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1 -llnitrr\ Sintes U)f Anr..riru pepartnrctrt -!f elerai Aftiation $,iminixtration F 6.pr tifiratl.,1 )or/". SROl058LA.71;'/ o*y'.ot' /t.;try'it 6245 Aerodrome Way Hangar 2 Georgetow n, Califom ia n /t/ru l/rz f/t"./orv" ), /./tr /77tul;,7r0/'r'//)///rltrr77,rr,r1ur/ z,r//t 1.//r l)tu/n/z},ztt tzztr/nrzrltzt.za) //rz j/t, o; ;V".ty'"r/,y'rtrr,z.//tzl) 1./rz nuzlrv/l)tr)) t'rt/rtt'rztrrnl,y'.lltt / 27*,y'2/u.7"r/.r'rr/..y't,ro1rtr,.2,7uh/'i,,;. *Certification basis is set forth in Type Certillcate Data Sheets II9EU and Hl leu / n/i, o/'lnzl/. Q.zt'1 )r./f)2,/r,. /.r),,,/,,. HSEU an{ FI 1 1 EU. 1.2,.1,. Eurocoltter / Aerospatiale./h,t/. AS350c, AS350D, AS350Dl, AS350B, AS350Bt. AS35082, AS350BA, AS350B3 and AS355E, AS355F. AS355lr1, A5355F2, AS355N y',,;rr'r7r7,r, r'/-77vr'(1rr;r7r, /,/*rr7" Installation of a camera nrount system, in accordance with FAA Approved Airfilm Camcra Systems Master Drawing List,Ali , Revision "A" dated June atrd for the AF200-l Mount. hrstallalion Document AF Revision ).1/C, Cated June 1, 2000 or later FAA Approved Revrsions ; for thc: AF200-2 Mount, Airfilm Carnera Systems lnstallation Documenl AF Revision N/C dated May 10, 2004 or later FAA Approved Revisions 'lt)t/tt1t,n; 'fhe,r,rf/r'r,l/rr,rr; installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any advers effect upon the arrrvorthiness of the aircraft. The approval of this rnodillcatron applies to thc above noted aircraft model series only. A copy of this STC must be included in the permanent recorcls of the modihed aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission..v/l,"r/.t/irrlr,rz.r///rrlt1,7rrv/tzt7,/o/o,'/&./,. r:i /lt /w;ly',t.r7vrrrrrr./t/ir/rrrrrztth zr,. r//t /rz/z/ )ttt't'z'ztr/rt'rr/ ;tt;ttztrhr/,,t'r,r,./, tr/r,r z //,/,///.//t///11,/t r/t/r u t,//rrrrt,ur.;1n/,1),/.ry'/l //tr..,i/trlt ritu/zz1t,t' ry'ht. 7r' l r'r, /.' /, t v tt 1. t 2,rr../', r/, a' n t; /2, tt /t t,zt (1,,1t' y',v71:,2/tr,, Selltember 79, 1999 llzz'r' nziittzy'.!/n1" t/,lluo',.n AUgUSt 4, 2000 (/rr1r rrrrr.t,.r/rr/. MafCh 10, 2003, September 9,2004. fr7.1a z r /) tz "/ t/n. l r1*, )tz; /trzltz IVtanager, Airframe Branch I=._q.q"AJrgsl_-e""s_Auqra-ft "C_q(if, satlq1no_ffi q_e* itir lo\ fln1 atteratun of tfiis ccrttficatt it p"rr"tiart a1 " Jrr,,rJ,*,,1r,,qitloc," np*"n**t ""t tx. ntr, :A.A F'orn I t 10 2 :10 58 ) ')[ns certifi:ate na1 6c trawferrcr[ h accoraarrci "rtf"tzq2 L +;

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4 6245 Aerodrome Way, Hangar #2 Georgetown, CA Supplement No. AF200-1 FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO THE EUROCOPTER AS 350 & AS 355 SERIES ROTORCRAFT FLIGHT MANUAL WHEN EQUIPPED WITH THE AF200 CAMERA MOUNT AND COUNTER WEIGHT ASSEMBLY REGISTRATION #: SERIAL #: The information in this supplement is FAA approved and must be attached to the appropriate FAA Approved Eurocopter Model AS 350 & AS 355 Series Rotorcraft Flight Manual when the Airfilm Model AF200 Camera Mount is installed in accordance with: STC No. SR 1058 LA 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 REISSUE DATE: Original Issue: 4 August 2000 Revised: 20 August 2000

5 Rotorcraft Supplement to 6245 Aerodrome Way, Hanger#2 Eurocopter AS 350 & AS 355 Series Flight Manuals Georgetown, CA when modified with the Camera Mount Supplement No. AF200-1 STC Number SR 1058 LA LOG OF PAGES Rev No. Pg No Date Description of Change FAA Approved Rei ssu e All 8 Sept 2004 Changed address in header. 2 2,3 Defined 2 mounts New Pictures Mgr, Flight Test Branch ANM-160L, FAA, Los Angeles ACO, Transport Airplane Directorate 3 Defined night operations with light obstruction Date: 4 Limitations and Placards Page i

6 Rotorcraft Supplement to 6245 Aerodrome Way, Hanger#2 Eurocopter AS 350 & AS 355 Series Flight Manuals Georgetown, CA when modified with the Camera Mount Supplement No. AF200-1 STC Number SR 1058 LA TABLE OF CONTENTS SECTION PAGE SECTION I GENERAL 2 SECTION 2 LIMITATIONS 3 SECTION 3 EMERGENCY PROCEDURES 4 SECTION 4 NORMAL PROCEDURES 4 SECTION 5 PERFORMANCE 5 TABLE OF FIGURES FIGURE PAGE FIGURE 1 FRONT VIEW WITH CAMERA RIGHT SIDE 2 FIGURE 2 SIDE VIEW WITH CAMERA FRONT 3 FAA Approved Date: 8 September 2004 Page 1 of 5

