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 ASAA0842530Skin · dentedRT WING INBOARD AFT FORE FLAP DENTED ON LOWER SURFACE IN 2 EACH PLACES 28" AND 29" FROM INBOARD END AND 6" FROM TRAILING EDGE. PREPARED AREA FOR REPAIR: FABRICATED REPAIR PARTS AND BONDED IAW B737 400 51 70 4 REPAIR 4.Jan 22, 2008 · N773AS · Boeing 7374Q8SDR 08FDEA00226Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING ARC4009 FORWARD INBOARD FASTENER HOLE FOUND CORROSION. LT WING, OUTBOARD FLAP R & R AS PER AMM 27-50-30-4. FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. TEST OF THE FLAP SYSTEM OPERATION/RANGE OF MOJan 22, 2008 · N617FE · Doug MD11FSDR 08FDEA00225Hinge Fitting · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING ARC4008 OUTBOARD FASTENER HOLE FOUND CORROSION. LT WING, OUTBOARD FLAP R & R AS PER AMM 27-50-30-4. FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. TEST OF THE FLAP OPERATION/RANGE OF MOVEMENT CARRIED OUJan 22, 2008 · N617FE · Doug MD11FSDR UPS08M52058Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE AFT LOWER O/B BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE LWR MOUNT O/B BORE & SPOTFACE CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 PG 602-607R.60. FPI C/Jan 21, 2008 · N294UP · Doug MD11SDR UPS08M52057Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING HINGE MOUNTED SIDE ATTACHMENT UPPER BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE BARREL NUT UPR BORE & SPOTFACE CORROSION REMOVED & FOUND WITHIN LIMIT PER CMM57-44-08 PG 613-615R.6Jan 21, 2008 · N294UP · Doug MD11SDR UPS08M52056Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE AFT LOWER I/B BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE LWR MOUNT I/B BORE & SPOT FACE CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 PG602-607R.60. FPI CJan 21, 2008 · N294UP · Doug MD11SDR UPS08M52054Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE SIDE ATTACHMENT LOWER BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE BARREL NUT LWR BORE & SPOTFACE CORROSION REMOVED & FOUND WITHIN LIMIT PER CMM57-44-08 PG 613-615R.6Jan 21, 2008 · N294UP · Doug MD11SDR DHL2008765014Structure · crackedDURING C CHECK: DISCREPANCY - RIGHT WING INBOARD FLAP, MID FLAP AFT IS CRACKED ON BOTH INBOARD AND OUTBOARD SIDE WBL 90.69 AND WBL 104.0. REMOVED NR 5 AND 6 TEAR DROP FAIRINGS AND RIGHT INBOARD MID FLAP LOWER SKIN TO GAIN ACCESS IAW SRM 51-30-2. REMOVED CRACJan 21, 2008 · N765AT · Boeing 727264SDR 2008UALA00330Support Fitting · crackedRIGHT WING OUTBOARD FLAP FAIRING, SUPPORT FITTING CRACKED, LOCATED INBOARD OF AILERON. ACCOMPLISHED MAJOR REPAIR.Jan 20, 2008 · N527UA · Boeing 757222SDR QXEA200800135Skin · chafedPDX - C4 CHECK - RIGHT INBOARD FLAP HAS A CHAFE SPOT ON THE UPPER SURFACE APPROXIMATELY 6 INCHES OUT FROM INBOARD END AND 19 INCHES UP FROM THE TRAILING EDGE. BLENDED OUT CHAFE WITH SCOTHBRITE PAD, FOUND TO BE IN LIMITS IAW Q400 SRM 57-51-30 PG 102. INSPECTEJan 19, 2008 · N405QX · Bombdr DHC8402SDR QXEA200800134Skin · chafedPDX - C4 CHECK - RIGHT OUTBOARD FLAP, INBOARD END, LOWER SIDE OF LEADING EDGE IS LIGHTLY CHAFED FOR APPROXIMATELY 5 INCHES. REPAIRED IAW RD8/4-57-0920, AND Q400 NDTM PT-6 51-00-01, Q400 SRM 51-25-10 AND 51-25-15.Jan 19, 2008 · N405QX · Bombdr DHC8402SDR IXXA08SMN020SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP LOWER SURFACE HAS IMPROPER REPAIR AT STATION XW 59.