nacelle damage description - Taca International Airlines

ENGINEERING ORDER
EO. No:
A320PR54-029/13 R0
Rev. Date:
05/17/2013
Date: 05/17/2013
Pag 2 of 15
EFFECTIVITY:
P/N
AIRCRAFT MODEL /
COMPONENT
FAN COWL DOOR
745-4000-503
REFERENCES:
S/N
5470001
REMARKS
Currently installed on A/C N522TA - MSN
5219
COMPLIANCE
/A/
TACA EO A320TR54-027/13
NONE
/B/
TACA EO A320IN54-028/13
NONE
/C/
RDAS: ROHR/S067/2013 Issue A
PCW
/D/
TACA Message: TAI-SAL-13-051713/000
NONE
/E/
Message between Goodrich and TACA: Dated 20/09/2013
FCW
DUE DATE:
On or before the A/C reaches 1666 FC
FORM QA-073/96 TS-F R0
ENGINEERING ORDER
EO. No:
Date: 05/17/2013
A320PR54-029/13 R0
Rev. Date:
05/17/2013
DISTRIBUTION LIST
(Planning will distribute all copies)
Pag 3 of 15
PUBLICATIONS AFFECTED
Chapter
Technical Records
..............
Stockroom
..............
Reliability
..............
Line Maintenance
..............
Hangar Maintenance
..............
Flight Operations
..............
Quality Control
..............
Quality Assurance
..............
Technical Publicactions
..............
Warranty
..............
Other
..............
None
Publications
None
X
X
Comments:
None.
SUPPORT DOCUMENTATION
DOCUMENT NUMBER
DOCUMENT TYPE
TITLE
12-34-24 PB 201
AMM
Aircraft Grounding
54-20-00 Repair 004
Goodrich SRM
FAN COWL HONEYCOMB DENT REPAIR
LABOR ESTIMATE:
SKILLS:
CREW:
MAN-HRS:
ELAPSED:
STR
1
3
3
INS
1
1
0
2
4
3
TOTAL:
FORM QA-073/96 TS-F R0
ENGINEERING ORDER
EO. No:
Date: 05/17/2013
A320PR54-029/13 R0
Rev. Date:
05/17/2013
Pag 4 of 15
PARTS AND MATERIALS (Per Unit)
PART NUMBER
DESCRIPTION
QTY
UNIT
P.O./M.R.
REMARKS
01428
LPS PRESOLVE
1
Gal
Or alternative. Use as required
WDC
WHITE WIPE
8
Oz.
use as required.
BJO-0930
PHENOLIC MICROBALLON
1
Lbs
Use as required
1635477
LIJA 240
3
EA
Or alternative. Use as required
30002
MARKING PEN
1
EA
Use as required
EA934NA
EPOXI RESIN QUART KIT
1
KIT
Alternative PN CG-1305A/B can be
used. Use as required.
TOOLS
PART NUMBER
None
DESCRIPTION
QTY
P.O.
REMARKS
None
FORM QA-073/96 TS-F R0
ENGINEERING ORDER
E.O. No:
Rev. No:
A320PR54-029/13
0
DATE:
PAGE:
05/17/2013
5 of 15
SUBJECT:
ATA 54 - FAN COWL - O/B FAN COWL DENTS - PERMANENT REPAIR
FREQUENCY:
TAIL:
STATION:
DATE:
N/A
MECHANIC
Q.C.
INSTRUCTIONS
XXX
XXX
ACCOMPLISHMENT INSTRUCTIONS
XXX
XXX
A. GENERAL
NOTE: Obey all of the WARNINGS and CAUTIONS included in the
referenced manuals and procedures.
XXX
XXX
B. JOB SET-UP
1. Make sure that the aircraft is electrically grounded as per AMM Task
12-34-24 PB 201.
XXX
2. Locate the O/B Fan Cowl Door installed on ENG #1.
3. Confirm the Fan Cowl data is P/N 745-4000-503 and S/N 5470001:
YES
NO
NOTE: In case answer is no, contact planning department for further
disposition.
4. Confirm the damage is according to ref. /D/.
YES [
]
NO [
]
If YES, continue with the next step
If NO, contact engineering department before further flight.
XXX
XXX
C. REPAIR INSTRUCTIONS
1.
Repair the dents separately by means of Goodrich SRM 54-20-00
Repair #4 “FAN COWL HONEYCOMB REPAIR”
NOTE: Heat lamps are to be used in order to apply heat to the
affected area when the curing of compound EA 934NA is to be
performed, use a thermometer in order to keep track of the
temperature.
FORM QA-073/96-TS-F R0
ENGINEERING ORDER
E.O. No:
Rev. No:
A320PR54-029/13
0
DATE:
PAGE:
05/17/2013
6 of 15
SUBJECT:
ATA 54 - FAN COWL - O/B FAN COWL DENTS - PERMANENT REPAIR
FREQUENCY:
TAIL:
STATION:
DATE:
N/A
MECHANIC
Q.C.
