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 DALA2020010600067Bolt · corrodedCORROSION FLAP TRACK 3 AND 4 INNER PIVOT BOLT ON LH WING (2 EA) REFERENCE RII AMDS CARD 2750-4001S - LT. REPLACED INER PIVOT BOLT OF FLAP TRACK 3 AND 4 L/H WING AS PER A320 FAM AMM 27-54-62-400-001-A AND PERFORMED OPERATIONAL TEST FLAP SYSTEM AS PER A320 FAM ASDR DALA2020010600066Bolt · crackedCRACK FLAP TRACK 3 OUTER PIVOT BOLT CHOMIUM PLATING WITH CRAK ON RH WING REFERENCE RII AMDS CARD 2750-4001S-RT. REPLACED FLAP TRACK 3 OUTER PIVOT BOLT ON R/H WING AS PER A320 FAM AMM 27-54-62-400-001-A AND PERFORMED OPERATIONAL TEST FLAP SYSTEM AS PER A320 FAMSDR SWIA2020013148027Fastener · loose*MULTIPLE LOOSE FASTENERS ON L/H OTBD FLAP UPPER SURFACE AT THE MID SECTION. MARKED WITH RED GREASE PENCIL. (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED MULTIPLE RIVETS ON THE LH OTBD FLAP UPPER SKIN REF REO. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARSDR DALA2020010800128Cover · missingDURING WALK AROUND FOUND A FLAP TRACK FAIRING COVER MISSING FROM MOVEABLE FAIRING NBR 5 ON RIGHT HAND, ZONE 634 COVER FIN 634CR. DEFERRED PER CDL 57-00-07-REPLACED CAP ON NBR 5 RIGHT FLAP TRACK FAIRING. LP 6678931SDR DALA2020010200008Skin · dentedR/H O/B FLAP LOWER SURFACE HAS DENT FROM I/B EDGE 57 INCH CROSS L/E 13 INCH. C/A R/H O/B FLAP LOWER SURFACE REPAIRED AS PER B767-400 SRM 57-53-01 -2R-1 & SRM 51-70-03, RELEASE 58.00 (1426778)SDR SWAA2022030148405Flap · delaminatedLEFT HAND WING INBOARD MAIN FLAP LOWER O/B SURFACE DELAMINATED / REMOVED $ REPLACED L/H I/B MAIN FLAP IAW B737 AMM 27-51-11-000-801 & AMM 27-51-11-400-801. ADJUSTMENT CHECK IS GOOD IAW B737 AMM 27-51-11-820-801. (POS:LH; TAG NO:547763; P/N OFF:113A2100-71; S/NSDR SWIA2020020648252Vane · chafedR/H INBD. FLAP VANE (INBD. L/E CHAFFED) (C-CHECK) RO 2/04/2020 RH INBOARD FLAP REPLACED WITH A SERVICEABLE UNIT AND WORK ACCOMPLISHED ON JOB 2785691 OP 94 (MX TRANS# 20197325).SDR SWIA2020020648251Vane · chafedR/H INBD. FLAP VANE (OUTBD. L/E CHAFFED) (C-CHECK) RO 2/04/2020 RH INBOARD FLAP REPLACED WITH A SERVICEABLE UNIT AND WORK ACCOMPLISHED ON JOB 2785691 OP 94 (MX TRANS# 20197325).SDR SWAA2020011340408Skin · delaminatedL/H WING INBOARD MAIN FLAP LOWER OUTBOARD SURFACE DELAMINATED. / R&R MAIN FLAP IAW AMM.SDR ASOA2020030403024Skin · damagedDURING C CHECK INSPECTION RIGHT INBOARD FLAP UPPER SURFACE HAS DAMAGED COMPOSITE AT INBOARD EDGE. MAINTENANCE REPAIRED COMPOSITE DAMAGE AT UPPER SKIN INBOARD EDGE I/A/W SRM 57-52-00.SDR SWIA2020021848662Skin · dentedEVALUATE DENT ON BOTTOM OF THE LEFT INBD. FLAP. (MARKED) (C-CHECK) RO:2/14/2020REPAIRED LH I/B FLAP DENT DAMAGE AS PER CRJ 700 SRM. COMPLIED WITH AND SWA M-337 FOR MAJOR REPAIR.SDR AALA2020010319037Spar · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT WING OUTBOARD TRAILING EDGE FLAP ON AFT SPAR 8 INCHES INBOARD OF RIB 5A. REPLACED FLAP PER TASK CARD 26L00027009.SDR DALA2019123107667Fitting · damagedL/H INBD FLAP TRUNNION FITTING FOUND DAMAGED BEYOND REPAIR, REPLACED L/H INBD FLAP TRUNNION FITTING PER ERA 584216-14AD REV " O"SDR SWIA2020012147951Door · wornREPLACE WORN BUTE DOOR CAM ON L/H OUTBOARD FLAP VANE AT WS296. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED NEW BUTE DOOR CAM P/N 601R14560-5 ON L/H OUTBOARD FLAP VANE. REF: DWG AND SWA M-337.SDR SWIA2020021448503Beam · chafedRH INBD FLAP VANE INBD ACTUATOR SLIDING BEAM CHROME SURFACE CHAFED BY CONTACT WITH ROLLER. (C-CHECK) RO 2/10/2020 RMEOVED AND REPLACED RH IB FLAP ASSY IAW CRJ200 AMM. RIG AND OPS C/W ON CP# 20005908 W/O 1018130 6000 0011 AND CP# 20005909 W/O 1018130 6000 0SDR IPXA2020011350846Skin · gougedINSPECTION TYPE:C2GOUGE ON EXISTING REPAIR OF TOP PANEL OF RH OUTBD AFT FLAPREPAIR I.A.W BOEING SRID : 3-4592189605 AND UPS EO B747-5750-64795-BSDR SWAA2020010840252Flap · delaminatedL/H WING OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED ON PREVIOUS REPAIR. / REPAIRED AFT FLAP IAW SRM.SDR LR7A2019123082222Skin · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB2703, FOUND THE LH OUTBOARD WING FLAP LEADING EDGE CRACKED AT OWFS84L. REPAIRED IAW SMP583 SRM FIG. 51-140-12.SDR SWAA2022022435325Flap · delaminatedLEFT WING; OUTBOARD AFT FLAP; LWR INBD CORNER IS DELAMINATED. / REPAIRED DAMAGE ON L/H O/B AFT FLAP INBD CORNER. BONDED REPLACEMENT CORE AND REPAIR DOUBLER AND CURED. TAP TEST GOOD. RESTORED PROTECTIVE FINISH. IAW B737-800SRM 57-53-01-2R-4 REV 68; SRM 51-70-10SDR SWAA2020010840272Flap · delaminatedL/H WING OUTBOARD AFT FLAP, LOWER INBOARD CORNER DELAMINATED. / REPAIRED AFT FLAP IAW SRM.SDR NACA2109123024152Bolt · corrodedLEFT WING OUTBOARD FLAP OUTBOARD GIMBAL BUSHING RETENTION BOLT CORRODED. REPLACED THE LEFT WING OUTBD FLAP OUTBAORD GIMBAL BUSHING AND RETENTION BOLT IAW AMM 27-51-37 REV 90.SDR NACA2019123024151Bushing · wornLEFT WING OUTBOARD FLAP, OUTBOARD FOREFLAP SEQUENCE CARRIAGE HARDWARE WAS CORRODED AND BUSHINGS WORN. THE HARDWARE & BUSHINGS WERE REPLACED IAW AMM 27- 51-37 C (2) (A), REV 90.SDR DALA2019122747577Skin · crackedCRACK ON UPPER SKIN AT RH OUTBD MAIN FLAP STA WS=509 APROX AT RT WING. CRACK ON UPPER SKIN AT RH OUTBD MAIN FLAP STA WS=509 APROX AT RH WING WAS REPAIRED PER B-757 S.R.M. (1415444)SDR SWIA2020012147947Skin · chafedRH FLAP UPPER SKIN PANELS 684AT AND 684BT ARE CHAFFED. (C-CHECK) RO:1/17/2020REMOVED AND INSTALLED 2 EA NEW PANELS 684AT AND 684BT. REF CRJ 200 SRM. / FABRICATED NEW PANELS P/N 601R14007-52 (684AT) AND 601R14007-54 (684BT) USING 2024-T3 .080" PO# T522SDR DALA2019122537539Fairing · damagedDURING INSPECTION, FOUND THE LEFT INBD FLAP TRACK FAIRING TAILCONE MISSING. REPLACED BROKEN AND MISSING NUTPLATES AND REINSTALLED FLAP TRACK FAIRING TAILCONE IAW DRAWING 1113A9352.SDR SWAA2019123039991Plate · crackedL/H WING TRAILING EDGE INBOARD OF THE #3 FLAP TRACK