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Суб 02 Мар 2013 21:25:10
Я медведь, такие дела.
Суп /б. Сегодня у меня был ужасный день. Меня подарили тян на день рождения. В 6 утра меня вытащили на вокзал в подарочном пакете, который начал расклеиваться на морозе. Сначала я ехал в автобусе, в том же самом пакете, пять часов. Потом кун-мудак прождал её пол часа под снегопадом, в результате чего моя мягкая шёрстка намокла. Он хотел вытащить и показать меня ей прямо на морозе. К счастью, она попросила подождать его до дома. Меня принесли к ней домой, усадили. Я уж обрадовался, но буквально через пару часов моя нынешняя хозяйка использовала меня как платок и поплакалась в меня. У меня намок бок, после чего эти два злых человека не раз открывали окно, так что я чуть не простудился. И это только первый день. Как теперь жить, двач? Алсо, выполняю реквесты на дабл, только учти, я - детская игрушка.


Суб 02 Мар 2013 21:27:58
>>44302414
У моей тян есть твой брат-близнец

Суб 02 Мар 2013 21:30:51
>>44302593
Как ему живется? Его кормят манной кашкой?

Суб 02 Мар 2013 21:31:46
>>44302414
>два злых человека не раз открывали окно
Зачем?

Суб 02 Мар 2013 21:34:16
>>44302771
>Как ему живется?
Полагаю, что не плохо он, по крайней мере, не жалуется
>Его кормят манной кашкой?
Нет, впроголодь живет но все никак не похудеет

Суб 02 Мар 2013 21:35:53
>>44302888
>впроголодь живет
>все никак не похудеет
Вся суть жиробасов.

Суб 02 Мар 2013 21:38:11
>>44302414
Мишутка! А зачем ты фоткаешься на айпад? Качество же фу!
Алсо,реквесты сексуального характера принимаются?

Суб 02 Мар 2013 21:40:46
>>44303247
Это твоя хозяйка?

Суб 02 Мар 2013 21:46:06
>>44303107 Айфон у неё вечно разряжен. Я тут, вообще, один, у неё больше нет игрушек.

Суб 02 Мар 2013 21:47:27
>>44303349 К сожалению, нет

Суб 02 Мар 2013 21:52:37
>>44303555
>Есть ли подводные камни?
Их нет. Наоборот: сплошная польза: никакого слоя каш на шерстке нет не нужно ее часто мыть не будет терять цвет
>у неё больше нет игрушек.
Сколько же ей лет?

Суб 02 Мар 2013 22:02:05
>>44302414
Куда съебался?

Суб 02 Мар 2013 22:09:14
>>44302414
Все, накамвхорился?

Суб 02 Мар 2013 22:09:27
>>44302414
вероника залогинься, я тебе его дарил

Суб 02 Мар 2013 22:11:56
>>44304813
Не пизди, скотина!
Мою хозяйку не так зовут

Суб 02 Мар 2013 22:20:04
>>44304813 Её не Вероника зовут

Суб 02 Мар 2013 22:21:25
>>44305403
Твоя хозяйка - пидорас?
Ты что, пониеб или что у тебя на пикче?

Суб 02 Мар 2013 22:23:50
>>44305467
Чому же?
Бампаю рандомными пикчами из её коллекции.
Алсо, она не пониёб

Суб 02 Мар 2013 22:25:18
http://2ch.hk/b/res/44300605.html

Суб 02 Мар 2013 22:26:08
>>44305592
Если не пониеб, то зачем коллекция этого ужаса?

Суб 02 Мар 2013 22:26:47
>>44305662 Ой. Создавал тред с айпада, не получалось вроде.

Суб 02 Мар 2013 22:30:14
>>44305741
Получалось. Там вон сколько ответов и реквестов

Суб 02 Мар 2013 22:31:07
>>44305919 Уже отписался там

Суб 02 Мар 2013 22:33:27
>>44305962
Так ты сейчас в каком треде будешь?

Суб 02 Мар 2013 22:35:13
>>44306086 Я повсюду, лол

Суб 02 Мар 2013 22:36:29
>>44306171
Тогда полижи письку у хозяйки

Суб 02 Мар 2013 22:37:38
>>44306237
Ролл

Суб 02 Мар 2013 22:38:32
>>44306299
ДАБЛ!!!
Запиливай с супом!

Суб 02 Мар 2013 22:38:46
>>44302414

нищеброд в треде, все в кадилак.

Покупал своей тни такого же медведя только белого( цена отличается рублей на 300 )

Суб 02 Мар 2013 22:39:38
>>44302414
САЖИ ШЛЮХЕ!!

Суб 02 Мар 2013 22:40:21
Ну что же вы, хуесосы? Нахуя вам этот забитый омежка об которого только слезки вытирать можно, когда есть я. Короче я только что знатно поебался и сижу здесь с ноута моей тян которая пошла вытягивать морковку с задницы. Задавайте свои вопросы охуенному медведю.

Суб 02 Мар 2013 22:41:40
>>44306432
Хули ты без супа?

Суб 02 Мар 2013 22:42:09
Как там можно деанонить, если фотки сделаны с айфона? Помню местоположение одной шлюхи вычислили по одной фотографии.

Суб 02 Мар 2013 22:44:13
>>44306500
Ты знаеш как тяжело писать,когда у тебя плюшевые лапы которыепромокли от вагинального сока таян? Нет! Тогда не пизди.

Суб 02 Мар 2013 22:45:40
Сажи шлюхе, рака яичников ей, устроила тут шмара, уютный чатик !

Суб 02 Мар 2013 22:47:18
>>44306636
Сам не пизди, гондон плюшевый!
ОП вон суп запилил, так что не выебывайся, затычка для пизды

Суб 02 Мар 2013 22:47:55
>>44306718
Двачую этого. Все нижеотписавшиеся без сажи - пиздолисы и никчёмные яйценосцы.

