Appendix A: Restricted Type Certificate Data Sheet – SAMPLE

National Defence
National Defence Headquarters
Ottawa, Ontario
K1A 0K2
Alternative format
- Annex A to TAA Advisory 2014-02 (PDF, 103 Kb)
Number: TAA-###
Issue No.:
Approved Date:
Issue Date:
This Data Sheet, which is part of Restricted Type Certificate (RTC) No. TAA-###, prescribes conditions and limitations under which the UAS must be operated.
Type Certificate Holder:
- Model:
- Engine(s):
- Propeller(s):
- Serial Numbers Eligible:
- Approved Configurations:
- SOI Reference – Types of Operations:
- Approved:
- Prohibited:
- Design Information:
- Applicable Design or Airworthiness Standards
- Equivalent Safety Items
- Design Operating Limitations:
- Fuel (reference the publication where this information is located)
- Oil (reference the publication where this information is located)
- Airspeed Limits (KIAS)
- Maximum Operating Speed:
- Maximum Operating Mach Number:
- Maximum Flap Extension Speed:
- Landing Gear Extended:
- Manoeuvering Speed:
- Cross Wind Landing Limit:
- Turbulent Air Penetration Speed:
- Maximum Weight:
- Ramp:
- Takeoff:
- Landing:
- Zero Fuel:
- C of G Limits:
- Datum:
- Levelling Means:
- Minimum Crew:
- Fuel Capacity:
- Tank:LH:RH:
- Cap:LH:RH:
- Usable:LH:RH:
- Arm:LH:RH:
- Max Operating Altitude:
- Outside Air Temperature Limits
- Placards
- Maintenance Requirements:
- listing of all life-limited components
- Certification Maintenance Requirements
- structural integrity/damage tolerance inspections
- Approved Publications:
- Instructions for Continuing Airworthiness
- Flight Manual and/or Operating Instructions
Note
This sample is for information purposes only.
If you wish to obtain more information or a copy of the original template, please contact DTAES 3-5, the advisory OPI.
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