Mooney Service Bulletins
Provided by Mooney International, and shared here as a resource for our membership.
Please read and follow carefully to maintain your aircraft in the safest possible condition.
MODELS/S/N AFFECTED:
Refer to the CONTINENTAL AEROSPACE TECHNOLOGIES SERVICE BULLETIN No. SB19-09 Dated 2019- 12- 13 Subject: Champion Aerospace Slick Service Bulletin SB2- 19 (see attached document for more information).
TIME OF COMPLIANCE:
Reference detailed compliance requirements as directed by the attached Champion Aerospace Slick Service Bulletin SB2- 19.
INTRODUCTION:
Continental Aerospace Technologies] (Continental) recommends customer compliance, as specified in Champion Aerospace Slick Service Bulletin SB2- 19. Perform required inspection of any 4200/4300/4700 series or 6200/6300/6700 series impulse coupled magnetos as specified in Champion Aerospace Slick Service Bulletin SB2- 19. For your convenience, please use the following cross- reference table to identify affected Continental Part Numbers found in the Attached document. (see attached document for more information)
MODELS/S/N AFFECTED:
Refer to the CONTINENTAL AEROSPACE TECHNOLOGIES SERVICE INFORMATION LETTER No. SIL19-10 Dated 2019- 12- 16 Subject: Disposable Oil Filter Removal (see attached document for more information)
TIME OF COMPLIANCE:
During Engine Oil Change
INTRODUCTION:
Continental Aerospace Technologies] (Continental) has received field reports of engine damage resulting from oil filter media clogging oil passages as a result of improper oil filter removal; such as, piercing the oil filter housing with a screwdriver or other sharp object.
MODELS/ SN AFFECTED:
Mooney M20V - 33-0001 THRU 33-0018
TIME OF COMPLIANCE:
Before Next Flight
INTRODUCTION:
There was a report in the field, of an M20V Acclaim Ultra with an alternator wire damaged on the RH exhaust crossover tube. Mooney Engineering has determined the wire was incorrectly positioned. This allowed the wire to contact the RH exhaust crossover tube causing a short circuit to the alternator. This resulted in damage to the wire and crossover tube. This requires mandatory compliance by owners. The attached compliance card needs to be filled out and returned to Mooney International Corporation upon completion of this Service Bulletin M20- 340A.
MODELS/S/N AFFECTED:
Refer to the FAA SPECIAL AIRWORTHINESS INFORMATION BULLETIN No. NE-19-16 Dated Oct. 30, 2019 - Subject: Traffic Advisory System: Failure to Display Traffic. (see attached document for more information)
TIME OF COMPLIANCE:
Refer to the FAA SPECIAL AIRWORTHINESS INFORMATION BULLETIN No. NE-19-16 Dated Oct. 30, 2019 - Subject: Traffic Advisory System: Failure to Display Traffic. (see attached document for more information)
INTRODUCTION:
This Special Airworthiness Information Bulletin (SAIB) informs owners and operators of an issue with certain Avidyne SkyTrax6XXA (TAS6XXA) series traffic advisory system flight software versions that may cause traffic to not display on an interfaced display system. This issue affects TAS6XXA, part number (P/N) 700- 00185- ( ), with flight software P/N 510- 00296- 000 Revision 00, Revision 01, and Revision 02, commonly known as Release 2.0.0, 2.0.1, and 2.0.2. This issue is corrected in flight software Revision 03 (Release 2.0.3).
MODELS/S/N AFFECTED:
G1000, Cirrus Perspective, Embraer Prodigy, G950, and G900X systems with GDU version 14.99 or earlier, G2000, G3000, and G5000 with GDU version 4.99 or earlier, GNS 400W/500W Series with main version 5.0x or earlier, and GTN 6xx/7xx Series with main version 5.12 or earlier are affected. (see attached document for more information)
TIME OF COMPLIANCE:
Refer to the Garmin Service Advisory No. 1372 Rev. D Dated November 1, 2019 - Subject: Unavailable RNAV (GPS) Approaches Due to Lack of VDA. (see attached document for more information)
INTRODUCTION:
A limited number of RNAV (GPS) approaches, including all service levels, are unavailable for selection when the approach includes LP minima and also has no published vertical descent angle (VDA). See the example in Figure 1 (see attached document for more information).
