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.

SDR SWAA2021070791713Plate · crackedRIGHT WING TRAILING EDGE STRUCTURE HAS A CRACKED WIGGLE PLATE I/B OF #7 FLAP TRACK AND O/B OF PANEL 651DB. / REMOVED DAMAGED WIGGLE PLATE AND INSTALLED NEW PLATE PER SRM 51-40-02.Jun 3, 2020 · N250WN · Boeing 7377H4SDR IPXA2020062977051Doubler · crackedINSPECTION TYPE:3C, RH WING O/B FLAP UPPER SURFACE I/B FWD CORNER PRODUCTION DOUBLER IS CRACKED.REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED IN RH WING O/B FLAP UPPER SURFACE I/B FWD CORNER IAW DRWG NRC6753. (MINOR)Jun 3, 2020 · N262UP · Doug MD11FSDR SWAA2021081688949Skin · delaminatedLEFT WING INBD FLAP WEDGE HAS AREA OF DELAMINATION / REMOVED AND REPLACED LEFT WING INBRD FLAP O/B WEDGE WITH SERVICEABLE WEDGE PER SRM 51-40-02 CLEARANCE AND OPS CHECKS C/W ON N/R D441347Jun 2, 2020 · N8319F · Boeing 7378H4SDR SWAA2020061688515Skin · delaminatedLEFT OTBD AFT FLAP WAS DELAMINATED ON THE LOWER INBD CORNER. DELAMINATION AREA WAS 13' X 10'. REMOVED AND REPLACED THE FLAP IAW AMM 27-51-22. ADJUSTMENT AND OPS CHECKED GOOD IAW AMM 27-51-22.Jun 1, 2020 · N8319F · Boeing 7378H4SDR IPXA2020060356044Skin · dentedINSPECTION TYPE N/A LT WING INBD AFT FLAP TE WEDGE UPPER SKIN DENT 1.187 X 1.287 X .50, LOCATED 5.625 FROM TE AND 84.5" FROM OTBD EDGE OF FLAP. REMOVED DAMAGED SKIN AND CORE FROM 1 AREA FOR REPAIR. REMOVED PAINT. CONFIRMED DAMAGED WAS REMOVED. INSTALLED REJun 1, 2020 · N307UP · Boeing 76734AFSDR YEWA20200630001Flap Track · brokenDURING FLIGHT, THE NR 4 FLAP I/B FLAP TRACK BROKE INTO TWO PIECES ALLOWING THE FLAP TO CANT CAUSING IT TO JAM AND NOT ALLOW TRAVEL TO THE APPROACH POSITION. BECAUSE THE FLAP WAS CANTED IT ALSO ALLOWED IT TO CONTACT THE RT AILERON INDUCING A RESISTANCE IN THE May 26, 2020 · N911ZC · Beech C90ASDR FDEA202005261048Rib · crackedLEFT HAND WING CENTER FLAP SHOWING INDICATION AT RIB 27 AFT CRACKED. REPAIRED LEFT CENTER FLAP RIB 27 IAW SRM 57-50-00 PG 203 AND PG 220 AND EA 6-5750-T0354210-P1.May 26, 2020 · N675FE · Airbus A300F4605RSDR IPXA2020061556621Beam · crackedINSPECTION TYPE:2C RT O/B FLAP I/B HINGE AFT BEAM IS CRACKED. REMOVED, FABRICATED AND REPLACED BEAM IAW DWG ARC 2419 AND SRM 51-31-01. (MINOR)May 24, 2020 · N276UP · Doug MD11FSDR UIEA2020052701046Fitting · brokenRT WING NR 6 FLAP TRACK CANOE FAIRING FWD SUPPORT FRAME I/B ATT BONDING FOUND BROKEN. RT WING NR 6 FLAP TRACK CANOE FAIRING FWD SUPPORT FRAME DETAILED VISUAL INSPECTION CARRIED OUT OF THE INSTALLED REPAIR AND ALL ADJACENT VISIBLE SURFACE OF THE INITIAL FRAME TMay 23, 2020 · N850GT · Boeing 74787UFSDR UIEA2020052711094Rib · crackedLHW I/B FLAP T/E #3 MOVEABLE FAIRING FWD FRAME FOUND CRACKED. RIB REPAIRED IAW RI-57-50-14045 REV AMay 23, 2020 · N850GT · Boeing 74787UFSDR UIEA2020052701141Rib · crackedRHW I/B FLAP T/E #2 RIB LOWER END FOUND CRACKED(<P>RIB REPAIRED IAW RI-57-50-14037 REV A. </P>)May 23, 2020 · N850GT · Boeing 74787UFSDR SWIA2020080751640Skin · dentedRIGHT INBD FLAP LOWER SURFACE HAD TWO DENTS. REPAIRED THE FLAP LOWER SURFACE DENTS IAW SRM.May 22, 2020 · N751EV · Cndair CL6002C10SDR SWIA2020080751639Skin · dentedLEFT INBD FLAP LOWER SURFACE HAS DENTS. REPAIRED DENTS ON THE LT INBD FLAP, LOWER SURFACE IAW SRM. RESTORED FINISH TO REWORK