Программа обслуживания С172

Вопросы технического обслуживания самолетов Cessna. Запчасти, ремонт. Обучение персонала. Обсуждение сервис-центров.

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Viktor
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Программа обслуживания С172

#1 Сообщение Viktor » 23 сен 2008, 22:00

Народ интерисовался отвечаем.
Программа обслуживания утверждённая и выполняемая.

к сожалению на английском перевести давольно муторно :oops:

ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
1
This Maintenance Program will be used for maintaining the aircraft
CESSNA F172N ES-ECR S/N F17201950
with engine O-320-H2AD S/N L-8019-76T
and propeller McCauley P/N 1C160-DTM7557 S/N: 81644
operated by
This Maintenance Program is based on Cessna Model 172 series 1977 thru 19 86 Service Manual
issued 20 March 1985 latest revision doc. D2065 -3-13 (Revision 3 from 01. July, 1995) and will be
reviewed and updated by the owner in connection with airworthiness review of this aircraft and
every time when changes in the TC holder’s re commendations, modifications, FAA, EASA or
service experience require amendment to this Program.
Practices and procedures to satisfy this Program will be the standards specified in the Type
Certificate Holder’s Maintenance Instructions.
The Progressive Care Maintenance Program is used.
Signed by: Approved by:
_________________ 31st August 2007 ____________________ ___ ______ 2007
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
2
CONTENT,
REVISION NUMBER &
EFFECTIVE PAGES
Page Description Revision
Number
Date
1 Preface 1 01.09.07
2 Content, Revision no.,
Effective Pages
1 01.09.07
3 General 1 01.09.07
4 Inspection Terms and
Guidelines
1 01.09.07
5-17 Primary Inspections 1 01.09.07
18-21 Additional Inspections 1 01.09.07
22 Cessna Mandated Time
Limits Operations
1 01.09.07
23-25 Aircraft Storage 1 01.09.07
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
3
PROGRESSIVE CARE PROGRAM
1. General
A. The program is divided into four primary operations (operations 1 thru 4) which cover all 50
hour, 100 hour and 200 hour inspection requirements. The remaining operations include all
of the inspection requirements due at other intervals.
B. The Cessna established component time limits section is included as Operation TL 1 to
Operation TL 6 with specified intervals to comply with SM Sec.2.
C. Differeces of this Program from Cessna Model 172 series 1977 thru 1986 Service Manual
recommendations:
(1). Item D 11 - Wheel Bearings - Clean, inspect and lube – is included into OP4 and will
be done each 200 hrs instead of 500 hrs recommended by SM
(2). Item J 3 – Engine Controls and Linkage - should be replaced every 1500 hours. Based
on maintenance experience, engine controls will be replaced at engine overhaul, or in case
if maximum linear movement does not exceed .050 inch
(3). Item J 13 - Starter, Starter Solenoid, and Electrical Connections – “Check solenoid and
electrical connections” is included into OP2 and OP4 and will be done each 100 hours and
J13a: “Inspect each 500 hours condition of starter brushes, brush leads, and commutator” is
included in OP9.
(4). Item J 31 - Drain oil sump and oil cooler, replace filter, and refill with recommended
grade aviation oil. First 25 hours: Drain oil sump, clean pressure screen or replace oil filter,
and refill with MIL-L-6080 aviation grade straight mineral oil. Beginning with the 50 -hour
oil change and thereafter, refil l oil sump with MIL-L-22851 ashless dispersant oil – is
included into Operations 1-4 – means that filter change will be done every 50 hrs not 100
hrs as recommended.
(5). Vacuum system relief valve filter replacement every 100 hours is included into OP2
and OP4
(6). Engine evaluation procedure added as OP14 before engine TBO extension. TBO may
be extended maximum for 20% from recommended by manufacturer, provided that engine
condition is evaluated every 100 hours or 1 year.
2. Procedures
A. The Progressive Care Charts have been developed based on normal usage under average
environmental conditions. The inspection intervals shall not deviate from the inspection
time limits shown in this Program except as provided below
B. Each inspection interval can be exceeded or ca n be performed early by 10 hours (if time
controlled), or by 30 days (if date controlled). The next operation in sequence remains at
due point from the time the operation was originally scheduled.
C. Maintenance planning is based on aircraft total flight hou rs, starting count from “0” flight
hrs. Additional transition maintenance may be nessesary to adjust the operations on
changed engines, propellers, other components with aircraft scheduled maintenance.
D. Recurrent inspections, tests, required by AD’s, SB’s, SL ’s and not jet included into Primary
Operations or Additional Operations of this Program, will be marked in Maintenance
Planning Program with their indication number.
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
4
3. Inspection Terms and Guidelines
Operation 1
A. Description
Operation 1 consists of all 50 hour interval inspection items and those 100 or 200 hour
interval inspection items to meet their required time interval.
If a component or system is disturbed (due to maintenance being performed) after
completion of an initially r equired operational or functional test, then that specific test must
be re-confirmed after completion of any maintenance prior to returning the system or
component to service. Refer to the appropriate chapter in Service Manual for removal,
installation, operational test and functional tests of components and/or systems.
For items or components requiring lubrication as applicable, refer to SM Sec. 2, Servicing -
General, and Contents for lubricant, lubricating points and method.
B. General Inspection Criteria
(1) During accomplishment of each of the specific inspections within this operation,
additional general inspections of the surrounding areas should be performed while
access is available. These general inspections are intended to detect obvious
conditions which may warrant further action.
C. Post Inspection Checks.
(1) Replace all fairings, doors, floorboard and access covers previously removed.
(2) Inspect Pilot's Operating Handbook and Approved Flight Manual for condition and
latest revision(s) Ensure all required airplane documents are in good condition and
properly displayed.
(3) Conduct a preflight inspection upon completion of this Operation to ensure all
required items are properly serviced; refer to the Pilot's Operating Handbook and
Approved Flight Manual.
(4) Start and operate the engine per the Pilot's Operating Handbook. Perform a complete
operational check on any system that has had maintenance performed on it.
(5) Perform engine shutdown per the Pilot's Operating Handbook and Approved Fli ght
Manual. Inspect the engine compartment for oil and fuel leaks. Pay close attention to
components that have been removed or replaced. All leaks shall be corrected prior to
returning the airplane to service.
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
5
Operation 1
Item
Code
Tasks – based on Cessna Doc D2065-3-13 (Revision 3 from
01. July, 1995)
Mechanic Inspector
B13 Aileron, Elevator, and Rudder Stops - Check for damage
and security N/A
B15 Seat Tracks and Stops - Inspect seat tracks for condition
and security of installation. Check seat tr ack stops for
damage and correct location. Ensure inspection of seat
rails for cracks. Refer to Section 3.
N/A
C1 Wing Surfaces and Tips - Inspect for skin damage, loose
rivets, and condition of paint. N/A
C2 Wing Struts and Strut Fairings - Check for dents, cracks,
loose screws and rivets, and condition of paint. N/A
C7 Vertical and Horizontal Stabilizers, Tips and Tailcone -
Inspect externally for skin damage and condition of paint. N/A
C8 Vertical and Horizontal Stabilizers and Tailcone str ucture -
Inspect bulkheads, spars, ribs, and skins for cracks,
wrinkles, loose rivets, corrosion, or other damage. Inspect
vertical and horizontal stabilizer attach bolts for looseness.
