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 UPS04242854Skin · delaminatedINSPECTION TYPE: C, RIGHT WING O/B AFT FLAP HONEYCOMB FILLER DELAMINATED AT I/B END. AFT FLAP FITTINGS REMOVED FROM UNSERVICEABLE FLAP AND FITTED TO REPLACEMENT AFT FLAP IAW OHM 20-50-01 AND OHM 57-52-11. FLAP ASSY REPLACED IAW MM 27-51-12 AFT FLAP ADJUSTED SDR DHL2004745516Skin · delaminatedDURING A C-CHECK, LEFT I/B FORE FLAP LOWER SURF AT L/E WBL 124 HAS SKIN DELAMINATED. REMOVED LEFT I/B FORE FLAP IAW 727 MM 27-51-01, CUT OUT LWR SKIN 5.5 X 4.5 INCHES, FABBED FILLER 6.5 X 4.5 INCHES AND DOUBLER 9.5 X 6 INCHES FROM 2024-T3 .016 PO 900573 IAW 7SDR 04FDEA01938Hinge · corrodedCOMPLY WITH EA 8-5750-79542, WINGS RIGHT INBOARD FLAP - FLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/N ARC2512. COMPLIED WITH EA 8-5750-79542.SDR SWAA041890Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T/E FLAP PER MM.SDR 04FDEA01918Vane · damagedLEFT HAND INBOARD FLAP VANE, LOWER SKIN DAMAGED AT OUTBOARD STOP. REMOVED AND INSTALLED OVERHAULED VANE AT LEFT HAND INBOARD FLAP IAW FEDEX WORKCARD E-8-5750-7-5002 C PT3.SDR 04FDEA01922Rib · crackedRIGHT HAND INBOARD FLAP, INBOARD TRACK UPPER FAIRING, FORWARD RIB CRACKED. REMOVED CRACKED RIB IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW RIB IAW DAC DWG ARC 2340. INSTALLED RIB IAW DC10 SRM 51-35-01 VOL 2 AND DC10 SRM 51-35-02 VOL 2.SDR 04FDEA01923Skin · crackedRIGHT HAND INBOARD FLAP, INBOARD, AFT HOIST POINT, SKIN CRACKED/DAMAGED. REMOVED TRAILING EDGE WEDGE, FABRICATED REPAIR DOUBLER IAW DC10 SRM 51-21-01 VOLUME 2. REINSTALLED TRAILING EDGE WEDGE IAW DC10 SRM 51-31-01 VOLUME 1.SDR 04FDEA01928Angle · crackedLEFT HAND OUTBOARD FLAP, OUTBOARD SUPPORT FITTING, FAIRING ATTACH STRUCTURE LOWER, INBOARD L-ANGLE BRACKET IS CRACKED. REMOVED L-ANGLE BRACKET IAW DC10 SRM 51-35-01 VOL 2, 51-33-01 VOL 2. FABRICATED ANGLE AND INSTALLED NEW ANGLE IAW DC10 SRM 51-35-01 VOL 2 ASDR 04FDEA01917Vane · delaminatedRIGHT HAND INBOARD FLAP VANE, UPPER SKIN HAS MULTIPLE AREA OF DENTS AND DELAMINATION. REMOVED AND REPLACED WITH OVERHAULED VANE RIGHT HAND INBOARD FLAP VANE IAW FEDEX WORKCARD E-8- 5750-7-5002 C PT4.SDR IXXA060443SFitting · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING FLAP HINGE FITTINGS CORRODED AT STATIONS XW219 AND XW97. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060441SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP TRAILING EDGE SKIN CRACKED AT STATION XF300. REPAIRED PER ALL APPLICABLE DATA.SDR UPS04242852Skin · crackedINSPECTION TYPE: C, CRACK ON I/B MID FLAP LOWER T/E SKIN AT I/B AFT FLAP ACTUATING ROD CUTOUT O/B AFT CORNER (LT). HFEC CONFIRMED CRACK AND MARKED END. DAMAGED AREA TRIMMED OUT IAW SRM 51-10-1. REPAIR CARRIED OUT IAW AAAE EO 2004-068-006.SDR USAA040385Skin · delaminatedPIT - FOUND FLAP T/E SECTION HAS 2 INCH AREA DELAMINATION, 25 INCHES FROM INBOARD EDGE, 3 