AEROWAY TECHNICAL REFERENCE
STD: 29.92 inHg
AEROWAY.ORGREF-01
Aeronautical Reference Architecture
15 SPECIALIZED ENGINES // 4 HUBS + E6B SUITEPublished: Directory Updated:

Aeronautical Calculation Engines

Deterministic, client-side aviation computation tools adhering to ICAO Doc 7488, FAA-H-8083, and 14 CFR Part 91 standards. Pure math, zero trackers, zero server dependencies.

MASTER FLIGHT COMPUTER

E6B Flight Computer Suite

An all-in-one digital slide rule unifying wind, time/distance, fuel consumption, altitude, airspeed, and unit conversions without duplicating mathematical engines.

Launch E6B Suite →
HUB-A

Atmosphere & Airspeed

5 Calculators
Primary Workflow Flow: Pressure Altitude → Density Altitude → Performance Context | TAS → Mach
HUB-B

Wind & Navigation

3 Calculators
Primary Workflow Flow: Runway + Wind → Headwind/Crosswind | Course + TAS + Wind → WCA + Heading + Groundspeed
HUB-C

Flight Planning & Performance

4 Calculators
Primary Workflow Flow: Distance + Groundspeed → ETE → Fuel Burn | Altitude Loss + GS → TOD / FPM | ROC + GS ↔ Climb Gradient
HUB-D

Aircraft Loading & CG

2 Calculators
Primary Workflow Flow: Fuel Volume ↔ Fuel Mass → Loading Stations / Moments → Total CG Location