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 SWIA2019110446635Skin · chafedLEFT INBD FLAP VANE MIDDLE SECTION LEADING EDGE IS CHAFFED. (C-CHECK) RO: 11/1/2019 LH INBD FLAP VANE (OTBD MIDDLE) LEADING EDGE IS FOUND TO BE OUT OF LIMITS AND REPLACED WITH NEW.SDR SWIA2019110446634Skin · chafedLEFT INBD FLAP VANE OUTBD LEADING EDGE IS CHAFFED. (C-CHECK) RO: 11/1/2019 LH INBD FLAP VANE OTBD LEADING EDGE IS FOUND TO BE OUT OF LIMITS AND REPLACED WITH NEW.SDR IPXA2019110448607Skin · dentedINSPECTION TYPE:N/ALH O/B T/E FLAP UPPER SKIN DENT. DENT MEASURES 2.85" INBD/OTBD X 1.85" FWD/AFT X .303 DEEP. LOCATED 3.5" FROM INBD EDGE AND 16.25" FROM T/EREPAIRED L/H WING O/B FLAP T/E DENT IAW A300 5750-74296-C. THIS CLEARS M686198SDR SWIA2020010947548Bolt · corrodedR/H WING OUTBD FLAP OUTBD HINGE BOX AFT ATTACHING ANTI-MIGRATION TAB HARDWARE CORRODED. (C-CHECK) RO 01/06/2020 REMOVED & REPLACE HARDWARE R/H WING OUTBOARD FLAP OUTBOARD WING BOX AFT IAW CRJ200 AMMSDR SWIA2020010947547Bushing · corrodedR/H WING OUTBD FLAP OUTBD HINGE BOX FLAP ACTUATOR HARDWARE ON TRAILING EDGE OF WING CORRODED. (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED HARDWARD R/H WING OUTBOARD FLAP OUTBOARD HINGE BOX FLAP ACTUATOR IAW CRJ200 AMM TORQUE WRENCH S/N 2250. STS CAL: DUE DESDR SWIA2020010947546Bolt · corrodedR/H WING OUTBD FLAP INBD FLAP HINGE BOX ANTI-MIGRATION HARDWARE CORRODED. (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED HARDWARE AT R/H WING OUTBOARD FLAP, INBD HINGE BOX ANTI-MNIGRATION TAB IAW CRJ 200 AMM.SDR IPXA2019111148854Bracket · crackedINSPECTION TYPE:2CR/H O/B FLAP I/B HINGE AFT SIDE ANGLE BRACKET IS GOUGED.REMOVED, FABRICATED AND REPLACED BRACKET IAW DWG. ARC2149 AND SRM 51-31-01. (MINOR)SDR DALA2019110400239Cover · missingLEFT WING NBR 3 FLAP TRACK FAIRING FORWARD COVER MISSING. INSTALL SPEED TAPE AND DEFERRED PER CDL 57-00-07 UNTIL FIXED FAIRING CAP AVAILABLE TO REPLACE. LP 6378791SDR FDEA201910312811Skin · crackedLH WING OUTBOARD FLAP UPPER SURFACE SKIN HAS TWO CRACKS LOCATED AT THE INBOARD HINGE AREA 0000608631 : F - 01-NOV-2019 01:12 REPAIRED REF MD10 SRM 57-10-00 TRACKING EA 8-5750-T0350557 PART 1SDR SWIA2019121847011Skin · wornRH LEADING EDGE FLAP VAIN SKIN HAS A .035 DEEP WORN SPOT ,P/N601R14303-44 OTBD.. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED FLAP VANE SKIN CAP IAW CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.SDR RAIA2019112570019Hinge · crackedL/H WING T/E O/B FLAP SHROUD I/B FWD HINGE HALF IS CRACKED....R&R L/H WING T/E O/B FLAP SHROUD I/B FWD HINGE HALF.SDR RAIA2019112570018Hinge · crackedL/H WING T/E O/B FLAP SHROUD O/B AFT HINGE HALF IS CRACKED....R&R L/H WING T/E O/B FLAP SHROUD O/B AFT HINGE HALF.SDR RAIA2019112570017Hinge · crackedL/H WING T/E O/B FLAP SHROUD O/B FWD HINGE HALF IS CRACKED....R&R L/H WING T/E O/B FLAP SHROUD O/B FWD HINGE HALF.SDR RAIA2019112070014Hinge · crackedRH WING O/B FLAP SHROUD I/B FWD HINGE HALF HAS 3 CRACKED LUGS- REMOVED HINGE FROM FLAP SHROUD & STARTED DRILL UP. R&R RH WING O/B FLAP SHROUD I/B HINGE.SDR RAIA2019112090013Hinge · crackedRH WING O/B FLAP SHROUD I/B AFT HINGE HALF IS CRACKED AT O/B END- REMOVED RH O/B FLAP I/B HINGE, STARTED TO DRILL UP. R&R RH WING O/B SHROUD I/B AFT HINGE.SDR IPXA2019102878351Skin · puncturedINSPECTION TYPE:M4L/H WING OB AFT FLAP HAS A PUNCTURED HOLE IN FLAP DOT 33-11REPAIRED PUNCTURED FLAP IAW B757 SRM 57-53-01-2R-1 (TABLE 2) AND 51-70-04 350F CURESDR HALA2019102900235Cover · missingDURING INSPECTION, RIGHT WING INBOARD FLAP TRACK FIXED FAIRING COVER MISSING. REPLACED NEW CAP ON WING FIXED FLAP TRACK. LP 6785353SDR HALA2019102900236Cover · missingDURING PDC, FOUND ONE COVER MISSING ON RIGHT WING OUTBOARD AFT FIXED FLAP TRACK FAIRING. REPLACED FLAP TRAK COVER 634BL. LP 3223747SDR IPXA2019110848773Skin · gougedINSPECTION TYPE:12YRRT WING I/B FLAP UPPER SKIN IS GOUGED AT RIB 12 AND BETWEEN STRINGERS 2.1 & 2.2.REPAIRED GOUGED RT WING I/B FLAP UPPER SKIN AT RIB 12 AND BETWEEN STRINGER 2.1 & 2.2 IAW A300 SRM 57-50-00 PAR. E, FIG. 205. (MAJOR)SDR DALA2019102406131Skin · debondedMTC TASK - RH WING O/B FLAP LOWER SURFACE O/B LOWER PANEL FOUND SUSPECTED DISBOND AT OTEF STA187. RH WING O/B FLAP LOWER SURFACE O/B LOWER PANEL AT OTEF STA187 REPAIRED AS PER B767-400 SRM57-53-01-2R-1 & SRM51-70-10-2R-4. (LP1329320)SDR SWAA2019102838250Skin · delaminatedL/H WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED APPROXIMATELY 4" X 1" AT THE TRAILING EDGE 5.5" OUTBOARD OF THE INBOARD END. / R&R AFT FLAP PER AMM.SDR SWAA2019102838249Skin · delaminatedL/H WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED APPROXIMATELY 4" X 1" AT THE TRAILING EDGE 5.5" OUTBOARD OF THE INBOARD END. R&R AFT FLAP PER MM.SDR SWIA2019102346596Skin · chafed*R/H INBD FLAP VANE LEADING EGDE IS CHAFED AT 3EA LOCATIONS. INBD,CNT, AND OTBD. (C-CHECK) RO: 10/22/19. BLENDED OUT CHAFFING AT 3 EACH LOCATIONS ON THE RH IB FLAP VANE TO A SMOOTH CONTOUR.FOUND THE O/B AND I/B WITH IN LIMITS AND MIDDLE OUT OF LIMITS. REMOVESDR SWIA2019102346591Skin · chafedRH INBD FLAP UPPER L/E SKIN CHAFED BY CONTACT WITH WING T/E LWR SURFACE. (C-CHECK) RO: 10/21/19. SERVICEABLE FLAP RECEIVED. WORK ACCOMPLISHED BY AAR.SDR SWIA2019102346590Skin · corrodedRH INBD FLAP LWR SKIN TOP COAT HAS ERROSION DAMAGE. (C-CHECK) RO: 10/21/19. RECEIVED SERVICEABLE FLAP. WORK ACCOMPLISHED BY AAR.SDR SWIA2019121847019Bushing · damagedLH AND RH OTBD FLAP HINGE ARMS AT WS220 HAS DAMAGED HARDWARE THAT REQUIRES REPLACEMENT (C-CHECK) RO 12/14/2019 INSTALLED SERVICEABLE HARDWARE ON R/H AND L/H OTBD FLAP AT WS 220 IAW AMM 57-53-02-400-803SDR SWIA2019121847013Hinge Arm · crackedRH FLAP HINGE ARM ASSY AT W.S. 220 HAS CRACKED ATTACHMENT BRACKET ON OUTBOARD SIDE (C-CHECK) RO:12/14/2019 FABRICATED AND INSTALLED IB AND OB RH FLAP HINGE ARM ASSY ATTACHMENT BRACKETS IAW CRJ200 SRM. SEE CONTINUATION CARD FOR WORK PERFORMED.SDR SWIA2019121847010Vane · chafedLEFT INBOARD FLAP VANE UPPER SKIN TRAILING EDGE IS CHAFED 2EA LOCATIONS APPROX. W.S.100 AND CHAFED AT W.S.56 (C-CHECK) RO:12/14/2019 REPAIRED IAW CRJ 200 SRM.SDR SWIA2019121847009Vane · chafedRIGHT INBOARD FLAP VANE UPPER SKIN TRAILING EDGE IS CHAFED 2EA. LOCATIONS APPROX. W.S.100 (C-CHECK) RO:12/14/2019 REPARIED.SDR IPXA2019102328155Skin · damagedINSPECTION TYPE:N/ART INBD MAIN FLAP LWR SKIN AND STRINGER DAMAGED.REMOVED DAMAGE. HFEC FOR CRACKS. PERFORMED STRINGER REPAIR. INSTALLED FILLER AND DOUBLER. COMPLETED EO A300-5750-74381A.SDR UIEA2019101105700Flap Track · corrodedEVIDENCE OF LIGHT SURFACE CORROSION ON ALL EIGHT FLAP TRACKS.(<P>FOR #4 AND #5 FLAP TRACK REPAIR, REF EI NO. T2019A57M-3693 REV. 1 AND T2019A57M-3700 REV.1. REFERENCE J/C ATTACHING SHEET FOR REPLACEMENT OF FLAP TRACKS #1, #2, #3, #6, # 7, AND #8. CONDITION CHESDR SWIA2019121847007Fairing · damagedL/H FLAP STUB FAIRING ASSY IS DAMAGED BEYOND REPAIR & FWD HALF-HINGE IS DAMAGED BEYOND REPAIR (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED LH FLAP STUB FAIRING AND FWD HINGE HALF IAW CRJ 200 SRM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED AND CLEARANCE SDR REXA2019111801633Access Panel · wornPART RACK. WEAR ON ACCESS PANEL 584ET, 684ET, 584EB, 684EB AT RH/LH FLAPS.
