Page:CAB Accident Report, Pennsylvania Central Airlines Flight 19.pdf/28

 The dome of the left propeller had an impression in it about six inches in diameter, apparently caused by impact. All three blades of this propeller had been broken off close to the shank. Two blades had the tips torn off and were otherwise badly bent and twisted. The third blade was located some 1800 feet from the point of impact and, while it was intact, it was quite badly twisted in the form which would indicate a power bend. The gear segments on all three blades of the left propeller were split in the same way as those on the right. The rotating cams on both propellers had stopped in a position which would indicate to a pitch angle of the blades of about 24 degrees.

The National Bureau of Standards examined the propeller parts and reported that there was no evidence of mechanical, structural or fatigue failure or lightning strike prior to impact.

All radio equipment, including receivers, transmitter, accessories, and antennae systems, was badly damaged. Careful inspection failed to reveal any arcing or burning effect which might to expected from a lightning strike. The anti-static discharge cartridge had not been discharged. The anti-static loop antenna was adjusted in the anti-static position (parallel with the fuselage). The loop tuning dial was turned to the Richmond radio range. Minute inspection of all wiring did not indicate any burning or fusing. Only one the pilots' radio headbands was found and it was badly twisted. None of the radio earphones was found. These parts, composed of hard rubber, may have completely disintegrated at the time of impact.