DronePiesLLCStephenLouallen652NSpoutSpringStNixa,Missouri65714stephenlouallen@ymail.comDecember6,2015U.S.DepartmentofTransportationDocketManagementSystem1200NewJerseyAve.,SEWashington,DC20590Re:ExemptionRequestSection333oftheFAAReformActandPart11oftheFederalAviationRegulationsfrom14C.F.R.45.23(b);14CFRPart21;14CFR61.113(a)&(b);91.7(a);91.9(b)(2);91.103(b);91.109;91.119;91.121;91.151(a);91.203(a)&(b);91.405(a);91.407(a)(1);91.409(a)(2);91.417(a)&(b).DearSirorMadam:PursuanttoSection333oftheFAAModernizationandReformActof2012(theReformAct)and14C.F.R.Part11,DronePiesLLC,developerandoperatorofSmallUnmannedAircraftSystems("sUASs")equippedtoconductaerialelectronicdatacollectioncandaerialphotographyforthecommercialvideoindustry,herebyappliesforanexemptionfromthelistedFederalAviationRegulations("FARs")toallowcommercialoperationofitssUASs,solongassuchoperationsareconductedwithinandundertheconditionsoutlinedhereinorasmaybeestablishedbytheFAAasrequiredbySection333.Asdescribedmorefullybelow,therequestedexemptionwouldpermittheoperationofsmall,unmannedandrelativelyinexpensivesUASundercontrolledconditionsinairspacethatis1)limited2)predetermined3)controlledastoaccessand4)wouldprovidesafetyenhancementstothealreadysafeoperationsintheaerialfilmingandmonitoringindustrypresentlyusingconventionalaircraft.ApprovalofthisexemptionwouldtherebyenhancesafetyandfulfilltheSecretaryofTransportation's(theFAAAdministrator's)responsibilitiesto"...establishrequirementsforthesafeoperationofsuchaircraftsystemsinthenationalairspacesystem."Section333(c)oftheReformAct.cAerialDataCollection"whichincludesanyremotesensingandmeasuringbyaninstrument(s)aboardtheUA.Examplesincludeimagery(photography,video,infrared,etc.),electronicmeasurement(precisionsurveying,RFanalysis,etc.),chemicalmeasurement(particulatemeasurement,etc.),oranyothergatheringofdatabyinstrumentsaboardtheUA1The name and address

of the applicant

is: Drone Pies LLC Stephen Louallen Ph: 417-693-0562 Email: stephenlouallen@ymail.com Address: 652
N Spout Spring St, Nixa, Missouri, 65714 Regulations from which the exemption

is requested: 14 CFR Part 21 14 C.F

. R 45.23(b) 14 CFR 61.113 (a) & (b) 14 C.F.R. 91.7 (a) 14 CFR 91.9 (b) (2) 14 C.F

. R. 91.103 14 C.F.R. 91.109 14 C.F. R. 91.119 14 C.F.R. 91.121 14 CFR 91.151 (a) 14 CFR 91.203 (a) & (b) 14 CFR 91.405 (a) 14 CFR 407 (a) (1) 14 CFR 409 (a) (2) 14 CFR 417 (a) & (b) This exemption application

is expressly submitted

to fulfill Congress' goal
in passing Section 333(a) through
(c) of the Reform Act. This law directs the Secretary

of Transportation

to consider whether certain unmanned aircraft systems may operate safely

in the national airspace system (NAS) before completion

of the rulemaking required under Section 332 of the Reform Act. In making this determination,

the Secretary

is required

to determine which types of sUASs do not create

a hazard

to users of the NAS or the public or pose

a threat
to national security

in light of the following: • The sUAS's size, weight, speed, and operational capability; • Operation

of the sUAS

in close proximity

to airports and populated areas • Operation

of the sUAS within visual line of sight of the operator. Reform Act§ 333 (a). Lastly,

if the Secretary determines that such vehicles "may operate safely

in the national airspace system, the Secretary shall establish requirements

for the safe operation

of such aircraft

in the national airspace system."

ld. §333(c) (emphasis added)

A A Applicant interprets this provision

to place the duty on the Administrator

to not only process applications

for exemptions under section 333, but for the Administrator

to craft conditions
for the safe operation

of the sUAS,

if it should
be determined that the conditions
set forth herein do not fulfill the statutory requirements

for approval.

2TheFederalAviationActexpresslygrantstheFAAtheauthoritytoissueexemptions.Thisstatutoryauthoritybyitstermsincludesexemptingcivilaircraft,asthetermisdefinedunder§40101oftheAct,thatincludessUASs,fromtherequirementthatallcivilaircraftmusthaveacurrentairworthinesscertificate.TheAdministratormaygrantanexemptionfromarequirementofaregulationprescribedundersubsection(a)or(b)ofthissectionoranysections44702-44716ofthistitleiftheAdministratorfindstheexemptioninthepublicinterest.49U.S.C.§44701(f)Seealso49USC§44711(a);49USC§44704;14CFR§91.203(a)(1).DronePiesLLC'ssUASsarerotorcraft,weighting55orfewerlbs.includingpayload.Theyoperate,undernormalconditionsataspeedofnomorethan50knotsandhavethecapabilitytohover,andmoveintheverticalandhorizontalplanesimultaneously.TheywilloperateonlyinlineofsightandwilloperateonlywithinthesterileareadescribedintheFlightSafetyManual,attachedasExhibitB(hereinafter"theManual").SuchoperationswillinsurethatthesUASwill"notcreateahazardtousersofthenationalairspacesystemorthepublic."8GiventhesmallsizeofthesUASsinvolvedandtherestrictedsterileenvironmentwithinwhichtheywilloperate,theapplicantfallssquarelywithinthatzoneofsafety(anequivalentlevelofsafety)inwhichCongressenvisionedthattheFAAmust,byexemption,allowcommercialoperationsofUASstocommenceimmediately.AlsoduetothesizeofthesUASsandtherestrictedareasinwhichtherelevantsUASswilloperate,approvaloftheapplicationpresentsnonationalsecurityissue.GiventhecleardirectioninSection333oftheReformAct,theauthoritycontainedintheFederalAviationAct,asamended;thestrongequivalentlevelofsafetysurroundingtheproposedoperations,andthesignificantpublicbenefit,includingenhancedsafety,reductioninenvironmentalimpacts,includingreducedemissionsassociatedwithallowingsUASsforcommercialvideooperations,thegrantoftherequestedexemptionsisinthepublicinterest.Accordingly,theapplicantrespectfullyrequeststhattheFAAgranttherequestedexemptionwithoutdelay.AIRCRAFTANDEQUIVALENTLEVELOFSAFETYTheapplicantproposesthattheexemptionrequestedhereinapplytocivilaircraftthathavethecharacteristicsandthatoperatewiththelimitationslistedherein.Theselimitationsprovideforatleastanequivalentorevenhigherlevelofsafetytooperationsunderthecurrentregulatorystructurebecausetheproposedoperationsrepresentasafetyenhancementtothealreadysafecommercialvideofilmingoperationsconductedwithconventionalaircraft.8ReformActSection333(b).3TheselimitationsandconditionstowhichDronePiesLLCagreestobeboundwhenconductingcommercialoperationsunderanFAAissuedexemptioninclude:1.ThesUASwillweighlessthan55lbs.2.Flightswillbeoperatedwithinlineofsightofapilotand/orobseiVer.3.Maximumtotalflighttimeforeachoperationalflightwillbe20minutes.Flightswillbeterminatedat25%batterypowerreseiVeshouldthatoccurpriortothe20minutelimit.4.Flightswillbeoperatedatanaltitudeofnomorethan400feetAGLor,notmorethan200feetaboveanelevatedplatformfromwhichfilmingisplanned.5.MinimumcrewforeachoperationwillconsistofthesUASPilot,theVisualObseiVer,andtheCameraOperator.6.sUASpilotwillbeanFAAlicensedairmanwithatleastasportorrecreationalcertificateandavaliddriver'slicense.Theobse!Verwillalsoholdavaliddriver'slicense.7.sUASPilotwillbePilotinCommand(PIC).IfapilotcertificateholderotherthanthesUASPilot,whopossessthenecessaryPICqualifications,isalsopresentonset(i.e.theAerialCoordinator),thatpersoncanalsobedesignatedasPIC.8.ThesUASwillonlyoperatewithinaconfined"SterileArea"asdefinedintheManual.SectionCoftheManualrequirestheestablishmentofa"SecurityPerimeter"fortheflightoperationsarea.9.AbriefingwillbeconductedinregardtotheplannedsUASoperationspriortoeachday'sproductionactivities.Itwillbemandatorythatallpersonnelwhowillbeperformingdutieswithintheboundariesofthesafetyperimeterbepresentforthisbriefing.10.TheoperatorwillfileaFAAForm7711-1,oritsequivalent,asmodifiedinlightoftherequestedexemption,withtheappropriateFlightStandardsDistrictOffice.11.Theoperatorwillobtaintheconsentofallpersonsinvolvedinthefilmingandensurethatonlyconsentingpersonswillbeallowedwithin100feetoftheflightoperation,andthisradiusmaybereducedto30feetbaseduponanequivalentlevelofsafetydetermination,asrequiredbySectionFoftheManual.WiththeadvancedpermissionoftherelevantFSDO,operationsatcloserrangecanbeapproved.(SeeSectionBintheManualAppendixB)12.TheoperatorwillsubmitawrittenPlanofActivitiestothelocalFSDOwithjurisdictionovertheareaofproposedfilming.Thethree-daynotificationmaybewaivedwiththeconcurrenceoftheFSDO.13.PilotandobseiVerwillhavebeentrainedinoperationofsUASgenerallyandreceivedupto-dateinformation'ontheparticularsUAStobeoperatedasrequired.14.ObseiVerandpilotwillatalltimesbeabletocommunicatebyvoice.15.Writtenand/ororalpermissionfromtherelevantpropertyholderswillbeobtained.16.Allrequiredpermissionsandpermitswillbeobtainedfromterritorial,state,countyorcityjurisdictions,includinglocallawenforcement,fire,orotherappropriategovernmentalagencies.17.IfthesUASlosescommunicationsorlosesitsGPSsignal,thesUASwillhavecapabilitytoreturntoapre-determinedlocationwithintheSecurityPerimeterandland.18.ThesUASwillhavethecapabilitytoabortaflightincaseofunpredictedobstaclesoremergencies.14C.F.R.Part21,SubpartH:AirworthinessCertificates14C.F.R.§91.203{a){1)4

### Subpart

H, entitled Airworthiness Certificates, establishes

the procedural requirements

for the issuance

of airworthiness certificates

as required

by FAR §91.203
(a) (1 ). Given the size and limited operating area associated with the aircraft
to be utilized
by the Applicant,

an exemption from Part 21 Subpart

H meets the requirements

of an equivalent level of safety under Part 11 and Section 333 of the Reform Act. The Federal Aviation Act (49 U.S.C.§44701



### (f)) and Section 333 of the Reform Act both authorize the FAA to exempt aircraft from the requirement for an airworthiness certificate, upon consideration

of the size, weight, speed, operational capability, and proximity

to airports and populated areas of the particular sUAS.

In all cases,
an analysis

of these criteria demonstrates
that the sUAS operated without
an airworthiness certificate,

in the restricted environment
and under the conditions proposed
will 

### be at least as safe, or safer, than

a conventional aircraft (fixed wing or rotorcraft) operating with an airworthiness certificate without the restrictions
and conditions proposed. The sUAS
to be operated hereunder

is less than 55 lbs. fully loaded, carries neither

a pilot nor passenger, carries
no explosive materials

or flammable liquid fuels, and operates exclusively within

a secured area as set out in the Manual. Unlike other civil aircraft, operations under this exemption
will be tightly controlled and monitored

by both the operator, pursuant

to the Manual's requirements,

and under the requirements
and in compliance with local public safety requirements,

to provide security for the area of operation

as is now done with conventional filming. The FAA will have advance notice
of all operations. These safety enhancements, which already apply
to civil aircraft operated

in connection with motion picture and television production, provide

a greater degree

of safety
to the public and property owners than conventional operations conducted with airworthiness certificates issued under 14 C.F.R. Part 21, Subpart

H. Lastly, application

of these same criteria demonstrates
that there

is no credible threat
to national security posed by the sUAS, due to its size, speed
of operation, location

of operation, lack of explosive materials

or flammable liquid fuels, and inability

to carry

a substantial external load. 

### 14 C.F.R.



### § 45.23 (b). Marking

of the Aircraft The regulation requires: When marks include only the Roman capital letter "N" and the registration number

is displayed

on limited, restricted

or light-sport category aircraft
or experimental

or provisionally certificated aircraft, the operator must also display on that aircraft near each entrance

to the cabin, cockpit,

or pilot station,

in letters not less than

2 inches nor more than

6 inches high, the words "limited," "restricted," "light-sport," "experimental,"

or "provisional,"

as applicable. Even though the sUAS will have no airworthiness certificate,

an exemption may be needed
as the sUAS will have no entrance

to the cabin, cockpit
or pilot station
on which the word "Experimental"

can be placed. Given the size of the sUAV, two-inch lettering will be

5

### impossible. The word "Experimental"

will be placed on the fuselage

in compliance with §45.29 

### (f). The equivalent level of safety will be provided

by having the sUAV marked
on its fuselage

as required

by §45.29



### (f) where the pilot, observer and others working with the sUAV will see the identification

of the sUAS as "Experimental."

The FAA has issued the following exemptions

to this regulation

to Exemptions Nos.

1 0700, 8738,

1 0167 and

1 0167 A. 14 C.F.R.

§ 61.113 (a) & (b): Private Pilot Privileges and Umitations: Pilot in Command. 

### Sections 61.113 (a) & (b) limit private pilots to non-commercial operations. Because the sUAS will not carry

a pilot or passengers,

the proposed operations
can achieve the equivalent level of safety
of current operations

by requiring the PIC operating
the aircraft

to have

a private pilot's license rather than

a commercial pilot's license
to operate this small sUAS. Unlike

a conventional aircraft that carries the pilot and passengers,

the sUAS

is remotely controlled with no living thing on board. The area of operation

is controlled and restricted, and all flights are planned and coordinated

in advance

as set forth
in the Manual. The level of safety provided

by the requirements included

in the Manual exceeds that provided

by a single individual holding

a commercial pilot's certificate operating

a conventional aircraft. The risks associated with the operation

of the sUAS are so diminished from the level of risk associated with commercial operations contemplated

by Part 61 when drafted, that allowing operations

of the sUAS as requested with

a private pilot as the PIC exceeds the present level of safety achieved

by 14 C.F.R. §61.113
(a) 

### & (b). 14 C.F.R. §91.7(a): Civil aircraft airworthiness. 

### The regulation requires that no person may operate

a civil aircraft unless

it is in airworthy condition.

As there will be no airworthiness certificate issued for the aircraft, should this exemption

be granted,

no F 

### M regulatory standard will exist for determining airworthiness. Given the size of the aircraft and the requirements contained

in the Manual for maintenance and use of safety check lists prior to each flight, as set forth

in Sections C & D, an equivalent level of safety will be provided. 14 C.F.R.

