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 FDEA2018091172416Fitting · corrodedLT O/B FLAP VANE HORN FITTING 'E' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHT 1. EXISTING SLOT HOLE: LENGTH 0.857", WIDTH 0.581", FINAL SLOT HOLE: LENGTH 0.952", WIDTH 0.652". REPAIR LIMIT - LENGTH 0.940", WIDTH 0.SDR FDEA2018091172415Bracket · corrodedLT WING I/B FLAP I/B DRIVE LINK IDLER BRACKET BORE CORROSION. DRIVE LINK IDLER BRACKET BORE REWORKED PER CMM 57-52-03. EXISTING HOLE DIA 1.00", FINAL HOLE DIA 1.316". REPLACEMENT BUSHING FOR ARC3087-1 & ARC3086-1 FABRICATED PER EA 1-5750-T0342037 P1 STEP 4, 4ASDR FDEA2018091172414Hinge · corrodedLT WING O/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA: 1.148' FINAL HOLE DIA: 1.163" MAXIMUM ALLOWABLE HOLE: 1.150" OVERSIZED BUSHING FABRICATESDR FDEA2018091172413Hinge Bracket · corrodedLT WING O/B FLAP I/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.158", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING FABRICATSDR FDEA2018091172378Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188" - 1.283, FINAL HOLE DIA: 1.3785", MAXIMUM ALLOWABLE DIA: 1.220. REPAISDR FDEA2018091172377Hinge · corrodedRT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188"-1.290, FINAL HOLE DIA: 1.328", MAXIMUM ALLOWABLE DIA: 1.220. REPAIR BSDR FDEA2018091172376Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188"-1.256, FINAL HOLE DIA: 1.282", MAXIMUM ALLOWABLE DIA: 1.220. REPAIR BSDR FDEA2018091172375Hinge · corrodedLT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA 1.188"-1.220, FINAL HOLE DIA: 1.250", MAXIMUM ALLOWABLE DIA 1.220. REPAIR BUSSDR SWAA2018091225081Skin · delaminatedRT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED AT UPPER INBOARD SURFACE. R&R AFT FLAP PER AMM.SDR SWAA2018091124935Skin · delaminatedLT WING OUTBOARD AFT FLAP INBOARD LOWER SKIN DELAMINATED. R&R AFT FLAP PER SRM.SDR SWAA2018091024914Fairing · delaminatedLT WING NR 3 MAIN FLAP TRACK FAIRING 542BB INTERNAL LOWER SKIN DELAMINATED. REPAIRED FAIRING IAW SRM.SDR A6WA2018091046042Skin · crackedRIGHT I/B FLAP LOWER SKIN HAS POSSIBLE CRACK ON CENTER TRAILING EDGE. REPAIRED SKIN IAW SRM 57-52-00.SDR IPXA2018090533575Skin · dentedRT IB MAIN FLAP UPPER SKIN HAS DENT WITH DELAM 20.5" FROM OB EDGE AND 24.75" FROM T/E. REPAIRED PER EO B757-5750-68417-B.SDR IPXA2018090533574Skin · dented3 DENTS ON MAIN I/B FLAP UPPER RT SIDE UPPER SKIN. REPAIRED PER EO B757-5750-68417-B.SDR P5CA2018091100261Support Fitting · crackedLT WING T/E FLAP NR 2 AFT FAIRING AFT SUPPORT FRAME FOUND CRACKED. SUPPORT FRAME CRACKED AREA REPAIRED AS PER RI-57-50-12969.SDR P5CA2018091100278Support Frame · crackedLT WING T/E FLAP NR 3 AFT FAIRING FWD SUPPORT FRAME FOUND CRACKED. LT WING T/E FLAP NR 3 AFT FAIRING FWD SUPPORT FRAME CRACKED AREA REPAIRED AS PER RI 57-50-12970.SDR DALA2018090405416Trunnion · gougedLEFT HAND WING INBOARD FLAP TRUNNION GOUGED. REPLACED TRUNNION IAW ERA 571221-14AD AND 5751-01025-01C.SDR