Magni Gyro M-24 Instructions for use

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 1
TITLE: M24 MAINTENANCE SCHEDULE
CODE: 045-00-24_A
PRODUCT: M-24

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 2
CONTENTS
1
FOREWORD ........................................................................................................4
1.1 SCOPE............................................................................................................. 4
1.2 ATTACHMENTS ................................................................................................. 4
1.3 REFERENCES.................................................................................................... 4
2 RESPONSIBILITIES AND STANDARDS................................................................5
2.1 OWNER/OPERATOR RESPONSIBILITIES................................................................ 5
2.2 CERTIFYING PERSONS RESPONSIBILITIES............................................................ 5
2.3 GENERAL INSPECTION STANDARDS..................................................................... 5
2.4 AIRWORTHINESS LIFELIMITATIONS(RETIREMENT/SCRAPLIVES)....................................... 5
2.5 AIRWORTHINESS DIRECTIVES............................................................................ 5
2.6 OVERHAUL, ADDITIONAL INSPECTIONS AND TEST PERIODS................................... 6
2.7 INSTRUCTIONS FOR CONTINUING AIRWORTHINESS.............................................. 6
2.8 CHANGES (REPAIRS OR MODIFICATIONS)............................................................ 6
2.9 DUPLICATE INSPECTIONS .................................................................................. 6
2.10 SCHEDULED MAINTENANCE WORKSHEETS ........................................................... 6
2.11 DEFINITIONS.................................................................................................... 7
3 PERMIT MAINTENANCE RELEASE .......................................................................8
3.1 MAINTENANCE AUTHORISATION ......................................................................... 8
3.2 PILOT MAINTENANCE......................................................................................... 8
4 CHECK CYCLE AND VARIATIONS ......................................................................10
4.1 THE MAINTENANCE CHECK CYCLE ......................................................................10
4.2 PERMITTED VARIATIONS (SEE NOTES)................................................................11
5 PRE-FLIGHT .....................................................................................................12
5.1 PILOT’S PRE-FLIGHT CHECK/CHECK A – PRIOR TO FIRST FLIGHT OF THE DAY..........12
6 SCHEDULED MAINTENANCE..............................................................................20
6.1 SCHEDULED MAINTENANCE WORKSHEETS ..........................................................20
6.2 FINAL CHECKS (INCLUDE WITH ALL CHECKS)......................................................21
6.2.1 Ground Run:........................................................................................21
6.2.2 Certification:........................................................................................21
6.2.3 Type Certificate and Schedule Review:.....................................................21
6.3 25 HOUR CHECK (ONLY TO BE CARRIED OUT AFTER FIRST 25 HOURS/6 MONTHS): ..22
6.3.1 Flying Controls:....................................................................................22
6.3.2 Engine: ...............................................................................................23
6.4 100 HOUR CHECK: ...........................................................................................24
6.4.1 Structural/Zonal:..................................................................................24
6.4.2 Landing Gear: ......................................................................................25
6.4.3 Flying Controls:....................................................................................25
6.4.4 Liquid, Air and Gas Systems:..................................................................28
6.4.5 Equipment and Environmental:...............................................................28
6.4.6 Engine: ...............................................................................................29
6.4.7 Rotors:................................................................................................29
6.4.8 Gyroplane Lubrication: ..........................................................................31
6.4.9 Powerplant Installation:.........................................................................31
6.4.10 Air Induction:.......................................................................................32

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 3
6.4.11
Exhaust:..............................................................................................32
6.4.12 Fuel System:........................................................................................32
6.4.13 Electrical System:.................................................................................32
6.4.14 Instrument Systems: ............................................................................34
6.4.15 Ignition:..............................................................................................34
6.5 2-YEAR CHECK.................................................................................................35
6.5.1 Instrument Systems: ............................................................................35
6.6 300 HOUR / 3-YEAR CHECK ...............................................................................35
6.6.1 Flying Controls:....................................................................................35
6.7 500 HOUR CHECK ............................................................................................36
6.7.1 Flying Controls:....................................................................................36
6.7.2 Rotor:.................................................................................................36
6.8 1000 HOUR CHECK...........................................................................................37
6.8.1 Powerplant Installation:.........................................................................37
7 LIFED ITEMS ....................................................................................................38

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 4
1FOREWORD
1.1 SCOPE
The scope of this document is to provide a detailed breakdown of the maintenance tasks to
be carried out to provide continued airworthiness, and the required intervals.