INCHES FROM L/E. REMOVED AND REPLACED DAMAGED/DISBONDED AREA AND INSTLALED REPAIR DOUBLER PER BOEING SRM 51-70-10. (M)SDR 04FDEA01902Support Fitting · corrodedRT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE FOUND CORRODED. RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE AT ATTACHMENT AREA, FORWARD MOUNT FITTING, OUTBOARD AFT HOLE REPAIRED PER FEDEX EA NR 1-5750-7675SDR 04FDEA01903Fitting · corrodedRT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING, THREE (3) HOLES FOUND CORRODED. RT OUTBOARD FLAP, INBOARD FLAP SIDE HINGE ATTACHMENT AREA, FORWARD MOUNT FITTING CORROSION REMOVED AS PER SRM 51-21-00 VOLUME II. (1) OUTBOARD MSDR 04FDEA01901Hinge · corrodedDURING P TO F MODIFICATION AND TRANSATION CHECK FOUND LEFT OUTBOARD FLAP HINGE FWD SECTION STA XW 486 WITH OXIDATION WHERE CONTACT STUD BOLTS. REMOVED CORROSION AT BARREL NUT CORRESPONDING SIDE LOAD FITTING BOLT HOLE IAW CMM 57-44-08, INSTALLED BUSHING IAW CSDR SWAA041860Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT INBOARD AFT FLAP PER MM.SDR DL767040614Structure · corrodedWHILE ACCOMPLISHING THE I/B TRAILING EDGE MAIN FLAP ATTACH BOLT REPLACEMENT PER EA 01-085672-12AD, CORROSION WAS FOUND IN THE BORES OF THE FWD TWO AND AFT ATTACH FOUR HOLES OF THE 9-10 BEAM AND THE ASSOCIATED MATING HOLES ON THE FLAP AND THE FOUR HOLES COMMON SDR 04FDEA01908Hinge · corrodedRIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.443, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - SDR 04FDEA01907Hinge · corrodedRIGHT OUTBOARD FLAP OUTBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.458, FINAL DIAMETER = 0.517. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS SDR 04FDEA01906Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING OUTBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.521, FINAL DIAMETER = 0.620. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RSDR 04FDEA01905Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD AFT HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.628. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS - RSDR 04FDEA01904Hinge · corrodedRIGHT OUTBOARD FLAP INBOARD FLAP SIDE HINGE ATTACHMENT AREA FORWARD MOUNT FITTING INBOARD MIDDLE HOLE FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. ORIGINAL DIAMETER = 0.568, FINAL DIAMETER = 0.656. COMPLIED WITH FEDEX EA 1-5750-76755, WINGS -SDR DHL2004745558Skin · debondedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT IB MID FLAP TE TOP SKIN DEBONDED AREA WBL 203. CUT OUT DAMAGED AREA OF L/W IB MID FLAP UPPER SKIN APPROX 4.2500 INCHES X 5.7500 INCHES IAW SRM 51-40 -20 FIG 30 FABRICATED ONE FILLER APPROX 4.2500 ISDR DHL2004745554Skin · debondedDURING A C-CHECK, RT INBOARD MID FLAP T/E UPPER SKIN SHOW DISBONDED AREAS WBL 160 TO OUTBOARD. CUT OUT DELAMINATED ARE OF RW I/B MIDFLAP T/E UPPER SKIN APPROX 6.5 X 4.25 INCHES & 2 EA DOUBLERS APPROX 