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Mark A Gast

from Fulton, MO
Age ~68
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Also known as:
Mark Alan Gast, Mark M Gast, Mark A Cast, Matt Gast
Phone and address:
4475 Richland Heights Rd, Hams Prairie, MO 65251
Related to:
Cindy L Schiro, 67Deborah J Gast, 56Gerald W O'Bryan, 81Mary Jane Kraska, 56Angela J Anderson, 55Billy C Schiro, 69Cynthia L O'Bryan, 59
Connected to:
Allen J Gast, 49Barbara J Gast, 82Bart S Gast, 58Christie L Gast, 37Danny D Gast, 76Edward Gast, 105Elena M Gast, 32Joelyn L Gast, 76Laurie M Gast, 63Mark R Gast, 74

Mark Gast Phones & Addresses

  • 4475 Richland Heights Rd, Fulton, MO 65251
  • 7727 Silver Dr, Fulton, MO 65251
  • 993 Huntington View Dr, Ballwin, MO 63021
  • Houston, TX
  • Saint Louis, MO

Resumes

Resumes

Mark Gast Photo 1

Branch Manager

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Location:
Benton, IL
Industry:
Banking
Work:
American Bank of Missouri
Branch Manager
Mid Nation Mortgage Corporation Dec 2011 - Jul 2012
Branch Manager
Allied Home Mortgage Jun 1999 - Nov 2011
Branch Manager
Union Home Mortgage Corp. Jun 1999 - Nov 2011
Branch Manager
Skills:
Loan Origination
Fha
Mortgage Lending
Mortgage Banking
Loans
First Time Home Buyers
Usda
Real Estate
Government Loans
Investment Properties
Residential Mortgages
Banking
Refinance
Credit
Underwriting
Mortgage Underwriting
Residential Homes
U.s. Federal Housing Authority
Real Estate Transactions
Management
Relocation
Reverse Mortgages
Certified Mortgage Planning
Construction Loans
Credit Analysis
Fha Financing
Va Loans
Working With First Time Home Buyers
Va
Conventional
Mortgage
Purchase
Mark Gast Photo 2

Branch Manager

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Location:
Columbia, MO
Industry:
Real Estate
Work:
Allied Home Mortgage
Branch Manager
Mark Gast Photo 3

Mark Gast

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Mark Gast Photo 4

Mark Gast

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Mark Gast Photo 5

Mark Gast

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Mark Gast Photo 6

Mark Gast

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Business Records

Name / Title
Company / Classification
Phones & Addresses
Mark Gast
Manager
Allied Home Mortgage Capital Corporation
Mortgage Banker/Correspondent · Mortgage Broker · Real Estate Credit · Individual and Family Services
108 Saint Louis Ave, Hams Prairie, MO 65251
2625 Fairway Dr #A, Fulton, MO 65251
(573) 592-8900

Publications

Us Patents

Autopilot/Flight Director Underspeed Protection System

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US Patent:
58365460, Nov 17, 1998
Filed:
Jan 10, 1997
Appl. No.:
8/782507
Inventors:
Mark E. Gast - Seabrook TX
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C 1316
B64C 1308
G05D 0100
G05D 0108
US Classification:
244 76B
Abstract:
An underspeed protection system for an aircraft under autopilot control selects a target speed based upon the greater of a minimum maneuver speed and a stick shaker speed. The system then compares a monitored speed to the target speed to produce an error signal. The system also monitors vertical speed to determine if tie aircraft begins to descend. If the error signal due to the underspeed condition causes the aircraft to descend, the system provides a hold zero vertical speed signal in place of the error signal such that the aircraft seeks to maintain its altitude. The hold zero vertical speed signal overrides the underspeed error signal such that the aircraft does not pitch forward to seek an increased speed.

Autopilot/Flight Director Underspeed Protection System

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US Patent:
57463921, May 5, 1998
Filed:
May 15, 1995
Appl. No.:
8/441468
Inventors:
Mark E. Gast - Seabrook TX
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C 1308
G05D 100
G05D 108
US Classification:
244 76B
Abstract:
An underspeed protection system for an aircraft under autopilot control selects a target speed based upon the greater of a minimum maneuver speed and a stick shaker speed. The system then compares a monitored speed to the target speed to produce an error signal. The system also monitors vertical speed to determine if the aircraft begins to descend. If the error signal due to the underspeed condition causes the aircraft to descend, the system provides a hold zero vertical speed signal in place of the error signal such that the aircraft seeks to maintain its altitude. The hold zero vertical speed signal overrides the underspeed error signal such that the aircraft does not pitch forward to seek an increased speed.

Autopilot/Flight Director Overspeed Protection System

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US Patent:
58331778, Nov 10, 1998
Filed:
May 15, 1995
Appl. No.:
8/441685
Inventors:
Mark E. Gast - Seabrook TX
Assignee:
The Boeing Company - Seattle WA
International Classification:
G05D 100
US Classification:
244195
Abstract:
An aircraft overspeed protection system produces proportional and integral commands for input to an autopilot controlling the aircraft. The proportional and integral commands are produced by comparing actual monitored speed of the aircraft with a target speed from a target speed selector. The target speed selector selects as the target speed a trigger speed above a nominal maximum operating airspeed of the aircraft until the trigger speed is reached by the aircraft. When the trigger speed is reached by the aircraft, the overspeed control goes into Overspeed Protect Command active mode and the target speed selector selects a new target speed below the nominal maximum operating speed of the aircraft. The overspeed protection system remains in Overspeed Protect Command active mode until the pilot takes a positive action by selecting a new autopilot mode or by disengaging the autopilot. To accommodate for a reduced effectiveness of the overspeed protection system at severe roll angles, the overspeed proportional and integral commands are weighted by a weighting factor that is a function of the measured roll angle of the aircraft.

Autopilot/Flight Director Stall Protection System

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US Patent:
58034080, Sep 8, 1998
Filed:
May 15, 1995
Appl. No.:
8/441683
Inventors:
Mark E. Gast - Seabrook TX
Assignee:
The Boeing Company - Seattle WA
International Classification:
B64C 1316
US Classification:
244178
Abstract:
In an aircraft under autopilot control, a stall protection system overrides established autopilot parameters in response to a monitored angle of attack for the aircraft exceeding a trigger angle of attack. The trigger angle of attack is established with reference to a stick shaker angle of attack for the aircraft. When the aircraft exceeds the trigger angle of attack, the stall protection system produces an error signal causing the autopilot to seek an angle of attack 1 degree below the stick shaker angle of attack. Initially, the stall protection system provides a boost command to the error signal to accelerate the response of the aircraft to the error signal. The boost command is produced by a driving signal generator that selects one of four driving signals in response to monitored flap angle and impact pressure.
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Mark A Gast from Fulton, MO, age ~68 Get Report