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MAINTENANCE MANUAL 

SAVANNAH S

 

Doc. No.:

 

MM-SVNH-EN 

Revision:

                       

07 

Rev. Date:

 

07/11/2022 

Proj. Ref.: 

SVNH S 

 

A/C: 

Savannah S

 

 

Applies to Generic Serial Number:

 yy-mm-54-xxxx 

Page:

 104/132  

 

DOC  

        

 FMM00 

- 

Verify the installation of the push-pull rod of the steering, going to the front landing gear. The 
length of the rods should not modified from design dimensions; 

- 

The nose wheel must be longitudinally aligned when the rudder pedals are straight; 

- 

If  the  Rudder  pedals  (left  pilot  side  is  the  reference)  are  not  aligned  when  the  wheel  is 
longitudinally  straight,  move  the  pedals  to  obtain  the  alignment.  Then  adjust  properly  the 
push-pull rods uniball to obtain the nose wheel straight consequently. The uniball adjustment 
must be always done by closing the uniball (shortening the rod in respect of design values); 

- 

With  the  Rudder  pedals  always  aligned  together,  pull  the  cables  at  the  proper  tension  by 
means of Nonio tender (11-15 [lbs]); 

- 

Check the Rudder surface is aligned longitudinally straight to the Fuselage; 

- 

If the Rudder is not longitudinally aligned, modify the cables length by regulating the Nonio 
tender  with  same  number  of  holes,  unsymmetrically  (the  one  adding  and  the  other  one 
subtracting holes); 

- 

Verify the Rudder alignment and when found correct check again the cable are tensioned as 
prescribed. 

  

7.1.5.2. 

Rudder ground adjustable (flettner) tab deflection 

The  ground  adjustable  tab  installed  on  the  Rudder  surface  is  necessary  to  obtain  a  directional 
alignment (sideslip ball centered) of the airplane during leveled cruise flight at 75% of power (5000 
[RPM]), no turbulence, no wind, below 2500 [ft] of Density Altitude and approximately 500 [kg] of 
weight with two occupants of same weight on-board (side CG centered if differently obtainable).  
During  this  flight  condition,  set  the  roll  at  zero  Bank  angle  eventually  maintained  by  piloting  with 
control stick and then free the Rudder pedals control; weight the condition is stable an observe if the 
airplane  goes  directionally  on  the  left  or  right,  therefore  the  sideslip  ball  is  on  the  left  or  right 
respectively. In case of left, land the airplane and set the ground adjustable tab bent lightly on the 
left. Then flight again and observe consequently the behavior and correct newly if required. 
The following 

Table 36 

reports the design dimension of the push-pull rods of the directional control 

system, from uniball to uniball center (codes on CM and SPC of reference documents in 

Chapter 

1.2

): 

Code 

Length [mm] 

SL075 (left) 

313 +/-2 

SL076 (right) 

335 +/-2 

Table 36: Directional CS (steering) push-pull rods dimension 

 

7.1.6.  Elevator Trim Tab setup 

The  elevator  trim  tab  setup  is  verifiable  only  in-flight;  the  initial  setup  is  done  with  the  design 
dimension of the push-pull rods of the trim tab actuator, reported in 

Table 37

. With the airplane in 

flight at leveled condition with full power, no turbulence, no wind, below 2500 [ft] of Density Altitude, 
approximately 500 [kg] of weight (two occupants) and 5 kg in the baggage compartment, the trim tab 
should  maintain  the  aircraft  trimmed  leveled  at  the  full  nose  down  trim  position  and  coherent 
indication. If the aircraft rise the nose up with controls free, in that speed and trim full down conditions, 

Содержание SAVANNAH S

Страница 1: ...chnical Manager Federico Peronato Approved DIG Accountable Manager Tancredi Razzano Manufacturer data Name I C P Srl Contacts Phone 39 011 9927503 Address S P 16 km 15 150 Website www icp it Castelnuovo Don Bosco Email info icp it AT Italy 14022 Airworthiness tecnico icp it The technical data and the information embodied therein are property of I C P Srl and shall not be disclosed in whole or in p...

Страница 2: ...on Issued by 00 15 11 2009 First issue Andrea Caglio 01 21 07 2010 Ch 3 4 Pag 11 12 Andrea Caglio 02 29 04 2010 Ch 3 Pag 9 Andrea Caglio 03 19 05 2011 Ch 3 Andrea Caglio 04 11 03 2015 General revision all Pag Michele Bassetti 05 22 06 2016 Ch 3 7 Pag 11 12 Michele Bassetti 06 18 12 2018 Ch 1 Pag 1 3 Federico Peronato 07 07 11 2022 New issue of the Maintenance Manual superseding all the previous ve...

Страница 3: ...1 1 5 Spare parts purchase 12 1 6 Warranty 13 1 7 Maintenance Request Form to ICP manufacturer 13 1 8 Feedback Form to ICP manufacturer 13 1 9 Aircraft protection and anchoring 14 1 10 Aircraft cleaning 14 1 11 Consumable materials 15 1 12 Nominal diameters 16 1 13 Tightening torques 16 1 14 Safetying practices 19 1 14 1 Safety wires 19 1 14 2 Castle nut and cotter pin 20 1 14 3 Threaded fasteners...

Страница 4: ...intenance Schedule 37 4 1 50 Hours maintenance checklist 39 4 2 100 Hours 1 Year maintenance checklist 55 4 3 200 Hours maintenance checklist 57 4 4 1000 hours maintenance checklist 59 4 5 2000 Hours maintenance checklist 64 5 Unscheduled Maintenance 67 5 1 Heavy landing 67 5 2 Fuel system leakage in fuselage 68 5 3 Wing tank or cup fuel leakage 68 5 4 Radiator suspension breakage 68 5 5 Windshiel...

Страница 5: ...ystem 85 6 8 Cabin heating and ventilation 86 6 9 Electrical system 87 6 10 Configuration equipment instruments and avionics 89 6 11 Painting 95 7 Maintenance descriptions 97 7 1 Control surface travel setting 97 7 1 1 Flaperon as aileron 97 7 1 2 Flap indications 100 7 1 3 Flight check of Flaperons 100 7 1 4 Elevator control system 100 7 1 5 Rudder control system 103 7 1 5 1 Rudder pedals alignme...

Страница 6: ...9 ANNEX B Feedback about ICP Aircraft 121 ANNEX C Maintenance work record Model 123 0 3 Figure Index Figure 1 Safety wires example 20 Figure 2 Cotter pin example 20 Figure 3 Threaded fasteners 22 Figure 4 Nonio cable tender 23 Figure 5 Fuel hose on fitting 23 Figure 6 Fuel hose on corrugated pipe 24 Figure 7 Oil hose on corrugated pipe 24 Figure 8 Water hose on corrugated pipe 24 Figure 9 Daily pr...

