Garside'S Aircraft & Engine Parts & Svc INC
Holds 32 approved modifications. FAA spelling: Garside's Aircraft & Engine Parts & Svc Inc.
Approved modifications 32 · newest first
1984-02-01SA4-281 · Horizontal stabilizer angle of incidence change. · Lockheed 18
1984-02-01SA4-58 · Oil tank assembly for increased oil supply. · Lockheed 18
1984-02-01SA4-732 · Alternate fuel source on aircraft with Wright Cyclone engines with flow meter installation. · Lockheed 18
1984-02-01SA4-59 · Cockpit seats. · Lockheed 18
1984-02-01SA4-274 · Outer wing fuel tanks, revised fuel system, change in angle of incidence of horizontal stabilizer one degree and... · Lockheed 18
1984-02-01SA4-155 · Sperry Model A-12 automatic pilot installation modification. · Lockheed 18
1984-02-01SA4-29 · Radar nose for Bendix C-Band, Bendix X-Band or RCA C-Band. · Lockheed 18
1984-02-01SA4-256 · Horizontal stabilizer angle of incidence change and modified stabilizer tips, wing and flap trailing edge. · Lockheed 18
1984-02-01SA4-264 · Two Jato motors 15KS-1000A1 in fuselage. · Lockheed 18
1984-02-01SA4-1552 · Pittsburgh Plate Glass Company electrically-heated windshield. · Lockheed 18
1984-02-01SA4-136 · Wright R-1820-56A, -66, -72A engines, modified rudder spring mechanism and tab, elevator spring tab, retractable... · Lockheed 18
1984-02-01SA4-273 · Installation of heat-shroud, propeller anti-icing alcohol tank, and modified DC-3 exhaust system. · Lockheed 18
1984-02-01SA4-257 · Picture window. · Lockheed 18
1984-02-01SA4-1010 · Autolite generator 2CM70B9 on Wright engines R1820-56A, -66, and -72A. · Lockheed 18
1984-02-01SA4-275 · Installation of PacAero wing tip. · Lockheed 18
1984-02-01SA4-366 · Horizontal stabilizer tip, rudder spring tab, Learstar tail cone, elevator spring tab, Goodyear wheels and brakes,... · Lockheed 18
1984-02-01SA4-71 · Rudder spring tab assembly. · Lockheed 18
1984-02-01SA4-307 · Lear L-102A automatic pilot. · Lockheed 18
1984-02-01SA4-171 · Approval to use 1,350 hp for takeoff with Wright R1820-56A, -66 and -72A engines and 1,300 hp, with Wright R-1820-56... · Lockheed 18
1984-02-01SA4-738 · Modification to 'Learstar' (NOTE12 of Aircraft Spec A-723) except installation of Wright R1820-56A, -66, or -72A... · Lockheed 18
1984-02-01SA4-715 · Westinghouse air brake AH-5 decelostat anti-skid unit. · Lockheed 18
1984-02-01SA4-283 · 60154 stabilizer tip. · Lockheed 18
1984-02-01SA4-1317 · Gross weight modification including: increase power, installation of two JATO motors, outer wing tank, and Goodyear... · Lockheed 18
1984-02-01SA4-130 · Horizontal stabilizer incidence angle change to one degree. · Lockheed 18
1984-02-01SA4-838 · Sperry A-12 autopilot. · Lockheed 18
1984-02-01SA4-1138 · Gross weight modification including: increase power, installation of Goodyear wheels and brakes, two JATO motors,... · Lockheed 18
1984-02-01SA4-368 · Picture window. · Lockheed 18
1984-02-01SA4-425 · Modification per STC SA4-69 except gross weight modification per Dwg. 600030B, engine per Dwg. 606399 and DCN-1,... · Lockheed 18
1984-02-01SA4-131 · Drag reduction fairing addition. · Lockheed 18
1984-02-01SA4-644 · Lear L-5B autopilot. · Lockheed 18
1984-02-01SA4-1014 · Radio shelf structure No. 1 baggage. · Lockheed 18
1984-02-01SA47WE · Interior and equipment installation. · Lockheed 18
Source: FAA Dynamic Regulatory System (type certificate data sheets, supplemental type certificates, technical standard order authorisations). An organisation's name is as the FAA spelled it on each record; related spellings are separate pages.