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 FDEA202104100875Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND BARREL NUT WALL THICKNESS THICKNSDR FDEA202104100874Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57SDR FDEA202104100873Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SDR FDEA202104100872Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD FORWARD MOUNT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD FORWARD MOUNT LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER SDR FDEA202104100871Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD MOUNT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD FORWARD MOUNT LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PSDR FDEA202104100870Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- SDR FDEA202104100869Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA202104100868Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA202104100867Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT INBOARD HOLE BORE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT INBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA202104100866Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRISDR AALA202104119012Wedge · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP TRAILING EDGE WEDGE DELAMINATED. REPLACED WEDGE ASSEMBLY PER SRM 51-40-02.SDR SWIA2021072859766Hinge Arm · damagedL/H OUTBOARD FLAP HINGE ARM AT FLAP ATTACH POINT IS DAMGAGED ON INNER FLANGE FROM COUNTER SUNK SCREW BEING LEFT IN HINGE ARM AREA. (C-CHECK RO 7/24/2021) REPAIRED LH OUTBOARD FLAP OB HINGE ARE AT WS 264.00 IAW MHIRJ REO 601R-57-21-3468 DATED 2021-05-02 SDR FDEA202104080845Flap System · unknownAFTER TAKEOFF IN MODERATE TURBULENCE FLAPS 5 LIMIT SPEED (210 ITS)EXCEEDED. SPEED REACHED 213 ITS FOR 3 SECONDS WHILE FLAPS IN TRANSIT TO FLAPS 1. PERFORMED PHASE 1 INSPECTION REF B 757 AMM 05-51-08-2. NO DEFECTS NOTED A/C OK FOR SERVICE.SDR SWIA2021090360703Skin · corrodedR/H WING O/B FLAP UPPER SURFACE PANELS HAVE CORRODED HARDWARE (C-CHECK RO 8/31/21) REPLACED CORRODED HARDWARE ON R/H O/B FLAP AND INSTALLED ALL NEW HARDWARE IAW CRJ 700 SRM 51-21-00-001-001-A01SDR FDEA202104070836Rub Strip · crackedL/W O/B FLAP O/B TRACK CARRIAGE ASSY 2[EA] INNER PHENOLIC PLATES CRACKED REPAIRED PLATES PER FEDEX EA# F-5750-T0360814-P1SDR SWIA2021090360639Skin · damagedL/H WING O/B FLAP UPPER EXTERNAL SKIN HAS NUMEROUS SMOKING RIVETS. (C-CHECK RO 8/31/2021)REMOVED AND REPAIRED 56 SMOKING RIVETS ON L/H WING O/B FLAP UPPER EXTERNAL SKIN AS REQUIRED IAW REO 670-57-53-275 REV A DATED 2021-05-20. FORM 337 AND MAJOR REPAIR TASKSDR SWIA202157914Hinge Box · corrodedR/H WING, OUTBD FLAP, OUTBD FLAP HINGE BOX, HAS CORRODE HARDWARE ON BUTE DOOR COMPRESSION SPRING AND BOLTS AT SAFETY PLATES 6 PLACES (MARKED) (C-CHECK RO 4/25/2021) REMOVED AND REPLACED WITH NEW R/H WING, OUTBD FLAP, OUTBD FLAP HINGE BOX, HARDWARE ON SDR JJBA20210404049Flap Track · wornRH OB FLAP OB FLAP TRACK SHOWS SIGNS OF WEAR IN MULTIPLE AREAS. REMOVED AND REPLACED RH OB FLAP OB FLAP TRACK.SDR DALA2021050302496Skin · dentedWHILE ON LAYOVER IN MSP, MTC REPORTED A DENT TO THE LH SIDE INBD AFT FLAP LOWER SKIN ON THE TE WEDGE JUST AFT OF THE WEDGE SPAR. THE DAMAGE IS REPORTED TO BE 0.190 DEEP AND 8.750 LONG ON THE SMALLEST DIAMETER. THE DENT IS OUT OF ALLOWABLE DAMAGE LIMITS PER TSDR AALA202104069019Skin · debondedAIRCRAFT WAS GROUNDED: RIGHT WING OUTBOARD FLAP PREVIOUSLY INSTALLED DOUBLER FAILED / DISBONDED DUE TO MOISURE INGRESS. REPAIRED FLAP PER EA 326753.SDR SWIA202158783Rib · crackedTRANSFERED FROM CAMP 22538869 JOB 97628101 OP 493 - L/H I/B FLAP I/B CLOSE OUT RIB HAS A DENT APPROX .200 DEEP AND POSSIBLE CRACK AT A NUTPLATE HOLE LOCATION. (C-CHECK RO 6/11/2021) PERFORMED A MAJOR REPAIR BY REMOVING AND REPLACING THE L/H I/B FLAP I/SDR VNAA2021040299915Hinge · crackedCRACK INDICATION DETECTED DURING NDT IN AFT INBOARD BOLT HOLE OF FLAP FWD HINGE SUPPORT FITTING AT WS 128.00 LH WING. CRACK LOCATED .150" FROM SKIN SURFACE, .090" LENGTH, 040" DEEP.
