JASC 5753
Service difficulty reports · 31,515
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 QXEA200601446Flap Track · corrodedPDX - C4 RIGHT INBOARD FLAP TRACK (NR 1 UPPER) HAS DIVOTS WTH CORROSION SPOTS AT THE 0 AND 5 DEGREE POSITIONS TOP SIDE OF TRACK. REPAIRED IAW RD 8-57-985.SDR QXEA200601445Flap Track · corrodedPDX C4 - RIGHT INBOARD FLAP TRACK (NR 1 LOWER) HAS DIVOTS WTH CORROSION SPOTS AT THE 0, 5 AND 15 DEGREE POSITIONS TOP SIDE OF TRACK. REPAIRED IAW RD 8-57-985.SDR QXEA200601399Flap Track · corrodedPDX C4 RIGHT HAND INBOARD FLAP TRACK NR 1 UPPER TRACK HAS DIVOTS WITH CORROSION SPOTS AT THE 0 AND 5 DEGREE POSITIONS ON BOTTOM SIDE OF TRACK. REPAIRED IAW RD 8-57-985.SDR SWAA061955Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR SWAA061954Flap · delaminatedDURING SCHEDULED C2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RIGHT FLAP PER MM.SDR MALA060369Skin · damagedLEFT FLAP SUSTAINED HAIL DAMAGE WS 181.5, 4.75 INCHES FROM THE T/E. REPAIRED IAW EOS51031.SDR MALA060368Skin · damagedLEFT FLAP SUSTAINED HAIL DAMAGE WS 245, 2 INCHES FROM T/E. REPAIRED IAW EOS51031.SDR MALA060367Skin · damagedLEFT FLAP SUSTAINED HAIL DAMAGE WS 278.5, 2.25 INCHES FROM T/E. REPLACED IAW EOS51031.SDR MALA060371Skin · damagedLEFT FLAP SUSTAINED HAIL DAMAGE WS 78, 7.75 INCHES FROM T/E. REPAIRED IAW EOS51031.SDR MALA060370Skin · damagedLEFT FLAP SUSTAINED HAIL DAMAGE WS 197, 4.75 INCHES FROM T/E. REPAIRED IAW EOS51031.SDR 06FDEA2229Hinge · corrodedRIGHT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG. 626-627. FABRICATED BUSHING AND INSTALLED AS PER E.A.1-5750-97765. REPAIR. REPAIR CLASSIFIED AS MAJOR SDR 06FDEA2228Hinge · corrodedRIGHT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG. 621-622. ORIGINAL THK. 1.1565" FINAL 1.1895" MAX. ALLOWABLE 1.150". FABRICATED BUSHING AND INSTALLEDSDR QXEA200601672Skin · dentedYYC C3 RIGHT HAND OUTBOARD FLAP UPPER SURFACE HAS TWO DENTS AT YW209.19 AFT OF LEADING EDGE FROM SCREW DAMAGE SHROUD. REPAIRED IAW DHC-8-400 SRM 51-14-00-350-803 AND EA 6-57-472.SDR QXEA200601642Structure · chafedPDX: LT OUTBOARD FLAP, INBOARD END, CHAFED 15.5 INCHES FWD OF TRAILING EDGE. MAINTENANCE REPAIRED IAW Q400 SRM 51-26-10, SRM 51-42-05, SRM 57-52-30-320-801, Q400 NDTM PART 1, 51-00-04, NDTM PART 6, 51-00-01-250-801 AND HORIZON EA 6-57-490.SDR SWAA061943Flap · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.SDR 06FDEA2207Hinge · corrodedLEFT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. FABRICATED BUSHING AND INSTALLED AS PER E.A. 1-5750-97767. REPAIR CLASSIFIED AS MAJOR PER GMM 6-SDR 06FDEA2206Hinge · corrodedLEFT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA2205Hinge · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA2204Hinge · corrodedRIGHT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG. 442-444. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR QXEA200601673Shroud · out of positionYYC C3 LEFT HAND WING 11B FLAP SHROUD ASSEMBLY P/N 85730351 BETWEEN YW43.52 - YW155 HAS UNSUFFICIENT CLEARANCE BETWEEN 11B FLAP ASSEMBLY. REPAIRED IAW RD 8/4-57-001, ISSUE 6.SDR SWAA061929Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED T/E AFT FLAP PER SRM.SDR 06FDEA2199Skin · dentedRIGHT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SURFACE FOUND DENTED. REPAIRED AS PER SRM 57-10-00 VOLUME I FIGURE 34. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100.SDR MALA060366Skin · damagedDURING 4K CHECK IN BNA FOUND RIGHT FLAP UPPER SURFACE HAS COMPOSITE DAMAGE AND HAS BEEN REPAIRED IAW MESABA EOS51031.SDR UIEA200600125Skin · gougedRIGHT TRAILING EDGE AFT FLAP HAS A GOUGE ON THE UPPER SURFACE APPROX ONE INCH LONG, .125 INCH DEEP AND .250 WIDE. LOCATED 3 FEET OUTBOARD OF NR 7 TRACK CANOE. FOUND DURING C-4 CHECK AT PIK, N/ROUTINE NR 148. GOUGE REPAIRED IAW SRM 57-53-01 FIG 101. COVE PASDR UIEA200600124Skin · dentedRT INBOARD AFT FLAP HAS A DENT ON THE UPPER SURFACE APPROX ONE SQUARE INCH AND APPROX .250 DEEP,12 INCHES OUTBOARD OF NR 6 FLAP TRACK CANOE. FOUND DURING C-4 CHECK, N/ROUTINE NR 147. PERMANENT REPAIR CARRIED OUT TO DAMAGE AREA AS PER SRM 51-70-10 FIG 203 ANDSDR