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1 llhttilel Amlrira p epartmr nt fi '@.r anxqnr tatinn -![ eiler al lhialirm ltminixtr allnr. 6.yrlifirxtt t46-"/"* SR01654LA \,%la 4'dy'aar,* ta,yzet/to Airfilm Carnera Systems 6245 Aerodrome Way Hangar No. 2 Georgetown, Califorma cca,foc^t, f'/os t/i- dongzt in' //.e /y7ze&^try.nofr* /./.ef&,ru'lgzv,to/ctz/ ra"7,/ /lz Z,,.ni/n/rb.nt. zzl /lon"fr* tr-ll7tzoy'nifif1p,r7nn rneeat /,12 za?.aor/,/,rhz^td.re7z,/ternen/^). o/,4*n/ 27 y'fl,f""*t*,/,4*ro,na-,92nvo&s"ot"t. 0)17r>nrl%*r*r,ot,$7r' 7"nlf,:arz -4.6n'1"* H2SW,,r//6o1n,.. Bell '1t6o,* , A, B, 81, L,L1,L3,L4,407. Oeue7/hn "/.Q7r" %ag* Tllo,g2.' Installation of Airfilm Model Gl Nose Mounted Utility Bracket and/or G3 Landing Light on Bell Series rotorcraft in accordance with FAA Approved Airfilm Camera Systems Master Drawing List No. AF-G1-010, Revision N/C, dated April 14, 2004, andlor AF-G3-010, Revision, N/C, dated April 14,2004. Rotorcraft Flight Manual Gl dated September 8,2004, or later FAA Approved Revision. Instructions for Continued Airworthiness AF-G1-008, Revision NC, dated April 14, 2004, andlor Instructions for Continued Airworthiness AF-G3-008, Revision NC, dated Aprll 14, izt'/,r/'tbzat utr/7:o't"y'u;t'/onut.' This approval should not be extended to rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously applied modifications, including changes in tlpe de$ign, will introduce no adverse effect upon the airworthiness of that rotorcraft. If the holder agrees to permit another persofi to use this certificate to alter the product, the holder shall give the other person written evidence ofthat permission. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.,%/;t' rzz'/y'icz/cz.r///z JrzTqo:4hgz is,-,,o1t"/io,t. //r- /b^t.t.f,. -TyrnorroZ t/ta%t<,'ttrzrte ht, qfta7 tztt/zlaz.nrnbtcd,u*yecn,&-.{,eao,l"e,/az a /ez:2r,14.a,/tbn La./,e r,i a././/t:ruad;l el/n,14;1,/n//l f/i",y'6r*nltat/ra/rtr"//i",%1t*/,t6uaz,/.t'ott,,,/d*tonat/,rzz/obn. 9,2t" "fovq August 8, 2003 %a.le,oet taez March I, o,/.. 1",*ttr"n-... September 10,2004.4a/t,,ztnz,t*.r/ June 6, 2008.%/ 41L (Signafure) I & Administrative Support (Title) An1 atteratian of tfiis certfuate is punisfia\fe fu a fine of not e4cee[in g1,000, or imprisonment not e4:ee[ing t J*rt * 6"th FAA Form 811,0-2 (10-68) Page 1 of 2 Itfiis certf'rate ma1 6e transferre[in accorfance witfi FAK21.47

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3 A i r F i l m C a m e r a S y s t e m s REPORT INSTALLATION INSTRUCTIONS G1 UTILITY MOUNT AND OPTIONAL G2 COUNTERWEIGHT DATE ISSUED: 4/14/2004 Airfilm Camera Systems 6245 Aerodrome Way, Hangar No. 2 PO Box 1352 Georgetown, Ca LOG OF REVISIONS REVISION DATE PAGES EFFECTED COMMENTS N/C 4/14/2004 ALL Original submittal A 9/7/ and 6 Placards added, revised W & B B 2/17/2005 Title Page, 2-4 and 7 Revised Title Page. Added additional installation information, revised W & B added Appendix A C 10/20/2006 3, 13, AND 14 Added Blanking panel, Added CINEFLEX STYLE C 10/20/ , 16 Added FLIR STYLE & DT Install Drawing C 10/20/ THRU 7 Revised Counter Weight

