JASC 5753
Service difficulty reports · 31,521
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 SWAA050225Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.SDR IXXA050197SDoubler · gougedDURING ROUTINE C-CHECK FOUND LEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN REPAIR PATCH GOUGED AT CENTER HINGE. REMOVED FASTENERS AND DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW DOUBLER, AND FASTENERS IAW DC8 SRM 5SDR IXXA0500186SAngle · crackedDURING ROUTINE C-CHECK FOUND LEFT WING OUTBOARD FLAP INBOARD CENTER AFT INSIDE PANEL NUMBER 551 AREA ANGLE CRACKED AND 3 FASTENERS MISSING. REMOVED FASTENERS, AND ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW ANGLE AND INSTSDR SWAA050220Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LT WING T/E AFT FLAP PER MM.SDR IXXA0500194SHinge · gougedDURING ROUTINE C-CHECK FOUND RIGHT HAND INBOARD FLAP, INBOARD HINGE, OUTBOARD ARM GOUGED AND CHAFED. REMOVED DAMAGE, ORIGINAL THICKNESS WAS .250, REMOVED .081 MATERIAL, REMAINING THICKNESS .169, OUT OF LIMITS. FABRICATED REPAIR PARTS, LOCATED, DRILLED, PRIMESDR IXXA0500193SSkin · gougedDURING ROUTINE C-CHECK FOUND RIGHT HAND OUTBOARD FLAP UPPER SKIN IS GOUGED AT PREVIOUS REPAIR. REMOVED DAMAGED REPAIR, FABRICATED, NEW REPAIR PART, ALODINED, PRIMED AND INSTALLED NEW REPAIR PART IAW DC8 SRM 57-2-0, 51-1-20D, AND 51-1-8.SDR IXXA0500189SDoubler · tornDURING ROUTINE C-CHECK FOUND LEFT WING INBOARD FLAP OUTBOARD FORWARD HINGE FAIRING PANEL DOUBLER TORN. REMOVED FASTENERS AND DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW DOUBLER WET WITH SEALANT, AND INSTALLED FASSDR IXXA0500187SSupport Angle · crackedDURING ROUTINE C-CHECK FOUND RIGHT WING OUTBOARD FLAP INBOARD EDGE AT STATION XW 129 TRAILING EDGE SUPPORT ANGLE CRACKED. REMOVED FASTENERS, AND DAMAGED SUPPORT ANGLE. FABRICATED NEW SUPPORT ANGLE. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW SUPPORTSDR QXEA200500398Flap Track · crackedYYC - RIGHTHAND WING FLAP TRACK NR 5 CANOE FAIRING BRACKET CRACKED. REPAIRED IAW Q400 SRM 51-42-05-330-001.SDR SWAA050200Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.SDR IXXA0500180SClip · crackedDURING ROUTINE C-CHECK, FOUND LEFT WING OUTBOARD FLAP INBOARD SUPPORT HINGE TRAILING EDGE UPPER WING SUPPORT CLIP CRACKED. REMOVED FASTENERS, FABRICATED NEW CLIP, TREATED, PRIMED, AND INSTALLED NEW CLIP AND FASTENERS IAW DC8 SRM 57-2-0, 51-1-21, AND 51-1-8.SDR IXXA0500178SSkin · dentedDURING ROUTINE C-CHECK FOUND LEFT WING INBOARD FLAP LOWER SKIN DENTED SEVERAL PLACES. BLENDED TWO DENTS WITHIN LIMITS ONE DENT OUT OF LIMITS. REPAIRED OUT OF LIMIT DENT IAW DC8 SRM 57-2-0. TREATED AND PRIMED ALL DENTS IAW DC8 SRM 51-1-8.SDR IXXA0500176SBracket · wornDURING ROUTINE C-CHECK FOUND LEFT WING OUTBOARD FLAP AT OUTBOARD FLAP TRACK UPPER SURFACE HAS BRACKET WORN / CHAFED THROUGH AND BAD FASTENERS. REMOVED BAD FASTENERS, FABRICATED NEW BRACKET, TREATED, PRIMED, INSTALLED NEW BRACKET AND FASTENERS IAW DC8 DRAWING SDR QXEA200500397Skin · chafedYYC - RIGHTHAND OUTBOARD FLAP HAS A CHAFING MARK SEVERAL FEET LONG FROM CONTACT WITH THE UPPER FLAP TOP SURFACE. REPAIRED IAW Q400 SRM 57-20-30-320-801, 57-52-30-940-001.SDR QXEA200500376Skin · chafedYYC - RIGHTHAND INBOARD FLAP HAS THREE AREAS WHERE IT IS CHAFING WITH THE UPPER SHROUD AND HAS WORN THROUGHT TO THE METAL. REPAIRED IAW Q400 SRM 57-51-30-940-001, 57-51-30-320-801.SDR QXEA200500375Skin · chafedYYC - LEFTHAND INBOARD FLAP HAS TWO AREAS WHERE IT IS CHAFING WITH THE UPPER SHROUD AND HAS WORN THROUGH TO THE METAL FLAP SURFACE. REPAIRED IAW DHC-8 400 SRM 