# Service difficulty reports: JASC 5740

A list on [JASC 5740](https://openairdocs.org/jasc/5740.md).

Reports filed under 5740 · Wing, Attach Fittings, newest first.

Page 1 of 61 · 3,003 reports

- [SDR FDEA202609231416](https://openairdocs.org/sdr/FDEA202609231416.md): Attach Fitting · cracked · Sep 23, 2026 · N595FE · Doug MD11F
  > LEFT WING- LEADING EDGE COMPARTMENT ATTACH FORMER XOS 939 FOUND CRACK ABOUT 0.6 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED FORMER AT XOS 939 REMOVED IAW SRM 51-33-01-0G AND MD-11 SRM 51-35-01-06. FABRICATED FORMER PER DRAWING ARB 1292 REVISION
- [SDR HYIA20260923002](https://openairdocs.org/sdr/HYIA20260923002.md): Fitting · corroded · Sep 21, 2026 · N3249M · Cessna 402C
  > DURING SCHEDULED WING FITTING INSPECTION, A SMALL AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND FORWARD UPPER WING ATTACH FITTING. THIS CORROSION MEASURES APPROXIMATELY.500 INCHES LONG,.125 INCHES WIDE, AND.020 INCHES DEEP ON THE TOP FACE OF TH
- [SDR IPXA2026092172110](https://openairdocs.org/sdr/IPXA2026092172110.md): Bracket · cracked · Sep 16, 2026 · N355UP · Boeing 76734AF
  > CRACKED BRACKET, LT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY AT ISS 285.233. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.
- [SDR SWAA2026101693391](https://openairdocs.org/sdr/SWAA2026101693391.md): Nut Plate · corroded · Sep 9, 2026 · N8656B · Boeing 7378H4
  > CORROSION RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE OFSS 449 LT WING. REPLACED THE RAIL NUT PLATES IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 40, REV A.
- [SDR SWAA2026090760777](https://openairdocs.org/sdr/SWAA2026090760777.md): Attach Angle · cracked · Sep 2, 2026 · N284WN · Boeing 7377H4
  > RIGHT WING UPPER SHELF PANEL, ATTACH ANGLE CRACKED INBD AND ABOVE NR 2 AFT BOOST PUMP. REMOVED & REPLACED THE ATTACH ANGLE IAW SRM 51-40-02.
- [SDR DALA2026082604845](https://openairdocs.org/sdr/DALA2026082604845.md): Bushing · migrated · Aug 26, 2026 · N803NW · Airbus A330323
  > LEFT RIB 6 FITTING FWD LUG ECCENTRIC PIN BUSHING MIGRATED. CORRECTED IAW ERA 635960-14 REV ORIGINAL. (1777705) AIRCRAFT WAS GROUNDED.
- [SDR SWAA2026092313059](https://openairdocs.org/sdr/SWAA2026092313059.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4
  > CRACKED NUT PLATE, OFSS 604, INTERNAL CAVITY LEADING EDGE, RT WING. REPLACED THE NUT PLATE BTWN OSS 362.51 - 384.24. IAW SRM 51-40-02, & DWG 112A4402, SHEET 14, REV-.
- [SDR SWAA2026092106314](https://openairdocs.org/sdr/SWAA2026092106314.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4
  > CRACKED NUT PLATE, OFSS 404, INTERNAL CAVITY L/E OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.
- [SDR SWAA2026092127237](https://openairdocs.org/sdr/SWAA2026092127237.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4
  > CRACKED RAIL NUT PLATE LOC OFSS 570, INTERNAL CAVITY LEADING EDGE OF RT WING. REMOVED THE NUT PLATE IAW SRM 51-40-01 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREAS AND DID NOT FIND OTHER DAMAGE. REPLACED THE NUT PLATE IAW SRM 51-40-01, SRM 51-40-02, SRM
- [SDR SWAA2026092130117](https://openairdocs.org/sdr/SWAA2026092130117.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4
  > CRACKED RAIL NUT PLATE, OFSS 491 INTERNAL CAVITY LEADING EDGE IN THE RT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.
- [SDR SWAA2026092127663](https://openairdocs.org/sdr/SWAA2026092127663.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4
  > CRACKED RAIL NUT PLATE, OFSS 588 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02-0G-0, & DWG 112A4402, SHEET 13, REV-.
