Hawker_400XP_Pre-Course.pdf
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Hawker 400XP Pre-Course Package
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Transcript of Hawker_400XP_Pre-Course.pdf
Hawker 400XP Pre-Course
Package
- 2 -
Contents
Introduction…………………………………………………………………………………………………………3 Hawker 400XP Overview………………………………………………………………………………………….4
General Description and Dimensions Weights and Fuel Capacities Performance Fuselage Wings Empennage Landing Gear Powerplant Cockpit and Avionics Interior Baggage Compartment
Hawker 400XP Systems Overview…………………………………………………………………………….22
Thrust Reversers Flight Controls Fuel System Hydraulic System Electrical System Pressurization and Environmental System Oxygen System Ice and Rain Protection System
- 3 -
Introduction Welcome to the Hawker 400XP! To help begin the learning process, this package is designed to provide you with general information concerning the Hawker 400XP. A brief description of the aircraft and aircraft systems is also provided to assist in the transition of learning a new aircraft that may not be familiar to you. Simplified schematics of selected systems are included to help prepare you for the challenges that lay ahead when you embark on the journey to the maintenance initial course. The following is a brief history of the Hawker 400XP and its beginning. The Hawker 400XP was originally designed in Japan by Mitsubishi. The aircraft was known as the MU-300 or simply as the Diamond 1. Mitsubishi produced 91 aircraft and some are still currently flying. Soon after the introduction of the Diamond 1, Mitsubishi began development of an improved version of the aircraft known as the MU-300-1 or the Diamond II. Mitsubishi built 11 Diamond II’s before Beechcraft approached the company and expressed interest In possibly purchasing the aircraft. Beechcraft did not offer a jet in its product line so two options were presented: Option 1 involved Beechcraft developing a jet from the ground up, a costly and challenging proposition. Option 2 would allow Beechcraft to purchase an aircraft already on the market to substantially reduce their workload and development costs. Beechcraft opted for the latter and purchased the Diamond II from Mitsubishi. Beechcraft purchased the 11 aircraft already assembled as well as the manufacturing rights. Beechcraft renamed the Diamond II the BeechJet 400. The company also improved several of the aircraft systems including the powerplant and electrical system. The first 11 BeechJet 400 aircraft have dual serial numbers, a Mitsubishi serial number and a new designation from Beechcraft, “RJ”. Beechcraft eventually built RJ-12 through RJ-65 and that ended the BeechJet 400 model. The “RK” series was introduced and RK-1 became the first improved BeechJet 400 and was known as a BeechJet 400A. The model 400A was a greatly improved model over the BeechJet 400. The systems that were improved were the electrical system, the fuel system and the environmental system and minor changes to the flight controls just to name a few. Beechcraft built 353 BeechJet 400A’s before the company decided that production might be discontinued. To improve sales and marketing of the BeechJet 400A, Beechcraft decided to re-brand the model 400A and rename the aircraft the Hawker 400XP. The first Hawker 400XP was RK-354. Although The aircraft is a Hawker 400XP in designation, the data plate is still identified as a 400A. The Hawker 400XP designation is a name change only. The U.S. Air Force operates 180 of these aircraft in a “TT” configuration and the Japanese defense Forces are equipped with 13 models known as a “TX” version..
Hawker 400XP Overview General Description and Dimensions Notes
- 4 -
- 5 -
Weights and Fuel Capacities Notes
Performance
- 6 -
Notes
- 7 -
Fuselage Notes
- 8 -
Wings Notes
Empennage
- 9 -
Landing Gear Notes
- 10 -
Powerplant Notes
- 11 -
Cockpit and Avionics Notes
- 12 -
- 13 -
Hawker 400XP 3-Tube EFIS
Collins Pro-Line 4
- 14 -
- 15 -
- 16 -
- 17 -
- 18 -
Interior Notes
- 19 -
- 20 -
Baggage Compartment Notes
- 21 -
Hawker 400XP Systems Overview
Thrust Reversers Notes
Flight Controls
- 22 -
Fuel System Notes
Hydraulic System
A hydraulic valve package located aft of the right main landing gear wheel well houses the hydraulic component modules for the landing gear, flaps and speed brakes.
