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 SWIA2020033049540Vane · chafedLEFT HAND INBOARD FLAP VANE €“ LEADING EDGE INBOARD €“ CHAFED (MARKED) (C CHECK) RO 3/27/2020 BLENDED, REMOVED, REPLACED AND RESTORED FINISH OF THE LEFT HAND INBOARD FLAP VANE LEADING EDGE CAP REF CRJ200 SRM.SDR SWIA2020033049538Vane · damagedRH INBOARD FLAP VANE LEADING EDGE INBOARD, MID, OUTBOARD SIDE AND INBOARD END HAS ABRASION DAMAGE AS MARKED. (C CHECK) RO 3/27/2020 BLENDED OUT CHAFFING TO A SMOOTH CONTOUR ON THE RH FLAP VANE IB END 2 AREAS REF CRJ 200 SRM AND THE IB LEADING EDGE CAP REF SDR SWIA2020032649355Hinge Arm · gouged* RH INBOARD FLAP INBOARD HINGE ARM GOUGED AT ATTACHMENT TO HINGE BOX (MARKED). (C-CHECK) RO 3/25/2020 BLENDED GOUGE ON RH INBOARD FLAP INBOARD HINGE ARM AT ATTACHMENT TO HINGE BOX REF CRJ-200 SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM. RSDR REXA2020021260210Vane · dentedLH INBD FLAP VANE CHAFED 1""L X .5""W JUST OTBD OF ACCESS PANEL 584ET.
REMOVED AND REPALCED LH FLAP VANE INBD L/E ON INBD FLAP IAW CRJ 200 SRM 51-40-11, 51-42-10 AND 51-25-16.SDR SWIA2020033049707Vane · chafedLH INBD FLAP, FLAP VANE MACHINED T/E CHAFED AT 3EA LOCATIONS BY CONTACT WITH WING T/E AT FLS104.5 TO FSL99.0 AND AT FSL55.5. (C-CHECK) RO:3/26/2020REAPAIRED FLAP VANE AT 3 LOCATIONS IAW BOMBA REO.SDR SWIA2020033049706Skin · chafedLH INBD FLAP, FLAP VANE L/E SKIN CHAFED BY CONTACT WITH BUMP BLOCK AT FLS57.0 (C-CHECK) RO:3/26/2020REMOVED & REPLACED FLAP VANE SKIN IAW CRJ200 SRM.SDR SWIA2020033049705Skin · chafedLH INBD FLAP, FLAP VANE L/E SKIN CHAFED BY CONTACT WITH BUMP BLOCK AT FLS104.5 (C-CHECK) RO:3/26/2020REMOVED DAMAGED SKIN,INSTALLED NEW SKIN IAW CRJ SRM.SDR SWAA2020021741419Plate · corrodedWIGGLE PLATE ABOVE #3 FLAP TRACK CRACKED. / REMOVED AND REPLACED WIGGLE PLATE ABOVE #3 FLAP TRACK PER SRM 51-40-02 .SDR SWAA2020021741418Plate · crackedWIGGLE PLATE ABOVE #6 FLAP TRACK CRACKED. / REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.SDR SWAA2020021041188Plate · crackedL/H WING WIGGLE PLATE ABOVE #3 FLAP TRACK CRACKED. / R&R WIGGLE PLATE PER SRM.SDR SWAA2020021041187Plate · crackedR/H WING WIGGLE PLATE ABOVE #6 FLAP TRACK CRACKED. / R&R WIGGLE PLATE PER SRM.SDR SWAA2021081926666Turnbuckle · corrodedRIGHT WING AFT SIDE OF LANDING GEAR WALKING BEAM JUST I/B OF # 6 FLAP TRACK FAIRING 2 EACH PANEL SUPPORT ROD ENDS CORRODED. RSS 209 / CONFIRMED EFFECTIVITY OF (2) TURN BUCKELS IAW 737 B IPC 57-50-00-22 ITEM #8 PN # 115A2950-62; REMOVED AND INSTALLED 2 NEW TURNSDR SWIA2020030348968Cap · damagedREPLACE LH INBD FLAP CENTER OTBD LEADING EDGE VANE CAP (C-CHECK) RO 2/28/2020 BLENDED LH INBD FLAP CENTER OTBD LEADING EDGE VANE CAP REF CRJ200 SRM. ORIGINAL THICKESS 0.050", REMAINING THICKNESS 0.00", 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS. REPLACSDR HALA2020020730051Cover · missingDURING PDC FOUND COVER ON FLAP