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 UALA2010061402060Bearing · migratedRT WING NR 8 FLAP TRACK FWD MOUNT BEARING MIGRATION. ACP BEARING REPLACEMENT IAW SB 747-57-2325, REV 2 AND FIELD REPAIR RECORD UAL-744-0635. REPAIRS ACCOMPLISHED ON THE NR 8 FLAP TRACK FWD MOUNT.Jun 12, 2010 · N194UA · Boeing 747422SDR UALA2010061402059Bearing · migratedRT WING NR 7 FLAP TRACK FWD MOUNT BEARING MIGRATION. ACP BEARING REPLACEMENT IAW SB 747-57-2325, REV 2 AND FIELD REPAIR RECORD UAL-744-0634. NON ROUTINE 270160.Jun 12, 2010 · N194UA · Boeing 747422SDR UALA2010061402058Bearing · migratedRH WING #6 FLAP TRACK FWD MOUNT BEARING MIGRATION. ACP BEARING REPLACEMENT IAW SB 747-57-2325 REV 2 AND FIELD REPAIR RECORD UAL-744-0633.Jun 12, 2010 · N194UA · Boeing 747422SDR UALA2010061402057Bearing · looseLT WING TE FLAP NR 2 TRACK FWD FITTING BEARING ROTATION. ACP BEARING REPLACEMENT IAW SB 747-57-2325 REV 2 AND FIELD REPAIR RECORD UAL-744-0632.Jun 12, 2010 · N194UA · Boeing 747422SDR UALA2010061402056Bearing · looseLT WING T/E FLAP NR 1 TRACK FITTING BEARING ROTATION. ACP BEARING REPLACEMENT IAW SB 747-57-2325 REV 2 AND FIELD REPAIR RECORD UAL-744-0631.Jun 12, 2010 · N194UA · Boeing 747422SDR UALA2010061402090Skin · puncturedRT INBD T/E FLAP HAS PUNCTURE ON TOP SIDE. PUNCTURE WITHIN LIMITS IAW SRM. SEALED WITH SPEED TAPE, INSPECT EACH "A CHECK". DO A REPAIR NO LATER THAN THE NEXT "C CHK". SHOP 273 WILL NEED T/E AFT FLAP REMOVED FOR IN SHOP REPAIR. 5 SHIFT SLOT RQSTD FOR TE FLAP Jun 12, 2010 · N648UA · Boeing 767322SDR IPXA10M61079Skin · chafedINSPECTION TYPE:4C, RT INBD FLAP LOWER OTBD SKIN CHAFED ALL THE WAY AROUND THE AFT FAIRING. BLENDED RT INBD FLAP LOWER OTBD SKIN AT XIFH 269. REPAIRED IAW EO MD11 5750-38704 AND EA 011-5700-01-A2518.Jun 11, 2010 · N280UP · Doug MD11FSDR IPXA10M60834Vane · delaminatedINSPECTION TYPE:4C, RT INBD FLAP VANE DELAMINATED ON LWR SURFACE AND 65 INCH FROM IB END, CUT OUT DAMAGE ON RT INBD FLAP VANE LWR SURFACE. PREPPED AND BONDED DISC REPAINT AREA REF SRM 51-50-80 REPAIR 2 PARA 4D.Jun 11, 2010 · N280UP · Doug MD11FSDR ASAA1047913Skin · delaminatedLT INBOARD AFT FLAP LOWER SURFACE HAS AREAS OF DELAMINATION. REMOVED DAMAGE AND BONDED REPAIR.Jun 11, 2010 · N763AS · Boeing 7374Q8SDR SWAA103444Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.Jun 11, 2010 · N631SW · Boeing 7373H4SDR HALA2010061000287Attach Bracket · crackedATTACH BRACKET CRACKED, FOR RT FLAP MID HINGE FWD FAIRING (BRACKET MOUNTED ON FOOTBALL PANEL, 620EB. REMOVED AND REPLACED BRACKET FOR FWD FLAP MID HINGE FAIRING.Jun 10, 2010 · N486HA · Boeing 717200SDR FDEA201006101933Hinge Fitting · corrodedRT WING - INBD FLAP, OTBD HINGE FITTING (FLAP SIDE) ACTUATOR ATTACHMENT LUG INBD SURFACE FOUND CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140351, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.Jun 10, 2010 · N560FE · Doug MD1010FSDR FDEA201006101932Hinge Fitting · corrodedLT WING - INBD FLAP, OTBD