190-01284-00 March 2011 Rev. B - Garmin

C.2 Aircraft Zoning Diagrams ............................................................................................................. C-1 C.3 Single Propeller Aircraft................................................................................................................ C-2 C.4 Aircraft with Two Propellers ......................................................................................................... C-4 C.5 Aircraft with Multiple Jet Engines ................................................................................................ C-7 C.6 Aircraft with Multi-Propellers ....................................................................................................... C-8 C.7 Figure Identification for Each Aircraft Model .............................................................................. C-9 LIST OF FIGURES Figure 2-1. Through Mount Teardrop Footprint Antenna ........................................................................ 2-2 Figure 2-2. Garmin ARINC 743 Footprint Antenna ................................................................................. 2-2 Figure 2-3. Antenna Installation Location ................................................................................................ 2-5 Figure 2-4. GA 35 Antenna Dimensions ................................................................................................ 2-10 Figure 2-5. GA 36 Antenna Dimensions ................................................................................................ 2-11 Figure 2-6. GA 37 Antenna Dimensions ................................................................................................ 2-12 Figure A-1. Doubler Design, Teardrop Footprint Antenna...................................................................... A-3 Figure A-2. Doubler Design, ARINC 743 Footprint Antenna ................................................................. A-4 Figure A-3. Skin Cutout Detail, Teardrop Footprint Antenna ................................................................. A-5 Figure A-4. Skin Cutout Detail, ARINC 743 Footprint ........................................................................... A-6 Page ii Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 Figure A-5. Sample Doubler Location..................................................................................................... A-7 Figure A-6. Doubler Installation, Teardrop Footprint Antenna ............................................................... A-8 Figure A-7. Doubler Installation, ARINC 743 Footprint Antenna .......................................................... A-9 Figure A-8. Through Mount Teardrop Footprint Antenna Installation.................................................. A-10 Figure A-9. GA 37 ARINC 743 Footprint Antenna Installation ........................................................... A-10 Figure B-1. Hawker Beechcraft 90 and 200 Series Antenna Location .................................................... B-1 Figure B-2. Doubler Design, ARINC 743 Footprint Antenna, Hawker Beechcraft 90 and 200 Series ... B-2 Figure B-3. Hawker Beechcraft 90 and 200 Series Fuselage Skin Cutout Detail .................................... B-3 Figure B-4. Hawker Beechcraft 90 and 200 Series GA36 Antenna Installation...................................... B-4 Figure B-5. Hawker Beechcraft 90 and 200 Series GA36 and GA 37 Antenna Installation ................... B-5 Figure C-1. Zoning Legend...................................................................................................................... C-1 Figure C-2. Single Prop (Zoning for a Low or High Wing Single Prop)................................................ C-2 Figure C-3. Single Rear-Mounted Prop with a Curved Fuselage (Zoning For a Low or High Wing Aircraft with a Curved Fuselage) ....................................................................................... C-3 Figure C-4. Single Rear-Mounted Prop Above Fuselage (Zoning for a Low or High Wing Aircraft with a Rear-Mounted Prop Above Fuselage)................................................................................ C-3 Figure C-5. Twin Front-Mounted Props (Zoning for a Low or High Wing Twin Prop Aircraft with Front- Mounted Propellers. The distance d1 and d2 are the same on both engines) .................... C-4 Figure C-6. Twin Rear-Mounted Props (Zoning for a Low or High Wing Twin Prop Aircraft with Rear- Mounted Propellers)........................................................................................................... C-5 Figure C-7. Front and Rear-mounted Props (Zoning for Low or High Wing with a Front and Rear Mounted Propellers)........................................................................................................... C-6 Figure C-8. Twin Jet Engines (Zoning for a Low or High Wing Twin Jet Engine Aircraft) .................. C-7 Figure C-9. Triple Front-Mounted Props (Wings and Above Fuselage) ................................................. C-8 LIST OF TABLES Table 1-1. Antenna Models....................................................................................................................... 1-1 Table 1-2. Environmental Qualification Form Reference......................................................................... 1-2 Table 2-1. Installation Materials ............................................................................................................... 2-1 Table 2-2. Antenna Installation ................................................................................................................. 2-7 Table 2-3. Ground Plane Requirements .................................................................................................... 2-8 Table 2-4. Antenna Information.............................................................................................................. 2-10 Table 3-1. Recommended Fastener Torque .............................................................................................. 3-2 Table A-1. Antenna Doubler Design and Installation.............................................................................. A-1 Table C-1. Approved Model List and Reference Figures ........................................................................ C-9 Garmin GPS and XM® Antenna STC Installation Manual Page 1-1 190-01284-00 Rev. B 1 GENERAL DESCRIPTION 1.1 Introduction This manual presents mechanical and electrical installation requirements for installing the Garmin antennas listed in Table 1-1 and the information contained herein is STC approved. 1.2 Scope This installation manual applies to the installation of antennas identified in the following table. This STC installation manual does not include antenna product information. Refer to the antenna specific installation manual in Table 1-1. Table 1-1. Antenna Models Model Garmin Part Number Aero Antenna Part Number Color Description Footprint Mount Style Ref Figure Installation Manual Part Number GA 35 013-00235-00 AT575-93GW-TNCF-000-RG-27-NM White GPS/WAAS Tear Drop Figure 2-1 190-00848-00 013-00235-01 AT575-93GB-TNCF-000-RG-27-NM Black 013-00235-02 AT575-93GO-TNCF-000-RG-27-NM Olive Green GA 36 013-00244-00 AT575-126GW-TNCF-000-RG-27-NM White GPS/WAAS ARINC 743 Figure 2-2 190-00848-00 013-00244-01 AT575-126GB-TNCF-000-RG-27-NM Black 013-00244-02 AT575-126GO-TNCF-000-RG-27-NM Olive Green GA 37 013-00245-00 AT2300-126GW-TNCF-000-RG-27-NM White GPS/WAAS + XM Antenna ARINC 743 Figure 2-2 190-00848-00 013-00245-01 AT2300-126GB-TNCF-000-RG-27-NM Black 013-00245-02 AT2300-126GO-TNCF-000-RG-27-NM Olive Green In the event of a discrepancy between the information provided in this manual and the installation manuals listed in Table 1-1, the information contained within this document shall take precedence. Instructions for antenna installation in aircraft with pressurized cabin are limited to Hawker Beechcraft 90 and 200 Series. Antenna installation in pressurized aircraft other than Beechcraft models listed may require additional manufacturer’s data and FAA approval. Structural aspects of antenna installation in composite or fabric aircraft are beyond the scope of the instructions in this installation manual. Additional manufacturer’s data may be necessary and FAA approval may be required to cover the installation of the antenna in composite or fabric aircraft. Refer to Section 4, Limitations, for additional limitation information. It is possible for installers to seek evaluation and approval of an alternate installation by means of the field approval process. This manual and all the data contained within may be used by the installer in pursuit of a field approval. 