Product Catalogue 2018/19.

Transcription

1 Product Catalogue 2018/19

2 Excellence by Design 21jAeroDesign Limited 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.

3 PART DESIGN Re-engineering problem parts to improve reliability while reducing cost, or simply designing a cost effective spare part. Working closely with our production partners a robust supply chain is guaranteed. REPAIR DESIGN Case specific and generic repair design approval for metallic and composite aircraft structures. Component repair allowing for the efficient recovery of BER and no repair parts. CONSULTATION SERVICES Verification of regulatory compliance, including physical aircraft inspection. Part 21J start-up and development. Bespoke Part 21J and Part 21G training courses, groups and one-to-one. AOG SUPPORT Using our team of structural repair specialists, rapid recovery of damaged operational aircraft when there is a need to avert or resolve an AOG event. 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. AIRCRAFT MODIFICATION STC and minor change approval for aircraft modification. Our scope covers composite and metallic structures, cabin safety, aircraft interiors and hydro- mechanical systems. From seats to slats, lavatories to liveries, please contact us with your requirement. OUR VALUES We stand by our word and do what we say while cutting out the things that don t matter to keep us lean and able to deliver best customer service.

4 Parts ATA 12 Servicing AP High Vis Remove Before Flight Flag All BACKGROUND 21jAeroDesign s AP High Vis RBF Flag was developed in response to an EASA Airworthiness Directive with Safety leading the design. Our High Vis RBF Flag is effective in all lighting conditions, however shows the biggest advantage over legacy flags in reduced visibility or darkness. With its highly visible edging, 21jAeroDesign s AP High Vis RBF Flag offers operators a low cost means of increasing the visibility of tooling used in variable lighting conditions, or simply as a straight replacement for legacy flags. As opposed to the cumbersome legacy split ring our High Vis RBF Flag is fitted with a clever Cable Ring that can be either openable or permanently swaged closed. FEATURES Improves Safety Size; 470mm (18.5 ) x 76mm (3 ) Effective in all lighting conditions Edged with highly visible reflective material The clever Cable Ring design can be either openable or permanently swaged closed Produced from MIL specification fabric Printed both sides Used by Europe s largest A320 operator PART RELEASE Certificate of Conformity BESPOKE DESIGN SERVICE If you have a Flag, Tag or Streamer requirement please contact us, we will be happy to work with you on a design and specification that meets with your specific requirements.

5 Parts BACKGROUND The Cover secures the Firewire to the Core Fire Detector Support Rail. The Cover can be lost or found damaged during repair/overhaul of the Core Fire Detector Assembly or during removal/installation of the Firewire. 21jAeroDesign s AP49-1 Cover has been introduced as a result of the OEM part becoming non-procurable. Our AP49-1 Cover offers a cost saving over the OEM part with an equivalent level of safety and performance. FEATURES Direct replacement for OEM Part Number TA01P45 EASA approved minor modification PART RELEASE DELIVERABLES AP49-1 Cover 21jAeroDesign Design Change Document 21jAeroDesign Aircraft Manual Supplement(AIPC) APIC A SOLE DISTRIBUTER ATA 26 Fire Protection AP49-1 Cover, Core Fire Detector Assy A318, A319, A320 and A321. AllMSNs.

6 Parts ATA 71 Power Plant AP Key Tool Assembly A318/A319/A320/A321 - All MSNs. BACKGROUND EASA and FAA Airworthiness Directives have been issued as a result of several in-flight Fan Cowl Door losses. The Airworthiness Directives mandate modification of the Fan Cowl Door by installation of a new front latch with locking device, requiring a special Key Tool Assembly for opening. Two Key Tool Assemblies must be stowed within the flight deck. 21jAeroDesign s AP Key Tool Assembly offers a cost-effective replacement for lost or damaged OEM parts, or when additional tooling provision is required for maintenance. 21jAeroDesign s Key Tool Assembly has the benefit of a replaceable flag in the case it is soiled or damaged. FEATURES Direct replacement for OEM Part Number HA Highly visible superbright day/night flag Replaceable flag Used by Europe s largest A320 operator EASA AMOC EASA approved minor modification PART RELEASE DELIVERABLES AP Key Tool Assembly EASAAMOC approval certificate Modification Summary AIPC supplement EASA AD (V2500) FAA AD (V2500) Airbus SB A (V2500) EASA AD superseding AD (CFM56) FAA AD (CFM56) Airbus SB A (CFM56) SOLE DISTRIBUTER