Суб 02 Мар 2013 22:49:16
>>44306718
Пошел нахуй, ничего не знаю не о каких шлюхах, теперь это мой личный тред

Суб 02 Мар 2013 22:50:48
>>44306926
Анус себе личный тред, пёс медвед.

Суб 02 Мар 2013 22:51:06
Суп /б. Сегодня у меня был ужасный день. Меня нашел битард на помойке.
И это только первый день. Как теперь жить, двач? Алсо, выполняю реквесты на дабл, только учти, я - битардская игрушка.

Суб 02 Мар 2013 22:51:54
>>44306816
Так у него лапы сухие, а у меня карандаш из рук выскальзывает

Суб 02 Мар 2013 22:52:09
Не забывайте, что у шмары уже есть главный пиздолис, на хую которого она будет вертеться !

Суб 02 Мар 2013 22:53:05
>>44307079
Возьми в рот карандаш

Суб 02 Мар 2013 22:56:32
>>44302579
Ебать крипота.

Суб 02 Мар 2013 22:59:13
>>44307341
У тебя дома баня? Алсо, нарисуй на стене вокруг него пентаграмму со всякими латинницой и цифрами, облей красной краской и напиши внизу СЕКТА ТИРЕЧА

Суб 02 Мар 2013 23:00:04
>>44307134
Извини чувак, карандаш тян забрала. Видите ли ей мало было того, что я ее три часа морковкой пердолил, так она еще и карандаш спиздила. Но есть другая фотка, может понравится

Суб 02 Мар 2013 23:01:25
>>44307459
Ролл.

Суб 02 Мар 2013 23:02:06
>>44307582
реролл

Суб 02 Мар 2013 23:02:38
>>44307619
реролл2

Суб 02 Мар 2013 23:03:21
>>44307656
последний реролл.

Суб 02 Мар 2013 23:03:52
>>44307696
так близко реролл

Суб 02 Мар 2013 23:06:17
>>44307459
Хуй сам всем в жопу

Суб 02 Мар 2013 23:06:53
>>44305704
Это флаффи. Это искусственно выращенные пушистые пидоры, которые как бы пародия на пони, просто всё как я ненавижу: мелкие, с короткими лапками, пушистые, тупые, умеют говорить (хоть и хуево). Есть схороненный тред, в котором раскрывается вся суть этих сучек. А может, это и не флаффи.

Суб 02 Мар 2013 23:09:29
>>44307874

Ну что пиздолизы ебаные, подумайте кто снимал щлюху на камеру и представте себе этого быдлана !

Суб 02 Мар 2013 23:09:43
>>44307874
Оставь зверушку в покое, потаскуха.

Суб 02 Мар 2013 23:09:49
>>44302414
Засунь свою лапу ей во влагалище

Суб 02 Мар 2013 23:11:26
>>44307874

Сделай ей анилингус, чтобы она стояла раком.

Суб 02 Мар 2013 23:11:50
>>44308154

реролл

Суб 02 Мар 2013 23:12:14
>>44308053

А теперь представьте, как тупорылый быдлан ебёт шлюху-коротышку !

Суб 02 Мар 2013 23:12:14
>>44308154
реролл, блджад.

Суб 02 Мар 2013 23:12:14
>>44308069
Даблы, даблы евривэр!

Суб 02 Мар 2013 23:12:59
>>44308211

О да.

Суб 02 Мар 2013 23:13:20
>>44308069
реролл

Суб 02 Мар 2013 23:13:29
>>44307907
Дело в том, что постя пикчи, комиксы и пасты, где этих флаффи неистово и абсолютно чудовищно мучают, истязают и убивают, одинокие битарды проецируют свою невыраженную агрессию. Неполноценность, социопатия, биомусор. Такие пикчи вызывают симпатию и увлечение только у психологически, социально и генетически ущербных людей. И я не пониеб, просто это гораздо более омерзительней чем обычное гуро.

Суб 02 Мар 2013 23:13:46
>>44308261
Ролл

Суб 02 Мар 2013 23:14:00
>>44308211

Пили с супом, медвед.

Суб 02 Мар 2013 23:15:02
Photosensitive Seizures
A very small percentage of people may experience a seizure when exposed to certain
visual images, including flashing lights or patterns that may appear in video games.
Even people who have no history of seizures or epilepsy may have an undiagnosed
condition that can cause these photosensitive epileptic seizures while watching video
games.
These seizures may have a variety of symptoms, including lightheadedness, altered
vision, eye or face twitching, jerking or shaking of arms or legs, disorientation,
confusion, or momentary loss of awareness. Seizures may also cause loss of
consciousness or convulsions that can lead to injury from falling down or striking
nearby objects.
Immediately stop playing and consult a doctor if you experience any of these
symptoms. Parents should watch for or ask their children about the above symptoms
children and teenagers are more likely than adults to experience these seizures. The
risk of photosensitive epileptic seizures may be reduced by taking the following
precautions: Sit farther from the screen; use a smaller screen; play in a well-lit room;
and do not play when you are drowsy or fatigued.
If you or any of your relatives have a history of seizures or epilepsy, consult a doctor
before playing.

Суб 02 Мар 2013 23:16:08
Getting Started
System Requirements
Operating System: Windows XP SP2 (32-bit), Vista / 7 (32 or 64-bit)
Processor: 3 GHz Single core or 2 GHz Dual Core
Memory: 1 GB RAM
HDD: 4 GB free hard disk space
Graphics: Shader Model 3.0 (Geforce 6 Series, Radeon X1600-Series), 256 MB,
DirectX 9.0c
Drive: DVD-ROM
Modern Times campaign
Tropico 4: Modern Times features a new campaign, consisting of 12 new
missions. The new campaign can be accessed from the main menu by clicking
on Play and then selecting Modern Times Campaign. The campaign from the
original Tropico 4 is located under the name Campaign.
Timeline
The Timeline is a set of events that affect the economy and the politics of your
island. Timeline events will also unlock new building options in Tropico.
During the course of gameplay, the Timeline events will be triggered when a
specific year arrives. Each different game will generate its own different set of
events that will unravel in time. You can see what Timeline events will occur in
the next years by looking at the Timeline Interface (see below). Some Timeline
events, like the Vietnam War Unrest or the Cuban Missile Crisis, are based on
actual historical events.