1.3 Technical Specifications Refer to the specific antenna installation manual listed in Table 1-1 for antenna technical specifications. Page 1-2 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 1.4 Environmental Specifications It is the responsibility of the installing agency to obtain the latest revision of the antenna Environmental Qualification Form. This form is available directly from Garmin. Refer to Table 1-2 for the Environmental Qualification Form Part Number for the antenna models covered in this manual. Table 1-2. Environmental Qualification Form Reference Model Environmental Qualification Form Part Number GA 35 Aero Antenna: TSO575-126G GA 36 Aero Antenna: TSO575-126G GA 37 Aero Antenna: TSO2300-126 To obtain a copy of this form, see the dealer/OEM manuals portion of the Garmin web site (www.garmin.com). 1.5 Regulatory Compliance The antennas covered by this installation manual are TSO approved. Refer to the antenna specific installation manual listed in Table 1-1 for more details. Garmin GPS and XM® Antenna STC Installation Manual Page 2-1 190-01284-00 Rev. B 2 INSTALLATION OVERVIEW 2.1 Introduction This section provides equipment and hardware information for installing the desired antenna. Installation of any antenna should follow the aircraft TC or STC requirements. For technical information on a specific antenna, refer to the respective publication as listed in Table 1-1. 2.2 Pre-Installation Information Always follow acceptable avionics installation practices per FAA Advisory Circulars (AC) 43.13-1B, 43.13-2A, or later FAA approved revisions of these documents. Follow the installation procedure in this section as it is presented for a successful installation. Read the entire section before beginning the procedure. Prior to installation, consider the structural integrity of the antenna installation as defined in AC 43.13-2B, Chapter 1 and 3. 2.3 Installation Materials The antenna is provided with a kit of parts and may vary depending on the model of antenna being installed. Refer to the antenna installation manual Table 1-1 for the specific materials that are supplied with the antenna. Table 2-1 lists the materials that are required for installation. Table 2-1. Installation Materials Antenna Model GA 35 GA 36 GA 37 Reference Antenna Figure Figure 2-1 Figure 2-2 Figure 2-2 Through Mount Teardrop Footprint Antenna X X ARINC 743 Footprint Antenna X X Materials Required Garmin PN Alternate Description 115-00846-00 [1] Doubler Plate 1 1 115-00846-10 [1] Doubler Plate 1 115-00873-00 [2] Doubler Plate 1 1 210-10004-09 AN365C832 Nut, Self-locking .1640-32UNJC-3B 4 MS21044C08 N/A MX20426AD4-( ) [3] Rivet, Solid X [4] X [4] X [4] 211-60212-20 MS51958-67 Screw, Machine .1900-32 UNF-2Ax1” N/A MX24693-C276 Screw, Machine .1900-32 UNF-2Ax1” 4 4 N/A MS28775-116 O-ring, Nitrile 1 Size 2-121 O-ring, Nitrile 26.64mm IDx2.62mm W N/A MS28775-142 O-ring, Nitrile 1 1 253-00002-00 N/A Gasket, Neoprene 253-00138-00 N/A Gasket, Neoprene Notes: [1] Doubler plate may be fabricated per drawings in Appendix A [2] Doubler plate may be fabricated per drawings in Appendix B [3] Length determined at installation [4] Quantity determined at installation Page 2-2 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 Figure 2-1. Through Mount Teardrop Footprint Antenna Figure 2-2. Garmin ARINC 743 Footprint Antenna Garmin GPS and XM® Antenna STC Installation Manual Page 2-3 190-01284-00 Rev. B 2.4 Antenna Installation Considerations NOTE Although the signal coax cable is not installed under this STC, when choosing a location for the antenna, you should consider the coax routing distance from the existing or planned location of the receiver to the proposed antenna location. The receiver installation manual should include information you can use to check whether the planned coax routing distance will support intended receiver signal gain and loss requirements. The following sub-sections include requirements for this STC installation. 2.4.1 Placement of Antenna for Lightning Protection Antennas must be installed in an aircraft lightning zone that matches their qualifications. The DO-160 Section 23 qualifications of the antennas support installation in Lightning Zones 1C, 2A or 3. See Section C.1 for the zone applicable to each antenna. This typically places the antenna at least 51.2 inches (1.3 meters) aft of the aircraft nose. The exact distances are provided by the lightning zones identified in Appendix C. Antennas shall not be installed in fuel bay areas where the fasteners or antenna stud penetrate the wet or dry fuel bay. 2.4.2 GA 35 and GA 36 GPS/WAAS Antennas The GPS antenna is a key element in the overall system performance and integrity for a GPS/WAAS navigation system. The mounting location, geometry, and surroundings of the antenna can affect the system performance and/or availability. The following guidance provides information to aid the installer in ensuring that the most optimum location is selected for the installation of the GPS antenna. The installation guidelines presented here meet the intent of AC 20-138A section 16. The greater the variance from these guidelines, the greater the chance of decreased antenna performance. Approach procedures with vertical guidance are the most sensitive to these effects. LNAV only approaches, terminal operations, and enroute operations may also be affected. Because meeting all of these installations guidelines may not be possible on all aircraft, these guidelines are listed in order of importance to achieve optimum performance. Items 3a, 3b, and 3c below are of equal importance and their significance may depend on the aircraft installation. The installer should use their best judgment to balance the installation guidelines. 1. Mount the antenna as close to level as possible with respect to the normal cruise flight attitude of the aircraft. If the normal flight attitude is not known, substitute with the waterline, which is typically referenced as level while performing a weight and balance check. 2. The GPS antenna should be mounted in a location to minimize the effects of airframe shadowing during typical maneuvers. Typically mounting farther away from the tail section reduces signal blockage seen by the GPS antenna. 3a. The GPS antenna should be mounted no closer than two feet from any VHF COM antenna or any other antenna which may emit harmonic interference at the L1 frequency of 1575.42 MHz. An aircraft EMC check (reference VHF COM interference check in Post Installation Checkout procedures for the GPS receiver installation) can verify the degradation of GPS in the presence of interference signals. If an EMC check reveals unacceptable interference, insert a GPS notch filter in line with the offending VHF COM or the (re-radiating) ELT transmitter. NOTE This check can only be performed if a GPS receiver exists on the aircraft or one is being installed, GPS receiver installation is not covered by this STC. Page 2-4 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 NOTE When mounting a combination antenna, the recommended distance of two feet or more is not applicable to the distance between the antenna elements in a combination antenna (ex. GPS and XM) provided the combination antenna is TSO authorized and has been tested to meet Garmin’s minimum performance standards. 3b. The GPS antenna should be mounted no closer than two feet from any antennas emitting more than 25 watts of power. An aircraft EMC check can verify the degradation of GPS in the presence of interference signals. 3c. To achieve the best possible low-elevation antenna gain (by minimizing pattern degradation due to shadowing and near-field interaction), the GPS antenna shall be mounted with clearance from other antennas, including passive antennas such as another GPS antenna or XM antenna. When practical, installers shall use 12 inch center-to-center spacing between antennas. If 12 inch spacing is not practical, installers shall use the maximum center-to-center spacing from adjacent antennas, but never less than 9 inch center-to-center spacing. Spacing less than 9 inches center- to-center results in unacceptable GPS/WAAS antenna pattern degradation. 4. To limit degradation by windscreen effects, avoid mounting the antenna closer than 3 inches from the windscreen. Also see Section 2.6.1 for ground plane effect on antenna gain pattern. NOTE Antennas on certain airplanes with a maximum speed over 250 KIAS must install the antennas at least 24 inches aft of the windscreen, unless another location has been certified. See Section C.7 for affected models. 