TRACK FAIRING 631CB MISSING. APPLIED SPEED TAPE AND DEFERRED PER CDL 57-07 UNTIL FLAP TRACK FAIRING COVER IS AVAILABLE TO REPLACED. LP 7240659SDR HALA2020020400027Cover · missingOPEN - ON PDC FOUND COVER ON FLAP TRACK FAIRING (631 CB) MISSING. (RIGHT WING).SDR SWAA2021081723010Strap · damaged#6 FLAP FAIRING AFT TAIL CONE SPLICE STRAP HAS DAMAGED HOLES / REMOVED AND REPLACED WITH NEW SPLICE STRAPS ON #6 FLAP FAIRING AFT TAIL CONE USING 2024 T3 .063 LOT # 5086648-1 IAW SRM 51-40-05; SRM 51-40-02 AND DWG 113A9352SDR SWIA2020042450292Spring · corrodedLEFT WING #3 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #3 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING IAW CRJ 200 AMM.SDR SWIA2020042450291Spring · corrodedLEFT WING #4 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #4 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRIING IAW CRJ200 CMM.SDR SWIA2020042450290Bolt · corrodedLEFT WING #3 FLAP HINGE BOX AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #3 FLAP HINGE BOX AFT ATTACHING HARDWARE IAW CRJ200 AMM TASK TOOL = STS-2250 S/N = AB77460 CAL DUE = 25NOV20SDR SWIA2020042450289Fastener · corrodedLEFT WING #4 O/B FLAP HINGE BOX AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #4 OUTBOARD FLAP HINGE BOX AFT ATTACHING HARDWARE IAW CRJ200 AMM TOOL = STS-2250 S/N = AB77460 CAL DUE = 25NOV20SDR SWIA2020042450288Fastener · corrodedLEFT WING #5 O/B FLAP HINGE BOX AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #5 O/B FLAP HINGE BOX AFT ATTACHING HARDWARE IAW CRJ200 AMM TOOL = STS-2250 S/N = AB77460 CAL DUE = 25NOV20SDR SWIA2020041050085Support Bracket · crackedR/H OUTBOARD FLAP CENTER HINGE SUPPORT BRACKET FOUND TO BE CRACKED. REF CAMP # 20390223 (C-CHECK) RO 4/9/2020 R/H OUTBOARD FLAP IS BEING REPLACED ON NR0219 CAMP# 20262710 FLAP ORDERED/RECIEVED ON REQ# 00028611SDR EE4Y202002010585Skin · wornLH WING O/B MID FLAP LOWER SURFACE WITH WEAR AT WBL 255. THE MENTIONED PART WAS REPAIRED IAW BOEING ID #3-4620339317 AND COOPESA E.O. COO-EO-2020-10540-R01SDR SWIA2020042450286Fastener · corrodedRIGHT WING #5 FLAP HINGE ARM ASSEMBLY AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACEDR/H WING #5 FLAP HINGE ARM ASSEMBLY AFT ATTACHING HARDWARE IAW CRJ200 AMM TW:ID STS 2250 / CAL DUE:25 NOV 2020SDR SWIA2020042450285Fastener · corrodedRIGHT WING #4 FLAP HINGE ARM ASSEMBLY AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED R/H #4 HINGE ARM ASSEMBLY AFT ATTACHING HARDWARE IAW CRJ200 AMM.SDR SWIA2020042450284Fastener · corrodedRIGHT WING #4 FLAP HINGE ARM ASSEMBLY FWD ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED R/H WING #4 FLAP HINGE ARM ASSEMBLY FWD ATTACHING HARDWARE IAW CRJ 200 AMM. TW; STS 2250 CAL DUE;25 NOV 20SDR SWAA2020021741421Plate · crackedWIGGLE PLATE IS CRACKED AT ATTACH FASTENER INBOARD OF #6 FLAP TRACK. / REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.SDR