7 Rotorcraft Supplement to 6245 Aerodrome Way, Hanger#2 Eurocopter AS 350 & AS 355 Series Flight Manuals Georgetown, CA when modified with the Camera Mount Supplement No. AF200-1 STC Number SR 1058 LA SECTION I GENERAL The Airfilm AF200 Camera Mount System consists of a frame structure that attaches externally to the aircraft. This frame structure will accommodate either a nose mounted or a left or right side mounted camera installation. A Counter Weight box containing weights which is attached to the landing gear aft cross tubes and hard point attachments located on the shoulder of the fuselage and is located under the tail boom for a nose mount or on the side opposite the camera. There are two mounts, a -1 or -2, both with the same fit & function. The counter weight is utilized to maintain the center of gravity within the rotorcraft limits. A pitot tube extension hose is attached from the basic pitot tube to the pitot extension located on top of the camera sphere. Figure 1 Front View with Camera Right Side FAA Approved Date: 8 September 2004 Page 2 of 5

8 Rotorcraft Supplement to 6245 Aerodrome Way, Hanger#2 Eurocopter AS 350 & AS 355 Series Flight Manuals Georgetown, CA when modified with the Camera Mount Supplement No. AF200-1 STC Number SR 1058 LA Figure 2 Side View with Camera Front SECTION 2 LIMITATIONS 1. If a video monitor is installed it must be turned off at night or shaded from the pilot s view. 2. The camera package is limited to a maximum allowable frontal area of 9.62 sq. ft. and a weight of 275 lbs at any mounting location. The counter weight must be installed and ballast added to maintain the CG within limits. 3. Reduce published V NE by 40 KIAS for aircraft with a 155 KIAS V NE and by 35 KIAS for aircraft with a 150 KIAS V NE with camera and counter weight installed. 4. Stow or secure control console prior to takeoff and landing. FAA Approved Date: 8 September 2004 Page 3 of 5

9 Rotorcraft Supplement to 6245 Aerodrome Way, Hanger#2 Eurocopter AS 350 & AS 355 Series Flight Manuals Georgetown, CA when modified with the Camera Mount Supplement No. AF200-1 STC Number SR 1058 LA 5. If the camera mounted on the nose obscures the landing light 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. 6. Pitot Heat must remain OFF or the circuit breaker pulled to prevent damage to the pitot tube with Auxilary Pitot Tube installed. PLACARDS LIMITATIONS Reduce the published V NE by 40 KIAS for aircraft with a 155 KIAS V NE Reduce the published V NE by 35 KIAS for aircraft with a 150 KIAS V NE with a camera and counter weight installed The pitot heat must remain OFF and/or the circuit breaker pulled with the auxilary pitot tube installed SECTION 3 EMERGENCY PROCEDURES No change SECTION 4 NORMAL PROCEDURES 1. External Inspection. Prior to the first flight each day the pilot shall visually inspect the following: FAA Approved Date: 8 September 2004 Page 4 of 5

10 Rotorcraft Supplement to 6245 Aerodrome Way, Hanger#2 Eurocopter AS 350 & AS 355 Series Flight Manuals Georgetown, CA when modified with the Camera Mount Supplement No. AF200-1 STC Number SR 1058 LA (a) Pitot tube extension on nose mount configuration. (b) All attachment points and hardware for security. (c) Support structure for signs of stress, distortion, fatigue cracks or damage. 2. The mount and camera may be installed or removed by trained technician, or mechanic, and must be recorded in accordance with FAR SECTION 5 PERFORMANCE When using climb performance charts a performance penalty of 100 feet per minute must be used. FAA Approved Date: 8 September 2004 Page 5 of 5

11 This document was created with Win2PDF available at The unregistered version of Win2PDF is for evaluation or non-commercial use only.

12 INSTALLATION INSTRUCTIONS AF AirFilm Camera Systems INSTALLATION DOCUMENT REPORT NO. AF DATE ISSUED: 4/14/2004 LOG OF REVISIONS REVISION REVISION DATE PAGES EFFECTED COMMENTS N/C 5/10/2004 ALL ORIGINAL SUBMITTAL A 8/10/ REV WEIGHT AND BALANCE A 8/10/ PLACARDS REVISED B 10/1/ ADDED APPENDIX C INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 1 of 20

13 INSTALLATION INSTRUCTIONS AF Introduction and General Description: The system is used and Installed on Eurocopter AS350 & AS355 Helicopters, It can be installed on High or Low Gear aircraft. The mount system can be installed in the following configurations: Nose Mount Only Side Mount Only Counter Weight Only Or any combination of above Calculate weight and balance for Installed items and check for proper loading of aircraft. A modification to the forward belly panel is required. Antenna, lights, and additional installed equipment may need to be relocated to provide clearance for the camera mount system. The AF200-2 mount system consists of a center mounted support bar that attached to the forward lower aircraft hard points. This center cross tube bar allows the nose mount section to be attached. A counter weight section is used when using the nose mount. The mount will accept various spherical camera systems with a 40 diameter ball and weighing 275#. A counter weight box is provided to accept a maximum of 150# The AF200-2 PN A996 consists of these main assemblies. AF200-2 NOSE MOUNT ASSEMBLY P/N A900 AF200-2 COUNTER BALANCE ASSEMBLY P/N A964 AF200-2 SIDE MOUNT P/N A969 INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 2 of 20