§ 91.9 (b) 

### (2): Civil Aircraft Flight Manual

in the Aircraft. 

### Section 91.9 (b) (2) provides: No person may operate

a U.S.-registered

civil aircraft

... (2) For which an Airplane

or Rotorcraft Flight Manual

is not required
by §21.5 of this chapter, unless there

is available

in the aircraft

a current approved airplane

or Rotorcraft Flight Manual, approved manual material, markings, and placards,

or any combination thereof.



### 6

### The sUAS, given its size and configuration

has no ability or place to carry such

a flight manual on the aircraft, not only because there

is no pilot on board, but because there

is no room or capacity

to carry such

an item on the aircraft. The equivalent level of safety will be maintained

by keeping the flight manual

at the ground control point where the pilot flying the sUAS will have immediate access

to it. The FAA has issued the following exemptions

to this regulation: Exemption Nos. 8607, 8737, 8738, 9299, 9299A,9565,9565B,
10167, 10167A, 10602,32827,and 10700. 14 C.F.R.

§ 91.103: Preflight action This regulation requires each pilot in command

to take certain actions before flight to insure the safety
of flight. As FAA approved rotorcraft flight manuals will not be provided
for the aircraft
an exemption
will be needed.
An equivalent level of safety will be provided

as set forth in the Manual. The PIC will take all actions including reviewing weather, flight battery requirements, landing and takeoff distances and aircraft performance data before initiation

of flight. 14 C.F.R. §91.109: Flight instruction: Section 91.103 provides that no person may operate

a civil aircraft (except

a manned free balloon) that
is being used for flight instruction unless that aircraft has fully functioning dual controls. sUASs and remotely piloted aircraft,
by their design do not have fully functional dual controls. Flight control

is accomplished through the use of a control box that communicates

with the aircraft via radio communications.

The FAA has approved exemptions

for flight training without fully functional dual controls for a number

of aircraft and for flight instruction

in experimental aircraft. See Exemption Nos.5778K



### & 9862A. The equivalent level of safety provided

by the fact that neither

a pilot nor passengers

will be carried

in the aircraft and by the size and speed of the aircraft. Safe simulation and practice flight will be carried out in controlled environments.

All simulations

will be carried out on a computer using the drone controls. Any practice flying will take place

in a safe environment,
with no risk to human life below. 14 C.F.R. §91.119: Minimum safe altitudes Section 91.119 establishes safe altitudes
for operation

of civil aircraft. Section 91.119 (d) allows helicopters

to be operated

at less than the minimums prescribed, provided the person operating
the helicopter complies with any route or altitudes prescribed

for helicopters

by the FAA. As this exemption

is for a sUAS that
is a helicopter and the exemption requests authority to operate

at altitudes

up to 400 AGL, or not more than 200 above an elevated platform from which filming

is planned,

an exemption may be needed

to allow such operations.

As set forth herein the sUAS will never operate

at higher than 400 AGL.

It will however

be operated

in a


### 7

### restricted area with security perimeter, where buildings and people will not be exposed

to operations without their pre-obtained consent. The equivalent level of safety will 

### be achieved given the size, weight, speed
of the sUAS as well as the location where

it is operated.
No flight will be taken without the permission

of the property owner
or local officials. Because

of the advance notice
to the property owner and participants

in the filming activity,

all affected individuals
will be aware
of the planned flight operations

as set forth
in the Manual. Compared

to flight operations with aircraft
or rotorcraft weighting
far more than the maximum 551bs. proposed herein

and the lack of flammable fuel, any risk associated with these operations

is far less than those presently presented with conventional aircraft operating

at or below 500 AGL
in the movie industry.

In addition, thelowaltitude operations

of the sUAS will ensure separation between these smaii-UAS operations and the operations

of conventional aircraft that must comply with Section 91.119. 

### 14 C.F.R. §91.121 Altimeter Settings This regulation requires each person operating

an aircraft

to maintain cruising altitude
by reference

to an altimeter that
is set

" ... to the elevation

of the departure airport
or an appropriate altimeter setting available before departure."

As the sUAS may not have

a barometric altimeter, but instead

a GPS altitude read out, an exemption may be needed.
An equivalent level of safety will be achieved

by the operator, pursuant

to the Manual and Safety Checklist, confirming
the altitude

of the launch site shown on
the GPS altitude indicator before flight. 

### 14 C.F.R.

§ 91.151(a): Fuel Requirements

for Right
in VFR Conditions Section 91.151 (a) prohibits
an individual from beginning

"a flight

in an airplane under VFR conditions unless (considering wind and forecast weather conditions) there

is enough fuel to fly to the first point of intended landing, and, assuming normal cruising speed

- (1) During the day, to fly after that for at least 30 minutes;

or (2) At night,
to fly after that for at least 45 minutes." The battery powering the sUAS provides approximately

25 minutes

of powered flight. To meet the 30 minute reserve requirement

in 14 CFR §91.151, sUAS flights would be limited
to approximately

20 minutes

in length. Given the limitations

on the sUAS's proposed flight area and the location

of its proposed operations within

a predetermined area,

a longer time frame for flight

in daylight

or night VFR conditions

is reasonable. Applicant believes that an exemption from 14 CFR §91.151
(a) falls within the scope
of prior exemptions.
See Exemption 10673 (allowing Lockheed Martin Corporation

to operate without compliance with FAR 91.151 (a)). Operating
the small sUAS,

in a tightly controlled area where only people and property owners
or official representatives

who have signed waivers will be allowed, with less than 30 minutes

of reserve fuel, does not engender
the type of risks that Section 91.151(a) was intended

to alleviate given the size and speed
of the small sUAS. Additionally, limiting sUAS flights
to 20 minutes would greatly reduce the utility for which the exemption
will be granted.



### 8

### Applicant believes that an equivalent level of safety can be achieved

by limiting flights
to 20 minutes

or 25% of battery power whichever happens first. This restriction would be more than adequate

to return the sUAS
to its planned landing zone from anywhere

in its limited operating area. Similar exemptions have been granted

to other operations, induding Exemptions 2689F, 57 45,

1 0673, and

1 0808. 14 C.F.R. §91.203


### (a) and (b): Carrying Civil Aircraft Certification
and Registration The regulation provides

in pertinent part: (a) Except
as provided in§ 91.715, no person may operate

a civil aircraft unless



### it has within

it the following: (1) An appropriate
and current airworthiness certificate .... (b) No person may operate

a civil aircraft unless the airworthiness certificate required

by paragraph

(a) of this section
or a special flight authorization issued under §91. 715
is displayed

at the cabin or cockpit entrance

so that

it is legible to passengers

or crew. The sUAS fully loaded weighs
no more than 55 lbs and is operated without
an onboard pilot. As such, there

is no ability or place to carry certification
and registration documents

or to display them on the sUAS. An equivalent level of safety will be achieved

by keeping these documents

at the ground control point where the pilot flying the sUAS will have immediate access

to them,
to the extent they are applicable

to the sUAS. The FAA has issued numerous exemptions

to this regulation. A representative sample

of other exceptions includes Exemption Nos. 9565, 9665, 9789, 9789A, 9797, 9797A, 9816A, and 10700. 14 C.F.R. §91.405 

### (a); 407 (a) (1); 409 (a) 

### (2); 417(a)



### & (b): Maintenance Inspections These regulations require that an aircraft operator

or owner "shall have that aircraft inspected as prescribed

in subpart

E of this part and shall between required inspections, except
as provided

in paragraph

(c) of this section, have discrepancies repaired

as prescribed

in part 43 of this chapter

... ," and others shall inspect
or maintain the aircraft

in compliance with Part 43. Given that these section and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply to the applicant. Maintenance

will be accomplished

by the operator pursuant

to the flight manual and operating handbook

as referenced

in the Manuai.(See Sections

B, D and G) An equivalent level of safety will be achieved because these small sUASs are very limited

in size and will carry

a small payload and operate only
in restricted areas for limited periods

of time.

If mechanical issues arise the sUAS can land



### 9immediatelyandwillbeoperatingfromnohigherthan400feetAGL.AsprovidedintheManual,theoperatorwillensurethatthesUASisinworkingorderpriortoinitiatingflight,performrequiredmaintenance,andkeepalogofanymaintenanceperformed.Moreover,theoperatoristhepersonmostfamiliarwiththeaircraftandbestsuitedtomaintaintheaircraftinanairworthyconditiontoprovidetheequivalentlevelofsafety.Pursuantto14C.F.R.Part11,thefollowingsummaryisprovidedforpublicationintheFederalRegister,shoulditbedeterminedthatpublicationisneeded:Applicantseeksanexemptionfromthefollowingrules:14C.F.R.§21,subpartH;14C.F.R45.23(b);14C.F.R.§§61.113(a)&(b);91.7(a);91.9(b)(2);91.103(b);91.109;91.119; 91.121;91.151(a);91.203(a)and(b);91.405(a);91.407(a)(1);91.409(a)(2);91.409(a)(2)and91.417(a)&(b)tooperatecommerciallyasmallunmannedvehicle(551bsorless)inmotionpictureandtelevisionoperations.ApprovalofexemptionsallowingcommercialoperationsofsUASsinthefilmindustrywillenhancesafetybyreducingrisk.Conventionalfilmoperations,usingjetorpistonpoweraircraft,operateatextremelylowaltitudesjustfeetfromthesubjectbeingfilmedandinextremeproximitytopeopleandstructures;andpresenttherisksassociatedwithvehiclesthatweighintheneighborhoodof4,0001bs.,carryinglargeamountsofjetAorotherfuel.Suchaircraftmustflytoandfromthefilmlocation.Incontrast,asUASweighingfewerthan55lbs.andpoweredbybatterieseliminatesvirtuallyallofthatriskgiventhereducedmassandlackofcombustiblefuelcarriedonboard.ThesUASiscarriedtothefilmsetandnotflown.ThesUASwillcarrynopassengersorcrewand,therefore,willnotexposethemtotherisksassociatedwithmannedaircraftflights.TheoperationofsmallsUASs,weightinglessthan55lbs.,conductedinthestrictconditionsoutlinedabove,willprovideanequivalentlevelofsafetysupportingthegrantoftheexemptionsrequestedherein,includingexemptingtheapplicantfromtherequirementsofPart21andallowingcommercialoperations.Theselightweightaircraftoperateatslowspeeds,closetotheground,andinasterileenvironmentand,asaresult,arefarsaferthanconventionaloperationsconductedwithturbinehelicoptersoperatingincloseproximitytothegroundandpeople.sUASsDetails:SeeAppendixCSafetyFeatures:•Emergency"Return-To-Home"oAtthebeginningofeachflightahomepointisset.Thishomepointissetinaccordancewiththemanualtoallowforasafetakeoffandreturn.Shouldthepilot'scontrollosesignalwiththesUAS10

### Privacy

or manually request

a return, the sUAS will return
to the starting point. All flights will occur over private
or controlled access property with the property owner's prior consent and knowledge. Filming will be of people who have also consented

to being filmed
or otherwise have agreed

to be in the area where filming will take place. Satisfaction

of the criteria provided

in Section 333 of the Reform Act of 2012-size, weight, speed, operating capabilities, proximity

to airports and populated areas and operation within visual line of sight and national security

- provide more than adequate justification

for the grant of the requested exemptions allowing commercial operation

of applicant's sUAS

in the commercial video production industry pursuant

to the Manual appended hereto. 

# 1J;re~ Drone Pies LLC Stephen Louallen

11

# Appendix

A: No-Fly

Zones Drone Pies LLC's Pilots will not be operating within

5 nautical miles of any airport. As a safety precaution, Drone Pies LLC's pilots will not be operating within

5 nautical miles of any airport similar
to the permission granted

in Exemption
No. 11153

- Regulatory Docket No. FAA20140519,
page 25, "20. The UA may not operate within

5 nautical miles of an airport reference point as denoted
on a current FAA-published aeronautical chart unless

a letter of agreement
with that airports management

is obtained, and the operation

is conducted

in accordance
with

a NOT AM as required
by the operators GOA. The letter of agreement
with the airport management must be made available

to the Administrator upon request." As well as in Exemption
No. 11195

- Regulatory Docket No. FAA20140884,
page 12, "19. The UA may not operate within

5 nautical miles of an airport reference point as denoted
on a current FAA-published aeronautical chart unless

a letter of agreement with that airports management

is obtained, and the operation

is conducted

in accordance
with

a Notice
to Airmen (NOT AM), as required

by the operators Certificate

of Waiver
or Authorization (COA). The letter of agreement with the airport management must be made available

to the Administrator upon request." Drone Pies LLC requests the same flexibility

as exemptions 11153 and 11195 for acquiring agreement with the airports' management should operations

fall within

5 nautical miles of an airport.

12AppendixB:SafetyManualA.Maintenancea.ThesUASmustbeinspectedbyafactorytrainedtechnicianevery10flighthours.AllmaintenancerecordswillbemaintainedforinspectionassetforthinSectionB.b.Ifanymaintenanceisundergone,thesUASmustpassaflighttestwithbothapilotandamanufacturertrainedtechnicianbeforeflight.B.RecordKeepinga.Adigitalrecordwillbekeptforallflights,flighttimes,andmaintenancerecords.C.SecuringFlightSitea.FSDOSubmissionsi.ThesUASoperatorwillfileaFAAForm7711-1,oritsequivalent,asmodifiedinlightoftherequestedexemption,withtheappropriateFlightStandardsDistrictOffice.b.SafetyParameteri.Beforefilmingoccurs,a100yardperimeterfromtheplannedflightpathwillbeidentifiedinordertoseta"sterile"environmentfortheoperation.1.DronePiesLLCmustobtainwrittenororalpermissionfromalllandownersinsterileenvironment.2.48hoursbeforefilming,allresidentsorbusinesseswithin100yardsofthefilmingwillbenotifiedwithprintedflyers.a.Flyerswillcontaindateofflight,timeofflight,andcontactinformation.3.Streetsandsidewalksthatcrossintothesterileenvironmentwillbemarkedwith'WarningLowflyingAircraft-StayBack150ft"signstowarnthepublic.4.AtalltimesDronePiesLLCwillcarry$1mmingeneralliabilityinsuranceincaseofanydamagetopropertyorpersonswithinthesafetyparameterc.Identifypotentialobstaclesi.Beforeeachflight,aninventorywillbetakenforallpotentialobstaclesthatmustbeavoidedwhileinflight.Including:1.Powerlines2.CellPhoneTowers3.Trees4.Flocksofbirdsthatmaytakeflight5.Heavilytraveledroadways6.Utilitywires7.Elevatedstructures8.Atleast5nauticalmilesfromthenearestairportorhelipad.D.Pre-FlightChecklist13

# a. Take Off Location/ "Home" 

# i. The sUAS will mark its take off location
as a safe area to return
to should the sUAS lose signal with the control
or if the pilot signals the craft to return
to its "home" location. 1. Take off location will be in an area with

a 25ft radius with no obstructions, maintaining said radius vertically 200ft. 2. The sUAS will take off and land
in the same location. 3. GPS Altimeter
will be marked
as 0' elevation 

# b. Flight Canceling Events 

# i. All flights will be cancelled
for a minimum

of 2 hours



# if any of the below occur: 1. Police activity

in the area 2. Low flying aircraft

in the area 3. MedicaVNews Helicopters active

in the area 4. Wind exceeding

10 mph 5. Any emergency requiring emergency services occurs within the sterile environment 6. PIC
is unable

to complete flight without losing visual
of the sUAS 7. Any precipitation 8. Heavy bird presence

in the area that could cause

a mid-air collision. 9. Any defects

or damage found during preflight exam c. Physicallnspection


# i. Before each flight the sUAS will be checked

to ensure that

it is safe for flight. 1. Battery voltage

will be checked

to ensure

it is > 

# 75% 2. Blades will be inspected

to ensure they are tightened and free of damage 3. Camera mount and gimbal will be inspected

to ensure

it is fully attached and operating. 4. sUAS will be checked
for any damage that may have taken place in transit. 5. The sUAS will be tested
at a low altitude

to ensure

all controls are responding correctly. 6. Battery checked
for damage that could affect its charge ii.