Retorque as necessary. Check security of inspection
covers, fairings, and tips
N/A
E1 Ailerons and Hinges - Check condition, security and
operation N/A
E2 Aileron Structure, Control Rods, Hinges, Balance Weights,
Bellcranks, Linkage, Bolts, Pulleys, and Pulley Brackets -
Check condition, operation, and security o f attachment.
N/A
E5 Aileron Controls - Check freedom of movement and proper
operation through full travel with and without flaps
extended
N/A
F1 Flaps - Check tracks, rollers, and control rods for security
of attachment. Check operation N/A
F2 Flap Actuator Threads - Clean and lubricate. Refer to
paragraph 2-43 for detailed instructions. N/A
G1 Elevator Control - Check freedom of movement and proper
operation through full travel with and without flaps
extended
N/A
G2 Elevator, Hinges, and Cable Attachment - Check condition,
security, and operation. N/A
H1 Elevator Trim Tab and Hinges - Check condition, security,
and operation. N/A
I1 Rudder - Inspect the rudder skins for cracks and loose
rivets, rudder hinges for condition, cracks and security;
hinge bolts, hinge bearings, hinge attach fittings, and
bonding jumper for evidence of damage and wear, failed
fasteners, and security. Inspect the rudder hinge bolts for
proper safetying of nuts with cotter pins. Inspect balance
weight for looseness and the supporting structure for
damage
N/A
I3 Rudder, Tips, Hinges, and Cable Attachment - Check
condition, security, and operation N/A
J1 Cowling - Inspect for cracks, dents, and other damage,
security of cowl fasteners, and cowl mounte d landing lights
for attachment.
N/A
J2 Engine - Inspect for evidence of oil and fuel leaks. Wash
engine and check for security of accessories. N/A
J3 Engine Controls and Linkage - Check general condition,
freedom of movement through full range. Che ck for proper
travel, security of attachment, and for evidence of wear.
Check friction locks for proper operation.
N/A
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
6
J4 Ignition Switch and Electrical Harness - Inspect for
damage, condition, and security. N/A
J5 Firewall Structure - Inspect for wrinkles, damage, cracks,
sheared rivets, etc. Check cowl shock mounts for condition
and security.
N/A
J6 Engine Shock Mounts, Engine Mount Structure, and
Ground Straps - Check condition, security, and alignment. N/A
J7 Induction System - Check security of clamps, tubes, and
ducting. Inspect for evidence of leakage. N/A
J8 Induction Airbox, Valves, Doors, and Controls - Remove
air filter and inspect hinges, doors, seals, and attaching parts
for wear and security. Check operation.
N/A
J9 Induction Air Filter - Remove and clean. Inspect for
damage, and service per Paragraph 2 -22 and 2-22A Filter
may be washed 20 times maximum, cleaned by compressed
air
N/A
J10 Alternate Induction Air System - Check for obstructions,
operation, and security. N/A
J11 Alternator, Mounting Bracket, and Electrical Connections -
Check condition and security. Check alternator belts for
condition and proper adjustment. Check belt tension per
Section 16, Paragraph 16-38.
N/A
J14 Oil Cooler - Check for obstructions, leaks, and security of
attachment N/A
J15 Exhaust System - Inspect for cracks and security. Special
check in area of heat exchanger. Refer to Section 11,
Paragraph 11-73 for inspection procedures.
N/A
J17 Engine-Driven Fuel Pump - Check for evidence of leakage,
security of attachment, and general condition. N/A
J18 Magnetos - Check external condition, security, and
electrical leads for condition. N/A
J21 Ignition Harness and Insulators - Check for proper routing,
deterioration, and condition of terminals. N/A
J22 Spark Plugs - Remove, clean, analyze, test, gap, and rotate
top plugs-to-bottom and bottom plugs-to-top.
J23 Cylinder Compression - Perform differential compression
test
J24 Carburetor - Drain and flush carburetor bowl, clean inlet
strainer, and drain plug. Check general condition and
security
J25 Engine Primer - Check for leakage, operation, and security N/A
J26 Hoses, Metal Lines, and Fittings - Inspect for signs of oil
and fuel leaks. Check for abrasion s, chafing, security,
proper routing and support and for evidence of
deterioration.
N/A
J27 Cold and Hot Air Hoses - Check condition, routing, and
security N/A
J28 Engine Cylinders, Rocker Box Covers, and Pushrod
Housings - Check for fin damage, cracks, oil leakage,
security of attachment, and general condition.
N/A
J29 Engine Baffles and Seals - Check condition and security of
attachment N/A
J30 Crankcase, Oil Sump, and Accessory Section - Inspect for
cracks and evidence of oil leakage. Che ck bolts and nuts
for looseness and retorque as necessary. Check crankcase
breather lines for obstructions, security, and general
condition
N/A
J31 Engine Oil With Oil Filter - Drain oil sump and oil cooler,
replace filter, and refill with recommende d grade aviation
oil. First 25 hours: Drain oil sump, clean pressure screen or
replace oil filter, and refill with MIL-L-6080 aviation grade
straight mineral oil. Beginning with the 50 -hour oil change
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
7
and thereafter, refill oil sump with MIL-L-22851 ashless
dispersant oil.
K1 Fuel Tanks or Integral Fuel Bays - Check for evidence of
leakage and condition of fuel caps, adapters, and placards. N/A
K3 Fuel System - Inspect plumbing and components for
mounting and security N/A
K4 Fuel Tank or Bay Drains - Drain water and sediment N/A
K5 Fuel Tank Vent Lines and Vent Valves - Check vents for
obstruction and proper positioning. N/A
K7 Fuel Strainer, Drain Valve, and Controls - Check freedom
of movement, security, and proper operation. Disassemble,
flush, and clean screen and bowl.
N/A
L1 Propeller Mounting - Check for security of installation N/A
L2 Propeller Blades - Inspect for cracks, dents, nicks,
scratches, erosion, corrosion, or other damage. N/A
L3 Spinner - Check general condition and attachment N/A
L4 Spinner and Spinner Bulkhead - Remove spinner, wash,
and inspect for cracks and fractures. N/A
L5 Propeller Mounting Bolts - Inspect mounting bolts and
safety-wire for signs of looseness. Retorque mounting
bolts as required
N/A
L6 Propeller Hub - Check general condition N/A
M2 Heater Components, Inlets, and Outlets - Inspect all lines,
connections, ducts, clamps, seals, and gaskets for
condition, restriction, and security.
N/A
M4 Pitot Tube and Stall Warning Vane - Check for condition
and obstructions N/A
N3 Vacuum Pump - Check for condition and security. Check
vacuum system breather line for obstructions, condition,
and security
N/A
O4 Battery - Check general condition and security. Check
level of electrolyte. N/A
O5 Battery Box and Cables - Clean and remove any corrosion.
Check cables for routing, support, and security of
connections.
N/A
O7 Alternator Control Unit - Inspect wiring, mounting,
condition, and wire routing N/A
O10 External Power Receptacle a nd Power Cables - Inspect for
condition and security. N/A
End of Operation 1 items
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
8
Operation 2
Item
Code
Tasks – based on Cessna Doc D2065-3-13 (Revision 3 from
01. July, 1995)
Mechanic Inspector
B1 Fuselage Surface - Inspect for skin damage, loose rivets,
condition of paint, and check pitot -static ports and drain
holes for obstruction. Inspect covers and fairings for
security
N/A
B6 Emergency Locator Transmitter - Inspect for security of
attachment and check operation by verifying transmi tter
output Check cumulative time and useful life of batteries
in accordance with FAR Part 91.207. Refer to Section 16 -
Emergency Locator Transmitter - Checkout Interval.
