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.
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 04FDEA01753Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD SPOTFACE FOUND CORRODED.SDR 04FDEA01752Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR OUTBOARD BORE FOUND CORRODED.SDR 04FDEA01751Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR INBOARD BORE FOUND CORRODED.SDR 04FDEA01750Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE SPOTFACE FOUND CORRODED.SDR 04FDEA01749Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE BORE FOUND CORRODED.SDR 04FDEA01748Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND CORRODED.SDR 04FDEA01747Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED.SDR 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- 76775SDR 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 FASSDR CA040615015Hinge · corroded(CAN) WING FLAP HINGE HAS INTERGRANULAR CORROSION ON THE LEADING EDGE OF HINGE JUST BELOW THE WING SKIN AND FLAP HINGE FAIRING.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 NSDR 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 RSDR 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 = 1.25SDR 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 INSDR 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.SDR 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=0.5SDR 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 CASDR 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.SDR 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.SDR 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.SDR 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.SDR IXXA060437SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF208. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060401SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP UPPER LEADING EDGE SKIN DENTED AT STATION XW58. REPAIRED SKIN PER ALL APPLICABLE DATA.SDR 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.SDR CA040708009Skin · cracked(CAN) SMALL CRACKS AT RIVETS, 4 PLACES, WERE FOUND ON THE RT FLAP.SDR IXXA060395SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP UPPER SKIN DENTED AT STATION XF440. REPAIRED PER ALL APPLICABLE DATA.SDR 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.SDR 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 SDR 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 BRACKESDR 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 RIGSDR 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 BRASDR 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 SDR 04FDEA01686Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE HOLE CORRODED.SDR 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 - LESDR 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 BRSDR 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 RIGSDR 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 BRACKSDR 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 SDR 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 SDR 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 ASDR 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 BSDR 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 RSDR 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 HINGESDR 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 - LEFTSDR 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 SDR 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 A
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