AALA2018090431003Hinge Fitting · corrodedCORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTING. REPLACED HINGE FITTING IAW AMM 57-40-01.SDR ABXA20180831100Support Beam · gougedGOUGE IN THE NR 7 FLAP SUPPORT BEAM NR 1 HOLE AT THE 12:00 POSITION. THE GOUGE DAMAGE WAS REMOVED BY REAMING THE HOLE BEYOND THE MAXIMUM PRODUCTION SIZE. THE AIRPLANE WAS GROUNDED.SDR IPXA2018083133429Skin · puncturedRIGHT INBD MAIN FLAP WAS PUNCTURED. REPAIRED THE FLAP UPPER SKIN IAW SRM 51-70-07-0G, GENERAL REV.SDR SWAA2018090424762Flap · delaminatedRT WING OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR DALA2018090405418Trunnion · gougedLEFT FLAP TRUNNION GOUGED. REMOVED TRUNNION SLIDE PANEL INSTALLED NEW TRUNNION AND THEN REINSTALLED SLIDE PANEL. COMPLIED WITH ERA 571190-14AD.SDR A6WA2018090446029Skin · dentedRIGHT I/B FLAP LOWER SKIN HAS 2 DENTS. REPAIRED RIGHT I/B FLAP LOWER SKIN IAW REO 601R-57-52-1544 REV-.SDR AALA2018092109008Bolt · corrodedCORROSION ON RIGHT WING NR 3 FLAP TRACK PIVOT BOLT. REPLACED THE BOLT IAW AMM 27-54-62-400-001-A.SDR AALA2018092109007Bolt · corrodedCORROSION ON THE RIGHT WING NR 2 FLAP TRACK PIVOT BOLT. REPLACED THE BOLT IAW AMM 27-54-62-400-001-A.SDR AALA2018091429005Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON THE RT WING TRAILING EDGE FLAP TRACK NR 4 PIVOT BOLT. REPLACED THE PIVOT BOLT IAW AMM 27-54-62-400-001.SDR FDEA201808292260Hinge · corrodedLT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT O/B BORE CORROSION. HINGE PIVOT O/B BORE (HOLE A & B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.255", FINAL HOLE DIA: 1.283", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABRSDR FDEA201808292259Hinge Bracket · corrodedLT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. HINGE PIVOT INBD BORE (HOLE G & F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.282", FINAL HOLE DIA: 1.326", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABSDR FDEA201808292258Hinge Bracket · corrodedRT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT O/B BORE CORROSION. HINGE PIVOT OUTBD BORE (HOLE B & A) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.218", FINAL HOLE DIA: 1.251", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING SDR FDEA201808292257Hinge Bracket · corrodedRT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. HINGE PIVOT INBD BORE (HOLE G & F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.2565", FINAL HOLE DIA: 1.281", MAXIMUM ALLOWABLE DIA: 1.220Ï¿½. OVERSIZE BUSHISDR SWAA2018090424719Skin · delaminatedLT WING OUTBOARD TRAILING EDGE AFT FLAP INBOARD END DELAMINATED ON LOWER AND UPPER SIDE. R&R AFT FLAP PER AMM.SDR FOTR20180829023Skin · corrodedLEFT OTBD FLAP UPPER AREA INSIDE FLAP WAS CORRODED.SDR SWAA2022022294651Plate · delaminatedLEFT INBOARD FLAP 'ELEPHANT EAR' HAS DELAMINATION ON MOUNTING SURFACE / REPAIRED LEF TINBOARD FLAP LOWER PLATE (ELEPHANT EAR) IAW EA 180438 REV. P1-IR STEPS 1-7 AND SWA EA 1-757-154986 