As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE NACELLE OVERHEAT. *S/D* ENGINE 2.95 STABILITY BLEED VALVE WAS OPEN ON TAKEOFF. REPLACED 2.95 STABILITY BLEED VALVE, 2.95 BLEED SOLENOID AND 2.95 BLEED PNEUMATIC RELAY VALVE. SOLENOID AND RELAY VALVES TESTED OK. THE 2.95 BLEED VALVE WAS FOUND LEAKING AT THE PISTON RING SEALS PW75-130, WHICH IS ACCOMPLISHED AT VALVE OVERHAUL IMPROVES VALVE PISTON RING SEALS.