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 04FDEA01753Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD SPOTFACE FOUND CORRODED.Jun 16, 2004 · N587FE · Doug MD11SDR 04FDEA01752Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED.Jun 16, 2004 · N587FE · Doug MD11SDR 04FDEA01751Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED.Jun 16, 2004 · N587FE · Doug MD11SDR 04FDEA01750Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.Jun 16, 2004 · N587FE · Doug MD11SDR 04FDEA01749Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED.Jun 16, 2004 · N587FE · Doug MD11SDR 04FDEA01748Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED.Jun 16, 2004 · N587FE · Doug MD11SDR 04FDEA01747Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED.Jun 16, 2004 · N587FE · Doug MD11SDR 04FDEA01755Hinge · corrodedLT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, ORIGINAL DIAMETER=1.187", FINAL DIAMETER=1.255 AND REPAIRED AS PER FEDEX EA 1-5750- 76775Jun 16, 2004 · N587FE · Doug MD11SDR IXXA060165SDoubler · gougedDURING ROUTINE C-CHECK, FOUND LEFT WING INBOARD FLAP UPPER OUTBOARD REPAIR DOUBLER GOUGED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED. INSTALLED NEW DOUBLER AND NEW FASJun 15, 2004 · N605AL · Doug DC873FSDR CA040615015Hinge · corroded(CAN) WING FLAP HINGE HAS INTERGRANULAR CORROSION ON THE LEADING EDGE OF HINGE JUST BELOW THE WING SKIN AND FLAP HINGE FAIRING.Jun 15, 2004 · Cirrus SR22SDR CA040615014Hinge · corroded(CAN) FLAP HINGE ASSEMBLY HAS INTERGRANULAR CORROSION ON THE FORWARD EDGE OF THE HINGEJUST BELOW THE BOTTOM WING SKIN ABOVE THE HINGE FAIRING.Jun 15, 2004 · Cirrus SR22SDR CA040615013Hinge · corroded(CAN) FLAP HINGE ASSEMBLY HAS INTERGRANULAR CORROSION ON THE FORWARD EDGE OF THE HINGEJUST BELOW THE BOTTOM WING SKIN ABOVE THE HINGE FAIRING.Jun 15, 2004 · Cirrus SR22SDR CA040615012Hinge · corroded(CAN) FLAP HINGE ASSEMBLY HAS INTERGRANULAR CORROSION ON THE FORWARD EDGE OF THE HINGEJUST BELOW THE BOTTOM WING SKIN ABOVE THE HINGE FAIRING.Jun 15, 2004 · Cirrus SR22SDR UPS04142613Skin · chafedINSPECTION TYPE: C, LEFT WING INBOARD DAMAGED INTERIM REPAIR MADE IAW EO A300-5750-19043-A 1500 FLT CYCLE LIMIT (D263708). REPAIRED I/B FLAP WITH PERMANENT REPAIR IAW A300-600 SRM 57-50-00.Jun 15, 2004 · N120UP · Airbus A300F4622RSDR 04FDEA01737Vane · corrodedRIGHT WING O/B FLAP VANE, OVAL SHAPE HOLE ON NR 2 TEE FITTING SECOND FROM I/B SIDE FOUND CORRODED. REMOVED AS PER CMM 20-10-02; ORIGINAL OVAL HOLE=0.860 X 0.566; REWORKED OVAL HOLE=0.870 X 0.610; FPI CARRIED OUT IAW CMM 20-30-02 REV 42 FOUND NO CORROSION AND NJun 15, 2004 · N610FE · Doug MD11SDR 04FDEA01738Vane · corrodedLEFT WING O/B FLAP VANE - OVAL SHAPE HOLE ON NR 1 TEE FITTING (FIRST FROM I/B SIDE) FOUND CORRODED. LT WING OUTBOARD FLAP VANE REMOVED AS PER CMM 20-10-02; ORIGINAL HOLE OVAL SIZE=0.860 X 0.560, REWORKED TO SIZE=0.870 X 0.600; FPI CARRIED OUT IAW CMM20-30-02 RJun 15, 2004 · N610FE · Doug MD11SDR 04FDEA01732Hinge Bracket · corrodedLEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AND EXCEEDED LIMITS PER CMM 57-52-03, PAGES 442 - 443. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.25Jun 14, 2004 · N610FE · Doug MD11FSDR 04FDEA01731Hinge Bracket · corrodedLEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.282 INJun 14, 2004 · N610FE · Doug MD11FSDR 04FDEA01730Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION. REMOVED AND EXCEED LIMITS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.Jun 14, 2004 · N610FE · Doug MD11FSDR 04FDEA01725Hinge Bracket · corrodedRT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL THICKNESS=0.652 INCH, REMAINING THICKNESS=0.5Jun 14, 2004 · N610FE · Doug MD11FSDR 04FDEA01724Hinge Bracket · corrodedRT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIA 1.187 INCH, FINAL DIA 1.282 INCH. REPAIR CAJun 14, 2004 · N610FE · Doug MD11FSDR SWAA041675Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING AFT OUTBOARD T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING AFT OUTBOARD T/E FLAP PER MM.Jun 13, 2004 · N357SW · Boeing 7373H4SDR AWXA200400739Skin · debondedDURING C-04 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF LT IB FLAP AT IB END. MAINTENANCE CUTOUT DISBOND AREA ON UPPER SURFACE OF LT IB FLAP; FABRICATED A DOUBLER AND CORE FILLER; BONDED REPAIR PARTS TO FLAP IAW E.R. 26-5752-04178-ES3.Jun 12, 2004 · N633AW · Airbus A320231SDR 04FDEA01700Hinge · corrodedLEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE - I/B STRAP BORE HOLE AT PIVOT POINT BADLY CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE - I/B STRAP P/N ARC2517U501 REMOVED AND NEW STRAP REPLACED AS PER DRAWING ARC2512 AND SRM 51-33-01 VOL 2.Jun 12, 2004 · N610FE · Doug MD11SDR 04FDEA01703Angle · gougedLEFT I/B FLAP, AFT END OF I/B FAIRING, ANGLE