# TCDS R00033LA: Airobotics Inc. - Type: Type certificate data sheet - Status: Current - Holder: Airobotics Inc. - Revision: 0 - Revised: September 5, 2023 - Product: Aircraft, Unmanned Aircraft System - Certification basis: Part 21 - Data sheet PDF: https://openairdocs.org/files/sha256/b0/65/b0655a6d8ba49dbba66c14137148280513355f5baf090747197ad62515c32d1f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174550037420230906222851.0001 - Page: https://openairdocs.org/tcds/R00033LA ## Models (1) As the data sheet lists them. - OPTIMUS 1-EX ## What the data sheet says Some pages are OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. R00033LA This data sheet, which is part of Type Certificate No. R00033LA, prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Title 14, Code of Federal Regulations (14 CFR). Type Certificate Holder Airobotics Inc. 411 Waverley Oaks Rd Suite 114 Waltham, MA 02452 Page No. 1 2 3 4 5 6 7 8 Rev. No. 0 0 0 0 0 0 0 0 R00033LA Rev. 0 Airobotics Inc. OPTIMUS 1-EX September 5, 2023 R00033LA Page 2 of 8 I. Model OPTIMUS 1-EX (Special Class) Approved September 5, 2023 Low Risk UA This is a low risk Unmanned Aircraft (UA) comprised of the aircraft, the removable battery, and the removable sensors/payloads. UA Configuration Rotorcraft Unmanned Aircraft Dimensions Dimensions (without propellers): 29.9 in. x 29.9 in. x 15.2 in. (with propellers): 49.6 in. x 49.6 in. x 15.2 in. Battery 8S 23.2 Amp Hour (Ah) LiPo type battery The max voltage is 33.6 Volts, Nominal voltage 29.6 Volts (VDC) and the capacity is 23.2 Ah or 686.72 Watt hours Battery ambient operating temperature = 39.6-97.2degF” (4.2° – 36.2 °C) Motor Manufacturer: T-Motor Part Number (P/N): AU05529-CW/AU05530-CCW Type: Permanent magnet brushless DC Number of Motors: 4 Motor Limits Max Thrust: 11.9 lbs. /axis is at 24V (4 total 47.6 lbs.) Propeller Manufacturer: T-Motor Propeller P/N: 001310-CW/001311-CCW Number of Blades: 2 per propeller Diameter: 28 in. Type: Fixed Pitch (9.2 degrees pitch) Propeller limits Approved Optimal operational 1500 – 3700 rpm Groundspeed Limits Vno Maximum cruise groundspeed: 27.2 knots Center of Gravity (C.G.) Range X (forwards/aft) +1.18 in. to -1.18 in. (+ 3.0 cm to – 3.0 cm) Y (port/starboard) + 0.39 in. to - 0.39 in. (+ 1.0 cm to – 1.0 cm) R00033LA Page 3 of 8 Empty Weight C.G. Range N/A The UA is authorized to fly with the approved Payloads only. The above-stated C.G. Range covers all payload configurations. Flights without a payload are not authorized. Figure 1: C.G Range Datum of the OPTIMUS 1-EX UA at Winch Ball Center Figure 2: UA Dimensions-1 R00033LA Page 4 of 8 Measurements - Motor to Motor Measurements - Prop Tip to Prop Tip 29.9 in (760 mm) 49.6 in (1260 mm) 70.2 in (1783 mm) Figure 3: UA Dimensions-2 1020 PR Figure 4: UA Axes Origin R00033LA Page 5 of 8 Leveling Means Place the aircraft (with landing legs installed) on a flat level surface. Maximum Weights Max gross takeoff weight: 23.1 lbs. ± 0.4 lbs. (10.5 ± 0.2 kg.) Empty Weight Empty weight (with battery, no Pl): 18.9 lbs. ± 0.4 lbs. (8.6 ± 0.2 Kg.) (Pl – Payload) Payload Capacity Up to 3.3 lbs. (1.5 kg.) Command and Control Information Cellular connectivity to Airobotics Cloud for automated operations. Flight Termination System (FTS) using Lora transmitter and Manual Control of the UA using Futaba RC with Lora transmitter. Command and Control Frequencies 4G/LTE cellular bands: B2 (FDD 1900), B4 (FDD 1700/AWS) B12 (FDD 700ac), B13 (FDD 700c), B14 (FDD 700PS), B66 (FDD1700/AWS-3), B71 (FDD 600) LoRa Transmitter on 902 to 928 MHz Minimum Crew One UA Pilot Max. Operating Altitude 1404 ft (429 m) ASL Min. Operating Altitude 107 ft. AGL (does not include takeoff and landing phases of flight) Flight Endurance In accordance with Unmanned Aircraft Flight Manual (UFM) for specific environment (US-OPT2-O-003 Rev. IR dated August 29, 2023). Flight Limitations This UA must be operated in accordance with an FAA approved UFM (US-OPT2-O-003 Rev. IR dated 29-August-2023) Serial Numbers Approved UA 354 to UA 358 Reliability Category RC-B Certification Basis 14 CFR 21.17(b). The certification basis is documented in Federal Register Notice 2022-06380. Date of Application for Type Certificate September 25, 2019 TC Issue Date September 5, 2023 Production Basis Production Certificate NONE. Note: because