- 23 -
28-2 FOR TRAINING PURPOSES ONLY
HAWKER 400XP/BEECHJET 400A MAINTENANCE TRAINING MANUAL
RIGHT AUXILIARYFUEL TANK(UNDER CABIN FLOOR)
LEFT AUXILIARYFUEL TANK
(UNDER CABIN FLOOR)
LEFT MIDFUSELAGE TANK
(UNDER CABIN FLOOR)
RIGHT MIDFUSELAGE TANK(UNDER CABIN FLOOR)
COLLECTOR CHAMBER
AFT FILLERTANK
AFT FUSELAGETANK
COLLECTOR CHAMBER
RIGHT WING TANKLEFT WING TANK
LEFT VENTSURGE TANK RIGHT VENT
SURGE TANK
WING FUEL
FUSELAGE FUEL
COLLECTOR TANK FUEL
VENT SURGE TANK
LEGEND
Figure 28-1. Fuel Storage Tanks Location
29-2 FOR TRAINING PURPOSES ONLY
HAWKER 400XP/BEECHJET 400A MAINTENANCE TRAINING MANUAL
HY
DR
AU
LIC
PA
CK
AG
E
DR
AIN
CO
CK
FIL
TE
R
BY
PAS
SV
ALV
E(5
0 P
SID
)
FIL
TE
RF
ILT
ER
BY
PAS
SV
ALV
E (
50 P
SID
)B
YPA
SS
VA
LVE
(50
PS
ID)
CH
EC
KV
ALV
E
CH
EC
KV
ALV
E
CH
EC
KV
ALV
E
RE
LIE
F V
ALV
E(1
,650
–1,8
50 P
SI)
BY
PAS
SV
ALV
EB
YPA
SS
VA
LVE
BR
AK
ES
YS
TE
M
CH
EC
KV
ALV
EC
HE
CK
VA
LVE
L H
YD
PU
MP
(OU
TP
UT
1,5
00 P
SI)
R H
YD
PU
MP
(1,5
00 P
SI O
UT
PU
T)
CH
EC
KV
ALV
E
VA
LVE
PAC
KA
GE
TH
RU
ST
RE
VE
RS
ER
SY
ST
EM
CH
EC
KV
ALV
E
CH
EC
KV
ALV
E
L LO
W P
RE
SS
UR
ES
WIT
CH
(75
0 P
SI)
R L
OW
PR
ES
SU
RE
SW
ITC
H (
750
PS
I)P
RE
SS
TR
AN
S-
DU
CE
R
L S
HU
TOF
FV
ALV
ER
SH
UTO
FF
VA
LVE
CA
SE
DR
AIN
CA
SE
DR
AIN
SU
CT
ION
SU
CT
ION
PR
ES
SU
RE
PR
ES
SU
RE
CH
EC
KV
ALV
EV
AC
UU
MR
ELI
EF
OV
ER
BO
AR
DV
EN
T
BLE
ED
OR
IFIC
E
GR
OU
ND
SU
CT
ION
CO
NN
EC
TIO
N
GR
OU
ND
PR
ES
SU
RE
CO
NN
EC
TIO
N
DO
OR
RE
TU
RN
SY
ST
EM
RE
TU
RN
SY
ST
EM
PR
ES
S
SY
ST
EM
RE
TU
RN
SY
ST
EM
PR
ES
S
SY
ST
EM
PR
ES
SS
YS
TE
MR
ET
UR
N
RE
TU
RN
PR
ES
SU
RE
RE
TU
RN
PR
ES
SU
RE
NO
RM
NO
RM
RE
LR
EL
HY
DH
YD
PR
ES
SP
RE
SS
L H
PM
PL
H P
MP
PRES
S LO
PRES
S LO
R H
PM
PR
H P
MP
PRES
S LO
PRES
S LO
HYD
HYD
LEVE
L LO
LEVE
L LO
LEV
EL
LOW
FLO
AT S
WIT
CH
(0.6
1 G
AL)
RE
SE
RV
OIR
CA
PAC
ITY
(1.1
GA
LLO
N)
15-S
EC
TIM
E D
ELA
Y15
-SE
CT
IME
DE
LAY
HY
DR
AU
LIC
PR
ES
SU
RE
GA
UG
E
PR
ES
SU
RE
RE
LIE
FV
ALV
E
RE
SE
RV
OIR
15P
SI
BLE
ED
AIR
CA
P
LE
GE
ND
SU
PP
LY
PR
ES
SU
RE
RE
TU
RN
BLE
ED
AIR
FIL
TE
R
Fig
ure
29-
1.