WIGGLE PLATE CRACKED. R&R WIGGLE PLATE REF SRM.SDR FDEA2019122313276Skin · chafedREWORK REQUIRED OF EA F-5750-T0351491 PT1 STEP 3. REPAIR ACCOMPLISHED IAW SRM 57-53-01-2R REPAIR 2 AND EA F-5750-T0351491 A P1 WING - FLIGHT SURFACES. RT INBOARD MAIN FLAP LEADING EDGE SKIN REPAIR.SDR ABXR2019122100332Beam · corroded#2 FLAP 1-2-3 BEAM CODE C HOLES CORRODEDSDR FDEA2019122093264Bracket · corrodedLEFT HAND WING INBOARD FLAP INBOARD DRIVE ROD FITTING HOLE FOUND CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP INBOARD DRIVE ROD FITTING HOLE REWORKED AS PER SRM 51-21-01-OG AND FOUND EXCEED LIMIT AS PER DRAWING ARC2761. REPLACEMENT BUSHINGS 02 EACH FASDR SWIA2020013147992Vane · chafed* L/H INBD FLAP VANE OUTBD L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 BLEND LEFT I/B FLAP VANE O/B CAP REF REO. FOUND TO BE OUT OF LIMITS REF REO. REMOVED AND REPLACED VANE CAP REF CRJ200 SRM, BOMBARDIER DRAWING. COMPLIED WITH SKY CARD.SDR SWIA2020013147991Skin · chafed* L/H INBD FLAP VANE MIDDLE L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED WITH NEW 1EA. L/H I/B FLAP MIDDLE L/E VANE CAP (P/N 601R14303-51S). REF CRJ200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD.SDR SWIA2020013147990Vane · chafed* R/H INBD FLAP VANE OUTBD L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 BLENDED RH INBOARD FLAP VANE OUTBOARD LE CAP CHAFE REF. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH INBOARD FLAP VANE OUTBOARD LE CAP REF BOMBARDIER DWG AND CRJ200 SDR SWIA2020013147989Vane · chafed* R/H INBD FLAP VANE MIDDLE L/E CAP IS CHAFFED, (FLAGGED) (C-CHECK) RO 1/28/2020 BLENDED RH INBOARD FLAP VANE MIDDLE LE CAP CHAFE REF REO. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH INBOARD FLAP VANE MIDDLE LE CAP REF BOMBARDIER DWG AND CRJ200SDR SWIA2020013147988Vane · chafed* R/H INBD FLAP VANE INBD L/E CAP IS CHAFFED, (FLAGGED (C-CHECK) RO 1/28/2020 BLENDED RH INBOARD FLAP VANE INBOARD LE CAP CHAFE REF REO. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH INBOARD FLAP VANE INBOARD LE CAP REF BOMBARDIER DWG AND CRJ2SDR AALA202001239029Skin · debondedAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE SKIN EXISTING REPAIR DOUBLER IS DEBONDED BETWEEN RIB 12-13 AND 12 INCHES FROM THE TRAILING EDGE . REPAIRED FLAP LOWER SURFACE SKIN PER SRM 57-54-00-300-005 AND EA 265778B.SDR DALA2019121607346Skin · dented(LOG 1404684) DURING INSPECTION FOUND SEVERAL DENTS ON AFT I/B FLAP UPPER AND LOWER SURFACE AT RH WING. AFT I/B FLAP LOWER SURFACE AT RH WING WAS REPAIRED PER. B737-800 SRM 51-70-10.SDR FDEA2019121753246Guide · crackedLEFT WING ,OUTBOARD FLAP,AFTFLAP,INBOARD TRACK,GUIDE CRACKED. REPAIRED LEFT WING ,OUTBOARD FLAP,AFT FLAP,INBOARD TRACK,GUIDE CRACKED BY REMOVING DAMAGE AND APPLYING HOT BOND FIBERGLASS OVERLAY REPAIRS IN 2 EACH AREAS ,CURING,SHAPING AND RESTORING FINISH IASDR SWAA2022030148130Flap · delaminatedL/H I/B MAIN FLAP LOWER