14 INSTALLATION INSTRUCTIONS AF AF200-2 NOSE MOUNT INSTALLATION INSTRUCTIONS: NOSE MOUNT SUPPORT 1) Confirm that the mount will not interfere with any exterior kits, antennas, and other exterior mounted assemblies. 2) Remove the forward belly panel Use caution for any antennas located on the panel. Disconnect any cabling before removing the panel. 3) Attach the HAMMER WEIGHT -T BRACKETS (A952) to the hammer weight existing bolts Place the brackets up to the underside of the hammer weight attachment nuts. SEE FIG 1 FIG NO 1 3A) Using a 6mm-socket remove an existing metric nut off of the hammer weight. Replace with special nuts provided 6 each side (A700) INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 3 of 20

15 INSTALLATION INSTRUCTIONS AF B) Torque to in lbs. (USE CAUTION WHEN USING THE ¾ SOCKET WRENCH TO TIGHTEN BOLTS- REMEMBER THAT THE BOLTS ARE 6MM DIA AND PROPER TORQUE WILL BE ACHIEVED QUICKLY). Safety Wire.032 all nuts from turning. SEE FIG NO. 2 FIG NO. 2 4) Attach the modified forward belly panel. Check that clearance holes allow the t- brackets to extend through the panel. SEE FIG NO. 3 FIG NO. 3 INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 4 of 20

16 INSTALLATION INSTRUCTIONS AF ) Attach the cross tube assembly (A911) to the underbelly hard points Qty 2 located under the forward landing gear cross tube. Use the following hardware to attach. SEE FIG NO. 4 QTY TYPE - NUMBER ITEM 2 AN7-35A HEX HEAD BOLTS 4 AN WASHERS 4 AN A STOP NUTS Torque as per FAA AC A In Lbs. Fig No. 4 The cross-tube will self align to the proper angle of the hard points. Check that the existing hardware is secure and for proper torque of in lbs. INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 5 of 20

17 INSTALLATION INSTRUCTIONS AF ) Install the nose mount truss ass (Left and Right sides A909) (SEE ABOVE FIG) to the main cross tube by attaching the aft open clamps around the main cross tube. Attach the clamps together by using the following hardware each side. Truss fits flush with end of cross tube. See Fig 5 QTY TYPE - NUMBER ITEM 2 AN6-13A HEX HEAD BOLTS 8 AN WASHERS 8 AN A STOP NUTS Torque as per FAA AC A In Lbs. Fig No. 5 INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 6 of 20

18 INSTALLATION INSTRUCTIONS AF ) Insert the nose mount yoke Assy (A909) into the forward part of the (A909) truss. Attach using the following hardware. QTY TYPE - NUMBER ITEM 4 AN6-34A HEX HEAD BOLT 8 AN WASHERS 4 AN A STOP NUTS Torque as per FAA AC A In Lbs. 8) Raise the full assembly up to the T-brackets and attach using the following hardware, QTY TYPE - NUMBER ITEM 2 NAS NAS HIGH STRENGHT BOLT 2 AN WASHERS 2 AN WASHERS (AFT SIDE) 2 AN A STOP NUTS Torque as per FAA AC A InLbs. INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 7 of 20

19 INSTALLATION INSTRUCTIONS AF ) Attach supplied hose to aircraft pitot tube and Pitot tube extension, use supplied aero seal (QS100-M8W) hose clamp. Tighten hose clamp around hose at both ends to secure. Check that the hose clamp is secure and hose is well retained 10) CHECK ENTIRE MOUNT FOR PROPER BOLT TORQUE SETTINGS, SECURITY. 11) FOR CAMERA INSTALLATION SEE APPENDIX A INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 8 of 20

20 INSTALLATION INSTRUCTIONS AF AF200-2 SIDE MOUNT INSTALLATION INSTRUCTIONS: SIDE MOUNT SUPPORT INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 9 of 20

21 INSTALLATION INSTRUCTIONS AF ) Attach the SIDE MOUNT LOWER SUPPORT (A967) ( left and right) to the AIRCRAFT CROSS FWD AND AFT CROSS TUBE. Insure that the aircraft is properly protected by using the supplied (A795) rubber sleeve. (See above figures) Attach using the items below for each side. QTY TYPE - NUMBER ITEM 4 AN6-37A HEX HEAD BOLTS 8 AN WASHERS 4 AN A STOP NUTS Torque as per FAA AC A In Lbs. INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 10 of 20

22 INSTALLATION INSTRUCTIONS AF ) Attach SIDE MOUNT YOKE ASSY (A970) to the SIDE MOUNT HORIZONTAL TUBE (A967) LEFT AND RIGHT SIDES by placing the open clamps on the yoke assembly around the horizontal tube as show above. Tighten the two clamps using the following hardware. QTY TYPE NUMBER ITEM 2 AN6-27A HEX HEAD BOLTS 4 AN WASHERS 2 AN A STOP NUTS Torque as per FAA AC A In Lbs. 3) Attach the FORK TUBE ASSY (A970) to SIDE MOUNT YOKE ASSY (A970) LEFT AND RIGHT HAND SIDES Use the following hardware for each side. QTY TYPE NUMBER ITEM 2 AN6-14A HEX HEAD BOLTS 4 AN WASHERS 8 AN A STOP NUTS Torque as per FAA AC A In Lbs. 4) CHECK ENTIRE MOUNT FOR PROPER BOLT TORQUE SETTINGS, SECURITY. 5) FOR CAMERA INSTALLATION SEE APPENDIX A INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 11 of 20

23 INSTALLATION INSTRUCTIONS AF AF200-2 COUNTER WEIGHT INSTALLATION INSTRUCTIONS: COUNTER WEIGHT SUPPORT INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 12 of 20