5. For multiple GPS installations, the antennas should not be mounted in a straight line from the front to the rear of the fuselage. Also varying the mounting location will help minimize any aircraft shading by the wings or tail section (in a particular azimuth, when one antenna is blocked the other antenna may have a clear view). Figure 2-3 shows the recommended placement of antennas. Garmin GPS and XM® Antenna STC Installation Manual Page 2-5 190-01284-00 Rev. B Figure 2-3. Antenna Installation Location Page 2-6 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 2.4.3 XM® Antennas The XM antenna must be mounted on top of the aircraft for greatest satellite visibility. For best performance, select a location with an unobstructed view of the sky above the aircraft when in level flight (see Figure 2-3). Location of communication antennas too close to the XM antenna may not only degrade the transmission through reflection, but can also absorb and re-radiate the transmission causing a condition similar to having two COM antennas located in close proximity to each other. The antenna should be mounted (edge to edge) no closer than 1.25 inches from any passive (receive only) antenna such as a GPS or another XM antenna, five inches from a VHF active antenna such as VHF Comm. transmitting antennas or ACARS, five inches from an active radar altimeter (4 GHz), and 12 inches from a UHF/Microwave transmitting antennas such as a transponder, DME, active TCAS, UAT, SATCOM, or Flitephone. Maintain about three feet from heater, ignition, autopilot, and other control surface actuators and motors. Maintain about five feet from fluorescent lamps, related ballast, air conditioners, blowers, strobe lights and power supplies. Follow installation spacing guidelines from other nearby antennas. 2.4.4 GA 37 Combination GPS/WAAS and XM® Antenna For the GA 37 combination GPS and XM antennas, follow mounting location considerations for both GPS/WAAS antennas and for XM Radio Antennas. Garmin GPS and XM® Antenna STC Installation Manual Page 2-7 190-01284-00 Rev. B 2.5 Antenna Installation The specific mounting instructions depend on which antenna model is installed and what type of aircraft the antenna is being installed on. Use Table 2-2 in determining which data to use for installation. Table 2-2. Antenna Installation Antenna Model GA 35 GA 36 GA 37 Antenna Mount Teardrop Footprint ARINC 743 Footprint ARINC 743 Footprint Installation on Non-Pressurized Aircraft with Metallic Skin Appendix A Appendix A Appendix A Installation on Pressurized Aircraft with Metallic Skin Appendix B Appendix B Appendix B 2.5.1 Non-Pressurized Aircraft Installation This installation manual covers structural installations of the antennas listed in Table 1-1 on metal aircraft with 2024-T3 aluminum skin 0.020 to 0.080 inches thick. Structural installation defined by this STC requires the antenna to be installed using a doubler plate as shown in Appendix A. Aircraft structure must not be weakened as a result of installation of the antenna and doubler. Mounting areas should be selected such that no structural members other than aircraft skin are altered. Refer to the aircraft manufacturer’s specifications and AC 43.13-2B Chapters 1 and 3 for appropriate guidance on structural modifications and antenna installation. Make use of any available reinforcements where appropriate. 2.5.2 Pressurized Aircraft Installation Refer to Appendix B for antenna installation on pressurized aircraft. Antenna installations on metal aircraft models with pressurized cabin other than listed in Appendix B require FAA approved installation design and engineering substantiation data whenever such installation incorporate alteration (penetration) of the cabin pressure vessel by connector holes and/or mounting arrangements. This STC provides data for pressurized aircraft antenna installation only on certain aircraft that are listed in Appendix B. Page 2-8 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 2.6 Antenna Grounding Antenna grounding is required to provide the appropriate antenna performance and safely dissipate any lightning currents from a lightning attachment to the antenna. The antenna performance is also dependent on the size of the ground plane and further guidance is provided below. This metallic ground plane must be electrically bonded, to the rest of the metallic aircraft structure or aircraft ground plane, to safely carry any lightning currents. This STC does not provide data to mount the antenna on composite fairing. The aircraft skin provides the required ground plane in metallic aircraft for antenna performance and lightning protection. 2.6.1 Ground Plane For optimum antenna performance, a metallic ground plane or skin sized at least 7.5 inches beyond the perimeter of the antenna is required. Table 2-3 lists the ground plane perimeter required for each antenna. If ground plane is added to the aircraft, round its edges to be as circular as practical for best performance. Table 2-3. Ground Plane Requirements Antenna Model GA 35 GA 36 GA 37 Ground Plane Extend Beyond Antenna Perimeter (inches) 7.5 7.5 7.5 2.6.2 Bonding Requirements Antennas, ground planes, and supporting brackets must be electrically bonded to the aircraft’s main structure. The aircraft ground plane must be electrically bonded to the antenna baseplate. Refer to SAE ARP 1870 section 5 when surface preparation is required to achieve electrical bond. The electrical bond must achieve direct current (DC) resistance less than or equal to 2.5 milliohms to structure local to where the equipment is mounted. Compliance should be verified by inspection using a calibrated milliohm meter. An equivalent OEM procedure may also be substituted. Typically it is not necessary to remove paint under the footprint of the antenna on the metal skin of the aircraft to meet the antenna bonding requirements. The painted surface prevents corrosion and should be left intact if possible. If paint needs to be removed for bonding, be careful to avoid excessive chipping or cracking beyond the antenna baseplate, which could become a source for corrosion. The resistance of 2.5 milliohms can usually be achieved through the antenna mounting screws which attach to the antenna doubler. To verify that the bonding requirements have been met, perform the following steps: 1. Disconnect coaxial cable(s) from the antenna connector(s). 2. Measure the resistance between the antenna connector (TNC external ground) and a nearby exposed portion of conductive aircraft structure (example: Measure the resistance between the antenna connector body and nearby exposed rivet on fuselage stringer). 3. Verify the resistance is equal to or less than 2.5 milliohms. 2.7 Coax Cable Installation Installation of the coax cable is beyond the scope of this STC. Refer to the interfaced receiving equipment for installation instructions, selection of coax cable, and signal loss requirements that may affect antenna placement. To support protection of the GPS antenna from the indirect effects of lightning, the cable routing must be within the fuselage and must not be routed behind an exterior composite structure. Garmin GPS and XM® Antenna STC Installation Manual Page 2-9 190-01284-00 Rev. B 2.8 Weight and Balance Weight and balance computation is required after the installation of the antenna. Follow the guidelines as established in AC 43.13-1B, Chapter 10 Section 2. Make appropriate entries in the equipment list indicating items added, removed, or relocated along with the date accomplished. Include your name and certificate number in the aircraft records. Table 2-4 lists the specific antenna, doubler, and installation kit weights, as well as cross reference to figures displaying antenna dimensions and CG information. Page 2-10 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 Table 2-4. Antenna Information Antenna Model GA 35 GA 36 GA 37 Mount Style Through Through Through Antenna Weight 0.47 lbs 0.47 lbs 0.50 lbs (0.23 kg) (0.21 kg) (0.21 kg) Doubler Weight 0.09 lbs 0.17 lbs 0.17 lbs (0.08 kg) (0.04 kg) (0.08 kg) Dimensions and CG Information Figure 2-4 Figure 2-5 Figure 2-6 TNC CONNECTOR 0.81 [20.6] 0.81 [20.6] 1.62 [41.3] 0.65 [16.5] 1.75 [44.4] 4.68 [118.9] 1.00 [25.4] 1.90 [48.3] 3.00 [76.2] R0.40 [R10.2] TYP CENTER OF GRAVITY 0.26 [6.6] 2.60 [66.0] Figure 2-4. GA 35 Antenna Dimensions Garmin GPS and XM® Antenna STC Installation Manual Page 2-11 190-01284-00 Rev. B R1.00 [R25.4] 4X Ø0.22 THRU C'SINK Ø.385-100°±.50° 1.60 [40.6] 0.70 [17.8] 3.00 [76.2] 3.30 [83.8] 0.70 [17.8] 4.70 [119.4] DO NOT PAINT 0.65 [16.5] 0.37 [9.3] 0.73 [18.6] CENTER OF GRAVITY TNC FEMALE CONNECTOR FORWARD R0.38 0.00 [0.0] 0.61 [15.5] 1.65 [41.9] 2.35 [59.7] 1.65 [41.9] 2.35 [59.7] 0.00 [0.0] 0.80 [20.3] 1.50 [38.1] 0.80 [20.3] 1.50 [38.1] 2X R2.35 [R59.7] NOTES: 1. DIMENSIONS IN INCHES [MM]. Figure 2-5. GA 36 Antenna Dimensions Page 2-12 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 R1.00 [R25.4] 4X Ø0.22 THRU 1.60 [40.6] 3.00 [76.2] 3.30 [83.8] 0.70 [17.8] 4.70 [119.4] DO NOT PAINT 0.65 [16.5] 0.37 [9.3] 0.73 [18.6] CENTER OF GRAVITY GPS TNC FEMALE CONNECTOR [BLUE] 2X R2.35 [R59.7] FORWARD R0.38 0.00 [0.0] 0.61 [15.5] 1.65 [41.9] 2.35 [59.7] 1.65 [41.9] 2.35 [59.7] 0.00 [0.0] 0.80 [20.3] 1.50 [38.1] 0.80 [20.3] 1.50 [38.1] NOTES: 1. DIMENSIONS IN INCHES [MM]. 