Epstein Secrets

k and date work completed.) Modified the existing Third Comm & Nat Systems by removing the Gables G6860-09 Conun/Nav Control Head, and installing a Collins CTL-23 Digital Control Head, P/N 622-9851-001. The third Comm / NAV system's interface was retained as previously installed with the exception of th

cord. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished - • . (It more space is required, attach additional sheets. Identify withaircralt nationality and registration mark and date work comp

5.1353 (aXe) Based on 14 CFR §§ 21 115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Collins Profile 21 FMS-6100 with LPV Approach enabled and UASC TAWS was determined to be TCDS Al 6SW and the following later regulations: AmdclOriginall

rd An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished (amore space is required. meal adoVthanai sheets. ?dismay Mthilifera nalionlgeY and regisrmtion mad( and date wadi aombraterl) USA N49

AVOliCS Callenlien Center 400 Collins Road NE Mad Station 164100 Cedes Rapids. IA 52498 Tel. 319295.2185 Fax 319 295O337 Rockwell Collins May 14, 2003 W0030737.DOC Flight Options 26180 Curtiss-Wright Parkway Cleveland, 011 44143 Tel: (216) 797-3500 Attention: Subject: Mr. Jody

cord. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date work accomplish

ing Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VORIDME from the Collins No. 1 and No. 2 VORIDME systems in accordance with manufacture's InstalatIon and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or lat

cord. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration math and date work accomplish

y additional aircra performed using this STC. My fax number is data before we can authorize additional installations. (s) to me for installations Collins needs to receive this EFTA00012069 % % a ..) EFTA00012070 ••• Flight Options STC ST00881WI-D May 14, 2003 Page 3 WO030737.DOC Flight Op

cord. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. B. Description of Work Accomplished (If more space is required, attach additional sheets, Identify with aircraft nationality and registration mark and date worn accomplish