EuroFOX - ngc.org.il

Eurofox 4X-HSEמערך האחזקה למטוס

P 1 of 26 : REV. 0 25.7.2019

מערך אחזקה לכלי טיס

מסוג

EuroFOX

4X-HSE (S/N 56219)


P 2 of 26 : REV. 0 25.7.2019

תוכן העניינים

עמוד נושא

תוכן העניינים

2

3 זיהוי כלי הטייס והצהרת מפעיל

4 רשימת תפוצה וביאור קיצורים

5 בקרת מהדורות, ביקורת שנתית למערך ורשימת עמודים ישימים

6 ישימים )המשך(רשימת עמודים

7-9 בדיקה יומית וב. לפני טיסה

10,11 ביקורת גוף

12 ביקורת גוף )המשך( והסבר על בדיקות המנוע.

13 הסבר בדיקות המנוע )המשך(

14-19 ביקורת המנוע

20,21 הנחיות שימור המנוע

22 מעקב רכיבים

23 שקילה ואיזון

24-26 ביקורת מכשירים ואויוניקה


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GENERAL

מכון בדק סוג הפעלה כתובת מפעיל שם מפעיל

11חצב מרכז דאיה נגב מכבים רעות גרירת דאונים

2000אחזקות

א"ק יצרן מודלEuroFOX

AEROPRO 4X-HSE

ENG S/N A/C S/N שנת יצור 7704724 56219 2019

תחזוקה REV תאריך

:לפי

רכיב יצרן דגם

7.12.2009 0 M/M EuroFOX

AEROPRO גוף

6.12.2017

0 M/M

(Online)

912 IS ROTAX מנוע

14/09/2016 G

DUC

Manual

Windspoon DUC מדחף

AIR OPERATOR STATEMENT 1.4

The maintenance program is approved by the undersigned and must be complied with, as applicable, in

order toto ensure that all maintenance is carried out on time and to approved standards and that the

program is reviewed and updated as required.

This maintenance program lists the tasks and identifies the practices and procedures specified by the

applicable type certificate holder, which form the basis for the scheduled maintenance of the aircraft.

The provisions of this maintenance program do not pervert the necessity for complying with any new

or amended regulation(s) published by the CAAI from time to time, where these new or amended

regulations may override element of this program.

The data contained in this program will be reviewed for continued validity at least annually to ensure

that it reflect the current type certificate holder(s) recommendations and operating experience, as the

CAAI requirements.

It is understood that the CAAI reserves the right to suspend, vary or cancel the approval of the

maintenance program if the CAAI has objective evidence that the requirements of the maintenance

program are not being followed or required standards of airworthiness are not being maintained.

Name: Amnon Harari Position: head of owner’s managing committee.

Signature_________________ :


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רשימת תפוצה

עותק

מספר

פרטי התקשרות שם הנציג גוף

1

כשירות אוירית -רת"א דוד גרוסמר

מר יהודה קדוש

050-6212825

מרכז דאיה נגב בעלים / מפעיל 2

מיכאל פינקוס

054-4667166

מכון הבדק 3

2000אחזקות

בדק מטוסים

בע'מ

09-9548448

Abbreviations

AFM - Airplane Flight Manual.

AMM - Aircraft Maintenance manual.

CAAI- Civil Aviation Authority.

DI- Daily Inspection.

FAA- Federal Aviation Administration.

MCM –Maintenance Control Manual

MOPM – Maintenance Procedure Manual.

O/C- On Condition.

STC- Supplement Type Certificate.

SRM- Structure Repair Manual

TC- Type Certificate

TSO- Time since Overhaul

MOD – modification

רשות התעופה האזרחית הישראלית –רת"א


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REVISION CHEK LIST

INSERTED BY HIGHLIGHTS DERIVED FROM

REV DATE INSERTED REV

מערך ראשון מ. פינקוס

M/M R.1

Rotax 912IS MM

DUC prop Manual

12.6.2019 0

Annual MP Inspection

Remarks Signature Inspected by Date

LIST OF EFFICTIVE PAGES

SUBJECT PAGE

NO DATE OF REVISION

SUBJECT

12.6.2019 1 כותרת המסמך

2 12.6.2019

GENERAL

3

12.6.2019

וביאור קיצורים רשימת תפוצה 4 12.6.2019

List of effective pages 5

12.6.2019

List of effective pages 6

12.6.2019

DI 7

12.6.2019

DI 8

12.6.2019

D.I + PRE-FLIGHT 9

12.6.2019

ביקורות גוף10

12.6.2019

11 ביקורות גוף 12.6.2019

כללי ביקורות המנוע 12

12.6.2019

12.6.2019 13 כללי ביקורות המנוע


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12.6.2019 14 מערך ביקורת המנוע

