will be closed December 23rd - January 3rd for the Holidays.
Regular business hours will resume on Monday, January 6th.
AOG Services are available.
will be closed December 23rd - January 3rd for the Holidays.
Regular business hours will resume on Monday, January 6th.
AOG Services are available.
FEATURES
SPECIFICATIONS
| Size: | 6.31"W x 3.0"H x 11.19"L | Weight: | 6.0 lbs. |
| Reference Documents: | RTCA DO-160, FAA AC 90-45A (Area Nav) | Environmental Categories: | AASKPZBBA |
| Temperature Range: | -20 to +55C | Altitude Range: | Up to 35,000 feet |
| DME Trasnmitter Power: | 50W minimum (100W typical) | DME Sensitivity: | -82dbm (-85 typical) |
| DME Range: | 0-200 nm | DME Accuracy: | 0 to 99.9nm: +-.2nm; 100 to 200nm: +-.3nm |
| NAV Frequency Range: | 200 channels, 108.00 to 117.95 with 50kHz spacing | NAV Sensitivity: | 2uv Max. (hard) will provide a flyable course indication |
| NAV Selectivity : | 6db at +-16kHz, 65db at +-40kHz | Spurious Responses (NAV): | At least 50db down |
| VOR Accuracy: | Typically less than +- 1 deg. error | Waypoint Angle (RNAV): | Selectable on digital display in .1 deg. increments |
| Bearing and Distance Accuracy (RNAV): | Meets FAA Advisory Circular 90-45A accuracy requirements | GS Frequency Range: | 40 channel, 329.15 to 335.00MHz with 150KHz spacing |
| GS Sensitivity: | 16uv (hard) for half flag | GS Selectivity: | >6db @ +-25KHz, >40db @ +-150KHz |
| Number of Deviation Loads (GS): | Up to 5 floating 1000 Ohm loads | OBS resolver: | 30Hz meeting ARINC requirements |
| Course Deviation (Output): | Up to 5 floating 1000 Ohm loads | VOR/LOC Warning Flags: | Up to 3 floating 1000 Ohm loads |
| TO/FROM Indication: | Up to 3 floating 200 Ohm loads | DME Audio Ouput: | 18mw Max. into 500 Ohm |
| NAV Audio Output: | 50mw Max. into 500 Ohm | Search Time: | 1.0 second nominal |
| Part Number: | Description: |
|---|---|
| 066-4008-00 | Standard version with NAV/RNAV/DME/ILS (glideslope), standard lens |
| 066-4008-01 | WIth NAV/RNAV/DME/ NO glideslope, standard lens |
| 066-4008-02 | With NAV/RNAV/DME/ILS (glideslope), shiny lens |
| 066-4008-03 | With NAV/RNAV/DME/ NO glideslope, shiny lens |
Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact questions@seaerospace.com
In relation to NE (New) parts, many OEMs change their prices and availability without any notice to dealers or the industry. Therefore, through the REQUEST or RFQ indication, we ask that customers contact us for the most accurate price and availability.
In relation to SV & OH parts, the used parts aftermarket in the aviation industry is not an infinite supply. It is a dynamic, constantly changing market that is significantly affected by and susceptible to highs and lows in supply and demand. Therefore, although we attempt to, at times, we are unable to predict the exact moment when an item may be available. Once again, through the REQUEST or RFQ indication on our website, we ask that customers contact us for the most current and accurate price and availability.
Neither the KNS-80 or KNS-81 Nav Systems contain FM immunity. Likewise, there are no modifications or service bulletins that can be incorporated to achieve FM immunity. However, the KNS-81 can be used in conjunction with KA-155 FM filter to achieve FM immunity. KNS-81 units must have Mod 14 to be compatible with the KA-155. KNS-81 units above serial number 8309 already have this mod incorporated. According to Revision 4 of the KA-155 installation manual, the KNS-80 can be used with the KA-155 filter as well.
Negotiating the exchange price of a unit only limits the allowable repair cap for the core unit. Southeast Aerospace's exchange transactions are based on the return of economically repairable core unit. Once the core is received and evaluated, the core repair cost incurred by SEA cannot exceed 75% of the original exchange price. That is, it cannot cost SEA more than 75% of the original OH/SV exchange price collected from the customer. Therefore, when and if an SEA exchange price is discounted, there is a risk that additional charges may be assessed once the core is returned and evaluated.
The KNS-81 meets TSO C40a (VOR), C36c (LOC), and C34c (Glideslope). The KNS-80 does not meet any TSOs. The VOR/LOC/GS section of the KNS-80 is very similar to that of the KNS-81. The KNS-80 also include integrated DME. The DME section of the KNS-80 is similar to that of a stand-alone KN-64 DME. The KN-64 is not a TSOd DME. Therefore, with the inclusion of the Non-TSO DME, the KNS-80 is not TSOd overall.
It should be noted that although the KNS-80 is not TSOd, it does meet the Area Navigation System specification as per FAA Advisory Circular 90-45A
Although the specific KNS-80 and KNS-81 installation manuals only specify certain King indicators as compatible, there are many different indicators that can be used with these navigation systems. The King installation manuals indicate the following nav indicators as compatible:
KI-206
KNI-520
KPI-552
KPI-553
(note: the manual does list some much older indicators as well which are obsolete and unsupportable)
In addition, the following indicators will interface and provide the necessary functions for VOR/LOC/GS navigation:
KI-202 (VOR/LOC only)
IND-350 (VOR/LOC only)
IND-350A (VOR/LOC only)
IND-351
IND-351A
IND-351D
More or less, any "non-converter" indicator should function properly with the KNS-80 and KNS-81. Please note that it is ultimately the responsibility of the installer to verify system performance, functionality, and airworthiness.