Страница 7: ...gure 36 Electrical wiring of engine compartment 87 Figure 37 Electrical wiring firewall backward 88 Figure 38 Flaperon jig SA200VG and position on the first wing rib 98 Figure 39 Position of jig SA200VG near the first rib rivets line aligned to wing trailing edge 98 Figure 40 ZERO setting of the left inner Flaperon Marks of 0 5 of tolerance 99 Figure 41 Push pull rods for Flaperon setup 99 Figure ...

Страница 8: ...79 Table 26 Fuel system volumes 82 Table 27 Oil system capacity 83 Table 28 Cooling system capacity 83 Table 29 Battery type 87 Table 30 Minimum Equipment List 89 Table 31 Standard configuration 90 Table 32d a d Optional configuration avionics and equipment 94 Table 33 Painting products 95 Table 34 Lateral CS push pull rods dimensions 100 Table 35 Longitudinal CS push pull rod dimension 103 Table ...

Страница 9: ...relevant manufacturers manuals The present manual do not show any equipment information WARNING The owner and finally the pilot should verify that every maintenance and checks are carried out as prescribed by the manufacturer of each system including airframe WARNING Any modification to the aircraft that could potentially affect the structural integrity or flight characteristics that has not been ...

Страница 10: ...other equipment checks and maintenance always refer to the original approved Maintenance Manual and Service Bulletins issued by the manufacturer of each relative system i e Propeller parachute rescue system I C P Srl does not take any responsibility for any damage to people property and aircraft due to failures in applying any Service Bulletins including the ones of the aircraft WARNING Inspection...

Страница 11: ...ge 1 3 Aircraft identification placard The aircraft is identified by means of Serial Number reported in two different placards the first one is located in the right side of the fuselage tail below the stabilizer the second is made of stainless steel and it is attached to the firewall starting from A C delivered in 2022 A generic Serial Number is composed like this yy mm 54 xxxx Where yy and mm cor...

Страница 12: ...intenance Workshop Individual authorized and licensed by a National CAA can perform the function or a Person authorized by I C P Srl where possible All other Scheduled or Unscheduled maintenance items with time limits Starting from the 100 hrs 1 year scheduled maintenance only Maintenance workshop or Individual authorized and licensed by a National CAA and National Dealer of I C P Srl authorized t...

Страница 13: ...Logbook or the Maintenance Record pages correctly filled in and updated to the current state of maintenance of the aircraft The module of Request is attached to the present manual and shown in the ANNEX A Request of Technical Intervention on the Aircraft NOTE The ICP workshop can not be booked without all the information requested by the dedicated module shown in ANNEX A Request of Technical Inter...

Страница 14: ... of in flight rain maintain Visual Meteorological Condition and possibly perform a route going out of shower To protect the aircraft mainly from rain entering in the cabin cover the wing and fuselage with a thin water repellent sheet paying attention to not damage the vortex generators Before flight open the door and or fuselage trap door to eventually dry the water or humidity To secure the aircr...

Страница 15: ...dahl High speed chain Rotating parts general additional lubrication Anti seize Copper based anti seize paste CFG Landing gear spring fixing bolt nut Thread locker Blue Loctite 243 see below possible positions Fuel fitting sealant Yellow Loctite 577 Seals fuel fittings on tank or junction Verification green marks Green Paint Marker Manufacturer production verifications of bolted connections Bolt nu...

Страница 16: ... A AN5 bolt 5 16 7 9 N A AN6 bolt 6 16 9 5 N A AN3 hole 4 9 0 1 0 2 AN4 hole 6 5 0 1 0 3 AN5 hole 8 0 0 1 0 3 AN6 hole 9 6 0 1 0 3 Flight Control Surfaces hinge line bushing internal diameter 4 9 0 1 FCS hinge line bushing external diameter 5 9 0 1 FCS hinge line horn hole for bushing 6 0 0 2 Table 3 Nominal diameters 1 13 Tightening torques Standard application Screw size Torque Nm Tolerance Nm A...

Страница 17: ... radial free play Flight control surfaces hinges AN3 Touching as required for teeth alignment for pin Allows rotation without axial and radial free play Nonio tender bolt AN3 6 0 5 Pulley axis bolt AN3 Touching as required for teeth alignment for pin Allows rotation without axial and radial free play Torque tube rear horn roll AN3 Touching as required to lock Prevent tube ovalization Flaperon mixe...

Страница 18: ...rn can rotate Brake caliper outer bolts nuts M6 15 1 Brake caliper inner bolts M6 10 1 Engine mount internal ring on engine housing M10 40 2 Engine mount silent block AN5 20 1 5 Fuel metal clamp N A Maximum possible screw closure Not excessive prevent hose cutting Fuel shut off valve fittings N A Touching 1 4 turn Not excessive prevent only fuel loosing Tank fitting and drain valve 1 4 N A Touchin...

Страница 19: ...rma metal clamp M6 Surfaces of clamp touching or if possible 13 Prevent compression of inner pipe Terminals for engine electric wirings starter motor starter relay M6 4 1 0 Exhaust collectors on cylinder bent flange M8 15 Attention leave a minimum of 1 screw thread free after the nut Exhaust terminal collar N A Max possible closure N A Table 5c a c Tightening torques for unusual application 1 14 S...

Страница 20: ...d the other one horizontally in respect of the nut cutting In both cases the cotter pin is considered properly installed if it is tight not moving the loop is not deformed and constrained The free edges of the pin must touch the bolt constrain the pin itself and not touch the surrounding structure In case of vertical pin orientation the loop is within the nut cutting instead the horizontal pin ori...

Страница 21: ...ication see Table 16 and size The thickness of the connection must be lower than the bolt length plus minimum one washer on the nut side and minimum two free thread pitches over the nut end If the bolt is longer than required add required number of washers to respect the correct installation The fasteners is normally closed by holding the head of the bolt and rotating the nut only in few cases the...

Страница 22: ...d add the rivet chosen correspondent with the hole diameter and with a proper length exceeding the sheet of almost 1 5 times the rivet diameter excluding the ones described differently in the Construction Manual Pull the rivet properly and repeat the operation Always control the result of the special riveting process check the head of rivet is pressing entirely and parallel to the skin not damaged...