HINGE FITTING (FLAP SIDE) PIVOT POINT OTBD LUG BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT PER MD10 CMM 57-52-01 REVISION 50. NEW BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-01 REVISION 50. REPAIR CLASSIFIED AS MINOR Jun 10, 2010 · N560FE · Doug MD1010FSDR FDEA201006101931Hinge Fitting · corrodedLT WING - INBD FLAP, OTBD HINGE FITTING (FLAP SIDE) LOWER LUG INBD SIDE FOUND CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140350, REPAIR CLASSIFIED MINOR PER GMM 6 -2-100 REVISION 110.Jun 10, 2010 · N560FE · Doug MD1010FSDR A6WA201040419Panel · chafedLT INBD FLAP STUB PANEL HAS CHAFING. REMOVED UNSERVICEABLE FLAP STUB FROM LT INBD FLAP AND INSTALLED SERVICEABLE FLAP STUB.Jun 10, 2010 · N438AW · Cndair CL6002B19SDR SWAA103498Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Jun 10, 2010 · N772SW · Boeing 7377H4SDR SWAA103497Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND R/H WING O/B AFT FLAP I/B LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.Jun 10, 2010 · N772SW · Boeing 7377H4SDR SWAA103496Flap · puncturedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.Jun 10, 2010 · N772SW · Boeing 7377H4SDR IPXA10B60478Wedge · dentedINSPECTION TYPE:C, DMI D423196 - LT WING INBD FORE FLAP T/E WEDGE UPPER SURFACE CRACK /DENT. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A FIG 5 REV 56.Jun 10, 2010 · N577UP · Boeing 74744AFSDR IPXA10B60477Panel · puncturedINSPECTION TYPE:C, DMI D421159 - LT WING INBD MID FLAP T/E COVE PANEL LOWER SURFACE PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A FIG 5, REV 56.Jun 10, 2010 · N577UP · Boeing 74744AFSDR IPXA10161064Skin · scratchedINSPECTION TYPE:10YR, RT WING INBD FLAP UNDER SURFACES T/E HAS 4EA SCRATCHES ABOUT 8 TO 11 INCHES WITHIN EACH OTHER. ACCOMPLISHED REPAIR IAW EO A300-5750-38698-A AND STA-SA, EA 300-5750-01-A2525, REV I/R.Jun 9, 2010 · N126UP · Airbus A300F4622RSDR IPXA10161027Skin · chafedINSPECTION TYPE:10YR, LT OTBD FLAP INBD L/E CHAFED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-00 PARA 4H FIG 208.Jun 9, 2010 · N121UP · Airbus A300F4622RSDR IPXA10160993Skin · chafedINSPECTION TYPE:10YR, LT INBD FLAP UPPER SKIN REPAIR DOUBLER IS CHAFED ACCOMPLISHED REPAIR IAW STA EA 300-5750-01-A2498, REV I/R AND EO A300-5750-38651-A.Jun 9, 2010 · N121UP · Airbus A300F4622RSDR IPXA10160960Skin · chafedINSPECTION TYPE:10YR, RT OTBD FLAP INBD L/E IS CHAFED. ACCOMPLISHED REPAIR IAW SRM57-50-00 PARA.4 FIG 208.Jun 9, 2010 · N121UP · Airbus A300F4622RSDR FDEA201006092367Skin · damagedRT WING - FLAP OTBD T/E SKIN SURFACE DEBONDED (1360MM LENGHT BY 190MM WIDTH) BETWEEN RIB 2 AND RIB 4. RT WING FLAP OTBD WAS REPAIRED IAW EA 6-5750-140260.Jun 9, 2010 · N447FE · Airbus A310222SDR IPXA10160802Skin · gougedINSPECTION TYPE:10YR, LT CTR FLAP UPPER SKIN REPAIR IS GOUGED IN SEVERAL PLACES. ACCOMPLISHED REPAIR IAW SRM 57-50-00 PARA 4E, FIG 205.Jun 9, 2010 · N121UP · Airbus A300F4622RSDR IPXA10660600Wedge · crackedINSPECTION TYPE:C, LT WING OTBD T/E FLAP T/E WEDGE INBD AREA LWR SURFACE CRACKED. FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5G, FIG 14, REV 47.Jun 9, 2010 · N320UP · Boeing 76734AFSDR SWIA201024709Flap · crackedLEFT NACELLE FLAP CRACKED. (C-CHECK) LEFT NACELLE FLAP REPLACED.Jun 8, 2010 · N221SW · Emb EMB120ERSDR IPXA10660606Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 54.5" FROM OTBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 9, REV 47.Jun 8, 2010 · N320UP · Boeing 76734AFSDR IPXA10660601Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP T/E LWR SURFACE AT 127" FROM OTBD EDGE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 9, REV 47.Jun 8, 2010 · N320UP · Boeing 76734AFSDR UIEA2010060800029Panel · brokenDURING A2-CHECK INSP, MX FOUND THE RT WBL 515 - OTBD MID FLAP L/E & AMP; RT WING FIXED T/E WITH CRACK/DAMAGE. WBL 515 - L/E OF RT OTBD MID FLAP BROKEN . THE DIMENSION IS 0.787 & .787 ) WBL 515 RT WING FIXED T/E FAIRING PANEL BROKEN AT WBL 515.. (1)PERMANENT RJun 8, 2010 · N409MC · Boeing 74747UFSDR FDEA201006081863Skin · damagedRT WING - INBD FLAP ASSY LOWER SURFACE FOUND MULTIPLE DENT AND SCRATCHES. REPAIRED SRM 57-10-00, FIG 3 VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAWGMM 6-2-100, REV 110.Jun 8, 2010 · N560FE · Doug MD1010FSDR FDEA201006081862Support Fitting · chafedLT WING - INBD FLAP INBD TRACK MOST FWD SUPPORT FITTING FOUND CHAFED. REPAIRED AS PER E.A. 1-5740-140356, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 110.Jun 8, 2010 · N560FE · Doug MD1010FSDR IPXA10160327Skin · damagedRT WING INBD FLAP LOWER SURFACE DAMAGED. REPAIRED IAW EO A300-5750-36683-B.Jun 7, 2010 · N137UP · Airbus A300F4622RSDR FDEA201006071858Fitting · corrodedLT OTBD FLAP; OTBD SIDE LOAD FITTING; ACFT SIDE; FWD HOLE IS CORRODED. BLENDED CORRODED AREA IAW SRM 51-21-01, VOL II. FOUND TO BE OUT OF LIMITS DUE TO EXFOLIATION. R &R SIDE LOAD FITING IAW SRM 51-33-01, VOL II AND DWG ARC 0501, REV "B4".Jun 7, 2010 · N357FE · Doug MD1010FSDR DALA1012183266Trunnion · wornDURING M-CHECK FOUND LT WING INBOARD FLAP TRUNNION WEAR MAXIMUM REWORK DEPTH EXCEEDS 0.236 INCHES, DEPTH MEASUREMENT IS 0.3375 INCHES. REPLACED LT WING INBD FLAP TRUNNION SUPPORT IAW ERA 482530-14AD.Jun 6, 2010 · N366NW · Airbus A320212SDR DALASupport · wornDURING M-CHECK FOUND LT WING INBD FLAP TRUNNION WEAR MAXIMUM REWORK DEPTH EXCEEDS 0.236 INCHES, DEPTH MEASUREMENT IS 0.3375 INCHES. REPLACED LT WING INBD FLAP TRUNNION SUPPORT IAW ERA 482530-14AD.Jun 6, 2010 · N366NW · Airbus A320212SDR IPXA10160429Skin · gougedINSPECTION TYPE:5YR, REPAIR SURVEY SEQUENCE NR167-W3-02 REPAIR DOUBLER GOUGED IN 4 PLACES ON LT CTR FLAP UPPER SKIN BETWEEN RIBS 13-15 STGR 2.6 AND 2.7. REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 57-50-00 PB 201 PARA 4E, FIG 205 AND SRM 57-5Jun 5, 2010 · N167UP · Airbus A300F4622RSDR CALA2010060800252Flap Track · corrodedRT WING NR 8 FLAP TRACK AFT ATTACH POINT EMITTING