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Inspection
Guide Only
Use
Maintenance Manual for specific guidance/instructions
Aircraft Data
OWNER:
COMMANDER MODEL: SERIAL No.:
___ REG #: _____
ENGINE MODEL: ___________ ENGINE S/N:
PROP MODEL & S/N:
TACH TIME: ENGINE TT:
PROP TT:
OIL:
Brand Type
Weight Quantity/QTS
NON-DETERGENT
DETERGENT
General Ite
General Items
1.
Check log books and verify last Pitot/Static and Transponder certification,
ELT battery replacement and recommended time life items.
2.
Certificate of Registration
in aircraft and properly displayed.
3.
Certificate of Airworthiness in aircraft and properly displayed.
Aircraft equipment
list, Weight & Balance, and FAA req’d placards in aircraft.
Engine and engine compartment
mechanic
inspector
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1. Run up engine in accordance w/
maintenance manual and note all discrepancies. |
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2. Remove entire engine cowling.
Inspect engine and equipment for signs of fluid leakage. Note suspect
areas and clean engine. Inspect cowling for wear and cracks to include
fasteners and cowl flaps. Record as necessary. |
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3.
Perform and record a hot engine differential compression check.
Cyl - 1: Cyl - 2:
Cyl - 3: Cyl - 4:
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4.
Drain oil (ref Lycoming Service letter L121) |
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5.
Remove and clean suction screen. Particle check. Reinstall screen and
safety wire. |
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6.
Replace oil filter element and safety. Particle check. |
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7.
Remove fuel screen from gascolator/strainer assembly. Clean & reinstall
using new gaskets. Check drain function. Safety wire. |
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8.
Spark plugs - inspect, clean, gap, test and reinstall or replace as
appropriate. Install using 360 - 420 in lbs. torque. Lyc SI 1042. |
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9.
Check magneto, point condition and timing. 500 hr service if appropriate. |
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10.
Check induction air filter and alternate air valve. Remove filter.
Inspect, service
, or replace
, and reinstall. |
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11.
Remove & clean injector finger screen. Reinstall and safety. |
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12.
Remove, clean, & replace injector nozzles |
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13.
Inspect following items for condition, security, cleanliness, and
operation:
a)
Spark plug leads (high tension lead test)
b)
Manual priming system and lines
c)
Intake system
d)
All studs and nuts
e)
All fluid carrying lines and fittings
f)
All wiring and connectors
g)
Engine controls and linkage (condition and travel) Lubricate.
h)
Firewall and all firewall mounted components
i)
Engine mount and attach structure
j)
Crankcase, accessory section & all accessories
k)
Cylinders, hold downs, push rod housings
l)
Engine baffling and baffle seals
m)
Alternator, connections and drive belt. Check belt tension.
n)
Cowl flap condition and operation
o)
Prop governor and governor oil line
p)
Blast tubes, heat and cooling hoses
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14.
Install lower cowling. Insure oil cooler to cowling is in place
and landing light is connected. |
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15.
Install upper cowling. Check for proper position of baffle seals. |
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Propeller
mechanic inspector
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1.
Remove prop spinner |
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2.
Inspect spinner & bulkhead for cracks or dents |
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3.
Inspect propeller hub, bolts, & control mechanism, for security &
condition. |
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4.
Inspect blades for nicks, cracks, abrasions, & track. Service as
req’d. |
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5.
Reinstall prop spinner |
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Airframe
mechanic inspector
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1.
Remove applicable inspection panels and inspect wings, wing center
section, flaps, & ailerons for dents, cracks, distortion, security & general
condition. |
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2.
Inspect fuel cell areas for external leakage and operation of gauge
transmitters and fuel selectors |
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3.
Check all fuel lines and fittings. Check all fuel vents, lines, &
fittings. Check operation of all fuel tank drain valves. |
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4.
Remove & clean fuel vent drain assembly (if applicable) |
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5.
Inspect wing fuel caps and anti-siphoning fuel valves for proper fit. |
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6.
Check for appropriate fuel placards |
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7.
Check for proper operation of the stall warning system |
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8.
Inspect wing landing light, lens, & assembly (if applicable) |
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9.