If any party of the inspecting shows

a damaged part or parts, the sUAS

is deemed non-usable
and must be inspected

by a factory trained technician./ 

# d. Post Flight Inspections/Checklist 

# i. After each flight, the the sUAS will be thoroughly inspected
for any damage that occurred

in flight. 1. Body inspected
for any damage 2. Blades visually checked
for any damage

at all 3. Battery checked
for damage



# 14

# E. Mid-Air Safety Protocol a. Max Speed i. Ascent 

# 1. 10m/s ii. Descent 1. 4m/s iii. Flight Speed 1. The sUAS

is never
to exceed

1 Om/s 

# b. Altitude
i. The sUAS

is never
to exceed 400ft 

# c. Emergency


# i.

If it appears that the sUAS, any property

or humans are at risk, the sUAS will be grounded immediately

to a safe location. 

# d. Sight


# i. The pilot must keep the sUAS within eyesight

at all times unassisted

by any technology. 

# F. Participation

by non-pilot staff a. All staff involved

in the production

or filming using the sUAS will consent

to maintain

a safe distance

of at least 30 ft during the filming. 

# G. Pilot/Spotter Training a. Before flying, both the Pilot and spotter will receive updated information

on the sUAS and its firmware. 

# i. The controller allows for a simulator training, both the pilot and spotter are allowed

to run through the simulator training



# 15

# f f
:tao :tao

# ~**~** 0

# ~~ c:**:s:~** 

# en

# l;;~

# a:~**~** Q,Q. 

# !.. )('**~'i** 

# !.. (I) 

# • • t:J 

# •• h1

# ~ (I)


# .. :::J 

# S'ct (') 0' 

# :ee:**~** 

# ... 

# .. Q

... £» 

# >< 

# -·**~** 

# 2**~** c::: 

# -o Cil 

# -**~~** if



# ... Dl 

# j j fi 

# i


# - -

# Appendix

D: User Manual 

# Scout

X .... 

# deVenlion Auto Takeoff Auto Landing Follow me mode Circle flight Fence flight c Single Waypoint flight Altitude hold mode One key Return To Home 

# Automatic Cruise Hyper IOC mode Backtracking Waypoint record 

# Match with GCS Ground Station Software Quick Start Guide and Systems Flowchart • Specifications

: Ma•n

R o tor D1a

2 3 3mm Overall

(L 

## x W 

## x H): 335


## x 335


## x 2 75mm 

### Weight: 1770g(Battery included} Takeoff 

### We19hL <2270g Transmotter

: 

### DEVO F12E Receover 

### DEV0-RX707iCE)

I 

### RX709iFCCJ Brushless Motor WK-WS-34-002 Brushle
ss E S C

: WST-16AH (RIG

) Maon 

### Contro

U er

: FCS-X4 Ballery

: 2 2

. 2\1 5400mAh L>-Po Ground Station

. GCS 2 4G Bluetooth Oatahnk: 

### BT-2401NAiFCC) 124018(FCC) **BT-2402N~CE)**



### I 2402B(CE)



# M1 • H **1-~'41111:::1\~:..:c.:**

FH 1-/.4tJ7HLCf-' Hti:\f!f"'.,

...... W ... I'l<) IL'Tif:.

: **1)-~** hC'hlr-. 

# e F &qt,l **T11n~** 

### ;\.lu·

• · "- c.:d:: 25·n•nulc:. **L~rtdt!d** G,n,b.a **.:~nd** Ctttrlt•rtt 2\JTI'I'L·.IIes 

# e M **:~.n** rctatc



### 1r. c:ock•N•se

. motO-"S are the

. e ... 

### :x;yram thread 

# e **~/2:•,·1-!** rotate

1r co::,;rterc:ock.'N

**~ rf10~o--s**  ar'?' 

### the dext"ogyrate **~.,rea-::**



# ...., e In **n~t,.,l prnp~.lf-'·;-:**  su+->w

,,, lh:•• o: pos:\f-!

d u-•clulfl <:1\lhf-'

;i ... fO'l.'7" Unscrew

•r

· **~n-....**



### •i **rf>'~:t·on**
**""~ ttrrov.~** 



# M3



# 17Contents10Devicesthatsuppo<tGroundStation:AndroidandApplephone······································································12.0Downloadandsoftwareinstallation----------------------------------------------------·------------------------------------------13.0lnstal6ngPropellers--••---·--·---·---·-··--··-.---·--·-·--------·--·············-·····-----·-·-····-···························-14.0Restoreorassembletheland1ngstuds/bindingtheradio·······························································-···········1-350Maonscreeninstructions--······································································································36.0Routeediting-----------------------------------------------··-••-----------------------------·---------------------··47.0CompassCalibration······-····································································································480G-30J-ax1sbrushlessGimbalInstallation·························································································59.0lnstaltingtheilook+1080pcamerawith58ghzvideo•••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••510.0MotorUnlockIlock···········································································································5110GPSindicatorhghts·612.0Functionandstickcontrolinterfacedescription·················································································6-913.024GBluetoothDalalink.......···••··••·••··•·9-14140Groundstatoonsoftwaresettongs·········••··-·····-····-··---·-------·----·······································15-17150Instructionlorsw1tchingloomDEVOF12EcontrollingtoGCScontroiWng····························································17Goouloploy-.googlaondTTS--.tlbolt_______JISimpleoperatingstepsI=1_.1-codebi'ldingEl181.0DevicesthatsupportGroundStation:AndroidandApplephoneAndroidphonerequirements:(1)TheAndroidver.;ionshouldbe4.0orabove.1hescreenresolutionshouldbe480x800pixelsorabove.(2)Googleplayservices,googleplaystoreandTTSsoftwareshouldbepreinstalledinthephone.(1)Downloadthe"GCSGroundStation"softwarefromofficialWalkerawebsite(wwwwalkera.com)IGoogleforAndroidversion4.0above(2)ApplelOSsystem,downloadthe"GCSGroundStation'softwarefromAPPStoreSuggeatlon:setthephonetoHightmodewhenyouanusingtheGCSsaftwlntocanlrolthetugllt.C'.\.)C'.\.)T,"t'3 1Install"forward"propeller.;(clockwisearrowmarl<s).then"rear·propellers(counter-clockwisearrowmarl<s).3.2MatchthearrowsonthepropellerstothearrowsontheannnexttoeachmotorScreweachpropellerontothemotor.sea.orebyhand,noneedfortoots.4.1Landingskidsassembled(restorationlcodebinding)I&J,J"F....'3.3Propellersandskidlandinggearinstalled.TheLandinggearisshippedontheretractedpos•tionDONOTtrytoextendthelandinggearbypullingonit.Thetand•nggearwilldeploythef.rsttrmethesystemispowered.Follow•nstruclionscarefully:..4.1.1InstallthefullychargedbatteryDONOTtumonthebatteryuntillater"Pleasecheckthechargermanualforcharginginstructions.I\...,.....4.1.2TumtheX4onitsbackwiththebellyandretraclablelegslacingupMAKESUREnothingisblockingthelegsPowerswitch•button4.1.3TumthepowerSWitchto'ON".thenpresson1hepowerbuttonfo<3-5sec.untiltheGreenpowerindicatorlightsaresolid.I-':'.&..;.A.'3.4Propellersinstalled(nogearassembly).I0-f>ow•SWI:d\...,::.:61UOOOOihr.indicmorlight;•••14---rGrMnltQhtl41.4Tumonthepowerswitchof1he2.4GBluetoothThegreenhghtwittnashquicklywailingrortheconnectionwiththephonebluetoolh.4.15Enterphonesettingsandopenthebluetoothlunctron.Inthebluetoothsearchlistfindandtouch"waakera---·.inputpassword1234toconnectTheconnectionissuccessfulifitdisplays"connected"Exitthesetllngswhenfinished•1.19

# 4 1 6 Touch GCS icon
in 

# the middle
of 

# the mobile screen. 

# the GCS software
wiU seardl automatically


# and dispay 

# matched bluelooth. 

# then select 

# the matched blueloolh and louchlhe 

# GO icon to enter

I he maon 

# screen

In 

# lhe main screen

, loudl



# l
· 

# 'i icon theo touch 

# st>ck mode
lo enter the 

# stidt control and selling sCieen (The landing skids automatocally extend

)



# -- 

# . r-•
:; : ,_

. ;._. 

# •

•

' ,J/Jr 

# ...,..,.,

.

.



# .. **~** 

# -+

-+

-+ 

# .. , . , 

# .. **~·-** Touch GCS icon

Touch 

# GO icon



# !

E nler 

# the main 

# saeen. touch 

# •con Tooch .. icon provides instruction hinls 

# •

**~** 

# ~



# . ,1' 

# +-

' 

# -;/~I **~** l

, 

# c



# ' J **~**



# '- 

# \

l After successful binding

. place 

# the **a~roraft** 

# on a stable surface
Within



# approx

. 

# 40 sec 

# the red LEO lighl will stop flashing indicating lhat the code binding has finished 

# 4.2 Landings skids unassembled(assembling
landing skids/code binding) •r 

# .. _



# I 

# -·

..

.... 4 2 1 Unpack lhe
2 landing gears. 

# skid land.ng modules AlB

. 

# and M2 5x20 SCieWS 

# 4 2 5 Put lhe aircraft into the horizontal position

, slide the power SWitch ON

. lhen press the power button for 3-5 seconds until the green power ondicator lights up

.



# -

-

.r. 

# )

- . **~** 

# I 4 2

. 2 Place the landing gears into 

# lhe gears slots

. -.

, ,.. Power 

# I . -=::; Swtlch 

# t **~** 

# . -:::::: **B:··-~')(11'1** ,..

'• JO::,.;.I

jl"• 

## !IN:df1dt

•tQ


# I', A
/ 

# &{:

.

**~** 

# .. 

# 1 ..... J& 

# .. **~ ,.,**  **~** 

# ¥·



# - · l t \1 •

. 2 3 

# Screw down the 

# landtng gear 

# modules ustng 

# the M2.5x20 

# screws. 4 2 6 Turn on lhe
2

. 4G Bluetooth Dalahnk. The green **~ght** 

# wiH flash quickly

, 

# wailing lor the connectoon wrth the phone btuetooth

.



# I 

# I Willi! !iii'iii !Jii

- 

# • Touch 

# stick mode Enter 

# Slick control 

# and selling screen 

# •

6 t.

. , 

# c;r

. , .J 

# "

**~** 

# .. j



# \ 4 2 4 Landtng 

# skid installation finlshed. 4

. 2 7 Enter phone setttngs and open the bluetooth lunctoon

. In 

# lhe bluetooth search list 

# fond and touch "walkera-·-

" . 

# inpul password 1234 to connect. The oonneclton

is successlul

if 

# il displays ·connected"
Exit the settings when finished

. 

# . 2

.



# 20

# 4

. 2

. 8 Touch the GCS ooonon the middle


# of the 

# mobile screen

. 

# the GCS software will search autDmalically
and display matched blueloolh

, 

# then selecl the matched 

# bluet.ooth 

# and touch 

# the GO 

# icoo to ente< into 

# the main 

# scr-..

In 

# the main 

# screen

. touch 

# icoo then touch 

# stick mode 

# to en1er 

# the stick control 

# and selling screen

. 

# ... 

# ...... Toucll GCS icon 

# t:!!';!"

i **:;.**
**,- t,,~**  

# -

. 

# ., . 

# ---___:

.. Touch GO ooon



# ' Touch icon provides instruction hints

- 

# Route adning **-- -----~**  

# Setting 

# Retum TOt-T

o m" To "-le



# Alti

t u de

- Am:raft 

# potching degree 

# ...... **~**



# .. ..... **~tl l:**  **·**



# . :



# ., **"~** 

# ... ;- _;;. **'!•~** 

# "";- **.;,-;·~** 

# -. /.

J 

# • ;

· -· •
· · - i eee

**:~**

. 

# -~-~

**·· ~**  I, 

# ..-;_ **~**

. 

# ·'


# '""'



# .

( 

# .

·4
.

. **~**

'" \ ·- 

# .

"



# ~ 

# '\..: **~** 

# . . ... Enter 

# the main 

# screen

, touch 

# icoo
Touch 

# stick mode 

# ~ Within approx

. 40 sec

. 

# the red LED 

# light wiR 

# stop flashing indicating 

# that the code binding 

# has 

# finished

.
Enter 

# Slick control 

# and setting 

# screen 

# • 3 •

FIX the position



# or airaaft
or 

# operator Sticl<. control and settings 

# Map selection 

# ~



# Ba ttery capac;ily 

# Satellite quaolity 

# - Aighttime 

# E3

O is t:ant::e
to the next 

# waypolnt t-- -----

- O <Sp la y r rlOG

• **C~mbing** 

# rate Ground speed Velocity Aircraft **rol~ng** 

# degree 

# Aircraft steering 

# degree



# 21In the main screen

. touch icon and enter the route editing screen

. VI/hen finished editing. touch icon to upload the route inlo the aircraft. Position hold function

: fix the position ol the aorcraft
or operator Map selection- ----

- 1·.::1 Route write into aircraft.

- -- Readout route from airciaft

- Route recorded onto phone Readout route from motMie phone Waypoont increase Route eaot

: ng Delete waypoinllong press icon to clean up all waypoints onside the aorcraft ·' icon then touch stick mode
to enter stick control and setliog scr-.. ---Compass calibration icon **~**

**~** IMPORTANT:
Make sure the motors are locked belore calibration (Aircraft red LED indicator

is NOT flashing). Factory default setting,

is lor the motors

to be locked after completing

the 10 binding process. (For **deta~s** on lockong and unlocking
the mocors see point 10.) Compass calibratoon ocon 7 1 Touch the icon and enter compass calibration. The red LED on the aorcraft will flash rap.dly 7 5 NOSE DOWN rotation. Rotate the aircraft faCing the nose down

. rotate smoothly

on 90 deg increments Pausong

1 second for each 90 deg. {0190 11801270 1360)

**~** 

# ..

' 

# - **---~ ~---**  

# / J
\



# '

7 2 FORWARD rotallon Smoothly rotate the aircraft forward

on 90 degree increments. pausing for
1 second every 90 deg. 10190/1801270
1360) 

### • 

# . ... 7 6 Put aircraft

in the ho<izontal position, Wait approx.
40 sec. for the red LEO loghtlo stop flashing indicating that the code binding has finished.

