Sunset sky over a dark mountain ridge, seen from a light aircraft.

Services

What we do

Inspections and certification, new installations, and the wiring work in between.

Certification

Pitot-static & altimeter

Static system leak checks, altimeter calibration and airspeed indicator checks. The altimeter and static system are due every 24 months for IFR, or VFR in Class B, C or transponder Class D airspace.

Details on pitot-static and altimeter checks
  • Static & pitot leak tests
  • Altimeter scale-error check
  • Airspeed indicator check
What the regulations say
Who needs it

If you fly IFR, or VFR in Class B or C airspace, or Class D airspace designated as transponder airspace, your altimeter must be calibrated at least every 24 months (Standard 625, Appendix C, item 13).

What counts

The rule covers more than the altimeter itself: air data computers, altitude encoders, autopilots and altitude alerters that use static pressure all count as "altimetry devices".

How we test

We test to Standard 571, Appendix B, including a static system leak check. An unpressurized aircraft may lose no more than 100 ft of indicated altitude in one minute.

Records

The test date and the maximum altitude tested are recorded on the altimeter and in your aircraft's records.

Certification

Transponder & encoder

Transponder bench-level checks on the aircraft, plus altitude encoder correspondence with your altimeter. Due every 24 months, VFR or IFR.

Details on transponder and encoder checks
  • Mode C / Mode S checks
  • Encoder correlation
  • Done together with the pitot-static check
What the regulations say
Who needs it

You need a transponder with altitude reporting to fly in transponder airspace (CAR 605.35).

How often

Every installed transponder, including its altitude reporting, must be tested every 24 months, to Standard 571, Appendix F (Standard 625, Appendix C, item 14).

Altitude agreement

The altitude your transponder reports must agree with your altimeter within 125 ft (Standard 571, Appendix F).

Scheduling

Both checks run on 24-month cycles, so we usually do them together in one visit.

Installations

Panel upgrades

Glass displays, GPS navigators, audio panels, autopilots and ADS-B. We plan the panel and build the harness.

Details on panel upgrades
  • Brands: Garmin (over-the-counter and experimental), Dynon, Advanced Flight Systems, Trig Avionics, Aspen Avionics, BendixKing, PS Engineering, Jupiter Avionics and more
  • Panel layout & harness build
  • Weight & balance updates
What the regulations say
Classification

Every modification is classed as major or minor using Transport Canada's criteria (Standard 571.06 and Standard 571, Appendix A). That decides the approved data and paperwork needed.

Reporting

A major modification is reported to Transport Canada within 30 days of the aircraft returning to service (Standard 571.12 and Standard 571, Appendix L).

Weight and balance

If the work changes your aircraft's empty weight or balance, the journey log entry is made before its next flight; after any change to the installed equipment, the weight and balance equipment list is updated (Standard 571, Appendix C).

Repair

Troubleshooting

Intermittent radios, dead annunciators, charging faults. Methodical wiring diagnosis instead of swapping boxes until it works.

Electrical

Wiring & harnesses

New harness fabrication, connector repair and cleanup of legacy wiring left behind by past installs.

Safety

ELT & instruments

Recertification, calibration and troubleshooting for both ELTs and instruments.

Details on ELT and instrument work
What the regulations say
121.5 MHz ELTs

121.5 MHz ELTs with standard batteries: maintenance at least every 12 months.

406 MHz ELTs

406 MHz ELTs (which also transmit on 121.5) with standard batteries: an operational test at least every 12 months, and a full performance test at least every 24 months.

Water-activated batteries

ELTs with water-activated batteries: at least every five years.

Battery rules

Batteries are replaced on the manufacturer's schedule, and after any emergency use, an inadvertent activation of unknown duration, or once transmissions add up to more than one hour, with an operational test after each replacement.

Test procedure

We never transmit a live 406 MHz signal during testing, and operational tests are kept to the first five minutes of the hour (UTC), five seconds at most, so they can't be mistaken for a real emergency.

(All from Standard 625, Appendix C, item 12, and Standard 571, Appendix G.)

Request a quote

Tell us about the aircraft

The registration and what you need done is enough to start. We'll reply with a price and an open date.

Request a quote