EasyManuals Logo

Cirrus SR22T User Manual

Cirrus SR22T
506 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Page #323 background imageLoading...
Page #323 background image
Cirrus Design Section 8
SR22T Handling and Servicing
P/N 13772-005 8-23P/N 13772-005 8-23
If sampling reveals contamination, the gascolator and tank drains must
be sampled again repeatedly until all contamination is removed. It is
helpful to gently rock the wings and lower the tail slightly to move
contaminates to the drain points for sampling. If after repeated
samplings (three or more), evidence of significant contamination
remains, do not fly the airplane until a mechanic is consulted, the fuel
system is drained and purged, and the source of contamination is
determined and corrected.
If sampling reveals the airplane has been serviced with an improper
fuel grade, do not fly the airplane until the fuel system is drained and
refueled with an approved fuel grade.
To help redu ce the oc cu rrence of c on taminated fuel c om ing fro m the
supplier or fixed based operator, pilots should assure that the fuel
supply has been checked for contamination and that the fuel is
properly filtered. Also, between flights, the fuel tanks should be kept as
full as operational conditions permit to reduce condensation on the
inside of fuel tanks.
Draining Fuel System
The bulk of the fuel may be drained from the wing fuel tanks by the use
of a siphon hose placed in the cell or tank through the filler neck. The
remainder of the fuel may be drained by opening the drain valves. Use
the same precautions as when refueling airplane. Refer to the AMM
for specific procedures.
Battery Service
The aircraft is delivered with a maintenance free, rechargeable,
sealed, lead acid primary battery. Battery #1 is mounted to the forward
right side of the firewall and access is gained by removing the upper
cowl. The battery vent is connected to an acid resistant plastic tube
that vents gases and electrolyte overflow overboard
A capacity check must be performed at initial 24 months or 1200 hours
in service and then every 12 months or 200 hours thereafter. Refer to
the AMM for additional information on Battery #1 Overhaul and
Replacement Schedule and Scheduled Maintenance Checks.
• Note
For aircraft equipped with conventional lead acid battery
requiring periodic electrolyte level check: Refer to the AMM for
information on Battery Overhaul and Replacement Schedule
and Scheduled Maintenance Checks
Original Issue

Table of Contents

Other manuals for Cirrus SR22T

Questions and Answers:

Question and Answer IconNeed help?

Do you have a question about the Cirrus SR22T and is the answer not in the manual?

Cirrus SR22T Specifications

General IconGeneral
ManufacturerCirrus Aircraft
EngineContinental TSIO-550-K
Horsepower315 hp
Max Takeoff Weight3, 600 lbs
Service Ceiling25, 000 ft
Cabin Width49 in
Cabin Height50 in
Seating Capacity4
AvionicsCirrus Perspective+ by Garmin
CategorySingle-engine piston aircraft
PropellerHartzell 3-blade composite
Wingspan38 ft 4 in
Length26 ft
Height8 ft 11 in
Maximum Cruise Speed213 KTAS
Fuel Capacity92 gallons
Stall Speed64 knots
Safety FeaturesCirrus Airframe Parachute System (CAPS)
Cruise Speed183 knots

Related product manuals