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Part #: 622-6667-001

Model: PWR-230




Collins Aerospace


HF Power Amplifier

Part Number :

  • Power amplifier used in HF-230 HF System
  • 100-W pep output
  • Remote mounted
TSO: C31c, C32c RTCA: DO-160A
FCC: Type accepted, parts 83,87 Env. Categories: F3/B/MN/XXXXXXBBBBB
Dimensions: 5.0"W x 5.04"H x 11.70"L Weight: 7.25 lb.
Temperature: -55 to +55C (continuous) Altitude: 55000 ft.
Power Output: 100 watts pep, 25 watts average +-1.5 dB into a 50-ohm load Input Impedance: 50 ohms resistive within a 1.5:1 vswr
Warmup Time: None Input Drive Level: Not more than 65 mW pep required to drive PWR-230 to 100 W pep +-1.5 dB
Tuning Operation: Output limited to 20 W during tune cycle Harmonic Attenuation: 63-dB minimum below mean power
Tuning Time: 1 second maximum Mismatched Load: PWR-230 is protected by internal circuits against high vswr mismatches
Part NumberHF Power Amplifier Description::
622-6667-001 see features above


Serial # 922
Condition OH
Mods 1
Tag Date 01/09/24
Shop Southeast Aerospace Inc.
Warranty 6 Months
- HF Power Amplifier

NSN: 5895-01-306-4529

Price Condition Status

Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact

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.

In most cases, a Supplemental Type Certificate is not required for the installation of an HF system. Major changes or alterations to an aircraft may include those which affect weight, balance, structural aspects, reliability, operational characteristics, airworthiness characteristics, etc. Some major alterations can be performed using the FAA Form 337 with approved data. This approved data can be in the form of engineering data with a FAA designee approval (i.e. DER, DAR). The DER or DAR then issues an FAA Form 8110 which is considered approved data adequate to proceed with the installation.

HF installations in the USA are installed and approved in the method detailed above. STCs are not required for almost all HF installations since the change to the existing aircraft Type Certificate (TC) is not so intensive as to require one.