BRITISH MICROLIGHT AIRCRAFT ASSOCIATION HOMEBUILT AIRCRAFT DATA SHEET (HADS) NO: HM10 ISSUE: 15

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1 TYPE MXP-740 Savannah 1 (1) MANUFACTURER Individual aircraft are amateur constructed. BMAA is responsible for continued airworthiness. (2) UK IMPORTER UK Importer of Kits, Sandtoft Ultralights Partnership, c/o Low Lodge, Main Street, West Haddlesey, YO8 8QA Kits are manufactured by ICP Srl, Via Torino 12, Piovà Massaia, Italy. (3) CERTIFICATION BCAR SECTION S Issue 2. Except that: Ignition switches on early aircraft may be fitted in the reverse sense so long as the originally supplied, guarded, switches are fitted. (4) DEFINITION OF BASIC STANDARD Savannah/Savannah VG/Savannah XLS Construction Manual. (5) COMPLIANCE WITH THE MICROLIGHT DEFINITION (a) MTOW (b) No. Seats 2 (c) Maximum Wing Loading 450 kg Classic : 35.0 kg/m² VG & XLS : 37.9 kg/m² (d) Vso Classic : 28 kts CAS 2 (e) Permitted range of occupant weights (f) Typical Empty Weight (ZFW) (g) ZFW kg crew + 1 hr fuel (21 litres / 15 kg) (h) ZFW + 86 kg pilot + full fuel (77 litres / 55.4 kg) (i) Max allowed ZFW at initial permit issue 3 VG & XLS : 29 kts CAS Min 55 kg total weight Max 120 kg per seat 261 kg 448 kg kg 263 kg (Jabiru 2200 variants) 267 kg 4 (Jabiru 2200 variants) 270 kg (Suzuki LS100 variants) 1 Note: During aircraft construction, this HADS is to be used with the Savannah stage inspection sheets, form BMAA/AW/022 (Savannah). If there is a conflict between the two, the latest HADS will always take precedence. 2 V SO is based upon aerodynamic stall at aft CG, apparent stall speed may increase by up to 7kts CAS at further forward CG positions. 3 The maximum ZFW is the lower of [(a)-(172kg+1hrs fuel)] or [(a)-(86kg+full fuel)]. 4 Use of the higher maximum ZFW requires maximum continuous power to be limited to 2800 rpm by placard. HADS HM10 issue 15 Page 1 of 16

2 (6) POWER PLANTS BRITISH MICROLIGHT AIRCRAFT ASSOCIATION Designation Savannah Jabiru(1) Savannah Jabiru(2) Savannah Jabiru(3) Engine Type Reduction Gear Exhaust System Jabiru 2200 After serial 22A710 Direct Drive Jabiru Tractor exhaust, stainless steel (not yet approved) Intake System Bing type 64/32 carb + single K&N Filter. Engine oil carb-body heater fitted. Propeller Type GT 2 2 blade laminated wood GT2/151/107 Powerfin 2 blade square tip Warp Drive 2 blade (High Power Hub) Propeller Dia x Pitch 151cm x 107cm (59.5 x 42 ) 64 x 10 64, pitch TBD Noise Type Cert No. 182M Issue 1 182M Issue 1 TBA MAAN approving TBA Designation Savannah Jabiru(4) Savannah Jabiru(5) Savannah LS(1) Engine Type Jabiru 2200 After serial 22A710 Suzuki LS1000 (Bilsam modified) Reduction Gear Direct Drive Internal 2.4:1 Exhaust System Jabiru Tractor exhaust, stainless steel Savannah/Suzuki, stainless steel Intake System Bing type 64/32 carb + single K&N Filter. Engine oil carb-body heater fitted. Fuel injected with Rapier oiled filter Propeller Type GT 2 2 blade laminated wood GT2/157/98 GT 2 2 blade laminated wood GT2/157/100 Kiev 273/ blade Propeller Dia x Pitch 157cm x 98cm (62 x 38.6 ) 157cm x 100cm (62 x 39.4 ) 170cm, 53cm radius Noise Type Cert No. 182M Issue 2 182M Issue 2 182M Issue 3 MAAN approving HADS HM10 issue 15 Page 2 of 16

