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 RT VERT STAB TO FUSELAGE ATTACH DRAG ANGLE IAW MAC NDT INSP PROCEDURE ET-2. DRAG ANGLE IS CONFRIMED CRACKED AND END OF CRACK IS MARKED. REMOVED RT AFT DRAG ANGLE IAW SRM 51-42-27-001-001-A01, 51-42-21-001-A01 & 51-42-13-001-001-A01. INSTALLED ANGLE AND STARTED INSTALLING FASTENERS IAW SRM 51-42-13 AND 57-42-22-001-001-A01. INSTALL COLLARS ON ALL LOCK FASTERNERS FOR LT SIDE DRAG ANGLE. INSTALLED ALL COLLARS ON ALL FASTENERS FOR LT SIDE DRAG ANGLE AND APPLIED A023 REFLECTIVE COATING ALL WORK DONE IAW SRM 51-42-21-001-001-A01 AND SRM 51-25-01-001-001-A01.