N/A
B8 Pilot's and Copilot's Inertia Reels - Inspect for security of
installation, proper operation, and evidence of damage. N/A
B9
B10
Seats, Seat Belts, and Shoulder Harnesses - Check general
condition and security. Check operation of seat stops and
adjustment mechanism. Inspect belts for condition and
security of fasteners.
N/A
B10 Windows, Windshield, Doors, and Seals - Inspect general
condition. Check latches, hinges, and seals for condition,
operation, and security of attachment.
N/A
B12 Flight Controls - Check freedom of movement and proper
operation through full travel with and without flaps
extended. Check electric trim controls for operation (as
applicable).
N/A
B14 Portable Hand Fire Extinguisher - Inspect for proper
operating pressure, condition, security of installation, and
servicing date.
N/A
B15 Seat Tracks and Stops - Inspect seat tracks for condition
and security of installation. Check seat track stops for
damage and correct location. Ensure inspection of seat
rails for cracks. Refer to Section 3.
N/A
B17 Fuel Line and Selector Valve Drain(s) - Remove plug and
drain N/A
D1 Brakes, Master Cylinders, and Parking Brake - Check
master cylinders and parking brake mechanism for
condition and security. Check fluid level and test operation
of toe and parking brake.
N/A
D 2 Main Gear Tubular Struts - Inspect for cracks, dents,
corrosion, condition of paint or other damage. Check axles
for condition and security.
N/A
D 4. Wheels, Brake Discs, and Linings - Inspect for wear,
cracks, warps, dents, or other damage. Check wheel
through-bolts and nuts for looseness
N/A
D 5 Tires - Check tread wear and general condition. Check for
proper inflation. N/A
D 6 Wheel Fairings, Strut Fairings, and Cuffs - Check for
cracks, dents, and condition of paint N/A
D 7 Main landing Gear Attachment Structur e - Check for
damage, cracks, loose rivets, bolts and nuts and security of
attachment
N/A
D 8 Nose Gear Steering Mechanism - Check for wear, security,
and proper rigging. N/A
D 9 Nose Gear - Inspect torque links, steering rods, and boots
for condition and security of attachment. Check strut for
evidence of leakage and proper extension. Check strut
barrel for corrosion, pitting, and cleanliness. Check
shimmy damper and/or bungees for operation, leakage,
attach points for wear and security.
N/A
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
9
D 10 Nose Gear Fork - Inspect for cracks, general condition, and
security of attachment N/A
D 12 Nose Gear Attachment Structure - Inspect for cracks,
corrosion, or other damage and security of attachment N/A
H 2 Elevator Trim System - Check cables, push-pull rods,
bellcranks, pulleys, turnbuckles, fairleads, rub strips, etc.
for proper routing, condition, and security
N/A
J 1 Cowling - Inspect for cracks, dents, and other damage,
security of cowl fasteners, and cowl mounted landing ligh ts
for attachment
N/A
J 2 Engine - Inspect for evidence of oil and fuel leaks. Wash
engine and check for security of accessories. N/A
J 3 Engine Controls and Linkage - Check general condition,
freedom of movement through full range. Check for proper
travel, security of attachment, and for evidence of wear.
Check friction locks for proper operation.
N/A
J 7 Induction System - Check security of clamps, tubes, and
ducting. Inspect for evidence of leakage. N/A
J 9 Induction Air Filter - Remove and clean. Inspect for
damage, and service per Paragraph 2 -22 and 2-22A Filter
may be washed 20 times maximum, cleaned by compressed
air
N/A
J 10 Alternate Induction Air System - Check for obstructions,
operation, and security N/A
J 11 Alternator, Mounting Bracket, and Electrical Connections -
Check condition and security. Check alternator belts for
condition and proper adjustment. Check belt tension per
Section 16, Paragraph 16-38.
N/A
J 13 Starter, Starter Solenoid, and Electrical Connections -
Check solenoid and electrical connections N/A
J 14 Oil Cooler - Check for obstructions, leaks, and security of
attachment N/A
J 15 Exhaust System - Inspect for cracks and security. Special
check in area of heat exchanger. Refer to Section 11,
Paragraph 11-73 for inspection procedures
N/A
J 26 Hoses, Metal Lines, and Fittings - Inspect for signs of oil
and fuel leaks. Check for abrasions, chafing, security,
proper routing and support and for evidence of
deterioration.
N/A
J 29 Engine Baffles and Seals - Check condition and security of
attachment N/A
J 31 Engine Oil With Oil Filter - Drain oil sump and oil cooler,
replace filter, and refill with recommended grade aviation
oil. First 25 hours: Drain oil sump, clean pressure screen or
replace oil filter, and refill with MIL-L-6080 aviation grade
straight mineral oil. Beginning with the 50 -hour oil change
and thereafter, refill oil sump with MIL-L-22851 ashless
dispersant oil.
K 4 Fuel Tank or Bay Drains - Drain water and sediment. N/A
K 6 Fuel Selector Valve - Check controls for detent in each
position, security of attachment, and for proper placarding N/A
L 1 Propeller Mounting - Check for security of installation. N/A
L 2 Propeller Blades - Inspect for cracks, dents, nicks,
scratches, erosion, corrosion, or other damage N/A
L 3 Spinner - Check general condition and attachment N/A
M 4 Pitot Tube and Stall Warning Vane - Check for condition
and obstructions. N/A
N 1 Vacuum System - Inspect for condition and security. N/A
N 2 Vacuum System Hoses - Inspect for hardness,
deterioration, looseness, or collapsed hoses N/A
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
10
N 4 Vacuum System Air Filter - Inspect for damage,
deterioration and contamination. Clean or replace, if
required.
N/A
N 5 Vacuum System relief Valve - Inspect for condition and
Security. Replace filter N/A
N 6 Instruments - Check general condition and markings for
legibility N/A
O 2 Instrument, Cabin, Navigation, Beacon, Strobe, and
Landing Lights - Check operation, condition of lens, and
security of attachment.
N/A
O 3 Circuit Breakers and Fuses - Check operation and
condition. Check for required number of spare fuses N/A
Q 1 Brakes - Test toe brakes and parking brake for proper
operation. N/A
End of Operation 2 items
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
11
Operation 3
Item
Code
Tasks – based on Cessna Doc D2065-3-13 (Revision 3 from
01. July, 1995)
Mechanic Inspector
B 13 Aileron, Elevator, and Rudder Stops - Check for damage
and security. N/A
B 15 Seat Tracks and Stops - Inspect seat tracks for conditi on
and security of installation. Check seat track stops for
damage and correct location. Ensure inspection of seat
rails for cracks. Refer to Section 3.
N/A
C 1 Wing Surfaces and Tips - Inspect for skin damage, loose
rivets, and condition of paint N/A
C 2 Wing Struts and Strut Fairings - Check for dents, cracks,
loose screws and rivets, and condition of paint. N/A
C 3 Wing Spar and Wing Strut Fittings - Check for evidence of
wear. Check attach bolts for indications of looseness and
retorque as required.