0.70 [17.8] GPS XM XM TNC FEMALE CONNECTOR [YELLOW] Figure 2-6. GA 37 Antenna Dimensions Garmin GPS and XM® Antenna STC Installation Manual Page 3-1 190-01284-00 Rev. B 3 INSTALLATION PROCEDURE 3.1 Non-Pressurized Aircraft Refer to Appendix A for antenna installation details. 3.1.1 Metallic Aircraft 3.1.1.1 Antenna Doubler 1. Use Garmin P/N 115-00846-10 for teardrop footprint antenna installation, or Garmin P/N 115-00846-00 for ARINC 743 footprint antenna installation. Refer to Appendix A for information on selecting the appropriate doubler design based on the aircraft skin thickness at the antenna location. 2. Make the doubler from 2024-T3 aluminum (AMS-QQ-A-250/5), 0.063 inch sheet thickness. 3. For doubler installation with MS20426AD4-X rivets, countersink the rivet holes if aircraft skin thickness is 0.020 to 0.050 inches. For doubler installation with NAS1097AD4-X flush head rivets, countersink the rivet holes if aircraft skin thickness is 0.020 to 0.031 inches. 4. Sixteen rivet holes exist in the part when using Garmin P/N 115-00846-10 doubler for teardrop footprint antenna installation, or Garmin P/N 115-00846-00 doubler for ARINC 743 footprint antenna installation. 5. For installation of Garmin P/Ns 115-00846-00 and 115-00846-10 in aircraft skins between 0.020 and 0.035 inches thick, only 12 rivets are required as identified in doubler design detail (Figure A-1 and Figure A-2) and in the skin cutout detail (Figure A-3 and Figure A-4). 6. For installation of Garmin P/Ns 115-00846-00 and 115-00846-10 in aircraft skins between 0.063 and 0.080 inches thick, 4 additional fastener holes have to be drilled since 20 rivets are required as identified in doubler design detail (Figure A-1 and Figure A-2) and in the skin cutout detail (Figure A-3 and Figure A-4). 3.1.1.2 Antenna Installation 1. Refer to Appendix A for guidance on selecting the appropriate antenna mounting cutout. 2. Drill or punch the holes in aircraft skin to match the doubler. 3. Install a doubler plate to reinforce the aircraft skin, as required. Refer to Section 3.1.1.1 for doubler preparation. Refer to Appendix A for additional guidance on the doubler installation for teardrop and ARINC 743 footprint antennas. 4. Dimple the aircraft skin for doubler installation with MS20426AD4-X rivets when skin thickness is 0.020 to 0.050 inches. For doubler installation with NAS1097AD4-X flush head rivets, dimple the aircraft skin when skin thickness is 0.020 to 0.031 inches. 5. Countersink the aircraft skin for doubler installation with MS20426AD4-X rivets when skin thickness is 0.051 to 0.080 inches. For doubler installation with NAS1097AD4-X flush head rivets countersink the aircraft skin when skin thickness is 0.032 to 0.050 inches. 6. For the GA 35 through mount teardrop footprint antenna, secure O-ring in the O-ring groove on the underside of the antenna. 7. For the GA 36 and GA 37 ARINC 743 footprint antennas, secure the O-ring in the O-ring groove on the underside of the antenna. 8. MS21044C08 self-locking nuts (No. 8, supplied) and NAS1149FN832P washers are required to secure GA 35 teardrop footprint antenna. Page 3-2 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 9. MS24693-C276 stainless steel countersunk head machine screws (No. 10, supplied) are required to secure GA 36 and GA 37 ARINC 743 footprint antennas. MS21047L3 low height self-locking nutplates are installed on ARINC 743 footprint antenna doubler. 10. Torque antenna fasteners per Table 3-1. Torque should be applied evenly across all fasteners to avoid deformation of the mounting area. Table 3-1. Recommended Fastener Torque Fastener Size No. 8 0.1640-36UNF-2A No. 10 1900-32UNF-2A Recommended Torque 12 to 15 in-lbs 15 to 20 in-lbs 11. Ensure that the antenna base and aircraft skin are in continuous contact with the gasket or O-ring, as appropriate to the antenna model. Verify electrical bonding of the antenna by inspection using a calibrated milliohm meter. Any metallic part of the antenna or it’s fasteners may be used to verify the electrical bond to the doubler. See Section 2.6.2 for final bonding check requirements. 12. Seal the antenna and gasket by running a bead of the MIL-A-46146 Non-Corrosive RTV Silicone Adhesive-Sealant along the edge of the antenna where it meets the exterior aircraft skin. Use caution to insure that the antenna connectors are not contaminated with sealant. CAUTION Do not use construction grade RTV sealant or sealants containing acetic acid. These sealants may damage the electrical connections to the antenna. Use of these type sealants will void the antenna warranty. Garmin GPS and XM® Antenna STC Installation Manual Page 3-3 190-01284-00 Rev. B 3.2 Pressurized Aircraft Refer to Appendix B for antenna installation details 3.2.1 King Air 90 and 200 Series model aircraft. 3.2.1.1 Antenna Doubler 1. Use Garmin P/N 115-00873-00 doubler for GA 36 and GA 37 ARINC 743 footprint antenna installation. 2. Alternatively, fabricate the doubler from 2024-T3 aluminum (AMS-QQ-A-250/5), 0.050 inch sheet. Refer to Figure B-2 for information on doubler design. Countersink rivet holes and install NAS1473A3 capped, self-locking nutplates in the doubler with MS20426AD3-3 solid rivets. Prime antenna doubler with MIL-PRF-23377 High Solids Epoxy Primer (preferred), or TT-P-1757 Alkyd Base One Component Primer (optional). 3.2.1.2 Antenna Installation 1. Determine antenna location on top of the fuselage. Refer to Figure B-1 and Figure B-3 for antenna location and fuselage skin cutout details. 2. If needed to meet bonding requirements, remove paint and primer from the fuselage skin underneath the antenna footprint and prepare skin surface for electrical bonding per SAE ARP1870 Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety, Section 5. Antennas have to be electrically bonded meeting requirements defined in Section 2.6.2 3. Drill or punch the holes in aircraft skin to match the doubler. Countersink aircraft skin for doubler installation with NAS1097AD4-5 flush head rivets. 4. Install doubler and rivets wet with MIL-S-8802 High Adhesion Temperature Resistant Sealant. 5. Secure the O-ring in the O-ring groove on the underside of the GA 36 and GA 37 ARINC 743 footprint antennas. 6. MS24693-C276 stainless steel countersunk head machine screws (No. 10, supplied) are required to secure GA 36 and GA 37 ARINC 743 footprint antennas. NAS1473A3 capped, self-locking nutplates are installed on ARINC 743 footprint antenna doubler. 7. Torque antenna fasteners per Section 20-01-00 of King Air 90 series, or 200 series Maintenance Manual, or per Table 3-1. Torque should be applied evenly across all fasteners to avoid deformation of the mounting area. 8. Ensure that the antenna base and aircraft skin are in continuous contact with the O-ring. Verify electrical bonding of the antenna by inspection using a calibrated milliohm meter. Any metallic part of the antenna or its fasteners may be used to verify the electrical bond to the doubler. See Section 2.6.2 for final bonding check requirements. 9. Seal the antenna and gasket by running a bead of the MIL-A-46146 Non-Corrosive RTV Silicone Adhesive-Sealant along the edge of the antenna where it meets the exterior aircraft skin to the fuselage using. Use caution to insure that the antenna connectors are not contaminated with sealant. 3.3 Instructions for Continued Airworthiness (ICAW) Ensure that the appropriate aircraft information is filled in on the ICAW is completed and inserted in the aircraft permanent records. 1. Fill in the Aircraft Make, Model, Registration Number, S/N, and antenna location(s) information on the cover of the ICAW (Garmin document 005-00638-09). 2. Insert the completed ICAW in the aircraft permanent records. Page 3-4 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 This page intentionally left blank Garmin GPS and XM® Antenna STC Installation Manual Page 4-1 190-01284-00 Rev. B 4 LIMITATIONS Installation of the antenna identified in Section 2 of this document into an aircraft does not alter the operation approvals previously granted to the aircraft. Additional operation approvals may require FAA evaluation of all systems installed in a particular aircraft and is outside the scope of this document. 4.1 Installation The antennas must be installed on top of the fuselage, or within the area in line with the top of the fuselage (for high-wing airplanes or biplanes), unless there is another otherwise acceptable position that is NOT in line with any control surfaces. Antennas shall not be installed in fuel bay areas where the fasteners or antenna stud penetrate the wet or dry fuel bay. Antennas shall not be located and installed directly on airplane windshield, canopy, or window(s) made from transparent materials like Acrylic Plastic Sheet (Methacrylate) as these materials do not facilitate required antenna grounding and are not suitable for mechanical installation involving fastener penetration. Except for pressurized aircraft models listed in Appendix B of this document, penetration of the pressure vessel of pressurized aircraft is not approved under the STC. Further evaluation and/or certification approval is required for penetration of the pressure vessel of pressurized aircraft. Structural aspects of antenna installation in composite or fabric aircraft are beyond the scope of the instructions in this installation manual. Additional manufacturer’s data may be necessary and FAA approval may be required to cover the installation of the antenna in composite or fabric aircraft. 