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 UIEA2021041800931Structure · corrodedLHW I/B MID FLAP I/B FLAP PANEL UPPER CHORD FOUND CORROSION.(<P>LHW I/B MID FLAP I/B FLAP PANEL UPPER CHORD CORROSION AREA REWORKED AS PER SRM 57-30-02-1A-1</P>)May 16, 2021 · N429MC · Boeing 747481SDR UIEA2021050501066Fairing · delaminatedLHW O/B FORE FLAP O/B L/E FAIRING FOUND DELAM(<P>DELAMINATED AREA HAVE BEEN REPAIRED WITH COMPOSITE HOT BOND REPAIR METHOD </P>)May 16, 2021 · N429MC · Boeing 747481SDR UIEA2021050501067Fairing · delaminatedLHW I/B FORE FLAP L/E FAIRING FOUND DELAM(<P>DELAMINATED AREA HAVE BEEN REPAIRED WITH COMPOSITE HOT BOND REPAIR METHOD </P>)May 16, 2021 · N429MC · Boeing 747481SDR UIEA2021050501068Skin · delaminatedRHW I/B FORE FLAP UPPER SURFACE O/B ZONE FOUND DELAM(<P>DELAMINATED AREA HAVE BEEN REPAIRED WITH COMPOSITE HOT BOND REPAIR METHOD </P>)May 16, 2021 · N429MC · Boeing 747481SDR FDEA202105161230Skin · dentedRH WING T/E CENTER FLAP I/B SECTION LWR SURFACE GOT A DENT, JUST BEHIND #3 TRACK. PFM. PATCH REPAIR. THE EXTERNAL PLATE VERIFIED TO BE 2024T3-056T CLAD, BN 680810 I.A.W. A300-600F SRM 57-50-00-201 FIG. 205 AND P. 218.May 16, 2021 · N652FE · Airbus A300F4605RSDR FDEA202105161229Skin · dentedLH WING I/B FLAP UPPER SKIN GOT A DENT AT RIB3 STGR2.2 PFM. SKIN PATCH REPAIR. THE EXTERNAL PLATE VERIFIED TO BE 2024T3-056 CLAD,BN 680810 I.A.W. A300-600F SRM 57-50-00-201 FIG. 205 AND P. 218.May 16, 2021 · N652FE · Airbus A300F4605RSDR SWIA2021072159633Vane · gouged* LH INBOARD FLAP. INBOARD VANE ACTUATOR HAS GOUGES IN SKIN ON THE OUTBOARD RIB, OUTBOARD SIDE (BEHIND PANEL 584AB) MARKED (C-CHECK RO 7/18/2021) BLEND WAS PERFORMED TO A SMOOTH CONTOUR, REMAINING THICKNESS IS NOT LESS THEN REPORTED, NO DEFECTS NOTED, RMay 15, 2021 · N878AS · Cndair CL6002B19SDR SWIA2021072159630Skin · dentedL/H INBD FLAP - APROX WS 75 - SEVERAL DENTS ON BOTTOM FLAP SKIN BEHIND MLG OTBD TIRE (C-CHECK RO 7/18/2021) REPLACED L/H INBD FLAP SKIN WITH FABRICATED SKIN REF MHIRJ EO 601R14008 SNIEO S12 2021-06-14 AND EO 601R14002 SNIEO S23 2021-06-14, DWG 601R140May 15, 2021 · N878AS · Cndair CL6002B19SDR SWAA2021060473219Skin · debondedRIGHT WING INBOARD MAIN FLAP TRAILING EDGE SKIN DISBONDED AT OUTBOARD END / REPAIRED AREA OF DELAMINATION ON I/B R/W MAIN FLAP LOWER SKIN. IAW B737-700 SRM 57-53-01-2R-7;SRM 51-70-10-2R-4; SRM 51-70-10-2R-0; AMM 51-21-99-300-801.; STEP 12 OK; SUMMARY STATEMENTMay 15, 2021 · N220WN · Boeing 7377H4SDR SWIA2021072159662Fastener · corroded* LEFT WING I/B TRAILING EDGE HAS CORRODED FASTENERS AT APPROX W/S 139 ON BUMP STOP BRACKET (C-CHECK RO 7/18/2021) REMOVED AND REPLACED LH WING I/B TRAILING EDGE CORRODED FASTENERS AT APPROX W/S 139 ON BUMP STOP BRACKET. IAW CRJ 200 SRM 51-41-04. TUC55May 14, 2021 · N878AS · Cndair CL6002B19SDR SWIA2021072159661Fastener · corroded* LEFT WING I/B TRAILING EDGE HAS CORRODED FASTENERS AT APPROX W/S 104 ON BUMP STOP BRACKET (C-CHECK RO 7/18/2021) REMOVED AND REPLACED LH WING I/B TRAILING EDGE CORRODED FASTENERS AT APPROX W/S 104 ON BUMP STOP BRACKET. IAW