MiG-29 Fulcrum (Deimos Inc.) Checklists
| Walkaround Cockpit Panels | |
|---|---|
| Speeds Payloads Lights | |
| Engine Start Pre Taxi Taxi Pre Takeoff Takeoff > WIP - values needed | |
| Penetration Pattern Turn to Final Final Go Around | |
| Park Shutdown | |
CAUTIONUNCHECK Elevator Trim Axis: Reverse Axis before flight in this a/c. | |
Walkaround | Back to the top |
| Fuselage Nose | Nose Landing Gear | Right Forward Fuselage | Right Main Landing Gear | Right Wing | Fuselage (Right Aft Side) | Empennages | Left Aft Fuselage | Left Wing | Left Main Landing Gear | Left Forward Fuselage | |
| Custom control assignments | |
| Toggle Afterburner 1 | Unassign |
| Reverse Thrust | YES | also deploys brake chute when revs are up |
| Brake Chute | see above |
COCKPIT PANELS | Back to the top |
| Electrical Power Panel | |
 | |
| BAT-GND SUPPLY LH RH | Batteries |
| DC GEN, AC GEN | Generators |
| PTO | AC/DC convertor |
| ENG SYS | Power to various engine components |
| FUEL PUMP, ANTI SURGE | |
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PAYLOADS | Back to the top |
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| DeimoS Mig29 Weapon's Patch | |
| Paste the folder "deimosinc_fulcrum_armed" in to the community folder | https://flightsim.to/file/60830/deimos-mig29-weapon-s-patch |
| Only on liveries beginning with 0 | |
LIGHTS | Back to the top |
| Default lights on with engine started | NAV, BCN, STRB |
SPEEDS | Back to the top |
| Flap limiting | 250 kt |
| Gear limiting | 250 kt |
SCRAMBLE | Back to the top |
| Master Arm / Avionics | ON |
| HUD | Day / Night (VCP) |
| Altimeter | RESET |
| Note runway altitude | |
| Course | Set to RWY HDG |
| HDG | Set to 90 deg left of RWY HDG |
| Fuel State | |
| MFD 2 - Shows Centre | MFD 5 shows none | |
| MFD 1: COM, NAV, ADF, ATC | ON |
| IFF | 7000 |
| Lights | Check that NAV, BEACON, STROBE, FORM on |
| Landing Light | ON |
| De-Ice | As required |
| Flaps | Stage one | 20 deg |
| Speedbrake | Check retracted |
| Trim | For takeoff |
CAUTIONParking Brake OFF, tap toe brakes and check Hydraulic Brake Pressure Indicator is live. | |
| MFD 4 | > Moving Map > Zoom > Centred > Auto-Refresh ON |
| Parking Brake | OFF |
| Toe Brakes | HOLD |
| Throttle | Afterburner |
| Toe Brakes | Release |
| Rotate | 120 kts? |
| Once Positive rate of climb established | |
WARNINGGear & Flaps up < 250 kts | |
| Trim | Adjust |
| Throttle | Adjust |
| Climb rate = xx,000 feet per minute | |
| Landing lights | OFF |
Engine Start | Back to the top |
| ENGINE CONTROL UNIT | The ECU optimizes the fuel flow for thrust demand, which is controlled by the throttle, by consideration of environmental and engine-specific parameters. |
| ENGINE STARTING SYSTEM | Ground starting of both engines is achieved by the APU via an ENG GBX for each engine. Electrical start-up power is supplied by an external power uni1 or by two internal batteries. |
| Engine Start Lamp | ЗАПУСК |
| As soon as 35 % RPM is reached, ignition will be switched off. | |
| When engine speed reaches 50 % RPM the APU and the starting system automatically shut-down under control of the engine fault detection unit. | |
| Now the engine winds up to IDLE by itself. | |
| The engine starting system allows two ground start modes and four relight modes: | automatic relight | semi-automatic relight | manual relight | preventive relight. | |
| Ground start: | Manual start in any order |
| Automatic start | |
| Relight: | Automatic relight |
| Semi-automatic relight | |
| Manual relight | |
| Preventive relight | |
| AUTOMATIC START OF BOTH ENGINES | |
| Start-up mode switch | Set to START BOTH engines |
| APU switch | Guarded position START NORM |
| Throttles 1 and 2 | Idle |
| GND START button | Press |
| The APU will drive the RH engine first. When APU shut-off speed is reached, the APU will be shut-off and restart for LH engine start after a break of 1.O sec. | |
| MANUAL START | |
| LEFT ENGINE first | |
| Throttle 1 | Idle position |
| APU switch | Guarded position START NORM |
| Start-up mode switch | LH |
| GND START button | Press |
| Depressing the GND ST ART button activates the APU system, engine ignition system, and the friction clutch control unit. | |
CAUTIONBefore the start sequence of the RH engine is initiated by pressing the GND START button, the LH engine has to run in IDLE for at least 40 sec. | |
| RIGHT ENGINE second | |
| Throttle 2 | Idle position |
| Start-up mode switch | RH |
| GND START button | Press |
| Engine metrics | |
| Oil Temp Limit (Luftwaffe) | 195 c |
| Oil Press (Observed) | 4.5 |
| Idle RPM (Observed) | 14,640 |
| Bus (Observed) | 28 V |
Pre Taxi | Back to the top |
| For foreign object damage (FOO) prevention, the air intakes are closed after landing and generally on the ground. With the intake ramps closed, engine air is taken in through a series of louvers in the upper surface of the wing root. | |
Taxi | Back to the top |
Pre Takeoff | Back to the top |
Takeoff | Back to the top |
| Gear limiting speed | 250 kts |
| Flaps limiting speed | (250 kts) |
Penetration | Back to the top |
Pattern | Back to the top |
| Alt | 600 ft |
| Spd | 250 kts |
| Gear down | 250 kts |
| Flaps down full | (250 kts) |
Turn to final | Back to the top |
Final | Back to the top |
| Check gear and flaps down | |
| Speed Brake | As necessary |
| Approach (observed) | 110 kts |
| Use AOA indicator in HUD | |
| Put FPI on landing zone | |
| Touchdown (observed) | 95 kts |
| Brake Chute | HOLD Launch Bar Retract (Reverse Thrust) |
Go Around | Back to the top |
| Throttle | BURNER |
| Speed Brake | Check RETRACTED |
| Gear | UP |
| Flaps | UP before 250 kts |
Park | Back to the top |
Shutdown | Back to the top |
| Canopy open | On ground |
| Engines stopped | |
| Battery off | |
| END CHECKLIST | |