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Airfilm Camera Systems AF200, Installation Instructions Manual

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Airfilm Camera Systems AF200 Installation Instructions Manual Download Page 16

INSTALLATION INSTRUCTIONS            AF200-007 - REV E 

DATE 2/26/2015  

 

 Airfilm Camera Systems 

                                                                                               

Page 

16

 of 

31

 

 6245 Aerodrome Way Hangar No. 2 
 Georgetown, Ca 95634

 

 

 
 
6) Attach the 

COUNTER WEIGHT or COUNTER WEIGHT BOX or SENSOR 

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 PAYLOAD AT ATTACHMENT POINT 
 

 
7) CHECK ENTIRE MOUNT FOR PROPER BOLT TORQUE SETTINGS, SECURITY. 
 
 
 

 
 

 
 

Summary of Contents for AF200

Page 1: ...RT NO AF200 007 REV E REV DATE ISSUED 2 26 2015 LOG OF REVISIONS REVISION REVISION DATE PAGES EFFECTED COMMENTS N C 5 10 2004 ALL ORIGINAL SUBMITTAL A 8 10 2004 19 ADDED WEIGHT AND BALANCE A 8 10 2004 17 PLACARDS REVISED B 10 1 2005 20 ADDED APPENDIX C C 2 1 2011 19 REVISED NOTES D 6 5 2013 18 19 REVISED W B NOTES E 2 26 2015 ALL ADDED APPENDIX D PAYLOAD PART A735 A734 P N CHANGE MINOR NOTES ADDED...

Page 2: ...nce 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 payload systems with a Max frontal area 9 2 sq ft Max Weight 275 Lbs 124 7 Kg Determi...

Page 3: ...nted 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 QUICK CLAMP A956 MAY BE SUBSTITUTED FOR A952 FIG NO 1 3A Using a 6mm socket remove an e...

Page 4: ...e to 72 84 in lbs USE CAUTION WHEN USING THE 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 ...

Page 5: ...oints 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 AR AN960 716L WASHERS 4 AN365 720A STOP NUTS Torque as per FAA AC43 13 1A 450 500 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 160 19...

Page 6: ...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 Note cross bar should be installed in direction as picture See Fig 5 QTY TYPE NUMBER ITEM 2 AN6 11A HEX HEAD BOLTS 4 AN960 616 WASHERS 2 AN365 624A STOP NUTS Torque as per FAA AC43 13 1A 160 190 In ...

Page 7: ...truss Attach using the following hardware QTY TYPE NUMBER ITEM 4 AN6 34A HEX HEAD BOLT 8 AN960 616 WASHERS 4 AN365 624A STOP NUTS Torque as per FAA AC43 13 1A 160 190 In Lbs 8 Raise the full assembly up to the T brackets and attach using the following hardware QTY TYPE NUMBER ITEM 2 NAS6206 21 NAS HIGH STRENGTH BOLT 4 AN970 616 WASHERS AFT SIDE 2 AN365 624A STOP NUTS OR EQV Torque as per FAA AC43 ...

Page 8: ...ure nut is tight against lock washer 9 Attach supplied hose to aircraft pitot tube and Pitot tube extension use supplied aero seal QS100 M8W hose clamp Cut hose to length as required 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 APPENDI...

Page 9: ...TALLATION INSTRUCTIONS AF200 007 REV E DATE 2 26 2015 Airfilm Camera Systems Page 9 of 31 6245 Aerodrome Way Hangar No 2 Georgetown Ca 95634 AF200 2 SIDE MOUNT INSTALLATION INSTRUCTIONS SIDE MOUNT SUPPORT ...

Page 10: ...FT CROSS TUBE Insure that the aircraft is properly protected by using the supplied A795 rubber sleeve channel shape See above figures Additional rubber strips are used to protect the landing gear Do not let the metal clamp come in contact with the landing gear Attach using the items below for each side QTY TYPE NUMBER ITEM 4 AN6 37A HEX HEAD BOLTS 8 AN960 616 WASHERS 4 AN365 624A STOP NUTS Torque ...

Page 11: ... following hardware Protect horizontal tube with rubber strips QTY TYPE NUMBER ITEM 2 AN6 27A HEX HEAD BOLTS 4 AN960 616 WASHERS 2 AN365 624A STOP NUTS Torque as per FAA AC43 13 1A 160 190 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 AN960 616 WASHERS 8 AN365 6...

Page 12: ...ATION INSTRUCTIONS AF200 007 REV E DATE 2 26 2015 Airfilm Camera Systems Page 12 of 31 6245 Aerodrome Way Hangar No 2 Georgetown Ca 95634 AF200 2 COUNTER WEIGHT INSTALLATION INSTRUCTIONS COUNTER WEIGHT SUPPORT ...

Page 13: ... 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 Scallop washer to be installed as shown see figure above QTY TYPE NUMBER ITEM 1 AN6 25A HEX HEAD BOLTS 2 AN960 616 WASHERS 1 AN365 624A STOP NUTS Torque ...

Page 14: ...ttach 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 Additional rubber strips are used to protect the landing gear Do not let the metal clamp come in co...

