Part #: 622-6667-001
Model: PWR-230
Part Number :
Select part number above to view pricing and availability.
NSN: 5895-01-306-4529
* Price & Availability valid as of 06/02/20 20:41:00 EDT *
SEA Repair Capabilities: Yes
Average Repair: $1,462.50
Due to the variation in condition of units, repair costs can vary significantly. The Average Repair Price indicated is a historical average only and is NOT a fixed or flat rate price. An actual cost to repair or overhaul an item can only be determined by proper bench testing at our repair station.
PWR-230
FEATURES
- Power amplifier used in HF-230 HF System
- 100-W pep output
- Remote mounted
SPECIFICATIONS
| 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 Number | HF Power Amplifier Description:: |
|---|---|
| 622-6667-001 | see features above |
622-6667-001
- HF Power Amplifier
NSN: 5895-01-306-4529
| Price | Condition | Delivery |
|---|---|---|
| $3,950.00 | OH OUTRIGHT | VIEW STOCK |
| $1,950.00 | OH EXCHANGE | VIEW STOCK |
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
Is an STC required for an HF system installation?
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.
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.
| Serial # | 2363 |
|---|---|
| Condition | OH |
| Mods | 1-3 |
| Tag Date | 11/12/19 |
| Shop | Southeast Aerospace Inc. |
