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 ASAA0944487Flap Track · corrodedRUST ON NR 1 FLAP TRACK BEARING CONTACT SURFACES. REMOVED CORROSION AND TREATED IAW EA 400 57EA 00306.SDR MASA2009022100075Vane · chafedRIGHT WING OUTBOARD FLAP VANE CHAFED ALONG LEADING EDGE NEAR OUTBOARD END. BLENDED DAMAGE.SDR MASA2009022100073Vane · damagedRT OUTBOARD FLAP VANE HAS CHAFE DAMAGE. BLENDED DAMAGE.SDR IPXA09555130Skin · gougedINSPECTION TYPE:C LEFT O/B FLAP I/B UPPER SKIN PREVIOUS REPAIR HAS 2 (EA) EVENLY SPACED GOUGES LOCATED BEHIND NR 3 SPOILER ACTUATOR 25 INCHES FWD OF T/E PER E.0. B757-5100-30760-B APPENDIX 'C' CONTACT ON SITE ENGR FOR DISPO. OUT OF LIMITS SRM 57-53-01-1A. REMSDR IPXA09555129Skin · gougedINSPECTION TYPE:C LEFT O/B FLAP I/B UPPER SKIN PREVIOUS REPAIR HAS A GOUGE REPAIR LOCATE 35.0 INCHES FROM I/B EDGE 25 INCHES FWD OF T/E PER EO B757-5100-30760-B APPEN 'C', CONTACT ON SITE ENGR FOR DISPO. OUT OF LIMIT SRM 57-53-01-1A (2) REMOVED PREV REPAIR SRSDR FDEA200902200610Stop Fitting · crackedLT WING OTBD FLAP SECONDARY UP STOP CRACKED. CRACKED FITTING REMOVED AND REPLACED NEW FITTING AT LT WING OUTBD FLAP AS PER SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR FDEA200902190577Skin · crackedLT WING INBD FLAP LWR SKIN BROKEN. REPAIRED AREA IAW SRM 57-00-01, FIG 4, SHT 2, VOL I.SDR IPXA09856125Skin · misrepairedINSPECTION TYPE:SV SS 852-W4-24, RT O/B FLAP LOWER SKIN REPAIR AT XF 215, DOES NOT HAVE .5 MINIMUM CORNER. REPAIRED PER TIMCO REO-G12754 REV B, AND UPS DC8-5750-33544-A.SDR DL757090210Skin · dentedLT INBD MAIN FLAP LEADING EDGE DENTED. REPAIRED PER SRM 57-53-01 REPAIR 2 ON ATS NR 00693.SDR FDEA200902170563Rib · damagedWHILE PEFORMING EA 6-5750-5000 PT3 "WINGS - INBD FLAP NOSE RIB 7 REPLACEMENT LT"; SEVERAL HOLES WERE FOUND TO BE ELONGATED. COMPLIED WITH EA 6-5750-127920.SDR FDEA200902170559Vane · delaminatedLEFT WING INBOARD FLAP VANE FOUND DELAMINATION ON LOWER SURFACE. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-22-5.SDR ABXA201003260016Skin · corrodedINBOARD FLAP FWD HALF UPPER SKIN IS BULGING OFF OF PANEL 555JT. REPLACED LEFT WING I/B FWD FLAP ASSY IAW 767 MM 27-51-03-4.SDR UPS09654723Wedge · damagedINSPECTION TYPE:N/A RIGHT O/B FLAP T/E WEDGE DAMAGED CUTOUT 3.5 X 6.0. REPAIRED PER EO B767-5750-32178-B.SDR FDEA200902150522Vane · delaminatedRIGHT WING INBOARD FLAP, FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM CENTER TO OUTBOARD VANE TRACK. REMOVED AND REPLACED AS PER AMM 27-50-22-4. RT WING INBOARD FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 FOUND STISFACTORY.SDR ASAA0944548Skin · dentedLEFT O/B FORE FLAP DENTED ON UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA0944537Skin · dentedRIGHT I/B AFT FLAP LOWER SURFACE IS DENTED 2 PLACES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10 REP 4.SDR IPXA09855947Skin · misrepairedINSPECTION TYPE:SV SS#852-W3-18, LT INBD FLAP UPPER SKIN DOUBLER XW66, 2 INCH DIA DOES NOT CORRELATE TO SRM REPAIR. REMOVED AND REPLACED REPAIR PER DC8 SRM 57-02-01-0 FIG 002Q SHT 1.SDR ASAA0944909Flap Track · corrodedNR 1 FLAP TRACK HAS PITTING CORROSION ON ROLLER CONTACT AREA. REMOVED AND REPLACED NR 1 FLAP TRACK IAW B737 400 MM 27 51 49.SDR ASAA0944883Flap Track · damagedNR 7 FLAP TRACK PITTED. REMOVED