7 Parts BACKGROUND A320FAM operators have experienced heavy exfoliation corrosion effecting the Thrust Reverser Adapter Ring Outer Flange on CFM56-5B powered aircraft. The corrosion typically appears on the four lower flange segments at positons #7, #8, #9 and #10. Analysis has shown that the OEM part corrodes due to a combination of factors; low resistance to stresscorrosion cracking (SCC), residual fit-up stress, insufficient surface protection. 21jAeroDesign AP ( )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. FEATURES Direct replacement for OEM Part Number ( )0( )-0 (Segments #7, #8, #9 and #10) High resistance to stress-corrosion cracking (SCC), with immunity from exfoliation Significantly improved surface protection EASA STC FAA STCST04019NY PART RELEASE DELIVERABLES AP ( )01-0 Flange Assy EASA/FAA STC certificate Approval Summary and EngineeringBulletin AIPC supplement Goodrich Aerostructures SB RA SOLE DISTRIBUTER ATA 78 Exhaust AP ( )01-0 Thrust Reverser Adapter Ring Outer Flange Segments CFM56-5A/5B Powered A318/A319/A320/A321

8 Repairs ATA 25 Equipment/ Furnishings Cockpit Door Bolting System Repair A318/A319/A320/A321 - All MSNs REPAIR DESCRIPTION Inspection of the Cockpit Door Bolting System P/N AR4753-1/-7 commonly reveals damage affecting the Upper and Lower Latch Assemblies P/N AR4755-( ), and the Centre Latch Assembly P/N AR4754-( ). The damage typically consists of fretting 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 the damaged Bolt removed. The damaged Bolt is repaired by replacing missing material and dressing to initial profile. Cost effective recovery and repair of damaged part. Includes repairs not cover by Adams Rite Aerospace, Inc. CMMs and Repair performed by partner company CRS Technics Limited with guaranteed turnaround time. ATA PART NUMBER AR Cockpit Door Bolting System AR Cockpit Door Bolting System EASA approved minor repair REPAIR RELEASE Airbus CMM Adams Rite Aerospace, Inc. CMM Adams Rite Aerospace, Inc. CMM SOLE REPAIR STATION

9 Repairs REPAIR DESCRIPTION The Core Fire Detector Rail Assembly is commonly removed from CFM56-5B powered A320FAM aircraft due to damage affecting the Support Tube. The damage typically consists of full or partial severing of the tube at its joint with the attach plate. The damaged Support Tube is repaired by separating the tube at the break, inserting a repair rod and re-joining the severed sections by fusion/butt welding. Cost effective recovery and repair of damaged part. Repair performed by partner company CRS Technics Limited with guaranteed turnaround time. ATA PART NUMBER RAILASSY-CORE FIRE RAILASSY-CORE FIRE RAILASSY-CORE FIRE EASA approved minor repair REPAIR RELEASE ROHR, Inc. A318/A319/A320/A321 PPIPC , Figure1 ROHR, Inc. A318/A319/A320/A321 PPIPC , Figure2 SOLE REPAIR STATION ATA 26 Fire Protection Core Fire Detector Rail Assembly Repair CFM56-5B Powered A318/A319/A320/A321

10 Repairs ATA 38 Water/Waste Drain Mast Assembly Repair A318/A319/A320/A321 - All MSNs REPAIR DESCRIPTION The Drain Mast Assembly is vulnerable to impact damage due to its location on the aircraft belly and typically experiences corrosion 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 Cost effective recovery and repair of damaged part. Includes repairs not cover by Airbus CMM Repair performed by partner company CRS Technics Limited with guaranteed turnaround time. ATA PART NUMBER H DRAIN MAST ASSEMBLY EASA approved minor repair REPAIR RELEASE Airbus CMM A318/A319/A320/A321 AIPC SOLE REPAIR STATION