AREA IAW SRM.May 22, 2020 · N751EV · Cndair CL6002C10SDR FDEA202005221032Skin · crackedLEFT HAND CENTER FLAP UPPER SKIN AT RIB 11 HAS 10.5" CRACK FWD OF REAR SPAR REPAIRED CRACK AT RIB 11 IN LEFT HAND CENTER FLAP IAW SRM 57-50-00 FIG 202 AND FIG 2 205. CAT "A" MAJOR REPAIRMay 22, 2020 · N674FE · Airbus A300F4605RSDR DU4R2020052000034Flap · chafedCHAFING AT RT WING OB FLAP INBD OF MID FLAP LOWER L/E.May 20, 2020 · N430YK · Boeing 737436SDR COEA2020062403921Beam · corrodedFLAP BEAM AT RIB 13R HAD CORROSION ON OUTBOARD SURFACE. REPAIRED IAW ES_0120046_01.16321 ISSUE A.May 18, 2020 · N921FX · Aerosp ATR42300SDR SWAA2020052679095Skin · delaminatedLEFT WING OUTBOARD AFT FLAP INBD CORNER LOWER SKIN IS DELAMINATED. REMOVED; CLEANED; SEALED AND APPLIED DECORATIVE FINISH ON LEFT WING O/B AFT FLAP I/B CORNER LOWER SKIN IAW SRM 57-53-01-2R-4 REV 70; SRM 51-70-10-2R-0 REV 70 AND AMM 51-21-99-300-801 REV 71. AMay 18, 2020 · N922WN · Boeing 7377H4SDR SWIA2020062351165Panel · chafedPANEL 684ET CHAFED. (C-CHECK) RO 6/21/2020 BLENDED OUT DAMAGE FLAP PANEL 684ET REF SRM. ORIGINAL MATERIAL THICKNESS .050" REF SRM. REMAINING THICKNESS .030". MATERIAL LOSS .020". MAX MATERIAL LOSS ALLOWED .010" (20%). FOUND TO BE OUT OF LIMITS REF SRM. OMay 16, 2020 · N748SK · Cndair CL6002C10SDR SWIA2020062651258Mount Bolt · corrodedRIGHT WING INBOARD FLAP, INBOARD FLAP VANE UPPER MOUNT BOLTS ARE CORRODED. (C-CHECK) RO 6/24/2020 REMOVED AND INSTALLED WITH NEW FROM STOCK 2EA BOLTS PN THE RT WING INBOARD FLAP INBOARD FLAP VANE UPPER MOUNT REF AMM.May 15, 2020 · N748EV · Cndair CL6002C10SDR SWAA2020060882938Stiffener · chafedRIGHT FLAP TRACK SUPPORT STIFFENER AT BS727A COMMON TO STR20R IS CHAFED. REMOVED CHAFED DAMAGED RT FLAP TRACK SUPPORT STIFFENER AT BS727A COMMON TO STR20R IAW SRM 51-40-02-0G-0. NO DAMAGE LIMITS GIVEN IN SRM. PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-May 15, 2020 · N483WN · Boeing 7377H4SDR SWAA2020060882939Stiffener · chafedLEFT FLAP TRACK SUPPORT STIFFENER AT BS727A COMMON TO STR20L IS CHAFED. REMOVED CHAFED DAMAGED STIFFENER AT BS727A COMMON TO STR20L LT FLAP TRACK SUPPORT IAW SRM 51-40-02-0G-0. NO DAMAGE LIMITS GIVEN IN SRM. PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-0May 15, 2020 · N483WN · Boeing 7377H4SDR SWAA2021081687004Skin · debondedDEBONDED IB MAIN FLAP WEDGE PANEL LOWER SKIN LOC AT 3IN FROM O/B EDGE ON T/E AREA AT RT WING / REPAIRED I/B MAIN FLAP WEDGE PANEL LOWER SKIN LOC AT 3 IN FROM O/B EDGE ON T/E AREA AT RT WING AS PER B737-700 SRM 57-53-01-2R-7 REPAIR 7 TOOL USED CALIPER PN:700-11May 14, 2020 · N924WN · Boeing 7377H4SDR SWAA2021070788802Plate · crackedLEFT WING TRAILING EDGE WIGGLE PLATE IS CRACKED AT ORSS 261. / REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE PER SRM 51-40-02May 14, 2020 · N7869A · Boeing 73779PSDR SWAA2021081289256Skin · delaminatedR/H I/B MAIN FLAP O/B WEDGE LOWER SKIN HAS DELAMINATION / REMOVED AND REPLACED R/H I/B MAIN FLAP O/B WEDGE PER SOPM 20-50-01.May 13, 2020 · N244WN · Boeing 7377H4SDR SWIA2020062651177Skin · dentedEVALUATE 2 DENTS ON THE LEFT INBD FLAP, INBD BOTTOM SIDE. ( TIRE PLANE OF ROTATION) (C-CHECK) RO 6/24/2020 REPAIRED 2 DENTS ON THE LEFT INBD FLAP, INBD BOTTOM SIDE AS PER REO. OPS CHECK GOOD REF AMM. M-337 AND