Ameri-King AK-950L Installation & Operation Manual

INSTALLATION & OPERATION MANU AL for ·-· ·------ -- ----- PIN AK-950 L- GNS 430/ /530/S30W (GARMIN INTERNATfONAL INC.) GPS 1 NAV SWITCHING & ANNUNCIATOR PANEL '' Per TSO-C129a, RTCA D0-208 and D0-160c Requirements AMERI-KING CORPORATION 17881 Sampson Lane Huntington Beach, CA 92648 Tel: (714) 842-8555 Fax: (714) 842-4235 Email: [email protected] Website: www.ameri-king.com : ; ~ 24-62·91

1.2 1.3 1.4 1 .4.1 1.4.2 1.4.3 1. 5 1.6 1. 7 2.1 2.2 2 .2.1 2.2.2 2.2.3 2.2.4 2.2.5 2.3 2.4 2.4.1 2.4.2 INS 1 ALLA li UN ANU Uf't:ll" IIUI" IVI"I"U"L, "IUUI:L Hl\ .,;_,v GPS 1 NAV SWITCI-IING & ANNUNCIATOR PANEL TABLE OF CONTENTS Table of Contents ··············································· SECTION 1 GENERAL INFORMATION Scope ................................................................ 3 Description . . . . . .. . . . .. . . . . . .. .. .. . . . . . . . . .. . . . .. .. . . . . . . .. . . . .. . . . . 3 Technical Characteristics ...................................... 6 Front Panel Contrais and Annunciations . . . . . . . . . . . . . . . . . . 8 Contrais ....................................................... 8 Annunciations . . .. . . . .. . .. . . . . . . . . . . . . . . .. . . .. . . . . . . . . . . . . . . . 9 Interface . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . .. . .. . . . . . . . . . . . . . . 1 0 Equipment Limitations .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. . .. .. .. .. 11 Major Components . . . . . .. . .. . . . .. . .. . . . .. .. . . . .. . . . .. . . .. .. . . . .. . 11 Accessories supplied .. . .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. . .. .. . .. .. 11 SECTION Il INSTALLATION AND TEST Unpacking and lnspecting Equipment . . . . . . . . . . . . . . . . . . . . . . 1 3 Mechanical Installation .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. 13 Equipment Location . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 3 Cooling ......................................................... 13 Additional Annunciations .. .. .. . .. . .. .. . .. .. .. .. .. .. .. . .. . 1 5 Additional Rel a ys . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 5 Rou ting of Ca bles . .. . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . 1 5 Electrical Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 5 Post Installation Test .. .. .. .. .. .. . .. .. .. . .. .. .. .. .. . .. .. .. .... ... 21 Pre Installation Tests . .. .. .. .. .... ...... ..... .. .. .. ...... .. . 21 Operating Instructions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 1 3.1 3.2 4.1 4.2 4.3 1 . 1 2.1 3.1 3.2 3.3 INS 1 ALLA li UN ANU UPtHA li UN MANUAL, MUUEl AK-!IbU GPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL ... ,., TABLE OF CONTENTS CCONT"D) SECTION Ill OPERATION General .............................................................. 23 Operation SECTION IV WARRANTY AND SERVICE 23 Limited Warranty . . .. . . . . . .. .. . . .. .. .. . .. .. .. .. . .. .. .. .. .... . .. ... 25 Repair Service . . . . . . .. . . . . . . .. . . .. . . . .. . .. .. . .. . . .. . . .. . . .. .. .. . .. . 27 Factory Comprehensive Test Service ...................... 27 LIST OF FIGURES Outline Drawing for ali Series .. . .. . .. .. .. .. .. . .. .. .. . .. .. .. .. 4 Cutout Dimensions for Panel Mounting . . . . . . . . . . . . . . . . . . . 14 Schematic Pino ut for Connecter .. ~......................... 16 E~ectrical Schematic Diagraîn .. .. .. .. .. . .. . .. .. .. .. .. .. .. .. .. 18 Wiring Diagram ....................................... :.. .. .. .. .. .. 19 APPENDIX A Environmental Qualification form RTCA 1 D0160C .... 28 2 24-62·91

OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL SCOPE SECTION 1 GENERAL INFORMATION This manual contains information necessary for the installation, test and operation of the model AK-950L, GPS 1 NA V Switching and Annunciator Panel, manufactured by Ameri - King Corporation, California, U.S.A. DESCRIPTION The AK-950L is a self-contained GPS 1 NAV Switching and Annunciator Pimel. lt combines ali the necessary functions required for switching HSI 1 CDI data inputs between a conventional NA V (VOR) receiver and the approach-certified GPS receiver. ln addition, the AK-950L contains several GPS status annunciations used to indicate modes selected by the front panel switches and various inputs from the GPS receiver. Features include Incandescent lamps with 16,000 hours average li fe, built in Automatic Dimming and Test for Annunciator Panel. Refer to figure 1-1 for Outline Drawing for ali Series for ali Models' Annunciation Displays and Switches. The following GPS system are applicable: Model AK-950 L- GNS 430/' /530/530W for GNS 430/ /S30/S30W Garmin International Inc. 3 INSTALLATION AND OPERATION MANUA1, MODEJ,;AK-860 OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL 2.830 l l ~ 1.050 ~ FIGURE 1-1a. OVERALL DIMENSIONS Ql.JlJINE DRAWING PIN AK-950 L- GNS 430/;, "" /530/530W GPS/NAV Switching and Annunciator Panel 4 24-62·91

OPI 1 NAV SWITCHINO lo ANHUNCIATOR PANEL 5 INSTALLATION AND OPERATION MANUAL, MOOEL AK-960 OPS 1 NAV SWITCHINO .. ANNUNCIATOR PANEL 1.3 TECHNICAL CHARACTERISTICS §PECIFICATIONS: TSO COMPLIANCE: PHYSICAL CHARACTERISTICS: • PANEL CUTOUT SIZE AND WEIGHT: GENERAL SPECIFICATIONS: • POWER INPUT: • LAMP BULB TYPE: • RELAY TYPE: - No. of avallable Polos: - Switching Current 1 Voltage: - Carrying Current 1 Voltage: • Contact Resistance: Contact Material: • Switching lime: - lnsulation Resistance: - lite Expectancy: - Coll Resistance CHARACTERISTICS; ISO· C129a Panel Mounted, 1.00" x 2.12" 0.31bs (10.0- 32.2) Vdc (5.9 -'7.4) Watts Nominal 0.214 Amp. @ 28 Vdc, Nominal. 0.630 Amp.@ 14 Vdc, Nominal. 0.654 Anip. @ 28 Vdc, Momentary Test Mode only. 1.575 Amp. @ 14Vdc, Momentary TE!st Mode ~nly. Dual lamp' for each Annunclator. PIN 6838 for 28 Vdc. P/N 8111 for 14 Vdc. Tl Incandescent; 16,000 hours average lite. 3 Polos; bouble throws 2 Amp /•220 Vdc maximum 2 Amp 1 220 Vdc maximum 60 milli • ohm max Gold overtay ( 1 · 2) milli • seconds 1,000 r:n~ga ·ohm @ 600 Vdc 1 00 million mechanical operations .2 million electrical operations @30Vdc 2880 Ohm @ 24 Vdc; · 1028 Ohm @ 12 Vdc. 6 ' 24-62·91

OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL • AUTO DIMMING: Built in ENVIRONMENTAL TEST SPECIFICATIONS: • RTCA D0-208 A 1/D1 • RTCA D0-160C ENV. CAT.: ClAC/XXXSXXXSXXXXBXB • TEMP. AND ALTITUDE: Low Temperature: High Temperature: • TEMP. VARIATION: • HUMIDITY: • SHOCK: • VIBRATION: • MAGNETIC EFFECT: • POWER INPUT: Category A2 & D1 -20 deg. C Operating; -55 deg. C Storage. + 70 deg. C Operating; + 85 deg. C Storage. Category C 2 deg. C minimum per minute Category A 95% RH, 50 hours operating 6 G, 11 + 1- 2 msec, operational 1 5 G, 11 + 1-2 msec, crash safety Categories M and N Category A Less than 0.3 m Category B Normal Operating: ( 10.0- 15.1) Vdc (20.0- 30.3) Vdc Abnormal Opera ting: ( 11 .0 -16. 1) V de (22.0- 32.21 Vdc • VOLTAGE SPIKE: Category B • AUDIO FREO. CONDUCTED SUSCEPTIBILITY: Category B • INDUCED SIGNAL SUSCEPTIBILITY: Category A • RF SUSCEPTIBILITY: Category T • EMISSION OF RF ENERGY: Category A 1.4 1.4.1 1.4. 1. 1 INSTALLATION AND OPERATION MANUAL, MODEL AK-960 GPS 1 NAV SWITCHING & ANNUNCIATOR PANEL FRONT PANEL CONTROLS AND ANNUNCIATIONS CONTROLS CONTROLS FOR MODELS AK-950- GNS530 (GARMIN): CDI Switch: OBS Switch: TEST: Momentary action Switch, when pressed, will select NA V (VORI or GPS presentation on HSI 1 CDI. Momentary Switch, when pressed, will select AUTO 1 HOLD OBS Sequence Mode. Push Button switch for TEST function for ali Annunciation lamps. 8 24-62·91