N/A
C 4 Wing Structure - Inspect spars, ribs, skins, and stringers for
cracks, wrinkles, loose rivets, corrosion, or other damage. N/A
C 5 Metal Lines, Hoses, Clamps, and Fittings - Check for leaks,
condition, and security. Check for prope r routing and
support
N/A
C 6 Wing Access Plates - Check for damage and security of
installation N/A
C 7 Vertical and Horizontal Stabilizers, Tips and Tailcone -
Inspect externally for skin damage and condition of paint. N/A
C 8 Vertical and Horizontal Stabilizers and Tailcone structure -
Inspect bulkheads, spars, ribs, and skins for cracks,
wrinkles, loose rivets, corrosion, or other damage. Inspect
vertical and horizontal stabilizer attach bolts for looseness.
Retorque as necessary. Check se curity of inspection
covers, fairings, and tips.
N/A
E 1 Ailerons and Hinges - Check condition, security and
operation. N/A
E 2 Aileron Structure, Control Rods, Hinges, Balance Weights,
Bellcranks, Linkage, Bolts, Pulleys, and Pulley Brackets -
Check condition, operation, and security of attachment.
N/A
E 3 Ailerons and Cables - Check operation and security of
stops. Check cables for tension, routing, fraying, corrosion,
and turnbuckle safety. Check travel if cable tension requires
adjustment or if stops are damaged. Check fairleads and rub
strips for condition.
N/A
E 5 Aileron Controls - Check freedom of movement and proper
operation through full travel with and without flaps
extended
N/A
F 1 Flaps - Check tracks, rollers, and control rod s for security
of attachment. Check operation N/A
F 2 Flap Actuator Threads - Clean and lubricate. Refer to
paragraph 2-43 for detailed instructions. N/A
F 3 Flap Structure, Linkage, Bellcranks, Pulleys, and Pulley
Brackets – Check for condition, operation and security. N/A
F 4 Wing Flap Control – Check operation through full travel
and observe Flap Position indicator for proper indication N/A
F 5 Flaps and Cables – Check cables for proper tension,
routing, fraying, corrosion, and turnbuckle sa fety. Tension,
routing, fraying, corrosion, and turnbuckle Check travel if
cable tension requires adjustment.
N/A
F 7 Flap Motor, Actuator, and Limit Switches (electric flaps) –
Check wiring and terminals for condition and security.
Check actuator for condition and security.
N/A
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
12
G 1 Elevator Control – Check freedom of movement and proper
operation through full travel with and without flaps
extended
N/A
G 2 Elevator, Hinges, and Cable Attachment – Check condition,
security, and operation N/A
H 1 Elevator Trim Tab and Hinges – Check condition, security,
and operation N/A
H 4 Elevator Trim Tab Stop Blocks – Inspect for damage and
security N/A
H 6 Elevator Trim Tab Actuator – Free-Play limits inspection.
Refer to Section 9 for cleaning, ins pection, and repair
procedures
N/A
I 1 Rudder – Inspect the rudder skins for cracks and loose
rivets, rudder hinges for condition, cracks and security;
hinge bolts, hinge bearings, hinge attach fittings, and
bonding jumper for evidence of damage and wear, failed
fasteners, and security. Inspect the rudder hinge bolts for
proper safetying of nuts with cotter pins. Inspect balance
weight for looseness and the supporting structure for
damage.
N/A
I 3 Rudder, Tips, Hinges, and Cable Attachment – Check
condition, security, and operation. N/A
I 4 Rudder – Check internal surfaces for corrosion, condition
of fasteners, and balance weight attachment. N/A
J 1 Cowling – Inspect for cracks, dents, and other damage,
security of cowl fasteners, and cowl mounted landing lights
for attachment
N/A
J 2 Engine – Inspect for evidence of oil and fuel leaks. Wash
engine and check for security of accessories. N/A
J 3 Engine Controls and Linkage – Check general condition,
freedom of movement through full ran ge. Check for proper
travel, security of attachment, and for evidence of wear.
Check friction locks for proper operation
N/A
J 4 Ignition Switch and Electrical Harness – Inspect for
damage, condition, and security. N/A
J 7 Induction System – Check security of clamps, tubes, and
ducting. Inspect for evidence of leakage N/A
J 8 Induction Airbox, Valves, Doors, and Controls – Remove
air filter and inspect hinges, doors, seals, and attaching parts
for wear and security. Check operation.
N/A
J 9 Induction Air Filter – Remove and clean. Inspect for
damage, and service per Paragraph 2 -22 and 2-22A Filter
may be washed 20 times maximum, cleaned by compressed
air
N/A
J 10 Alternate Induction Air System – Check for obstructions,
operation, and security N/A
J 11 Alternator, Mounting Bracket, and Electrical Connections –
Check condition and security. Check alternator belts for
condition and proper adjustment. Check belt tension per
Section 16, Paragraph 16-38.
N/A
J 14 Oil Cooler – Check for obstructions, leaks, and security of
attachment N/A
J 15 Exhaust System – Inspect for cracks and security. Special
check in area of heat exchanger. Refer to Section 11,
Paragraph 11-73 for inspection procedures.
N/A
J 17 Engine-Driven Fuel Pump – Check for evidence of leakage,
security of attachment, and general condition N/A
J 18 Magnetos – Check external condition, security, and
electrical leads for condition. N/A
J 21 Ignition Harness and Insulators – Check for proper routing,
deterioration, and condition of terminals N/A
J 22 Spark Plugs – Remove, clean, analyze, test, gap, and rotate
top plugs-to-bottom and bottom plugs-to-top
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
13
J 24 Carburetor – Drain and flush carburetor bowl, clean inlet
strainer, and drain plug. Check general conditio n and
security
J 25 Engine Primer – Check for leakage, operation, and security N/A
J 26 Hoses, Metal Lines, and Fittings – Inspect for signs of oil
and fuel leaks. Check for abrasions, chafing, security,
proper routing and support and for evidence of
N/A
J 27 Cold and Hot Air Hoses – Check condition, routing, and
security N/A
J 28 Engine Cylinders, Rocker Box Covers, and Pushrod
Housings – Check for fin damage, cracks, oil leakage,
security of attachment, and general condition.
N/A
J 29 Engine Baffles and Seals – Check condition and security of
attachment N/A
J 30 Crankcase, Oil Sump, and Accessory Section – Inspect for
cracks and evidence of oil leakage. Check bolts and nuts
for looseness and retorque as necessary. Check crankcase
breather lines for obstructions, security, and general
condition.
N/A
J 31 Engine Oil With Oil Filter – Drain oil sump and oil cooler,
replace filter, and refill with recommended grade aviation
oil. First 25 hours: Drain oil sump, clean pressure screen o r
replace oil filter, and refill with MIL-L-6080 aviation grade
straight mineral oil. Beginning with the 50 -hour oil change
and thereafter, refill oil sump with MIL-L-22851 ashless
dispersant oil.
