Cessna T303 User manual

CESSNA
MODEL
T303 MAINTENANCE MANUAL
CESSNA
PROGRESSIVE
CARE
MODEL T303
OPERATION
NO.
1
DEALER
INFORMATION
CUSTOMER
AND
AIRCRAFT INFORMATION
ZONE
NAME
SERVICING
DEALER NAME
ADDRESS
SERVICING
DEALER CODE CITY
& STATE
A C MODEL
AND SERIAL NO
DATE
ENG
SERIAL
NO
LEFT HAND
ZONE CODE
SELLING
DEALER CODE
CUSTOMER
AND AIRCRAFT
INFORMATION
REG NO
ENG SERIAL NO
R.H
WARRANTY
START DATE
A. Placards (Chapter
11).
(1) Placards and
Decals - Inspect for
legibility.
security, presence and
B. Environmental
Systems (Chapter
21).
(1) Heater -
Check condition
and operation.
(2)
Nose Ram Air - Check
clamps and
hose.
(3)
Nose Ram Air Valve - Check
security and proper operation.
(4) Distribution Outlet Vents - Inspect outlet vents for open and
closed
position. Check windshield
defroster outlets.
(5) Heater/Vent Fan - Check operation.
C. Communications
(Chapter
23).
(1)
Static Wicks - Inspect for
security, corrosion and condition.
D.
Hydraulic Power
(Chapter 29).
(1) Hydraulic
Power Pack
- Inspect for
leaks, security
of installa-
tion, cleanliness and proper service.
(2) Relief Valves - Check function.
(3) Pressure Switch - Check function.
(4) Hydraulic Power
Pack Filter Screen - Inspect.
E. Landing Gear (Chapter 32).
* (1) Nose Gear
Assembly - Check for security
of installation,
cracks and evidence of damage.
*50-Hour Requirement,
Refer to
Paragraph 5-22, B.
D5267-13
5-23
Page 1 of 9

CESSNA MODEL
T303 MAINTENANCE
MANUAL
CESSNA
PROGRESSIVE
CARE
MODEL
T303
OPERATION
NO.
1
MECH
INSP
REMARKS
* (2) Nose Gear Shock Strut - Check for evidence of leakage, proper
extension; check strut barrel for corrosion, pitting and cleanli-
ness.
(3) Nose Gear Shock Strut - Service.
* (4) Nose
Gear Torque Links - Inspect
for wear and condition.
*(5) Nose
Gear Torque Links
- Lubricate.
* (6) Nose
Gear Trunnion and Pivot
Bearings - Lubricate.
(7) Nose Gear Fork - Inspect for cracks, general condition and
security
of attachment.
* (8) Shimmy Dampener - Check for security of installation, attach
points
for wear and
condition, lubricate.
(9) Shimmy Dampener - Service.
(10) Nose Gear Door Actuator and Door Mechanism - Inspect for
condition.
* (11) Nose Gear Wheel - Inspect for nicks, cracks, finish abrasions
and corrosion.
* (12) Nose Gear Tire - Check for wear, cuts and proper inflation.
(13) Nose Gear Wheel Bearings - Inspect for corrosion, evidence
of damage, clean and repack.
(14) Nose
Gear Steering
System - Check
turnbuckle
tension and
gimbal
bolts for condition
and torque.
(15) Nose Gear
Steering Stop Block -
Check security.
F. Ice and Rain Protection (Chapter 30).
(1) Pitot Heater
- Check
operation.
G. Navigation and Pitot/Static (Chapter 34).
(1) Pitot
Tube and Lines - Inspect
for security of installation,
cleanliness and evidence of damage. Check sumps for cracks,
leaks
and presence of water,
drain sumps.
H. Lights (Chapter 33).
(1) Nose
Baggage Compartment -Inspect
light and switch
for
security of
installation and
operation.
I. Doors (Chapter 52).
(1) Nose Baggage Door
- Check condition, operation
and security
of hinges, latches and assist cylinder.
*50-Hour
Requirement,
Refer
to
Paragraph
5-22,
B.
Page 2 of 9

CESSNA
MODEL T303
MAINTENANCE
MANUAL
CESSNA
PROGRESSIVE
CARE
MODEL T303
OPERATION
NO. 1
MECH INSP REMARKS
5-24.
FUSELAGE.
A. Fire Protection
(Chapter
26).
(1) Fire
Warning Lights - Check
operation.
(2) Portable Hand Fire Extinguisher - Inspect for proper
operating pressure, security of installation and evidence
of damage.
B. Flight Controls (Chapter 27).
1) Aileron
Trim Tab Control and
Indicator - Inspect for se-
curity and evidence of damage. Operate control and
check freedom of movement. Inspect turnbuckle safety-
ing.
(2) Rudder
Trim Tab Control and
Indicator - Inspect for se-
curity and evidence of damage. Operate control and
check rudder trim tab for freedom of movement.
(3) Elevator Trim Tab Control and Indicator - Inspect for se-
curity and evidence of
damage. Operate both
manually
and electrically.
C. Oxygen (Chapter 35).
(1) Oxygen System
- Checkinstallation
and pressure.
(2)
Oxygen Regulator -
Check pressure and flow
rate.
(3) Oxygen
Masks and Hoses - Check
operation and clean.
(4) Oxygen
Cylinder - Inspect condition,
check hydrostatic
test date.
D. Equipment/Furnishings (Chapter 25).
(1) All Seats - Inspect seat rails for cracks, refer to Chapter
for limitations.
5-25. WINGS.
A. Wings (Chapter 57).
* (1) Wings
- Check for
loose rivets, cracks,
loose
mounting
fasteners and security.
(2) Wing Wheel Well - Check fume proofing.
(3) Wing Access Plates
- Inspect for security of installation
and
evidence of damage.
(4) Wing
Spar Fittings - Check bolts for
working and security.
*50-Hour
Requirement, Refer
to Paragraph 5-22,
B.
Page 3 of 9

