JASC 5753

Service difficulty reports · 31,521

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.

SDR 04FDEA01196Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.397 MATERIAL REMOVED: 0.001 REMAINING TMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01195Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01194Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.514, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.513 AMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01193Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.093 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT ANDMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01191Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT AND RTMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01192Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.500, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.498May 10, 2004 · N597FE · Doug MD11SDR 04FDEA01190Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.4May 10, 2004 · N597FE · Doug MD11SDR 04FDEA01188Hinge · corrodedRT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG SPOTFACE CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.406, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0.405 AMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01187Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.502 MATERIAL REMOVED: 0.002 REMAINING THICKNESMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01186Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.094 AND REPAIRED AS PER FEDEX EAMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01185Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.500 MATERIAL REMOVED: 0.008 REMAINING THICKNESMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01184Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B PIVOT BORE HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.093 FINAL DIAMETER: 1.127 AND REPAIRED AS PER FEDEX EA 1May 10, 2004 · N597FE · Doug MD11SDR 04FDEA01183Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL THICKNESS: 0.391 MATERIAL REMOVED: 0.002 REMAINING THMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01182Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. RT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.189 AND REPAIRED AS PER FEDEXMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01181Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.222 AND REPAIRED AS PER FEDEXMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01180Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.003, REMAINING THICKNESSMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01179Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE FOUND CORRODED. LT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL. II. ORIGINAL DIAMETER: 1.062 FINAL DIAMETER: 1.223 AND REPAIRED AS PER FEDEX May 10, 2004 · N597FE · Doug MD11SDR 04FDEA01178Hinge · corrodedLT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.505, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.503 ANMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01177Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. O/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.095 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AND RMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01176Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.502, MATERIAL REMOVED 0.004, REMAINING THICKNESS 0.498 AMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01175Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.093, FINAL DIA 1.126 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT ANDMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01174Actuator · corrodedLT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.405, MATERIAL REMOVED 0.002, REMAINING THICKNESS 0.403May 10, 2004 · N597FE · Doug MD11SDR 04FDEA01173Actuator · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, O/B ACTUATOR LUG HOLE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.222 AND REPAIRED AS PER FEDEX EA 1-5750-74315, LT ANMay 10, 2004 · N597FE · Doug MD11SDR 04FDEA01172Actuator · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG SPOTFACE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG SPOTFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIG THICKNESS 0.401, MATERIAL REMOVED 0.001, REMAINING THICKNESS 0May 10, 2004 · N597FE · Doug MD11SDR 04FDEA01171Actuator · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE, I/B ACTUATOR LUG HOLE CORRODED. LT AFT (FLAP SIDE) O/B FLAP O/B HINGE. I/B ACTUATOR LUG HOLE REMOVED CORROSION AS PER SRM 51-21-01 VOL II. ORIG DIA 1.062, FINAL DIA 1.221 AND REPAIRED AS PER FEDEX EA 1-5750-74315. LT AMay 10, 2004 · N597FE · Doug MD11SDR IXXA060134SSkin · tornDURING ROUTINE C CHECK, FOUND RIGHT HAND OUTBOARD FLAP OUTBOARD TRAILING EDGE WEDGE LOWER SKIN GOUGED AND TORN. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTMay 8, 2004 · N605AL · Doug DC873FSDR SWAA041299Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD FOREFLAP L/E, CRACKED. REPAIRED L/E FOREFLAP PER EA.May 7, 2004 · N707SA · Boeing 7377H4SDR SWAA041298Wedge · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD MID FLAP WEDGE, CRACKED. REPAIRED RT WING MID FLAP WEDGE PER SRM.May 7, 2004 · N693SW · Boeing 737317SDR AWXA200400536Skin · delaminatedMCN - MAJOR REPAIR - DURING C-03 CHECK FOUND THE LT INBOARD FLAP DELAMINATED AT THE UPPER INBOARD END BETWEEN WS 700 AND WS 707 LT. MAINTENANCE CUT OUT DELAMINATED AREA OF LT INBOARD FLAP UPPER SKIN BETWEEN WS 700 AND WS 707 LT; FABRICATED A CORE FILLER AND DMay 7, 2004 · N636AW · Airbus A320231SDR AWXA200400531Skin · delaminatedMCN - MAJOR REPAIR - DURING C-03 CHECK RT INBOARD FLAP LOWER INBOARD REPAIR WAS FOUND DELAMINATED IN 3 PLACES. MAINTENANCE REMOVED EXISTING REPAIR AND CUT OUT DAMAGE IN RT INBOARD FLAP AT RIB 3 + 5 INCH; FABRICATED A CORE FILLER AND A DOUBLER; BONDED REPAIR May 7, 2004 · N636AW · Airbus A320231SDR AWXA200400509Skin · debondedMCN - MAJOR REPAIR - DURING C-03 CHECK FOUND A DISBOND AREA ON THE LT OUTBOARD FLAP UPPER SKIN AT INBOARD END RIB 3 + 2 INCH. MAINTENANCE CUTOUT DAMAGED SKIN ON UPPER LT OUTBOARD FLAP AT RIB 3; FABRICATED A DOUBLER AND REPAIR CORE; BONDED REPAIR PARTS TO FLAPMay 7, 2004 · N636AW · Airbus A320231SDR 04FDEA01170Stop Fitting · crackedLT WING O/B FLAP STOP FITTING FOUND CRACKED. REMOVED DAMAGED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT LT WING O/B FLAP AS PER SRM 51-33-01 VOL II.May 7, 2004 · N597FE · Doug MD11SDR 04FDEA01169Stop Fitting · crackedRIGHT WING O/B FLAP STOP FITTING FOUND CRACKED. REMOVED CRACKED STOP FITTING AS PER SRM 51-31-01 VOL II AND INSTALLED NEW FITTING AT RT WING O/B FLAP AS PER SRM 51-33-01 VOL II.May 7, 2004 · N597FE · Doug MD11SDR 04FDEA01164Bracket · corrodedCOMPLY WITH EA 8-5740-77349 WINGS - RIGHT I/B FLAP REWORK OF TRACK/DRIVE BRACKET P/N ARC2761. COMPLIED WITH EA 8-5740-77349- WINGS RIGHT I/B FLAP, REWORK OF TRACK / DRIVE BRACKET.May 7, 2004 · N68056 · Doug DC1010SDR 04FDEA01162Support Fitting · corrodedCOMPLY EA 85740-77347- LEFT OUTBOARD BRACE SUPPORT FITTING CORROSION REPAIR. COMPLIED WITH EA 8-5740-77347.May 7, 2004 · N68056 · Doug DC1010SDR UPS04842445Doubler · gougedINSPECTION TYPE:C-2 LW OB FLAP UPPER SURFACE DOUBLER GOUGED AT I/B ICE BREAKER