Details of the approved method of undertaking the appropriate maintenance is outlined in
the Magni Gyro M24 (M24C) maintenance manual (Ref 1).
This document refers only to airframe maintenance and those engine ancillaries which are
specific to the M24 (M24C) Gyroplane. All engine maintenance should be undertaken in
accordance with the appropriate engine manufacturer’s maintenance schedule.
1.2 ATTACHMENTS
None.
1.3 REFERENCES
Ref 1 M24_A Maintenance Manual
Ref 2 ROTAX 914 UL Maintenance Manual

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 5
2RESPONSIBILITIES AND STANDARDS
2.1 OWNER/OPERATOR RESPONSIBILITIES
Owners/operators are responsible for the accomplishment of the maintenance prescribed in
this schedule.
2.2 CERTIFYING PERSONS RESPONSIBILITIES
Certifying persons must use their engineering skill and judgment in determining the depth of
inspection needed and other matters which could affect the airworthiness of the gyroplane.
In order to claim any alleviation on subsequent inspections, the gyroplane maintenance
records must record the extent of previous inspections upon which the alleviation is based.
Certifying persons are responsible for recording in the appropriate log book or worksheet,
any defects, deficiencies or additional maintenance required as a result of implementation of
the schedule.
2.3 GENERAL INSPECTION STANDARDS
The general inspection standards applied to individual task inspections must meet the
recommended standards and practices of Magni Gyro Srl and are published in M24 (M24C)
maintenance manual.
In the absence of general inspection standards, refer to other standards recommended by
Magni Gyro Srl or Authorities’ recommended standard s and practices.
Inspections may be carried out without component removal or dismantling unless considered
necessary or where required by the schedule.
2.4 AIRWORTHINESS LIFE LIMITATIONS (RETIREMENT/SCRAP LIVES)
Airworthiness life limitations shall be those published by the Authorities and those defined in
Section 7 of this report. Airworthiness life limitations shall be recorded according to local
requirements.
2.5 AIRWORTHINESS DIRECTIVES
All applicable Airworthiness Directives and Mandatory Permit Directives, issued by the
relevant Authorities, must be complied with.
Compliance with Airworthiness Directives and Mandatory Permit Directives shall be recorded
accordingly with local requirements.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 6
2.6 OVERHAUL, ADDITIONAL INSPECTIONS AND TEST PERIODS
Overhaul, additional inspections and test periods are those recommended by Magni Gyro Srl.
The local Authority may vary or mandate overhaul and test periods and additional
inspections by the issue of an Airworthiness Directive or Generic Requirement.
The overhaul, additional inspections and test periods shall be recorded accordingly with local
requirements.
2.7 INSTRUCTIONS FOR CONTINUING AIRWORTHINESS
Instructions for continuing airworthiness consist of in-service data published by Magni Gyro
Srl and must be considered by the owner/operator in addition to this maintenance schedule
in order to ensure the approved maintenance schedule remains valid for the M24 (M24C).
Instructions for continuing airworthiness (Service Bulletins, Service Letters, etc.) should be
formally technically assessed by the owner/operator and adopted if required to ensure
operational safety and reliability.
Instructions for continuing airworthiness applicable to the gyroplane shall be included in the
gyroplane documentation accordingly with local requirement and form part of this
maintenance schedule.
Compliance with adopted continuing airworthiness information shall be recorded accordingly
with local requirements.
2.8 CHANGES (REPAIRS OR MODIFICATIONS)
Approved ‘changes’ which have been carried out to the gyroplane, engine, components and
radio after original manufacture, must be recorded in the appropriate log book(s).
