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 DALA2021032901849Skin · crackedSHIP 672 INITIAL INSPECTION: SEVERAL CRACKS ON LOWER SKIN OF INBOARD MAIN FLAP LH WING. CORRECTIVE ACTION:SUMMARY OF NRC 00174: LOWER SKIN OF INBOARD MAIN FLAP LH WING WAS REPAIRED PER B757-200 SRM. (1764765)SDR SWIA202159270Bolt · corrodedLEFT AND RIGHT FLAP BPSU HAVE CORRODED MOUNTING HARDWARE. (C-CHECK RO 6/29/2021) REPLACED ALL MOUNTING HARDWARE AT LH AND RH FLAP BRAKE POSITION SENSOR UNIT PER CRJ 700 AMM 27-52-03-000-801-A01 AND AMM 27-52-03-400-801-A01 / TORQUE WRENCH WVACT204427 CASDR SWIA2021070159269Bolt · corrodedL/H WING OUTBOARD FLAP HINGE BOX FORWARD ATTACH FITTING AT WS 264.00 MOUNTING BOLTS CORRODED. (C-CHECK RO 6/29/2021) REMOVED AND INSTALLED NEW SERVICEABLE MOUNT BOLTS IN L/H WING OUTBD FLAP HINGE BOX FWD FITTING @ WS 264.00 IAW CRJ 700 AMM 57-54-02-400SDR SWIA2021070159248Anchor Fitting · chafedLEFT AND RIGHT FLAP STUB FAIRING FORWARD ATTACH BRACKETS ARE CHAFED APPROXIMATELY 50%. (C-CHECK RO 6/29/2021) REMOVED AND INSTALLED NEW SERVICABLE LEFT AND RIGHT FLAP STUB FAIRING FORWARD ATTACHMENT BRACKETS IAW CRJ 700 SRM 51-42-21-001-001-A01SDR SWIA202158780Skin · chafedCUSTOMER REQUEST REPAIR OF RH IB FLAP VANE CAP FOR CHAFING DAMAGE AT WS 56.30, WS 104.099, AND WS 139.924 (C-CHECK RO 6/11/2021) REMOVED AND REPLACED RH IB FLAP VANE CAPS AT WS 56.30, WS 104.099.AND WS 139.924 IAW CRJ 200 SRM 51-40-11 AND 51-42-13 REV. SDR SWIA202158162Skin · chafed* R/H INBOARD FLAP VANE SKIN IS CHAFED AT THE OUTBOARD LEADING EDGE. (C-CHECK RO 5/16/2021) BLENDED CHAFE ON R/H INBOARD FLAP VANE LEADING EDGE SKIN, OUTBOARD LOCATION. REF: CRJ 200, BOMBARDIER REO 601R-57-52-004, REV-D, DATE: 2012-12-19. EVALUATED ANDSDR SWIA202158161Skin · chafed* R/H INBOARD FLAP VANE SKIN IS CHAFED AT THE CENTER LEADING EDGE. (C-CHECK RO 5/16/2021) BLENDED CHAFE, BLENDED AREA IS FOUND TO BE OUT OF LIMITS REF REO 601R-57-52-004 REV D DATED 2012-12-19. INSTALLED NEW FLAP VAIN SKIN PN 601R14303-10. REF. CRJ200 SDR SWIA202158160Skin · chafed* R/H INBOARD FLAP VANE SKIN IS CHAFED AT THE INBOARD SIDE LEADING EDGE. (C-CHECK RO 5/16/2021) REMOVED CHAFE ON R/H I/B FLAP I/B SIDE LEADING EDGE SKIN, & FOUND TO BE OUT OF LIMIT PER REF BOMBARDIER REO 601R-57-52-004, REV -D, DATE 2012-12-19, REMOVEDSDR IPXA2021041368167Stiffener · wornINSPECTION TYPE:C2RH I/B FLAP MOVABLE HINGE FAIRING L/E WORN STIFFENER.REMOVED,FABRICATED AND REPLACED WORN HINGE FAIRING STIFFENER IAW SRM 51-31-01 (MINOR).SDR FDEA202103230747Seat Track · corrodedCABIN - STATION 1741 TO STATION 1761, X = 8.5 SEAT TRACK FOUND CORRODED AROUND FASTENER HOLES . CABIN - STATION 1741 TO STATION 1761 X = 8.5 CORROSION AT SEAT TRACK AROUND FASTENER HOLES REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE SDR SWIA202157913Attach Fitting · corroded* R/H FORWARD FLAP HINGE BOX ATTACH LUG ON WING AT WS178.00 HAS 2 CORRODED BOLTS, MARKED. (C-CHECK RO 4/25/2021) REPLACED CORRODED HARDWARE