24 INSTALLATION INSTRUCTIONS AF )Attach the COMBO SIDE FITTING ASSY (A972) to the aircraft hard point on the right side of the aircraft. The combo fitting will allow for the attachment of both the side mount and the counterweight installations. The left side does not require a combo fitting because the counterweight does not attach to the left side aircraft hard point. (see figure above) QTY TYPE NUMBER ITEM 1 AN6-25A HEX HEAD BOLTS 2 AN WASHERS 1 AN A STOP NUTS Torque as per FAA AC A In Lbs. INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 13 of 20

25 INSTALLATION INSTRUCTIONS AF ) Attach the COUNTER WEIGHT YOKE TENSION TUBE to the COMBO SIDE FITTING (A972). Use the following hardware (SEE ABOVE FIGURE) QTY TYPE NUMBER ITEM 1 AN6-22A HEX HEAD BOLTS 2 AN WASHERS 1 AN A STOP NUTS Torque as per FAA AC A In Lbs. 3) Attach the LOWER SIDE MOUNT SUPPORT ASSY ( left and right) to the AIRCRAFT CROSS AFT CROSS TUBE. Insure that the aircraft is properly protected by using the supplied (A795) rubber sleeve. Note:The counterweight supports are located inside of the side mount installation on the aft cross tube (See above figure) Attach using the items below for each side. QTY TYPE - NUMBER ITEM 4 AN6-37A HEX HEAD BOLTS 8 AN WASHERS 4 AN A STOP NUTS Torque as per FAA AC A In Lbs. INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 14 of 20

26 INSTALLATION INSTRUCTIONS AF )Attach the COUNTERWEIGHT TENSION TUBE to the LOWER SIDE MOUNT SUPPORT TUBES LH AND RH (see above figure) Use the following hardware: QTY TYPE NUMBER ITEM 1 AN6-22A HEX HEAD BOLTS 2 AN WASHERS 1 AN A STOP NUTS Torque as per FAA AC A In Lbs. 5)Attach the LOWER SIDE MOUNT SUPPORT TUBES LH AND RH (see above figure) Use the following hardware: QTY TYPE NUMBER ITEM 1 AN6-14A HEX HEAD BOLTS 2 AN WASHERS 1 AN A STOP NUTS Torque as per FAA AC A In Lbs INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 15 of 20

27 INSTALLATION INSTRUCTIONS AF ) Attach the COUNTER WEIGHT to the COUNTER WEIGHT ASSEMBLY using the 1 diameter bolt supplied. Tighten bolt so taper fit is tight and secure with no free play. Safety bolt to bracket with.032 safety wire. SEE ABOVE FIGURE The standard weight box can (A125) be installed if more counterweight is required. When adding weight to box be sure to check that the weight is secure and has little free movement. Also check that the box lid latches qty 2 are secure and locked. 150 LBS MAX WEIGHT IN BOX / ADDED TO INSIDE OF BOX 7) CHECK ENTIRE MOUNT FOR PROPER BOLT TORQUE SETTINGS, SECURITY. INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 16 of 20

28 INSTALLATION INSTRUCTIONS AF FINAL INSTALLATION INSTRUCTIONS: 1. CHECK ENTIRE MOUNT FOR SECURITY AND PROPER BOLT TORQUE SETTINGS. 2. CALCULATE WEIGHT AND BALANCE 3. INSTALL APPROPRIATE PLACARDS IN COCKPIT V NE = Reduce the published V NE by 40 KIAS for aircraft with a 155 KIAS V NE V NE = Reduce the published V NE by 35 KIAS for aircraft with a 150 KIAS V NE with a camera and counter weight installed The pitot heat must remain OFF and/or the circuit breaker pulled With the auxiliary pitot tube installed. 4. MAKE LOG BOOK ENTRIES AS REQUIRED BY FAR S 5. RETURN AIRCRAFT TO SERVICE REMOVAL INSTRUCTIONS: FP200 MOUNT. To remove FP200-2 mount from aircraft: Follow directions in reverse order and replace all original hardware / fixtures that were removed for installation of FP200-2 mount. If Any Remove any FP200-2 mount placards from cockpit Calculate weight and balance Make appropriate log book entry Return Aircraft to service INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 17 of 20

29 INSTALLATION INSTRUCTIONS AF APPENDIX A CAMERA INSTALLATION Installation Supplement Wescam Type End Fitting 1) Install Camera System to Mount Support using 1 x 8 UNC 2 ¾ Bolt and camera provided. Safety Wire main bolt to mount end fitting drilled fitting. Torque ft lbs. 2) Route and install power conditioner / route cables along brackets securely using plastic tie straps to secure. 3) Make appropriate power connection on the battery or in the rear baggage, or on the main power buss through a 20a breaker. Connect system battery cable with knife connectors. Follow instructions that are attached to the electrical system provided by the camera manufacture. 4) If required secure control unit to rear seat belt 5) Check all systems for flight integrity and that no system interferes with the operation helicopter flight controls. INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 18 of 20

30 INSTALLATION INSTRUCTIONS AF APPENDIX B WEIGHT AND BALANCE AF200-2 WEIGHT AND STATIONS FOR CAMERA SYSTEMS AS350 & AS355 REV AF200-2-A WEIGHT LONGITUDINAL LATERAL ITEM DESCRIPTION LBS ARM INCHES ARM INCHES NOSE MOUNTED CAMERA - (USE CAMERA WEIGHT) NOSE MOUNT SUPPORT COUNTER WEIGHT SUPPORT COUNTER WEIGHT BOX EMPTY (LOAD 150 LBS MAX) ADD WEIGHT IN BOX (USE ACTUAL WEIGHT) RH SIDE MOUNT LH SIDE MOUNT R/H SIDE MOUNTED CAMERA OR COUNTERWEIGHT (USE ACTUAL WEIGHT) L/H SIDE MOUNTED CAMERA OR COUNTERWEIGHT (USE ACTUAL WEIGHT) TAIL CONE W/ WEIGHT MAX (SEE EUROCOPTER SB) Note: MULTIPLE FLYING CONFIGURATIONS APPROVED: Nose mount, counterweight, side mounts can be installed and flown with or without installed camera / and or counterweights. Example: Nose and side mount installed and camera is located on nose so counterweight box would be located on aft section to achieve correct weight and balance. Use proper weight and balance for multiple configurations installed. INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 19 of 20

