BOTTOM OF

3 (FF-STP-002-X-A-)

55.4

BOTTOM OF

2 (FF-STP-001-X-A-)

55.5

3

2

4

2

3

1

EXPLODED VIEW

Step 1 (This Step needs to be completed before riveting the centre fuselage side & front skins.)Starting from the bottom of the firewall cleco the strips parts 2 & 3 onto the firewall part 1.See the identification diagram to find the correct sides of the strips to start with.

Step 2Cleco the reinforcement angle part 4 in place.

IDENTIFICATION DIAGRAM

R

DESCRIPTION

D

MOUNTING STRIPS

Sling

DESCRIPTION pg 1

FIREWALL FORWARD

pg 1

A

DETAIL A

ITEM NO. PART NUMBER Description QTY.1 FF-FWL-001-C-A- Firewall 12 FF-STP-001-X-A- Wide Cowling Mounting Strip 23 FF-STP-002-X-A- Front Skin Mounting Strip 24 FF-ANG-001-C-A- Reinforcing Piece 1

FF-STP-001-X-A-0

FF-STP-002-C-A-0

FF-FWL-001-C-A-

FF-ANG-001-C-A-

FF-STP-002-C-A-

FF-STP-001-X-A-

4 Date:2016/11/18 Revision 1

11

16

ITEM NO. PART NUMBER Description QTY.1 EN-ASS MNT-C-A- Engine Mounting - As Welded 12 FF-FWL-001-C-A- Firewall 13 FF-SPC-001-X-A- Bracket Spacer 44 CF-BKT-020-L-A- Top Steel Bracket - Left 15 CF-BKT-020-R-A- Top Steel Bracket - Right 16 CF-TNG-003-X-A- Tang for Parachute 27 HW-ANW-500-X-X- AN 5 Thin Washer 28 HW-ANB-510-X-X- AN 5 - 10 Bolt 29 HW-ANB-507-X-X- AN 5 - 7A Bolt 210 FF-PLT-001-X-A- Firewall Forward Plate 211 HW-ANL-500-X-X- AN 5 Locknut 612 HW-ANB-505-X-X- AN 5 - 5 Bolt 213 CF-BKT-019-L-A- Galvanised Steel Bracket - Bottom & Left 114 CF-BKT-019-R-A- Galvanised Steel Bracket - Bottom & Right 115 CF-CHL-023-C-A- Firewall Mounting Channel - Bottom 116 HW-ANW-500-X-X- AN 5 STD Washer 4

10

2

15

1

11

14

5

Step 1

Cleco and then rivet the steel plates part 10 onto the firewall part 2 .

Step 2Bolt the rest of the parts together.

EXPLODED VIEW

DESCRIPTION pg 2

Date:2016/11/18 Revision 3Sling 4

Fitting engine mount - for parachute plane

12

13

34

6

9

8

7

As shown in the exploded view.

94

36

8

SEE DETAIL A

2

5

Step 1Drill four Ø3.3 holes in the coupling pipe part 1 corresponding to the holes in the plate part 8 tabs. (See Detail A)Do not rivet through the holes yet, the coupling will be riveted through the air hose during installation.

Step 2Cleco and then rivet the side panels parts 6 onto the housing part 8 .

Step 3Cleco and then rivet the the cable mounting angle part 7 onto the closing plate and then the closing plate part 3 onto the hinge part 2 . (See Detail B for position and orientation of parts)

Step 4Mark and cut 3mm Heat Resistant Foam part 9 , which is glued onto the closing plate part 3 with heat resistant glue.

Step 5Cleco all the parts together, do not rivet them yet, this is done through the firewall.

EXPLODED VIEW

7

121212

13

11

8

USE EXISTING HOLES IN TAB PART 8 TOLOCATE DRILLING POSITIONS ON COUPLING PIPE

1

ASSEMBLED VIEW

4

3

DETAIL B

DETAIL A

ITEM NO. PART NUMBER QTY.1 FF-PPE-001-C-A- 12 FF-HNG-001-C-A- 13 FF-PLT-007-C-A- 14 FF-ANG-013-C-A- 15 FF-ANG-012-C-A- 16 FF-PNL-002-X-A- 27 FF-PLT-006-C-A- 18 FF-CHL-006-C-A- 19 CF-FOM-001-X-X- 111 HW-SBM-312-X-X- 112 HW-MTW-030-X-X- 313 HW-MTL-030-R-X- 1

Date:2016/11/18 Revision 3Sling 4

DESCRIPTION pg 3

Cabin heat splitter box (V)

Cabin Heat Installation 2016/11/25 – Revision 1

Attaching Muffler & Clamps

EN-CLM-006-X-X-

EN-CRV-002-X-A-

As seen to the left when

installing EN-CVR-002-X-A-

ensure that the rivet holes are

positioned at the bottom.

