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 SWIA2020060950929Skin · chafedRT INBOARD FLAP VANE SKIN IS CHAFED OUTBOARD OF PANEL 684ET. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED RT I/B FLAP VANE SKIN (CAP) OUTBOARD OF PANEL 684ET REF SRM AND DWG.SDR SWIA2020060950928Skin · chafedRT INBOARD FLAP VANE SKIN IS CHAFED INBOARD OF PANEL 684DT. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED RT I/B FLAP SKIN (CAP) INBOARD PANEL 684DT REF SRM AND DWG.SDR SWIA2020060950926Skin · dentedLEFT OUTBD FLAP. DENT MEASURING L=0.8" W=0.69" D=-.035". PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/27/2020 REPAIRED THE LEFT OUTBOARD FLAP REF SRM.SDR FDEA2020042750785Filler · wornDURING AGING AIRCRAFT INSPECTION OF EXISTING REPAIR ON RIGHT WING OUTBOARD FLAP INBOARD LEADING EDGE SKIN FOUND FLUSH SKIN FILLER TO BE WORN REMOVED WORN FILLER IAW B757 SRM 51-40-02. FABRICATED AND INSTALLED NEW REPAIR FILLER IAW B757 SRM 57-53-01-2R REPASDR SWAA2020061082603Stiffener · chafedRT FLAP TRACK SUPPORT STIFFENER AT BS727A COMMON TO STR20R IS CHAFFED. REMOVED AND REPLACED RT FLAP TRACK SUPPORT STIFFENER BS 727A COMMON TO STR 20R IAW SRM 51-40-02; SRM 51-40-05; DWG# 149A7506.SDR IPXA2020042454593Carriage · obstructedINSPECTION TYPE:NA**SUPPLEMENTAL SDR** ** EMERGENCY DECLARED ** LANDED WITHOUT INCIDENT ** TRAILING EDGE FLAPS JAMMED IN THE STOWED 0 POSITION. DEFERRED DISCEPANCY PER FERRY PERMIT NO 9001 C/W ENGINEERING MAINTENANCE ACTIONS PER FORM 52-19-014A.FOUND FOD LODGESDR SWIA20205060538Vane · chafedRIGHT INBD FLAP VANE LEADING EDGE OUTBD HAS CHAFFE (48 MO INSP) RO 5/6/2020 REMOVED AND INSTALLED NEW LEADING EDGE FLAP AT RIGHT INBOARD FLAP OUTBD. REF. CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH AND SEE CONTINUATION CARD FOR DETAILSSDR SWIA20205060537Vane · chafedRIGHT INBD FLAP VANE LEADING EDGE INBD HAS CHAFFE (48 MO INSP) RO 5/6/2020 REPLACED RH INBD FLAP VANE INBD CAP. REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUE CARD FOR ADDITIONAL DETAILS. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)SDR SWIA20205070536Vane · chafed* LEFT INBD FLAP VANE LEADING EDGE OUTBD HAS CHAFFE (48 MO INSP) RO 5/6/2020 BLENDED THE CHAFE ON LEFT INBD FLAP VANE LEADING EDGE OUTBD CAP REFERENCE CRJ200 SRM. EVALUATED AND FOUND TO BE OUT OF ,LIMITS. REPLACED LH INBD FLAP VANE OUTBOARD CAP. REF CRJSDR IPXA2020060856218Skin · crackedINSPECTION TYPE:3C LT WING UPPER SURFACE T/E WEDGE SKIN IS CRACKED JUST O/B OF I/B AILERON. CUTOUT DAMAGE AREA AND ACCOMPLISHED PERMANENT REPAIR ON LT WING UPPER SURFACE T/E WEDGE SKIN JUST O/B OF I/B AILERON IAW SRM 57-50-01, REPAIR 6 FIG 202 REV-66 (MAJOR).SDR IPXA2020042454586Yoke · damagedINSPECTION TYPE:CTRAILING EDGE OF #3 FLAP TRACK HAS SEVERAL GOUGE MARKSAFTER FURTHER INSPECTION GVI NOTED NO DAMAGE NO DEFECTS TO #3 FLAP TRACK FURTHER INSPECTION NOTE 7 DINGS ON FWD FACE OF YOKE REMOVED 7 DINGS NICKS ON FWD FACE OF YOKE AFTER REWORK NO MARKS SDR HALA2020041600088Cover · missingRT WING OUTBOARD FLAP TRACK #4 MISSING COVER. // REPLACED MISSING RT WING FLAP TRACK #4 COVER. OK FOR SERVICESDR SWIA20205060487Rivet · looseLH O/B FLAP UPPER SURFACE HAS SMOKING RIVETS (C-CHECK) RO 5/4/2020 / COMPLIED WITH REPAIR OF LH OB FLAP UPPER SURFACE SMOKING RIVETS REF BOMBARDIER REO COMPLIED WITH SKYWEST TASK CARD.SDR ASOA202004147036Flap · delaminatedL/H I/B FLAP HAS AREAS OF DELAMINATION ON TRAILING EDGE. REPAIRED DELAMINATION IAW EA12-2020-055. FLAP WAS RETURNED TO STOCK.SDR FDEA2020041090727Skin · gougedRW INBOARD FLAP UPPER SURFACE HAS GOUGES REPAIRED RW INBOARD FLAP UPPER SURFACE GOUGES IAW B757 SRM: 51-40-02, 57-53-01-2A, 51-70-10, 51-20-05, AMM: 51-21-10/701, NDTM PT. 6 51-00-16, 51-00-19, NDTM PT. 4 51-00-05 & EA #F-5750-T0353383; F-5750-T0353383-P1 SDR LR7A2020040902252Skin · crackedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB2703, FOUND THE LH OUTBOARD FLAP UPPER SURFACE CRACKED AT THE OWFS256L JACKSCREW CUTOUT TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 193497.SDR LR7A2020040902250Skin · crackedDURING SCHEDULED B-3 CHECK UNDER JOB CARD HB2703, FOUND THE LH INBOARD FLAP LOWER SKIN CRACKED AT CWS130.5L, 