• 4
•


# _ , __ 

# -1- 

# --- 7

. 3 CLOCKWISE rotallon. Rocate the aorcraft around the roll axis smoothly

in 90 deg increments Pausing

1 second for each 90 deg. (0
I 90 1180

I 270 1360)

**~**



# ' 7 4 HORISONTAL .-n<m Rotate the aorcraft around the YAW axis smoothly

in 90 deg increments. Pausing

I second for each 90 deg. (0 190/180 1270/360) M'ORTANT:

The

- """""'
of ftight5

, you 1MJ exponinc;ot
the oin:nlldrllling. n::wmal **;>~** ::c•·tn

• ...e :n ,.,.. lrlt:: __ raT. **marv-~**

.... lit:: lhe **s·~slem** rv 'H'tf1:S tN: **cal•tr~** After

5 · tC **""'"~!>.** lane

l .r;O and **~** lr'.e **mota~**

to Avt: '"" •motOYE'd -.ngs NotiCe The sa.ght ctrrfhng mav oontfOIJe
fOf" a couple

of battenes yoy WI" nottoe **~~ •mpro-o~emer\1** 

tn **~he** GPSh:)fd

& **~· atM~r** 

4 5 bal1eneS **Nol~a>** Alwoys pet1Dr'Tl "''" calltnobon iMa'J 1-om olein<: fiel<2s ano melal OtJrl;oca•. Tr"Vl3

: 0""""' brands NNe difhlrvnt catibnlborl procM&as.
tnt& process

;s tyo.cafly **'~~**

U) as ·me C..JbrM.on **~noe**

·



### 22IMPORTANT: REMOVE the battery from the Scout X4 wh<le you install the gimbal T1e **~i'T'bal**

1S a h'9h-performance

e etroMecha'l.cal des1qr a"ld siloukj
be handled w1th 9reat care

. AVOID us1ng force wner. **install~ng** B 1 Prepare the G-30 g>mbal M3x12 screw. spnng

. 9.1 Screw the shO<t

" mushroom

· antenna 1n1o

I he camera

. use 1he included wrench

to gently secure the antenna.
do not use force ...

8 2 Slide the g>mbal onto the qwck

8

. 3 lnstah the springloaded mount rail from front toward the M3x12mm ·finger screw·

at rear of the aircraft as far as possible

. the from of the gimbal

to secure the g>mbal 9

. 2 Release the two M2x4 scre"'-s sP.C"unng the carr..era mounting bracket

9

. 3 Install the camera into the gimbal with the M2x4 screws (make sure that you posihon the bracket wtlh

a gap between
the bracket and the camera lens)

. 9 5 The ilool<+ camera >Snow successfully •nstalled mto the G-30 g>mbal 10.1 Motor Unlock

8 4 Conned the 9Pff'l wtute data cable
to the ·complex data port' on the bottom

of the X4. then coonect the cable
to the back of !he G-30 gimbal 9.4 Connect the camera

·s power cable
to the power port on the G-30 gimbal controller. After successfully bind>ng push the !hrot!Je control ball to the lowest point under stable mode Long press the stable mode icon when **~he** rec

..... :=c

i n d1c...::tor tl)rr. S:)k: **f.'c~ ~...,~**  **no~.::.r**

s. **.Jr.lc.~ke:**

In this c.Ondi\1on. when you move the throttle control ball up the motor will run Note: For safety. the motors will automat>c.aily
lock after 10 seconds

If you do not start nyn-.g
'" 10 seconds. you will have
to unlock the motors aga1n 10.2 Motor Lock After unlocking
the motors push the throttle control baR to the lowes: ;>oint.

I hen long press "AUTO Take Off" •con 

### 9

. ... .-ren !11'2 Ked

i .. _I:·D **11!1~1-~n·.w**
ryn1 :}nf-'s ou' ,lhe motors are locked and won't start

if you push the throme control ball up

l0ft9 pre• sblble mode icon: Motor unlocke-d
l.oftg pre-ss AUTO take off icon

.. mvlcw **~** • 5

.



### 23IMPORTANT:

For SAFE flight
in GPS flight mode: the BLUE indicator light should
at least "double" blink. (two blinks
at a **~me)** In

I he main screen. lauch oconthen touch stick mode
to enter stick conlrot and setting screen

. Long press stable mode k::on

/ to unlock motor. As shown

in figure interface Function

Icon 

# .... +-

It is highly recommeoded

that you wait for "1rippe blink"

8 sla!Mtes before starmg the ftight NEVER -mpt

to AUTO-START
with lea than "1rlple bllnb" Touch AUTO take oil icon 

## 9 or push throltle control baP

. Touch display iron Instructions 

# .... +-
Touch display/hide
ocon 

# ~ Touch senior function icon Sable (,__I) 

# e Toucll icon

- Switch

to c:ommoo night

. using tho conWol ball to control the Aircrd. Long P"8SS the ICon to unlock the molof mode

- 

# 9 **l:%~o~**
**t;lil**

- Unlod< **Mote~**

- Toudl icon

- The aircraft will aut<Jmatically takeoll. AUTO



## ..... ..... 

## .,.._ Tab Off



# -= You can use 1M; luncbon only wl1en receiving

a slrong GPS signal

I ·----

-



## -

-----

- --- --· 1 Auto



# 0 Landing

Toudl

icon

- The aorcraft.,. lend automatically Toucl\ """'

- T"" ""craft ...U en1ef onto AUude hold mode **a~~tomatK:ally**

! Altitude hold 

# G N<*S:

I mode

(1) You can use thos fur>dlon onty"""'n -..ng

a sl""'!! GPS signal (2) "ll>ere

os no GPS sign;ll 011he **~** iSn

' t In good condlbon.
the aorcran **.n~** entet automalc8ly annude hold mode ins1ead

of holding

at one position, One key Return 

# e Toucll""'"

- The aM'Cfllft W>ll au10malicaly return

10 the poont of ongin 

# -= To Home

You can "'"' 1M; function only

- receiving

a strong GPS signal

. . 6

.



### 24

# Function 

# Map selection Stick 

## mode selection 

### Compas5 

## callbtatlon Gravity Sensor DATA Switch HyperiOC mode 

## Waypolnl 

## re<:ord 

## Follow me mode



# Icon 

# 0 

# e Instructions **Map~'"'"** Thefe al'e

11 **~'?e!\**
**n~** 

### st•ck mooe...c. Comoass catibratton The default setting

tS or. after turmng oo. the device

1s switched

to gravi-:y sens01 conrm4 

# t Lo•c 'c·w.,.o 

# t.. **:l** 

# .. • .....

t

**~· ~.,** 



# .. 

# ... **·~ ~.**  

# !t **~** .

l A 

# v. 

# ....



# .... **Rig'"lt-leani~** ' le3n b.'}Ckward

' Backward FactO') oefauNs are set 

### :o ·ope-n' JOC means tnat tne arrcraft

s 11jght direction



### is n!laled

to 

### tne position

of 

### the fu"st GPS signets. rather than the dtrectiOf"l 

### the ain:raft



### is potnted 

### Notes: (1) YO<J 

### can use th<S 

### tune1ooo only when you 

### :we receovony

a slfong 

### GPS sognaJ (l) Duung **l'li!J~l I~**  ctrone w•U **~ter** 

### hvpet IOC nl()C(: whef't the distance **bel~n** 

### ltle 1ltght po&tlon



### ol the drone 

### anc 1t\e 

### •nth

.• **·t~** 

### OOSihoo ...-.tlet'e tne 

### GPS S'9AAI was estabksned

•s more tnan 1Om (3) In **~he** IOC mode. regardtess



### of whH:h way lne aLTcraft

1s 

### pointing. you jus: need
to press and 

### hold back the controi ball to 

## nwce 1t1e aircraft


### Oy back to 

### tho onginallakeoff pmition T 

### ouUl teon ---...... 

### The am: raft 'Mil record ttle 

### f)tgtlt points autornaric.aolly

. Noles: YO<o can use 

### tr.s k;ocloor. 

### only when 

### voo are re<JeMng

a strong GPS 

## S9"'l ToOCfl 100n -..-. 

### T!"'e artcratl oouiC fOllOw the 

### locahon



### of mobile automabcat.ly Tuvdllhc icor. 

# Q **uod~r** 

### 11.ghl cond1t10n



# ..... **o.,o:•·~** 

# -

v

· 

# .

.



# ' 

# .

. 

# ~~· **m** 

# ...&... **--~** 

# :=--d"'

('. . . **~'** 

# •

r --! **~ I~**  

# too 0\Jtoma!ocaU-y allolude selling lxJK. **~to** en\llronftlef11 

### cttoose 

# ·Normsr

or '"Fast'"
to set att.tude 

### Notes: Yoo can use this funct10r. only when you CM"U mceivWlg

a strong GPS 591al 

## • 7

.



# 25

# Function Automallc CfVise 

### Bac:ktracking 

## Cin:le flight 

## Single 

## Waypolnt flight 

## Fence flight


# Icon 

# o: Instructions Toudl tCOn 

## --+ The 

### 8lf'Ct'att wtH cnnse au10mat'ICalty 

### Toucnooon

1toe 

# "''"""'...a aul<w•oatc:ally auooe a<:COrdtng



### to pre-set 

### route Ounog 

### lligtll.

**~** 

### you 

### want to edit

a ,_ roolo. 

### long press 

### ll1e Automatic Cruase 

### Icon 1o upload


### to 111e ain:rWI tho 

### new route.



### Ooolols 

## """'YJX*ll Cruise accanting



### lo edit route Record



### to mobile phone 

### Wr4e Into 

### 8H'craft 

### _, You can ....., lhs tuncboo 

### only 

### when rocetW>g



### a strong GPS s.gnal 

### TOU<:h o000

- 

### Tile 

### atrcr3ft wtllauiOmatleally 

## return
lo the poonl 

### ol 

## orlgon In aulomatte crurse mode, looch 

### lhe ooon. 

### and 1he aon:raft Will comes 

### bad! au1omabe311y llC<l<lrlllngto

the pre-set route 

# -: ( 1 ) You can u.o 

### this funclio<l 

### only when 

### recaMng

o wong 

### G?S 

## SIQMI (2) You musttouctl!ho



### ocon 

### bel""' trw: ao<C>art 

### reaches **~~>e** 

### 1as1 **~**



### ., ordo<to 

# -aci< along 

### tile- pall> T<ll!d> c:on

- 

### The 

### aircr.oft will aulomabcally begin


### to Clldot 

### Touct> 

## theoron

. 

# ~

In 

## the auiOmabC radous 

### selling 

### bo•

. you 

## can set 

## r_,. aooordrng



### to 

### anvironmenl
and IOU<tllhe 

### Go icon lo 

### start -: Ycu can """ 

### 1hiS function only 

## wnen re<:eMng

a strong GPS signal 

### T<ll!d> ooon

- 

### Tile aitcrart wMI ...Uer

a 

## t.o- when arriving



### al 

### !he llighl 

### point 

# ..... Touchll1e 

### ooon

Q 

## ·~ •

•

•

•

• IJ



## ~

· " • 

# ~.· **~,~** •.•

'

4 

# ~.

**••**

I 

# .::,~ 

# ... **.-::J ~--~~**  

# . .:ili

_ In 1he 

### autometic altitude sehng 

### box. ycu 

### con set alldude ao::onlong



### to etl-l
and 

### !ouch 

### OK ooon Ill 

### start. -: You con use 

### til,. function **only""""'·~**

a 

### sttong 

### GPS Signal 

### Tau<:t> 

### ocon

- Autornalocally

# enlefAfter 

### toudling
ll1e 

### imn, the 

### airl:r.lft 

### will fty 

### Wlflm lhe sol ;na 

### The ainT.Ift,. return aulomatically when 

### rvachlng 

### the 

## edvo- -: Ycu can use 

### this luoction only 

### when 

## ,..,...;ng

a 

### strong GPS 

### sigoal 

## . 8

.



# 26

# Function



# I Icon



# I Instructions 

# - -- Sldd!Mdlng



# I 

# --
ToucP> 

### lt>e ICOn 10 

## make"" landing 

### skids 

## r-

up 

### folded



# - 

# ~
**~** dlstaMe 

## Control the 

### gimb81tiltlng 

## Conlral the 

### gimbal 

## rdllng

Toudllhe 

### icon to 

### malle 1he 

### landing.- 

### .-.rfold Rewm 

### dlslanoe 

## 0% 

# t 0% 

# Con-YConlrolledvanallle 

## The 2.4G Bluetooth Datalinll 

## consists

of an IVr 

## end and Ground 

## end, which 

## PfO¥ide ,...... and stable long disQnce 

## wirwless transmission 

## when GrD11ncl Station 

## 50ftware

is used. 

## The signal flow is 

## as shown 

## below. Slgnale 

### lfom 

# Glound--. 

# I **Fl~=trol**



# !

---

[ **~~r**


# r Slgnalefram 

### Fight
.. 

# c **~ ~IIIOCIWe)** 



# l · Ground 

# Stallon(~ 

# --· ...... Alr-d

: 5runO 

### UMge



# u BT

· :U01NA(FCC)fBT·2402HA(CE)

. 111"-
**BT 2~A(CE)u** 



# an UllfTIIIIe 

## Ground 

## emt IWnll 

## usage 

## u. BT-2A0181FCC')IBT-2.02.8(CE

), taU BT 

## ,240281CE:) nan enmple. 

# 13.1 Antenna Installation 

# BT-
2 4 02 8 2.4G Bluetooth Datalink 

## ~.==-----: **====** .. **,~:.:· ::_-**  **--"== ---'----'** 



# +-



# m **-~**

- -=- 

# -= tt:J . 9

.