CRJ 200 SRM 51-41-04. TUC55May 14, 2021 · N878AS · Cndair CL6002B19SDR SWIA2021072159660Fastener · corrodedRIGHT WING INBOARD TRAILING EDGE STOP ASSY @WS 56.30 HAVE CORRODED FASTENERS. MARKED (C-CHECK RO 7/18/2021) REMOVED CORRODED HARDWARE FROM RIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY NEW 1EA WASHER AND NEW 1EA NUT @WS56.30 REF CRJ200 SRM 51-41-02May 14, 2021 · N878AS · Cndair CL6002B19SDR SWIA2021072159658Stop · corrodedRIGHT WING INBOARD TRAILING EDGE STOP ASSY @WS 104.00 HAS CORRODED FASTENERS. MARKED (C-CHECK RO 7/18/2021) REMOVED AND REPLACED WITH NEW. NEW HARDWARE INCLUDES 2 FASTENERS AND 2 WASHERS. PER CRJ 200 AMM 51-41-02.May 14, 2021 · N878AS · Cndair CL6002B19SDR IPXA2021052969952Rub Strip · wornINSPECTION TYPE:A300LT WING I/B FLAP L/E TOP SURFACE RUB PLATES #1,#5,#6,&#8 HAS WEAR MARKREMOVED AND REPLACED IAW SRM 51-40-21May 14, 2021 · N134UP · Airbus A300F4622RSDR IPXA2021052769905Rub Strip · crackedINSPECTION TYPE:A300LT WING MID FLAP LE TOP SURFACE ROLLER RUB PLATE CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21May 14, 2021 · N134UP · Airbus A300F4622RSDR IPXA2021052369707Bracket · brokenINSPECTION TYPE:CLT WING MID FLAP O/B EDGE ANGLE BRACKET BROKENREMOVED AND REPLACED IAW SRM 51-40-21May 14, 2021 · N134UP · Airbus A300F4622RSDR SWAA2021051872858Skin · crackedRH I/B FOREFLAP LOWER SURFACE HAS APROX 1' CRACK WITH ASSOCIATED DELAMINATION 5' FROM TRAILING EDGE AND 72' FROM O/B END. MARKED ; / COMPLIED WITH EA 21-157-01315; COMPLIED WITH EA 21-157-01315; COMPLIED WITH EA 21-157-01315May 14, 2021 · N478WN · Boeing 7377H4SDR SWAA2021051872862Skin · crackedRH I/B FOREFLAP LOWER SURFACE HAS APROX 1' CRACK WITH ASSOCIATED DELAMINATION 5' FROM TRAILING EDGE AND 72' FROM O/B END. MARKED ; / COMPLIED WITH EA 21-157-01315; COMPLIED WITH EA 21-157-01315; COMPLIED WITH EA 21-157-01315May 14, 2021 · N478WN · Boeing 7377H4SDR DU4R2021051400072Structure · damagedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND A DENT AND CRACK IN THE L/H TRAILING EDGE OF THE MID FLAP THAT WAS STOP DRILLED AND SEALED. S/O 660006 N/R 38151May 14, 2021 · N362NC · Boeing 737330SDR SWIA2021072159657Hinge Fitting · corrodedRIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY @ WS 139.924 STOP ASSY HAS CORRODED FASTENERS. MARKED (C-CHECK RO 7/18/2021) REMOVED CORRODED HARDWARE FROM RIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY AND INSTALLED NEW 1EA WASHER AND NEW 1EA NUT May 13, 2021 · N878AS · Cndair CL6002B19SDR SWIA2021072159656Hinge Fitting · corrodedRIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY @ WS 139.924 HAS A CORRODED CASTLE NUT. MARKED (C-CHECK RO 7/18/2021) REMOVED CORRODED HARDWARE FROM RIGHT WING INBOARD TRAILING EDGE HINGE ASSEMBLY AND INSTALLED NEW HARDWARE 1EA NEW NUT AND1 NEW WASHERMay 13, 2021 · N878AS · Cndair CL6002B19SDR DALA2021052002801Vane · damagedREMOVED RUBSTRIP TO FACILITATE REPAIR B717 SRM 57-53-01-2R-1, REMOVED UPPER DAMAGED SKIN AND CORE PER B717 SRM 57-53-01-2R-1. PREPPED FOR CORE REPLACEMENT PER B717 SRM 57-53-01-2R-1. SUPPLEMENTAL