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 TAMF20100047SSupport · chafedDURING SC3 CHECKS, INSP FOUND CHAFING DAMAGE ON THE 113T1307-15, OTBD FLAP NR 1 SUPPORT, MAIN DRIVE LINK ASSY, DAMAGE ON LOWER FLANGE 113T1399-2, OTBD FLAP NR 1 SUPPORT, MAIN DRIVE LINK, SIDE LINK, INBD SIDE LINK. REPAIRED, ACCOMPLISHED IAW EWO 767-57-063R0 ANSDR SWAA104158Skin · puncturedDURING SCHEDULED 12Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.SDR SWAA104146Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA104143Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP I/B LOWER CORNER SKIN DELAMINATED. REPAIRED AFT FLAP PER EA.SDR SWAA104142Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.SDR SWAA104131Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING O/B AFT FLAP T/E DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR IPXA10661193Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP L/E FOUND DELAMINATION COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5.SDR USAA2010071991456Flap · debondedPIT - MAJOR REPAIR - S4 - DISBONDED 3 INCHES BY 5 INCHES AREA ON LEFT OUTBOUND FLAP TRAILING EDGE AT NR 3 FLAP TRACK. REPAIRED LEFT OUTBOUND FLAP TRAILING EDGE AT NR 3 FLAP TRACK IAW A319 SRM 57-52-00 FIGURE 211.SDR AALA20110217TUL14Skin · damagedTOP OF SKIN LEFT INBOARD MAIN FLAP INBOARD END DENT IS DELAMINATED. REMOVED 2 BY 4 INCHES SKIN AND CORE, HOT BONDED NEW CORE, FABRICATED AND INSTALLED HOT BONDED DOUBLER PER SRM 51-71-10-2R FIGURE 209.SDR USAA2010081091639Skin · delaminatedSAL - Q4 - MAJOR REPAIR - DELAMINATION ON RIGHT WING OUTBOARD FORE FLAP UPPER SURFACE BETWEEN WBL 202 TO WBL 224. REPLACED RIGHT WING OUTBOARD FORE FLAP IAW JOB CARD 03C40927013.SDR USAA2010081091631Flap · delaminatedSAL - Q4 - MAJOR REPAIR - DELAMINATION ON RIGHT WING INBOARD FORE FLAP LOWER SURFACE BETWEEN WBL 88 TO WBL 106. REPLACED RIGHT WING INBOARD FORE FLAP IAW JOB CARD 03C40927014.SDR IPXA10B61603Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NO-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP. REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 57.SDR IPXA10B61602Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD REPAIR. FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5.C, FIG.2, REV.57.SDR IPXA10B61601Wedge · misrepairedINSPECTION TYPE:C LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5 C, FIG 2, REV 57.SDR IPXA10B61600Wedge · misrepairedINSPECTION TYPE:C LH WING I/B FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5.C FIG.2 REV 57.SDR IPXA10B61599Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5 C, FIG 2, REV 57.SDR IPXA10B61598Wedge · misrepairedINSPECTION TYPE:C, LT WING INB FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5 C, FIG 2, REV 57.SDR IPXA10B61597Wedge · misrepairedINSPECTION TYPE:C LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 57.SDR SWAA104111Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA104109Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING T/E FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR FDEA201007122476Rib · crackedRT WING NR 16 L/E SLAT TRACK SUPPORT RIB FOUND SUSPECTED CRACK. CRACKED RIB NR 16 REMOVED AND REPLACED NEW RIB AT RH WING L/EDGE AS PER DOUGLAS DRAWING ARB7565 REV. C. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-10 REV 110. RH WING NR 8 SLAT CABLES ADJUSTMESDR F3LA2010072500472Flap · damagedREFERENCE HEAVY MAINTENANCE NON ROUTINE N0001. TEMPORARY REPAIR TO LIGHTNING STRIKE DAMAGE ON RIGHT WING OUTBOARD FLAP TRAILING EDGE 4.25 INCHES FROM OUTBOARD EDGE AND 3.5 INCHES FROM TRAILING EDGE. DAMAGE MEASURED 1.75 X 0.50 INCH. INSTALLED PERMANENT REPASDR FDEA201007122491Support Fitting · crackedLT WING INBD FLAP ENCLOSURE AREA, INBD FLAP ROLLER SUPPORT FITTING FOUND CRACKED. REPAIR CARRIED OUT IAW EA 8-5340-140419, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.SDR IPXA10B61593Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61514Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61505Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FORE FLAP T/E WEDGE UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61502Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SEM 