11 Repairs REPAIR DESCRIPTION Inspection of Pylon Precooler Fairings repaired in accordance with SRM Task has revealed further crack damage 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. Cost effective recovery and repair of damaged part. Repair performed by partner company IMT Aviation Limited with guaranteed turnaround time. ATA PART NUMBER D * COVER(LH) D * COVER(RH) *Before modification 33844P8341 EASA approved minor repair REPAIR RELEASE AIPC , Figure 03 SRM Task SOLE REPAIR STATION ATA 54 Nacelles/ Pylons Pylon Precooler Fairing (Cover) Repair A318/A319/A320/A321

12 Repairs ATA 57 Wings Interconnecting Strut Housing Repair A318/A319/A320/A321 - All MSNs REPAIR DESCRIPTION Inspection commonly reveals fretting damage affecting the Interconnecting Strut Housing. The fretting damage is caused by contact between the Housing and an armoured cable. The fretting action results in cross-sectional material loss on the outer surface of the Housing s end diameter. The fretting damage is repaired by removing material from the end diameter, replacing the removed material using high velocity oxygen fuel spraying (HVOF) and machining back to production drawing tolerances. Cost effective recovery and repair of damaged part. Includes repair not cover by Airbus CMM Repair performed by partner company CRS Technics Limited with guaranteed turnaround time. ATA PART NUMBER D Housing D Housing D Housing Installed on Interconnecting Strut Assemblies: D , D , D , D , D , D , D , D , D , D , D , D , D , D , D , D , D , D EASA approved minor repair REPAIR RELEASE Airbus CMM SOLE REPAIR STATION

13 Repairs REPAIR DESCRIPTION Inspection during repair and/or overhaul of the CFM56-5B Air Inlet Cowl commonly reveals attachment fastener hole elongation affecting the part number Access Door Assembly. The Access Door Assembly is disassembled, a new access door panel fabricated from aluminum alloy sheet and the part re-assembled. Cost effective recovery and repair of damaged part. Repair performed by partner company IMT Aviation Limited with guaranteed turnaround time. ATA / PART NUMBER DOOR ASSY-ACCESS Installed on Air Inlet Cowl Assemblies: EASA approved minor repair REPAIR RELEASE Goodrich Aerostructures CMM , IPL Figure 1 SOLE REPAIR STATION ATA 71 Power Plant Air Inlet Cowl Access Door Assy Repair CFM56-5B Powered A318/A319/A320/A321

14 Repairs ATA 71 Power Plant Air Inlet Cowl Pressure Relief Door Assembly Repair CFM56-5B Powered A318/A319/A320/A321 REPAIR DESCRIPTION Inspection during repair and/or overhaul of the CFM56-5B Air Inlet Cowl commonly reveals fretting damage affecting the part number Pressure Relief Door Assembly. The fretting damage typically consists of cross-sectional material loss affecting the integral lug to which the part number S700M Lanyard attaches. The damaged lug is trimmed away from the Pressure Relief Door Assembly and a new lug installed. Cost effective recovery and repair of damaged part. Repair performed by partner company IMT Aviation Limited with guaranteed turnaround time. ATA / PART NUMBER PRESSURE RELIEF DOOR ASSY Installed on Air Inlet Cowl Assemblies: EASA approved minor repair REPAIR RELEASE Goodrich Aerostructures CMM , IPL Figure 1 SOLE REPAIR STATION

15 Repairs REPAIR DESCRIPTION Over 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 thecorner break at the latch cutout(s). Two cover plates are fabricated from CRES steel sheet and installed. Cost effective recovery and repair of damaged part. Repair performed by partner company IMT Aviation Limited with guaranteed turnaround time. ATA / PART NUMBER DOOR ASSY-OIL TANK ACCESS DOOR ASSY-OIL TANK ACCESS Installed on Left Hand Fan Cowl Assemblies: , , , , , , 642M , 642M EASA approved minor repair REPAIR RELEASE Goodrich Aerostructures CMM , IPL Figure 1 SOLE REPAIR STATION ATA 71 Power Plant Oil Tank Access Door Assembly Repair CFM56-5B Powered A318/A319/A320/A321

16 21JAeroDesign Limited. DOA Approval No: EASA.21J.632. Head Office Saffron House, Bearwalden Business Park Wendens Ambo Saffron Walden Essex, CB11 4JX, United Kingdom Tel: +44 (0) Option 4 Mob: +44 (0) info@21j.co.uk Satellite Office Capability House, Building 31 Wrest Park Enterprise Wrest Park Silsoe Bedfordshire, MK45 4HR, United Kingdom