# SDR IXXA06SMN077S

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 9, 2006
- Submitted: June 9, 2006
- Operation: Air carrier
- Aircraft: [N602AL](https://openairdocs.org/aircraft/N602AL), registered now
- Make and model: Doug DC-8-73F
- Registry model: [Doug DC-8-73F](https://openairdocs.org/model/douglas-dc-8-73f) (OpenAirDocs)
- Aircraft serial: 45991
- Aircraft time: 97,112 hours, 31,235 cycles
- System (JASC): [5753 · Trailing Edge Flaps](https://openairdocs.org/jasc/5753)
- Part: Structure
- Condition: Dented
- Location: T/E Flap
- Part time: 97,112 hours, 31,235 cycles
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/IXXA06SMN077S

## Discrepancy

DURING ROUTINE C-CHECK INSPECTION, LT WING FLAP L/E INBOARD PANEL LWR PART DENTED 3 INCHES, STA XW 79.000.  PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1.  REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0,  DC8 SRM 51-1-21.  FABRICATED PLATING (AL 2024T3 0.032) + BONDED FINGER DOUBLER (AL 2024T3 0.020) IAW DC8 SRM 57-7-1 FIG 1 ITEMS B, L.  BONDED BOTH PARTS WITH HYSOL IAW DC8 SRM 51-1-9, DC8 SRM 51-1-9A.  CLEANED, TREATED AND PRIMED AREA + NEW PANEL PLATING IAW DC8 SRM 51-1-8B.  APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11.  INSTALLED NEW PANEL PLATING IAW SRM 51-1-21.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
