Epstein Secrets

1041 SEE REVERSE SIDE NSN; 0052.00.6934000 EFTA00011755 A A This airworthiness certificate is issued under the authority of Public Law 104, 49 United Slates Code" (USC) 44704 and Title 14 Code of Federal Regulations (CFR), aB The ainuorthiness ceifificale authorizes the manufacturer named on the reve

radols are performed in accordance wit Pat 21, 43, and 91 of the Federal Aviation Regulations, as appropriate, and the ate is relisleted ih to Utd States. DATE OF ISSUANCE DESIGNATION NUMBER R3/06/2014 GL-25 Arty allergen, reprodudon, Of misuse of Oils rdicale may be puhishab'e by a fine rId we

ociated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins FMS-6100, Localizer Performance with Vertical Guidance (LPV) approach capability and Universal Avionics System Company (UASC) Terrain Awareness Warning System (TAWS)

PROPELLER O APPLIANCE Two Manufacturer S ConfomiltyStetement A. Agencys Name and Address B. Kind Of Agency tams Bergen Ak ServkeASok•OMplen U. S. densidned wawa I Manufacturer Ads.“ SS Or I ma vein Foreman Commend mechanic C. Certificate No. Cry ft isethedels ore' FL x Cortietled Seate

ia of Advisory Circular AC 20-130A and AC 25-15. Satellite navigation data is based upon use of only the Global Positioning System (GPS) operated by the United States. Additionally, Russian GLONASS satellites provide increased accuracy but are not used for integrity or Receiver Autonomous Integrity Monitoring (RAI

8JE BOEING 20115 3) Press the APP-65A Autopilot Control Panel [AP ENG]-button to couple the AP to the selected FD. The Autopilot will track pseudo-Localizer and pseudo-Glidesbpe signals from the FMS. b. Advanced Approach Operations 1) Advanced approaches may be identified in the data base by the prefi

ia of Advisory Circular AC 20-130A and AC 25-15. Satellite navigation data is based upon use of only the Global Positioning System (GPS) operated by the United States. Additionally, Russian GLONASS satellites provide increased accuracy but are not used for integrity or Receiver Autonomous Integrity Monitoring (RAI

8JE BOEING 20115 3) Press the APP-65A Autopilot Control Panel [AP ENG]-button to couple the AP to the selected FD. The Autopilot will track pseudo-Localizer and pseudo-Glideslope signals from the FMS. b. Advanced Approach Operations 1) Advanced approaches may be identified in the data base by the pref