Service difficulty report · Blade · Bell 206L3

Difficulty date
July 30, 2003
Submitted
October 15, 2003
Operation
General aviation
Make and model
Bell 206L3
Engine
Allsn 250C30P
Part
Blade
Part number
206015001115
Part serial
A4267
Condition
Damaged
Location
Main Rotor
Part time
757 cycles
Stage of operation
DE
How discovered
9
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

(AUS) M/R BLADE UPPER SKIN TORN IN AREA LOCATED AT BLADE TIP IMMEDIATELY INBOARD OF TIP CAP. INSP FOUND SKIN HAD LIFTED IMMEDIATELY BEHIND SPAR &TORN IN SPAN WISE DIRECTION FROM TIP TO APPROX 50.8MM INBOARD OF TIP & 25.4MM AFT OF SPAR.SKIN & ADHESIVE HAD SEPARATED FROM THE CORE MATERIAL WITH EVIDENCE OF CORROSION UNDER THE ADHESIVE. BLADE R & FWDED TO REPAIR FACILITY. FURTHER INSP AT REPAIR FACILITY REVEALED OTHER AREAS OF CORROSION AND PITTING IN GRIP DOUBLERS ON LOWER SURFACE OF BLADE & ALSO IN AREA UNDER THE LATCH PLATES BONDED TO GRIP TANGS. PHOTOGRAPHS REVEALED CORROSION IN DOUBLERS STARTING IN MIDDLE OF BONDED JOINT & NOT EMANATING FROM MOISTURE INGRESS FROM EDGE OF JOINT AS WOULD NORMALLY BE EXPECTED.

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