Stormworks: Build and Rescue

Stormworks: Build and Rescue

87 ratings
Bell-Boeing MV-22B "Osprey" Flight Manual
By Ghost and 1 collaborators
This is a detailed flight manual for Ghost's MV-22B Osprey. Information in this manual is primarily derived from the 2006 NATOPS manual, modified for my rendition in Stormworks. Included are cockpit diagrams, systems descriptions, checklists, and operational procedures.
2
2
2
4
2
   
Award
Favorite
Favorited
Unfavorite
Foreword
The MV-22B, as you see it, is a culmination of upwards of 800 man-hours of effort, and development. A large majority of that time was spent on the development of the aircraft's glass cockpit system, which is proprietary, and one of the most advanced currently on the workshop. To construct the osprey, we used the NATOPS manual (circa 2006), podcasts, as well as an ongoing interview with a real MV-22B Pilot of VMM-[REDACTED]. They provided various bits of information on MFD systems, aircraft systems, and autopilot. Because of this, I'm proud to say, our rendition of the Osprey is the most accurate ever to be built in Stormworks.

Our Osprey is equipped with 18 foldable passenger seats, as well as a rescue hoist. It has a range of well over 200km, but in case you need fuel, it's capable of HIFR and AAR.


THE OSPREY
The JVX (Joint Vertical Lift/Experimental) program began in 1981, after the disastrous Operation Eagle Claw. In 1983, Bell and Boeing partnered to work on the V-22, and flight testing began in 1989.

The Osprey is one of a kind, with wingtip nacelles housing Rolls Royce turboprop engines that deliver upwards of 6000 shaft horsepower each. Each nacelle is capable of 96° of vertical traverse, allowing for vertical landings and transitional flight. A unique interconnected drive system (ICDS) allows the aircraft to fly nominally on a single engine, and the aircraft's triple-redundant hydraulic flight control system is designed to take a beating. Having the capability to change between conventional and helicopter flight modes made the Osprey an incredibly versatile tool for the Marine Corps. First seeing combat in Afghanistan in 2009, the aircraft then went on to establish itself as a powerful logistical and tactical tool for military and humanitarian operations. Ospreys were pivotal in the relief efforts after the 2010 Haiti earthquake, as well as the extraction of Osama Bin Laden's body from Pakistan.

This specific aircraft, VMM-161's CAG with BuNo 168033, was responsible for carrying Vice President Biden aboard the John C Stennis in 2016.
Aircraft Systems
Systems described are simulated.

The Osprey is equipped with twin Rolls-Royce T406-AD-400 Turbines, one mounted in each nacelle. A unique interconnected driveshaft allows single-engine operation. Mounted at various points along this driveshaft, are two Constant-frequency generators, as well as two variable-frequency generators. These generators are responsible for AC power delivery to the aircraft, in conjunction with the battery. When the APU is active, it is clutched to the MWGB, and the Number 3 CFG. During this time, the APU is also driving the Number 3 Hydraulic Pump, providing the 5000 PSI required to operate the hydraulic start motors on the engines. The pressure from this system, if on the ground, is ported into Systems 1 and 2 to allow for full control, as part of the "ground checkout" system. This results in pressure being slightly below optimal for all 3 systems but is optimal for flight control checks before engine start. Various systems, such as the Rear Ramp/Door, as well as the rescue hoist, are also hydraulically powered. These systems will not function without the Hydraulic Isolation Valve open. By default, the aircraft opens the valve when the landing gear are lowered, however, if you wish to use these systems with the gear raised, you must open the valve in the HYD STAT layer.

The aircraft is equipped with retracting tricycle landing gear, that is powered by the No. 3 Hydraulic System. The gear has an emergency canister that is capable of lowering the gear in an emergency, such as damage. This canister will operate once, and when it does, the landing gear will be unable to be retracted. To rectify this, you can refill the canister inside the nose gear well, and the gear will resume normal operation. Moving the landing gear handle without No. 3 pressure will do nothing.

