Export Control
EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.Copyright
© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).Applicability
All
Common Information
TASK 73-22-49-200-404 Fuel System Air Tubes - Related Parts - Examine The Fuel System Air Tubes Bracket, Inspection-004
General
This TASK gives the procedure for the inspection of the fuel system air tube brackets. For the other fuel system air tubes and parts, refer to Inspection-000 TASK 73-22-49-200-400 and Inspection-000 TASK 73-22-49-200-100 in the Component Maintenance Manual (CMM-THDV2500- 1IA).
Fig./item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig./item numbers are used. For the Service Bulletin alpha variants refer to the IPC.
The policy that is necessary for Inspection is given in the SPM TASK 70-20-01-200-501.
All the parts must be cleaned before they are examined. Refer to Cleaning-000 TASK 73-22-49-100-400.
All the parts must be visually examined for damage, corrosion and wear. Any defects that are not identified in the procedure must be referred to IAE.
The procedure for those parts which must have a crack test is given in the relevant SUBTASK. Do the crack test before the part is visually examined.
Do not discard a part until you are sure there are no repairs available. Refer to the instructions in repair before a discarded part is used again or oversize parts are installed.
Parts which must be discarded can be held although no repair is available. The repair of a discarded part could be shown to be necessary at a subsequent date.
All parts must be examined to make sure that all the repairs are completed satisfactorily.
Practices and processes referred to in the procedure by the TASK/SUBTASK number are in the SPM.
NOTE
References
Refer to the SPM for data on these items:
Definitions of Damage - Specified Types of Damage, SPM TASK 70-02-02-350-501,
Inspection Policy and Inspection of Parts, SPM TASK 70-20-01-200-501.
Some data on these items is contained in this TASK. For more data on these items refer to the SPM:
Methods of Testing for Crack Indications
Chemical Processes
Surface Protection
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
NONESpares
NONESafety Requirements
NONEProcedure
Refer to Cleaning-001 TASK 73-22-49-100-401.
Clean the brackets.
Refer to SPM TASK 70-23-02-230-501.
Brackets.
Reject.
Cracked.
Do a crack test of the parts that follow.
SUBTASK 73-22-49-220-107 Examine the Bracket for Cracks
SUBTASK 73-22-49-220-108 Examine the Surface of the Brackets
Reject.
Rivets loose or missing.
Examine the rivets.
SUBTASK 73-22-49-220-151-001 Examine the Rivets on Bracket (03-800, 5A9169) (Pre SB 70-0101)
Reject.
Rivets loose or missing.
Examine the rivets.
SUBTASK 73-22-49-220-151-002 Examine the Rivets on Bracket (03-800, 5A0834) (SB 70-01-0101)
Reject.
Bolt hole burred.
Reject.
Other than in Step.
Worn.
Examine the EEC inlet duct mounting holes.
NOTE
The hole position is on each side of the tube bracket adjacent to the three tube holes.
SUBTASK 73-22-49-220-109 Examine the Bracket Bolt Holes (03-800, 5A9169) and (03-800, 5A0834) (Pre SB 70-0101) (SB 70-0101)
Reject.
Other than in Step.
Worn.
Examine the hole.
NOTE
The clip position is adjacent to the square cut-out.
SUBTASK 73-22-49-220-157-001 Examine the Clip Position Bolt Hole (03-800, 5A9169) (Pre SB 70-0101)
Accept.
If the hole diameter is between 0.255 in. (6.50 mm) and 0.270 in (6.86 mm).
Reject.
If the diameter is larger than 0.270 in (6.86 mm).
Worn.
Examine the hole.
SUBTASK 73-22-49-220-157-002 Examine the Clip Position Bolt Hole (03-800, 5A0834) (SB 70-0101)
Accept.
If the hole diameter is between 0.214 in (5.45 mm) and 0.226 in (5.75 mm).
Reject.
If the diameter is larger than 0.226 in (5.75 mm).
Worn.
Examine the hole.
SUBTASK 73-22-49-220-157-003 Examine the Clip Position Bolt Hole (03-800, 6A7420) (SB 73-0140)
Reject.
Other than in Step.
Worn.
Examine the holes.
SUBTASK 73-22-49-220-155-001 Examine the Mounting Flange Bolt Hole (03-800, 5A9169) and (03-800, 5A0834) (Pre SB 70-0101) (SB 70-0101) (Pre SB 73-0140)
Accept.
If the hole diameter is between 0.284 in (7.20 mm) and 0.290 in (7.38 mm).
Reject.
If the diameter is larger than 0.290 in (7.38 mm).
Worn.
Examine the holes.
SUBTASK 73-22-49-220-155-002 Examine the Mounting Flange Bolt Hole (03-800, 6A7420) (SB 73-0140)
Reject.
Other than in Step.
Worn.
Examine the holes.
SUBTASK 73-22-49-220-153-001 Examine the Electrical Receptacle Mounting Holes (03-800, 5A9169) and (03-800, 5A0834) (Pre SB 70-0101) (SB 70-0101) (Pre SB 73-0140)
Reject.
Other than in Step.
Worn.
Examine the holes.
SUBTASK 73-22-49-220-153-002 Examine the Electrical Receptacle Mounting Holes (03-800, 6A7420) (SB 73-0140)
Reject.
Tube hole burred.
Accept.
If the hole diameter is 0.570 in. (14.5 mm).
Reject.
If the diameter is larger than 0.570 in. (14.5 mm)
Worn.
Examine the tube mounting hole in bracket.
SUBTASK 73-22-49-220-110-001 Examine the Tube Mounting Hole on the Bracket (03-800, 5A9169) and (03- 800, 5A0834) (Pre SB 70-0101) (SB 70-0101) (Pre SB 73-0140)
Reject.
Tube hole burred.
Accept.
If the hole diameter is 0.570 in. (14.5 mm).
Reject.
If the diameter is larger than 0.570 in. (14.5 mm).
Worn.
Examine the tube mounting hole in the bracket.
SUBTASK 73-22-49-220-110-002 Examine the Tube Mounting Hole on the Bracket (03-800, 6A7420) (SB 73-0140)
