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 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 (20SDR AALA20090630TUL01Vane · wornFLAP VANE LEADING HAS WEAR AT OUTBOARD FLAP INBOARD HINGE. INSTALLED DOUBLER PER SRM 51-70-2.SDR 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-SDR 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.SDR IPXA09656472Skin · dentedINSPECTION TYPE:N/A RIGHT TRAILING EDGE I/B AFT FLAP LOWER SKIN DENT. REPAIRED PER EO B767-5750-34041-A.SDR 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.SDR 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, CLSDR SWAA094195Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING INBOARD AFT FLAP DELAMINATED AT OUTBOARD CORNER. REPAIRED FLAP PER EA.SDR 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.SDR ASAA0976023Angle · chafedLEFT I/B MAIN FLAP I/B AFT FLAP TRACK CLOSE OUT ANGLE IS CHAFED BEYOND SRM LIMITS. REMOVED AND REPLACED WITH NEW.SDR 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.SDR SWAA094111Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT T/E. REMOVED AND REPLACED FLAP PER MM.SDR 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 REPSDR 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 SDR 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.SDR IPXA09156385Flap · dentedINSPECTION TYPE:N/A LT CENTER FLAP L/E DENT BETWEEN FRAME 16 - 17. REPAIRED PER EO A300-5750-32857-B.SDR 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.SDR 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.SDR 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 REVISSDR 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 REVISSDR 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 RESDR 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 1-5750SDR 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.SDR 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.SDR 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 CSDR 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.SDR 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.SDR FDEA200906192468Skin · damagedRIGHT WING FLAP INBD LOWER SKIN SURFACE WITH DEBONDING AT T/E CARRIAGE NR 2 IT WAS REPAIRED IAW E.A.6-5710-131030SDR 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.SDR 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.SDR 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 WITHSDR 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.SDR 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.SDR 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.SDR 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.SDR SWAA093982Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR 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 REPAISDR 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.SDR 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 MATERSDR 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.SDR 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)SDR 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 & FOUNSDR 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 TRISDR 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.SDR 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 SDR 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).SDR 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).SDR 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.SDR 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 SDR 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-UP
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