NOTIFICATION BULLETIN No. RTC-053b
EVEKTOR SportStar RTC · Service Bulletins
Overview
This document is a service bulletin for the EVEKTOR SportStar RTC aircraft, specifically addressing the installation of a pulsation damper in the fuel system. It outlines the necessary actions, materials, and procedures required for the installation to improve fuel pressure stability.
- Applies to all SportStar RTC airplanes with Rotax 912 S engine.
- Installation of TC1-9073-06-01 pulsation damper is recommended.
- The bulletin must be recorded in the aircraft logbook.
- Installation should be performed by authorized maintenance organizations.
- Costs for the installation are covered by the aircraft operator/owner.
- No impact on weight and balance.
- No changes to accompanying technical documentation.
- Work procedures are detailed in the bulletin.
Document
Source
Originally published by website-files.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Service Bulletins
- Year ·
- 2020
- File size ·
- 366 KB
- Publisher ·
- website-files.com
- Language ·
- en
What is the NOTIFICATION BULLETIN No. RTC-053b?
The NOTIFICATION BULLETIN No. RTC-053b is a service bulletins for the EVEKTOR SportStar RTC, dated 2020.
Where does the NOTIFICATION BULLETIN No. RTC-053b come from?
This copy of the NOTIFICATION BULLETIN No. RTC-053b was originally published by website-files.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the NOTIFICATION BULLETIN No. RTC-053b published?
The NOTIFICATION BULLETIN No. RTC-053b — the EVEKTOR SportStar RTC service bulletins on file — is dated 2020.
Most owners only have the POH. Here's the essential set for the EVEKTOR SportStar RTC.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More EVEKTOR SportStar RTCmanuals & documents
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In this document
Required Actions
Install the TC1-9073-06-01 pulsation damper to the fuel system and record the implementation in the logbook.
Work Procedure
Detailed steps for removing the existing hose and installing the new pulsation damper are provided.
Necessary Material
A list of required materials and tools for the installation is included.
Influence on Airplane Documentation
The operation technical documentation remains unaffected, but a logbook entry is required post-installation.
Safety Notes
The document emphasizes the need for authorized personnel to perform the installation.
Full document text
Letecká 1008, 686 04 Kunovice, Czech Republic QS-406/F-08I tel: +420 632 537 428 fax: +420 632 537 901 e-mail: evektor@evektor.cz https://www.evektor.cz page: 1/2 issues NOTIFICATION BULLETIN No. RTC-053b TECHNICAL CONTENT OF THIS DOCUMENT IS APPROVED ON THE BASIS OF AUTHORIZATION DOA NO. EASA.21J.057. 1. CONCERNING TO: All airplanes SPORTSTAR RTC equipped with the Rotax 912 S engine. 2. REASON: The aircraft manufacturer introduced by an option design change installation of the TC1-9073-06-01 pulsation damper in the fuel system. By installing the pulsation damper, it is possible to reduce the contingent oscillation of fuel pressure below the lower limit (for more than 5 sec.). 3. REQUIRED ACTIONS: 1. Install the TC1-9073-06-01 pulsation damper to the fuel system. 2. Record the bulletin implementation in the Logbook. 4. LATEST DAY OF THE ACTION: As necessary. 5. CARRIED OUT BY: Organization with authorization for maintenance/repairs of this type of airplane in accordance with Part M or Part 145. 6. COSTS COVERED BY: Operator / owner of the airplane. 7. NECESSARY MATERIAL: In accordance with the text of the bulletin. 8. WORK PROCEDURE: In accordance with the text of the bulletin. 9. APPENDICES: None. Valid from: 06. 05. 2020 Letecká 1008, 686 04 Kunovice, Czech Republic QS-406/F-08I tel: +420 632 537 428 fax: +420 632 537 901 e-mail: evektor@evektor.cz https://www.evektor.cz page: 2/2 1. Work procedure 1.1 Necessary tools See Airplane Maintenance Manual for SportStar RTC (doc. No. ERTC022-10-AS), Section 28-20. 1.2 Necessary material (RTC053B) Name Marking Nomencl. Quantity ---------------------------------------------------------------------------------------------------------------- Nipple 9/5.7 840745 765981 1 pc Pulsation damper TC1-9073-06-01 766336 1 pc Fitting 840735 766334 1 pc Sealing ring 250425 765983 1 pc Sealing ring A8x13 950143 766331 2 pc Cobra clamp Cobra 13.0/8 W4 074510 2 pcs Cobra clamp Cobra 14.0/8 W4 074509 2 pcs Fuel hose 10502008 055634 0.3 m Pyrojacket PJA-08 055607 0.35 m Pyrojacket PJA-16 055608 0.4 m Lockwire 0.81 mm (0.032“) 118898 0.002kg Thread sealant Loctite 577 096249 1 pc Cable tie - 060371 1 pc Material shall be supplied by the airplane manufacturer. 