Kelly Manufacturing RCA 2610-2 P Original operating instructions

KELLY MANUFACTURING COMPANY
555 SOUTH TOPEKA
WICHITA, KS 67202
[phone]
FAX [phone]
KELLYMFG.COM
RCA 2610-3
P/N 102-0403-03-01
P/N 102-0403-05-02
RCA 2610-2
P/N 102-0403-03-01
P/N 102-0405-05-02
Rev CDecember 10, 2018
KELLY MANUFACTURING COMPANY
KMC
KMC PUBLICATION NO. 1401-3
With Pitch Sync
Without Pitch Sync
RCA 2610-3-G
P/N 102-0403-03-03
P/N 102-0403-05-04
RCA 2610-2-G
P/N 102-0402-03-03
P/N 102-0402-05-04
RCA2610 SERIES
ELECTRIC DIGITAL HORIZON
INSTALLATION/OPERATION GUIDE
10
10
20
20
30
DIM
PITCH SYNC
DIM
10
10
20
20
30
10
10
20
20
30
DIM
10
10
20
20
30
DIM

RCA2610 Series Installation/Operation Guide
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KELLY MANUFACTURING COMPANY
KMC
KMC Publication No.1401-3
TABLE OF CONTENTS
PAGE
SECTION 1 INSTRUMENT DESCRIPTION 2
1.1 General Description ........................................................... 2
1.2 Physical Description ........................................................... 2
1.3 Display Features ................................................................ 5
 1.4 OptionsandCongurations................................................ 5
SECTION 2 INSTALLATION 6
2.1 General Information ........................................................... 6
2.2 Handling ............................................................................. 6
2.3 Pre-Installation Inspection .................................................. 6
2.4 Installation .......................................................................... 6
SECTION 3 OPERATION 7
3.1 Pre-Flight Procedures......................................................... 7
3.2 In-Flight Procedures - Pitch Sync....................................... 7
3.3 In-Flight Procedures - Dimmer ........................................... 8
3.4 Flight Limitations ................................................................ 8
3.5 Emergency Procedures...................................................... 8
SECTION 4 GENERAL INFORMATION 9
4.1 Flight Testing and Adjustments........................................... 9
4.2 Instrument Care.................................................................. 9
4.3 Optional Slip Indicator ........................................................ 9
4.4 Frequently Asked Questions (FAQs)................................. 10
APPENDIX A DO-160G ENVIRONMENTAL QUALIFICATION FORM 11
LIST OF ILLUSTRATIONS
Figure 1.1, General Dimensions................................................... 3
Figure 1.2, General dimensions (-G Models) ............................... 4
Figure 1.2, Typical Display Features ............................................ 5
Figure 3.1, Pitch Sync Controls.................................................... 7
Figure 3.2, Dimmer Controls ........................................................ 8
Figure 4.1, Inclinometer Installation ............................................. 9
LIST OF TABLES
Table 1.1, Leading Particulars...................................................... 2
 Table1.2,OptionsandCongurations ......................................... 5
REVISION DETAIL
REVISION DATE DETAIL
A03-07-2017 Initial Release.
B11-01-2017 Corrections made to Table 1.1 Leading Particulars.
C12-10-2018 Update software and part number changes. Add Flight Testing Section 4.1.

