Service difficulty report · Bleed Air Sys · Cessna 680CE

Difficulty date
September 29, 2020
Submitted
October 1, 2020
Operation
General aviation
Filed by
DXTR401D
NJS145 LLC
Aircraft
N388QS
Make and model
Cessna 680CE
Aircraft serial
680A0113
Aircraft time
12,030 hours, 7,939 cycles
Engine
Pwc PW306C
Part
Bleed Air Sys
Condition
Hot
Location
Zone 100
Stage of operation
CR
How discovered
O
Nature of condition
B
Precautionary procedure
O

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

What was found

DURING AND AFTER APU START UP IN FLIGHT WITH APU BLEED OFF WE HAD AN ELECTRICAL SMOKE SMELL COMING FROM THE COCKPIT GASPERS. AFTER SHUTDOWN OF THE APU THE SMELL WENT AWAY. FOUND WIRE BUNDLE DAMAGED FROM APU BLEED DUCT COUPLING IN TAIL CONE. REMOVED SECTION OF APU BLEED DUCT AND REMOVED WATER SEPARATOR DUCTING TO GAIN ACCESS TO WIRE BUNDLE FOR EVALUATION. RESOLUTION: UPON INSPECTION FOUND FOUR WIRES EXHIBITING A BURNED/CHAFE APPEARANCE. DETERMINED THREE OF THE FOUR WIRES TO BE COSMETIC ISSUES, AS THE CENTER CONDUCTOR WAS NOT COMPROMISED. FOUND THE FINAL WIRE TO BE DAMAGED TO THE CENTER CONDUCTOR AND IS MARKED AS 1ET004-3PTO65B. DETERMINED THIS WIRE IS CURRENTLY UNUSED, REFERENCING THE CESSNA 680 WIRING DIAGRAM MANUAL 49-00-01 FIGURE 06 SHEET 3 AND THE CITATION STANDARD PRACTICES MANUAL 20-30-15. APPLIED HEAT SHRINK AND END CAP TO UNUSED (1ET004-3PTO65B) WIRE. REAPPLIED PROTECTIVE TAPE AND RESECURED WIRE BUNDLE, IN REF TO CESSNA STANDARD PRACTICES MAN. 20-30-15.