G III first officer reported an engine failure climbing through FL350 and is shortly thereafter info...

Attributes
ACN	878505
Time
Date	201003
Local Time Of Day	1201-1800
Place
Locale Reference	ZZZ.Airport
State Reference	US
Environment
Flight Conditions	VMC
Light	Daylight
Aircraft 1
Make Model Name	Gulfstream III (G1159A)
Operating Under FAR Part	Part 135
Flight Phase	Climb
Flight Plan	IFR
Component
Aircraft Component	Cabin Window
Person 1
Function	Pilot Flying First Officer
Person 2
Function	Captain Pilot Not Flying
Qualification	Flight Crew Multiengine Flight Crew Instrument Flight Crew Flight Instructor Flight Crew Air Transport Pilot (ATP)
Experience	Flight Crew Last 90 Days 121 Flight Crew Total 3000 Flight Crew Type 1037
Events
Anomaly	Aircraft Equipment Problem Critical

Narrative:

During climb through approximately 35;000 ft; we heard what sounded like a compressor stall followed by a loss of power from the right engine. We were told that part of the exterior pane of the fourth window on the right side of the aircraft had departed the aircraft. We assumed that the pane was ingested into the right engine. There was no loss of pressurization and we decided not to attempt an engine restart due to probable FOD contamination. At this point we declared an emergency; executed all appropriate checklists and began a normal descent so as not to induce any additional stress on the remaining pane. We determined that the best destination given our descent rate and altitude was to return to departure airport. The flight distance allowed for us to continue our normal safe rate of descent at near idle power. We considered alternate destinations for our landing but determined that any alternate would have required the same amount of time to descend. We were vectored for a visual approach and landed uneventfully in good weather.

Original NASA ASRS Text

Title: G III First Officer reported an engine failure climbing through FL350 and is shortly thereafter informed that the outer pane of a cabin window had departed the aircraft on that side. An emergency was declared and flight returned to their departure airport.

Narrative: During climb through approximately 35;000 FT; we heard what sounded like a compressor stall followed by a loss of power from the right engine. We were told that part of the exterior pane of the fourth window on the right side of the aircraft had departed the aircraft. We assumed that the pane was ingested into the right engine. There was no loss of pressurization and we decided not to attempt an engine restart due to probable FOD contamination. At this point we declared an emergency; executed all appropriate checklists and began a normal descent so as not to induce any additional stress on the remaining pane. We determined that the best destination given our descent rate and altitude was to return to departure airport. The flight distance allowed for us to continue our normal safe rate of descent at near idle power. We considered alternate destinations for our landing but determined that any alternate would have required the same amount of time to descend. We were vectored for a visual approach and landed uneventfully in good weather.

Data retrieved from NASA's ASRS site as of April 2012 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.

G III first officer reported an engine failure climbing through FL350 and is shortly thereafter informed that the outer pane of a cabin window had departed the aircraft on that side. An emergency was declared and flight returned to their departure airport.