4 INTRODUCTION AND DESCRIPTION: The Airfilm G1-1 utility bracket mount allows for the attachment of utility equipment such as cameras, lights, and sensor instruments to be hard mounted on the Bell Aircraft 206 A, B, & L and 407 Series helicopters. The G1-1 mount attaches to the exterior of the aircraft landing light housing area. The G1-1 bracket can carry a maximum load of 130 lbs. The mount can be installed and removed without any permanent aircraft modifications. The G1-1 mount prohibits the use of the standard aircraft landing and taxi light. If night operations are required the Airfilm G3-1 Landing light kit may also be installed. Depending on the mounted load and weight and balance requirements of each helicopter an optional G2-1 Counter Weight Assembly kit is available. This G2-1 Counterweight kit is attached to the aft cross tube and aft jacking pad. This kit does not interfere with the installation or operation of Microwave or Cargo Hook accessories. Page 1 of 17

5 G1-1 NOSE MOUNT BRACKET 1. Remove existing landing light cover, disconnect landing lights. Using the original cover as a template, align forward edge of original cover on G1-1 mount forward top edge. Equally space original cover longitudinally on G1-1 mount. Using original cover as template carefully mark existing 8 holes on to G1-1 mount. Be sure to check all 8 hole locations for sufficient edge distance. Insure G1-1 mount does not interfere with existing aircraft equipment. (See Figure 1) Fugure 1 Align forward top edge of original light cover and G1-1 mount Equally space original light cover and G1-1 mount longitudinally, mark original 8 holes. Page 2 of 17

6 2. Drill marked holes with no.30 drill, due to curvature of G1-1 mount; the use of drill guide block is recommended. Cleco original cover to mount, check for sufficient edge distance. Drill no.30 holes to final size, no.10 drill. Deburr holes. 3. The original landing light housing (Bell 407) or landing light plexi-glass window may be replaced with the G-7 Blanking Panel. This panel sandwiches between the aircraft and G-1 mount if required. 4. Install and secure the G1-1 Mount bracket to the aircraft using QTY 6, AN3-5A bolts on two most forward holes and QTY 2 AN3-11A on aft holes use MS Lock washers at all 8 places. (See Figure 2) Due to airframe variations any gap between blanking cover and G1-1 mount in excess of in at hole locations can be shimmed using one standard flat washer of corresponding thickness. If washer shims are used ensure supplied hardware will be sufficient in length to remain in safety. Torque the bolts Inch Lbs. Figure 2 Install AN3-5A bolts at 6 places. If required use washer shims between mount and light cover blanking plate at bolt hole locations Install AN3-11A bolts at fwd 2 places Page 3 of 17

7 5. Install camera / sensor to G1-1 mount. (SEE APPENDIX A FOR DETAILS AND CONFIGURATIONS). 6. Route any control wire into aircraft so as not to interfere with the operation of doors or the operation of any flight controls or systems. 7. Check entire G1-1 assembly for flight integrity. System should be secure and not have free play movement. 8. Revise weight and balance per the following table: The following table presents the location of the weight center of gravity of the mount and payload sensor/camera for adjustment of the aircraft weight and center of gravity with the mount installed. DESCRIPTION WEIGHT (lbs) STATION (in) G1-1 Bracket Assy PAYLOAD Use Actual Wt MAX 130 pounds. 9. Attach the following Placard in full view of pilot BL (in) Reduce the published V NE by 20 KIAS (23 MPH) 10. Make appropriate log book entry for installation. 11. Return to service. 12. Removing G1-1 system. Follow instructions in reverse order to remove. Remove entire G1-1 mount assembly and associated hardware. Reconnect landing light wiring if changed. Re-install original light cover with original hardware. Page 4 of 17

8 G2-1 COUNTER WEIGHT (NOT REQUIRED) The G2-1 Counter Weight Installation is optional if needed for maintaining the Center of Gravity limits of the helicopter. 1. Install the G2-1 counter weight assembly; Insure that the installation does not interfere with the operation other installed accessory kits. Page 5 of 17

9 2. Install the G2-2 Counterweight around the aft cross tube approximately 9 inches left of aircraft the centerline per the photograph below. Exact placement is not required at this step. Tighten fasteners only to remove slack but also allowing the kit to be adjusted. Page 6 of 17

10 3. Raise the G2-1 counterweight assy upward so that the aft fitting (G2-2) aligns with the aircraft aft jacking pad. Attach using QTY 1 AN5-27A bolt, QTY 2 AN Washers, QTY 2 G2-5 Cone Spacers. The cone spacers are installed against the jack pad to insure proper alignment and fit. Torque Inch Lbs. Page 7 of 17