המנועמערך ביקורת 15 12.6.2019

12.6.2019 16 מערך ביקורת המנוע

17 מערך ביקורת המנוע

12.6.2019


12.6.2019 ביקורות גוף


12.6.2019

20 הוראות שימור המנוע 12.6.2019

מנועביקורות 12.6.2019 21 הוראות שימור המנוע

22 מעקב רכיבים 12.6.2019

דוח שקילה

23

12.6.2019

ביקורת מכשירים ואויוניקה

24 12.6.2019


25

12.6.2019


26

12.6.2019


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בדיקה יומית ובדיקה לפני טיסה

כפי PILOT OPERATING MANUAL-מבוסס על הפרק זה

שפורסם על ידי יצרן המטוס בתוספת הבדיקות היומיות/לפני טיסה כפי

על ידי יצרנית המנוע OPERATORS MANUAL-שפורסמו ב

ROTAX (REVISION 0 EDITION 4 01/11/2016)

Daily Inspection

10

11

1

322

4

55 6

7

9

3

12

8

13

1. Cockpit

POH and other documentation review and available to pilot

master switch OFF

backup battery switch OFF

Strat power switch OFF

ignition OFF

Fuel pump switch A OFF

Fuel pump switch B OFF

fuel valves OPEN, fuel quantity check

instruments INSPECT

safety belts INSPECT

flaperon tie rods INSPECT

control stick INSPECT, freedom of movement

rudder pedals INSPECT, freedom of movement

brakes INSPECT

trim freedom of movement, proper function

engine controls INSPECT, freedom of movement

loose objects in cockpit remove

cockpit windows INSPECT

door INSPECT, shut and locked

2. Main landing gear


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gear legs and attachment INSPECT

wheels INSPECT, tire pressure 29 PSI

brakes INSPECT

3. Wings INSPECT – wing, struts, hinges, surface 4. Pitot tube INSPECT

5. Flaperons INSPECT –hinges, surface freedom of movement

counterweights attachment.

6. Rear cockpit cover INSPECT, secured

7. Fuselage INSPECT

8. Stabilizer, elevator, hinges INSPECT –surface, hinges, attachment of stabilizer struts

freedom of movement of elevator and trim tab.

9. Fin, rudder, hinges INSPECT surface, attachment, freedom of movement

condition and attachment of balance tab.

10. Nose wheel INSPECT, tire pressure – 29 PSI

11. Propeller INSPECT / blades, propeller hub, check of locking propeller nuts (when visible)

12. Engine Remove the top engine cowling and

INSPECT - engine mount

INSPECT - air intake, carburettors and controls

INSPECT - exhaust system

INSPECT – coolant, quantity (0.4 inch above bottom) - (between MIN and MAX marks), leakages –(see picture 1)

INSPECT – oil, quantity (between MIN and MAX marks), leakages. The oil level should be at least in the middle between marks when planning a long term operation.

INSPECT - fuel system, filter and carburettors

INSPECT - electrical system, ignition, cable connections

13. Fuel

Quantity (between MIN and MAX, at least middle for longer flights)

INSPECT - draining off water and dirt from the central tank. Fuel system must be sampled daily to assure lack of contamination. Inspect the type of fuel.

Fuel caps secured, correct vent orientation – open end against air in flight.

Pre-Flight Inspection Make a brief walk around before you board the aircraft. This short inspection might discover damages or problem occurred during the last flight. It is especially important to make this inspection when you are taking over the aircraft from another pilot.

Use chocks for main wheels when possible and practical to prevent the aircraft from moving. Always make sure that the person you asked to remove your chocks while engine is running is aware of propeller danger. The best practise is to use chocks only for engine warm-up and engine check, shut down the engine and remove chock while the engine is stopped. Before using chock make sure they do not collide with wheel fairings preventing any damage.

Cockpit - INSPECT COCKPIT INTERIOR EQUIPMENT

- INSPECT SAFETY BELTS

- CONTROL SYSTEM-FREEDOM OF MOVEMENT, DAMAGES


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wings - INSPECT WING SURFACES

- INSPECT WING AND STRUTS SUSPENSIONS

- INSPECT FLAPERONS.