Any recurring inspection or maintenance task resulting from approved ‘changes’ shall be
recorded accordingly with local requirements.
2.9 DUPLICATE INSPECTIONS
When required to perform a critical task inspection or following initial assembly or disturbance of
a control system or vital point, tit is mandatory to duplicate inspections.
Certifications must be recorded in the appropriate worksheet, log book or aircraft technical log.
2.10 SCHEDULED MAINTENANCE WORKSHEETS
Worksheets shown in Section 6 must be issued and the tasks certified for all scheduled
maintenance checks. These worksheets become part of the maintenance records required to be
kept by the owner/operator.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 7
All maintenance carried out in connection with a particular check should be certified on suitably
referenced worksheets and included in the gyroplane records. These worksheets must be cross-
referenced in the appropriate log book(s) giving general details of the additional maintenance
carried out.
2.11 DEFINITIONS
Throughout the schedule the following terms and abbreviations have the stated definitions:
Service/Lubrication (Service/LUB)
The term ‘Service or Lubrication’ requires that a component or system should be serviced and/or
replenished as necessary with fuel, oil, grease, water, oxygen, etc., to a condition specified in
the appropriate maintenance manual. The term ‘service’ may also be used to require filter
cleaning or replacement.
Inspect (INSP)
An ‘Inspection’ is a visual check performed externally or internally in suitable lighting conditions
from a distance considered necessary to detect unsatisfactory conditions/discrepancies using,
where necessary, inspection aids such as mirrors, torches, a magnifying glass etc. Surface
cleaning and removal of detachable cowlings, panels, covers and fabric may be required to be
able to satisfy the inspection requirements.
Operational Check (OP/C)
An ‘Operational Check’ is a test used to determine that a system or component or any function
thereof is operating normally.
Functional Check (F/C)
A ‘Functional Check’ is a detailed examination of a complete system, sub-system or component
to determine if operating parameters are within limits of range of movement, rate of flow,
temperature, pressure, revolutions per minute, degrees of travel, etc., as specified in the M24
(M24C) maintenance manual. Measured parameters should be recorded.
Check (CHK)
A ‘Check’ is the verification of compliance with Magni Gyro Srl recommendations.
Continuing Airworthiness
Means all of the processes ensuring that, at any time in its operating life, the gyroplane complies
with the airworthiness requirements in force and is in a condition for safe operation.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 8
3PERMIT MAINTENANCE RELEASE
3.1 MAINTENANCE AUTHORISATION
It is mandatory to comply with local rules and requirements. If locally not specified follow
the recommendations by Magni Gyro Srl. Except for maintenance permitted to be carried out
by the pilot (see Section 3.2), the aircraft shall be certified as fit for flight following
maintenance by the issue of a Permit Maintenance Release (PMR).
The Permit Maintenance Release shall be issued covering the particular maintenance carried
out and is required (if not locally otherwise specified) for scheduled maintenance, overhaul,
modification, repair, replacement, defect rectification or compliance with Directives.
The aircraft logbooks/worksheets shall contain particulars of the maintenance carried out
and shall include the following certification statement:
The work recorded above has been completed to my satisfaction and in that
respect the aircraft is considered fit for flight.
Signed ......................... Date .........................
Authorisation Ref. ......................... (Just if required)
Permit Maintenance Release (PMR) shall be issued only by persons specifically authorised by
Authority for the purpose.
3.2 PILOT MAINTENANCE
Pilot maintenance may be carried out in accordance with relevant rules and requirements
and accordingly to Magni Gyro Srl instructions.
NOTE: For pilot maintenance the issue of a Permit Maintenance Release (PMR) is not
required. The pilot must enter details of the maintenance carried out and include his pilot’s
licence number with his signature in the appropriate log books.