Суб 02 Мар 2013 23:16:28
давайте обмениваться фотографиями лика войны?

Суб 02 Мар 2013 23:16:39
The events that unlock new buildings (like the Solar Power Plant, or the Seven-
Star Hotel) occur at the same date in every game. The unlocked buildings may
be entirely new or they may replace old buildings with similar functionality (e.g.
the Bio Farm which replaces the Farm). Once the replacement new buildings are
unlocked, the respective old buildings can no longer be constructed.
The Timeline Interface gives you an overview of upcoming events. It can be
accessed from the clock-shaped icon next to the Almanac icon (above the upper
right corner of the minimap).
6
The Timeline on-screen notifications provide in-game information about the
Timeline events which are currently active or have just happened. The Timeline
On-screen notifications appear above the minimap.

Суб 02 Мар 2013 23:16:40
>>44308278
>Такие пикчи вызывают симпатию и увлечение только у психологически, социально и генетически ущербных людей.
Да.

Суб 02 Мар 2013 23:16:56
>>44308438
Отклеилась?

Суб 02 Мар 2013 23:17:30
>>44308261
реРолл

Суб 02 Мар 2013 23:17:31
ДаваЙ

Modern Apartment
Description
Modern building that replaces and upgrades the Apartment. It has better housing
quality and produces less crime and pollution.
Parameters
Price: $10,000
Blueprint cost: $4,000
Housing quality: 75
Number of families: 12
Electricity: 5 MW
Work modes
Normal Maintenance - maintains respectable living conditions.
Roach Patrol - the maintenance needed for the building is cut in half, but the
housing quality is lowered by 30%.
Upgrades
Climate Control - improves housing quality by 15.
Doorman Kiosk - reduces crime in a small area around the building.
Modern Condominium
Description
Modern building that replaces and upgrades the Condominum. Generates less
pollution and crime and requires less upkeep. Houses more citizens.
Parameters
Price: $12,000
Blueprint cost: $6,000
Housing quality: 95
Number of families: 8
Electricity: 10 MW
Work modes
Normal Maintenance - maintains respectable living conditions
Roach Patrol - the maintenance needed for the building is cut in half,

Суб 02 Мар 2013 23:19:03
Нужна пикча с Тарантино.

Суб 02 Мар 2013 23:19:13
>>44308527
лей

Суб 02 Мар 2013 23:19:32
К сожалению у меня нет ничего подобного, но есть много технических мануалов к военной технике.


.4.5.2.3 SEND Option. (U) The SEND option (PB1) sends the GPS and AS/SV crypto keys displayed on the
GPS ENTRY format to all powered JDAM weapons. This causes the SMS and the JDAM weapons to become
classified if not previously classified.
2.4.5.2.4 CLR Option. (U) The CLR option (PB20) clears the current field under the data entry box.
2.4.5.2.5 0-9 Options. (U) Since UFC support is not provided for the GPS ENTRY format, 0 through 9
Digit options (PB6-15) are provided to enter or edit GPS crypto key fields. Digits for each data field are entered
from left to right. Selection of the first digit for a given data field clears the current 5-digit number before entering
the selected digit (Figure 2-17). When the last digit of a field is entered, the data entry box automatically steps to the
next data field and the finished entry is saved. When the last digit in the last field for any column is entered, the next
column is selected, in order.
2.4.6 STORES FORMAT. (U) The STORES format (Figure 2-18) provides control of weapon selection and
management. JDAM acronyms are displayed on the wing planform when a JDAM variant is inventoried. JDAM
weapon select options (PB6-10) are available for every inventoried variant, including JDAM training.
J-84
J109
J-83
JDAM
JDAM Weapon
Select Options
578
1
J-83
1
JDAM
1
J-84
1
J-109
ADV CDATA
DATA
MENU
WIND
Figure 2-18
STORES FORMAT OPTIONS (U)
SECRET
2-17

Суб 02 Мар 2013 23:20:12
Медвед, сфотографируйся сидя на унитазе.

Суб 02 Мар 2013 23:20:37
>>44308640
ОТЛИЧНО!

Суб 02 Мар 2013 23:20:56
2.8.3.1 Wheel Brake Assembly. Each main landing gear wheel is fitted with hydraulically actuated
multiple disk brakes. There are two independent sets of brake lines running to each wheel brake
assembly: the normal brake line pressurized by HYD 2A and the emergency brake line pressurized by
HYD 2B or the brake and APU accumulators. See figure 2-17. Only one set of brake lines can be
pressurized at any given time. A shuttle valve on each wheel brake assembly switches from normal to
emergency brake pressure, depending on which is applied.
Each wheel brake assembly has a brake wear indicator pin, located on the inboard side of the wheel.
When the brakes are applied and the indicator pin is flush or below flush with the brake housing, the
brake pads require changing.
Each wheel assembly incorporates a fuse plug which is designed to melt and deflate the tire at
temperatures below those which would result in a catastrophic tire blowout.
2.8.3.2 Wheel Brake Operation. Each main wheel brake is controlled by a separate brake pedal,
integrated into the rudder/brake pedal mechanism. Pilot applied force to the top of each brake pedal
is transmitted by a series of cables and pulleys directly to the brake control hydraulic servovalves,
located in the nose wheelwell. The amount of hydraulic pressure applied to the wheel brakes by the
servovalves is directly proportional to brake pedal force. Dual brake pedal action provides symmetric
braking, while individual brake pedal action provides differential braking.
2.8.3.3 Normal Braking. Normal braking is enabled when HYD 2A is operable and the EMERG
BRK handle is in the stowed position. The emergency brake valve is closed and the emergency brake
lines are unpressurized. During normal braking, HYD 2A pressure is applied through the left and right
servovalves proportional to the amount of pilot applied brake pedal force and is routed to the main
wheel brakes. When the ANTI SKID switch is ON, the anti-skid system modulates pilot applied brake
pressure in order to prevent wheel skid. When the ANTI SKID switch is OFF, the pilot must regulate
brake pedal force to prevent wheel skid.
2.8.3.4 Anti-skid System. The anti-skid system performs 4 basic functions which are designed to
maximize braking effectiveness during landing rollout: touchdown protection, wheel spin-up override,
skid control, and locked wheel protection. The anti-skid system is enabled when the ANTI SKID
switch is ON and the LDG GEAR handle is DN.

