Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003)

Horizontal pivot tension incorrectly set Re-tension horizontal pivot Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 6 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS Product Description General a. The Rosen Sunvisor System consists of two visor assemblies which have been designed to improve pilot comfort during standard cockpit operations. The visor assemblies are fastened to the airframe in the same mounting positions as the factory installed visors. Installation Instructions for Piper Comanche (Kit R1210001, R1210002) This is an FAA STC’d Installation requiring a log book entry upon completion. Pease read through these instructions completely before beginning. Hardware: 4 MS16995-20B #6-32 X ¾ Socket Head Cap Screw 8 AN960-C6L #6 Aluminum Washers 1 5/32 Hex Key 1 7/64 Hex Key 1 9/64 Hex Key NOTE: These instructions cover both the standard Rosen Sunvisor for the Comanche (Kit RCOM-300-1) and the Comanche Third Axis Unit (Kit RCOM- 300-1A)  The common factor in the Comanche is the upper front windscreen trim and the #6-32 screws that hold it in place.  First remove your present Sunvisor and replace the screw in the inboard hole leaving the outboard hole exposed.  Remove the outermost #6-32 fasteners from the trim piece on both the pilot and co-pilot side.  Install the pilot mounting bracket and slide assembly using the provided stainless steel #6-32 X ¾ inch socket head cap screws with washers on both sides of the mounting bracket as shown. A 7/64 Allen key is provided to ensure a snug fit. Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 7 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS  To be sure you are mounting the units on the correct side the brackets as viewed from above should look as follows.  And as seen from the seats looking forward:  Repeat procedure for the co-pilot side.  To operate simply tension the visor movement to your desired tension with the Allen keys provided. o Motion to the side window is controlled with the cap screw in the back of the block. o Motion to rotate the visor to the overhead is controlled by the socket head cap screw in the side of the block. o Third axis tension, if equipped, is controlled by the #10-32 socket head cap screw as shown.  The visors will extend in the slides and should move far enough to the rear to cover the entire face. Tension can be adjusted with the red thumb knob. Note: The red knob will be towards the windscreen.  Your visors can be stowed overhead in several different positions as indicated right.  Because of different pilot heights and seat positions the stowage position wills be different for different pilots. On the co-pilot side a forward stowage position is recommended to keep clear of the doorway when open. Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 8 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS Installation Instructions for Piper Comanche with Knots2U Arapaho Windshield (Kit R1210003) This is an FAA STC’d installation requiring a log book entry upon completion. Please read through these instructions completely before beginning. Hardware: 6 MS24693-C48BP #8-32 X .375 Phillips Flat Head Screw 100 (Black/Patch) 6 A8K75 #8-32 Rivnut 1 5/32 Hex Key 1 7/64 Hex Key 1 9/64 Hex Key These instructions cover the installation for a Piper PA30, PA39, and PA40 with the Knots2U Arapaho windshield configuration. The longer Arapaho windshield eliminates the mounting position over the windshield.  If there are existing visors, remove them.  On the pilot side remove enough of the interior linings to gain access to the aircraft interior metal structure in the upper corner where the side window meets the front window.  Do the same on the copilot side where the door jam is.  On each side, position the round mount against the structure and orient it so the post is as vertical as possible. Both sides should be at the same height in the aircraft.  Mark the three mounting holes on each side.  Drill all marked locations to .221/.226 diameter. Note: Drill only through interior sheet metal. Maximum depth must not exceed 1/4 inch. It is the installer’s responsibility to assure that there are no wires or controls damaged in this operation.  Use a small rat tail file to put a 1/32” notch in each hole for the key in the rivenut.  Install the rivnut using appropriate tooling. Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 9 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS  Trim and or return the interior linings into position. (If necessary cut a hole for each mounting screw.)  Install and tighten each mount in location with the swivel post pointing down.  Apply a small amount of lube to the full diameter of the swivel post.  Mount the visor assembly on each side and secure with a 8-32 X .625 cap screw and #8 high collar washer. Note: The red knob is closest to the windscreen. Note: The 8-32 mounting screw is offset and must align with the recess in the swivel.  