31 INSTALLATION INSTRUCTIONS AF APPENDIX C QUICK CLAMP INSTALLATION INSTRUCTIONS: AF Aerodrome Way Hangar No. 2 Georgetown, Ca Page 20 of 20

32 DOCUMENT AF INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AF200-2 UNIVERSAL MOUNT FOR EUROCOPTER AS350 / AS355 SERIES HELICOPTERS STC NO: SR01058LA AIRFILM CAMERA SYSTEMS 6245 AERODROME WAY, HANGAR NO. 2 GEORGETOWN, CA Revision: N/C Jan. 17, 2004

33 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, 2004 RECORD OF REVISIONS No. Revision Inserted Date By No. Revision Inserted N/C Date By LIST OF EFFECTIVE PAGES TITLE PAGES REVISION Cover N/C Record of Revisions 1 N/C List of Effective Pages 1 N/C Table of Contents 2 N/C 1.0 General 3 to 4 N/C 2.0 Airworthiness Limitations 5 N/C 3.0 Inspection Requirements 6 to 9 N/C 4.0 Removal, Disassembly, Reassembly And Installation 10 N/C 5.0 Weight and Balance 11 N/C REVISION: N/C PAGE 1

34 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, 2004 TABLE OF CONTENTS SECTION TITLE PAGE RECORD OF REVISIONS...1 LIST OF EFFECTIVE PAGES...1 TABLE OF CONTENTS GENERAL INTRODUCTION PURPOSE SCOPE APPLICABILITY DOCUMENT CHANGE CONTROL AIRWORTHINESS LIMITATIONS INSPECTION REQUIREMENTS SCHEDULED INSPECTIONS HOUR INSPECTION INTERVALS...8 TABLE HOUR TIME IN SERVICE INSPECTIONS ON HELICOPTER HOUR TIME IN SERVICE INSPECTION INTERVAL...9 TABLE FITTING INSPECTIONS...9 TABLE FORK END / HARDWARE INSPECTIONS...9 TABLE TUBE INSPECTIONS INSPECTION LIMITS REMOVAL, DISASSEMBLY, REASSEMBLY AND INSTALLATION WEIGHT AND BALANCE...11 REVISION: N/C PAGE 2

35 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, GENERAL 1.1 INTRODUCTION This manual presents the Instructions for Continued Airworthiness (ICA) for the installation of the model AF200-2 Universal Mount. This mount is to be installed on the Eurocopter AS350 / AS355 SERIES with Supplemental Type Certificate (STC) SR01058LA. The AF200-2 Universal Mount consists of a aluminum structure tubes with aluminum machined fittings. The mount is designed to facilitate the attachment of equipment such as video cameras or searchlights. The cover page of this document shows the typical mount installation with a searchlight on the Eurocopter AS350 / AS355 helicopter. The AF200-2 Mount attaches to the aircraft using the following: Side Aircraft Hard Points (350A ), located on the side of aircraft: Aircraft Hard Points (350A ) located on forward cross tube. Aircraft Asorber Vibration, RH & LH (350-A ) Forward / Aft aircraft cross tubes REVISION: N/C PAGE 3

36 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, PURPOSE The purpose of this document is to provide Instructions for Continued Airworthiness to inspect the Model AF200-2 Universal Mount. REVISION: N/C PAGE 4

37 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, SCOPE The scope of this document is limited to information, procedures, requirements and limitations for this Supplemental Type Certificate. When a requirement specified in the appendix to the regulations is not applicable to this Supplemental Type Certificate the requirement will not be included in the Instructions for Continued Airworthiness. 1.4 APPLICABILITY These Instructions for Continued Airworthiness are applicable to the AF200-2 Universal Mount installed on the Eurocopter AS350 AND AS355 series helicopter. 1.5 DOCUMENT CHANGE CONTROL Changes to this document will be distributed to registered owners of the AF200-2 Universal Mount within 10 days after the revision is approved. Changes to this document will be indicated by a revision number in the footer, vertical lines adjacent to the change, and in the Record of Revisions. REVISION: N/C PAGE 5

38 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, AIRWORTHINESS LIMITATIONS SEE FAA APPROVED RFM FOR COMPLETE LIMITATIONS Vne= 110 KIAS with camera installed REVISION: N/C PAGE 6

39 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, INSPECTION REQUIREMENTS REVISION: N/C PAGE 7

40 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, SCHEDULED INSPECTIONS The scheduled inspections required by this ICA are contained on the following checklists. This checklist, when completed, is to become a permanent part of the AF200-2 Universal Mount records. NOTE: There are no field repairs or overhaul allowed for the AF200-2 Universal mount. If the mount fails the following inspections, the mount is to be removed from the helicopter and returned to HOUR INSPECTION INTERVALS The 100 hour time in service inspections consist of visually inspecting the critical area of the AF200-2 Universal Mount installation. Due to the simplicity of the mount structure, all scheduled 100 hour inspections consist of the same items since the mount is inspected while installed on the helicopter. The inspections per Table are required while the AF200-2 Universal Mount is installed on the helicopter at the time in service interval as specified. The inspection is to be performed by maintenance personnel. REVISION: N/C PAGE 8