K 1 Fuel Tanks or Integral Fuel Bays – Check for evidence of
leakage and condition of fuel caps, adapters, and placards. N/A
K 3 Fuel System – Inspect plumbing and components for
mounting and security N/A
K 4 Fuel Tank or Bay Drains – Drain water and sediment N/A
K 5 Fuel Tank Vent Lines and Vent Valve s – Check vents for
obstruction and proper positioning. N/A
L 1 Propeller Mounting – Check for security of installation N/A
L 2 Propeller Blades - Inspect for cracks, dents, nicks,
scratches, erosion, corrosion, or other damage N/A
L 3 Spinner - Check general condition and attachment N/A
L 4 Spinner and Spinner Bulkhead - Remove spinner, wash,
and inspect for cracks and fractures N/A
M 2 Heater Components, Inlets, and Outlets - Inspect all lines,
connections, ducts, clamps, seals, and gaskets f or condition,
restriction, and security.
N/A
M 4 Pitot Tube and Stall Warning Vane - Check for condition
and obstructions N/A
N 3 Vacuum Pump - Check for condition and security. Check
vacuum system breather line for obstructions, condition,
and security
N/A
O 4 Battery - Check general condition and security. Check
level of electrolyte N/A
O 5 Battery Box and Cables - Clean and remove any corrosion.
Check cables for routing, support, and security of
connections.
N/A
End of Operation 3 items
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
14
Operation 4
Item
Code
Tasks – based on Cessna Doc D2065-3-13 (Revision 3 from
01. July, 1995)
Mechanic Inspector
A 1 Placards and Decals - Inspect presence, legibility, and
security. Consult Pilot's Operating Handbook and FAA -
Approved Airplane Flight Manual for required placards
N/A
B 1 Fuselage Surface - Inspect for skin damage, loose rivets,
condition of paint, and check pitot -static ports and drain
holes for obstruction. Inspect covers and fairings for
security
N/A
B 2 Internal Fuselage Structure - Inspect bulkheads, doorposts,
stringers, doublers, and skins for corrosion, cracks,
buckles, and loose rivets, bolts and nuts
N/A
B 3 Control Wheel Lock - Check general condition and
operation N/A
B 4 Fuselage Mounted Equipment - Check for general condition
and security of attachment N/A
B 5 Antennas and Cables - Inspect for security of attachment,
connection, and condition N/A
B 6 Emergency Locator Transmitter - Inspect for security of
attachment and check operation by verifying tran smitter
output. Check cumulative time and useful life of batteries
in accordance with FAR Part 91.207. Refer to Section 16 -
Emergency Locator Transmitter - Checkout Interval
N/A
B 7 Instrument Panel Shock Mounts, Ground Straps, and
Covers - Inspect for deterioration, cracks, and security of
attachment.
N/A
B 8 Pilot's and Copilot's Inertia Reels - Inspect for security of
installation, proper operation, and evidence of damage. N/A
B 9 Seats, Seat Belts, and Shoulder Harnesses - Check general
condition and security. Check operation of seat stops and
adjustment mechanism. Inspect belts for condition and
security of fasteners
N/A
B 10 Windows, Windshield, Doors, and Seals - Inspect general
condition. Check latches, hinges, and seals for condit ion,
operation, and security of attachment
N/A
B 12 Flight Controls - Check freedom of movement and proper
operation through full travel with and without flaps
extended. Check electric trim controls for operation (as
applicable).
N/A
B 14 Portable Hand Fire Extinguisher - Inspect for proper
operating pressure, condition, security of installation, and
servicing date.
N/A
B 15 Seat Tracks and Stops - Inspect seat tracks for condition
and security of installation. Check seat track stops for
damage and correct location. Ensure inspection of seat
rails for cracks. Refer to Section 3.
N/A
B 16 Control Column - Inspect pulleys, cables, sprockets,
bearings, chains, bungees, and turnbuckles for condition
and security
N/A
B 17 Fuel Line and Selector Valve Drain(s) - Remove plug and
drain N/A
D 1 Brakes, Master Cylinders, and Parking Brake - Check
master cylinders and parking brake mechanism for
condition and security. Check fluid level and test operation
of toe and parking brake.
N/A
D 2 Main Gear Tubular Struts - Inspect for cracks, dents,
corrosion, condition of paint or other damage. Check axles
for condition and security.
N/A
ES-ECR MAINTENANCE PROGRAM
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D 4 Wheels, Brake Discs, and Linings - Inspect for wear,
cracks, warps, dents, or other damage. Check wheel
through-bolts and nuts for looseness
N/A
D 5 Tires - Check tread wear and general condition. Check for
proper inflation N/A
D 6 Wheel Fairings, Strut Fairings, and Cuffs - Check for
cracks, dents, and condition of paint. N/A
D 7 Main landing Gear Attachment Structure - Check for
damage, cracks, loose rivets, bolts and nuts and security of
attachment
N/A
D 9 Nose Gear - Inspect torque links, steering rods, and boots
for condition and security of attachment. Check strut for
evidence of leakage and proper extension. Check strut
barrel for corrosion, pitting, and cleanliness. Check shimmy
damper and/or bungees for operation, leakage, and
attach points for wear and security
N/A
D 11 Wheel Bearings - Clean, inspect and lube
D 12 Nose Gear Attachment Structure - Inspect for cracks,
corrosion, or other damage and security of attachment N/A
G 3 Elevator Control System - Inspect pulleys, cables,
sprockets, bearings, chains, and tumbuckles for condition,
security, and operation.
N/A
H 2 Elevator Trim System - Check cables, push-pull rods,
bellcranks, pulleys, tumbuckles. fairleads, rub strips, etc.
for proper routing, condition, and security
N/A
H 3 Trim Controls and Indicators - Check freedom of
movement and proper operation through full t ravel. Check
pulleys, cables, sprockets, bearings, chains, bungees, and
tumbuckles for condition and security. Check electric trim
controls for operation as applicable.
N/A
I 2 Rudder Pedals and Linkage - Check for general condition,
proper rigging, and operation. Check for security of
attachment
N/A
J 1 Cowling - Inspect for cracks, dents, and other damage,
security of cowl fasteners, and cowl mounted landing lights
for attachment
N/A
J 2 Engine - Inspect for evidence of oil and fuel leaks. Was h
engine and check for security of accessories N/A
J 3 Engine Controls and Linkage - Check general condition,
freedom of movement through full range. Check for proper
travel, security of attachment, and for evidence of wear.
Check friction locks for proper operation.
N/A
J 7 Induction System - Check security of clamps, tubes, and
ducting. Inspect for evidence of leakage N/A
J 9 Induction Air Filter - Remove and clean. Inspect for
damage, and service per Paragraph 2 -22 and 2-22A Filter
may be washed 20 times maximum, cleaned by compressed
air
N/A
J 10 Alternate Induction Air System - Check for obstructions,
operation, and security. N/A
J 11 Alternator, Mounting Bracket, and Electrical Connections -
Check condition and security. Check alterna tor belts for
condition and proper adjustment. Check belt tension per
Section 16. Paragraph 16-38
N/A
J 13 Starter, Starter Solenoid, and Electrical Connections -
Check solenoid and electrical connections
J 14 Oil Cooler - Check for obstructions, leaks, and security of
attachment. N/A
J 15 Exhaust System - Inspect for cracks and security. Special
check in area of heat exchanger. Refer to Section 11,
Paragraph 11-73 for inspection procedures.
