Airworthiness Directives for Cirrus SR22T G6

DESCRIPTION OF WORK PERFORMED OR APPROVED DATA USED Repair Station No. 5T2R901C 530 Airport Rd. Lititz, PA 17543 Phone: 717-735-5179 DATE: 7/31/2020 A/C TSN: 105.1 HOBBS: 130.8 AGENCY & CERTIFICATE NO. WORK PERFORMED/RETURNED TO SERVICE Cirrus CMX 100hr Airframe Inspection: Serviced gascolator IAW Cirrus AMM 28-20. Performed servicing of Induction Air Filter. Inspection/ Check of aircraft exhaust system. Inspection of alternate air door and air intake ducts. Inspected the #1 battery connectors for general condition and operation. Inspection of cabin heat box and ducts. Complied with brake wear check. Serviced brake fluid reservoir. Inspected/check the nose landing gear oleo strut. Lubricated aircraft IAW Cirrus AMM 12-10 lubrication schedule. All AD's current through 2020-15... Re-bonded the co-pilots pouch to side panel as required..... Removed and replaced the NLG wheel cover, strut fairing and towbar protection Aerotect Paint Protection Film.... C/W SB 2X-91-02 Backshell Strain Relief Inspection: Removed, and reinstalled back shell strain relief correctly at Iridium Unit connector, GDL69A, and GTS800 unit.... Hartzell ASB-081 Alternator Castellated Hex-Nut Inspection Not Applicable by Alternator Date of Manufacture (08-2020). Maintenance Release The aircraft and/or component(s) on N200DR was repaired and inspected in accordance with the current rules and regulations of Title 14 of the Code of Federal Regulations, was found Airworthy and was returned to service. DATE: 7/31/2020 SIGNE Joshua J. Ferry Work Order: 7428-07-2020 Printed by EBis 3 (datcomedia.com) Certified Repair Station No. 5T2R901C NO. TO SERVICE DATE OF COMPLETION AIRCRAFT TIME IN SERVICE MAKE: Cirrus MODEL: SR22 S/N: 4860 REG. NO: N200DR WORK ORDER: 3690-10-2020 MAINTENANCE RECORD F.A.R. 43.9 DESCRIPTION OF WORK PERFORMED OR APPROVED DATA USED 1 of 2 DeltaFox Aviation DeltaFox Repair Station No. 897R016D AVIATION 10771 James Payne Court Manassas, VA 20110 Phone: 703.438.8450 AGENCY & CERTIFICATE NO. WORK PERFORMED/RETURNED TO SERVICE DATE: 11/16/2020 A/C TSN: 126 FLIGHTTIME: 126 . Airframe Entries Complied with Annual Inspection IAW Cirrus SR22 AMM Inspection Guide 5-20. Removed cowlings, access panels, wing tips, landing gear fairings and interior. Inspected wings, fuselage and flight controls. Removed wheels, inspected wheals and brakes, re-installed wheels. Performed inspection and servicing of gascolator, Replaced oring and stat-o-seal. Inspected for leaks and general condition. Inspected electrical wiring for chafing and security. Verified AD compliance through bi-weekly issue 2020-23 Researched all Cirrus SR22 Service Bulletins for this S/N aircraft. Lubricated as required per Cirrus AMM 12-20. Re-installed cowlings, access panels, wing tips, landing gear fairings and interior. • Tested the ELT, P/N: A3-06-2749-1 S/N: 251-15840, as required by CFR 91.207. All tests passed. Battery expiration date is Jan. 2026. Next test due 11/30/2021. . C/W visual inspection of both interior and exterior wing fittings. No defects noted. • Inspected Engine mount weldment and lower mount attach fittings. No defects found. .Removed and replaced induction air filter P/N: BA24 IAW Cirrus SR22 AMM Chapter 71-60. Removed and replaced both LH and RH brake pads P/N: 31392-105 IAW Beringer MM. Inspected Fire Extinguisher. No defects found. Weight: 2lbs 7.4oz. Next Inspection due 11/30/21. Inspected Beringer Wheels & Brakes per ICA. No defect noted. DATE OF COMPLETION AIRCRAFT TIME IN SERVICE MAINTENANCE RECORD F.A.R. 43.9 DESCRIPTION OF WORK PERFORMED OR APPROVED DATA USED 2 of 2 AGENCY & CERTIFICATE NO. WORK PERFORMED/RETURNED TO SERV . C/W Beringer SB 016. Drained brake system of brake fluid. Removed Parking Brake Valve. Found the parking brake valve to be affected by part number/batch number (Parking Brake Valve P/N: FP-003N(B), Batch #: 32-19.1). Installed new Parking Brake Valve P/N: FP-003N(B), Batch #: 19-20 per Cirrus SR22 AMM 32-42. Bled brakes, ops and leak checked good. · AD 2020-16-11 is N/A by engine