Страница 23: ...tep by step pitch variation of 0 4 mm A bolt with stop nut is installed and closed to fix the selected length When changed the cable tension always control the wear of the nonio eyelets and the closure of the stop nut Figure 4 Nonio cable tender 1 14 8 Hose assembly Hereafter are shown some pictures of rubber hoses installation and normal closure of the metallic clamp The free edge of the rubber m...

Страница 24: ...N Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 24 132 DOC FMM00 Figure 6 Fuel hose on corrugated pipe Figure 7 Oil hose on corrugated pipe Figure 8 Water hose on corrugated pipe ...

Страница 25: ...ion panel opening or other Cutter Several Pliers Several Grip pliers Several Safety wire twister Safety wiring Air compressor with manometer Structures Oil filter wrench Rotax engine oil filter 4 tooth lockring spanner 24mm M17 Nose landing gear axle lock ring M17 4 tooth lockring spanner 32mm M24 Landing gear axle lock ring M24 Table 7 Standard tools 1 15 2 Unusual maintenance tools Tool Main app...

Страница 26: ...ing tools 1 16 Terms and Definitions The following list of terms is relative to the maintenance tanks to apply Term Definition Flight hours Sum of the entire period between the take off and landing of the aircraft Operating hours Sum of the entire period between the system is active i e the powerplant is rotating mainly Time limit Life cycle or period when to replace the system or parts even if th...

Страница 27: ...orter in respect of the schedule Regarding items subject of time limits the tolerance is 5 of the time or 6 month which one is minor 1 19 Aircraft lifting There are many possibility to lift up the aircraft the only important concept is to distribute the pressure around the touching point and to press only in structurally rigid areas Follows some examples First point fuselage rear cone lower skin w...

Страница 28: ...culate the aircraft Weight and Center of Gravity apply the following procedure Level the aircraft ref Chapter 1 20 Zeroing of the scales Place the aircraft on three scales one for each wheel Take note of the weights indicated by the scales Apply the calibration delta to the values if present a calibration table of the scales Vertically project with a plumb line the wing leading edge position on th...

Страница 29: ...ve almost all the not usable fuel incline the aircraft backward touching the tail skid on ground and drain from the same point after a normal purge To drain the oil brakes open the bleeding screw on the lower side of brake caliper and then add pressure from the top brake pump unscrew to open the pump embodied tank by means of air compressor The engine oil draining can be executed by opening the lo...

Страница 30: ...on Manual CM SVNH EN Savannah_S_Spare Parts Catalogue RevXX Savannah S Spare Parts Catalogue SPC SVNH EN Sxxxx name RevXX Savannah S Technical Specification number xxx name Sxxxx SBxxx Service Bulletin number xxx SBxxx Table 13 Approved documents WARNING Periodically updates the airplane approved documentation by monitoring and downloading the new file revisions in the I C P Srl aviation website w...

Страница 31: ...ecks are reported in the Flight Manual Pilot s Operating Handbook of the aircraft CAUTION Performing the check around the aircraft pay particular attention to deformation cracks bolts not tight absent safety wires or cotter pins abnormal parts or shapes excessive free play or parts loosing lubrication abnormal leaking CAUTION To perform each maintenance task or verification procedure related to th...

Страница 32: ...rn on when pressing test button 01 11 Light switches on and verify externally stroboscopic and navigation light 01 12 Master switch OFF when checks of electrical items completed 01 13 Throttle control smooth around the entire travels Set to idle 01 14 Carburetor heating knob check remains open when activated then set closed 01 15 Seats belts and harnesses check good state of latches closure and at...

Страница 33: ...ing gear bungee and wheel fork integrity Verify nose wheel axle safety wires 03 12 Verify nose wheel fairing rigid if installed 03 13 Verify plastic bushing guide correct position and free play within tolerance 03 14 Verify top plate of nose landing gear leg present and fixed 03 15 Verify tyre pressure if visually flat 03 16 Install engine cowling top 03 17 Verify the engine cowling is rigid and a...

Страница 34: ...skid fin and rudder skins correct shape and rivets 08 02 Verify fin attachments 08 03 Verify fin and rudder tip covers 08 04 Check rudder correct operation and excursion 08 05 Check rudder hinge cotter pins and bushing free play Rear fuselage left side 09 01 Verify external skin correct shape and rivets 09 02 Verify side inspection port closed 09 03 Verify parachute extraction area closed and cent...

Страница 35: ...Fuel filters x Fuel vent pipes x Electric fuel pump x Fuel sediment bowl valve o ring on collector tank bottom x Fuel cup support ring on wing fuel tank o ring x Fuel fitting on fuel tanks o ring x Oil system rubber hoses x Oil radiator silent block x Engine oil and filter x Cooling system rubber hoses x Cooling radiator silent block x Engine Coolant x Engine silent block and its stop nuts x Air i...

Страница 36: ...n the following Warning box Engine Rotax 912 ULS with S N from 6775790 is increased at 15 years ELT battery expires after 5 year or before as reported on the battery itself ELT self test every 3 month by pressing self test button Table 16b a b Time limits Tolerance of time limits is 5 or 6 month which one is minor WARNING Parts highlighted with the star mark are only given as a general indication ...

Страница 37: ... record in the aircraft maintenance logbook the maintenance performed and any variations in respect of the scheduled list or unscheduled maintenance The maintenance action can be executed with a tolerance of 5 Operating Hours or 1 month where applicable for this section between two consecutive scheduled works The next maintenance action must be planned by adding the interval from the Operating act...

Страница 38: ...reen marks remaining after manufacturer production verifications Verify bolt nut red cross check marks alignment Make a new mark with not erasable pen or cross check red torque seal Lubricate Clean and lubricate if needed disassembly to clean and then lubricate Measure Measure a hole diameter or distance clearance free play Table 18 Main maintenance tasks If during a verification or check or other...

Страница 39: ... the firewall to nose 01 02 Wing attachments Verify cabin frame welding no crack and attachments fork to wing plates integrity 01 03 Strut and landing gear attachments Verify struts attachments integrity shape and welding no crack Verify attachments connection to the fuselage integrity and bolts present 01 04 Horizontal Tail attachments Verify horizontal tail attachments angulars integrity no crac...

Страница 40: ... 14 Windshield and side windows Verify front windshield and doors windows are clear from big scratches or obscured areas Verify no big cracks If small cracks adjacent to rivets are present perform stop hole at the end of crack Clean if necessary 01 15 Doors Verify rigidly hinged on cabin frame and closing correctly Verify shape and integrity of door structure Verify door handle properly working fr...

