JASC 5753
Service difficulty reports · 31,513
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 TRBA20120910003Guide · corrodedDURING B INSPECTION, FOUND THE LT WING HAS 4 INTERNAL FLAP CAM GUIDES WITH CORROSION OUT OF LIMITS. THE ACFT WAS REMOVED FROM SERVICE. LT WING 4 INTERNAL FLAP CAM GUIDES REMOVAL AND REPLACEMENT COMPLETED IAW MM 57-53-12. THE ACFT WAS RETURNED TO SERVICE.SDR IPXA2675215Skin · dentedRT OTBD T/E FLAP HAS DENT 1.5 X 4.2 CUTOUT. REPAIRED IAW EO B767-5750-48487-A.SDR FDEA201209073255Skin · chafedLEFT WING OUTER FLAP INBD SIDE L/E CHAFED MARK APPROX LENGTH IS 1 INCH AND WIDTH IS 0.50 REF AMM 27-00-00-06, ZONE 580. REPAIRED WING OUTER FLAP IAW A300-600 FSRM 57-50-00 PARA 4.H. PG 231 THRU 233 AND FIG 208 AND EA 6-5750-160186 PT. 1.SDR SWAA2012091707648Flap · puncturedRIGHT WING INBOARD FORE FLAP PUNCTURED. REPAIRED FORE FLAP IAW SRM.SDR SWAA2012091007494Spindle · corrodedNR 2 FLAP CARRIAGE SPINDLE CORRODED. REMOVED AND REPLACED NR 2 SPINDLE PER MT.SDR USAA2012090600008Strut · wornRON CHECK - LEFT WING INTERCONNECTING STRUT BETWEEN INBOARD & OUTBOARD FLAP IS WORN TO LIMITS PER JOB CARD. REPLACED LEFT WING INTERCONNECTING STRUT IAW A319 AMM 27-57-44-000-001-A.SDR FDEA201209063248Skin · damagedLEFT INBD FLAP LOWER SURFACE HAS 22 DENTS AND 12 GOUGES LOCATED FROM STGR 2.10 TO T/E AND RIB 3A TO RIB19A, COMPLIED WITH EA 6-5730160178.SDR ABXA20120906252Bushing · wornLEFT WING OUTBOARD FLAP, INBOARD LINKAGE NR 10 JOINT (FLAP SIDE). BOTH BUSHING LOOSE ON INBOARD SIDE OF CARRIAGE. REPLACED 3-10 JOINT IAW B767 AMM CH 27-51-27-4, ACFT WAS GROUNDED.SDR A6WA20120920020Hinge Fitting · gougedGOUGE ON RIGHT I/B FLAP, I/B HINGE ARM FWD SIDE. REPAIRED THE GOUGE ON RIGHT I/B FLAP HINGE ARM FWD SIDE IAW BOMBARDIER REO 601R-57-54-226.SDR IPXA12175324Skin · chafedINSPECTION TYPE:3C, LT WING OTBD FLAP INBD BULLNOSE AT RIB 1 HAS CHAFE DAMAGE. ACCOMPLISHED REPAIR ON LT WING OTBD FLAP INBD BULLNOSE IAW SRM 57-50-00, PARA 4H, FIG 208.SDR USAA2012090700011Skin · wornC5 CHECK - WEAR ON UPPER LEADING EDGE SKIN OF RIGHT OUTBOARD FORE FLAP 6 INCHES FROM INBOARD EDGE. REPLACED RIGHT OUTBOARD FORE FLAP IAW B737-400 AMM 27-51-37-404-009.SDR SWAA2012091007474Skin · delaminatedLEFT WING OUTBOARD AFT FLAP INBOARD CONNER UPPER SURFACE DELAMINATED. REPAIRED DOUBLER IAW SRM.SDR SWAA2012090607407Flap · delaminatedLEFT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.SDR SWAA2012090507366Flap · chafedLEFT WING O/B FORE FLAP CHAFED. REMOVED AND REPLACED FORE FLAP PER AMM.SDR SWAA2012090407260Spindle · crackedRIGHT WING O/B MID-FLAP NR 8 SPINDLE CRACKED. REMOVED AND REPLACED NR 8 SPINDLE PER MT.SDR USAA2012100400007Flap · corrodedQ6 CHECK - PITTING CORROSION ON LEFT INBOARD FLAP AT LEADING EDGE AND OUTBOUND END OF CARRIAGE TORQUE SHAFT. REPLACED LEFT INBOARD FLAP IAW JOB CARD 03C30727030.SDR A6WA20120920019Vane · chafedRIGHT I/B FLAP VANE WORN AND CHAFED IN THREE PLACES ON THE LEADING EDGE. BLENDED O/B AND CENTER LEADING EDGE. REMOVED 0.008" FROM O/B LEADING EDGE. REMOVED 0.010" FROM CENTER LEADING EDGE. OUTBOARD AND CENTER LEADING EDGE ARE WITHIN ALLOWABLE DAMAGE LIMITSSDR R61A201208310489Skin · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT INBOARD FLAP UPPER SKIN CRACKED FROM FASTENER ON INBOARD END. (COMPOSITE) MAINTENANCE REPAIRED RIGHT INBOARD FLAP UPPER SKIN IAW EMB 170 SRM 51-71-08. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECSDR UALA2012083004886Wedge · damagedDAMAGE TO RIGHT I/B FLAP AFT I/B TRAILING EDGE WEDGE. MEASURES APPROX 8IN BY 3IN. WILL REQUIRE PERM REPAIR PER SRM. MATERIAL ETA 0730 UNDER OSTF'S LISTED. REPAIRED DAMAGED FLAP PER SRM 57-53-01 & SRM 51-70-17. PRIMED & PAINTED TO MATCH.SDR USAA2012091300028Skin · delaminatedQ6 CHECK - DELAMINATION ON LEFT INBOARD AFT FLAP SKIN UPPER & LOWER SURFACE AT BUTT END APPROX 5 INCHES INBOARD OF THE OUTBOARD END EXTENDING TO THE END. REPAIRED LEFT INBOARD AFT FLAP SKIN IAW BOEING DRAWING 65-46434.SDR UIEA2012090700391Skin · corrodedRT INBT FORE FLAP LOWER SURFACE NEAR CENTER FORE FLAP TRACK AREA FOUND MINOR CORROSION. RT INBD FORE FLAP OTBD LOWER SURFACE PANEL REPLACED AND INSTALLED IAW SRM 51-10-02, SRM 51-40-02.SDR QXEA2012083000935Flap Track · damagedLT INBD FLAP, INBD UPPER FLAP TRACK IS DAMAGED. BLENDED OUT DAMAGE REF RD 8/4-57-1352. REMAINING THICKNESS NOTED .174" CONFIRMED CRACK FREE CONDITION REF NTM 51-00-04-910-801, PT 1 AND 51-00-06-910-801, PT 1. MATERIAL LOSS FOUND TO BE IN LIMITS IAW RD 8/4-5SDR QXEA2012083000930Flap Track · wornLEFT NR 4 FLAP TRACK BEAM INBD WEB COATING AT FWD END WORN. BLENDED IAW RD 8/4-57-1238. MIN REMAINING THICKNESS .155" REF NTM 51-00-04-910-801 PT 1. MATERIAL LOSS FOUND TO BE IN LIMITS IAW RD 8/4-57-1238. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 8.2.1.SDR IPXA12175656Skin · chafedINSPECTION TYPE: 10YR, RT OTBD FLAP INBD BULLNOSE SKIN IS CHAFED. REPAIRED FLAP, INBD BULLNOSE SKIN IAW EO A300-5750-44932-A.SDR AALA20120830004Wedge · dentedRIGHT WING TRAILING EDGE: DENT IN BOTTOM SIDE OF INBOARD FLAP, 9 INCHES FROM INBOARD END. INSTALLED PERMANENT FLUSH DOUBLER REPAIR PER SRM 57-01-00 FIGURE 5 SHEET 2.SDR USAA2012091800009Skin · delaminatedQ6 CHECK - DELAMINATION ON UPPER SURFACE OF LEFT OUTBOARD AFT FLAP BETWEEN WBL 230.68 TO WBL 235.68 APPROX 1 INCH FROM INBOARD EDGE & 5 INCHES FROM TRAILING EDGE. REPAIRED UPPER SURFACE OF LEFT OUTBOARD AFT FLAP IAW B737 SRM 51-70-10-2R-4, REPAIR 4, FIG 202.SDR USAA2012091300027Skin · delaminatedQ6 CHECK - DELAMINATION ON LEFT OUTBOARD FOREFLAP SKIN UPPER AT TRAILING EDGE SURFACE 12 INCHES OUTBOARD OF INBOARD END. REPAIRED LEFT OUTBOARD FOREFLAP SKIN UPPER AT TRAILING EDGE IAW B737 SRM 51-70-10.SDR USAA2012091300020Strut · corroded2S CHECK - CORROSION ON INTERNAL HOUSING OF RIGHT WING INTERCONNETING STRUT BETWEEN WS 407 TO WS 486 ALSO BETWEEN RIB 8 TO RIB 9. REPLACED RIGHT WING INTERCONNETING STRUT IAW A319 AMM 27-51-44 & JOB CARD 26C67057001.SDR USAA2012091200002Strut · corroded2S CHECK - CORROSION ON INTERNAL AREA AT HOUSING OF LEFT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862 & BETWEEN RIB 8 TO RIB 9. REPLACED LEFT WING INTERCONNECTING STRUT IAW JOB CARD 26C57057001.SDR AALA20120828017Skin · crackedCRACK ON LOWER SKIN AND BULGE ON UPPER SKIN ALONG TRAILING EDGE 5 INCHES FROM