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 FDEA201811203325Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSIONS. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. REPAIR BUSHING FABRICATED AS PER EA 1-5750-T0343705 P1 STEP 1A. TRACK SUSDR FDEA201811203324Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NO. 4 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSIONS. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343882 PART 1 STEP 1A. TSDR FDEA201811203323Support Fitting · corrodedLEFT WING OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSION. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343882 PART 1 STEP 1A. TRASDR A6WA2018112146168Skin · dentedL/H INBOARD FLAP HAS APPROX. 1" X 1" DENT BETWEEN W.S.47.61 AND W.S.56.30 (LOWER SIDE). REPAIRED L/H INBD FLAP LOWER SKIN IAW EA# AWAC-CRJ257-01096.SDR FDEA201811193298Bracket · corrodedRIGHT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSIONS. CORROSION AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM SDR FDEA201811193296Bracket · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR FDEA201811193295Bracket · corrodedRIGHT WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SDR SWAA2018112126999Flap · delaminatedRT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD CORNER. REPAIRED AFT FLAP PER SRM.SDR AALA2018112099001Wedge · delaminatedRIGHT WING OTBD TRAILING EDGE FLAP, TRAILING EDGE WEDGE NR 1 WAS DELAMINATED. THE AIRCRAFT WAS GROUNDED. REPLACED THE TE FLAP WEDGE IAW EA 287170.SDR SWAA2022022579634Flap · delaminatedSUPPLEMENTAL INFORMATION: RT WING O/B AFT FLAP LOWER IS DELAMINATED ON I/B LOWER CORNER / DELAMINATION ON I/B LOWER CORNER OF RT. WING O/B AFT FLAP WAS REPAIRED AT CSD ON WORK ORDER # 511517; FLAP WAS REMOVED FROM THE AIRCRAFT & WILL BE REINSTALLED ON NRC T865SDR SWAA2022022420452None · delaminatedL/H OUTBD AFT FLAP I/B CORNER IS DELAM. LOCATION - OB AFT FLAP IB AFT CORNER 1.375' X 1.00' UPPER SKIN. / APPLIED PERMANANT REPAIR TO L/H OUTBD AFT FLAP I/B CORNER UPPER SKIN I.A.W. B737-700 SRM'S 57-53-01-2R-4 REV 69 & 51-70-10-2R-0 REV 69 & 57-53-01-01-4 REVSDR SWAA2018113027247Skin · delaminatedRT WING INBOARD AFT FLAP DELAMINATED ON LOWER SURFACE. R&R AFT FLAP IAW AMM.SDR FDEA201811163255Bracket · corrodedLEFT WING INBOARD FLAP DRIVE LINK IDLER BRACKET BORE FOUND CORROSION. IDLER BRACKET BORE REWORKED AS PER CMM 57-52-03 AND LOCAL BLEND AT 9' CLOCK POSITION INSIDE THE BORE HOLE FOUND EXCEED LIMIT AS PER BLUEPRINT LIMIT IN ACCORDANCE WITH EA 1-5750-T0343644 P1 FSDR FDEA201811163236Hinge Fitting · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSIONS AT RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03.SDR FDEA201811163235Hinge Fitting · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSIONS AT RIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE (HOLE A ND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. SDR FDEA201811163234Hinge Fitting · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE ( FLAP SIDE ) OUTBOARD PIVOT LUG HOLE BORE ( HOLE B AND A ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CSDR FDEA201811163233Hinge Fitting · corrodedLEFT HAND INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE ( FLAP SIDE ) INBOARD PIVOT LUG HOLE BORE ( HOLE G AND F ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR FDEA201811163228Hinge Fitting · corrodedRIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION CORROSION AT RIGHT INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE B AND A) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. OVSDR FDEA201811163227Hinge Fitting · corrodedRIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION CORROSION AT RIGHT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03.SDR FDEA201811163226Hinge Fitting · corrodedLEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE COROSION CORROSION AT LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT OUTBOARD HOLE BORE (HOLE B AND A) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. SDR FDEA201811163225Hinge Fitting · corrodedLEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION CORROSION AT LEFT HAND INBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE (HOLE G AND F) REOWRKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. SDR A6WA2018111246176Skin · dentedLH INBD FLAP LOWER SKIN PANEL DENTED AND DINGED WITH HEAVY PITTING. REPLACED REPLACED LH INBD FLAP LOWER SKIN PANEL IAW CRJ 200 SRM 57-42-13SDR FOTR20181115010Flap · corrodedRT O/B MAIN FLAP HAS INTERNAL CORROSION AROUND FASTENERS HOLE APPROX WBL 493.SDR Q2SA20181114409Skin · chafedAIRCRAFT GROUNDED. LT WING OUTBD MID FLAP LOWER SKIN IS CHAFED NEAR INBD FLAP TRACK CUTOUT. REPLACED LT OUTBD MID FLAP. INSTALL AND