SWAA061913Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED INBOARD SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.SDR QXEA200601444Flap Track · corrodedPDX - C4 LEFT NR 2 FLAP TRACK UPPER SURFACE OF LOWER TRACK HAS DIVOTS WITH PITTING AT O, 5 AND 15 DEGREE ROLLER POSITIONS. REPAIRED IAW RD 8-57-986.SDR ASAA0680679Wedge · gougedFLAP T/E WEDGE IS GOUGED. REPAIRED PER SRM 51-90-0.SDR SWAA061908Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED LOWER SURFACE. REMOVED AND REPLACED RT WING FLAP PER MM.SDR 06FDEA2190Skin · dentedLEFT WING INBOARD FLAP UPPER SURFACE HAS CHAFED AND DENTS (THREE AREAS).SDR QXEA200602200Skin · dentedPDX: RT WING OUTBOARD FLAP, BTM SKIN PANEL HAS A DENT .058 DEEP AND 2.5 DIA AT FWD EDGE OF PREVIOUSLY REPAIRED BETWEEN STA YW 197 TO YW 212 AND STR 3 TO REAR SPAR. MAINTENANCE REPAIRED IAW HORIZON EA 6-57-477, RD 8/4-57-306 AND NDTM PART 6, 51-00-01 AND PART SDR 06FDEA2181Skin · gougedFOUND LT OB FOREFLAP LE IS GOUGED 3 INCHES FROM IB END. ACCOMPLISHED FED EX EA 7-5750-100934.SDR 06FDEA2180Flap Track · corrodedNR 6 FLAP TRACK IS CORRODED ON SPOILER BEAM MOUNT PAD AREA ON FLAP TRACK ITSELF. REPLACED NR 6 FLAP TRACK, FLAP TRACK WILL BE INSTALLED ON FED-EX CARD 27X5708-03.SDR USAA060747Skin · chafedLEFT WING O/B MAIN FLAP I/B LEADING EDGE CHAFED. REMOVED DAMAGE & INSTALLED REPAIR PER SRM 57-53-01 PG 201. DEFECT SIZE: 4"L X 0.200"W X 0.020"D.SDR USAA060748Skin · chafedLEFT WING I/B MAIN FLAP O/B LEADING EDGE CHAFED. REMOVED DAMAGE & INSTALLED DOUBLER REPAIR PER SRM 57-53-01 FIG 201. DEFECT SIZE: 7.125"L X 0.187"W X 0.012"D.SDR AWXA200601540Flap · delaminatedPHX - LEFT WING O/B T/E FLAP DELAMINATED 6 IN AREA LOCATED JUST O/B OF R/B NR 5 OF FLAP. REPAIRED LEFT WING O/B T/E FLAP 6 IN AREA LOCATED JUST O/B OF R/B NR 5 OF FLAP IAW ER NR 25-5753-06150-RA1308A.SDR AALA20060435Structure · corrodedAFW - FOUND CORROSION AT THE LEFT WING INBOARD MAIN FLAP ON THE LOWER FACE OF THE HORIZONTAL FLANGES AT TWO LOCATIONS. FIRST LOCATION AT STATION 160 WAS REWORKED TO A 1.5 INCH BY 0.7 INCH AREA WITH A MAXIMUM BLEND DEPTH OF 0.019 INCHES. THE SECOND LOCATION ASDR USAA060735Skin · delaminatedINBOARD END OF RT AFT I/B FLAP DELAMINATED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-53-02, DEFECT SIZE: 2 X 3 INCH.SDR USAA060736Skin · gougedINBOARD SIDE OF RT INBOARD FOR FLAP GOUGED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-10. DEFECT SIZE: 5 X 1 INCH.SDR USAA060737Structure · chafedINBOARD END LOWER L/E OF LEFT OUTBOARD MID FLAP CHAFED. INSTALLED STAINLESS DOUBLER IAW SRM 20-42-01, DEFECT SIZE: 8.0"X.250"X.030".SDR SWAA061878Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD FORE FLAP INBOARD T/E CRACKED. REPAIRED FORE FLAP PER SRM.SDR SWAA061877Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP, INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR DHL2006873526Skin · wornLT OUTBOARD FLAP UPPER SKIN WORN STA XF 345.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-19-06, DWG AST060510 DATED 05-13-06. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED SECTION IAW DWG AST060510. PERFORMED NDTSDR MALA060388Skin · damagedLEFT FLAP SUSTAINED HAIL DAMAGE WS 278.5, 2.25 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060392Skin · damagedLEFT FLAP SUSTAINED HAIL DAMAGE WS 181.5, 4.75 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060391Skin · damagedLEFT FLAP SUSTAINED DAMAGE WS 78, 7.75 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060390Skin · damagedLEFT FLAP SUSTAINED HAIL DAMAGE WS 181.5, 4.75 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR MALA060389Skin · damagedLEFT FLAP SUSTAINED HAIL DAMAGE WS 245, 2 INCHES FROM TRAILING EDGE. REPAIRED IAW EOS51031.SDR QXEA200601395Skin · chafedPDX - C4 RIGHT WING OUTBOARD FLAP IS CHAFED ON TOP SKIN APPROXIMATELY 1 INCH FROM INBOARD EDGE, 18 INCHES FROM TRAILING EDGE. REPAIRED IAW DHC-8-200 RD 8-57-1022 AND SRM 51-20-16, 51-20-26.SDR 06FDEA2040Strut · corrodedRT WING O/B FLAP O/B HINGE FITTING AFT NR 1 BOLT HOLE FOUND CORROSION. REPAIRED AS PER FEDEX EA 1-5750-99660, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.
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