SURFACE IS DELAMINATED ON O/B END / UPON EVALUATION OF DELAMINATED AREA ON L/H I/B MAIN FLAP LOWER SURFACE O/B END FOUND IT BEYOUND ALLOWABLE LIMITS OF B737 SRM 57-53-01-1A-1. REPAIRED I-A-W SRM 57-53-01-22-7 AND 51-20-10-2R-4 AND 51-70SDR SWAA2022030148131Flap · delaminatedR/H I/B MAIN FLAP LOWER SURFACE IS DELAMINATED ON O/B END / REPAIRED DELAMINATION DAMAGE ON LOWER SURFACE OF R/H I/B MAIN FLAP IAW 737 SRM 57-53-01-2R-7 AND SRM 51-70-10-2R-4SDR SWAA2019123039947Skin · delaminatedR/H INBOARD MAIN FLAP LOWER SURFACE DELAMINATED ON OUTBOARD END. REPAIRED MAIN FLAP IAW SRM.SDR SWAA2019123039946Skin · delaminatedLEFT INBOARD MAIN FLAP LOWER SURFACE DELAMINATED ON OUTBOARD END. REPAIRED THE MAIN FLAP IAW SRM.SDR IPXA2019121850170Hinge Fitting · corrodedINSPECTION TYPE:SVR/H O/B FLAP UPPER O/B ACTUATOR ATTACH LUG HAS PITTING CORROSION IN THE BORE.REPAIRED CORRODED R/H FLAP UPPER O/B ATTACH LUG IAW UPS EO MD11-5740-74906-B.SDR SWAA2022030111439Wedge · delaminatedL/H I/B MAIN FLAP HAS DELAMINATION AT MOST O/B T/E WEDGE. / INSTALLED NEW L/H I/B MAIN FLAP O/B T/E WEDGE PER SOPM 20-50-01.SDR FDEA2019121323233Skin · gougedRT WING OB FLAP L/E HAS GOUGE. BLENDED GOUGE FOUND AREA OUT OF LIMITS. RT WING O/B FLAP L/E SKIN IAW SRM 57-53-01-1A FIG 101 DET I, REMOVED EXISTING REPAIR SKIN PLATE IAW SRM 51-40-02-OG. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SKIN REPAIR PART IAW SSDR SWIA2020020348136Vane · chafed* R/H INBD FLAP VANE L/E HAS CHAFFED ON OUTBD SIDE (C-CHECK) RO:1/29/2020INSTALLED R/H INBD FLAP VANE L/E . P/N 601R14303-44 REF CRJ 200 SRM AND BOMBARDIER DWG.SDR SWIA2020020348135Vane · chafed* R/H INBD FLAP VANE L/E HAS CHAFFED ON MIDDLE SIDE (C-CHECK) RO:1/29/2020INSTALLED NEW R/H INBD FLAP VANE L/E MIDDLE SIDE . P/N 601R14303-52 . REF CRJ200 SRM AND BOMBARDIER DWG.SDR SWIA2020020348133Vane · chafed* L/H INBD FLAP VANE L/E IS CHAFFED OUTBD EDGE (C-CHECK) RO:1/29/2020L/H INBD FLAP VANE L/E (OUTBD) IS OUT OF LIMITS AND REPLACED WITH NEW REF BOMBARDIER DWG CRJ 200 SRM AND SEE CONTINIUATION CARD FOR DETAILSSDR REXA2019122011727Skin · dented"RH IB FLAP LOWER T/E SKIN DENTED. MARKED WITH TAPE.
""C/W FALP REPAIR AT 2 LOCATIONS ON LOWER SURFACE OF RH IB FLAP IAW CRJ700 SRM 57-52-01-201-001-A01. WVAC EMP 712 STAMP
"SDR A6WA2019121847067Vane · gougedL/H I/B FLAP VANE L/E BETWEEN FLAP STA 69.631-FLAP STA 79.257 HAS GOUGE DAMAGE. AIRCRAFT REMOVED FROM SERVICE CUT OUT DAMAGED SKIN ON L/H I/B FLAP VANE AT FLAP STA 77.5 . CUTOUT DIMENSIONS ARE 1.3"W X .7"L . FABRICATED FLAP VANE INSERT AND VANE BUTT STRASDR FDEA2019121313222Skin · chafedR/H WING INBD FLAP LWR L/E SURFACE HAS 2EA GOUGES AT THE INBD HINGE WHERE THE AERODYNAMIC COVER PANEL MAKES CONTACT (INBD AND OTBD OF THE LUG FITTINGS) REPAIRED R/H WING INBD LWR L/E SURFACE AT THE INBD HINGE WHERE THE AERODYNAMIC COVER PANEL MAKES CONTACT
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