41 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, HOUR INSPECTION INTERVALS TABLE HOUR TIME IN SERVICE INSPECTIONS ON HELICOPTER Inspect. Interval Inspection Hours 100 Visually inspect welds for cracks Visually inspect aluminum brackets for cracks, nicks or deep scratches Visually inspect tubes for dents, deep scratches, or cracks. Visually inspect hardware for cracks, dents, deep scratches or damage Maintenance Personnel Initial HOUR TIME IN SERVICE INSPECTION INTERVAL The 1000 hour time in service inspection is to be performed every 1000 hours time in service. The mount must be removed from the helicopter and disassembled per Section 4.0. TABLE FITTING INSPECTIONS Inspect. Interval Inspection Hours 1000 Visually inspect bolt holes for damage Visually inspect brackets for cracks, nicks or deep scratches Maintenance Personnel Initial TABLE FORK END / HARDWARE INSPECTIONS Inspect. Interval Inspection Hours 1000 Visually inspect bolt holes for damage Visually inspect threads for signs of damage Visually inspect body for cracks, nicks, and scratches Maintenance Personnel Initial TABLE TUBE INSPECTIONS Inspect. Interval Inspection Hours 1000 Visually inspect welds for cracks Visually inspect bolt holes for signs of cracks, elongation or damage. Visually inspect tubes for dents, deep scratches, or cracks. Visually inspect threads for signs of damage Maintenance Personnel Initial REVISION: N/C PAGE 9

42 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, INSPECTION LIMITS The AF200-2 Universal Mount is to be removed from service and returned to if the following inspection limits are exceeded. Cracks: Bolt hole elongation Dents, scratches or nicks Tube Dents: Tube scratches: Any indication Any Indication Greater than inches Greater than inches Greater than inches REVISION: N/C PAGE 10

43 AIRFILM CAMERA SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DOCUMENT No. AF Dated: Jan. 17, REMOVAL, DISASSEMBLY, REASSEMBLY AND INSTALLATION For latest update refer to the Airfilm Camera systems Installation Instructions AF WEIGHT AND BALANCE The weight and balance location for the AF200-2 Universal Mount is: AF200-2 WEIGHT AND STATIONS FOR CAMERA SYSTEMS AS350 & AS355 REV N/S WEIGHT LONGITUDINAL LATERAL ITEM DESCRIPTION LBS ARM INCHES ARM INCHES NOSE MOUNTED CAMERA - USE CAMERA WEIGHT NOSE MOUNT SUPPORT COUNTER WEIGHT SUPPORT COUNTER WEIGHT BOX EMPTY COUNTER WEIGHTS INSTALLED (175 max) COUNTER WEIGHT SOLID TYPE RH SIDE MOUNT LH SIDE MOUNT R/H SIDE MOUNTED CAMERA OR COUNTERWEIGHT - SEE LIST L/H SIDE MOUNTED CAMERA OR COUNTERWEIGHT - SEE LIST TAIL CONE W/ WEIGHT MAX (SEE EUROCOPTER SB) Note: MULTIPLE FLYING CONFIGURATIONS APPROVED: Nose mount, counterweight, side mounts can be installed and flown with or without installed camera / and or counterweights. Example: Nose and side mount installed and camera is located on nose so counterweight box would be located on aft section to achieve correct weight and balance. Use proper weight and balance for multiple configurations installed. REVISION: N/C PAGE 11

44 AIRFILM CAMERA SYSTEMS HELICOPTER CAMERA MOUNT 6245 AERODROME WAY, HANGAR NO 2 DRAWING LIST NO. AF PO Box 1352 DATE 8/10/2004 GEORGETOWN, CA REV: D MASTER DOCUMENT LIST AF200 CAMERA MOUNT AS-350/ AS 355 SERIES HELICOPTERS LOG OF REVISIONS REVISION REVISION DATE PAGES EFFECTED N/C 4/01/2000 ALL Original Submittal A 2/27/2000 ALL ADDED A431 & A524 COMMENTS B 1/20/2001 ALL A100, A108, A127, A134A, A , A205, A207 A300, A305, A310, A311, A350, A400-A404, A426, A475 A477, A500, A515-A517, A565-A569 C 5/10/ ADDED REPORT LISTING 5/10/ THRU 9 AF200-2 SYSTEM ADDED D 8/10/ AF REV A INSTALL DOC

45 AIRFILM CAMERA SYSTEMS HELICOPTER CAMERA MOUNT 6245 AERODROME WAY DRAWING LIST NO. AF HANGAR NO 2 DATE 8/10/2004 PO BOX 1352 REV: D GEORGETOWN, CA PAGE 1 OF 8 MASTER DOCUMENT LIST AF200 CAMERA MOUNT - AS-350/ AS 355 SERIES HELICOPTERS REPORTS LIST REPORT NO. TITLE DATE REV AF Structural Substantiation 3/25/04 C AF Flight Test Report AF Rotorcraft Flight Manual Supplement AF AF200-1 Installation Manual 4/18/04 AF AF200-2 Installation Manual 8/10/04 A AF AF200-1 Maintenance Instructions 4/18/04 AF AF200-2 Maintenance Instructions 4/18/04