Permitted pilot maintenance includes the following actions:
1. Replacement of landing gear tyres. Including removal and replacement of
wheels, cleaning and servicing of wheel bearings, application of creep marks,
removal and refitting of brake units to the extent required for wheel removal and
the removal and the renewal of brake pads/linings when special tools are not
required. Replenishment of hydraulic brake system fluid level;
2. Replacement of defective safety wiring or split pins excluding those in engine,
transmission, flight control and rotor systems (but including those designed to
be pilot-maintainable and shown in the pilots handbook, e.g. the teeter-bolt split
pin and rotor assembly bolts);

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 9
3. Repairs to upholstery and decorative furnishing of the cabin or cockpit interior
when repair does not require dismantling of any structures or operating system
or interfere with an operating system or affect the structure of the aircraft;
4. Removal, replacement and refitting of side doors;
5. Repairs (including removal and refitting), not requiring welding, to fairings,
wheel spats, non-structural cover plates and cowlings;
6. Replacement of safety belts or safety harness;
7. Replacement of seats or seat parts not involving dismantling of any structure or
of any operating system;
8. Replacement of bulbs, reflectors, glasses, lenses or lights;
9. Replacement of any cowling not requiring removal of the propeller, rotors or
disconnection of engine or flight controls;
10. Replacement of spark plugs (including removal, cleaning, gapping, testing and
refitting of all spark plugs);
11. Replacement of batteries;
12. Replacement of rotors, tail surfaces and controls, the attachments of which are
designed to provide for assembly immediately before each flight and dismantling
after each flight;
13. Replacement of main rotor blades that are designed for removal where special
tools are not required (as is the case for Magni gyroplanes);
14. Removal and refitting of rotor blades from/to the hub bar;
15. Replacement of VHF communications equipment, only if is not combined with
navigation equipment;
16. Manufacture and installation of required cockpit placards and notices;
17. Lubrication of the aircraft (including prior cleaning of hinges);
18. Inspection of engine induction air filter, including removal, cleaning and refitting
(with wirelock);
19. Inspection and/or replacement of fuel filters, including removal, cleaning and
refitting;
20. Changing of engine oil (including removal, cleaning/replacement, refitting of oil
filter, and wirelock of sump bolt);
21. Adjustment of the lateral position of the trim spring.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 10
4CHECK CYCLE AND VARIATIONS
4.1 THE MAINTENANCE CHECK CYCLE
Check title Content Period Certification
Check A Check A Prior to the first flight of the day. Pilot
25 hour check 25 hour check items. Not exceeding 25 flying hours. Depending on local
regulations
100 hour check 100 hour check items. Not exceeding 100 flying hours. Depending on local
regulations
Annual check 100 hour and annual check items. Not exceeding 12 months (see Note 5). Depending on local
regulations
2yr 2 year check items. 2 years. Depending on local
regulations
300 hour/3yr 300 hour / 3 year check items. 300 flying hours or 3 years, whichever is sooner. Depending on local
regulations
500 hour check 500 hour check items. Not exceeding 500 flying hours. Depending on local
regulations
1000 hour check 1000 hour check items. Not exceeding 1000 flying hours. Depending on local
regulations

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 11
4.2 PERMITTED VARIATIONS (SEE NOTES)
Tasks controlled by flying hours Maximum Variation
25 hour 10%
100 hour 10%
500 hour 10%
600 hour 10%
Tasks controlled by calendar time Maximum Variation
6 Months 1 Month
Annual None
3 year / 300 hours 3 months / 10%
Tasks controlled by more than one limit The more restrictive limit shall be applied unless otherwise specified
NOTES:
1. Permitted variations may not be applied to applicable airworthiness life limitations, airworthiness directives, Generic Requirements or
overhaul and test periods.
2. Permitted variations for tasks controlled by flying hours should not be understood to be a maintenance planning tool, but as an
exceptional means to allow the operator to fly for a limited period of time until the required maintenance is performed.
3. Any application of a permitted variation to the maintenance check cycle period must be recorded in the appropriate log book(s) together
with the reason for the variation by a person who is authorised to sign the log book entry for that particular check. Details of the
permitted variation must be made visible to the pilot.