Страница 41: ...d Right Flaperon 03 01 Structure Verify skin shape integrity and rivets all present Verify connection plates and bolt with stop nut closed between the inboard and outboard flaperon 03 02 Hinges Verify hinge points with castle nut and cotter pin properly fixed and free play within tolerances Clean and lubricate if necessary 03 03 Control system horn Verify control horn bolts and stop nuts closed Ve...

Страница 42: ...Jury strut Verify jury strut integrity and shape rigid connection to spar 04 07 Pitot tube Verify pitot is rigidly installed aligned to the wing lower skin and straight Verify hole is free and no moisture in the pipes looking under the instrument panel the ASI pipes 04 08 Vortex All present 04 09 Landing light Verify structure is rigid Check light function if installed 04 10 Tip Verify tip corners...

Страница 43: ...nt 07 04 Surface travel Verify elevator free in its entire travel Check surface deflection angles if cable tension has been modified Verify elevator angular free play within tolerance with control fixed 07 05 Tip cover Verify rigidly supported Trim Tab 08 01 Structure Verify skin and riveted lines 08 02 Hinge Verify central horn same of elevator hinge point free play within tolerance and castle nu...

Страница 44: ...k free around the entire travel and corners including roll Verify control stick cuff if installed integrity and not limiting the stick travel 11 02 Stick Verify stick grip integrity and not rotating 11 03 Joint and hinges rotating points Verify all the joint of control stick with castle nut and cotter pin properly installed or self locking nut closed Verify push pull rods and uniball properly clos...

Страница 45: ...mall sign of oil is acceptable Main landing gear 12 01 Support structure Verify integrity of landing gear attachments Verify vertical bolt and nut correctly closing the spring with red rubber vulcolan and lower plate in correct position and integrity 12 02 Spring Verify landing gear spring no damages no unsymmetrical shape within tolerances 12 03 Axle Verify ring nut with teeth washer closed both ...

Страница 46: ...osed with safety wires 13 04 Free play Check the free play of the landing gear leg lower sliding plates not major than 2 mm if necessary replace 13 05 Lubrication Lubricate with white grease the nose landing gear sliding and rotating points 13 06 Shock absorber Verify bungee enough strong against compression it must stay totally extended at empty weight after return from a 5 cm manual compression ...

Страница 47: ... tail wheel cables are in tension and springs present 13b 04 Alignment Verify rudder aligned with tail wheel 13b 05 Lubrication Lubricate with white grease all the rotating points Engine cowling 14 01 Integrity Remove the upper and lower cowling and verify all the parts of the cowling internal and external upper part 14 02 Attachments Verify cowling to fuselage attachments and connections between ...

Страница 48: ...nits and their suspension spark plug harnesses wirings pipes accessories 16 04 Cleaning If necessary clean the engine parts Powerplant controls 17 01 Throttle lever Verify throttle knob push pull bar and passage in firewall Check throttle run and friction only left side present 17 02 Throttle torque tube and supports Verify tube its plastic bushing and lateral supports no crack in horns welding 17...

Страница 49: ... pull to activate and it returns automatically deactivated 17 12 Choke system lubrication If needed clean and lubricate all the rotating points knob axle and wire 17 13 Propeller control electric if provided Check switch function on propeller blades pitch RPM increase switch up pitch decrease Fuel system 18 01 Leakages Verify no leakages following all the system parts hoses fitting pipes 18 02 Pip...

Страница 50: ... as required Water system 19 01 Coolant level Verify coolant level in the expansion tank over the transparent bubble dot Verify level in the overflow bottle approximately half Verify coolant cleanness and if required flush or replace the coolant 19 02 Leakages Verify no leakages following all the system parts hoses fitting pipes radiator 19 03 Coolant tanks Verify expansion tank integrity supporte...

Страница 51: ...installation and supporting 20 05 Hoses Verify hoses installation in all pipes connection and fitting metal clamp closed firmly 20 06 Radiator Verify radiator supports and silent block integrity and wearing 20 07 Oil filter Verify closed firmly or red marking aligned 20 08 Instrument Verify oil pressure and temperature probes connected to the electric wires oil pump and filter area Verify oil pres...

Страница 52: ...ting points and wire Electrical system 24 01 Battery Verify battery support and absence of corrosive fluids or structure corrosion Verify wires terminals on poles are fixed 24 02 Circuit breakers Verify wiring terminals all connected to the breaker below the instrument panel 24 03 Wirings Verify wirings all suspended behind the panel no connectors free or uncovered no wires worn no oxidation Verif...

Страница 53: ... propeller knob is pulled if provided hydraulic control governor 26 08 Carburettor balancing If needed check and align Flight check 27 01 Primary flight controls Check on ground smooth and free around the entire travel Check in flight normal flying qualities controls response 27 02 Secondary controls Check function 27 03 Primary instruments Check function and normal parameters 27 04 Engine instrum...

Страница 54: ...escription Maintenance close out 30 03 Cowling trap doors inspection panels Verify all cowling fairing and inspection panels are installed and closed 30 04 Fuel shut off valve Verify the fuel shut off valve is open and with safety wire 30 05 Maintenance record Fill in the aircraft maintenance logbook and equipment logbook with correspondent maintenance and effective flight hours Table 19q a q 50 h...

Страница 55: ...ting structure with no crack and all rivets Verify bell crank castle nut and cotter pin Verify push pull rod not scratching laterally 11 09 Flaperon control system Verify torque tube support structure fuselage bulkhead Verify torque tube hinges free play not excessive and bolt with stop nut closing properly the roll bell crank Verify hinges free play and bolt with stop nut closed of the bell crank...

Страница 56: ...ith overload clutch Record friction torque in Nm 16 11 Engine turning Inspect and record the torque only in case of suspected hard movement Oil system 20 10 Oil Drain oil from oil tank reduced at 50 hrs if used more than 30 of leaded fuel 20 11 Oil filter Remove oil filter inspect the filter by cutting it and then install a new one reduced at 50 hrs if used more than 30 of leaded fuel Record findi...

Страница 57: ...d blades hub bolts torque Make a new safety wiring on each bolt Reinstall the spinner and check closure of its screws 15 05 Balancing Verify presence of balance weights in marked position If absent lost or reported abnormal vibrations perform propeller balancing and blades pitch verification maximum Prop RPM Engine 16 01 Engine Maintenance Manual Apply manufacturer approved documentation for Maint...

Страница 58: ...heck radiator silent blocks nuts are closed Oil system 20 14 Oil radiator Check radiator silent blocks nuts are properly closed on radiator supports 20 15 Oil tank Check oil tank and clean if contaminated reduced at 100 hrs if used more than 30 of leaded fuel Intake system 21 07 Airbox Clean the airbox internally and lubricate the hinge of the air valves 21 08 Airbox drains Check airbox drain pipe...