AT RH FWD FLAP HINGE BOX ATTACH LUG ON WING AT WS178.00 REF. CRJ200 AMM 57-21-37-400-801. LEAK CHECK GOODSDR SWIA202157912Attach Fitting · corroded* R/H FORWARD FLAP HINGE BOX ATTACH LUG ON WING AT WS220.00 HAS 2 CORRODED BOLTS, MARKED. (C-CHECK RO 4/25/2021) REPLACED CORRODED HARDWARE AT RH FWD FLAP HINGE BOX ATTACH LUG ON WING AT WS220.00 REF. CRJ200 AMM 57-21-37-400-802. LEAK CHECK GOODSDR SWIA202157911Attach Fitting · corroded* R/H FORWARD FLAP HINGE BOX ATTACH LUG ON WING AT WS264.00 HAS A CORRODED BOLT, MARKED. (C-CHECK RO 4/25/2021) REPLACED CORRODED HARDWARE AT RH FWD FLAP HINGE BOX ATTACH LUG ON WING AT WS264.00 REF. CRJ200 AMM 57-21-37-400-803. LEAK CHECK GOODSDR SWIA202157910Attach Fitting · corroded* L/H FORWARD FLAP HINGE BOX ATTACH LUG ON WING AT WS264.00 HAS A CORRODED BOLT, MARKED. (C-CHECK RO 4/25/2021) REPLACED CORRODED HARDWARE AT LH FWD FLAP HINGE BOX ATTACH LUG ON WING AT WS264.00 REF. CRJ200 AMM 20-21-00-910-801. LEAK CHECK GOODSDR SWAA2021050357871Skin · debondedDEBONDED IB MAIN FLAP SKIN ON WEDGE PANEL TRAILING EDGE AREA AT LT WING / REPAIRED IB MAIN FLAP SKIN ON WEDGE PANEL TRAILING EDGE AREA AT LT WING AS PER B737-700 SRM 57-23-01-2R -7 REPAIR 7 TOOL USED CALIPER PN 500-197-30 SN 15121550 DUE DATE 24-MAY-21 HOT BONSDR SWIA202157909Hinge Arm · corrodedRH INBD FLAP HIMNGE ARMS HAVE CORRODED HARDWARE (C-CHECK RO 4/25/2021) ORDERED AND RECIEVED NEW FROM STOCK 1 BUSHING, 1 BOLT, 6EA NUTS AND 6EA COTTER PINS. INSTALLATION OF NEW HARDWARE ACCOMPLISHED ON JOB 2754965 OP 5913 MX TRANS #21982154.SDR U2RA2020121600008Fairing · damagedNR 6 FLAP TRACK FIXED FAIRING P/N 65B15532- 26, S/N UNKNOWN, DAMAGED. ACCOMPLISHED INTERIM EXTERNAL DOUBLER MAJOR REPAIR(S) IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC ENGINEERING ORDER CONTROL NUMBER 21056-6 REVISION IR DATED 03/20/2021, DATA APPROVEDSDR U2RA2021032500006Skin · damagedREFERENCE NATIONAL AIRLINES AIRCRAFT MAINTENANCE LOG ITEM 45453-1: RIGHT INBOARD AFT FLAP P/N 65B02070-52, S/N 000158; LEADING EDGE SKIN PANELS DAMAGED. ACCOMPLISHED INTERIM EXTERNAL DOUBLER MAJOR REPAIR(S) IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC SDR U2RA2021032500005Skin · damagedRIGHT INBOARD MID FLAP P/N 65B02025-86, S/N 000159; LEADING EDGE SKIN PANEL DAMAGED. ACCOMPLISHED INTERIM EXTERNAL DOUBLER MAJOR REPAIR(S) IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC ENGINEERING ORDER CONTROL NUMBER 21056-3 REVISION IR DATED 03/20/2021SDR U2RA2021032500004Skin · damagedLEFT INBOARD AFT FLAP P/N 65B02070-103, S/N 0002993; LEADING EDGE SKIN PANEL DAMAGED. ACCOMPLISHED INTERIM EXTERNAL DOUBLER MAJOR REPAIR(S) IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC ENGINEERING ORDER CONTROL NUMBER 21056-2 REVISION IR DATED 03/20/202SDR U2RA2021032500003Skin · damagedLEFT INBOARD MID FLAP P/N 65B02025-77, S/N 000269; LEADING EDGE & UPPER SKIN PANELS DAMAGED. ACCOMPLISHED INTERIM EXTERNAL DOUBLER MAJOR