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

Down load Cont.(' Strength of the welded joint. The weld area is .176" x .176" x .25" Shear Stress of weld for a 6061-T6 material : 9,000 psi (ref. Lockheed weld design manual). P. = Area x Shear Stress T .707 S en' \2G . Area =tx L • 11 6" P = [(.707 x .176 x .25)1 x 9,000 = 280 lbs weld strength

date work completed.) 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKE/MODEL/DESCRIPTION STATION 622-7293-101 3 Collins VHF-422b Comm C37c, C38c 450.0 2. The following equipment was installed in the aircraft. • PART NUMBER QTY MAKE/MODEL/DESCRIPTION ISO ,j= S

Model CL-600-2B16 and -2Al2 series airplanes: iJ I British Aerospace Model 125-800A: Gulf:stream Model Gil, GLIB. GIII. and GIV series airplanes- Lockheed Model L-1011 series airplanes; McDonnell Douglas Model DC-9-10, -20, -30-, -40, and -50; DC-10-10, -15..30. and -444 ;It s MD-11: and DC-9-80 series

..7.- MACH ADC Marin Alespeec indicator AIRSPEED INDICATOR - TRUE N Tree Airspeed Indicattre16:' AUTOMATIC DIRECTION FINDER .Oval Col1Inv0P-20 Collins 51W .A0F Receiv4r1,:- CollIAS 614L-I3 Oval AOt pilteo Remote:MagOdtic• Indicator ' AUTOMAT It'll' ILOT . . Sperry SP-Su:Autopilot , • BATTERY,

2176-601 1 each Collins ONE-40 Interrogator . 622-1233 .0001 2 each Collins 390R-20 0141 Mount . . . . 2 each each FLIGHT DATA RECORDER • Lockheed LAtolgo Flight Data Recorder. 1 each ,.FLIOHT eIRECTOR • Collins 614E-228 Remote Slewing.Control 192.6221-004 2 each Collins 614E-23R Mode Sele