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KELLY MANUFACTURING COMPANY
KMC
KMC Publication No.1401-3
SECTION 1: INSTRUMENT DESCRIPTION
1.1 GENERAL DESCRIPTION
Anattitudeindicator,alsoknownasagyrohorizonorarticialhorizon,isaninstrumentusedinanaircrafttoinformthepilotofthe
orientation of the airplane relative to the earth. It indicates pitch (fore and aft tilt) and bank (side to side tilt), and is a primary instru-
mentforightininstrumentmeteorologicalconditions.Attitudeindicatorsalsohavesignicantapplicationsundervisualightrules.
The RCA2610 Digital Electronic Attitude Indicator receives digital information from a series of accelerometers which is processed
to actuate a display that has two dimensions of freedom, simultaneously displaying pitch and bank. The display is colored to
indicate the horizon as the division between the two colored segments (blue for sky and brown for ground), and is intended to be
intuitive to use.
Because the RCA2610 has no mechanical gyroscope, it is much more stable than traditional horizons. The unit is designed to
work in 360 degrees of pitch and roll and, unlike a mechanical unit, the RCA2610 can tolerate angles in pitch and roll that would
cause a gyroscopic unit to tumble.
On the attitude indicator you will see two yellow horizontal lines with a dot between them. The horizontal lines represent the wings
and the dot represents the nose of the aircraft. If the symbolic airplane dot is above the horizon line (more blue background) - the
aircraft is nose up. If the symbolic airplane dot is below the horizon line (more brown background) - the aircraft is nose down.
Whenthedotandwingsareonthehorizonline,youareinlevelight.Ifthelinesrepresentingthewingsrolltotheleftortheright,
the aircraft is probably starting a turn. The actual bank angle is calibrated around the circumference of the instrument dial. The
pitch angle is indicated by a series of calibration lines, each representing 5° or 10° of pitch.
1.2 PHYSICAL DESCRIPTION
There are two basic models, the RCA2610 which has Pitch Sync and the RCA2610-G (G for general use) which does not have
Pitch Sync. The Pitch Sync feature allows the pilot to adjust the symbolic airplane to match the horizon during pitch up or pitch
downlevelight.Bothversionscomeinstandard3inchand2inchsizes.Refertotable1.1belowforleadingparticulars.
OPERATING VOLTAGE.......................................................................................................................................... 9 to 32VDC
STARTING CURRENT............................................................................................................ 9VDC: 0.18 to 0.22 AMPs MAX
RUNNING CURRENT ...................................................................................... (14VDC SYSTEM) ..................0.20 AMP MAX
(28VDC SYSTEM) ..................0.15 AMP MAX
CIRCUIT BREAKER SIZE............................................................................................................................................... 2 AMP
SETTLING ERROR........................................................................................................... 1º MAXIMUM IN ROLL AND PITCH
OPERATING TEMPERATURE RANGE.............................................................................................................-20º TO +55º C
MATING CONNECTOR ........................................................................................................MS3116E8-4S OR EQUIVALENT
WEIGHT ........................................................................................................... RCA2610-3 ......................................... 6.75 oz
RCA2610-2 ......................................... 4.75 oz
DIMENSIONS/PANEL CUTOUT .....................................................................................................SEE FIGURES 1.1 and 1.2
EYE VIEWING ANGLE ENVELOPE ....................................................................Horizontal Left and Right: 35°Left, 35°Right
Vertical Up and Down: 35°Up, 35°Down
Minimum distance from display surface: 6 inches
Maximum distance from display surface: 48 inches
SOFTWARE VERSION..............................................................................................................Version 2.0.6 and 2.0.7 (NVG)
FAA SPECIFICATION CONFORMANCE..........................................TSO-C4c, TSO-C113a, DO-160G and DO-178B Level C
MEETS OR EXCEEDS ..........................................................................................................................AS8034B and AS396B
TABLE 1.1, LEADING PARTICULARS

RCA2610 Series Installation/Operation Guide
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KMC
KMC Publication No.1401-3
Figure 1.1, General Dimensions
3.17
1.237
(TYP)
2.474
(TYP)
0.08 1.22 0.40
3.37
3.37
A
BC
D
0.928
(TYP) 1.855
(TYP)
2.28
2.40
2.75 0.12 1.22 0.40
A
BC
D
Ø 0.170 THRU
(4 PLACES)
Ø 0.170 THRU
(4 PLACES)
DIM
10
10
20
20
30
10
10
20
20
30
10
10
20
20
30
10
10
20
20
30
NOTE
•
All dimensions in inches.
•
Mounting Hardware (both units)
6-32 screw - 0.5” plus panel thickness
•
Mating Connector (both units)
MS3116E8-4S or equivalent.
PANEL CUTOUT
REAR MOUNTING
PANEL CUTOUT
REAR MOUNTING
RCA2610-3
RCA2610-2
A
B
D
C
GROUND
9-32 VDC
SPARE
SPARE
A
B
D
C
GROUND
9-32 VDC
SPARE
SPARE
DIM
PITCH SYNC
DIM
PITCH SYNC
DIM

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KELLY MANUFACTURING COMPANY
KMC
KMC Publication No.1401-3
Figure 1.2, General Dimensions (-G Models)
A
BC
D
3.17
1.237
(TYP)
2.474
(TYP)
3.37
3.37
0.928
(TYP) 1.855
(TYP)
2.28
2.40
2.75
A
BC
D
Ø 0.170 THRU
(4 PLACES)
Ø 0.170 THRU
(4 PLACES)
DIM
0.08 1.22 0.40
0.12 1.22 0.40
10
10
20
20
30
10
10
20
20
30
DIM
DIM
10
10
20
20
30
DIM
10
10
20
20
30
NOTE
•
All dimensions in inches.
•
Mounting Hardware (both units)
6-32 screw - 0.5” plus panel thickness
•
Mating Connector (both units)
MS3116E8-4S or equivalent.
PANEL CUTOUT
REAR MOUNTING
PANEL CUTOUT
REAR MOUNTING
RCA2610-3-G
RCA2610-2-G
A
B
D
C
GROUND
9-32 VDC
SPARE
SPARE
A
B
D
C
GROUND
9-32 VDC
SPARE
SPARE