GPS 1 NAV SWITCHING & ANNUNCIATOR PANEL ANNUNCIATIONS 1 .4.2.1 ANNUNCIATIONS FOR AK-950 l - GNS 430 / 530 IGARMINl: VLOC (White): NAV (VORI information presented on the GNS GPS (Green): GPS information presented on the GNS TERM (Green): GPS is active engaged in the Terminal mode. APR (Green): GPS is actively engaged in the approach mode. OBS (Green): GPS waypoint Sequencing is in Hold Mode. AUTO (White): GPS waypoint Sequencing is in Auto Mode. MSG (Amber): GPS message alert, from the GPS receiver. WPT (Amber): GPS waypoint alert, from the GPS receiver. INTEG (Amber): INTEG lntergrity Alert, from the GPS receiver. 9 INSTALLATION AND OPERATION MANUAL, MODEL AK-960 GPS 1 NAV SWITCHING & ANNÙNCIATOR PANEL 1.4.3 INTERFACE 1.4.3.1 INTERFACE FOR P/N AK-950 l - GNS 430 1 530 COl Switch: (Pin 67) OBS Switch: (Pin 73 l VLOC: (Pin 62) GPS: (Pin 66) AUTO: (Pin 72) OBS: (Pin 74) TERM: (Pin 77) APR: (Pin ·71; Provides a momèntary logic low, to the GNS receiver, for Switching between VLOC and GPS Source. Provides a momentary logic law, to the GNS . recèi~er, for Switching between ., ,. Automatic and Hold Mode, for GPS Waypoint Sequencing. Receives an alternate logic law from the GNS to annunciata VLOC. Receives an alternate logic law from the GNS to annunciata GPS. l' ' - Receives an alternate logic- law from the GNS to annunciata AUTO. Receives an alternate logic law from the GNS to annunciata OBS. Receives an alternate logic law from the GNS to annunciata TERM. Receives an alternate logic law from the GNS to annunciata APR. MSG 1 WPT 1 INTEG: (Pins 75 1 Receives an alternate logic Law from the GNS to annunciate MSG 1 WPT 1 INTEG. 76 1 62) 10 24-62·91

GPS/NAV SWITCHING & ANNUNCIATOR PANEL 1.5 EQUIPMENT LIMITATIONS The AK-950 series control units contain specifie dash numbers to be used with various GPS receivers. The installer must match the correct controller part number with the GPS receiver being installed. This equipment GPSINA V switching & Annunciator Panel is approved for installation with the following mode! number only: GPS mode! GNS 430 1 530 1 530W Garmin International Inc. Installation of this equipment to any other GPS is disapproved. The condition and tests required for TSO approval of this article are minimum performance standards. lt is the responsibility ofthose desiring to install this article either on or within a specifie type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. The article may be installed only if further evaluation by the applicant documents an acceptable installation and is approved by the Administrator. NOTE: Anytime the AK-950 is disconnected or removed from the aircraft, the HSI 1 CDI will be inoperative in both NAY (VOR) and GPS. 1.6 MAJOR COMPONENTS The system is comprised of one major component, the AK-950, GPSINA V Switching and Annunciator Panel. 1.7 ACCESSORIES SUPPLIED 1.7.1 INSTALLATION KIT: PARTNO. DESCRIPTION 9500001 Pl, Mating Connector Kit. High Density D Subminiature Conn. Plug, 78 Female Crimped Pins, with Backshell and Thumbscrews. PIN 162X 11989X & FK22SL05 (Conec Corporation) 11 INSTALLA Tl ON AND OPERA Tl ON MANU AL, MO DEL AK-950 GPSINA V SWITCHING & ANNUNCIA TOR PANEL 9500002 Optional Pre-fabricated Cable Assembly with MIL-SPEC shielded Cable, including: MIL-W-22759118-24-9 M27500-l-24-TG-2-T-14 M 17500-1-24-TG-3-T -14 TYPE OF MA TING CONNECTOR Hi Density D-Subminiature Connector, 78 Female Sockets Plug. Information for Crimping Tool. l. Hand Crimping Tool: M22520/2-0 1 2. Positioner: 3. Extract/Removal Tool: 4. V endor Sources: Daniel PIN AFMA M22520/2-06 Daniel PIN K41 M81969/1-04 Daniel PIN 91067-1 Daniel Manufacturing Inc. 6103 Anno Ave. Orlando, FL 32809 Tel (407) 855-6161 Fax(407)855-6884 12 24-62·91

OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL SECTION Il INSTAllATION AND TEST 2.1 UNPACKING AND INSPECTING EOUIPMENT 2.2 2.2.1 Extreme care when unpacking the equipment. Visual inspection of the equipment for evidence of damage incurred during shipment. Any claim should be promtly filed with the transportation company. Save the shipping container to subtantiate the claim. Retain the container and packaging material for possible future use. MECHANICALINSTALIATION The AK-950 is designed with the installer in mind. Ali accessories which are required for completing system installation are provided, including Pre-fabricated Wiring Cable Assembly. EOUIPMENT LOCATION The AK-950 must be mounted as close to the pilot's field of view as possible. The preferable location is near the HSI 1 CDI that will be displaying the FPS information. The unit depth, with connecter atttached, must also be taken into consideration. A void mounting close to heater vents or other high he at sources. The indicator is secured in place behind the panel since it is designed for re ar mount only. Make a panel cutout as shown in Figure 2-1. Secure the indicator in place with four 4-40 x 3/8 to 1 .0" flat head phillips screws. 2.2.2 COOLING No direct cooling is required. As with any electronic equipment, overall reliability may be increased if the AK-950 is not located near any high heat source or crowded next to ether equipment. Means of providing a gentle air flow will be a plus. •13 INSTALLATION AND OPERATION MA~~AL, MODEL AK-960 OPS 1 NAY SWITCHINO a. ANNUNCIATOR PANEL R.130 { 4 PLS) l~ +cv 1.000 o. 750 0.175 ~2.120-~ 2.470 ~~----1 (11.125 fhru hole for 4-40 screw (4 PLS) FIGURE 2.1 CUTOUT DIMENSIONS FOR PANEL MOUNTING 14 24-62·91

OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL ADDITIONAL ANNUNCIATIONS Depending upon the installation and approving agency, you may be required to provide additional NA V Source Select external annunciators near the HSI 1 COl. Spare relay contacts on the AK-950 connector may be used for this purpose. ADDITIONAL RELAYS ROUTING OF CABLES Care must be taken not to bundle the AK-950 logic and low level signal lines with any high energy sources. Examples of these sources include 400 Hz AC, Comm, DME, HF and transponder transmitter coax. Always use shielded wire when shawn on the installation print. A void sharp bends in cabling and routing near aircraft control cables. 2.3 ELECTRICALINSTALLATION Refer to figure 3-1 for Schematic Pinout Assignment for Connector, and figure 3-2 for Electrical Schematic Diagram. Wire the aircraft harness according to figure 3-3 Use at least 24 AWG wire for ali connections. Vou MUST use shielded wire where shawn. A void sharp bends and routing cable near high energy sources. Care must be taken to tie the harness away from aircraft contrais and cables. Normal installation techniques should be applied. 15 IN8TALLATION AND OPERATION MANUAL, MODEL Al-160 OPS 1 NAV SWITCHINO. ANNUNCIATOR PANEL CONNECTOR REAR VIEW OF" CONNECTOR 1 2 3 4 5 6 7 8 9 10 Il 12 13 14 15 16 17 18 19 20 • • • • • • • • • • • • • • • • • • • • 21 22 23 24 25 26 27 28 29 JO 31 32 JJ 34 J5 36 37 38 39 • • • • • • • • • • • • • • • • • • • 40 4 1 42 43 44 45 46 4 7 48 49 50 51 52 53 54 55 56 57 58 59 • • • • • • • • • • • • • • • • • • • • 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 • • • • • • • • • • • • • • • • • • • 000 78, HI-Oenslty 0-Subminloture Connecter r-;- 2 3 4 5 f.------·. 6 7 8 9 10 11 12 1------ 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 M FIGURE 3-1 a SCHEMA TIC PINOUT FOR CONNECTOR 16 24-62·91

