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 FDEA201004191236Fitting · corrodedLT OTBD FLAP; INBD HINGE LOCATION SIDE LOAD FITTING MOUNTING SURFACE IS CORRODED. REPAIRED SIDE LOAD FITTING MOUNTING SURFACE IAW CMM 57-44-08.SDR FDEA201004191233Fitting · corrodedLT OTBD FLAP; INBD HINGE LOCATION NR 4 BORE IS CORRODED. REMOVED BUSHING. VERIFIED BORE DIAMETER. REMOVED CORROSION. ETCHED BORE. FLAP-PEENED BORE. CAD PLATED BORE. PRIMED BORE. MATERIAL ID FOR REPAIR BUSHING. MACHINED REPLACEMENT BUSHING. CAD PLATSDR FDEA201004191231Fitting · corrodedLT OTBD FLAP; OTBD HINGE LOCATION NR 3 INBD BORE IS CORRODED. VERIFIED BORE SIZE AND REMOVED CORROSION IAW CMM 57-44-09. ROTO-PEENED; ETCHED; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED IAW BSOP 20-10-02. PRIMED IAW CMM 57-44-09.SDR FDEA201004191230Lug · corrodedLT OTBD FLAP; OTBD HINGE LOCATION NR 3 OTBD LUG FACE OUTER SURFACE IS CORRODED. REPAIRED NR3 LOCATION LUG FACE IAW CMM 57-44-09.SDR FDEA201004191229Fitting · corrodedLT OTBD FLAP; OTBD HINGE LOCATION NR3 MOUNTING SURFACE IS CORRODED. VERIFIED LUG THICKNESS AND REMOVED CORROSION IAW CMM 57-44-09. ETCHED; FLAP- PEENED; CLEANED; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-01. PRIMED SURFACE; MATERIALSDR IPXA10559330Wedge · damagedFLAP T/E WEDGE SKIN DAMAGED REPAIRED IAW B757-5750-36938-B.SDR AALA20100415TUL06Skin · dentedINBOARD AFT FLAP LOWER SURFACE HAS NUMEROUS GRAVEL DENTS. REMOVED .25 INCH DIAMETER SKIN TO REPAIR DING AT 27 INCHES FROM INBOARD END AND 6.2 INCHES FROM TRAILING EDGE. NO CRACKS FOUND. FABRICATED 3.4 INCHES DOUBLER PER SRM 51-70-10-2R. FILLED AREAS OF LIGSDR IPXA10159848Skin · gougedINSPECTION TYPE:10YR, LT CTR FLAP UPPER SKIN REPAIR DOUBLER GOUGED. REPAIRED IAW EO A300-5750-37795-A AND EA 300-5750-01-A2276, REV. I/R.SDR IPXA10159847Skin · gougedINSPECTION TYPE:10YR LT INBD FLAP UPPER SKIN REPAIR DOUBLER GOUGED REPAIRED IAW EP NR A300-5750-37801-A AND SAA EA 300-5750-01-A2278 REV. I/RSDR IPXA10159776Skin · damagedINSPECTION TYPE:10YR LT INBD FLAP L/E DENTED 4 PLACES APPROX 52 TO 64 IN'S FROM INBD END. REPAIRED IAW SRM 57-50-00, FIG 208, PARA 4H.SDR IPXA10559594Skin · gougedINSPECTION TYPE:C1, LT WING OTBD MAIN FLAP UPPER SURFACE 35" FROM INBD END AND 23" FWD OF T/E IS GOUGED. LT WING OTBD MAIN FLAP WAS REPAIRED IAW SRM51-70-10-2R, REPAIR 4 AND SRM51-70-10-2R REPAIR, GENERAL.SDR IPXA10659390Wedge · crackedINSPECTION TYPE:C RT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AFT EDGE AREA CRACKED. COMPOSITE PREP REG LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14.SDR FDEA201004151197Wedge · crackedRT WING INBD FLAP TAIL AT RIB 25A IS CRACKED. FABRICATED AND BONDED NEW WEDGE SKIN; DOUBLER; SPAR BRACKET AND CORE OF END FLAP TAIL WEDGE PN 57960014 IAW EA 6-5750-136642 "WING - RT INBD FLAP T/E WEDGE AT RIB 25A"; DWG A57960014 AND TPS 1001 REV "E".SDR SWAA102168Skin · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA102155Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR ASAA1047700Skin · dentedLEFT