This document provides instructions for installing and maintaining the SkyView HDX Autopilot servos in the Piper PA-34 Seneca series of airplanes. Autopilot servo installation in any airplane with modifications to areas where the servos will be installed is not addressed in this document. See Section...
Installation Compliance Airplanes on the AML meet a minimum required configuration for applicability of the STC. However, some airplanes may have been modified, and consequently, it may be difficult to use the information in this manual to completely substantiate the installation in compliance with the STC.
Control Cable Verification The SkyView HDX Autopilot system for the Piper PA-34 Seneca series of airplanes is designed to attach to the airplane's original 1/8" diameter control cables. It is important for installers to verify the diameter of the control cables before starting installation activities. The diameter of...
Materials The materials identified in Table 1 are required to install the roll servo into a Piper PA-34 series airplane. ITEM numbers refer to call-out numbers in the figures in Section 8.2: Roll Servo Parts, Assemblies, and Installation. Table 1: Roll Servo Installation Materials ITEM DYNON P/N DESCRIPTION...
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The materials identified in Table 2 are required to install the pitch servo into a Piper PA-34 series aircraft. ITEM numbers refer to call-out numbers in the figures in Section 8.3: Pitch Servo Parts, Assemblies, and Installation. Table 2: Pitch Servo Installation Materials ITEM DYNON P/N DESCRIPTION...
Servo Bracketry Installation and Bridle Cable Preparation This section provides instructions for installing the roll and pitch servo bracketry, and then fabricating the bridle cable assemblies that attach to the aileron and elevator control cables. The instructions apply to all Seneca model airplanes except for serial numbers 34-7570001 through 34-8170092, when equipped with pneumatic de-ice boots.
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5.1.2.1 Mount and Base Bracket Installation (With Factory-installed Autopilot) Complete the following steps to temporarily install the roll servo mount bracket and base bracket in an airplane equipped with a factory autopilot roll servo that is installed in the same general position.
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5.1.2.2 Mount and Base Bracket Installation (Without Factory-installed Autopilot) Complete the following steps to temporarily install the roll servo mount bracket and base bracket in an airplane not equipped with a factory autopilot pitch servo. To temporarily install the mount and base brackets: 1.
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5.1.2.3 Brace Installation (All Airplanes) Using Figure 9 as reference, complete the following steps to temporarily install the roll servo brace. To temporarily install the roll servo brace: 1. Place brace into position, and then secure brace to mount bracket. 2.
5.2 Roll Servo Bridle Cable Preparation This section provides instructions for preparing the roll servo bridle cable assembly for final installation. Performing these tasks after installing the roll servo bracketry, and before permanently installing the roll servo, simplifies the overall installation. The instructions in this section assume the roll servo is still temporarily installed in airplane per procedures in Section 5.1.
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5.2.3 Temporary Bridle Cable Connection to Aileron Cable Reference Figure 11 Figure 12 when performing the following procedure. To temporarily connect bridle cable ends to the airplane's aileron crossover cable: 1. Secure ailerons in neutral position. 2. Connect inboard and outboard cable ends to airplane's aileron crossover cable. Loosely secure to permit cable slippage.
5.3 Pitch Servo Bracketry Installation The pitch servo mount bracket, base bracket, and gusset mount directly to the airplane (see Figure 23 for complete installation example). The mount bracket positions the base bracket and becomes fastened to the base bracket. The pitch servo gusset is fastened to base bracket and the airplane's existing structure.
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6. Temporarily secure mount bracket to crossover cable guide assembly so that: • Servo capstan is centered above right-side outboard elevator control cable, as shown Figure • Servo capstan is aligned with right outboard elevator control cable so that the bridle cables will feed onto grooves in the capstan.
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5.3.2.2 Mount and Base Bracket Installation (Without Factory-installed Autopilot) Complete the following steps to install the pitch servo mount bracket and base bracket in an airplane not equipped with a factory autopilot pitch servo. To temporarily install the mount and base brackets: 1.
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5.3.2.3 Gusset Installation (All Airplanes) Using Figure 19 as reference, complete the following steps to temporarily install the pitch servo gusset. To temporarily install the gusset: 1. Remove temporary fasteners from 3-4 aft holes on base bracket horizontal flange. 2. If there is an existing hole and fastener in pulley mounting bracket at FS 128, then remove fastener.
