Hughes 269 (H269)
ICAO H269 Light

Hughes 269

Single Rotorcraft

The Hughes 269 is a lightweight two-seat piston helicopter that became one of the most successful training helicopters in aviation history. First flown in 1956, it was designed by Howard Hughes' aircraft division as a simple, rugged trainer with docile handling characteristics that made it ideal for ab-initio rotorcraft instruction. The U.S. Army adopted it as the TH-55 Osage in 1964, training thousands of Vietnam-era pilots on the type, and civilian flight schools worldwide embraced it for its low operating costs and forgiving flight envelope. The 269 features a three-blade main rotor, a piston Lycoming HIO-360 engine producing 190 horsepower, and an aluminum semi-monocoque fuselage with excellent visibility from its bubble canopy. Its never-exceed speed of 86 knots and service ceiling around 10,200 feet made it modest in performance but perfectly suited to the training mission, where predictability mattered more than speed. After Hughes left the helicopter business, production continued under Schweizer Aircraft as the 300 series from 1983 onward, with the 300C and 300CBi variants adding fuel injection and minor refinements while preserving the original's straightforward design philosophy. The type remains in service today at flight schools, for pipeline patrol, and in private hands, valued for its mechanical simplicity and relatively low maintenance burden compared to turbine trainers. SkyMeter has tracked 121 flights across 42 airframes and 28 operators, with NORTH TEXAS HELICOPTERS INC the largest observed operator.

✈
ACTIVE AIRFRAMES
42
last 7 days
🏢
OPERATORS
28
unique airlines
📊
FLIGHTS
121
tracked
⏱
AVG DURATION
1h 39m
per flight
⚠
INCIDENT RATE
1.7%
2 flagged
ⓘ

Safety in context

The incident rate counts flights with ANY safety event detected by SkyMeter: go-arounds (a routine response, not a failure), unstable-approach gate flags (advisory thresholds), rejected takeoffs (the system working as designed), and runway events. It is NOT an accident rate or fatality rate. For accident statistics, refer to the NTSB Aviation Accident Database (USA) or the Aviation Safety Network. See methodology for what each event type measures.

Performance

Speed envelope & approach

Vref
—
Vref range
—
Vmo
—
Mmo
—
Approach category
—

Dimensions

Airframe geometry

Wingspan
—
Length
—
Tail height
—
Wheelbase
—
Gear width
—
Wake category
L

Weight & identification

Operating limits

MTOW
1,850 lb
MALW
—
Manufacturer model
269
FAA designator
—
Registered
—

Recent incidents

Flagged flights of H269

20
10/10/2026
59m
△ Low approach-stability score
10/3/2026
43m
△ Low approach-stability score
10/2/2026
34m
△ Low approach-stability score
9/19/2026
37m
△ Low approach-stability score
9/8/2026
21m
△ Low approach-stability score
8/31/2026
22m
△ Low approach-stability score
8/29/2026
52m
△ Low approach-stability score
8/28/2026
43m
△ Low approach-stability score
8/26/2026
45m
△ Low approach-stability score
8/24/2026
43m
△ Low approach-stability score

Recent flights

Real flights of H269 · airborne ≥ 20 min

30
10/11/2026
40m
No alerts
10/11/2026
1h 32m
No alerts
10/11/2026
4h 4m
No alerts
10/11/2026
47m
No alerts
10/11/2026
42m
No alerts
10/11/2026
39m
No alerts
10/11/2026
42m
No alerts
10/10/2026
35m
No alerts
10/10/2026
2h 37m
No alerts
10/10/2026
1h 3m
No alerts
10/10/2026
3h 6m
No alerts
10/10/2026
29m
No alerts
10/10/2026
1h 29m
No alerts
10/10/2026
1h 12m
No alerts
10/10/2026
59m
△ Low approach-stability score
10/10/2026
31m
No alerts
10/10/2026
51m
No alerts
10/10/2026
1h 22m
No alerts
10/10/2026
6h 37m
No alerts
10/10/2026
36m
No alerts
10/10/2026
36m
No alerts
10/9/2026
30m
No alerts
10/9/2026
5h 3m
No alerts
10/9/2026
43m
No alerts
10/9/2026
5h 23m
No alerts
10/9/2026
3h 32m
No alerts
10/9/2026
32m
No alerts
10/9/2026
7h 50m
No alerts
10/9/2026
3h 20m
No alerts
10/9/2026
49m
No alerts
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© SkyMeter · All flight data subject to ODbL attribution · Tracking window: 7 days (free tier)