OPS 1 NAV SWITCHINO a. ANNUNCIATOR PANEL OC GROUND INTEG Annunciator Alternate Ground Input VLOC Annunciator Alternate Ground Input CDI Momentary Switch Output - GPS Annunciator Ground Input APR Annunciator Ground Input -AUTO Annunciator Alternats Ground Input - OBS Momentary Switch Output . OBS Annunciator Alternats Ground Input MSG Annunciator Alternats Ground Input - WPT Annunciator Alternats Ground Input TERf.!l Annunciator Alternats Ground Input + 14/28 VDC POWER INPUT FIGURE 3-"1 b SCHEMA TIC PINOUT FOR CONNECTOR 17 MTALLATION AND OPERATION MANUAL, MODEL Al-860 OPS 1 NAV SWITCHINO a. ~NMUMCIATOR PAfiEl AK-950 L- GNS 430/' ·/530/530W - +14/2e VDC I'OW[P llfi'Ul -OC CROUHD 62 INTEG Amber Annunc. {Aiternate Ground Input) VLOC White Annunc. (Alternat~: Grou nd Input) GPS Green Annunc. (Aiternate. Gn:>Und Input) WPT Alllher Annunc. (Aiternate Gràund Input) 77 TERM Green Annunc. (Aiternate Ground Input) 71 APR Green Annunc. (Aiternate Ground Input) 75 MSG Amber Annunc. (Aiternate Ground Input) 74 OBS Green Annunc. (Aiternate Ground Input) AUTO White Annunc. (Aiternate Ground Input) COl Mom Switch (Mometary Ground Output) OBS Mom Switch (Momentary Ground Output) FIGURE 3-2 ELECTRICAL SCHEMA TIC DIAGRAM 18 24-62·91

~ c E ... co ~ INSTALLATION AND OPERATION MANUAL, MODEL AK-960 OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL PIN AK-950 L- GNS 430/" ---- r : INTEG Anrl ~ 62 ~ INTEG Amber Annunc. VLOC Ann. 1 66 VLOC White Annunc. GPS Annunc 2 70 GPS Green Annunc. WPT Annunr 3 76 WPT Amber Annunc. TERM Ann. 4 77 TERM Green Annunc. · APR Annunc. 5 71 APR Green Annunc_ MSG Ann. 6 76 MSG Amber Annunc. OBS Annunc- 7 74 OBS Green Annunc. [ . 1 72 AUTO White Annunc. COl Mom Sw 7'l 57 COl Mom Switch OBS Mom..êV~ 71 73 OBS Mom Switch ,- 40 - OC CROUND ......... Ps~q, ri-- 78 ____ +14/28 VDC POW[R INPUT + VV' +14/28 VOC () 6- 2A /530/S30W NOJU: 1. Reler 16 GPS Monuloclurer's lnslollolion Manuel lor Acluol lnsloll'llion. 2. Ali Wlres ore 24 AWG minimum. FIGURE 3_3 WJRJNG DIAGRAM for AK-950L- ( ) for GNS 430/' /530/530W Garmin International Inc. 1~ 24-62·91

GPS 1 NAV SWITCHING & ANNUNCIATOR PANEL COHN[ClOR AK-950 L - GNS 430 1 530 r ~ INTEG Ann. 9 62 INTEG Amber Annunc. VLOC Ann. 1 66 VLOC White Annunc. GPS Annunc 2 70 GPS Green Annunc. WPT Annunr 3 76 WPT Amber Annunc. fTERM Ann. 4 77 TERM Green Annunc. APR Annunc. 5 1-- 71 APR Green Annunc. MSG Ann. 6 75 MSG Amber Annunc. OBS Annunc. 7 74 OBS Green Annunc. AUTO Ann. 8 72 AUTO White Annunc. CDI Mom Sw 7~ ,_ 67 CDI Mom Switch OBS Mom Sv 71 1-· 73 OBS Mom Switch 1 40 -- OC CROUND '-r P400,1 ri- 78 1 - + 14/28 YDC POWfR INPUT ,l, ~ +14/28 YDC 0 0- 2A NOT~?: 1. Refer 16 GPS Monufoclurer's lnslollolion Monuol for Acluol lnslall'llion. 2. Ail Wires ore 24 AWG minimum. FIGURE 3.3 WIRING DIAGRAM for AK-950L- ( ) with GNS-430 (Garmin International lnc.) 19 24-62·91

GPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL POST INSTALLATION TEST After completing the mechanical installation, the following Post Installation Function Tests must be performed. 2.4.1 PRE INSTALLATION TESTS 2.4.2 With the AK-950L disconnected, turn on the avionics master switch and verity that the aircraft power of 14 1 28 Vdc are on Connector Pin 78 (Annunciator Power). Using an Ohm Meter, verity that Pin 40 is aircraft ground. OPERATING INSTRUCTIONS Refer ta GPS Manufacturer' s Installation Manual for complete GPS System Operating Instructions. The following paragraphs described Lamp BAT 1 DIM 1 Test and VLOC 1 GPS Switching function only. 2.4.2.1 OPERA TING INSTRUCTIONS FOR MODEL AK-950l- GNS530 (GARMIN): Turn off the avionics master switch and connect the mating connector ta the AK-950L. Turn on the avionics master switch and the AK-950L should come on with the following annunciations: 1 . VLOC or GPS 2. AUTO or OBS Momentarily press the TEST Switch, ali annunciations should light. Select VlOC using the COl Button. The presentation on the GNS- will now be information from the VOR receiver. Select GPS using the COl Button. The presentation on the GNS- will now be information from the GPS receiver. 21 INSTALLATION AND OPERATION MANUAL, MODEL AK-960 GPS 1 NA V SWITCHING & ANNUNCIA TOR PANEL Please refer ta the GNS~530 Garmin's Installation Manual for· the remaining system tests. No periodic maintenance or calibration is necessary for continued airworthiness of the AK-950. 2.4.2.6 AUTO DIMMING TEST: A Photocell provides the Auto Dimming function. This can be tested by covering the Photocell by hand and observing the change in brightness. NOTE: 1 . There is an Adjustment Potentiometer located on the side of the unit. Adjustment should be made when the unit is installed in aircraft, and with night time lighting conditions. 2. Rotate the Potentiometer clockwise ta dim the annunciators. Rotate the Potentiometer coun~er-clockwise to make the annunciators brighter. 3. Do not use excessive in ward force on the alignment tool, and do not use excessive rotational force. Damage may result. 22 24-62·91

GPS 1 NAV SWITCHING & ANNUNCIATOR PANEL GENERAL SECTION Ill OPERATION This section describes the operation of the GPS 1 NA V Switching and Annunciator Panel, Madel AK-950L. OPERATION 3.2.1 OPERATION FOR MODELS AK-950L- GNS530 IGARMIN): VLOC/GPS Pushing the CDI Switch selects the MOMENTARY navigation source IVOR 1 ILS 1 LOC or GPS) SWITCH ta be displayed or. the GNS GPS OBS SWITCH MSG WPT ANNUNC. Pushing the GPS OBS switch will cycle the GPS receiver Waypoint Sequences, between AUTO and HOLD mode. The MSG annunciator is automatically lit when the GPS receiver initiates a message lairspace warnings, steep turns, etc.). MSG annunciation is automatically extinguished by the GPS receiver. The WPT annunciator flashes as the active waypoint in the GPS receiver is approached along the route of flight. 23 INSTALLATION AND OPERATION MANUAL, MODEL AK-950 GPS 1 NAV SWITCHING & ANNUNCIATOR PANEL VLOC GPS AUTO OBS TERM APR MSG WPT ANNUNC. The VLOC 1 GPS 1 AUTO 1 OBS 1 TERM 1 APR MSG 1 WPT Annunciator is automatically lit upon the GNS- initiates the corresponding status 1 mode Indication. 24 24-62·91

OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEl LIMITED WARRANTY SECTION IV WARRANTY Ali equipments manufactured by Ameri-King Corp. are guaranteed against defective materials and workmanship for a period of two years. Any equipment found to be defective due to material and workmanship during this limited warranty will be repaired and put in original manufactured operating condition. An option of extended third and fourth year limited warranty become valid at the end of this second year, which will warrant to the original owner. This Ameri-King Corp. warranty is void unless the Warranty Registration Card is filled out and returned to Amer-King Corp. within 15 days after original installation. Ameri-King Corp. 's liability und er this warranty is limited to servicing, repairing, replacing or adjusting any equipment returned prepaid to the factory by express written or oral authorization for that purpose and to repair or replace defective parts thereof. Repaired equipment will be returned to the equipment user freight pre-paid. Shipping charge will be paid one way only by Ameri-King Corp. Upon discovery of a condition believed to be caused by a defect in manufacturing, Amer-King Corp. must be notified. No equipment to be shipped to Ameri-King Corp. without prior authorization. Any equipment returned to Ameri-King Corp. should be accompanied by a failure report, in writing, giving full particulars in support of the claim. This limited warranty does not caver or apply to any of the followings, including: misuse of the equipment; installation or operation not in accordance with factory instructions; accidents or negligent damage; alterations of any manner; repair by other 25 INSTAllATION AND OPERATION MANUAL, MODEl AK-960 OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEl factory; changes in calibration occuring as a result of normal use of the equipment; the cast of labor, material, or other expense incidental to the repair, installation, removal from the aircraft or replacement of the equipment; damaged during shipment or installation; any persona! injuries or damage to property resulting from the installation or the operation of the equipment or the failure of the equipment or any part thereof, the equipment user assumes the risks of ali such injuries or damage. ln such cases, the repair will be bitled at cast. An estimate will be submitted for approval before ~epair is initiated. Any equipment which is returned for warranty and found not to be defective shall be charged a minimum handling and service charge and returned e.a.o. No warranty will be activated. for Ameri-King Corp. products unless the installation is approved by an FAA Certified Installer and the warranty card is completed by the supplying dealer or upon receipt by Ameri-King Coq~. of form(s) 337 or 8130-(). THE IMPLIED WARRANTY AND ALL OTHER IMPLIED WARRANTIES ARE HEREBY EXCLUDED. AMEAI- KING CORP. MAKES NO OTHER WARRANTY OR REPRESENTATION OF ANY KI ND WHA TSOEVER EXPRESSED OR IMPLIED, AND ALL IMPLIED WARRANTIES INCLUDING ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE ARE HEREBY DISCLAIMED. AMER! - KING CORP.'S MAXIMUM LIABILITY HEREUNDER IS LIMITED TO THE PURCHASED PRICE OF THE PRODUCT. IN NO EVENT SHALL AMER!- KING CORP. BE LIABLE FOR ANY CONSEOUENTIAL, INDIRECT, INCIDENTAL OR SPECIAL DAMAGES OF ANY NATURE ARISING FROM THE SALE OR USE OF THE PRODUCT, WHETHER BASED IN CONTRACT, TORT, STRICT LIABILITY OR OTHERWISE. 26 24-62·91

OPS 1 NAV SWITCHINO & ANNUNCIATOR PANEL 4.2 REPAIR SERVICE Ali equipments manufactured by Ameri-King Corp. must be repaired at the facility of Ameri-King Corp. Ali the repair services shall be performed and completed within 3 days upon repairing estimate is approved by equipment user or installation dealer. 4.3 FACTORY COMPREHENSIVE TEST SERVICE Factory Comprehensive Test Service is available. There is a service charge for this service. Ali equipments returned for Factory Comprehensive Test Service must be sent freight prepaid. 27 24-62·91

