Offers multiple user-uploaded, high-resolution scans of the Boeing 737-800 panel for simulation.
: Houses less frequently adjusted systems, such as the Inertial Reference System (IRS) and oxygen controls. Integration of Critical Systems
: Detailed documentation on general aircraft systems including the forward overhead.
A standard "new" 737-800 PDF guide typically highlights these critical regions: Key Controls Electrical Manages power from APU, Engines, or Battery Battery Switch, Standby Power, Generator Switches Controls fuel flow and crossfeed Fuel Pump Switches, Crossfeed Valve Hydraulics Powers flight controls and landing gear Engine & Electric Motor Pump Switches Pneumatics Manages cabin air and engine start Bleed Air, Isolation Valve, Pack Switches Prevents ice buildup on wings/engines Wing and Engine Anti-Ice Switches 🔄 What’s "New" in Recent Versions? boeing 737800 overhead panel pdf new
The 737-800 overhead panel follows a specific philosophy: Unlike older aircraft where switches were scattered, the 737 NG organizes them by system.
Manages the release of air from the cabin. It can be manually controlled if the automatic pressurization controller fails. 7. Lights (Exterior & Interior)
Located at the top, these panels control the flight control hydraulic systems and the navigation systems (IRS) that allow the aircraft to know its position, speed, and altitude. 2. Electrical Power Systems A standard "new" 737-800 PDF guide typically highlights
What (e.g., MSFS, X-Plane, Prepar3D) are you currently using?
: Located primarily on the left, this section manages the battery, external power, and engine-driven generators.
The electrical panel contains the Battery Switch , Standby Power switch, and Generator Drive Disconnects (GEN1 and GEN2). A notable feature is the TR UNIT (Transformer Rectifier) lights, which indicate DC power availability. During normal flight, the Bus Transfer and Bus Tie switches remain closed, allowing automatic load sharing. Pilots are trained to monitor the BAT DISCHARGE light during engine start. It can be manually controlled if the automatic
Whether you are mastering the Cold-and-Dark startup procedure or learning how to handle in-flight emergencies (such as an engine flame-out or electrical bus failure), the overhead panel will be your primary interface.
| Control | Normal | Function | |---------|--------|----------| | AUTO/STBY | AUTO | Dual auto controllers | | FLT ALT | Set cruise FL | e.g., FL350 → 350 | | LAND ALT | Set destination field elevation | | | CABIN RATE | 300–500 fpm typical | Climb/descent rate | | AUTO FAIL Light | OFF | Pressurization auto fail |
Located on the upper left, this section manages bleed air from the engines or APU. The L and R Engine Bleed switches, APU Bleed switch, and Isolation Valve control the high-pressure hot air used for pressurization, anti-ice, and engine start. Below these, the Pack (Air Cycle Machine) switches (L and R) control environmental conditioning. The Pressurization Panel includes the Flight Altitude Selector and Landing Altitude indicator, crucial for cabin climb management.