Hyd
rau
lic S
yste
m S
chem
atic
Electrical System Notes
- 26 -
24-2 FOR TRAINING PURPOSES ONLY
HAWKER 400XP/BEECHJET 400A MAINTENANCE TRAINING MANUAL
BAT
TE
RY
RE
LAY
BO
X
BAT
TE
RY
RE
LAY
BO
X
MA
IN P
OW
ER
DIS
TR
IBU
TIO
NB
OX
(A
FR
AM
E)
MA
IN P
OW
ER
DIS
TR
IBU
TIO
NB
OX
(A
FR
AM
E)
MA
IN B
ATT
ER
Y(4
0AH
LE
AD
AC
ID)
(36A
H N
ICA
D)
MA
IN B
ATT
ER
Y
EX
TE
RN
AL
PO
WE
RR
EC
EP
TC
ALE
ELE
CT
RIC
AL
DIS
TR
IBU
TIO
NPA
NE
LS (
CB
)
ELE
CT
RIC
AL
DIS
TR
IBU
TIO
NPA
NE
LS (
CB
)
STA
RT
ER
-G
EN
ER
ATO
R(4
00 A
MP
)
LEF
T S
TAR
TE
R-
GE
NE
RAT
OR
L LO
AD
BU
S P
OW
ER
L LO
AD
BU
S P
OW
ER
R L
OA
D B
US
PO
WE
R
R L
OA
D B
US
PO
WE
R
EM
ER
GE
NC
Y B
US
PO
WE
R
EM
ER
GE
NC
Y B
US
PO
WE
R
RIG
HT
STA
RT
ER
GE
NE
RAT
OR
STA
ND
BY
BAT
TE
RY
STA
ND
BY
BAT
TE
RY
STA
ND
BY
BU
S P
OW
ER
STA
ND
BY
BU
S P
OW
ER
Fig
ure
24-
1.
Ele
ctri
cal P
ow
er S
yste
m L
ayo
ut
24-6 FOR TRAINING PURPOSES ONLY
HAWKER 400XP/BEECHJET 400A MAINTENANCE TRAINING MANUAL
RIG
HT
GC
U
LEF
TG
EN
RE
LAY
RIG
HT
GE
NR
ELA
Y
EX
TE
RN
AL
PO
WE
RR
EC
EP
TAC
LE
EX
TE
RN
AL
PO
WE
RR
ELA
Y
BAT
TE
RY
RE
LAY
BAT
TE
RY
FE
ED
ER
PR
OT
EC
TIO
NU
NIT
BAT
TE
RY
TIE
-IN
RE
LAY
RIG
HT
STA
RT
ER
-G
EN
ER
ATO
R
LEF
T S
TAR
TR
ELA
YR
IGH
T S
TAR
TR
ELA
Y
VC
MM
OD
ULE
LEF
T L
OA
D B
US
RIG
HT
LO
AD
BU
SE
ME
RG
EN
CY
BU
S
LEF
T R
AD
IO B
US
LEF
T M
AIN
BU
S
STA
RT
BU
S
STA
RT
BU
S
HO
T B
ATT
ER
Y B
US
BAT
TE
RY
CH
AR
GE
BU
S
LEF
T G
CU
LEF
T S
TAR
TE
R-
GE
NE
RAT
OR
RIG
HT
RA
DIO
BU
S
STA
ND
BY
BU
S
LEF
T N
ON
-E
SS
EN
TIA
L B
US
LEF
TO
VE
RH
EA
D B
US
RIG
HT
OV
ER
HE
AD
BU
SR
IGH
T N
ON
-E
SS
EN
TIA
L B
US
GA
LLE
Y B
US
RIG
HT
MA
IN B
