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|
Attributes | |
ACN | 1751873 |
Time | |
Date | 202007 |
Local Time Of Day | 0601-1200 |
Place | |
Locale Reference | N90.TRACON |
State Reference | NY |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | Hawker 900 |
Operating Under FAR Part | Part 135 |
Flight Phase | Climb |
Route In Use | Vectors |
Flight Plan | IFR |
Component | |
Aircraft Component | Fire/Overheat Warning |
Person 1 | |
Function | Captain Pilot Flying |
Qualification | Flight Crew Multiengine Flight Crew Air Transport Pilot (ATP) Flight Crew Instrument |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy Deviation - Procedural Weight And Balance |
Narrative:
Captain and I were flying aircraft X on a 135 leg between ZZZ and ZZZ1. Prior to this leg; we had repositioned the aircraft from ZZZ2 without incident. Due to the leg length; we fueled with 9;000 lbs. Of fuel prior to departure. During climbout; at approximately 7;000 ft. MSL; the master warning system flashers activated; followed shortly thereafter by a rear bay overheat indication. The indication went away after a few (less than 10) seconds; followed by a reactivation of the mws with no rear bay overheat indication. I was the pilot flying while captain was pilot monitoring. I continued to fly while he handled the other duties. I believed the best course of action was to get the aircraft on the ground as soon as practicable; my training and systems knowledge (the bay overheat sensor is part of the fire detection and suppression system) led me to believe that this is an emergency detection system without a suppression component; I.e there is no way to mitigate the effects of the overheat condition other than closing the air bleed valves. I knew that we would be faced with an overweight landing condition since we had just departed with a takeoff weight approximately 3;000 lbs. Above maximum landing weight. For that reason; I advocated landing at an airport with a long runway; the closest of which was ZZZ3. Since the indication had gone away we did not request priority handling with ATC. Approach and landing were made without incident; and in accordance with the overweight landing checklist. I explained the situation to the passengers once we landed and conducted an exterior walkaround of the aircraft; with no abnormalities noted. Landing weight was approximately 26;000 lbs.at the time of the incident; I was under the impression that the memory items for this indication had been completed; however since then I have learned that there was a delay in the event and completing the memory items. Obviously; I should have been aware of this at time of the incident and represents less than optimal communication between ourselves. I do not however; believe this would have impacted the ultimate decision; which was to terminate the flight based on an emergency indication. To have continued the flight; or to have delayed landing after such an indication in the interest of continuity of an operation; would have been unwise.
Original NASA ASRS Text
Title: Captain reported a Rear Bay Overheat Warning; causing a diversion.
Narrative: Captain and I were flying Aircraft X on a 135 leg between ZZZ and ZZZ1. Prior to this leg; we had repositioned the aircraft from ZZZ2 without incident. Due to the leg length; we fueled with 9;000 lbs. of fuel prior to departure. During climbout; at approximately 7;000 ft. MSL; the Master Warning System flashers activated; followed shortly thereafter by a REAR BAY OVERHEAT indication. The indication went away after a few (less than 10) seconds; followed by a reactivation of the MWS with no REAR BAY OVERHEAT indication. I was the pilot flying while Captain was Pilot Monitoring. I continued to fly while he handled the other duties. I believed the best course of action was to get the aircraft on the ground as soon as practicable; my training and systems knowledge (the bay overheat sensor is part of the Fire Detection and Suppression system) led me to believe that this is an emergency detection system without a suppression component; I.e there is no way to mitigate the effects of the overheat condition other than closing the air bleed valves. I knew that we would be faced with an overweight landing condition since we had just departed with a takeoff weight approximately 3;000 lbs. above maximum landing weight. For that reason; I advocated landing at an airport with a long runway; the closest of which was ZZZ3. Since the indication had gone away we did not request priority handling with ATC. Approach and landing were made without incident; and in accordance with the overweight landing checklist. I explained the situation to the passengers once we landed and conducted an exterior walkaround of the aircraft; with no abnormalities noted. Landing weight was approximately 26;000 lbs.At the time of the incident; I was under the impression that the memory items for this indication had been completed; however since then I have learned that there was a delay in the event and completing the memory items. Obviously; I should have been aware of this at time of the incident and represents less than optimal communication between ourselves. I do not however; believe this would have impacted the ultimate decision; which was to terminate the flight based on an emergency indication. To have continued the flight; or to have delayed landing after such an indication in the interest of continuity of an operation; would have been unwise.
Data retrieved from NASA's ASRS site 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.