Once you have placed your

clamps around the exhaust you

are then able to first cleco then

rivet EN-CVR-002-X-A- into

place onto EN-CLM-006-X-X-.

Inlet Pipe

EN-CRV-002-X-A-

EN-PLT-005-X-A-

AC-TUB-001-X-X-

Once Muffler is in place, Cleco AC-TUB-001-

X-X- & EN-PLT-005-X-A- together.

After you are happy with the Clecoed parts

attach both to the muffler by cleco’ing and

then riveting all parts together. This will be

done on both openings in the Muffler.

Hose Installation

Start by attaching the hose to the outlet point of the muffler, the hose must go over the outlet pipe

and must be clamped.

This hose when being routed up

to the Cabin Heat box as seen,

can be cable tied to the bottom

of the engine mount to be held in

position.

When attaching the hose to the

Cabin heat box, the hose must be

clamped into position over the

Cabin Heat box pipe.

TURBO SERVER

RDAC ATTACH USING M5 RIVNUTS,M5 RUBBER MOUNT STUDSAND M5 NYLOC LOCK NUTS.

TCU COMES WITH THE ENGINEWITH FIXINGS.

AMBIENT PRESSURE SENSORATTACH USING M5 x 16mm BUTTONHEADSCREWS AND M5 WASHER.

BATTERY BOXATTACH USING 3.2mm RIVETS.

STARTER RELAYATTACH USING M5 RIVNUTS, M5 RUBBERMOUNT AND M5 NYLOC LOCK NUT.

CABIN HEAT SPLITTER BOXATTACH USING M3 RIVNUTS ANDM3 x 16mm BUTTOHEAD SCREWS.

FUEL PUMPATTACH USING M5 RIVNUTS AND M5 x 16mmBUTTON HEAD SCREWS.

OIL TANKATTACH USING2 x Clamp 130-150.

FF-ANG-016-X-X- ATTACH USING M4 RIVNUTS ANDM4 x 16mm BUTTONHEAD SCREWSFIT M5 RIVNUT ONTO THE TOP HOLE.

FF-ANG-015-X-X- ATTACH USING M4 RIVNUTS AND M4 x 16mm BUTTONHEAD SCREWS.

OVER FLOW BOTTLE ATTACH USING7.5 CABLE TIES TO TIE ITONTO THE BRACKETS.

OVER FLOW BOTTLE BRACKETATTACH USING THE 3.2mm RIVETS TO ATTACH FF-ANG-004-X-A-

BRAKE RESERVIOR BRACKETATTACH USING 4.8mm RIVETS.

FF-BKT-008-X-A-ATTACH USING3.2mm RIVETSGPS TO BE TIED WITH

4.5mm CABLE TIES.

OIL TANK BRACKET ATTACH USINGUSING 4mm RIVETS.

ATTACH USING M3 RIVNUTS ANDM3 x 16mm BUTTONHEAD SCREWS.

FUEL PUMP COVERATTACH USING M4 RIVNUTSAND M4 x 16mm BUTTONHEAD SCREWS.ADD THE HEAT SHEILD ONTO THE COVER.

FIT THE BATTERY STRAPBETWEEN THE FIREWALLAND FF-PLT-009-C-A-0USING THE 4mm RIVETS.

FRONT

Date:2016/11/08 Revision 1Sling 4

DESCRIPTION pg 4

REGULATORFIT M6 RIVNUTS ONTO THEFIREWALL, THEN USE THE M6RUBBER MOUNTS TO ATTACH THEREGULATOR AND CLOSE IT OFF WITHAN M6 WASHER AND M6 NYLOC NUT.