Using the hex keys, adjust the tensions so the motion is smooth but tight. o Motion to the side window is controlled with the cap screw in the back of the block. o Motion to rotate the visor to the overhead is controlled by the socket head cap screw in the side of the block. o Third axis tension, if equipped, is controlled by the #10-32 socket head cap screw as shown.  The visors will extend in the slides and should move far enough to the rear to cover the entire face. Tension can be adjusted with the red thumb knob. Note: The red knob will be towards the windscreen.  Your visors can be stowed overhead in several different positions as indicated right.  Because of different pilot heights and seat positions the stowage position will vary for different pilots. On the copilot side a forward stowage position is recommended to keep clear of the doorway when open. Removal a. Reverse installation procedure. Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 10 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS Weight and Balance Because operators calculate Weight and Balance differently the actual station number must be determined by the installer’s calculations. With the visor located in forward use position, the R1210001 system adds 1.13 lbs., the R1210002 system adds 1.19 lbs., and the R1210003 system adds 2.08 lbs. located at the mount point of the visor. When the original visors are removed they must be weighed and removed from the calculation. Repair General a. All components that do not meet the requirements for continued use must be replaced. Instructions for Continued Airworthiness  (On the ground only) o Periodically clean the lenses with a soft cloth, mild soap and water or Rosen Cleaner, Polisher and Protectant. Do not use abrasives on the lens. o Periodically adjust the pivot tensions on the visor assemblies. Airworthiness Limitations The Airworthiness Limitations Section is FAA approved and specifies maintenance required under §43.16 and §91.403 of the Federal Aviation Regulations unless an alternative program has been FAA approved. There are no airworthiness limitations associated with this installation. Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 11 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS Illustrations and IPC 1210001 1210002 1210003 Fig 1 Fig 2 Fig 3 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 12 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fig 6 Fig 4 Fig 5 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 13 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fig 8 Fig 7 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 14 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fig 9 Fig 10 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 15 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fig 13 Fig 12 Fig 11 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 16 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS Part List Fig. No Fig. Item Part Number Description Reference Eff QTY 1 1 R1210001-0 Complete System RCOM-300-1 System 2 2 R1210002-0 Complete System 3rd Axis RCOM-300- 1A System 3 3 R1210003-0 Complete System Knots 2U (Arapaho) 3rd Axis System 4 4 R1210001-1 Pilot Side RCOM-300- 1P 1 4 5 R1210001-2 Copilot Side RCOM-300- 1C 1 5 6 R1210002-1 Pilot Side RCOM-300- 1AP 1 5 7 R1210002-2 Copilot Side RCOM-300- 1AC 1 6 8 R1210003-1 Pilot Side 1 6 9 R1210003-2 Copilot Side 1 7-11 10 1010003 Lens Strip 2 7-11 11 1010000-5 Slide Assembly 2 7-10 12 AN960-C6L Washer #6 Flt 8 7,8 13 1020001 Original Block 2 7-11 14 8HCLW Washer #8 High Collar Lock 4 7-11 15 MS16995-28B Scr #8-32 X .75 Hex Socket Head Cap SST Black 2 7-11 16 MS16995-27B Scr #8-32 X .625 Hex Socket Head Cap SST Black 2 7, 8 17 2407-1041 Label 2 7, 9 18 1210101-001 Mounting Bracket, Pilot 2 7-10 19 1210102 Swivel 2 7-10 20 MS16995-20B Scr #6-32 X .75 Socket Head Cap 4 7-11 21 MS24693-C50B Scr #8-32 X .50 Phillips Flt Hd Screw 100 (Black) 4 7-11 22 1210201 Lens 2 7-11 23 MS24693- C48BP Scr #8-32 X .375 Flt Hd Phil 100 SST Black Patch 6 8,10 24 1210101-002 Mounting Bracket, Copilot 2 9-11 25 1020100-001 Mod Block Assembly 2 11 26 MS24693-C54B Scr #8-32 X 1.00 Flt Hd Phil 100 Blk Patch 6 11 27 1160101-1 Mounting Plate 2 11 28 A8K75 #8-32 Rivnut Grip .10-.075 6 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (P/N R1210001, R1210002, R1210003) Rosen Sunvisor Systems LLC Data 9051-0121-001 Rev C Page 17 of 17 Company Proprietary Information. This document may not be disclosed without the permission of RSS 11 29 1160102-1 Swivel 2 12 30 1020003-001 Modified Block “A” 2 12 31 2801-0010 Washer Flt (Seastrom 5710-61- 30) SST 8 12 32 1020003-001 Modified “B” Block 2 12 33 MS16996-12B Scr #10-32 X .75 Socket Head Cap 2 12 34 10HCLW Washer #10 High Collar Lock 2 13 35 99-701 Knob dia ½ Knurled Red #8-32 X .75 2 13 36 B-19679 Compression Spring 2 13 37 90295A110 Washer .06 X .405 OD - .175 ID Nylon 2 13 38 1010001-5 Female Slide - Universal 2 13 39 1010002-3 Male Slide – Universal 2