A highly advanced custom-designed MFD system is used to control various functions inside the aircraft and gives the pilot various pieces of flight-critical information. There are 19 different layers that can be individually selected and interacted with on each of the 4 MFDs. This, in combination with the CDU, allows for more than 15 thousand combinations of displays and information.

The aircraft has multiple autopilot modes and is capable of holding its GPS position based on the INS system.
Operations Checklists
This section contains the simplified operational checklists for the MV-22B.

For a full-length start, the order you should follow is:
BATTERY
ALL START
ENGINE START
PRE-TAXI
TAXI

In reality, not all of these steps are required for aircraft operation. Those that are critical are marked with an asterisk on the right side.

BATTERY
ITEM
STATUS
CRITICAL?
BATTERY
ON
*
APU
RUN/ENGAGE
*
FDP/SFD
SET
*
MFDs/CDU/EICAS
ON
*
APU INDICATOR
CHECK RUN
HYD pressures
CHECK 4800-5300 PSI
NORM FLT OPS
SELECTED
*
Avionics
ON as required
External Lights
SET
Cockpit Lighting
SET
BFWS to FLT RDY
AS REQ
PRES SYST STAT
CHECKED
C/A Summary
CHECKED
INS ALGN
NOT ACTIVE
ALL START
EXECUTE
*

ALL START
GEAR INDICATOR
LOCKED
PARK BRK
SET/FORWARDS
*
PWR STEER/NOSE LOCK
OFF/AS REQ
ROTOR BRK
CYCLE/OFF
*
AFCS or PFCS RESET
RESET
RAMP/DOOR
AS REQ
FLIGHT CONTROL CHECKS
SEE FCC LIST
ECS PFBIT
CHECKED
REFUEL PROBE
EXTEND/RETRACT
CDU
DEFAULT/CDU

ENGINE START
INTERIM PWR
CHECKED/OFF
BFWS
FLT RDY
SET MFDs
ROTOR BRAKE
OFF
*
NACELLES
90
AIRCRAFT
CLEAR
*
ECL
L or R to START
*
NG,NP,NR
STABILIZED
*
ECL
SELECTED TO FLY
*
OTHER ECL
MOVE to START
*
APU
STOP
*
RAMP/DOOR
AS REQ
MAIN DOOR
AS REQ
ECLs
FLY
*
STAT LAYERS
CHECKED

PRE-TAXI
APU
VERIFIED OFF
PWR STEER/NOSE LOCK
AS REQ
*
ECLs
Verified FLY
*
COMM/NAV/FDP
SET/AS REQ
MFDs and CDU/EICAS
SET
C/A SUMMARY
CHECKED
PARK BRAKE
OFF

