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 FDEA200905041497Mount · corrodedCORROSION, RT WING OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT FWD AND AFT SURFACE AT WING SIDE. REWORKED AS PER EA 1-5750-129202, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR SWAA092783Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWIA200922093Lug · crackedLEFT OUTBOARD FLAP HINGE BOX LUG CRACKED. (C CHECK) REPAIRED PER AMM.SDR UALA2009050401276Skin · delaminatedRIGHT INBD AFT TE FLAP HAS DELAMINATION 3.5, LENGTH BY 1.875, WIDTH. CENTER OF DAMAGE IS LOCATED 10 OUTBOARD OF FLAP'S INBOARD EDGE (WBL 73). DAMAGE BEYOND LIMITS. REMOVED DAMAGED SECTION. PER SRM 57-53-02 P112. ITEM REPAIRED PER SRM. ITEM MUST HAVE PERMAMESDR IPXA09M55936Wedge · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ W4-05, RT INBD FLAP T/E WEDGE HAS AN EXISTING REPAIR BETWEEN XIFH207-225 THAT IS NOT PER SRM, NOT ON MRCSSR, DISCREPANCY IS WITH FASTENERS. REMOVED AND REINSTALLED RT INBD FLAP TE WEDGE REPAIR REF EO MD11-5750-3 3513-A ANSDR IPXA09M55935Skin · misrepairedINSPECTION TYPE:2C REPAIRED SURVEY SEQ NR W3-07, LT INBD FLAP UPPER SKIN EXISTING REPAIR BETWEEN XIFH213.050-219 NOT PER SRM, NOT ON MRCSSR. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER AND INSTALLED REF MD11 SRM VOL 1 57-10-00 FIG 38.SDR IPXA09M55934Wedge · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ W3-08, LT INBD FLAP T/E WEDGE BETWEEN XIFH165-171 NOT PER SRM, NOT ON MRCSSR, DISCREPANCY IS WITH FASTENERS. REMOVED LT INBD FLAP TE WEDGE, FABRICATED 2 Z-ANGLES AND INSTALLED Z-ANGLE AND T/E WEDGE REF SRM VOL1 57-10-00 FISDR IPXA09M55927Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W3-06 LT INBD FLAP LWR SKIN EXISTING REPAIR NOT PER SRM AND NOT ON MRCSSR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW MD-11 SRM VOL 1 57-10-00 FIG 38.SDR IPXA09M55868Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ. W4-07, RT INBD FLAP LWR SKIN, EXISTING REPAIR BETWEEN XIFH 249-255 IS NOT PER SRM, NOT ON MRCSSR. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 38 AND 57-10-00 PG 1 PARA 1.SDR ASAA0945420Skin · gougedRIGHT I/B E GATE UPPER SKIN GOUGED BEYOND REPAIR. REMOVED AND REPLACED RIGHT I/B E GATE UPPER SKIN MATERIAL 2219 T62.SDR ASAA0945419Skin · delaminatedLEFT I/B FORE FLAP UPPER T/E SKIN IS DELAMINATED 34 INCHES FROM O/B END AND 8.5 INCHES FROM AFT END. REPAIRED LEFT I/B FORE FLAP UPPER T/E SKIN IS DELAMINATION. MATERIAL USED 2024 T3.SDR USAA2009062391562Fitting · crackedMCN - C22 - MAJOR REPAIR - CRACK IN NR 6 FLAP TRACK FIXED FAIRING INTERFACE FITTING. REPAIRED NR 6 FLAP TRACK FIXED FAIRING INTERFACE FITTING IAW US AIRWAYS EA 130262.SDR SWAA092819Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACED DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR QXEA2009050100301Vane · damagedPDX - C5 - RT FLAP OUTBOARD MOVEABLE VANE BRACKET AT WS 220 HAS WEAR AND SHARP EDGES. REMOVED SHARP EDGES, WEAR WITHIN LIMITS REF SRM 57-53-01-101-001-A01 TABLE 2. PREPPED AND RESTORED FINISH TO AFFECTED AREA REF SRM 51-25-01 PAGE 12 PARA 2-A-G.SDR QXEA2009050100300Vane · damagedPDX - C5 - RT FLAP OUTBOARD MOVEABLE VANE HAS CHAF ON LOWER LEADING EDGE AT WS 272.00. BLENDED AREA TO MAX DEPTH OF .014 INCH WITHIN LIMITS REF SRM 57-53-01-101-001-A01 TABLE 1. PREPPED AND RESTORED FINISH TO BLENDED AREA REF SRM 51-25-01 PG 12 PARA 2-A-G.SDR QXEA2009050100299Skin · chafedPDX - C5 - RT FLAP OUTBOARD MOVEABLE VANE HAS CHAFING ON INBOARD UPPER SURFACE AT WS 166.00. BLENDED DAMAGE TO MAX DEPTH OF .004 INCH WITHIN LIMITS REF SRM 57-53-01-101-001-A01 TABLE 1 PREPPED AND RESTORED FINISH TO BLENDED AREA REF SRM 51-25-01 PG 12 PARA 2-SDR ASAA0945391Skin Panel · wornTRAILING EDGE PANEL I/B SUPPORT IS WORN ON LT WING. REMOVED AND REPLACEDSDR ASAA0945387Rib · crackedFOUND I/B FORE FLAP TRACK RIB INSTALLATION I/B RIB TO BE CRACKED AT LOWER FLANGE ON RIGHT O/B MID FLAP. THE I/B FOREFLAP TRACK I/B RIB WAS REMOVED AND REPLACED WITH NEW PER SRM 51 40 02.SDR ASAA0945386Frame · crackedLEFT O/B MIDFLAP NR 2 CARRIAGE A FRAME IS CRACKED. REPLACED CRACKED A FRAME OF THE LEFT O/B MIDFLAP NR 2 CARRIAGE. CFE SERVICEABLE PART PO 311981 AND INSTALLED TO THE NR 2 CARRIAGE PER SOPM 20 50 01.SDR IPXA09M55896Skin · damagedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W4-04 EXISTING REPAIR HAS A GOUGE ON RT INBD FLAP UPPER SKIN BETWEEN XIFH 231-243. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW IPXA EO MD11-5750-33490-A AND SAA EA 011-5753-01-A1764.SDR IPXA09M55717Skin · dentedINSPECTION TYPE:N/A LT WING UPPER SKIN DENTED ON I/B FLAP. REPAIR PER EO MD-11-5750-33299A.SDR IPXA09555725Flap · damagedINSPECTION TYPE:C4 ASSOCIATED PAINTERS RESPONSIBILITY: LT WING I/B AFT FLAP DAMAGED AT I/B UPPER SURFACE CORNER. FLAP WAS REPAIRED PER SRM 51-70-04.SDR IPXA09B55756Flap · delaminatedINSPECTION TYPE:C RIGHT - I/B FOREFLAP TE LWR I/B AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.SDR USAA2009062491582Skin · delaminatedMCN - C22 - MAJOR REPAIR - DELAMINATION ON LEFT OUTBOARD FORE FLAP UPPER SKIN 81 & 87 INCHES FROM INBOARD END. REPLACED LEFT OUTBOARD FORE FLAP IAW US AIRWAYS TASK CARD R3M27022.SDR ASAA0945382Skin · chafedLEFT O/B MIDFLAP L/E SKIN CHAFED 4 INCHES AT I/B END. REPAIRED LEFT O/B MIDFLAP L/E SKIN PER SRM 57 53 01.SDR ASAA0945381Skin · chafedRIGHT O/B MIDFLAP L/E SKIN CHAFED 3 INCHES FOR I/B END. RIGHT O/B MIDFLAP L/E SKIN WAS REPAIRED PER SRM 57 53 