XXX
XXX
INSTRUCTIONS
D. CLOSE-UP
1.
Make sure that the work area is clean and clear of tools and
materials.
2.
Restore the aircraft to a normal operating condition.
XXX
XXX
End of this E.O.
XXX
XXX
The following step is for documentation purposes only and is not related to
the actual tasks performed on the subject aircraft
TECHNICAL RECORDS: Insert a copy of this Engineering Order in the
records of the subject aircraft and component.
Name: ______________________________
XXX
XXX
Title: _______________________________
Date: _______________________________
Signature: ___________________________
FORM QA-073/96-TS-F R0
A320PR54-029/13.R0
Ref. /C/
Page 07 of 15
A320PR54-029/13.R0
Ref. /D/
Page 08 of 15
Rohr, Inc., operating as Goodrich Aerostructures Group
NACELLE DAMAGE DESCRIPTION
AFTERMARKET TECHNICAL SERVICES ENGINEERING
850 Lagoon Drive, Chula Vista, CA 91910-2098
*DATE REQUIRED: 05/17/2013
REQUEST TYPE:
CRITICAL REPAIR (Work Stoppage)
AOG (2-4 Hrs) A/C LOCATION
EL SALVADOR
05/17/2013
ROUTINE REPAIR
A/C NEXT SCHEDULED FLIGHT
GENERAL INFORMATION
A/C TAIL REGISTRATION NUMBER N522TA
Inaccurate or missing information can result in delays. Please forward all other information available (photo, etc.) to help provide a clear and complete
damage description. Pictures may be inserted under the “Damage Description” section. For AOG Request, please contact the Goodrich Spares Sales
Desk at (619) 691-2089 or [email protected] and a response will be provided within 2 to 4 hours after receipt of the complete damage.
Important Note: All *RED highlighted blocks must contain an entry in order to process a repair request.
CUSTOMER INFORMATION
Maintenance Facilities Name: TACA AIRLINES
Date: 05/17/2013
*Operator:
TAI
Location:
EL SALVADOR C.A.
Contact:
Jorge Salinas
Ref No.:
TAI-SAL-13-051713/000
Tel:
(503) 2366-7544
Fax:
E-mail:
[email protected]
P.O. No.
AIRCRAFT INFORMATION
*Engine Type:
V2500-A5
*Aircraft Type:
A319-132
Engine S/N:
N/A
*Aircraft Registration:
N522TA
*Engine Position:
POSITION #1
*Aircraft MSN:
5219
Engine Flight Hours:
N/A
*Aircraft Flight Hours:
2598
Engine Flight Cycles:
N/A
*Aircraft Flight Cycles: 1166
PARTS INFORMATION
DESCRIPTION
*A/C Component:
*PART NUMBER
745-4000-503
*NAME
*SERIAL NUMBER
FAN COWL DOOR
5470001
Affected Part
Affected Part
Affected Part
*SUMMARY
During a routine inspection several dents were found on inboard fan cowl door outer skin of engine pos #1 as depicted in
Figure 1. The damage dimensions are out of repair scope in accordance with SRM.
*REPORT ANY PREVIOUS REPAIR IN THE DAMAGED AREA
NONE.
Rohr, Inc., a subsidiary of the Goodrich Corporation, operating as Goodrich Aerostructures Group
FORM NO. E8210-4
A320PR54-029/13.R0
Ref. /D/
Page 09 of 15
Rohr, Inc., operating as Goodrich Aerostructures Group
NACELLE DAMAGE DESCRIPTION
AFTERMARKET TECHNICAL SERVICES ENGINEERING
850 Lagoon Drive, Chula Vista, CA 91910-2098
DAMAGE DESCRIPTION
PAGE 2 OF 7
ENG POS #1 – FAN COWL DOOR (O/B) – OUTER SKIN – DENT DAMAGE
REFERENCES:
/A/ - Fan Cowl Door P/N 745-4000-503, S/N 5470001.
DESCRIPTION:
While performing a routine inspection on ref. /A/ several dents were found on outer skin. The damage
consists in 6 (EA) dents shown in Figure 1.
Refer to Figure 1 for location and details.
TACA kindly proposes to leave those dents (as depicted in Figure 1) “as is” for a period of 500 FC with
repetitive DVI inspection every 50 FC.
ACTION:
Based in the condition above described TACA kindly requests GOODRICH the following:
1. Please confirm if the proposal is acceptable as temporary repair for the damage conditions as
depicted in Figure 1.
2. An answer within 4 hours would be highly appreciated.
Best Regards.