# 27Important:(1)Ifthereareobstaclesbetweenthegroundandatrendstheradiosignalbetweentl:e2JGBluetoothDatahnkw1tlbeweak:makeSlirethattheantennasarealwaysvisi!:t!yunobstructedduringtheflightHu'"f1ar.bodies.treesbu1hngsorhillswilldisc-..onnectthehnkbetweentheAirendanctheGroundend(2)MakesurethattheantennaoftheAtrend1spou1!1ngdown.andtheantennaoftheGroundend15poinling;1t'sbesttoputtheGroundendatahighplacetogetfurthertransmissiondistance13.2ThecognitionofBT-2402NA(CE)theAirendAntenna-IIdelJenbr-"}mBT-2402NAU•'IR"":xJ2.4GBtuet.ootllDotollnk-;BlueLEDI."'CE0'-Antenna--V'"'_.IIADEINCHINAUpgradebunon"""7Ia'fiiii0UPGRADEThebackofBT-2402NA(CE)friIIGreenLED:DatareceMngortransmittingindicatorbetweentheAirandGroundendTheendoftheAntennashouldbepointedupwardsandunobstructedtoensuremaxtransmitbngd•stancePWM1signaloutput_.,......PWM2signaloutput1'\'IMJsignaloutputPPMOUTf11--PPMsignaloutputPW1.14OUTSll"reportPV.'M1signal'"PUIFWM2signalinput"-?WM3signalinputPPMsignalinputBlueLED:Datarece1v1ngortransminingind1calorbetweentheAirendandflightcontroller.•10•2813.3BT-2402B(CE)Groundendinstruction@------1@--++-@..@)®E£BmIBT-240281'119.1MIFtJ.."CD@I41-'•a®®®=.JL=@CDON-OFF:Powerswitch0PowerLED:Powerindtcalor(RED)0COM-TXLED:Indicatorofdatareceivingfromgroundstationtothegroundend(Green)0LED:Indicatorofdatatransmittingfromthegroundendtothegroundstation(Blue).®LED:Indicatorofdatareceivingfromthen•ghtcontrollertogroundend(White)®RF-TXLED:Indicatorofdatatransmttlingfromthegroundendtothefhghtcontroller(Yellow)01USBDownloadSW®2UARTDownloadSW®Bluetoolh:Bluetooth•ndicator(Green)@Charge:Chargingindicator(Red)@UART@USB:USBport@Antenna·11·2913.4CablesconnecttingillustrationDATAPORTFCS-X4MaincontrollerDATABUS•deUenliontl.-cDBT-2402NA....)>·--Z.4GBluetoolhDatalinkCE!'MADEINCHINAd.1II0]lll'PWM2OUhPIT-•OUT•:::=:.'-JPWM40UT•f'PWM21N•..__iiPWM31N•L-PPMIN•J,,--------........,'.AUX4....AUX5....,_&--:AUX6..,..-iDEVORX707(CE)IRX709(FCC)Receiver·12.3013.5 Program Upgrade Both lhe A

i r end and lhe Ground end p<ogram can be upgraded

at the Walkera we!)slle Upgrade loot UP02 and UP02 adaptor

. 13.5.1 Air end Upgrading ( 1) Insert the blue. yellow, black color plug to the corresponding upgrading connection socket and insert the other end to the UART port. 

## JJJrion **~**


## 1

.... BT-2402NA UP02

UP02 **~**

**~**



# ..... .._ 

## ........... (21 Press the

· uPGRADE

" bullon

to supply power and enter the upgradmg state 

# w ;:..

1\g 

## © •

II Upgrade the button UPGRADE 

## toJ. The back of BT-2402NA(CE)

,;::; o

no. 13.5.2 Ground end Upgrading (1) Insert the red yellow

, blue

, black color flat cable into lhe UART port

. 

# C€! ltAOE
Ull CM .....

**PWl.l~ OU1~o**  P\\'U2 our

.. P'W\t:JOUT,. PPU C\JT

1o PWU4 OU'ilo PWt.l

i -"4• **PWU2~•** PVIU.l

, ._.,. **~,,.,.,.** UP02

UP02 Adapter
UART port



# . 

# )~~:!! **~ ~** 
t§b 

# Ill~ **~** =ti;:B 

# ..,., **~[** (2) Tum the switch "UART Download SW" ("ON" pos1tion) 1. USB Down

. , ••

, 

### sw



# t **~t:'_ o.!.'!**  **sr ~**  111



# r

t 2.UART Download
SW



## £ :-;=1

I l 

# 1 

# D = :ON

----. 2 

## -=-

· '"' ... ,

......,

: 

# Jlil;n (3) Turn on the power switch
to enter into upgrading status

( "on" pos

i tion) ·13·



### 31

## 13.6 LED Indicator descriptions 

# LED status

Status instructions 

# 1!1:

6 

# JII!B ttashes quickly

The AJr end and Grouod end are receivingitransmitting

data **1!1~** 

# ·CIII!J k.eeps sohd

The Air end and Ground end are not receive.'transmit

data 

## The 

# Air 

# end mi!!!I!!:J nashes **qu.c~ly**



### The AJr end and Fhght control end are receiving.transmitting

data **keeps** 

### solid

The

Air end and Fhght control end are not receive

• transmit data 

## and **~**

The AJr end and Ground end have lost signal nashes slowly :
.. **~~**



### ...

: keeps sohd m'!m

Normal power voHage 

# '•·fft&,

**;..' flas~es**  **lm!l**

Power voltage

15 less

I han


### 3 .3V 

# 'j I I 

## ll!ft?Jf
II 

# #IN Clashes

- qu•ckly

The Ground end
1S receiving Ground Station data 

## I 

# ~~ l!mii3!3•J

keeps solid ...

The Ground end
is 

### not rece1ving dala 

### from the ground station. I

I 

# 1311!1Ji!3!ll•

l nashes GJI!Iq uicf<ly

The Ground end
is transmitting data to the Ground Station I

I 

## The Ground **G•~!!iU!3• keeps** 


## so

! kl m!l

The Ground end
1S not transm1Wng data to the ground station. 

## end



# I RF-RX LE[)j HashesiWhitelquickly

The Ground end



### is receiving Flignt Control data 

# 'I

'

I



# I

RF-RX LED! keeps solidiWhrtel

The Ground end
rS 

### not recervrng Fhght Control data RF-TX LED flashes Yellow quickly

The Ground end

rs lransm1\ting data to the Flight Control

I 

# ., ( 

### :

**~** 

### T 

## .1!. L. 

# :o keep

s sohd Yr

The Ground end
IS 

### not transmrtting data to the Flight Control RFNVhiteland 

## Yellow' LED flashes slowly

The Ground end lost contact w1th the Air end 1 

### E!!IIBII LED flashes 

# IZ:J qurckly Bluebooth unconnected 

## I I I Cl'CI!I!mJ LED 

### flashes **slowly** Blucbooth connnccted 

## l EiiE!m!I LED keep

s so

l id 

# Iiiii

Chargrng 

# l!ll'!!D!m LED l1ghts out

Chargrng **~nished** 

### :normal Situation 

## · 14.



# 32

## 14

. 1 Channel setting tn the maon screen

. tovch 

## icon to enter into the setbng 1nterface ELEV

. AILE

. THRO

. RUDO defau« setting

is "NORMAL" **•l!li:!•[~,** 

## 14.2 Parameter Setting ( 1) 

### Gsensor Reverse If the gravity sensor



### is act1vated and the **a~rcralt** 

### acts differently from 

### the correspondong tablet 

## pc or phones mpu!S (please refer to 

### page



## 7 for Gravity Sensor explanation). please press·.,·

to reverse



### it. (2) 

### FollowMe Height 

### Set Defautt he19ht=tOm 

### You can change the height with new serungs(5-200m). (3) One Key Takeoff Default heoght=t 

## Om You can change the 

### height with new sethngs(5- 

### 15m) (4) **Waypo~nt** 

### DefauttAitiude Defaun height=



## 1 5m You can change the height 

### with new settings(5-400m).



## · 15

·



# 3314.3BatteryvoltagepointParameter.;FlightModePidsBalleryiFSGeoFenceBatteryMonitorDisabledFailSafeDisabled.....................Pwmm!JGPSJsEnllbll!-GCSFsENd:ltuSti>r>d.vdb.mt<y22.21Alatmaaur•lowballerywarning21.4V14.4GeoFenceParametersCalibrationFlightModePidsBallery/FSGaoFenceGaoFence0Tlc:kdyouneedlo.....AltitudeandcircleRll.orland'd"',,.,l:r'14.5BluetoothUpgrading14.5.1BT-2401B(FCC)/BT-2402B(CE)Groundendupgrading(1)Tumontheswrtctl"2.UARTDownloadSW'(posrtion"ON")+---1S•1000m+---15-1000m+---15-80m;I:§!Dll!l«¥llJl1D=(oN-:2_,.::---r--r--lWb·nnn(2)ConnecttheGroundendtotheGroundStationsoftwareGCSandenterintotheupgradeinterface(3)ChoosethecorrectGroundendftletoupgrade14.5.2BT-2401NA(FCC)/BT-2402NA(CE)Airendupgrading(1)TumONswitches"1.USBDownloadSW"and"2.UARTDownloadSW'1.USBDowolo•dSWpst[):JitI2.UARTDownloadSW·.·····-1ON;·2(2)ConnectthegroundendBT-2401B{FCC)IBT-2402B(CE)totheGroundstationsoftwareGCSandenterintotheupgradetnlerface(3)ConnecttheAtrendBT-2401NA(FCCVBT-2402NA(CE)totheGroundendBT-2401B(FCC)IBT-2402B(CE)(4)Choosethecorrectendfiletoupgrade·16·34

### ........ **~** Tops: Please reroonect and upgrade again

if tile upgrading can"t be finished suroessfully within one minute. 15.0 Instruction

for switching from DEVO F12E controlling

to GCS controlling Switching operation flew chart Alrcrafllaking

olf must be controlled byDEVOF12E

The thrott1e stick bad<
to tile middle position. tum tile control mode SWJtch
to "1" posibOn (switch

to altijude hold mode)
Toggle the controlling mode switch
to

·· o· poSition quiCkly """ then toggle

d back. \o -,
.. po:slhOil 1 position

0 position Toggle back to

Swolch

to GCS __,.

1 software

to control the aircraft 0 Manual 

# ~

**~**

1

'

I DEVO F12E(white)control
mode switch:

1 GPS 2 RetumHome DEVO F12E(black)control
mode switch: MIX 

# ll(ffi)

**aa (§JI]**  

# II

D


# ti

**~** ·1\

-

.

. .. o ..

J 

## D 

# . .,

Eb c . ""

;

dd )1 **.~-**

· -

( 1 ) M<*e SUte the transtrltl8l' and GCS ronnect

1o the **~** wall. (2) The GCS will has VOICe rem4nd when the switching done. ·17.



### 35Tel.:(8620)8491511584915116Fax.:18620184915117Email:heli@walkera.cominfo@walkera.comAdd.:TaishiIndustrialPark,DongchongTownnanshaDistrict,511475GuangzhoudelJenlionSpecifications,contentsofpallSandavsilabilityamsubjecttodlange,Wakeraisnotresponsilleforinadverterrors(€Kinthispublication.._..'-'-c-.<:'Web:www.walkera.com36

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# c !!.Usingthismanuallegends0WaningLtmpatantBeforeRight*HintsandTipsillReiEnlnceThelolbwingtubrialsandmarualshavebeenprodlcedtoemueyo.atomakelUIuseol)Ourlnspi'e11.01SCiamer2.1nlleBox3.1nspire1QuickS1artGuide4.SaletyGuidelines5.1nspire1UserMa1Ual6.1nlelligentAighlBanerySaletyGuidelinesWatchingauthetutorialvideosa1dreadingtheDisclaimerbeloreflighlisrecanmanded.Afterwards,prepaebrywrlirstflightbyusingthelnspi"e1QuickStartGuide.Refertothismaruallormorecomprehensiveintormalion.WatchthevideotutorialsPleasewatchtheLibrialvideobebwtoleanhowbuselnspi"e1oorredlya1dsafely:www.dji.canlproduct,4nspire-1/oldaoDownloadtheDJIPilotappDownbadand11slaUtheDJIbeloreuse.Sca1theORcodeorvisit'hftp:Hrn.dji.net/djipibl'todownloadtheapp.1!1-IJ....·.·ooJ•Forthebestexperierlca,usemobiledevicawill.tvldriodV4.1.2oralxM!.FIEq.JiresiOS8.0orlaler.238-ContentsUsingthismanualLegmdsBe1oreAigttWatchthevideotutorialsDownloadtheDJIPilotappProGictProfleIntroductionFeatureHighlight!;A.ssanbletheNt:ra1tAl'aaltDiagramRanoteControlerDiagramAircraftFlightControlerFlightModeFlightSlatuslndicataReturntoHome(RTH)DynamcHomePM!tVisionPoSiloongSystemFlightReoorderAttac:tungandDetachingthePropelersDJIlnteligentFlightBatteryRemoteControllersRanoteControlerProhleRanoteControlerOperalonsDualRemoteControlersModeRanoteControlerStatusLEDlinkingtheRemoteControlerRemoteControlerVersimGimbalandcameraCameraProfileGintlal2222667991212121315161717182424293132333536339DJIPilotAppCamera40Map43Academy43UserCenter43FlightFhghtEnvuonmentRequ11ements45Fllghti.JITIItsAgttRestnc:IJOnArea45PrefightChecklist49Caltlraklgthe49AutoTak&-ollandAutlLanchrg50Starurg/StQA>li"IQtheMotors51FlightTest51FAQAppenclxSpeahcatJOns57lntelhgentOnenta!JOnControl(IOC)60HowtoUpdateFumware6162440Product Profile rhis chapter describes
the features

of Inspire

1 instructs you to assemble
the aircraft and explains the components

on the aircraft and remote controllers.