OPS 1 NAV SWITCHINO 1. ANNUNCIATOR PANEl APPENDIX A ENVIRONMENTAL QUALIFICATION FORM RTCA 1 D0160C NOMENCLATURE: AK-950 GPS 1 NAV SWITCIUNG AND RELAMPADLI! ANNUNCtATOR PANEL MODEL NO: AK-950 TSO NO: Cl29 CLASS Al MANUFACTURER: AMERI- KING CORP. Conditions Temp. & Altitude Low temperature High Temperature ln-Fiight Loss of Cooling Altitude Decompression Overpressure Tcmp. Variation Humidity Shock Operational Crash Safety Vibration Explosion Waterproofness 18842 BROOKIIURST ST. FOUNTAIN VALLEY, CA 92708 Section Description of Conducted Tests 4.0 Equipment tested to Categories A2&D1 4.5.1 4.5.2 & 4.5.3 4.5.4 Cooling air not requited 4.6.1 4.6.2 4.6.3 5.0 Equipment tested to Categoty C 6.0 Equipment tested to Category A 7.0 Equipment tested pel' D0-160C 7.2 Par. 1.2.1 7.3 8.0 Equipment tested wîthout shock- mountS to Categories M & N (Table 8-1) 9.0 Equipment identified as Category X; no test required 10.0 Equipment identified as Category X, no test requîred . 28 INSTALLATION AND OPERATION MANUAL, MODEL AK-960 OPS 1 NAV SWITCHINO 1. ANNUNCIATOR PANEL ENVIRONMENTAL QUALIFICATION (Cont'd) ' ' Conditions Section Description of Conducted Tests '' Fluids Susceptibility 11.0 Equipment identified as Category X, no test required Sand and Oust 12.0 Equipment identified as C::ategory X, no test required Fungus 13.0 Equipment identified as Category X, no test required / Salt Spray 14.0 Equipment identified as C~tegqry X, no test required Magnetic Effect 15.0 •i /• '1. Equipment tested to Class A ! .,, Power Input 16.0 1 ~quipment tested to Category B Voltage Spike 17.0 Equipment tested to Category B ,_ ... Audio Frequency 18.0 Equlpment tested. to Category B Susceptibility . ' 1. lnduced Signal 19.0 . Equipment tested to Category A Susceptibility Radio Frequency 20.0 Squipment tested to Category T Susceptibility Radio Frequency 21.0 Equipment tested to Category A Emissions 1 •i Lightning Induced 22.0 Equipment identified as Transient éategory X, no test required : Susceptibility ( Lightniug Direct 23.0 Equipment ideotified as Effects Category X, no test required Icing 24.0 Equipment identified as Category X, no t~t required 29 24-62·91

GPS 1 NAV SWITCHING & ANNUNCIATOR PANEL APPENDIX B FAA TSO 1 PMA 1 STC approved Letters for Model AK-950- ( ) 30 24-62·91

TRANSPORT AIRPLANE DIRECTORA TE AIRCRAFT CERTIFICATION SERVICE LOS ANGELES AIRCRAFT CERTIFICATION OFFICE 3960 PARAMOUNT BOULEVARD LAKEWOOD, CALIFORNIA 90712-4137 Arneri-King Corporation Mr. Keith Van 18842 Brookhurst Street Fountain Valley, California 92708 DearMr.Van: Ameri-King Corporation, GPS/NA V Switching and Annunciator Panel, Technical Standard Order C 129a Y our application dated November 7, 1996, requesting the issuance of a Technical Standard Order (TSO) authorization in accordance with the procedural requirements of Federal Aviation Regulation (FAR) Part 21, Subpart O. Based upon your data and statement ofconformance certifying your article(s) has met the requirements of FAR Part 21, Subpart 0, and the minimum performance standards ofTSO C 129a (Ref FAR 21.605), authorization is hereby granted for the following DESCRIPTION AK-950-( ) Series GPS/NAV Switching and Annunciator Panel For your information, the conditions and tests required for TSO approval are minimum performance standards. The article(s) may be installed on or within a specifie type or class of aircraft only iffurther evaluation by the user/installer documents an acceptable installation that is approved by the Administrator The quality control procedures contained in your quality control manual, currently on file at the Phoenix Manufacturing Inspection Satellite Oftice, and your statement that those procedures will be applied to the manufacturer of the subject article(s) at the above address, are considered adequate in accord ance with FAR 2 1 143. Effective this date, your authorization to use TSO procedures is extended to include the subject article(s) Y ou may identity the article(s) with the applicable TSO markings as required by TSO Cl29a. As recipient of this TSO authorization, exceptas provided in FAR 2U(d), you are required ta report any failure, malfunction, or defect in any product or part manufactured by you or your contracted suppliers, and which y ou have determined has resulted or cou Id result in any of the occurrences listed in FAR 21 3(c) The report should be communicated initially by telephone to the Superviser, Technical and Administrative Support Staff, ANM-1 03L, (31 0) 627-5300, within 24 hours after it has been determined the failure has occurred, and followed up with a written notice. FAA Form 8010-4 (Malfunction or Defect Report) or other appropriate format is acceptable in transmitting the required details. As required by FAR 21.613(b), you must also notity the FAA when you no longer manufacture a TSO approved article This authorization pertains only ta manufacturing operations at the above address This office must be notified in ad vance of any proposed facility relocation to preclude interruption while awaiting quality control approval ofthat fàcility Sincerely, , .. Michael Murphy, Manager, Technical and Administrative Support Staff ANM-IOJL 24-62·91