# JASC 5744: Wing, Control Surface Attach Fittings

- Type: JASC system/component code (FAA)
- ATA chapter: 57 Wings
- Title in the code table: WING, CONT. SURFACE ATTACH FITTINGS
- Service difficulty reports: 2,713
- FAA code table: https://www.faa.gov/sites/faa.gov/files/JASC_Code.pdf#page=54
- Page: https://openairdocs.org/jasc/5744

## What it covers

The fittings on the wing used for attachment to the control surface.

## Service difficulty reports (2,713, newest 50)

- [SDR IPXA2026100217405](https://openairdocs.org/sdr/IPXA2026100217405), Sep 6, 2026: Airbus A300F4622R. STIFFENER. CRACKED. LH WING, FLAP KRUEGER HAS A CRACK UNDERNEATH TEFLON ROLLER BASE , STIFFENER REMOVED AT LH WING, FLAP KRUEGER UNDERNEATH  (N146UP)
- [SDR IPXA2026100217425](https://openairdocs.org/sdr/IPXA2026100217425), Sep 6, 2026: Airbus A300F4622R. BRACKET. CRACKED. LH WING, FIXED LEADING EDGE, INSIDE FLAP KRUEGER COMPARTMENT I/B SIDE HAS A BRACKET WITH CRACK (DOT 64-018) (N146UP)
- [SDR REXA2026090801779](https://openairdocs.org/sdr/REXA2026090801779), Sep 6, 2026: Cndair CL6002D24. FITTING. DAMAGED. FOUND R/H AILERON SIDE BEARING LUGS LABELED H AND I TO BE OVERSIZED. REPAIRED R/H AILERON LUG LABELED H AND I IAW MHIRJ  (N549CA)
- [SDR REXA2026090401774](https://openairdocs.org/sdr/REXA2026090401774), Aug 20, 2026: Cndair CL6002D24. BUSHING. ABNORMAL. RIGHT AILERON CENTER HINGE FITTING BUSHING LUG MARKED C FOUND TO BE O/S UPON BUSHING REMOVAL. REPAIRED RT AILERON SIDE L (N549CA)
- [SDR DALA2026080404489](https://openairdocs.org/sdr/DALA2026080404489), Aug 3, 2026: Boeing 717200. MOUNT. CORRODED. CORROSION ON FASTENERS HOLES HOLDING (8 EA) ALSO MOUNTING FLANGE (UPPER HOLES) AT RIGHT WING FLAP INNER HINGE. REPAIRED  (N932AT)
- [SDR REXA2026073001348](https://openairdocs.org/sdr/REXA2026073001348), Jul 28, 2026: Cndair CL6002D24. LUG. DAMAGED. FABRICATE OVERSIZE BUSHINGS FOR LUGS R1, R2, R5 & R6. LUG R1 WAS REWORKED AND BUSHINGS OVERSIZE FOR LUGS R2, R5 & R6 WER (N925XJ)
- [SDR DALA2026072804382](https://openairdocs.org/sdr/DALA2026072804382), Jul 28, 2026: Boeing 717200. LUG. GOUGED. GOUGES ON INBD LUG (OUTB FACE) AND WEAR ON OUTBD LUG (INNER FACE) ALSO CORROSION AND SCRATCHES ON BUSHINGS AT LEFT FLAP  (N932AT)
- [SDR DALA2026072804381](https://openairdocs.org/sdr/DALA2026072804381), Jul 28, 2026: Boeing 717200. LUG. WORN. WORN OUTBD LUG INBD FACE AT RIGHT FLAP FWD HINGE FITTING NO. 3. CORRECTIVE ACTION: REPAIRED PER ERA 628285-14. (1724181) (N932AT)
- [SDR UATA2026072835701](https://openairdocs.org/sdr/UATA2026072835701), Jul 23, 2026: Casa C212CC. HINGE FITTING. CORRODED. RT & LT INNER FLAP, OTBD PYLON, OTBD HINGE FITTINGS FOUND CORRODED. APPROXIMATE WS 2900. REMOVED DAMAGED FITTINGS. COPIE (N440RA)
- [SDR DALA2026072304309](https://openairdocs.org/sdr/DALA2026072304309), Jul 23, 2026: Airbus A330223. BRIDGE. CRACKED. RIGHT WING NR 3 FLAP TRACK CARRIAGE ASSY OTBD BRIDGE CRACKED. REPLACED THE RT WING NR 3 FLAP TRACK CARRIAGE ASSY OTBD BR (N859NW)
- [SDR REXA2026072201084](https://openairdocs.org/sdr/REXA2026072201084), Jul 21, 2026: Cndair CL6002D24. LUG. DAMAGED. "DURING THE REMOVAL OF THE RT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG LABELED D (HINGE NR 2 OTBD) WAS PREV (N147PQ)