Страница 59: ...rk 01 23 Rudder hinge horn holes Check all the hinge horn holes internal diameter within 0 2 mm tolerance in respect of nominal bushing diameter Right wing 02 09 Attachments Check all the attachments internal diameter within 0 3 mm tolerance in respect of nominal bolt diameter 02 10 Struts fork Check all the attachments internal diameter within 0 3 mm tolerance in respect of nominal bolt diameter ...

Страница 60: ...er pins and bushings of control surface 05 07 Hinge horn holes Check all the hinge horn holes internal diameter within 0 2 mm tolerance in respect of nominal bushing diameter Stabilizer 06 05 Attachments Check all the attachments internal diameter within 0 2 mm tolerance in respect of nominal bolt diameter 06 06 Attachment bolts and stop nuts Replace all the connection bolts nuts and check proper ...

Страница 61: ...horn holes internal diameter within 0 2 mm tolerance in respect of nominal bushing diameter Flight Control System 11 14 Joints Replace all the bolts stop nuts castle nuts with cotter pins and bushings of control system joints from stick pedals to surfaces horns 11 15 Flaperon mixer Inspect all the rotating point check the free play and correct function and installation of all the rotating points o...

Страница 62: ...ll the propeller hub bolts and nut Check proper torque closure add mark and safety wire where required 15 07 Pitch setting and balancing If changed blades pitch during hub disassembly perform blades pitch setup and propeller balancing Check propeller maximum speed on ground and in flight Engine 16 01 Engine Maintenance Manual Apply manufacturer approved documentation for Maintenance 16 19 Gearbox ...

Страница 63: ...muffler and seal all the manifolds From the terminal tube add constant pressure and check for any point around welding where the air leaks especially in the cabin heating chamber Flight instrument 29 02 Altimeter Check pressure setting and if needed perform altimeter calibration 29 03 Vertical Speed Indicator Check zero indication on ground and if needed perform calibration 29 04 Compass Check cal...

Страница 64: ...ates between the inboard and outboard Flaperon SC021 SC024 Replace the bolt and stop nut Distance between flaperon trailing edge must be 18 mm Left wing 04 17 Main spar attachment plate Replace the attachment plate 04 18 Front strut attachment plates Replace the strut attachment 04 19 Strut fork Replace all the struts forks and reassembly with new bolts and nuts 04 20 Flaperon horns Replace flaper...

Страница 65: ...ll the rudder hinge horns SG013 and SG010 which is on fuselage assembly Rudder 10 09 Hinge horns Replace all the rudder hinge horns SA087 3 SA087 4 10 10 Control system horn Check the rudder control system horn plate holes within tolerance of 0 2 mm in respect of the nominal bolt diameter ST508 Flight Control System 11 17 Pulley Replace the cables pulley its safety cotter pins and bolts nuts 11 18...

Страница 66: ...ed documentation for Maintenance 15 08 Overhaul Propeller overhaul Engine 16 01 Engine Maintenance Manual Apply manufacturer approved documentation for Maintenance 16 21 Overhaul Engine overhaul Fuel system 18 19 Wing tank cup Replace the fuel tanks cup support o ring Replace the cups o ring 18 20 Wing tanks Clean the tank internally 18 21 Collector tank Clean the tank internally 18 22 Auxiliary f...

Страница 67: ...about the description always contact the manufacturer to establish the correct maintenance action procedure and parts to replace 5 1 Heavy landing Control the aircraft before the next flight Main landing gear Verify the landing gear spring shape and integrity the attachments area the fuselage surrounding areas the spring constrain brackets and its bolts red rubber Vulcolan wheel rims tyres wheel a...

Страница 68: ...ing tank or cup fuel leakage When observed leakage from wing tank compartment open the inspection panel and find the source drain the fuel if required clean the humid area and replace the parts affected by the problem If the leakage comes from the tank support replace the entire tank If the leakage comes from a tank fuel fitting installed directly on the tank replace the fitting check if the tank ...

Страница 69: ...the propeller manufacturer maintenance manual or contact them directly As a general consideration if the propeller is intact in the all the blades shape verify the propeller pitch setting and perform the propeller balance If the engine has stop during the propeller strike apply the engine manufacturer maintenance manual 5 8 Engine failure Apply the engine manufacturer maintenance manual and all th...

Страница 70: ...the airplane 5 14 Flight envelope exceeding If any flight envelope or operational limitation not below described has been exceeded contact the manufacturer 5 14 1 Airspeed exceeding If the maximum airspeed Vne has been exceeded for more than 15 seconds and at more than 250 km h IAS verify all the structure and attachments of the wing struts and tailplane verify also the control system lines surfac...

Страница 71: ...f only with half flap extended at more than 145 km h verify all the flaperon structure shape and surfaces attachment horns and lateral control system joints hinges and control horns If any parts are not regular contact the manufacturer of the airplane 5 14 5 Take off mass exceeding If the maximum take off mass has been exceeded at more than 650 kg in combination with observed turbulence in flight ...

Страница 72: ...AINTENANCE MANUAL SAVANNAH S Doc No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 72 132 DOC FMM00 Left intentionally blank ...

Страница 73: ...kers type flaperon aileron flap to improve manoeuvrability at low speed The wings are rectangular in plan with small dihedral and without washout A virtual washout is introduced by different angle between inboard and outboard flaperons Wing structure is composed of main and aft spars with a torque box Two wing struts are connecting the wing and the fuselage Horizontal Tail plane is composed of sta...

Страница 74: ...NUAL SAVANNAH S Doc No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 74 132 DOC FMM00 Figure 11 Cabin floor Figure 12 Fuselage rear cone ...

Страница 75: ...L SAVANNAH S Doc No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 75 132 DOC FMM00 Figure 13 Cabin frame and windshield Figure 14 Left wing ...

Страница 76: ...c No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 76 132 DOC FMM00 Figure 15 Left inboard flaperon Figure 16 Left outboard flaperon Figure 17 Stabilizer ...

Страница 77: ... MANUAL SAVANNAH S Doc No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 77 132 DOC FMM00 Figure 18 Elevator Figure 19 Fin and Rudder ...

Страница 78: ...ted cables for the second section up to the elevator central horn Deflections are approximately 25 LATERAL the Flaperon are connected entirely by means of push pull rod which 15 5 of rotation The flap function is assured by the mechanical mixer shown in Figure 20 with 27 of down rotation Figure 20 Longitudinal and lateral controls DIRECTIONAL the rudders 28 of rotation is connected by means of cab...