MODELS/ S/N AFFECTED:
G1000, Cirrus Perspective, Embraer Prodigy, G950, and G900X systems with GDU version 14.99 or earlier, G2000, G3000, and G5000 with GDU version 4.99 or earlier, GNS 400W/500W Series with main version 5.0x or earlier, and GTN 6xx/7xx Series with main version 5.12 or earlier are affected. (see attached document for more information)
TIME OF COMPLIANCE:
Refer to the Garmin Service Advisory No. 1372 Rev. C Dated Oct. 29, 2019 - Subject: Unavailable RNAV (GPS) Approaches Due to Lack of VDA. (see attached document for more information)
INTRODUCTION:
A limited number of RNAV (GPS) approaches, including all service levels, are unavailable for selection when the approach includes LP minima and also has no published vertical descent angle (VDA). See the example in Figure 1 (see attached document for more information).
MODELS/ S/N AFFECTED:
Refer to the Continental Aerospace Technologies Service Bulletin No. SB19- 05 Dated Oct. 24, 2019 - Subject: Valve Guide Application, Installation and Reaming Procedures. (see attached document for more information)
TIME OF COMPLIANCE:
Refer to the Continental Aerospace Technologies Service Bulletin No. SB19- 05 Dated Oct. 24, 2019 - Subject: Valve Guide Application, Installation and Reaming Procedures. (see attached document for more information)
INTRODUCTION:
Continental Aerospace Technologies (Continental ) valve guides are reamed- in- place after installation. Dimensional specifications for valve guides are provided in Table 1 and Tables 3 through 7. All measurements must be made using properly calibrated and certified precision measuring devices. Reference the current Illustrated Parts Catalog (IPC) for the most current replacement part (see Parts Supersede History at: http://continental.aero/support/parts-supersedure-history.aspx).
MODELS/ S/N AFFECTED:
Refer to the Continental Aerospace Technologies Service Information Letter No. SIL19- 04 Dated Oct. 11, 2019 - Subject: Oil Brand Selection. (see attached document for more information)
TIME OF COMPLIANCE:
Refer to the Continental Aerospace Technologies Service Information Letter No. SIL19- 04 Dated Oct. 11, 2019 - Subject: Oil Brand Selection. (see attached document for more information)
INTRODUCTION:
Continental Aerospace Technologies] (Continental[) would like to remind our customers and maintenance partners the ashless-dispersant oil specification for Continental aircraft piston engines is MHS- 24. The latest version of publication M- 0, Standard Practice Maintenance Manual, Chapter 3, lists qualified oil suppliers and brands which meet the requirements of MHS- 24.
MODELS/ SNAFFECTED:
M20M: 27-0343, 27-0351, 27-0352, 27-0355M20R: 29-0412 thru 29-0525M20TN: 31-0002 thru 31-0143M20U: 32-0001 and M20V: 33-0001
TIME OF COMPLIANCE:
AT NEXT ANNUAL OR WITHIN NEXT 100 FLIGHT HOURS
INTRODUCTION:
Mooney International Corporation has determined an “Optional” solution to prevent inadver-tent rudder trim slipping during extreme deflections during take off. Use of a new cable anda special GSE 030035- 507 tool during installation are advised to prevent a permanent setin springs
MODELS/ SN AFFECTED:
ALL M20 SERIES AIRCRAFT
TIME OF COMPLIANCE:
AS REQUIRED WHEN TOWING AIRCRAFT
INTRODUCTION:
Mooney International Corporation wants to emphasize the importance and care while towing a Mooney aircraft in close quarters, in the hangar and on the ramp. The Mooney Aircraft Flight Manual and Mooney Service and Maintenance Manual recommends that the use of only a Mooney approved hand tow bar be used for moving all Mooney aircraft models.The tow bar attaches into the nose gear axle crossbar. A turn limit indicator and turn limit placards are visible on the nose gear assembly, proper care should be taken to stay within these specified limits. Towing by tractor or other powered equipment is NOT RECOMMENDED.
MODELS/ SN AFFECTED:
M20U - All, M20V - All
TIME OF COMPLIANCE:
AS REQUIRED
INTRODUCTION:
When an Aircraft is placed in storage or remains dormant for an extended period of time (more than 3 weeks), it is best to disconnect the batteries or use a Battery Tender. This practice will eliminate unnecessary drain on the battery if parasitic loads are present. Parasitic load scan deplete battery capacity and result in battery sulfation or low state of charge condition.