RUST. REMOVED NR 8 FLAP TRACK. INSTALLED NEW SERVICEABLE FLAP TRACK REF M/M 27-51-49-404-006.Jun 5, 2010 · N17614 · Boeing 737524SDR CALA2010060800251Flap Track · corrodedEVIDENCE OF RUST BETWEEN NR 7 FLAP TRACK AND LWR SURFACE OF REAR SPAR REMOVED NR 7 FLAP TRACK ASSY. ROTABLE PARTS CHANGE WAS INDICATED - 24-5753-9-9001 TRACK, FLAP, OB OFF 24-5753-9-9001 1614 ON. REMOVED NR 7 FLAP TRACK. INSTALLED NEW SERVICEABLE FLAP TRACJun 5, 2010 · N17614 · Boeing 737524SDR A6WA201040406Vane · chafedLT INBD FLAP VANE CHAFING DAMAGE TO L/E IN 3 PLACES DAMAGE MINOR IN PAINT ONLY. HAND BLENDED IAW SRM 57-52-00 AND 57-00-31. REAPPLIED PRIMER AND TOP COAT IAW SRM 51-25-06 AND 51-25-26. DELETED DAMAGE MINOR IN PAINT ONLY.Jun 4, 2010 · N438AW · Cndair CL6002B19SDR IPXA0160648Skin · gougedINSPECTION TYPE:5YR, LT OTBD FLAP IB L/E TIP IS GOUGED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-00 PARA. 4H FIG 208.Jun 4, 2010 · N167UP · Airbus A300F4622RSDR IPXA0160609Skin · gougedINSPECTION TYPE:5YR, RT WING OTBD FLAP INBD L/E GOUGED. CUT OUT DAMAGED L/E SKIN, FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-00 PARA 4 H FIG 208.Jun 4, 2010 · N167UP · Airbus A300F4622RSDR FDEA201006041822Skin · delaminatedLT INBD FLAP T/E AT MIDSPAN HAS 2EA DISBONDED AREAS ON TOP AND BOTTOM SKINS APPROX 24" (INCHES) LENGTH TOTAL. REMOVED PREVIOUS REPAIR DOUBLER, LT INBD FLAP T/E UPPER SKIN MIDSPAN IAW SRM 51-77-11. CUT OUT DISBONDED UPPER SKIN IAW SRM 57-53-12, PAR 13 B(5). CJun 4, 2010 · N404FE · Airbus A310203SDR FDEA201006031810Angle · crackedRT WING INBD MID FLAP LOWER T/E CHORD ANGLE IS CRACKED, 2 PLACES, WBL 100. R & R DUE TO DELAMINATION ON SNRM NR N00544, WO NR00048343.Jun 3, 2010 · N267FE · Boeing 727233SDR UIEA2010060300024Skin · tornLT WING INBD T/E MID FLAP INBD FUSELAGE SEAL UPPER SURFACE TORN. REQUIRES REPLACEMENT. (EO 4457A263/ NON MEL MDDR 17280 RAISED FOR LW T/E INBD MID FLAP TEMP REPAIR PER PT 1 OF EO AND REPEAT INSP IAW PT 2 WITH PERM REPAIR TO BE CARRIED OUT AT THE NEXT A CHECKJun 3, 2010 · N493MC · Boeing 74747UFSDR IPXA10161016Structure · damagedINSPECTION TYPE:10YR, IMPACT DAMAGE TO RT INBD T/E FLAP OTBD T/E. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW EA 300-5753-01-A2458 I/R AND UPS EO A300-5750-38674-A.Jun 2, 2010 · N121UP · Airbus A300F4622RSDR SWAA103206Spindle · crackedDURING SCHEDULED MV2 CHECK, FOUND T/E FLAP NR 2 SPINDLE CRACKED. REMOVED AND REPLACED NR 2 SPINDLE PER MM.Jun 2, 2010 · N685SW · Boeing 7373Q8SDR SWAA103205Spindle · crackedDURING SCHEDULED OTS CHECK, FOUND T/E FLAP NR 8 SPINDLE CRACKED. REMOVED AND REPLACED NR 8 SPINDLE PER SI.Jun 2, 2010 · N684WN · Boeing 7373T0SDR AALA20100601TUL02Rub Strip · wornRIGHT WING NUMBER 3 FLAP VANE INBOARD END RUB STRIP IS WORN THROUGH AT LEADING EDGE. HOT BOND METAL DOUBLER ON RIGHT WING NUMBER 3 FLAP VANE RUB STRIP TRAILING EDGE PER SRM 51-70-02.Jun 1, 2010 · N7531A · Doug DC982
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