V0XD20200217001Skin · dentedRH INBRD FLAP DENTED ON LOWER SKIN AND RIB BETWEEN FLS. 30.00 AND 36.00 APPOXIMATLEY 9.1 INCHES FROM TRAILING EDGE . CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR TO RH INBRD FLAP LOWER SKIN BY CUTTING OUT DAMAGED SKIN, FABRICATING AND INSTALLING REPPAIR PASDR AALA202002079032Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP SKIN SURFACE HAS DEBONDED AREA BETWEEN RIB 3 AND RIB 4 45 INCHES FROM THE IBOARD EDGE. REPAIRED FLAP PER SRM 57-54-00-300-005.SDR SWAA2020020651092Plate · crackedR/H WING WIGGLE PLATE CRACKED AT ATTACH FASTENER INBOARD OF #6 FLAP TRACK. / R&R WIGGLE PLATE PER SRM.SDR DALA2020020310796Skin · damaged(LOG 1469797) DURING INSPECTION FOUND NICKS ON PREVIOUS REPAIR ON LOWER SKIN OF AFT INBOARD FLAP LH WING. NEW REPAIR DOUBLER WAS REPLACED PER B-737-800 SRM 57-53-01-2R REPAIR 7 PAR.4.C AND B-737-800 SRM 51-70-10-2R REPAIR GENERAL PAR.19.F AND PAR.20.B.SDR SWAA2021081206813Wedge · delaminatedLEFT WING I\B MID FLAP O\B T\E WEDGE LOWER SURFACE DELAM APPROX 15'X9' AT THE AFT EDGE STARTS 9' I\B OF THE AFT END. / LEFT WING I\B MID FLAP O\B T\E WEDGE LOWER SURFACE DELAM APPROX 15'X9' AT THE AFT EDGE STARTS 9' I\B OF THE AFT END. COMPLIED WITH EA: 1-757-SDR IPXA2020033053711Panel · corrodedINSPECTION TYPE:D1CORROSION ON PANEL ASSY (P/N:65B08423-502)OF R/H INBD MID FLAP NEAR WBL 347.069.REPAIR I.A.W.BOEING SRID:4-4703222604 AND UPS EO B747-5750-75991-A.SDR DALA2020013000718Fairing · missingRIGHT WING, ONE COVER ON FLAP TRACK FAIRING MISSING. DEFERRED PER CDL 57-00-07 UNTIL COVER IS AVAILABLE TO REPLACE. LP 6376698SDR FDEA202001300243Skin · dentedNUMEROUS DENTS LOCATED ON LEFT WING INBD MAIN FLAP UPPER SURFACE. REMOVED AND INSTALLED A NEW INBD MAIN FLAP LT SIDE IAW AMM 27-51-02-4, ACCOMPLISHED OPERATIONAL TESTED THE FLAP FOUND GOOD IAW IAW AMM 27-51-02-5.SDR DALA2020020300838Skin · dentedSHIP 5647 AWR. DENT OUT LIMITS ON MF STA 261 AND DISBOND AREA ON MF STA 238 AT RH INBD MAIN FLAP UPPER SKIN TRAILING EDGE AREA. (IN REF LOG 0438019). CORRECTIVE ACTION: SUMMARY OF N.R.C. SERIAL NO.00661: DENT OUT LIMITS ON MF STA 261 AND DISBOND AREA ON MF STASDR IPXA2020013191542Angle · damagedRIGHT WING CENTER FLAP OUTBOARD END HAD A MISSING ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-21.SDR SWIA2020031649325Skin · chafed* RIGHT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED IN 4 EA. PLACES. (C-CHECK) RO 3/13/2020 RECEIVED, LOCATED, AND DRILLED NEW INBD FLAP VANE OTBD LEADING EDGE CAP REF CRJ-200 SRM. INSTALLED NEW RIGHT INBOARD FLAP VANE LEADING EDGE REF CRJ-200 SRM.SDR REXA2020021280201Fitting · crackedR/H FLAP STUB FAIRING FWD FITTING IS CRACKED AND BENT
REMOVED AND REPLACED RH FLAP STAB FAIRING FWD FITTING IAW CRJ 200 SRM 51-42-20 AND TR 51-42 WVAC EMP #750 MTCSDR REXA2020020580182Skin · chafedLH INBD FLAP VANE CHAFED 1"L X .5"W JUST INBD OF ACCESS PANEL 584DT.
