Staggerwing Museum Foundation INC.
Holds 123 approved modifications, most of them for the Beechcraft TC-45. FAA spelling: Staggerwing Museum Foundation Inc..
Approved modifications 123 · newest first
Beechcraft TC-45 69Beechcraft C-45 28Beechcraft D18 26Beechcraft E18 26Beechcraft C18 20Beechcraft UC-45 15Beechcraft G18 2
2008-10-06SA4-32 · Internal combustion heaters. · C18S, D18S, E18S
2006-10-06SA2-213 · Installation of modified wing tips. · Army AT-11, C18S, C-45G
2006-10-06SA2-725 · Installation of oil cooler, G & O Mfg. Co. #E703, modified with Fullerton Syphon DV5 thermostat. · Army AT-11, C-45G, C-45H
2006-10-06SA2-625 · Delete righthand rudder tab and system; install rudder control system bungee and shut-off valve. · C-45G, C-45H, TC-45G
2006-10-06SA31SO · Tricycle landing gear and revised nose assembly with optional radome. (Model may also be designated as Conrad 10,200.) · C-45G, C-45H, D18S
2006-10-06SA2-338 · Installation of two (2) 25,000 BTU Janitrol Heaters installed one (1) in each wheel well. · C18S, D18S
2006-10-06SA53CE · Stewart-Warner heater 940B/24 in fuselage. · C18S, C-45G, C-45H
2006-10-06SA4-113 · Safety performance kit, increase gross weight to 9,000 lbs. takeoff and landing. Installation of P&W R-985-AN10,... · C-45G, C-45H, D18S
2006-10-06SA2-820 · Increase in take-off weight to 9800 pounds, and increase in landing weight to 9400 pounds, when P&W R-985-AN14B;-AN4... · C-45G, C-45H, D18S
2006-10-06SA2-383 · Raise horizontal stabilizer and installation of elevator seal assembly. · C-45G, C-45H, D18S
2006-10-06SA2-621 · Installation of Hartzell propellers, Model HC-93Z30-2C, -2D/10152-5 1/2, or HC-B3Z30-2D/10152-5 1/2. · C-45G, C-45H, E18S-9700
2006-10-06SA2-1261 · Install Fiberglas bubble tail wheel enclosure doors (enclosing entire wheel). · Army AT-11, C18S, C-45G
2006-10-06SA4-152 · Two Model 940 Stewart-Warner heaters, install one in each wheel well. · C-45G, C-45H, D18S
2006-10-06SA2-523 · Revise horizontal stabilizer angle of incidence from -3.6 degrees to-0.5 degrees. · Army AT-11, C18S
2006-10-06SA138SO · D18S landing gear 404-188400 on C18S. · C18S
2006-10-06SA4-119 · Revised horizontal stabilizer angle of incidence from -2 degrees to -1/2 degrees. · C-45G, C-45H, D18S
2006-10-06SA3-732 · Full-view passenger window. · D18C-T, C18S, C-45G
2006-10-06SA4-21 · Fuel system modified to provide dual wobble pumps and suction crossfeed and attendant plumbing. · Army AT-11, C18S
2006-10-06SA2-623 · Approval of existing installation of47 gallon nose fuel tanks. · C-45G, C-45H, TC-45G
2006-10-06SA4-120 · Dual airspeed system. · Army AT-11, C18S, C-45G
2006-10-06SA4-128 · Engines, propellers, revised nacelles, wheel-well doors, air- speed system, fuel system and elevator seal strips. · Army AT-11, C18S
2006-10-06SA2-328 · Installation of Hartzell propeller unfeathering crossfeed system. · Army AT-11, Navy SNB-1, C18S
2006-10-06SA2-993 · Installation of P&W R-985 Fuel Injection Engines, as modified by STC SE1-391. · E18S, E18S-9700
2006-10-06SA2-204 · Installation of one-peice windshield and flush cockpit side-windows. · Army AT-11, C18S, C-45G
2006-10-06SA2-280 · Increase in take-off weight to9800 pounds, and increase in landing weight to 9400 pounds, when P&W R-985-AN14B, or... · E18S, E18S-9700
2006-10-06SA3-383 · Beech D18S Goodyear wheels and brake assembly. · C18S
2006-10-06SA4-34 · Main landing gear door. · Army AT-11, C18S, C-45G
