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ice; Avionics Division work order #71301 completed on October 4, 2006. A. Installed an AirCell Iridium Antenna P/N S67-1575-109 in accordance with DER Services drawing number 2006-173-1 approved per FAA form 8130-3 signed by Robert Belgau DERT designation number DERT-510024-CE. B. The above installation
al when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors,
oved 2) This approval is valid for the aircraft model and serial number listed below 3) This approval is based on structural analysis on file at DER Services corporate office in Ft. Lauderdale, TV. Model No. B727-3I Serial No. 20115 PURPOSE Approve data for antenna installation (Structures Only) OF
al when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors,
ice; Avionics Division work order #71301 completed on October 4, 2006. A. Installed an AirCell Iridium Antenna P/N S67-1575-109 in accordance with DER Services drawing number 2006-173-1 approved per FAA form 8130-3 signed by Robert Belgau DERT designation number DERT-510024-CE. The above installation was
al when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors,
2. aspects only of the above listed data are approved is valid for the aircraft model and serial number is based on structural analysis on file at DER Services office in Ft. Lauderdale, FL. No. B727-31 Serial No. 20115 1) The structural herein. 2) This approval listed below 3) This approval cor
al when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors,
Entities connected to both DER Services and Frequency Management

Samantha Power
PERSONCONDUCTED
ORGANIZATIONManagement Systems
ORGANIZATIONTriple Honeywell Inertial Reference Sensors
ORGANIZATIONDERT-810028-NE
ORGANIZATIONJEGE INC.
ORGANIZATIONLake City
LOCATIONJohn K. Urso
PERSONRegistration Mark
PERSONthe Federal Aviation Administration
ORGANIZATION
HONEYWELL
ORGANIZATIONRonald K. Bystrom
PERSONLee Wagener Blvd
PERSONCLASSIFICATION(S
ORGANIZATIONCurran
PERSON
George W. Bush
PERSONL. Palm
PERSONUNIVERSAL AVIONICS CORP.
ORGANIZATION
United States
LOCATIONTHE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC
ORGANIZATION