N/A
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16
J 26 Hoses, Metal Lines, and Fittings - Inspect for signs of oil
and fuel leaks. Check for abrasions, chafing, security,
proper routing and support and for evidence of deterioration
N/A
J 29 Engine Baffles and Seals - Check condition and security of
attachment N/A
J 31 Engine Oil With Oil Filter - Drain oil sump and oil cooler,
replace filter, and refill with recommended grade aviation
oil. First 25 hours: Drain oil sump, clean pressure screen or
replace oil filter, and refill with MIL-L-6080 aviation grade
straight mineral oil. Beginning with the 50-hour oil change
and thereafter, refill oil sump with MIL-L-22851 ashless
dispersant oil.
K 4 Fuel Tank or Bay Drains - Drain water and sediment. N/A
K 6 Fuel Selector Valve - Check controls for detent in each
position, security of attachment, and for proper placarding N/A
L 1 Propeller Mounting - Check for security of installation. N/A
L 2 Propeller Blades - Inspect for cracks, dents, nicks,
scratches, erosion, corrosion, or other damage. N/A
L 3 Spinner - Check general condition and attachment N/A
M 3 Cabin Heat and Ventilation Controls - Check freedom of
movement through full travel. Check friction locks for
proper operation.
N/A
M 4 Pitot Tube and Stall Warning Vane - Check for condition
and obstructions N/A
N 1 Vacuum System - Inspect for condition and security N/A
N 2 Vacuum System Hoses - Inspect for hardness,
deterioration, looseness, or collapsed hoses. N/A
N 4 Vacuum System Air Filter - Inspect for damage,
deterioration and contamination. Clean or replace, if
required.
N/A
N 5 Vacuum System relief Valve - Inspect for condition and
Security. Replace filter N/A
N 6 Instruments - Check general condition and markings for
legibility N/A
N 7 Instrument Lines, Fittings, Ducting, and Instrument P anel
Wiring - Check for proper routing, support, and security of
attachment
N/A
N 8 Static System - Inspect for security of installation,
cleanliness, and evidence of damage N/A
N 9 Navigation Indicators, Controls, and Components - Inspect
for condition and security N/A
N 12 Instrument Panel Mounted Avionics Units (Including Audio
Panel, VHF Nav/Com(s), ADF, Transponder, DME, and
Compass System) - Inspect for deterioration, cracks, and
security of instrument panel mounts. Inspect for security o f
electrical connections, condition, and security of wire
routing
N/A
N 13 Avionics Operating Controls - Inspect for security and
proper operation of controls and switches and ensure that
all digital segments will illuminate properly.
N/A
N 14 Remote Mounted Avionics - Inspect for security of units
and electrical connectors, condition and security of wire
routing. Also, check for evidence of damage and
cleanliness.
N/A
N 15 Microphones, Headsets, and Jacks - Inspect for
cleanliness, security, and evidence of damage N/A
N 16 Magnetic Compass - Inspect for security of installation,
cleanliness, and evidence of damage N/A
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
17
O 1 General Airplane and System Wiring - Inspect for proper
routing, chafing, broken or loose terminal s, general
condition, broken or inadequate clamps, and sharp bends
in wiring.
N/A
O 2 Instrument, Cabin, Navigation, Beacon, Strobe, and
Landing Lights - Check operation, condition of lens, and
security of attachment
N/A
O 3 Circuit Breakers and Fuses - Check operation and
condition. Check for required number of spare fuses N/A
O 6 Switch and Circuit Breaker Panel, Terminal Blocks, and
Junction Boxes - Inspect wiring and terminals for condition
and security
N/A
O 8 Switches - Check operation, terminals, wiring, and
mounting for conditions, security, and interference N/A
O 9 Instrument Panel and Control Pedestal - Inspect wiring,
mounting, and terminals for condition and security. Check
resistance between stationary panel and instrument panel
for proper ground.
N/A
Q 1 Brakes - Test toe brakes and parking brake for proper
operation. N/A
End of Operation 4 items
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
18
A. Additional Operations
Description
If a component or system is disturbed (due to maintenance being performed) after
completion of an initially required operational or functional test, then that specific test must
be re-confirmed after completion of any maintenance prior to returning the system or
component to service. Refer to the appropriate chapter in Service Manual for remo val,
installation, operational test and functional tests of components and/or systems.
For items or components requiring lubrication as applicable, refer to SM Chapter 2,
Servicing - General, and Contents for lubricant, lubricating points and method.
General Inspection Criteria
(1) During accomplishment of each of the specific inspections within operations,
additional general inspections of the surrounding areas should be performed while
access is available. These general inspections are intended to detect o bvious conditions
which may warrant further action.
(2) These operations should be performed concurrently with one of the operations, one thru
four, which falls nearest to its due point.
Operation 5 – every 100 hrs or 1 year
Tasks – based on Cessna Doc. D2065-3-13 (rev.3 01. July,
1995).
Mechanic Inspector
J18 Check magnetos timing to engine and internal timing if
requires adjustment first 100 hrs and every 100 hours or one
year
N/A
End of Operation 5 Inspection Items
Operation 6 – 100 hrs or 90 days
Tasks – based on Cessna Doc. D2065-3-13 (rev.3 01. July,
1995).
Mechanic Inspector
O 4a Battery - Check general condition and security. Check level
of electrolyte level and clean battery box each 100 hrs or 90
days.
N/A
End of Operation 6 Inspection Items
Operation 7 – every 1 year
Tasks – based on Cessna Doc. D2065-3-13 (rev.3 01. July,
1995).
Mechanic Inspector
K 8 Fuel Quantity Indicators - Check for damage, security of
installation, and perform accuracy test each 1 year.
End of Operation 7 Inspection Items
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
19
Operation 8 – every 400 hrs or 1 year
Tasks – based on Cessna Doc. D2065-3-13 (rev.3 01. July,
1995).
Mechanic Inspector
B 11 Upholstery, Headliner, Trim, and Carpeting - Check
condition and clean as required Each 400 hrs or each 1 year. N/A
D 3 Brake Lines, Wheel Cylinders, Hoses, Clamps, and Fittings
- Check for leaks, condition, and security and hoses for
bulges and deterioration. Check brake lines and hoses for
proper routing and support. Each 400 hrs or each 1 year
N/A
M 1 Ventilation System - Inspect clamps, hoses, and valves for
condition and security. Each 400 hrs or each 1 year N/A
End of Operation 8 Inspection Items
Operation 9 – every 500 hrs
Tasks – based on Cessna Doc. D2065-3-13 (rev.3 01. July,
1995).
Mechanic Inspector
J 13 Starter - inspect the commutator and brushes each 500
hours.
J 12 Alternator - Check brushes, leads, commutator or slip ring
for wear.
J 20 1. Inspect contact points for condition and adjust or replace
as required.
2. Inspect carbon brush, high-tension lead, and distributor
block for condition and clean or replace as re -quired.
3. Inspect impulse coupling and pawls for condition and
replace as required. Use light pressure only, do not force
pin (or drill bit) when checking pawls.
4. Inspect bearings and lubricate, replace bearings, if
required.
5. Lubricate contact point cam.
Each 500 hours and eng. overhaul. Ref. Overhaul and
Maintenance Manual, Publication No. 1037C1 -13, covering
Model 4200/6200 series magnetos.
N 4 Vacuum System Air Filter – Replace every 500 hrs
End of Operation 9 Inspection Items
Operation 10 – every 500 hrs or 1 year
Tasks – based on Cessna Doc. D2065-3-13 (rev.3 01. July,
1995).