4. Permitted variations are not required to be deducted from the next scheduled check.
5. The annual check may be anticipated by a maximum period of 62 days without loss of the continuity of the maintenance check cycle.
Thus, for example, where the full 62 days is invoked, the following annual check would become due 14 months after the completion of
the annual check which was anticipated. The period by which the annual check was anticipated and the date of the next annual check
shall be recorded in the appropriate log book(s).

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 12
5PRE-FLIGHT
5.1 PILOT’S PRE-FLIGHT CHECK/CHECK A – PRIOR TO FIRST FLIGHT OF THE DAY
Pre-flight checks / Check A are to be carried out in accordance with the Gyroplane Flight Manual.
NOTE: Initially the daily/pre-flight checks may seem a long procedure, but with experience the pilot will soon become familiar with all
aspects of the aircraft and what is correct or not. The check is organised into a logical pattern that makes one complete circuit of the
gyroplane and becomes second nature with practice. This pattern starts with the inspection of the instrument panel and continues around the
gyroplane.
A1 Instrument Panel
Master “ON”.
Check operation of:
a) TCU (Turbo Control Unit);
b) Operation of TCU Servo;
c) Strobe/hazard light units;
d) Electrically powered instruments;
e) Ignition Warning Light.
Master “OFF”.
Check:
a) Instruments zeroed, where applicable;
b) Set altimeter to QFE;
c) Instruments secure;
d) Operation of drift indicator;
e) Nameplates and markings are present and legible.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 13
A2 Pedals
Check:
a) Rudder pedals full, free, positive and correct movement;
b) Condition of rudder cables and travel along keel mounted pulleys;
c) Presence of safety wiring on cable turnbuckles.
A3 Control Columns
Check:
a) Operation of cyclic controls, left and right for:
i. Full and free movement;
ii. Synchronised operation of left and right control sticks;
iii. Condition of all joints/hinges/bearings.
b) Functioning of pre-rotator lever on pilot control stick.
A4 Inside of Cockpit
Check:
a) No debris, equipment or cargo will cause any restriction to the controls;
b) Any signs of fouling of controls in cockpit;
c) Seats are secure and free from damage.
A5 Cockpit/Fuselage Right Hand Side
Check:
a) State of external surface of fuselage and remove foreign objects and dirt;
b) Inspect transparencies for fixing, damage and cleanliness;
c) Pilot and passenger restraint system and make sure are not damaged. Pay particular attention to any cut, chafing,
contamination worn latch or boss, loose or pulled stitching and any other factors that may call into doubt the harness
serviceability;
d) State and safety of fuel cap;
e) Check doors (if fitted) are secure; hinges are secure and undamaged, locking mechanism working correctly.
A6 Coolant Level
Check:
a) Carefully open expansion tank on the engine and check the correct level of coolant in tank.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 14
A7 Engine Oil Level
Check:
a) Correct engine oil level using the dipstick inside the oil tank.
A8 Freedom and Integrity of Control Rods
Check:
a) Condition and security of the safety points on the control rods, linkages, bearings and fiberlock nuts. There should be
insignificant play in the “Uniball” rod-end bearings and no evidence of corrosion or damage. The control rods should be
straight and undamaged. The control rods should be free to rotate slightly around their axis when gripped and given a light
twist. Any undue force needed or inability to twist the bearing may indicate a problem of the bearing and should be further
investigated.
A9 Rotor Head – Right Hand Side
Check:
a) All the rotor head securing nuts are secure and that all the safety locking systems are present and functional;
b) Examine as far as possible the rotor head and hub-bar assemblies for cracks, damage, wear, corrosion and rubbing;
c) The state of the pre-rotator ring-gear teeth and make sure they are not damaged or excessively worn;
d) Make sure the pre-rotator flexible shaft and the Bendix pre-rotation gear are adequately coated with grease.
A10 Undercarriage Right Hand Side
Check:
a) State and safety of the undercarriage leg and mounting bolts.