Fuselage - INSPECT

tail unit - INSPECT

landing gear - INSPECT

break system - INSPECT

engine and propeller – INSPECT

Oil level (oil dipstick) check Note

The oil level should be in the upper half (between the "50%" and the "max" mark) and should never

falls below the "min" mark. Prior to long flights oil should be added so that the oil level reaches the

"max" mark.

Avoid oil levels exceeding the "max" mark, since excess oil could be poured out through the venting

system.

difference between max.- and min.- mark = 0.45 litre (0.95 liqpt).

End of Preflight check


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גוףיקורות ב שלוש ביקורות שגרתיות:הפרק כולל

שעות 50. ביקורת כל 1

שעות 100. ביקורת כל 2

חודשים 12שעות / 200. ביקורת כל 3

4X-HSE Inspection schedule AF Hours: ___________ Engine Hrs: ___________

Date: ___________

IMPORTANT:

Read all inspection requirements paragraphs

prior to using these charts.

Service/hours Propeller

INSPECTOR

SIGN S.i.i. 50 100 200

Spiner

Spinner bulkhead

Blades

Bolts and nuts

Spacer

Service/hours Engine compartment

INSPECTOR

SIGN S.i.i. 50 100 200

Check for evidence of oil and fuel leaks, then clean entire engine

and compartment if needed, prior to inspection.

Engine oil, filler cap, dipstick, drain plug, filter element

Oil cooler

1 Induction air filter

Induction air box, doors and controls

Cold and hot air hoses

Cylinders, rocker box covers and push rod housings

Crankcase, oil sump, accessory section and crankshaft seal

Gear drive case and propeller shaft seal

2 Hoses, metal lines and fittings

3 Intake and exhaust system

Ignition harness

Spark plugs

Compression check

Electrical wiring

4 Engine controls and linkage

Engine shock mounts, mount structure and ground straps

Cabin heat doors and controls

Starter, solenoid and electrical connections

Voltage regulator mounting and electrical leads

Carburetors

Firewall

Engine Cowling

Service/hours Fuel system

INSPECTOR

SIGN S.i.i. 50 100 200

Fuel drain valve

Fuel tank vent, cap and placards

Fuel tank sump drains

5 Drain fuel and check outlet screen

Fuel shut-off valve and placards

9 Replace fuel filters


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Service/hours Landing gear

INSPECTOR

SIGN S.i.i. 50 100 200

Main gear wheels and fairings

Nose gear wheel and fairing

6 Wheel bearings

Tires

Brake fluid, lines and hoses, linings, discs, brake assembly, master

cylinder and Parking brake

Main gear struts

Service/hours Airframe

INSPECTOR

SIGN S.i.i. 50 100 200

Aircraft exterior

Aircraft frame structure

Windows, windshield, doors and seals

Seat belts and shoulder harnesses

Seat structure, mounting and upholstery

Control bearings, pulleys, cables and rod connections

Instruments and markings

5 Magnetic compass compensation

Instruments and wiring

Instrument panel, ground straps, covers, decals

Heating and ventilation system

Lights, switches, circuit breakers

Exterior lights

Pitot and static system

Radios and avionics

Antennas and cables

7 Battery

Perform Avionics inspection every 24 months (see P.24-26)

Service/hours Control systems

INSPECTOR

SIGN S.i.i. 50 100 200

In addition to the items listed below, always check for correct

direction of movement, correct travel and correct cable tension.

Trim control holder, rope and brake of the movement of lever

Travel stops

Flap control holder, brake of the movement of lever

Flap and alerons mixer and rods

Decals and labeling

Elevator and trim tab hinges and control rods

8 Elevator trim tab

Rudder pedal assembly and linkage

Skins of control surfaces

Check the tow release handle and Bowden cable

Check condition of the tow hook, cleanliness, lubricate with

WD40.

End of airframe inspection schedule.

Special inspection items (S.i.i. as outlined in chart above)

1. Check filters per paragraph 2.16. Replace if required.

2. Replace hoses at engine overhaul or after 5 years, whichever comes first.

3. General inspection every 50 hours, Refer to Section 11 for 100 hour inspection.

4. Each 50 hours for general condition and freedom of movement. These controls are not

repairable. Replace as required at each engine overhaul.