Page 15: ...BES LH AND RH see above figure Use the following hardware QTY TYPE NUMBER ITEM 1 AN6 22A HEX HEAD BOLTS 2 AN960 616 WASHERS 1 AN365 624A STOP NUTS Torque as per FAA AC43 13 1A 160 190 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 AN960 616 WASHERS 1 AN365 624A STOP NUTS Torque as per FAA AC43...

Page 16: ...ighten 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 PAYLOAD AT ATTA...

Page 17: ...d VNE by 35 KIAS for aircraft with a 150 KIAS VNE 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 AF200 MOUNT To remove AF200 2 mount from aircraft Follow directions in reverse order and replace all origin...

Page 18: ...ed fitting Torque 101 110 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 camer...

Page 19: ...INSTALLATION INSTRUCTIONS AF200 007 REV E DATE 2 26 2015 Airfilm Camera Systems Page 19 of 31 6245 Aerodrome Way Hangar No 2 Georgetown Ca 95634 APPENDIX B WEIGHT AND BALANCE ...

Page 20: ...LATION INSTRUCTIONS AF200 007 REV E DATE 2 26 2015 Airfilm Camera Systems Page 20 of 31 6245 Aerodrome Way Hangar No 2 Georgetown Ca 95634 APPENDIX C QUICK CLAMP PROCEDURE THE SAME FOR R H OR L H INSTALLATION ...

Page 21: ...not listed in the installation manual of equal or lesser than the limit case are accepted with this follow on test plan 2 Sensor Camera payload Make Model ________________________________ 3 Test Team Pilot s _________________________________ ________________________________ Print Name Mechanic and or Engineer and or Camera Operator _______________________________ _____________________________ Prin...

Page 22: ...ost critical CG is considered to be at the aft limit for most tests this configuration is mounted forward of the mast should not approach the aft limits This also depends on crew loading The test team conducts the following tests and evaluations and mark initial the box at the end of each section if the configuration successfully passes the requirements 6 2 FAR 29 51 Takeoff 6 2 1 Applicable Regul...

Page 23: ... maximum weight and d At the rotor speed or speeds selected by the applicant 6 3 2 Method of Compliance 1 Performance capabilities during stabilized autorotative descent are useful pilot tools to assist in the management of a Category B rotorcraft when all engines fail This information is also useful in determining the suitability of available landing areas along a given route segment 2 Two speeds...

Page 24: ...ess than 17 knots must be established in which the rotorcraft can be operated without loss of control on or near the ground in any maneuver appropriate to the type such as crosswind takeoffs sideward flight and rearward flight with 1 Critical weight 2 Critical center of gravity 3 Critical rotor rpm and 4 Altitude from standard sea level conditions to the maximum altitude capability of the rotorcra...

Page 25: ...roll control The helicopter will be flown between 1000 and 3000 feet above ground The test altitude will be dependent on traffic and terrain and conditions close to sea level pressure are desirable VNE will be the value stated in the RFM for the test density altitude Qualitative measurement techniques pilot opinion will be used The tests will include Takeoff Climbing flight Forward flight to VNE n...

Page 26: ...wer condition 6 6 2 Method of Compliance This flight requirement may be both a qualitative and quantitative flight evaluation Section 29 571 a contains the flight load survey requirement that results in accumulation of vibration quantitative data Section 29 629 generally requires quantitative data to show freedom from flutter for each part of the rotorcraft including control or stabilizing surface...

Page 27: ...ds up to VH and ii In the most severe icing condition for which certification is requested 2 The pilots must have a window that i Is openable under the conditions prescribed in subparagraph 1 of this paragraph and ii Provides the view prescribed in that subparagraph 6 7 2 Method of Compliance The section outlines requirements for pilot view in fairly general terms The aircraft was approved with th...

Page 28: ...ny of the escape facilities provided for use after an emergency landing or 2 Have sufficient strength to withstand the conditions specified in Sec 29 561 including the means of restraint and their attachments required for the maximum authorized weight of cargo and baggage at the critical loading distribution d If cargo compartment lamps are installed each lamp must be installed so as to prevent co...

Page 29: ...he major emphasis for this type of equipment should be to ensure it does not interfere with the operation of systems that are required for safe operation of the rotorcraft and that the failure modes are acceptable and do not create any hazards During flight operations operate all avionics and electrical systems Complete the matrix below The matrix is laid out with the newly installed equipment lis...

Page 30: ...rgetown Ca 95634 6 9 3 Findings Interference Camera Sensor Light Position Controller Camera Sensor Light Position Controller VHF Comm 1 VHF Comm 2 VHF Comm 3 VHF NAV 1 VHF NAV 2 ADF 1 XPONDER 1 Other Radios Audio 1 Audio 2 Standby Compass Engine Inst Fuel Gage Clock Voltmeter Ammeter Other EMI RFI Comments Satisfactory _________ ...

Page 31: ...f 31 6245 Aerodrome Way Hangar No 2 Georgetown Ca 95634 Signatures General test findings ________________________________ Pilot Signature ____________________________ Mechanic Engineer ____________________________ Other Flt Personnel Signature Function ______________________________________ ...

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