I/B FORE FLAP UPPER SURFACE DENTED 18 INCHES FROM O/B END. REMOVED DAMAGED AREA, FABBED PARTS AND BONDED.SDR DALA107796306Skin · delaminatedDURING "L" CHECK, FOUND RT WING AFT FLAP LOWER SURFACE WAS DELAMINATED IN 2 LOCATIONS. REPAIRED IAW SRM 51-70-07-5A.SDR IPXA10559445Wedge · debondedINSPECTION TYPE:C1, WHILE WORKING CARD NR 85220 WINGS 5040 FOUND RT INBD MAIN FLAP UPPER SURFACE T/E WEDGE DISBONDED AT DENT 59" OTBD OF INBD END 9" FWD OF T/E. RT INBD MAIN FLAP T/E WEDGE WAS REPAIRED IAW SRM 51-70-07-0G.SDR AALA20100413TUL07Skin · damagedOUTBOARD AFT FLAP INTERIM (PATCH) REPAIR HAS DELAMINATION. REMOVED, DRILLED AND COUNTERSINKED NEW LEADING EDGE SKIN PER SRM 51-10-2.SDR AALA20100413TUL06Skin · wornINBOARD FLAP LOWER SKIN HAS AREA OF LIGHT WEAR, OUTBOARD END OF INBOARD FLAP, FORWARD END OF FLAP. BLENDED LIGHT WEAR ON OUTBOARD END OF LEADING EDGE OF FLAP. FOUND TO BE WITHIN LIMITS PER SRM 57-53-01-1A-1 FIGURE 103. TREATED, PRIMED AND APPLIED TEFLON PAISDR SWAA102107Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING T/E INBOARD FORE FLAP DELAMINATED NEAR INBOARD END. REMOVED AND REPLACED FLAP PER MM.SDR AALA20100412TUL03Skin · corrodedINBOARD AFT FLAP, TRAILING EDGE OF UPPER SURFACE IS CORRODED APPROXIMATELY 28 TO 48 INCHES FROM INBOARD CORNER. FABRICATED DOUBLER AND FILLER PIECES. HOT BONDED PER 51-70-10-2R.SDR IPXA10559593Skin · gougedINSPECTION TYPE:C1, PREVIOUS REPAIR LOCATED ON LT WING OTBD MAIN FLAP UPPER SURFACE 95" OTBD FROM INBD END AND 23.5" FWD OF T/E IS GOUGED (436-W3-07) L/W OTBD MAIN FLAP WAS REPAIRED IAW SRM51-70-10-2R, REPAIR 4 AND SRM 51-70-10-2R GENERAL.SDR FDEA201004121151Skin · crackedRT INBD FLAP SKIN PANEL COVERING RIB 25A (REMOVED AT THE TIME OF INSP), INDICATES MULTIPLE CRACKS WITH EDDY CURRENT, ALL PROTRUDING FOR AND AFT ALONG RIB 25A LOCATION. LOCATED, DRILLED AND COUNTERSUNK SKIN SECTION REF SRM 51-72-10. FOR INSTALLATION SEE EO ESDR UALA2010041201225Bearing · looseNR 8 FLAP TRACK FWD MOUNT FITTING BEARING ROTATION. REPAIRED IAW FIELD REPAIR RECORD (FRR) UAL-744-0624.SDR UALA2010041201224Bearing · looseNR2 FLAP TRACK FWD MOUNT FITTING BEARING ROTATION. REPAIRED IAW FIELD REPAIR RECORD (FRR) UAL-744-0623.SDR UALA2010041201223Bearing · looseNR 1 FLAP TRACK FWD MOUNT FITTING BEARING ROTATION. REPAIRED IAW FIELD REPAIR RECORD (FRR) UAL-744-0622.SDR SWAA102051Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP LOWER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA102050Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING FORE FLAP UPPER SURFACE DELAMINATED BETWEEN WBL 153 TO WBL 156. REPAIRED FORE FLAP PER SRM.SDR SWAA102049Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP LOWER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR IPXA10M59511Skin · dentedINSPECTION TYPE:1C, LT INBD FLAP OUTER SKIN HAS A DENT ON OTBD WEDGE REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 011-5750-01-A2270 IR AND EO MD11-5750-37542-A.SDR IPXA10159415Skin · misrepairedINSP TYPE:3/C, REPAIR SURVEY SEQ NR 