Суб 02 Мар 2013 23:21:35
Няша, фотки ступней или я уебываю

Суб 02 Мар 2013 23:21:39
Figure 2-17. Wheel Brake and Anti-skid System
Failure of either wheel speed sensor can lead to an antiskid failure,
resulting in a complete loss of brakes. Placing the ANTI SKID switch to
the OFF position or pulling the EMERG BRK handle will bypass the
faulty system and restore braking ability. Judicious braking must be
used, as the antiskid system is not available. Refer to the BRAKES
FAILURE/EMERGENCY BRAKES procedure.
The system contains two wheel speed sensors, an anti-skid control unit, and an anti-skid control
valve. The anti-skid control unit senses wheel speed and operates by electronically limiting the amount
of HYD 2A pressure that is applied to the wheel brakes through the anti-skid control valve and the
normal brake lines. Anti-skid is not available when emergency brakes are selected.
Touchdown protection delays initial brake application on landing by completely dumping brake
pressure until (1) weight is on the right main landing gear and wheel speed is over 50 knots or (2), if
a wet runway delays wheel spin-up, for 3 seconds after landing. This function prevents landing with
locked main wheels (tire blowouts) even if full brake pedal force is applied at touchdown.
Wheel spin-up override is activated at 50 knots wheel speed to allow normal braking if the right
WonW switch fails.

Суб 02 Мар 2013 23:22:16
>>44308751
Пожаловался на вайп без сажи

Суб 02 Мар 2013 23:23:50
НО ВЕДЬ ТАК КУКЛОСКРИПТ СКРОЕТ !

Skid control is enabled when sensed wheel speed differs from what the anti-skid control unit
determines it should be (e.g., hydroplaning is detected). If the system detects wheel skid, anti-skid
limits the amount of HYD 2A pressure applied to both brakes as required to prevent skidding. If no
skid exists, full pilot-applied brake pressure is routed to the brakes.
If the speed of one wheel drops 40% below the other wheel, locked wheel protection dumps brake
pressure to both wheels until the speed of the slower wheel returns above 40% of the other. Locked
wheel protection is removed below 35 knots, so that full braking performance (including locking a tire)
is available for taxi and turning operations. Below 14 knots, anti-skid is completely disabled. Below 35
knots, judicious braking is required to avoid flat spotting tires.
NOTE
Hot brakes and/or melted wheel assembly fuze plugs can be expected
any time maximum effort braking is used at heavy gross weights with
or without anti-skid, e.g., aborted takeoff or heavy weight landing
(above 46,000 lb GW) with high taxi brake usage.
2.8.3.4.1 ANTI SKID Switch. The ANTI SKID switch, located on the lower left main instrument
panel, is used to manually disable the anti-skid system, e.g., for carrier operations or following an
anti-skid failure (ANTISKID caution displayed). The switch is lever-locked in the OFF position.
ON Anti-skid system enabled for use with normal braking.
OFF Anti-skid system disabled (SKID advisory displayed when the landing gear is
down).
2.8.3.4.2 Anti-skid BIT and the ANTISKID Caution. The anti-skid control unit performs two types of
BIT: initiated and periodic. IBIT is performed when power is initially applied to the anti-skid system:
(1) when the landing gear is lowered, (2) when the ANTI SKID switch is selected from OFF to ON
inflight, or (3) on the ground with the parking brake set. IBIT performs a complete test of the anti-skid
system 9 seconds after power is applied and runs for 4.5 seconds. With WonW, IBIT is inhibited with
the parking brake released, as wheel motion will cause a false BIT failure and brake pressure would be
dumped if brakes were applied. PBIT only performs a partial anti-skid test and runs whenever power
is applied and IBIT is not running.
If an anti-skid failure is detected by either BIT, the ANTISKID caution will be displayed at BIT
completion. If an anti-skid failure is detected by PBIT, cycling the ANTI SKID switch will command
an IBIT and a more complete test of the system. When IBIT is running, the ANTISKID caution is
inhibited or is removed if previously displayed. If the ANTISKID caution returns after IBIT, the
ANTI SKID switch must be placed to OFF in order to isolate the failure and make sure that normal
braking (without anti-skid) is available.
For instance, assume the right wheel speed sensor has failed and an ANTISKID caution is displayed.
If the ANTI SKID switch is left ON during landing, touchdown protection circuitry will dump and
never restore brake pressure to both wheels. Normal braking will be lost. In this case, placing the ANTI
SKID switch to OFF will restore normal braking (without ant

