Kurzbetriebsanleitung Junkers Ju 87 D-3 Für Den Flugzeugführer - English

8/10/2019 Kurzbetriebsanleitung Junkers Ju 87 D-3 Für Den Flugzeugführer - English

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Abbreviated Pilot's Manual for Junkers Ju 87 D-3

I. Starting the Engine & Warm Up

1. Dive Break retracted, control lever in osition '!'". #la s retracted, control lever in osition '!'

3. $PM control lever full% for&ard (i)(er $PM*+. u erc(ar)er control lever us(ed in to settin) 'Auto atic'

. /(rottle on idle or ini all% for&ard0. on en)ine start ull back $PM control lever lo&er $PM*7. 2ncrease $PM to 0!! 8!! until oil ressure )au)e s(o&s reaction8. 2n case oil ressure )au)e s(o&s no reaction &it(in 1! seconds i ediatel% sto en)ine.4. 2ncrease $PM to 1!!! and (old t(ere1!. Be)in &ar u until t(e follo&in) values are reac(ed5

6oolant /e erature5 in. 0! 6il /e erature5 in. "! 6il Pressure5 . 4.! at9

11. 2ncrease $PM to a: 10!!1". 6ontinue &ar u until t(e follo&in) values are reac(ed5

6oolant /e erature5 in. 0! 6il /e erature5 in. 3! 6

13. /o reac( ini u il /e erature of 3! 6 faster close radiator so t(at t(e 6oolant /e eraturereac(es 8! to 1!! 6.

II. Taxiing

1. et tail &(eel arrestor lever to 'loose'". #ull% o en radiator and oil cooler 3. et fla s to '/ake- ff' osition+. il /e erature durin) ta:iin) ust not e:ceed 0! 6 ;inter* or 7 6 u er*

. se brakes carefull%, not not brake continuousl% to avoid over(eatin)0. /urnin) on a &(eel is strictl% ro(ibited<7. Ma:i u $PM durin) ta:iin)5 10!! to 18!!

III. Take-Off

1. $oll stri)(t for a fe& eters to ali)n tail &(eel, t(en set tail &(eel arrestor to 'lock'". 6(eck t(at fla s are in '/ake- ff' osition3. $PM control lever full% for&ard+. oot(l% increase t(rottle until a:

. 1- in-settin)5 "0!! $PM at 1.+! ata0. After liftin) off i ediatel% ull back t(rottle and $PM control lever to 3!- inute-settin) of 1." ata at

"+!! $PM7. Do not retract fla s until reac(in) a certain altitude ca "!! * and = ! > 18! k ?( because t(e aircraft

&ill lose altitude &(en t(e fla s are bein) retracted8. $educe o&er settin) no later t(an 3! inutes after /ake- ff to a:i u continous out ut "" !

$PM at 1.1 ata*




IV. Flight

Optimum Climb Speed ;ei)(t /able see 6(a . =2*

Weight +8!! k) 3!! k) 8!! k) 00!! k)

V !km"h# "!! - "1! "1! ""! "3!

Engine Data

a) RPM and Manifold Pressure

$% anif'ld %re((ure ata

)- inute-Setting "0!! 1.+!

* - inute-Setting "+!! 1."

ax. C'ntin'u( Setting "" ! 1.1

E+'n'mi+ Setting 14!! 1.!!

b) Oil Temperature

Temperature

Mini uMa:i u

3! 61! 6

c) Coolant Temperature

Maximum Temperatures at altitude (km)

,ltitude in km 1 + 8

C 11! 1!! 4!

2f set to auto atic t(e su erc(ar)er &ill s&itc( auto aticall% at around 3!!! @- 3!! *.

V. anding

). eave $PM control lever at "" ! at $PM in case of touc(-and-)o*/. et fla s as re uired*. #ull% o en coolin) fla s0. De endin) on &ei)(t conduct final a roac( at 1 ! 10! k ?(

1. ;it( fla s full% e:tended and a )ross &ei)(t of +4!! k) roll distance is about +!!2. ;(enever ossible landin) s(ould be conducted into t(e &ind




VI. Weight Table

'ad'ut Weight !in kg#

7,4" : 1!!! +8!!

1: 6 " ! @ +: 6 7! +3!

1: 6 !! 3"!

1: 6 !! @ +: 6 7! 08!

1: 6 !! @ ": 6 " ! 88!

3: 6 " ! 7 !

1: 6 1!!! 8!!

1: 6 18!! 00!!

Attention< Ma:i al take-off &ei)(t is 4!!k). /(e loadout containin) t(e 6 18!! e:ceeds t(is li itand is not to be used unless s ecificall% ordered< verload considerabl% c(an)es take-offc(aracteristics see table belo&*<

Take-Off Weight $ollin) Distance in ift- ff s eed in k ?( Distance to reac(altitude of "!

88! k) !! 1 7 !

00!! k) 7!! 10 - 17! 1!!!

VII. ,ppr'a+hing the Target & 3i4e ,tta+k

1. en botto &indo&". et $PM to "" ! $PM a: $PM for divin)*3. u erc(ar)er control re ains on 'Auto atic'+. Cn)a)e siren if ordered*

. $educe t(rottle to idle belo& !.8 ata*

0. 6lose coolin) fla s7. /ri aircraft so e&(at front-(eav% so t(at it can be ke t in t(e dive &it( ini al stick ressure8. C:tend dive brake. Attention5 C:tendin) t(e dive brake &(ile alread% divin) is ro(ibited< Do not

co ence dive until t(e brake is full% e:tended<4. 6o ence divin) attack1!. $etract dive brake after ullin) out of t(e dive.11. Disen)a)e siren belo& 3 ! k ?(*1". et $PM to "+!! $PM13. et t(rottle to 1." ata1+. #ull% o en coolin) fla s1 . 2n case of ene % defenses 1- inute- o&er 1.+! ata at "0!! $PM* can be used.

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Kurzbetriebsanleitung Junkers Ju 87 D-3 Für Den Flugzeugführer - English