the FAA has not issued a Production Certificate, before original airworthiness certification of each aircraft (UAS) an FAA representative must perform a detailed inspection for workmanship, materials, conformity with the approved technical data, and check of the flight characteristics. In the event of an application for a standard airworthiness certificate or, if an applicant intends to produce a new aircraft under 14CFR 21.183(d), and the applicant is manufacturing, building of assembling to another person’s type certificate, the applicant must provide written evidence of permission from the type certificate holder. Conduct for such activity without written evidence of permission may be a violation of 49 U.S.C. 44704(a)(3). R00033LA Page 6 of 8 Environmental Environmental compliance in accordance with the published Rule of Particular Applicability, “Final Rule for Airobotics Model Optimus 1- EX (July 3, 2023)” [July 3, 2023], which can be found through the Noise page in the FAA’s Office of Environment and Energy webpage, or using the following URL: https://www.faa.gov/about/office_org/headquarters_offices/apl/aee/nois e/uas_noise_certification Type Design The UA Type Design consists of the aircraft, payloads (sensors), and battery. See Optimus 1-EX UAS MDL and Type design Data, OPT2.TC-M-167, Rev. 06 dated 02-August-2023. Associated Elements (AE) The AE identified in document, Airobotics AE Interface Document OPT2.TC-P-459, Rev. IR dated 04-May-2023, was used during type certification. All AE, including those identified in the AE interface document, require FAA approval for operations and must not invalidate the type certification. FAA Flight Standards may coordinate any AE changes proposed by an operator with the appropriate AIR Certification Branch in order to determine any potential effects to the TC or UFM. R00033LA Page 7 of 8 NOTES: NOTE 1 A current weight and balance report, including a list of equipment included in the certificated empty weight and loading instructions, when necessary, must be provided for each aircraft at the time of original certification. NOTE 2 All placards required by either the FAA-approved Unmanned Aircraft Flight Manual, the applicable operating rules, or the Certification Basis must be installed as specified. NOTE 3 This aircraft shall be maintained in accordance with the Airobotics Optimus 1-EX UA maintenance manual, or other methods approved or accepted by the FAA (UMM OPT2-M-004 Rev IR, dated 01-August- 2023). NOTE 4 UA shall be operated under 14 CFR part 91 or 107, operating requirements, as mitigated. Operations shall be conducted in accordance with authorizations, exemptions or waivers of flight regulations applicable to the operation, including but not limited to 14 CFR § 91.113, issued by the Administrator and specific to the intended operation, including geographical and environmental limitations. NOTE 5 This UA is considered a ‘Low-Risk UA’ based on its design and Concept of Operations (CONOPS); the type certificate was issued accordingly using durability and reliability testing. NOTE 6 Any change to the operating limitations must be evaluated by the FAA Aircraft Certification Service’s Certification Branch for this TC to determine whether it is a major change per § 21.93. NOTE 7 This UA has not been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation. NOTE 8 The FAA Flight Standards will grant operating approvals based on the CONOPS and the reliability category achieved by demonstrations conducted during the UA’s type certification testing. NOTE 9 All Associated Elements must be evaluated and receive an FAA operational approval. NOTE 10 Operations of this aircraft over human beings are prohibited unless such operations are approved by the FAA. (i.e. 14 CFR 107.140) NOTE 11 The Approval of the Type Design is applicable to these aircraft serial numbers only. The Type Design as defined in the MDL (OPT2.TC-M-167 Rev. 06, dated 02-August-2023), to include drawing revision levels, may not be used for any further certification or manufacturing purposes. R00033LA Page 8 of 8 NOTE 12 These unmanned aircraft must be Part 89 Compliant at issuance of an Airworthiness Certificate. END ``` ## ADs None name its models. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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