MODELS/S/N AFFECTED:
New and rebuilt Continental Aerospace Technologies (Continental) IO- 550- A, B, C, D, E, F,G, L, N, P, R; IOF- 550- B, C, D, E, F, L, N, P, R aviation gasoline (AvGas) engines.(see attached document for more information)
TIME OF COMPLIANCE:
Reference attached Hartzell Engine Technologies (HET) Alert Service Bulletin (ASB) No. 078,(Alternator Inspection, section 1.E. Compliance). Compliance with section 3.A of ASB No.078 is required prior to next flight. (see attached document for more information)
INTRODUCTION:
Hartzell Engine Technologies LLC (HET) has issued Alert Service Bulletin (ASB) No. 078 requiring the inspection, removal, and replacement of an identified alternator. Reference Hartzell Engine Technologies Alert Service Bulletin (ASB) No. 078 for the applicable alternators (serial number(s) and shipment date(s)). Continental recommends compliance with HET Alert Service Bulletin (ASB) No. 078. (see attached document for more information)
MODELS/S/N AFFECTED:
GFC 500 system installed per STC SA01866WI, MDL 11, in the Mooney M20M, M20R,andM20S are affected.(see attached document for more information).
TIME OF COMPLIANCE:
(see attached document for more information).
INTRODUCTION:
The type certificated Mooney air conditioning system will prevent the installation of a GFC500 in Mooney M20M, M20R, and M20S air frames.
MODELS/S/N AFFECTED:
New and rebuilt O- 200- A, B, D, X; IO- 240- A, B; IO- 360- KB; LTSIO- 360- KB,RB; TSIO- 360- CB, FB, GB, KB, LB, MB, RB, SB; O- 470- R, S, U; IO- 470- C,F, J, K, L, N, S, V, VO; IO- 520- A, BA, BB, C, CB, D, F, J, L, M; LTSIO- 520-AE;TSIO-520-AE,AF,BE,C,CE,DB,G,H,M,P,R,T,UB;IO-550-B,C,D,F, L; and TSIO- 550- C, E (see attached document for more information).
TIME OF COMPLIANCE:
Reference detailed compliance requirements as directed by the attached Champion Aerospace Slick Service Bulletin SB19- 02A (SB1- 19). (see attached document for more information).
INTRODUCTION:
Mandatory inspection of impulse coupled Slick magnetos.Continental1 recommends customer compliance, as specified in Champion Aerospace Slick Service Bulletin SB1- 19. (see attached document for more information).
MODELS/S/N AFFECTED:
Garmin Flight Stream 510 (011- 03595- ( )) units with software version 2.41 or earlier are affected. (see attached document for more information).
TIME OF COMPLIANCE:
Optional: This STC Service Bulletin may be incorporated at the owner’s discretion and is not warranty reimbursable. (see attached document for more information)
INTRODUCTION:
Flight Stream 510 Software Version 2.42 adds support for Bluetooth Low Energy.(see attached document for more information).
MODELS/ SN AFFECTED:
M20U:32-0002 thru 32-0005; M20V:33-0002, 33-0004, 33-0005 and 33-0007
TIME OF COMPLIANCE:
Within next 25 hours
INTRODUCTION:
Mooney International Corporation has determined the possibility of aluminum tape covering ventilation holes in the lower LH and RH rear vent channels. This will require a1-Time inspection and procedure (if found incorrect) for the affected aircraft.
MODELS/ SN AFFECTED:
M20TN (ACCLAIM): 31-0039, 31-0042, 31-0044, 31-0046, 31-0047, 31-0049, 31-0050, 31-0052, 31-0053, 31-0056,31-0057
TIME OF COMPLIANCE:
MANDATORY - BEFORE NEXT FLIGHT
INTRODUCTION:
This Service Bulletin is written in conjunction with Teledyne Continental Motors (TCM) ServiceBulletinMSB07- 4andKelly Aerospace Service Bulletins 023& 027(Attached). This Service Bulletin is to remove and replace the specified turbocharger(s) (TCM P/N 646677) from Mooney Air-craft M20TN (Acclaim) in accordance with attached TCM/Kelly Aerospace Service Bulletins.
MODELS/S/N AFFECTED:
All Continental Motors, Inc. (CMI), O- 470, IO- 470, IO- 520, GIO- 550, GTSIO- 520, IO- 550,IOF- 550, L/TSIO- 520, TSIO- 550, TSIOF- 550 and TSIOL- 550 aviation gasoline (AvGas) engines using flanged nut (P/N 652541) (see attached document for more information).
TIME OF COMPLIANCE:
At the next 100- Hour/Annual Inspection or next maintenance event.
INTRODUCTION:
Continental Motors, Inc. (CMI) has seen evidence of dimensional non-conforming conditions for a limited production of flanged nuts (P/N 652541). The manufacturer’s stamp is used to identify those flanged nuts which require replacement(maker’s mark, “ZB” on the outer- edge of the nut head, see Figure 1 on attached document).
