Taken from Janusz Ledwoch's excellent book 'Bv 138'




	Service delivery	March -41
	Numbers built 	227 (of which 72 were built before end of -42),				(src: #64Bv138)
			 although also most B-1s were modified to roughly the same status		(src: AirInt)
     
	Crew		5-6 ;  Nose gunner, Pilot, Navigator, Radio Operator, Rear gunner, Upper rear gunner.

     
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	Dimensions
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	Overall measures:
	------------------
	Wingspan			26,936 m						(src: Handbuch)
	Total length		19,90 m						(src: Handbuch)
	Height without propellers	 5,30 m						(src: Handbuch)
	Height with running propellers	 6,60 m						(src: Handbuch)

	Wing
	------------------
	Area			112,00 m2						(src: Handbuch)
	Spanwidth			26,936 m						(src: Handbuch)
	Depth, deepness inner		5,04 m						(src: Handbuch)
	Depth, deepness outer		2,60 m						(src: Handbuch)
	laterally proportion(ratio)	1:6,5						(src: Handbuch)
	Materials			Steel, tin, fabric, and 					(src: Handbuch)
				some aluminium.

	Hull
	------------------
	Length			15,10 m						(src: Handbuch)
	Width at the step		2,60 m						(src: Handbuch)
	Height			3,15 m						(src: Handbuch)
	Materials			Steel, aluminium,					(src: Handbuch)
				and covering of tinplates.		
     
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	Weight
	- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -		
	Empty		11770 kg 							(src: Nowarra, Ital, #64Bv138)      
			25948 lb							(src: Germ)
			  8955 kg without propellers and engines				(src: RLM)
			11355 kg with propellers and engines				(src: RLM)
			12200 kg  (leergewicht)						(src: Handbuch)
			11930 kg (when transported in parts)				(src: Handbuch)
          
	Maximum loaded	17400kg							(src: RLM)
			17650 kg (38912 lb)						(src: Nowarra, Ital, #64Bv138, Germ)
			18000 kg  (using RATOs, of which 500 kg)				(src: Handbuch)
			18200 kg  (catapult launched)					(src: Handbuch)
          
	Normally loaded	14390kg							(src: RLM)
			14500 kg (31967 lb)						(src: Nowarra, #64Bv138, Germ)
          
          
	Weight of load	
			normal=3035kg, max=6045kg					(src: RLM)
			2900 - 5400 kg						(src: #64Bv138)
			max 6000 kg  (fuel, crew and ammunition not included)			(src: calculated from Handbuch)

	Horizontal acc. limit
	(for catapult starts?)	Nx = 3.5 g							(src: Handbuch)
          
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	Speed
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	Max speed		285km/h - 300km/h						(src: AirInt)
			300km/h max permissible level speed				(src: Handbuch, Bedienung)
			285km/h normal load at sea level					(src: RLM, Nowarra, #64Bv138)
			283km/h 14513 kg at sea level					(src: Rus)
			270km/h max load at sea level					(src: RLM)
			177 mph 31967 lbs at sea level					(src: Germ)

	Max permissible 
	dive speed		400km/h							(src: Handbuch, Bedienung)				
          
	Cruising speed	250km/h normal load						(src: RLM)
			235 km/h max load						(src: RLM)
			216-265km/h						(src: #64Bv138)	
			146 mph at 3280 ft						(src: Germ)
			234 km/h at 1000 m						(src: Rus)
          
	Economy		200 km/h							(src: Nowarra)
          
	Takeoff speed	110 km/h							(src: #64Bv138)
	Landing speed	115 km/h							(src: #64Bv138)

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	Climb rate
	- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
			24 min to 10390 ft						(src: Germ)
			24 min to 3170 m						(src: Rus)
			22 min to 3000 m						(src: #64Bv138)

	Best climb speed	180-190 km/h						(src: Handbuch)

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	Service ceiling
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	No load		5000 m							(src: Nowarra)
     
	Normal load	5000 m							(src: Ital, #64Bv138)
			5000 m (16400 ft) at 31967 lb		    			(src: Germ)
			5000 m at 14513 kg						(src: Rus)
			4200 m RLM normal load					(src: RLM)
     
