product catalogue 2018/19 21jaerodesign... · ata 26 – fire protection product ap49-1 cover, core...

Email: [email protected]

Product Catalogue 2018/19

Established in 2015 and strategically located near Stansted airport in the UK, 21jAeroDesign forms part of the IMT Aviation group of companies. 21jAeroDesign is headed by Adam Duke, a highly-regarded aviation professional with over 30 years’ experience in design, maintenance, CAMO and airlines.

Before forming 21jAeroDesign Adam held the position of Head of Design and Structures at easyJet, where he founded the company’s Part 21J design organisation and Part M structures fleet technical management team. With his extensive experience and expertise; Adam brings with him a customer focused approach and a full understanding of the importance of value engineering and operational efficiency.

ExcellenceDesignby

21jAeroDesign Limited

21jAeroDesign - Product Catalogue 2018/192

EPA PARTSIncreased reliability with reduced cost, or simply a cost effective replacement part. Working closely with our production partners a robust supply chain is guaranteed.

REPAIR Case specific and generic repair approval for metallic and composite structures. Fuselage, wings, empennage, nacelle, we’ve got it covered.

MODIFICATIONSTC and minor change approval. Structures, cabin interiors, safety equipment, placards and markings, external liveries, hydro-mechanical systems and more, please contact us with your specific requirement.

AOG SUPPORTUsing our team of design and structural repair specialists, rapid recovery of operational aircraft when there is a need to avoid or resolve an AOG event.

BER PARTRECOVERYEconomic and efficient recovery of ‘BER’ and ‘no repair’ parts through the use of case specific repair approval and EPA replacement parts.

PMA PART INTERGRATIONEASA approval and integration of parts approved under the FAA PMA system. Effective inventory management and cataloguing of replacement PMA parts.

“We have a passion for our customers and believe in the benefit of

collaboration and pooling expertise. A collective approach helps define

your specific requirements and enables our mission to deliver you best value through innovative design and

engineering solutions.”

21jAeroDesign - Product Catalogue 2018/19 3

ATA 25 – Equipment/ FurnishingsPRODUCT

Installation of a Low Frequency Underwater Locating Device (LF-ULD)

APPLICABILITY

A318/A319/A320/A321

ATA25-65

APPROVALEASA approved minor modifi cation

DELIVERABLES• Approval Summary and Engineering Bulletin• Aircraft Manual Supplement - AMM• Aircraft Manual Supplement - AIPC• Novega SID88 Component Maintenance Manual• Novega SID88 LF-ULB• Installation kit

REFERENCESICAO Annex 6 amendment 36 (Nov 2012)COMMISSION REGULATION (EU) 2015/2338 of 11 Dec 2015TSO-C142a - Non-Rechargeable Lithium Cells and BatteriesETSO-C142a - Non-Rechargeable Lithium Cells and BatteriesTSO-C200a - Airframe Low Frequency Underwater Locating Device (Acoustic) (Self-Powered)ETSO-C200a Low-frequency Underwater Locating Device (ULD)

DESCRIPTIONCAT.IDE.A.285(f) (COMMISION REGULATION (EU) 2015/2338) makes installation of a underwater locating device operating at a frequency of 8,8 kHz ± 1 kHz mandatory by the 01 Jan 2019, unless the aeroplane is operated over routes on which it is at no point more than 180 NM from the shore.

The purpose of the LF-ULB is to assist search and rescue teams in locating aircraft wreckage undersea.

Two brackets are attached to the aircraft structure onto which an adapter panel is installed. The LF-ULB is mounted to the adapter panel.

BENEFITS• 100+ installations completed.• Location of the LF-ULB is the same as the Airbus build

standard, maintaining commonality with factory fitted aircraft.

• The installed Novega SID88 LF-ULB is the same as the Airbus build standard, maintaining commonality with factory fitted aircraft.

• Installation time <2 hours for one mechanic.• The LF-ULB, all parts and fasteners required to perform

the installation are supplied as a kit allowing for efficient planning and material management.

Modifications


ATA 26 – Equipment/ FurnishingsPRODUCT

AP49-1 Cover, Core Fire Detector Assy

APPLICABILITY

A318, A319, A320 and A321. All MSNs.

