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Eurofox 4X-HSEמערך האחזקה למטוס
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מערך אחזקה לכלי טיס
מסוג
EuroFOX
4X-HSE (S/N 56219)
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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
18 מערך ביקורת המנוע
12.6.2019 ביקורות גוף
19 מערך ביקורת המנוע
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
ביקורת מכשירים ואויוניקה
25
12.6.2019
ביקורת מכשירים ואויוניקה
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
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-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
Interval operating hours Points of inspection
1000 600 200 100 50 25* No periodic maintenance requirement after the
first 25 hours of operation
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
Interval operating hours Points of inspection
1000 600 200 100 50 25* No periodic maintenance requirement after the
first 25 hours of operation
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
Interval operating hours Points of inspection
1000 600 200 100 50 25* No periodic maintenance requirement after the
first 25 hours of operation
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
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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
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
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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
60 EXCHANGE ALL RUBBER HOSES OF
FUEL SYSTEM
180 EXCHANGE ALL ROTAX TEFLON
HOSES OF FUEL
SYSTEM
60 EXCHANGE ALL RUBBER HOSES OF
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.
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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: ___________