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Part # 442CW-OH SERIES
Tempest offers a complete line of new and overhauled FAA-PMA approved dry air pumps.
All new and overhauled Tempest dry air pumps come with patented WIP™ (Wear Indicator Port) that allows for internal observation of the pump’s vanes. The WIP™ helps determine if the pump should be replaced and avoid unscheduled maintenance due to a pump exceeding its life cycle. They also include finned stators for increased cooling and an “ultra-hard” finish on the internal wear surfaces of the stator for low friction and extended life.
New Tempest dry air pumps offer a closed coupling area and patented “LRT” diverter. These design features will help you detect and prevent pump contamination from external sources.
The 240 and 400 series dry air pumps are rugged, light-weight, and designed with today’s high-performance aircraft in mind. These pumps use a heat-treated, stainless-steel conical pressure plate spring and torsional dampening springs to provide a harmonics-free pressure plate control and smooth temperature compensation. The larger pumps also use hardened stainless-steel pressure plates that are precision ground and lapped to reduce internal leakage and wear.
For these reasons and more, Tempest is the preferred dry air pump of aviation maintenance technicians worldwide
Each pump is meticulously and professionally hand assembled to insure proper tolerances and clearances. This assures optimum performance. After assembly, each pump is functionally tested. After this initial testing, the pump is disassembled, inspected for any unusual wear or abnormalities, and reassembled for a second test run. This extensivetesting procedure assures that only first-class products leave the facility.
When Tempest receives a core, it is disassembled and all carbon is discarded. Tempest never re-uses carbon. A new stator is used on all 200 series pumps. The larger 400 series pumps have the hard anodize stripped from the center stator and the stator is inspected for cracks. Then the I.D. is reconditioned. After the reconditioning process, each 400 series stator is meticulously inspected for proper dimensions. The stator then receives a new hard anodize coating. All re-used parts are inspected in the overhaul process to make sure that each part meets the FAA-PMA approved requirements process specification 203-6-1009.
WARNING: Cancer and/or Reproductive Harm - California Proposition 65 Resources
| Make | Model | Start S/N | End S/N | Comment | Eligibility Chart |
|---|---|---|---|---|---|
| Beechcraft F33A | F33A | S/N CE-290 – CE631 | CE631 | Comment | Eligibility Chart 1545 |
| Beechcraft F33C | F33C | S/N CJ-26 – CJ179 | CJ179 | Comment | Eligibility Chart 1545 |
| Beechcraft V35B | V35B | S/N D9858 – D9999999 | D9999999 | Comment | Eligibility Chart 1545 |
| Beechcraft V35B-TC | V35B-TC | S/N D9858 – D9999999 | D9999999 | Comment | Eligibility Chart 1545 |
| Beechcraft 36 | 36 | S/N E184 – E184 | E184 | Comment | Eligibility Chart 1545 |
| Beechcraft 36 | 36 | S/N E197 – E197 | E197 | Comment | Eligibility Chart 1545 |
| Beechcraft 36 | 36 | S/N E203 – E2179 | E2179 | Comment | Eligibility Chart 1545 |
| Beechcraft A36 | A36 | S/N E184 – E184 | E184 | Comment | Eligibility Chart 1545 |
| Beechcraft A36 | A36 | S/N E197 – E197 | E197 | Comment | Eligibility Chart 1545 |
| Beechcraft A36 | A36 | S/N E203 – E2179 | E2179 | Comment | Eligibility Chart 1545 |
| Beechcraft A36TC | A36TC | S/N EA-1 – EA-272 | EA-272 | Comment | Eligibility Chart 1545 |
| Beechcraft B36TC | B36TC | S/N EA-273 – EA502 | EA502 | Comment AND EA504, WITH STANDBY SYSTEM | Eligibility Chart 1545 |
| Beechcraft G50 | G50 | S/N GH-94 – GH-119 | GH-119 | Comment | Eligibility Chart 1545 |
| Beechcraft H50 | H50 | S/N HH-120 – HH-149 | HH-149 | Comment | Eligibility Chart 1545 |
| Beechcraft 95-55 | 95-55 | S/N TC-1 – TC-190 | TC-190 | Comment | Eligibility Chart 1545 |