- [SDR SWAA2026092109501](https://openairdocs.org/sdr/SWAA2026092109501.md): Nut Plate · cracked · Aug 17, 2026 · N259WN · Boeing 7377H4
  > CRACK RAIL NUT PLATE LOC OFSS 449 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG:112A4402, SHEET 40, REV A.
- [SDR SWAA2026081997521](https://openairdocs.org/sdr/SWAA2026081997521.md): Attach Bracket · cracked · Aug 15, 2026 · N7748A · Boeing 7377BD
  > RIGHT WING INBD FIXED T/E PANEL SUPPORT BEAM, FWD ATTACH BRACKET CRACKED. REMOVED AND REPLACED RT WING INBD FIXED T/E PANEL SUPPORT BEAM FWD ATTACH BRACKET IAW SRM 51-40-02.
- [SDR HYIA20260731001](https://openairdocs.org/sdr/HYIA20260731001.md): Fitting · cracked · Jul 28, 2026 · N375R · Cessna 402C
  > DURING SCHEDULED WING FITTING INSPECTION 2 CRACKS WERE VISUALLY IDENTIFIED IN THE LOWER RADIUS OF THE RIGHT SIDE LOWER AFT WING ATTACH FITTING (OEM: 0822550-44). THE INBOARD CRACK MEASURES APPROXIMATELY 2.750 INCHES LONG AND THE OUTBOARD CRACK MEASURES APPROXI
- [SDR SWAA2026080334290](https://openairdocs.org/sdr/SWAA2026080334290.md): Attach Angle · cracked · Jul 17, 2026 · N8545V · Boeing 7378H4
  > LEFT WING TRAILING EDGE OTBD ATTACH ANGLE AT TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE OTBD ATTACH ANGLE AT TRANSVERSE WEB ABOVE NR 1 AFT PYLON TIP IAW SRM 51-40-02 AND AIPC 57-42-51-03.
- [SDR CALA2026071317731](https://openairdocs.org/sdr/CALA2026071317731.md): Bracket · cracked · Jul 12, 2026 · N87507 · Boeing 737824
  > RIGHT WING ABOVE 651GB,FIXTURE PANEL HAS BRACKET CRACKED THAT ATTACHES TO FLAP DEFLECTION FITTING. REMOVED AND REPLACED RH WING,FIXTURE PANEL BRACKET IAW B737 SRM 51-40-02 AND BAC DWG# 115A6200 REV:B DOT REMOVED.
- [SDR HNAA2026082400747](https://openairdocs.org/sdr/HNAA2026082400747.md): Attach Fitting · chafed · Jul 11, 2026 · N935AE · Emb EMB145LR
  > F138484 LT WING NR 1 LEADING EDGE INTERNAL INBD ATTACHMENT FLANGE IS CHAFED. REMOVED DAMAGE FROM LT WING NR 1 LEADING EDGE INTERNAL INBD ATTACHMENT FLANGE (LOWER SURFACE) IAW SRM 51-10-03. FOUND TO BE WITHIN ALLOWABLE LIMITS IAW ETD 2026-145-013669 REV: A, A
- [SDR IPXA2026081116351](https://openairdocs.org/sdr/IPXA2026081116351.md): Bracket · cracked · Jul 5, 2026 · N144UP · Airbus A300F4622R
  > LEFT WING, BRACKET WITH CRACK AT FIXED LEADING EDGE (INTERNAL STRUCTURE) INSIDE THE FLAP KRUEGER COMPARTMENT. INSTALLED NEW ANGLE ON WING INBOARD SECTION, LOWER SURFACES IAW SRM 51-40-21.
- [SDR SWAA2026072764870](https://openairdocs.org/sdr/SWAA2026072764870.md): Attach Angle · cracked · Jul 2, 2026 · N486WN · Boeing 7377H4
  > LEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE #1 PYLON AFT TIP O/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE TRANSVERSE WEB ABOVE #1 PYLON AFT TIP O/B ATTACH ANGLE IAW SRM 51-40-02. VERIFIED CORRECTIVE ACTION
- [SDR FXTA20260628001](https://openairdocs.org/sdr/FXTA20260628001.md): Bolt · loose · Jun 28, 2026 · N409BA · Textrn 408
  > FLAP ACTUATOR ATTACHMENT HARDWARE FOUND LOOSE
- [SDR ECPR202606004](https://openairdocs.org/sdr/ECPR202606004.md): Bracket · corroded · Jun 24, 2026 · N4445V · Piper PA28161
  > THE RIGHT WING CENTER FLAP HINGE BRACKET WAS FOUND WITH CORROSION PITTING THAT WAS BEYOND REWORK LIMITS NECESSITATING THE REPLACEMENT OF THE BRACKET. THE ORIGIN OF THE CORROSION WAS THE BONDING WIRE ATTACHMENT POINT.
