Sat. |
Unsat. |
N/A |
Item |
Notes |
|
|
|
|
|
|
|
|
Regulatory
Prerequisites and Placards: |
|
|
|
|
|
|
X |
|
|
Has
construction manual |
|
X |
|
|
Weight and
Balance done, and shows within designer limits |
Current
W&B can be completed for purchaser at
time of sale. |
|
|
|
All
controls, both flight and engine, marked as to use |
|
X |
|
|
Throttle,
open/close |
|
|
X |
|
Flaps,
up/down, degrees indicated, take off setting marked |
No current
markings, Can be installed at time of sale |
|
|
X |
Fuel,
on/off |
|
X |
|
|
Fuel
quantity and type marked at each cap |
Panel Gauge |
|
|
|
|
|
|
|
|
Cockpit and
Interior: |
|
|
|
|
|
|
X |
|
|
Seat belts
function |
|
X |
|
|
Shoulder
harness functions |
|
X |
|
|
Shoulder
belt anchor points firm, no interference |
|
X |
|
|
Seat belt
anchor points firm, no interference |
|
X |
|
|
Seat and
seat tracks OK, stops on aft rails |
Good secure
lock, free movement |
|
|
|
|
|
|
|
|
Instruments
and Required Equipment: |
|
|
|
|
|
|
|
|
X |
ELT
properly installed, with remote switch |
|
|
|
X |
ELT battery
date recorded in aircraft records |
|
X |
|
|
Fuel Gauge,
each tank, functions correctly |
|
|
|
|
VFR day
requirements (instruments marked with red and green lines): |
|
X |
|
|
Altimeter |
2 Pointer,
no Kollsman |
X |
|
|
Airspeed |
No range
marking, can be installed at time of sale.
ASI is proper range for this aircraft's flight speeds. |
X |
|
|
Tach.
Tach time: |
Total Time:
24.3 |
X |
|
|
Oil
Quantity |
Oil
reservoir has low level indicator light on
panel. |
|
|
X |
Oil temp |
|
X |
|
|
Compass |
|
X |
|
|
EGT |
No
range marking, can be installed at time of
sale. |
X |
|
|
CHT |
No
range marking, can be installed at time of
sale. |
|
|
|
Hobbs
time is: |
24.3 |
|
|
|
VFR Night
Requirements: |
|
|
|
X |
Position
lights |
|
X |
|
|
Anti-collision
lights/rotating beacon |
3 White
Strobes |
X |
|
|
Spare fuses |
|
X |
|
|
Electrical
energy sufficient for duration of A/C range plus reserve |
|
|
|
|
|
|
|
|
|
Electrical: |
|
|
|
|
|
|
X |
|
|
Battery and
electrical system wiring adequate size, and secure |
Battery
mount is adequate, but can be secured a
little better. Sealed
battery |
X |
|
|
Switches
marked for operation and wired properly |
Wiring is
all good. Master and Strobe
switches need placards. |
X |
|
|
Circuit
breakers or fuses labeled for value and function, wired properly |
|
X |
|
|
Ground on
battery to airframe and wired properly |
|
|
|
X |
Ammeter |
|
|
|
X |
Voltmeter |
|
|
|
X |
Landing
lights wired correctly |
|
|
|
X |
Position
lights wired correctly |
|
|
|
X |
Cockpit
lights/instrument lights wired correctly |
|
|
|
X |
Battery
case and battery securely mounted |
|
|
|
X |
Battery
vented overboard |
|
|
|
|
|
|
|
|
|
Avionics: |
|
|
|
|
|
|
X |
|
|
Antennas
properly installed and have proper doubler or support plate |
Radio
antenna currently mounted on bottom of wing,
horizontally. Could be moved
to top of aircraft. |
X |
|
|
Coax cable
secured, with enough slack to prevent disconnect |
|
|
|
X |
Radios/avionics
and cooling fans mounted securely |
|
|
|
X |
Avionics
gear wired properly and functions |
|
|
|
X |
Transponder
mode "C" check done, and recorded in aircraft records |
|
|
|
|
|
|
|
|
|
Fuel