RCA2610 Series Installation/Operation Guide
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KELLY MANUFACTURING COMPANY
KMC
KMC Publication No.1401-3
Figure 1.3, Typical Display Features
1. ROLL POINTER
The Roll Pointer points to the degree of roll against the Roll Dial.
2. ROLL DIAL
The Roll Dial shows the degree of roll against the Roll Pointer.
3. HORIZON LINE
Indicates earth horizon relative to aircraft pitch and roll.
4. SLIP INDICATOR (Option available for all RCA2610 models)
Also referred to as an Inclinometer, the Slip Indicator measures the relative strength of the force of gravity and the force of
inertia caused by a turn; thus indicating whether the aircraft is slipping or skidding.
5. SYMBOLIC AIRPLANE
Represents the orientation of the aircraft’s wings and nose in relation to the horizon. The dot represents the nose of the air-
craft and indicates Pitch. The wings indicate roll.
6. PITCH DIAL
Indicates the Pitch angle as determined by the Symbolic Airplane dot.
1.4 OPTIONS AND CONFIGURATIONS
Foravailableoptionsandcongurations,refertoTable1.2,below.
Panel Tilt Angle setting Set to customer requirements
Mating Connector MS3116E8-4S or equivalent
Slip Indicator Optional add-on (order P/N 444-0010-01)
Color Scheme Standard Blue & Brown
Display pointer style Fixed
Power Flag All models
Brightness Adjust All models
Pitch Synchronization As Selected
Table 1.2, Options and Congurations
1.3 DISPLAY FEATURES
See Figure 1.2 below for typical display features. RCA2610-3 shown.
10
10
20
20
30
DIM
PITCH SYNC
1 ROLL POINTER
2 ROLL DIAL
3 HORIZON LINE
4 SLIP INDICATOR
5 SYMBOLIC
AIRPLANE
6 PITCH DIAL

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KELLY MANUFACTURING COMPANY
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KMC Publication No.1401-3
SECTION 2, INSTALLATION
2.1 GENERAL INFORMATION
The conditions and test required for the TSO approval of this article are minimum performance standards. It is the responsibility of
thoseinstallingthisarticleeitheronorwithinaspecictypeorclassofaircrafttodeterminethattheaircraftinstallationconditions
are within the TSO standards. TSO articles must have a separate approval for installation in an aircraft. The article may be installed
only if performed under 14CFR Part 43 or the applicable airworthiness requirements.
ForcertainclassesofPart23aircraftlevelCofDO-178Bcerticationmaynotbesu󰀩cient-checkwithyourlocalregulatory
authority prior to installation.
2.2 HANDLING
Although the RCA2610 Series instruments are totally electronic, improper handling can cause damage. Please observe the
following precautions while handling.
1. Do not drop, jar or shake instrument. Store instrument in shipping container until installation.
2. Instruments should be transported in the original shipping container when moved to and from aircraft. If container is not
available, carefully carry by hand in upright position.
3. Avoid touching the screen. This is the most vulnerable part of the instrument. Improper handling and cleaning can cause
permanent scratching of the screen surface (See Instrument Care on Page 9).
4. To prevent further damage, a malfunctioning instrument should be handled as carefully as a new instrument. Most mal-
functioning instruments can be repaired and returned to service. Contact Kelly Manufacturing Company for repair and
warranty information.
2.3 PRE-INSTALLATION INSPECTION
1. Whentheinstrumentisrstreceived,inspectcontainerforanyshippingdamage.
2. Carefully remove the instrument from shipping container and retain container for later storage or shipping.
3. Inspecttheinstrumentforanysignsofdamage.ContactyourShippertoleanyclaimduetoshippingdamage.
4. Check labeling on the instrument to assure that the instrument panel tilt angle is correct for your aircraft.
2.4 INSTALLATION
Install the instrument on the aircraft by using the aircraft manufacturer’s recommendations and by the following steps:
1. The RCA2610 Series Horizon uses standard panel cutouts. Refer to Figures 1.1 and 1.2 “General Dimensions” for
instrument and cutout dimensions.
2. Instrument Pinout is: A = GND, B = PWR, C = SPARE, D = SPARE. CAUTION: Do not apply power to Spare pins
as damage may occur. See table 1.1 “Leading Particulars” for additional electrical information.
3. Attach aircraft electrical connector to the instrument and insert into the instrument panel cutout (See Figures 1.1
and 1.2).
4. Secure instrument with supplied screws. Use 6-32 UNC-2b screws or equivalent. Screw length should not ex-
ceed .5 inches plus bezel and panel thickness. Do not tighten.
5. With the aircraft on level surface, apply power to the instrument and allow it to warm up for 3 minutes.
6. Adjust roll position of the instrument by visually aligning the roll pointers. The Horizon Line should be level and
unbroken. Tighten screws.
Do Not modify the instrument in any way.AnymodicationswillvoidthewarrantyandrevoketheFAAcertications.