- [SDR REXA2026072201083](https://openairdocs.org/sdr/REXA2026072201083), Jul 21, 2026: Cndair CL6002D24. LUG. DAMAGED. "DURING THE REMOVAL OF THE RT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG LABELED C (HINGE NR 2 INBD) WAS PREV (N147PQ)
- [SDR REXA2026072201085](https://openairdocs.org/sdr/REXA2026072201085), Jul 20, 2026: Cndair CL6002D24. LUG. DAMAGED. WHILE RPLACING BUSHINGS IN LT AILERON FOUND LUGS MARKED AS B, C, F, AND G TO BE OVERSIZED. COMPLIED WITH BOMBARDIER REO  (N923XJ)
- [SDR REXA2026072201082](https://openairdocs.org/sdr/REXA2026072201082), Jul 20, 2026: Cndair CL6002D24. LUG. DAMAGED. WHILE RPLACING BUSHINGS IN RT AILERON, FOUND LUGS B, C, F, AND G TO BE OVERSIZED. COMPLIED WITH BOMBARDIER REO 670-57-61 (N923XJ)
- [SDR REXA2026073001347](https://openairdocs.org/sdr/REXA2026073001347), Jul 18, 2026: Cndair CL6002D24. LUG. CORRODED. CORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 336.4015 (LUG L1), 337.657 (LUG L2), 342.911 (LUG L5), 344.1665 (LUG (N925XJ)
- [SDR VNAA202609010025](https://openairdocs.org/sdr/VNAA202609010025), Jul 12, 2026: Cndair CL6002D24. HINGE FITTING. CORRODED. AFTER BUSHING REMOVAL CORROSION WAS FOUND ON CENTER HINGE FITTING L2 AND L6 IN REF TASK CARD TRFKE00GM97B. LUG BORE L2 W (N642NN)
- [SDR VNAA202609010024](https://openairdocs.org/sdr/VNAA202609010024), Jul 12, 2026: Cndair CL6002D24. HINGE FITTING. CORRODED. AFTER BUSHING REMOVAL CORROSION WAS FOUND ON CENTER HINGE FITTING R2 AND R5 IN REF TASK CARD TRFKE00GM9V5. LUG BORES R2  (N642NN)
- [SDR JR2R20260711966](https://openairdocs.org/sdr/JR2R20260711966), Jul 11, 2026: Emb ERJ170200LL. BUSHING. WORN. LEFT NR 3 SLAT STOP SPINS IN HOLE ON ADJUSTMENT. REPLACED THE BUSHING. (N86324)
- [SDR REXA2026072301088](https://openairdocs.org/sdr/REXA2026072301088), Jul 6, 2026: Cndair CL6002D24. LUG. DAMAGED. RH AILERON HAS 1 #9 BEARING LUG MARKED E FOUND TO BE OVER SIZED UPON BEARING REMOVAL. COMPLIED WITH STEPS 1 THRU 3 OF MH (N147PQ)
- [SDR REXA2026072301087](https://openairdocs.org/sdr/REXA2026072301087), Jul 6, 2026: Cndair CL6002D24. LUG. DAMAGED. LH AILERON BEARING LUG MARKED E FOUND TO BE OVERSIZED UPON REMOVAL OF BEARING. RECEIVED MHIRJ REO 690-57-61-534 REV -- D (N147PQ)
- [SDR REXA2026063000994](https://openairdocs.org/sdr/REXA2026063000994), Jun 29, 2026: Cndair CL6002D24. FITTING. DAMAGED. UPON REMOVAL OF THE RT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG LABELED -F- (HINGE NR 3 OTBD) HAS DAMAGE IN (N153PQ)
- [SDR SWIA2026062876822](https://openairdocs.org/sdr/SWIA2026062876822), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. LEFT SLAT TRACK 1-1 GROOVED. REPLACED WITH A NEW SERVICEABLE LT 1-1 DRIVEN SLAT TRACK IAW AMM 27-81-41-400-801-A01. OPS  (N719SK)
- [SDR SWIA2026062876816](https://openairdocs.org/sdr/SWIA2026062876816), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. RIGHT SLAT TRACK 3-3 GROOVED. COMPLIED WITH REO 670-57-42-2549 REV - FOR RT SLAT TRACK 3-3. COMPLIED WITH TASK CARD 51-9 (N719SK)
- [SDR SWIA2026062876810](https://openairdocs.org/sdr/SWIA2026062876810), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. RIGHT SLAT TRACK 1-3 GROOVED. REPAIRED THE RT SLAT TRACK 1-3. IAW SRM 51-12-00-001-001-A01, AND COMPLIED WITH REO 670-57 (N719SK)