ATA25-21

APPROVALEASA Supplemental Type Certifi cate

DELIVERABLES• Approval Summary and Engineering Bulletin• Copy of EASA Supplemental Type Certifi cate• Placards for fl ight deck door and fl ight deck pedestal

DESCRIPTIONFor logistical and economic reasons, various aircraft operators have requested design approval for a zero-passenger seat cabin configuration, whereby all passenger seats are removed from the passenger cabin.

BENEFITSAllows operation of the aircraft with minimum flight crew and no passenger seats installed in the passenger compartment.No Aircraft Flight Manual (AFM) supplement required.

Modifications


ATA 12 – Servicing

PRODUCT

AP120-0012-001 High Vis Remove BeforeFlight Flag

APPLICABILITY

All

FEATURES• Improves Safety• Size; 470mm (18.5”) x 76mm (3”)• Effective in all lighting conditions• Edged with highly visible refl ective material• The clever Cable Ring design can be either openable or permanently

swaged closed• Produced from MIL specifi cation fabric• Printed both sides• Used by Europe’s largest A320 operator

PART RELEASECertifi cate of Conformity

BESPOKE DESIGN SERVICEIf you have a Flag, Tag or Streamer requirement please contact us, we will be happy to work with you on a design and specifi cation that meets with your specifi c requirements.

BACKGROUND21jAeroDesign’s AP120-0012-001 High Vis RBF Flag wasdeveloped in response to an EASA Airworthiness Directive withSafety leading the design. Our High Vis RBF Flag is effective inall lighting conditions, however shows the biggest advantageover legacy flags in reduced visibility or darkness.

BENEFITSWith its highly visible edging, 21jAeroDesign’s AP120-0012-001High Vis RBF Flag offers operators a low cost means ofincreasing the visibility of tooling used in variable lightingconditions, or simply as a straight replacement for legacy flags.

As opposed to the cumbersome legacy ‘split ring’ our High VisRBF Flag is fitted with a clever ‘Cable Ring’ that can be eitheropenable or permanently swaged closed.

Parts


ATA 26 – Fire ProtectionPRODUCT

AP49-1 Cover, Core Fire Detector Assy

APPLICABILITY

A318, A319, A320 and A321. All MSNs.

FEATURESDirect replacement for OEM Part Number TA01P45

APPROVALEASA approved minor modifi cation

PART RELEASEEASA Form 1

DELIVERABLESAP49-1 Cover21jAeroDesign Design Change Document21jAeroDesign Aircraft Manual Supplement (AIPC)

REFERENCESAPIC 26-12-17-01A

SOLE DISTRIBUTER

BACKGROUNDThe Cover secures the Firewire to the Core Fire DetectorSupport Rail. The Cover can be lost or found damaged duringrepair/overhaul of the Core Fire Detector Assembly or duringremoval/installation of the Firewire.

21jAeroDesign’s AP49-1 Cover has been introduced as a resultof the OEM part becoming non-procurable.

BENEFITSOur AP49-1 Cover offers a cost saving over the OEM part withan equivalent level of safety and performance.

Parts


ATA 71 – Power Plant

PRODUCT

AP120-0013-001 Key Tool Assembly

APPLICABILITY

A318/A319/A320/A321 - All MSNs.

FEATURES• Direct replacement for OEM Part Number HA2273-1• Highly visible ‘superbright’ day/night fl ag • Replaceable fl ag• Used by Europe’s largest A320 operator

APPROVALEASA AMOCEASA approved minor modifi cation


DELIVERABLESAP120-0013-001 Key Tool AssemblyEASA AMOC approval certifi cateModifi cation SummaryAIPC supplement

REFERENCESEASA AD 2016-0053 (V2500)FAA AD 2017-13-10 (V2500)Airbus SB A320-71-1069 (V2500)EASA AD 2016-0257 superseding AD 2016-0069 (CFM56)FAA AD 2018-05-04 (CFM56)Airbus SB A320-71-1068 (CFM56)

SOLE DISTRIBUTER

BACKGROUNDEASA and FAA Airworthiness Directives have been issued as aresult of several in-flight Fan Cowl Door losses. TheAirworthiness Directives mandate modification of the Fan CowlDoor by installation of a new front latch with locking device,requiring a special Key Tool Assembly for opening. Two KeyTool Assemblies must be stowed within the flight deck.

