Schweizer Aircraft Corporation 269c (CH60)
ICAO CH60 Light

Schweizer Aircraft Corporation 269c

Single Rotorcraft

The Schweizer 269C is a light three-seat piston helicopter that traces its lineage back to the Hughes 269 of the late 1950s. Originally designed by Hughes Helicopters as a simple, rugged trainer, the type was adopted by the U.S. Army as the TH-55 Osage for primary rotorcraft instruction during the Vietnam era. Schweizer Aircraft acquired the design in 1983 and continued production through 2010, refining the airframe with improved avionics and powerplant options while preserving the original's reputation for docile handling and low operating costs. The 269C variant introduced a more powerful Lycoming HIO-360 engine and an enlarged tail rotor, making it the most capable version of the family. With a maximum gross weight just over 2,000 pounds and a never-exceed speed of 100 knots, the 269C occupies the entry-level segment of the helicopter market. Its fully articulated three-blade main rotor and aluminum semi-monocoque fuselage deliver predictable flight characteristics that have made it a staple of civilian flight schools worldwide. The type's simplicity (no hydraulics, no complex systems) translates to straightforward maintenance and relatively affordable operating economics for a turbine-free helicopter. Endurance is modest at roughly two hours, but the 269C's forgiving nature and excellent visibility from the bubble canopy continue to make it a popular choice for ab-initio training and personal use. SkyMeter has tracked 144 flights across 55 airframes and 27 operators, with BRAMPTON FLYING CLUB the largest observed operator.

✈
ACTIVE AIRFRAMES
55
last 7 days
🏢
OPERATORS
27
unique airlines
📊
FLIGHTS
144
tracked
⏱
AVG DURATION
41m
per flight
⚠
INCIDENT RATE
4.2%
6 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
2,050 lb
MALW
—
Manufacturer model
269C
FAA designator
—
Registered
—

Recent incidents

Flagged flights of CH60

20
10/18/2026
1h 1m
△ Low approach-stability score
10/14/2026
53m
△ Low approach-stability score
10/13/2026
2h 22m
△ Low approach-stability score
10/13/2026
41m
△ Low approach-stability score
10/11/2026
26m
△ Low approach-stability score
10/11/2026
48m
△ Low approach-stability score
10/10/2026
40m
△ Low approach-stability score
10/5/2026
22m
△ Low approach-stability score
10/3/2026
53m
△ Low approach-stability score
9/30/2026
48m
△ Low approach-stability score

Recent flights

Real flights of CH60 · airborne ≥ 20 min

30
10/19/2026
1h 20m
No alerts
10/19/2026
20m
No alerts
10/19/2026
1h 41m
No alerts
10/19/2026
1h 37m
No alerts
10/19/2026
1h 33m
No alerts
10/19/2026
1h 47m
No alerts
10/19/2026
47m
No alerts
10/19/2026
33m
No alerts
10/19/2026
29m
No alerts
10/19/2026
1h 21m
No alerts
10/19/2026
1h 24m
No alerts
10/19/2026
25m
No alerts
10/19/2026
38m
No alerts
10/19/2026
38m
No alerts
10/19/2026
53m
No alerts
10/19/2026
2h 5m
No alerts
10/19/2026
1h 31m
No alerts
10/19/2026
48m
No alerts
10/19/2026
1h 19m
No alerts
10/18/2026
46m
No alerts
10/18/2026
26m
No alerts
10/18/2026
3h 36m
No alerts
10/18/2026
41m
No alerts
10/18/2026
56m
No alerts
10/18/2026
1h 11m
No alerts
10/18/2026
1h 1m
△ Low approach-stability score
10/18/2026
1h 3m
No alerts
10/18/2026
2h 3m
No alerts
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© SkyMeter · All flight data subject to ODbL attribution · Tracking window: 7 days (free tier)