Mechanic Inspector
J 9 Induction Air Filter - Replace filter each 500 hours or 1
year whichever comes first
End of Operation 10 Inspection Items
ES-ECR MAINTENANCE PROGRAM
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20
Operation 11 – every 1000 hrs
Tasks – based on Cessna Doc. D2065-3-13 (rev.3 01. July,
1995).
Mechanic Inspector
K 2 Fuel Tanks or Integral Fuel Bays - Drain fuel and check
tank interior and outlet screens every 1000 hrs.
End of Operation 11 Items
Operation 12 – every 1000 hrs or 3years
Tasks – based on Cessna Doc. D2065-3-13 (rev.3 01. July,
1995).
Mechanic Inspector
H 5 Elevator Trim Tab Actuator - Clean, lubricate, and check
free play. Lubricate the actuator each 1000 hours or 3 years,
whichever comes first.
End of Operation 12 Inspection Items
Operation 13 – every 2 years
Tasks – based on Cessna Doc. D2065-3-13 (rev.3 01. July,
1995).
Mechanic Inspector
N 10 Airspeed Indicator, Vertical Speed Indicator, and Magnetic
Compass - Calibrate. Each 2 years
N 11 Altimeter and Static System - Inspect in accordance with
FAR Part 91.411. Each 2 years
End of Operation 13 Inspection Items
Operation 14
Engine condition evaluation - every 100 hrs or 1 year
before TBO extension:
Mechanic Inspector
1. Engine - Inspect for evidence of oil and fuel leaks. Wash
engine and check for security of accessories.
2. Engine Cylinders, Rocker Box Covers, and Pushrod
Housings - Check for fin damage, cracks, oil leakage,
security of attachment, and general condition.
3. Crankcase, Oil Sump, and Accessory Section - Inspect for
cracks and evidence of oil leakage. Check bolts and nuts for
looseness and retorque as necessary. Check crankcase
breather lines for obstructions, security, and general
condition.
4. Engine Shock Mounts, Engine Mount Structure, and
Ground Straps - Check condition, security, and alignment.
5. Hoses, Metal Lines, and Fittings - Inspect for signs of oil
and fuel leaks. Check for abrasions, chafing, security,
proper routing and support and for evidence of
deterioration.
6. Ignition Harness and Insulators - Check for proper routing,
deterioration, and condition of termina ls.
7. Propeller – check radial and axial play
8. Spark plugs – check for condition, normal color, evidence
of oil
9. Check oil consumption
10. Cylinder Compression - Perform differential compression
test. If there is weak cylinder compression, refer to Chapter
71, IO-360-L2A Troubleshooting, for further procedures.
11. Cylinders, Piston Head, Valves Seats - Perform borescope
inspection
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
21
12. Engine Oil – Drain oil sump and oil cooler. Check for metal
particles or foreign material in filter, on sump drain plug,
and on engine suction screen. Ref. Textron/Lycoming S.I.
1492 and SB 480 latest revision
13. Engine run
End of Operation 14 Inspection Items
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
22
Cessna Mandated Replacement Time Limits Operations
Operation TL1
Tasks – based on Cessna Doc. D2065-3-13 (rev.3
01. July, 1995).
Part number Mechanic Inspector
1 Engine TBO – 2000 hrs, if accumulates more
than 40 hrs per month from installation, add 200
hrs. Ref.: SI 1009 latest revision.
End of Operation TL1
Operation TL2
Tasks – based on Cessna Doc. D2065-3-13 (rev.3
01. July, 1995).
Part number Mechanic Inspector
1 Magnetos TBO – 2000+200
End of Operation TL2
Operation TL3
Tasks – based on Cessna Doc. D2065-3-13 (rev.3
01. July, 1995).
Part number Mechanic Inspector
1 Engine Compartment Flexible Fluid Carrying
Rubber Hoses (Cessna Installed) Except Drain
Hoses - every 5 years or at eng overhaul
(2000+200 hrs) whichever occurs first
End of Operation TL3
Operation TL4
Tasks – based on Cessna Doc. D2065-3-13 (rev.3
01. July, 1995).
Part number Mechanic Inspector
1 Engine Flexible Hoses (Lycoming Installed)
Replace at eng. Overhaul - 2000+200 hrs
End of Operation TL4
Operation TL5
Tasks – based on Cessna Doc. D2065-3-13 (rev.3
01. July, 1995).
Part number Mechanic Inspector
1 Propeller – TBO 2000 hrs or 72 months. Ref.:
McCauley SB 137 latest revision
End of Operation TL5
Operation TL6
Tasks – based on Cessna Doc. D2065-3-13 (rev.3
01. July, 1995).
Part number Mechanic Inspector
1 Locator Beacon Battery Pack. Ref. FAR 91.207
End of Operation TL6
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
23
Flyable Storage
A. The flyable storage is a maximum of 30 days storage with no engine operation and/or the first 25
hours of intermittent engine operation.
During the 30 day nonoperational storage or the first 25 hours of intermittent engine operation, every
seventh day the propeller shall be rotated through five revolutions, without running the engine. If the
aircraft is stored outside, tie -down in accordance with paragraph 2-7SM. In addition, the pitot tube,
static air vents, air vents, openings in the engine cowling, and other similar openings shall have
protective covers installed to prevent entry of foreign material. After 30 days, aircraft should be fl own
for 30 minutes or ground run-up until oil has reached operating temperature (lower green arc range).
CAUTION. Excessive ground operation shall be avoided.
B. RETURNING AIRCRAFT TO SERVICE. After flyable storage, returning the aircraft to service is
accomplished by performing a thorough preflight inspection. At the end of the first 25 hours of engine
operation, drain engine oil and clean oil screens (or change external oil filter). Service engine with
correct grade and quantity of engine oil. See figure 2-4 and paragraph 2-21 for correct grade of engine
oil.
Temporary Storage
A. Temporary airplane storage .
(1) Temporary storage is defined as aircraft in a nonoperational status for a maximum of 90 days. The
aircraft is constructed of corrosion resist ant alclad aluminum, which will last indefinitely under normal
conditions if kept clean, however, these alloys are subject to oxidation. The first indication of corrosion
on unpainted surfaces is in the form of white deposits or spots. On painted surfaces, the paint is
discolored or
blistered. Storage in a dry hangar is essential to good preservation and should be procured, if possible.
Varying conditions will alter the measures of preservation, but under normal conditions in a dry
hangar, and for storage periods not to exceed 90 days, the following methods of treatment are
suggested:
a. Fill fuel tanks or bays with the correct grade of gasoline.
Warning. during all fueling procedures, fire fighting equipment must be available. Two ground wires
from different points on the airplane to separate approved ground stakes shall be used to prevent
accidental disconnection of one ground wire. ensure that fueling nozzle is grounded to the airplane.