A11 Wheels and Wheel Spats
Check:
a) State and safety of the anchoring of the wheel, hub, axle and wheel spats;
b) All the tyres for damage and check tyre pressures are correct;
c) Check for damage, rubbing marks on the tyres and position of creep marks;
d) The brake lines and make sure there is no evidence of bending or chafing.
Either roll the gyroplane forward or remove the wheel spats to check the whole of each tyre.
Ensure any dirt and debris has been removed from inside the wheel spats.
Check the function of the braking system.
Check the braking system for signs of leaks or damage.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 15
A12 Engine Mount – Right Hand Side
Check:
a) Welds on the engine mount for cracks, damage or chafing;
b) The vibration dampers for damage or cracks and make sure the fixing bolts are not loose.
A13 Engine – Right Hand Side
Check:
a) The following components for security, corrosion, condition, levels, leaks, damage and chafing:
- carburettors, linkages and cables
- airbox fixing
- wiring and connections
-coolingsystem
- oil reservoir and oil
- oil filter
- radiator and oil radiator
- spark plugs and their caps
- engine bearers, connectors and fasteners
- oil, fuel and coolant hoses and clamps
- on the Rotax 914 engine – the Turbo Control Unit (TCU) and its mounting bracket
- exhaust system, springs, joints and mounts
- pre-rotation assembly, belts, cables and flexible shaft
b) The state of the battery and look for signs of overheating, excessive venting, corrosion of terminals or leakage of acid;
c) The voltage regulator and the starter contactor for signs of overheating, short circuits or corrosion.
A14 Exhaust System – Right Hand Side
Check:
a) Verify the integrity of the exhaust system, checking that there are no cracks in the exhaust pipes;
b) Security of the exhaust gas temperature probes.
A15 Radiators
Check:
a) The radiant surfaces and verify that there are no leaks of liquid, damage or chafing;
b) The security of the radiator baffles system and the security of the clamps and fixing points;
c) Check integrity and security of the cabin heating duct (if fitted).

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 16
A16 Propeller
Check:
a) The spinner attachments;
b) The entire surface of each blade for any signs of damage or de-bonding. Make sure the blades are clean.
A17 Pre-Rotation System
Check:
a) Correct positioning of the pre-rotation assembly and the belt tension;
b) Functioning of the pre-rotation system and the freedom of movement of the belt tensioning pulley lever;
c) Correct positioning of the pulley’s brake shoe and check for excess pulley wear.
A18 Tailplane
Check:
a) All the lower and upper surfaces and make sure they are free from cracks or damage;
b) Security of the tail plane;
c) Security of the rudder and make sure it is completely free to move (push down on the tail so that the nose wheel lifts,
allowing the rudder and nose-wheel to move freely);
d) Tail wheel for condition and free movement.
A19 Engine – Left Hand Side
Check:
a) The following components for security, corrosion, condition, levels, leaks, damage and chafing:
- carburettors, linkages and cables
- airbox fixing
- wiring and connections
-coolingsystem
- radiator and oil radiator
- spark plugs and their caps
- engine bearers, connectors and fasteners
- oil, fuel and coolant hoses and clamps
- exhaust system, springs, joints and mounts
b) Condition and security of the air filter;
c) The ROTAX 914 turbocharger unit, air filter, waste gate and springs, waste gate motor and cable.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 17
A20 Trim System
Check:
a) Security of the trim actuator and integrity of the control cable, springs and electric connections.
A21 Fuel System
Check:
a) That the quantity of fuel is adequate for the flight planned;
b) The fuel pipes and connectors for serviceability and any sign of leakage;
c) The fuel filter is clean and that there are no signs of leaks;
d) The fuel tank surfaces and seams.
Draw a sample of fuel from the drain point and check the sample for any water or other contaminant.
A21 Fuel Level
Check:
a) The fuel level.
WARNING: This operation must be done using the tank sight gauge on the rear left-hand side of the fuel tank (open cowling flap to view).
