Beech 17 Staggerwing Parts Catalog
Beechcraft D17S Staggerwing · Parts Catalog
Overview
This document serves as a parts catalog for the Beechcraft D17S Staggerwing and its variants. It provides detailed information on the various models of the Staggerwing, including specifications, powerplants, and design features. The catalog is intended for maintenance personnel, pilots, and aviation enthusiasts interested in the historical and technical aspects of the Beechcraft Staggerwing series. It outlines the evolution of the aircraft from its inception in the early 1930s through its various configurations and modifications over the years, highlighting the unique characteristics that distinguish each model.
- Model: Beechcraft D17S Staggerwing
- Powerplant: Pratt & Whitney R-985, 450 hp
- Wingspan: 34 ft 6 in
- Maximum Speed: 250 mph
- Service Ceiling: 20,000 ft
- Climb Rate: 2,000 ft/min
- Maximum Takeoff Weight: 5,200 lb
Document
Source
Originally published by www.aeroresourcesinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Parts Catalog
- Year
- 1981
- Pages
- 3
- File size
- 2.4 MB
- Publisher
- www.aeroresourcesinc.com
Common. Rarer than 24% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Beechcraft D17S Staggerwing.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the BEECH D17S Staggerwing to your watchlist and track it in one place.
More Beechcraft D17S Staggerwingmanuals & documents
See all 16 →- Emergency Procedures for Beechcraft D17S StaggerwingEmergency Procedures
- Hans Groenhoff Photographic CollectionChecklist
- Aircraft at IWM DuxfordChecklist
- Type Acceptance Report TAR 4/21B/16 – Beech G17SOther Documents
- Airworthiness Directive ScheduleAirworthiness Directives
- Vintage AirplaneOther Documents
- Type Acceptance Report TAR 95/09 — BEECH D17SOther Documents
- VINTAGE AIRPLANEService Bulletins
- Normal Procedures for the Beechcraft D17S StaggerwingNormal Procedures
- VINTAGE AIRPLANEPerformance Data
- Walter H. and Olive Ann Beech CollectionFlight Manual
- The Beech 17Checklist
If you fly the Beechcraft D17S Staggerwing, you may also be researching these.
In this document
Model Overview
The Beechcraft D17S Staggerwing is a biplane known for its distinctive negative stagger wing configuration. It features a 450 hp Pratt & Whitney R-985 engine and has a wingspan of 34 ft 6 in. The aircraft is designed for high performance and luxury, catering to the carriage trade.
Specifications
The D17S has a maximum speed of 250 mph and a service ceiling of 20,000 ft. It can climb at a rate of 2,000 ft/min and has a range of 750 statute miles. The aircraft's empty weight is approximately 3,150 lb, with a maximum takeoff weight of 5,200 lb.
Powerplant Information
The D17S is powered by the Pratt & Whitney R-985 engine, which produces 450 hp at 2,300 rpm. This engine provides the Staggerwing with its notable performance capabilities, making it one of the fastest biplanes of its time.
Design Features
The D17S incorporates several innovative design features, including retractable landing gear and a full NACA cowling that enhances aerodynamics. The aircraft's structure includes a welded steel-tube fuselage and wooden wings, contributing to its lightweight and robust design.
Historical Context
The Beechcraft Staggerwing was introduced during the Great Depression and marked a significant advancement in biplane design. It was one of the first high-performance airplanes available to the public, showcasing Beech's commitment to quality and innovation in aviation.
Full document text
G N I w • 5 \ y Beech 17s A D R E T 5 E The Staggerwing was the first of Beech's carriage-trade designs BY PETER M. BOWERS One of the all-time classic airplanes of American general aviation is the Beechcraft Model 17, universally known as the Stag- gerwing. It is notable on several counts-it was one of the first high-performance air- planes available to the public; it was intro- duced during the Depression and was a con- tinuation of another company's aircraft; it had an unconventional configuration that resulted in an inaccurate but accepted name; and it had a remarkable production longevi- ty for a biplane in the age of the monoplane. The Model 17 originated during the peri- od when many major aircraft production plants were either cutting back, changing the orientation of their product lines or shutting down completely and surrendering to the Depression. By 1932, Walter H. Beech had built an impressive career in aviation. Starting with Swallow Aircraft in Wichita, he quit over a disagreement with the bos~, J.M. Mollen- dick, on design philosophy and became one of the co-founders of the Travel Air Aircraft Company in the same city in late 1924. When the giant Curtiss-Wright conglomer- ate bought Travel Air in 1929, Beech, presi- dent of Travel Air, became a vice president of Curtiss-Wright. With the Depression re- ally under way in 1930, Curtiss-Wright closed its Travel Air division and moved much of the staff and tooling, including Beech, to its St. Louis plant. Here Beech was charged with carrying on some of the Travel Air models and establishing new