	Max load		2300 m RLM max load						(src: RLM)
			2800 m full load 						(src: Nowarra)
			2800 m (9185 ft) at 38912 lb		  			(src: Germ)
			2800 m at 17666 kg						(src: Rus)
     
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	Wing loading
	- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
	normal		128.5 kg/sq.m
	max		155.3 kg/sq.m

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	Endurance
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	Maximum endurance	18 hrs catapulted						(src: Nowarra)
			20 hrs							(src: Nowarra)
			18 hrs							(src: calculated, Rus)
			16-17 hrs							(src: #64Bv138)
	 		16h 23min no bombs						(src: #64Bv138)
	 		15h 18min 6x SC50 						(src: #64Bv138)
     
	Normal endurance	6.5 hrs							(src: Nowarra, Germ, Rus)
     
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	Range
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	Maximum range	1840 km normal load						(src: RLM)
			3880 km maximum load						(src: RLM)
			2670 miles (with 825 Imp.gal)					(src: Germ)
			4300 km with overload						(src: Nowarra)
			5000 km							(src: Ital)
			3413 km							(src: #64 Bv138)
			4272 km (with 3750 l, catapulted?)					(src: Rus)
			4250 km catapulted 						(src: #64 Bv138)
     
	Normal range	758 miles (at 122 mph)						(src: Germ)
			1250 km							(src: Nowarra)
			1212 km (at 195 km/h)						(src: Rus)
     
	Takeoff distance	650 m							(src: #64Bv138)
     
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	Armament/Loadout
	- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
			1x MG151 20mm cannon in bow turret
			1x MG151 20mm cannon in stern turret
			1x MG131 13mm machine gun in open position aftward central engine
	     (optional)	1x MG15  7.9mm machine gun through hatch in starboard side of hull
     
	     (Early version)	3x 50kg (110 lbs) bombs on racks beneath starboard wing centre section or
			2x(3x) 150 kg depth charges
     
	     (U1 version)	6x 50kg (110 lbs) bombs or
			4x 150kg depth charges
     
     
	Other loadouts:  2x RATO packs
    
	Also able to carry 10 soldiers with equipment (in addition to the usual five man crew) or other loads
	totalling about 1000 kg. This depending on the amount of fuel carried, see the section on weight for more info.

 
	Ammunition:
	Forward MG151/20 cannon:	500 shells (+500 spares)					(src: Handbuch)
	Rearward MG151/20 cannon:	500 shells (+500 spares)					(src: Handbuch)
	Central MG131 machinegun:            1400 bullets (+600 spares)				(src: Handbuch)

	Turret type:			HD 151/1A and HD 151/1B
	Front turret movement:		320 dgr, (backwards 160 degrees )
     
	Type of bombs:
	SC 50:	   50 kg								(src: Nowarra, #64Bv138, Handbuch)
	Fl.W.B.150:  150 kg								(src: #64Bv138, Handbuch)
     
     
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	Control surfaces
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	Horizontal Stab and elevator
	-------------------------------
	Total area				16,56 m2					(src: Handbuch)
	Depth				2,45 m					(src: Handbuch)

	Horizontal stabilizer:
	  Area				10,67 m2					(src: Handbuch)
	  Spanwidth				7,20 m					(src: Handbuch)
	  Depth				1,54 m					(src: Handbuch)
	  Attitude against horizontal		+5° +2°					(src: Handbuch)
					-4°
	  Material				Tin-plate					(src: Handbuch)

	Elevator:
	  Total area				5,89 m2					(src: calculated)
	  Area behind turnaxle, including trimmrudder	4,34 m2					(src: Handbuch)
	  Counterbalance area			1,55 m2					(src: Handbuch)
	  Spanwidth				7,00 m					(src: Handbuch)
	  Depth with counterbalance part		0,915 m					(src: Handbuch)
	  Depth without counterbalance part	0,675 m					(src: Handbuch)
	  Position of turnaxle from backward edge	27,5 %					(src: Handbuch)
	  Deflection upwards			29°					(src: Handbuch)
	  Deflection downwards			27°					(src: Handbuch)
	  Material				Tin-plate and fabric				(src: Handbuch)

	Trimming rudder:
	  Area				0,348 m2					(src: Handbuch)
	  Spanwidth				2,05 m					(src: Handbuch)
	  Depth to turnaxle			0,15 m					(src: Handbuch)
	  Material				fabric					(src: Handbuch)
     