51-70-07, PAR 5A (1) FIG 5, REV 56.SDR SWAA104081Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR IPXA0B61955Skin · dentedINSPECTION TYPE:C, LT WING INBD AFT FLAP LWR SKIN FOUND SEVERAL DENTS. SKIN METAL HOT BOND INTERIM REPAIRED IAW HX RS R57-51-36778 REV A AND EO B747-5750-39125-A. THIS IS A MAJOR REPAIR WITH ALUMINUM SHEET: 2024T3-0020IN. REPAIR PATCH SIZE: 36.5" X 19". FINSDR IPXA10B61501Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61500Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 5, REV 56.SDR UIEA2010070900096Skin · corrodedCORROSION WAS FOUND ON THE RT INBD MID FLAP UPPER SKIN AT WBL 315 AND 388. LEVEL 1 CORROSION. (THE CORROSION WAS BLENDED OUT TO A MINIMUM THICKNESS OF 0.070 INCH, NDI INSPECTED, THE SURFACE FINISH WAS RESTORED AND A BONDED FILLER AND REPAIR DOUBLER WAS INSTALLSDR ASAA1048095Skin · gougedRIGHT O/B MID FLAP INBOARD LEADING EDGE IS GOUGED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER AND INSTALLED REPAIR.SDR ASAA1048070Skin · chafedLEFT O/B FORE FLAP OUTBOARD LOWER SKIN CHAFED. REMOVED REPAIR DOUBLER AND INSTALLED NEW DOUBLER.SDR UIEA2010070900097Skin · dentedDURING SPECIAL CHECK INSP BEING PERFORMED; DAMAGE WAS FOUND TO THE RT WING - INBD & OTBD T/E MID & AFT FLAPS WITH DENT/DELAMINATION AREAS AS DESCRIBED BELOW: RT WING INBD T/E MID FLAP INBD L/E FAIRING DENT (REF N/CR 50072 AND FIG 1). RT WING OTBD T/E AFT FLAP SDR FDEA201007092439Skin · crackedRT WING OTBD FLAP ASSY UPPER SURFACE FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIG 85, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR AALA20100708TUL04Skin · delaminatedCORROSION - TRAILING EDGE OF INBOARD FLAP HAS DELAMINATION BLISTERS ON UPPER SURFACE, MARKED. FABRICATED REPAIR PARTS AND INSTALLED TWO EACH PERMANENT HOT BOND REPAIRS ON UPPER FLAP SKIN AT TRAILING EDGE PER SRM 51-70-10-2R 4.SDR AALA20100708TUL07Vane · wornLEFT WING DEEP WEAR IN NUMBER 3 FLAP VANE LEADING EDGE ABOVE OUTBOARD FLAP INBOARD HINGE. INSTALLED BONDED REPAIR DOUBLER PER SRM 51-70-02.SDR IPXA10B61513Wedge · delaminatedINSPECTION TYPE:C RT WING INBD FORE T/E WEDGE LWR SURFACE DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61512Wedge · delaminatedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) REV 56.SDR IPXA10B61510Wedge · delaminatedINSPECTION TYPE:C LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE INBD AREA DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-50-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61507Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61491Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV 56.SDR FDEA201007082407Skin · damagedLEFT INBOARD TRAILING EDGE FLAP LOWER SURFACE 01 EACH EXISTING REPAIR FOUND AT INBOARD LOWER SEGMENT AREA XIFH 150.300. EXISTING REPAIR AT LEFT HAND INBOARD TRAILING EDGE FLAP LOWER SURFACE INBOARD LOWER SEGMENT AREA XIFH 150.300 REMOVED AS PER MD10 SRM 51-SDR IPXA10B61426Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD FORE FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT, IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 56.SDR IPXA10B61423Fairing · puncturedINSPECTION TYPE:C, LT WING INBOARD FORE FLAP L/E FAIRING PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR. 5A (1) FIG 5, REV 56.SDR ASAA1048057Flap · chafedRIGHT OUTBOARD FORE FLAP OUTBOARD END IS CHAFING ON FIXED TRAILING EDGE PANEL. REMOVED REPAIR DOUBLER. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW B747 400 SRM 57 53 01.SDR ASAA1048056Skin · delaminatedLEFT INBOARD AFT FLAP DELAMINATED TRAILING EDGE OUTBOARD SIDE LOWER. REPAIRED LEFT INBOARD AFT FLAP LOWER SIDES IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1048055Skin · delaminatedLEFT INBOARD AFT FLAP DELAM OUTBOARD TRAILING EDGE CORNER UPPER SIDE. REPAIRED LEFT INBOARD AFT FLAP UPPER SIDE IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA1048054Skin · dentedRIGHT INBOARD AFT FLAP IS DENTED ON LWR SURFACE 9.5 INCHES FROM INBOARD EDGE 4.5 INCHES FROM T/E WITH EXPOSED COMPOSITE. REPAIRED RIGHT INBOARD FLAP IAW B737 400 SRM 51 70 06 REPAIR 2.
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