Суб 02 Мар 2013 23:24:48
Figure 2-18. Emergency/Parking Brake Handle
Do not cycle the ANTI SKID switch in response to an ANTISKID
caution immediately prior to landing. Cycling the ANTI SKID switch
removes the ANTISKID caution for up to 13.5 seconds as the system
performs IBIT even though the anti-skid system may still be failed
and, if the system is not failed, wheel motion at touchdown may cause
a false BIT failure and a dump of normal brake pressure when brakes
are applied.
If the ANTI SKID switch is not placed to OFF with an ANTISKID
caution displayed, normal braking capability may be lost completely.
2.8.3.5 Emergency Braking. Emergency braking is enabled when the EMERG BRK handle is pulled
to detent. This action opens the emergency brake valve and applies backup hydraulic pressure to the
hydraulic servovalves. If available, backup pressure from HYD 2B is utilized through the aft isolation
and arming valves, which are open with WonW. If HYD 2 is failed completely, backup pressure from
both the brake and APU accumulators is used. Check valves are incorporated to prevent the loss of
accumulator pressure if HYD 2B is failed. With backup pressure applied, the servovalves isolate HYD
2A pressure, if still available, so that the normal brake lines are unpressurized.
During emergency braking, backup pressure is applied through the left and right servovalves
proportional to the amount of pilot applied brake pedal force and is routed to the main wheel brakes
through the emergency brake lines. These lines bypass the anti-skid control valve, so the pilot must
regulate brake pedal force to prevent wheel skid.
Hydraulic accumulators and the brake accumulator pressure gauge are discussed in the Hydraulic
Power Supply System section.
2.8.3.5.1 EMERG BRK Handle. The EMERG BRK handle is combined with the PARK BRK handle
and is located on the lower left main instrument panel in the front cockpit. When the handle is in the
stowed, emergency position (horizontal), the EMERG label appears upright. See figure 2-18. To
select emergency brakes, the handle must be pulled to the detent while in the horizontal position.
I-2-54
ORIGINAL
A1-E18GA-NFM-000
Stowed Emergency brake valve closed. Normal braking selected.
(unmarked)
PULL Emergency brake valve open. Emergency braking selected.
(to detent)

Суб 02 Мар 2013 23:25:13
>>44308880
> НО ВЕДЬ ТАК КУКЛОСКРИПТ СКРОЕТ !
А то блять, думаешь Нариманка дурачок?

Суб 02 Мар 2013 23:27:10
>>44308955
А можно без медведя и не в профиль?

Суб 02 Мар 2013 23:27:19
>>44308955

Спасибо. Добра

Суб 02 Мар 2013 23:27:24
>>44308955
У твоей хозяйки растяжки на жопе или она мочалкой не пользуется?

Суб 02 Мар 2013 23:28:17
>>44308955
Сфоткайся на фоне голых сисек хозяйки.

Суб 02 Мар 2013 23:28:41
Парень выбирал игрушку, хотел своей подружке приятно сделать, а она с его подарком так по-блядски обошлась. Хорошо, что он этого не видит, тян бы разбила ему сердце.

Суб 02 Мар 2013 23:28:42
The position of the EMERG BRK handle is the only indication that
emergency braking is selected: no warning or caution is displayed. The
EMERG BRK handle must be fully stowed to make sure that normal
braking with anti-skid is available.
Due to friction in the EMERG BRK handle mechanism, the handle may
not return to the fully stowed position unless positively pushed.
2.8.3.6 Parking Brake System. The parking brake is used to lock the main landing gear wheels when
the aircraft is parked. The parking brake is activated when the PARK BRK handle is rotated and
pulled to the locked position. This action places the emergency brake valve in the parking brake mode.
Backup hydraulic pressure from HYD 2B or the brake and APU accumulators is applied to the wheel
brake hydraulic servovalves and routed to the main wheel brakes through the emergency brake lines.
The PARK BRAKE caution will come on to alert the pilot that the parking brake is still set when
both throttles are advanced above about 80% N2 rpm (INS on).
2.8.3.6.1 PARK BRK Handle. The PARK BRK handle is combined with the EMERG BRK handle
and is located on the lower left main instrument panel in the front cockpit. From the stowed
(horizontal) position, the handle must be rotated 90` counterclockwise and pulled to the locked
position, in order to activate the parking brake. When the handle is in the vertical position, the
PARK label appears upright. See figure 2-18. If emergency brakes are selected, the handle must be
returned to the stowed position before the parking brake can be activated. Rotating the handle 45`
counterclockwise releases the lock and allows the handle to return to the stowed (horizontal) position.
Stowed Parking brake released. Normal braking selected.
(unmarked)
TURN/ Parking brake set.
PULL
Several aircraft systems utilize parking brake activation to enable or disable logic. A set parking
brake is used to enable anti-skid BIT logic, GEN TIE logic, and INS alignment and is used to trigger
the PARK BRAKE caution.

Суб 02 Мар 2013 23:29:15
2.8.3.7 Main Wheel Anti-Spin. The anti-spin function stops main landing gear wheel rotation prior
to landing gear retraction. When the LDG GEAR handle is moved to the UP position, main landing
gear retract pressure is supplied to the anti-skid control valve. Normal brake pressure is blocked and
this anti-spin pressure is routed to the wheel brakes through the normal brake lines. Unlock and
I-2-55
ORIGINAL
A1-E18GA-NFM-000
retraction of the main landing gear is delayed until anti-spin pressure is applied and main wheel
rotation has stopped.
2.8.4 Launch Bar System. The launch bar is electrically controlled, hydraulically extended, and
mechanically retracted. With weight on the nosegear, placing the LAUNCH BAR switch to EXTEND
energizes the launch bar control valve and routes HYD 2A pressure to unlock, lower, and hold down the
launch bar. The green L BAR advisory light indicates that the launch bar has been extended.
With the launch bar extended, returning the LAUNCH BAR switch to RETRACT deenergizes the
launch bar control valve, isolates HYD 2A pressure, and allows dual retract springs to mechanically
return the launch bar to the up and locked position. A launch bar proximity switch is energized when
the launch bar is fully retracted.
When the launch bar is fully extended it is held against the deck by HYD 2A pressure. Deck load
springs allow vertical movement of the launch bar during taxi over the catapult shuttle. When the
aircraft is placed in tension on the catapult, the launch bar is held captive in the extended position by
the shuttle. Once in tension, the LAUNCH BAR switch should be placed to RETRACT in order to
remove HYD 2A pressure from the launch bar. When the LAUNCH BAR switch is placed to
RETRACT, the green L BAR light should go out.

