# SDR SWAA2022081518695

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 14, 2022
- Submitted: August 15, 2022
- Operation: Air carrier
- Aircraft: [N951WN](https://openairdocs.org/aircraft/N951WN), registered now
- Make and model: Boeing 737-7H4
- Registry model: [Boeing 737-7H4](https://openairdocs.org/model/boeing-737-7h4) (OpenAirDocs)
- Aircraft serial: 36665
- Aircraft time: 39,132 hours, 23,683 cycles
- System (JASC): [5754 · Leading Edge Devices](https://openairdocs.org/jasc/5754)
- Part: Slat
- Condition: Cracked
- Location: R/H Wing
- Stage of operation: IN
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/SWAA2022081518695

## Discrepancy

#6 SLAT CRACKED AT L/E NOSE SKIN AT ACTUATOR RIB (MARKED) / [01] REQUEST NDI VERIFICATION CRACK CONDITION EXIST.[08] FABRICATED REPAIR DOUBLER FROM 7075T6; 0.071'; LOT #1478276-1. REPAIR FILLER FROM 7075T6; 0.063'; LOT#1461523-1. DRILLED  COUNTERSUNK AND CHAMFERED REPAIR PARTS AS REQUIRED. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS AND BARE AREAS AND CUTOUT EDGES OF SLAT REPAIR AREA IAW SRM 57-42-01-2R-8 PARA.4.F.[12] INSTALLED REPAIR PARTS ON #6 SLAT SKIN IAW SRM 57-42-01-2R-8 PARA. 4. F. AND FIG.202. OK TO INSTALL COVE PANELS 623CB;623DB;623EB.;[13] VERIFIED CORRECTIVE ACTION ITEM 12.<BR>OK TO INSTALL COVE PANELS 623CB;623DB;623EB GIVEN.;[14] INSTALLED 623CB;623DB AND 623EB. INSTALLED SLAT FLEX SKIN AND AERODYNAMIC FILLET SEAL. WORK DONE IAW SRM 57-42-01-2R-8 PARA. 4. AND FIG. 202.;

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