EFTA01198313.pdf

Gulfstream A OENEHAL DYNAMICS COMPANY MEMORANDUM Check Boxes as Appropriate Action Date: June 25, 2015 Information Only Reply Requested To: James White cc: Steve Forman, Michele Nierenberg, John Maxon, Paul Conti. Scott Kendall, Michael Clune, Alex Cameron, Justin Janzen From: Charles Roberts, II Job #AC-15-076 MV-I5-077 Subject: A/C 1085 Cabin Vibration Investigation Attachments: High Speed Vibration and Cabin Noise Data Introduction The owner of CV s/n 1085 has been experiencing high levels of low frequency vibration during the climb and cruise phase of flight. The customer scheduled a "drop in" visit to the GAC Brunswick Service Center on 06/19/2015 to perform a maintenance flight to identify the source of the vibration. Summary Accelerometers were placed on the pilot inboard seat track, the copilot inboard seat track, the Window 2 left outboard seat track, and the Window 2 right outboard seat track. A microphone was placed at the Window 2 center position. Engine vibration data was acquired from the left and right broadband outputs located in the forward left and right radio racks. A normal taxi and take-off was executed. Data was recorded during a normal climb up to 45000 feet. Results Analysis of the recorded data showed a 12/ harmonic on the left engine's Ni spool during climb through 36000 feet. The frequency of the 12/ harmonic was 61.7 Hz with a vibration level of 0.16 in/s and a sound pressure level of 71.9 dB (Figures 1 & 2). The vibration was also measured on the Window 2 left and right outboard seat tracks (Figure 3). When the left engine was decelerated to idle, the 12/ NI harmonic went away. During climb, the left engine's NI vibration levels were as high as 0.14 in/s and the right engine's Ni vibration levels were as high as 0.20 in/s. Recommendation To mitigate the felt vibration during climb to 45000 feet, it is recommended to perform a 180° clocking of the left engine fan followed by a fan trim-balance on both engines. The fan trim- balance should achieve NI vibration levels no greater than 0.10 in/s from MCT to idle on both engines. Job #AC-15-076 GAO Acoustics/Vibration FS-AN-15-077 6/25/2015 EFTA01198313 Gulfstream A CIENEHAL DYNAMICS COMPANY MEMORANDUM NOTE: Performing Vibration Surveys and Fan Trim Balancing in windy conditions can produce inaccurate vibration measurements that may lead to erroneous balancing solutions. If these actions must be performed in windy conditions, then the aircraft should be pointed nose-into-the- wind to minimize the effects. Data Acquisition The engine vibration was recorded using the EVM broadband B-n-C outputs located in the upper left and right radio racks. Engine vibration was measured with the primary and secondary accelerometers located on the engine's fan case. The primary and secondary accelerometers were oriented in the in-service position in the radial direction. The engine accelerometers measure acceleration, which is integrated by the on-board signal conditioning unit, to obtain velocity. Thus, the measured output form the maintenance port is velocity, not acceleration. Data Reduction The recorded data was processed using the ArtemiS Clasic software package which was developed by Head Acoustics. This software package provides a spectrogram and a peak hold spectrum plot of the acoustic and vibration data. Job #AC-15-076 GAO Acoustics/Vibration FS-AN-15-077 6/25/2015 EFTA01198314 Left Engine Vibration During Climb Up To 45000 feet 5,5.551.1 i 0.00389.96,E . ..15,....15355.50.0,....5 300 150 100 50 rlinls ISM O., 5 11 1111 kinW=INI 171111 111W1==rANWA , 50,5 'WENI NVAINEWIRMEIMMIANY New Figure 1 Gulfstivam EFTA01198315  Sound Pressure Level at Window 2 Center 0.5C2261.1 ( 0.00323.36 O.FFT vs. Time (16321.50.09,HAN) 9112 300 250 200 150 100 SO 1,11519P14 90 rillIEM=1 41= 80 1111M7LIMM21 40 801 -_ Gulfs-tram EFTA01198316 Vibration Measured on Seat Tracks REC236I 1 (0 00.383 36 8)687 (peak hold)lp02816384 50.0Y,HAN) a(g 20m 7.5,8 15m (2.5m 00.1 7.501 5m 2.5m SO 100 200 2.53 30L Ch 3 Pilot Inboard Seat Track Ch 4 Co-Pilot Inboard Seat Track Ch 5 Window 2 Left Outboard Seat Track Ch 6 Window 2 Right Outboard Seat Track Figure 3 GulfstirAm EFTA01198317