Pilatus PC-12 eQRH 4+

This PC-12 Electronic Quick Reference Handbook ( eQRH) is a pilot assistance tool for the quick and easy review of emergency procedures and other important recommendations. The use of this eQRH is solely the responsibility of the pilot/operator.

The eQRH covers the versions PC-12/45 (MSN 321, 401-683, not 545), PC-12/47 (MSN 684-888), PC-12/47E (MSN 1001-1450, not 1300), PC-12/47E (MSN 1300, 1451-1942, not 1720) and PC-12 / 47E (MSN 1720, 2001 upwards) and shall only be used upon verification of the specific aircraft, which must comply with the eQRH version selected.
The eQRH is based on selected data and information contained in the EASA approved Airplane Flight Manual (AFM) which is part of the Pilot’s Operating Handbook Report No. 02211 at revision 12 (for QRH PC-12/45 and PC-12/47) and Report No. 02277 at revision 16 (for both QRH PC-12/47E). The AFM has been examined and approved by the competent authorities and represents the sole authorized document for the operation of the aircraft. IN THE EVENT OF ANY CONFLICT THE POH SHALL PREVAIL OVER THE eQRH.

THIS ELECTRONIC QUICK REFERENCE HANDBOOK DOES NOT RELEASE THE OPERATOR IN ANY WAY FROM ITS OBLIGATION TO STRICTLY COMPLY IN ALL RESPECTS WITH THE APPROVED POH AND ALL OF ITS REVISIONS AND TO KEEP CONTINUALLY UP TO DATE.

No update service of the eQRH will be provided. Pilatus will at its sole discretion decide if a software update should be made available. Whenever the update-function of the app shows the availability of a software update for the application it should always be implemented.

PILATUS REJECTS ALL AND ANY RESPONSIBILITY OR LIABILITY for the completeness and/or accuracy of the eQRH. This ELECTRONIC QUICK REFERENCE HANDBOOK does not contain and shall not be deemed to contain any representations, warranties and/or covenants regarding the specifications, performance and /or operation of the PC-12/45, PC-12/47 and PC-12/47E aircraft and PILATUS REJECTS ANY AND ALL LIABILITY with respect to any handling, maintenance and/or operation of the PC-12/45, PC-12/47 and PC-12/47E aircraft which is not in full and strict compliance with the provisions of the POH.