COMPLETED REPAIR IN AFT INBD BOLT HOLE OF FLAP FWD HINGE SUPPORT FITTING ATSDR AALA202104029001Tab · debondedAIRCRAFT WAS GROUNDED: LEFT WING OUT BOARD FLAP TAB IS DEBONDED ON BOTH UPPER AND LOWER SURFACES.. REPAIRED FLAP TAB PER EA 326690.SDR DALA2021040501984Skin · nickedSHIP 5807 INITIAL INSPECTION: NICKS (4 EAS) ON INBD MAIN FLAP, LOWER SKIN BTW. MF STA 240 TO MF STA 300 AT RH WING. CORRECTIVE ACTION:SUMMARY OF NRC 00980 NICKS ON INBD MAIN FLAP, LOWER SKIN BTW. MF STA 240 TO MF STA 300 AT RH WING WERE BLENDED OUT PER B-757-3SDR UIEA2021031600604Skin · delaminatedRHW I/B FORE FLAP FOUND DELAMINATION(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)SDR UIEA2021031700605Skin · delaminatedRHW O/B MID FLAP FOUND DELAMINATION (<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)SDR UIEA2021031900617Skin · delaminatedLHW I/B FORE FLAP L/E FOUND SEVERAL DELAMINATION(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)SDR UIEA2021032000622Skin · delaminatedLHW I/B AFT FLAP UPPER SURFACE FOUND DELAMINATION (<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)SDR UIEA2021032000623Skin · delaminatedLHW I/B MID FLAP L/E FOUND DELAMINATION (<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)SDR UIEA2021032000624Skin · delaminatedRHW I/B MID FLAP FOUND DELAMINATION (<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5.A</P>)SDR UIEA2021032400707Skin · corrodedRHW I/B AFT FLAP LOWER SKIN SEVERAL LOCATION FOUND CORROSION.(<P>RHW I/B AFT FLAP REPLACEMENT AS PER AMM 27-51-03.</P>)SDR UIEA2021032900741Panel · chafedLHW O/B AFT FLAP MOST O/B PANEL PREVIOUS PATCH FOUND DEEP CHAFING.(<P>LHW O/B AFT FLAP MOST O/B PANEL CARRIED OUT METAL HOT BOND REPAIR AS PER RI NO. RI-57-55-14467 REV A.</P>)SDR UIEA2021040200792Spar · corrodedCORROSION - DAMAGE ON UPPER CHORD OF LH WING INBD MID FLAP REAR SPAR, AT FS 205.390. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02 REV 91. BLENDED OUT THE DAMAGED AREA IAW SRM 51-10-02 REV 91. PFM NDT INSP REFER TO JOB CARD ATTACHING SHEET NO 0263122. ACCOMPLSDR UIEA2021040100778Skin · delaminatedLHW I/B FORE FLAP FOUND DELAMINATION(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5A, REV 111.</P>)SDR UIEA2021040100779Skin · delaminatedRHW I/B FORE FLAP FOUND DELAMINATION(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5A, REV 111</P>)SDR UIEA2021040100780Skin · delaminatedRHW O/B FORE FLAP FOUND DELAMINATED(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5A, REV 111</P>)SDR UIEA2021040100781Skin · puncturedLHW I/B AFT FLAP FOUND PUNCH HOLE(<P>PUNCH AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5A REV 111</P>)SDR UIEA2021040100783Skin · delaminatedRHW I/B FORE FLAP FOUND DELAMINATED (FROM O/B EDGE 74")(<P>DELAMINATED AREA PERFORMED REPAIR AS PER SRM 51-70-07 PAR 5A REV 111</P>)SDR FDEA202103300804Skin · crackedRH WING I/B FLAP- O/B SIDE LWR SURFACE HAS A MINOR DENT (MKD) R&R FRANGIBLE SKIN @ R/H WING I/B FLAP O/B SIDE PER DWG ARC3098 & SRM 51-31-01 VOL II.SDR KCSA202103291032Skin Panel · damagedWING O/B AFT FLAP PANEL IS DAMAGED ON EXISTING REPAIRSDR AALA202103309031Wedge · delaminatedAIRCRAFT WAS GROUNDED: RIGHT WING OUT BOARD FLAP OUT BOARD TRAILING EDGE WEDGE LOWER SURFACE IN BOARD END IS DELAMINATED AND SPLIT ON THE TRAILING EDGE. **SUPPLEMENTAL REPORT: REPLACED FLAP TRAILING EDGE WEDGE PER EA 326641SDR AALA202103299025Wedge · delaminatedAIRCRAFT WAS GROUNDED: RIGHT WING OUT BOARD FLAP INBOARD TRAILING EDGE WEDGE LOWER SURFACE OUT BOARD END IS DELAMINATED AND SPLIT ON THE TRAILING EDGE. ** SUPPLEMENTAL REPORT: REPLACED FLAP TRAILING EDGE WEDGE PER EA 326641SDR FDEA202103270785Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMMSDR FDEA202103270784Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 5SDR FDEA202103270783Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG BORE HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD- MD-SDR FDEA202103270782Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR ACTUATOR LUG BORE HOLE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 SDR YENA2021033100194Flap Track · crackedDURING HEAVY MAINTENANCE, CRACK O/B FLAP LEADING EDGE AREA BTW FLAP TRACK 3 AND FLAP TRACK 4 ON L/H WING; (REF AEROMAN N/R 2021-115357) PERFORMED PERMANENT REPAIR ON O/B FLAP LEADING EDGE L/H WING IAW SRM A320-57-30-00-300-029 FIG 001(SHEET 5 AND 6) PROCEDURESDR 2021FA0000091Vane · damagedSKIN DISBONDED FROM CORE, ALSO HAS CORROSION AND DENTS ON SKIN.SDR FDEA202103250767Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING BUSHSDR FDEA202103250766Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING BUSHING FA
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