5. Each 1000 hours or to coincide with engine overhaul.


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6. First 100 hours and each 200 hours thereafter. More often if operated under prevailing wet or

dusty conditions.

7. Check battery voltage per paragraph 2.17 each 100 hours.

8. Check linkage for cracks and free play, lubricate with regular grease every 50 hours.

9. Replacements after first 100 engine hours and thereafter every 200 Hrs.

ביקורות מנועכפי MANUAL MAINTENANCE -מתוך ה 05-20-00פרק זה מבוסס על פרק

-של כל דף מפורט ב REVISION-)ה ROTAXשפורסם על ידי יצרנית המנוע

LIST OF EFFECTIVE PAGES)

( :600-ו 200, 100, 25הפרק כולל ארבע סוגי ביקורת חובה )

שעות מנוע ראשונות 25. ביקורת לאחר 1

שעות מנוע 100. ביקורת במרווחים של 2

עשעות מנו 200. ביקורת במרווחים של 3

שעות מנוע 600. ביקורת במרווחים של 4

ביקורות תקופתיות:

חלק זה כולל רשימת בדיקות תקופתיות שחייבות להתבצע אחרי פרקי זמן . הגדרה: 1

מוגדרים של תפעול מנוע

600, 200, 100, 25-ביקורות תקופתיות הן אלה החייבות להתבצע ב. מרווחים: 2

.5.1חלק 05-20-00שעות. המרווחים הם בהתאם לפרק

שעות תפעול יש לבצע ביקורת 100המשמעות של המרווחים היא, לדוגמא, שכל 2.1

את סעיפי הביקורת הייחודים ובנוסף 100שעות תפעול יש לבצע ביקורת 200. כל 100

.200לביקורת

מרווחים בשעות

25 100 200 300 400 500 600 700 עד 2000

X X X X X X X X X 100

X X X 200

X 600

בכדי לשמור על כשירות אווירית מתמשכת, חובה על המנוע : 100. ביקורת 3

חודשים. 12שעות עבודה או 100לעבור ביקורת אחרי כל

(. פער זה -+/ 10שעות ) 10למרווחים בין הביקורת ניתן להוסיף/להפחית 3.1

בוצעה 100אפשרי אך אין לחרוג ממנו. המשמעות של זה היא כי אם ביקורת


P 13 of 26 : REV. 0 25.7.2019

-ב ולאשעות -+/10שעות 200-שעות, הביקורת הבאה תבוצע ב 110לאחר

שעות. -+/10 210

המרווח שנקבע, הביקורת הבאה תבוצע לאחר לפניאם ביקורת מבוצעת 3.2

שעות 87הראשונה בוצעה לאחר 100אותו מרווח )לדוגמא: אם ביקורת

.שעות תפעול 187הבאה תבוצע לאחר 100תפעול, אזי ביקורת

שעות תפעול במשך שנה, חייבת להתבצע 100-אם מנוע צבר פחות מ 3.3

ת. לביקורת שנתית שכזו חודשים מהביקורת הקודמ 12לאחר 100ביקורת

חודשים 2 -ישנו טולרנס של +/

50מערך ביקורת זה כולל גם טור של ביקורת . ביקורת שעות מיוחדת: 4

חובה, למעט שעות. ביקורת זו מומלצת על ידי יצרן המנוע אך היא אינה

LEADEDהחלפת שמן במנועים המתודלקים עם דלק מטוסים עם עופרת )

AVGAS)

בכדי לשמור על כשירות אווירית מתמשכת, חובה על שעות: 25. ביקורת 5

שעות התפעול הראשונות. 25המנוע לעבור ביקורת לאחר

שעות ראשונות היא אותה ביקורת 25הביקורת המבוצעת בביקורת 5.1

. סעיף זה מתייחס הן למנועים חדשים והן למנועים 100המבוצעת בביקורת

(OVERHAULEDשעברו שיפוץ )

24אויוניקה תבוצע כל ציוד ה. ביקורת כיול מדי גבה ומהירות וביקורת 6

למערך זה. 26-24עמודים חודשים לפי מערכי הבדיקה ב


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DATE:

PROP

Hrs

ENGINE

Hrs

AIRCRAFT

Hrs

AIRCRAFT REG:

4X-HSE

BRP – Rotex Maintenance manual line

Maintenance schedule Perform the following tasks at the intervals shown in the maintenance check list. See chapter 05-20-00

of the MM

Legend X = do the task

Blank = no task required

NOTE

If the first 3 are checks (general note, differential pressure chack and inspection fine fuel filter) are

acceptable then continue with the maintenance schedule.

