORN, DISCOVERED DURING C-CHECK INSPECTION. REPLACED 5 BUTTE DOOR ROLLERS ON LT OTBD FLAP PER CRJ200 AMM TASK 20-24-00-910-801.SDR ASAA0640532Skin · chafedLT WING OB MID FLAP LE SKIN IS CHAFED AT IB CORNER. BLENDED CHAFED AREA CHECKED OUT OF LIMITS. REPAIRED IAW SRM 57 53 01 FIG 201 REPAIR 8.SDR QXEA200601247Panel · chafedPDX - C3 FLAP PANEL 684 HT HAS CHAFING. REPAIRED IAW SRM 57-52-02, SRM 51-25-01, AND SRM 51-12-00.SDR QXEA200601246Panel · chafedPDX - C3 FLAP PANEL 684 EB HAS CHAFING. REPAIRED IAW SRM 57-52-02, SRM 51-25-01, AND SRM 51-12-00.SDR QXEA200601245Panel · chafedPDX - C3 FLAP PANEL 684JB HAS CHAFING. REPAIRED IAW SRM 57-52-02, SRM 51-25-01, AND SRM 51-12-00.SDR QXEA200601248Panel · chafedPDX - C3 FLAP PANEL 684 ET HAS CHAFING. REPAIRED IAW SRM 57-52-02, SRM 51-25-01, AND SRM 51-12-00.SDR QXEA200601249Skin · chafedPDX - C3 FLAP PANEL 684 LB HAS CHAFING. REPAIRED IAW SRM 57-52-02, SRM 51-25-01, AND SRM 51-12-00.SDR ASAA0640528Skin · chafedRT OB FORE FLAP CHAFED ON IB LE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57 53 01 FIG 201 REPAIR 1.SDR QXEA200601622Skin · chafedYYC - C3 LEFT WING, OUTBOARD FLAP, UPPER SURFACE CHAFED FROM YW191 TO YW281. REPAIRED IAW RD 8/4-57-649 AND EA 6-57-466.SDR UPS06146869Intercostal · crackedINSPECTION TYPE:5YR RIGHT T/E AT NR 4 MOVEABLE FLAP TRACK FAIRING I/B & O/B INTERCOSTALS CRACKED. REMOVED & REPLACED INTERCOSTALS PER A300 SRM 51-40-00 & 51-40-21.SDR 06FDEA1635Skin · corrodedRT WING I/B FLAP LOWER SURFACE FOUND SURFACE CORROSION. CLEANED AS PER AMM 12-26-02 AND TREATED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
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