| Beechcraft 95-A55 | 95-A55 | S/N TC-191 – TC-379 | TC-379 | Comment | Eligibility Chart 1545 |
| Beechcraft 95-B55A | 95-B55A | S/N TC-1608 – TC-2456 | TC-2456 | Comment | Eligibility Chart 1545 |
| Beechcraft 95-B55A | 95-B55A | S/N TC-502 – TC-1607 | TC-1607 | Comment | Eligibility Chart 1545 |
| Beechcraft 56TC | 56TC | S/N TG52 – TG94 | TG94 | Comment DEICE | Eligibility Chart 1545 |
| Beechcraft 56TC | 56TC | S/N TG84 – TG94 | TG94 | Comment NON-DEICE | Eligibility Chart 1545 |
| Beechcraft 60 | 60 | S/N P-4 – P246 | P246 | Comment NON-DEICE W/ AUTO PILOT | Eligibility Chart 1545 |
| Beechcraft A60 | A60 | S/N P4 – P246 | P246 | Comment DEICE | Eligibility Chart 1545 |
| Beechcraft A60 | A60 | S/N P4 – P246 | P246 | Comment NON-DEICE W/ AUTO PILOT | Eligibility Chart 1545 |
| Beechcraft B60 | B60 | S/N P-247 – P307 | P307 | Comment DEICE, SINGLE INSTRUMENT | Eligibility Chart 1545 |
| Beechcraft B60 | B60 | S/N P-247 – P99999 | P99999 | Comment NON-DEICE, DUAL INSTRUMENT | Eligibility Chart 1545 |
| Beechcraft B60 | B60 | S/N P308 – P378 | P378 | Comment DEICE, DUAL INSTRUMENT | Eligibility Chart 1545 |
| Beechcraft B60 | B60 | S/N P379 – P99999 | P99999 | Comment DEICE | Eligibility Chart 1545 |
| Beechcraft A65 | A65 | S/N LC-240 – LC9999 | LC9999 | Comment NON-DEICE | Eligibility Chart 1545 |
| Beechcraft A65 | A65 | S/N LC271 – LC9999 | LC9999 | Comment DEICE | Eligibility Chart 1545 |
| Beechcraft 70 | 70 | S/N LB-1 – LB9999 | LB9999 | Comment DEICE AND NON-DEICE | Eligibility Chart 1545 |
| Britten-Norman (Pilatus) BN-2A | BN-2A | S/N 0 – ZZZZZZZZZZZZZZZ | ZZZZZZZZZZZZZZZ | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310C | 310C | S/N 35772 – 39031 | 39031 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310D | 310D | S/N 39032 – 39299 | 39299 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310E (USAF U-3B) | 310E (USAF U-3B) | S/N 310M0001 – 310M0036 | 310M0036 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310F | 310F | S/N 310-0001 – 310-0156 | 310-0156 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310G | 310G | S/N 310G0001 – 310G0156 | 310G0156 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310H | 310H | S/N 310H0001 – 310H0148 | 310H0148 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310I | 310I | S/N 310I0001 – 310I0200 | 310I0200 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310J | 310J | S/N 310J0001 – 310J0200 | 310J0200 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310J | 310J | S/N 310J0001 – 310J0200 | 310J0200 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310K | 310K | S/N 310K0001 – 310K0245 | 310K0245 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 310R | 310R | S/N 310R0001 – 310R99999 | 310R99999 | Comment DEICE | Eligibility Chart 1545 |
| Cessna E310H | E310H | S/N 310H0001 – 310H0148 | 310H0148 | Comment DEICE | Eligibility Chart 1545 |
| Cessna E310J | E310J | S/N 310J0001 – 310J0200 | 310J0200 | Comment DEICE | Eligibility Chart 1545 |
| Cessna T310P | T310P | S/N 310P0001 – 310P0240 | 310P0240 | Comment DEICE | Eligibility Chart 1545 |
| Cessna T310Q | T310Q | S/N 310Q0001 – 310Q1160 | 310Q1160 | Comment DEICE | Eligibility Chart 1545 |
| Cessna T310R | T310R | S/N 310R0001 – 310R2140 | 310R2140 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 320 | 320 | S/N 320-0001 – 320-0110 | 320-0110 | Comment WITH DEICE, W/ CONVERSION KIT | Eligibility Chart 1545 |
| Cessna 320-1 | 320-1 | S/N 320-0001 – 320-0110 | 320-0110 | Comment WITH DEICE, W/ CONVERSION KIT | Eligibility Chart 1545 |
| Cessna 320A | 320A | S/N 320A0001 – 320A0047 | 320A0047 | Comment WITH DEICE, W/ CONVERSION KIT | Eligibility Chart 1545 |
| Cessna 320B | 320B | S/N 320B0001 – 320B0062 | 320B0062 | Comment WITH DEICE, W/ CONVERSION KIT | Eligibility Chart 1545 |
| Cessna 320C | 320C | S/N 320C0001 – 320C0073 | 320C0073 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 320D | 320D | S/N 320D0001 – 320D0130 | 320D0130 | Comment DEICE W/ CONVERSION KIT | Eligibility Chart 1545 |