- [SDR AALA202608075316](https://openairdocs.org/sdr/AALA202608075316.md): Attach Fitting · worn · Jun 23, 2026 · N9017P · Airbus A319115
  > AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD FLAP NTERCONNECTING STRUT ATTACH FITTING WORN - REPLACED ATTACH FITTING PER SRM 51-42-11.
- [SDR ECPR20260624001](https://openairdocs.org/sdr/ECPR20260624001.md): Bracket · corroded · Jun 23, 2026 · N4426 · Piper PA28161
  > THE LEFT WING CENTER FLAP HINGE BRACKET WAS FOUND WITH CORROSION PITTINING THAT WAS BEYOND REWORK LIMITS NECESSITATINING THE REPLACEMENT OF THE BRACKET. THE ORIGIN OF THE CORROSION WAS THE BONDING WIRE ATTACHMENT POINT.
- [SDR SWAA2026072471735](https://openairdocs.org/sdr/SWAA2026072471735.md): Nut Plate · corroded · Jun 20, 2026 · N8650F · Boeing 7378H4
  > CORRODED RAIL NUT PLATE, OFSS 449 RT WING LE. REPLACED RAIL NUT PLATE AND FASTENERS IAW SRM 51-40-02-0G, AND DWG 112A4402, SHEET 40, REV A. CORROSION WAS NOT FOUND ALLOWABLE, DAMAGE IAW SRM.
- [SDR IPXA2026061904932](https://openairdocs.org/sdr/IPXA2026061904932.md): Bracket · cracked · Jun 17, 2026 · N334UP · Boeing 76734AF
  > CRACKED BRACKET, LT WING L/E INBD PANEL 511KB TORQUE TUBE SUPPORT LES 281. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.
- [SDR 2026F00127](https://openairdocs.org/sdr/2026F00127.md): Nut Plate · corroded · Jun 17, 2026 · N576QS · Cessna 560XL
  > LEFT MLG WHEEL WELL HAS 6 NUTPLATES WITH EVIDENCE OF CORROSION LOCATED AROUND 6 NUTPLATES WHERE ACCESS PANEL 512DB ATTACHES. REPAIRED CORRODED PANEL LAND COMMON TO PANEL 512DB PER AQRD RFTS-117476 REV.0 TITLE "N576QS (560-5708) PANEL 512DB NUTPLATE CORROSION";
- [SDR FDEA202606160765](https://openairdocs.org/sdr/FDEA202606160765.md): Not Reported · not reported · Jun 16, 2026 · N934FD · Boeing 75721B
  > WRI 57-40-5108 FACTED IN ERROR. EA: F-5740-T0387288 P1. CREATED WRI 5740-5115 FOR SDR OF WRI 5740-5108 BEING FACTED IN ERROR. REF MAJOR REPAIR E.A. F-5740-T0387288 P1.
- [SDR IPXA2026061548249](https://openairdocs.org/sdr/IPXA2026061548249.md): Bracket · cracked · Jun 13, 2026 · N353UP · Boeing 76734AF
  > CRACKED BRACKET, RT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY, ISS 285.233. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 95 AND DWG NO. 114T1240 SH. 6 REV. -.
- [SDR ABXR2026060400010](https://openairdocs.org/sdr/ABXR2026060400010.md): Angle · cracked · Jun 4, 2026 · N1997A · Boeing 76733A
  > RIGHT WING L/E #9 SLAT AREA INTERNAL ANGLE CRACKED AT LOWER FWD WEB LOWER ANGLE. LES668. FABRICATED NEW ANGLE IAW B767 SRM 57-41-13 REPAIR 1
- [SDR IPXA2026061694292](https://openairdocs.org/sdr/IPXA2026061694292.md): Angle · cracked · Jun 3, 2026 · N161UP · Airbus A300F4622R
  > LEFT WING, FIXED L/E, INBD SIDE, INTERNAL STRUCTURE, JUST NEXT TO KRUEGER FLAP COMPARMENT, ANGLE WITH A CRACK 1/2 LONG. REMOVED ANGLE WITH CRACK IAW SRM 51-40-21. INSTALLED ANGLE IN LT WING, FIXED L/E, INBD SIDE, INTERNAL STRUCTURE IAW SRM 51-40-21.
