20010306005709I

Incident · Substantial damage

FAA incident report · Dhav DHC-8-102 · Portland, OR · March 6, 2001

Date
March 6, 2001 · 07:53 local
Place
Portland, OR
Airport
Portland International
Phase of flight
Normal Cruise
Operating rules
Air carrier (Part 121)
Operator
QXEA
Damage
Substantial damage
Aircraft
N822PH
NTSB investigation
NTSBSEA01FA059
Reported as
Dhav DHC8102
Reported engine
Pratt & Whitney PW120A
People aboard
33
Fatal injuries
0
Pilot’s flight hours
6,240 total3,789 in this make and model201 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) A/c enroute from sea to pdx, crew noticed vibration on #2 engine and smell of smoke in cabin. Crew declared an emergency and landed at pdx. During rollout the #2 engine fire warning came on, fire bottles were emptied into the engine and the crew and passengers evacuated the plane. During post event inspection it was noted that the #5 bearing had failed and caused a fire in the bearing breather cavity that eventually caused the failure of an external breather line allowing the fire to enter the engine nacell. Damage was limited to the nacell.

As the FAA filed it

(-23) A/C ENROUTE FROM SEA TO PDX, CREW NOTICED VIBRATION ON #2 ENGINE AND SMELL OF SMOKE IN CABIN. CREW DECLARED AN EMERGENCY AND LANDED AT PDX. DURING ROLLOUT THE #2 ENGINE FIRE WARNING CAME ON, FIRE BOTTLES WERE EMPTIED INTO THE ENGINE AND THE CREW AND PASSENGERS EVACUATED THE PLANE. DURING POST EVENT INSPECTION IT WAS NOTED THAT THE #5 BEARING HAD FAILED AND CAUSED A FIRE IN THE BEARING BREATHER CAVITY THAT EVENTUALLY CAUSED THE FAILURE OF AN EXTERNAL BREATHER LINE ALLOWING THE FIRE TO ENTER THE ENGINE NACELL. DAMAGE WAS LIMITED TO THE NACELL.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N822PH · 3

Matched to the same aircraft by N-number and date.