Rohr, Inc., a subsidiary of the Goodrich Corporation, operating as Goodrich Aerostructures Group
FORM NO. E8210-4
A320PR54-029/13.R0
Ref. /D/
Page 10 of 15
Rohr, Inc., operating as Goodrich Aerostructures Group
NACELLE DAMAGE DESCRIPTION
AFTERMARKET TECHNICAL SERVICES ENGINEERING
850 Lagoon Drive, Chula Vista, CA 91910-2098
DAMAGE DESCRIPTION
PAGE 3 OF 7
Figure 1 – Sheet 1/5
Rohr, Inc., a subsidiary of the Goodrich Corporation, operating as Goodrich Aerostructures Group
FORM NO. E8210-4
A320PR54-029/13.R0
Ref. /D/
Page 11 of 15
Rohr, Inc., operating as Goodrich Aerostructures Group
NACELLE DAMAGE DESCRIPTION
AFTERMARKET TECHNICAL SERVICES ENGINEERING
850 Lagoon Drive, Chula Vista, CA 91910-2098
DAMAGE DESCRIPTION
PAGE 4 OF 7
Figure 1 – Sheet 2/5
Rohr, Inc., a subsidiary of the Goodrich Corporation, operating as Goodrich Aerostructures Group
FORM NO. E8210-4
A320PR54-029/13.R0
Ref. /D/
Page 12 of 15
Rohr, Inc., operating as Goodrich Aerostructures Group
NACELLE DAMAGE DESCRIPTION
AFTERMARKET TECHNICAL SERVICES ENGINEERING
850 Lagoon Drive, Chula Vista, CA 91910-2098
DAMAGE DESCRIPTION
PAGE 5 OF 7
Figure 1 – Sheet 3/5
Rohr, Inc., a subsidiary of the Goodrich Corporation, operating as Goodrich Aerostructures Group
FORM NO. E8210-4
A320PR54-029/13.R0
Ref. /D/
Page 13 of 15
Rohr, Inc., operating as Goodrich Aerostructures Group
NACELLE DAMAGE DESCRIPTION
AFTERMARKET TECHNICAL SERVICES ENGINEERING
850 Lagoon Drive, Chula Vista, CA 91910-2098
DAMAGE DESCRIPTION
PAGE 6 OF 7
Figure 1 – Sheet 4/5
Rohr, Inc., a subsidiary of the Goodrich Corporation, operating as Goodrich Aerostructures Group
FORM NO. E8210-4
A320PR54-029/13.R0
Ref. /D/
Page 14 of 15
Rohr, Inc., operating as Goodrich Aerostructures Group
NACELLE DAMAGE DESCRIPTION
AFTERMARKET TECHNICAL SERVICES ENGINEERING
850 Lagoon Drive, Chula Vista, CA 91910-2098
DAMAGE DESCRIPTION
PAGE 7 OF 7
Figure 1 – Sheet 5/5
Rohr, Inc., a subsidiary of the Goodrich Corporation, operating as Goodrich Aerostructures Group
FORM NO. E8210-4
A320PR54-029/13.R0
Ref. /E/
Page 15 of 15
Jorge Alberto Salinas Viaud
From:
Sent:
To:
Cc:
Subject:
Britton, Charlie UTAS <[email protected]>
Friday, September 20, 2013 12:22 PM
Jorge Alberto Salinas Viaud
Manzano, Juan UTAS
RE: Curing Procedure EA 934NA
Jorge,
The most common way to heat the area is with the heat lamps. No problem.
Charlie Britton – Airline Support Manager – Aerostructures
UTC AEROSPACE SYSTEMS
850 Lagoon Drive, Chula Vista, CA 91910 USA
Tel: 1 619 691 2836 Mobile: 1 619 917 2836 Fax: 1 619 498 7322
[email protected] www.utcaerospacesystems.com
Subject to the EAR, ECCN [9E991]. This information is subject to the export control laws of the United States, specifically including the Export
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From: Jorge Alberto Salinas Viaud [mailto:[email protected]]
Sent: Friday, September 20, 2013 11:17 AM
To: Britton, Charlie UTAS
Cc: Manzano, Juan UTAS
Subject: [External] Curing Procedure EA 934NA
Importance: High
Dear Charlie,
Currently we are going to perform a repair on a Fan Cowl using the Goodrich SRM 54-20-00 Repair 04, within the
instructions of this repair procedure it is allowed to use the material EA 934NA improving the curing time by adding heat
(93 Celsius).
Our concern is that in the SRM is not specified the procedure to achieve this temperature to the compound EA 934NA
and in the specifications of the material is not included either.
Could you be so kind to inform us if is allowed to use heat lamps with a thermometer (in order to keep track of the
temperature) or if hot bonding is to be used?
Thank you for your help,
Jorge Salinas
Support Engineer
Aeropuerto Internacional de El Salvador
+503 – 2366-7544
[email protected]
1