NSN: |
5841-01-543-2160 |
OEM: |
Collins Aerospace |
Desc: |
Mode S Transponder |
Price | Condition | Status | More Info | |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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REQUEST | SV OUTRIGHT | REQUEST LEAD TIME |
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MAKE OFFER | AS REMOVED | REQUEST LEAD TIME |
Price | Condition | Status | More Info | |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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REQUEST | OH EXCHANGE | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | RFQ | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | RFQ | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | SV OUTRIGHT | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | SV OUTRIGHT | REQUEST LEAD TIME |
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Price | Condition | Status | More Info | |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
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REQUEST | OH EXCHANGE | REQUEST LEAD TIME |
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FAA TSO: | TSO-C112, class 2A | RTCA: | DO-181, DO-144 |
Software: | DO-178A, level 2 | EUROCAE: | ED-12A |
ICAO: | Annex 10 | Environmental: | DO-160B (FAA); ED-12A (EUROCAE) |
Size: | 3.33"H x 4.90"W x 12.50"L | Weight: | 8.5 lbs. |
Power Requirements: | Requirements: 27.5 +-2.5Vdc at 28 watts nominal, 30 watts max | Power output: | 250 watts min, 625 watts max |
Recevier IF: | 60 MHz | Receiver Sensitivity: | -77 dBm +-3dBm |
Part Number | ATC Mode S Transponder Description: |
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622-9210-001 | original version, see features above |
622-9210-002 | Auto Altitude Mode; Same as -001 but with upgraded TCAS interface performance, and added altitude input improves the "Burst" control interface necessary for several system configurations |
622-9210-003 | Auto Altitude Mode; Same as -002 but with updated improvements to Mode S transponder requirements per RTCA and installation configuration options are expanded and enhancements to its diagnostic and maintenance performance is implemented |
622-9210-004 | Supersedes -003; Auto Altitude Mode; ADS-B Compatible |
622-9210-005 | Supersedes -004; Auto Altitude Mode; Same as -004 but with improved altitude resolution status for aircraft that have digital source of altitude information |
622-9210-006 | Auto Altitude Mode; Same as -005 but with improved software for TCAS flag |
622-9210-007 | Supersedes -004/005/006; Auto Altitude Mode; Enhanced Mode S; Can be installed in aircraft WITHOUT Pro Line 4 or 21 |
622-9210-008 | Supersedes -007; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21; Can also be installed in aircraft WITHOUT Pro Line 4 or 21 if STRAP is set properly |
622-9210-108 | Supersedes -007/008; ADS-B capability; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21; Can also be installed in aircraft WITHOUT Pro Line 4 or 21 if STRAP is set properly |
622-9210-207 | Supersedes -007; Auto Altitude Mode; Enhanced Mode S; Can be installed in aircraft WITHOUT Pro Line 4 or 21 |
622-9210-308 | Supersedes -008; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21 |
622-9210-309 | Supersedes -004/005/006/007/008/207/308 |
622-9210-310 | Supersedes -007/008/207/308/309 |
622-9210-408 | Supersedes -108; Enhanced Mode S; Can be installed in aircraft WITH Pro Line 4 or 21 |
622-9210-409 | Supersedes -004/005/006/007/108/207/408; ADS-B capable (DO-260A) |
622-9210-410 | Supersedes -007/008/108/207/308/309/408/409; ADS-B Capable (DO-260A) - CSDB data source |
622-9210-500 | ADS-B Capable (DO-260B) - fixed wing application |
622-9210-501 | ADS-B Capable (DO-260B) - fixed wing application |
622-9210-502 | Automatically generates flight ID if absent |
622-9210-550 | ADS-B Capable (DO-260B) - rotorcraft application |
622-9210-551 | ADS-B Capable (DO-260B) - rotorcraft application |
NSN: 5895-01-670-0766
Price | Condition | Status |
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$16,500.00 | SV OUTRIGHT | 1 IN STOCK |
Price | Condition | Status |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
Price | Condition | Status |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
NSN: 5895-01-424-3785
Price | Condition | Status |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
NSN: 5895-01-459-8632
Price | Condition | Status |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
NSN: 5895-01-497-7758
Price | Condition | Status |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
REQUEST | SV OUTRIGHT | REQUEST LEAD TIME |
$250.00 | AR OUTRIGHT | REQUEST LEAD TIME |
NSN: 5895-01-588-0997
Price | Condition | Status |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
REQUEST | OH EXCHANGE | REQUEST LEAD TIME |
NSN: 5895-01-514-7241
Price | Condition | Status |
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RFQ | RFQ | RFQ |
NSN: 5841-01-543-2160
Price | Condition | Status |
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RFQ | RFQ | RFQ |
Price | Condition | Status |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
NSN: 5841-01-623-5101
Price | Condition | Status |
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REQUEST | SV OUTRIGHT | REQUEST LEAD TIME |
Price | Condition | Status |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
NSN: 5895-01-576-8741
Price | Condition | Status |
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REQUEST | SV OUTRIGHT | REQUEST LEAD TIME |
Price | Condition | Status |
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REQUEST | OH OUTRIGHT | REQUEST LEAD TIME |
REQUEST | OH EXCHANGE | REQUEST LEAD TIME |
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.
No, it is not economical to upgrade a -006 or lower. -007 and higher units should be pursued instead.
The first revision of the TDR-94/94D manual is dated April 1989
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.
In installations where two TDR-94D transponders are used, but space is not available to install four antennas, special relays can be used to operate the two TDR-94D transponders with only two antennas. This configuration can also be used to operate two TDR-94 transponders with one antenna. The diagram below shows a Coaxial Switch from Ducommun (P/N: D2-729B002) completing the configuration. The described PN has been replaced by a more recent version, D2-729B003. This new version is available from Southeast Aerospace.
"As Removed" or condition "AR" parts are in the same condition as they were removed from an aircraft. The reasons for removal include aircraft upgrades, teardowns, or certain types of incidents. In most cases, AR parts have not been inspected or tested. They do not include airworthiness certification such as FAA Form 8130 or EASA Form 1. Southeast Aerospace encourages avionics in this condition to be tested and recertified before using in an aircraft.