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 SWIA2018080244947Skin · dentedRIGHT WING INBOARD FLAP, DENT ON LOWER SKIN NEAR TRAILING EDGE APPROXIMATE WS72.00. (C-CHECK) RO: 08/01/2018 REPAIRED THE RIGHT HAND INBOARD FLAP LOWER SKIN AT WS 72.00 IAW SRM.SDR SWIA2018080244949Vane · chafedRT SIDE INBOARD FLAP( VANE) HAS CHAFING WEAR AT INBOARD, CENTER, AND OUTBOARD LEADING EDGE SECTION OF FLAP VANE. (C-CHECK) RO: 08/01/2018 REMOVED DAMAGE FROM INBD FLAP VANE CAPS IAW REO.SDR A6WA2018071845936Skin · damagedLEFT I/B FLAP LOWER SKIN HAS LARGE AREA OF DINGS AND PITS. REPLACED LEFT I/B FLAP I/B LOWER SKIN IAW SRM 51-25-16.SDR SWAA2018070223175Flap · delaminatedRT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD TRAILING EDGE. R&R AFT FLAP PER AMM.SDR KCSA201806231153Wedge · delaminatedLT I/B AFT FLAP HAS A DELAM ON THE T/E WEDGE ON I/B END 18" O/B FROM I/B END.SDR SWIA2018073144929Vane · chafedLT INBOARD FLAP - FLAP VANE CHAFED AT 2 LOCATIONS ON TOP TRAILING EDGE (CHAFES LOCATED AT 49" AND 54" FROM INBOARD SIDE OF VANE). (C-CHECK) RO: 07/28/2018 BLENDED OUT DAMAGE IAW REO AND SRM.SDR DALA2018062304165Support Fitting · crackedRT WW TRAPEZOIDAL AND FLAP ACTUATOR SUPPORT FITTING MID-SECTION CRACKED. REMOVED AND REPLACED RT MLG W/W FLAP ACTUATOR SUPPORT FITTING IAW DRAWING 9910155 REV ED, REV DY, 5936030 REV AV, AND SRM 51-30-5. CRACK DIM 2.0".SDR SWAA2022021524218Flap · delaminatedLH OTBD AFT FLAP UPPER SURFACE DELAMINATED ON INBD AFT CORNER. / APPLIED BONDED DOUBLER AND CURED PER SRM 51-70-10-2R-4.SDR SWAA2018062522967Skin · delaminatedRT WING INBOARD AFT FLAP DELAMINATED ON LOWER SURFACE. R&R AFT FLAP PER AMM.SDR SWAA2022021546907Flap · delaminatedRH O/B AFT FLAP I/B CORNER IS DELAMINATED FROM I/B EDGE TO 9' O/B OF I/B EDGE AND FROM T/E TO 101/2' FWD OT T/E / ACCOMPLISHED TIME LIMETED REPAIR PER REPAIR-57EA-05340; WILL BE TRACKED PER INSP-57EA-05341 FINAL REPAIR TO BE ACCOMPLISHED PER EA REPAIR-57EA-053SDR DALA2018062004116Skin · dentedLT WING NR 1 FLAP VANE LWR SURFACE HAS DENTS. ACCOMPLISHED PERMANENT REPAIR ON LT WING NR 1 FLAP VANE LWR SURFACE IAW SRM 57-03 AND SRM 51-70-2 PAR 18 B.SDR SWAA2018062022916Flap · delaminatedRT WING OUTBOARD AFT FLAP INBOARD CORNER DELAMINATED. REPAIRED AFT FLAP PER ER.SDR O2GA2018070986701Fastener · not reportedPREFLIGHT HEARD LOUD GRINDING SOUND COMING FROM LEFT FLAP. MAINTENANCE REPLACED FLAP HARDWARE. OPERATION CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE.SDR FDEA201806181537Flap Track · looseRT WING, NR 7 AND NR 8 FLAP TRACKS LOOSE AT AFT ATTACH POINT TO REAR SPAR. REPLACED NR 7 AND NR 8 FLAP TRACK ATTACHING HARDWARE (WITH FLAP TRACKS REMOVED) IAW AMM 27-51-15 SEE SNRM N00558 FOR DETAILED WORK STEPS.SDR FDEA201806181536Flap Track · looseLT WING, NR 1 AND NR 2 FLAP TRACKS LOOSE AT AFT ATTACH POINT TO REAR SPAR. REPLACED NR 1 AND NR 2 FLAP TRACK ATTACHING HARDWARE (WITH FLAP TRACKS REMOVED) IAW AMM 27-51-15 SEE SNRM N00557 FOR DETAILED WORK STEPS.SDR SWIA2018070944874Vane · chafedRT INBOARD FLAP VANE MIDDLE LEADING EDGE PANEL HAS CHAFE DAMAGE. (C-CHECK) 07/08/2018 REPAIRED RT INBOARD FLAP VANE, MIDDLE LEADING EDGE CAP IAW REO.SDR SWIA2018070944873Vane · chafedLT INBOARD FLAP VANE MIDDLE LEADING EDGE PANEL HAS CHAFE DAMAGE. (C-CHECK) 07/08/2018 REPAIRED LT INBOARD FLAP VANE, MIDDLE LEADING EDGE IAW REO.SDR DALA2018061804040Flap · damagedRT FLAP TRAILING EDGE DAMAGED. REMOVED AND REPLACED RT IB TRAILING EDGE FLAP PER W/C 2751-5324.SDR SRXR201806160055Angle · gougedRT WING OTBD FLAP INBD HINGE FAIRING ANGLE IS GOUGED. REMOVED, FABRICATED AND INSTALLED RT WING OTBD FLAP INBD HINGE FAIRING ANGLE PER EA 011-5750-52-A7298 I/R REF NRC A041748.SDR REXA2018070300571Skin · chafedRT INBD FLAP VANE LE SKIN CHAFED AT OTBD BUMP STOP CONTACT POINT. BLENDED CHAFE FOUND TO BE OUT OF LIMITS, REMOVED & REPLACED LE IAW REO601R-57-52-004 & SRM 51-40-11 PG 1413, 51-42-10 PG 10&15.SDR SWAA2018061822811Doubler · missingRT WING OUTBOARD TRAILING EDGE FLAP INBOARD LOWER SKIN REPAIR DOUBLER MISSING. R&R AFT FLAP IAW AMM.SDR AALA201806159001Skin · damagedTHREE AREAS OF CONDENSATION ON THE RT OUTBOARD TRAILING EDGE FLAP. ALL THREE LOCATIONS ARE 6.5 INCHES FWD OF THE TRAILING EDGE OF THE FLAP. THE DIMENSIONS FROM INBOARD TO OUTBOARD ARE AS FOLLOWS: 3.0 INCHES BY 4 INCHES AT WBL 539.5, 2.0 INCHES BY 2.0 INCHESSDR DALA2018061504022Skin · gougedLT WING OB TE FLAP HAS GOUGE IN UPPER SURFACE APPROX 43 IN FROM IB EDGE. REPAIRED PER PRI 569265-14 REV 0 AND 1. COMPLIED WITH ER/A 569265-14 REV ORIGINAL.SDR FDEA201806141489Hinge Fitting · worn3EA WEAR GOUGES ON INBOARD FLAP O/B HINGE WING ATTACHED HINGE. PERFORMED REPAIR FOR WEAR DAMAGE TO HINGE FITTING IAW SRM 57-20-00 FIG 17 V1.SDR FDEA201806141488Skin · damagedRT IN/BD MAIN FLAP, PUNCTURE ON THE LOWER SURFACE OF TRAILING EDGE PANEL REPAIRED PUNCTURE ON THE LOWER SURFACE OF THE R/H IN/B MAIN FLAP 80" FROM IN/B EDGE AND 7" FROM AFT EDGE IAW EA F-5750-T0340210 P1.SDR SWAA2018071823501Skin · delaminatedRT WING OUTBD AFT FLAP DELAMINATED ON UPPER SUFACE. R&R FLAP PER MM.SDR AALA2018071319017Pivot · corrodedCORROSION FOUND ON THE PIVOT BOLT, TRACK 3 RT, BETWEEN WS 6699 AND 7316, RIBS 12 AND 13. REPLACED THE PIVOT BOLT TRACK IAW AMM 27-54-62.SDR AALA201807119005Bolt · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON PIVOT BOLT FLAP TRACK 2, STA 3059 OF RIGHT HAND WING. REPLACED BOLT PER AMM 27-54-61.SDR AALA201807119018Bolt · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON OUTBOARD FLAP PIVOT BOLT THAT ATTACHES AT CARRIAGE OF TRACK 4 ON RIGHT HAND WING. REPLACED NR 4 PIVOT BOLT TRACK PER AMM 27-54-62.SDR A6WA2018061845885Rib · gougedLEFT INBD FLAP, INBD CLOSEOUT RIB WAS GOUGED ON THE FWD END. REPLACED THE RIB IAW SRM 51-42-22, AND 51-42-15.SDR J7SA20180612001Bracket · brokenLT AND RT IB FLAP ROLLER BRACKET TABS BROKEN. R&R FLAP TRACK ROLLER BEARING BRACKET.SDR JGVR201806132003Fitting · corrodedMECHANICALLY BLENDED FOUR AREAS OF CORROSION ON THE LT WING OTBD FLAP PUSHROD ATTACH FITTINGS, PERFORMED AN EDDY CURRENT INSPECTION AND AN ULTRASONIC THICKNESS INSPECTION. FOUND INBOARD FITTING BEYOND LIMITS. PROTECTED BARE METAL IAW SRM 51-10-02 TO AREAS WITSDR ABXA2018062011060Tee Fitting · corrodedCORROSION ON THE LEFT WING TRAILING EDGE PANEL SUPPORT BEAM TEE ABOVE THE MAIN LANDING GEAR. THE TEE WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR