Service difficulty report · Spar · Cessna 680A

Difficulty date
September 2, 2020
Submitted
September 3, 2020
Operation
Air carrier
Filed by
JGVR194F
Duncan Aviation Inc
Aircraft
N338QS
Make and model
Cessna 680A
Aircraft serial
6800011
Aircraft time
12,700 hours, 8,608 cycles
System (JASC)
5711 · Wing Spar
Part
Spar
Condition
Corroded
Location
Lt Mlg Ww
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

LT MLG WHEEL WELL LOWER AFT SPAR HAS 2 AREAS OF VERIFIED CORROSION. REMOVED 3 EACH HI-LOKS FROM LT MLG WHEEL WELL LOWER AFT SPAR FOR ACCESS. BLENDED 2 EACH AREAS OF CORROSION ON LT MLG WHEEL WELL LOWER AFT SPAR. OTBD AREA WAS FOUND TO BE MILD SURFACE CORROSION PER CESSNA 680 SRM 51-10-01 AND CLASSIFIED LEVEL 1 PER NJA GMM 2.2.2. REPAIRED OTBD BLENDED AREA PER CESSNA 680 SRM 51-70-02 AND 51-20-01. INBD AREA WAS FOUND TO BE BEYOND LIMITS PER CESSNA 680 SRM 51-70-02 AND CLASSIFIED LEVEL 2 PER NJA GMM 2.2.2. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS OF INBD AREA. REPAIRED BLENDED AREA AND REINSTALLED HI-LOKS PER TEXTRON AVIATION FIELD REPAIR FR-680-0011-8314, INITIAL REVISION, DATED 8-27-2020. RT MLG WHEEL WELL LOWER AFT SPAR HAS 1 AREA OF VERIFIED CORROSION. BLENDED 1 AREA OF CORROSION ON RT MLG WHEEL WELL LOWER AFT SPAR. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. BLENDED AREA WAS FOUND TO BE BEYOND SRM LIMITS PER CESSNA 680 SRM 51-70-02 AND LEVEL 2 PER NJA GMM 2.2.2. REPAIRED BLENDED AREA PER TEXTRON AVIATION FIELD REPAIR FR-680-0011-8314, INITIAL REVISION, DATED 8-27-2020.

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