33 INCHES FWD OF THE TRAILING EDGE (FS641.5). / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 57-70-10. NR# 192738.SDR SWIA20205060486Rivet · looseLH AND RH O/B FLAP UPPER SURFACE HAVE SMOKING RIVETS (C-CHECK) RO 5/4/2020 COMPLIED WIITH ALL STEPS OF REO FOR SMOKING RIVETS OF RH O/B FLAP COMPLIED WITH SKYWEST TASK CARD. LH OB FLAP SMOKING RIVETS REPAIRED ON JOB 710207101 OP193 CAMP 20827389SDR FDEA202004080722Support Fitting · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE # 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE # 5 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- SDR FDEA202004080721Support Fitting · corrodedRIGHT HAND WING - OUTBOARD FLAP VANE # 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE # 4 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- SDR FDEA202004080720Support Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP VANE NR 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION. SUPPORT FITTING REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ECCENTRIC BUSHING FABRICATED BY MACHINING AS PER SRMSDR FDEA2020041780747Skin · canningR/H I/B FLAP TOP FORWARD CENTER SKIN IS OIL CANNING. SUSPECT DELAM. REPAIRED R/H IB FLAP REF. SRM 57-00-01-2R REPAIR 1. REF. EA 1-5750-T0353561. R/H INBD FLAP UPPER SURFACE - DENT, RSC TRACKING. MAJOR REPAIRSDR IPXA2020041054041Skin · dentedINSPECTION TYPE:N/ARH INBD TE AFT FLAP UPPER SURFACE DENT 19" FROM TE AND 9.5" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTALL. 4SDR IPXA2020041054040Skin · dentedINSPECTION TYPE:N/ALH INBD TE AFT FLAP HAS UPPER SURFACE DENT 19.5" FROM TE AND 8.5" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTSDR IPXA2020041054039Skin · dentedINSPECTION TYPE:N/ALH INBD TE AFT FLAP HAS UPPER SURFACE DENT 19.2" FROM TE AND 57" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTASDR IPXA2020041054038Skin · dentedINSPECTION TYPE:N/ALH INBD TE AFT FLAP HAS UPPER SURFACE DENT 19.5" FROM TE AND 93" FROM IB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTASDR IPXA2020041054037Skin · dentedINSPECTION TYPE:N/ALH INBD TE AFT FLAP HAS UPPER SURFACE DENT 20.5" FROM TE AND 97" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTASDR IPXA2020041054036Skin · dentedINSPECTION TYPE:N/ARH INBD TE AFT FLAP HAS UPPER SURFACE DENT 21" FROM TE AND 157.5" FROM OB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI PART1 51-05-01, GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTSDR IPXA2020041054035Skin · dentedINSPECTION TYPE:N/ARH INBD AFT FLAP HAS UPPER SURFACE DENT 20.5" TROM TE AND 89" FROM IB EDGEREMOVED SURFACE FINISH AND FABRICATED REPAIR DOUBLER PER SRM 51-70-10-2R BPT 0558813 4-8-20 PERFORMED NDI 51-05-01. GOOD. VERIFIED DAMAGE REMOVAL. OK TO INSTALL 45011SDR HALA2020040900079Rib · corrodedDURING C CHECK, WHILE PERFORMING EM 5753-01164 (A330 SB 57-3124 R3), CORROSION WAS FOUND ON THE RH RIB 6 FWD LUG. CORROSION HAS BEEN REMOVED BY OVERSIZING AS PER R575-58471 ISSUE D WITH DEVIATIONS PER AIRBUS TECHNICAL ADAPTATION 80691523/046/2019 ISSUE 2 AND ESDR HALA2020040900078Rib · corrodedDURING C CHECK, WHILE PERFORMING EM 5753-01164 (A330 SB 57-3124 R3), CORROSION WAS FOUND ON THE LH RIB 6 FWD LUG. CORROSION HAS BEEN REMOVED BY OVERSIZING AS PER R575-58471 ISSUE D WITH DEVIATIONS PER AIRBUS TECHNICAL ADAPTATION 80691523/046/2019 ISSUE 2 AND ESDR UIEA2020040600521Structure · corrodedLHW O/B MID FLAP T/E #587NT UPPER CHORD FOUND CORROSION.(<P>LHW O/B MID FLAP T/E #587NT UPPER CHORD CORROSION AREA REPAIRED AS PER SRM 57-53-02-1A-1.</P>)SDR UIEA2020040600522Access Panel · corrodedRHW I/B MID FLAP ACCESS PANEL ( #677JT ) FOUND CORROSION.(<P>RHW I/B MID FLAP ACCESS PANEL ( #677JT ) CORROSION AREA REPAIRED AS PER SRM 57-53-01-1A-0.</P>)SDR UIEA2020040600523Access Panel · corrodedRHW I/B MID FLAP UPPER ACCESS PANEL ( 677KT ) FOUND CORROSION.(<P>RHW I/B MID FLAP UPPER ACCESS PANEL ( 677KT ) CORROSION AREA REPAIRED AS PER SRM 57-53-01-1A-0.</P>)SDR REXA2020042800550Skin · dentedL/H INBD FLAP HAS (1) SHARP DENT APPROX 6"" UP FROM T/E ON FLAP ON BOTTOM SKIN, APPROX WS 108.00. DENT IS APPROX .125" L X .062" W X .015" D. (MARKED WITH TAPE).