ADJUSTMENTS TO BE ACCOMPLISHED ON CARD 8017551.SDR Q2SA20181114407Flap · dentedAIRCRAFT GROUNDED. RT INBD MID FLAP DENTED, 18Ï¿½ IN FROM EXHAUST GATE AND 5 Ï¿½ INCHES FROM THE T/E. OK TO INSTALL. REPAIRED R/H INBD MID FLAP IAW SRM 51-70-102R-2. SEE ATTACHED SHOP FOR WORK ACCOMPLISHED.SDR Q2SA201902275043Skin · chafedLH WING OB MID FLAP LOWER SKIN IS CHAFFED NEAR IB FLAP TRACK CUTOUT. FLAP REPLACED WITH P/N 65C26320-17, S/N 1953.SDR Q2SA201022796074Skin · dentedRH INBD MID FLAP DENTED, 18.0" FROM EXHAUST GATE AND 5.5" FROM TE.SDR SWAA2018111926877Flap · delaminatedLT WING INBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.SDR FDEA201811143204Hinge Bracket · corrodedRIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11 CSDR FDEA201811143203Hinge Bracket · corrodedRIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD- 11 CMSDR FDEA201811143202Hinge Bracket · corrodedRIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE SURFACE CORROSION. CORROSION AT RIGHT OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM SDR FDEA201811143200Hinge Bracket · corrodedRIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE BORE (#3 BORE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11SDR FDEA201811143199Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11SDR Q2SA201902286073Skin · dentedRH IB AFT FLAP DENTED 10.0" IN FROM EXHAUST GATE 1.5" FROM TE.SDR SWAA2018121027435Fairing · looseRT WING NR 7 FLAP TRACK FAIRING LOOSE AT FORWARD AND AFT ATTACH POINTS. R&R FAIRING IAW CMM.SDR SWAA2018121027434Fairing · looseLT WING NR 3 FLAP TRACK FAIRING LOOSE AT FORWARD AND AFT ATTACH POINTS. R&R FAIRING IAW CMM.SDR FDEA201811133195Stop Fitting · crackedLEFT HAND WING OUTBOARD FLAP STOP FITTING CRACKED. STOP FITTING ON LEFT HAND WING OUTBOARD FLAP AT STATION XOVH 537 REMOVED AND REPLACED AS PER MD11 SRM 51-33-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FXTA2018F00146Attach Bracket · elongatedUPPER AFT INBOARD FLAP BELLCRANK ATTACH BRACKET IS ELONGATED WHERE THE FLAP BELLCRANK ATTACHES ON BOTH RIGHT AND LEFT SIDE.SDR DALA2018112406755Cover · missingDURING INSPECTION FOUND RIGHT WING FLAP TRACK FAIRING NR 5 COVER MISSING. DEFERRED PER CDL 57-00-07 UNTIL COVER IS REPLACED.SDR FDEA201811113177Fitting · corrodedRIGHT HAND WING, RIGHT HAND OUTBOARD FLAP VANE HORN FITTING "D" FOUND HOLE BORE CORROSION. FITTING "D" HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. SLOT OVERSIZED BUSHING FABRICATED PER EA 1-5750-T0343466 P1 STEP 1A AND INSTALLESDR FDEA201811113176Fitting · corrodedRIGHT HAND WING, RIGHT HAND OUTBOARD FLAP VANE HORN FITTING "F" FOUND HOLE BORE CORROSION. FLAP VANE FITTING "F" HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. SLOT OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343466 P1 STEP 1ASDR FDEA201811113175Fitting · corrodedRIGHT HAND WING, RIGHT HAND OUTBOARD FLAP VANE HORN FITTING "E" FOUND HOLE BORE CORROSION. FLAP VANE FITTING "E" HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. SLOT OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343466 P1 STEP 1ASDR FDEA201811113174Fitting · corrodedRIGHT HAND WING, RIGHT HAND OUTBOARD FLAP VANE HORN FITTING "B" FOUND HOLE BORE CORROSION. FLAP VANE FITTING "B" HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. SLOT OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343466 P1 STEP 1ASDR AALA201812179015Doubler · debondedAIRCRAFT WAS IN BASE MAINTENANCE. DEBONDED LEFT HAND OUTBOARD FLAP. REPAIRED OUTBOARD FLAP DOUBLER REPAIR AT LEVEL RIB 12 ON LEFT HAND WING PER EA 287401.SDR AALA201812179014Doubler · debondedAIRCRAFT WAS IN BASE MAINTENANCE. DEBONDED LEFT HAND OUTBOARD FLAP. REPAIRED OUTBOARD FLAP DOUBLER REPAIR AT LEVEL RIB 9 ON LT WING PER EA 287401.SDR SWIA2018121245362Vane · chafedREPLACE LH INBOARD FLAP VANE L/E SKIN, CENTER LOCATION DUE TO OUT OF LIMITS CHAFE DAMAGE. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED LH INBOARD FLAP VANE L/E SKIN, CENTER LOCATION IAW SRM.SDR SWIA2018121245361Vane · chafedREPLACE LH INBOARD FLAP VANE L/E SKIN, OUTBOARD LOCATION DUE TO OUT OF LIMITS CHAFE DAMAGE. (C-CHECK) RO: 12/11/2018 REMOVED AND REPLACED LH INBOARD FLAP VANE L/E SKIN, OUTBOARD LOCATION IAW SRM.SDR SWAA2018121427676Skin · delaminatedLT WING OUTBOARD AFT FLAP DELAMINATED ON TOP SIDE AT INBOARD END. REPAIRED AFT FLAP IAW SRM.SDR FDEA201811093163Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD AFT (FLAP SIDE) HINGE PIVOT INBOARD BORE HOLE CORROSION. HINGE PIVOT INBOARD HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-04 AND EA 1-5750-1309745 B P2 SDR SWAA2018111926821Skin · crackedRT WING INBOARD AFT FLAP CRACKED ON LOWER SURFACE. REPAIRED AFT FLAP IAW SRM.
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