Airbus · helicopter
Airbus H160 accident history and safety score
Airbus H160 is indexed from the Track Plane Crash fleet catalog. It has zero candidate incident rows in our current NTSB/ASN/BAAA ingestion corpus — a positive signal, not proof of zero global accidents.
Diagnostic Safety & Security Metrics
Occupant Survivability Rate
Percentage of cabin occupants surviving indexed crash incidents.
55%
Class average: 60%
Weather Resilience
Tolerance to crosswinds, turbulence, and structural icing thresholds.
6.5/10
Class average: 5.8/10
Mechanical Integrity
Structural robustness, system MTBF, and power plant reliability indicators.
8/10
Class average: 8/10
Operational Control Demand
Pilot experience and workload sensitivity (higher indicates more demanding flight handling).
8.5/10
Class average: 7.2/10
Flight System Redundancy
Multi-engine safety margins, backup avionics, and flight envelope protection.
7.5/10
Class average: 4/10
Performance Profile
Five-axis safety ratings · hover vertices for metric explanation
Metric ratings
Average survival rate of occupants in recorded serious airframe occurrences. Higher percentage indicates better energy absorption and crashworthiness.
Actuarial Insurance Underwriting Calculator
Adjust annual utilization and operating parameters below to calculate the custom hull liability policy score for a **Airbus H160** (helicopter class) starting from its fixed baseline safety score of **76**.
Calculated Policy Score
81
Regular coverage parameters. Baseline rates apply with standard pilot warranties.
• Day Visual Flight Rules operations maximize survivability margins.
How We Calculate
These diagnostic indicators are compiled by Track Plane Crash analysts using historical incident data, manufacturer specifications, NTSB/FAA investigation materials, and fleet class coefficients.
They serve as qualitative safety benchmarks for aircraft classes and families, and do not represent insurance actuarial loss ratings for individual tail numbers.
Fleet Specs & Flight Profiles
Cabin & Seating Configuration Matrix
VIP / Corporate transport layout (Max pax: 8)
Executive Cabins
Capacity: 8 seats
Seat Pitch
45 in
Seat Width
22 in
Cabin Onboard Amenities
High-Speed Wi-Fi
Satellite broadband equipped
Audio / Video Screen
None
Seat Power Outlets
Individual AC
USB charging slots
Integrated smart ports
Flightradar24 Telemetry & Cruising Profiles
260 km/h / 140 knots
12,000 ft (3,650 m)
1,500 ft/min (7.6 m/s)
800 km (430 nmi)
2x Turboshaft engines (Turbomeca / Pratt & Whitney)
Rigid four-bladed main rotor system
Mode-C transponder
0233 (Executive Private)
Risk themes
GEO rule: aircraft pages must separate model involvement from accident cause. A crash involving a model is not automatically a model defect.
Source links
Past accident rows
Incidents currently linked to Airbus H160
No source-backed incident rows linked yet.
Recent crashes
Recent plane crashes involving Airbus H160
2013-03-06
Airbus DCA13WA062 NTSB dataset event at Chicago, IL, USA
Chicago, IL, USA · Pending verification
0
Fatalities
2004-04-17
Airbus occurrence at Cairo International Airport (CAI)
Cairo International Airport (CAI) · Qatar Airways
0
Fatalities
2000-07-31
Airbus occurrence at Hong Kong-Chek Lap Kok International Airport (HKG)
Hong Kong-Chek Lap Kok International Airport (HKG) · Cathay Pacific Airways
0
Fatalities