REPAIR(S) IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC ENGINEERING ORDER CONTROL NUMBER 21056-1 REVISION A DATED 03/SDR DALA2021032401733Hinge · excess playTHE LT O/B FLAP HINGE HAS EXCESSIVE PLAY AT HINGE BOLT. DEFERRED FOR SDR REPORTING. NRC 331: REPAIRED PER PRI 590529-14 REV 0,1,2,3,&4 AND ER/A 590529-14 REV ORIG. (LP #1761231)SDR DALA2021032301719Cover · missingA FLAP COVER ON LEFT WING (CIRCLER 2" DIAMETER COVER) ON UNDER SIDE IS MISSING LOCATED NEAR FUSELAGE BY GEAR BAY. MAINTENANCE INSTALLED A NEW COVER. (LP #7576961)SDR YENA2021040700211Skin · chafedDURING HEAVY MAINTENANCE, CHAFING MARKS WERE REPORTED AT THE LH WING INBOARD AFT FLAP (PN 190-38006-403/ SN 00009) UPPER SKIN AT RIB 1A. SEE REF /1/ ETI FOR DETAILS. THE MARKS ARE 2 PLIES DEEP CAUSING DAMAGE TO THE COPPER MESH. IT IS REPORTED THE DAMAGED ISSDR FDEA202103200728Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR FDEA202103200727Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG LUG HOLE BORE (F AND G HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57SDR FDEA202103200725Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- SDR FDEA202103200723Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG LUG HOLE BORE (F AND G HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-5SDR SWIA202157239Panel · brokenLH WING FLAP PANEL 584ET HAS A BROKEN NUT PLATE. (C-CHECK RO 4/1/2021) REMOVED AND REPLACED 1EA. BROKEN NUT PLATE WITH NEW TO LH WING FLAP PANEL 584ET REF CRJ 700 SRM 51-45-00-001-001-A01.SDR SWIA202157952Hinge Box · corroded* LH INBD WING FLAPHINGE BOX, CENTER MOUND PLATE IS CORRODED. FLAGGED (C-CHECK RO 5/3/2021) BLENDED LH INBD FLAP HINGE BOX CENTER MOUNT PLATE, WITHIN LIMITS REF REO 601R-57-21-3453 REV -- DATE 2021-04-05. COMPLIED WITH 51-900-1003-SKY.SDR SWIA202158805Bolt · corrodedL/H I/NB FLAP O/B UPPER FITTING THROUGHT BOLT AND NUT HARDWARE CORRODED. (C-CHECK RO 6/11/2021) REPLACED L/H I/B FLAP O/B UPPER FITTING THROUGH BOLT AND NUT HARDWARE. TO BE INSTALLED ON CAMP CP22000952.SDR SWIA202157948Lug · gouged* RH INBD FLAP, OTBD HINGE ARM LUG GOUGED (C-CHECK RO 5/3/2021) COMPLIED WITH REO 601R-57-52-2414 REV -- DATE 2021-03-19 STEPS 1-4 . ENSURED BLENDOUT OF GOUGE TO A SMOOTH CONTOUR USING (20:1 TRANSITION RATIO). ENSURED BLENDOUT DIMENSION ARE NOT MORE THASDR SWIA202157947Lug · gouged* RH INBD FLAP, INBD HINGE ARM LUG GOUGED (C-CHECK RO 5/3/2021) COMPLIED WITH REO 601R-57-52-2414 REV -- DATE 2021-03-19 STEPS1-4. ENSURED BLENDOUT OF GOUGE WAS PERFORMED TO A SMOOTH CONTOUR USING A (20:1 TRASITION RATIO). ENSURED BLENDOUT DIMENSION WESDR SWIA202157946Lug · gouged* LH INBD FLAP, INBD HINGE ARM LUG GOUGED (C-CHECK RO 5/3/2021) REPAIRED GOUGE ON LH INBD FLAP, INBD HINGE ARM LUG PER REO 601R-57-52-2413 REV -- DATED 2021-03-19 / COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWAA2021031756233Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED AT IRSS 140.00 UPPER POSITION LT WINGSDR SWIA202158222Skin · dented*LEFT