CESSNA MODEL
T303 MAINTENANCE
MANUAL
CESSNA PROGRESSIVE
CARE
MODEL T303
OPERATION
NO.
1
MECH
INSP REMARKS
B.
Landing Gear
(Chapter 32).
* (1)
Main Gear
System -
Check
actuating
time and
free fall (both
flight and ground check).
*
(2)
Main Gear
Assembly
- Check
security
of
installation
and
attach
points for wear
and condition.
(3)
Perform
landing gear
rigging
inspection.
*
(4)
Main Gear
Shock
Struts
- Check
for
evidence
of leakage
and
proper
extension;
check
strut
barrel
for corrosion,
pitting
and
cleanliness.
(5)
Main
Gear Shock
Struts
- Service.
* (6)
Main
Gear
Wheel
-
Inspect
for
nicks,
cracks,
finish,
abrasion
and
corrosion.
(7) Main
Gear
Wheel
Bearings
- Inspect
for corrosion,
evidence
of damage,
clean and
repack.
(8)
Brake
System
Plumbing
- Inspect
for leaks,
condition
and
security;
check
for
proper
routing
and
support.
(9)
Brake
Assemblies
- Check
lining
wear
and
disc warpage.
* (10)
Main
Gear Tires
- Check
for
wear, cuts
and
proper
inflation.
* (11)
Main Gear
Retraction
Upper
Arms -
Lubricate.
C.
Fuel (Chapter
28).
(1) Fuel
Lines - Inspect
for
deterioration,
chafing, fuel
leaks and
security
of installation.
(2)
Fuel
Inlet Float
Valves
-
Check
with tester.
(3)
Fuel
Pressure
Switch
and
Auxiliary
Pump
Micro
Switch
-
Check operation.
D.
Electrical
Power
(Chapter
24).
* (1)
Battery
Installation
- Inspect
overboard
vent
and
vent line
for
damage
and
obstruction.
* (2)
Battery
Cables
-Inspect
for corrosion
and deterioration.
*
(3)
Battery
Electrolyte
-
Inspect
for spewage
and level
in each
cell.
*
(4) Fuseholder - Ensure
all
fuses
are functional
and
spares
are
available.
*50-Hour
Requirement,
Refer
to Paragraph
5-22,
B.
Page
4
of 9

CESSNA
MODEL T303
MAINTENANCE MANUAL
CESSNA
PROGRESSIVE
CARE
MODEL T303
OPERATION
NO.
1
MECH INSP
REMARKS
5-26.
NACELLES.
A.
Fire Protection
(Chapter 26).
(1) Detection
Control Unit
- Inspect
for security and
evidence of
damage.
5-27.
TAILCONE.
A.
Flight Controls
(Chapter 27).
(1) Rudder
- Inspect
the rudder
skins for cracks
and loose
rivets, rudder hinges,
hinge bolts, hinge
bearings and
hinge
attach
fittings for
evidence of
damage or
wear,
failed
fasteners and
security.
Check the
rudder hinge
bolts
for proper safety
of
nuts with
cotter pins.
(2)
Rudder Bellcrank
- Inspect
bellcrank
stop
bolts for
prop-
er safetying,
corrosion,
evidence
of damage
and safety.
Inspect bellcrank
cables
for proper safetying.
(3) Rudder
Cables
- Check condition,
routing, tension,
turnbuckle safetying;
cables
in pulleys
and not
rubbing
on
structure.
(4) Rudder
Trim Tab
- Inspect skins
for cracks
and loose
rivets. Inspect
hinge for
security
and
evidence
of dam-
age,
hinge
pin for
proper
installation
and
cotter
pin
safetying.
Check
trim
tab travel.
Inspect
pushrods
for
evidence of
damage
and security.
(5)
Rudder
Trim
Tab
Actuator
-
Inspect
actuator
for
security
and
evidence
of
damage, service.
(6)
Rudder
Trim
Cables
- Inspect
condition,
routing,
ten-
sion,
turnbuckle safetying;
cables
in pulleys
and not
rubbing
on structure.
(7) Rudder
Gust
Lock
- Check
security,
wear
and
travel.
(8)
Yaw Dampener
Actuator
and
Cables
-
Inspect
actuator
for
security,
mount
for cracks
and structure
for
evidence
of damage.
Inspect
cables
for fraying,
chafing,
routing,
cleanliness,
cable
tension
and
turnbuckle
safetying.
In-
spect chains
for proper
alignment
on actuator
sproc-
kets.
(9)
Elevator
- Inspect
the
elevator
skins
for cracks
and
loose
rivets.
Check
elevator
hinges
for
condition,
cracks
and
security.
Inspect
hinge bolts, hinge
bearings,
torque
tube,
horn
and
attach
fittings
for
evidence
of
damage
or
wear.
Check
travel
and
friction.
*50-Hour
Requirement,
Refer
to Paragraph
5-22,
B.
Page 5 of 9