Service difficulty report · Connector · Dhav DHC8311

Difficulty date
October 9, 2000
Submitted
January 19, 2001
Operation
General aviation
Make and model
Dhav DHC8311
Engine
Pwa PW123
Part
Connector
Part number
AN81510D
Condition
Sheared
Location
Press Manifold
Part time
11,837 hours, 23,312 cycles
Stage of operation
AP
How discovered
O
Nature of condition
K, J
Precautionary procedure
O

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

What was found

(CAN) THE FOLLOWING WAS REPORTED TO US: INFO GATHERED FROM RETURNING ENGINEER (TODAY 10TH OCT) STATES THAT CAPTAIN REPORTED ON APPROACH HE NOTICED THAT NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED AND WITHIN 3 SECONDS OBSERVED TOTAL LOSS OF NR 2 HYDRAULIC FLUID IN THE SYSTEM.PER QRH, ALT EXT WAS CARRIED OUT AND AIRCRAFT LANDED UNEVENTFULLY. AIRCRAFT WAS REPORTED TO HAVE STOPPED AT 7,500 FEET FROM POINT OF TOUCH DOWN. CAPTAIN REQUESTED AIRCRAFT BE TOWED TO GATE.MAINTENANCE:REPLACED MANIFOLD ASSEMBLY AND UNION, NR 2 HYDRAULIC SYSTEM FLUID REPLENISHED, SYSTEM BLED AND AIRCRAFT RELEASED AS SERVICEABLE.