Inspect static wicks for condition, security, & cleanliness |
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10.
Inspect wing to fuselage attachments |
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11.
Remove wing and fuselage inspection panels and inspect following
items for leaks, condition, & cleanliness:
a)
All electrical wiring and connectors
b)
All fluid carrying lines
c)
All internal structures
d)
Ventilating ducts
e)
Front landing light and lens
f)
Nose wheel structure |
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12.
Inspect all control surfaces and trim tabs for condition, security,
operation, & proper travel. Ref. Figure 7-13 Record:
LT Flap _____ RT Flap ____ LT Aileron ______
RT Aileron _______ Elevator _______ Elevator Trim ______
a)
Check all control surface cable tensions. Record.
Aileron ____ Rudder ______ Elevator _______ Elevator trim ______
b)
Check all rod ends and actuating mechanisms
c)
Check rudder aileron interconnect rigging
d)
Check aircraft rigging to factory specs
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13.
Inspect exterior of the fuselage |
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14.
Inspect cabin windows and windshield for security, cracks, &
cleanliness |
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15.
Inspect cabin doors and door seals for condition, security, and
operation |
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16.
Inspect baggage door, door seal, and interior |
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17.
Aircraft battery:
a)
GENERAL: - Remove applicable inspection panels and inspect battery
compartment for corrosion and general condition.
b)
Check battery vent clear of obstructions, terminal connections,
electrolyte specific gravity and service battery (if applicable)
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18.
Check hydraulic power pack fluid level and clean filter lines (if
applicable) |
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19.
Inspect following items for condition, security, & operation:
a)
Engine and Flight instruments, instrument panel, & markings
b)
Check behind instrument panel. Verify all wiring, hoses, etc. are
properly secured. Verify there is no interference w/ flight control
movements. |
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20.
Inspect seats, seat locks, shoulder & seat belts for condition and
security. |
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21.
Change vacuum filters (every 500 hours only or as needed) |
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22.
Change suction relief valve (every 500 hours or as needed) |
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23.
Check Pitot/static lines and fittings for proper routing, security,
and moisture content. Check Pitot and static ports for obstructions and
security. Check Pitot heat. |
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24.
Inspect antennas and all other items of installed equipment and/or
systems for condition, security, cleanliness, and operation. |
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25.
Check and/or service ELT. Check date of expiration.
ELT expiration date: ____/____/____ |
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26.
Remove applicable panels and tailcone assembly and inspect empennage
for dents, cracks, distortion, and general condition. Check drain holes.
Lubricate equipment as req’d. |
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27.
Check anti-collision lights, position lights, and wiring in addition
to other items of installed equipment for condition, security, cleanliness
and operation. |
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28.
Check lower vertical fin upper rib for cracks (ref SB-114-12A or
SB-112-56 |
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Landing Gear & Brake System
mechanic inspector
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1) Check landing gear
properly down and locked. |
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2)
Ensure parking brake is disengaged and chock aircraft. Secure tail stand to
tail tie down ring. Lubricate all recommended fittings and areas. Ref.
Maintenance manual Fig. 2-15 and associated Figures. (incl zerk ftg on nose
gear and 14641 & gear actuator rod ends |
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3)
Check all landing gear struts for proper hydraulic fluid, servicing, and
inflation.
Nose Gear: 90 PSI Main Gear: 150 PSI |
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4)
Inspect following items for condition (undue/excessive wear, fatigue,
distortion), security, and cleanliness:
a) Nose & Main landing
gear struts
b) Sidebraces &
Scissors
c) Microswitches and
Wiring
d) Landing gear doors
and linkage
e) Landing gear
actuating cylinders, hydraulic lines and attach points
f) Shimmy damper
(service if req’d), nosewheel steering/cylinder and cables.
g) Landing/taxi
lights, lens, and assembly (if installed on gear)
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5)
Perform a complete landing gear rigging and operational check including the
emergency gear extension system. NOTE: Ensure gear warning system lights
(4), gear warning bell, overcenter limits in drag braces, squat safety
switch and proper closing of gear doors are checked. W/ gear in UP
position the warning horn should actuate when the throttle is reduced to
between 12 and 15 inches of MP or | |