46 AIRFILM CAMERA SYSTEMS HELICOPTER CAMERA MOUNT 6245 AERODROME WAY DRAWING LIST NO. AF HANGAR NO 2 DATE 8/10/2004 PO BOX 1352 REV: D GEORGETOWN, CA PAGE 2 OF 8 MASTER DOCUMENT LIST AF200 CAMERA MOUNT AS-350/ AS 355 SERIES HELICOPTERS DRAWINGS DWG NO TITLE DWG DATE REV A996 AF200-2 SYSTEM 1/1/2004 N/C A900 AF200-2 NOSE MOUNT 12/20/2003 N/C A909 NM TRUSS ASSY 5/11/2004 N/C A918 NM YOKE ASSY 1/19/2004 N/C A911 NM CROSS TUBE ASSY 1/19/2004 N/C A952 T-BRACKET ASSY 2/2/2004 N/C A917 NM COUPLE ASSY 1/19/2004 N/C A919 NM PITOT ASSY 1/19/2004 N/C A920 NM END FITTING ASSY WESCAM STYLE 1/19/2004 N/C A964 AF200-2 COUNTER WEIGHT ASSY 2/23/2004 N/C A958 CW WEIGHT ASSY 1/19/2004 N/C A END FITTING WESCAM STYLE ASST 1/19/2004 N/C A969 AF200-2 SIDE MOUNT ASSY 1/19/2004 N/C A970 FORK TUBE ASSY 1/19/2004 N/C A968 SM YOKE SUPPORT ASSY 1/19/2004 N/C A967 SM HORZ SUPPORT ASSY 1/15/2004 N/C A972 COMBO SIDE FITTING ASSY 12/22/2003 N/C A700 SPECIAL NUT 11/18/2003 N/C A701 T BRACKET 11/18/2003 N/C A703 HALF CLAMP A 11/18/2003 N/C A704 HALP CLAMP B 11/18/2003 N/C A705 MALE TAPER WESCAM STYLE 11/18/2003 N/C A709 END FITTING WESCAM STYLE 11/18/2003 N/C A710 THREADED TUBE 3/15/2004 N/C A BOSS FITTING FEMALE 11/18/2003 N/C

47 AIRFILM CAMERA SYSTEMS HELICOPTER CAMERA MOUNT 6245 AERODROME WAY DRAWING LIST NO. AF HANGAR NO 2 DATE 8/10/2004 PO BOX 1352 REV: D GEORGETOWN, CA PAGE 3 OF 8 MASTER DOCUMENT LIST AF200 CAMERA MOUNT AS-350/ AS 355 SERIES HELICOPTERS A717 2/5 INTERCONNECT 11/18/2003 N/C A INTERCONNECT 11/18/2003 N/C A719 END FITTING PLATE 11/18/2003 N/C A TUBE 3/15/2003 N/C A721 FORK END 11/18/2003 N/C A722 PITOT TUBE EXT 11/18/2003 N/C A HALF CLAMP A 11/18/2003 N/C A HALP CLAMP B 11/18/2003 N/C A TUBE TO THREAD ADAPT 11/18/2003 N/C A726 SM 2.5 HORZ TUBE 11/18/2003 N/C A727 SM YOKE 11/18/2003 N/C A729 CW STEEL WEIGHT 50 LBS 11/18/2003 N/C A730 EYEBOLT 11/18/2003 N/C A TUBE 3/15/2003 N/C A741 SM SCALLOP TUBE 11/18/2003 N/C A FORK END FITTING 1/30/2004 N/C A750 HARD POINT ATTACH A 11/18/2003 N/C A751 SCALLOP WASHER 11/18/2003 N/C A752 HARD POINT ATTACH B 11/18/2003 N/C A760 CENTER TRUSS BRACKET 12/20/2003 N/C A BOSS FITTING 12/20/2003 N/C A762 NM YOKE 12/20/2003 N/C A764 NM ATTACH BRACKET FWD 3/23/2004 N/C A765 NM ATTACH BRACKET AFT 12/20/2003 N/C A768 NM CROSS TUBE SPRT BRKT 12/20/2003 N/C A773 EYE BOLT 1/26/2003 N/C A774 PITOT EXT ADAPT PLATE 12/20/2003 N/C A775 NM SUPPORT BRACKET 4/17/2004 N/C A794 RUBBER SLEAVE 5/17/2004 N/C

48 AIRFILM CAMERA SYSTEMS HELICOPTER CAMERA MOUNT 6245 AERODROME WAY DRAWING LIST NO. AF HANGAR NO 2 DATE 8/10/2004 PO BOX 1352 REV: D GEORGETOWN, CA PAGE 4 OF 8 MASTER DOCUMENT LIST AF200 CAMERA MOUNT AS-350/ AS 355 SERIES HELICOPTERS A795 RUBBER SLEEVE 5/17/2004 N/C A796 SM GUSSET 5/17/2004 N/C A706 AFT BRACKET 11/18/2004 N/C A956 CLAMP STYLE T- BRACKET (ALTERNATE) 1/19/2004 N/C A733 T-BRACKET CLAMP A 11/18/2003 N/C A734 T-BRACKET CLAMP B 11/18/2003 N/C A735 T-BRACKET CLAMP C 11/18/2003 N/C

49 AIRFILM CAMERA SYSTEMS HELICOPTER CAMERA MOUNT 6245 AERODROME WAY DRAWING LIST NO. AF HANGAR NO 2 DATE 8/10/2004 PO BOX 1352 REV: D GEORGETOWN, CA PAGE 5 OF 8 MASTER DOCUMENT LIST AF200 CAMERA MOUNT AS-350/ AS 355 SERIES HELICOPTERS Below items are AF200-1 A50ML MATERIALS AND FINISH LIST 1/20/2001 B A100 COUNTERWEIGHT ASSY 1/8/2001 A A101 CW YOKE ASSY 1/10/2000 N/C A104 CW ETUBE 1/10/2000 N/C A105 CW SLEEVE 1/10/2000 N/C A106 CW CROSS TUBE RH 1/10/2000 N/C A108 CW YOKE TUBE 8/2/2001 N/C A109 CW INSERT TUBE 1/10/2000 N/C A125 CW BOX ASSY 1/10/2000 N/C A126 BOTTOM PLATE 1/10/2000 N/C A127 RH SIDE PLATE 1/5/2001 A A129 BACK PLATE 1/10/2000 N/C A130 TOP PLATE 1/10/2000 N/C A131 FRONT PLATE 1/10/2000 N/C A132 HINGE 1/10/2000 N/C A133 LATCH RCV STOP 1/10/2000 N/C A134 STD TAPER MALE 1/10/2000 N/C A150 CW TUBE LOW ASSY 1/10/2000 N/C A151 CW LOWER TUBE 1/10/2000 N/C A175 CW TENSION TUBE ASSY 1/5/2001 A A176 CW TENSION TUBE FWD 1/5/2001 A A177 CW TENSION TUBE AFT 1/5/2001 A