US
EM
ER
GE
NC
YB
US
PO
WE
RR
ELA
Y
EM
ER
GE
NC
YB
US
TIE
RE
LAY
STA
ND
BY
PO
WE
RS
UP
PLY
GA
LLE
Y B
US
RE
LAY
AH
RS
AU
XB
ATT
ER
Y
NO
. 1IN
VE
RT
ER
NO
. 2IN
VE
RT
ER
LOA
DS
HE
DR
ELA
Y
LOA
DS
HE
DR
ELA
YN
O. 2
INV
ER
TE
RR
ELA
Y
VC
MP
OW
ER
RE
LAY
CO
ND
ITIO
N 2
: AIR
CR
AF
T O
N G
RO
UN
D, B
AT
TE
RY
SW
ITC
H O
N, S
TAN
DB
Y P
OW
ER
AR
ME
D
STA
ND
BY
PO
WE
RS
WIT
CH
STB
YS
TBY
PW
RP
WR
AR
MA
RM
ON
ON
NO
TE
:
NO
N-E
SS
EN
TIA
L B
US
LO
AD
SH
ED
RE
LAY
S O
NLY
FIT
TE
D
ON
RK
-98,
RK
-110
AN
D A
FT
ER
LE
GE
ND
CU
RR
EN
T T
RA
NS
FO
RM
ER
RE
MO
TE
CO
NT
RO
L C
IRC
UIT
BR
EA
KE
R
CIR
CU
IT B
RE
AK
ER
SW
ITC
H
CIR
CU
IT B
RE
AK
ER
GR
OU
ND
STA
ND
BY
BAT
TE
RY
PO
WE
R
MA
IN B
ATT
ER
Y P
OW
ER
Fig
ure
24-
2.
Ele
ctri
cal P
ow
er D
istr
ibu
tio
n S
yste
m (
2 o
f 12
)
24-106 FOR TRAINING PURPOSES ONLY
HAWKER 400XP/BEECHJET 400A MAINTENANCE TRAINING MANUAL
0
505010
010
0
150
150
N0.
1 IN
VN
0.1
INV
N0.
2 IN
VN
0.2
INV
26V
26V
26V
26V
115V
115V
115V
115V
SE
CO
ND
AR
Y11
5 V
AC
BU
S
PR
IMA
RY
115
VA
C B
US
PR
IMA
RY
115
VA
CS
HE
D B
US
SE
CO
ND
AR
Y26
VA
C B
US
PR
IMA
RY
26 V
AC
BU
SP
RIM
AR
Y26
VA
CS
HE
D B
US
AC
BU
S S
HE
DA
C B
US
SH
ED
2
2
2
2
AC
PR
I BU
S
AC
SE
C B
US
26V
26V
115V
115V
A U T O
INV
SE
LIN
V S
EL
NO
.1N
O.1
INV
SE
LIN
V S
EL
NO
.2N
O.2
NO
.2N
O.2
NO
.1N
O.1
ON
ON
OF
FO
FF
INV
ER
TE
RIN
VE
RT
ER
PIT
CH
TR
IMP
OS
L LO
AD
BU
S
No.
1 IN
VE
RT
ER
R L
OA
DB
US
EM
ER
BU
S
AU
TOM
ATIC
TR
AN
SF
ER
L O
IL P
RE
SS
R O
IL P
RE
SS
FLA
P P
OS
CO
ND
ITIO
N 1
: NO
RM
AL
OP
ER
AT
ION
No.
1 IN
VE
RT
ER
115
VA
C
No.
2 IN
VE
RT
ER
115
VA
C
28 V
DC
PO
WE
R
No.
1 IN
VE
RT
ER
26
VA
C
No.
