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.

SDR IPXA09556792Skin Panel · chafedINSPECTION TYPE:C CHAFE MARK AT RT WING INBOARD MAIN FLAP TRAILING EDGE ABOVE NR 6 FLAP MOVABLE FAIRING. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01 FIG 101. CUT OUT DAMAGED AREA IAW SRM 51-70-10 FIG 202 REP 4. FAB REPAIR PARTS ON MAE TR T9/798715 (20Jun 30, 2009 · N447UP · Boeing 75724APFSDR AALA20090630TUL01Vane · wornFLAP VANE LEADING HAS WEAR AT OUTBOARD FLAP INBOARD HINGE. INSTALLED DOUBLER PER SRM 51-70-2.Jun 30, 2009 · N477AA · Doug DC982SDR FDEA200906302410Skin · damagedFOUND DAMAGED AND ELONGATED HOLES ON RT INBOARD FLAP RIB 25A AND SB 57-6098 NOT PROPERLY INSTALLED. REPAIR PERFORMED BY REPLACEMENT VARIOUS PARTS ON RIB 25A AND CUT OUT THE SKIN AND INSTALLING A REPAIR PATCH IAW. RAS/FOK/139/2009 ISS. B, APPROVED BY EA 6-5750-Jun 30, 2009 · N746FD · Airbus A300B4622RSDR COEA2009062903816Hinge Fitting · corrodedHEAVY CHECK: FOUND LEVEL 2 CORROSION ON LT WING OTBD FLAP, INBD HINGE FITTING AT LOWER HINGE POINT. REMOVED AND REPLACED LT OTBD FLAP INBD FITTING ASSY.Jun 29, 2009 · N816FX · Aerosp ATR72212SDR IPXA09656472Skin · dentedINSPECTION TYPE:N/A RIGHT TRAILING EDGE I/B AFT FLAP LOWER SKIN DENT. REPAIRED PER EO B767-5750-34041-A.Jun 28, 2009 · N329UP · Boeing 76734AFSDR CA090702003Bolt · damaged(CAN) WHILE PERFORMING, ACFT DAILY INSP, IT WAS VISUALLY NOTED THAT RT INBD MID FLAP, INBD CARRIAGE, DEAD WEIGHT ROLLER BOLT WAS DAMAGED. CARRIAGE HSG ASSY WAS REPLACED WITH A SERVICEABLE UNIT AND THE ACFT WAS RETURNED TO SERVICE.Jun 27, 2009 · Boeing 727225ASDR F3LA2009063000096Structure · damagedREF NON ROUTINE C062722, C062723, C062724, C062725. DURING DEN C2 C-CHECK, INSP NOTED THAT THE RT INBD FLAP HAD 4 AREAS OF LIGHTNING STRIKE DAMAGE LOCATED ON CTR RUB STRIP. MX REMOVED RUBSTRIP AND PERFORMED MAJOR REPAIR TO THE FLAP BY SANDING DAMAGED AREA, CLJun 27, 2009 · N947FR · Airbus A319111SDR SWAA094195Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED AT OUTBOARD CORNER. REPAIRED FLAP PER EA.Jun 26, 2009 · N375SW · Boeing 7373H4SDR ASAA0976024Plate · gougedRIGHT I/B MAIN FLAP I/B AFT FLAP PROGRAMMING TRACK CLOSE OUT PLATE IS GOUGED BEYOND SRM LIMITS. REMOVED AND REPLACED WITH NEW.Jun 26, 2009 · N617AS · Boeing 737790SDR ASAA0976023Angle · chafedLEFT I/B MAIN FLAP I/B AFT FLAP TRACK CLOSE OUT ANGLE IS CHAFED BEYOND SRM LIMITS. REMOVED AND REPLACED WITH NEW.Jun 25, 2009 · N617AS · Boeing 737790SDR FDEA200906252307Hinge Bracket · corrodedLT WING OTBD FLAP INBD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER E.A. 1-5750-132121, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Jun 25, 2009 · N572FE · Doug MD11SDR SWAA094111Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT T/E. REMOVED AND REPLACED FLAP PER MM.Jun 24, 2009 · N375SW · Boeing 7373H4SDR UIEA201000179Skin · damagedLT T/E INBD MID FLAP INBD L/E SKIN PANEL WBL 137.55 WITH A GOUGE HOLE/DAMAGE (ONE FACE SKIN AND HONEYCOMB DAMAGE WITHOUT INTERNAL SKIN DAMAGE MEASURING 1.0 IN X 10.0 IN. "TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS OF EO 4457A195. SCHEDULE REPJun 23, 2009 · N412MC · Boeing 74747UFSDR UIEA201000160Skin · gougedLT T/E INBD MID FLAP - INBD L/E SKIN PANEL - WBL 137.55 WITH A GOUGE HOLE/DAMAGE. (ONE FACE SKIN AND HONEYCOMB DAMAGE WITHOUT INTERNAL SKIN DAMAGE). MEASURING 1.0 IN X 10.0 IN. "EA4457A195: DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN Jun 23, 2009 · N412MC · Boeing 74747UFSDR QXEA2009062900476Skin · chafedPDX - C5 CHECK. LT INBOARD FLAP UPPER SKIN CHAFED. REMOVED RIVETS FROM AREA AND BLENDED OUT DAMAGE. DAMAGE AFTER BLENDING WAS BEYOND LIMITS. PERFORMED REPAIR IAW R/D 8/4-57-1194 STEPS 6&7.Jun 23, 2009 · N403QX · Bombdr DHC8402SDR IPXA09156385Flap · dentedINSPECTION TYPE:N/A LT CENTER FLAP L/E DENT BETWEEN FRAME 16 - 17. REPAIRED PER EO A300-5750-32857-B.Jun 23, 2009 · N133UP · Airbus A300F4622RSDR FDEA200906232240Stop Fitting · crackedRT WING OTBD FLAP SECONDARY STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.Jun 23, 2009 · N617FE · Doug MD11FSDR AALA20090622TUL01Vane · debondedRIGHT WING FLAP-VANE BELOW GROUND-SPOILER HAS DISBONDING AT RUBSTRIP. REMOVED RUBSTRIP AND REPLACED DAMAGED CORE AND FABRICATED AND INSTALLED DOUBLERS WITH HOY-BOND PER SRM 57-04-00.Jun 22, 2009 · N9620D · Doug DC983SDR FDEA200906222234Hinge Bracket · corrodedRT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. REPAIR CARRIED OUT AS PER EA 1-5750-130979, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISJun 22, 2009 · N572FE · Doug MD11SDR FDEA200906222233Hinge Bracket · corrodedRT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. REPAIR CARRIED OUT AS PER EA 1-5750-130979, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISJun 22, 2009 · N572FE · Doug MD11SDR FDEA200906222232Hinge Bracket · corrodedLT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. REPAIR CARRIED OUT AS PER EA 1-5750-130978, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6- 2-100 REJun 22, 2009 · N572FE · Doug MD11SDR FDEA200906222231Hinge Bracket · corrodedLT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. EXISTING HOLE DIAMETER = 1.1885", FINAL HOLE DIAMETER = 1.252". REPAIR CARRIED OUT AS PER EA 1-5750Jun 22, 2009 · N572FE · Doug MD11SDR IPXA09156548Skin · gougedINSPECTION TYPE:4C REPAIR SURVEY 126-W3-02, CENTER FLAP UPPER SURFACE REPAIR DOUBLER GOUGED, LT WING. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER PER A300-600 SRM 57-50 00 PAGE 220 FIGURE 205.Jun 21, 2009 · N126UP · Airbus A300F4622RSDR ASAA0945983Wedge · dentedRIGHT I/B MIDFLAP T/E WEDGE LOWER SURFACE DENTED IN SEVERAL LOCATIONS. REMOVED DAMAGED AREAS, FABRICATED, TREATED, PRIMED AND BONDED FILLER AND DOUBLER IAW SRM.Jun 21, 2009 · N788AS · Boeing 737490SDR FDEA200906212193Fairing · crackedLT FLAP OPS MECHANISM FAIRING 571BB ANGLE STIFFENER FOUND CRACKED AS MARKED. CRACKED FAIRING NR 571BB STIFFENER REPAIRED IAW E.A. F-5710-126220 TITLED: LT MLG TRUNNION AFT FAIRING CRACK REPAIR IAW SB757-57-0029. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CJun 21, 2009 · N933FD · Boeing 7572B7SDR AALA20090620TUL01Vane · wornLEFT WING NR 4 FLAP VANE HAS HOLE WORN ON TOP FROM CONTACT WITH I/B SPOILER. PERFORMED HOT BOND REPAIR ON VANE PER SRM 57-03-00.Jun 20, 2009 · N9615W · Doug DC983SDR FDEA200906202192Support Bracket · dislodgedRT INBD T/E FLAP, MAIN FLAP FAIRING PIN SUPPORT BRACKET AT MF STA 235 DISLODGED. REMOVED AND REPLACED AS PER SRM 51-40-02 REV. 97. CIC APPLICATION CARRIED OUT AS PER DWG B57-51-001. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 20, 2009 · N933FD · Boeing 75721BSDR FDEA200906192468Skin · damagedRIGHT WING FLAP INBD LOWER SKIN SURFACE WITH DEBONDING AT T/E CARRIAGE NR 2 IT WAS REPAIRED IAW E.A.6-5710-131030Jun 19, 2009 · N801FD · Airbus A310324SDR IPXA09556537Skin · puncturedINSPECTION TYPE:C2 WHILE WORKING CUSTOMER CARD 808334, FOUND PUNCTURE IN RT WING I/B AFT FLAP (MARKED). REMOVED DAMAGE AND REMOVED MOISTURE FROM REPAIR AREA, FABRICATED REPAIR PLIES, INSTALLED REPAIR PLIES AND CURED. RESTORED FINISH IAW SRM 51-20-17-0G.Jun 19, 2009 · N467UP · Boeing 75724APFSDR IPXA09556536Skin · debondedINSPECTION TYPE:C2 RT WING O/B MAIN FLAP T/E HAS DISBOND ON UPPER SURFACE 26 INCHES FROM I/B, 8 INCHES FROM T/E. REMOVED DAMAGE, FABRICATED REPAIR PLIES, INSTALLED REPAIR PLIES, CURED REPAIR AND RESTORED FINISH IAW SRM 51-20-06-0G.Jun 19, 2009 · N467UP · Boeing 75724APFSDR IPXA09156467Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ W4-02 RIGHT I/B FLAP UPPER SKIN REPAIR FOUND TO HAVE A DISCREPANT FASTENERS INSTALLED AT RIB 1C. REMOVED EXISTING DISCREPANT FASTENERS FROM RT WING, INNER FLAP, UPPER SKIN BETWEEN RIB 1C-3 AND STR 2.1-2.2 AND REPLACED WITHJun 19, 2009 · N121UP · Airbus A300F4622RSDR IPXA09656429Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1) FIG 5 REV 44.Jun 19, 2009 · N309UP · Boeing 76734AFSDR IPXA09656428Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B L/E FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1) FIG 5 REV 44.Jun 19, 2009 · N309UP · Boeing 76734AFSDR MALA090093Skin · dentedDURING 6Y/4Y INSPECTION IN CWA, LT FLAP UPPER PANEL 541AT HAS DISBONDED DENT LOCATED AT WS 76.8 AND 8.25 FROM TRAILING EDGE. REPAIRED IAW S57060.Jun 19, 2009 · N422XJ · Saab 340BSDR USAA2009070891749Flap · delaminatedSAL - C21 - MAJOR REPAIR - DELAMINATION ON LEFT WING OUTBOARD AFT FLAP TRAILING EDGE AT INBOARD END BETWEEN WBL 202.6 TO WBL 414.4. REPAIRED LEFT WING OUTBOARD AFT FLAP TRAILING EDGE AT INBOARD END BETWEEN WBL 202.6 TO WBL 414.4 IAW B737 SRM 51-70-10.Jun 18, 2009 · N314AW · Boeing 7373S3SDR SWAA093982Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.Jun 18, 2009 · N613SW · Boeing 7373H4SDR IPXA09M56578Skin · misrepairedINSPECTION TYPE:2C REPAIR SEQ 257-W4-01 REPAIR DOUBLER NOT CORRELATED TO SRM. REMOVED EXISTING REPAIR AND ENLARGED EXISTING CUTOUT TO .5R ON RT I/B FLAP LOWER SKIN AT STA XIFH 282.360 - 311.851 AND BELOW YIFH 7.600. FABRICATED AND INSTALLED REPLACEMENT REPAIJun 17, 2009 · N257UP · Doug MD11FSDR IPXA09156477Skin · chafedINSPECTION TYPE:4C LT WING INBOARD FLAP UPPER SURFACE CHAFED, AFT OF NR 1 SPOILER. REMOVED DAMAGE AND FABRICATED AND INSTALLED REPAIR DOUBLER PER E0-A30 0-5750-34048-A.Jun 16, 2009 · N121UP · Airbus A300F4622RSDR IPXA09656438Hinge Fitting · crackedINSPECTION TYPE:C RT WING I/B MAIN FLAP I/B AFT FLAP HINGE ARM FTG FOUND CRACKED (CRACK 1.5 INCH LENGTH). RT WING I/B MAIN FLAP I/B AFT FLAP HINGE ARM FTG REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATERJun 16, 2009 · N309UP · Boeing 76734AFSDR USAA2009061991525Skin · delaminatedCLT - C6 - MAJOR REPAIR - DELAMINATION ON LEFT WING OUTBOARD AFT FLAP INBOARD LOWER SURFACE. REPLACED LEFT WING OUTBOARD AFT FLAP IAW B737 AMM 27-51-39.Jun 16, 2009 · N504AU · Boeing 7373B7SDR A6WA200940378Flex Drive · corrodedFLEXSHAFT ON FLAP FOUND WITH HEAVY CORROSION ON 70 PERCENT OF THE COIL SURFACE AND SEIZED IN ACTUATOR. B-NUT FOUND IMPROPERLY TORQUED AT THE SEIZED END. SUBSEQUENT DAMAGE ON TERMINAL. C/A IN PROGRESS. (K)Jun 15, 2009 · N462AW · Cndair CL6002B19SDR IPXA09M56570Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NUMBER 275-W4-006, RT WING, INBOARD FLAP INNER SURFACE STA XIFH 237 NEEDS VALIDATION FOR REPAIR. EXISTING REPAIR DOUBLER AT AFFECTED AREA REMOVED. DAMAGED AREA TRIMMED OUT AT STA XIFH 249.5. HFEC C/O ON TRIMMED EDGES & FOUNJun 15, 2009 · N275UP · Doug MD11FSDR IPXA09M56565Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NUMBER 275-W3-001, LT WING, INBOARD FLAP, INBOARD LWR FAIRING NEEDS VALIDATION FOR REPAIR. LT WING, INBOARD FLAP, INBOARD LWR FAIRING EXISTING REPAIR DOUBLER REMOVED. EXISTING SKIN TRIMMED OUT PER EN1271-09. HFEC C/O ON TRIJun 15, 2009 · N275UP · Doug MD11FSDR IPXA09156446Skin · gougedINSPECTION TYPE:4/C LEFT WING CENTER FLAP UPPER SURFACE GOUGED APPROX 18 INCHES ABOVE RUB TRIP O/B OF NR 3 FLAP TRACK. FABBED AND INSTALLED REPAIR DOUBLER IAW IPXA EO A300-5750-34021-A, AND SAA EA 300-5753-01-A1859.Jun 15, 2009 · N121UP · Airbus A300F4622RSDR WRLA2009163Skin · debondedDURING C-CHK IN TPE, INSP/MX FOUND DISBOND. RIGHT INBOARD FLAP VANE LOWER SKIN DISBOND 21X15 INCHES AT XIFH 190.8-205.8 AND 39X12 INCHES AT XIFH 216.8-255.8. REMOVED FLAP VANE, REPAIRED THE DAMAGED AREA IAW EGAT EI W2009A57B-696 REV 00. REINSTALLED THE FLAP Jun 14, 2009 · N381WA · Doug MD11FSDR WRLA2009159Rib · crackedDURING C-CHK IN TPE, INSP/MX FOUND CRACK. THE STOP RIB OF RIGHT WING OUTBOARD T/E FLAP L/E HAS CRACKED (REF EGAT NRC U05014).Jun 14, 2009 · N381WA · Doug MD11FSDR WRLA2009158Rib · crackedDURING C-CHK IN TPE, INSP/MX FOUND CRACK. STOP RIB OF LEFT WING OUTBOARD T/E FLAP L/E HAS CRACKED (REF EGAT NRC U05013).Jun 14, 2009 · N381WA · Doug MD11FSDR IPXA09M56574Flap · damagedINSPECTION TYPE:2C DMI LOG D402285- LT WING OUTBD FLAP T/E REPAIR. REMOVED DAMAGE AND REPAIRED IAW SAA EA 011-5750-01-A1862 AND IPXA EO MD11-5750-33801-D.Jun 13, 2009 · N257UP · Doug MD11FSDR IPXA09M56554Stop Fitting · crackedINSPECTION TYPE:C RT WING O/B TRAILING EDGE FLAP STOP FITTING SUSPECT CRACK AS MARKED. HFEC INSP C/O ON STOP FITTING, FOUND CRACK AS MARKED. STOP FITTING REMOVED PER SRM 51-33-01 VOL II REV 40. NEW STOP FITTING HOLES PICK-UP. NEW STOP FITTING INSTALLED ON Jun 13, 2009 · N275UP · Doug MD11FSDR IPXA09M56553Stop Fitting · crackedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP STOP FITTING SUSPECT CRACK AS MARKED. HFEC INSP C/O ON STOP FITTING & FOUND CRACK AS MARKED. LT WING O/B TRAILING EDGE FLAP STOP FITTING REMOVED PER SRM 51-33-01 VOL II, REV 40. NEW STOP FITTING HOLES PICK-UPJun 13, 2009 · N275UP · Doug MD11F
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