Страница 79: ... 78 hp 58 kW 5500 RPM 92 hp 69 kW 5500 RPM Gear reduction ratio 2 27 2 43 Inner cylinder cooling Air Head cooling Liquid Engine EASA TCDS E 121 Engine ASTM CoC ASTM F2339 17 Compliance Statement FB 16 012 1 Q Table 24 Engines 6 3 2 Propeller Follows the installable propellers list and their specifications Manufacturer Model Type Diameter DUC Hélices Swirl Swirl R Swirl L Swirl 3 Swirl 3L On ground...

Страница 80: ...sion 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 80 132 DOC FMM00 6 4 Fuel system Follows the layout of the fuel system Figure 22 Airframe fuel system parts Figure 23 Wing standard fuel system ...

Страница 81: ... 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 81 132 DOC FMM00 Figure 24 Wing double fuel tank system interconnected tanks Figure 25 Wing double fuel tank system with transfer pumps Figure 26 Fuselage and Rotax 912 UL ULS fuel system ...

Страница 82: ...S fuel system The fuel system volumes are the following Tank Total capacity lt Fuel volume lt Not usable lt Wing tanks standard 2x36 72 2x35 70 2x0 5 1 Double wing tanks optional 4x36 144 4x35 140 4x0 5 2 Collector tank 6 standard 6 6 0 Collector tank 18 optional 18 18 0 Draining sump N A 0 25 0 25 Lines N A 0 5 0 5 Table 26 Fuel system volumes 6 5 Oil system Figure 28 Rotax 912 UL ULS iS standard...

Страница 83: ...3 132 DOC FMM00 Figure 29 Rotax 912 UL ULS iS oil system with thermostat Item Capacity lt Oil tank 2 5 3 Lines and radiator 0 5 TOTAL 3 5 Table 27 Oil system capacity 6 6 Cooling system Follows cooling system layout Item Capacity lt Expansion tank engine and pump 0 25 0 56 0 1 0 91 Overflow bottle 0 5 Lines and radiator 0 6 TOTAL 2 Table 28 Cooling system capacity ...

Страница 84: ...N Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 84 132 DOC FMM00 Figure 30 Rotax 912 UL ULS iS standard cooling system Figure 31 Rotax 912 UL ULS iS cooling system with thermostat ...

Страница 85: ...lies to Generic Serial Number yy mm 54 xxxx Page 85 132 DOC FMM00 6 7 Brake system Follows the layout of the braking system Figure 32 Standard brake system only right side is shown the left is identical symmetrical Figure 33 Brake system with parking brake only right side is shown the left is identical symmetrical ...

Страница 86: ...ial Number yy mm 54 xxxx Page 86 132 DOC FMM00 Figure 34 Double side brake system only right side is shown the left is identical symmetrical 6 8 Cabin heating and ventilation Figure 35 Cabin heating system The ventilation of the cabin is assured by two round ports called snap vent installed on the side window of the door one per each ...

Страница 87: ... at 14 2 0 3 V DC nominal with maximum 22 A current The engine start and the non continuous operations without generator active min 30 minutes are assured by the aircraft battery which can be selected between the followings Battery Model Nominal Voltage Energy Ah UNIBAT sealed lead acid VRLA standard CBTX20CH BS 12 6 18 UNIBAT sealed lead acid VRLA light CTZ10S BS 12 6 8 6 UNIBAT lithium LiFePo4 l...

Страница 88: ...MANUAL SAVANNAH S Doc No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 88 132 DOC FMM00 Figure 37 Electrical wiring firewall backward ...

Страница 89: ...ystem Auxiliary Electric Fuel Pump Facet ICP Exhaust Throttle lever Intake carburettor filters 4 points Seat Harnesses ICP Wheel and Tyres any Brakes system ICP Compass ICP 80 mm Airspeed Indicator km h ICP 80 mm Altimeter ft ICP 80 mm RPM Hourmeter Indicator VDO ICP Oil Pressure Luciano Sorlini H2O Temperature Rx or Lx VDO Manuals Flight Manual POH Wheel Seats Powerplant Systems Flight Instrument...

Страница 90: ...ator Compass ICP 80 mm Airspeed Indicator km h ICP 80 mm Altimeter ft ICP 80 mm Vertical Speed Indicator ft min ICP 80 mm Round Slip Indicator ICP 57 mm RPM Hourmeter Indicator VDO ICP Oil Pressure Luciano Sorlini Oil Temperature Motometer H2O Temperature Rx VDO H2O Temperature Lx VDO Fuel Pressure Strumentazione Industriale Voltmeter VDO Airbox External Temperature Indicator ICP Other 12V Plug La...

Страница 91: ...Tail Dragger 6 tail wheel MATCO 8 Tail wheel MATCO standard 4 Wheels Fairing 6 Wheels Fairing Flap Electrical actuation Panel Switch Position Indicator Double Control Stick Ray Allen Stick Grip Left Trim Control Button PTT Ray Allen Stick Grip Right PTT 140 lt Double Wing Fuel Tank 18 lt Collector Tank Indicator Unit Shut off valve for left Wing only Right side Brake Pedals Parking Brake System Do...

Страница 92: ...er for dual control stick Document drawer rudder cables cover Cabin upholstery Courtesy mats Tie down kit Lifting Hook Towing Bar Cabin Cover Integral Parts Primer Custom colors and design Arrow Cowling Tail decals Custom decals Construction Manual Technical Specification SXXXX Airspeed Indicator Winter 57 mm Altimeter Winter 57 mm Vertical Speed Indicator Winter 57 mm Winter Slip Indicator Turn a...

Страница 93: ... Artex 345 Manifold Pressure ICP Flybox Vigilus Garmin G3X system monitor modules Dynon EMS D10 monitor modules Dynon SV D700 monitor modules Dynon SV D1000 monitor modules Dynon SV HDX1100 7 10 monitor modules MGL iEFIS Discovery 7 MGL iEFIS Explorer 8 5 AVMap EngiBOX Kanardia NESIS EFIS EIS 7 10 Kanardia EMSIS EIS UMA 2 1 4 in mechanical manifold pressure gauge Airgizmos Rack AERA 660 Airgizmos ...

Страница 94: ...lugs on Baggage compartment COM Funke ATR833 II TRX Funke TRT800H COM TQ KRT2 TRX TQ KTX2 COM Trig TY91 TY92 TRX Trig TT21 TT22 ELT ACK E 04 ELT Artex ELT345 ELT Kannad 406 COM Dynon SV COM X83 TRX Dynon SV XPNDR 26X COM Garmin GTR200 200B TRX Garmin GTX335 COM X Com VHF Radio and Comant 121 Antenna TRX Microair T2000 Mode S or Mode C Transponder Intercom Dynon SV INTERCOM 2S Intercom Flightcom 40...