- [SDR SWIA2026062876805](https://openairdocs.org/sdr/SWIA2026062876805), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. CORRODED. RIGHT SLAT TRACK 1-2 CORRODED. REPAIRED THE RT SLAT TRACK 1-2 IAW SRM 51-21-06-001-001-A01, AND COMPLIED WITH REO 670-57 (N719SK)
- [SDR SWIA2026062876803](https://openairdocs.org/sdr/SWIA2026062876803), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. CORRODED. RIGHT SLAT TRACK 3-2 CORRODED. COMPLIED WITH REO 670-57-42-2550 REV- FOR RT SLAT TRACK 3-2. COMPLIED WITH TASK CARD 51-9 (N719SK)
- [SDR SWIA2026062876802](https://openairdocs.org/sdr/SWIA2026062876802), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. LEFT SLAT TRACK 2-1, GROOVED AND CORRODED. REPAIRED LT SLAT TRACK 2-1 IAW SRM 51-21-06-001-001-A01, & SRM 51-12-00-001-0 (N719SK)
- [SDR SWIA2026062876801](https://openairdocs.org/sdr/SWIA2026062876801), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. RIGHT SLAT TRACK 2-1 GROOVED. REPAIRED THE RT SLAT TRACK 2-1. IAW SRM 21-12-00-001-001-A01, AND COMPLIED WITH REO 670-57 (N719SK)
- [SDR SWIA2026062876797](https://openairdocs.org/sdr/SWIA2026062876797), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. LEFT SLAT TRACK 3-3 GROOVED AND CORRODED. REPAIRED RT SLAT TRACK 3-3 IAW SRM 51-21-06-001-001-A01, SRM 51-12-00-001-001- (N719SK)
- [SDR SWIA2026062876796](https://openairdocs.org/sdr/SWIA2026062876796), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. RIGHT SLAT TRACK 3-1 GROOVED. COMPLIED WITH REO 670-57-42-2535, REV- FOR RT SLAT TRACK 3-1,COMPLIED WITH TASK CARD 51-90 (N719SK)
- [SDR SWIA2026062876795](https://openairdocs.org/sdr/SWIA2026062876795), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. CORRODED. LEFT SLAT TRACK 2-2 CORRODED. REPAIRED LT SLAT TRACK 2-2 IAW REO 670-57-42-2547, REV -A. AND SRM 51-21-06-001-001-A01. C (N719SK)
- [SDR SWIA2026062876793](https://openairdocs.org/sdr/SWIA2026062876793), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. CORRODED. LEFT SLAT TRACK 3-2 CORRODED. REPAIRED LT SLAT TRACK 3-2. IAW SRM 51-21-06-001-001-A01, AND COMPLIED WITH REO 670-57-42- (N719SK)
- [SDR SWIA2026062876784](https://openairdocs.org/sdr/SWIA2026062876784), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. CORRODED. LH SLAT TRACK 3-1 CORRODED. REPAIRED LT SLAT TRACK 3-1. IAW SRM 51-21-06-001-001-A01, AND COMPLIED WITH REO 670-57-42-25 (N719SK)
- [SDR SWIA2026062876782](https://openairdocs.org/sdr/SWIA2026062876782), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. LEFT SLAT TRACK 2-3 GROOVED. REPAIRED LT SLAT TRACK 2-3 IAW SRM 51-12-00-001-001-A01, AND COMPLIED WITH REO 670-57-42-25 (N719SK)
- [SDR SWIA2026062876780](https://openairdocs.org/sdr/SWIA2026062876780), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. RIGHT SLAT TRACK 2-3 GROOVED. REPAIRED THE RT SLAT TRACK 2-3. IAW SRM 51-12-00-001-001-A01, & COMPLIED WITH REO 670-57-4 (N719SK)
- [SDR SWIA2026062876777](https://openairdocs.org/sdr/SWIA2026062876777), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. CORRODED. LEFT SLAT TRACK 1-3 CORRODED AND GROOVED. REPAIRED LT SLAT TRACK 1-3 IAW SRM 51-21-06-001-001-A01 AND SRM 51-12-00-001-0 (N719SK)
- [SDR SWIA2026062876775](https://openairdocs.org/sdr/SWIA2026062876775), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. GROOVED. RIGHT SLAT TRACK 1-1 GROOVED. REPAIRED THE RT SLAT TRACK 1-1. IAW SRM 51-12-00-001-001-A01, AND COMPLIED WITH REO 670-57 (N719SK)