	Vertical Stabs and rudders
	-------------------------------
	Total area				12,60 m2					(src: Handbuch)

	Vertical stabilizer:
	  Area				2x 4,12 m2					(src: Handbuch)
	  Spanwidth (height)			2,70 m					(src: Handbuch)
	  Depth midheights (length)		1,53 m					(src: Handbuch)
	  Material				Tin-plate					(src: Handbuch)

	Vertical rudders:
	  Area behind turnaxle, including trimmrudder	2x 1,59 m2					(src: Handbuch)
	  Counterbalance area			2x 0,59 m2					(src: Handbuch)
	  Spanwidth (height)			2,70 m					(src: Handbuch)
	  Depth with counterbalance (length)	0,95 m					(src: Handbuch)
	  Depth without counterbalance (length)	0,65 m					(src: Handbuch)

	  Position of turnaxle from backward 
	  edge, midheights			28 %					(src: Handbuch)

	  Deflection inwards			29°					(src: Handbuch)
	  Deflection outwards			29°					(src: Handbuch)

	  Material				Tin-plate and fabric				(src: Handbuch)

	Trimming rudders:
	  Area				2x 0,143 m2					(src: Handbuch)
	  Spanwidth				1,425 m					(src: Handbuch)
	  Depth (length)			0,100 m					(src: Handbuch)
	  Material				Tin-plate					(src: Handbuch)
     
	Ailerons
	-----------------
	Total area:				2x 3,07 m2					(src: calculated)

	Area behind turnaxle			2x 2,30 m2					(src: Handbuch)
	Counterbalance area			2x 0,77 m2					(src: Handbuch)
	Spanwidth				5,06 m					(src: Handbuch)
	Depth with counterbalance (length)		0,64 m					(src: Handbuch)
	Depth without counterbalance (length)	0,48 m					(src: Handbuch)

	Position of turnaxle from backward 
	edge of wing, inner:			11,7 %					(src: Handbuch)
	Position of turnaxle from backward
	edge of wing, outer:			18,5 %					(src: Handbuch)

	Deflection upwards			29°					(src: Handbuch)
	Deflection downwards			21°					(src: Handbuch)
	Deflection when used as flaps (14°)
		upwards			39°					(src: Handbuch)
		downwards			11°					(src: Handbuch)

	Material				Tin-plate and fabric				(src: Handbuch)

	Trimming rudder (only on the left side):
	  Area				0,089 m2					(src: Handbuch)
	  Spanwidth				1,05 m					(src: Handbuch)
	  Depth (length)			0,085 m					(src: Handbuch)
	  Material				Tin-plate					(src: Handbuch)
     
	Flaps
	-----------------
	Total area:				9,58 m2					(src: Handbuch)

	Inner:
	   Area				2x 1,87 m2					(src: Handbuch)
	   Spanwidth			2,550 m					(src: Handbuch)
	   Depth				0,726 m					(src: Handbuch)
	   Max deflection			30°					(src: Handbuch)
	   Material				Tin-plate					(src: Handbuch)

	Outer:
	   Area				2x 2,92 m2					(src: Handbuch)
	   Spanwidth			4,43 m					(src: Handbuch)
	   Depth (length), mid			0,66 m					(src: Handbuch)
	   Max deflection			60°					(src: Handbuch)
	   Material				Tin-plate					(src: Handbuch)
	
	Ailerons:
	   Aileron-deflection as flap		14°					(src: Handbuch)

     
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	Floats
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	Displacement (each)			1,50 m3					(src: Handbuch)
	Distance from hullcenter		9,53 m					(src: Handbuch)
     
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	Engines
	- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
	Name		Junkers Jumo 205D (version 1,2,3 and 5)
	Type		Six cylinder vertical opposed-piston,
			 compression-ignition two-stroke diesel engines
	Fuel		Diesel - Type K1						(src: #64Bv138)
	Cooling		Glychole							(src: Junk)
	weight		595 kg	(650 kg src: RLM)					(src: Junk)
	length		2.236 m							(src: Junk)
	width		0.645 m							(src: Junk)
	height		1.271 m							(src: Junk)
	Fuel Consumption	217.5 g/kWh						(src: Junk)
	Airscrew drive	1.58:1							(src: Handbuch)
     