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. Jan 19, 2008 · N41CX · Doug DC863FSDR USAA920080307Rib · crackedMCN - MAJOR REPAIR - C20 CHECK - NR 6060828, RIGHT WING OUTBOARD MIDFLAP RIB CRACKED, WBL 387.06. REPLACED RIGHT WING OUTBOARD MIDFLAP RIB IAW B737 SRM 51-40-02.Jan 19, 2008 · N313AW · Boeing 7373S3SDR USAA920080217Skin · delaminatedCLT - MAJOR REPAIR - C1 CHECK - RIGHT WING OUTBOARD FORE FLAP, INBOARD TRAILING EDGE HAS 6 INCH AREA OF DELAMINATION. REPLACED RIGHT WING OUTBOARD FOREFLAP IAW B737 AMM 27-51-37.Jan 19, 2008 · N450UW · Boeing 7374B7SDR SWIA200819521Structure · corrodedLEFT INBOARD FLAP INTERIOR STRUCTURE HAS SIGNS OF CORROSION, FOUND AT C-CHECK. REPLACED FLAP ASSEMBLY PER CRJ200 AMM 57-52-08.Jan 15, 2008 · N983CA · Cndair CL6002B19SDR DHL2008765013Skin · gougedDURING C CHECK, LT OUTBOARD FORE FLAP OUTBOARD LEADING EDGE REPAIR IS GOUGED 2 PLACES. REMOVED OLD DOUBLER REPAIR IAW SRM 51-30-2. FABRICATED NEW DOUBLER REPAIR IAW SRM 57-50-2 FIG 4. TREATED AND PRIMED NEW DOUBLER IAW SRM 51-10-2. INSTALLED NEW DOUBLER IAJan 15, 2008 · N765AT · Boeing 727264SDR DHL2007873523Skin · wornRT OUTBD FLAP UPPER SKIN WORN AT STA XF 210.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-14-08 EVA NR 0857-00032 REV IR DATED 01-05-08 SEMAN DWG ED-4680 DATED 01-02-08. REMOVED DAMAGE SKIN SEGMENT IAW SRM 51-1-21. FABRICATED NEW SJan 15, 2008 · N873SJ · Doug DC873FSDR USAA920080276Flap · corrodedMCN - MAJOR REPAIR - C11 CHECK - CORROSION ON LEFT WING INBOARD FLAP TRAILING EDGE, FLAP STATION 238 - FLAP STA 241. REPAIRED LEFT WING INBOARD FLAP TRAILING EDGE, FLAP STATION 238 - FLAP STA 241 IAW B757 SRM 51-70-10 REPAIR 4.Jan 15, 2008 · N915AW · Boeing 757225SDR USAA920080275Flap · corrodedMCN - MAJOR REPAIR - C11 CHECK - CORROSION ON LEFT WING INBOARD FLAP TRAILING EDGE, FLAP STATION 254.88 - FLAP STA 300. REPAIRED LEFT WING INBOARD FLAP TRAILING EDGE, FLAP STATION 254.88 - FLAP STA 300 IAW B757 SRM 51-70-10 REPAIR 4.Jan 15, 2008 · N915AW · Boeing 757225SDR USAA920080250Skin · delaminatedMCN - MAJOR REPAIR - C18 CHECK - RIGHT WING INBOARD MID FLAP LOWER SURFACE HAS AREA OF DELAMINATION, WBL 73 - WBL 75. REPAIRED RIGHT WING INBOARD MID FLAP LOWER SURFACE, WBL 73 - WBL 75 IAW B737 SRM 57-70-10-2R4. Jan 15, 2008 · N334AW · Boeing 7373Y0SDR 2008UALA00282Hinge Fitting · crackedLT INBOARD FLAP CENTER HINGE FITTING CRACKED INBOARD SIDE. ACP EQ5256 TE FLAP FITTING INSPECTION. MANDATED BY AD 2003-13-01. REMOVED DAMAGED FLANGES. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR ANGLES. ACFT OK FOR SERVICE.Jan 15, 2008 · N667UA · Boeing 767322SDR 2008UALA00281Hinge Bracket · crackedRIGHT WING INBOARD FLAP, FORE TO AFT FLAP CENTER HINGE BRACKET CRACKED. ACP EQ5256 TE FLAP FITTING INSPECTION. MANDATED BY AD 2003-13-01. REMOVED DAMAGED FLANGES. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR ANGLES. ACFT OK FOR SERVICE. Jan 15, 2008 · N667UA · Boeing 767322SDR SWAA080334Flap · debondedDURING SCHEDULED 20Y CHECK, FOUND RT WING FORE FLAP T/E DISBONDED. REPAIRED FLAP PER SRM.Jan 15, 2008 · N697SW · Boeing 7373TOSDR IXXA08SMN007SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING JOINT FLAP DELAMINATED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. FABRICATED NEW SKIN. REMOVED CORE AND CLEANED AREA. INSTALLED CORE AND NEW FASTENERS AND REPAIRED PARTS IAW DC8Jan 14, 2008 · N41CX · Doug DC862FSDR