151-W4-01 RT WING INBD FLAP REPAIR DOUBLER ON UPPER SKIN DOES NOT CORRELATE WITH SRM. REPAIRED IAW EA 300-5750-01-A2262, IR AND UPS EO A300-5750-37445-A.SDR USAA2010041290774Flap · debondedCLT - C6 - MAJOR REPAIR - AREA OF DISBOND ON LEFT WING OUTBOARD AFT FLAP UPPER OUTBOARD END. REPLACED LEFT WING OUTBOARD AFT FLAP IAW B737 AMM 27-51-39.SDR DALA107669859Vane · delaminatedDURING L-CHECK FOUND RT WING INBD FLAP VANE TOP SIDE EXISTING REPAIR IS CHAFED AND DELAMINATED. REPAIRED IAW SRM 27-51-03, 51-70-02, 57-03, 57-50-9, 51-10-3.SDR IPXA10B59154Skin · damagedLT INBD AFT FLAP LWR SKIN DAMAGED. DAMAGE LOCATED APPROX 188" FROM INBD END OF FLAP AND 4.25" FROM FWD EDGE OF PANEL. REPAIRED REF EOB747-57-50-37299SDR SWAA102022Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B FORE FLAP SKIN DELAMINATED BETWEEN WBL 132 TO WBL 136. REPAIRED FORE FLAP PER SRM.SDR SWAA102017Flap · delaminatedDURING SCHEDULED 6Y CHECK, FOUND RT WING I/B MAIN FLAP DELAMINATED. REPAIRED FLAP PER AAR EA.SDR SWAA102003Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA101931Flap · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA1047660Skin · chafedRIGHT WING OUTBOARD MID FLAP LOWER SURFACE SKIN T/E CHAFED JUST OUTBOARD OF NR 8 TRACK. CUT OUT DAMAGE, INSTALLED FILLER AND TWO EACH EXTERNAL REPAIR DOUBLER IAW 400 57EA 03179.SDR SWAA102040Flap · delaminatedDURING SCHEDULED HC1 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA10B59081Skin · damaged2 DENTS ON LT AFT FLAP APPROX 89" OTBD OF INBD EDGE AND 7.5" FWD OF MID SEAM AND 92" OTBD OF INBD EDGE AND 10" FWD OF MID SEAM. REPAIRED IAW EO B747-5750-33005-E AND SRM 51-70-10-2R.SDR AALA20100405TUL04Vane · wornLEFT WING HAS NUMBER 3 VANE WORN ON LEADING EDGE ABOVE OUTBOARD FLAP INBOARD HINGE. HOT BONDED METAL DOUBLER ON NUMBER 3 VANE TRAILING EDGE OUTBOARD FLAP PER SRM 51-70-02.SDR IPXA10159129Skin · gougedINSP TYPE:3C, RT WING INBD FLAP UPPER SKIN IS GOUGED IN 5 PLACES APPROX 18IN FWD OF RUB STRIP. REMOVED DAMAGE, FABRICATED AND INSTALLED EXTERNAL PLATE IAW SRM 57-50-00 FIG 208 AND EO A300-5750-37322-A.SDR IPXA10B59079Skin · damagedLT INBD AFT FLAP LOWER SKIN DAMAGED. REPAIRED IAW EO B747-5750-33005-D.SDR IPXA10159146Skin · gougedINSPECTION TYPE:3/C, RT WING INBD FLAP UPPER SKIN IS GOUGED IN 5 PLACES APPROX. 18 IN. FWD OF RUB STRIP. REPAIRED IAW EO A300-5750-37322-A AND SAA EA 300-5753-01-A2250, REV I/R.SDR IPXA10159118Skin · damagedINSPECTION TYPE:3/C, RT WING INBD FLAP UPPER SKIN DENTED IN 3 PLACES BELOW RUB STRIP. REPAIRED IAW EA 300-5730-01-A2241, REV A AND EO A300-5750 -37298-B.SDR ASAA1047649Wedge · dentedRIGHT I/B MID FLAP WEDGE LOWER SURFACE DENTED 15 INCHES FROM I/B END 6 INCHES FROM AFT EDGE. REPAIRED BY INSTALLING 2024 T3 .016 FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.SDR IPXA10659128Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A, FIG 5, REV 46.SDR IPXA10659126Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03, PAR 5A (1) FIG 5, REV 46.
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