50 AIRFILM CAMERA SYSTEMS HELICOPTER CAMERA MOUNT 6245 AERODROME WAY DRAWING LIST NO. AF HANGAR NO 2 DATE 8/10//2004 PO BOX 1352 REV: D GEORGETOWN, CA PAGE 6 OF 8 MASTER DOCUMENT LIST AF200 CAMERA MOUNT AS-350/ AS 355 SERIES HELICOPTERS A178 CW INTERCONNECT 1/5/2001 A A200 HAMMER ATTACH ASSY 1/10/2000 N/C A201 T BRACKET 1/10/2000 N/C A202 CAPTURE NUT 1/10/2000 N/C A203 CROSS TUBE ASSY 1/10/2000 N/C A204 HARD POINT ASSY 1/10/2000 N/C A205 MAIN X TUBE 1/10/2000 N/C A206 CW TAB BRACKET 1/10/2000 N/C A207 PIVOT HINGE ASSY 1/17/2001 N/C A210 SPLIT PANEL MOD 1/5/2001 N/C A300 SIDE MOUNT ASSY 1/5/2001 A A305 LH SIDE TUBE SUPPORT ASSY 1/5/2001 A A306 SM LH INSERT TUBE 1/5/2001 A A307 SM LH ANGLE TUBE 1/5/2001 A A308 SM LH MAIN TUBE 1/5/2001 A A309 SM GUSSET BOX 1/10/2000 N/C A310 TENSION TUBE ASSY 1/5/2001 A A311 TENSION TUBE 1/5/2001 A A325 SIDE MOUNT LH ASSY 1/10/2000 N/C A350 YOKE FRAME ASSY 1/5/2001 A A352 YOKE FRAME 1/10/2000 N/C A356 CLAMP ASSY 1/10/2000 N/C A400 NOSE MOUNT ASSY 1/10/2000 N/C

51 AIRFILM CAMERA SYSTEMS HELICOPTER CAMERA MOUNT 6245 AERODROME WAY DRAWING LIST NO. AF HANGAR NO 2 DATE 8/10/2004 PO BOX 1352 REV: D GEORGETOWN, CA PAGE 7 OF 8 MASTER DOCUMENT LIST AF200 CAMERA MOUNT AS-350/ AS 355 SERIES HELICOPTERS A401 NM AFT TUBE ASSY 1/5/2001 A A402 NM BAR CLAMP TUBE 8/3/2001 A A403 NM AFT TUBE LOWER 8/3/2001 A A404 NM AFT TUBE UPPER 8/3/2001 A A405 GUSSET BLADE 1/10/2000 N/C A406 END CAP 1/10/2000 N/C A425 NM CENTER ASSY 6/27/2000 A A426 NM WEB BLADE 9/15/2000 A A427 NM C TUBE 1/10/2000 N/C A428 NM D TUBE 1/10/2000 N/C A429 NM GUSSET 1/10/2000 N/C A430 NM BRACKET 1/10/2000 N/C A431 NM CENTER TUBE 6/27/2000 A A450 FWD TUBE ASSY 1/10/2000 N/C A475 NOSE MOUNT YOKE ASSY 1/10/2000 N/C A477 NM YOKE FRAME 8/3/2001 A A478 NM CENTER TUBE 1/10/2000 N/C A500 CLAMP GEAR ASSY 7/20/2000 A A501 SADDLE WASHER 1 1/10/2000 N/C A502 SADDLE WASHER /10/2000 N/C A503 SADDLE WASHER 2.0 1/10/2000 N/C A504 SADDLE WASHER 2.5 1/10/2000 N/C A505 PITOT TUBE EXTENSION 1/10/2000 N/C A506 END FITTING NO.1 1/10/2000 N/C A507 END FITTING NO.2 1/10/2000 N/C A509 END FITTING BACKING PLATE 1/10/2000 N/C A510 PIN.250 1/10/2000 N/C A511 PIN.375 1/10/2000 N/C

52 AIRFILM CAMERA SYSTEMS HELICOPTER CAMERA MOUNT 6245 AERODROME WAY DRAWING LIST NO. AF HANGAR NO 2 DATE 8/10/2004 PO BOX 1352 REV: D GEORGETOWN, CA PAGE 8 OF 8 MASTER DOCUMENT LIST AF200 CAMERA MOUNT AS-350/ AS 355 SERIES HELICOPTERS A512 THREADED WELDED INSERT 1/10/2000 N/C A513 TAB INSERT B 1/10/2000 N/C A514 FORK END FITTING A 1/10/2000 N/C A515 BOSS INSERT 2.0 1/5/2001 B A516 BOSS INSERT /1/2000 A A517 BOSS INSERT 2.5A 10/21/2000 A A518 BOSS INSERT 1.0 1/10/2000 N/C A519 BOSS INSERT 1.0A 1/10/2000 N/C A520 END FITTING W/O PITOT ASSY 1/10/2000 N/C A521 END FITTING W/ PITOT ASSY 1/10/2000 N/C A522 TAB INSERT 1/10/2000 N/C A523 FORK END -B.065 1/10/2000 N/C A524 END FITTING EXTENSION 6/10/2000 A A565 EYE BOLT 1/5/2001 N/C A566 MALE FITTING 1/5/2001 N/C A567 FE-MALE SADDLE 1/5/2001 N/C A568 END CLAMP ASSY 7/20/2001 A A569 SADDLE WASHER 2.0 A 1/5/2001 N/C