曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

breathingi s suppliedt o the crew under pressurefr om an
on-board oxygen generating system with stored gaseous
oxygen as backup. The cockpit arrangement provides
minimum duplication of control capability, which, of
necessity, requires two crewmen for flight.
1.1.2.1 Pilot Cockpit. The forward station of the
cockpit is arrangeda nd equippedf or the pilot (FO-3). In
addition to threee lec,tronicd isplays for viewing tactical,
flight, navigational, and ECM data, the pilot instrument
panel also contains armament controls, flight and engine
instmments. Engine controls, fuel management, auxiliary
devices, autopilot, and communication control panels
are on the left console. Display, power, lighting, and
environmental controls are on the right console.
1.1.2.2 RIO Cockpit. The aft station of the cockpit
is equipped for the RIO (FO-4). This instrument panel
l-l ORIGINAL
NAVAIR 0%F14AAD-1
Figure 1-I. Aircraft Dimensions
contains controls and three electronic displays for the
radar, tactical, and navigational flight instruments. Armament
controls, sensor controls, and communication
panels are on the let? console. The right console contains
a navigational display, data entry unit, ECM controls,
data-link controls and lighting, and the IFF panel.
1.1.3 Electronic Nomenclature. Figure 1-3 is an
alphabeticalisting ofthe tactical, communication, navigation,
flight control, and instruments in the aircraft.
1.1.4 Technical Directives. As technical changes
are made to the aircraft, those that affect aircraft operation
or pilot and RIO need-to-know operation will be
incorporated in the appropriate sections and listed in the
Summary of Applicable Technical Directives in the
front of this manual. In some instances, technical directives
may be incorporated on the aircrag while it is still
on the production line before delivery. Check the Technical
Directives Section of the Aircraft Log Book for
applicable modifications. The following are types of
technical directives used in this manual:
ACC
ACC
AFC
Aviation Armament Change
Aircrew System Change
Airhame Change
AVB Avionics Bulletin
AVC Avionics Change
AYC Accessories Change.
1.1.5 Block Numbers. The following production
block numbers correspond to aircrag serial numbers
@No). Selectedb locks 85a nd 110a reu pdatedto F-14D/
block 170 configuration.
BlockNo.
160
165 163693 - 163904
170 164340 - 164351and
164599 - 164604
85
110
Serial No. (BuNo)
163412 - 163416
159610,159613.159600,
159629,159628.159619,
159592,159595,159603,
159635,159633,159018,
159630,159608,159631
161159,161158,161166.
161163,161154.
ORIGINAL 1-2
NAVAIR Ol-Fl4AAD-1
Length
Height (Tail)
62
16
8.5” Cross bleed 2 min continuous then 10 min off
0” I Start Cari 5 min continuous then 10 min off
Wingspan @ 20’ wingsweep
Wingspan @ 68’ wingsweep
Wingspan in oversweep
Wing Area
FF = 950 - 1400 PPH HYD PRESS = 3000 psi
EGT = 780 - 935°C NO2 POS INFLIGHT
AOB < 45”
Roll SAS on
Min 200’ AGL for flaps/slats up on takeoff
Min 800’ AGL for dirty-up
Min 180 MS for retraction of flaps
12 units AOA for all transitions
15kt.S m/n speed for antiskid operation
165 MS mex wheel braking (51 .O k A/C)
190kts max tire speed
20 MS max 90” crosswind component
6Okts max canopy open
HOT START: 890°C (will normally peak
@ 30 - 40% RPM)
HUNG START Hung RPM below63% with rising EG
No lightoff within 20 set of
throttle to IDLE
RPM = 96%
EGT = 950 f 10°C
(initiates engine overtemp alarm)
= 10,500 pph
AOA = 18i05UNlTS
FUEL = 2,000 i 200# (all tapes and windows)
LIGHTS: Land R FUEL LOW
20% Mln RPM with throttle at idle
30% Max RPM with pneumatic starter
30% RPM must fall below for generator
auto-reset
50% Engine crank switch automatically shuts off
60% Generator comes on line
50% Generator light illuminates (if RPM falling)
60% Ensure engine crank off (ovsplvalve)
62 - 78% Normal idle
75 - 90% Auto throttle range
95 - 104% MIL & above
107.7% Overspeed (chevrons flash)
110.0% Engine secures (fuel shutoff)
M/n auxiliary canopy (3000 psi)
M/n normal canopy (3000 psi)
CHS accumulator
FHS accumulator
M/n emergency gear preflight
M/o emergency gear extension
Wheel brake accumulator (2 gages)
Arresting hook dashpot
800 psi
1200 psi
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：F-14D 飛行手冊 Flight Manual 1(54)