- [SDR KCSA202606021044](https://openairdocs.org/sdr/KCSA202606021044.md): Attach Fitting · corroded · Jun 2, 2026 · N712CK · Boeing 7474B5F
  > LEFT INBD FOREFLAP INBD CARRIAGE ATTACHMENT FITTING HAS CORROSION.
- [SDR AALA202605286613](https://openairdocs.org/sdr/AALA202605286613.md): Attach Angle · cracked · May 28, 2026 · N973NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE AT STA 663.5 AND LBL 9. REPAIRED ANGLE PER SRM 57-10-10-2R-5.
- [SDR IPXA2026053056047](https://openairdocs.org/sdr/IPXA2026053056047.md): Attach Bracket · cracked · May 26, 2026 · N341UP · Boeing 76734AF
  > CRACK - BRACKET, L/H WING INBOARD L/E COMPARTMENT. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.
- [SDR IPXA2026053056997](https://openairdocs.org/sdr/IPXA2026053056997.md): Attach Bracket · cracked · May 26, 2026 · N341UP · Boeing 76734AF
  > RIGHT WING INBOARD L/E CAVITY, PANEL RIB ATTACH BRACKET CRACK, ISS 285. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.
- [SDR SWAA2026062206215](https://openairdocs.org/sdr/SWAA2026062206215.md): Fitting · cracked · May 24, 2026 · N951WN · Boeing 7377H4
  > CRACKED LOWER SURFACE AROUND FASTENER ON LEFT WING ACTUATOR FITTING SLAT 4. PERFORMED A PERMANENT REPAIR ON THE NOSE SKIN SLAT 4, LT WING IAW SRM 57-42-01-2R-8, REPAIR 8, & SRM 51-40-02.
- [SDR AALA202605222750](https://openairdocs.org/sdr/AALA202605222750.md): Attach Angle · cracked · May 17, 2026 · N801NN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPA VAPOR BARRIER ATTACH ANGLE AT BS 663.5 AND RBL 2. REPLACED ANGLE PER SRM 57-10-10-R2-5.
- [SDR IPXA2026051880648](https://openairdocs.org/sdr/IPXA2026051880648.md): Bracket · cracked · May 14, 2026 · N371UP · Boeing 767300
  > CRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. REMOVED DAMAGED BRACKET IAW SRM 51-40-02-0G, REV.95. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND DWG 114T1240, SH 6, REV-.
- [SDR SWAA2026060103789](https://openairdocs.org/sdr/SWAA2026060103789.md): Fitting · cracked · May 10, 2026 · N477WN · Boeing 7377H4
  > REMOVE AND REPLACE SLAT NR 8 DUE TO CRACKED ACTUATOR FITTING. REPLACED LEADING EDGE SLAT 8 AT RT WING IAW AMM 27-81-21-401. TESTED OK.
- [SDR CALA2026051116126](https://openairdocs.org/sdr/CALA2026051116126.md): Bracket · corroded · May 8, 2026 · N13113 · Boeing 757224
  > LEFT T/H WHEEL WELL PTU BRACKET HAS EXFOLIATION. REMOVED AND REPLACED BRACKET AT LH WHEEL WELL PTU IAW SRM 51-10-02 AND 51-40-02.
- [SDR SWAA2026060195830](https://openairdocs.org/sdr/SWAA2026060195830.md): Fitting · cracked · May 5, 2026 · N477WN · Boeing 7377H4
  > CRACK LOWER SURFACE OF LEADING EDGE SLAT 8 NOSE SKIN AT ACTUATOR LOC. AROUND FASTENER AT RT WING. SLAT 8 HAS BEEN REPLACED BECAUSE THE ACTUATOR FITTING WAS FOUND TO BE CRACKED IN TWO HOLES DURING THE ROTO TEST INSPECTION FOR SLAT REPLACEMENT.