4.2 Preservation of Previous Systems It is the installer’s responsibility to preserve the essential characteristic of the aircraft being modified by this manual to be in accordance with the aircraft manufacturer’s original design. Page 4-2 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 This page intentionally left blank Garmin GPS and XM® Antenna STC Installation Manual Page A-1 190-01284-00 Rev. B Appendix A NON-PRESSURIZED AIRCRAFT ANTENNA INSTALLATION A.1 Metallic Skin Aircraft This appendix describes the structural aspects of antenna installation in metallic skin aircraft. One acceptable method is to use Garmin P/N 115-00846-10 doubler plate for the teardrop footprint antenna or Garmin P/N 115-00846-00 doubler plate for the ARINC 743 footprint antenna. Another acceptable method is to fabricate a doubler. Teardrop footprint antenna doubler is shown in Figure A-1. and ARINC 743 footprint antenna doubler is shown in Figure A-2. Doubler design, including number of rivets and fastener hole preparation, varies depending on the thickness of the skin and choice of rivet. Table A-1 provides a summary of design and installation details for the antenna doubler. Table A-1. Antenna Doubler Design and Installation Aircraft Skin Thickness Type of Rivet [1] - NAS1097AD4-X Rivet, Solid, Flush Shear Head 100° Number of Rivets Hole Size Doubler Preparation Skin Preparation 0.020 to 0.031 inch 12 Ø0.129 inch Countersink Ø0.225×100° Dimple 0.032 to 0.035 inch 12 Ø0.129 inch None Countersink Ø0.189×100° 0.036 to 0.050 inch 16 Ø0.129 inch None Countersink Ø0.189×100° Aircraft Skin Thickness Type of Rivet [1] – MS20426AD4-X Rivet, Solid, Countersunk 100° Number of Rivets Hole Size Doubler Preparation Skin Preparation 0.020 to 0.035 inch 12 Ø0.129 inch Countersink Ø0.225×100° Dimple 0.036 to 0.050 inch 16 Ø0.129 inch Countersink Ø0.225×100° Dimple 0.051 to 0.062 inch 16 Ø0.129 inch None Countersink Ø0.225×100° 0.063 to 0.080 inch 20 Ø0.129 inch None Countersink Ø0.225×100° Design References Doubler Holes and Cutouts in Aircraft Skin Doubler Installation Antenna Installation Figure Number Figure A-1 Figure A-2 Figure A-3 Figure A-4 Figure A-5 Figure A-6 Figure A-7 [2] Figure A-8 Figure A-9 [3] Notes: [1] Rivet length determined at installation, dependent on thickness of material (rivet length = grip length + 1.5*rivet diameter) [2] Doubler installation figure show skin cutouts for GA 37 antenna as an example; use only the skin cutouts required for the antenna being installed. [3] For installations shown in Figure A-8 surface under the washer shall be prepared for electrical bond, see also section 2.6.2. Page A-2 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 Figure A-3 shows the details of aircraft skin cutout required for teardrop footprint antenna installation and Figure A-4 shows the details of aircraft skin cutout required for ARINC 743 antenna installation. Note the number of doubler fastener holes varying with aircraft skin thickness. Figure A-6 and Figure A-7 show installation of the doubler on aircraft skin. Figure A-5 shows an example of the doubler location between stringers on the top fuselage skin, just off centerline. The location should be flat, with no gaps between the skin and doubler, to keep from deforming the skin during installation. Figure A-8 shows installation of the through mount teardrop footprint antenna (GA 35). Figure A-9 shows installation of the ARINC 743 footprint antenna with O-ring (GA 36 and GA 37). Garmin GPS and XM® Antenna STC Installation Manual Page A-3 190-01284-00 Rev. B (0.063 [1.60]) NOTES: 1. DIMENSIONS: INCHES. 2. MATERIAL: 0.063" THICKNESS 2024-T3 ALUMINUM (AMS-QQ-A-250/5). 3. TOLERANCE: .XX +/- 0.030", .XXX +/- 0.010". 4. THESE HOLES CAN BE OMITTED IF REQUIRED NUMBER OF FASTENERS IS LESS THAN 16. 5. THESE HOLES HAVE TO BE ADDED IF REQUIRED NUMBER OF FASTENERS IS GREATER THAN 16 6. REMOVE BURRS AND BREAK SHARP EDGES. FORWARD 2X 0.75 [19.1] 2X 1.00 [25.4] 4X 1.95 [49.5] 2X 1.07 [27.2] 2X 0.19 [4.8] 6X 1.20 [30.5] 2X 0.40 [10.2] 2X 0.40 [10.2] 6X 1.20 [30.5] 1.50 [38.1] 0.00 [0.0] 2X 0.69 [17.5] 2X 1.57 [39.9] 4X 2.45 [62.2] 2X 0.81 [20.6] 2X 0.81 [20.6] 0.00 [0.0] 2X 2.25 [57.2] ØA Ø0.625 4X R0.25 4X Ø0.188 4 4 5 5 5 5 Ø0.129 0.020 TO 0.031 INCH 0.032 TO 0.035 INCH ØA MS20426AD4-XX NUMBER Ø0.225 100° 12 20 AIRCRAFT SKIN THICKNESSES FASTENER HOLE SPECIFICATION 16 NAS1097AD4-X COUNTERSINK NONE 0.036 TO 0.050 INCH 0.051 TO 0.062 INCH 0.063 TO 0.080 INCH Ø0.225 100° NONE 1.50 [38.1] 2X 2.75 [69.9] Figure A-1. Doubler Design, Teardrop Footprint Antenna Page A-4 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 FORWARD (0.063 [1.60]) MS21047L3 NUTPLATE (4X) MS20426AD3-4 RIVET (8X) 4X 4.130 [104.9] 4X 0.770 [19.6] 1.070 [27.2] 2.350 [59.7] 1.000 [25.4] 6X 1.450 [36.8] 2X 0.000 [0.0] 6X 1.450 [36.8] 1.750 [44.5] 2X 3.300 [83.8] 2X 2.690 [68.3] 2X 0.670 [17.0] 2X 0.000 [0.0] 4X Ø0.203 2X Ø0.625 A 4X R0.25 2X 0.050 [1.3] 2X 3.410 [86.6] 2X 0.800 [20.3] 2X 0.485 [12.3] 2X 0.485 [12.3] 2X 0.800 [20.3] ØA 9 NOTES: 1. DIMENSIONS: INCHES [MM] 2. MATERIAL: 0.063" THICKNESS 2024-T3 ALUMINUM (AMS-QQ-A-250/5) 3. TOLERANCE: .XX ±0.030", .XXX ±0.010" 4. REMOVE BURRS AND BREAK SHARP EDGES 5. RESERVED. 6. HOLE OPTIONAL, GA 36 ANTENNA INSTALLATION. 7. THESE HOLES CAN BE OMITTED IF REQUIRED NUMBER OF FASTENERS IS LESS THAN 16. 8. THESE HOLES HAVE TO BE ADDED IF REQUIRED NUMBER OF FASTENERS IS GREATER THAN 16. 9. MS21059L3 MAY BE USED IN PLACE OF MS21047L3. 0.688 [17.48] 0.344 [8.74] Ø0.203 2X Ø.098 THRU CS'K Ø0.172 X 100° DETAIL A (4 PLCS) 1.750 [44.5] 4.430 [112.5] Ø0.129 0.020 TO 0.031 INCH 0.032 TO 0.035 INCH ØA MS20426AD4-XX NUMBER Ø0.225 100° 12 20 AIRCRAFT SKIN THICKNESSES FASTENER HOLE SPECIFICATION 16 NAS1097AD4-X COUNTERSINK NONE 0.036 TO 0.050 INCH 0.051 TO 0.062 INCH 0.063 TO 0.080 INCH Ø0.225 100° NONE 8 8 8 8 7 6 7 Figure A-2. Doubler Design, ARINC 743 Footprint Antenna Garmin GPS and XM® Antenna STC Installation Manual Page A-5 190-01284-00 Rev. B 4.227 [107.4] 2.590 [65.8] Ø0.625 [Ø15.9] THRU SKIN DOUBLER OUTLINE ANTENNA OUTLINE ØA 4X Ø0.188 [Ø4.8] THRU SKIN TO MATCH DOUBLER 2 2 0.000 [0.0] 2x 0.190 [4.8] 2x 1.000 [25.4] 2x 1.070 [27.2] 4X 1.950 [49.5] 2x 0.690 [17.5] 2x 0.750 [19.1] 1.570 [39.9] 2X 1.570 [39.9] 4X 2.450 [62.2] 0.000 [0.0] 2X 0.400 [10.2] 4X 0.813 [20.6] 6X 1.200 [30.5] 2X 0.400 [10.2] 4X 0.813 [20.6] 6X 1.200 [30.5] NOTES: 1. DIMENSIONS: INCHES [MM] 2. THESE HOLES CAN BE OMITTED IF REQUIRED NUMBER OF FASTENERS IS LESS THAN 16. 3. THESE HOLES HAVE TO BE ADDED IF REQUIRED NUMBER OF FASTENERS IS GREATER THAN 16. Ø0.129 0.020 TO 0.031 INCH 0.032 TO 0.035 INCH ØA MS20426AD4-XX NUMBER DIMPLE 12 20 AIRCRAFT SKIN THICKNESSES FASTENER HOLE SPECIFICATION IN AIRCRAFT SKIN DIMPLE COUNTERSINK Ø0.189 100° 16 NAS1097AD4-X RIVET TYPE FORWARD 0.036 TO 0.050 INCH 0.051 TO 0.062 INCH 0.063 TO 0.080 INCH COUNTERSINK Ø0.225 100° 3 3 3 3 Figure A-3. Skin Cutout Detail, Teardrop Footprint Antenna Page A-6 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 FORWARD 4.70 [119.4] 2.90 [73.7] Ø0.625 [Ø15.9] THRU SKIN DOUBLER OUTLINE ANTENNA OUTLINE ØA TO MATCH DOUBLER 2 2 2x 0.670 [17.0] 2x 0.000 [0.0] 2x 0.050 [1.3] 4X 0.770 [19.6] 2.350 [59.7] 2x 2.690 [68.3] 3.300 [83.8] 2X 3.410 [86.6] 4X 4.130 [104.9] 0.000 [0.0] 2X 0.490 [12.4] 2X 0.800 [20.3] 6X 1.450 [36.8] 2X 0.480 [12.2] 2X 0.800 [20.3] 6X 1.450 [36.8] 4X Ø0.213 [Ø5.4] THRU SKIN TO MATCH DOUBLER NOTES: 1. DIMENSIONS: INCHES [MM] 2. THESE HOLES CAN BE OMITTED IF REQUIRED NUMBER OF FASTENERS IS LESS THAN 16. 3. THESE HOLES HAVE TO BE ADDED IF REQUIRED NUMBER OF FASTENERS IS GREATER THAN 16 4. HOLE CENTER FOR GA 37 ARINC 743 STYLE ANTENNA. 5. HOLE CENTER FOR GA 36 AND GA 37 ARINC 743 STYLE ANTENNA. 