3 X 4.5 INCHES FROM 2024-T3 .016 PO 900962 IAW B727 SRM 57SDR 04FDEA01885Hinge · corrodedDURING PAX TO FREIGHTER MODIFICATION AND TRANSITION CHECK, FOUND LT OUTBOARD FLAP FWD HINGE SECTION STA XW 486 WITH CORROSION AT THE FACE OF BORE FOR BEARING. CORROSION REWORK FWD INNER HINGE NR 4 LUG FACE IAW CMM 57-44-08 IN LIMIT REF FIG 401 SH 1 CMM 57-44-SDR 04FDEA01884Hinge · corrodedN-12476 DURING PASSENGER TO FREIGHTER MODIFICATION AND TRANSITION CHECK LT OUTBOARD FLAP, FWD HINGE SECTION STA XW 486 WITH CORROSION IN THE BORES OF BUSHINGS ACTUATOR ATTACH POINTS. REMOVED CORROSION AND CHECK LIMITS IAW CMM 57-44-08 AND INSTALLED BUSHING SDR 04FDEA01896Wedge · dentedRIGHT HAND OUTBOARD FLAP HAS DENT OUT OF LIMITS AT STATION 478 INBOARD END. REMOVE WEDGE IAW DC10 SRM 51-40-2 VOL 2. REMOVE WEDGE SKIN IAW DC10 SRM 51-40-2 VOL 2, FABRICATED NEW SKIN IAW FED-EX EA 8-57-50-77573 AND DC10 DAC DWG ARC 1949. INSTALLED NEW SKIN SDR 04FDEA01895Wedge · dentedRT OUTBOARD FLAP NR 2 TRAILING EDGE WEDGE STATION 556 HAS DENT OUT OF LIMITS. FABRICATED SKIN ASSEMBLY IAW DAC DWG ARC 1953 AND INSTALLED SKIN ASSEMBLY IAW DC10 SRM 57-21-01 VOL 2 AND DC10 SRM 51-40-01 VOL 2.SDR 04FDEA01894Bracket · brokenRIGHT HAND OUTBOARD FLAP INBOARD HINGE HAS A BROKEN BRACKET PART NUMBER ARC 2149-25. DISASSEMBLED HINGE PANEL STRUCTURE IAW DC10 SRM 51-35-01 VOL 2. REMOVED BROKEN BRACKET IAW DC10 SRM 51-35-01 VOL 2. FABRICATED NEW BRACKET IAW DAC DWG ARC 2149. INSTALLED SDR R2J2004F00000Brace · mismanufacturedWHILE REINSTALLING LT WING FLAP CABLES DURING PHASE 5 INSPECTION, NOTICED CABLE RUN TOO CLOSE TO STRUCTURE. INVESTIGATION AND NOTIFIED MFG TECH SUPPORT. IT WAS DETERMINED LT BRACE 5511037-3 AND RIB 5525130, CABLE PASS THRU WERE INCORRECTLY LOCATED DURING MANSDR 04FDEA01878Vane · corrodedCOMPLY WITH EA 8-5750-78235 WINGS OUTBOARD FLAP ARC 1537 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-78235 WINGS O/B FLAP ARC1537 FLAP VANE SUPPORT CORROSION REWORK AT MAE.SDR 04FDEA01868Stop Fitting · crackedLEFT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. LEFT HAND WING - OUTBOARD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30 AND ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00, FOUND SATISFACTORY.SDR 04FDEA01867Stop Fitting · crackedRIGHT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. RIGHT HAND WING - OUTBOARD FLAP CRACKED STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL I.SDR 04FDEA01872Strap · corrodedRIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, OUTBOARD STRAP BORE HOLE AT PIVOT POINT BADLY CORRODED. RIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, OUTBOARD STRAP P/N ARC2518U502, REMOVED AND NEW STRAP REPLACED AS PER DRAWING ARC2512 AND SSDR AT0700072Skin · damagedLEFT FLAP DAMAGE DUE TO FOD. INSTALLED TWO DOUBLER REPAIR AT LEFT INBOARD AREA IAW AIRTRAN RES 06-05-19. MATERIAL USED 0.063 7075T6. SIZE 