MODELS/S/N AFFECTED:
Refer to - Continental Motors Aircraft Engine SERVICE BULLETIN SB18-08, Dated:12/10/2018 - Subject: Inspection and Maintenance Modifications of Cylinder Assem-blies.(see attached document for more information)
TIME OF COMPLIANCE:
If under 500 hours in service, perform radius blend inspection and modification no later than the next scheduled 100- Hour/Annual inspection. If 500 hours or greater, perform radius blend modification at the next maintenance event (not to exceed 50 hours).
INTRODUCTION:
Several field reports indicate the potential for fracture initiation on engines (exceeding 500hours of operation) at the radius edge of identified cylinder heads produced on or after 01NOV 2014 (see Figure 2). The affected cylinder casting can be identified by the “filled” top finflange area above the exhaust port as shown in Figure 1. found in the attached document.
MODELS/S/N AFFECTED:
Refer to - Continental Motors Aircraft Engine SERVICE BULLETIN SB18-07, Dated:11/19/2018 - Subject: Crankshaft Dowel (P/N 536563) Inspection and Replacement Instructions at Maintenance and Overhaul.(see attached document for more information)
TIME OF COMPLIANCE:
At the next maintenance requiring complete disassembly of the engine, no later than published TBO.
INTRODUCTION:
This Service Document summarizes the inspection and replacement instructions for the Crankshaft Dowel (P/N 536563).(see attached document for more information)
MODELS/S/N AFFECTED:
Refer to - GARMIN Service Advisory No. 0617 Rev B, Dated: 12/10/2018 - Subject:Temporary Flight Restriction (TFR).
TIME OF COMPLIANCE:
Refer to - GARMIN Service Advisory No. 0617 Rev B, Dated: 12/10/2018 - Subject:Temporary Flight Restriction (TFR).
INTRODUCTION:
TFR data received through Garmin data link products may be incomplete or out of date.(see attached document for more information)
MODELS/S/N AFFECTED:
Refer to - U.S. Department of Transportation Federal Aviation Administration, Information for Operators - Info #18013, Dated: 11/15/2018 - Subject: Hand-held/PortableFire Extinguisher Maintenance and Inspection.
TIME OF COMPLIANCE:
Refer to - U.S. Department of Transportation Federal Aviation Administration, Information for Operators - Info #18013, Dated: 11/15/2018 - Subject: Hand-held/Portable Fire Extinguisher Maintenance and Inspection.
INTRODUCTION:
This Info serves to remind aircraft owners, operators, air agencies, suppliers, distributors,and maintenance technicians that hand- held/portable fire extinguishers have the potential to leak, and should be inspected per the proper prescribing guidance.
MODELS/S/N AFFECTED:
All M20U and M20V Models:This Service Bulletin is applicable to the model MD302SAM Standby Attitude Module, part number series 6420302-( ) manufactured by MidContinent Instrument Co., Inc. (dba Mid-Continent Instruments and Avionics).
TIME OF COMPLIANCE:
Refer to - MidContinent Service Bulletin No.: SB MD302-08, Dated: August 29, 2018 -Subject:Product and Performance Enhancements
INTRODUCTION:
This service bulletin describes features associated with hardware changes that are identified at the product level as Modification (MOD) 3. Additionally, it describes an update to the product software represented by version 1.1.1.Refer to the attached for more information.
MODELS/ SN AFFECTED:
M20U OVATION ULTRA 32-0002 thru 32-0005; M20V ACCLAIM ULTRA 33-0002, 33-0003, 33-0005
TIME OF COMPLIANCE:
AS REQUIRED
INTRODUCTION:
Mooney International Corporation has developed a new door handle design.This Service Instruction has been written in 2 Steps, for convenience.Step 1:How to remove and replace existing door handle with the new design.Step 2:Sending the door panels to the factory for repair and recover.
MODELS/ SN AFFECTED:
M20R:29-0333 thru 29-0519; M20TN:31-0001 thru 31-0127 and 31-0129; M20U:32-0001 and On; M20V:33-0001 and On
TIME OF COMPLIANCE:
At Owners Discretion
INTRODUCTION:
It has been brought to our attention that Garmin will no longer manufacture the Integrated Avionics Unit GIA 63(W). However Garmin has stated that they will support/repair these units if required. Garmin's replacement for the GIA63(W) is the GIA 64(W) and it is not plug-n-play compatible with Mooney's Legacy G1000 Integrated Avionics System.
MODELS/S/N AFFECTED:
Garmin Flight Stream 510 (011-03595-( )) units with software version 2.40 or earlier are affected.