5

41:pcQ.t:!l:p0iii"ProductProfileIntroductionTheInspire1isbrandnewquadcopte-capableolcapliiTlg4Kvideoand•a'lsmitmga11-1)video{upto2km)bmunipledevicesstraightoutollh!box.Equippedwithretractablelanclirlggear,itcancapturea1unobstructed360degreeview!romitscane-aThebuill...,cane-ahasa1integratedgimbaltomaximizestabilityandweightefficiencywhilemirimizingspace.WhBlnoGPSsignaliSavailable,VisionPositioninglechnobgyprovideshoveringpreciSion.FeatureHighlightsCarnaaandGinbal:Upto4Kvideorecadingand12megapixelphotocapture.Reservedmountingspac:ebrNOlinerslorbetterexposurecontrol.Newquick-feleasemountalowsyoutoremovethe-.::r'l:!t"awrt!!aS-2!.HDVldaoDowt*lk:lowlate-1cy,HDdo'Mllinkpa.veredbyane-1hancedversionollleDJII..igl'ltbridgesystEm.nalsoprovidesdualcm•ollersmode.gear.Re•actablelandinggearthatenablesanunobshJCtedpaJaamic:viewlrcmthecamera.DJIInlaligatfFlidltBalefy:4500mMOJIIntelligentF19JtBaleryerrpoysnewbaltayeelsi!rldabatterymanagEmBltsystem.Contmla:Thenextgeneration!lightoontrollil"systEmprovidesamaereliablefl91texpEI'ienoe.Anew!lightrecorderstaeslle!lightdata!romeachflight....dViSionPosilioringenhaJoeshoveringpreciSionwhennoGPSisavailable.AssembletheAlraaftUnkx:QigTravelModeTheaircraftisinTrawlModeduringdelivery.FolbwthesestepstochangeitbLandingt.t:Jdebebreyourhrstllighl:1.lnsa111elnteUige-1tFlighlBaaeryinbllebalerycanpa1rnBlt2.Pa.vertheRemoteControllera1dllelntelliga'ltFlightBalery.3.ToggletheTranslamationSwitch'-"a1dc:bw1atleastburtimes.4.Pa.verotttheaircraft.tijt..........642

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# Akcrat Diagram Remote 

# Contrdler Diagram

INSPIRE

1 Useo Manual 

## [1] GPS [2] Prooeller 

## {P17) [3) M::br 

## [4) Po'l! LED 

## (P12) [5) La·..::Jng gear 

## [6) Gmbala'"l:J CacrEra(P35) 

## [7] hlalloge'11 Rr,;pl Ballery 

## (P18) 

## [8) .t\Jrc•all M•:ro-USB Pcrl 

## [9) Feao LED (P12) 

## [fJ) C;rn;ya M>.::::•o-USB Port 

## [11) Cirnera M>.::::ro-SDCarc

Sbl 

## (P35) [12] V1sKY1 Pos1I>.:Ymg Se'"lSOrs 

## (P16) [13) .t\!rc•all 

## Stai.Js hacalcx 

## {P13) 

## (1] AnEmas (P29J Relays ai'C'ail OYltOI a"'G 'y'K)30 

## Slg'lal. 

## [2) Mot»e Device Holder 

## llo.J'llng pla:::3I<Y 

## yru• m::Jb1le 03¥108. 

## [3] Control Stdl Corltrols **a~rcrall**

0' 

## 0911310'"1. [4) 

## Re\.lm Heme (RTH} 11111on 

## (P13) P•gss a'"l:l 'lola h3 b.Jib'l

to n1bat3 **Aat.JTT"~**



## to H::tm (RTH). [5] **Tra~slormalion** 

## Switch (P27) Tog-;;le he s'o\'11::'1 .Jp o• oow•1



## to ra1se or K:Jwer **~1e** 

## l.;n::ng gear.



## 9 "1J 

# c 

# "" "" n "1J 

# c it 

# 45-u 

### c c. c () -u 

### c =- it INSPIRE

1 u..,. MDnuDI [6] Batmry I.BIIel LEOs

[8] PoW9' Buttm Drsplays
**I~ c.rra-~1**  battery level. [7] S1ai:Js LED

Used

b p:M"er on or p:NI'er all he remole ccnlroller. [9] RTHLED Drsplays
the power slat.Js.
C1rcular lED aral.fid he RTH bu1bnd1Splays

RTH slalus. (10] Camera Se1blgs Dial T urrl l'le

d aal Ia adJuSt camera sellngs. O'lly t.J'lclo'lS w'len 1'19 •!filole ca'llrollar

rs CO'l'leclaa

Ia a mob1le Oe\IICe r.Jmng **I~** DJI P1k:Jtapp. (11] Playback Ell11on PlaybaO\
t1e capLJrec ma;JBS

or v10eos. (12] ShJ11erButtrn Pres.s

I:J la<.e

a pnolo.

II 1'1 burst moOs. tle set **'lumbe~**

at pnotas Will be l<io<.en wltl one press I 13] Riglt t.4ode Swit:h Used
lo sw1IC1 bel .... -ee'l
P. A **a~**

F mooe. (14] Video **RecxJ~g** Ell11on Press

Ia sla1 recardng vteie:J. Press agan
Ia slop recordr1g. (15] Gn-tlal Dial Use tlrs alalia co'llroll'le

bit at tle gmbal. [16] M-.HDMI Pat Comecl

a'l HD campal1ble mon11:Jr

Ia lhiS portia gel
a lr.-e HD VIOao prev19w

at W'lallhe ca"nera sees. (17] Micro-USB Pat 10 FO! C071eclng

tle remote crnlrollal'

Ia -your campuler.

[18] CAN Bus Port Reserved

lor luture use. [19] USB Port Comectla mobile devace

I:J access
all altha DJI P1lo1 app co'llrolsana

lea lures. [20] GPS Mcdlle Used
Ia pnpont he locallcn

ol he remo\3 controller. (21] Back Left Button Cusbm!Zabla bulbn

n DJI P1k:JI app. [22] Power Port CoCVleclta

a po·.wH source

Ia charge the remo\3 cantroller"s ntemal battery. [23] Back fli!tll Elltbn Cusbmtzabla bulbn

n DJI P1k:JI app.



### 46Aircra This chapter describes
the features

of the Flight Controller. Vision Positioning System and the Intelligent Flight Battery.

47)>-;;·AircraftFlightControllerTheInspire1's!ligtdisbasedonDJIllighloonlrOIIerwithsewralertlCI'Ioementssudlasnew!lightmodeandnewsalemode.TITeesalemodesareavailable:Failsafe,FlellmHaneCl'ldOyramicHanePoint.TheselealuresensuethesaleretumolyourairaalttheocmralsigralislostA!lightreccrdersbrescrucial!lightdatabreadlllight.FlightModeTh'ee!lightmodesareavailable.ThedetailsateadlflightmodeareIClJndinthesectionbelaov:Pmode(PosilcK*'Ig):Pmodeworti.SbestvmenGPSsignaliSstrcng.Thereareth'eediiiB'EinlstatesolPmode,vmidlwillbea.Jianatic.allyselectedbythelnspe1depelllklgonGPSSignalsrengllandVISionicrlingsensors:P-GPS:GPSc.JdVisa!bollaeavailable,andtheai'craltisusilgCf>Sicrposilicrling.P-OPTI:VisionPositoningisbuttheGPSsignaliSnot.iSusi"'gonlyVisonPasdicrlinglcrhoveringP-ATTI:NeilhEI'GPScrVisonPosdK:Jningavailable,ai'crallisusingonydsbaomei!rbrpo!itioning,soaltilldeiscontrolled.Amoda(AIHlude}:TheGPSVisonPosdicrlingS\'SIB'nisnotusedbrholdi"lgposiion.Theai'craltonlyusesdsbaomei!rtomaintainallillde.ndisstillreceivingaCf>Ssignal,theai'craltca1aulanalicallyrelumhanedlleRemoteCa!lrOllersignalisbstmdtheHemePointhasbeenrecordedsucx:esslllly.Fmode(Function):IntelligentOrientationConlrOI(IOC)iSactivai!dinthismode.Fcrmorei"'lcrmationabouiiOC,relatolleIOCinAppEI'ldix.:¢:UsetheRightConlrollermodeswddltochangelle!lightmodeoltheai'cralt,raterblle"FlightMadeSwit:h"onP271crmoreinbrmalicrl.FlightStatusIndicatorTheINSPIRE1comeswiththeFrontLED,ReaLEDmdAi'craltStatuslndic.abr.ThepositionsollleseLEOsaresh:lwninthelgtiebebw:TheandRearLEDsh:lwlleorientatK:Jnolthe.VaaltTheFrontLEDdisplayssolidredandtheReaLEDdisplayssolidgreen.ArcraftStatusshowsllesys.tEI'TIstatusollleUightconiJOIIBr.ReiertothetablebelaovbrmoreinlcrmalicrlaboutlleAircraftStatusIndicator:1248

# Aircraft Status Ind

i cator Description 

# Namll **®~**



# ....
.. Fled. GreB1 **a~d** Y elbw Flash Ahemativety 

# ~ ...•.. Green a1d Yfilow 

# Rasll .A*mC!tiuely 

# @ ···· ··GreS1 FlashesSbwty 

# J:GfX2 ······Green 

# FlaStles Twioe 

# ~

· · ···

· Yella.v Flashes Sbwty **Wamn;;~** 

# (~······Fast Yelbw Flastmg 

# ®.:······Slow
Red Aasmg :®······Fast Red Flashng 

# (jp

· · · · · ·Red Fla!;hilg .A*mC!tiuely $-SohdAad



# INSPIRE

1 Use.- Ma,..al 

# PoWB' on and sell-chad<. 

# Aft:ralt wannilg
I() 

# Sate to Fty(Pmode
with GPSand Vision Posilioring) 

# S.

b 

# f\1 (P 

# rmde will \tsi:l'1 

# Poatoili



# g tlU wlt'od 

# GIS) Sate to 

# Fly (A rmde 

# but 

# No GPS and Vision Posilioring) REmote Controller 5qlal Lost Low Battery Warring 

# Critical LON 

# Battery Warnng 

# IMJEtror Critical 

# Error \l 

# Y ······RedandYelowflatl'l Allemalwty C'..on..,assCalbatiel'l Aeqi.Wed 

# Aetum

to Home (ATH) The Aatlm

to Home (RTH) bc"ngs the ai'crall bac:k to the last reomdedHane 

# Pont Thae ae three cases that willtrggar RTH procedure; tley ,_e Smart RTH. LON 

# Battery RTH a1d Failsafe RTH. 

# m
GPS Home 

# Pont

**~** 

# ... SmartRTH



# - **Desc~O'I** 

# The Home 

# Pont
is the location

at '1\tichyo"

a mall 

# tlkss on whEI'I 

# tle GPS signal

is strong. Yru 

# can -view the GPS signal 

# sbmglh turugtl the GPS icon

( **~.d**



# ). 

# II you are usng the Dynamic: Home Point setli'lg, l1a 

# Hans Pont will 

# be updated

to yeo cuii'EI'It 

# po&iiD1 as you move around and "1\tBl 

# the Ai'aalt 

# Stalls ndcalor **~~** 

# greB'I. 

# Usng the RTH bufton on tle rEmote controls (reler
to tiTH bunon· on P28 br more nbm1alia1)

or the RTH bulbn

n the DJI Pilol app whB1 

# GPS
is available

b Ellablas smart RTH. The amalt **re~**



# b the latest recorded Home Pont. you may control tle ai'cralfs orientation

to 

# 8\IOid collision **~ilg** 

# tle 

# Sma1 RTH

. Prss.s the Smart RTH button once
to start the process, pl'ess the Smart RTH button agan
to mit Smart RTH and reg<Dl the control.



# 13 )> **~·** 

# n 

# ~ 

# 49):> 2 

# '" INSPIRE

1 

### u..., **Manu<~**

I Low Battery RTH T'E bw baftg•y IENslla1isale

rs **l·~•o3d** W'E'l t'le **DJII!11ell~t** Rtgnl Battery

rs deple1ed

b a p:unt tnat may allect t'E salo3 retJn
ol t'E arrcrah. Users a:e a:ivoseo

b return rome
cr land the arrcratt mmediatety 'o\''E'l t'Ese **wa~1ngs** are S'lOW'l DJI P1bt app will aa-.;ose **e~ser**
Ia return the arrcraft

b tle 1-tlme Po!l1 wrE'l b.\• battery war-ll'lg

1s lrg;;areo. Aircraft w1ll aubmabcalty reh.IITI
to the Henle Po111
no act10n

IS ta-<a'l alta•
10 wco·x:s co.J'll'.xJW'l. User ca•• Ga'l::el l'le RT H by pressng cr.ce O'l t!le RTH b-.Jtton. The I'Has'lokls

b• t'les.e '•\'af'll'lo;JS are **ae~tcrnatocalty** deterrnneo basea
cr. the **c.n~t a~~crab**  altrtude arrd rts Clsla'l::e lrorn t'l9 Horne Pont. ,!<,•craft w1ll ia'laa.Jbmabca!ly

1t t'le curre'l! battery i<!wl Gall O'lly **s..~pport** t!le alfcratt

b 13lo

b tne grocnd t•om t•a **c.J~e'lt** aitlt.J.:E. Use• ca'l .JSo3 l'le •€nlote CO'ltroller

to control the arrcratrs cremabon d·.Jnng the la'lC ng pro-::ess. f'E Baftery· level haocator

fS CISOiayeO

n t'E D.JI P1bt app, a'lO ISOeSCTIOOo beth\• 

# j__

b
T 

# cS Batay l.atet Rllll"8fk

Aiaaft 9at.ts ruJPtotw

Flgtt lnstudms 'Walmg

lntil3of

Tap 'G:J-nome·

to have the **a~rcratt rele~m** 

b the

F ty the arrcrab 1-tlme po nt a'ld lana back

a '10 la'ld Low battery
l'le

battery A1rcratt stat.JS

a.Jiornatcatty,

or ·ea...cer

to

rt as soon as lgvelwar'lrlg

poo\12

• IS la.v. l'l:1ocabr t.ln<s resi.ITie

normal t!ght

It no poSSible, tlB'l Plaase la'lC l'le act01rs **la~en.** r.e arrcraft aJrcrah

RED

sb.vty.

will a.lornabcalty

go rnme stop

the motors a'lO 13ld after 10 secrn<is.
a'lO

replace tne A€nlote o:J!11roller
w1ll sound

baftery. an alarm. CrrtiGCIIL.ow

The **a~rcratt** Aircr all status The

DJI Pibt app screen will The aircraft bailey le\Ell musl la'ld

lld icabr bl.l*s tlastl

red a'ld aircratt sla1s to will begirl
to nrnediaE!ty

. RED quck.ty. des::B'ld.

RErnale callrolter descend and land wamng

wilt soUid a'l alarm. autanatically. btrnateo Eslmaleo ra'Tlan 1'1·;; r;rT\31'll'lQ

lig'lt

N/A

N::A

N,IA I g'lllrne t::asea

m c.Jrre'l! banery evel. 14



### 50INSPIRE

1 User Manu

..
! :\j:

• **V\h~'l** 1'18 **·~·;t** battery **~vel** wa"ll'l;J **a·~llvates** a1a l'le atr'-<all

IS aesce'lang

to la'la a.Jtcrnat•:alty.

yo.J -nay c·.JS'l t1e **h•an~** .JI='•''d"C

b 'lcNe' l'le **a~•cralt** <na **'Ev.g<~le**

rt to a more **app•ap·~l2** I:J·:aiKYlla•la•l:J

ng. **•v:J~'J'** .£0'185 a'l·:! 'Tla''\9'5
01 t1e banecy level n-::n:alor •el.act eslrnalac ra'Tlanng hg'lllrna a'l:! a.'e a:!J.JSte::: a.Jicrnalcaity, accoran;;

to t1e atrcralfs c.Jrr8'11 s1ai.JS. Failsafe RTH FaJ!sale RTH

1 s a-..;t•v·ate;:: a.Jb-nal>:ally

;I •ecrrJte o:J'll•aller 5>;;'\31( **~1Cf.x::ng** v.coo relay s.g•al)

tS bsl br **'TJCY~** t1a:1

3 **~=a·r..:s** p•ov>:!ea I'Jal f-b"TE POI'11'tas be8'1 s.Jccessi.JityrecCYa.aa

a-1a oompa5.s 15'•\'=lt'-<.trlg 'EY-nalty·. Rei.J''l ·1crne p·o·:ess ·nay be ne••.Jpe

- :: a1-::: tH! ope•ator c<n re;;an ·:n'll•al over l'le **a~rcralt**

11 a •e-nola GCYll'alle· S>;<"B

I 1s •es.Jme:!. Failsafe Illustration 1 Re=rd Herne Pont(HP)

2 Con1.rrn Herne Pont

3 Aemole Callroller Sognal l..osl 

# ..,..

)l.,u!l



# ..,.. **~**



# ~ '"'



# .. **~** :3rll-iJtY.; Git::tt:n

**3uf.t~n·:;** &e.oc5"1

**r~~~**

9

: ri<.:rK.J **V~ltl'AI** 4 Stgla!LLS Lasts 3!Bcs.