S/N per Continental MSB 18-08B Section II. I certify that the above stated maintenance was performed in accordance with the current regulations of the FAA and the aircraft/engine/component identified above is presently airworthy and approved for return to service. DATE: 11/16/2020 SIGNED: Gudmundur J. Thorleifsson Certified Repair Station No. 897R016D Work Order: 3690-10-2020 Printed by EBis 3 (datcomedia.com) DUNCAN AVIATION DATE OF COMPLETION AIRCRAFT TIME IN SERVICE MAINTENANCE RECORD F.A.R. 43.9 DESCRIPTION OF WORK PERFORMED OR APPROVED DATA USED AGENCY & CERTIFICATE NO. WORK PERFORMED/RETURNED TO SERVE 2 of 2 Duncan Aviation Inc. d/b/a Duncan Avionics Inc. 15290 N. 78th Way Ste D-100 SCOTTSDALE AZ. 85260 CRS JGV5194F Phone (480) 922-3575 Fax (480) 315-0874 A/C TT 205.6 REG N200DR TYPE SR22 S/N 4680 Tested and Inspected the Pilot, the Co-Pilot, and Standby static pressure System, ADAHRS and standby altimeter I/A/W title 14 CFR Part 91.411 and ATC transponder systems I/AW Title 14 CFR Part 91.413 and found to comply with title 14 CFR part 43, Appendices E and F. All work performed I/A/W Cirrus Airplane Maintenance Manual Models SR22 and SR22T 34-10, 34-20, and G1000 System Maintenance Manual (Standard Piston/TurboProp) Section 9.3, Rev E Dated 5/27/11. The #1 ADAHRS P/N 36745-001 S/N 3KY003898, The #2 ADAHRS P/N 36741-001 S/N 3KY003921, and MD302 Standby Attitude Module P/N 6420302-6 S/N G17-10469 were tested to 25,000 ft on 11/23/2021. The #1 and #2 Encoder Data Correspondence was tested to 25,000 ft on 11/23/2021. The Pilot, Co-Pilot, and Standby Static Pressure System were tested and Inspected on 11/23/2021. The ATC Transponder was tested on 11/23/2021. The above described repair or maintenance is approved for retum to service. A detailed record of the work performed is on file at this repair station under W.O. #8JRDA SIGNED DUNCAN QI 2551 DATE 11/23/2021 DATE OF COMPLETI DATE OF COMPLETION AIRCRAFT TIME IN SERVICE KEYSTONE AVIATION. MAINTENANCE RECORD F.A.R. 43.9 DESCRIPTION OF WORK PERFORMED OR APPROVED DATA USED 15001 N Airport Dr. Scottsdale, AZ 85260 Ph. 623-562-3040 CRS# K4LR032E AGENCY & CERTIFICATE NO. WORK PERFORMED/RETURNED TO SERVICE AIRFRAME LOG ENTRY DATE: Nov 24, 2021 Aircraft Make: Cirrus Serial Number: 4860 Aircraft Model: SR22 Hobbs: 257.7 Accomplished the Following Scheduled Airframe Maintenance Functions: Tail Number: N200DR Flight: 205.6 C/W preliminary inspection, visual walk-around of exterior and interior of aircraft for damage and airworthiness concerns. Found no additional discrepancies other than the customer work scope. Comply with 100hr/Annual Inspection: Complied with Annual/100 Hr. Inspection IAW 14 CFR 43 Appendix D IAW Cirrus SR22/22T 100 Hr/Annual Inspection Checklist AMM- Chap. 5-20. * Comply with FAR 91.207(d) 12 Month Inspection: Reference model E-01 installation manual/operational manual Rev. Date 5/7/2002. No defects noted. Complied with #2 Main Battery Replacement: Removed old #2 batteries. Installed new batteries P/N: 50979-001. System ops checks good. IAW SR22 AMM 24-30. Comply with Monthly/Annual Portable Fire Extinguisher Check: Inspected portable fire extinguisher, no defects noted. IAW manufacturers Maintenance instructions located on bottle. Perform Gascolator Inspection/Clean: Removed gascolator bowl. Cleaned out fuel screen, no defects noted. Reinstalled filter bowl with new o-ring P/N: MS29513-137, new stat-o- seal P/N: NAS1523-8B. Ran system no leaks noted. IAW Cimus SR22 AMM 28-20. Perform 91.411/91.413 Checks, See Duncan Aviation Log Book Entry W/O# 8JRDA for resolution. Alt 1 Due Insp, C/W 2 Yr/500 Hr inspection of the #1 alternator. No defects noted. IAW Cirrus SR22 AMM 24-30. Alt 2 Due Insp, C/W 2 Yr/500 Hr inspection of the #2 alternator. No defects noted. IAW Cirrus SR22 AMM 24-30. Magnetometer due Func Test, C/W magnetometer functional check. No defects noted. IAW Cirrus SR22 AMM 34-20. Perform Adj Test of the GSM 86, Performed adjustment/test of GSM 86 servos per Cirrus SR22 MM Ch 22-10. Ice Protection Filter due change, Replaced TKS filter