3 Designation Engine Type Savannah VG Jabiru(1) Savannah VG Jabiru(2) Savannah VG Jabiru(3) Jabiru 2200 After serial 22A710 Savannah VG Jabiru(4) Reduction Gear Direct Drive Exhaust System Jabiru Tractor exhaust, stainless steel Intake System Bing type 64/32 carb + single K&N Filter. Engine oil carb-body heater fitted. Propeller Type Arplast Ecoprop 166 4T R110/2 2 blade GT 2-2 blade laminated wood GT2/157/98 GT 2-2 blade laminated wood GT2/157/102 Sensenich 2A0J5R62H 2 blade Propeller Dia x Pitch 166cm, tip 157cm x 98cm (62 x 38.6 ) 157cm x 102cm (62 x 40.2 ) 60 x 13.5º 3 from tip Noise Type Cert No. 182M Issue 4 182M Issue 4 182M Issue 4 182M Issue 4 MAAN approving Designation Engine Type Reduction Gear Exhaust System Savannah VG Jabiru(5) Savannah XLS Jabiru(1) Jabiru 2200 After serial 22A710 Direct Drive Jabiru Tractor exhaust, stainless steel Intake System Propeller Type Bing type 64/32 carb + single K&N Filter. Engine oil carb-body heater fitted. Hercules 2 blade, 61 x 41 Dwg S Hercules 2 blade, 61 x 42 Dwg S Propeller Dia x Pitch 61 x x 42 Noise Type Cert No. 182M 182M MAAN approving HADS HM10 issue 15 Page 3 of 16

4 (7) MANDATORY LIMITATIONS BRITISH MICROLIGHT AIRCRAFT ASSOCIATION (A) Max Take-Off Weight 450 kg (B) CG Limits See Annex C (C) CG datum See Annex C (D) Cockpit Loadings Port Starboard Total Min 55 kg - 55 kg Max 120 kg 120 kg 240 kg 5 (E) Never Exceed Speed Classic : 110 kts CAS (V DF 122 kts CAS) VG & XLS : 113 kts CAS (V DF 125 kts CAS) (F) Other limiting speeds V A: 60 kts CAS V F: 56 kts CAS (G) Permitted Manoeuvres Bank Limits 60 Non Aerobatic Normal acceleration limits, +4 / -2g (H) Fuel Contents (Max Useable) 77 litres 5 Cockpit limit subject to overall aircraft weight and balance limits. HADS HM10 issue 15 Page 4 of 16

5 (I) Power Plant Engine Jabiru 2200 Suzuki LS1000 Max RPM 3, ,000 (5 mins) (5,000 continuous) Max CHT 175 C (150 C continuous) n/a Max EGT n/a n/a Fuel Spec 83 MON or 90 RON minimum unleaded to BS(EN)228 or AVGAS 100LL. 83 MON or 90 RON minimum unleaded to BS(EN)228 or AVGAS 100LL. Engine Oil Spec As required by engine manual SAE 10W/40 API SH Gearbox oil spec n/a SAE 80W/90 API GL4 Fuel/Oil Mix 4-stroke, no oil to be used 4-stroke, no oil to be used Max. Coolant Temperature n/a 100 C Max. Oil Pressure 525kPa / 76psi / 5.25 bar 7 bar Min. Oil Pressure 220 kpa / 31psi normal use. 80 kpa / idle 0.5 bar Max. Oil Temperature 118 C cont. 120 C (8) INSTRUMENTS REQUIRED ASI Altimeter RPM EGT Compass Slip ball Required to V NE + 5% CAS (calibrated) on scale, and V NE + 10% CAS before stop Required to 10,000 ft Required to 10% above max revs for engine fitted. Coolant temp CHT Oil Temp. Oil. Press. Optional Required Required Fuel pressure At least one required Required Required Optional VSI 6 This RPM limit is specific to the Savannah and is less than given in the engine manual HADS HM10 issue 15 Page 5 of 16