4 Ø0.625 [Ø15.9] THRU SKIN 1.040 [26.4] 5 Ø0.129 0.020 TO 0.031 INCH 0.032 TO 0.035 INCH ØA MS20426AD4-XX NUMBER DIMPLE 12 20 AIRCRAFT SKIN THICKNESSES FASTENER HOLE SPECIFICATION IN AIRCRAFT SKIN 16 NAS1097AD4-X RIVET TYPE 0.036 TO 0.050 INCH 0.051 TO 0.062 INCH 0.063 TO 0.080 INCH COUNTERSINK Ø0.225 100° DIMPLE COUNTERSINK Ø0.189 100° 3 3 3 3 Figure A-4. Skin Cutout Detail, ARINC 743 Footprint Garmin GPS and XM® Antenna STC Installation Manual Page A-7 190-01284-00 Rev. B FORWARD BULKHEAD STRINGER STRINGER DOUBLER AIRCRAFT C VIEW LOOKING DOWN SKIN OMITTED FOR CLARITY L Figure A-5. Sample Doubler Location Page A-8 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 FORWARD NOTES: 1. RIVET SELECTION (LENGTH) AND INSTALLATION DETERMINED USING THE GUIDANCE FOUND IN AC43.13-1B. 2. THESE RIVETS CAN BE OMITTED IF REQUIRED NUMBER OF FASTENERS IS LESS THAN 16. DOUBLER RIVETS SEE TABLE FOR REQUIRED TYPE AND NUMBER AIRCRAFT SKIN 2 0.020 TO 0.031 INCH 0.032 TO 0.035 INCH MS20426AD4-XX DOUBLER FASTENER REQUIREMENTS RIVET TYPE NUMBER 12 20 AIRCRAFT SKIN THICKNESSES 16 0.036 TO 0.050 INCH 0.051 TO 0.062 INCH 0.063 TO 0.080 INCH NAS1097AD4-X Figure A-6. Doubler Installation, Teardrop Footprint Antenna Garmin GPS and XM® Antenna STC Installation Manual Page A-9 190-01284-00 Rev. B FORWARD NOTES: 1. RIVET SELECTION (LENGTH) AND INSTALLATION DETERMINED USING THE GUIDANCE FOUND IN AC43.13-1B. 2. THESE RIVETS CAN BE OMITTED IF REQUIRED NUMBER OF FASTENERS IS LESS THAN 16. DOUBLER RIVETS SEE TABLE FOR REQUIRED TYPE AND NUMBER AIRCRAFT SKIN 2 0.020 TO 0.031 INCH 0.032 TO 0.035 INCH MS20426AD4-XX NUMBER 12 20 AIRCRAFT SKIN THICKNESSES DOUBLER FASTENER REQUIREMENTS 16 RIVET TYPE 0.036 TO 0.050 INCH 0.051 TO 0.062 INCH 0.063 TO 0.080 INCH NAS1097AD4-X Figure A-7. Doubler Installation, ARINC 743 Footprint Antenna Page A-10 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 AIRCRAFT SKIN WITH DOUBLER INSTALLED THROUGH MOUNT TEARDROP FOOTPRINT ANTENNA 2-121 O-RING 4X #8-32 SELF LOCKING NUT TORQUE 12 TO 15 in-lbs 4X NAS1149FN832P (AN960-8) #8 WASHER #8-32 SCREW, OVAL HEAD, SS FORWARD Figure A-8. Through Mount Teardrop Footprint Antenna Installation AIRCRAFT SKIN WITH DOUBLER INSTALLED ARINC 743 FOOTPRINT ANTENNA MS28775-142 O-RING 4X MS24693-273 SCREW 10-32 1.00[25.4] TORQUE 20 TO 25 IN-LBS FORWARD Figure A-9. GA 37 ARINC 743 Footprint Antenna Installation Garmin GPS and XM® Antenna STC Installation Manual Page B-1 190-01284-00 Rev. B Appendix B PRESSURIZED AIRCRAFT ANTENNA INSTALLATION B.1 Hawker Beechcraft 90 and 200 Series Aircraft This appendix provides details of GA 36 and GA 37 ARINC 743 footprint antenna installation on Hawker Beechcraft B90, C90, C90A, C90GT, 200, 200C, B200, and B200C model airplanes (summarized as “90 and 200 Series” elsewhere in this document). Antenna location is shown in Figure B-1 and Figure B-3. One method is to use Garmin P/N 115-00873-00 doubler. Alternatively, antenna doubler can be fabricated from 2024-T3 aluminum. Refer to Figure B-2 for doubler design details and to Figure B-4 for doubler installation. Antenna installation requires connector and fastener holes in fuselage pressure vessel. Refer to Figure B-3 for details of fuselage skin cutout and fastener hole preparation. Antenna installation is shown in Figure B-4 and Figure B-5. DETAIL A Figure B-1. Hawker Beechcraft 90 and 200 Series Antenna Location Page B-2 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 FORWARD NOTES: 1. DIMENSIONS: INCHES [MM]. 2. TOLERANCE: .XX ±0.030", .XXX ±0.010". 3. MATERIAL: 0.050" THICKNESS 2024-T3 ALUMINUM (AMS-QQ-A-250/5). 4. REMOVE BURRS AND BREAK SHARP EDGES R 0.010 MAX. 5. INSTALL NAS1473A3 NUTPLATEs AS SHOWN USING MS20426AD3-3 RIVETS 6. FINISH: PRIMER AFTER NUTPLATE INSTALLATION. PREFERRED PRIMER SPECIFICATION: MIL-PRF-23377 TYPE 1 CLASS C2. OPTIONAL PRIMER SPECIFICATION: TT-P-1757 TYPE 1, CLASS C, YELLOW 3X 0.000 [0.0] 3X 0.675 [17.1] 3X 1.350 [34.3] 2X 1.650 [41.9] 1.900 [48.3] 4X 2.250 [57.2] 3X 0.675 [17.1] 3X 1.350 [34.3] 2X 1.650 [41.9] 1.900 [48.3] 4X 2.250 [57.2] 7X 0.000 [0.0] 2X 0.400 [10.2] 8X 0.800 [20.3] 5X 1.200 [30.5] 2X 0.400 [10.2] 8X 0.800 [20.3] 5X 1.200 [30.5] 1.450 [36.8] 1.450 [36.8] 2.500 [63.5] 2.500 [63.5] 23X 0.128 [Ø3.3] 2X 0.625 [Ø15.9] 4X 0.125 [R3.2] (0.050 [1.3]) NAS1473A3 NUTPLATE (4X) MS20426AD3-3 RIVET (8X) A DETAIL A 4 PLCS 0.344 [8.7] 0.344 [8.7] Ø0.201 [Ø5.1] 2X 0.098 [Ø2.5] C'SINK Ø0.185x100° Figure B-2. Doubler Design, ARINC 743 Footprint Antenna, Hawker Beechcraft 90 and 200 Series Garmin GPS and XM® Antenna STC Installation Manual Page B-3 190-01284-00 Rev. B AIRCRAFT 4.500 [114.3] 4.500 [114.3] 4.000 [101.6] FORWARD CL FS147.60 Ø0.625 [Ø15.9] 4X 0.201 [Ø5.1] 23X Ø0.128 [Ø3.3] CSK Ø0.182x100° 1.600 [40.6] 3.300 [83.8] Ø0.625 [Ø15.9] BULKHEAD FS 148.0 REF. FS158.0 BULKHEAD FS 158.0 REF. STIFFENER, RADIO ANTENNA RH REF. STIFFENER, RADIO ANTENNA LH REF. FUSELAGE SKIN REF. 23X Ø0.128 [Ø3.3] CSK Ø0.182x100° 4X 0.201 [Ø5.1] 2X 0.625 [Ø15.9] 3.300 [83.8] 1.600 [40.6] ANTENNA DOUBLER REF. ANTENNA DOUBLER REF. NOTES: 1. DIMENSIONS: INCHES [MM]. 2. TOLERANCE: .XX ±0.030", .XXX ±0.010". 3. MATCH DRILL RIVET HOLES TO ANTENNA DOUBLER. 4. HOLE IS OPTIONAL FOR GA 36 ANTENNA INSTALLATION. 0.800 [20.3] 0.975 [24.8] 0.975 [24.8] 0.800 [20.3] DETAIL A LOOKING DOWN 4 3 3 Figure B-3. Hawker Beechcraft 90 and 200 Series Fuselage Skin Cutout Detail Page B-4 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 FUSELAGE SKIN REF. BULKHEAD FS 148.0 REF. BULKHEAD FS 158.0 REF. ANTENNA DOUBLER REF. FORWARD MS28775-142 ORING REF. (SUPPLIED WITH ANTENNA) 4X MS24693-C276 SCREW, MACHINE, FLAT, COUNTERSUNK HEAD .1900-32UNF-2A, 1.00 IN LONG TORQUE 15 TO 20 IN-LB. GA36 GPS/WAAS ANTENNA (GARMIN P/N 013-00244-00), OR GA37 GPS/WAAS + XM ANTENNA (GARMIN P/N 013-00245-00) AIRCRAFT CL 23X NAS1097AD4-5 RIVET, SOLID, 100 DEG, FLUSH SHEAR HEAD NOTES: 1. INSTALL WET WITH SEALANT, MIL-S-8802B OR EQUIVALENT. 2. UNLESS OTHERWISE NOTED, TORQUE ALL FASTENERS PER THE KING AIR 90/200/B200 SERIES MAINTENANCE MANUAL, SECTION 20-01-00. 3. ANTENNAS SHALL BE ELECTRICALLY BONDED. REMOVE PAINT AND PRIMER UNDER ANTENNA FOOTPRINT. THE SURFACE PREPARATION SHALL BE PER SAE ARP 1870, SECTION 5. 4. THE ELECTRICAL BOND SHALL ACHIEVE A DIRECT CURRENT (DC) RESISTANCE OF 2.5 MILLIOHMS OR LESS BETWEEN THE ANTENNA CONNECTOR AND AIRCRAFT STRUCTURE (WITH THE COAX DISCONNECTED). COMPLIANCE SHALL BE VERIFIED USING A CALIBRATED MILLIOHMMETER. 1 1 3 2 Figure B-4. Hawker Beechcraft 90 and 200 Series GA36 Antenna Installation Garmin GPS and XM® Antenna STC Installation Manual Page B-5 190-01284-00 Rev. B BULKHEAD FS 148.0 REF. BULKHEAD FS 158.0 REF. REF. GA37 GPS/WAAS + XM ANTENNA (GARMIN P/N 013-00245-00) AIRCRAFT CL NOTES: 1. AFTER INSTALLATION, FILLET SEAL AROUND ANTENNA WITH - MIL-S-8802 SEALING COMPOUND, TEMPERATURE–RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION, OR MIL-A-46146 NON-CORROSIVE RTV SILICONE ADHESIVE-SEALANT. REF. GA36 GPS/WAAS ANTENNA (GARMIN P/N 013-00244-00) 1 1 FUSELAGE SKIN REF. FORWARD Figure B-5. Hawker Beechcraft 90 and 200 Series GA36 and GA 37 Antenna Installation Page B-6 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 This page intentionally left blank Garmin GPS and XM® Antenna STC Installation Manual Page C-1 190-01284-00 Rev. B Appendix C LIGHTNING ZONING C.1 Location of Antennas The table below lists the qualified lightning zones for the antennas installed under this STC: Antenna Zone GA 35 1C, 2A, or 3 GA 36 1C, 2A, or 3 GA 37 1C, 2A, or 3 Each antenna must be installed completely within the limits of zones for which it is qualified. For example, an antenna qualified for Zone 1C with the antenna center in Zone 1C but with the antenna body extending into Zone 1B or 1A is not allowed. C.2 Aircraft Zoning Diagrams The following figures show the zoning for several different types of fuselages. Only the fuselage and sometimes the wings are pictured in these diagrams. The antennas in this STC must be mounted only on the upper surface of the fuselage. Which figure to use for each aircraft model included in this STC is identified in Section C.7. Note that after every Zone A, a 5.9 inches (0.15 m) Zone B follows. Although these Zone B areas are marked on the diagrams, sometimes their widths are not defined. Note that although all diagrams show low wing aircraft, the same zoning can be applied to high wing planes. Instead of Zone 2A extending outboard for 19.7 inches (0.50 m), in most places it has been increased to 23.6 inches (0.60 m) to allow for a safety margin. The 23.6 inches should be measured from the outboard-most edge of the fuselage or the tip of the propeller, whichever is longer. The values d1 and d2 are defined as follows: d1 = 51.2 inches (1.3 m) d2 = 102.4 inches (2.6 m) All diagrams use the legend shown in Figure C-1. Zone 1A Zone 1B Zone 1C Zone 2A Zone 2B Zone 3 Figure C-1. Zoning Legend Page C-2 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 C.3 Single Propeller Aircraft Zoning of low or high wing planes with single propellers is shown in Figure C-2. The tip of the nose forward of the propeller, and the propeller itself, are Zone 1A. The area of the nose immediately aft of the propeller is Zone 3. The 23.6 inches (0.60 m) should be measured from the outboard-most edge of the fuselage or the tip of the propeller, whichever is longer. Figure C-2 shows the case where the propeller is longer than the fuselage. Figure C-3 shows the case of an aircraft with a curved fuselage. 