System: |
|
|
|
|
|
|
X |
|
|
Caps fit,
and vented on all tanks |
Vented cap
system (typical) |
|
|
X |
Fuel drain
installed at lowest portion of tank |
|
|
|
X |
Fuel drain
installed at lowest point in system |
|
X |
|
|
Fuel vent
system vented properly |
|
|
|
X |
Shutoff
valve/selector switch operates easily and is clearly marked |
|
X |
|
|
Fuel line
routing is of proper material and diameter |
|
X |
|
|
Fuel filter
installed |
|
|
|
X |
Fuel
strainer functional and safety wired or self closing |
|
X |
|
|
Fuel lines
protected from chafing and secure |
1 location
needs small shroud |
X |
|
|
Fuel line
routing avoids areas of heat |
|
|
|
|
|
|
|
|
|
Gear,
Wheels, Brake Systems: |
|
|
|
|
|
|
|
|
X |
Clearance
on fairings |
|
X |
|
|
Brake
system lines routed correctly |
|
X |
|
|
Reservoir/pumps
functional |
Mechanical,
smooth function |
|
|
X |
Wheel pants
secure |
|
|
|
X |
Tail spring
secure, clear of rudder |
|
|
|
|
|
|
|
|
|
General
Condition, Fuselage, Wing, Tail Assembly: |
|
|
|
|
|
|
X |
|
|
Skin
condition, wrinkles, rivets, tape |
Good
quality clear coat, some slight fading on top
surfaces of colored portion of wings.
Pylon cover is not clear coated (all other surfaces are) |
X |
|
|
Vertical
fin, movement and condition |
|
X |
|
|
Ailerons,
movement and condition |
|
X |
|
|
Flaps,
movement and condition |
|
X |
|
|
Elevator
assembly, movement and condition |
|
|
|
X |
Trim tabs
function, no binding |
|
X |
|
|
Control
travel stops |
|
X |
|
|
Control
cables safety wired correctly |
|
X |
|
|
Windshield
overall condition |
Small scuff
on top of windscreen, easily polished out. |
X |
|
|
Wing attach
brackets and hardware |
|
X |
|
|
Tail group
attach brackets and hardware |
|
|
|
|
|
|
|
|
|
Flight
Controls: |
|
|
|
|
|
|
X |
|
|
Proper
tension of cables |
|
X |
|
|
Safety
wiring of cables |
|
X |
|
|
Clearance
on controls, no hitting panel, sides, floorboards |
|
X |
|
|
Freedom of
movement |
|
X |
|
|
Proper
direction |
|
X |
|
|
Everything
safety wired |
|
X |
|
|
Rudder
hinges, horns, and attachments |
|
X |
|
|
Aileron
hinges, horns and attachments |
|
X |
|
|
Elevator
hinges, horns and attachments |
|
|
|
|
|
|
|
|
|
Engine
Compartment: |
|
|
|
|
|
|
X |
|
|
Throttle
cables anchored and functional |
|
X |
|
|
Throttle
defaults to open position |
Default is
closed position on all Rotax 2 cycle engines. |
|
|
X |
Choke cable
anchored and functional |
Primer
system installed, no choke |
X |
|
|
Clearances
in engine compartment |
|
X |
|
|
Fuel line
routing to avoid heat and bends |
|
X |
|
|
Sufficient
fuel line diameter |
|
X |
|
|
Fuel and
oil hoses proper material |
|
X |
|
|
Oil system
hose and cooler installed correctly |
|
X |
|
|
Engine
mount secure, no cracks |
|
X |
|
|
Signs of
oil leaks |
|
X |
|
|
Muffler/exhaust
condition |
Using Rotax
springs, suggest upgrading to stainless
clamps |
|
|
|
|
|
|
|
|
Propeller: |
|
|
|
|
|
|
X |
|
|
Prop nicks
and/or cracks |
68 X 30
Tennessee Propeller, excellent condition. |
X |
|
|
Safety
wired bolts of sufficient size |
Nylock
nuts, per installation instructions |
X |
|
|
Bolts clear
engine |
|
X |
|
|
Prop is
correct length to clear airframe |
Approximately
4" |
X |
|
|
Hub has no
cracks or corrosion |
|