5 Go K:Jme{Xlm
can be set)

6 Land11g aller Hover11g 15secs **--- -~-.-**  **=JII"** 

## ~ .... -··

· --

- - -


# ~ **~**

I



# ..,..

.. r



# .. ' 

## y 

# ~



# .. .;r.: !)ir LkrY.;

'r ("I ·.
· .A

**r.::e~ Smt~.n** 
**'I'~** 

### u.,

**f.:t~~ rfot.!rr;**  'Ve ll'A 

### Lt,

• . **.!11··~·an** a.Jicrnatcalty· cesce·1:::s a·1::: la'l:::s

;I RTH
1s tr•;;ge•ea 'o\"leri t1a a1rcralt hes Wllnn

a Xl •nele• (65 !eel) •aa1.JS oll'le 1-t.Jne Pont. • AJ•.:;•an -:a'l''YJI avm::: absl'.x::ID'l ·:J.J'I'l;J he Fa1fsala RTH. I'Erelore

1! IS mporta'll

b set a.'1 '8aYJ'lable Fatisale albt.J:::e bei:J•e ea::'l

I >;<'11 l.aJtc'l t•1e DJI P1lol app a.'lC e•1ter 'Caona•a' vew a-1::: see-:;1 **1.~-:..JDE'Ia** sell'le **Fa~tsale**

aii

i i.JOO

. •

. .!\,•.:;•an w1t: stop as-::e·t:::n;; a'l::: **rTTneaLater~· •eu~11o** 
he Ho"TE Pon

1! yo.J move t1e l'lfollle sic<:

1! t1e al'·:;·all ·ea::'les
20 -n a

l biJ:::es

cr bey>:n:::

a ..l'ng Fa1fsale. Dynamic Home 

### Potnt Dy•am1·:: '1a'TE **~VJI'11**

1s .Js.a!.JI

1'1 stl.Jallcrts W'le'l yo.J are
r1 ·noto•1 a1a **'i?::.Jt~e**

a Hacoo Ponl I"Bl
IS a;Here'lll•om

l'la ta<:ooll p-JI'll. GPS ·no:::.Jie

1s tl·::ate::: all'le **~':lslb0'1** s'l•:J'•\"1

,., 1·1-:

I ;;.r-: bebw: 

### Lt, E·1s.J•e l'1e space above l'le GPS

. -no

- ::.J

i e

1 5 'lot abst'

.J

· :I2::: W'E'1 ..r.;n;; **D~{'la-nc** 1-t.Tne Pont.

15 )> ;:; o;


### 51)> 

### ,. . 0 iii INSPIRE

1 

### u...,. Manual Tha-e are two opticJ'ls tar Dynamic Hane Pot!

I. 1. Set the ate raft cunenl coordinate

as the new Heme Point. 2. Set the rEmote **ca-~taller"s** oocrdinale

as tle new Home Point. Setm1g l.IJ! Dyranic Home Pon Folbw tha steps bebwto se'-!p Dynamic Heme Point

: 1. Coonect

b the rrobile device and laiSich tle DJI Pilot app a1d gob tle ·eanua· page. 2. Tap ..

. a1d setect"gf.

b reset the rEmote oontrolla'

's coordi'lates

as the new Hane Pcint. 3. Tap'9

· a1d setect4.•

· . b resettle ;Wcr.lft

' s coordinates

as the new Home F'onl 4. Tha awcraft slak.ls indicatcr blnks green
to show Home Point issei suocessi\JIV. Vision Positioning System DJI Vis10n PosilicJ'lng

is a posilicJ'lng syslem that uses IJ!rascmic and mage data

b help the ai'aalt tdelllity
its cunent pos1llon. With the help
at VisicJ'l Positioning, yoor InSpire

1 can hCM!r

in place rmre precisely a1d fly ndocrs
or n other envirooments 'AtlS"e thS"e

is no GPS signal available. The main oomponents

of OJI Vision Posilcning
ae bcated on tle botbm
at yoor Inspire

1. nckmlg

[1 )lwo SO'Ia senscrs a1d[2}one mooocular camera. 

# ~ --------' I..IYlg Viisicrl P05iliomg **Visia-~** Posdcnng

is activated automaticaDy when tle Inspire

1 is powered
a1. No manual actioo

is required. VISIOn Posilionng

is typiCally used
in the indoor environment 'AtlS"e
no GPS
is available.

By usng the sensors
a1 the Vision PosdicJ'lng S}6tem. Inspire

1 can pa1am precisicJ'l hOIIa'llg even when no GPS
is available.



# -

/ 

# "! 

# y **~** 

# v **~** 

# ~ 16



### 52INSPIRE

1 User Ma ... al Follow the steps below
to usa VISion Posi!i:mi1g

: 1. Toggle lle swdch

b -p· as shown the l91e

b lle right 2. Pla::e the Inspire

1 rn a llal surlace. Notioa flat lle Visicrl Positilnilg sysiB'Tl camot work properly

rn surlaces without pal IBm variations. 3. Power rn lle rnpi'e

1 . The ai"crall slaus ildicabr
win llash t.Yice

i1 green ligtll. which ildicatas
the VisicJl PoslicJlilg systB'Tl

is **rea~.** Gent¥ pu!h l1e tuotlle up b lift on. a"ld lle lnspl"e

1 win h:rwr

n pla::e.



# a & The perlamanoe

ol ywr nspire

1

' s Visicrl PosdicJlilg System

is subject

to lle su1ace yw **~** llyng 0\19"

. The

u ""asrnic waws may not be able

b acaJralely measure
the dislaloe aver !DU1d al::lsabtlg materials. and the camera may notllnction carecly

i1 &bopti'nal enllironments

. The ai'cralt will switch rom ·p· rrode
to "A" rrode aJicrllaticaUy **~both** GPS end Vision Posilionilg SystB'Tl are rot available.

So operata the ai'cralt cautic11slywhen

n **a~yollle** blowi'lg siklalicJls

: • Ayng <M!rmrnocl'l'crlle su1aces(e.g

. pure black. pU"ewhile, flt'e red. pure grem). • Ayilg aver

a highly rellective sulaoes

. • Ayilg

at high speeds(011er8nVs

at2 meters
or 011er .-n,ls
at 1 meter). • Ayilg 011erwater

or **"ansp~nt** su1aces. • Ayilg 011ermovilg su1acesorobjects. • Ayng

11 an area where lle lighlilg changes **l~entlyor** drasicaDy. • Ayng <M!rex1fB'Tlely
dark (lux
< 10) a bright (lull
> 10.000) surlaces. • Ayng 011er surlaces that can absorb soU1d waves(e.g

. thick carpel)

. • Ayng 011er surlaces wdhoul clear patlerns

a tex1ure. • Ayilg aver surlaces with identical repealilg pal'smsor IB.dlres(e

. g

. tiles with same deSign)

. • Ayilg 011er nclned surlaces that wiD dellec:t SOJnd waves **a~** Iran the ai'crall

. 

### • n the e\la"ll

at loss ot remote crnroller

' s Signal. the ai'crall will ho\19" Ia 8 S&C<Jlds and 11&1 auto-land

d it IS 11 -p· rrode. **~**

• Keep lle sensors clean at aU tmes. Dir1
a other debris may adversely al\!ct the ellectiwness at lle S&lsas. • The elleclive ho\la"ng altdudesol

the ai'crall

is Iran


### o b 2.5 meters. • VisicJl Posdmng systB'Tl may rot IU1cti:m properlywhm

lle airaalt

is **~g** aver water. • VISm Posdianng systB'Tl may not be able to recognize paltan on the gi'OU'Id

i1 low light oond itions (less than 100lull). • Do not use ollEI' u""asonic devices with

.. equmcy

at «l KHz whm Visicrl Posilicrlilg sysiBm

is n operaticJl. • VesicJl Posdianilg systB'Tl may rot be able
to stabilize the ai'cralt when lyilg dase
to the groU1d {below

0

. 5 meters)

i1 last speed. 

### 0 Keep the anrnals <may tram the ai'cralt wh&l Vision PosdicJlilg sysiBm

is activated. The sonar sensor BTl its high

.. equmcy SOJnd that
is rnly audible

to Scrlle **a~imals.** Fligh

t Recorde

r Rtghl data

is aJbmaticaHy staed

n lle niB mal storage device

at the ai'crall. User **ca~** gail access

b llesa data llrough lle OJI Pilot app. This ncludes !light du'atian, aiB'Italian, dislalce, ai"cral1 stalus ntamatian

. speed. and other J)<'WalleiEI'S. Attaching and Detac

hi ng 

### the Propellers Use only OJI approved propellers with ywr n5JWe

1. The grey or black rut on the propeler indicates lle rotation direcb::m

at the propeller and where

d shoukl be attached.

To attach the propei!En. properly.
17 )> 

## "'' n 

### ~ 

### 53

# 1> 

# c: **~** 

# IN S.PIRE

1 **u~r M"nu~l**  **'To<~l·:::.'l** 

# t1e ·ut w•t11'1il -::ots '.l'll'E -n:JtJ•s



# ol yoJ• hspo•e

1: 

# Plopaks



# GAl¥ cap(1345)



# Ella cap(1345R) **~~:f.Jre**



# c=:

• • ==:::t. 

# Allae'l 

# On lolbi::Hs

..... **~nout**



# a 

# blacK dol 

# Mobrs **w~h**



# a bladl dol L-e-;;;e·1cs



# f':)~ LOG<.:

T J .. ll'lil 

# IYO~-ail3•s

1'1 tlil 

# I'IGK;a!~ :JI'eclo:J'l

tJ 'llOU'll il.'lG bg'll9'1 

# 'b, U"lrJG<.:

T J"l t1e vopel>ars

n l'E n:::.:;ate:::: co•e::bo'llo looseo1 a'l·:: 'ifilOIIe 

# Atta<:hing
1he Propellers 1. /J.ilaG'l t1e p•o **~oel>a**


# •s w1t1



# a ;;•ey

'1 Jl o·110



# a •nolO' **w~'IOJ!**



# a bla-::;<. ·:JOI a'l-::: spn l'le p•o P3lle•s-::; bc<.wose lo sa:::.J•e l'e-n

,., Pia·:::e

.. 411a.::;·, tle c··opele·s w·l'l-3 bla·:::.< 'lJI O'llo

**<~** 

# CTDD' wotl

a blac< .;::o! 

# a"l·:l spn I'Ie **p·o~:--oei'='s** 

# -:;oJ'lle• 

# -::b:;<'•'''se

Ia secJ•e

1ls pos1IKT!.
Be sJ'.;! lo o:vnpBiety **llg~e'l** 

# eaC'l propeller



# by 'la'l:J coelo·:



# I >g'IL



# ~ 

# ~~"~ **~** 

# ~

**~** 

# 6

• E.·1sJ•e p•opel!3·sa.'eanac·l9:l



# I::J 

# •Is o:Y'espo•1::n;; 

# rmi:Ys. otle"o\'15'3

t1e 

# a•'·:::"allca'TY.llla"il

oK. • Ha-1-::in;;
I'E [;.oope!e·s w1t1 -:::.a·e. • **Ma'lJal~·** 

# 1>;1113'1 sa::;•JrJf I'E P'OI=o3ii:!•s

0'1 tE .:;owesp::n-::n;; 'TIJIO"S

I:J 

# e'l!U'e

11 LS aftdCEG lrmlf. 

# Detaching
the Propellers Hoi:: I'E moi•:Y slili. T'E'l SPI'li'E o·oc·e!e•

n t1e J'lrJc< -.;::o•eclo:J'l nc•:;ae..;:: O'li'E oroc--aler rls.ell. 

# Detaching 1345s Quick-Release Propellers Press l'le 13·15s **OJ.:::.<.-Relea~.e** 

# p•ocoelle•s -::ow'lwa·:: 11-:-nty l'le'l ·otae t'le propelle·

n l'le J'lloC< :::i'9:;l>:J'll0 J..,O:JG< tlil D'O[);!i8•s. 

# ,&

• Co:.:=< I"BII>: **p·~-ale•sa"Y..:** 

# 'TYJI•:Ys a•e nslaie:: **•:Y-J~eclty** 

# a"l·:J

I •mty l--aiCYe iNery

t **g~.** 

# • E.·1sJ'e t1a1 all **o·o~-oella·s**


# a'e

n -;;oo:: W'l:Jrlcn oola<e ea:::.'l

I >;<'11. 

# D:J NOT Js.tl 

# ole. **c'lopp~.** 

# CY t•'O<(·:n prope IIB"S. 

# • Toa·...-Jc rlJJCf. STAND **CLE..~**



# ol a•:: D8 N'JT bJ(.."'l p-opele•sO"rrol:xsw•il'l



# hey are spoTII'lg. 

# • 0 N L 

# Y Jse •:Y>;; na: 

# ru

I L."O **~oeie** 

# ·s 

# 1::1 • a t:-all"' a.-:: sale·

I •;; '11 ex per >3"1ce. 

# OJI lntelfiQent Flight 

# Battery he DJI t·Jta:h;,;e-11 Fit;J'll Balle•y 'IdS

a G<!DaGI!y

•JI **·~50(}nkl.** 

# volla;;e

of 

# 222\i, a•HJ smartG'l<Hge**Ct~'la.'·;;e** 

# tJ.:::.IYJ'Ia!rly

II ·:::.a·1 o·1ty· coe **.:;·~a•-;;e-::**



# w rtl a·1 app•op'8le



# DJI apprCNec C'l<l.'ger. 

# /IC§J] **o~~**



# I 18



# 54

## INSPIRE

1 Useo Manual 

# & Ballery

m JSI be lulty cnargea belore LISITlg



## rt br the hrst

1 me. Reier

to "Ct!arg ng tle lnte lhgent Flg'll Battery· P21 b• more nbrmaiiCTI. 

## DJIInte

Oi gert Fight 

# Battery Functions 1. Battery Level D•spiay·: LEDsmsplay

tle ·::..arrent battery le\Ell. 

## 2. Battery Lila DISplay: L£Dsa1Splay

tle currant battery po'o\'EHcycle. 3. A..rto-diS(.-,arg

1rtg F..a'l:b:J'l: T'le baltery· **ac~tomabcaJI)'·** 

## diSCharges

b beO.V 65% ollotal PJWar

· M191

rt 1s die

( _ press tna po'o\'91 bullm

b C'lec<. ballery level will causa battery

b ax.rt Idle slate) tor more **tl<r~** 

## 10 O<l}o·s
to prav·e'll swgllng.lll.;t.;esaro..and

2 

## oays lodiSGtlarge

the battery

to 65%.llisnormal

b leal macerate 'leal emrtb!lg tram Ina battery a..arng Ina discharge process. DISd1age thresholds can be set
n l'le OJI Pilot app. 

