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 FDEA2019101422607Hinge Fitting · corrodedLEFT 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 1-5750-159801 H, PART 3, SDR IPXA2019102878347Hinge · gougedINSPECTION TYPE:2CL/H I/B FLAP O/B HINGE FITTING IS GOUGED AT STA. XIFH=261.REPAIRED GOUGED L/H I/B FLAP O/B HINGR FITTING AT STA. XIFH=261. IAW VT-SAA EA 011-5750-01-A7937 REV. I/R AND UPS EO MD11-5740-74451-A.SDR A6WA2019101546926Vane · chafedLEFT WING INBOARD FLAP VANE SKIN CHAFFED ON I/B SIDE. REMOVED AND REPLACED L/H INBOARD FLAP VANE, INBOARD VANE SKIN IAW SRM 51-42-10SDR A6WA2019101546928Vane · chafedLEFT WING INBOARD FLAP VANE SKIN CHAFFED IN MIDDLE OF VANE. REMOVED AND REPLACED L/H WING INBOARD FLAP VANE SKIN MIDDLE OF VANE IAW SRM 51-42-13SDR AALA201910149022Rib · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD TRAILING EDGE FLAP SUPPORT BACKUP RIB CRACKED. REPAIRED RIB PER EA 299232.SDR IPXA201910147797Skin · dentedRH INBD MID FLAP TOP SKIN DENTS. REPAIRED IAW E.O. B747-5750-74286-A.SDR FDEA201910102564Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08 AND EA 1-5750-T0350113, PART 1, STEP 1A, AND STEP 1. THSDR SIMA20191010003Skin · dentedDENTS ON LEFT INBOARD FLAP LOWER SIDE 17 INCHES FROM INBD EDGE 4 INCHES FROM THE TRAILING EDGE. -C/A-REPAIRED LH INBD FLAP LOWER SIDE IAW SRM 57-52-01-991-812.SDR SIMA20191010002Skin · dentedRT WING INBOARD FLAP UNDER SIDE HAD FOUR DENTS. COMPLIED WITH REPAIR IAW ERS-CR-57MR-1173 01SDR IPXA2019101197722Slat · chafedINSPECTION TYPE:12YR, LEFT WING NR 3 SLAT LWR T/E WEDGE WAS CHAFED. REPAIRED THE LT WING NR 3 SLAT IAW EO A300-5750-74288 & EA 300-5754-01-A7921. (MINOR REPAIR)SDR IPXA2019101197721Skin · damagedINSPECTION TYPE:12YR RIGHT WING #3 SLAT UPPER T/E IS KNIFE EDGED.REPAIRED R/WING #3 SLAT UPPER T/E KNIFE EDGE IAW EO A300-5750-74224 & EA 300-5754-01-A7920 I/R. (MINOR REPAIR)SDR IPXA2019100947713Skin · chafedRIGHT WING CENTER FLAP L/E WAS CHAFED. ACCOMPLISHED A REPAIR OF THE RT WING CENTER FLAP IAW EO A300-5750-74124-A, & EA 300-5754-01-A7901.SDR IPXA2019100947710Skin · chafedRIGHT WING FLAP UPPER SURFACE CHAFED JUST AFT OF MAJOR REPAIR W4-003. ACCOMPLISHED REPAIR OF THE RT WING FLAP UPPER SURFACE IAW SREO A300-5750-26228-D.SDR IPXA2019100947708Skin · chafedREPAIR W4-003 IS CHAFED ON RT WING CENTER FLAP UPPER SURFACE. ACCOMPLISHED REPAIR OF THE RT WING CENTER FLAP UPPER SURFACE IAW EO A300-5730-74190-A & EA 300-5730-01-A7906.SDR IPXA2019100947706Doubler · chafedREPAIR W3-002 HAS POSSIBLE CHAFE LOCATED ON LT WING INBD MAIN FLAP. REMOVED AND REPLACED THE CHAFED DOUBLER IAW SRM 57-50-00 PARA 4E FIG 205. MAJOR REPAIR.SDR IPXA2019101657949Vane · damagedINSPECTION TYPE:2CLT WING I/B FLAP VANE L/E I/B END PREVIOUS REPAIR IS DAMAGED.REPAIRED DAMAGED LT WING I/B FLAP VANE L/E I/B END IAW MD-11 SRM 57-50-80, REPAIR 2, PAR. 2.A.(2).(A)(5), FIGURE 201. (MAJOR)SDR FDEA2019101082493Skin · chafedLW O/B FLAP TOPSIDE SKIN HAS 2 CHAFED SPOTS REMOVED CHAFING AND FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. SURFACE PROTECTED BLEND AREAS IAW A300-600 SRM 51-21-10. REMOVED, FABRICATED, AND INSTALLED NEW CHAFING PLATES IAW EA NO: 6-5750-93355 A P2.SDR IPXA2019100987681Skin · dentedLEFT WING INNER FLAP LOWER SURFACE WAS DENTED AT THE T/E AREA. REPAIRED THE DENTS IAW EO A300-5750-74199-A & EA 300-5753-01-A7908.SDR SWAA2022040532153Flap · debondedLH WING MAIN FLAP UPPER SURFACE PANEL 553ET SHOWS DISBOND AT DENT LOCATED 32' I/B FROM OTBD EDGE AND 4' FWD FROM AFT EDGE OF PANEL / NO PUBLISHED REPAIR INSTRUCTIONS; REMOVED AND REPLACED DISBONDED PANE + 553ET ON LH WING MAIN FLAP UPPER SURFACE IAW SRM 51-40-SDR SWAA2022022463672Flap · debondedLEFT HAND INBOARD AFT FLAP LOWER SURFACE DISBOND AT 29' FROM O/B AND 4' FROM T/E / DISBOND ON LEFT HAND I/B AFT FLAP WAS TO PROTECTIVE PLIES ONLY AT 4' FROM T/E AND 29' FROM O/B EDGE. REPAIR DISBOND PER SRM 57-53-01-2R-4 PARA 3D AND SRM 51-70-05-2R-0.SDR FDEA201910042436Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52SDR FDEA201910042435Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA201910042434Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA201910042433Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE ) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR SCNA2019101403187Fairing · damaged3 LH FLAP FAIRING AFT INBD HAS SCREWS RECESSED INTO SKIN. REMOVED, REPAIRED, AND INSTALLED #3 LH FLAP FAIRING IB; 113A9356 TAILCONE IN REF. TO B737-800 AMM 27-51-18 PG. 401 AND B737-800 AMM 27-51-18-010-003.SDR SWIA2019101646469Vane · out of limitsRIGHT INBD FLAP VANE L/E OUTBOARD PANEL IS FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED RH INBD FLAP VANE LE OTBD PANEL IAW SRM.SDR SWIA2019101646468Vane · damagedRIGHT INBD FLAP VANE L/E CENTER PANEL IS FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED RH INBD FLAP VANE LE (CENTER OTBD PANEL) IAW SRM.SDR DALA2019100205634Support · damagedDURING A LINE CHECK, FOUND DAMAGE ON THE RIGHT TRUNNION FROM TRUNNION SLIDE. REMOVED FAIRING PANEL 194BB ON RT SIDE WITH SLIDING PANEL WIP 130166. INSPECTED TORSION SUPPORT ASSY IAW CMM57-52-21, MEASURED MAX DEPTH OF CHAFE MARKS .155". REMOVED AND REPLACED TSDR FDEA2019100312394Bracket · crackedLEFT WING NR 2 FLAP TRACK FAIRING OTBD ATTACH BRACKET CRACKED REMOVED AND REPLACED LT. WING #2 FLAP TRACK FAIRING OB ATTACH BRACKET IAW A300-600 SRM 51 600 SRM 51-40-21 AND AB DWG A57942502SDR A6WA2019100146898Vane · chafedRH WING I/B FLAP VANE LEADING EDGE IS CHAFED AT I/B SECTION REMOVED AND REPLACED RH WING IB FLAP VANE LEADING EDGE SKIN IB SECTION IAW CRJ 200 SRM 51-42-13SDR SWAA2022030132152Flap · delaminatedLEFT HAND INBD MAIN FLAP PN 113A2100-65 S/N V0144 LOWER SKIN DELAMINATED. NEEDS REPAIRED OR REPLACED PER SWA WORK INSTRUCTION #REPAIR-57EA-07084 / REPAIRED L/H MAIN DFLAP P/N - 113A2100-65 S/N - V0144 LOWER SKIN IAW B737-800 SRM'S 57-53-01-2R-4 + 51-70-10-2R-0SDR A6WA2019100246901Skin · chafedRH WING INBD FLAP VANE LEADING EDGE IS CHAFFED AT CENTER SECTION. REPLACEDSDR SWAA2019100237492Skin · delaminatedL/H WING INBOARD MAIN FLAP LOWER SKIN DELAMINATED. REPAIRED MAIN FLAP IAW AMM.SDR ABXA2019100129157Skin · corrodedCORROSION ON THE LOWER SKIN OF THE RIGHT OUTBOARD FLAP NEAR THE INBOARD HINGE. THE FLAP WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR SWAA2019100137392Skin · delaminatedR/H OUTBOARD AFT FLAP UPPER SKIN DELAMINATED ON INBOARD END. R&R R/H OUTBOARD AFT FLAP PER MM.SDR R61A2019102271114Fitting · crackedWHILE AC WAS IN FOR HVY CK FOUND CRACK ON RH WING INBD AFT FLAP FITTING. AAR MX REPLACED RH WING INBD AFT FLAP FITTING PN 170-39187-002 IAW AMM 20-10-01-910-801-A. FOR DETAILS OF WORK PERFORMED SEE AAR NRC 4500474-6000-0008.SDR IPXA2019092547227Angle · crackedINSPECTION TYPE:12TR LT MID FLAP HAS BROKEN ANGLE AT O/B END. REMOVED AND REPLACED ANGLE ON LT WING MID FLAP O/B SIDE IAW SRM 51-40-21. (MINOR REPAIR)SDR P5CA2019092300198Access Panel · chafedLT WING O/B AFT FLAP, O/B ACCESS PANEL #588IT, FOUND DEEP CHAFING FROM O/B 15", AS MARKED. PERFORMED PERMANENT REPAIR OF LT WING O/B AFT FLAP, O/B ACCESS PANEL #588IT AS PER HX RI NR. RI-57-00-13720 REV A.SDR P5CA2019092300199Doubler · delaminatedLT WING, O/B AFT FLAP, UPPER PNL, EXISTING REPAIR - DOUBLER FOUND DELAMINATED. PERFORMED PERMANENT REPAIR OF LT WING O/B AFT FLAP, UPPER O/B PANEL #588IT AS PER HX RI NR RI-57-00-13720 REV A.SDR IPXA201910147808Skin · chafedINSPECTION TYPE:12YRREPAIR DOUBLER ON RT WING I/B FLAP UPPER SURFACE BETWEEN RIBS 11 & 12 AND STR. 2.3 & STR. 2.4 IS CHAFED.REPAIRED CHAFED RT WING I/B FLAP UPPER SURFACE REPAIR DOUBLER BETWEEN RIBS 11 & 12 AND STR. 2.3 & STR. 2.4 IAW VT-SAA EA 300-5752-01-A79SDR IPXA201910147807Skin · chafedRT WING I/B FLAP UPPER SURFACE BETWEEN RIBS 12 & 14 IS CHAFED.REPAIRED CHAFED RT WING I/B FLAP UPPER SURFACE BETWEEN RIBS 12 & 14 IAW VT-SAA EA 300-5752-01-A7918 REV. IR AND UPS EO A300-5750-74253-A. (MAJOR)SDR IPXA2019091947000Doubler · delaminatedINSPECTION TYPE:C1 LT O/B AFT FLAP LOWER SURFACE REPAIR LOCATED BETWEEN AFSTA 345.765 AND 353.065 AND 6.5" FROM T/E TO CENTER OF REPAIR FAILED ULTRASONIC LF BOND TEST 1. SEVERAL AREAS MARKED IN RED. REPAIRED IAW SRM 51-70-05 PER SRM 57-53-01-2R-1 FIGURE 201 TASDR SWIA2019101646467Vane · damagedLEFT INBD FLAP VANE OTBD L/E IS CHAFED OUT OF LIMITS. (CHECK) RO: 10/13/2019 LOCATED, DRILLED, AND INSTALLED REPLACEMENT FLAP OTBD L/E VANE PANEL IAW SRM.SDR SWIA2019101646466Vane · damagedLEFT INBD FLAP VANE CNTER L/E IS CHAFED OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 LOCATED, DRILLED, AND INSTALLED REPLACEMENT FLAP CENTER VANE PANEL IAW SRM.SDR FDEA201909172260Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE FOUND ORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT OUTBOARD LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-52-03. REPAISDR FDEA201909172259Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND ORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE PIVOT INBOARD LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-52-03. REPAIRSDR FDEA201909172272Skin · dentedRIGHT WING I/B MAIN FLAP LOWER SURFACE HAS A DENT. REPAIRED RW I/B MAIN FLAP LOWER SURFACE IAW SRM 57-53-01-1A AND 51-70-10-1R AND EA H- 2750-T0349512 FLIGHT CONTROL T0349512 FLIGHT CONTROL-T/E FLAPS - RT INBD MAIN FLAP, LOWER SKIN, DENT, RSC SRM REPAIR TRACKSDR IPXA2019091746883Skin · not reportedINSPECTION TYPE:N/A LT I/B FLAP NOSE SKIN REPAIR. REPAIRED IAW EO A300-5750-72841-B.SDR SWIA2019103046624Vane · chafedR/WING INBD FLAP VANE LEADING EDGE CHAFED IN 3 PLACES, I/B- 1.0 X .600 X .015, MID- 1.0 X .500 X .015, O/B- 1.0 X .450 X .010 (C-CHECK) RO: 10/26/2019 BLENDED I/B AND MID CHAFES ON R/H WING I/B FLAP VANE LEADING EDGE SKIN IAW REO. REPLACED O/B LEADING EDGE SKISDR SWIA2019103046623Vane · chafedL/WING INBD FLAP VANE LEADING EDGE CHAFED IN 3 PLACES, I/B- 1.0 X .750 X .015, MID- 1.0 X .700 X .015, OUTBD- 1.0 X .650 X .010 (C-CHECK) RO: 10/26/2019 BLENDED I/B AND O/B CHAFES ON L/H WING I/B FLAP VANE LEADING EDGE SKIN IAW REO. REPAIRED MID LEADING EDG
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