TAXI
WHEEL BRAKES
OFF
BRAKES
CHECKED
NWS
CHECKED

PRE-TAKEOFF
FLAPS
AUTO
LIGHTING
SET
FUEL
CHECKED
ECLs
FLY
INTERIM POWER
AS REQ
RAMP/DOOR
CLOSED/AS REQ
CREW
BRIEFED
Overhead Panel - Diagram
Overhead Panel - Left
Label
In-Cockpit Name
Actual Name
Function
A1
CABIN LIGHTING
Cabin Lighting Button
This button, when actuated, activates the internal lighting in the main cabin.
A2
VOLTS
Battery Voltage Indicator
This dial indicates the current voltage of the Aircraft's onboard battery. If the battery goes below 2 volts, external power is required for APU start.
A3
BATTERY OFF/ON
Battery Switch
This switch connects the aircraft's battery to the BATTERY/ESS power distribution bus. This is required for start, and operation of many critical systems within the aircraft.
A4
RAMP
Ramp Extension Gauge
This gauge shows the rear aircraft's ramp position in a percentage.
A5
DOOR
Master Caution Indicator Light
This gauge shows the rear aircraft's upper door position in a percentage.
A6
RAMP CLOSE
Ramp Close Switch
Depressing this will move the ramp towards the closed position, provided the ramp has hydraulic power.
A7
DOOR CLOSE
Door Close Switch
Depressing this will move the upper door towards the closed position, provided the upper door has hydraulic power.
A8
RAMP OPEN
Ramp Open Switch
Depressing this will move the ramp towards the open position, provided the ramp has hydraulic power.
A9
DOOR OPEN
Door Open Switch
Depressing this will move the upper door towards the open position, provided the upper door has hydraulic power.
A10
BLADE FOLD/WING STOW
BFWS Button
Pushing this button will move the BFWS System towards the pre-selected BFWS Position. This button must be held for the entirety of the BFWS Sequence.
A11
FUEL DUMP OFF/ON
Fuel Dump Switch
This switch is currently inoperative. This switch is normally responsible for the dumping of fuel from the aircraft's internal tanks.
A12
PWR STEER OFF/ON
Power Steering Switch
This switch, when actuated, activates the aircraft's power steering, or nosewheel steering system. It will not function without Hydraulic power available.
Overhead Panel - Center
B1
NIGHT LIGHTING
Cockpit Night Lighting Switch
This activates the cockpit's internal night lighting.
B2
CKPT DOME
Cockpit Dome Lighting Switch
This activates the cockpit's internal dome lighting.
B3
APU FAIL/ENGAGE
APU State Indicator
This indicator will indicate red when the APU is not ready, and green when it is engaged and operational.
B4
APU STOP / RUN/ENGAGE
APU Control Switch
This switch controls the APU's operation. When the APU is in RUN/ENGAGE mode, it is clutched to the MWGB, and providing electrical and hydraulic power to critical parts of the aircraft.
B5
AFCS RESET
Automatic Flight Control System Reset
This button resets the AFCS in the event of a failure. Failures are typically caused by competing autopilot conditions.
B6
AFCS FAIL
AFCS Failure indicator
This indicates when the AFCS has encountered a fault, and needs to be reset.
B7
INTERIM PWR ACTIVE
Interim Power State Indicator
This indicator will illuminate when Interim Power has been activated. It will flash if the aircraft is currently not within Interim Power parameters.
B8
INTERIM PWR
Interim Power Button
This button, when pressed, toggles the Interim Power system, changing the aircraft's gearing to provide increased torque to the rotors. This system is designed to counteract the loss of transitional lift, when leaving APLN mode and transitioning to vertical flight.
B9
RIGHT ECL SET AFT
Right Engine Control Lever Aft
This button moves the respective simulated Engine Control Lever aft, through OFF, CRANK, START, and FLY. The ECL Cannot move past CRANK if the rotor brake is engaged.
B10
LEFT ECL SET AFT
Left Engine Control Lever Aft
This button moves the respective simulated Engine Control Lever aft, through OFF, CRANK, START, and FLY. The ECL Cannot move past CRANK if the rotor brake is engaged.
B11
RIGHT ECL SET FORE
Right Engine Control Lever Fore
This button moves the respective simulated Engine Control Lever forwards, through OFF, CRANK, START, and FLY. The ECL Cannot move past CRANK if the rotor brake is engaged.
B12
LEFT ECL SET FORE
Left Engine Control Lever Fore
This button moves the respective simulated Engine Control Lever forwards, through OFF, CRANK, START, and FLY. The ECL Cannot move past CRANK if the rotor brake is engaged.
B13
RIGHT ECL IND
Right Engine Control Lever Position
This indicator is responsible for communicating the current position of the respective simulated ECL. O is for OFF, C is for CRANK, S for START, and F for FLY.
B14
LEFT ECL IND
Left Engine Control Lever Position
This indicator is responsible for communicating the current position of the respective simulated ECL. O is for OFF, C is for CRANK, S for START, and F for FLY.
B15
FIRE SUPP ARM RIGHT ENG NORM/ARM
Right Engine Fire Suppression Arm T-Handle
This switch arms the Fire-suppression system on the respective engine, and also shuts the engine down immediately.
B16
FIRE SUPP ARM LEFT ENG NORM/ARM
Left Engine Fire Suppression Arm T-Handle
This switch arms the Fire-suppression system on the respective engine, and also shuts the engine down immediately.
B17
DISCHARGE
Fire Suppression Discharge
This button activates the armed fire suppression system.
B18
FIRE MWING
MWING Gearbox Fire Indicator
This indicator flashes when the onboard system detects a fire in the midwing gearbox.