HW-GRM-003-X-X-6x10x13 GROMMETELECTRICS EARTHING CABLE

CABIN HEAT INSIDE COVERATTACH WITH 3.2mm RIVETS

HW-GRM-005-X-X-10x12x18 GROMMETTHROTTLE CABLE

REAR

HW-GRM-005-X-X-10x12x18 GROMMETTHROTTLE CABLE

HW-GRM-006-X-X-12x20x24 GROMMETFUEL LINE RETURN

HW-GRM-003-X-X-6x10x13 GROMMETENGINE CHOKE CABLE

HW-GRM-003-X-X-6x10x13 GROMMETHEATER CABLE

HW-GRM-006-X-X-12x20x24 GROMMETFUEL LINE

HW-GRM-006-X-X-12x20x24 GROMMETBRAKE LINE

HW-GRM-003-X-X-6x10x13 GROMMETENGINE CHOKE CABLE

UP-PLT-001-X-A-FIT THE LEATHER BOOTBETWEEN UP-PLT-001-X-A-AND THE FIREWALL USING3.2mm RIVETS.

Date:2016/11/08 Revision 1Sling 4

DESCRIPTION pg 5

FIREWALL SETUP FOR 914 UL (REAR)

HW-CRM-302-X-X- (CRIMP)

HW-HCP-011-X-X-

RUBBER CONNECTOR

CF-BKT-026-X-A-

CF-BKT-025-X-A-

CF-BKT-025-X-A-

TO ATTACH THE BRACKET AND FUEL PUMPUSE THE HW-CLM-106-X-X- (CLAMP)

914 FUEL PUMP

TO BE JOINT USING 4mmRIVETS.

Date:2016/11/09 Revision 2Sling 4

DESCRIPTION pg 6

FUEL PUMP 914

Return from regulator

to fuel selector.

Supply from fuel

pumps to regulator.

Supply from fuel

selector to fuel pumps.

Fuel pressure sensor

tapped off from regulator.

Fuel flow sensor in line

with fuel to right carb.

Fuel to left carb.

HW-ANL-040-R-X-

HW-ANW-040-X-X-

FF-BSH-002-X-X-

HW-MTW-063-X-X-

HW-MTW-063-X-X-

HW-ANB-425-X-X-

TURBO SERVO

WASHER AND THE NUT TOBE FITTED ON THE INSIDE OFTHE FIREWALL.

TURBO SERVO

Date:2016/11/25 Revision 2Sling 4

DESCRIPTION pg 7

TURBO SERVO

To Oil Thermostat(Oil Pickup)

B

Oil Tank(As Viewed From Firewall)

90 Push On Hose End+ 22 OET Clamps / C Clamps(Inlet & outlet of Oil Tank)

InletOutlet

5/16'' I/D Hose

5/16'' I/D Hose

A

Oil Thermostat(As Viewed From Above)

To Oil Cooler

To Oil Pump

5/16'' Barb(x4) Push On Fitting+ 22 OET Clamps /C Clamps(Inlet & Outlet Side of Thermostat)

5/16'' Barb Push On Fitting+ 22 OET Clamps /C Clamps(Inlet & Outlet Side of Oil Cooler)

C

Engine Oil System For Rotax 912UL / 912IS / 914 UL (Refer To Manual Of Specific Engine Supplied For Further Details )

Oil Cooler(As Viewed from Firewall)

To Oil Pump

From Oil Sump(Return to Oil Tank)

D

NOTE:All Hoses 5/16'' I/DThroughout Oil System

LegendPart Name

A Oil TankB Rotax 912 ULS Engine (Top View)C Detail of Oil ThermostatD Oil Cooler Date:2016/11/08 Revision 1Sling 4

DESCRIPTION

ENGINE OIL SYSTEMSCHEMATIC

pg 8

914 OIL SYSTEM INSTALLATION 2016/11/24 – Revision 0

Oil Reservoir Overflow Hose In

Overflow Hose Out

Oil Cooler

Hose Out 1 of 2

Hose Out 1 of 2

Hose Out 2 of 2

Jaco

Stamp

OIL THERMOSTAT MOUNTING

2016/11/25 – REVISION 0

4 x HW-ACS-612-X-X-

1 x EN-TMS-001-X-X-

4 x HW-MTW-062-X-X-

2 x HW-MTL-060-X-X-

2 x HW-MTW-062-X-X-

1 x EN-BKT-001-X-X-

2 x HW-RBM-060-X-X-

I

Engine Top ViewNote: Some components omitted

For Clarity

Radiator coolant Hose - Right25mm I/D

To Water Pump

C

Engine Water Cooling System For Rotax 912 ULS, 912 IS & 914 UL(Refer To Manual Of Specific Engine Supplied For Further Details)

