Keystone XLB-3

{{short description|Prototype Biplane Bomber}}

{{More footnotes|date=April 2017}}

{{Infobox aircraft begin

|name= XLB-3

|image= File:Keystone XLB-3A.jpg

|image_border= yes

|caption= XLB-3A

}}{{Infobox aircraft type

|type= Light bomber

|national origin= United States

|manufacturer= Keystone Aircraft

|designer=

|first flight= ca. December 1927

|introduced=

|retired=

|status=

|primary user= United States Army Air Corps

|number built= 1

|developed from=

|variants with their own articles=

}}

The Keystone XLB-3 (originally built under the Huff-Daland name) was a prototype bomber biplane developed in the United States in the late 1920s. It was a twin-engine development of the single-engine LB-1, brought about by a change in policy by the United States Army Air Corps (USAAC).

Design and development

The shift from a nose-mounted engine to engines mounted in nacelles on the lower wing created an opportunity to provide stations for two extra crewmembers: a bombardier and a nose-gunner, bringing the total to five. The LB-1's single tailfin and rudder was augmented by an extra rudder either side of it.

Operational history

A single prototype was constructed, and delivered to the USAAC for evaluation at the end of 1927. Evaluation, however, showed that performance was actually inferior to that of the single-engine LB-1. The decision was taken to change the XLB-3's air-cooled inverted Liberty engines for air-cooled radials, at which point it was redesignated XLB-3A. With performance still unsatisfactory, development was abandoned in favor of a parallel design, the LB-5.

Variants

Specifications (XLB-3A)

{{Aircraft specs

|ref=Jane's Encyclopedia of AviationTaylor 1989, p. 559.

|prime units? = imp

|crew=Five – pilot, copilot, bombardier, two gunners

|length m=13.72

|length ft=45

|length in=0

|span m=20.42

|span ft=67

|span in=0

|height m=5.13

|height ft=16

|height in=10

|wing area sqm=1,038

|wing area sqft=105.8

|empty weight kg=2,756

|empty weight lb=6,065

|gross weight kg=5,310

|gross weight lb=11,682

|eng1 number=2

|eng1 name=Pratt & Whitney R-1340

|eng1 kw=305

|eng1 hp=410

|max speed kmh=186

|max speed mph=116

|range km=870

|range miles=544

|ceiling m=3,400

|ceiling ft=11,210

|climb rate ms=2.8

|climb rate ftmin=550

|armament = *2 × trainable .303 in (7.7 mm) Lewis guns in open position in nose

  • 2 × trainable .303 in (7.7 mm) Lewis guns in open dorsal position
  • 1 × trainable .303 in (7.7 mm) Lewis gun in ventral hatch
  • 2,205 lb (1,000 kg) of bombs

}}

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

}}

References

=Notes=

{{reflist}}

=Bibliography=

{{refbegin}}

  • Taylor, Michael J. H. Jane's Encyclopedia of Aviation. London: Studio Editions, 1989.
  • World Aircraft Information Files. London: Bright Star Publishing, File 899, Sheet 09.

{{refend}}