Cessna Hawk XP R172K Pilot Operating Handbook page 57

ITEM NO
ARM INS
EQUIPMENT LIST DESCRIPTION
REF DRAWING WT lBS
D25-S
D28-R
D38-R
D41-R
D43-R
D49-A
D55-R
D64-S
D64-A-2
D64-A-3
'D67-A
D82-A
D85-R
D88-S
088-0-1
088-0-2
D91-A
E05-R
E05-0
E07-R
E07-0
E09-S
ED9-0
ElI-A
CLOCK, ELECTRIC
COMPASS INSTALLATION. MAGNETIC
INSTRUMENT CLUSTER, LH
&
RH FUEL
INSTRUMENT CLUSTER. OIL TEMP
&
OIL PRES.
INST. CLUSTER, AMMETER, CYL HEAD TEMP.
INDICATOR. ECONOMY MIXTURE (E.G.T.)
GAGE, MANIFOLD PRESSURE
&
FUEL FLOW
GYRO INSTALLATION, ATTITUDE
&
DIRECTIONAL
(NON NAV-O-MArIel
DIRECTION INDICATOR (AV. OF FOUR)
ATTITUDE INDICATOR (AV. OF THREE)
GYRO INSTALLATION (SIMILAR TO D64-A-l
EXCEPT DIRECTION IND. HAS A MOVABLE
HEADING POINTERJ(INDICATOR NET CHANGE)
GYRO INSTALLATION FOR 300 NAV-O-MATIC
DIRECTIONAl INDICATOR (ARCI
ATTITUDE INDICATOR (AV. OF THREE)
NOTE--THE ABOVE GYRO SYSTEMS REQUIRE
A61-A VACUUM SYSTEM
RECORDER, FLIGHT HOUR
GAGE. OUTSIDE AI~ TEMP IC668507-01011
TACHOMETER INSTALLATION
RECORDING TACH HEAD
TACH FLEXIBLE SHAFT
TURN COORDINATOR
TURN COORDINATOR (FOR AUTO-PILOT USE)
TURN
&
BANK INDICATOR
INDICATOR. RATE OF CLIMB
E. CABIN ACCOMMODATIONS
C664508-0 101
0513262
C669511-0102
C669512-0103
C669514-0101
0501043
C662037-0108
C661075
C661076
1201126
0501054
40760
C661076
0501052
0500221
0506005
C668020-0105
S-1605-'4
C661003-0504
S-1302N2
C6610BO-0101
0514122
0514123
0514122
0514124
0514125
0501009-6
S-1746-5
0515002
12.6
23.0
12.6
23.0
22.0
23.0
8.4*
0.8
6.7
0.4
0.5
0.5
0.5
0.5
0.6
1.1
6.1*
2.7
2.2
6.6*
0.5
6.8*
3.3
2.2
0.8
0.1
1.0*
0.6
0.3
1.3
1.9
2.0
1.0
16.3
26.0
16.2
16.2
16.2
7.8
16.5
12.9*
13.2
13.4
12.9*
13.2
12.5*
13.3
13.4
5.9
28.6
13.0*
15.5
2.0
15.8
14.5
14.5
15.7
44.0
41.5
44.0
41.5
79.5
79.5 .•
lOI.1~
100.8
100.8
SEAT. ADJUSTABLE FORE
&
AFT, PILOT
SEAT. INFINITE ADJUSTING, PILOT
SEAT. ADJUSTABLE FORE
&
AFT, CO-PILOT
SEAT. INFINITE ADJUSTING, CO-PI LOT
SEAT, REAR lONE PIECE BACK CUSHION)
SEAT. REAR (TWO PIECE BACK CUSHION)
SEAT INSTALLATION, CHILD'S FOLD-AWAY
LAP BELT ASSEMBLY
SEAT ASSEMBLY, CHILD'S
ITEM NO
ARM INS
EQUIPMENT LIST DESCRIPTION
REF DRAWING WT lBS
EI5-R
El5-S
E19-0
E23-S
E27-S
E27-0
E33-0
E35-A-l
E35-A-2
E37-A
E39-A
E43-A
E49-A
E50-A
E51-A
E53-A
E55-S
E57-0
E65-R
E71-A
E75-A
E85-A
E87-S
E89-A
FOI-R
FOI-O-l
FOI-O-2
F04-R
FlO-S
FI0-0-1
BELT ASSEMBLY, PILOT LAP
SHOULDER HARNESS ASSEMBLY, PILOT
INERTIA REEL-SEAT BELT INSTALLATION,
PILOT
&
CO-PILOT (NET CHANGE)
BELT
&
SHOULDER HARNESS ASSY. CO-PILOT
SEAT BELT ASSEMBL y, REAR (SET OF TWO)
BELT
&
SHOULDER HARNESS ASSY, 2ND ROW (2)
CARPETING, BLACK, NET CHANGE FOR STANDARD
SEAT COVERING, VINYL, NET CHANGE
SEAT COVERING, LEATHER, NET CHANGE
WINDOW. RIGHT DOOR HINGED (NET CHANGE)
WINDOWS, OVERHEAD CABIN TOP (NET INCREASE)
VENTILATION SYSTEM, REAR SEAT
CUP HOLDER, RETRACTABLE (SET OF TWO)
HEADREST. FRONT (SET OF TWO)
HEADREST, REAR (SET OF TwO)
MIRROR. REAR VIEW
SUN VISORS (SET OF 2)-R.o~.N
TINTED GLASS (All AROUND) (NET CHANGE)
BAGGAGE TIE DOWN NET
RINGS. CARGO TIE DOWN
STRETCHER INSTALLATION - BOXED (USE ACTUAL
WEIGHT AND ARM CHANGE
CONTROLS. DUAL (CO-PILOT'S WHEEL, PEDALS
AND TOE BRAKES)
CONTROL WHEEL WITH PROTECTIVE PADDING
RUDDER PEDAL (SET OF TWO)
RUDDER TRIM SYSTEM
ALL PURPOSE CONTROL WHEEL - NET CHANGE
F. PLACARDS
&
WARNING
5-2275-103
5-2275-201
0501046-1
5-2275-3
S-1746-13
5-2275-8
CES-1l51
0511803
0511800
0700322
0501023
1215073
1215073
0500312
0500040
2015009-6
0500042
0100164
0506005
0510402
0513290
0760020
0505053
0505053
0505053
0523112
0505063
0505055
PLACARD. OPERATIONAL LIMITATIONS VFR DAY
PLACARD, OPERATIONAL LIMITATIONS VFR DAY-
NIGHT
PLACARD, OPERATIONAL LIMITATIONS IFR DAY-
NIGHT
STALL WARNING HORN (PNEUMATIC)
PILOTS CHECK LIST (STANDARD
A/C)
(STOWED)
PILOTS CHECK LIST (200A NAV-O-MATIC)
1.0
0.6
2.0
1.6
2.0
3.2
0.0
0.0
2.0
2.3
0.9
1.7
0.1
1.5
1.5
0.3
0.9
0.0
0.5
1.0
2.0
1.1
1.9
0.0
0.0
0.0
0.0
0.5
0.0
0.0
37.0
37.0
82.0
37.0
70.0
70.0
62.0
47.0
41.9
50.9
15.5
47.0
86.0
15.5
32.8
95.0
12.4*
26.0
6.8
<;.4
28.5