### I **LIST OF ATTACHMENTS**

The following attachments are referenced in the request for exemption which follows. These documents provide additional evidence in support of Petitioner ’s request to amend granted 333 Exemption to the FAA. Attachment A PHANT OM 3 Operations Users Manual Attachment B INSPIRE Operations Users Manual Attachment C S 900 Operations Users Manual

**I I**  **DESCRIPTION OF PROPOSED ADDITIONAL**  **SUAS’** The PHANTOM 3 , INSPIRE and S
- 9 00 SUAS’ Manual describes, in detail, the policies and p rocedures for Petitioners request to amend granted 333 to add these SUAS to it . To assist the FAA in its safety assessment of Petitioners proposed additional SUAS ’ , below is a summary of operational limitations and conditions which the additional UAS are all of within similar and existing flight charateristics envelope which will ensure an equivalent or higher level of safety to operations conducted under current regulatory guidelines: 1. The SUAS’ will weigh less than 25 lbs. depending on sensor requirements
. 2. Flights will be operated within line
- of
- sight of the trained PIC and PO. 3. Flights will be terminated at 25% power reserve. 4. Flights will be operated at an altitude of no more than 2 00 feet AGL. 5. Minimum crew for each operation will consist of the SUAS P ICand V O. 6. The SUAS PI C will be FAA licensed commercial , private or sport utility pilot.

### Below is an overview of the Petitioners PHANTOM 3 specifications. Additional operational

information is available in the PHANTOM 3 Operations User Manual (Attachment A). 

## Phantom 3

**Battery** 6000 mAh LiPo 2S
**Phantom 3 Ad**  **vanced Weigh t**  1280g (with battery & propellers)

**Hover A ccuracy**  **(Ready to Fly)** Vertical: +/- 0.1 m (when Vision

Positioning is active) or +/- 0.5 m Horizontal:1.5m
**Ma x A** **scent / Descent Speed**  Ascent: 5m/s

Descent: 3m/s
**Ma x Flight Speed**  16m /s((ATTI mode, no wind)
**Dia gonal Length**  590mm **Controllable Range of Gimbal**  Pitch - 90°to +30°

### Below is an overview of the Petitioners IN SPIRE specifications. Additional operational

information is available in the INSPIRE Operations Users Manual (Attachment B ). 

## Inspire 1

**Weight** 2935g (Battery Included) **Takeoff Weight** 3400g **Hovering A ccuracy**  **(GPS mode)** Vertical : 0.5m ; Horizontal : 2.5m **Ma x A**  **ngular Velocity** Pitch : 300°/s ; Ya w : 150°/s **Ma x Tilt A**  **ngle** 35° **Ma x A** **scent/Descent Speed** 5/4 m/s **Ma x Speed**  22m /s ( ATTI mode , no wind ) **Ma x Flight A**  **ltitude** 4500m **Ma x Wind Speed Resistance**  10m /s **Operating Temperature Range** - 10°~40°C **Ma x Flight Time**  Approximately 18 minutes **Indoor Hovering** Enabled by default

### Below is an overview of the Petitioner s S - 9 00 SUAS specifications. Additional

operational information is in the S - 9 00 Operations User s Manual (Attachment C ). **Spreading Wings S900**

**Features** Lightweight, Strong , Easy to Carry , Sp arkproof Plug , Low Gimbal Mounting, Retractable Landing Gear, Folding Propeller **Product Specifications** Diagonal W heelbase : 900mm Frame Arm Length : 358mm Frame Arm W eight (with Motor, ESC, Propeller ) : 316g **Motor** Stator Size : 41x14mm , KV : 400rpm/V **ESC** Current : 40A OPTO , Voltage : 6S LiPo

Signal Frequency : 30Hz~450Hz Drive PW M Frequency : 8KHz , We ight(with Radiators) : 35g **Foldable Propeller (1552/1552R)**  Material : High strength performance engineered plastics Size : 15x5.2 inch , We ight : 13g **Flight Parameters** Takeoff W eight : 4.7Kg ~ 8.2Kg , Total W eight: 3.3Kg Power BatteryLiPo , (6S 、 10 000mAh~15000mAh 、 (Min)15C) Ma x Power Consumption : 3000W Hovering Power Consumption:1000W Hover Time : 18min (@12000mAh & Takeoff W eight 6.8Kg)