     
	Power
	---------
    	MW injection (80 s):    1000 hp (746kW)						(src: AirInt)
	Brief, start (60 s):	880 hp (656 kW) at 2800 rpm					(src: all)
	Brief, (30 min):	750 hp (559 kW) at 2450 rpm					(src: all)
	Lasting, normal:	650 hp (485 kW) at 2350 rpm					(src: all)
	Lasting, economy:	525 hp (391 kW) at 2175 rpm					(src: all)

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	Propellers
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	Outward engines
	type:		VDM continuously variable pitch, (9-11275 A-1)				(src: Handbuch)
	blades:		three							(src: Handbuch)
	diameter:		3000 mm							(src: Handbuch)
	material:		wood (some had metal)						(src: #64Bv138, Handbuch)
	weight		~160 kg/propeller						(src: Handbuch)
	Pitch:		continuously variable from feathered to fine 

     
	Central engine
	type:		VDM continuously variable pitch, (9-11273 A-1)				(src: Handbuch)
	blades:		four							(src: Handbuch)
	diameter:		3100 mm							(src: Handbuch)
	material:		metal							(src: Handbuch)
	weight		~190 kg/propeller						(src: Handbuch)
	Pitch:		continuously variable from feathered to negative
     
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	Fuel system
	- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
	Fueltanks:		3x 760 l each, 1x inside hull and 2x inside center wings, 			(src: Handbuch)
	Reservtanks:	3x 980 l each, inside spar of center wings,				(src: Handbuch)
	Total volume:	5220 liters							(src: #64Bv138)
          
	Fuel consumption per engine:
	Average:		120 l/h (=112 kg/h) at 2300 rpm and 650HP				(src: #64Bv138)
	Economy:		 95 l/h at 1900 rpm and 510HP					(src: #64Bv138)
	Max:		185 l/h at 2800 rpm and 880HP					(src: #64Bv138)
     
	Fuel type:		Diesel - Type DK1 or K1 					(src: Handbuch) 
	Diesel weight:	0.933 kg/l							(src: calculated)
    
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	Oil system
	- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
	Oiltanks:		3x 60 liters in each engine					(src: #64Bv138)
			1x 300 liters							(src: #64Bv138)
     
	Oil consumption:	5.5 - 8.2 kg/h						(src: #64Bv138)

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	MW injection system (Later in the war)
	- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
	Tank:		1x 36 liter in starboard wing root, used by all engines			(src: AirInt)
	
	Time available:	80-90 seconds 						(src: AirInt)
	Consumption:	24-27 liter/minute						(src: calculated)

	Boost mixture:	80% methanol, 20% water					(src: AirInt)
     
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	Rocket assisted take-off units
	- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
	One mounted below each wing outward engine gondola.
	Two possible versions:
     
	Walter 109-501
	Force:		1000 kg	(=1366HP?)						(src: #64Bv138)
	Time:		42 seconds							(src: #64Bv138)
     
	Walter 109-502
	Force:		1500 kg	(=2049HP?)						(src: #64Bv138)
	Time:		30 seconds							(src: #64Bv138)

RLM Flugzeugtypenblatt

	~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
	~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
	Sources:
	Ital:		Italian site, http://www.50megs.com/luftwaffe/index.html
	Nowarra:		Blohm & Voss Bv 138 by Heinz J. Nowarra, Schiffer Military History
	#64 Bv138:		Bv 138 #64 by Janusz Ledwoch, Wydawnictwo Militaria
	Germ:		German Armed Forces in WWII, http://www.uwm.edu/~jpipes/start.html **
	RLM:		RLM Flugzeugtypenblatt
	Junk:		The Junkers Engine Pages, http://ourworld.compuserve.com/homepages/hzoe/ju_eng.htm
	Rus:		Russian site, http://195.218.252.26/wol/bv/138.htm **
	AirInt:		Air International magazine
	Handbuch:		BV138C-1 Flugzeug Handbuch
	Bedienung:		BV138C-1 Bedienungsvorschrift-Fl
	calculated:		Means that other given data lead to this result
     
	** Probably using the same source, and most probably a lot of the others too (or each other).

	For further info regarding sources, please refer to the 'More' section.


Observe! This page is beeing re-edited as I now have the original mechanics handbook and flight manual.