What was found
CREW ESCAPE HATCH STEP PROFILE AND EDGE GAPS TO FUSELAGE SKIN ARE OUT OF LIMITS. ADJUSTMENT OF THE CREW ESCAPE HATCH CARRIED OUT IAW CRJ MM 52-22-00. NO FAULTS FOUND ON FUNCTIONAL TEST OF CREW ESCAPE HATCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CREW ESCAPE HATCH STEP PROFILE AND EDGE GAPS TO FUSELAGE SKIN ARE OUT OF LIMITS. ADJUSTMENT OF THE CREW ESCAPE HATCH CARRIED OUT IAW CRJ MM 52-22-00. NO FAULTS FOUND ON FUNCTIONAL TEST OF CREW ESCAPE HATCH.