Service difficulty report · Drag Angle · Cndair CL6002C10

Difficulty date
May 24, 2010
Submitted
May 28, 2010
Operation
Air carrier
Aircraft
N748EV
Make and model
Cndair CL6002C10
Aircraft serial
10158
Aircraft time
15,717 hours, 10,821 cycles
Part
Drag Angle
Condition
Cracked
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

PERFORMED EDDY CURRENT INSP OF LT VERTICAL STAB TO FUSELAGE ATTACH DRAG ANGLE IAW MAC NDT INSP PROCEDURE ET-2, DRAG ANGLE IS CONFIRMED CRACK AND END OF CRACK IS MARKED. REMOVED LT SIDE AFT DRAG ANGLE & LOCATED HOLES IN NEW DRAG ANGLE IAW SRM 51-42-27-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01. INSTALLED FASTENERS IN SERVICEABLE ANGLE AT BASE OF VERTICAL STAB ON LT SIDE IAW SRM 51-42-20-001-001-A01, COLLARS REQUIRE TIGHTENING ABOVE APU INLET DUCT. TIGHTENED 3 COLLARS FWD APPLIED A023 PROTECTIVE COATING ALL WORK DONE IAW SRM 51-42-21-001-001-A01 AND SRM 51-25-01-001-001-A01.