GUIDE TRACK STA XF219. REMOVED DAMAGED DOUBLER FAB NEW DOUBLER ALODINED AND PRIMED INSTALLED NEW DOUBLER.May 6, 2004 · N818UP · Doug DC873FSDR UPS04842536Structure · bentINSPECTION TYPE:C-2, RIGHT WING I/B FLAP I/B END (LIP) BENT AT AFT AREA, CHAFING FILLET PANEL 192 U. FABBED NEW WEB AND DOUBLER REPAIR IAW REO G09806.May 5, 2004 · N818UP · Doug DC873FSDR 04FDEA01146Support Fitting · chafedLEFT I/B FLAP DRIVE FITTING AFT MOST TOP ROLLER BRACKET-F O/B FWD EDGE FOUND WITH CHAFE MARKS. COMPLIED WITH FEDEX EA 1-5750-75933 - WINGS - LEFT INBOARD FLAP, ROLLER UPPER AFT FITTING ASSEMBLY.May 4, 2004 · N601FE · Doug MD11SDR 04FDEA01145Support Fitting · damagedLEFT I/B FLAP DRIVE FITTING AFT MOST TOP ROLLER BRACKET-F O/B BUSHING BORE FOUND ELONGATED. COMPLIED WITH FEDEX EA 1-5750-75933, WINGS - LEFT INBOARD FLAP, ROLLER UPPER AFT FITTING ASSEMBLY.May 4, 2004 · N601FE · Doug MD11SDR 04FDEA01144Hinge · crackedRIGHT O/B FLAP, I/B HINGE FITTING TENSION STRAP SUPPORTS FOUND EXISTING CRACK ON HINGE HOLES BIGGER IN SIZE COMPARE TO EO 1-5750-7-5004 01 PT2 AS CALL OUT ON STEP 1B. COMPLIED WITH FEDEX EA 1-5750-75942 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE, TENSION STRMay 4, 2004 · N601FE · Doug MD11SDR 04FDEA01143Bracket · corrodedRIGHT AFT I/B FLAP O/B HINGE, O/B STRAP PIVOT HOLE FOUND WITH MINOR CORROSION. COMPLIED WITH FEDEX EA 1-5750-76651 - WINGS - TRAILING EDGE FLAPS, LT & RT INBOARD FLAP, OUTBOARD BRACKET PIVOT BORE CORROSION REPAIR.May 4, 2004 · N601FE · Doug MD11SDR 04FDEA01154Support · corrodedRIGHT O/B FLAP VANE ASSY NR 4 VANE TRACK MOUNT AFT BOLT HOLE IS CORRODED. REPLACED SUPPORT ASSY TO BE INSTALLED AT MAE.May 4, 2004 · N68056 · Doug DC1010SDR 04FDEA01153Fitting · corrodedRIGHT O/B FLAP NR3 VANE FITTING FWD BOLT HOLE IS CORRODED. REPLACED NR 3 VANE FITTING TO BE INSTALLED ON EO 8-5750-7-5000 C PT 4 AT MAE.May 4, 2004 · N68056 · Doug DC1010SDR IXXA0400072SVane · elongatedROUTINE C-CHECK INSP FOUND RT IB VANE SLOT ELONGATED HOLES AT STA XS. 250.089. REPAIR WAS ACCOMPLISHED. REMOVED ALL FASTENERS WITHIN REPAIR AREAS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW DWG V82-R07. PERFORMED NDT INSP IAW NDT SPM PARMay 3, 2004 · N830BX · Doug DC871FSDR SWAA041251Wedge · debondedDURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD MID FLAP T/E WEDGE PANEL DISBONDED. REMOVED AND REPLACED LT WING INBOARD MID FLAP PER MM.May 3, 2004 · N686SW · Boeing 737317SDR 04FDEA01140Vane · corrodedRT WING, OUTBOARD FLAP VANE NR 2 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK.May 3, 2004 · N590FE · Doug MD11SDR 04FDEA01139Vane · corrodedRIGHT WING, OUTBOARD FLAP VANE NR 4 TEE-FITTING CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, TRAILING EDGE & TRAILING EDGE DEVICES RT OUTBOARD FLAP NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK.May 3, 2004 · N590FE · Doug MD11SDR 04FDEA01138Vane · corrodedRIGHT WING, OUTBOARD FLAP VANE NR 4 TEE-FITTING CORRODED. COMPLIED WITH FEDEX EA 1-5750-76688, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP NR 1, 2, 3 & 4 VANE TO TRACK SUPPORT REWORK.May 3, 2004 · N590FE · Doug MD11SDR 04FDEA01137Vane · corrodedLEFT WING, OUTBOARD FLAP VANE NR 2 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAILING EDGE DEVICES LT OUTBOARD FLAP NR 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORK.May 3, 2004 · N590FE · Doug MD11SDR 04FDEA01136Vane · corrodedLEFT WING, OUTBOARD FLAP VANE NR 3 TEE-FITTING SLOT CORRODED. COMPLIED WITH FEDEX EA 1-5750-76687, TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP NR 2, 3, 4 & 5 VANE TO TRACK SUPPORT REWORKMay 3, 2004 · N590FE · Doug MD11
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