What was found
WRONG BOLTS INSTALLED AT LOWER FUSELAGE STRUT TO BIRDCAGE STRUCTURE. AN6-A INSTALLED, SHOULD BE AN176-13A CLOSE TOLERANCE BOLTS, AS PER DEHAVILLAND DRAWING C2FS5123A.
- Difficulty date
- November 12, 2005
- Submitted
- June 6, 2006
- Operation
- General aviation
- Make and model
- Dhav DHC2MKI
- System (JASC)
- 1430 · Fasteners
- Part
- Bolt
- Part number
- AN6A
- Condition
- Wrong Part
- Location
- Landing Gear
- Part time
- 288 hours
- Component
- Frame Assembly · Dhav · C2FS3203A
- Stage of operation
- NR
- How discovered
- 9
- Nature of condition
- E
- Precautionary procedure
- A, C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.