- [SDR SWIA2026062876774](https://openairdocs.org/sdr/SWIA2026062876774), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. CORRODED. RIGHT SLAT TRACK 2-2 CORRODED. REPAIRED THE RT SLAT TRACK 2-2 IAW SRM 51-21-06-001-001-A01, AND COMPLIED WITH REO 670-57 (N719SK)
- [SDR SWIA2026062876764](https://openairdocs.org/sdr/SWIA2026062876764), Jun 28, 2026: Cndair CL6002C10. SLAT TRACK. CORRODED. LEFT SLAT TRACK 1-2 CORRODED. REPAIRED THE LT SLAT TRACK 1-2 IAW SRM 51-21-06-001-001-A01, AND COMPLIED WITH REO 670-57- (N719SK)
- [SDR SWIA2026062776352](https://openairdocs.org/sdr/SWIA2026062776352), Jun 27, 2026: Cndair CL6002B19. HINGE BOX. GOUGED. LEFT FLAP HINGE BOX (WS178.00), AFT INBOARD LOWER FLANGE GOUGED (NEAR LUG HOLE). BLENDED LH FLAP HINGE BOX (WS178.00), A (N971SW)
- [SDR ECPR20260624003](https://openairdocs.org/sdr/ECPR20260624003), Jun 24, 2026: Piper PA28161. BRACKET. CORRODED. THE LEFT WING CENTER FLAP HINGE BRACKET WAS FOUND WITH CORROSION PITTINING THAT WAS BEYOND REWORK LIMITS NECESSITATINING (N551PU)
- [SDR ECPR20260624002](https://openairdocs.org/sdr/ECPR20260624002), Jun 24, 2026: Piper PA28161. BRACKET. CORRODED. THE LEFT WING CENTER FLAP HINGE BRACKET WAS FOUND WITH CORROSION PITTINING THAT WAS BEYOND REWORK LIMITS NECESSITATINING (N553PU)
- [SDR AALA202608066999](https://openairdocs.org/sdr/AALA202608066999), Jun 23, 2026: Airbus A319115. BEARING. EXCESS PLAY. AIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTNG BEARING HAS EXCESSIVE PLAY - R (N9017P)
- [SDR VNAA202608010022](https://openairdocs.org/sdr/VNAA202608010022), Jun 9, 2026: Cndair CL6002D24. LUG. CORRODED. CORROSION ON LUG L2 OF CENTER FITTING HINGUE ASSY WAS FOUND IN REF TRFKE00GEUWB. LUG L2 WAS REPAIRED PER REO: 670-57-61- (N644NN)
- [SDR CALA2026052716556](https://openairdocs.org/sdr/CALA2026052716556), May 24, 2026: Boeing 737824. FITTING. GOUGED. LEFT WING, O/B MAIN FLAP #1 FLAP TRACK FITTING IS GOUGED. REMOVED AND REPLACED LH O/B FLAP TRACK #1 FITTING IAW B737 AMM (N37255)
- [SDR VNAA202607010016](https://openairdocs.org/sdr/VNAA202607010016), May 22, 2026: Cndair CL6002C10. HINGE. EXCESS PLAY. AFTER REMOVAL, FREE PLAY WAS FOUND ON HINGES OF STUB FAIRINGS 171DL AND 172DR. HINGES OF STUB FAIRINGS 171DL AND 172DR W (N530EA)
- [SDR VNAA202607010015](https://openairdocs.org/sdr/VNAA202607010015), May 22, 2026: Cndair CL6002C10. LUG. CORRODED. CORROSION AND WEAR ON RH AILERON BORE LUGS OF HINGES: HINGE 1=[AIL STA=311.539] R1=[AIL STA=336.4015], R2=[AIL STA=337.6 (N530EA)
- [SDR VNAA202608010021](https://openairdocs.org/sdr/VNAA202608010021), May 21, 2026: Cndair CL6002D24. LUG. CORRODED. CORROSION ON LUG R6 OF CENTER FITTING HINGUE ASSY WAS FOUND IN REF TRFKE00GEV2Y. LUG R6 WAS REPAIRED PER REO: 670-57-61- (N644NN)
- [SDR VNAA202608010014](https://openairdocs.org/sdr/VNAA202608010014), May 21, 2026: Cndair CL6002D24. HINGE FITTING. CORRODED. CORROSION ON LH/RH AILERON HINGE FITTING NO.2 AND NO.3. ON SEATLMENT AREA OF BONDING JUMPER (4EAS). LH/RH AILERON HINGE  (N644NN)
- [SDR AALA202605266449](https://openairdocs.org/sdr/AALA202605266449), May 20, 2026: Boeing 737823. BRACKET. CORRODED. AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WING SLAT 7 OUTBOARD ALTERNATE TRACK TORSION ROD ATTACH BRACKET LO (N801NN)