TIME OF COMPLIANCE:
Optional: This bulletin may be incorporated at the owner’s discretion and is not warranty reimbursable.
INTRODUCTION:
This modification consists of upgrading Flight Stream 510 software to version 2.41 (P/N006-B2021-41). Refer to the attached for more information
MODELS/S/N AFFECTED:
Aircraft equipped with Continental Motors, Inc. (CMI) IO-520, GTSIO-520, TSIO-520,IO-550, IOF-550, TSIO-550, TSIOF-550, and TSIOL- 550 model engines(operating with AVGAS)
TIME OF COMPLIANCE:
Refer to - (FAA) Federal Aviation Administration Special Airworthiness InformationBulletin No.: SAIB NE-18-16, Dated: June 20, 2018 - Subject: POWERPLANT - Alternator Drive Coupling
INTRODUCTION:
This Special Airworthiness Information Bulletin (SAIB) alerts registered owners, operators,and certified repair facilities of all airplanes equipped withContinental Motors, Inc. (CMI)IO-520, GTSIO-520, TSIO-520, IO- 550, IOF-550, TSIO-550, TSIOF-550, and TSIOL-550 model engines (operating with AVGAS) with direct drive alternator systems of the possiblefailure of the alternator drive coupling following maintenance events and/or improper installation.
MODELS/S/N AFFECTED:
Refer to - GARMIN Service Bulletin No.: 1831 Rev A - Dated: May 31, 2018 - Subject:Flight Stream 510 Software Upgrade to Version 2.40 (See attached document)
TIME OF COMPLIANCE:
Refer to - GARMIN Service Bulletin No.: 1831 Rev A - Dated: May 31, 2018 - Subject:Flight Stream 510 Software Upgrade to Version 2.40 (See attached document)
INTRODUCTION:
Flight Stream 510 Software Version 2.40 contains the following changes:• Improved robustness of flight data log streaming• Improved Bluetooth reliability• Fixed issue that caused the GTN to not install databases loaded to the Flight Stream510 from a PC• Fixed issue that caused SXM weather to no be sent to the portable device when theFlight Stream 510 is installed with a GDL 69 SXM without an audio subscription• Other functionality enabled by a future display LRU software updateRefer to the attached for more information.
MODELS/ SN AFFECTED:
M20M: 27-0343, 27-0351, 27-0352, 27-0355 & ON; M20R: 29-0412 & ON; M20TN: 31-0002 & ON; All Mooney M20U and M20V
TIME OFCOMPLIANCE:
AT NEXT ANNUAL OR WITHIN NEXT 100 FLIGHT HOURS
INTRODUCTION:
Mooney International Corporation has determined a solution to prevent inadvertent ruddertrim slipping during extremedeflections duringtake off. Use of a new cable anda special GSE030035 tool during installation are advised to prevent a permanent set in springs.
MODELS/S/N AFFECTED:
Refer to − Federal Aviation Administration (FAA), DOT [Docket No. FAA-2016-6673;Directorate Identifier 2015-NM-092-AD; Amendment 39-18978; AD 2017-16-01] (Seeattached; AD begins on page 10 of the attached document)
TIME OFCOMPLIANCE:
Refer to − Federal Aviation Administration (FAA), DOT [Docket No. FAA-2016-6673;Directorate Identifier 2015-NM-092-AD; Amendment 39-18978; AD 2017-16-01] (Seeattached; AD begins on page 10 of the attached document)
INTRODUCTION:
We are adopting a new airworthiness directive (AD) for certain Ameri-King Corporation emer-gency locator transmitters (ELTs) as installed on various aircraft. This AD was prompted bymultiple reports of ELT failure and a report of noncompliance to quality standards and manu-facturer processes related to Ameri-King Corporation ELTs.
MODELS/S/N AFFECTED:
MOONEYS EQUIPPED WITH G900X, G950, G1000, Cirrus Perspective®, and EmbraerProdigy® systems with GDU software versions 15.20 and earlier are affected.
TIME OF COMPLIANCE:
Refer to - the GARMIN SERVICE ADVISORY - NO.: 1729 Rev A -Registered G900X,G950, G1000, Cirrus Perspective®, and Embraer Prodigy® Owners and Operators-Is-suedSept 7, 2017.
INTRODUCTION:
Loading GDU software versions 15.10 through 15.20 may permanently lock saved waypoints.Updating the Jeppesen navigation database on systems with GDU software versions 15.10through 15.20 may also permanently lock saved waypoints.(see attached for more details).