B19
FIRE R ENG
Right Engine Fire Indicator
This indicator flashes when the onboard system detects a fire in the right engine nacelle.
B20
FIRE L ENG
Left Engine Fire Indicator
This indicator flashes when the onboard system detects a fire in the left engine nacelle.
Overhead Panel - Right
C1
FORM LIGHTS
Formation Lights Switch
This activates the aircraft's external electroluminescent formation lights.
C2
ANTI COLLISION LIGHTS
Anti-collision Lighting Switch
This switch activates the aircraft's external anti-collision strobe.
C3
POSITION LIGHTS
Position Lighting Switch
This switch activates the aircraft's external position lights.
C4
HOT MIC OFF/ON
Radio Hot Mic Control Switch
This switch changes the radio's mode from PTT to Hot Microphone. Hot Microphone triggers whenever someone talks using ingame VOIP.
C5
CH SELECT
Channel Select Up
This button increases the selected channel for the onboard radio.
C6
CH
Currently Selected Channel
This dial indicates what channel is currently selected for the onboard radio.
C7
CH SELECT
Channel Select Down
This button decreases the selected channel for the onboard radio.
C8
EMERGENCY OXY OFF/ON
Emergency Oxygen System Toggle
This button is responsible for activating the aircraft's Emergency Oxygen system. It is currently inoperative, due to a lack of an oxygen system available to vehicles.
C10
ROTOR BRAKE DISABLE
Rotor Brake Control Lever
This switch disengages the Rotor Brake. With the rotor brake active, the ECLs cannot move past CRANK.
C11
NOSE LOCK OFF/ON
Nose Lock Control Switch
This button engages the Nose Lock, and locks the Nosewheel in it's current position.
Center Console
Label
In-Cockpit Name
Actual Name
Function
1
ACK
CDU C/A Acknowledge
This button, when actuated, dismisses any active EICAS warnings from the CDU. This will not dismiss them from the C/A Page.
2
C/A
CDU Caution/Advisory Page
This button toggles the CDU to the caution/advisory page, and back again. This is used to check outstanding system warnings for faults.
3
CDU/EICAS
Central Data Unit/Engine Instrument Crew Alerting System
This multifunction Central Data Unit is used for various purposes, including waypoint entry, systems monitoring, and warnings.
4
ENTER
CDU Keypad Enter
This button is used to submit data to the CDU for processing. A current usage of this is waypoint programming.
5
CDU KEYPAD
CDU Scratchpad
This keypad is used for entering numerical values into the CDU for processing. A current usage of this is waypoint programming.
6
PILOT TCL
Pilot Thrust Control Lever
This throttle lever is the pilot's primary method of input for commanding aircraft thrust. This input is synced to the Copilot's TCL. When one moves, the other moves as well.
7
CDU
CDU Page Select
This button changes the CDU to display it's default home menu.
8
EICAS
EICAS Page Select
This button changes the CDU to display the EICAS, which shows engine statistics and hydraulic state. EICAS is designed to give engine state at a glance.
9
FLAP IND
Flap Lever Indicator
This indicates the current state of the simulated flap lever. A means the flaps are in Auto. O means the flaps are Off. H means the flaps are in Half, and F means they're at full deflection.
10
CYCLE FLP
Cycle Flap Lever
This button is used to cycle the simulated flap lever between it's 4 positions.
11
PARK BRK
Parking Brake Lever
This button is used to move the parking brake between set and disengaged. When the physical parking brake is aft, it is disengaged.
12
GEAR HANDLE
Landing Gear Handle
This switch is used to control the aircraft's tricycle landing gear assembly. When the switch is in the forward position, the gear is commanded to retract. This will not occur if there is insufficient hydraulic pressure, so observe the GEAR LOCK IND on retraction and extension.
13
STAT
CDU STAT Layer
This button switches the CDU to display the STAT menus, as found in the MFDs. Interactions can be completed through the CDU, if desired.
14
GEAR EMERG DOWN
Landing Gear Emergency Deployment
This button activates the Emergency deployment sequence of the landing gear, and uses a pressurized canister to force the landing gear into the down position. This should be reserved for emergency situations. In the event it has been triggered, to reset the landing gear, you can EMERG LG CANISTER REFILL in the nose gear well.
15
GEAR LOCK IND
Landing Gear State Indicator
This light is the "3 green" in the aircraft. It indicates when all 3 landing gear are in the down and locked position.
16
LEFT NAC CTRL DIS
Left Nacelle Control Disable
This switch disables nacelle control for the Copilot, and triggers a critical conversion fault in the CDU.
17
RIGHT NAC CTRL DIS
Left Nacelle Control Disable
This switch disables nacelle control for the Pilot, and triggers a critical conversion fault in the CDU.
Flight Director Panel (FDP)
Label
In-Cockpit Name
Actual Name
Function
1
MASTER ALERT SWITCH
Master Alert Switch
This button, when actuated, clears outstanding faults, and dismisses the Master Caution warning.
2
PFCS RESET
Primary Flight Control Reset Switch
This button, when actuated, clears outstanding faults within the AFCS, and dismisses the PFCS FAIL warning.
3
CPLD
CPLD Button
This button is used to toggle the aircraft's autopilot to it's CPLD state. The aircraft must be CPLD to have normal operation of HDG HOLD, SPD HOLD, and ALT HOLD.