11 5. After counterweight is fully attached to the aircraft, tighten all remaining bolts to final torque. Torque In Lbs. 6. Check entire G2-1 assembly for flight integrity. System should be secure and not have free play movement 7. Revise weight and balance: The following table presents the location of the weight center of gravity of the mount and payload sensor/camera for adjustment of the aircraft weight and center of gravity with the mount installed. HELICOPTER MODEL WEIGHT (lbs) STATION (in) BL (in) Bell 206 A & B Bell 206 L Bell 407 Model: Page 8 of 17

12 8. Make appropriate log book entry 9. Return to service 10. Removing G2-1 Assy: Follow instructions in reverse order and remove. Page 9 of 17

13 APPENDIX A If camera / sensor installations require additional power or system requirements beyond the placarded OEM auxiliary power outlet, additional certification(s) may be required. The weight and size limits for the Camera / Sensor is: Frontal area = 3.0 ft 2 /.278 square meter Weight = 130 Lbs pounds / 58.9 kilogram The following drawings provide details for the type of equipment installed on the mount. For Wescam MX-15 or equivalent attachment pattern use: Page 10 Drawing No. G1-1A For DT-1 (Dove Tail type installations or equivalent) use: Page 11 Drawing No. G1-1B For Wescam style male taper fittings use: Page 12 Drawing No. G1-1 For Cineflex HD Camera installation use: Page 13 Drawing G1-1C For Cineflex HD style camera installation with V Vibration Isolator (FAA/PMA) use: Page 14 Drawing -G1-1C For Flir Ultra Media Series / Flir Systems style installations use Page 15 Drawing -G1-1B FLIR USE ACTUAL WEIGHTS OF SYSTEM(S) INSTALLED Page 10 of 17

14 Page 11 of 17

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21 AirFilm Camera System 6245 Aerodrome Way /P.O. Box 1352 Georgetown, CA Supplement No. G FAA/EASA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO THE BELL 206 A, B, B1, L, L1, L3, L4 & 407 ROTORCRAFT FLIGHT MANUAL WHEN EQUIPPED WITH THE G-1 NOSE CAMERA MOUNT AND COUNTER WEIGHT ASSEMBLY REGISTRATION #: SERIAL #: The information in this supplement is FAA/EASA approved and must be attached to the appropriate FAA Approved Bell Model 206 A, B, B1, L1, L3, L4, and 407 Rotorcraft Flight Manual when the Airfilm Model G1 Nose Camera Mount is installed in accordance with: STC No. SR LA EASA.IM.R.S The information contained in this document supplements or supersedes the basic manual only in those areas listed herein. For limitations, emergency procedures, normal procedures, and performance information not contained in this supplement, consult the basic FAA Approved Rotorcraft Flight Manual. FAA APPROVED: Manager, Flight Test Branch, ANM-160L Federal Aviation Administration Los Angeles Aircraft Certification Office Transport Airplane Directorate FAA DATE: Originally Approval Date: 8 September 2004

22 AirFilm Camera System Rotorcraft Supplement to 6245 Aerodrome Way, Hanger #2/P.O. Box 1352 Bell 206 A, B, B1, L, L1, L3, L4, & 407 Georgetown, CA Flight Manuals when modified with the Camera Mount STC Number SR LA Supplement No. G EASA IM.R.S LOG OF PAGES Rev No. Pg No Date Description of Change FAA Approved N/C All 8 Sept 2004 Initial Issue Mgr, Flight Test Branch ANM-160L, FAA, Los Angeles ACO, Transport Airplane Directorate Date: Page i

23 AirFilm Camera System Rotorcraft Supplement to 6245 Aerodrome Way, Hanger #2/P.O. Box 1352 Bell 206 A, B, B1, L, L1, L3, L4, & 407 Georgetown, CA Flight Manuals when modified with the Camera Mount STC Number SR LA Supplement No. G EASA IM.R.S LOG OF PAGES Rev Pg Date Description FAA Approval A Added EASA July Number to cvr 2006 & all pages. 2,3 4 5 Added typical to pictures Added pilot limitation & reformated section. Cleaned up Airseed wording Deleted technician wording for removal and installation of camera/sensor Added weight & balance section Manager, Flight Test Branch ANM160L FAA, LA ACO Transport Airplane Directorate Date: Page i

24 AirFilm Camera System Rotorcraft Supplement to 6245 Aerodrome Way, Hanger #2/P.O. Box 1352 Bell 206 A, B, B1, L, L1, L3, L4, & 407 Georgetown, CA Flight Manuals when modified with the Camera Mount STC Number SR LA Supplement No. G EASA IM.R.S INTENTIONALLY LEFT BLANK Page iii

