JASC 5744

Service difficulty reports · 2,731

Reports filed under 5744 · Wing, Control Surface Attach Fittings, 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 = '5744'
  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 05FDEA02868Attach Fitting · corrodedRIGHT WING - O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87638.Sep 14, 2005 · N574FE · Doug MD11SDR IXAA05RNG058SFitting · crackedDURING MAINTENANCE CHECK, FOUND RT OUTBOARD FLAP, INBOARD FLAP HINGE FITTING STA XF 219.459 CRACKED. DAMAGE WILL BE REPAIRED IAW EWO ATI-57-041 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.Sep 8, 2005 · N721CX · Doug DC872SDR 05FDEA02818Hinge · corrodedLT WING, I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87635.Sep 8, 2005 · N574FE · Doug MD11SDR 05FDEA02816Hinge · corrodedRT WING, I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87636.Sep 8, 2005 · N574FE · Doug MD11SDR 05FDEA02815Hinge · corrodedRT WING, I/B FLAP O/B HINGE (WING SIDE), PIVOT BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87636.Sep 8, 2005 · N574FE · Doug MD11SDR 05FDEA02133Gusset · crackedLT WING BELOW NR 5 SPOILER INBD ATTACH POINT HAS A GUSSET CRACKED.Jul 28, 2005 · N670FE · Airbus A300F4605RSDR SWIA200515378Bolt · corrodedLT OB FLAP OB ACTUATOR HINGE TRUNNION BLOCK BOLT CORRODED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED BOLT IAW AMM 27-54-05-400-801.Jul 19, 2005 · N406SW · Cndair CL6002B19SDR 05FDEA01975Hinge · corrodedRT WING, O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED.Jul 17, 2005 · N575FE · Doug MD11SDR 05FDEA01974Hinge · corrodedRT WING-O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG 602-607. REPAIR CARRIED OUT AS PER CMM 57-44-08.Jul 17, 2005 · N575FE · Doug MD11SDR 05FDEA01973Hinge · corrodedRT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87610. (CLOSED)Jul 17, 2005 · N575FE · Doug MD11SDR 05FDEA01940Hinge · corrodedRT WING, O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED IAW CMM 57-44-09 PG 402-407.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01939Hinge · corrodedRT WING , O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT BARREL NUT BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87608.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01938Hinge · corrodedRT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE, FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG 402-407. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87608.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01937Hinge · corrodedRT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG 402-407. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87609.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01908Hinge · corrodedLT WING-O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PG 612-615.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01907Hinge · corrodedLT WING-O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 1-5750-87605.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01906Hinge · corrodedLT WING-O/B FLAP I/B HINGE (WING SIDE), FWD ATTACHMENT O/B BORE FOUND CORRODED. REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. FABRICATED BUSHING AND INSTALLED IAW EA 1-5750-87605.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01905Hinge · corrodedLT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87605.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01904Hinge · corrodedLEFT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. REPAIR CARRIED OUT AS PER EA 1-5750-87605.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01903Hinge · corrodedLT WING-O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 PG 602-607. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87605.Jul 13, 2005 · N575FE · Doug MD11SDR 05FDEA01594Support Fitting · corrodedCOMPLY WITH EA 8-5750-55487, WINGS - FLAP VANE SUPPORT CORROSION REWORK (RIGHT OUTBOARD FLAP). COMPLIED WITH EA 8-5750-55487.Jun 13, 2005 · N391FE · Doug MD1010FSDR PIDA200500015Support Angle · crackedNUMBER 5 SPOILER O/B HINGE I/B SUPPORT ANGLE CRACKED. REPLACED SUPPORT ANGLE PER SRM 51-10-2.Apr 19, 2005 · N374PA · Boeing 73736MSDR PIDA200500014Support Angle · crackedNUMBER 5 SPOILER I/B ATTACH BRACKET SUPPORT ANGLES CRACKED. REPLACED ANGLES PER SRM 51-10-2.Apr 19, 2005 · N374PA · Boeing 73736MSDR UPS05M44418Bracket · corrodedINSPECTION TYPE:1C DURING REMOVAL OF LT OUTBOARD FLAP ACTUATOR AIRCRAFT SIDE MOUNT HOLES PITTED & LITE CORROSION. REPAIRED MOUNT HOLES IAW CMM 57-44-09, CMM 57-52-04, MM 27-52-02, SAA SK 253-637 & FAA FORM 8100-9 DATED 25 APR 2005.Apr 13, 2005 · N253UP · Doug MD11FSDR C1HA200595003Angle · crackedLEFT WING LOWER ANGLE CRACKED AT STA