BENEFITS21jAeroDesign’s AP120-0013-001 Key Tool Assembly offers acost-effective replacement for lost or damaged OEM parts, orwhen additional tooling provision is required for maintenance.21jAeroDesign’s Key Tool Assembly has the benefit of areplaceable flag in the case it is soiled or damaged.

Parts


ATA 78 – Exhaust

PRODUCT

AP321-458-( )01-0 Thrust ReverserAdapter Ring Outer Flange Segments

APPLICABILITY

CFM56-5A/5B Powered A318/A319/A320/A321

FEATURES• Direct replacement for OEM Part Number 321-458-( )0( )-0

(Segments #7, #8, #9 and #10)• High resistance to stress-corrosion cracking (SCC), with immunity

from exfoliation• Signifi cantly improved surface protection

APPROVALEASA STC 10061662FAA STC ST04019NY


DELIVERABLESAP321-458-( )01-0 Flange AssyEASA Form 1EASA/FAA STC certifi cateApproval Summary and Engineering BulletinAIPC supplement

REFERENCESGoodrich Aerostructures SB RA32078-128

SOLE DISTRIBUTER

BACKGROUNDA320FAM operators have experienced heavy exfoliation corrosion effecting the Thrust Reverser Adapter Ring OuterFlange on CFM56-5B powered aircraft. The corrosion typicallyappears on the four lower flange segments at positons #7, #8,#9 and #10. Analysis has shown that the OEM part corrodesdue to a combination of factors; low resistance to stresscorrosion cracking (SCC), residual fit-up stress, insufficientsurface protection.

BENEFITS21jAeroDesign AP321-458-( )01-0:• Interchangeable with all OEM part number variants.• Perfect fit = no use of clamps to install = no residual stress.• High resistance to SCC & immune to exfoliation corrosion.• Structure protected by anodising and a tough layer of

adhesive primer.• Polyamide epoxy paint applied at interface with engine

acoustic panel to protect structure from fretting.

Parts


ATA 25 – Equipment/FurnishingsPRODUCT

Cockpit Door Bolting System Repair

APPLICABILITY

A318/A319/A320/A321 - All MSNs

ATA25-20

PART NUMBER APPLICABILITYAR4753-1 - Cockpit Door Bolting SystemAR4753-7 - Cockpit Door Bolting System

APPROVALEASA approved minor repair

REPAIR RELEASEEASA Form 1

REFERENCESAirbus CMM 25-20-28Adams Rite Aerospace, Inc. CMM 25-20-28Adams Rite Aerospace, Inc. CMM 25-20-32

SOLE REPAIR STATION

REPAIR DESCRIPTIONInspection of the Cockpit Door Bolting System P/N AR4753-1/-7commonly reveals damage affecting the Upper and LowerLatch Assemblies P/N AR4755-( ), and the Centre LatchAssembly P/N AR4754-( ). The damage typically consists offretting to the Bolt where it contacts the door frame, resulting in cross-sectional material loss at its edge.

The discrepant Latch Assembly is disassembled and thedamaged Bolt removed. The damaged Bolt is repaired byreplacing missing material and dressing to initial profile.

BENEFITS• Cost effective recovery and repair of damaged part.• Includes repairs not cover by Adams Rite Aerospace, Inc.

CMMs 25-20-28 and 25-20-32.• Repair performed by partner company CRS Technics

Limited with guaranteed turnaround time.

Repairs


ATA 26 – Fire ProtectionPRODUCT

Core Fire Detector Rail Assembly Repair

APPLICABILITY

CFM56-5B Powered A318/A319/A320/A321

REPAIR DESCRIPTIONThe Core Fire Detector Rail Assembly is commonly removedfrom CFM56-5B powered A320FAM aircraft due to damageaffecting the Support Tube. The damage typically consists offull or partial severing of the tube at its joint with the attachplate.