INBOARD END OF FLAP. REMOVED DAMAGE TO UPPER AND LOWER SKINS AND HOT BONDED REPAIR FILLER AND DOUBLER PER SRM 51-70-10.SDR IPXA12B75183Skin · delaminatedINSPECTION TYPE: D, RT WING OTBD MID FLAP T/E UPPER SURFACE DELAMINATED AT 34" OTBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 63.SDR IPXA12B75181Skin · delaminatedINSPECTION TYPE: D, RT WING OTBD T/E MID FLAP T/E UPPER SURFACE DELAMINATED AT 51" FROM OTBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5.SDR IPXA12B75171Fairing · delaminatedINSPECTION TYPE: D, RT WING O/B T/E FORE FLAP L/E FAIRING DELAMINATED AT MOST O/B. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1), FIG 5, REV 63.SDR IPXA12B75169Fairing · delaminatedINSPECTION TYPE: D, RT WING OTBD FORE FLAP L/E FAIRING DELAMINATED AT MID AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 63.SDR SWAA2012083007199Flap · delaminatedRIGHT WING NR 8 O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER AMM.SDR IPXA2175056Skin · damagedA HOLE WAS FOUND IN LOWER SKIN OF RT INBD FLAP. 26.5" FROM T/E AND 25.25" INBD OF P PANEL EDGE. REPAIRED IAW EO A300-5750-48318B.SDR SWAA2012090607400Flap · delaminatedLEFT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW EA.SDR IPXA2B75049Skin · damagedRIGHT INBD AFT FLAP LOWER SURFACE DAMAGE 139 INCHES FROM INBD EDGE AND 9.5 FROM AFT EDGE. REPAIRED IAW EO B747-5750-48340.SDR SWAA2012082707075Spindle · corrodedLEFT WING NR 1 SPINDLE CORRODED. REMOVED & REPLACED NR 1 SPINDLE ASSY PER MT.SDR A6WA201240828Roller · chafedLEFT OTBD FLAP ROLLER FITTING CHAFED. PERFORMED REPAIR OF LT OTBD FLAP INBD ROLLER FITTING IAW REO 601R-57-53-943.SDR USAA2012092400022Fitting · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING AT INTERNAL AREA OF LEFT OUTBOARD FLAP, INBOARD SIDE OF FRONT SPAR AT RIB 14. REPLACED LEFT OUTBOARD FLAP IAW JOB CARD 26L00027009.SDR AALA20120828007Skin · puncturedPUNCTURE IN THE UPPER SURFACE OF THE LEFT INBOARD AFT FLAP. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.SDR SWAA2012091207535Flap · delaminatedRIGHT WING O/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR A6WA201240811Fairing · chafedRT FLAP STUB FAIRING HAS CHAFING AND A DENT AFT END ASSEMBLED REPLACEMENT SERVICEABLE RT STUB FAIRING IAW SRM 51-40-11 AND 51-42-06.SDR IPXA12B75182Fairing · delaminatedINSPECTION TYPE: D, LT WING OTBD FORE FLAP L/E FAIRING DELAMINATED AT INBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 63.SDR IPXA12B75170Fairing · delaminatedINSPECTION TYPE: D, LT WING INBD FORE FLAP L/E DELAMINATED AT NR 3 FLAP TRACK INBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 63.SDR SWAA2012082907137Flap · delaminatedLEFT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM & AMM.SDR SWAA2012082807094Flap · delaminatedLEFT WING O/B FORE FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR CA120825001Bracket · loose(CAN) DURING 300 HR INSPECTION THE FLAP BELLCRANK ATTACHMENT BRACKET ATTACHMENT BOLTS WERE FOUND LOOSE. NO DAMAGE WAS NOTED AND HARDWARE WAS RE-TORQUED.SDR SWAA2012091907759Flap · delaminatedRIGHT WING OUTBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.
Back to JASC 5753