FLAP TRACK, RECEIVED NEW TRACK AND INSTALLED IAW 400 57EA 00617.SDR ASAA0944871Skin · chafedRIGHT O/B FORE FLAP I/B LEADING EDGE CHAFED. REMOVED DAMAGED SECTION OF LEADING EDGE SKIN FABRICATED AND INSTALLED REPLACEMENT SECTION OF LEADING EDGE SKIN IAW B DWG 65C35705.SDR ASAA0944850Flap Track · corrodedNR 7 FLAP TRACK PITTED. REMOVED FLAP TRACK RECEIVED NEW TRACK AND INSTALLED IAW ASA EA 400 57EA 006617.SDR ASAA0944735Skin · dentedLEFT O/B AFT FLAP DENTED 31 INCHES FROM OUTBOARD EDGE LOWER SURFACE. REMOVED DAMAGED AREA, FABRICATED AND BONDED SKIN AND DOUBLER REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA0944734Doubler · delaminatedLEFT O/B AFT FLAP OUTBOARD TRAILING EDGE CORNER SPLIT AND DELAMINATED. REMOVED PREVIOUS REPAIR, FABRICATED AND BONDED DOUBLER AND SKIN REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.SDR SWAA091116Slat · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT CRACKED. REPAIRED SLAT PER SRM.SDR UPS09654783Hinge Fitting · crackedINSPECTION TYPE:C RT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG FOUND CRACKED. 0.375 INCH LENGTH. RT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02-2R 1 FIG 201.SDR IPXA09654821Hinge Fitting · crackedINSPECTION TYPE:C LT WING - I/B MAIN FLAP I/B AFT FLAP HINGE FTG FOUND CRACKED. CRACK 1 INCH LENGTH. LT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02-2R1 FIG 201.SDR UPS09654782Repair · chafedINSPECTION TYPE:C RT WING I/B AFT FLAP UPPER I/B AREA FOUND DEEP CHAFED ON EXISTING REPAIR PATCH. METAL HOT BOND REPAIR PERFORMED ON RT WING I/B AFT FLAP UPPER I/B AREA EXISTING REPAIR PATCH AS PER SRM 51-70-10 REPAIR 4 FIG 202.SDR UPS09654760Flap · delaminatedINSPECTION TYPE:C LT WING O/B FLAP I/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5 REV 43.SDR UPS09654759Flap · misrepairedINSPECTION TYPE:6C RT WING I/B MAIN FLAP LOWER T/E MID AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A(1) FIG 5 REV 43.SDR UPS09654758Flap · damagedINSPECTION TYPE:6C LT WING O/B FLAP LWR TRAILING EDGE I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-06 PARA 5A(1) FIG 9 REV 43.SDR UPS09654757Fairing · delaminatedINSPECTION TYPE:N/A RT WING - I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03, PARA 5A (1) FIG 5 REV 43.SDR IPXA09M54843Wedge · crackedINSPECTION TYPE:4C RT INBOARD FLAP T/E WEDGE CRACKED. REPAIRED RT INBOARD FLAP T/E BY FABRICATION OF 3 EA ATTACH Z-ANGLES AND REPLACEMENT WEDGE REF MD11 SRM VOL 1 57-20-00.SDR AALA2009021600123Skin · damagedFOREIGN OBJECT DAMAGE LOWER SKIN INBOARD WEDGE. REMOVED TEMPORARY REPAIR, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FLUSH PERMANENT REPAIR DOUBLER AND FILLER PER SRM 57-01-00 FIGURE 5 SHEET 2.SDR SWAA091002Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR MALA090020Skin · dentedDENT LOCATED IN LT FLAP ASSY 38.5 INCHES OUTBOARD FROM INBOARD EDGE ON PANEL 541AT, REPAIRED.SDR MALA090019Skin · dentedDENT LOCATED IN RT FLAP ASSY TOP SKIN 19.5 INCH FROM INBOARD EDGE, 3 INCHES FROM, AFT EDGE. REPAIREDSDR SWAA090953Flap · delaminatedDURING SCHEDULED SPV CHECK, LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA090948Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING I/B AFT FLAP O/B LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0944462Skin · dentedRT WING I/B MID FLAP HAS DENTS ON UPPER SURFACE. PREPPED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED REPAIR DOUBLER 12 INCHES FROM I/B 24 INCHES FROM T/E IAW ASA EA 400 57EA 00703.SDR ASAA0944445Skin · dentedLT WING O/B MID FLAP HAS A DENT AT UPPER SURFACE 81 INCHES FROM O/B END. REMOVED DAMAGE AT 75 INCHES AND 81 INCHES FROM OB END, FABRICATED REPAIR DOUBLERS AND BONDED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10.SDR ASAA0944444Skin · dentedLT WING O/B MID FLAP HAS A DENT AT UPPER SURFACE 119 INCHES FROM O/B END. REMOVED DAMAGED SKINS AT 117 INCHES AND 119 INCHES FROM O/B END, FABRICATED REPAIR DOUBLERS AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 4.SDR CA090209006Roller · brokenLT FLAP OUTBOARD LOWER ROLLER BROKE COMPLETELY UP CAUSING THE FLAP TO SEIZE INTO THE FLAP TRACK DURING THE FLAPS BEING RETRACTED AFTER TAKEOFF. WITH THE FLAP SEIZE THE FLAP MOTOR CONTINUED TO PULL THE SLAVE FLAP UNTIL THE RETRACT CABLE SNAPPED IN FLIGHT. THE SDR ASAA0944465Skin · damagedRT OTBD MID FLAP AFT PANEL UNDER NR 3 AND NR 4 AFT FLAP TRACKS CHAFED AND GOUGED. PREPPED AREA FABRICATED FILLER DOUBLER AND BONDED REPAIR DOUBLER AND FILLER IAW B737 400 SRM 57 53 01 REPAIR 9.SDR WRLA2009053Hinge Bracket · brokenDURING C-CHECK IN TPE INSPECTION FOUND RT O/B FLAP I/B FORWARD FAIRING HINGE BRACKET BROKEN (REF EGAT N/R U05125). REPLACED BRACKET AT RT O/B FLAP I/B FWD FAIRING HINGE IAW SRM VOL 2 51-35-01 REV 40.SDR C8GA20090060Skin · delaminatedWHILE IN HEAVY MAINTENANCE IS WAS NOTED THAT LT OTBD AFT FLAP HAS DELAMINATION AT WBL 300. DAMAGE WAS REMOVED APPROX DIM 5.5 INCH BY 2 INCH, FABRICATED FILLER FROM 2024 T3 .016 INCH DIM 5.5 INCH BY 2 INCH AND DOUBLER FROM 2024 T3 .016 DIM 7 INCH BY 3.5 INCH. SDR C8GA20090051Skin · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT WING INBD AFT FLAP LEADING EDGE IS CRACKED AT 4TH TRACK. STOP DRILLED CRACK PERFORMED HFEC INSP NO CRACKS NOTED. FABRICATED REPAIR DOUBLER FROM 2024 T3 .050 INCH DIM 5.375 INCH BY 3.125 INCH. INSTALLED REPSDR C8GA20090049Skin · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT WING OUTBOARD AFT FLAP LEADING EDGE IS CRACKED AT THE 2ND TRACK. STOP DRILLED CRACK, PERFORMED HFEC INSP, NO CRACKS WERE NOTED. FABRICATED DOUBLER FROM 2024 T3 .050 INCH DIM 5.75 INCH BY 4 INCH INSTALLED REPSDR C8GA20090045Skin · delaminatedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT WING INBOARD AFT FLAP UPPER SURFACE HAS 2 SPOTS OF DELAMINATION WBL 80-90. REMOVED DAMAGED SKIN AND CORE DIM 7.5 INCH BY 9.5 INCH. FABRICATED NEW CORE FROM 5052-44-3/16. FABRICATED FILLER DIM 7.5 INCH BY 9SDR C8GA20090042Web · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT TRAILING EDGE FALSE SPAR, AFT WEB IS CRACKED AT LOWER RIVET AT WBL 130. REMOVED SPOILER ACTUATOR FITTING AND DOUBLER TRIM WEB. FABRICATED NEW LOWER CHORD FROM P/N BAC 1514-14377075T6511 DIM 20.5 INCH LONG ASDR C8GA20090041Skin · debondedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT INBD AFT FLAP UPPER SURFACE APPROX 64 INCHES FROM OTBD END IS DIS-BONDED. DAMAGED AREA REMOVED DIM 9 INCH BY 4.5 INCH. FABRICATED FILLER DIM 9 INCH BY 4.5 INCH AND DOUBLER DIM 12 INCH BY 6 INCH FROM 2024 T3
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