The damaged Support Tube is repaired by separating the tubeat the break, inserting a repair rod and re-joining the severedsections by fusion/butt welding.

BENEFITS• Cost effective recovery and repair of damaged part.• Repair performed by partner company CRS Technics


Repairs


ATA26-12

PART NUMBER APPLICABILITY238-0855-505 - RAIL ASSY-CORE FIRE642-5855-501 - RAIL ASSY-CORE FIRE642-5855-503 - RAIL ASSY-CORE FIRE



REFERENCESROHR, Inc. A318/A319/A320/A321 PPIPC 26-10-00, Figure 1ROHR, Inc. A318/A319/A320/A321 PPIPC 26-12-15, Figure 2

SOLE REPAIR STATION

ATA 38 – Water/Waste

PRODUCT

Drain Mast Assembly Repair

APPLICABILITY

A318/A319/A320/A321 - All MSNs

REPAIR DESCRIPTIONThe Drain Mast Assembly is vulnerable to impact damage dueto its location on the aircraft belly and typically experiencescorrosion damage at the tube exit hole. The scope covered by this repair includes:

• Paint repair• Repair of crack/split in seam• Dent removal• Repair of corrosion at tube exit hole• Replacement of tube assembly

BENEFITS• Cost effective recovery and repair of damaged part.• Includes repairs not cover by Airbus CMM 38-34-11.• Repair performed by partner company CRS Technics



ATA38-32

PART NUMBER APPLICABILITY4-60000-H833-00 – DRAIN MAST ASSEMBLY



REFERENCESAirbus CMM 38-34-11A318/A319/A320/A321 AIPC 30-71

SOLE REPAIR STATION

Repairs

ATA 54 – Nacelles/PylonsPRODUCT

Pylon Precooler Fairing (Cover) Repair

APPLICABILITY

A318/A319/A320/A321

REPAIR DESCRIPTIONInspection of Pylon Precooler Fairings repaired in accordancewith SRM Task 54-52-11-300-004 has revealed further crackdamage affecting the lower repair doublers, typically consisting of a thru crack initiating at the lower radius edge of an outlet slit away.

The crack end is stop-drilled and a weld repair carried out.

BENEFITS• Cost effective recovery and repair of damaged part.• Repair performed by partner company IMT Aviation Limited

with guaranteed turnaround time.


ATA54-52

PART NUMBER APPLICABILITYD5461018600200* – COVER (LH)D5461018600300* – COVER (RH)*Before modifi cation 33844P8341



REFERENCESAIPC 54-52-11, Figure 03SRM Task 54-52-11-300-004

SOLE REPAIR STATION

Repairs

ATA 57 – Wings

PRODUCT

Interconnecting Strut Housing Repair

APPLICABILITY

A318/A319/A320/A321 - All MSNs

ATA57-52

PART NUMBER APPLICABILITYD5757030620000 - HousingD5757030620400 - HousingD5757030620600 - Housing

Installed on Interconnecting Strut Assemblies:D5757030500000, D5757030500100, D5757030500200,D5757030500600, D5757030500800, D5757030501000,D5757030501100, D5757030501200, D5757030501300,D5757030501500, D5757030501600, D5757030501700,D5757030501900, D5757030502100, D5757030502300,D5757032200000, D5757032200200, D5757032201100



REFERENCESAirbus CMM 57-52-17

SOLE REPAIR STATION

REPAIR DESCRIPTIONInspection commonly reveals fretting damage affecting theInterconnecting Strut Housing. The fretting damage is causedby contact between the Housing and an armoured cable. The fretting action results in cross-sectional material loss on theouter surface of the Housing’s end diameter.

The fretting damage is repaired by removing material from theend diameter, replacing the removed material using highvelocity oxygen fuel spraying (HVOF) and machining back toproduction drawing tolerances.

