Garmin GTX 33 Installation Manual - Page 52

A-1. Upward Static Load Test, GTX 33 Installation Manual, A-2, Rev. F

Get Garmin GTX 33 PDF manuals and user guides View all Garmin GTX 33 manuals
Add to My Manuals
Save this manual to your list of manuals

Page 52 highlights

6. Hook a calibrated force gauge through both loops and apply a sustained pull for at least 3 seconds in each of the other three directions (upward, sideward and forward) at the above calculated forces (i.e. 25.8 lb. upward, 19.4 lb. sideward and 77.4 lb. forward). 7. Examine the support structure carefully. If there has been damage or permanent deformation, the structure is not suitable and must be replaced with one that is strong enough to withstand the test loads. Examine all aircraft stringers, bulkheads and skin surfaces, which may have direct or indirect contact with the fabricated shelf. If it is determined that no damage or permanent deformation has occurred, the structure is of sufficient strength and the GTX 33 equipment rack may be permanently mounted on it. Figure A-1. Upward Static Load Test Figure A-2. Forward Static Load Test GTX 33 Installation Manual Page A-2 190-00906-00 Rev. F

  • 1
  • 2
  • 3
  • 4
  • 5
  • 6
  • 7
  • 8
  • 9
  • 10
  • 11
  • 12
  • 13
  • 14
  • 15
  • 16
  • 17
  • 18
  • 19
  • 20
  • 21
  • 22
  • 23
  • 24
  • 25
  • 26
  • 27
  • 28
  • 29
  • 30
  • 31
  • 32
  • 33
  • 34
  • 35
  • 36
  • 37
  • 38
  • 39
  • 40
  • 41
  • 42
  • 43
  • 44
  • 45
  • 46
  • 47
  • 48
  • 49
  • 50
  • 51
  • 52
  • 53
  • 54
  • 55
  • 56
  • 57
  • 58
  • 59
  • 60
  • 61
  • 62
  • 63
  • 64
  • 65
  • 66
  • 67
  • 68
  • 69
  • 70
  • 71
  • 72
  • 73
  • 74
  • 75
  • 76
  • 77
  • 78
  • 79
  • 80
  • 81
  • 82
  • 83
GTX 33 Installation Manual
190-00906-00
Page A-2
Rev. F
6.
Hook a calibrated force gauge through both loops and apply a sustained pull for at least 3
seconds in each of the other three directions (upward, sideward and forward) at the above
calculated forces (i.e. 25.8 lb. upward, 19.4 lb. sideward and 77.4 lb. forward).
7.
Examine the support structure carefully. If there has been damage or permanent deformation, the
structure is not suitable and must be replaced with one that is strong enough to withstand the test
loads. Examine all aircraft stringers, bulkheads and skin surfaces, which may have direct or indi-
rect contact with the fabricated shelf. If it is determined that no damage or
permanent deformation has occurred, the structure is of sufficient strength and the GTX 33 equip-
ment rack may be permanently mounted on it.
Figure A-1. Upward Static Load Test
Figure A-2. Forward Static Load Test