2 IN
VE
RT
ER
26
VA
C
GR
OU
ND
LE
GE
ND
AC
BU
SS
HE
DD
ING
RE
LAY
No.
2 IN
VE
RT
ER
PO
WE
R R
ELA
Y
No.
2 IN
VE
RT
ER
Fig
ure
24-
39.
Haw
ker
400X
P/B
eech
jet
400A
AC
Po
wer
Sys
tem
(1
of
6)
Pressurization and Environmental System Notes
- 28 -
CA
BIN
PR
ES
SU
RE
CO
NT
RO
LL
ER 1
2
3
26
28
24
SL
45
67
8
910
30 35
40
50
45
DIF
FP
RE
SS
DIF
FP
RE
SS
CO
NT
RO
LLE
R
CABIN
CA
BIN
ACFT
X1000ALTFT
MA
NU
AL
PR
ES
SU
RE
CO
NT
RO
LV
ALV
E
NE
ED
LE
VA
LV
EL
EF
TO
UT
FL
OW
SA
FE
TY
VA
LV
E
S2
SO
LE
NO
IDV
ALV
E(N
.C)
S3
SO
LE
NO
IDV
ALV
E(N
.C)
S1
SO
LE
NO
IDV
ALV
E(N
.O.)
SC
RE
EN
SC
RE
EN
SC
RE
EN
TE
ST
SH
UT
OF
FV
ALV
E
CH
EC
KV
ALV
EJE
TP
UM
PE
JE
CT
OR
15
PS
IP
NE
UM
AT
ICA
IRS
UP
PLY
DU
MP
VA
LV
E
TE
ST
PO
RT
No
.1
TE
ST
PO
RT
No
.2
TE
ST
PO
RT
No
.3
MA
NP
RE
SS
CO
NT
MA
NP
RE
SS
CO
NT
INC
DE
C
0
5 10
15
20
25
304050
12 3 4
56
78910
CA
BIN
ALT
1000
FT
CA
BIN
CL
IMB
CA
BIN
CL
IMB
0
1 1
2 2
4 4
6
.5 .5
UP
DO
WN T
HD
SF
EE
TP
ER
MIN
TH
DS
FE
ET
PE
RM
IN
MA
NIF
OL
D
MA
NIF
OL
D
MA
NIF
OL
D
AIR
GN
D
LT
HR
US
TL
EV
ER
SW
RT
HR
US
TL
EV
ER
SW
LG
ND
SA
FE
TY
SW
ITC
H
>85º
N2
>85º
N2
<85º
N2
<85º
N2
LL
OA
DB
US
CA
BIN
PR
ES
S
PN
EU
MA
TIC
RE
LA
Y
AIR
FIL
TE
R
RIG
HT
OU
TF
LO
WS
AF
ET
YV
ALV
E
MIN
MIN
MIN
MIN
MIN
MA
X
MA
X
MA
X
MA
X
MA
X
VA
CU
UM
RE
GU
LA
TO
R
LE
GE
ND
RE
GU
LA
TE
DV
AC
UU
M
AM
BIE
NT
AIR
PR
ES
SU
RE
PN
EU
MA
TIC
RE
LA
YR
EF
ER
EN
CE
PR
ES
SU
RE
CO
NT
RO
LL
ER
RE
FE
RE
NC
EP
RE
SS
UR
E
15
PS
IP
NE
UM
AT
ICP
RE
SS
UR
E
CA
BIN
AIR
PR
ES
SU
RE
Pre
ssurization
Contr
olS
yste
mC
ON
DIT
ION
:A
IRC
RA
FT
ON
TH
EG
RO
UN
DIN
TH
EU
NP
RE
SS
UR
IZE
DM
OD
E
ALT
ITU
DE
LIM
ITE
R
ALT
ITU
DE
LIM
ITE
R
RIG
HT
ALT
ITU
DE
LIM
ITC
ON
TR
OL
LE
R
LE
FT
ALT
ITU
DE
LIM
ITC
ON
TR
OL
LE
RPR
ES
SU
RE
HU
LL
Oxygen System
- 30 -
OX
YG
EN
SU
PP
LY
CY
LIN
DE
R
HIG
H P
RE
SS
UR
ER
UP
TU
RE
DIS
C(2
700-3
000 P
SI)
CH
EC
KV
ALV
E
CH
EC
KV
ALV
E
OV
ER
BO
AR
DD
ISC
HA
RG
EIN
DIC
AT
OR
RE
GU
LA
TO
R A
ND
SH
UT
OF
F V
AL
VE
SE
CT
ION
(7
0P
SI)
LO
WP
RE
SS
UR
ED
ISC
(6
0P
SI)
28
VD
C
28
VD
C
5A
CB
11
1
OX
YG
EN
CO
NT
PA
SS
EM
ER
BU
SS
08
8
OX
YG
EN
AL
TIT
UD
EB
AR
OM
ET
RIC
SW
ITC
H
TO
EM
ER
GE
NC
YP
RE
SS
VA
LV
E C
ON
TR
OL
PA
SS
EN
GE
R O
XY
GE
NS
HU
T O
FF
VA
LV
EV
L1
13
MA
NU
AL
AN
D
SO
LE
NO
IDO
PE
RA
TE
DP
AS
SE
NG
ER
MA
SK
CO
MP
AR
TM
EN
T(2
MA
SK
S)
PA
SS
EN
GE
R M
AS
KC
OM
PA
RT
ME
NT
(SIN
GL
E M
AS
K)
PA
SS
EN
GE
R M
AS
KC
OM
PA
RT
ME
NT
(SIN
GL
E M
AS
K)
PA
SS
EN
GE
R M
AS
KC
OM
PA
RT
ME
NT
(SIN
GL
E M
AS
K)
PA
SS
EN
GE
R M
AS
KC
OM
PA
RT
ME
NT
(SIN
GL
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AS
K)
PA
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R M
AS
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PA
RT
ME
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(SIN
GL
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AS
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PA