REV. IR.SDR SWAA2022021820798Wedge · delaminatedLEFT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE HAS AN AREA THAT IS DELAMINATED. THE DELAMINATION IS 21' X 9' STARTING 7' FROM THE OUTBOARD EDGE ON THE LOWER SIDE OF WEDGE. / INSTALLED PANEL PER M/M REF. 20-50-11.SDR SWAA2018102226146Flap · delaminatedLT WING OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED. R&R AFT FLAP IAW SRM.SDR SWAA2018082824664Skin · crackedLT WING INBOARD TRAILING AFT FLAP LOWER SURFACE CRACKED. REPAIRED AFT FLAP PER EA.SDR SRXR201808260035Vane · delaminatedRIGHT INBD FLAP VANE OUTER SKIN WAS DELAMINATED AROUND PANEL 643CT. ACCOMPLISHED A REPAIR IAW EA 011-5750-52-A7381 I/R.SDR DALA2018082705283Skin · crackedDURING INSPECTION, FOUND A CRACK ON THE INBD FLAP LOWER SURFACE ON THE LT WING. REPAIRED IAW SRM 57-53-01, REPAIR 4, AND SRM 51-70-10, REPAIR GENERAL.SDR IPXA2018082743201Angle · crackedLEFT WING TE FLAP 536BB INTERNAL ANGLE WAS CRACKED. REPAIRED IAW REO G21546, REV IR.SDR SWAA2018100925804Flap · delaminatedLT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP IAW AMM.SDR SWIA2018091045041Vane · chafedRT INBOARD FLAP VANE HAS CHAFING AT MIDDLE OF LEADING EDGE. (C-CHECK) RO: 09/07/2018. REPLACED RT INBOARD FLAP VANE MIDDLE LEADING EDGE CAP (P/N 601R14303-52) IAW SRM.SDR FDEA201808232177Skin · delaminatedDISBOND RIGHT OUTBOARD AFT FLAP TRAILING EDGE. REPAIRED THE RT OTBD AFT FLAP TE, HOT-BOND REPAIR IAW SRM 57-53-01- 2R, FIG 201, TABLE II, AND SRM 512R, FIG 201, TABLE II, AND SRM 51-70-04-OG, PARA 6, 4. G, & EA TF-5750 -T0341994, P1.SDR A6WA2018082846004Fitting · wornRIGHT OTBD FLAP FITTING AT FLAP STATION 280.66 WAS WORN TO LIMITS. REPLACED.SDR HNAA2018082400206None · noneNDIS 603 31-33 0015960 22AUG18 SBY CLOSE
MAINTENANCE FOLLOW UP: PREVIOUSLY RECORDED FDR DATA
VALIDATED ON 8/23/18 INDICATES THAT A/C EXCEDED THE
AIRSPEED/FLAP POSITION OPERAIONAL LIMIT
SDR FDEA2018082322150Skin · dentedRIGHT INBD FLAP TOP SURFACE WAS DENTED APPROX 39 INCHES FROM INBD EDGE, AND 6 INCHES FROM AFT EDGE. ACCOMPLISHED A REPAIR ON THE RTFLAP TOP SURFACE IAW SRM 57-53-01-01, AND SRM 51-70-10, REPAIR 2.SDR A6WA2018082846008Skin · dentedRIGHT INBD FLAP, LOWER INBD SKIN HAD NUMEROUS ROCK PITS. REPLACED THE FLAP.SDR A6WA2018082846005Vane · chafedLEFT INBD FLAP VANE LEADING EDGE WAS CHAFED AT WS 104.0. REPLACED THE FLAP VANE.SDR SWAA2022021853891Skin · delaminatedRIGHT WING OUTBOARD AFT FLAP UPPER SKIN IS DELAMINATED 3 INCHES IN DIAMETER 4 INCHES FROM INBOARD EDGE X 3 INCHES FROM AFT EDGE / SEALED DAMAGED AREA WITH SPEED TAPE ON R/H WING O/B AFT FLAP REF SRM 57-53-01-1A-4. SEE EC/TC REPAIR 57EA-05596 TSR TRACKING # 201SDR REXA2018082100775Skin · gougedLT INBD FLAP, FLAP VANE LEADING EDGE IS CHAFED INBD OF INBD VANE ACTUATOR. BLENDED FOUND OUT OF LIMITS IAW SRM51-42-13.SDR SWAA2018082724586Fairing · crackedLT WING NR 3 FLAP TRACK AFT FAIRING CRACKED. REPAIRED FAIRING IAW EA AND ER.
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