1.3 Work procedure 1.3.1 Remove the hose between the fuel pump and the fuel distribution block: 1.3.1.1 Switch the electrical network off and set the fuel cock to OFF position. 1.3.1.2 Remove the upper engine cowling according the procedure mentioned in the Airplane Maintenance Manual for SportStar RTC, Section 71-10 (doc. No. ERTC022-10-AS). 1.3.1.3 Cut off the cable ties securing the hose (2, Fig. 1) to the other parts. 1.3.1.4 Disconnect the hose (2) from the adapter (3). 1.3.1.5 Unscrew and remove the screw (7), sealing rings (6) and fitting (5) with hose from the block (8). 1.3.1.6 Remove the adapter (3) with the sealing ring (4) from the pump (1). 1.3.1.7 Use acetone to clean the thread hole on the pump (1) from adhesive residue. 1.3.1.8 Discard the removed parts (2; 3; 4; 5; 6). Letecká 1008, 686 04 Kunovice, Czech Republic QS-406/F-08I tel: +420 632 537 428 fax: +420 632 537 901 e-mail: evektor@evektor.cz https://www.evektor.cz page: 3/2 1 Engine fuel pump 5 Fitting 2 Hose 6 Sealing ring 3 Adapter 7 Screw fitting 4 Sealing ring 8 Fuel distribution block Fig. 1 – Hose removal 1.3.2 Install the hose with the pulsation damper between the fuel pump and the fuel distribution block: 1.3.1.1 Clean the thread of the nipple (4, Fig. 2) with acetone, fit the sealing ring (5) and apply Loctite 577 thread sealant to the nipple thread; screw the nipple (4) with sealing ring (5) into the pump. 1.3.1.2 Cut the supplied hose (2) into two parts so that one is approx. 100 mm long and the second approx. 200 mm long. 1.3.1.3 Cut the supplied pyrojacket (3) into two parts so that one is approx. 117 mm long and the second approx. 233 mm long. 1.3.1.4 Connect the hoses (2) on the necks of the damper (11); secure the hoses by the clamps (12) by means of pliers. Make sure that the damper and hoses are oriented correctly (see Fig. 2) Letecká 1008, 686 04 Kunovice, Czech Republic QS-406/F-08I tel: +420 632 537 428 fax: +420 632 537 901 e-mail: evektor@evektor.cz https://www.evektor.cz page: 4/2 1.3.1.5 Put on the appropriate parts of the pyrojacket (3) on both parts of the hose (2). 1.3.1.6 Connect the assembled hose with damper on the fitting neck (7); secure the hose by the clamp (6) by means of pliers. 1.3.1.7 Secure the ends of the pyrojackets (3) with a lockwire see Fig. 2). 1.3.1.8 Fasten the fitting (7) with the assembled hose to the block (10) using the screw (8) with sealing rings (9); tighten the screw with a torque 10 Nm. 1.3.1.9 Put on the pyrojacket (13) to the hose with the damper. 1.3.1.10 Connect the assembled hose with damper on the nipple neck (4); secure the hose by the clamp (6) by means of pliers. 1.3.1.11 Secure the ends of the pyrojacket (13) with a lockwire and fasten the hose with the damper to the other parts according to Fig. 3. 1.3.1.12 Do the engine check, check the fuel pressure and fuel system for leaks. 1.3.1.13 Install the engine cowlings according the procedure mentioned in the Airplane Maintenance Manual for SportStar RTC, Section 71-10 (doc. No. ERTC022-10-AS). Fig. 2 – Pulsation damper installation (page 1 of 2) Letecká 1008, 686 04 Kunovice, Czech Republic QS-406/F-08I tel: +420 632 537 428 fax: +420 632 537 901 e-mail: evektor@evektor.cz https://www.evektor.cz page: 5/2 1 Engine fuel pump 8 Screw fitting 2 Hose 9 O-ring 3 Pyrojacket PJA-08 10 Fuel distribution block 4 Nipple 9/5,7 11 Pulsation damper 5 O-ring 250425 12 Cobra clamp 14.0/8 W4 6 Cobra clamp 13.0/8 W4 13 Pyrojacket PJA-16 7 Fitting 840735 Fig. 2 – Pulsation damper installation (page 2 of 2) Fig. 3 – Installed pulsation damper 2. Influence on airplane documentation
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2.1 Accompanying technical documentation¨ Not affected. 2.2 Operation technical documentation The authorized person will carry out this record in the Aircraft Logbook after bulletin implementation: „Installation of the TC1-9073-06-01 pulsation damper in the fuel system was carried out according to the Information Bulletin No. RTC-053b“ and he will add the date and his signature. 3. Influence on weight and balancing Not affected.