H12-041 · DAILY
URBAN AIR MOBILITY · QUIET ELECTRIC VTOL
Cleared for a quieter sky.
Hangar 12 flies electric vertical-takeoff aircraft between city vertiports. Four seats, one pilot, sixty-two decibels — booked like a car, boarded in minutes, flown over the traffic instead of through it.
STATIC DRAWING — RANGE 120 KM · CRUISE 240 KM/H · NOISE 62 dB(A) · PAX 4
[ 01 · FLIGHT ARTICLE H12-A4 ]SHT 02 / 06
One airframe. No single point of failure.
The H12-A4 is a lift-and-cruise design: a fixed wing does the flying, four independent electric rotors do the taking off. Fewer moving parts than a helicopter, and every one of them has a backup.
TYPE DATA SHEET
- RANGE, FULL RESERVE
- 120 KM
- CRUISE SPEED
- 240 KM/H
- FLYOVER NOISE, 100 M
- 62 dB(A)
- SEATS
- 4 + 1 CREW
- ROTORS
- 4 × Ø 1.44 M
- MOTORS
- 4 × 140 KW
- MTOW
- 2,200 KG
- BATTERY
- 8 ISOLATED PACKS
- TURNAROUND
- 12 MIN CHARGE
Certification basis EASA SC-VTOL, Category Enhanced. Data sheet values are demonstrated, not projected — flyover noise measured per ISO 3744 at 100 m AGL.
[ 02 · ROUTE NETWORK ]SHT 03 / 06
Twelve minutes, not fifty-eight.
Five vertiports across the metro, city-pair service on a published timetable. Your seat holds to the minute — the road below does not.
H12-107 · DAILY
H12-118 · WEEKDAYS
H12-054 · DAILY
| DEP | FLIGHT | ROUTE | PAD | STATUS |
|---|---|---|---|---|
| 07:10 | H12-041 | MID ⟶ HRB | P2 | BOARDING |
| 07:16 | H12-107 | MID ⟶ EXP | P1 | ON TIME |
| 07:22 | H12-063 | MID ⟶ RVR | P3 | ON TIME |
| 07:31 | H12-118 | MID ⟶ SFD | P1 | SCHEDULED |
| 07:38 | H12-054 | MID ⟶ HRB | P2 | SCHEDULED |
| 07:45 | H12-129 | MID ⟶ EXP | P3 | SCHEDULED |
[ 03 · PERFORMANCE ]SHT 04 / 06
Quiet is a specification.
Noise measured per ISO 3744. A conventional light helicopter at the same point: 78–82 dB(A). The difference is why we are allowed downtown.
[ 04 · SAFETY & CERTIFICATION ]SHT 05 / 06
Boring by design.
Everything interesting about the H12-A4 happens on the drawing board, so nothing interesting happens in the air.
Distributed propulsion
Four independent motor–rotor channels on isolated power buses. The craft holds a stable hover with any single channel out — the certification basis assumes it, and the flight-test campaign has demonstrated it.
Triple-redundant flight control
Three dissimilar flight computers vote on every command, two hundred times a second. A disagreement grounds the disagreeing unit — not the aircraft.
Battery architecture
Eight isolated packs with cell-level fusing and vented containment. Reserve energy for a go-around plus a diversion is a hard floor — never touched in scheduled service.
Whole-aircraft recovery
A ballistic parachute covers the low-altitude envelope that autorotation never could. Below 120 m, the airframe itself is the last redundancy.
CERTIFICATION LEDGER
- SC-VTOL CERTIFICATION BASISAGREED · 2024
- STRUCTURAL TEST ARTICLECOMPLETE · 2025
- FLIGHT-TEST CAMPAIGN1,400 H LOGGED · IN PROGRESS
- TYPE CERTIFICATETARGET · 2027
- PART 135 OPERATIONS SPECTARGET · 2027
[ 05 · BOOK A SEAT ]SHT 06 / 06
Every seat is a window seat.
Four seats in the cabin, none of them middle. Pick one — the departure minute is the contract.
CABIN PLAN · NOSE ▲
AVAILABLE SELECTED
- Departure at 07:10:00 — boarding closes at T−2 minutes.
- Arrive ten minutes before wheels-up. Not two hours.
- Cancel free until T−60. 15 kg cabin allowance included.