RCA2610 Series Installation/Operation Guide
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KELLY MANUFACTURING COMPANY
KMC
KMC Publication No.1401-3
Figure 3.1, Pitch Sync
SECTION 3, OPERATION GUIDE
3.1 PRE-FLIGHT PROCEDURES
Duringpre-ightprocedures,theinstrumentmustbeprovidedwithadequateelectricalpowerundernormalvibrationconditions
(engine running). A red “X” appears across the screen indicating that the instrument is booting up. When the X disappears, the
instrument is ready. The startup process should be completed within three minutes.
NOTE
Ontail-draggeraircraft,theindicatorwillnotshowasleveluntilafterachievinglevelight.Noadjustmentare
necessarywhenlevelightisachieved.
3.2 IN-FLIGHT PROCEDURES - PITCH SYNC
(Selected models only)
Ifyoutypicallyyina“nosedown”or“noseup”pitchattitude, you can adjust the Airplane Symbol to match the Horizon Line on your
instrument. The Pitch Synchronization (Pitch Sync) feature allows you to instantly sync the Airplane Symbol to the Horizon.
NOTE
This feature is not necessary for most aircraft and is to be usedonlyinsituationswherenormalightpitchis
deviated from 0 degrees.
PITCH SYNC ACTIVATION
Onceyouhaveachievedthedesiredyingpitch,activatethePitchSyncfeaturebypressingBOTH PUSH BUTTONS simultaneously.
This synchronizes the Airplane Symbol to the Horizon Line.
TheSync‘On’indicatorwilldisplay“SYNC”whenthePitchSyncisactivated(seegure3.1).
PITCH SYNC DE-ACTIVATION
To return to True Pitch, press BOTH PUSH BUTTONS simultaneously. This moves the Airplane Symbol back to True Pitch Indica-
tion and the Sync ‘On’ indicator will disappear.
EXAMPLE
IntheexampleshowninFigure3.1,Theaircraftisyinglevelata10degreenosedownpitchwiththePitchSyncon.TheSync
‘On’ Indicator is being displayed. The True Pitch Horizon is indicated by the bottom Tick Mark on the Roll Dial which is aligned with
the 10 degree mark on the Pitch Dial. The Airplane Symbol is shown aligned with the Horizon Line at 0 degrees on the Pitch Dial.
20
10
30
10
40
10
20
10
40
30
DIM
DIM
PITCH SYNC
PUSH
BUTTONS
PUSH
BUTTONS
SYNC PITCH
INDICATION
TRUE PITCH
INDICATION
SYNC PITCH
INDICATION
TRUE PITCH
INDICATION SYNC 'ON'
INDICATOR
SYNC 'ON'
INDICATOR
RCA2610-2 RCA2610-3