WING, OUTBOARD FLAP LOWER SKIN IS DENTED AT THE INBOARD END. (MARKED) (C-CHECK RO 5/20/2021) REPAIRED DAMAGE ON L/H WING O/B FLAP LOWER SKIN AT I/B END, REF. CRJ700 SRM 57-53-01, REPAIR-001-A01 & SRM 57-53-01-201-001-A01, TYPE III, FIG. 57-53-SDR REXA2021041600232Panel · bentUPON INSPECTION OF LH I/B MFS, FOUND WING PANEL FWD OF MFS TO BE BENT. INSTALLED NEW SERVICEABLE SEAL AND CHANNEL IAW CRJ 900 SRM'S 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND
51-25-01-001-001-A01.SDR SWIA202157514Hinge Arm · gougedR/H INBOARD FLAP, OUTBOARD HINGE ARM, OUTBOARD FORWARD LUG HAS GOUGE DAMAGE. (C-CHECK RO 4/12/2021) REPAIRED RH INBD FLAP, OUTBD HINGE ARM, OUTBD FWD LUG IAW MHIRJ REO# 601R-57-54-322 REV-- DATE 2021-03-14. REFERENCE CONTINUATION CARD FOR WORK PERFORMEDSDR A6WA202103197718Skin · dentedINWARD DENT COMMON TO EXTERIOR SKIN, LOWER SIDE OF INBOARD RIGHT HAND FLAP AT APPROXIMATELY WING STATION 106.40. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT COMMON TO EXTERIOR SKIN, LOWER SIDE OF INBOARD RIGHT HAND FLAP AT APPROX. WING STATION 106.40SDR FDEA202103090674Angle · crackedRIGHT WING OUTBOARD FLAP INBOARD HINGE UPPER INBOARD SUPPORT IS CRACKED.(FLAP SIDE) REMOVED AND REPLACED R/H WING OUTB FLAP INB HINGE ANGLE ARC2149-5 PER DAC ARC2149 AND SRM 51-31-01 VOL. 2.SDR UIEA2021021900352Skin · corrodedLHW I/B AFT FLAP UPPER SKIN FOUND CORROSION.(<P>LHW I/B AFT FLAP UPPER SKIN CORROSION AREA REPAIRED AS PER SRM 57-53-01-1A-0.</P>)SDR UIEA2021021900353Skin · corrodedRHW I/B MID FLAP UPPER SKIN AFT T/E FOUND CORROSION.(<P>RHW I/B MID FLAP UPPER SKIN AFT T/E CORROSION AREA REPAIRED AS PER SRM 57-53-01-1A-0.</P>)SDR UIEA2021021900354Skin · corrodedLHW I/B MID FLAP UPPER SKIN FOUND CORROSION.(<P>LHW I/B MID FLAP UPPER SKIN CORROSION AREA REPAIRED AS PER SRM 57-53-01-1A-0.</P>)SDR UIEA2021022300410Fairing · chafedRHW #18 L/E V/C FLAP BULLNOSE FAIRING SKIN I/B EDGE CHAFING.(<P>RHW #18 L/E V/C FLAP BULLNOSE SKIN I/B EDGE CHAFING AREA. REPAIRED AS PER RI-57-00-14394 REV A.</P>)SDR UIEA2021030200451Skin · delaminatedLH O/B FORE FLAP L/E FAIRING FOUND DELAM.(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5A.</P>)SDR UIEA2021030200452Skin · damagedLHW O/B MID FLAP UPPER SURFACE SCREW HOLE FOUND ELONGATED.(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5K.</P>)SDR UIEA2021030200453Skin · delaminatedLH O/B MID FLAP AFT EDGE UPPER SURFACE FOUND DELAM.(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5A</P>)SDR UIEA2021030200454Skin · damagedLHW O/B MID FLAP UPPER SURFACE SCREW HOLE FOUND ELONGATED.(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5K.</P>)SDR UIEA2021030200455Skin · damagedLHW O/B MID FLAP UPPER SURFACE SCREW HOLE FOUND ELONGATED.(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5K.</P>)SDR UIEA2021030200456Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAM.(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR AS PER SRM 51-70-07 PAR 5A.
Back to JASC 5753