As Viewed From Firewall 25-40 C - Clamp25-40 C - Clamp

B

25-40 C - Clamp

As Viewed From Above

Coolant Hose6mm I/D Black

15 OET Clamp

C - Clamp(Supplied with engine)

A

As viewed From Left

Radiator coolant Hose - left25mm I/D

D

LegendPart Name

A Detail Of Expansion TankB RadiatorC Rotax 912 ULS EngineD Water Reservoir

Date:2016/11/08 Revision 1Sling 4

DESCRIPTION

ENGINE WATER SYSTEMSCHEMATIC

pg 9

Fitment of the Cowling 2016/11/25 Revision 0

Outline of procedure: 1. Prepare cowling. 2. Positioning of Dzus fasteners between top and bottom cowling. 3. Positioning of cowling on firewall. 4. Trimming rear of cowling to conform to firewall. 5. Transferring holes from firewall strips to cowlings. 6. Installing Dzus fasteners. 7. Assembly of cowl and final checks. STEP 1: Preparing cowling Stand the cowlings upright (spinner pointing upwards) and loosely fit the top and bottom cowlings together. Sand and file the top cowling’s edge line carefully until it conforms to the bottom cowling joggle.

Figure 1.

STEP 2: Positioning of Dzus fasteners between bottom and top cowling With reference to Figure 2 and with the cowlings standing upright (spinner pointing upwards), mark a point on the top cowling 55mm down from the front of the top cowling and 11mm from the edge line. From this point, measure and mark three holes with a common pitching of approximately 28.4mm, maintaining an 11mm edge distance (refer to Figure 3). Firmly join the top and bottom cowlings with masking tape. Carefully drill 2.5mm pilot holes through both cowlings at the points marked and use a clecoes before drilling the next hole.

Figure 2. Figure 3.

STEP 3: Positioning of Cowling on Firewall

With the assistance of a 2nd person, fit the top and bottom cowlings to the firewall to achieve the following:

a. the front of the cowling is concentric with the rear of the spinner, and b. there is a gap of approximately 5 mm between the back of the spinner and the front of the

cowlings.

Figure 4.

Using masking tape or similar to hold the cowlings (clecoed together) in place on the aircraft while you make adjustments. Note that the cowling will overlap the fuselage. Step 4: Trimming rear of cowling to conform to firewall Using pin-striping tape or similar, carefully mark a line across the rear of the top cowling to denote where to trim off excess cowling. Remember to slightly offset your mark rearwards to allow for fine adjustments later by sanding and filing. Once the fitment and alignment of the top cowling is completed, repeat the above step for the bottom cowling. Remember to monitor the alignment of the cowling with the spinner as you progress. STEP 5: Transferring holes from firewall strips to cowlings Remove the lower cowling and use the 8 mm holes in the firewall strips as best as possible to align an 8mm drill bit as you drill from the inside of the top cowling. This may be easier if you transfer the 8 mm hole from the firewall strip to the cowling with a marker. Remove the cowl from the aircraft and drill or grind the holes. Repeat the above process for the lower cowling. Remember to monitor the alignment of the cowling with the spinner as you progress.

Step 6: Installing Dzus Fastener SpringsOnce you are satisfied with the fitment and alignment

between the lower and upper cowlings and between the cowlings and the firewall, begin fitting the

Dzus fasteners springs as described below. The Dzus fasteners springs will be fitted to the bottom

cowling only (along the join between the top and bottom cowlings) and to the firewall strips.

Bottom Cowling – Cowling Join Line Enlarge the 2.5 mm pilot holes in the bottom cowling to 8 mm. Align the Dzus fastener springs ensuring the middle of the spring is centred with the 8 mm holes. Drill 3.3 mm holes through the coiled ends of the springs. Countersink these from the outside of the cowling. Rivet the spring to the inside of the bottom cowl using 3.2 x 8 mm aluminium countersunk blind rivets.

Figure 5. Figure 6.

Top Cowling – Cowling Join Line Enlarge the 2.5 mm pilot holes in the top cowling to 8 mm. Fit the Dzus clips to the top cowling using the required Dzus tool.

Figure 7. Figure 8.

Top and Bottom Cowling – Firewall Join Line Fit the Dzus clips to the top and bottom cowling using the required Dzus tool. Fit the Dzus fastener springs to the firewall strips using the same method as described above. STEP 7: Assembly of cowl and final checks Finally, test fit the cowling on the aircraft. Make fine adjustments by sanding and filing the rear edge If necessary.

Figure 9. Figure 10.