low-cost models for the greatly reduced market. These did not sell well enough to justify continued production, so the St. Louis plant was closed in 1931. Beech took advantage of this opportunity. He gathered a few of his former employees and founded Beech Aircraft Corporation on April 1, 1932, leasing a portion of the closed Cessna Aircraft plant in Wichita. (Clyde Cessna, who had quit Travel Air over another design dispute with Beech, was one of the three founders of Travel Air and still a good friend.) The object was to build a high-performance, deluxe four- to five- seat cabin biplane for the carriage trade, or what was left of it. Beech and one of his former Travel Air engineers, Ted Wells, had been doodling with the design in their spare time since 1930 and had hoped to get Cur- tiss- Wright to build it as a continuation of the Travel Air line. However, Waco was the major producer of 125- to 250-hp aircraft at that time-the co'mpany already had a near monopoly on the cabin biplane market, with its lower-powered and very boxy but efficient C-series. So, Beech's effort was doubly daring in taking on both the Depres- sion and the solidly established competition. While Model 17 seems an odd number for the first product of a new company, the number was significant to Beech. Model CW-16 was the last of the old Travel Air line that was built in St. Louis and 17 was the next number. When the Curtiss plant reopened a year later, it advertised but did not build its own CW-17 model. But the company did carryon the sequence with Models CW-19 through CW-25. Beech Model 17 was relatively conven- tional in overall structure. The welded- steel-tube fuselage was rounded out with wooden formers and stringers. The wings were rather innovative in using spars built up of steel-tube trusses, but they did retain wood-truss ribs. The fixed tail surfaces were wood, and the movable tail surfaces were steel tubing. The quality of the "Beechcraft finish" on the fabric covering became an in- dustry legend. Access to the four- to five- place cabin was through a large, single door on the left side, with two pilots sharing a throw-over control wheel. The powerplant was the 420-hp Wright R-975-E2 Whirl- wind under a snug NACA cowling. Cooling problems resulted in an odd modification- T7zefirst Beechcraft, the 420-hp Model17R (above), was born in 1932, despite the Depression and the challenges of an established competitor. {ontinued because the face of the cowling was closed, individual airscoops were provided for each of the nine cylinders. Significant design features, actually inno- vations on that class of airplane, were: re- tractable landing gear (introduced on the third airplane built); a full NACA cowling for a variety of radial engines that was inte- grated fully into the lines of the airplane, instead of being an add-on as it had been with most preceding designs; and, eventual- ly, wing flaps. As a biplane, the Model 17 broke with tradition on four major counts. For one, Beech was one of the first biplane designer's to mount the wing directly on top of the fuselage instead of holding it above the fu- selage on struts. (Waco was the only other manufacturer to use this significant advance in streamlining and structural simplification at the time.) The design's relatively high wing loading seemed to call for the use of conventional wing flaps, but Beech came up with something different. To serve as an air brake by adding drag, the rudder was split vertically to open toward both sides but still retain the rudder function. This short-lived innovation appeared only on the first two Model17s built and soon was deleted from one in favor of drag flaps, added to the un- dersurface of the upper wing. The most distinctive feature of the bi- plane was the arrangement of the wings rel- ative to each other. On most biplanes, the upper wing is positioned some distance ahead of the lower in a configuration known as positive stagger. Since the Model 17 eventually was to have retractable landing gear, the only convenient place to mount and stow it was on the lower wing, as in some contemporary low-wing monoplanes. Since the lower wing would be too far aft in positive stagger, the arrangement was re- versed, placing the lower wing ahead in the configuration known as negative stagger. This feature was so conspicuous that the
Show full textShow less