Страница 95: ...s for painting degreaser Lechler Hydro Cleaner Slow 00665 External paint External water based paint Lechler Hydrocryl 2K pigments hardener 50 water 15 Primer optional Parts integral primer water based Lechler Hydropur Primer hardener 15 water 25 Table 33 Painting products NOTE Different type of painting or product or mix to obtain RAL colors can be used to protect the airplane or protect parts dur...

Страница 96: ...AINTENANCE MANUAL SAVANNAH S Doc No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 96 132 DOC FMM00 Left intentionally blank ...

Страница 97: ...e voltage of the battery must be about 12 5 V the engine must be off Set the left inner Flaperon on the ZERO of the jig SA200VG The tolerance during the ground setting is 0 5 Set the right inner Flaperon on the ZERO of jig SA200VG Verify the setting with the following procedure Unlock the control stick and move it Move the left inner Flaperon by hand and set to the ZERO of the jig SA200VG Not touc...

Страница 98: ...07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 98 132 DOC FMM00 Figure 38 Flaperon jig SA200VG and position on the first wing rib Figure 39 Position of jig SA200VG near the first rib rivets line aligned to wing trailing edge ...

Страница 99: ...022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 99 132 DOC FMM00 Figure 40 ZERO setting of the left inner Flaperon Marks of 0 5 of tolerance Figure 41 Push pull rods for Flaperon setup Torque tube bell crank Push pull vertical rods Uniball ...

Страница 100: ...od Move the electric potentiometer in the proper position by monitoring the Flap indicator Master must be active Verify that for Full Flap the indicator goes down to the last lower LED indication Close the two screw of the electric potentiometer bracket Close the seat inspection panel with rivets 7 1 3 Flight check of Flaperons During flight at approximately 500 kg of weight two occupants of same ...

Страница 101: ...Table 35 Check the Elevator deflection with the digital level in the position shown in Figure 44 The angle read must be 19 with 0 5 of tolerance Figure 45 Attention the Elevator deflection angle in respect of its chord is rotated of 6 because the reading of the bubble is performed in the upper skin of the Elevator If the angle resultant is not correct perform the following procedure Change the Ele...

Страница 102: ...Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 102 132 DOC FMM00 Figure 43 Longitudinal line bell crank on the full nose up position against stop Figure 44 Digital spirit level position on Elevator First rib rivets line Elevator upper skin starts ...

Страница 103: ...n dimensions of the push pull rod of the longitudinal control system from uniball to uniball center codes on CM and SPC of reference documents in Chapter 1 2 Code Length mm SS035 530 0 5 Table 35 Longitudinal CS push pull rod dimension 7 1 5 Rudder control system 7 1 5 1 Rudder pedals alignment to rudder and nose wheel Basically the Rudder the nose wheel and the Rudders pedals must be aligned toge...

Страница 104: ...e airplane during leveled cruise flight at 75 of power 5000 RPM no turbulence no wind below 2500 ft of Density Altitude and approximately 500 kg of weight with two occupants of same weight on board side CG centered if differently obtainable During this flight condition set the roll at zero Bank angle eventually maintained by piloting with control stick and then free the Rudder pedals control weigh...

Страница 105: ...s an adjustment plate with many holes to tension or release the cable in function of the direction of rotation needed 7 1 8 Brake pedals position on Rudder pedals To orient the brake pedals is only necessary to regulate the length of the brake pumps When enlarged the end fitting of the pump rod the pedals goes back near to the pilot when shortening the length the pedals rotate forward Attention to...

Страница 106: ...l the cotter pin Attention do not close excessively the nut because it can force the hinge point around the rotation After the setup check the hinge point free play within tolerance and verify the cotter pin is installed rigidly Figure 46 Control surfaces hinges 7 4 Fuel system drainage To drain the fuel system basically open the fuel drain valve located below to the Collector tank If the airplane...

Страница 107: ...k The brake oil pump has the oil tank in its upper part where the section is larger The cup is just pressed and is not provided a perfect sealing therefore it is possible to see a very small amount of oil over the cup especially near the external seeger The presence of oil is acceptable only if is not in such a quantity that can drop in the aircraft floor If too much leaking is evaluated clean the...

Страница 108: ...must be followed to drain and change the engine lubricating oil Run the engine and warm up to 40 to 50 C of oil temperature Shut off the engine and check magnetos and master are off Open the engine cowling and let cool down the engine just a couple of minutes If not necessary a complete drainage jump this step Differently perform the following actions disconnect the return line IN from the oil tan...

Страница 109: ...n the engine upper cowling and let cool down the engine just a couple of minutes Rotate the propeller up to the oil tank is gurgling and verify newly the oil level If required replenish the oil up to the proper level middle between min and max is the optimum From min to max level of dipstick is approximately 0 5 lt 7 9 Coolant level verification CAUTION The complete instruction for this verificati...

Страница 110: ... to open the airbox by means of the two side screw nut Then remove the air filter check the condition of cleaning dust sand oil fuel contamination Clean the air filter by means of compressed air only If necessary replace the air filter with a spare new one Replace also in case of wears of the corner of the filter 7 12 Tyre change Replace the tyre when time table limits prescribes or tyre expiring ...

Страница 111: ... leave the aircraft on ground 7 13 Windshield cracks Stop the crack with a small hole about 1 mm diameter The improper cleaning or improper detergent of the windows are the main causes of the cracks consider to change the method If excessive cracks of scratches are found which causes the vision blurred or obscured vision replace the window of windshield with a spare new one 7 14 Wheel fairing crac...

Страница 112: ...INTENANCE MANUAL SAVANNAH S Doc No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 112 132 DOC FMM00 Left intentionally blank ...

Страница 113: ...n applied to the Aircraft and its equipment use the following table to record all the maintenance performed The maintenance of the engine must be recorded on its dedicated Engine Logbook Apply similarly where a separate Logbook is given by the manufacturer of the equipment i e the Propeller To have a complete details of each single action performed attach to the present record also the model shown...

Страница 114: ...H EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 114 132 DOC FMM00 Maintenance performed Effective Operating Hours Maintenance performed Description Date Signature Table 40b ...

Страница 115: ...H EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 115 132 DOC FMM00 Maintenance performed Effective Operating Hours Maintenance performed Description Date Signature Table 40c ...