WS 124 BELOW NR 7 SPOILER SUPPORT FITTING. REMOVED 2 EA AFT ATTACH BOLTS FROM I/B FLAP TRACK, REMOVED TRACKED LOWER ANGLE CHORD AND 2 EA REPAIR ANGLES IAW B727 SRM 51-30-2. CLEANED REPAIR ANGLES IAW B727 M/M 12-90-00, FABApr 8, 2005 · N295AS · Boeing 727290SDR USAA050538Support Angle · crackedBFM - FOUND SUPPORT ANGLE CRACKED 4 INCHES, LT WING TE NR 3 (INBOARD TO OUTBOARD) HINGE WS 573.872 WBL, 415.93. REMOVED, FABRICATED NEW, INSTALLED NEW SUPPORT ANGLE PER SRM 57-51-02, 51-40-05, 51-40-02. (M)Apr 7, 2005 · N374US · Boeing 7373B7SDR DHL2005783505Support · crackedNR 6 LEADING EDGE FLAP ACTUATOR SUPPORT IS CRACKED AT INBD LWR CORNER WING STA 304. REMOVED NR 6 L/E FLAP ACT I/B SUPPORT IAW 727 SRM 51-30-2. FABBED NEW FROM 7075 T6 .063 PO NR 9001660 DIM 7 1/2 INCH BY 3 !/2 INCH IAW 727 SRM 57-10-25 FIG 3. SUPPORT TREATEApr 3, 2005 · N783DH · Boeing 727227SDR UPS05844298Fitting · crackedINSPECTION TYPE:C2 RIGHT FLAP STA 3 SUPPORT FITTING HAS APPROX 6.125 INCH CRACK ON BOTTOM OF FITTING. REMOVED AND REPLACED RIGHT FLAP STA 3 SUPPORT FITTING IAW DC-8 SRM 51-3-0, 51-1-21, AND 51-1-20D.Mar 21, 2005 · N819UP · Doug DC873FSDR SA05005Fairing · missingDCA - DURING OVERNIGHT SERVICE WALK AROUND INSPECTION, MAINTENANCE FOUND THE LEFT WING FLAP TRACK 3A FAIRING ASSEMBLY MISSING THE FORWARD FAIRING AND DAMAGE TO THE AFT FAIRING. MAINTENANCE REMOVED THE AFT FAIRING. ENGINEERING AUTHORIZATION WAS OBTAINED TO OPJan 4, 2005 · N188US · Airbus A321211SDR 04FDEA03403Hinge · corrodedRIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-07 PAGES 403 TO 404.Dec 9, 2004 · N577FE · Doug MD11SDR 04FDEA03400Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), STOP BOLT ATTACHMENT, BARREL NUT BORE FOUND CORRODED. CORROSION REMOVED BY HAND-CLEAN AS PER CMM 20-11- 01.Dec 9, 2004 · N577FE · Doug MD11SDR 04FDEA03321Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. REPAIRED AS PER FEDEX EA 1-5750-77984.Dec 2, 2004 · N577FE · Doug MD11SDR 04FDEA03320Hinge · corrodedOUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09.Dec 2, 2004 · N577FE · Doug MD11SDR 04FDEA03319Hinge · corrodedLEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407,Dec 2, 2004 · N577FE · Doug MD11SDR 04FDEA03303Hinge · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03302Hinge · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03300Hinge · corrodedLT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PAGES 402-407, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.229, MAXIMUM ALLOWABLE DIAMETER=1.1Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03299Hinge · corrodedLEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 PAGES 402-407, ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.232, MAXIMUM ALLOWABLE DIAMETERDec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03298Hinge · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03297Hinge · corrodedRT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03296Hinge · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77986.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03295Hinge · corrodedRT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-77986.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03294Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER EA 1-5750-78056.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03293Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. BORE CORROSION REMOVED AND FOUND EXCEEDED LIMITS AS PER CMM 57-44-09. REPAIRED AS PER EA 1-5750-78056.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03292Hinge · corrodedRIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 PAGES 402-407.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03291Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09, PAGES 402-407.Dec 1, 2004 · N577FE · Doug MD11SDR 04FDEA03290Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), LOWER ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09, PAGES 402-407.Nov 30, 2004 · N577FE · Doug MD11SDR 04FDEA03163Attach Fitting · damagedLT WING FIXED TRAILING EDGE O/B AILERON O/B ATTACH FITTING.Nov 18, 2004 · N166FE · Boeing 727100SDR 04FDEA03062Hinge Fitting · corrodedCORROSION ON RT WING O/B AILERON I/B CTR FITTING A/C SIDE IS CORRODED ON LOWER SURFACE. REPAIRED PER MM 27-10-031-2, SRM 51-30-2, 51-30-5.Nov 9, 2004 · N166FE · Boeing 72722SDR IXXA0500087SHinge · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND LT OB FLAP HINGE CRACKED AT STATION XC 337.000. MAJOR REPAIR ACCOMPLISHED. REMOVED CRACKED SUPPORT FITTING IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SUPPORT FITTING IAW SRM 51-1-Nov 8, 2004 · N602AL · Doug DC873F
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