airplane was dubbed the negative-stagger Beech as soon as it appeared. (Actually, the statement was redundant because there was only one Beechcraft model and, therefore, no need for configuration distinction; the simple name "Beechcraft" would have been sufficient.) Since the name was a rather in- convenient mouthful, it soon was shortened in popular usage to Staggerwing, without the distinction as to positive or negative. This quickly became a convenient substitute for the various Model 17 subdesignations when they appeared. Simply say Stagger- wing and everyone knows what airplane you are talking about without needing the manufacturer's name or the model number. A relatively minor feature that contribut- ed to the racy lines of the airplane was a single I wing strut on each side instead of the traditional N struts. These had been used mostly on racers in the past and, there- fore, were associated with speed. The original landing gear were enclosed in large fairings that were referred to as spats. Though the gear appeared to be fixed, they actually were partly retractable. The wheels drew up into the spats slightly, leaving only a small portion projecting. Only four of the first 11 airplanes had this feature, all others had fully retractable gear that folded in toward the belly, flush with the lower wing and center section. Since it was known that the airplane would be tricky on the ground, the tail- wheel was fixed and nested partway into the fuselage. Though a definite asset on takeoff and during the landing roll, it made turns on the ground difficult. This feature was used only on the first two Model 17s and was quickly deleted from one of them. The first Staggerwing, Model 17R, made its initial flight on November 4, 1932. It performed as expected, and work began on a second 17R that differed only in minor de- tail, principally a wider-track landing gear. The third Model 17 was notably different from the previous two models by having fully retractable landing gear, a revised wing-tip shape, a Clark- Y airfoil instead of the Navy N-22 section, solid-wood instead of steel-truss spars and other minor struc- tural refinements. This was the B17 mod- el-the baby of the Staggerwing line with a 225-hp Jacobs L-4 engine. Two more fixed-gear models with the old wing structure but without the split rudder and fixed tailwheel were built as A17s; with 690- to 710-hp Wright Cyclone engines, they were the most powerful of all the Model 17s. Various combinations of drag- flap and aileron locations were used on sub- sequent production Staggerwings. From the D model on, the ailerons were on the upper wing; conventional, full-span flaps were on the lower; the fuselage was lengthened 13 inches; and the airfoil was changed to the NACA 23012. Staggerwing prices ranged from a low of $8,000 for the B17L to nearly $20,000 for the A17s and the 450-hp models D through The third Model] 7 and, first production Beechcraft, Model B] lL, was the baby of the Staggerwing line with the 225-hp Jacobs engine. Many Beech ] 7s were put on floats and acquired the prefix S for seaplane. But this ]936 SCl7B was the only model to have amphibious floats. 130 • OCTOBER 1981 -- PHOTOGRAPHY FROM THE COllECTION OF THE AUTHOR ugely was deter- 19ine. ring which only £he Staggerwing public and real fariety of engine lions resulted in ~istinguished by 19 separate ap- P). (Since there htify individual ated models are C number. See was conceived ,n, World War II incipal custom- ,'937 with one airplane, iden- e Army bought !fied as UC-43, aches in foreign a total of 352 as GB-l and category, plus te owners. The YUC-43s-plus ~nts designated Thirty UC-43s '1 Air Force as a hardy survi- at started with as the North :s own Bonan- mpetitive with ch personally f a final G17 uilt but were :Custom orders. biplane as a ngs built from 00 are still on are registered red antiques is tags seen on up for sale- :00, more than ost expensive o 'orBoeing. But his II design contest. The heaviest, fastest and most powerful of all the 5taggerwings (top photograph, facing page) was the single A 17F5 with a 710-hp Wright Cyclone engine. BEECH 17 STAGGER WING A17FS B17L D17S Powerplant Wright R-1820-F3 Jacobs L-4 P&W Wasp Jr. SB 225 hp @ 2,000 rpm 450 hp @ 2,300 rpm Wingspan 34 ft 6 in 32 ft 32 ft 24 ft 3 in 24 ft 6 in 25 ft 11 in 338 sq ft 273 sq ft 296 sq ft 15.4 lb/sq ft 11.6 lb/sq ft 14.2 lb/sq ft 7.3 Ib/hp 14 lb/hp 9.5 lb/hp Navy 22 Clark Y NACA 23012 3,285 lb 1,800 Ib 2,540 Ib 5,200 lb 3,1501b 4,250 Ib High speed 250 mph 175 mph 212 mph 215 mph 162 mph 202 mph 65 mph 45 mph 55 mph 2,000 fpm 850 fpm 1,250 fpm 20,000 ft 15,500 ft 20,000 ft 750 sm 560 sm 800 sm155 gal 50 gal 100 gal Model' (Military Number Date Designation) Built Powerplant 496 Dee. 30, 1932 17R 2 Wright R-975-E2, 420 hp Aug. 8,1934 A17F I Wright R-1820-FII, 690 hp Dee. 4,1934 BI7L, BI7B 47 Jacobs L-4, 225 hp and Jacobs L-5, 285 hp May 9,1935 BI7E 4 Wright R-760-EI, 285 hp July 6,1935 AI7FS I Wright SR-1820-F3, 710 hp July 22, 1935 1J17R(UC-43H) 16 (3) Wright R-975-E2, 420 hp April 16, 1936 CI7L (UC-43J) 45 (13) Jacobs L-4, 225 h P and G) Jacobs L-5, 285 hp May 3,1936CI7R (UC-43E) 17 (5) Wright R-975-E2, 420 hp July 1936 Cl7E 3 Wright R-760-EI, 285 hp May 20,1937DI7R (UC-43A) 28 (13) Wright R-975-E3, 420 hp May 22,1937 EI7L 48 (31) Jacobs L-4, 225 hp and D) Jacobs L-5, 285 hp July 16,1937DI7S (UC-43B) 66" (13) P&W R-985, 450 hp Aug. 26, 1938 FI7D (UC-43C) 56 (38) Jacobs L-6, 330 hp NO\'.7,1939017 A (UC-43F) 2 (1) Wright R-760-E-2, 350 hp Oct. II, 1946 GI7S 20 P&W R-985-AN-4, 450 hp 559 UC-43s, GB-ls, GB-2s mentto the American Embassy in London, 'atriatePrince Bernhard of the Netherlands. Earlier 5taggerwings looked very much alike; but the G 175 was distinctive with its new cowl-to-fuselage lines and landing-gear closure fairings. , -- AOPA PILOT' 131