MODELS/ SN AFFECTED:
M20R - 29-0523 thru 29-0525; M20TN - 31-0142, 31-0143
TIME OF COMPLIANCE:
ONE-TIME INSPECTION WITHIN NEXT 20 FLIGHT HOURS
INTRODUCTION:
Mooney International Corporation has determined the possibility of the existence of oversized holes in the 340035-501 & 340035-502 attach plates. Discrepant plates were static tested to ultimate loads under several scenarios with no detectable yeilding to parts or hardware.This will require a 1- Timeinspection and repair (if found incorrect) for the affected aircraft.
MODELS/ SN AFFECTED:
M20R - 29-0523 thru 29-0525 (Factory installed); M20TN - 31-0140 thru 31-0143 (Factory installed)
TIME OF COMPLIANCE:
Comply with this AD within the compliance times specified, unless already done.
INTRODUCTION:
The purpose of this Service Bulletin is to identify the United Instruments, Inc. Service Bulletin No. 13, dated March25, 2016 and FAA AD 2017-04-06 UnitedInstruments, Inc.: Amendment 39-18801; Docket No. FAA-2016-9345; Directorate Identifier 2016-CE-028-AD.This AD applies to United Instruments, Inc. 5934 series altimeters that were manufactured between January 2015 and February 2016 and installed in airplanes and helicopters.
MODELS/ SN AFFECTED:
Refer to Service Instruction M20-88A dated 12/14/2016
TIME OF COMPLIANCE:
AT OWNERS DISCRETION. Previous compliance of Service Instruction M20-88 satisfies compliance with thisService Bulletin M20-325
INTRODUCTION:
The purpose of this Service Bulletin is to increase the visibility of Mooney Service Instruction M20-88A dated 12/14/2016. Service Instruction M20-88A- There have been occasions when the elevator trim control wheel has been manually turned to the extreme nose up or nose down condition and the electric trim system was unable to move the trim indicator nut off the stop at the next electrically activated command. Manual movement must be the initial action to get the trim indicator nut off the stop, then the electrical system will operate normally. Refer to Service Instruction M20-88A dated 12/14/2016 for more detailed information.
MODELS/S/N AFFECTED:
Lycoming new, rebuilt and overhauled 4 and 6 cylinder aircraft engines with the new rollertappet configuration.
TIME OFCOMPLIANCE:
Whenever the new roller tappet engines are serviced - Refer to LYCOMING SERVICEINSTRUCTION NO. 1514C (Supersedes Service Instruction No. 1514B) - Issued10/13/2016- Roller Tappets Part Information Update(see Attached).
INTRODUCTION:
As a product improvement, Lycoming is installing roller tappets on its aircraft engines. Wide deck engines with roller tappets are identified with an “E” suffix after the serial number dashnumber (Example – L- ******-48E.) On rebuilt and Lycoming overhauled wide deck engineswith roller tappets, the letter “A” suffix is replaced with the letter “E” suffix on the engine serial number.
MODELS/S/N AFFECTED:
All LYCOMING reciprocating aircraft engines(see Attached).
TIME OFCOMPLIANCE:
BEFORE FURTHER FLIGHT- Refer to LYCOMING MANDATORY SERVICE BULLETINNO. 533C (Supersedes Service Bulletin No. 533B) - Issued 10/18/2016 - Recommended Action for Sudden Engine Stoppage, Propeller/Rotor Strike or Loss of Propeller/Rotor Blade or Tip (see Attached).
INTRODUCTION:
This Service Bulletin identifies propeller/rotor damage conditions and gives corrective action recommendations for aircraft engines that have had propeller /rotor damage
MODELS/S/N AFFECTED:
Continental Motors (CM), IO-520-B, BA, BB, C, CB, M, MB; TSIO-520-B, BB, BE, D, DB, E,EB,J,JB,K,KB,L,LB,N,NB,UB,VB,WB;IO-550-A,B,C,G,N,P,R;TSIO-550-B,C,E,G, K, N, and TSIOL-550-A, B, C aviation gasoline (AvGas) engines. Refer to CONTINENTAL MOTORS SERVICE BULLETIN NO. SB16-6- Issued 10/19/2016 - Engine Damage Due to Kickback (see Attached).
TIME OFCOMPLIANCE:
Anytime a kickback incident occurs perform the inspections set forth in this Service Document prior to further engine operation. - Refer to CONTINENTAL MOTORS SERVICE BULLETIN NO. SB16-6 - Issued10/19/2016 - Engine Damage Due to Kickback (see Attached).