INFORMATION: BONDED CORE PER B717 SRM 57-53-01-2R-1. BONDED DOUBMay 12, 2021 · Boeing 717200SDR SWIA2021081060283Skin · chafed* LH INBOARD FLAP UPPER SKIN IS CHAFED UNDER PANEL 584CB (C-CHECK RO 8/9/2021) BLENDED DAMAGE AREA FROM UPPER SKIN UNDER PANEL 584CB PER CRJ 700 SRM 51-12-00-001-001-A01,NO DAMAGE ALLOW AREA , RECIEVED REO 670-57-52-352 REV -- DATE 2017-03-28 , NDT AREMay 11, 2021 · N614QX · Cndair CL6002C10SDR SWIA2021070959365Skin · dentedREPAIR L/H FLAP LOWER SKIN DENTS. PERFORMED INBD FLAP LOWER SKIN REPAIR IAW CRJ900 SRM 57-52-01-201-005-A01 SPLICE REPAIR FROM FLS42.00 TO FLS48.00 FIGURE 57-52-01-995-802 COMPLIED WITH 51-900-1002-SKY NO DEFECTS NOTEDMay 11, 2021 · N899SK · Cndair CL6002D24SDR SWIA2021070959364Skin · dentedREPAIR R/H FLAP LOWER SKIN DENTS (C-CHECK RO 7/7/2021) PERFORMED REPAIR TO RH INBD FLAP LOWER SKIN IAW CRJ900 SRM 57-52-01-201-005-A01, SPLICE REPAIR FROM FLS42.00 TO FLS48.00 FIGURE 57-52-01-995-802. COMPLIED WITH 51-900-1002-SKY NO DEFECTS NOTEDMay 11, 2021 · N899SK · Cndair CL6002D24SDR SWAA2021061471552Bearing · crackedCRACK OB FLAP BEARING ROLLER TRACK #1 AT LT WING (2 EA) ; 2021-217318 / REPLACED BEARING ROLLER ON O/B FLAP TRACK CARRIAGE #1 AT LT WING (2 EA) IAW AMM 27-51-23-400-803 STEP 7.C.(2)(A) TOOL USED TORQUE PN:QD2R1000A. SN:0319122619. D/D:04 MAR 22.; COMPLETEDMay 11, 2021 · N7818L · Boeing 73776NSDR FDEA202105111179Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUTHOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND BARREL NUT WALL THICKNESS LOWEMay 11, 2021 · N525FE · Doug MD11FSDR FDEA202105111178Support Fitting · corrodedRIGHT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION RIGHT WING - OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. RMay 11, 2021 · N525FE · Doug MD11FSDR FDEA202105111177Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIMay 11, 2021 · N525FE · Doug MD11FSDR FDEA202105111176Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIMay 11, 2021 · N525FE · Doug MD11FSDR FDEA202105111175Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 5 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 5 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIMay 11, 2021 · N525FE · Doug MD11FSDR FDEA202105111174Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FMay 11, 2021 · N525FE · Doug MD11FSDR SWIA2021081060161Vane · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA45394-670-57-53-218 N709SK MXCODEID50666-PR - LEFT OUTBD FLAP VANE LEADING EDGE HAS DAMAGE 8 IN FROM OUTBD EDGE. DAMAGE AREA IS 2.5 IN WIDE AND A DEPTH OF .039. DAMAGE IS OUT OF LIMITS PER SRM 57-53-01 PAGE 104. FOUNDMay 10, 2021 · N709SK · Cndair CL6002C10SDR SWIA2021080560086Hinge Arm · corrodedREMOVE AND INSTALL RH OTBD FLAP HINGE ARM ASSY'S AT WS178.00, WS220.00, AND WS264.00 (C-CHECK RO 8/1/2021) REMOVED AND INSTALLED RH OTBD FLAP HINGE ARM ASSY'S AT WS178.00, WS220.00 AND WS264.00 IAW CRJ-200 AMM 57-53-02-400-801, 57-53-02-400-803 AND 57-5May 10, 2021 · N945SW · Cndair CL6002B19SDR KCSA202105101056Skin · corrodedRIGHT INBOARD