Retrofit: End Position Detection IVO Propeller MANDATORY. Identifies an instruction, which if not followed, may cause serious injury or even death.

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Transcription:

Manufacturer Bulletin 01/2013 Retrofit: End Position Detection IVO Propeller MANDATORY Repeating symbols: WARNING: o CAUTION: NOTE: Identifies an instruction, which if not followed, may cause serious injury or even death. Denotes an instruction which if not followed, may severely damage the aircraft or could lead to suspension of warranty Information useful for better handling 1. Planning information 1.1 Reference All AutoGyro models with IVO variable pitch propeller installed. 1.2 Reason This retrofit provides cockpit indication when the variable pitch propeller has reached its end stops, thus improving ease of use, operational reliability and minimizing the risk of misuse. 1.3 Subject Retrofit 1.4 Compliance Prior to next flight, at latest with next scheduled inspection (25/100 hrs). CAUTION: Failure to comply with this instruction will cause the loss of eventual warranty on the actuating drive. 1.5 Approval The technical content is approved under the authority of AutoGyro GmbH 1.6 Manpower Accomplishment: 1.5 h 1.7 Mass data No change 11.04.2013 Seite 1 von 4

Manufacturer Bulletin 01/2013 1.8 Electrical load data No change 1.9 References In addition to this technical information refer to current issue of AutoGyro Parts catalogue www.auto-gyro.de 1.10 Other publications affected - 1.11 Interchangeability of parts Affected parts cannot be re-used and must be marked accordingly and/or discarded. 2. Material Information 2.1 Material cost and availability Price and availability will be supplied on request by AutoGyro GmbH. 2.2 Material requirement per gyro Should removal of a locking device (e.g. lock tabs, self-locking fasteners, etc.) be required when undergoing disassembly/assembly, always replace with a new one 2.3 Material requirement per spare part C.EL300 (Calidus) V.EL301 (Cavalon) M.EL302 (MTOsport / MT 03) Retrofit kits have to be ordered through AutoGyro s International Partners. 2.4 Rework of parts None 2.5 Special tooling/lubricant-/adhesives-/sealing compound None 11.04.2013 Seite 2 von 4

Manufacturer Bulletin 01/2013 3. Accomplishment / Instructions 3.1 Determination of Necessity If not installed 3.2 Instructions A detailed instruction is part of each retrofit kit. 3.3 Test run Perform ground test run. 3.4 Summary These instructions (section 3) have to be conducted in accordance with section 1.4. The execution/completion of the mandatory Service information must be annotated in the aircraft logbook 11.04.2013 Seite 3 von 4

Manufacturer Bulletin 01/2013 4. Function Description / Flight Manual Supplement This controller monitors the electrical current of IVO variable pitch propeller actuating motor. This allows the detection of both (FINE and COARSE) end positions, hard stops, but also possible defects, such as worn-out brushes or cable breaks. Cockpit indication consists of 2 orange status LEDs. Indication logic according to the following table: Both LEDs off Upper LED blinking Lower LED blinking Upper LED steady ON lower LED steady ON Both LEDs flashing fast Propeller is in no end position and no pitch change activated. Propeller changing pitch to FINE Propeller changing pitch to COARSE End position FINE reached and electronic pitch change inhibit FINE activated. * End position COARSE reached and electronic pitch change inhibit COARSE activated. * Actuating motor does not word despite rocker switch activation. Possible defects: brushed worn-out, cable break, ** * Electronic pitch change inhibit will be deactivated after activating pitch change in opposite direction for at least 1 second. ** Indication can only be reset by switching the master switch temporarily to OFF and then back ON. In order to avoid pilot distraction, indication of a possible defect is re-triggered after another activation of the rocker switch. 11.04.2013 Seite 4 von 4

Aircraft Maintenance Manual AutoGyro 61-10-00 8-2 RETROFIT: END POSITION DETECTION IVO PROPELLER BAS GENERAL, REFERENCES AND REQUIREMENTS Operational task, which can be performed by a licensed pilot or instructed personnel! SPECIAL TOOLS, CONSUMABLE MATERIALS AND PARTS C.EL300 V.EL301 M.EL302 Retrofit Kit Calidus Retrofit Kit Cavalon Retrofit Kit MT 03 / MTOsport PRECAUTIONS AND SAFETY MEASURES CAUTION: Failure to comply with this instruction will cause the loss of eventual warranty on the actuating drive. PROCEDURES Contents of the Kit: 1. IVO-Control with pin assignment 2. 2 x Shrinking Hose to isolate unused connectors 3. 2 x LED-Mount für 5mm Status LEDs 4. 3 x Cable Ties to fixate cables and installation 5. Blind Plug to cover installation bore of removed thermo switch Pin assignment of wiring harness (top to bottom): - green/white - orange/white - black - green - orange - red AMM-XX-E_12-08-01 Part E - 61-10-00 8-2 Page 1 of 3

Aircraft Maintenance Manual AutoGyro Step 1: - Remove all connectors from rocker switch - Remove resistor pack (if installed) and discard - Remove thermo switch and close bore with blind plug Step 2: The black ground cable has an extension with a second connector. - Isolate this second connector with the supplied shrinking hose. Sqeeze extending hot hose with pliers. Step 3: - Drill 2 8mm holes right hand from the rocker switch as depicted in attached photo. - Deburr holes - Insert LEDs without mounting ring and fastening nut. Step 4: - Fixate LED with mounting ring and nut from behind. AMM-XX-E_12-08-01 Part E - 61-10-00 8-2 Page 2 of 3

Aircraft Maintenance Manual AutoGyro Step 5: - Connect cockpit controls to control beard. - DO NOT MISMATCH POSITION!!!! Control board can be destroyed! - Refer to photo provided (left hand side, condensors showing up): 1. white/orange (IVO) 2. white/violett (IVO) 3. black (GND) 4. violett/orange (12V+) Step 6: - Connect control board with rocker switch: Switch Conn./Cable 1a (top) green/white 1 (middle) black 1b (bottom) orange/white Step 7: - Insert LEDs in mount (use pliers, if needed) - LED with cable color orange goes in upper position, green in bottom position - Check switching and indication logic (Master switch ON ) Press rocker fine position: upper LED must blink, propeller must adjust to fine ( take-off) Press rocker switch coarse pos.: lower LED must blink, propeller must adjust to coarse ( cruise) Step 8: - Fixate cables and control board with cable ties Step 9: - Perform a functional check according to function description (see Manufacturer Bulletin) AMM-XX-E_12-08-01 Part E - 61-10-00 8-2 Page 3 of 3