01.SDR ASAA0945380Skin Panel · gougedLEFT O/B MIDFLAP O/B AFT LOWER AFT PANEL UPPER SURFACE IS GOUGED AT NR 3 AND NR 4 AFT FLAP TRACK. REPAIRED CHAFING DAMAGE ON LEFT O/B MID FLAP O/B LWR AFT SKIN PANEL UPPER SURFACE.SDR ASAA0945379Skin · chafedRIGHT O/B MIDFLAP O/B AFT LOWER PANEL UPPER SURFACE IS CHAFED AT NR 3 AND NR 4 AFT FLAP TRACK. REPAIRED RIGHT O/B MIDFLAP O/B AFT LOWER PANEL UPPER SURFACE IS CHAFED AT NR 3 AND NR 4 AFT FLAP TRACK.SDR FDEA200904271423Skin · dentedFOUND DENT ON CENTER FLAP RT LOWER SKIN RIB 13-15 PATCH REPAIR PERFORMED IAW SRM 57-50-00 FIG 205.SDR IPXA09B55757Skin · delaminatedINSPECTION TYPE:C LEFT WING - O/B FORE FLAP T/E LWR SURFACE DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.SDR IPXA09B55755Skin · delaminatedINSPECTION TYPE:C RT WING O/B FORE FLAP T/E UPPER SURFACE I/B AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.SDR USAA2009042891002Flap · separatedPHX - RON - MAJOR REPAIR - SEPARATION ON RIGHT WING OUTBOARD AFT FLAP TRAILING EDGE APPROX 6 INCHES FROM OUTBOARD END. REPAIRED RIGHT WING OUTBOARD AFT FLAP TRAILING EDGE IAW B737 SRM 51-70-10.SDR USAA2009042891001Spindle · crackedPHX - RON - MAJOR REPAIR - RIGHT WING OUTBOARD FLAP SPINDLE UT INSPECTION INDICATES THAT THE SPINDLE IS CRACKED PER STEP 2 OF US AIRWAYS TASK CARD I3C57018. REPLACED RIGHT WING OUTBOARD FLAP SPINDLE IAW B737 AMM 27-51-44-4.SDR SWAA092639Flap · debondedDURING SCHEDULED 22Y CHECK, FOUND RT WING OUTBOARD AFT FLAP DISBONDED NEAR INBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.SDR ASAA0945298Support Angle · chafedLEFT PYLON I/B MID FLAP SPRING DOOR CUTOUT LOWER EDGE SUPPORT ANGLE AT AFT END HAS CHAFING DAMAGE. REMOVED DAMAGED STIFFENER AND INSTALLED NEW STIFFENER.SDR UIEA200900028Skin · dentedLT WING OUTBOARD AFT FLAP HAS A DENT ON TOP SURFACE SKIN. AT WBL 525.32 AND 14 INCHES FROM TRAILING EDGE. DENT IS 1.750 INCHES IN DIAMETER. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-09, FIG 5, SHEETS 7 AND 8, 250 DEGREE CURE PER SRM 51-40-12. ALSO, RESDR IPXA09M55899Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-013 LHW INBD FLAP INBD FAIRING INNER LWR SKIN FLUSH REPAIR SPLICE SECTION ON SCREW HOLE. REPAIR NEEDS VALIDATION. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W3-013 DOES NOT CORRELATE TO ANY SRM REPAIR. LHW INBSDR IPXA09B55848Panel · corrodedINSPECTION TYPE:D LT WING I/B TRAILING EDGE MID FLAP I/B LOWER FWD PANEL AFT 82 INCHES FOUND CORRODED. LT WING I/B TRAILING EDGE MID FLAP I/B LOWER FWD PANEL AFT 82 INCH AREA REPAIRED AS PER HX RS NO R57-55-36310 REV A & UPS EO B747-5750-33412-A.SDR IPXA09B55843Panel · corrodedINSPECTION TYPE:D LT WING I/B TRAILING EDGE MID FLAP I/B LOWER AFT PANEL AFT 82 INCHES FOUND