| Cessna 320E | 320E | S/N 320E0001 – 320E0110 | 320E0110 | Comment DEICE W/ CONVERSION KIT | Eligibility Chart 1545 |
| Cessna 320F | 320F | S/N 320F0001 – 320F0045 | 320F0045 | Comment DEICE W/ CONVERSION KIT | Eligibility Chart 1545 |
| Cessna 335 | 335 | S/N 335-0001 – 335-0065 | 335-0065 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 340 | 340 | S/N 340-0001 – 340-99999 | 340-99999 | Comment W/ DUAL INSTRUMENTS | Eligibility Chart 1545 |
| Cessna 340A | 340A | S/N 340A0001 – 340A99999 | 340A99999 | Comment NON-DEICE, DUAL INSTRUMENTS | Eligibility Chart 1545 |
| Cessna 340A | 340A | S/N 340A0201 – 340A99999 | 340A99999 | Comment DEICE | Eligibility Chart 1545 |
| Cessna 401B | 401B | S/N 401B0001 – 401B0100 | 401B0100 | Comment W/ AUTO PILOT | Eligibility Chart 1545 |
| Cessna 401B | 401B | S/N 401B0101 – 401B0300 | 401B0300 | Comment | Eligibility Chart 1545 |
| Cessna 402B | 402B | S/N 401B0101 – 401B999999 | 401B999999 | Comment | Eligibility Chart 1545 |
| Cessna 414A | 414A | S/N 414A0001 – 414A1212 | 414A1212 | Comment WITH DUAL INSTRUMENTS OR DEICE | Eligibility Chart 1545 |
| Piper PA-31 | PA-31 | S/N 31-7812098 – 31-99999999 | 31-99999999 | Comment DEICE, C/R OPTION RIGHT ENGINE W/ WING LOCKER | Eligibility Chart 1545 |
| Piper PA-31-350 | PA-31-350 | S/N 31-8052001 – 31-9999999 | 31-9999999 | Comment RIGHT, DEICE | Eligibility Chart 1545 |
Reference only: Please verify the product is eligible for your aircraft before adding to your cart.
Is an overhauled Dry Air Pump as good as a new pump?
We can only speak for Tempest overhauled pumps as we have no control over the quality of other overhaul shops. Before Tempest®/Aero Accessories, LLC offered an overhauled pump, they spent more than a year in research and testing to determine what was required to produce a quality overhauled pump that would last as long as a new pump producing the vacuum or pressure required for aircraft application. In 1984 Tempest®/Aero Accessories, LLC had its overhaul process specification approved by the FAA and began offering quality overhauled vacuum pumps to general aviation. Tempest takes great pride in their state of the art overhaul facility, and produce the best overhauled pump on the market today. Over the years they have acquired FAA-PMA’s for all component parts of the Dry Air Pumps, and have supplied replacement parts to all overhaulers worldwide.
When I start my engine the vacuum gauge reads zero vacuum, but as the engine RPM increases, the gauge will indicate vacuum. What causes this?
The carbon vanes inside the pump are sticking in rotor slots. Oil or solvent has entered the pump either from a bad oil seal in the engine case at the pump mounting area, or from pressure washing the engine with an oil-based solvent (spraying directly on the pump). The oil or solvent will work its way up into the pump through the drive end, mixing with graphite dust and turning into a paste like material.
A Dry Air Pump is just that: DRY. As the carbon rotor and vanes wear, they produce graphite dust which lubricates moving internal parts of the pump. When oil or solvent mixes with this graphite dust, it keeps vanes from moving freely in their slots and they stick. At low engine RPM, the vanes are recessed in their slots and create no vacuum, but as engine RPM increases, centrifugal force slings the vanes out, allowing them to grab air and create vacuum. Once a pump has become contaminated, its life expectancy is extremely short. The cause of pump contamination should be determined and corrected and the pump should be replaced as soon as possible.
What procedures should be taken when replacing a failed pump?
I frequently need to replace my Dry Air Pump. What could be causing this?
Should I use a cooling shroud on my dry air pump?
Yes, using a cooling shroud whether on a 200 series or 400 series dry air pump can reduce pump temperatures by as much as 10%. For more information, go to Vacuum Pump Cooling Kit.