BENEFITS• Cost effective recovery and repair of damaged part.• Includes repair not cover by Airbus CMM 57-52-17.• Repair performed by partner company CRS Technics



Repairs


PRODUCT

Air Inlet Cowl Access Door Assy Repair

APPLICABILITY


ATA54-12 / 71-11

PART NUMBER APPLICABILITY642-1014-503 – DOOR ASSY-ACCESSInstalled on Air Inlet Cowl Assemblies:642-1000-501642-1000-505



REFERENCESGoodrich Aerostructures CMM 71-11-19, IPL Figure 1

SOLE REPAIR STATION

REPAIR DESCRIPTIONInspection during repair and/or overhaul of the CFM56-5B AirInlet Cowl commonly reveals attachment fastener holeelongation affecting the part number 642-1014-503 AccessDoor Assembly.

The Access Door Assembly is disassembled, a new accessdoor panel fabricated from aluminum alloy sheet and the partre-assembled.




Repairs


PRODUCT

Air Inlet Cowl Pressure Relief DoorAssembly Repair

APPLICABILITY


ATA54-12 / 71-11

PART NUMBER APPLICABILITY642-1026-503 – PRESSURE RELIEF DOOR ASSY

Installed on Air Inlet Cowl Assemblies:642-1000-501642-1000-505




SOLE REPAIR STATION

REPAIR DESCRIPTIONInspection during repair and/or overhaul of the CFM56-5B AirInlet Cowl commonly reveals fretting damage affecting the part number 642-1026-503 Pressure Relief Door Assembly. Thefretting damage typically consists of cross-sectional materialloss affecting the integral lug to which the part numberS700M1412-093 Lanyard attaches.

The damaged lug is trimmed away from the Pressure ReliefDoor Assembly and a new lug installed.




Repairs


PRODUCT

Oil Tank Access Door Assembly Repair

APPLICABILITY


ATA54-14 / 71-13

PART NUMBER APPLICABILITY642-3013-501 – DOOR ASSY-OIL TANK ACCESS642-3035-501 – DOOR ASSY-OIL TANK ACCESSInstalled on Left Hand Fan Cowl Assemblies:642-3001-503, 642-3001-505, 642-3001-507, 642-3001-509,642-3001-511, 642-3001-513, 642M3001-503, 642M3001-505




SOLE REPAIR STATION

REPAIR DESCRIPTIONOver time the door panel’s aft edge at the latch cutout is worn by repeated opening and closing of the latch, until such time the worn section of material becomes weak and breaks away.

The damage is cleaned-up by applying a radius to the cornerbreak at the latch cutout(s). Two cover plates are fabricatedfrom CRES steel sheet and installed.

BENEFITS

• Cost effective recovery and repair of damaged part.• Repair performed by partner company IMT Aviation Limited



Repairs


PRODUCT

Air Inlet Cowl Assembly - Repair of Inner Barrel Panel Assembly

APPLICABILITY


ATA54-12 / 71-11

PART NUMBER APPLICABILITY642-1025-501, 642-1025-503, 642-1025-505, 642-1025-507, 642-1025-509, 642-1025-511, 642-1025-513, 642-1025-515, 642-1025-517 – PANEL ASSY-INR BRL

Installed on Air Inlet Cowl Assemblies:642-1000-501642-1000-505




SOLE REPAIR STATION

DESCRIPTIONInspection of the Air Intake Cowl during repair/overhaul typically reveals corrosion damage affecting the Inner Barrel Acoustic Panels at their interface with the Engine Attach Ring.

The Air Intake Cowl is disassembled and the corroded Acoustic Panel(s) removed. The corroded Internal Doubler is removed from Acoustic Panel Assembly and a new Internal Doubler fabricated and bonded in position.

The Air Intake Cowl is reassembled with the repaired Acoustic Panel(s).

BENEFITS• Significant cost saving by effective recovery and repair of

damaged part.• Repair performed by partner company IMT Aviation Limited



Repairs

Head OfficeSaffron House, Bearwalden Business ParkWendens AmboSaffron WaldenEssex, CB11 4JX, United Kingdom

Tel: +44 (0) 1799 542828 Option 4Mob: +44 (0) 7985 873381Email: [email protected]

Satellite OfficeCapability House, Building 31Wrest Park EnterpriseWrest ParkSilsoeBedfordshire, MK45 4HR, United Kingdom

21JAeroDesign Limited.DOA Approval No: EASA.21J.632.

product catalogue 2018/19 21jaerodesign... · ata 26 – fire protection product ap49-1 cover, core...

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