## -1. Bala!lcec Cnargng:

A

· ..rtomabcally bal<noes t'le voltage

at eadl ball3rycellwhen dlargng. 5

. Over C!large ProeciiCTI

: Chargnga>JtomaiiCalty

sbps wtlen the ball3ry

IS 

## lultycharged. G. **Temperale~•e** 

## Detecb:J•J: T!lB battery Will 

## only C'lage wnan 1!18 temperat.Jre

IS 

## belwe81

0 <C{320f) 31d -IO'C

( **104~F).** 

## 7. Over C..Jl'r9'11 Pratecb:Jn: Battery sbpscnargng
"o\'hen hgh crnperage {more than 10A) 1Sdel3cted. 8. Over DISUlarge Protecbon: DISC'largLrtg a.Jbmabcally sbps when the baltery 

## vonage reaches 1SV

b prerverll crver-diSC...argg aamagg 9

. Short Cl'c.JII Protecb:J'l

: A.Jbmalo;;allyc..rts

tle power supply w'le'l

a 

# s..,ort CII'O.Jrt

IS 

## dlelec::led. 10. Balterry Cell Damages Proteclr.TI:
DJI Pilot app s.nows warmng message 'M191 

## dcrnaged battery oall IS 

## ootectea. 11. Balery hbrmab:J'l H1stcry: S'low I'E last32 mines

at batl!lfy nbrmab:J'l reoords thalnclude wanng rnessage

s a !10 

## so 

## on. 12. Seep '-'boa: Sleep mode

IS 

## 3!113red al13

r 10 mn..al3s

at nac::IIVrty

b save power. 13. CorTTTl.J'liCabCYl: Batery

· vonage, capacrty

, c..arrem. 31d other relev311 ntormab:Jn

IS 

## prcrvlded

to the alfcratrs

to l'lB man oo-llroller. 

# &_ Reier
to 

## Dosclillmer ana 

## lnlelo'ogent **R~ghl** 

## Ba:ery Safe.y Guide,\ns bebre usa. Users lake lull res.pons1blirty

lor all aperab:J'lS a'lo cJSage. 

## Using 

# be 

# Batte!Y Powa-ing ON/OFF FbwetllQ 

# On: Press tle Power BLIIbn O'l:e. tnen press **agar~** 

## and 

## hole lor 2 saoonds

b power on. The Po.\er LED wrl\ t.J..-. reaa'lO 1'13 Baltery Levell'ld!:3orswrll drsplay tle clSfenl batl3ry level. Fbwer11g 

## Oft Pres.s l'la Po·,\'Br B..allo'l moe, l'lB'l pressagan
31d 'Pid 

## lor 2 sec::rnds

to power ott



## 19 )'> 

# c; a; 

# 55):> 

# c; 

# a; 

# = INSPIRE

1 Uoer Manual 

## Low 

# TerJ1)81ature **~e:** 

## 1. The perlormance

ol lhe l'llelhgenl Flghl Ballery

1s sgmlicanlly reduced when llyng

1n a low lemperalure e'lVIfonments {!hose .,...rt'l **a~r** 

## lemperalures below 5<-C). Ensure flalli1e ballery

IS 

## lully chargee and Ina cell voltage 1Sal4.35

V 

## be1ore eadl light. 2. Us1'1g lne l'liellgenl Fhgnl Ballery

1'1 exlremely
low lemperall.ll'e env1ronme111s {!hose wrth **a~r** 

## lemperall.l!es beiCM' -11YCi

IS nol rec:ommenOed. When ftyng

n WJVIfCJI'lmenls
Wlfl la'llperalures belween 5'C and ·10'C.

I he hlslhgenl Fhghl Ballsry sh:Juld be able Ia achieve lhe appropnale

.. ullage le.rels{above

4.2 

## V). but

rt 1s reoommB'ldeo

I hal you apply Ina nc:ludeo nsulallon siiCXer

b tie battery 1'1 order
Ia preVWJI

a rapKl orop

n lemperahnes. 3.

II l'le DJI P1lol app diSplays
Ina ·crrtcal Low Battery Level Warmng· when liyng

n low IErnperalure e'1VHCJI'lme'lls.
slop liyng <11d 13lc !he arrcrah **nrnoo~alsly.**


## Yru w1ll sbll be able Ia oonrol fle aircrall's m011eme!rt w•E'llhiS wam1!1g

IS 

## lroggared. 4. Sbre fle **hlellge~** 

## Fhghl Banary

n a room lemperalure B'1VII'Oflmenl
and €flsure !hal rts lsmperaure exceeds5'C belore LISI'lg



# rt n tne lcM•to;nJperalure B'lVIItTime!ll

. 5. Wne'l usng fle hsprre

1 n a bw lemperal.ne **env~ranmenl.** 

## begn by allan·ng lhe arrcraft

b rover at a la.v **albL~:Je,**


## lcr approxmalely

**cr~e** 

## mncJte.

b heat lhe ballery. 6. To e'lSure oplmiiTl perlorma"JCe. O<.eep lhe lniE!Ihgenl RIQhl BaiiE!ry's core IE!mperalure above 20"C W'l8'1



## n Jse. **~**



## 1'1 cole **e'liii!CJI'lma:-~ts.**


## nSE!f! 1'18 ballery rnlo

I he ballery canpartmem

a1d alicM' 

## the arcralt

Ia warm uplorapproxmaiE!Iy

1-2 mnutes be1ore ta<.ngoll. 

## Chedting 

# the battery 

# level The Ball81'lf Level lndcalors oiSplay how muc'l remanng power the battery has. When the battery

IS PD"It!rec
all. press tne Powlt!r Button once. Tile Ballery Level ndcatcrs willlgtrl


## up to diSplay lhe cunen1 ballery level. See below lor Oela1is. 

# (I] T'le Ballery Level l'ldcalors
Will also show tile current ballery level dunng charg111g and diSCharg 

## ng. T'le nccabrs are del

c 'leo below

. 

# c:;t LED ISon.

**LED** 

## ISI.asnng

. 

## <{

· LED ISO H.

• •. 

## Batayl.swl 

# LED1 LED2 L8)3 LED4

Batmcy 1..8\'11!1 

# c(

c(

c(

c( 87.5%-100% 

# ... c(

c(

c(


# ~ 75%-87.5% 

## -=(



# ..(

-=(



# <C 62.5%-75% 

## -=(

-=(


# ~



# < 50%-62.5% 

## -=(

-=(

<(



# <C 37.5%-50% 

# c(



# ~-

c(



# < 25%-37.5% 

## -=(



# <

<

< 12.5%-25% 

# ... **~**

c(

c(



# c( 0%-12.5% 

# <(

-=(



# <(

-=(

=0% 

# 20



# 56

## INSPIRE

1 **U~e<** 

## Manual 

# BatBryUB f'le ballsry
hie &'locales 'lCh\' ma'lY rro•e

I mas 1'19 ballery ca'l be d&scnargad and rechargea bebre 11 m.Jsl be repocec. **W'19:-~** 

## l'le bati!Yy

IS p:Jwe•ed
oH. pres.s a'lO 'Uia the Po'o'I'E!r B...tbn
lor 5 seccr1ds b G"E·:;<. he batte•y l•le. f'le Battery L.well'lacabrs ·.v&lll&ght
.Jp **ar~ri,br** 

## blrit as descnbed below tor 

# 2 secooas: 

# BalteryUfB 

# LED1 LE02 LE03 

# LED4 Bafyl.lle <(

<(

<(

<( 9:J%-100% 

# ·'· <(

<(

<(


# ~ 80%-90% 

# <(

<(

<(

<( 70%-80% 

## ~

**~**


# ~

<(

60%-70% 

# <(

<(

<(

<( 50%-60% 

# <(


# ~

<(



# < 40%-50% 

# <(



# <

<

< 30%-40% 

# ~

<(

<(

<( 20%-30% 

# . <(



# <

<

<

beO.v 20% 

# -

- 

# -- & W'le'l baiiE!ry·


## lila •eaG'les 0%.

rt **.:;<r~ :-~a**  

## k:J'lg6r be .J!!BO. 

# QJ FO" rrr.Ye rllormatoo abo.JI 

## l'le ballsry. **la..n:;:-~** 

## DJI P•lol app a'lO ens 

## eX he nbrmat&crl under tlB 

## balls
ry· lei 

## b. 

# Olargilg the lnteligent Fight 

# Batte!Y 1. Ca'necl Balle')' C1arga•

b a power SO.Jrce {100-240V 5(ll00Hz). 

## 2. 0pe'll'le Protac1o'l Cap a'lo GCT1'19CII'19 **1:--~IBII&ge'll**



## F hgnt Batlsry

Ia tie Battery Dlarger.

H tle ballsry **B~.·ei&S** 

## ab:Ne 95%. t.Jf'l 

## o'li"E battery betcre cnarg ng. 3. f'le Batle•y Level hccata•·.-.·•11

a •splay l'le c.J•r;nt baftery level **oc.~rng** 

## chargng. 4. f'le **ICJ!ell>g~l**


## Rg '11 Battery

•s t.Jity G'largec wnen Battery **Leveii~·HiK;abrs**



## are all 

## all. 5 .. Alr cool tle l·1telhge'll Fltgrll Baftery atlsr eac1 

## tigm. Allow
rts lsmpsratHe

Ia drop

b room IErnperaliJ'e belore sbn'lg

11 b• a'l 

## sxtenoec psroo. 

# &

• D'.J '101 C'large t1e l'llellogo;nl Flg'll Bailer!' a'lO •Ernale con !roller w&ln slclndara chargar{model: A 14-100P1A)all'19
same lrne, ol'ler,\'158
l'le charger may ave meal. • At.-.·a·;o:. ur.1 

## oft 1'19 balla'Y before nse<lrlg

11 or rErnovng

11 tram tle l!lSp"e

1. Never nsert or rinJOV9



## a balle!y W'l9'1

II IS 

## p:JWiHeO 0'1. 

# ~~beoc~ **~**

B

21
):> 

# 0 

# iii 

# 57

## l:> 

# ;:; 

# '" = INSPIRE

1 U.er Manual 

## Batey Lewl lndcatlm 

## whle **Ch•~** 

## LED1



# I LE02



# I LED3 LED4 

## <(



# Bana.y l..8wl 0%-25% •'• 

# <- 

# . ..

4 

# ~-


# ~ 

# ~

...

**~** 

# . . . **~-**


# ~ <t

<t



# < <t ·'· 

# ~ 

# ·'· **~** t<(



# < <t **~-** <( 25%-&1% 50%-75% 75%-100% FultyO.arged 

# Chargilg Protection 

# LED Display T'la !able be b.\• 

## shan-s baDary pralecbrn mec!'lamsmsana corrasponcing

LED paOems. 

## Battay l.swllndicatlm


## whle **Ch•~** 

# LED1 LED2 L.EOO 

# LED4 **Blri~Palem**



# I Baw.y 

# Plotadon 

# ,tam ·'· <(
**~-**


# <t <t LE.D2 **bl~s** 

### to\'108 

## per seccrJd Over current aelecled 

# -< **~** <( 

# <t LED2 bli1ks ttTee tmes per second Shat 

## cirwrt deEded 

# <C


# < **~**


# < LE.D3 **bl~s** 

### M'108 

## par secood Overcharge detected 

# < <( 

# ~


# "" LED3 blrlksltTee times perseCXJnd Over-voltage **cha~** 

## delecEd 

# <

I 

# <t

I 

# <t 

# ~

L E.D4 **bl~s**


## II\' 108 

## per seccrJd

Chargng tenpera1u-e

IS 

## too 

## bN { <O"C) 

# ·'· LED4 blrlks ltTee limes per second 

# Cha~ IErnpa-alue



## is 

## 100 hgtl 

# <t

I <(



# I <( 

# I~

{:>4

) 

## Aller any 

## a1

I 

## he atx:r.e me'lb<TJed 

## protect01 lSS;Jes are resolved, press tna bullon

b tum on the Ballery Lllvel natcator. lhpi.Jg 1'19 

## lmelltgem Fltg.'lt Battery tram tne charger **ar~d** 

## plug

tt back n b resume c'largLng. t'¥Jia 

## l'lal yo..t 

## do 'l:ll 'laaa


## Ia **..~npiJg ar~d**  

## pl..tg the charger

111 

## tle event
of a roam lemperaure error, 1'19 

## Clarger wtll resJne Clargng wnen tle lemperallre
falls wttln the 

# nama! range. 

# _& DJI does not tai<.e any resp:l'lstbthly

lor damage caused
by th"ci-party chargers. 

# :CJ 1-bw tl 

# <isctlaoge your lntellgent 

# Aigtll Batmry: 

# 22 To enectrvety calibrate
tne ballery capacrty,

rt IS 

## recorrrnenaed

b charge and diSCharge
tle baDery l'lora.Jghty-

lor <Nery 10 charge-aJci-diSCharge

c}Cie. 

## User shO.Jid nstall the battery crJb t'l9 arrcrah 

# ana 1'18'1 

## p::rNer 

# rn Ple am;ralllo lfltbaiB lhe diSCharge process, discharge
tle ballery ;J:lltl tle aJICrah

OS 

## powerea

on a.Jiamatcally.


## User !l'IOUid !hen fully charge lhe battery

IO SlSUI'e 1'19 

## ballery

IS

' o\'<l!".lflg

a1 rts opt mal Stow: Place Ple lmelhganl Rght Battery nto the lnsplfe

1

· s Banery Compartment
and 

## pov.'et'



# rt oo Leave

1t on umtllnare

IS 

## less l!1an5%

at panoer lett. or urdli the baDery can m !alger be l..tr'l9CO'l. 

## laJlcn lhe 

## DJI Ptlal app

b check baDery level. 

# Rapd: Ry lne **l~pwe**



## 1 O.Jtdoors urrttl there

IS 

## less than 5% at panoer **lei~** 

## or <Jlbl tle ba1Ery **c~** 'l:l 

# rnger be lurnea
<Tl

.



# 58

# p) 

# !!!.

**~** 

# ]J :-) 

# -. J 

# D. D 

# - D. 

# w :::r (/) 

# (t) rp



# ~ ;::;- r. 

# 3 p) 

# -. :::r rp p) 

# (i) ::l 

# 3 D. "0 

# 0 :::l 

# 0 

# Cii 

# Q 

# ro Cii -.

**~** 

# m 3 [j 

# D. 

# (t)
r. 0 0 

# m 0 

# iii :::l lfl 

# n

**~** n C)



# ~ C3 -. 

# 0 Q 

# ro IT



# ~



# ~ 

# m 

# :::J -. (/1 

# §

**~** -::r 

# -

**~**



# ~ 

# -::r 

# .., D. () 

# rp 

# 0 rp "0 

# Ci) ro :::l



# ~- n p)

N 

# c c 

# (t) () 

# D. 

# -. 

# .., :-) 

# ro rp ll) 

# V1 V1 

# en ""

(J1 

# co