- [SDR SWAA2026051192311](https://openairdocs.org/sdr/SWAA2026051192311.md): Attach Angle · cracked · Apr 23, 2026 · N8534Z · Boeing 7378H4
  > RIGHT WING TRAILING EDGE PANEL 651FB FWD ATTACH 'L' ANGLE CRACKED.<[01] REMOVED AND REPLACED RIGHT WING T/E PANEL 651FB FWD ATTACH 'L' ANGLE PER SRM 51-40-02; AND IPC 57-50-00-38.;[02] VERIFIED
- [SDR 2026F00081](https://openairdocs.org/sdr/2026F00081.md): Nut Plate · corroded · Apr 23, 2026 · N339QS · Cessna 680CE
  > FOUND 6 AREAS OF CORROSION AROUND NUT PLATES FOR PANEL 652DB, MECHANICALLY REMOVED 6 AREAS OF CORROSION WHERE 6 NUTPLATES LOCATED INSIDE RH WING ACCESS BAY 652DB WERE REMOVED IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 68
- [SDR 2026FA0000286](https://openairdocs.org/sdr/2026FA0000286.md): Attach Plate · misaligned · Apr 22, 2026 · N501LL · Cessna 525B
  > 8 EACH HOLES THROUGH THE YAW PLATE/WING ATTACH FITTING WERE NOT DRILLED PERPENDICULAR TO THE CONTOUR OF THE STRUCTURE CREATING A NONSHEAR CONDITION FOR THE FASTENER INSTALLATION. THESE HOLES WERE REQUIRED TO BE OVERSIZED BEYOND SRM LIMITATIONS TO CREATE A SHEA
- [SDR IPXA2026042563692](https://openairdocs.org/sdr/IPXA2026042563692.md): Hinge · worn · Apr 18, 2026 · N332UP · Boeing 76734AF
  > FOUND NR 8 TAI DOOR AFT HINGE WORN OUT. IAW AMM 57-41-58-434-044, ADJUSTED AND PERFORMED A BONDING TEST OF NR 8 TAI DOOR AFTER HINGE,RESULT WAS SATISFACTORY.
- [SDR SWIA2026040976354](https://openairdocs.org/sdr/SWIA2026040976354.md): Fitting · gouged · Apr 9, 2026 · N466SW · Cndair CL6002B19
  > LEFT WING REAR SPAR AT WS162.49 HAS A FITTING GOUGED & DAMAGED. REMOVED, REPLACED, AND INSTALLED FITTING ON LT WING REAR SPAR AT WS 162.49 IAW SRM 57-51-14,51-40-11,51-21-11,51-25-06,51-25-16,51-42-06, & 51-42-20,51-23-00.
- [SDR SWAA2026050587998](https://openairdocs.org/sdr/SWAA2026050587998.md): Attach Angle · cracked · Apr 9, 2026 · N928WN · Boeing 7377H4
  > LEFT WING TRAILING EDGE ATTACH ANGLE FOR OTBD END OF TRANSVERSE WEB CRACKED. REMOVED AND REPLACED LEFT WING TRAILING EDGE ATTACH ANGLE FOR OTBD END OF TRANSVERSE WEB IAW SRM 51-40-02-0G-0.
- [SDR HNAA2026042100321](https://openairdocs.org/sdr/HNAA2026042100321.md): Attach Fitting · gouged · Apr 8, 2026 · N905JH · Emb EMB145LR
  > F111356 LH AILERON DAMPER ATTACHMENT FITTING IS GOUGED 2 EACH. RAR LH AILERON DAMPER ATTACHMENT FITTING IAW EMB 145 SRM 51-40-02
- [SDR IPXA2026041094730](https://openairdocs.org/sdr/IPXA2026041094730.md): Bracket · cracked · Apr 8, 2026 · N352UP · Boeing 76734AF
  > CRACKED TORQUE TUBE SUPPORT BRACKET, RT WING L/E COMPARTMENT ACCESS PANEL 611LB. INSTALL A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & DWG 114T1240, SHT 6, REV -.
- [SDR SWAA2026051187258](https://openairdocs.org/sdr/SWAA2026051187258.md): Attach Angle · cracked · Apr 7, 2026 · N8534Z · Boeing 7378H4
  > HFEC VERIFIED BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED APPROX. RBL 9. REMOVED ALL FASTENERS ON R/H VERTICAL FLANGE IN REPAIR AREA STA 663 RBL 5 TO RBL 16 IAW SRM 57-10-10-2R-5. CUT AND REMOVED DAMAGED SECTION OF RH VAPOR BARRIER ATTACH ANGLE FROM RBL 5 TO
- [SDR CALA2026041415343](https://openairdocs.org/sdr/CALA2026041415343.md): Bracket · cracked · Apr 6, 2026 · N19136 · Boeing 757224
  > RIGHT WING LOWER ATTACH BRACKET HOLE NO.6 AS MARKED ON AIRCRAFT IS CRACKED REMOVED AND REPLACED BRACKET PER APB DWG 757-340 REV B AND B757-200 SRM 51-40-02

Next page: https://openairdocs.org/jasc/5740/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = '5740'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5740/reports

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