IXXA08SMN006SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING JOINT FLAP DELAMINATED SKIN. REMOVED DAMAGED JOINT FLAP. INSTALLED NEW JOINT FLAP IAW DC8 SRM 51-3-0, 51-3-1.Jan 14, 2008 · N41CX · Doug DC862FSDR HALA0800039Structure · corrodedLEVEL 2 CORROSION, RT WING INBD T/E AFT FLAP HAS LOOSE SEALANT, BULGING OF LWR SKIN AND EXFOLIATION CORROSION ADJACENT TO OUTER HINGE POINT, ASSESS PER SRM 57-53-02. ACCOMPLISHED CORROSION REPAIR PER AIR NEW ZEALAND TECHNICAL INSTRUCTION 19011691-0001 AND HALJan 14, 2008 · N586HA · Boeing 7673G5SDR HALA0800038Structure · corrodedLEVEL 2 CORROSION, LT WING INBD T/E AFT FLAP HAS LOOSE SEALANT AND EXFOLIATION CORROSION, ASSESS PER SRM 57-53-02. ACCOMPLISHED CORROSION REPAIR PER AIR NEW ZEALAND TECHNICAL INSTRUCTION 190111707-0001 AND HAL M105 586069.Jan 14, 2008 · N586HA · Boeing 7673G5SDR HALA0800064Skin · chafedLT INBOARD AFT FLAP HAS LEADING EDGE CHAFED ALONG IT LENGTH ASSESS DAMAGE PER SRM 57-53-02. AFT FLAP INCORRECTLY ADJUSTED, PULLING IN TIGHTLY AGAINST MID FLAP SEAL. BLENDED IAW SRM 57-53-01, FIG 101. RIG CHECK OF FLAPS OK.Jan 14, 2008 · N586HA · Boeing 7673G5SDR QXEA200800101Flap Track · corrodedPDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK LOWER SIDE THERE ARE TWO AREAS OF ROLLER CHAFE DAMAGE WITH PITTING CORROSION IN BETWEEN. MAINTENANCE BLENDED OUT CHAFE AND PITTING CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED.Jan 14, 2008 · N349PH · Dhav DHC8202SDR QXEA200800102Flap Track · corrodedPDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK INBOARD SIDE LOWER SURFACE OF UPPER FLANGE. THERE IS PITTING CORROSION AT ROLLER CONTACT AREA. MAINTENANCE BLENDED OUT THE PITTING CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED.Jan 14, 2008 · N349PH · Dhav DHC8202SDR QXEA200800103Flap Track · damagedPDX - C1 CHECK - RIGHT OUTBOARD FLAP AREA NR 5 FLAP TRACK. THERE ARE TWO ROLLER CHAFE AREAS ON THE UPPER SURFACE. MAINTENANCE BLENDED AREA, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED.Jan 14, 2008 · N349PH · Dhav DHC8202SDR USAA920080306Skin · debondedMCN - MAJOR REPAIR - C20 CHECK - NR 6033450, LEFT WING INBOARD FORE FLAP, UPPER SURFACE HAS AREA OF DEBOND, WBL 117.5 - WBL 119.5. REPAIRED LEFT WING INBOARD FORE FLAP, UPPER SURFACE IAW B737 SRM 51-70-10-2R REPAIR 3.Jan 14, 2008 · N313AW · Boeing 7373S3SDR UPS08851515Flap Track · damagedINSPECTION TYPE:C2 LT WING FLAP STA XW 340 FLAP TRACKS MISSING CHROME. REMOVED AND REPLACED L/WING FLAP TRACKS AT STA XW 340 IAW DC8 AMM 27-51-03-2.Jan 14, 2008 · N702UP · Doug DC871FSDR SWAA080277Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.Jan 12, 2008 · N639SW · Boeing 7373H4SDR UPS08151458Skin · chafedINSPECTION TYPE:1C LT CENTERFLAP IB UPPER SURFACE HAS HEAVY CHAFFING. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW A300-600 SRM 57-50-00.Jan 11, 2008 · N167UP · Airbus A300F4622RSDR ASAA0842529Skin · dentedLT INBOARD AFT FORE FLAP LWR SURFACE CLUSTER OF DENTS BEHIND NR 1 TIRE PREPARED AREA OF DENT DAMAGE. FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.Jan 10, 2008 · N773AS · Boeing 7374Q8SDR ASAA0842527Skin · dentedLT OUTBOARD T/E FLAP LWR SURFACE CLUSTER OF DENTS 2 INCHES TO 22 INCHES FROM INBOARD END AND 1 2" TO 8" FROM T/E. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, PREPARED AREA AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.Jan 10, 2008 · N773AS · Boeing 7374Q8SDR ASAA0842526Skin · dentedLT OUTBOARD AFT T/E FLAP DENTED ON UPPER SURFACE 68" FROM OUTBOARD B AND 1.5 INCH FROM T/E REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER PREPARED AREA AND BONDED IAW B737 400 51 70 10 REPAIR 2.Jan 10, 2008 · N773AS · Boeing 7374Q8SDR ASAA0842524Skin · dentedLT INBOARD AFT FORE FLAP LWR SURFACE CLUSTER OF DENTS BEHIND NR 2 TIRE. PREPARED DAMAGED AREA, FABRICATED EXTERAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.Jan 10, 2008 · N773AS · Boeing 7374Q8SDR ASAA0842523Skin · dentedLT INBOARD AFT FORE FLAP DENTED 11" FROM O B AND 3" FROM T/E ON UPPER SURFACE PREPARED DAMAGED AREA. FABRICATED EXTERNAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.Jan 10, 2008 · N773AS · Boeing 7374Q8SDR USAA920080228Flap · debondedMCN - MAJOR REPAIR - C-18 CHECK - LEFT WING OUTBOARD AFT FLAP HAS 2 AREA OF DISBOND, WBL 232 - WBL 241 AND WBL 247 - WBL 250. REPAIRED LEFT WING OUTBOARD AFT FLAP, WBL 232 - WBL 241 AND WBL 247 - WBL 250 IAW B737 SRM 51-70-10-2R4.Jan 10, 2008 · N334AW · Boeing 7373Y0SDR UIEA200800012Skin · delaminatedRIGHT INBOARD TRAILING EDGE MID FLAP (UPPER SURFACE) HAS EVIDENCE OF DISBONDING AROUND AN AREA OF 4 INCHES DIAMETER AT APPROX WBL 235 AND 29 INCHES FWD OF MID FLAP TRAILING EDGE. REPAIRED AREA IAW SRM 51-70-10 AND EO NUMBER 4457A116.Jan 10, 2008 · N497MC · Boeing 74747UFSDR UIEA200800013Skin · dentedRT TE MID FLAP UPPER SURFACE HAS DENT APPROX 1.0 INCHES IN DIAMETER LOCATED 28 INCHES FORWARD OF THE TRAILING EDGE AND 29 INCHES OUTBOARD OF THE CONTACT FACE OF THE ACCORDION SEAL. DENT BLENDED OUT FILLED OUT IN IAW SRM51-70-06 AND EO 4457A116 Jan 10, 2008 · N497MC · Boeing 74747UFSDR UIEA200800009Skin · crackedLT INBD MID FLAP WITH MULTIPLE AREAS OF DAMAGE TO THE INBD L/E FAIRING ADJACENT TO THE CONCERTINA SEAL. THIS DAMAGE COMPRISES OF A HOLE 1.2" BY 0.9", WITH AN ASSOCIATED 8.0" CRACK RUNNING OUTBD. TOTAL SIZE OF DAMAGE IS 9.2" LONG.Jan 10, 2008 · N412 · Boeing 74747UFSDR UIEA200800008Skin · dentedSMALL DENT ON THE LT I/B AFT FLAP LOWER SURFACE I/B OF NR 4 CANOE. DENT 0.250" DIAMETER, PIN HOLE IN CENTER 0.060" IS NOT NEAR AN EDGE IS MIDSPAN AND IS COVERED UNDER ALLOWABLE DAMAGE SRM 57-53-01 PAGE 102, C, D, F.Jan 10, 2008 · N412 · Boeing 74747UFSDR ASAA0842522Skin · dentedRT OUTBOARD AFT FLAP HAS AN AREA OF MULTIPLE DENTS ON UPPER SURFACE. PREPARED DAMAGED AREA, FABRICATED EXTERNAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.Jan 9, 2008 · N773AS · Boeing 7374Q8SDR MALA080007Skin · chafedFLAP PANEL 641AT SKIN BENEATH NR 6 ANTI-CHAFE STRIP HAS AN AREA OF CHAFING/SCRATCHES. COMPLETED REPAIRS IAW EO NR S57172. Jan 9, 2008 · N407XJ · Saab 340BSDR ABXA080043Structure · corrodedRIGHT WING OUTBOARD FLAP HAD CORROSION UNDERNEATH THE OUTBOARD SUPPORT BEAM. REMOVED AND REPLACED RIGHT OUTBOARD FLAP IAW B767 MM 27-51-20-4-10.Jan 8, 2008 · N787AX · Boeing 767281SDR DHL2007873510Doubler · crackedRT INBD FLAP FORMER ANGLE DOUBLER CRACKED 1" AT STA XW 125.000. REMOVED ANGLE DOUBLER IAW SRM 51-1-21. FABRICATED ANGLE DOUBLER 9AL7075T6 0.050") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOJan 8, 2008 · N873SJ · Doug DC873FSDR MALA080009Structure · dentedDENT LOCATED ON RT FLAP ASSY, IB PORTION OF LE, 9 INCH FROM FLAP PANEL AND 5 1/2 INCH FROM IB LE. REPAIRED IAW MAL EO NR S51031.Jan 8, 2008 · N407XJ · Saab 340B
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