25 AirFilm Camera System Rotorcraft Supplement to 6245 Aerodrome Way, Hanger #2/P.O. Box 1352 Bell 206 A, B, B1, L, L1, L3, L4, & 407 Georgetown, CA Flight Manuals when modified with the Camera Mount STC Number SR LA Supplement No. G EASA IM.R.S TABLE OF CONTENTS Section Page GENERAL...2 SECTION 1 LIMITATIONS...3 OPERATIONS... 3 WEIGHT & SIZE... 4 AIRSPEED... 4 PLACARDS... 4 LANDING LIGHT... 4 SECTION 2 NORMAL PROCEDURES...5 SECTION 2 EMERGENCY PROCEDURES...5 SECTION 3 PERFORMANCE...5 SECTION 4 WEIGHT & BALANCE...5 TABLE OF FIGURES Figure Page FIGURE 1 SIDE VIEW WITH CAMERA AND COUNTER WEIGHT 2 FIGURE 2 FRONT VIEW WITH CAMERA 3 FAA Approved Date: 13 July 2006 Page 1 of 5

26 AirFilm Camera System Rotorcraft Supplement to 6245 Aerodrome Way, Hanger #2/P.O. Box 1352 Bell 206 A, B, B1, L, L1, L3, L4, & 407 Georgetown, CA Flight Manuals when modified with the Camera Mount STC Number SR LA Supplement No. G EASA IM.R.S GENERAL The Airfilm G1 Nose Camera Mount System consists of an aluminum alloy bracket that attaches externally to the nose of the aircraft in the landing light area. A counter weight is attached to the aft landing gear cross tubes and aft jacking hard point located on the bottom of the fuselage. The counter weight is utilized to maintain the center of gravity within the rotorcraft limits. Figure 1 Side View with Camera and Counter Weight (typical) FAA Approved Date: 13 July 2006 Page 2 of 5

27 AirFilm Camera System Rotorcraft Supplement to 6245 Aerodrome Way, Hanger #2/P.O. Box 1352 Bell 206 A, B, B1, L, L1, L3, L4, & 407 Georgetown, CA Flight Manuals when modified with the Camera Mount STC Number SR LA Supplement No. G EASA IM.R.S Figure 2 Front View with Camera (typical) SECTION 1 LIMITATIONS Operations The pilot is prohibited from operating the camera or sensor system FAA Approved Date: 13 July 2006 Page 3 of 5

28 AirFilm Camera System Rotorcraft Supplement to 6245 Aerodrome Way, Hanger #2/P.O. Box 1352 Bell 206 A, B, B1, L, L1, L3, L4, & 407 Georgetown, CA Flight Manuals when modified with the Camera Mount STC Number SR LA Supplement No. G EASA IM.R.S Weight & Size The camera package is limited to a maximum allowable frontal area of 3.06 sq. ft. and a weight of 130 lbs at any mounting location. Airspeed Reduce published V NE by 20 KIAS (23 MPH) with camera/sensor system installed. No airspeed reduction with the Post Mount only installed. Placards Reduce the published V NE by 20 KIAS (23 MPH) with Camera/Sensor Installed Landing Light If the mounted camera obscure the landing light beam or produces reflection in the cockpit and alternate landing light sources are not installed the landing light will be considered inoperative. NOTE Check operational rules for landing light requirements. FAA Approved Date: 13 July 2006 Page 4 of 5

29 AirFilm Camera System Rotorcraft Supplement to 6245 Aerodrome Way, Hanger #2/P.O. Box 1352 Bell 206 A, B, B1, L, L1, L3, L4, & 407 Georgetown, CA Flight Manuals when modified with the Camera Mount STC Number SR LA Supplement No. G EASA IM.R.S SECTION 2 NORMAL PROCEDURES Prior to the first flight each day the pilot shall visually inspect the following: All attachment points and hardware for security. Support structure for signs of stress, distortion, fatigue cracks or damage. SECTION 2 EMERGENCY PROCEDURES No change SECTION 3 PERFORMANCE Hover performance - no change Climb performance 75 ft/min reduction SECTION 4 The Nose Mount payload CG is: 2.0 Longitudinal 0.0 Lateral WEIGHT & BALANCE The maximum weight of an external load on the Nose Mount is 130 pounds FAA Approved Date: 13 July 2006 Page 5 of 5