Страница 116: ...07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 116 132 DOC FMM00 Maintenance performed Effective Operating Hours Maintenance performed Description Date Signature Table 40d a d Maintenance record table ...

Страница 117: ... SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 117 132 DOC FMM00 Service Bulletin performed Operating Hours Date Signature Table 41 Service Bulletin performed table ...

Страница 118: ... MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 118 132 DOC FMM00 Change or Repair performed Operating Hours Date Signature Table 42 Change or Repair performed ...

Страница 119: ...te 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 119 132 DOC FMM00 ANNEX A Request of Technical Intervention on the Aircraft Module to fill in for a request of technical intervention on an aircraft to I C P Srl workshop ...

Страница 120: ...MAINTENANCE MANUAL SAVANNAH S Doc No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 120 132 DOC FMM00 ...

Страница 121: ...vision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 121 132 DOC FMM00 ANNEX B Feedback about ICP Aircraft Module to fill in with the purpose to send a feedback to I C P Srl about the airplane ...

Страница 122: ...MAINTENANCE MANUAL SAVANNAH S Doc No MM SVNH EN Revision 07 Rev Date 07 11 2022 Proj Ref SVNH S A C Savannah S Applies to Generic Serial Number yy mm 54 xxxx Page 122 132 DOC FMM00 ...

Страница 123: ...nce Manual NOTE OF MAINTENANCE Replaced parts unusual maintenance repairs other actions TEST FLIGHT Flight time airfield operator note other actions Operator and or Responsible signature Note attach to the present form the Maintenance Checklist copy performed and signed in the relevant section for the maintenance performed Info copy or print directly the Maintenance Logbook Model Pag 97 to 106 and...

Страница 124: ...n i e point not present Instead of the checks is also possible to add the signature of the person who performed the maintenance point The column Ind Ck stands for the Independent Check which identifies few verification points only the ones not highlighted grey that are required to be additionally verified by an independent personnel eventually involved in the maintenance organization Scheduled Mai...

Страница 125: ... 54 xxxx Page 125 132 DOC FMM00 Structure System N Check Ind Ck Note Right Wing 02 04 02 05 02 06 02 07 02 08 02 09 02 10 02 11 02 12 02 13 02 14 02 15 02 16 Right Flaperon 03 01 03 02 03 03 03 04 03 05 03 06 03 07 03 08 Left Wing 04 01 04 02 04 03 04 04 04 05 04 06 04 07 04 08 04 09 04 10 04 11 04 12 04 13 04 14 04 15 04 16 04 17 04 18 04 19 04 20 ...

Страница 126: ...26 132 DOC FMM00 Structure System N Check Ind Ck Note Left Flaperon 05 01 05 02 05 03 05 04 05 05 05 06 05 07 05 08 Stabilizer 06 01 06 02 06 03 06 04 06 05 06 06 06 07 06 08 06 09 06 10 06 11 Elevator 07 01 07 02 07 03 07 04 07 05 07 06 07 07 07 08 07 09 07 10 07 11 Trim Tab 08 01 08 02 08 03 08 04 08 05 Vertical Tail Fin 09 01 09 02 09 03 09 04 09 05 09 06 09 07 ...

Страница 127: ... 132 DOC FMM00 Structure System N Check Ind Ck Note Vertical Tail Fin 09 08 09 09 Rudder 10 01 10 02 10 03 10 04 10 05 10 06 10 07 10 08 10 09 10 10 Flight Control System 11 01 11 02 11 03 11 04 11 05 11 06 11 07 11 08 11 09 11 10 11 11 11 12 11 13 11 14 11 15 11 16 11 17 11 18 11 19 11 20 Main landing gear 12 01 12 02 12 03 12 04 12 05 12 06 12 07 12 08 12 09 12 10 ...

Страница 128: ...k Ind Ck Note Main landing gear 12 11 12 12 12 13 12 14 Main landing gear tail dragger if configured with 12b 01 12b 02 Nose landing gear 13 01 13 02 13 03 13 04 13 05 13 06 13 07 13 08 13 09 13 10 13 11 13 12 13 13 13 14 13 15 13 16 Tail landing gear if configured with 13b 01 13b 02 13b 03 13b 04 13b 05 13b 06 13b 07 13b 08 13b 09 Engine cowling 14 01 14 02 14 03 Propeller 15 01 15 02 15 03 15 04...

Страница 129: ...e 129 132 DOC FMM00 Structure System N Check Ind Ck Note Propeller 15 06 15 07 15 08 Engine 16 01 16 02 16 03 16 04 16 05 16 06 16 07 16 08 16 09 16 10 16 11 16 12 16 13 16 14 16 15 16 16 16 17 16 18 16 19 16 20 16 21 Powerplant controls 17 01 17 02 17 03 17 04 17 05 17 06 17 07 17 08 17 09 17 10 17 11 17 12 17 13 17 14 Fuel system 18 01 18 02 18 03 18 04 18 05 ...

Страница 130: ... mm 54 xxxx Page 130 132 DOC FMM00 Structure System N Check Ind Ck Note Fuel system 18 06 18 07 18 08 18 09 18 10 18 11 18 12 18 13 18 14 18 15 18 16 18 17 18 18 18 19 18 20 18 21 18 22 18 23 Water system 19 01 19 02 19 03 19 04 19 05 19 06 19 07 19 08 19 09 19 10 19 11 19 12 Oil system 20 01 20 02 20 03 20 04 20 05 20 06 20 07 20 08 20 09 20 10 ...

Страница 131: ...ucture System N Check Ind Ck Note Oil system 20 11 20 12 20 13 20 14 20 15 20 16 Intake system 21 01 21 02 21 03 21 04 21 05 21 06 21 07 21 08 21 09 21 10 Exhaust system 22 01 22 02 22 03 Cabin heating 23 01 23 02 23 03 Electrical system 24 01 24 02 24 03 24 04 24 05 24 06 24 07 24 08 24 09 Marking and placards 25 01 Ground run up check 26 01 26 02 26 03 26 04 26 05 26 06 26 07 26 08 ...

Страница 132: ...tem N Check Ind Ck Note Flight check 27 01 27 02 27 03 27 04 27 05 27 06 27 07 27 08 27 09 27 10 27 11 Avionics 28 01 Other equipment 29 01 29 02 29 03 29 04 29 05 Maintenance close out 30 01 30 02 30 03 30 04 30 05 30 06 Colour legend Colour Meaning 50 hrs maintenance 100 hrs maintenance 200 hrs maintenance 1000 hrs maintenance 2000 hrs maintenance To Apply to fill Not Applicable not to fill ...

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