CPLD can be treated like a "master" for the autopilot system.
4
REM HVR
Remote Hover Control Switch
This switch controls the REM HVR system. If HVR CPLD is active, this can be enabled, and allows for the aircraft's position in a hover to be controlled by the crew chief, in his station in the cabin.
5
HDG
Heading Hold Target
This dial shows the current target for the heading hold system. This can be adjusted by selecting the HDG hold, and using the TGT INC/TGT DECR arrows.
6
Speed
Speed Hold Target
This dial shows the current target for the speed hold system. This can be adjusted by selecting the SPD hold, and using the TGT INC/TGT DECR arrows. This speed can be adjusted from 50-250 knots.
7
ALT
Altitude Hold Target
This dial shows the current target for the altitude hold system. This can be adjusted by selecting the ALT hold, and using the TGT INC/TGT DECR arrows.
8
TGT INC
Target Increase
Depressing this will increase the target value for the selected autopilot system. CPLD must be active for this to function.
9
HVR CPLD
Hover Coupled Switch
This button activates the aircraft's HVR CPLD, which consists of an autohover, and altitude hold system. To turn the system on, tap the button once. To turn off the system, hold the button. A short press while the system is on will change the system between POSN HOLD and normal mode. Passing 90 knots while HVR CPLD is engaged will kick off the system.
10
CPLD
CPLD Button
This button is used to toggle the aircraft's autopilot to it's CPLD state. The aircraft must be CPLD to have normal operation of HDG HOLD, SPD HOLD, and ALT HOLD.

CPLD can be treated like a "master" for the autopilot system.
11
MASTER ALERT SWITCH
Master Alert Switch
This button, when actuated, clears outstanding faults, and dismisses the Master Caution warning.
12
PFCS RESET
Primary Flight Control Reset Switch
This button, when actuated, clears outstanding faults within the AFCS, and dismisses the PFCS FAIL warning.
13
MASTER ALERT
Master Alert Indicator
This indicator will flash when their has been a detected failure in one of the connected flight-critical systems.
14
PFCS FAIL
PFCS Fail Indicator
This indicator will flash when their has been a detected failure in the Primary Flight Control System.
15
CPLD ACT
CPLD Indicator
This indicator shows the current status of the aircraft's autopilot system. When the indicator is illuminated, the system is coupled, and active. The system can be coupled without any autopilot modes active.
16
PILOT CONTROL
Pilot Control switch
This switch controls the switching of flight controls between the two pilots. This is a fictional feature, and is only implemented to allow more crew cohesion, and preventing confusion in control inputs. When this switch is off, the Right pilot has control, and when it is enabled, the Left pilot has control.
17
HOLD ON (SELECTED)
Autopilot Hold On
This button has two functions. Double tapping this button will sync the currently selected system to the aircraft's current state (Sync heading to current aircraft heading, speed to current speed).