6 (9) CONTROL DEFLECTIONS BRITISH MICROLIGHT AIRCRAFT ASSOCIATION Elevator UP (stick back): Note Trim tab UP: Elevator DOWN (stick forward): Note Trim tab DOWN: Note 1 Ailerons (0 flap) UP: 15 2 Flaperons (MID FLAP, central stick): Note Ailerons (0 flap) DOWN: 15 2 Flaperons (FULL FLAP, central stick): Note Rudder LEFT: 25 2 Rudder RIGHT: 25 2 Notes: 1. These must be checked using BMAA SB Savannah Pitch Control and Trim Systems Configuration. 2. If optional mod 1 ( Mk 2 flap lever) is fitted, these values become: mid flap: 16 ±3 ; full flap: 32 ±5. Note 1 (10) PILOT S NOTES, MAINTENANCE MANUALS, PLACARDS (10.1) Manuals approved for use with this aircraft (a) MXP740 Savannah UK Operators Manual Issue 1 AL 1 (AL0 is acceptable for aircraft without optional modification No.4 fitted), or Savannah VG Operators Manual Issue 1, dated August 2007, or Savannah XLS Operators Manual Issue 1, dated July 2016 as applicable. (b) Manufacturer s engine manual (contained at Annex B of the operators manual for a particular aircraft) (c) Other manuals as listed at Annex F of the operators manual for a particular aircraft. (d) Construction to: Savannah Savannah VG Savannah XLS ICP Savannah Construction Manual SUp Savannah Construction Manual Part 2, Issue 2 (March 2006) SUp Savannah UK Build Manual Issue 3 (March 2006) ICP Savannah VG Construction Manual SUp Savannah VG Construction Manual Part 2, Issue 1 (October 2007) SUp Savannah VG UK Build Manual, Issue 1 (October 2007) ICP Savannah S Construction Manual SUp Savannah XLS Construction Manual Part 2, Issue 1 (March 2015) SUp Savannah XLS UK Build Manual, Issue 1 (March 2015) (e) Maintenance may be to Microlight Maintenance Schedule MMS-1 as amended by the Savannah/Savannah VG UK Operators Manual. (10.2) The following placards are to be fitted: (a) Flight Limitations Placard (to be visible to pilot) See Annex D. (b) Engine Limitations Placard (to be located near to engine instruments) See Annex D. (c) Fuel Limitations Placard (to be located near to filler cap) A placard is to be fitted showing fuel capacity (77 litres), fuel type(s), fuel:oil ratio (if relevant) and if MTOW can be exceeded with full fuel and maximum cockpit weight, the fuel loads at MTOW for cockpit weights at 10kg intervals down to the maximum fuel load. An example is shown at Annex D. HADS HM10 issue 15 Page 6 of 16

7 (d) ASI Placard A correction placard from 30 to V NE at no more than 10 kts intervals, and at Vso, Va, V F and best glide speed, must show the corrections from IAS to CAS. For values, see the approval MAAN for the particular aircraft. An example is shown at Annex D. In addition the ASI dial must be marked as follows (following calibration): - Yellow triangle at 40 kts CAS, (recommended approach speed). - White sector from 31 kts CAS to 56 kts CAS, (flap limits). - Amber sector from 60 kts CAS to V NE - Red radial line at V NE Note: It is recommended that airspeed placards are not fitted to new aircraft until after flight testing, due to the requirement for pitot-static system calibrations. (e) Pitch Trimmer Instructions See Annex D. (f) Switches See Annex D. (g) Stick position There is to be a line marked Take-off trim on the cabin floor at the correct stick position on the ground with take-off trim set. This is to be 60 mm forward of the front edge of the lateral bracket below the front of the seats. (Bungee trim system only) (h) Maximum continuous RPM If the increased maximum ZFW of 267kg for the Jabiru 2200 is used, a maximum continuous power of 2800 rpm must be placarded adjacent to the tachometer. (11) MANDATORY MODIFICATIONS / SERVICE BULLETINS / AIRWORTHINESS DIRECTIVES ETC See Annex A for required modifications. MPD Rear cross member modification. MPD Inspection and modification of anti-balance tab operating mechanism. BMAA SB (Mandatory) Inspection of the attachment plates of the front wing lift struts to the main wing spar (both sides). BMAA SB 2624 (Essential) - Savannah Pitch Control and Trim Systems Configuration (12) MINIMUM PERFORMANCE AT MAX TAKE-OFF WEIGHT Rate of Climb: See Annex F. Stall or Minimum Flying Speed: Full Flaps: 28 kts CAS (29 kts CAS, VG/XLS variant) Clean: 30 kts CAS (31 kts CAS, VG/XLS variant) at Aft CG, see Annex D Part (d) BMAA Approval: B J Syson Chief Technical Officer 12 February 2018 HADS HM10 issue 15 Page 7 of 16