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KMC Publication No.1401-3
3.4 FLIGHT LIMITATIONS
TherearenoightlimitationstotheRCA2610 Series Attitude Indicator. The instrument will operate in a full 360 degrees of turn and
may be used in light aerobatic type maneuvers.
Extreme turns may cause the instrument display to temporarily disable itself. This is indicated by a red “X” across the screen and
an “Exceed Bank Angle” warning notice at the bottom of the screen. The instrument should automatically reset the display within
3to10seconds.Thissituationisduetothespeedtheprocessorrepaintsthedisplay.Theattitudesensorsarenota󰀨ectedsoitis
not necessary to level the aircraft while the display resets. Unlike mechanical gyros, extreme maneuvers will not cause any harm to
the instrument.
NOTE
This article meets the minimum performance and quality control standards required by a technical standard
order (TSO). Installation of this article requires separate approval.
3.5 EMERGENCY PROCEDURES
In the rare event that your RCA2610 does not reset itself, you will need to pull power to the unit and reset the circuit breaker. This
willrestarttheunitandyoucancontinueonwithoutdamagetotheunit.Youdonotneedtobeyinglevelwhiletheunitresets.
In a low voltage situation, the RCA2610 will show a “Low Voltage” warning notice at the bottom of the screen. This notice will
appear when the voltage goes below 11 volts. This notice will also indicate the amount of voltage the instrument is receiving. At 8.5
volts, a red “X” will appear across the screen indicating that the instrument reading is unreliable.
It is recommended that you install the Kelly Manufacturing ESP-1 (Emergency Standby Power) backup battery unit. This will
ensure that your instrument will have power in the event of Aircraft power failure. Contact your R.C. Allen/Kelly Mfg. distributor for
additional information about this product.
Figure 3.2, Dimmer Controls
3.3 IN-FLIGHT PROCEDURES - DIMMER
On startup, the RCA2610 defaults at its maximum brightness. You may adjust the screen brightness at any time with the DIMMER
PUSH BUTTONS (DIM).
PressandholdtheDIM(▼)orBRIGHTEN(▲)PUSHBUTTONSuntilyoureachthedesiredsettingandrelease,ortapeachbut-
tonforincrementalsteps(Seegure3.2fordimmingcontrols).
On non-Pitch Sync models (-G models), pressing both buttons simultaneously will reset the brightness to maximum.
If you press both buttons simultaneously, you will turn the PITCH SYNC feature on (as shown by the PITCH
SYNC‘ON’INDICATOR).PressbothbuttonsagaintoturnthePITCHSYNCo󰀨ifitisnotneeded.Referto
Section 3.2 for more information on the PITCH SYNC feature.
WARNING
10
10
20
20
30
10
10
20
20
30
10
10
20
20
30
DIM
10
10
20
20
30
DIM
DIM BRIGHTEN
DIM BRIGHTEN
RCA2610-2-G RCA2610-3-G
DIM
DIM
PITCH SYNC
DIM BRIGHTEN
DIM BRIGHTEN
RCA2610-2 RCA2610-3

RCA2610 Series Installation/Operation Guide
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KMC Publication No.1401-3
SECTION 4, GENERAL INFORMATION
4.1 Flight Testing and Adjustments
Afterighttestingandevaluation,additionalcalibrationmyberequireddependingontheuser’sapplication.Communicateight
test data with Kelly Manufacturing Company to determine appropriate adjustments.
4.2 Instrument Care
The most easily damaged part of your instrument is the screen. Special care should be taken when cleaning the screen to prevent
scratches and other damage. Avoid touching the screen at all times.
To clean light spots and dust, use a soft, lint free cotton cloth slightly moistened with distilled water.
You may also use cleaners approved for LCD TV’s and laptop computer screens.
Always apply the cleaner to the cloth and not the screen.
-CAUTION-
●Do Not use paper towels, facial tissue or napkins. These products are made from recycled paper and
may contain metals and wood chips that will scratch the screen.
●Do Not use acetone, alcohol or cleaners containing ammonia.
By avoiding all screen contact and by using proper cleaning methods, the user will be rewarded with many years of service.
4.3 OPTIONAL SLIP INDICATOR
An optional Slip/Skid Indicator (inclinometer) is available for the RCA2610 (all models). The instrument can be purchased with
the Slip Indicator attached or purchased separately and installed by the user (part number 444-0010-01). The addition of a Slip
IndicatorsatisestherequirementsforFAA’sAC91-75.Theslipindicatormaybeattachedbeforeoraftertheinstrumenthasbeen
installed in the aircraft.
INSTALLATION
1. Apply power to the instrument to assure that it reads level in pitch and roll.
2. Remove two screws on the face of the instrument.
3. Align Inclinometer with holes and replace screws. Do not tighten.
4. Adjust the inclinometer until the bubble is centered and tighten screws just enough to secure Slip Indicator.
Do not over tighten.
SCREWS
SLIP INDICATOR
DIM
Figure 4.1, Inclinometer Installation

