Epstein Secrets

nt Administrator BY to the authority given persons specified below, the unit dentified in item 4 was inspected In the manner prescribed by the of the Federal Aviation Administration and is 0 APPROVED O REJECTED FM Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FM Designee X Repair Station

SITION AND OTHER NAVIGATION INFORMATION FROM THE NO. 1 UNS- ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF" INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH, PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES

Approval for Return To seniadlit4e ce Pursuant Administrator BY to the authority given persons specified below, the unit identified in item of the Federal Aviation Administration and is El APPROVED 4 was inspected in the manner prescribed by the REJECTED • FAA Flt. Standards Inspector Manufactora Inspection Authorizati

, &trash addltionatsheals. Identify with aircraft nationality and registration mark and date work completed.) REMOVED THE FOLLOWING EQUIPMENT: 2EA. HONEYWELL DIGITAL AIR DATA COMPUTERSP/N 7000700-962. INSTALLED THE FOLLOWING EQUIPTMENT: 2 EA. HONEYWELL DIGITAL AIR DATA COMPUTERS P/N 7000700-662 WITH STAT

tor. x,I.Z.-- L/C-6 -- , 7. Approval for Return to Sery Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 Was inspected in the manner prescribed by the K REJECTED Cs APPROVED FM Flt. Standards Inspector Manufacturer Insp

OSITION AND OTHER NAVIGATION INFORMATION FROM THE NO. 1 UNS-ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF' INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH, PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES

nspector. 16, U -V 7. Approval for Return to Service k Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 was inspected in the manner prescribed by the K REJECTED C4 APPROVED FAA Flt. Standards Inspector Manufacturer Ins

& RECEIVER / TRANSMITTER UNIT P/N 7012640-902 AND INSTALLED NEW WU- 880 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7021450-801 (TSO C63c). INSTALLED A HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM CONSISTING OF AN LP-860 PROCESSOR P/N 7011822-904 (TSO C110) AND AN AT-855 ANTENNA PIN 7014062-901 (TSO C110). THE

ursuant to the authority given persons specified below, th Oriitlid fie in item 4 was inspected in the manner prescribed by the •. Administrator of the Federal Aviation Administration and is. Q APPROVED 0 REJECTED ; ', ..- ! 1 0%,......"• O. BY FAA Flt Standards inspector Manufacturer Inspection Authorization Other (Spec

attach additional.sheets. Identify with aircraft nationality and registration mark and date work completed.) REMOVED THE FOLLOWING EQUIPTMENT; 2EA. HONEYWELL DIGITAL AIR DATA COMPUTERSP/N 7000700--962. INSTALLED THE FOLLOWING EQUIPTMENT: 2 EA. HONEYWELL DIGITAL AIR DATA COMPUTERS P/N 7000700-662 WITH STA

dividual Glenn Tietjen 7. Approval for Return to Service Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 was inspected in the manner prescribed by the APPROVED • REJECTED FAA Flt. Standards Inspector Manufacturer Inspe

ER AIRCRAFT EQUIPMENT. NO WIRING OR STRUCTURAL ALTERATIONS WERE ACCOMPLISHED. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER HONEYWELL MST67A MODE S TRANSPONDER SYSTEM MANUAL 006-00681-0006 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: G2B-20895-080 WAS CONDUCTED AND THE INSTALLE