TO 00-25-172 - Robins Air Force Base

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TO 00-25-172 Figure 4-2. Aircraft Tire Servicing 4-24
TO 00-25-172 CHAPTER 5 CONCURRENT SERVICING OPERATIONS 5.1 CONCURRENT SERVICING OF AIRCRAFT. NOTE On KC-135, MAF and Commercial aircraft, concurrent servicing is not required unless refueling/ defueling with JP-4, loading/downloading munitions or explosives, or servicing LOX while performing maintenance. Simultaneous servicing of fuel while loading passengers and cargo, performing maintenance, aircrew members performing inspections, or operating aircraft systems is considered to be a normal servicing operation. Restrictions listed in Paragraph 5.6 and Paragraph 5.7 still apply. Concurrent servicing is defined as the simultaneous servicing of fuel or oxygen with either passengers on board or the performance of minor maintenance, fleet servicing, or baggage or cargo loading/unloading. Refer to Chapter 6 for CSOs supporting the A-10, F-15, F-16 and F-22 aircraft. Concurrent servicing of aircraft with JP-4 or Jet B aircraft will require completion and approval of a System Safety Engineering Analysis (SSEA). As long as the provisions of this chapter are followed, a SSEA is no longer required for concurrent servicing of aircraft with high flashpoint fuels. Servicing operations pertaining to these aircraft when accomplished on a USAF installation are under the direct control of the USAF and will be accomplished in accordance with the provisions of this technical order. Fuel servicing and concurrent servicing of these aircraft will be done using approved checklists. Cargo containing explosives, oxygen or flammable gases or liquids shall not be loaded or unloaded during concurrent servicing operations. A Chief Servicing Supervisor (CSS) shall be provided by the USAF for all concurrent fuel servicing of contract airlift missions at military installations. 5.2 PERSONNEL REQUIREMENTS FOR FUEL SERVICING. Simultaneous fuel and oxygen servicing on an aircraft is NOT authorized. Defueling during concurrent operations shall be limited to the single point method (closed fuel system). C-130 and C-141 troop doors and emergency hatches on the right SPR, side of the aircraft must be closed during concurrent servicing operations to isolate the cargo compartment from the fuel servicing safety zone. The Air Force fuel servicing team will consist of the following: a. Chief Servicing Supervisor (CSS). b. SPR Monitor (SPRM) for each SPR in use (contractor aircrew member when servicing contract commercial carriers). 2F0X1 personnel trained and certified using MDS applicable procedures, or equivalent current training program, may perform simultaneous duty as both SPRM and fuels specialist. c. A refueling panel monitor (when the refueling panel and the SPR are adjacent to each other, one individual may monitor both). d. Fuel Specialists (2F0X1). e. Passenger compartment monitor, i.e., aircrew member (when passengers on board). 5.3 RESPONSIBILITIES OF CSS. a. Normal concurrent servicing operations. (1) A Chief Servicing Supervisor (CSS) shall be present during concurrent operations. The CSS will primarily be stationed at the nose of the aircraft and will monitor the wing fuel vent outlets on the opposite side of the aircraft from the SPR location. A transient alert individual can also function as a CSS. The CSS can be either a USAF employee or a contractor support employee. (2) When servicing is performed by contract, contractor personnel functioning as the CSS must have experience comparable to that required for an Air Force CSS. Base or unit commanders shall assure that the contractor’s CSS has the required experience and capability. (3) The CSS will wear a reflective vest with the letters CSS on the front and back. The letters will be at least six inches in height and four inches wide and made of reflective material at least one 5-1
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TO 00-25-172 TECHNICAL MANUAL GROUN
Page 3 and 4:
TO 00-25-172 TABLE OF CONTENTS Chap
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TO 00-25-172 TABLE OF CONTENTS - CO
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TO 00-25-172 FOREWORD 1 PURPOSE. Th
Page 9: TO 00-25-172 List of Related Public
Page 13 and 14: TO 00-25-172 CHAPTER 1 INTRODUCTION
Page 15 and 16: TO 00-25-172 mishap (accident or in
Page 17 and 18: TO 00-25-172 CHAPTER 2 ELECTROSTATI
Page 19 and 20: TO 00-25-172 (2) Undergoing electro
Page 21: TO 00-25-172 loss of continuity. Th
Page 24 and 25: TO 00-25-172 This supervisor shall
Page 26 and 27: TO 00-25-172 Figure 3-2. Fighter Re
Page 28 and 29: TO 00-25-172 In freezing weather, t
Page 30 and 31: TO 00-25-172 plicable information i
Page 32 and 33: TO 00-25-172 Table 3-1. Fire Protec
Page 34 and 35: TO 00-25-172 Table 3-1. Fire Protec
Page 37 and 38: TO 00-25-172 CHAPTER 4 FLIGHT LINE
Page 39 and 40: TO 00-25-172 for under-wing fuel se
Page 41 and 42: TO 00-25-172 Table 4-1. Approved/Au
Page 43 and 44: TO 00-25-172 plicable to aircraft d
Page 45 and 46: TO 00-25-172 the area. During servi
Page 47 and 48: TO 00-25-172 Figure 4-1. Hardened/P
Page 49 and 50: TO 00-25-172 c. Cargo aircraft load
Page 51 and 52: TO 00-25-172 equipment. The followi
Page 53 and 54: TO 00-25-172 shoes which fit closel
Page 55 and 56: TO 00-25-172 • Do not direct gase
Page 57 and 58: TO 00-25-172 4.24 HYDRAZINE HANDLIN
Page 59: TO 00-25-172 vice some aircraft, e.
Page 63 and 64: TO 00-25-172 (20) Prior to beginnin
Page 65 and 66: TO 00-25-172 poppet valve in the op
Page 67 and 68: TO 00-25-172 stitute of Petroleum (
Page 69: TO 00-25-172 Table 5-1. Concurrent
Page 72 and 73: TO 00-25-172 craft -6 TO inspection
Page 74 and 75: TO 00-25-172 Table 6-1. Hot Refueli
Page 76 and 77: TO 00-25-172 Table 6-1. Cla-Val Mod
Page 78 and 79: TO 00-25-172 6.10 EMERGENCY PROCEDU
Page 80 and 81: TO 00-25-172 Table 6-2. Provider EC
Page 82: TO 00-25-172 drums at a fuel system
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