INTRODUCTION:
Recent testing at Continental Motors (CM) has shown that “engine kickback” during engine start can result in high instantaneous torque loading of engine components and cause damage to the starter, adapter assembly or related components, up to and including damage tothe crankshaft gears and crankshaft gear's retaining screws. There have been occurrences where all six retaining screws holding the crankshaft gear have fractured.
MODELS/ SN AFFECTED:
M20M:27-0318, 27-0326 thru 27-0355; M20R:29-0333 thru 29-0525; M20TN:31-0001 thru 31-0143
TIME OF COMPLIANCE:
At Owners Discretion
INTRODUCTION:
Three optional packages with available subscription services are offered for Mooney Aircraft models equipped with G1000. Option 1 - Non-WAAS contains software only. Option 2&3 - WAAS Upgrade - Wide Area Augmentation System (WAAS) contains Option 1 software and additional features which provides GPS precision approach capability.
MODELS/S/N AFFECTED:
Refer to - SPECIAL AIRWORTHINESS INFORMATION BULLETIN No. CE-16-09 DatedNov 23, 2015 - AUTO FLIGHT - AUTOPILOT (see Attached).
TIME OF COMPLIANCE:
Refer to - SPECIAL AIRWORTHINESS INFORMATION BULLETIN No. CE-16-09 DatedNov 23, 2015 - AUTO FLIGHT - AUTOPILOT (see Attached).
INTRODUCTION:
This Special Airworthiness Information Bulletin advises you of an airworthiness concern, spe-cifically that certain Honeywell/Bendix King autopilots (AP) can experience inadvertent disen-gagement without clear annunciation to the pilot and may also fail to engage with conflictingannunciation to the pilot. These failure conditions are the result of a resistor that can fail openin the autopilot computer. (See Attached for more information).
MODELS/S/N AFFECTED:
Per LYCOMING Service Instruction No. 1458G - Dated 11/10/2015 - All supported Lycoming reciprocating aircraft engines (see attached).
TIME OFCOMPLIANCE:
Per LYCOMING Service Instruction No. 1458G - Dated 11/10/2015 - Whenever new connecting rods and/or new connecting rod bolts are being installed (see attached).
INTRODUCTION:
Per LYCOMING Service Instruction No. 1458G - Dated 11/10/2015 - Incomplete review of allthe information in this document can cause errors. Read the entire Service Instruction tomake sure you have a complete understanding of the requirements (see attached).
MODELS/S/N AFFECTED:
Refer to:LYCOMING Supplement 3 to Mandatory Service Bulletin No. 342G Issued November 2, 2015 - Approved Alternate Method of Compliance (AMOC) to AD2015-19-07 (see attached) (see attached).
TIME OFCOMPLIANCE:
Refer to: LYCOMING Supplement 3 to Mandatory Service Bulletin No. 342G Issued November 2, 2015 - Approved Alternate Method of Compliance (AMOC) to AD2015-19-07 (see attached) (see attached).
INTRODUCTION:
Refer to: LYCOMING Supplement 3 to Mandatory Service Bulletin No. 342G Issued November 2, 2015 - Approved Alternate Method of Compliance (AMOC) to AD2015-19-07 (see attached) (see attached).
MODELS/S/N AFFECTED:
Per LYCOMING Service Instruction No. 1443K - Dated 10/30/2015 - See Table 1 (see at-tached).
TIME OFCOMPLIANCE:
Per LYCOMING Service Instruction No. 1443K - Dated 10/30/2015 - Not Applicable (see at-tached).
INTRODUCTION:
Per LYCOMING ServiceInstruction No. 1443K - Dated 10/30/2015 - Incomplete review of all the information in this document can cause errors. Read the entire Service Instruction tomake sure you have a complete understanding of the requirements (see attached).
MODELS/S/N AFFECTED:
Per CONTINENTAL MOTORS® AIRCRAFT ENGINE SERVICE BULLETIN No. SB15-6Dated: October 15, 2015 - New and Rebuilt: IO346, GTSIO520, IO520, LIO520, LTSIO520,TSIO520, IO550, IOF550, TSIO550, and TSIOF550 (see attached).
TIME OFCOMPLIANCE:
Per CONTINENTAL MOTORS® AIRCRAFT ENGINE SERVICE BULLETIN No.SB15-6 Dated: October 15, 2015 - At cylinder repair, replacement, or engine major overhaul(see attached).
