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 IPXA09657513Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT O/B AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657512Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT MID AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657505Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT O/B AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657504Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT MID AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657476Hinge Fitting · crackedINSPECTION TYPE:N/A RIGHT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG FOUND CRACKED. INBOARD FLANGE CRACK LENGTH 1.5 INCH, OUTBOARD FLANGE CRACK LENGTH 0.875 INCH. RIGHT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02 -2R1 FIG 201 REV 45.SDR FDEA200909223349Skin · chafedLT WING UPPER SKIN ON CTR FLAP HAS 3 EA CHAFE MARKS ON RIVET HEADS. REMOVED DAMAGE AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57- 50-00 FIG. 205SDR IPXA09M57517Skin · delaminatedINSPECTION TYPE:4C DENT WITH DELAM ON RIGHT I/B FLAP VANE LOWER SKIN NEAR MID TRACK. REMOVED DAMAGE, APPLIED AND CURED REPAIR PLIES IAW MD-11 SRM 57-50-80 REPAIR 2, FIGURE 201.SDR IPXA09657515Doubler · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP L/E AREA THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5C FIG 2 REV 45.SDR IPXA09657503Fairing · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657502Fairing · delaminatedINSPECTION TYPE:C LEFT WING O/B TRAILING EDGE FLAP MID L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA09657477Support Fitting · crackedINSPECTION TYPE:C LT WING I/B MAIN FLAP I/B AFT FLAP SUPPORT FTG FLANGE FOUND CRACKED. INBOARD FLANGE CRACK LENGTH 1.5 INCH, OUTBOARD FLANGE CRACK LENGTH 0.625 INCH. LEFT WING I/B MAIN FLAP I/B AFT FLAP SUPPORT FTG REPAIRED AS PER SRM 57-53-02-2R1, FIG 201 RSDR SWIA200922665Paint · roughAIRCRAFT ROLLED TO RIGHT UNCOMMANDED WHEN FLAPS EXTENDED. (FLT 6140) SMOOTHED NEW PAINT RIDGES ON FLAP.SDR IPXA09557433Flap · damagedINSPECTION TYPE:C2 RT OUTBOARD AFT FLAP TRAILING EDGE TIP HAS FIBER DAMAGE AT OUTBOARD FLAP TRACK FAIRING. REMOVED DAMAGE & REPAIRED PER SRM 57-53-01-0I-1 FIG 2 SHEETS 1-10&13 & DETAIL VII ITEM.SDR SWAA096009Wedge · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING I/B TRAILING EDGE MID FLAP O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA096007Flap · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER MT.SDR FDEA200909213341Skin · dentedRT WING, INBD FLAP HAS A DENT UPPER SKIN MEASURING .5 DIA. X .06 INCH DEEP. CUT OUT DAMAGE AREA, NDT, NO CRACKS FOUND. FABBED AND INSTALLED DOUBLER IAW SRM 57-50-00, FIG. 205SDR FDEA200909213340Skin · chafedRT WING, INBD FLAP UPPER SKIN HAS 2EA CHAFE MARKS .2500 INCH X .1250 INCH AT RIB 8-20 INCHES FROM L/E. CUT OUT DAMAGE AREA, NO CRACKS IAW NDT, FABBED AND INSTALLED DOUBLER IAW SRM 57-50-00, FIG. 205.SDR FDEA200909213339Skin · gougedLT WING INBD FLAP TOP SKIN HAS 2 EA GOUGES MEASURING 2 INCHES LONG, PREVIOUSLY COVERED BY PAINT, LOCATION BETWEEN RIBS 7 AND 9, 10 INCHES FROM FRONT SPAR. BLENDED 2EA GOUGES, NDT, NO CRACKS NOTED, CUT OUT DAMAGE FABBED AND INSTALLED DOUBLER IAW SRM 57-50-00SDR IPXA09657514Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 45.SDR IPXA09M57439Skin · dentedINSPECTION TYPE:4C DENT WITH CRACK ON LOWER SURFACE OF LEFT I/B FLAP VANE, MID SPAN. REMOVED DAMAGE AND APPLIED REPAIR PLIES IAW MD-11 SRM 57-50-80 REPAIR 2 FIG 201 SHEET 1 AND 4.SDR SWAA095939Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0946716Skin · delaminatedLEFT INBOARD AFT FLAP UPPER SURFACE OUTBOARD END IS DELAMINATED. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED REPAIR.SDR IPXA09557434Skin Panel · crackedINSPECTION TYPE:C2 LEFT O/B MAIN FLAP LOWER SURFACE HAS POSSIBLE CRACK 11 INCHES FROM AFT AND 2 INCHES FROM O/B END. REPAIRED MAIN FLAP PER 757-200 PR SRM 57-53-01-2R-4.SDR IPXA09557550Skin · crackedINSPECTION TYPE:C REF SURVEY SEQUENCE 449-W3-02 EXISTING REPAIR DOES NOT CORRELATE WITH THE VALID REPAIR FOR THIS AREA AS SPECIFIED IN B757 SRM 57-53-01-2R4. REMOVED EXISTING SKIN, HFEC SKIN AND STOP DRILL HOLES IAW NDTM 51-00-19 PT6 AND HOLES IAW NDTM51-00-1SDR FDEA200909183331Skin · damagedWHILE PERFORMING FLAP OPERATIONAL TEST, BRACKET FOR RT NR 5 SPOILER ACTUATOR CAUSED A PUNCTURE IN UPPER FWD OTBD AREA OF RT CENTER FLAP. DAMAGED AREA 26MM X 24 MM. REMOVED DAMAGED SECTION AT RT CENTER FLAP RIB 27 FWD AND OTBD. FABRICATED REPAIR SKIN, BUTT STSDR AALA20090924TUL02Wedge · damagedLIGHTNING STRIKE DAMAGE JUST FORWARD OF RIGHT INBOARD FLAP WEDGE AREA. REPAIRED PER SRM 57-01 AND 51-00-014.SDR FDEA200909173317Angle · crackedLT INBD MID FLAP LWR T/E ON ACT ROD CUTOUT WBL 106 ANGLE IS CRACKED. REMOVED ANGLE CRACKED FROM LT I/B MID FLAP IAW SRM 51-30-2, FABRICATED NEW ANGLE IAW SRM 51-40-4 FIG 1 SRM 57-50-2 FIG 5. INSTALLED NEW ANGLE IAW SRM 51-30-2 SRM 57-20-2 INSTALLED LOWER SKISDR SWAA095902Flap · puncturedDURING SCHEDULED 10Y CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REPAIRED AFT FLAP PER SRM.SDR FDEA200909173318Angle · crackedRT WING INBD MID-FLAP, AFT LWR CHORD ANGLE IS CRACKED IN 2 PLACES AT WBL 100. REMOVED LWR SKIN PANEL IAW SRM 51-30-2. REMOVED LWR CHORD ANGLE ON IB MID FLAP IAW SRM 51-30-2 REV 101. FABRICATED NEW CHORD ANGLE 5 FT X 1.5 INCHES FROM BAC1503-100046 7075 T6, SDR USAA2009102292848Flap · delaminatedSAL - Q2 - MAJOR REPAIR - DELAMINATION ON TRAILING EDGE OF LEFT WING INBOARD AFT FLAP. REPAIRED TRAILING EDGE OF LEFT WING INBOARD AFT FLAP IAW B737 SRM 51-70-10.SDR WRLA20090916200Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF LEFT OUTBOARD T/E FLAP CRACK. ACCOMPLISH EI NR:W2009A57B-1093, REV 00 AND EI NR:W2009A57B-1205.SDR WRLA20090916199Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF RIGHT OUTBOARD T/E FLAP CRACK. ACCOMPLISH E.I NO:W2009A57B-1092, REV 00 AND E.I NR :W2009A57B-1207 REV 00.SDR A6WA299040585Vane · dentedDENT ON LT WING, INBD FLAP VANE L/E BTWN WS 75.27 TO WS 97.70 LT WING, INBD FLAP VANE L/E REPAIRED IAW SRM 57-52-00, PAGE 201. DUE TO DENT FOUND OUT OF LIMITSIAW SRM 57-52-00, FIG 101 (PAGE 102) REPAIR NR 01. (K)SDR FDEA200909163304Skin · chafedLT WING INBD FLAP TOP SKIN HAS (2 EA) CHAFE AREAS MEASURING .3750 INCH X .2500 INCH X .010 DEEP., SECOND CHAFE MARK .3750 INCH X .2500 INCH X .020 DEEP. LOCATED 15 INCHES BACK TO FRONT SPAR BETWEEN RIB 11 AND 12. REMOVED DAMAGE AREAS (2 EA) AND INSTALLED REPASDR FDEA200909163303Skin · chafedLT WING INBD FLAP TOP SKIN HAS (2 EA) CHAFE AREAS MEASURING .3750 INCH X .2500 INCH