Tie-down rings should be used as grounding points for all grounding wires during refueling procedures.
b. Clean and wax aircraft thoroughly.
c. Clean any oil or grease from tires and coat tires with a tire preservative. Cover tires to
protect against grease and oil.
d. Either block up fuselage to relieve pressure on tire s or rotate wheels every 30 days to
change supporting points and prevent flat spotting the tires.
e. Lubricate all airframe items and seal or cover all openings which could allow moisture
and/or dust to enter.
f. Remove battery and store in a cool, dry p lace; service battery periodically and charge as
required.
g. Disconnect spark plug leads and remove upper and lower spark plugs from each cylinder.
h. Using a portable pressure sprayer, atomize spray preservative oil through the upper spark
plug hole of each cylinder with the piston in a down position. Rotate crankshaft as each pair of
cylinders is sprayed.
i. After completing step "h," rotate crankshaft so that no piston is at a top position. If the
aircraft is to be stored outside, stop two -bladed propeller so that blades are as near horizontal
as possible to provide maximum clearance for passing aircraft.
j. Again, spray each cylinder without moving the crankshaft to thoroughly cover all interior
surfaces of the cylinder above the piston.
The preservative oil must be Lubricating Oil -Contact and Volatile, Corrosion Inhibited, MIL -
C-6529. Type I heated to 200°F-220°F spray nozzle temperature.
piston.
k. Install spark plugs and connect spark plug leads.
l. Apply preservative oil to the engine interior by spraying approximately two ounces of the
preservative oil through the oil filler tube.
m. Seal all engine openings exposed to the atmosphere, using suitable plugs or non -
hygroscopic
tape. Attach a red streamer at each point that a plug or tape is inst alled.
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
24
n. If the aircraft is to be stored outside, perform the procedures in paragraph 2 -7. In addition,
the pitot tube, static source vents. air vents, openings in the engine cowling. and other similar
openings should have protective covers installed to prevent entry of foreign material.
o. Attach a warning placard to the propeller to the effect that the propeller shall not be
moved while the engine is in storage.
B. Inspection during storage .
a. Inspect airframe for corrosion at least once a mont h and remove dust collections as
frequently as possible. Clean and wax aircraft as required.
b. Inspect the interior of at least one cylinder through the spark plug hole for corrosion at least
once a month.
NOTE. Do not move crankshaft when inspecting in terior of cylinder for corrosion.
c. If at the end of the 90 day period. the aircraft is to be continued in nonopertional storage, repeat the
procedural steps "g" thru "o" of paragraph 2 -10.
C Return the airplane to service.
After temporary storage. use the following procedures to return the aircraft to service.
a. Remove aircraft from blocks and check tires for proper inflation Check for proper nose gear
strut inflation. (See figure 1-1.)
b. Check battery and install.
c. Check that oil sump has prope r grade and quantity of engine oil.
d. Service induction air filter and remove warning placard from propeller.
e. Remove materials used to cover openings.
f. Remove spark plugs from engine.
g. While spark plugs are removed, rotate propeller several rev olutions to clear excess rust
preventive oil from cylinders.
h. Clean. gap and install spark plugs. Torque plugs to the value specified in Section 11 or 11A
and connect spark plug leads.
i. Check fuel strainer. Remove and clean filter screen if necessary . Check fuel tanks or bays
and fuel lines for moisture and sediment, drain enough fuel to eliminate moisture and
sediment.
j. Perform a thorough pre-flight inspection, then start and warm-up engine.
D Indefinite storage
Indefinite storage is defined as a ircraft in a nonoperational status for an indefinite period of time.
Engines treated in accordance with the following may be considered protected against normal
atmosphere corrosion, provided the procedures outlined in paragraph 2 -14 are performed at the
intervals specified.
a. Operate engine until oil temperature reaches normal operating range. Drain engine oil sump
and reinstall drain plug and safety.
b. Fill oil sump to normal operating capacity with corrosion preventive mixture which has
been thoroughly mixed.
NOTE Corrosion-preventive mixture consists of one part com-pound MIL-C-529. Type I.
mixed with three parts by volume of MIL-L-6082 mineral aircraft engine oil.
c. Immediately after filling the oil sump with corrosion -preventive mixture. fly the aircraft for
a period of time not to exceed a maximum of 30 minutes.
d. With engine operating at 1200 to 1500 rpm and induction air filter removed, spray
corrosion-preventive mixture into induction airbox, at the rate of one -hall gallon per minute,
until heavy smoke comes from exhaust stack, then increase the spray until the engine is
stopped.
CAUTION Injecting corrosion-preventive mixture too fast can cause a hydrostatic lock.
e. Do not rotate propeller after completing step "d".
f. Remove all spark plugs and spray corrosion-preventive mixture. which has been preheated
to 200°F to 220°F, into all spark plug holes to thoroughly cover interior surfaces of cylinders.
g. Install lower spark plugs or install solid plugs, and install dehydrator plugs in uppe r spark
plug holes. Be sure that dehydrator plugs are blue in color when installed.
h. Cover spark plug lead terminals with shipping plugs (AN4060 -1) or other suitable covers.
i. With throttle in full open position, place a bag of desiccant in the carbur etor intake and seal
opening with moisture resistant paper and tape.
ES-ECR MAINTENANCE PROGRAM
01.09.07 Rev.1 Page
25
j. Place a bag of desiccant in the exhaust tailpipe(s) and seal openings with moisture resistant
tape.
k. Seal cold air inlet to the heater muff with moisture resistant tape.
l. Seal engine breather by inserting a protex plug in the breather hose and clamping in place.
m. Seal all other engine openings exposed to atmosphere using suitable plugs or non -
hygroscopic
tape.
NOTE Attach a red streamer to each place plugs or tape is install ed. Either attach red
streamers outside of the sealed area with tape or to the inside of the sealed area with safety
wire to prevent wicking of moisture into the sealed area.
n. Drain corrosion-preventive mixture from engine sump and reinstall drain plug.
NOTE The corrosion-preventive, mixture is harmful to paint and should be wiped from
painted surfaces immediately.
o. Attach a warning placard on the throttle control knob, to the effect that the engine contains
no lubricating oil. Placard the propeller to the effect that it should not be moved while the
engine is in storage.
p. Prepare airframe for storage as outlined in paragraph 2 -10 thru step "f".
NOTE As an alternate method of indefinite storage. the aircraft may be serviced in accordance
with paragraph 2-10 providing the aircraft is run up at maximum intervals of 90 days and then
reserviced per paragraph 2-10.
E Inspection During Storage.
Aircraft in indefinite storage shall be inspected as follows:
a. Inspect cylinder protex plugs each 7 days.
b. Change protex plugs if their color indicates an unsafe condition.
c. If the dehydrator plugs have changed color in one half of the cylinders. all desiccant
material in the engine shall be replaced with new material.
d. Every 6 months respray the cylind er interiors with corrosion-preventive mixture.
NOTE Before spraying, inspect the interior of one cylinder for corrosion through the spark
plug hole and remove at least one rocker box cover and inspect the valve mechanism.

502
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#2 Сообщение 502 » 23 сен 2008, 22:09

Это обязательный документ по EASA? Для каждого борта надо писать? А можно в каком-нибудь приличном формате выложить (pdf/doc)? А так совсем нечитаемо...

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Viktor
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#3 Сообщение Viktor » 23 сен 2008, 23:37

Да документ обязательный он утверждается лётным депортаментом.
В Пдф нету сори.
Но попробуйте скопировать в Ворд додлжно получится

502
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Зарегистрирован: 25 авг 2006, 08:29
Member of AOPA: Yes
Откуда: Москва

#4 Сообщение 502 » 23 сен 2008, 23:41

Viktor писал(а):Да документ обязательный он утверждается лётным депортаментом.
Летным департаментом чего? Если частное лицо - оператор, то откуда департамент?

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