If one of the first 3 checks are not acceptable, the engine must be checked and required in accordance

with the BRP-Rotax instructions for continued airworthiness.

Points of inspection Interval operation hours Chapter reference signature

No periodic maintenance requirement

after the first 25 hours of operation

25* 50 100 200 600 1000

1) General note All (alert) services bulletins are

compiled with. If necessary to

preform these and documented.

X X X X X

All SI-PAC (service instruction part

and accessories) for additional

GENU-INE-ROTAX – parts and

accessories used on the relevant

aircraft are compiled with. If

necessary to perform these and

document it.

X X X X X

2) Differential pressure check

Check the compression by the

differential pressure method.

Test pressure _____ hPa (psl)

Pressure drop (% in fraction)

Cyl. # 1 2 3 4

Bar\

psl

X(1 X X X 12-20-00

Checking the

compression.


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Points of inspection Interval operation hours Chapter reference signature

No periodic maintenance

requirement after the first 25 hours

of operation

25* 50 100 200 600 1000

Use of leaded fuel more then 30% of

operation

3) Inspection of the GENUINE ROTAX fuel filter (on the air frame) Visual inspection of the GENUINE

ROTAX fuel filter for leaks.

X See MM of the aircraft

manufacturer

2) replacement of the GENUINE

ROTAX fuel filter (exclusive after

TSN or TSO <=100 ± permissible

tolerance).

X (2

Replacement of the GENUINE

ROTAX fuel filter (periodic at TSN

or TSO > 100 hour)

X

If there is no GENUINE ROTAX

fuel filter in use the specification of

the aircraft manufacturer must be

observed.

4) Spark plug Check the spark plug connectors fit

tightly on the spark plugs. Minimum

pull-off force is 30 N (7 lb)

X X X 12-20-00

Inspection of spark plugs

Remove all spark plugs and check

for spark plug defects (deposits,

melting…)

Check if GENUINE ROTAX spark

plugs are used.

X X X X X 12-20-00

Remove the spark plugs

Replacing spark plugs. 3) use the leaded fuel more than 30%

of operation.

X(3 X X X 12-20-00

Inspecting of spark plug

5) Inspecting the magnetic plug Check the magnetic plug X X X X X 12-20-00

Inspecting the magnetic

plug

6) Inspecting the oil filter Remove old filter from engine. Cut

old filter without producing any

metal

X(4 X 12-20-00

Signature Chapter

refernce

Interval operating hours Points of inspection

1000 600 200 100 50 25* No periodic maintenance requirement after the

first 25 hours of operation

Inspection of the oil

filter components

Chips and inspect components for wear and\or

missing material. Perform filter mat inspection:

Findings:

_______________________________________

use of leaded fuel more then 30% of operation. (4

7) visual inspection of the engine

12-20-00

Visual inspection

X X X X X General visual inspection of the engine for

damage or abnormalities. Check cooling air duct

and cooling fins of the cylinders for obstruction,


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cracks, wear and good condition. Take note of

change by temperature influence.

X X X Inspect temperature sensors and oil pressure

sensor for secure fit and signs of wear.

12-20-00

Leakage check

X X X X X Inspect all coolant hoses of the engine for

damage, including leakage, hardening from heat,

porosity, loose connections and secure

attachment. Verify routing is free of kinks and

restrictions.

12-20-00

Leakage check

X X X X X Carry out visual inspection of leakage bore at the

base of the water pump of the water pump for

signs of leakage.

12-20-00 X X X X X Inspect the expansion tank for damage and

abnormalities. Check coolant level replenish as

necessary. Inspect radiator cap. Inspect protection

rubber on expansion tank base for correct fit.

12-20-00

Overflow bottle

X X X X X Inspect the overflow bottle for damage and

abnormalities. Verify coolant level. Replenish as

necessary. Inspect line from expansion tank to

overflow bottle for damage. Leakage and clear

passage. inspect venting bore in cap of overflow

bottle for clear passage.


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Signature Chapter

refernce




12-20-00

Leakage check

X X X X X Inspect all oil lines for damage, leakage,

hardening from heat, porosity, security of

connections and attachments. Verify routing is

free of kinks and restrictions.

