This PC-12 Digital Airplane Flight Manual (Digital AFM) is a pilot assistance tool for verification of the weight and balance of the Pilatus PC-12 and the calculation of take-off, cruise and landing performance. It is for plausibility checks regarding aircraft data only. The use of this Digital AFM is solely under the responsibility of the pilot/operator. A cross wind calculator is also included.
The DIGITAL AFM covers the versions PC-12/41, PC-12/45, PC-12/47 and PC-12/47E and shall only be used upon verification of the specific aircraft, which must comply with the DIGITAL AFM version selected
The DIGITAL AFM is based on selected data and operation information relating to PC-12/41, PC-12/45, PC-12/47 and PC-12/47E aircraft contained in the Airplane Flight Manual (AFM), which is a part of the Pilots Operating Handbook (POH) report No. 01973 at revision 019 [POH section 5 and 6] for PC-12/41 and PC-12/45 , report No. 02211 at revision 011 [POH section 5, 6, 9 and supplement 33] for PC-12/45 and PC-12/47 and report No.02277 at revision 015 [POH section 5 and 6] for 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 CONTRADICTIONS THE POH SHALL PREVAIL OVER THE DIGITAL AFM.
THIS DIGITAL AFM DOES NOT RELEASE THE OPERATOR IN ANY WAY FROM HIS OBLIGATION TO STRICTLY COMPLY IN ALL RESPECTS WITH THE APPROVED POH AND ALL OF ITS REVISIONS AND TO KEEP HIMSELF UPDATED ON A CURRENT BASIS OF ANY SUCH REVISIONS.
No update of the DIGITAL AFM 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 definitely be implemented.
PILATUS REJECTS ALL AND ANY RESPONSIBILITY OR LIABILITY for the completeness and/or accuracy of the DIGITAL AFM. This DIGITAL AFM 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-12/41, PC-12/45, PC/12-47 and PC-12/47E aircraft and PILATUS REJECTS ALL AND ANY LIABILITY with respect to any handling, maintenance and/or operation of the PC-12/41, 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