45° 45° 0.6m 0.6m d2 d1 NOTE: Shown for propeller wider than fuselage. Figure C-2. Single Prop (Zoning for a Low or High Wing Single Prop) Garmin GPS and XM® Antenna STC Installation Manual Page C-3 190-01284-00 Rev. B TOP (VIEW LOOKING DOWN) 0.6m d1 d2 0.15m 0.6m d1 Figure C-3. Single Rear-Mounted Prop with a Curved Fuselage (Zoning For a Low or High Wing Aircraft with a Curved Fuselage) 0.6m TOP (VIEW LOOKING DOWN) d1 d2 Figure C-4. Single Rear-Mounted Prop Above Fuselage (Zoning for a Low or High Wing Aircraft with a Rear-Mounted Prop Above Fuselage) Page C-4 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 C.4 Aircraft with Two Propellers Zoning of low or high wing planes with twin propellers is shown in Figure C-5. The text below assumes the aircraft fuselage and wing are constructed of metal. If both propellers are in the reverse direction, the fuselage should be zoned as shown in Figure C-6. Note that Zone 2A can overlap onto the nacelles if they are within 23.6 inches (0.60 m) outboard of the fuselage. All but the last 5.9 inches (0.15 m) of the propellers should be Zone 1A. From 5.9 inches (0.15m) inward to the tips of the propellers should be Zone 1B. Figure C-7 shows an aircraft that has both front and rear propellers. LOOKING DOWN) 45° 45° d1 d2 45° 45° d1 d2 0.6m 0.6m 0.5m Figure C-5. Twin Front-Mounted Props (Zoning for a Low or High Wing Twin Prop Aircraft with Front-Mounted Propellers. The distance d1 and d2 are the same on both engines) Garmin GPS and XM® Antenna STC Installation Manual Page C-5 190-01284-00 Rev. B TOP (VIEW LOOKING DOWN) d1 d2 0.15m 0.15m 0.15m 0.15m 0.5m 0.6m 0.5m 0.6m NOTE: Although the engine nacelles are shown as Zone 3. They may be Zone 2A if the engine falls within the Zone 2 area of the wing (within 23.6 inches (0.60 m) outboard from the edge of the fuselage). Figure C-6. Twin Rear-Mounted Props (Zoning for a Low or High Wing Twin Prop Aircraft with Rear-Mounted Propellers) Page C-6 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 45° 45° 0.6m 0.6m TOP (VIEW LOOKING DOWN) d2 d1 NOTE: Nothing can be mounted in the tail booms of the aircraft. Figure C-7. Front and Rear-mounted Props (Zoning for Low or High Wing with a Front and Rear Mounted Propellers) Garmin GPS and XM® Antenna STC Installation Manual Page C-7 190-01284-00 Rev. B C.5 Aircraft with Multiple Jet Engines Zoning of low or high wing twin jet engine aircraft is shown in Figure C-8. TOP (VIEW LOOKING DOWN) d1 d2 0.6m 0.6m Figure C-8. Twin Jet Engines (Zoning for a Low or High Wing Twin Jet Engine Aircraft) Page C-8 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 C.6 Aircraft with Multi-Propellers Zoning of an aircraft with three front-mounted propellers is shown in Figure C-9. d1 d1 d2 45° TOP (VIEW LOOKING DOWN) d1 d2 0.15m 0.5m 45° 45° 0.6m 45° 45° 0.6m 45° d1 d2 d2 d1 d2 Figure C-9. Triple Front-Mounted Props (Wings and Above Fuselage) Garmin GPS and XM® Antenna STC Installation Manual Page C-9 190-01284-00 Rev. B C.7 Figure Identification for Each Aircraft Model The aircraft models included in this STC are listed below in Aircraft Make order. For each model, the applicable lightning zoning diagram is identified. Table C-1 provides model specific installation information and is not the FAA Approved Model List (AML). For the AML, refer to the FAA AML attached to the STC. Table C-1. Approved Model List and Reference Figures Aircraft Make (TCDS Holder) [common name or previous make] Aircraft Model (alias) Type Certificate Number (TCDS) TC Certification Basis Lightning Zoning Figure Notes Aermacchi S.p.A (Aermacchi S.p.A) [Siai Marchetti] S.205-18/F, S.205-18/R, S.205-20/F, S.205-20/R S.205-22/R, S.208, S.208A A9EU FAR 23 Figure C-2 Aermacchi S.p.A (Aermacchi S.p.A) [Siai Marchetti] F.260, F.260B, F.260C, F.260D, F.260E, F.260F A10EU CAR 3 Figure C-2 Aero Commander (Dynac Aerospace Corp) [Aero Commander] [Volaire] (Volaire) 10, (Volaire) 10A (Aero Commander) 100 (Aero Commander) 100A (Aero Commander) 100-180 1A21 CAR 3 Figure C-2 Aerostar (Aerostar Aircraft Corporation) [Piper Aerostar] PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601) A17WE FAR 23 Figure C-5 Atlantic Coast Seaplanes, LLC (Atlantic Coast Seaplanes LLC) [A.G. McKinnon; Viking Air Limited; Aero Planes] G-21C, G-21D, G-21E, G-21G 4A24 CAR 3 Figure C-5 Some WAAS based operations may have limited availability due to poor visibility B-N Group LTD. (B-N Group Ltd.) [Britten-Norman] BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-9, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T, BN-2T-4R A17EU FAR 23 Figure C-5 B-N Group LTD. (B-N Group Limited) [Britten-Norman] BN2A MK. III, BN2A MK. III-2, BN2A MK. III-3 A29EU FAR 23 Figure C-9 Cessna (Cessna Aircraft Company) 120, 140 A-768 CAR 3 Figure C-2 Cessna (Cessna Aircraft Company) 140A 5A2 CAR 3 CAR4a Figure C-2 Cessna (Cessna Aircraft Company) 150, 150A, 150B, 150C 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, A150M, 152, A152 3A19 CAR 3 FAR 23 Figure C-2 Cessna (Cessna Aircraft Company) 170, 170A, 170B A-799 CAR 3 Figure C-2 Cessna (Cessna Aircraft Company) 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S 3A12 CAR 3 FAR 23 Figure C-2 Cessna (Cessna Aircraft Company) 172RG, P172D, R172E, R172F, R172G, R172H, R172J, R172K, 175, 175A, 175B, 175C 3A17 CAR 3 Figure C-2 Cessna (Cessna Aircraft Company) 177, 177A, 177B A13CE FAR 23 Figure C-2 Cessna (Cessna Aircraft Company) 177RG A20CE FAR 23 Figure C-2 Cessna (Cessna Aircraft Company) 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K 5A6 CAR 3 Figure C-2 Cessna (Cessna Aircraft Company) 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, 182T, R182, T182, TR182, T182T 3A13 CAR 3 FAR 23 Figure C-2 Page C-10 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 Aircraft Make (TCDS Holder) [common name or previous make] Aircraft Model (alias) Type Certificate Number (TCDS) TC Certification Basis Lightning Zoning Figure Notes Cessna (Cessna Aircraft Company) 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 3A24 CAR 3 Figure C-2 Cessna (Cessna Aircraft Company) 190, 195, 195A, 195B A-790 CAR 3 Figure C-2 Cessna (Cessna Aircraft Company) 206, P206, P206A, P206B, P206C, P206D, P206E,TP206A, TP206B, TP206C, TP206D, TP206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, 206H, T206H A4CE CAR 3 FAR 23 Figure C-2 Cessna (Cessna Aircraft Company) 207, 207A, T207, T207A A16CE FAR 23 Figure C-2 Cessna (Cessna Aircraft Company) 208, 208B A37CE FAR 23 Figure C-2 Cessna (Cessna Aircraft Company) 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, T210N, 210R, T210R, 210-5, 210-5A 3A21 CAR 3 FAR 23 Figure C-2 Cessna (Cessna Aircraft Company) 310, 310A (USAF U-3A), 310B, 310C, 310D, 310E (USAF U-3B), 310F, 310G, 310H, E310H, 310I, 310J, 310J-1, E310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R 3A10 CAR 3 FAR 23 Figure C-5 Cessna (Cessna Aircraft Company) 320, 320A, 320B, 320C, 320D, 320E, 320F, 320-1, 335 3A25 CAR 3 FAR 23 Figure C-5 Cessna (Cessna Aircraft Company) 336 A2CE CAR 3 Figure C-7 Cessna (Cessna Aircraft Company) 337, 337A (USAF 02B), 337B, T337B, 337C, 337E, T337E, T337C, 337D, T337D, 337F, T337F, 337G, T337G, 337H, T337H, T337H-SP A6CE CAR 3 FAR 23 Figure C-7 Cessna (Cessna Aircraft Company) 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A A7CE CAR 3 FAR 23 Figure C-5 Cessna (Cessna Aircraft Company) 404, 406 A25CE FAR 23 Figure C-5 Cessna (Cessna Aircraft Company) Cessna FR172E, Cessna FR172F, Cessna FR172G, Cessna FR172H, Cessna FR172J, Cessna FR172K A18EU CAR 3 Figure C-2 Cessna (Cessna Aircraft Company) T303 (Crusader) A34CE FAR 23 Figure C-5 CPAC, Inc. (CPAC, Inc.) [Commander Aircraft Co.] 112, 112TC, 112B, 112TCA, 114, 114A, 114B, 114TC A12SO CAR 3 Figure C-2 deHavilland (Viking Air Limited) [deHavilland, Inc.) DHC-2 Mk. I, DHC-2 Mk. II, DHC-2 Mk. III A-806 CAR 3 Figure C-2 Dornier (Dornier-Werke G.m.b.H.) Do 27 Q-6 A8IN CAR 3/10 Figure C-2 Dornier Luftfahrt GmbH (Dornier Luftfahrt GmbH) Do 28 D, Do 28 D-1, Dornier 228-100, Dornier 228-101, Dornier 228-200, Dornier 228-201, Dornier 228-202, Dornier 228-212 A16EU FAR 23 Figure C-5 EADS-PZL “Warszawa-Okecie” (EADS- PZL “Warszawa-Okecie” S.A.) [Panstwowe Zaklady Lotnicze) PZL-KOLIBER 150A, PZL-KOLIBER 160A A69EU FAR 23 Figure C-2 EADS-PZL “Warszawa-Okęcie” (EADS- PZL “Warszawa-Okęcie” S.A.) [Panstwowe Zaklady Lotnicze] PZL-104 WILGA 80, PZL-104M WILGA 2000, PZL-104MA WILGA 2000 A55EU FAR 23 Figure C-2 Garmin GPS and XM® Antenna STC Installation Manual Page C-11 190-01284-00 Rev. B Aircraft Make (TCDS Holder) [common name or previous make] Aircraft Model (alias) Type Certificate Number (TCDS) TC Certification Basis Lightning Zoning Figure Notes Embraer (Empresa Brasileira de Aeronautica S. A.) EMB-110P1, EMB-110P2 A21SO FAR 23 FAR 25 Figure C-5 Found Aircraft Canada, Inc. (Found Aircraft Canada, Inc.) FBA-2C, FBA-2C1, FBA-2C2, FBA-2C3 A7EA CAR 3 FAR 23 Figure C-2 Found Brothers (Found Brothers Aviation Limited) FBA Centennial “100” A13EA FAR 23 Figure C-2 GA8 Airvan (Pty) Ltd (GA8 Airvan (Pty) Ltd) [Gippsland Aeronautics Pty. Ltd.] GA8 