12-20-00

Checking the fuel

lines

X X X X X Inspect all fuel lines for damage, leakage,

hardening from heat, porosity, security of

connections and attachments. Verify routing is

free of kinks and restrictions. Check steel fuel

lines for any cracks and\or scuffing marks.

12-20-00

Check of wiring

X X X X X Inspect the wiring (wiring harness) and its

connections for secure fit, damage and signs of

wear.

12-20-00

Checking the

engine suspension

X X X X X Inspect engine suspension and fasteners

(GENUINE ROTAX) for secure fit, including

damage from heat, deformation, cracks

X X X X X Check the airbox (GENUINE ROTAX) incl.

throttle body actuation. Inspect sensors for tight

fit, damage from heat, damage and signs of wear.

12-20-00

Cleaning the dry air

filter

X X X X X Checking the air filter

X X X X Inspection of the GENUINE ROTAX exhaust

system included in the standard delivery.

8) oil change

X X X X (5X X Drain oil from oil tank

Signature Chapter

refernce




12-20-00

Oil change,

cleaning the oil

tank

X (5X (5X Check the oil tank and clean the oil tank if

contaminated.

12-20-00

Purging the oil

system

X X X X (5X X Refill oil tank with approx. 3 liters of oil. For oil

quality, see operators manual latest edition.

12-20-00

Oil filter change

X X X X X X Install new oil filter

in the case more than 30% of operation with leaded fuel e.g.: AVGAS 100 LL(5

9) electric fuel pump

12-20-00

Fuel pumps

Every 1000 h Check the electric fuel pumps

10) fuel system

12-20-00

Fuel system

X Inspect the fuel system on the engine side for

leaks.

X Inspect the fuel system for damages

11) auxiliary alternator

X X X X X On configuration with auxiliary alternator, check

the attachment and the V-belt tension.


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12) Engine external parts

X Inspect screws and nuts of all external parts for

tight fit. Inspect safety wiring, replace as

necessary.

13) auxiliary alternator

X X Check all temperature sensors

X X Check all pressure sensors

X X Check all exhaust gas temperature sensors

X X Check all speed sensors

Signature Chapter

refernce




X X Check the throttle control sensor

X X Check the knock sensor

14) engine management

12-20-00

Checking ECU

X Check the ECU and its mountings

12-20-00

Read out the ECU

data memory

X X Download the ECU fault memory (fault and data

logs)

X X Check UCU wiring

X X Check the throttle valve adjustment

15) FUSE BOX

X Check the FUSE BOX and its mounting

X X Visual inspection of the fuses

16) checking the propeller gear box

See heavy

maintenance chap.

72-10-00

X Check gear set (pitting)

See heavy

maintenance chap.

72-10-00

X Check wear or tooth of overload clutches

05-50-00

Checking the

overload clutch

X (6X Gearbox with overload clutch

use of leaded fuel more than 30% of operation. (6

Inspect overload clutch

17) flushing the cooling system

12-20-00 When replacing the coolant Flushing the cooling system if large deposits

found in the expansion tank or


P 19 of 26 : REV. 0 25.7.2019

Signature Chapter

refernce




Flushing the

cooling system

On radiator cap and\or if the coolant manufacturer

requires a change interval.

18) engine cleaning

12-20-00

Engine cleaning

X X X X X X Engine cleaning

19) liquid level check

12-20-00

Fluid capacities

X X X X X Verify liquid level, replenish as necessary

20) engine test run

Observe the safety instructions!

12-20-00

Test run of engine

X X X X X Start the engine and run to operating temperature.

Limits see operators manual 912 iS.

Ignition check at _____ rpm engine speed. Speed

drop without LANE:

A (off) ________ rpm

B (off) ________ rpm

A\B (differnce) _______ rpm

Checking the idle speed.

After engine test run. Re-tighten oil filter by hand

(only at cold engine).

Check for leaks.

Returning engine to service

On the engine identified as per point 5, on the ____________________________ the _________ hr.

Check at ______ hr. (TSN____, TSO____) was carried out according to recommendations of the engine manufacture and was recorded in the

engine log book.