7" X 7.5" AND 6" X 8".SDR IXXA060131SAngle · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD FLAP OUTBOARD ANGLE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED NEW ANGLE, AND FASTENERS AT RIGHT WING INSDR SWAA041791Skin · delaminatedDURING SCHEDULED PM CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD AFT FLAP PER MM.SDR 04FDEA01850Fitting · wornRIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING MID AND AFT HOLES FOUND WORN. RIGHT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING REMOVED & REPLACED AS PER EO 1-5750-7-5005 PT2 TITLE : WINGS - TRAILING EDGE DEVICES - INSPECT/MODIFY I/B FLAP VASDR 04FDEA01849Tee Fitting · corrodedLEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING AFT HOLE FOUND WORN. LEFT HAND WING - INBOARD FLAP VANE, OUTBOARD TEE FITTING AFT HOLE REAMED AS PER SRM 51-31-01 VOL 2, ORIGINAL DIAMETER=0.875 INCH, FINAL DIAMETER=0.895 INCH, REPAIR CARRIED OUT AS PESDR 2004UALA00612Skin · chafedRT WING, INBOARD FLAP, UPPER SKIN CHAFED ON OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. REPAIRED WITH .032 INCH BONDED DOUBLER.SDR 04FDEA01848Vane · corrodedLEFT HAND WING OUTBOARD FLAP VANE NR 3 TEE FITTING FORWARD AND AFT BOLT HOLES CORRODED.SDR UPS04242669Angle · crackedINSPECTION TYPE: C, ANGLE CRACKED AT RT ELEPHANTS EAR. FABRICATED ANGLE IAW SRM 51-30-2, INSTALLED NEW ANGLE IAW SRM 51-20-01 FIG 7 AND BOEING DRG 65-26786.SDR AALA20040695Flap Track · corrodedTUL - NUMBER ONE LEFT HAND FLAP TRACK HAS LIGHT CORROSION INSIDE RADIUS AFT END OF NUMBER ONE FLAP TRACK ATTACH POINT BARREL NUT. CORRODED AREA IS ONE INCH BY ONE INCH. REPAIRED PER ESO 30595 REPAIR NUMBER 40 572000 3473 DATED JUNE 22, 2004.SDR AALA20040694Flap Track · gougedTUL - FLAP TRACK NUMBER ONE LIFT GOUGED INSIDE AFT ATTACH POINT BARREL NUT HOLE. AREA OF DISCREPANCY IS ONE INCH BY ONE INCH AND LOCATED AT STATION 3300. REPAIRED PER ESO 30595 REPAIR NUMBER 40 572000 3473 DATED JUNE 22, 2004.SDR QXEA200400466Flap Track · corrodedPDX - LEFT HAND NR 5 FLAP TRACK INBOARD LOWER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-989.SDR QXEA200400465Flap Track · corrodedPDX - LEFT HAND NR 4 FLAP TRACK OUTBOARD UPPER FLANGE HAS PITTING CORROSION. REPAIRED IAW RD 8-57-988.SDR QXEA200400464Flap Track · corrodedPDX - NR 4 FLAP TRACK HAS PITTING CORROSION ON LOWER OUTBOARD TRACK UPPER SURFACE. REPAIRED IAW RD 8-57-988.SDR P5CA0401125Angle · crackedLT WING IB MID FLAP IB FORE FLAP TRACK WBL535 CUT OUT IS CRACKED AT IB LEADING EDGE RIB. REMOVED CRACKED ANGLE IAW SRM 51-30-02, FABRICATED REPAIRED DOUBLER IAW SRM 51-40-02, FIG 2 TREATED AND PAINTED INST DOUBLER IAW SRM 51-30-02, INST ANGLE IAW SRM 51-30-02SDR UPS04242704Flap Track · corrodedINSPECTION TYPE:C, NR 4 FLAP TRACK, AFT PAD-B HAS CORROSION IN BORE HOLES F & G. REPAIR CARRIED OUT IAW AAAE EO 2004-061-003.
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