By transacting an exchange sale with Southeast Aerospace, you agree, understand, acknowledge, and accept the terms, conditions, and details indicated in this Exchange Policy.
An exchange sale is defined as a transaction of a standard exchange of a Serviceable or Overhauled certified part with a specific part number sold to a customer in exchange for the same part (i.e. part number)
returned by the customer in an unserviceable but repairable condition. The customer returned part is referred to as the “core”. Core must be received by Southeast Aerospace within 30 days of original exchange sale transaction date.
The core charge will be collected in advance and will be credited back once received by Southeast Aerospace, in accordance with the terms defined in this policy.
Exchange price is based on a standard exchange. Additional billing will only occur in rare cases where the cost needed to repair the core exceeds 75% of the Exchange price. This value is known as the “Repair
Cap”. Additional billing will occur in the event that a core is not returned or is deemed Beyond Economical Repair (BER) or unable to be repaired. Please see additional details below.
All exchange transactions are based on the return of a repairable core within 30 days of the same model and part number as supplied to the customer. A repairable core is defined as a part that is not corroded,
excessively damaged, missing the data plate/serial number, or contains obsolete service parts that are no longer available from the original equipment manufacturer.
Other specific serial number and/or core conditions may apply. Prototype/preproduction units may not be accepted as cores. Customer will be made aware of any other conditions at the time when order is placed.
All cores must be returned to Southeast Aerospace at 1399 General Aviation Drive, Melbourne, FL 32935 USA. All transportation costs for the return of the core are the responsibility of the customer. Any additional
fees incurred by Southeast Aerospace in relation to the transportation of the core return by the customer will be assessed and collected from the customer.
Customer exchange cores must be returned to Southeast Aerospace within 30 days. If no core is returned after 30 days, the core charge (i.e. difference between Outright & Exchange prices) will be billed to the customer.
Cores will be evaluated for acceptance within 2-4 weeks of receipt for parts repaired in-house by Southeast Aerospace. Core acceptance for parts not repaired in-house by Southeast Aerospace is subject to outside repair evaluation turn-times.
Any exceptions to the Billing, Core Conditions, and Core Return policy are subject to written approval by Southeast Aerospace.
If you have any questions or concerns regarding this policy, please contact a Southeast Aerospace representative.
Programmable fuel flow/pressure instrument (available with or without fuel pressure with use of PT-100GA Pressure Transducer)
Displays fuel flow to .1 gal/hr, pressure to .2 PSI
Displays fuel used, remaining and time to empty
Independent warning lights for fuel level and pressure
Automatic reminder to update fuel level
Two programmable low fuel warnings
Programmable time to empty warning
Programmable low fuel pressure warning
Programmable high fuel pressure warning
Programmable display for gallons, pounds, liters, or British gallons
Programmable default full fuel level
Programmable filter for fast response time
All limits are set by pilot from front panel
LCD backlit dislay
Similar to FP-5L but DOES NOT include GPS/Loran features such as fuel to destination and fuel reserve
See Voice Annunciator AV-17 to add voice warnings to this instrument
NOTE: Please specify the following information when ordering this instrument: - Fuel Pressure indication desired? (Package must include PT-100GA Pressure Transducer) - Fuel Flow transducer to be used?
If aircraft has gravity feed fuel system, FT-90 Flow Transducer must be used If aircraft engine is rated less than 300 hp, FT-60 Flow Transducer must be used If aircraft engine is rated between 300 and 500 hp, FT-90 Flow Transducer must be used If aircraft engine is rated over 550 hp, FT-180 Flow Transducer and IU-1 Interface Unit must be used - FFDM-1 Fuel Flow Differential Module must be used with FP-5 package to accomodate pressure carburetor with fuel return line back to fuel tank. Not needed for fuel return lines on injected engines - IU-1 Interface Unit used to interface magnetic pickup type flow transducer to FP-5
2 1/4" Mount, 3.65" depth
28 oz. kit
7.5 to 30 volts, .3 amps
viewable in direct sunlight, backlit for night operation