Location, date _____________________

Inspector _________________________

Aircraft mechanic __________________

Certificate No. _____________________


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המנוע הוראות שימור והחזרה לכשירות של

71-00-00פרק זה מבוסס על הוראות פרק

MAINTENANCE MANUAL (HEAVY MAINTENANCE)-מתוך ה

של יצרנית המנוע


P 21 of 26 : REV. 0 25.7.2019


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מעקב רכיבים ( או החלפה של הרכיבים השוניםTBOבפרק זה מובאים פרקי הזמן לפני שיפוץ )

של יצרנית המנוע MM-ועל ה של יצרנית המטוס MM-הפרק זה מבוסס על

תדירות

בחודשים

רכיב פעולה לביצוע תדירות בשעות

50 INSPECTION A/C 50 Hr

100 INSPECTION A/C 100 Hr

12 200 INSPECTION A/C 200 Hr

25לאחר שעות ראשונות בלבד INSPECTION ENG 25 Hr

12 100 INSPECTION ENG 100 Hr

200 INSPECTION ENG 200 Hr

600 INSPECTION ENG 600 Hr

24 INSPECTION RADIO/AVIONIC

12 CALIBRATION COMPASS

60 800 OVERHAUL PROPELLER

180 2000 (+ 5% / 6 MONTH) OVERHAUL ENGINE

60 EXCHANGE ALL RUBBER HOSES OF

COOLING SYSTEM


FUEL SYSTEM

180 EXCHANGE ALL ROTAX TEFLON

HOSES OF FUEL

SYSTEM


LUBRICATION SYSTEM

12 200 EXCHANGE FUEL FILTER

12 INSPECT FIRST AID KIT


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משקל ואיזון

Weight and C.G. Position Record

Serial Number 56219 Registr. Mark: 4X-HSE

Aircraft Levelling:

Values Weighed: Main wheels right-hand Mrh = kg L= 1425 mm

left-hand Mlh = kg L1= 495 mm

Nose wheel Mpr = kg

Resulting weight Mres = kg

C.G. position

B = (Mpr x L ) / Mres = [ mm]

X = L1 – B + 50 = [ mm ]

_

X = (X x 100) / 1300 = [ %MAC ]

Date: Performed by:


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ומכשירים ביקורת אוויוניקה פרק זה מבוסס על מערך ביקורת האוויוניקה כפי שפורסם על ידי אגף כושר אווירי

של רת"א

RADIO AVIONICS INSPECTION SCHEDULE

AC Registration number: 4X-HES

AC Serial number: 56219

Inspection date:

Flight hours: Airframe:

Maintenance personnel

Name Title Licence Number Signature

No. Reference

Document

System Manufacture

Part Number

Signature Remarks

1 Job Card No. 1

Harness

Condition Insp.

3 Job Card No. 3

A/C Battery

Check

4 Job Card No. 4

C/B Panel Insp.

5 Job Card No. 5

Antennas Insp.


P 25 of 26 : REV. 0 25.7.2019

6 Job Card No. 6 A.T.C.

Transponder &

Encoder Test

8 Job Card No. 8

V.H.F. Com

Test

10 Job Card No. 10 Intercom

System test

11 Job Card No. 11

Instruments

Lights Check

12 Job Card No. 12

Exterior lights

check

13 Job Card No. 13

Placards and

Markings insp.

14 Job Card No. 14

Airspeed

Indicators

Check

15 Job Card No. 15

Compass Swing

21 Job Card No. 21

Optional

Equipment

24 Job Card No. 24 Resistance,

Bonding and

Megger Test

26 Job Card No. 26

Headsets, Mic,

Speakers

מכשירי הבדיקה

P/N S/N Exp.

ATC Tester

Air Data Tester

COM / NAV Tester

I certify that the above inspections were performed in accordance with the manufacturer's instructions, the approved inspection schedule and the current ICAA regulations. Checked by: _________ Inspected by: ___________ Signature: ___________

Date:___________


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A.T.C TRANSPONDERENCODER & ALTIMETER TEST

Test Height ft Altimeter

(Actual)

Altimeter (1)

Tolerance ±

ft

Encoder

(Actual)

Encoder (1)

Tolerance ± ft

-1000 20 125

-500 20 125

0 20 125

1,000 20 125

2,000 30 125

3,000 30 125

4,000 35 125

6,000 40 125

Note: These tolerances refer to FAR 43 Appendix E.

AIRSPEED INDICATORS CHECK

Test Airspeed kmh Airspeed (Actual)

kmh

Airspeed Tolerance ±

kmh

50 2

80 3

120 4

Checked by: _________ Inspected by: ___________ Signature: __________

Date: ___________

Documents

EuroFOX - ngc.org.il