Суб 02 Мар 2013 23:29:41
At the end of the catapult stroke, launch bar/shuttle separation occurs and allows the retract springs
to return the launch bar to the up and locked position. When engaged, the launch bar uplock prevents
the launch bar from dropping to the deck due to g-loads during landing.
If the launch bar does not return to the up and locked position after catapult launch (launch bar
proximity switch not energized), the nose landing gear cannot be retracted. In this case, placing the
LDG GEAR handle UP will raise the main landing gear and leave the nose landing gear extended.
2.8.4.1 LAUNCH BAR Switch. The LAUNCH BAR switch, located on the lower left main instrument
panel in the front cockpit, is used to control the position of the aircrafts launch bar. The switch is
spring loaded to the RETRACT position and is electrically held in the EXTEND position only if
weight is on the nose gear.
RETRACT Launch bar control valve deenergized. Launch bar up.
EXTEND Launch bar control valve energized. Launch bar unlocked and extended by HYD
2A pressure. Green L BAR advisory light on.
2.8.4.2 LB Circuit Breaker. The LB circuit breaker is located on the left-hand circuit breaker panel
above the left console. The LB circuit breaker provides a secondary means to raise the launch bar
following a launch bar malfunction. When pulled, the circuit breaker manually deenergizes the launch
bar control valve, removing HYD 2A pressure and allowing the retract springs to raise the launch bar.
I-2-56
ORIGINAL
A1-E18GA-NFM-000
Typically, this action would be required only if (1) the LAUNCH BAR switch failed in the EXTEND
position with weight on the nosegear or (2) the nose gear failed WonW after launch and the pilot failed
to place the LAUNCH BAR switch to RETRACT.

Суб 02 Мар 2013 23:30:06
2.8.4.3 L BAR Warning/Advisory Lights. Two L BAR lights, one green and one red, are located on
the left warning, caution, and advisory lights panel. Both lights are controlled by the landing gear
control unit (LGCU), based on inputs from the LAUNCH BAR switch, the launch bar proximity
switch, and various landing gear proximity switches.
The green L BAR advisory light is used to indicate that the launch bar has been extended. The
LGCU illuminates the green L BAR light when all of the following conditions are met: weight on the
nose gear, the LAUNCH BAR switch in EXTEND, the launch bar not up (launch bar proximity switch
not energized), and the red L BAR warning light not on.
The red L BAR warning light is used to indicate failure of the launch bar to retract after catapult
launch or a failure in the launch bar control system (proximity switch failure). The LGCU illuminates
the red L BAR light when one of the following sets of conditions are met:
1.
2.
3.
4.
Launch bar not up and weight off the left main gear.
Launch bar not up and left main gear not down.
LAUNCH BAR switch in EXTEND and weight off the left main gear.
LAUNCH BAR switch in EXTEND and left main gear not down.
The first set of conditions is the primary L BAR warning, e.g., the launch bar does not retract fully
after catapult launch. The other three sets of conditions provide a backup L BAR warning if one or
more of the proximity switches which control launch bar functioning fail.

Суб 02 Мар 2013 23:30:24
>>44308955
Засунь лапу в ее вагинальный проход.

Суб 02 Мар 2013 23:30:40
2.8.5 Arresting Hook System. The arresting hook is always down-loaded by a nitrogen-charged
accumulator (arresting hook snubber) contained in the arresting hook retract actuator. Arresting hook
extension is therefore accomplished by mechanically releasing the arresting hook uplatch mechanism
(HOOK handle down) and allowing snubber pressure and gravity to extend the hook. The hook should
extend in less than 2 seconds. At touchdown, the arresting hook snubber controls hook bounce and
provides a hold down force for arresting cable engagement.
Arresting hook retraction is accomplished by raising the HOOK handle. This electrically opens the
aft isolation valve and the arresting hook selector valve, routing HYD 2B pressure to the arresting hook
retract actuator. HYD 2B pressure overcomes the snubber down-load pressure and raises the hook. The
arresting hook uplatch mechanism captures and locks the hook in the up position. The hook should
retract in less than 4 seconds. If HYD 2B pressure is lost, the arresting hook cannot be retracted.
2.8.5.1 HOOK Handle. The HOOK handle, located on the lower right main instrument panel in the
front cockpit, is used to control arresting hook extension and retraction.
Up Retracts the arresting hook utilizing HYD 2B pressure.
(unmarked)
Down Unlocks the arresting hook uplatch mechanism and allows arresting hook snubber
(unmarked) pressure and gravity to extend the hook.
2.8.5.2 HOOK Light. The red HOOK light is located on the lower right main instrument panel
directly above the HOOK handle. The HOOK light comes on any time hook position does not agree
I-2-57
ORIGINAL
A1-E18GA-NFM-000
with HOOK handle position. The light comes on when the hook leaves the up and locked position and
remains on until the hook is fully extended (hook proximity switch energized). With WonW, the hook
will strike the ground before it reaches full extension, so the HOOK light will remain on.
The green HOOK light is located in the rear cockpit on the left warning, caution, and advisory panel.
This HOOK light illuminates when the hook is down.

