{{No footnotes|date=January 2024}}<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft |name =B.I |image =AEG B.I 1914.jpg |caption = |type =Reconnaissance aircraft |manufacturer =AEG |designer = |first_flight =1914 |introduction =1914 |retired = |status = |primary_user = |more_users = |produced = |number_built = |unit cost = |variants = }}

The '''AEG B.I''' was a German two-seat biplane unarmed reconnaissance aircraft produced in very small numbers in 1914. It formed the basis for the more successful B- and C-type aircraft from AEG.

==Operators== *{{flag|German Empire}} **''Luftstreitkräfte''

==Specifications (AEG B.I)== thumb|AEG B.I {{Aircraft specs |ref= |prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->

<!-- General characteristics --> |genhide=

|crew=2 |capacity= |length m=10.5 |length ft= |length in= |length note= |span m=14.5 |span ft= |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm=44 |wing area sqft= |wing area note= |swept area sqm=<!-- swing-wings --> |swept area sqft=<!-- swing-wings --> |swept area note= |volume m3=<!-- lighter-than-air --> |volume ft3=<!-- lighter-than-air --> |volume note= |aspect ratio=<!-- give where relevant eg sailplanes --> |airfoil= |empty weight kg=650 |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg=1,040 |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg=<!-- lighter-than-air --> |lift lb=<!-- lighter-than-air --> |lift note= |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name=Mercedes D.I |eng1 type=6-cyl. water-cooled in-line piston engine |eng1 kw=<!-- prop engines -->74.5 |eng1 hp=<!-- prop engines --> |eng1 kn=<!-- jet/rocket engines --> |eng1 lbf=<!-- jet/rocket engines --> |eng1 note= |power original= |thrust original= |eng1 kn-ab=<!-- afterburners --> |eng1 lbf-ab=<!-- afterburners -->

|eng2 number=<!-- for different engine types --> |eng2 name= |eng2 type= |eng2 kw=<!-- prop engines --> |eng2 hp=<!-- prop engines --> |eng2 kn=<!-- jet/rocket engines --> |eng2 lbf=<!-- jet/rocket engines --> |eng2 note= |eng2 kn-ab=<!-- afterburners --> |eng2 lbf-ab=<!-- afterburners -->

|eng3 number=<!-- for different engine types --> |eng3 name= |eng3 type= |eng3 kw=<!-- prop engines --> |eng3 hp=<!-- prop engines --> |eng3 kn=<!-- jet/rocket engines --> |eng3 lbf=<!-- jet/rocket engines --> |eng3 note= |eng3 kn-ab=<!-- afterburners --> |eng3 lbf-ab=<!-- afterburners --> |more power=

|prop blade number=<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop note=

|rot number=<!-- helicopters --> |rot dia m=<!-- helicopters --> |rot dia ft=<!-- helicopters --> |rot dia in=<!-- helicopters --> |rot area sqm=<!-- helicopters --> |rot area sqft=<!-- helicopters --> |rot area note= <!-- Performance --> |perfhide=

|max speed kmh=100 |max speed mph= |max speed kts= |max speed note= |max speed mach=<!-- supersonic aircraft --> |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh=<!-- aerobatic --> |stall speed mph=<!-- aerobatic --> |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance=<!-- if range unknown --> |ceiling m=2,500 |ceiling ft= |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms=<!-- sailplanes --> |sink rate ftmin=<!-- sailplanes --> |sink rate note= |lift to drag= |wing loading kg/m2=24 |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note=

|power/mass= |thrust/weight=

|more performance= <!-- Armament --> |guns= |bombs=

|avionics= }}

==See also== {{Aircontent| |related= |similar aircraft= * AEG B.II * AEG B.III

}}

==Bibliography== *{{cite book |last1=Herris |first1=Jack |title=A.E.G. Aircraft of WWI: A Centennial Perspective on Great War Airplanes |date=2015 |publisher=Aeronaut Books |location=n. p. |isbn=978-1-935881-28-5|series=Great War Aviation Centennial Series|volume=16}}

==External links== {{Commons category}} *[https://web.archive.org/web/20051003210047/http://www.luftfahrtmuseum.com/htmi/itf/aegb1.htm AEG B.I at the Virtual Aviation Museum]

{{AEG aircraft}} {{Idflieg B-class designations}} {{World War I Aircraft of the Central Powers}}

B.I Category:Single-engined tractor aircraft Category:Biplanes Category:1910s German military reconnaissance aircraft Category:Aircraft first flown in 1914 Category:Aircraft with fixed conventional landing gear Category:Single-engined piston aircraft