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5.3.3 Permanent Pitch Servo Bracketry Installation This section provides instructions for permanently installing the mount bracket, base bracket, and gusset. To complete pitch servo bracketry installation: 1. Disassemble and remove all temporarily secured bracketry. 2. Deburr all holes in bracketry and fuselage skin/structure. 3.
5.4 Pitch Servo Bridle Cable Preparation This section provides instructions for preparing the roll servo bridle cable assembly for final installation. Performing these tasks after installing the roll servo bracketry, and before permanently installing the roll servo, simplifies the overall installation. The instructions in this section assume the pitch servo is still temporarily installed in airplane per procedures in Section 5.3.
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5.4.3 Temporary Bridle Cable Connection to Elevator Cable Reference Figure 21 when performing the following procedure. To temporarily connect bridle cable ends to the airplane's elevator cable: 1. Secure elevator in neutral position. 2. Connect inboard and outboard cable ends to airplane's elevator "up" cable. Loosely secure to permit cable slippage.
Servo Electrical Wiring For complete wiring and network configuration instructions, refer to the following: • 103261-000 SkyView HDX System General Installation Manual document • 103947-000 SkyView HDX Wiring Diagram - Twin Engine Route the servo electrical harnesses through the airframe structure as appropriate. Take precautions to prevent the servo harnesses from chafing against structure or interfering with the airplane's flight controls or other moving components.
Servo Maintenance This section provides information and procedures to maintain the roll and pitch servos. It serves as instructions for Continued Airworthiness. 7.1 Roll Servo Removal and Installation 7.1.1 Location and Access The roll servo is located beneath the cabin floor between the main spar and the rear spar carry- through structures on the left-hand side of the cabin as indicated in Figure Access requires removing the seats, carpeting, and the floor in accordance with the...
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5. Safety wire bolts to prevent them from loosening. Installers can safety wire bolts together (see Figure 13), to the mount bracket using provided holes in bracket, or a combination thereof, depending on preferred method and access. 6. Connect D9 electrical harness connector to roll servo. Use a clamp or other fastener to secure harness cable to avoid entanglement with moving components.
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8. Secure capstan/cable assembly onto servo shaft. (See Section 7.5: Servo Capstan Removal and Re-installation for instructions.) 9. Make sure control cable where bridle cable clamps will attach is clean and free of dirt and grease. 10. Connect inboard and outboard cable ends to airplane's aileron crossover cable (see Figure 11).
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To check the bridle cable installation: 1. Remove tape temporarily securing bridle cable to capstan. 2. Remove device securing flight controls in neutral position. 3. While moving control through full range of motion, verify the following: • Cable clamps do not contact any structures during entire travel. •...
7.2 Pitch Servo Removal and Installation 7.2.1 Location and Access The pitch servo is located beneath the cabin floor between the main spar and the rear spar carry through structure on the right-hand side of the cabin as shown in Figure Access requires removing the seats, carpeting, and the floor in accordance with the manufacturers service instructions.
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7.2.4 Pitch Servo Bridle Cable Installation Make sure all flight control cables are rigged and tensioned in accordance with the manufacturer’s servicing manual. Failure to do so may result in poor Autopilot system performance. To install pitch servo bridle cable: 1.
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• Cable clamps are located at the dimensions shown in Figure • Cable clamps are positioned to best avoid contacting any structures. 12. Tighten aft cable clamp fasteners. 13. Push or pull forward cable clamps outboard, applying 12-15 lbs. of tension to bridle cable. 14.
CALIBRATION > AP SERVO CALIBRATION > CALIBRATION) and follow the onscreen instructions to calibrate the servo(s). SkyView HDX checks the status of the AP Disengage Button. If SkyView HDX detects that the button is pressed (the input is grounded) upon entering AP SERVO CALIBRATION, the AP...
You may run this procedure on its own at any time after a successful servo calibration. SkyView HDX will not display AP status on the Top Bar until after this test procedure is successfully completed.
10. Install new cotter pin to secure castle nut to servo shaft. 7.6 Cable Guard Adjustment Servos come equipped with a cable guard installed. The cable guard may need to be repositioned to avoid interference with the flight control cables or the bridle cables during servo installation procedures.
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