IPXA2018061430668Flap · crackedINSPECTION TYPE:2C, RT IB FLAP T/E SPLIT AT STA XIFH183. REPAIRED FLAP T/E PER SRM 57-50-02 REPAIR 2 AND SRM 51-62-01. (MINOR)SDR IPXA2018061430669Flap · crackedINSPECTION TYPE:2C, LT IB FLAP T/E SPLIT AT STA XIFH 233. REPAIRED FLAP T/E PER SRM 57-50-02 REPAIR 2 AND 51-62-01. (MINOR)SDR SWIA2018073144924Vane · chafedRIGHT WING INBOARD FLAP VANE LEADING EDGE CHAFED INBOARD OF THE INBOARD SLIDING VANE ACTUATOR ATTACHMENT. (C-CHECK) RO: 07/28/2018. REPLACED RT INBD FLAP VANE CAP IAW SRM.SDR SWIA2018073144923Vane · chafedLEFT WING INBOARD FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE OUTBOARD SLIDING VANE ACTUATOR ATTACHMENT. (C-CHECK) RO: 07/28/2018 REMOVED CHAFE DAMAGE IAW REO AND SRM.SDR SWIA2018073144922Vane · chafedLEFT WING INBOARD FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE MIDDLE SLIDING VANE ACTUATOR ATTACHMENT. (C-CHECK) RO: 07/28/2018 REMOVED CHAFE DAMAGE IAW REO AND SRM.SDR CALA2018062101446Lock Bolt · shearedTHE TRAILING EDGE FLAP TRACK BALLSCREW GIMBALS, LOWER BUSHING RETAINING LOCK BOLTS WERE FOUND SHEARED OFF AND/OR BOLT COLLARS MISSING ON THE RT WING NR 5 & 6 T/E FLAP TRACK LOCATIONS.SDR FDEA2018061201436Skin · delaminatedRIGHT OUTBOARD MAIN FLAP HAD DELAMINATION ON THE UPPER T/E PANEL AREA. REPAIRED IAW SRM 57-53-02, DETAIL VII, SRM 57-53-01-2R, DETAIL III, TABLE III, AND SRM 51-70-07-0G, FIGURE 2, REV 124. ACCOMPLISHED EA F-5750-T0340213.SDR SWAA2022021753977Flap · delaminatedDELAMINATION FOUND ON RIGHT OUTBOARD AFT FLAP LOCATED ALONG TRAILING EDGE. DAMAGE MEASURES 1.625' LONG BY .5' WIDE AND STARTS AT THE INBOARD AFT EDGE. MOD / REPAIRED DAMAGE AREA AT R/W O/B AFT FLAP I/B AREA AS PER BOEING 737 SRM 51-70-10-2R-0 REPAIR1.MATERIAL SDR AALA2018060869031Wedge · delaminatedRIGHT WING OUTBOARD TRAILING EDGE FLAP WEDGE DELAMINATED. REPLACED THE FLAP WEDGE. AIRCRAFT WAS GROUNDED.SDR IPXA2018061230547Repair · debondedINSPECTION TYPE:C10, DISBOND ON EXISTING REPAIR OF LT WING INBD AFT FLAP UPPER SKIN AT IFS 240.5. REPAIR IAW SRID:3-4228853096 AND EO B767-5750-68832-A.SDR FDEA201806051393Skin · debondedRT INBD FWD FLAP UPPER SURFACE HAS A DISBONDED COMPOSITE REPAIR. REPAIRED RT INBD FWD FLAP UPPER SURFACE IAW SRM 51-71-10-2R REPAIR 4 & 57-53-01-2R FIG 201 DET I.SDR SWAA2022021700357Skin · delaminatedR/H O/B AFT FLAP SHOWS DELAM AT I/B LOWER CORNER. / REPAIRED DAMAGE PER SRM 57-53-01-2R-4.SDR J7SA20180604002Fitting · brokenLT AND RT IB FLAP ROLLER BRACKET TABS BROKEN. R&R FLAP TRACK ROLLER FITTINGS.SDR J7SA20180604001Fitting · brokenLT AND RT IB FLAP ROLLER BRACKET TABS BROKEN. R&R FLAP TRACK ROLLER FITTINGS.SDR J7SA20180602001Fitting · brokenLT AND RT IB FLAP ROLLER BRACKET TABS BROKEN. R&R FLAP TRACK ROLLER FITTINGS AND ROLLERS.SDR IPXA2018061230559Skin · dentedINSPECTION TYPE:C10, DENT ON LT WING INBD AFT FLAP UPPER SKIN AT IFS 151.25. REPAIR IAW SRM 57-53-01-2R-1 REPAIR 1 REV 71, SRM 51-70-10-2R REPAIR GENERAL REV 71.SDR AALA201806059025Strut · corrodedCORROSION FOUND ON THE INBOARD FLAP HOUSING OF THE INTERCONNECTING STRUT, RIGHT WING. REPLACED THE INTERCONNECTING STRUT.
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