57-51-30-320-801 AND 57-51-30-940-001.SDR SWAA050184Wedge · debondedDURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD MID FLAP T/E WEDGE DISBONDED. REMOVED AND REPLACED T/E WEDGE PER MM.SDR 05FDEA00152Support · corrodedCOMPLY WITH EA 8-5750-55430 WINGS - FLAP VANE SUPPORT CORROSION REWORK RIGHT O/B FLAP. COMPLIED WITH EA 8-5750-55430.SDR AWXA200500195Skin · delaminatedMCN - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 103.5 INCHES FROM THE OUTBOARD END. MAINTENANCE REMOVED DAMAGED AREA OF UPPER RT OUTBOARD FORE FLAP; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAISDR AWXA200500194Skin · delaminatedMCN - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP WAS FOUND DELAMINATED 10 INCHES FROM THE INBOARD END. MAINTENANCE REMOVED DAMAGED AREA OF UPPER RT OUTBOARD FORE FLAP; FABRICATED A CORE FILLER AND DOUBLER; BONDED REPAIR PASDR AWXA200500179Skin · delaminatedMCN - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OF THE LT INBOARD FORE FLAP WAS FOUND DELAMINATED 32.5 INCHES TO 37.5 INCHES FROM THE OUTBOARD END. MAINTENANCE CUT OUT DAMAGE IN UPPER SURFACE OF LT INBOARD FORE FLAP; FABRICATED A CORE FILLER AND EXTESDR SWAA050178Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED LEFT T/E AFT FLAP PER MM.SDR QXEA200500133Skin · chafedPDX - LEFT HAND WING OUTBOARD FLAP UPPER SKIN HAS CHAFE MARKS AT WS YW 211 AND YW 240. REPAIRED IAW Q400 SRM 51-25-05-370-801 AND HORIZON AIR EA 6-57-89A.SDR ASAA0540041Skin · dentedOKC - LT WING IB AFT FLAP LOWER SKIN HAS 2 DENTS TOGETHER, 17 INCHES FROM THE IB EDGE AND 7.5 INCHES FROM THE TE A=5.3, Y=.075, A/Y= 70. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM. (K)SDR 05FDEA00139Hinge · corrodedRIGHT WING INBOARD FLAP HINGE INBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMATER, FOUND TO BE OUT OF LIMITS IAW DAC CMM 57-52-01. ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01 VOL 2, FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE DSDR 05FDEA00136Hinge · corrodedRIGHT WING INBOARD FLAP HINGE OUTBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMETER, FOUND TO BE OUT OF LIMITS IAW CMM 57-52-01, ALODINE AND PRIMED BORE IAW DC10-10 SRM 51-21-01. FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INSIDE DIAMETER OSDR 05FDEA00134Vane · delaminatedLT HAND WING, INBOARD FLAP VANE LOWER CENTER SKIN FOUND DELAMINATED WHICH MEASURES 36.0 INCHES IN LENGTH AND 14.0 INCHES IN WIDTH AT STA 216.300 - 279.345 DELAMINATION AT LEFT HAND WING, INBOARD FLAP VANE LOWER CENTER SKIN AT STA 216.300 - 279.345 REPAIRED PERSDR QXEA200500174Fitting · corrodedYYC - LEFT OUTBOARD FLAP INBOARD GUIDE ROLLER FITTING HAS FRETTING CORROSION AND GOUGED. REPAIED IAW HORIZON AIR EA R-57-93 AND REO 670-57-53-017.SDR DHL2004809523Structure · wornRT WING OUTBOARD FLAP UPPER FWD PLATING WORN, XF 227.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 01-19-05, DWG X32-R04 REV-A DATE 01-19-05. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. TRIMMED OUT DAMAGED PLATING SEGMENT SDR SWAA050154Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E FLAP PER MM.SDR UIEA200500003Skin · delaminatedFLIGHT CT 603, PIK-LUX 08 JAN, 2005 - IB LOG ITEM, LT OB MID FLAP PANEL DELAMINATED. MAINTENANCE PICK-UP ITEM. DURING FLAP REPLACEMENT FOUND IB CARRIAGE ASSY CORRODED. (LEVEL 1) REPLACED LT OB MID-FLAP, MM 27-51-04, REF LOG PAGE 544103. REPLACED IB CARRIASDR ASOA05094Rib · crackedDURING A C-CHECK, THE RT IB FLAP L/E RIB WAS FOUND TO BE CRACKED BEYOND LIMITS AT RIB 6. MAINTENANCE REMOVED AND REPLACED THE RT IB FLAP L/E RIB AT RIB 6 IAW SRM. (K)SDR