A00011LA FAR 23 Figure C-2 Gulfstream American (Gulfstream American Corp) [Grumman] G-44, G-44A, SCAN Type 30 A-734 CAR 4a Figure C-5 Some WAAS based operations may have limited availability due to poor visibility Grumman (Grumman American Aviation Corporation) Grumman G-21, Grumman G-21A TC 654 Aero 7A Figure C-5 Some WAAS based operations may have limited availability due to poor visibility Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 18A, S18A TC 630 Aero 7A Figure C-5 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 18D, A18A, A18D, S18D, SA18A, SA18D A-684 Aero 7A Figure C-5 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 19A, B19, M19A, 23, A23, A23A, A23-19, A23-24, B23, C23, A24, A24R, B24R, C24R A1CE CAR 3 Figure C-2 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 35, A35, B35, C35, D35, E35, 35R, F35, G35 A-777 CAR 3 Figure C-2 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36, A36TC, B36TC 3A15 CAR 3 FAR 23 Figure C-2 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 3N, 3NM, 3TM, JRB-6, D18C, D18S, E18S, RC-45J (SNB- 5P), E18S-9700, G18S, H18, C-45G, C-45H, TC-45G, TC- 45H, TC-45J, UC-45J (SNB-5) A-765 CAR 3 Figure C-5 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 45 (YT-34), A45 (T-34A) or (B-45), D45 (T-34B) 5A3 CAR 3 Figure C-2 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 50(L-23A), B50(L-23B), C50, D50(L-23E), D50A, D50B, D50C, D50E, D50E-5990, E50(L-23D, RL-23D), F50, G50, H50, J50 5A4 CAR 3 FAR 23 Figure C-5 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 58TC, 58TCA A23CE FAR 23 Figure C-5 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 76 A29CE FAR 23 Figure C-5 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 77 A30CE FAR 23 Figure C-2 Page C-12 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 Aircraft Make (TCDS Holder) [common name or previous make] Aircraft Model (alias) Type Certificate Number (TCDS) TC Certification Basis Lightning Zoning Figure Notes Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 99, 99A, 99A(FACH), A99, A99A, B99, C99 A14CE FAR 23 Figure C-5 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] 200, 200C, B200, B200C A24CE FAR 23 FAR 25 Figure C-5 This model has specific location data, see Section 3.2.1. Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] B90, C90, C90A, C90GT 3A20 CAR 3 FAR 23 FAR 25 Figure C-5 This model has specific location data, see Section 3.2.1. Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] D55, D55A, E55, E55A, 56TC, A56TC, 58, 58A, 95, B95, B95A, D95A, E95, 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B (T-42), 95-C55, 95-C55A 3A16 CAR 3 FAR 23 Figure C-5 Hawker Beechcraft (Hawker Beechcraft Corporation) [Raytheon] [Beech] T-34C (T-34C-1) (34C) A26CE FAR 23 Figure C-2 HELIO (Helio Aircraft, LLC) [Alliance Aircraft Group, LLC] 500 A2EA CAR 3 Figure C-5 HELIO (Helio Aircraft, LLC) [Alliance Aircraft Group, LLC] H-250, H-295 (USAF U-10D), HT-295, H-391 (USAF YL-24), H-391B, H-395 (USAF L-28A or U-10B), H-395A, H-700, H-800 1A8 CAR 3 Figure C-2 HELIO (Helio Aircraft, LLC) [Alliance Aircraft Group, LLC] HST-550, HST-550A (USAF AU-24A) A4EA CAR 3 Figure C-2 Interceptor (Prop-Jets, Inc.) [Meyers] 200, 200A, 200B, 200C, 200D 3A18 CAR 3 Figure C-2 King’s Engineering Fellowship (The King's Engineering Fellowship) 4500-300, 4500-300 Series II A17CE FAR 23 Figure C-5 Lockheed (Lockheed Aircraft Corporation) 12-A (Army UC-40, UC-40A; Navy JO-1, JO-2) TC 616 Aero 7A Figure C-5 Lockheed (Lockheed Aircraft Corporation) 18 A-723 CAR 4a Figure C-5 Micco Aircraft Co., Inc. (MICCO Aircraft Company, Inc.) [Meyers] [LanShe] MAC-125C, MAC-145, MAC-145A, MAC-145B 3A1 CAR 4a FAR 23 Figure C-2 Mooney (Mooney Airplane Company, Inc.) M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S, M20TN 2A3 CAR 3 Figure C-2 Morane-Saulnier (SOCATA - Groupe Aerospatiale) M.S.760, M.S.760A, M.S.760B 7A3 CAR 3 Figure C-8 Antennas must be located 24 inches aft of windscreen to avoid vibration/buffet issues. MORANE SAULNIER (Rallye) Series (SOCATA - Groupe Aerospatiale) Rallye 100S, Rallye 150ST, Rallye 150T, Rallye 235E, Rallye 235C MS880B, MS885, MS894A, MS893A, MS892A- 150, MS892E-150 (Rallye 150GT), MS893E (Rallye 180GT), MS894E 7A14 CAR 3 Figure C-2 Moravan a.s. (Moravan a.s.) Z-242L, Z-143L A76EU FAR 23 Figure C-2 Navion (Sierra Hotel Aero, Inc) Navion (L-17A), Navion A (L-17B, L-17C), Navion B, Navion D, Navion E, Navion F, Navion G, Navion H A-782 CAR 3 Figure C-2 Pacific Aerospace Limited (Pacific Aerospace Limited) 750XL A50CE FAR 23 Figure C-2 PIAGGIO (Industrie Aeronautiche E. Meccaniche) [Piaggio & C.; Industrie Aeronautiche E Meccaniche] P.166, P.166B, P.166C, P.166 DL3 7A4 CAR 3 FAR 21 FAR 23 Figure C-6 Garmin GPS and XM® Antenna STC Installation Manual Page C-13 190-01284-00 Rev. B Aircraft Make (TCDS Holder) [common name or previous make] Aircraft Model (alias) Type Certificate Number (TCDS) TC Certification Basis Lightning Zoning Figure Notes Pilatus (Pilatus Aircraft Ltd.) PC-6, PC-6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, PC-6/C1-H2 7A15 CAR 3 Figure C-2 Pilatus (Pilatus Aircraft Ltd.) PC-7 A50EU FAR 23 FAR 25 Figure C-2 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-23, PA-23-160, PA-23-235, PA-23-250, PA-E23-250 1A10 CAR 3 Figure C-5 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-24, PA-24-250, PA-24-260, PA-24-400 1A15 CAR 3 Figure C-5 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-235, PA-28S-160, PA-28R-180, PA-28S-180, PA-28-181, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-28-201T, PA-28-236 2A13 CAR 3 FAR 23 Figure C-2 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-30, PA-39, PA-40 A1EA CAR 3 Figure C-5 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-31(PA-31-310), PA-31-300, PA-31-325, PA-31-350 A20SO CAR 3 FAR23 Figure C-5 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301(SP), PA-32R-301(HP), PA-32R-301T, PA-32-301, PA-32-301T, PA-32-301FT, PA-32-301XTC A3SO CAR 3 Figure C-2 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-34-200, PA-34-200T, PA-34-220T A7SO CAR 3 FAR 23 Figure C-5 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-38-112 A18SO FAR 23 Figure C-2 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-44-180, PA-44-180T A19SO FAR 23 Figure C-5 Piper Aircraft, Inc. (Piper Aircraft, Inc.) [New Piper] PA-46R-350T A25SO FAR 23 Figure C-2 Polskie Zaklady Lotnicze Spolka zo.o (Polskie Zaklady Lotnicze Spolka zo.o.) [PZL Mielec] PZL M26 01 A44CE FAR 23 Figure C-2 Quartz Mountain Aerospace Inc. (Quartz Mountain Aerospace Inc.) [Luscombe] 11A, 11E A-804 CAR 3 Figure C-2 Revo, Inc. (Revo, Incorporated) [Lake] [Global Amphibians LLC] Colonial C-1, Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, Lake LA-4-200, Lake Model 250 1A13 CAR 3 Figure C-4 GPS antennas located just aft of the windscreen may be best for this model. Some WAAS based operations may have limited availability due to poor visibility Rockwell International (Rockwell international Corporation) [North American] BC-1A, AT-6, AT-6A, AT-6B, AT-6C, AT-6D, AT-6F, SNJ-7, T-6G A-2-575 CAR 4a Figure C-2 Page C-14 Garmin GPS and XM® Antenna STC Installation Manual Rev. B 190-01284-00 Aircraft Make (TCDS Holder) [common name or previous make] Aircraft Model (alias) Type Certificate Number (TCDS) TC Certification Basis Lightning Zoning Figure Notes Short Brothers & Harland LTD (Short Brothers & Harland Ltd.) SC-7 Series 2, SC-7 Series 3 A15EU FAR 23 Figure C-5 SOCATA (SOCATA - Groupe Aerospatiale) TB 9, TB 10, TB 20, TB 21, TB 200 A51EU FAR 23 Figure C-2 SOCATA, S.A. (SOCATA, S.A.) [Grumman] GA-7 (Cougar) A17SO FAR 23 Figure C-5 STOL (Sky Enterprises, Inc.) [ Republic; Stol Amphibian; Seabee; Trident; TwinBee] RC-3 A-769 CAR 3 Figure C-3 STOL (STOL Aircraft Corporation) [United Consultants; Twin-Bee] UC-1 A6EA CAR 3 Figure C-5 Some WAAS based operations may have limited availability due to poor visibility TKEF (The King’s Engineering Fellowship (TKEF)) Model 44 (Angel) A2WI FAR 23 Figure C-6 True Flight Holdings LLC (True Flight Holdings LLC) [American General] [Tiger Aircraft LLC] AA-1, AA-1A, AA-1B, AA-1C A11EA FAR 23 Figure C-2 True Flight Holdings LLC (True Flight Holdings LLC) [American General] [Tiger Aircraft LLC] AA-5, AA-5A, AA-5B, AG-5B A16EA FAR 23 Figure C-2 Twin Commander (Twin Commander Aircraft Corporation) 500, 500-A, 500-B, 500-U, 500-S, 520, 560, 560-A, 560-E 6A1 CAR 3 Figure C-5 Twin Commander (Twin Commander Aircraft Corporation) 560-F, 680, 680E, 680F, 680FL 2A4 CAR 3 Figure C-5 Viking Air Limited (Viking Air Limited) [deHavilland] [Otter] DHC-3 A-815 CAR 3 Figure C-2 Viking Air Limited (Viking Air Limited) [de Havilland, Inc.] [Bombardier, Inc.] [Twin Otter] DHC-6-1, DHC-6-100, DHC-6-200, DHC-6-300 A9EA CAR 3 Figure C-5 WSK "PZL-MIELEC" OBR (WSK PZL MIELEC and OBR SK MIELEC) PZL M20 03 A68EU FAR 23 Figure C-5 Zenair (Zenair Ltd.) CH2000 TA5CH FAR 23 Figure C-2