WEAR ON ACCESS PANEL 584ET, 684ET, 584EB, 684EB AT RH/LH FLAPS WAS BLENDED PER CRJ-900 SRM 51-12-00-001-001-A01. ORIGINAL THICKNESS IS 0.090"" ON ACCESS PLATE 684 EB AND 584 EB MAXIMUMSDR SWAA2019102238048Structure · separatedR/H WING OUTBOARD AFT FLAP INBOARD CORNER SEPARATED. / REPAIRED AFT FLAP PER SRM.SDR LR7A2019101872209Skin · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND THE RH OUTBOARD FLAP LOWER SKIN CRACKED AT OWFS249R. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1000064442.SDR LR7A2019101872208Skin · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND THE RH OUTBOARD FLAP LOWER SKIN CRACKED AT OWFS243R. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1000064441.SDR LR7A2019101872207Skin · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND THE RH OUTBOARD FLAP LOWER SKIN CRACKED AT OWFS32-54.5R NEAR EXISTING REPAIR. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1000064439.SDR LR7A2019101872205Skin · dentedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5301, FOUND THE RH INBOARD FLAP LOWER SKIN DENTED AT CWS130R, 6" FROM THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1000062306.SDR LR7A2019101872204Skin · gougedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5301, FOUND THE LH INBOARD FLAP UPPER SKIN GOUGED AT CWS124L. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12.SDR FDEA201910172682Skin · dentedLEFT WING O/B FLAP LOWER SKIN HAS NUMEROUS DENTS. REPAIRED LEFT WING O/B FLAP LOWER SKIN DENTS IAW B767 SRM: 57-53-01-01A, 51-70-00-2R, 51-70-07-2R-G, 51-70-07-0G, AMM: 51-61-00-0, 51-21-10-307-020, 51-21-10-07; H-2750-T0350063- P1 FLIGHT CONTROL-T/E FLAPSDR FDEA2019101762666Vane · corrodedLEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' MOUNT HOLE FOUND WITH CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' MOUNT HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. OSDR FDEA2019101762665Vane · corrodedLEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'B' MOUNT HOLE FOUND WITH CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'B' MOUNT HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. OSDR FDEA2019101762658Hinge · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 5SDR FDEA2019101762657Hinge · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44SDR IPXA2019101447852Skin · damagedINSPECTION TYPE:N/ALEFT WING O/B T/E FLAP UPPER SURFACE 0.25 HOLE. REPAIRED IAW EO B757-5750-74261-ASDR DALA2019102906267Fairing · missingRH WING INBOARD FLAP HINGE SECONDARY FAIRING MISSING. INSTALLED RT WING FLAP TRACK FAIRING PER ERA 580914-14 REV ORIGINAL. (LP5587434)SDR FDEA2019101422613Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-04. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-04, AND EA 1-5750-76649 A, PART 2, STSDR FDEA2019101422610Hinge Fitting · corrodedRIGHT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159802 G, PART 3,SDR FDEA2019101422609Hinge Fitting · corrodedRIGHT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159802 G, PART 3, SDR FDEA2019101422608Hinge Fitting · corrodedLEFT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159801 H, PART 3, S
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