UPS05843851Stop Fitting · crackedINSPECTION TYPE: C3, RIGHT STA 98 FLAP UPSTOP FITTING CRACKED. GAINED ACCESS TO REPAIR SITE. REMOVED & REPLACED FITTING REF SRM 51-3-0, 51-1-8, 51-1-21, 51-1-15. RESTORED REPAIR AREA.SDR SWAA050106Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED T/E AFT FLAP PER MM.SDR SWAA050105Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR 05FDEA00111Hinge · corrodedLEFT WING INBOARD FLAP HINGE OUTBOARD PIVOT BUSHING GALLED AND PITTED. MEASURED BORE DIAMETER, FOUND TO BE OUT OF LIMITS IAW DAC CMM 57-52-01, ON NON-ROUTINE N00390. FABRICATED, INSTALLED AND HONED BUSHING TO A FINAL INNER DIAMETER OF .9995-1.0005 INCHES IAWSDR DL73G050031Spar · crackedDURING SHOP VISIT, THE NR 3 MID FLAP FRONT SPAR ASSEMBLY WAS FOUND WITH A CRACKED LOWER CHORD AND DENTED WEB. DAMAGE WAS DUE TO SERVICE DAMAGE. REPAIRED PER ERA 093135-14.SDR UPS05243700Bracket · crackedINSPECTION TYPE: C, NR 5 FLAP TRACK, FWD O/B FAIRING ATTACH ANGLE BRACKET IS CRACKED. BRACKET REPLACED IAW SRM 51-20-1.SDR UPS05843848Support Fitting · corrodedRT STA 98 FLAP SUPPORT FITTING (CANOE) HAS CORROSION UNDER FLAP TRACK AREA, O/B SURFACE .025 DEEP I/B SURFACE IS .006 DEEP. UNDERCUT AND REMOVED CORROSION .050 AND FABRICATED AND INSTALLED REPAIR FILLERS PER SB 27-164 PAGE 8.SDR SWAA050074Skin · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM.SDR UPS05243702Support Angle · crackedINSPECTION TYPE: C, NR 3 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED AT I/B AFT END. FAIRING SUPPORT ANGLE REPAIRED IAW SRM 51-20-01.SDR UPS05243701Support Angle · crackedINSPECTION TYPE: C, NR 4 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED AT O/B SIDE AT MLG BEAM. FAIRING SUPPORT ANGLE REPAIRED IAW SRM 51-20-1.SDR DHL2004809531Skin · damagedLT WING INBD FLAP UPPER SKIN DEFLECTED, XW 2.000 TO XW 91.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED DAMAGED PANEL PLATING IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW PANEL PLATING (AL2024-T3 0.050) IAW BOEING MESSAGE 1-XW84N, DWG SEMAN ESDR DL73S050011Fairing · looseAFTER T/O EXP VIBRATION, LIGHT TO MODERATE, APPROX 12,000 AND 300 KTS. SLOWED TO 250 VIBRATION SUBSIDED SOMEWHAT. EXPERIENCED VIBRATION THRU 210 KTS LIGHT. FOUND E/E DOOR SEAL OUT OF POSITION. REPAIRED SAME. FOUND 2 FLAP FAIRINGS LOOSE. TIGHTENED SAME.SDR SWAA050050Skin · delaminatedDURING SCHEDULED A2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA050048Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR 05FDEA00033Skin · damagedNON-ROUTINE NR N00380. RT WING REPAIR ON INBD FLAP LWR SURFACE T/E. VERIFIED THAT THE EXISTING REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-63790.SDR CA050106001Bearing · mismanufacturedTECHS FOUND DIFFICULTY WHILE ATTEMPING TO GREASE NEWLY INSTALLED FLAP CARRIAGE BEARINGS. BEARINGS WOULD NOT ACCEPT GREASE AS DIRECTED BY THE MM. A RECALL & INSPECT OF ALL INVENTORIED BEARINGS CARRIED OUT AT SPAR QUALITY DEPARTMENT. BEARINGS IN QUESTION WERE SDR IXXA0500179SAttach Fitting · crackedDURING ROUTINE C-CHECK, FOUND LEFT WING INBOARD FLAP OUTBOARD SUPPORT HINGE UPPER TRAILING EDGE ATTACH FITTING CRACKED. REMOVED FASTENERS AND DAMAGED BRACKET. RECEIVED NEW BRACKET, LOCATED, DRILLED, PRIMED AND INSTALLED NEW STEEL BRACKET IAW DC8 SRM 51-3-0, SDR AWXA200500153Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK, FOUND THE LT INBOARD MID FLAP WEDGE DELAMINATED AT THE OUTBOARD END BETWEEN WBL 164 AND WBL 168. MAINTENANCE REMOVED DAMAGED SKIN ON LT INBOARD MID FLAP WEDGE; FABRICATED A FILLER AND REPAIR DOUBLER; BONDED REPAIR PARTS
Back to JASC 5753