INTRODUCTION:
Per CONTINENTAL MOTORS® AIRCRAFT ENGINE SERVICE BULLETIN No.SB15-6 Dated: October 15, 2015 - NiC3 cylinders are initially being offered as an optionalreplacement for Continental Motors cylinders. Currently, only cylinders with 5.25” bore dia-meters are available. The nickel silicon carbide plating process applies a corrosion and wearresistant protective coating to the cylinder barrel. Continental Motors plans to expand theNiC3 cylinder offerings to our full product line in the near future (see attached).
MODELS/S/N AFFECTED:
Per LYCOMING Service Instruction No. 1533C - Dated 09/03/2015 - All Lycoming Reciprocating Aircraft Engines (see attached).
TIME OFCOMPLIANCE:
Per LYCOMING Service Instruction No. 1533C - Dated 09/03/2015 - All Lycoming Reciprocating Aircraft Engines (see attached).
INTRODUCTION:
Per LYCOMING Service Instruction No. 1533C - Dated 09/03/2015 - Incomplete review of allthe information in this document can cause errors. Read the entire Service Instruction tomake sure you have a complete understanding of the requirements (see attached).
MODELS/S/N AFFECTED:
Per LYCOMING Service Bulletin No. 621A (Supersedes Service Bulletins No. SB-621) Issued September 2, 2015 - IO-320, -360, -390, -540; -580, AEIO-320, -360, -390, -540; HIO-360,LIO- 320-B1A, LIO-360, O-540-L3C5D, and TO-360-C1A6D (see attached).
TIME OFCOMPLIANCE:
Per LYCOMING Service Bulletin No. 621A (Supersedes Service Bulletins No. SB-621) Issued September 2, 2015 - 50 hours from the issue date of this Service Bulletin or the next regularlyscheduled maintenance event (whichever occurs first) (see attached).
INTRODUCTION:
Per LYCOMING Service Bulletin No. 621A (Supersedes Service Bulletins No. SB-621) Issued September 2, 2015 - Incomplete review of all the information in this document can cause errors. Read the entire Service Bulletin to make sure you have a complete understanding of therequirements.
MODELS/S/N AFFECTED:
Per AmSafe Service Bulletin SB507592-401-25-01 - Dated 06/15/2015 - All Aircraft Types Affected (if AmSafe Belts are Installed) (see attached).
TIME OF COMPLIANCE:
Per AmSafe Service Bulletin SB507592-401-25-01 - Dated 06/15/2015 -Aircraft equippedwith TRW brand inflators used in conjunction with AmSafe Seatbelt Airbag System. A com-plete list of effected Inflator part numbers are referenced(see attached).
INTRODUCTION:
Per AmSafe Service Bulletin SB507592-401-25-01 - Dated 06/15/2015 -AmSafe's inflatorre commended service/storage life has been extended. Previously, AmSafe defined the inflators maximum service/storage life as ten (10) years. The current approved substantiating dataallows a maximum combined service/storage life of 12 years (from date of manufacture) withno required refurbishment.(see attached).
MODELS/S/N AFFECTED:
Per LYCOMING Service Instruction No. 1533B -Dated 07/29/2015 - All Lycoming Reciprocating Aircraft Engines (see attached).
TIME OF COMPLIANCE:
Per LYCOMING Service Instruction No. 1533B - Dated 07/29/2015 - As Required for Replacement (see attached).
INTRODUCTION:
Per LYCOMING ServiceInstruction No. 1533B - Dated 07/29/2015 - Incomplete review of all the information in this document can cause errors. Read the entire Service Instruction tomake sure you have a complete understanding of the requirements (see attached).
MODELS/S/N AFFECTED:
Per LYCOMING Service Instruction No. 1526G - Dated 07/24/2015 - All Lycoming Reciprocating Aircraft Engines (see attached).
TIME OF COMPLIANCE:
Per LYCOMING Service Instruction No. 1526G - Dated 07/24/2015 - As Required for Replacement (see attached).
INTRODUCTION:
Per LYCOMING ServiceInstruction No. 1526G - Dated 07/24/2015 - Incomplete review of allt he information in this document can cause errors. Read the entire Service Instruction tomake sure you have a complete understanding of the requirements.
MODELS/S/N AFFECTED:
Per LYCOMING Service Letter No. L247D - Dated 07/27/2015 - All Owners and Operators of Lycoming Aircraft Engines (see attached).
TIME OF COMPLIANCE:
LYCOMING Service Letter No. L247D Issued July 27, 2015 - Shelf Life Requirements(see Attached).
INTRODUCTION:
Per LYCOMING Service Letter No. L247D - Dated 07/27/2015 - Added part numbers andrevised shelf lives in Table 1 and removed Table 3 (see Attached).