All 2,713: https://openairdocs.org/jasc/5744/reports.md

## Other codes in chapter 57

- [JASC 5700](https://openairdocs.org/jasc/5700): Wing Structure (2,401 reports)
- [JASC 5710](https://openairdocs.org/jasc/5710): Wing Main, Frame Structure (4,449 reports)
- [JASC 5711](https://openairdocs.org/jasc/5711): Wing Spar (5,579 reports)
- [JASC 5712](https://openairdocs.org/jasc/5712): Wing, Rib/Bulkhead (6,954 reports)
- [JASC 5713](https://openairdocs.org/jasc/5713): Wing, Longeron/Stringer (2,086 reports)
- [JASC 5714](https://openairdocs.org/jasc/5714): Wing, Center Box (1,451 reports)
- [JASC 5720](https://openairdocs.org/jasc/5720): Wing Miscellaneous Structure (13,614 reports)
- [JASC 5730](https://openairdocs.org/jasc/5730): Wing, Plate/Skin (27,210 reports)
- [JASC 5740](https://openairdocs.org/jasc/5740): Wing, Attach Fittings (3,003 reports)
- [JASC 5741](https://openairdocs.org/jasc/5741): Wing, Fuselage Attach Fittings (544 reports)
- [JASC 5742](https://openairdocs.org/jasc/5742): Wing, Nacelle/Pylon Attach Fittings (258 reports)
- [JASC 5743](https://openairdocs.org/jasc/5743): Wing, Landing Gear Attach Fittings (3,097 reports)
- [JASC 5750](https://openairdocs.org/jasc/5750): Wing, Control Surfaces (1,157 reports)
- [JASC 5751](https://openairdocs.org/jasc/5751): Ailerons (5,077 reports)
- [JASC 5752](https://openairdocs.org/jasc/5752): Aileron Tabs (654 reports)
- [JASC 5753](https://openairdocs.org/jasc/5753): Trailing Edge Flaps (31,481 reports)
- [JASC 5754](https://openairdocs.org/jasc/5754): Leading Edge Devices (17,330 reports)
- [JASC 5755](https://openairdocs.org/jasc/5755): Spoilers (4,549 reports)
- [JASC 5797](https://openairdocs.org/jasc/5797): Wing System Wiring (81 reports)

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