8 ISSUE HISTORY HM10 Issue A HM10 Issue B HM10 Issue C Initial draft to permit prototype construction. Second draft, for flight testing. Final draft, for team checking prior to approval HM10 Issue 1 First approval of type; configuration Jabiru(1). Authorised by MAAN 1591 Issue 1. Signatory G B Gratton HM10 Issue 2 Corrections from Issue 1. Authorised by MAAN 1591 Issue 2. Signatory G B Gratton HM10 Issue 3 HM10 Issue 4 HM10 Issue 5 HM10 Issue 6 HM10 Issue 7 HM10 Issue 8 Approval of Jabiru(4) configuration, authorised by MAAN 1750 Issue 1. Addition of optional Mk.2 flap lever. Correction to powerplant configuration Jabiru(4). Clarification of aileron deflections, ignition switch approval, carb heater description, fuel capacity, addition of special inspection point 1. Change to max permitted empty weight for Jabiru variants to 263kg (details in post-approval file 2004). Increase in maximum cockpit loadings, addition of optional modifications 2-7 and mandatory modification 15 (authorised by MAAN 1945). Signatory J A F Viner. Addition of optional modification 8 (authorised by MAAN 1945 Issue 2). Addition of configuration Jabiru(5), authorised by MAAN 1975 Issue 1. Signatory J A F Viner Addition of configuration LS(1), authorised by MAAN Addition of Suzuki LS1000 engine data. Revised flap settings to reflect positions achieved using optional modification 1. Addition of MPD Rear cross member modification, (BMAA SB 2013/1). Signatory J A F Viner Addition of items in Annex E. Addition of mandatory modification 16. Addition of VG variant and associated data, including optional mods 9 & 10, authorised by MAAN Signatory J A F Viner HM10 Issue 9 Update of V NE for VG variant, authorised by MAAN 2061 Issue 2. Signatory J A F Viner HM10 Issue 10 Amendment of Annex E item 5. Addition of Savannah VG Jabiru(2) and VG Jabiru(3). Correction to elevator and tab deflections in Section 9. Corrections and improvements to wording and formatting. Addition of MPD Inspection and modification of anti-balance tab operating mechanism. Signatory B J Syson HM10 Issue 11 Addition of configuration Savannah VG Jabiru(3) approved by MAAN Addition of configuration Savannah VG Jabiru(4) approved by MAAN Addition of MPD Inspection for corrosion of the attachment plates of the front wing lift struts to the main wing spar (both sides). Additions to Section 11 and Annex E of this document. Signatory B J Syson HM10 Issue 12 Minor formatting changes. Addition of VG ASI calibration table. Correction of VG collector tank moment arm. Signatory B J Syson HADS HM10 issue 15 Page 8 of 16

9 HM10 Issue 13 HM10 Issue 14 Addition of VG Jabiru(5) configuration, and associated performance figures, approved by MAAN Signatory B J Syson Addition of XLS variant and XLS Jabiru(1) configuration, and associated performance figures. Max ZFW of 267kg for Jabiru 2200 subject to reduction in max continuous RPM. Approved by MAAN Correction to propeller diameter and pitch for VG Jabiru(5). Signatory B J Syson HM10 Issue 15 BMAA SB Savannah Pitch Control and Trim Systems Configuration. Section 9, Control Deflections, adjusted accordingly. Signatory B J Syson, 12 February 2018 HADS HM10 issue 15 Page 9 of 16

10 Illustration of Aircraft - 3 View - Savannah Classic Illustration of Aircraft Photograph - Savannah Classic HADS HM10 issue 15 Page 10 of 16