2006-10-06SA1-398 · Pratt & Whitney R-985 engine installation with Simmonds Aero- cessories 580047 fuel injector · C-45G, C-45H, D18S
2006-10-06SA24CE · Oval passenger windows. · D18C-T, C18S, C-45G
2006-10-06SA249SO · Increase in takeoff weight to10,200 lbs. and landing weight to9,800 lbs. and extension of aft C.G. limit to (+120.5)... · Army AT-11, C18S
2006-10-06SA2-1246 · Increase in take-off Gross Weight to10,200 pounds and landing weight to9800 pounds. Extension of Aft. C.G. limits to... · C-45G, C-45H, D18S
2006-10-06SA2-622 · Approval of existing Jack and HeintzA3A autopilot installation. · C-45G, C-45H, TC-45G
2006-10-06SA1-427 · Pratt & Whitney R-985 engine installation with Simmonds Aero- cessories 580047 fuel injector per STC SE1-391, and... · C-45G, C-45H, D18S
2006-10-06SA27SO · Increase in landing weight to 9800 lbs. and extension of Aft. C.G. limits to +120.5. These limitations applicable to... · C-45G, C-45H, D18S
2006-10-06SA2-1230 · Installation of extended tail wheel assembly. · Army AT-11, C18S, C-45G
2006-10-06SA2-992 · Installation of P&W R-985 Fuel Injection Engines, as modified by STC SE1-391. · C-45G, C-45H, D18S
2006-10-06SE1-391 · Pratt & Whitney R-985 engine and ATI fuel injection. · R-985 Series
2006-10-06SA814SO · Installation of wing spar strap Kit No. K7312. · 18D, A18A, A18D
2006-10-06SA2-1016 · Recertification under subparts B &G of CAR 3 and installation of SA4-120 airspeed system, SA4-21, fuel system, and... · C18S
2006-10-06SA2-686 · Installation of Fiberglas Nose. · C-45G, TC-45H, TC-45G
2006-10-02SA2437WE · Modifications for increase in maximum weights. · 3N, 3NM, 3TM
2005-08-13SA4-769 · Cambridge fuel air ratio analyzers. · C-45G, C-45H, D18S
2005-08-12SA3471WE · Modification for increase in maximum weight approved for model E-18S, serial number BA20. · E18S
2005-08-12SA289WE · Carburetor air scoops. · C-45G, C-45H, D18S
2005-08-12SA4-1299 · Voltage regulators moved to front side of forward bulkhead. · C-45G, C-45H, TC-45G
2005-08-12SA4-1198 · Aft bulkhead removal. · Army AT-11, C18S, C-45G
2005-08-12SA4-1035 · Modification of door frame between cabin and cockpit for installation of folding door. · C-45G, C-45H, D18C
2005-08-12SA2414WE · Modification for increase in maximum weights. · D18C, UC-45J (SNB-5), JRB-6
2005-08-12SA3-632 · Beech Kit 581-1, except angle of incidence change (Item 602) and stall strips (Item 607c) of Spec. A-765; with STC... · C-45G, C-45H, D18S
2005-08-12SA4-718 · Installed auxiliary nose fuel tanks per American Turbine Engine Company Drawing B-3, Sheet 1, Sheet 2 and Sheet 3. · C-45G, C-45H, D18S
2005-08-12SA4-1595 · Installed American Turbine Engine Co. drawing B-138 divan. · C-45G, C-45H, D18C
2005-08-12SA4-1368 · Replaced Airline Training Company L-12001B wing tips with American Turbine Engine Company wing tips · C-45G, C-45H, D18S
2005-08-12SA548WE · Air stair door. · C-45G, C-45H, D18S
2005-08-12SA4-1536 · Picture window G18 type. · C-45G, C-45H, D18S
2005-08-12SA332WE · Propeller spinners and increase in maximum continuous power to 450 hp. · C-45G, D18S, TC-45G
2005-08-12SA4-1486 · Additional seats. · C-45G, C-45H, D18C
2005-08-12SA4-1256 · Installed astrodome. · TC-45G, TC-45H
2005-08-12SA4-1116 · Three additional windows. · C-45G, C-45H, D18C
2005-08-12SA3-358 · Airplane and powerplant modifications related to civil conversion. · C-45G, C-45H, TC-45G
2005-08-12SA290WE · Main landing gear doors. · C-45G, C-45H, D18C
The first 60 of 123.
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.