Суб 02 Мар 2013 23:30:53
>>44309231
ролл

Суб 02 Мар 2013 23:31:07
2.9 WING FOLD SYSTEM
The aircrafts outer wing panels are designed to fold vertically to reduce the amount of deck space
occupied by the aircraft in the carrier environment. Each wing contains an independent wingfold
mechanism, which consists of two electric motors (one to lock/unlock the wings and one to spread/fold
the wings). During normal operation, the wings are spread, locked, unlocked, and folded in unison.
2.9.1 Wingfold Mechanism. Each wingfold mechanism contains a dc electric motor, which locks and
unlocks the wings, and an ac electric drive unit, which spreads and folds the wings. When the wings are
spread and locked, a locking bolt is electrically driven through the wingfold hinge, holding it in place.
When the wings are unlocked, a wing unlock flag (commonly called a beer can) protrudes from the
upper surface of the wing near the leading edge of the wingfold hinge, indicating that the locking bolt
is unstowed. The shaft of each beer can is painted red for easy identification. When the wings are
locked, the top of the beer can should be flush or near flush with the upper surface of the wing, and no
red should be showing.
Additionally, when the wings are folded, the ailerons are mechanically locked in the faired position
by a hook on the inboard aileron hinge, which engages an aileron locking pin. The aileron locking pin
is mechanically extended as the wings fold. The hook and locking pin are designed to prevent the
ailerons from blowing inboard over the TEFs when hydraulic power is not applied. If an aileron locking
pin should break, it is possible for the aileron to blow inward over the TEF. If this condition exists
during engine start, the TEF will retract into the aileron, damaging both surfaces.
If the wings are folded, note the position of the ailerons during the
preflight walk-around. If the aileron locking pins do not restrain the
ailerons in the faired position, make sure the ailerons are moved to a
faired or outboard position prior to engine start to preclude damaging the
ailerons and TEFs.
Each wingfold mechanism also contains a wing safety switch, which electrically prevents wingfold
movement. The safety switch is activated by a remove before flight pin inserted in the underside of
the wing near the wingfold hinge.
For ground crew operations, each wing can be manually unlocked, folded, or spread. The beer cans
can be manually extended by inserting a screwdriver into the wing unlock motor (underside, leading
edge). Once unlocked, the wings can be folded or spread by inserting a speed handle into the electric
drive unit (underside, trailing edge)

Суб 02 Мар 2013 23:31:15
Спасибо, ваша жалоба была отправлена.

Суб 02 Мар 2013 23:31:25
>>44309271
реролл

Суб 02 Мар 2013 23:33:35
>>44308955
Побрей себе голову.
Или сделай эрокез.

Суб 02 Мар 2013 23:35:32
Наешся какашек, курица !

2.9.3 WINGFOLD Switch. The WINGFOLD switch, located on the lower right main instrument
panel, is lever-locked in all three positions. The switch has a barrier guard to prevent inadvertent
actuation.
FOLD Unlocks the wings (WING UNLK caution displayed), fairs the ailerons, and, when
(& unlock) allowed by the FCCs, folds the wings.
HOLD Stops wing movement in an intermediate position. If spread, unlocks the wings.
(& unlock)
SPREAD Spreads and locks the wings. (WING UNLK caution removed when both wings are
(& lock) locked).
Ensure the WINGFOLD switch is lever-locked in the SPREAD position
during takeoff checks. If the wings are commanded to unlock or fold
during a catapult shot, the wings will unlock, the ailerons will fair, the
wings may fold partially, and the aircraft will settle.

Суб 02 Мар 2013 23:35:43
>>44309407
>эрокез
В голос и с подливой.

Суб 02 Мар 2013 23:36:25
Напиши на груди хозяйки ШЛЮХА МЕДВЕДЯ

Суб 02 Мар 2013 23:36:56
>>44309527
так что там насчет мануалов?

Суб 02 Мар 2013 23:38:00
>>44309596
РООЛЛ

Суб 02 Мар 2013 23:38:09
Слишком скучно, демоны тупорылые, я пошел спать !

2.9.4 Wingfold Overheat Cutout Protection. The wingfold electric drive units are designed to meet
the following duty cycle requirements: two (2) fold-spread cycles followed by a twelve (12) minute
cooldown period. If wingfold operation exceeds this duty cycle, overheat cutout protection may
shutdown wingfold operation to prevent actuator damage. Once overheat cutout protection has been
activated, normal wingfold operation is not restored until actuator temperature drops within limits;
however, the wings can still be unlocked, folded, or spread manually.
2.10 FLIGHT CONTROL SYSTEM (FCS)
The flight control system (FCS) is a fly-by-wire, full authority control augmentation system (CAS).
The FCS provides four basic functions: aircraft stability, aircraft control, departure resistance, and
structural loads management. Since the basic airframe is statically neutral to slightly unstable, a
primary function of the FCS is to maintain aircraft stability at all flight conditions. The FCS also
I-2-59
ORIGINAL
A1-E18GA-NFM-000
provides full authority control of the aircraft by implementing the basic flight control laws which
determine aircraft response to pilot inputs. Pilot inputs from the stick and rudder pedals send
electrical commands to two quad-redundant, digital flight control computers (FCC A and FCC B).
There is no mechanical linkage between the stick and rudder pedals and the flight control surfaces.
FCC software determines what commands are sent to the various flight control surfaces to exercise
pitch, roll, and yaw control of the aircraft. Additionally, the FCS provides departure resistance by
either refusing to accept or by tailoring pilot inputs that would otherwise lead to an aircraft departure.
Lastly, the FCS provides structural loads management by limiting g-available to prevent an aircraft
overstress or by retracting flight control surfaces at airspeeds that would otherwise exceed the
structural limits of the airframe. See figure 2-20 for a functional diagram of the flight control system.

Суб 02 Мар 2013 23:38:20
>>44309051
удваиваю реквест

Суб 02 Мар 2013 23:38:29
>>44309698
ЕЩЕ РОЛЛ

Суб 02 Мар 2013 23:39:03
>>44309723
ПОСЛЕДНИЙ РОЛЛ

Суб 02 Мар 2013 23:39:07
>>44309136
Сам не бампанёшь - никто внимания не обратит

Суб 02 Мар 2013 23:39:58
>>44309708
какой спать?