Holding this button activates the selected autopilot mode.
18
STATUS
Autopilot Hold On
This indicator is used to determine which autopilot systems are selected and active. When a system is selected, the orange bar is closest to the respective dial.
19
CYCLE SEL
Cycle Selected Autopilot
This button is used to cycle selection between the three different autopilot modes.
20
TGT DECR
Target Decrease
Depressing this will decrease the target value for the selected autopilot system. CPLD must be active for this to function.
21
HVR CPLD ACT
HVR CPLD Indicator
This indicator is used to show the current status of the HVR CPLD system. This indicator will illuminate solid if the aircraft is in NORM autohover mode. When this light is flashing, the aircraft is either over 50 knots, or POSN hold is active.
22
CPLD ACT
CPLD Indicator
This indicator shows the current status of the aircraft's autopilot system. When the indicator is illuminated, the system is coupled, and active. The system can be coupled without any autopilot modes active.
23
MASTER ALERT
Master Alert Indicator
This indicator will flash when their has been a detected failure in one of the connected flight-critical systems.
24
PFCS FAIL
PFCS Fail Indicator
This indicator will flash when their has been a detected failure in the Primary Flight Control System.
Multi-Function Displays
I designed a highly advanced custom MFD system, that allows the aircraft to display more than 20 seperate pages, or "layers" if you will, on each of the 4 displays.

MFD Operation
To operate the MFDs, follow this short checklist.
TASK
FUNCTION
MFD PWR
This switch activates the power to the respective Multifunction Display. Will not power on without an internal power source (Battery, APU, generators) active.
STBY Splash
While the MFD system is initializing, it will display a flashing "STBY" along with various self-test symbology. This will display for 10 seconds.
NORM FLT
Selection of this option begins the Inertial Navigation System alignment, and sets the MFDs to their defaults. This option can only be selected from one of the right two MFDs.
The 5 buttons at the top of the display are always active, and pressing them will send you to the respective layer. From left to right, those layers are:

PFD, NAV, FLIR, STAT, SYST
MFD Layers
This section has a short description of every MFD layer's function, and an image of what they look like, to identify them.
TASK
FUNCTION
PREVIEW
INIT
This layer shows on the right two MFDs on aircraft startup. Selecting "NORM FLT" initializes the INS and sets the MFDs to their startup defaults.
PFD
This layer shows an artificial horizon, a velocity vector, and a pitch ladder, as well as other flight-critical information. G2I2 represents that the aircraft is aligned within the G2 tolerance, and is on INS no. 2. Selecting "VID" with the FLIR camera powered up will give the PFD a video backdrop.
NAV
This layer shows a top-down view of the aircraft, with a map projected behind it, to provide pilots with a critical navigation tool. The map behind can only be projected if MMAP is enabled in the AVPR layer. Selecting ALGN will bring you to the ALGN layer.
ALGN
This layer shows which guidance system is currently in use. Selecting NAV CDU will change the CDU to display the waypoint entry layer.
FLIR
This layer is used to control the AN/AAQ-27A Forward-looking Infared Camera mounted on the nose. When the camera is not powered up in AVPR, the layer will display "OFF". When the camera is in it's warm-up sequence, it will display "NOT TIMED OUT". Various functions are available using the side keys on the MFD. Toggling FPV will send you to the FPV mode, where it can act as a PFD. Toggling ST activates the camera's heading-based stabilizer. IR toggles infrared view on the camera. FV changes field of view, and Z+ and Z- handle respective zoom within that field of view. Toggling PT activates Point Track.
FUEL STAT
This layer shows the current fuel totalized values, as well as values from individual tanks in various parts of the aircraft. The upper two tanks represent the wing tanks, the center readout is from the Wing Root, and the lower tanks are the sponsons. Selecting AAR will take you to the PRBE layer, where you have control over the Aerial Refueling Probe.
PRBE
This layer is used to control the AAR Probe's extension. Selecting EXT extends the probe. HOLD holds the probe's position, and RET retracts it.
FCS STAT
This layer shows the current status of the aircraft's hydraulic systems and flight controls. Provided at the bottom are the pressure values for all 3 hydraulic systems. By selecting ISOL, you can control the aircraft's isolation valve. The isolation valve is always open with the LDG deployed, however, when they are raised, it can be toggled on/off.
ENG STAT
This layer shows the current statistics for various parts of the powerplant. NR is for Rotor RPM, TRQ is torque, and MGT is gas generator temperature. This layer also shows the current fuel usage in PPM.
ELE STAT
This layer shows the current statistics for various parts of the electrical system onboard the aircraft. A component will be depicted as filled in green when operating to normal parameters.
ICE STAT
This layer shows the current statistics for the IPS, or Ice Protection System. You can monitor the current exterior temperature, icing, and switch the anti-ice between AUTO and OFF.
SYST
This layer acts as a menu for further system controls in the Osprey.
AVPR
This layer is used to control electrical power flow to various subsystems. The avionics are mostly powered automatically, however the Moving Map (MMAP) and FLIR camera have to be toggled in this MFD. Selecting ALL ON toggles all avionics to on.
PRSY
In the real Osprey, this layer functions as a diagnostic system for all pressure-operated systems onboard. In this rendition, it displays current values for the hydraulic system, and operation of the crew door locking system.
Credits
So many people have helped along the course of this incredible journey, and I just want to give them all the credit they deserve.

Littlerol - he is responsible for a majority of the interior and exterior detailing, as well as helping with much of the project's early research. He's also responsible for accidentally building several nuclear submarines during the course of it.

GERUNIMO - for his constant support in the creation of this project. He also provided what would eventually become the aircraft's PFD, it's most critical instrument.

Woodspeople and WALL-E - for their incredible help (and labor) put into the GPS-calculation system for the V-22's FLIR.

Sheepdog - for his awesome support over the course of the project, and his help with the cockpit diagrams in the manual.

Sir_Murtak - For his occasional testing of the aircraft, and advice on the implementation of various features.

There are probably a dozen more people who helped me with this project, and If I named all of them, I'd run out of space. Massive thanks to the community, and I hope you enjoy it!


Fair Skies, and Good Hunting!
37 Comments
Prosilver 28 Feb @ 7:14am 
what do i do if the lighting strikes the aircraft?
H3I70R 17 Feb @ 3:42pm 
bro why ts so hard
Canine 31 Jan @ 10:53am 
yeah this is a piece of shit
HEWERSUNNY 4 May, 2024 @ 12:04pm 
super cool replica i love it pls make more realistic replicas like this mabe a f/a 18 superhornet next ? btw how do you fold the rotor blades
Ghost  [author] 25 Jan, 2024 @ 8:28pm 
yea! check the actual workshop page, and it's one of the videos.
PrestiBoi 25 Jan, 2024 @ 11:54am 
Isn't there a video for a quick start like where tf is the HYD buttons and shit?
LucasJ 13 Jan, 2024 @ 3:23pm 
If you don't like it there's plenty of other creations. This dude did an amazing job replicating the realistic nature of the Osprey and took the complexity of Stormwork's builder to it's limits. No need to be a hater and spread negativity.
🅰🆂🆃🆁🅾 3 Aug, 2023 @ 4:52pm 
@ghost. you shouldnt need a manual and youtube video to start some engines bro, definition of over complexity, your talented but for anybody who just wants to play with it is not going to take the time to figure it out
LeBathtubFishe 5 Mar, 2023 @ 10:38pm 
@ghost I still can't start the dang thing
gerudah 18 Feb, 2023 @ 12:06am 
incomprehensible, thumbs up