TASK CARD COMPLIED WITH.May 12, 2020 · N748EV · Cndair CL6002C10SDR SWIA2020062651176Skin · dentedEVALUATE 2 DENTS ON RIGHT INBD FLAP, MIDDLE TOP SIDE. (C-CHECK) RO 6/24/2020 COMPLIED WTIH RT INBD FLAP DENT REPAIRS ON MIDDLE TOP SIDE AS PER REO. COMPLIED WITH M-337 AND TASK CARD.May 12, 2020 · N748EV · Cndair CL6002C10SDR SWIA2020062651175Skin · dentedEVALUATE SEVERAL DENTS ON RIGHT INBD FLAP, BOTTOM INBD SIDE (TIRE PLANE OF ROTATION). (C-CHECK) RO 6/24/2020 REPAIRED DENTS ON THE RT I/B FLAP REF SRM. OPS CHECK GOOD REF AMM.May 12, 2020 · N748EV · Cndair CL6002C10SDR FDEA2020051310920Frame · crackedRIGHTWING OUTBOARD FLAP, INBOARD HINGE FWD FAIRING FRAME IS CRACKED IN HALF A AND HAS ELONGATED RIVET HOLES. MARKED #58. REMOVED AND REPLACED FAIRING FRAME ON RH WING, OB FLAP INBD HINGE PANEL #635 BR PER DAC BLUE PRINT ARCO504.May 11, 2020 · N593FE · Doug MD11FSDR FDEA202005110918Frame · crackedNR 6 AFT FLAP TRACK FAIRING 672CB HAS DAMAGE ON FORWARD OUTBOARD FRAME. REPLACED FRAME IAW SRM 51-40-02 AND DRAWING 113N1752 ALSO REFER TO EA F-5720-T0353885 TITLE: WING-SECONDRY WING STRCT- NR 6 AFT FLAP TRACK FAIRING FRAME.May 11, 2020 · N917FD · Boeing 75723ASDR IPXA2020051155167Skin · puncturedINSPECTION TYPE:1CLH O/B AFT FLAP, OB UPPER SURFACE HAS PUNCTURE, MAKLED IN REDREPAIRED IAW B757 SRM REV107.00, 57-53-01-2R-1, AND SRM 51-70-04-OG, FIG 2, 350 DEG F CUREMay 11, 2020 · N427UP · Boeing 75724APFSDR IPXA2020051155164Repair · delaminatedINSPECTION TYPE:1CPREVIOUS REPAIR ON LOWER SURFACE OF LH AFT FLAP LOCATED 131 FROM IB EDGE BETWEEN AFSTA 464.655 AND 479.265 FAILS NDT ULTRASONIC BOND TESTREPAIRED IAW B757 SRM REV 107.00, 57-53-01-2R-1 AND SRM 51-70-04-OG, FIG 5, 350 DEG F CUREMay 11, 2020 · N427UP · Boeing 75724APFSDR IPXA2020051155160Skin · puncturedINSPECTION TYPE:1CLH OB AFT FLAP IS SHOWING A PUNCTURED HOLE, IB UNDERNEATH SURFACEREPAIRED IAW B757 SRM REV. 107.00, AND SRM 51-70-05-OG, FIG 5, 350 DEG F CUREMay 11, 2020 · N427UP · Boeing 75724APFSDR SWAA2021081676721Skin · delaminatedR/H WING INBOARD FLAP TRAILING EDGE DELAMINATED / REMOVED AND REPLACED 113A2500-14 TE WEDGE REF SRM 51-40-02 AND 51-40-05 REF SA-M 326 A1081275May 5, 2020 · N919WN · Boeing 7377H4SDR SWIA2020061051028Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE REQUIRES SKIN SEGMENT REPLACEMENT DUE TO MULTIPLE DENTS. R/H I/B FLAP LOWER SURFACE HAS BEEN REPAIRED IAW SRM, SPLICE REPAIR FROM FLS42.000 TO FLS48.000, FIG.COMPLIED WITH TASK CARDMay 5, 2020 · N752SK · Cndair CL6002C10SDR IPXA2020052645687Skin · dentedINSPECTION TYPE:2CLT WING I/B FLAP LOWER SURFACE HAS A DENT 10.2" FROM T/E AND 44" FROM O/B EDGE REQUIRES PERMANENT REPAIR.REPAIRED LT WING I/B FLAP DENT ON LOWER SURFACE BETWEEN XIFH 261 - 269 IAW VT-SAA EA 011-5750-01-A8177 REV IR AND UPS EO MD11-5750-76600-May 5, 2020 · N256UP · Doug MD11FSDR FDEA202005040886Attach Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" FOUND MOUNT HOLES CORROSION. CORROSION AT RIGHT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICMay 4, 2020 · N615FE · Doug MD11FSDR IPXA2020062256771Skin · gougedINSPECTION TYPE:3C WHILE INSTALLING THE LEFT MAIN LANDING GEAR FIXED BRACE ASSEMBLY, GEAR STAND DOOR OPENED AND CONTACTED THE LEFT I/B FLAP LOWER SKIN. REPAIRED GOUGED LT I/B FLAP LOWER SKIN BETWEEN XIFH 190 AND XIFH 213.05 IAW EA 011-5750-01-A8184 AND EO MD1May 2, 2020 · N261UP · Doug MD11FSDR FDEA2020051320873Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSMay 2, 2020 · N615FE · Doug MD11FSDR FDEA2020051320872Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "E" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "E" REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSMay 2, 2020 · N615FE · Doug MD11FSDR FDEA2020050420873Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "F" FOUND MOUNT HOLE CORROSION.May 2, 2020 · N615FE · Doug MD11FSDR FDEA2020050420872Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "E" FOUND MOUNT HOLE CORROSION.May 2, 2020 · N615FE · Doug MD11FSDR FDEA202004300855Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "C" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "C" REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATApr 30, 2020 · N615FE · Doug MD11FSDR FDEA202004300854Attach Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "B" FOUND MOUNT HOLES CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE ATTACH FITTING "B" REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED ECCENTRIC BUSHING FABRICATApr 30, 2020 · N615FE · Doug MD11FSDR SWAA2021081846108Fitting · brokenRH WING TRAILING EDGE FLAP WELL LOWER PANEL SUPPORT RAIL IS BROKEN AT RSS 281-287; 12' FROM REAR SPAR. / R/H WING T/E FLAP;PNL SUPPORT RAIL IS BROKEN; FITTING IS BROKEN AT RSS 281 TO RSS 287 12' FROM REAT SPAR. REMOVED BROKEN RAIL AND FITTING I/A/W SRM 51-40-0Apr 29, 2020 · N8631A · Boeing 7378H4SDR SWIA2020052950916Plate · chafedLEFT INBOARD FLAP VANE INBOARD LEADING EDGE CHAFED APPROXIMATELY 6€? FROM INBOARD END. (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED LT FLAP VANE SACRIFICIAL PLATE REF SRM.Apr 29, 2020 · N936EV · Cndair CL6002B19SDR SWIA2020052950915Plate · chafedRIGHT INBOARD FLAP VANE INBOARD LEADING EDGE CHAFED APPROXIMATELY 6€? FROM INBOARD END. (48 MONTH) RO 5/28/2020. REMOVED AND REPLACED RT FLAP VANE SACRIFICIAL PLATE REF SRM.Apr 29, 2020 · N936EV · Cndair CL6002B19SDR SWAA2021070776922Plate · crackedRIGHT WING; LOWER SHELF PANEL WIGGLE PANEL IS CRACKED; JUST AFT OF PYLON / REMOVED AND REPLACED; LOWER SHELF PANEL WIGGLE PLATE; RH WING JUST AFT OF PYLON PER SRM 51-40-02Apr 28, 2020 · N7889A · Boeing 73779LSDR SWIA2020060950932Skin · chafedLT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584FT. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E OUTBOARD SECTION WITH NEW PN 601R14303-43 PO# T-54677 REF DWG AND SRM. COMPLIED WITH CARD.Apr 28, 2020 · N652BR · Cndair CL6002B19SDR SWIA2020060950931Skin · chafedLT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584ET. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E CENTER SECTION WITH NEW PN 601R14303-51 PO# 7426-00010 REF DWG AND SRM. COMPLIED WITH CARD.Apr 28, 2020 · N652BR · Cndair CL6002B19SDR SWIA2020060950930Skin · chafedRT INBOARD FLAP VANE SKIN IS CHAFED OUTBOARD OF PANEL 684FT. (C-CHECK) RO 4/27/2020 REPLACED RT INBOARD FLAP VANE SKIN OUTBOARD OF PANEL 684FT PN 601R14303-44S REF DWG SRM, SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.Apr 28, 2020 · N652BR · Cndair CL6002B19
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