A23 Control Rods – Left Hand Side
Check:
a) Condition and security of the safety points on the control rods, linkages, bearings and fiberlock nuts. There should be
insignificant play in the “Uniball” rod-end bearings and no evidence of corrosion or damage. The control rods should be
straight and undamaged. The control rods should be free to rotate slightly around their axis when gripped and given a light
twist. Any undue force needed or inability to twist the bearing may indicate a problem of the bearing and should be further
investigated;
b) The rotor brake and cables for freedom of movement and correct function;
c) The state of the rotor tachometer pick-up and make sure it is secure.
A24 Cockpit and Fuselage – Left Hand Side
Check:
a) State of external surface of fuselage and remove foreign objects and dirt;
b) Check doors (if fitted) are secure; hinges are secure and undamaged, locking mechanism working correctly;
c) Inspect transparencies for fixing, damage and cleanliness.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 18
A25 Throttle Levers
Check:
a) That the full range of movement is available to the throttle levers, with no binding or restriction;
b) The condition of the brake levers. Make sure that the maximum braking power is available and that the lever springs back
when released.
A26 Nose Wheel
Check:
a) The condition of the nose wheel and tyre; check tyre pressure;
b) That the full range of movement is available to the wheel and that it operates in the correct direction with the rudder;
c) The fork for any sign of damage or distortion;
d) That the wheel is free to spin, without play in the bearings. Make sure the axle nut is secure.
A28 Pitot
Check:
a) That there are no obstructions, dirtiness or other clogging inside the pitot.
A28 Rotor Blades
Check:
a) That the rotor blades are free from any damage or other defect;
NOTE: Inspection of rotor blade root should account for confirmation that any cracks in this region conform to the appearance,
and remain within the limits, specified in SIL-002-2011 and also shown under task number 51 of this schedule.
b) Ensure that the rotor blades are clean.
A29 Communication and Navigation Systems
Check:
a) The functionality of all the navigation and communication systems.
A30 Lighting System
Check:
a) The functionality of all the internal and external lighting systems.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 19
A31 Door Warning System
Functioning of the door locking warning system should be confirmed by the following tests.
•With both doors in the ‘OPEN’ position and the MASTER switch ‘ON’ close the pilot’s door and then move the pilots
handle to the locked position. Then move the co-pilot’s handle to the locked position. The warning light should
remain illuminated and the rotor rpm gauge should remain inactive because the co-pilots door is open.
•Move the co-pilot’s handle to the open position; move the pilot’s handle to the open position and open the pilot’s
door. Close the co-pilot’s door and move the co-pilot’s handle to the locked position; then move the pilot’s handle
to the locked position. Again the warning light should remain illuminated and the rotor rpm gauge should remain
inactive because the pilot’s door is open.
•Move the pilot’s handle to the open position; close the pilot’s door and move the pilot’s handle into the locked
position. The warning light should extinguish and the rotor rpm gauge becomes active as all doors and handles
are now closed and locked. Open the co-pilot’s handle to confirm that the light becomes illuminated once
more and the rotor rpm gauge de-activates.
It is essential that the checks on the door warning system are performed as described and in this exact order. This will
enable each of the four switches functionality to be determined in turn and a single fault with any of the switches will
be able to be detected.

045-00-24_A M24 MAINTENANCE SCHEDULE
Issue A
Page 20
6SCHEDULED MAINTENANCE
6.1 SCHEDULED MAINTENANCE WORKSHEETS
Maintenance Organisation Name: Page 1 of
Site where maintenance was accomplished: Note: Enter total pages issued
A/C Reg: Type: Serial No: Workpack Ref:
Engine Type:
A/C Total Hours: Check Start Date: Operator:
Check Type: [25 FH/6 Months] [100 FH] [2 Year] [300 FH/3 Year] [500 FH] [1000 FH] [Annual]
Note: Delete checks which are not being carried out and identify any not applicable worksheet tasks as N/A.
Maintenance Manual Reference Issue/Revision No. Date
Airframe:
Engine: