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Document Mentions (4 shared documents)
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NO. 34-60-21. DATED 19 MARCH 200) writ NO DISCREPANCIES NOTED. AN EMI TEST. REPORT NO.: 8727.16236-080 REV IR. SHEETS I OF 5. DATED 06/19/2001. WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY CANER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMP
M approved Airplane Flight Manual 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 (I
2 mentions1 same-page
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AL NO. 5003. REVISION 03.07. DATED JULY 10, 1995 WITH NO DISCREPANCIES. AN EMI TEST. REPORT NO.: B727-16236-080 REV IR, SHEETS 5. DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMP
M approved Airplane Flight Manual 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 (I
2 mentions1 same-page
Page ?Same page
AL NO. 5003, REVISION 03.07, DATED JULY 10, 1995 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMP
A approved Airplane Flight Manual 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 (I
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2 mentions1 same-page
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S ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: B727-16236-080 REV IR, SHEETS 5, DATED 06/19/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER INSTALLED EQUIPMENT. MAGNETIC DIRECTION INDICATORS WERE CHECKED FOR ACCURACY AND COMP
A approved Airplane Flight Manual 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 (I
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Mutual Connections (186)
Entities connected to both CONDUCTED and Management Systems
RM
Registration Mark
PERSON5 w/ CONDUCTED·4 w/ Management
JU
John K. Urso
PERSON5 w/ CONDUCTED·4 w/ Management
the Federal Aviation Administration
ORGANIZATION5 w/ CONDUCTED·4 w/ Management
Samantha Power
PERSON5 w/ CONDUCTED·4 w/ Management
JEGE INC.
ORGANIZATION4 w/ CONDUCTED·4 w/ Management
Frequency Management
ORGANIZATION4 w/ CONDUCTED·4 w/ Management
Lake City
LOCATION4 w/ CONDUCTED·4 w/ Management
DERT-810028-NE
ORGANIZATION4 w/ CONDUCTED·4 w/ Management
DER Services
ORGANIZATION4 w/ CONDUCTED·4 w/ Management
Ghislaine Maxwell
PERSON6 w/ CONDUCTED·2 w/ Management
George W. Bush
PERSON5 w/ CONDUCTED·3 w/ Management
Triple Honeywell Inertial Reference Sensors
ORGANIZATION4 w/ CONDUCTED·4 w/ Management
UNIVERSAL AVIONICS CORP.
ORGANIZATION4 w/ CONDUCTED·3 w/ Management
K Additional Sheets Are Attached
ORGANIZATION4 w/ CONDUCTED·3 w/ Management
RB
Ronald K. Bystrom
PERSON4 w/ CONDUCTED·3 w/ Management
Servl
LOCATION4 w/ CONDUCTED·3 w/ Management
THE STATIC LOADING OF THE INSTALLED EQUIPMENT MEETS THE REQUIREMENTS OF AC
ORGANIZATION4 w/ CONDUCTED·3 w/ Management
CLASSIFICATION(S
ORGANIZATION4 w/ CONDUCTED·3 w/ Management
HONEYWELL
ORGANIZATION4 w/ CONDUCTED·3 w/ Management
UNS-1D Flight Management System
ORGANIZATION4 w/ CONDUCTED·3 w/ Management