REMOVED AND REPLACED LH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM TASKS 51-40-11 AND 51-42-10SDR REXA2020020580179Skin · chafedLH INBD FLAP VANE CHAFED 1"L X .5"W JUST OTBD OF ACCESS PANEL 584FT.
REMOVED AND REPALCED LH INB FLAP VANE L/E SKIN IAW CRJ 200 SRM TASKS 51-40-11 AND 51-42-10SDR REXA2020020580176Skin · chafedRH INBD FLAP VANE CHAFED 1"L X .5"W JUST OTBD OF ACCESS PANEL 684ET
REMOVED AND REPLACED RH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM TASKS 51-40-11 AND 51-42-10SDR REXA2020020580169Vane · chafedLH INBD FLAP VANE CHAFED 1""L X .5""W JUST OTBD OF ACCESS PANEL 584ET.
REMOVED AND REPLACED LH INBD FLAP VANE L/E SKIN IAW CRJ200 SRM TASKS 51-40-11 AND 51-42-10SDR AALA202002259037Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAING EDGE FLAP UPPER AND LOWER SURFACE DISBONDED. REPAIRED FLAP PER EA 303051.SDR SWAA2021071325410Skin · puncturedLT WING I/B AFT FLAP HAS A PUNCTURE WITH CRACKS & SHARP EDGES. 28.75' FROM OUTBOARD EDGE & 9.25' FROM TRAILING EDGE. L=.74' + W =.72' (TRANSFERRED FROM 0983930) / LT WING I/B AFT FLAP PUNCTURE 28.75' FROM O/B EDGE 9.25' FROM T/E WAS REPAIRED WITH A PERMANENT RSDR SWAA2021071307409Skin · crackedRT TRAILING EDGE IN BD FLAP HAS CRACK WITH A DENT. R&R RT INBOARD AFT FLAP PER AMM 27-51-12.SDR FDEA202001240220Bracket · corrodedRIGHT HAND WING INBOARD FLAP VANE CENTER HINGE FITTING CAVITY WALL CORROSION. RIGHT HAND WING INBOARD FLAP VANE CENTER HINGE FITTING CAVITY WALL CORROSION REMOVED AS PER SRM 51-21-01-0G AND MEASURE REWORKED AREA, ORIGINAL THICKNESS 0.100Ï¿½, MATERIAL REMOVSDR FDEA202001240219Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP VANE OUTBOARD HINGE FITTING CAVITY WALL CORROSION. RIGHT HAND WING INBOARD FLAP VANE OUTBOARD HINGE FITTING CAVITY WALL CORROSION REMOVED AS PER SRM 51-21-01-0G AND MEASURE REWORKED AREA. ORIGINAL THICKNESS 0.145Ï¿½, MATERIAL RSDR FDEA202001240218Vane · crackedLEFT HAND WING INBOARD FLAP VANE OUTBOARD LEADING EDGE CRACKED AT STATION XIFH 279.360 . LEFT HAND WING INBOARD FLAP VANE , CRACKED OUTBOARD LEADING EDGE AT STATION XIFH 279.360 REPAIRED AS PER E.A. # : 1-5750-T0338537 A P2 . TITLE : WINGS - FLIGHT SURFASDR REXA2020020540174Skin · damagedELONGATED RIVET HOLE FOUND AT THE INBOARD LEADING EDGE OF INBD FLAP VANE PANEL OUTBD OF ACCESS PANEL 584ET.
REMOVED TAPE. REMOVED AND REPLACED DAMAGED BUTT STRAP P/N 601R14303-24 IAW CRJ 200 SRM 51-42-06 AND 51-41-02. WVAC STAMP EMP # 722 MTC
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