11 ANNEX A MANDATORY MODIFICATIONS No. Brief Description of Modification 1. Introduction of lateral brackets to stiffen flap lever 2. Fitment of fuel-tap securing-bracket below floor 3. Addition of washers to flaperon linkages behind door and nylon washers fitted either side of flaperon horn 4. Either: (a) Soundproofing blanket fitted with Velcro to rear of baggage compartment, or (b) Solid rear cockpit wall (standard on later models) 5. Baggage retaining net at front of baggage compartment 6. Eliminate demist vent control on top of cowling 7. Fitment of guard strip around edge of coaming 8. Choke control to be coloured distinct from cabin heat control 9. <deleted> 10. Elevator full width anti-balance tab 11. Introduction of elevator bias spring mechanism within tail (not required if optional mod 4 fitted) 12. Introduction of bungee pitch trimmer in cockpit (not required if optional mod 4 fitted) 13. Deletion of original electric pitch trimmer (optional mod 4 is different from the original electric trimmer) 14. Marking graduations in litres alongside fuel sight tube. Means must be available to confirm correct reading in air and on ground (e.g. two sets of markings needed, clearly separated, respectively for the ground and flight attitudes, or flight attitude spirit level for use on ground) 15. Addition of master 15A circuit breaker/fuse immediately after battery 16. Rear cross-member modification MPD (BMAA SB 2013) 17. MPD (BMAA SB 2283) - Inspection and modification of anti-balance tab operating mechanism. This only applies to aircraft fitted with the bungee pitch trim. HADS HM10 issue 15 Page 11 of 16

12 ANNEX B APPROVED OPTIONAL MODIFICATIONS No. Brief Description of Modification 1. Mk.2 (shorter) flap lever mechanism (mandatory modifications 1 & 3 not required when fitted) 2. Two additional fuselage ribs to Canadian sport-plane standard. (Should be incorporated in kits from serial ) 3. Doubling (two plates) of lift-strut attachment plates to Canadian sport-plane standard. (Should be incorporated in kits from serial ) 4. Electric pitch trimmer, as supplied by SUP, using an electric actuator within the horizontal stabiliser, eliminating bungee and spring mechanisms in cockpit and fin respectively (mandatory modifications 11 & 12 not required when fitted) 5. Brass bushing on elevator and rudder control surfaces 6. Addition of tie-down points at lift-strut/wing interface 7. Installation of wing inspection panel at lift-strut/wing interface 8. Increased thickness wing attachment brackets (3mm to 5mm) as part of Canadian sport-plane standard. (Should be incorporated in kits from serial ) 9. Jury struts (if fitted, optional modifications 3 and 8 must also be fitted) 10. Intra-rib stringers HADS HM10 issue 15 Page 12 of 16

13 ANNEX C WEIGHING INFORMATION Savannah Savannah VG/XLS CG Datum Slat leading edge Wing leading edge Weighing attitude All 3 wheels on a level surface Mainwheel moment arm 0.755m aft of datum 0.655m aft of datum Nosewheel moment arm 0.710m fwd of datum (-0.710m) 0.810m fwd of datum (-0.810m) Fuel tank Collector tank Crew 0.595m aft of datum (77 litres maximum capacity) (treat as part of main fuel tank as above) 0.650m aft of datum (120kg max load per seat, min load 55kg on pilot s seat) 0.495m aft of datum (70 litres maximum capacity) 0.87m aft of datum (7 litres maximum capacity) 0.550m aft of datum (120kg max load per seat, min load 55kg on pilot s seat) Baggage 1.42m aft of datum, max capacity 20kg 1.32m aft of datum, max capacity 20kg Aft CG limit 0.550m aft of datum 0.445m aft of datum Fwd CG limit 0.429m aft of datum 0.331m aft of datum The aircraft must be shown to remain within CG limits for all permitted loadings up to and including the maximum baggage load. The capacity of the baggage compartment may be reduced to meet this requirement, to any value below the maximum of 20kg. The individual seat limits may be reduced, not below 86kg, if required to stay within CG limits. HADS HM10 issue 15 Page 13 of 16