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R M
AS
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PA
RT
ME
NT
(SIN
GL
E M
AS
K)
PA
SS
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R M
AS
KC
OM
PA
RT
ME
NT
(2 M
AS
KS
)
PA
SS
EN
GE
R M
AS
KC
OM
PA
RT
ME
NT
(2 M
AS
KS
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PA
SS
EN
GE
R M
AS
KC
OM
PA
RT
ME
NT
(2 M
AS
KS
)
PA
SS
EN
GE
R M
AS
KC
OM
PA
RT
ME
NT
(2 M
AS
KS
)
PA
SS
EN
GE
R M
AS
KC
OM
PA
RT
ME
NT
(2 M
AS
KS
)
OX
YG
EN
PR
ES
SU
RE
SE
NS
E S
WIT
CH
OX
YG
EN
PR
ES
SU
RE
SE
NS
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WIT
CH
PA
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OX
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RO
L K
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SY
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RO
L K
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PIL
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PIL
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NM
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12
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50
PS
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50
PS
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OR
SH
RO
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OR
OX
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L P
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EN
PR
ES
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AV
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BA
Y O
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SS
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LA
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RW
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DP
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KH
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PA
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R O
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ME
NT
(R
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0 A
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N M
AS
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GE
ME
NT
(R
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RU
RK
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EP
T R
K-9
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Oxyg
en
Syste
m S
ch
em
atic
HIG
H P
RE
SS
UR
E
LO
W P
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SS
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LE
GE
ND
Ice and Rain Protection System
- 32 -
10
8
7
7
6
5
4
3
2
1
1 ELEVATOR HORN2 HORIZONTAL STABILIZER LEADING EDGE3 ENGINE INTAKE DUCT4 HEATED WINDSHIELD5 WINDSHIELD WIPER (RK-1 THRU RK-242)6 HEATED PITOT TUBE7 ANGLE OF ATTACK TRANSMITTER8 WING LEADING EDGE10 HEATED STATIC PORTS
Anti Ice, Deice, and Rain Protected Locations