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KMC Publication No.1401-3
4.4 FREQUENTLY ASKED QUESTIONS
How long should my Digital Horizon last?
There isn’t a good answer for this question. There are no moving parts in the RCA2610 so there isn’t anything to wear out. The
RCA2610 should give hundreds of hours of trouble free operation.
At what voltage level will my Digital Horizon become unreliable?
Unlikemechanicalhorizons,theRCA2610doesn’thavearotorthatisa󰀨ectedbyvoltage.TheRCA2610willbereliablefrom9to
32VDC.
My instrument is showing a climb/dive, what can I do?
You can check your aircraft owner’s manual or contact the aircraft manufacturer to determine if your aircraft’s instrument panel
istilted(pitchedforeandaft).Thetiltangleisanydeviationfromverticalofyourinstrumentpanelinlevelight.Yourinstrument
needs to be calibrated to compensate for this angle.
Myinstrumentisshowingaturninlevelight,whatcanIdo?
It is very important to have the instrument level (left and right) in your panel. If the instrument is not level, it will show a turn when in
levelight.Toleveltheinstrument,refertoinstallationSection2.4.6.
How do I get my instrument repaired?
For any overhaul or repair questions you can contact Kelly Manufacturing Company. Our Service Center can repair or refurbish
any R.C. Allen instrument. The only thing really required is information. You can send us your instrument with a letter giving us your
name, return shipping address, phone number and a brief description of what is wrong with the instrument or download a form from
the Support page on our web site at: kellymfg.com/support.html.
Email us for more information: [e-mail].
Or, Visit our Web Site: kellymfg.com

RCA2610 Series Installation/Operation Guide
Page 11 of 11
Rev C
KELLY MANUFACTURING COMPANY
KMC
KMC Publication No.1401-3
APPENDIX A
Environmental Qualification: DO-160G Environmental Qualification Form
NOMENCLATURE: ELECTRIC DIGITAL HORIZON
MODEL NUMBER: RCA2610-series TSO NUMBER: C4c & C113a
MANUFACTURERS SPECIFICATIONS: STP 1501 Rev. A (12/20/2016)
MANUFACTURER: Kelly Manufacturing Company
ADDRESS: 555 S. Topeka, Wichita, KS 67202
REVISION & CHANGE NUMBER OF DO-160: Rev. G DATES TESTED: 4/26/16 thru 5/24/16
CONDITIONS
SECTION
DESCRIPTION OF TESTS CONDUCTED
Temperature and Altitude
Low Temperature
High Temperature
Altitude
4.0
4.5.1
4.5.2 & 4.5.3
4.6.1
Equipment tested to Category D1
Temperature Variation
5.0
Equipment tested to Category C
Humidity
6.0
Equipment tested to Category A
Operational Shocks and Crash Safety
7.0
Equipment tested to Category B
Vibration
8.0
Equipment tested to Category U2 curve F & F1
Explosive Atmosphere
9.0
Equipment identified as category X, no test performed
Waterproofness
10.0
Equipment identified as category X, no test performed
Fluids Susceptibility
11.0
Equipment identified as category X, no test performed
Sand and Dust
12.0
Equipment identified as category X, no test performed
Fungus
13.0
Equipment identified as category X, no test performed
Salt Fog Test
14.0
Equipment identified as category X, no test performed
Magnetic Effect
15.0
Equipment tested to Category Z
Power Input
16.0
Equipment tested to Category BRX
Voltage Spike
17.0
Equipment tested to Category A
Audio Frequency Susceptibility
18.0
Equipment tested to Category Z
Induced Signal Susceptibility
19.0
Equipment tested to Category ZC
Radio Frequency Susceptibility
(Radiated and Conducted) 20.0
Equipment tested for Conducted Susceptibility to Category W
Equipment tested for Radiated Susceptibility to Category F
Emissions of Radio Frequency Energy
21.0
Equipment tested to Category M
Lightning Induced Transient
Susceptibility 22.0
Equipment tested to
Pin Injection Test: Waveform set B, Level 3
Cable Bundle Test: Waveform set H, Level 3
Multiple Burst: Level 3
[B3H33]
Lightning Direct Effects
23.0
Equipment identified as category X, no test performed
Icing
24.0
Equipment identified as category X, no test performed
Electrostatic Discharge
25.0
Equipment tested to Category A
Fire, Flammability
26.0
Equipment identified as category X, no test performed
REMARKS
In the power input test, equipment was tested to subparagraph 16.5.1.4 b, requirement for equipment with digital
circuits
Equipment also tested to (and passed) section 20, SW/CW radiated susceptibility @100V/m from 100MHz to 1GHz