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
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Common Information
TASK 30-21-49-200-103 Anti-Ice Venturi Duct - Examine, Inspection-003
Effectivity
FIG/ITEM | PART NO. |
01-070 | 740-5151-513 |
01-070 | 745-5151-501 |
01-070 | 745-5151-503 |
01-070 | 740-5183-501 |
01-070 | 740-5183-503 |
General
This TASK gives the procedure for the inspection of the anti-ice duct venturi.
Fig/item numbers in parentheses in the procedure agree with those used in the IPC.
The policy that is necessary for inspection is given in the SPM TASK 70-20-00-200-501.
All the parts must be cleaned before any part is examined. Refer to Cleaning-000 TASK 30-21-49-100-100.
All 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 Step Do the test before the part is visually examined.
Do not discard any 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 should be discarded can be held although no repair is available. The repair of a discarded part could be shown to be necessary at a later date.
All parts must be examined to make sure that all the repairs have been completed satisfactorily.
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
References
Refer to the SPM for data on these items.
Definitions of Damage, SPM TASK 70-02-02-350-501.
Record and Control of the Lives of Parts, SPM TASK 70-05-00-220-501.
Inspection of Parts, SPM TASK 70-20-00-200-501.
Some data on these items is contained in this TASK. For more data on these items refer to the SPM.
Method of Testing for Crack Indications.
Chemical Processes.
Surface Protection.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
NONESpares
NONESafety Requirements
NONEProcedure
Reject.
Cracked.
Reject.
Defective weld.
Fluorescent penetrant examine for cracks. Refer to SPM TASK 70-23-01-230-501.
SUBTASK 30-21-49-230-053 Examine the Anti-Ice Duct Venturi (01-070) and all Welds for Cracks
Refer to Figure.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Up to 0.004 in. (0.10 mm) deep.
Reject.
More than in Step.
Nicked.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Up to 0.004 in. (0.10 mm) deep.
Reject.
More than in Step.
Scratched.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Up to 0.004 in. (0.10 mm) deep.
Rubbed.
Reject.
Dented.
SUBTASK 30-21-49-220-057 Examine the Anti-Ice Duct Venturi (01-070) at Location R
Refer to Figure.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Up to 0.010 in. (0.25 mm) deep.
Reject.
More than in Step.
Nicked.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Up to 0.010 in. (0.25 mm) deep.
Reject.
More than in Step.
On all areas of the support ring, except the seal face, location X.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Circumferential scratches up to 0.010 in. (0.25 mm) deep.
Reject.
Other than in Step.
Scratches on the seal face X.
Scratched.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Burred.
Reject.
Any distortion of the support lugs Y.
Distorted.
SUBTASK 30-21-49-220-058 Examine the Support-Ring W of the Anti-Ice Duct Venturi (01-070)
Refer to Figure.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Up to 0.010 in. (0.25 mm) deep.
Reject.
More than in Step.
On the edge Q and the faces K and P.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Circumferential scratches up to 0.010 in. (0.25 mm) deep.
Reject.
Other than in Step.
On the seal faces L and N.
Scratched.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Burred.
Repair, VRS2858 (Repair-003) TASK 30-21-49-300-003.
Up to 0.010 in. (0.25 mm) deep.
Reject.
More than in Step.
On the edge Q and the faces K and P.
Nicked.
Reject.
Any distortion of the end fittings.
Distorted.
Reject.
Any damage of the seal faces L and N.
Damaged.
SUBTASK 30-21-49-220-059 Examine the End Fittings of the Anti-Ice Duct Venturi (01-070)
Figure: Locations on the Anti-Ice Duct Venturi (01-070)
Locations on the Anti-Ice Duct Venturi (01-070)

Figure: Locations on the Anti-Ice Duct Venturi (01-070)
Locations on the Anti-Ice Duct Venturi (01-070)