p/n 21986-203 per Cirrus SR22 MM Ch 30-07. Nav Databases due, C/W updates on databases . Accomplished the Following ICA Maintenance Functions: Complied with Tannis Heater 100hr Inspection: Complied with Tanis engine heat ICA no defects noted operational and function checks were satisfactory all work was performed LAW Tanis ICA Document No. TICA3052 REV. A Dated AUG-29-2014. Verified AD Compliance through BW 2021-23 No AD's due at this time Accomplished the Following Un-Scheduled Maintenance Functions: LH/RH Brake Discs at limit, Removed and Replaced Right & Left Hand Brake Disk With New Brake Disk P/N: 31392-108 L.A. W Beringer C.M.M BRG-ALTP-02 LH/RH Brake caliper pistons stiff, Removed left and right brake calipers. Removed old seals and cleaned calipers. Installed new seals in both left and right brake calipers P/N: 31392-107. Reinstalled both left and right brake calipers. IAW Beringer BRG-ALTP-02 Doc Ref# MM-ETSO-001. Brakes need bled. C/W brake bleeding procedures. LH/RH Brake pads worn to limits, Removed And Replaced Right & Left Hand Brake Pads With New Brake Pads P/N: 31392-105 I.A. W Beringer C.M.M BRG-ALTP-02 ELT Intermittently transmits, Removed ELT p/n A3-06-2749-1 s/n 251-15840 and installed a new ELT s/n 323-02546. Batt Exp: Dec 2027. HEX ID: 2DC8A193E4FFBFF. LH MLG Tire worn, Removed left main wheel assy. Removed old tire P/N: 025-5012-1, S/N: 9004 S00137. Installed new tire P/N: 025-501-1, S/N: 1061 T00199, with new o-ring P/N: J-JTR-007N. Serviced tire to 65 psi, no leaks noted. Reinstalled wheel assy back on to the aircraft. IAW Beringer BRG-ALTP-02 Doc Ref# MM-ETSO-001. (Continued) MAINTENANCE RECORD F.A.R. 43.9 DATE OF COMPLETION AIRCRAFT TIME IN SERVICE (From Previous) DESCRIPTION OF WORK PERFORMED OR APPROVED DATA USED AGENCY & CERTIFICATE NO. WORK PERFORMED/RETURNED TO SERVICE Right Static Port QD found leaking, Replaced right side static port fittings p/n 51228-002 & 51228-003. IAW Cirrus SR22 AMM 34-00. System has no leaks noted. Stby Altimeter out of limits, Removed old standby altimeter P/N: 6420302-6, S/N: J19-12120. Installed overhauled standby module unit P/N: 6420302-6, S/N: G17-10469. Refere sqk 3 of this work order for functional and leak check. IAW Cirrus SR22 AMM 34-10 I certify that this aircraft has been Inspected/Repaired IAW 14 CFR 43 Appendix D IAW Cirrus SR22/22T 100 Hr./Annual Inspection Checklist AMM Chap. 5-20 P/N 13773-002, Rev. 3, dated 16 Jan 2020. This Aircraft has been determined to be in an airworthy condition and is approved to return to service in regards to the work accomplished. For additional details see W/O# 1021015 Signature: Cert: FAA CRS# K4LR032E wo: W-0122080 N200DR Flight: 254.6 KEYSTONE AVIATION. Keystone Aviation SDL 15001N Airport Dr. Scottsdale, AZ 85260 USA 623-562-3040 CRS#: K4LR032E CIRRUS DESIGN CORP, SR22, S/N: 4860 Hobbs: 316.1 Airframe page 1 of 2 June 01, 2022 1. Complied with preliminary inspection, no additional discrepancies found beyond customer discrep- ancies identified below. 2. During initial inspection found both No. 1 and No. 2 battery switches already on and both fully dead. Turned both off. No further troubleshooting possible at this time with the batteries dead. 3. Removed the upper engine cowling to gain access to the No. 1 Battery. Removed the installed battery (PN SN) and replaced with new Model RG24-11M Battery (PN 53030-001, SN 41216004). Initial battery ops check OK. Reinstalled upper engine cowling. Installed P/N RG24-11M - Battery Concord 24V S/N: 41216004. 4. While pulling required circuit breaker, found boost pump in on position. Placed boost pump in off position. Removed battery(s) #2 from aircraft P/N 50979-001 NSN(2 each). Installed new battery(s) P/N 50979-001 NSN (2 each) on aircraft. Ops check good. Work IAW SR22 MM 24-30. 5. Cleaned contaminants from the battery tray. Thoroughly dried the area. 6. Downloaded and uploaded chart database cycle 11-2022. Next charts database update due 10 June 2022. Work IAW Cirrus Perspective+ pilots guide 190-02183-02 Rev. A. All other databases not due update at this time.