Суб 02 Мар 2013 23:40:00
>>44309757
ролл

Суб 02 Мар 2013 23:40:21
>>44309051
ролл

Суб 02 Мар 2013 23:40:44
>>44309833
есть дабл! Выполняй!

Суб 02 Мар 2013 23:44:36
>>44309808

Профиту-то никакого, пусть жрут говно шмары, как будто никогда не видели сисек/пизды, идиоты.



2.10.1 Flight Control Surfaces. The aircraft has 12 primary flight control surfaces including leading
edge flaps (LEFs), trailing edge flaps (TEFs), ailerons, twin rudders, horizontal stabilators, and
spoilers. LEFs, TEFs, ailerons, and stabilators can be moved both symmetrically or differentially for
pitch and roll control. Flight control surface deflection limits are shown in figure 2-19.
Pitch control is accomplished with symmetric stabilators and, in some conditions, with rudder toe-in
or rudder flare. Roll control is accomplished with combinations of ailerons, differential stabilators,
differential LEFs, and differential TEFs dependent on flight condition and CAS operating mode. The
twin rudders deflect symmetrically for directional control. There is no dedicated speedbrake surface.
Instead, a speedbrake function is provided by partial deflection of several of the primary flight
control surfaces.
Hydraulic power to all flight control surface actuators is supplied by HYD 1 and HYD 2. Stabilator
and TEF actuators are powered simultaneously by one HYD circuit from each system. All other
actuators are powered by a single primary HYD circuit, with backup hydraulic power available through
a hydro-mechanical switching valve. See the Hydraulic System section, specifically the Hydraulic Flow
Diagram, to determine which HYD circuits power each flight control surface actuator.
Surface
Deflection limits *
Aileron 25` TEU to 42` TED
Rudder 40` left or right
Stabilator 24` TEU to 20` TED
LEF 5` LEU to 34` LED
TEF 8` TEU to 40` TED
LEX Spoilers 0` or 60` TEU
* Tolerance a1`, or a3` for spoilers.
Figure 2-19. FCS Surface Deflections

Суб 02 Мар 2013 23:46:59
>>44310096
ну и я тогда пошел.

Суб 02 Мар 2013 23:47:15
>>44310096
Вайпай блять, или слабак и сдаешься.

школьник понял свое бессилие

Суб 02 Мар 2013 23:47:23
Нарисуй на хозяйке АНКХ, что бы в центре "узла" находился пупок, стилизованный под глаз, а центральная палочка пусть длится до самого клитора .

Суб 02 Мар 2013 23:47:27
Дурачё !

.10.1.1 Spoilers. The spoilers are mounted on top of the fuselage near the aft end of the LEX. The
spoilers are controlled by the FCCs and have two fixed positions: 0` (down) or 60` TEU. The 60` TEU
position is activated by the speedbrake function or when more than 15` TED stabilator is commanded
(forward stick) above 22` AOA to aid in recovery from high AOA.

Суб 02 Мар 2013 23:52:15
>>44310232

Лучше шлюху на понт возьми, скот, сиди, дурак, смотри на то что видел миллион раз, но в худшем исполнении !

2.10.2 Flight Control Computers (FCCs). Two flight control computers (FCC A and FCC B) provide
the computations which implement the aircrafts flight control laws. A four-channel architecture is
used to provide FCS redundancy. Each FCC contains two individual central processing units (CPUs),
which each run one channel of the FCS. CH 1 and CH 2 are resident in FCC A, with CH 3 and CH 4
in FCC B.
Most inputs to the FCCs (rate gyros, accelerometers, air data sensors, stick and rudder pedal
position sensors) are quad-redundant, one input for each channel. Each of the four CPUs runs
independent and parallel flight control computations. Sensor inputs as well as CPU outputs are
continuously monitored by the FCCs for agreement. When there is disagreement, the erroneous signal
is discarded, if possible.
Rate and acceleration data are provided by two independent Attitude and Heading Reference Sets
(AHRS), one for each FCC. Each AHRS has two sets of ring laser rate gyros and two sets of
accelerometers, which provide four independent sources of pitch, roll, and yaw rate information, and
four independent sources of normal and lateral acceleration. The AHRS units have the capability to
provide attitude, heading, and longitudinal acceleration data, but it is not currently utilized. The
physical rate and acceleration sensors in each AHRS channel are not aligned with the aircrafts pitch,
roll, and yaw axis. This raw sensor data is converted to the aircrafts pitch, roll, and yaw axis by
microprocessors internal to each AHRS. As a result of this architecture, a single rate gyro failure in one
channel results in all three axis rates being unusable in that same channel (CAS P, R, Y in one channel
Xd out). Similarly, if any of the accelerometers fail, all acceleration data from that AHRS channel is
unusable (N ACC and L ACC in one channel will both be Xd out).
FCC channel outputs are transmitted to the appropriate flight control actuators and to other aircraft
systems such as the MCs. While FCC computations run in all four channels, all flight control actuators
are not commanded in all four channels. The stabilators and TEF actuators do receive command
signals from all four FCC channels. However, each aileron, rudder, spoiler, and LEF actuator only
receives command signals from two FCC channels, one from FCC A and one from FCC B. The
2-channel actuators on the left side of the aircraft receive inputs from CH 1 and CH 4 while the
2-channel actuators on the right side receive inputs from CH 2 and CH 3. This channel distribution can
be seen on the FCS format.

Суб 02 Мар 2013 23:54:48
>>44310480
Лол, знатно порвало, давай давай, вайпай как пойманный на слабо школьник или сдайся и съеби в позоре, недовайпер.


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