IS GOUGED. REMOVED ANGLE IAW SRM 51-31-01. FAB ANGLE ON TRAVLER T4/436154 IAW SRM 57-52-01. INSTALLED ANGLE IAW SRM 51-31-01.Jun 12, 2004 · N387FE · Doug DC1010SDR IXXA060437SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF208. REPAIRED PER ALL APPLICABLE DATA.Jun 11, 2004 · N41CX · Doug DC862SDR IXXA060401SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP UPPER LEADING EDGE SKIN DENTED AT STATION XW58. REPAIRED SKIN PER ALL APPLICABLE DATA.Jun 11, 2004 · N41CX · Doug DC862FSDR IXXA060400SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP TRAILING EDGE SKIN DENTED FROM STATION XRS172 TO XRS220. REPLACED SKIN PER ALL APPLICABLE DATA.Jun 11, 2004 · N41CX · Doug DC862FSDR CA040708009Skin · cracked(CAN) SMALL CRACKS AT RIVETS, 4 PLACES, WERE FOUND ON THE RT FLAP.Jun 11, 2004 · Cessna 172MSDR IXXA060395SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP UPPER SKIN DENTED AT STATION XF440. REPAIRED PER ALL APPLICABLE DATA.Jun 10, 2004 · N41CX · Doug DC862FSDR SWAA041659Spindle · brokenON SHORT FINAL HEARD A POP FOLLOWED BY A SLIGHT ROLL TENDENCY TO THE LEFT. LANDED NORMALLY. FOUND LEFT OUTBOARD FLAP INBOARD SPINDLE BROKEN. REMOVED AND REPLACED LEFT WING INBOARD AND OUTBOARD FLAP SPINDLES PER MM.Jun 10, 2004 · Boeing 7372H4SDR 04FDEA01691Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.502, REMAINING THICKNESS = 0.500, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT Jun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01690Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKEJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01689Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.500, REMAINING = THICKNESS = 0.472, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01688Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.148. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRAJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01687Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.399, REMAINING = THICKNESS = 0.397, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND Jun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01686Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE HOLE CORRODED.Jun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01685Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.412, REMAINING = THICKNESS = 0.410, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, WINGS - LEJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01684Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01683Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.513, REMAINING = THICKNESS = 0.511, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01682Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.092. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01681Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.497, REMAINING THICKNESS = 0.495, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT Jun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01680Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.094, FINAL DIAMETER = 1.128. COMPLIED WITH FEDEX EA #1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE Jun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01679Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.0417, REMAINING = THICKNESS = 0.415, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01678Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE O/B ACTUATOR BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.189. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01677Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.402, REMAINING THICKNESS = 0.402, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01676Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP O/B HINGE I/B ACTUATOR BORE HOLE CORRODED. CORROSSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.190. COMPLIED WITH FEDEX EA 1-5750-76739, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGEJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01675Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.508, REMAINING THICKNESS=0.506, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76738, WINGS - LEFTJun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01674Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG DIA 1.063, FINAL DIA 1.095. REPAIR CARRIED OUT AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA 1-5750-76738, WINGS - LEFT AND RIGHT Jun 10, 2004 · N610FE · Doug MD11SDR 04FDEA01673Hinge · corrodedRIGHT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG THICKNESS=0.490, REMAINING THICKNESS=0.488, MATERIAL REMOVED=0.002. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76738, WINGS - LEFT AJun 10, 2004 · N610FE · Doug MD11
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