FLAP HAS CORROSION APPROXIMATELY 73' FROM INBOARD EDGE ON MID FLAP UPPER PANEL SURFACEMay 10, 2021 · N703CK · Boeing 747412SDR KCSA202105101054Skin · corrodedPANEL #1 588HT HAS CORROSION ON L/H O/B AFT FLAPMay 10, 2021 · N703CK · Boeing 747412SDR SWIA2021081060290Lug · corroded* L/H #3 FLAP MECHANISM FWD LUG FITTING HAS CORRODED HARDWARE (C-CHECK RO 8/9/2021) REPLACED MOUNTING HDWR ON L/H # 3 FLAP MECHANISM FWD LUG FITTING PER REF CRJ700 AMM TASK 57-54-02-400-810 CONFIG A01 LEAK CHECK GOODMay 8, 2021 · N614QX · Cndair CL6002C10SDR SWIA202160017Vane · dentedD: FOUND SMALL DENT ON L/E OF LH OUTBOARD FLAP VANE, JUST INBOARD OF #3 HINGE ARM. INSPECTED DENT ON L/E OF LH OUTBOARD FLAP VANE IN REFERENCE TO SRM 57-53-00. DENT MEASURED 0.5" L X 0.25" W X 0.0175" D. DENT FOUND TO BE WITHIN ACCEPTABLE LIMITS AT THIS TIME.May 8, 2021 · N945SW · Cndair CL6002B19SDR CALA2021051000630Skin · debondedB767-06-3-7222 RHW I/B AFT FLAP UPPER AND BOTTOM SURFACE FOUND DISBOND - REFER NR LP 9130574. RHW I/B AFT FLAP DISBOND AREA PERFORMED REPAIR AS PER EC/RA 5752-01851 REV - REFER FORM 44-0008 ITEM 1-29 ACCOMPLISHED ADD EMP:V912779 RII INSPECTED OK BY HX198855 RMay 8, 2021 · N658UA · Boeing 767322SDR CALA2021051000629Bolt · missingPDA 2 RIGHT WING INBOARD FLAP FWD CANOE FAIRING MISSING 2 EACH ATTACH BOLTS PICTURE UPDATE REF L/P 6268454 REPLACED MISSING BOLTS AS REQUIRED. OK TO CONTINUE.May 8, 2021 · N26215 · Boeing 737824SDR FDEA202105071154Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57May 7, 2021 · N525FE · Doug MD11FSDR FDEA202105071153Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- May 7, 2021 · N525FE · Doug MD11FSDR IPXA2021050669051Angle · crackedINSPECTION TYPE:CR/H OB FLAP I/B HINGE FWD FRAME I/B SIDE HAS A SUPPORT ANGLE CRACKEDREMOVED, FABBED AND INSTALLED SUPPORT ANGLE IAW SRM 51-31-01 AND DRAWING ARC0553May 6, 2021 · N291UP · Doug MD11FSDR SWIA2021081060287Vane · corrodedL/H INBD FLAP MOVEABLE VANE UPPER MOUNTING HARDWARE CORRODED (C-CHECK RO 8/9/2021) REMOVED LHIB FLAP MOVABLE VANE UPPER MOUNTING HARDWARE REF CRJ700 AMM 27-52-23-000-801-A01 STEP 4.A.(3)(A)(B). INSTALLED NEW MOUNTING HARDWARE REF CRJ700 AMM 27-52-23-40May 5, 2021 · N614QX · Cndair CL6002C10SDR SWAA2021060269331Skin · delaminatedLH OUTBD AFT FLAP HAS A 3' X 3' DELAMINATION SPOT ON LOWER SURFACE AT THE INBD AFT CORNER / ACCOMPLISEHD REMOVED AND REPLACEMENT OF L/H AFT FLAP ON NR #D472971May 5, 2021 · N8667D · Boeing 7378H4SDR FDEA202105051113Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57May 5, 2021 · N525FE · Doug MD11FSDR FDEA202105051112Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED REPAIR BUSHINGMay 5, 2021 · N525FE · Doug MD11FSDR FDEA202105051111Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM May 5, 2021 · N525FE · Doug MD11FSDR FDEA202105051110Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57May 5, 2021 · N525FE · Doug MD11FSDR FDEA202105051109Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57May 5, 2021 · N525FE · Doug MD11F
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