X .010 DEEP., SECOND CHAFE MARK .3750 INCH X .2500 INCH X .020 DEEP. LOCATED 15 INCHES BACK TO FRONT SPAR BETWEEN RIB 11 AND 12. REMOVED DAMAGE AREAS (2 EA) AND INSTALLED REPASDR FDEA200909163302Skin · chafedRT WING INBD FLAP UPPER SKIN HAS CHAFE MARK APPROX 1 SQUARE INCH AT 10 INCHES FROM INBD SIDE AND 20 INCHES FROM L/E. REMOVED DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 57-50-00, FIG 205.SDR IPXA09M57429Skin · dentedINSPECTION TYPE:4C SMALL DENT ON UPPER SKIN I/B FLAP LT SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-00-01 FIG 201 REPAIR 1 SHEET 1 OF 4.SDR SWAA095899Flap · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA095876Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.SDR IPXA09557362Wedge · damagedINSPECTION TYPE:N/A LT WING O/B TRAILING EDGE FLAP WEDGE HAS A HOLE. REPAIRED PER EO-B757-5750-34923-A.SDR A6WA200940611Fitting · wornRT WING OTBD FLAP ALIGNMENT FITTING 601R10156 FOUND WITH ROLLER WEAR DAMAGE. RT WING, OTBD FLAP ALIGNMENT FITTING, REPAIRED IAW REO 601R57-51-149, REV NC. (K)SDR FDEA200909123315Spar · crackedRT WING LWR T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED LWR CHORD SECTION IAW DWG 27-57-038 REV C & DOUBLER IAW DWG SR27-57-038 REV C. TRIMMED OUT INBD AREA IAW DWG SR27-57-038, REV C & FABRICATED 2 ANGLES & HEAT TREATED ANGLES TO T6 IAW ER NR 2SDR FDEA200909123314Spar · crackedLT WING LOWER T/E, FALSE SPAR IS CRACKED AT INBD END, WBL 118. REMOVED DOUBLER, CUT-OUT LOWER CHORD, FABRICATED NEW WEB, 2 EACH ANGLES, NEW LWR CHORD, NEW DOUBLER, STRAPS, 2 FILLERS AND INSTALLED PARTS IAW DWG SR27-57-038 REV C.SDR A6WA200940571Lug · corrodedLT WING FLAP HINGE BOX AT WS 80.50 AFT LUG CORRODED UNDER BUSHING INBD LT WING FLAP HINGE BOX AT WS 80.50 AFT LUG INBD REPAIRED IAW REO 601R57-21-1164. (K)SDR QXEA2009091400678Skin · chafedRIGHT FUSELAGE SKIN CHAFED FROM AFT WING FLAP STAB FAIRING. REMOVED AFT INBOARD , TOP RIGHT WING PANNEL FOR ACCESS IAW SRM 51-42-21. ORINGIAL MATERIAL .063, BLENDED AREA TO DEPTH .012, WIDE .8 LENGTH 1.2 INCHES. SECONDARY STRUCTURE (APRON) BETWEEN FS 820 ANSDR QXEA2009091400677Vane · chafedRIGHT INBD FLAP VANE CHAFED ON TOP TRAILING EDGE. BLENDED CHAFE AT RT INBD FLAP VANE AT TOP OF TRAILING EDGE. FLAP VANE TOP T/E IS .050", BLENDED AREA OUT .002", REMAINING THICKNESS IS .048". BLENDED AREA WITHIN LIMITS OF SRM 57-52-02. ALL WORK DONE IAW SSDR RU3A0915Hinge Fitting · chafedLT OUTBOARD FLAP (INBOARD HINGE FITTING ON OUTBOARD SIDE) HAS SEVERE CHAFING DAMAGE (CAUSED BY AFT ROLLER BEARING) NEARLY TO THE POINT OF FAILURE.SDR RU3A0914Attach Fitting · wornRT OUTBOARD FLAP (INBOARD HINGE FITTING ON OUTBOARD SIDE) HAS BEARING WEAR. FLAP BEARING HAS CHAFED FLAP HINGE FITTING ALMOST THROUGH THE THICKNESS OF THE METAL. FLAP ROLLER BEARING ATTACH FITTING FAILURE WAS IMMINENT.SDR IPXA09B57331Flap · delaminatedINSPECTION TYPE:C LT WING I/B AFT FLAP L/E DENT / DELAM 147.5 INCHES FROM O/B EDGE INT REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5.C FIG 2 REV 53.SDR IPXA09M57440Skin · misrepairedINSPECTION TYPE:1/C REPAIR SURVEY SEQ 284-W4-01 RIGHT WING O/B FLAP LOWER SKIN REPAIR DOES NOT CORRELATE WITH SRM. REPAIRED IAW IPXA EO MD11-5750-35012-B AND SAA EA 011-5754-01-A2028 REF IPXA RCD 343248.
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