14 (a) Flight Limitations Placard (to be visible to pilot) Bank angle limits: Normal Acceleration Limits: Empty Weight: Max Take-Off Weight: Minimum Cockpit Weight: Maximum Cockpit Weight: ANNEX D EXAMPLE PLACARDS Savannah [VG/XLS] [Engine] [Registration] +/ / -2g kg ** 450 kg 55 kg 120 kg in each seat Aerobatics and deliberate spinning prohibited. ** This must match the most recent W&CG report for the aircraft. (b) Engine Limitations Placard (to be located near to engine instruments) All engine limitations must be shown as coloured markers (red for danger, amber for caution) on the instrument displays. (c) Fuel Limitations Placard (to be located near to filler cap) (d) ASI Placard kt CAS (calibrated) kt/mph* IAS (indicated) 28 VS0 FUEL Capacity 77 Litres Cockpit Weight (kg) Max. Fuel Load (litres) (including baggage) or below 77 litres (full) 83 MON or 90 RON minimum unleaded to BS(EN)228 or AVGAS 100LL 30 VS1 40 App Savannah Classic Glide Climb VF 60 VA Stall speeds given are at aft CG, they may appear to increase by up to 7kts CAS with forward CG kt CAS (calibrated) kt/mph* IAS (indicated) 29 VS0 31 VS1 40 App Savannah VG/XLS Glide VF VA & Climb VNE Stall speeds given are at aft CG, they may appear to increase by up to 7kts CAS with forward CG *delete as applicable. VNE HADS HM10 issue 15 Page 14 of 16

15 (e) Pitch Trimmer Instructions BRITISH MICROLIGHT AIRCRAFT ASSOCIATION PITCH TRIM nose down nose up (f) Switches (g) Flaps Also a line must be marked Take-off below the stick, 60mm forward of the seat front edge bulkhead (bungee trimmer), or one line below middle (electric trimmer). All switches are to be marked with function and sense (up=on, down=off). Note that the originally supplied, guarded ignition switches are down=on on early aircraft; this is acceptable due to the mode of operation but only applies to the original-specification ignition switches. Where possible the switches should be orientated up=on. Electric trim switches should be orientated nose up = lower part of switch to be pressed. The three flap lever positions are to be marked 0, 18 and 36, or 0, 16 and 32 if the Mk 2 flap lever is fitted. (h) Baggage compartment To be placarded with it s limit, which may not exceed 20kg. (See Annex C above for explanation) ANNEX E POINTS FOR SPECIAL ATTENTION In service, the following points have been found to be commonly recurring problems, and Inspectors must give special attention to the following both during initial approval, and during later inspections. 1. Special check at annual / 150hr inspection for any wear in control cables where they cross. 2. MPD must be complied with (BMAA SB 2013/1): modification of rear cross member. 3. Note that earlier examples may be placarded to a maximum seat weight of 86kg. This may be increased to 120kg provided a new weight and balance report is prepared and all relevant placards are altered accordingly. 4. It has been noticed on a couple of examples that the weld on the aileron torque tube (connecting the control stick to the bell crank mounted on the rear cross member) can come into contact with the nylon bush, causing wear on the bush. This should be checked occasionally and if necessary a new torque tube and bush should be sourced from SUp. 5. Piano hinges on the doors and anti-balance tabs should be crimped at the ends (to retain the hinge pins) at the factory. If crimping is not present, contact the kit importer. 6. Check for any rubbing of skins against fairings. 7. Corrected elevator and anti-balance tab deflections to be observed. 8. MPD must be complied with (BMAA SB 2283/1): inspection and modification of pitch antibalance tab mechanism (bungee pitch trim). 9. MPD must be complied with (BMAA SB 1918/3): inspection for corrosion and abrasion of the attachment plates of the front wing lift struts to the main wing spar (both sides). HADS HM10 issue 15 Page 15 of 16

16 ANNEX F SCHEDULED PERFORMANCE FOR APPROVED CONFIGURATIONS Classic variant: Configurations TODR, metres (unfactored in italics) LDR, metres Climb Rate, fpm Glide Ratio Jabiru 198 (152) :1 Suzuki LS (262) :1 VG variant: Configurations TODR, metres (unfactored in italics) LDR, metres Climb Rate, fpm Glide Ratio VG Jabiru(1)-(4) 228 (175) :1 VG Jabiru(5) 340 (260) hard rwy 350 hard rwy 600 (ISA 2000 ) 10:1 XLS variant: Configurations TODR, metres (unfactored in italics) LDR, metres Climb Rate, fpm Glide Ratio XLS Jabiru(1) 340 (260) hard rwy 350 hard rwy 600 (ISA 2000 ) 10:1 Unless otherwise stated, all scheduled performance values are for ISA, sea-level, still-air conditions, with a short dry-grass runway surface. HADS HM10 issue 15 Page 16 of 16

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