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 FDEA202001100101Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. SDR FDEA202001100100Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVSDR AALA202002109007Attach Bracket · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING TRAILING EDGE INBOARD FLAP INTERCONNECTING STRUT ATTACHMENT BRACKET HAS EXCESSIVE PLAY / WEAR AT WX4476.559 AND RIB 14. REPLACED BRACKET PER SRM 51-72-11.SDR AALA202002109006Attach Bracket · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WING TRAILING EDGE INBOARD FLAP INTERCONNECTING STRUT ATTACHMENT BRACKET HAS EXCESSIVE PLAY / WEAR AT WX4476.559 AND RIB 14. REPLACED BRACKET PER SRM 51-72-11.SDR FDEA202001100099Hinge Fitting · corrodedLEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZED SDR FDEA202001100098Hinge Fitting · corrodedLEFT WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZSDR SWIA2020012047824Skin · corrodedRACK - RH FLAP PANEL - PANEL 633BB AFT AIRFRAME MOUNT BOLT IS CORRODED. (C-CHECK) RO:1/14/2020REMOVED AND REPLACED RH FLAP PANEL 633BB AFT AIRFRAMEMOUNT BOLT. REFERENCE AMM.SDR SWIA2020041050111Hinge Arm · chafedRIGHT OUTBOARD FLAP CENTER HINGE ARM HAS BARE METAL/CHAFE AT BOTTOM OF HINGE AREA. (C-CHECK) RO 4/9/2020 R/H OUTBOARD FLAP IS BEING REPLACED ON NR0219 CAMP# 20262710 FLAP ORDERED / RECIEVED ON REQ# 00028611SDR SWIA2020030348989Plate · chafed* THE RH OUTBD FLAP CENTER HINGE ARM SIDE PLATE IS CHAFFED. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CHAFED AND INSTALLED NEW RH OUTBD FLAP CENTER HINGE ARM SIDE PLATE REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020030348988Plate · chafed* THE RH INBD FLAP INBD HINGE ARM INBD SIDE PLATE IS CHAFFED. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW R/H INBD FLAP INBD HINGE ARM ONBD SIDE PLATE REF CRJ200 SRM. ALL CHECKS GOODSDR SWIA2020030348987Plate · chafed* THE RH INBD FLAP OUTBD HINGE ARM OUTBD SIDE PLATE IS CHAFFED. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW R/H INBD FLAP OUTBD HINGE ARM OUTBD SIDE PLATE REF CRJ200 SRM. ALL CHECKS GOOD.SDR SWIA2020030348986Plate · chafed* THE RH INBD FLAP OUTBD HINGE ARM INBD SIDE PLATE IS CHAFFED. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW R/H INBD FLAP OUTBD HINGE ARM INBD SIDE PLATE REF CRJ200 SRM. ALL CHECKS GOODSDR SWIA2020030348983Fastener · corroded* THE RH OUTBD FLAP INBD HINGE ARM LOWER FITTING FLAP SIDE HAS CORRODED HARDWARE. (C-CHECK) RO 2/28/2020 REMOVED THE ANTI-ROTATION KEEPER (CORRODED HARDWARE) FROM THE INBD HINGE ARM OF THE R/H OUTBD FLAP. REF: CRJ 200 AMM. REMOVED THE CORRODED HARDWARE FRSDR SWIA2020030348982Fastener · corroded* THE RH OUTBD FLAP INBD HINGE BOX HAS CORRODED HARDWARE. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED 4EA SCREWS AND 4EA WASHERS LOACTED ON ON RH OUTBOARD FLAP, INBOARD MOST HINGE REF CRJ-200 SRM.SDR SWIA2020030348981Fastener · corroded* THE RH OUTBD FLAP CENTER HINGE ARM HAS CORRODED HARDWARE FOR KEEPER PLATE. (C-CHECK) RO 2/28/2020 REMOVED THE ANTI-ROTATION KEEPER (CORRODED HARDWARE) FROM THE CENTER HINGE ARM OF THE R/H OUTBD FLAP. REF: CRJ 200 AMM. INSTALLED THE ANTI-ROTATION KEEPER SDR SWIA2020030348915Hinge · corroded* THE RH OUTBD FLAP MIDDLE HINGE BOX HAS CORROSION ON THE AFT SIDE. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM RH OUTBD FLAP MIDDLE HINGE BOX AND FOUND REWORKED AREA ACCEPTABLE AS IS REF REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**SDR SWIA2020030348914Hinge · corroded* THE RH OUTBD FLAP INBD HINGE BOX HAS CORROSION ON AFT SIDE. (MARKED). (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM RH OUTBD FLAP INBD HINGE BOX AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RSDR SWIA2020030348913Hinge Arm · chafed* THE RH OUTBD FLAP CENTER HINGE ARM IS CHAFFED. (MARKED) (C-CHECK) RO 2/28/2020 PERFORMED BLEND OUT REPAIR TO CHAFE ON THE RH OUTBD FLAP CENTER HINGE ARM. REF: BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020021848738Intercostal · dentedWHILE PERFORMING DENT REPAIR OF LH INBD FLAP, MIDDLE SPAR INTERCOSTAL P/N CC670-14120-1 FOUND TO HAVE DENT DAMAGE. (C-CHECK) RO:2/14/2020REMOVED AND REPLACED WITH NEW PART REF CRJ 700 SRM.SDR DALA2020010900176Cover · missingRIGHT FLAP TRACK 5 FAIRING INBOARD AFT COVER MISSING. REPLACED FAIRING COVER. LP 722746SDR DALA2024012401104Skin · dentedDENT INSPECTION RHS AFT MOVABLE VANE, UPPER SKIN - QTY 6. #5) APPROX 25" FROM O/B EDGE & 4.5" FROM T/E. 5) DENT DIMENSIONS WIDTH 1.3" X DEPTH 0.024" APPROX 25" FROM O/B EDGE & 4.5" FROM T/E. IAW B717 SRM 57-53-01 AD 1 ACCOMPLISH DVI AND TAP TEST FOR POSSIBLE DSDR SWIA2020030348912Attach Fitting · gougedLEFT WING OUTBOARD FLAP BOX ATTACH FITTINGS #4 AFT INBOARD SIDE HAS A GOUGE AS MARKED. (C-CHECK) RO 2/28/2020 PERFORMED ALL STEPS OF BLEND OUT REPAIR TO GOUGE LEFT WING OUTBOARD FLAP BOX ATTACH FITTINGS #4 AFT INBOARD SIDE. REF CRJ 200 & BOMBARDIER REO. SSDR SWIA2020030348911Attach Fitting · gougedLEFT WING FLAP BOX ATTACH FITTINGS #1 AFT INBOARD HAS A GOUGE APPROX WS56.03 AS MARKED (C-CHECK) RO 2/28/2020 PERFORMED ALL STEPS OF BLEND OUT REPAIR TO GOUGE ON LEFT WING FLAP BOX ATTACH FITTINGS #1 AFT INBOARD APPROX WS56.03. REF. CRJ 200 & BOMBARDIER RESDR SWIA2020020648273Vane · chafedCHAFE ON L/E OF LH I/B FLAP VANE AT WS 139.90 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED L/E SKIN AT WS 139.90 ON L/H INB FLAP VANE IAW CRJ 200 SRM, AND SEALED L/E AREA IAW CRJ 200 SRM.SDR SWIA2020020648272Vane · chafedCHAFE ON L/E OF LH I/B FLAP VANE AT WS 104.00 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED L/E SKIN AT W.S. 104.00 ON L/H INB FLAP VANE IAW CRJ 200 SRM, WHOLE L/E SKIN CHANGED FROM WS 104.00 TO WS 120.30. SEALED L/E AREA IAW CRJ SDR SWIA2020020648270Vane · chafedCHAFFE ON L/E OF LH I/B FLAP VANE SKIN AT WS 56.00 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED L/E FLAP VANE AT W.S. 56.00 ON L/H INB FLAP VANE IAW CRJ 200 SRM, AND SEALED AREA IAW CRJ 200 SRM.SDR SWIA2020013148029Skin · wornLEFT OUTBOARD FLAP, UPPER SURFACE, TRAILING EDGE PREVIOUSLY INSTALLED CHERRY MAX RIVETS FS245 TO FS235 APPEAR TO BE WORN AND HAVE RECESSED BELOW THE UPPER SURFACE OF THE FLAP SKIN. (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED 10EA. BLIND RIVETS ON THE T/ESDR AALA202001159024Flap Track · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING #1 FLAP TRACK OUTBOARD SIDE HAS THICKNESS AND WIDTH REDUCTOIN. REPLACED FLAP TRACK PER AMM 57-54-21-400-801-B/400.**SUPPLEMENTAL REPORT TO ADD PART NUMBER TO SECTION 5**SDR RAIA2020011580003Shroud · not reportedR&R LH O/B FLAP O/B SHROUD I/B AFT HINGE HALF.SDR RAIA2020011580002Hinge · crackedLH O/B FLAP O/B SHROUD I/B FWD HINGE HALF CRACKED- REMOVED LH O/B FLAP SHROUD. REMOVED DAMAGED HINGE. LOCATED AND DRILLED AND INSTALLED NEW HINGE ON SHROUD. INSTALLED LH O/B FLAP SHROUD.SDR DALA2020010900165Skin · wornR/H WING I/B AFT FLAP HAS WORN AREA AT UPPER SURFACE AT I/B END OF FLAP. REPAIRED PER SRM 51-70-10. (LP 1436471)SDR SWIA2020031049113Panel · gougedLEFT HAND FLAP PANEL 584GB IS GOUGED (C-CHECK) RO 3/6/2020 REMOVED GOUGE FOUND OUT OF LIMITS. LOCATED AND DRILLED NEW LH FLAP PANEL 584GB. REF: CRJ900 SRM.SDR SWAA2021070712898Plate · looseLH WING TRAILING EDGE FLAPWELL LOWER INSPAR SKIN WIGGLE PLATE FASTENERS ARE LOOSE / BROKEN AT RSS 255-266. / REMOVED AND INSTALLED A NEW L/H WING T/E EDGE FLAP WELL LOWER SPAR SKIN WIGGLE PLATE AT RSS 255-266 IAW B737-700 SRM 51-40-02-OG-0SDR SWIA2020030348993Mount · chafed* RIGHT WING OUTBOARD FLAP VANE MOUNTS ARE CHAFFED / GALLED AT 4 PLACES. MARKED. (C-CHECK) RO 2/28/2020 REMOVED GOUGED OUT OF LIMITS VANE ASSY AND INSTALLED NEW RH OUTBOARD FLAP VANE ASSY. PART # 601R14502-2. REF CRJ200 SRM AND BOMBARDIER DWG. SEE ATTACHESDR SWIA2020030348908Skin · chafed* RIGHT WING INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED AT 3 SPOTS. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW RH INBD FLAP INBD FLAP VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020030348907Skin · chafed* LEFT WING INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED AT 3 SPOTS. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW LH INBD FLAP INBD FLAP VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020020648275Vane · chafedCHAFE ON L/E OF RH I/B FLAP VANE SKIN AT WS 139.90 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED R/H, I/B FLAP VANE L/E, AT W/S 139.90, PER CRJ-200, SRM TR 51-42SDR SWIA202020648274Vane · chafedCHAFFE ON L/E OF RH I/B FLAP VANE SKIN AT WS 104.00 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED R/H, I/B FLAP VANE L/E PER CRJ-200, SRM TR 51-42 AT W/S 104.00.SDR SWIA2020020648271Vane · chafedCHAFFE ON L/E OF RH I/B FLAP VANE SKIN AT WS 56.00 FOUND TO BE OUT OF LIMITS (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED L/E ON R/H I/B FLAP VANE AT WS 56.00 IAW CRJ 200 SRM.SDR SWIA2020020648269Vane · chafedCHAFING MARKS ON L/E OF RH I/B FLAPS VANE SKIN AT WS 56.00,WS 104.00 AND WS 139.90 (C-CHECK) RO 2/04/2020 ALL THREE AREAS CHAFING AT WS 56.00 WS 104.00 AND WS 139.90 ARE OUT OF LIMITS (OVER .030 MATERIAL LOSS) PER BOMARDIER REO EFFECTIVITY CL601R ALL. SEE SDR SWIA2020020648268Vane · chafedCHAFING MARKS ON L/E OF LH I/B FLAPS VANE SKIN AT WS 56.30,WS 104.00 AND WS 139.90 (C-CHECK) RO 2/04/2020 ALL THREE AREAS CHAFFING AT WS 56.3, WS104.00 AND WS 139.90ARE OUT OF LIMITS (OVER .030 MATERIAL LOSS. PER BOMBARDIER REO EFFECTIVITY ALL. SEE NR# 500SDR FDEA202001060025Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE 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 FDEA202001060024Bracket · 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 DALA2020010900161Flap · damagedLEFT OUTBD FLAP HAS DELAMINATION SPOT FOUND TO BE MISSING POTTING REMOVED OLD POTTING REPAIRED PER SRM 51-70-01. (LP 6376416)SDR DALA2020010600068Strut · corrodedCORROSION INTERCONNECTING STRUT IB FLAP ON RH WING (1 EA). REPLACED INTERCONNECTING STRUT IB FLAP ON RH WING (1EA) AS PER A320 FAM AMM 27-51-44-400-001-A AND PERFOMED OPERATIONAL TEST OF THE FLAPS SYSTEM AS PER A320 FAM AMM 27-54-00-710-001-A TEST IS GOOD.SDR FDEA202001050021Skin · dentedMAINT FOUND A MINOR DENT OF THE LE OF THE RH OUTBOARD FLAP; ABOUT 4" LONG X 1" WIDE REPAIRED AREA USING EA H-5750-T0351730 PART 1,SDR SWIA2020030548995Skin · dentedADM #1971. LEFT INBD FLAP ON THE BOTTOM SIDE SKIN, FLS 30.00+36.00. SMALL DENT THAT MEASURES 1" X 1" X .050" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 3/3/202SDR FDEA2020010650021Skin · dentedMAINT FOUND A MINOR DENT OF THE LE OF THE RH OUTBOARD FLAP; ABOUT 4" LONG X 1" WIDE REPAIRED AREA USING EA H-5750-T0351730 PART 1,SDR SWAA2020010840253Flap · delaminatedL/H WING OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED ON PREVIOUS REPAIR ON LOWER SURFACE. / REPAIRED AFT FLAP IAW SRM.SDR SWAA2020010740208Skin · delaminatedL/H WING OUTBOARD AFT FLAP INBOARD AFT LOWER SKIN CORNER DELAMINATED. / R&R L/H AFT FLAP ASSEMBLY PER AMM.
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