CORRODED. LT WING I/B TRAILING EDGE MID FLAP I/B LOWER AFT PANEL AFT 83 INCHES AREA REPAIRED AS PER HX RS R57-55-36310 REV A AND UPS EO B747-5750-33412-A.SDR IPXA09155802Skin · gougedINSPECTION TYPE:5YR LT WING CENTER FLAP UPPER SKIN GOUGED, 18 INCHES FWD OF RUB STRIP, JUST O/B OF NR 3 FLAP TRACK. FABBED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00, PG 217-218, PARAGRAPH 4E AND PG 220 FIG 205, AND 51-31-00, PG 23-24, TABLE 3 SHT 3.SDR UALA2009042701213Skin Panel · chafedRIGHT O/B MID FLAP LOWER AFT I/B SKIN PANEL IS CHAFED ON LOWER SURFACE 48 INCHES FROM I/B END OF PANEL ON PREVIOUS REPAIR DOUBLER. RIGHT I/B MID FLAP LOWER AFT SKIN WAS REPAIRED PER SRM 51-70-10.SDR ASAA0995307Flap Track · corrodedFOUND ON INSTALLATION OF INBOARD FLAP ON LT SIDE FOUND O/B TRAILING EDGE TRACK FOUND CORROSION ON O/B TRACK. REMOVED AND REPLACED TRACK.SDR ASAA0945270Skin Panel · chafedRIGHT O/B MID FLAP LOWER AFT I/B SKIN PANEL IS CHAFED ON LOWER SURFACE 48 INCHES FROM I/B END OF PANEL ON PREVIOUS REPAIR DOUBLER. RIGHT I/B MID FLAP LOWER AFT SKIN WAS REPAIRED PER SRM 51-70-10.SDR ASAA0945269Skin Panel · chafedRIGHT O/B MID FLAP LOWER AFT I/B SKIN PANEL IS CHAFED ON LOWER SURFACE 33 INCHES FROM I/B END OF PANEL ON PREVIOUS REPAIR DOUBLER. RIGHT O/B MID FLAP LWR AFT SKIN WAS REPAIRED PER SRM 51-70-10.SDR FDEA200904241398Structure · crackedLEFT INBOARD MIDFLAP LOWER TRAILING EDGE CHORD CRACKED AT WBL100. CUT OUT DAMAGED AREA DIM 48 INCH, FABRICATED NEW CHORD, SPLICE ANGLE AND INSTALLED REPAIR PARTS IAW SRM 51-40-2, 57-50-2 AND 51-30-2.SDR IPXA09M55890Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-W4-011, RT WING, INBD FLAP TOP SURFACE AT XIFH 228, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-011 DOES NOT CORRELATE TO SRM 57-10-00 FIG 38, VOLI, REV40. RHW INBD FLAP TOP SURFASDR IPXA09M55889Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-W4-010, RT WING, INBD FLAP TOP SURFACE AT XIFH 145, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-010 DOES NOT CORRELATE TO SRM 57-10-00, FIG 38, VOLI, REV40. EXISTING REPAIR DOUBLESDR IPXA09M55867Wedge · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-W4-012, RT WING, INBD FLAP, INBD T/E, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-012 DOES NOT CORRELATE TO SRM 57-20-00, FIG 3, VOL I, REV 40. EXISTING REPAIR REMOVED PER SRM 51SDR CA090424004Cable · frayed(CAN) FWD FLAP RETURN CABLE INSPECTED IN AREA UNDER PHENOLIC 1 INCH PULLEY AFT OF STN 44. FOUND ONE SHINY WEAR SPOT. ON REMOVAL DISCOVERED APPROX 7 WIRES BROKEN AT SHINY SPOT UNDER PULLEY AND APPROX 10 WIRES BROKEN AT FRAYED SPOT APPROX 2 INCHES FWD WHERE THE SDR SWAA092662Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.
Back to JASC 5753