REPAIRED L/H IB FLAP BOTTOM SKIN DENT AT WS 108.00 IAW CRJ SDR REXA2020042800549Skin · dentedL/H INBD FLAP HAS (2) DENTS IN CLOSE PROXIMITY ON BOTTOM SKIN OF FLAP AT APPROX W.S. 38.00. EACH DENT APPROX .1875"" DIA AND .010"" DEEP. (MARKED WITH TAPE)
REPAIRED DENTS ON L/H INBD FLAP IAW CRJ 900 SRM 57-SDR FDEA2020040640688Hinge Fitting · corrodedLEFT HAND WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORRSION. CORROSION AT LEFT HAND WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CSDR FDEA2020040640687Hinge Fitting · corrodedLEFT HAND WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORRSION. CORROSION AT LEFT HAND WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 5SDR IPXA2020050154788Support · crackedINSPECTION TYPE:2CL/H WING T/E I/B FLAP I/B HINGE FRAME SUPPORT IS CRACKED.REMOVED, FABRICATED AND REPLACED HINGE SUPPORT IAW DWG. ARC0165 AND SRM 51-35-01. (MINOR)SDR FDEA202004030671Hinge Bracket · corrodedLEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-SDR FDEA202004030670Hinge Bracket · corrodedLEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11SDR FDEA202004030669Hinge Bracket · corrodedLEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT ASDR FDEA202004030668Hinge Bracket · corrodedLEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS SDR FDEA202004030667Hinge Bracket · corrodedRIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMITSDR FDEA202004030666Hinge Bracket · corrodedRIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT ASDR SWAA2020040636058Skin · damagedL/H WING INBOARD TRAILING EDGE AFT FLAP LOWER SKIN HAS SURFACE DAMAGED. REF: REPAIR - 57EA-07903. / REMOVED AND REPLACED L/H I/B AFT TRAILING EDGE FLAP IAW AMM. 27-51-12. ' 'PN OFF: 113A2700-27 SN OFF: 000424 PN ON: 113A2700-15 SN ON: D-0123SDR COEA2020051518911Deflector · corrodedWO 213191 NR 500013 HEAVY CHECK COE/MAJOR REPAIR: L/H OUTBOARD FLAP INBOARD DEFLECTOR HAS LEVEL 2 CORROSION AT OUTBOARD CAM GUIDE. CORRECTIVE ACTION: REPAIRED PER SRM 575320-300-801-A01.SDR COEA2020051511911Guide · corrodedWO 213191 NR 500012 HEAVY CHECK COE/MINOR REPAIR: L/H OUTBOARD FLAP INBOARD DEFLECTOR THIRD CAM GUIDE FROM INBOARD HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.SDR SWIA20205110557Skin · dented* L/H INB FLAP LOWER SKIN HAS DENT NEAR INB END ( MARKED, HAS GREEN PRIMER PAINT AT DENT. ) (C-CHECK) RO 5/7/2020 L/H I/B FLAP LOWER SKIN AT THE I/B END HAS HAS THE DENT REPAIRED PER BOMBARDIER REO. SEE CONTINUATION SHEET FOR DETAILS. PERFORMED AN OPERATIOSDR SWIA20205110556Skin · dented* R/H INB FLAP LOWER SKIN HAS SEVERAL SMALL DENTS NEAR INB END OF FLAP. ( MARKED ) (C-CHECK) RO 5/7/2020 REPAIRED R/H INBOARD FLAP LOWER SKIN DENTS NEAR INBD END OF FLAP REF BOMBARDIER REO ALL STEPS COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS.
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