RAMON LUCAS TORRES
Pilots at 158 St, Miami, FL
License number
Florida A2209027
Issued Date
Nov 2015
Expiration Date
Nov 2017
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
17705 SW 158Th St, Miami, FL 33187
Professional information
Senior Accountant At Padro &Amp; Company, P.a.
Position:
SENIOR ACCOUNTANT at PADRO & COMPANY, P.A.
Location:
Miami/Fort Lauderdale Area
Industry:
Accounting
Work:
PADRO & COMPANY, P.A.
-
SENIOR ACCOUNTANT
Ramon Torres - Miami, FL
Work:
WALGREENS
Pharmacist
Pharmacist
Education:
COLUMBIA UNIVERSITY, - New York, NY
BS PHARMACY in SCIENCE;PHARMACY
BS PHARMACY in SCIENCE;PHARMACY
Skills:
management;supervise help;ordering;inventory checkup;communication with patients;computer operation;physician consultation;
Electrician At Paul Marineau, P.a.
Position:
electrician at Paul Marineau, P.A. (Sole Proprietorship)
Location:
Miami/Fort Lauderdale Area
Industry:
Management Consulting
Work:
Paul Marineau, P.A.
-
electrician
Aircraft Lock For Radios, Power Controls, And Flight Controls And Method
US Patent:
5082213, Jan 21, 1992
Filed:
Jul 10, 1990
Appl. No.:
7/551626
Inventors:
Ramon L. Torres - Miami FL
International Classification:
B64C 1314
US Classification:
244224
Abstract:
The use of a center lock bar which telescopingly receives two telescoping arms, each of which has a control column or shaft grip on its remote end is disclosed. The arms are secured to the parallel control columns by at least one gust lock pin. Provision is made for a throttle mixture lock plate to be secured to the lower portion of the radio lock pan which, in turn, has essentially parallel sidewalls with opposed openings through which the center lock bar passes. Optionally folding extension radio lock pans may be employed for a double stack installation. Finally, means are provided in the form of a lock, whether padlock or internally mounted, to lockingly secure the center lock bar to the two telescoping arms. The method of the invention looks to providing a lock for radios, throttles, and gust locks in a dual control aircraft by stabilizing the two control columns by means of a telescoping member which can accommodate differences in the distance between the parallel control columns of the aircraft. The step in addition to the foregoing of locking is done by securing at least one pin to one of the parallel control columns, and thereafter mounting a central radio stack and throttle control centrally of the central portion of the lock.