# N355LL: 2014 Agustawestland Philadelphia AW119MKII - Status: Valid registration - Airframe: Agustawestland Philadelphia AW119MKII (registry code 0260401, TCDS H7EU (OpenAirDocs match)) - Engine: Pratt & Whitney Canada PT6B-37A (registry code 52179, TCDS E21NE (OpenAirDocs match)) - Serial number: 14823 - Year built: 2014 - Type: Rotorcraft - Airworthiness: Standard, normal - Airworthiness date: May 15, 2014 - Certificate issued: June 23, 2014 - Expires: June 30, 2027 - Mode S code: A3F865 - Registered owner: Critical Care Services Inc DBA, Life Link III - Location: Blaine, MN - Owner's area on the map: 45.1764° N, 93.1839° W: Placed by OpenAirDocs at the center of ZIP code 55449, within about 3 miles (OpenAirDocs) - Page: https://openairdocs.org/aircraft/N355LL ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs matched by airframe (Agustawestland Philadelphia AW119MKII) (OpenAirDocs) - [AD 2026-17-07](https://openairdocs.org/ad/2026-17-07): Main rotor mast/swashplate · Leonardo A109A, A109A II, A109C and 6 more. Effective Oct 2, 2026 - [AD 2025-25-13](https://openairdocs.org/ad/2025-25-13): Powerplant System · Leonardo AW119 MKII and A119. Effective Jan 13, 2026 - [AD 2025-18-01](https://openairdocs.org/ad/2025-18-01): Main Rotor Head · Leonardo A109E, A109S, AW109SP and 2 more. Effective Sep 25, 2025 - [AD 2025-17-10](https://openairdocs.org/ad/2025-17-10): Main Rotor Control · Leonardo A109A, A109A II, A109C and 3 more. Effective Sep 9, 2025 - [AD 2025-09-06](https://openairdocs.org/ad/2025-09-06): Battery/charger system · Leonardo A119 and AW119 MKII. Effective Jun 16, 2025 - [AD 2024-18-01](https://openairdocs.org/ad/2024-18-01): Rotorcraft Flight Control · Leonardo A119 and AW119 MKII. Effective Nov 12, 2024 - [AD 2023-25-08](https://openairdocs.org/ad/2023-25-08): Main Rotor System · Leonardo A109E, A109S, AW109SP and 2 more. Effective Feb 2, 2024 - [AD 2023-17-07](https://openairdocs.org/ad/2023-17-07): Starter-Generator · Leonardo A119 and AW119 MKII. Effective Nov 1, 2023 - [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023 - [AD 2021-21-03](https://openairdocs.org/ad/2021-21-03): Rotorcraft Flight Control, Rotorcraft Servo System · Leonardo A109A, A109A II, A109C and 6 more. Effective Dec 10, 2021 - [AD 2021-20-18](https://openairdocs.org/ad/2021-20-18): Passenger compartment doors · Leonardo AW119 MKII. Effective Nov 3, 2021 - [AD 2021-16-06](https://openairdocs.org/ad/2021-16-06): Tail Rotor Drive Shaft · Leonardo A119 and AW119 MKII. Effective Sep 27, 2021 - [AD 2021-14-14](https://openairdocs.org/ad/2021-14-14): Instrument System Wiring · Leonardo AW119 MKII. Effective Jul 26, 2021 - [AD 2021-03-15](https://openairdocs.org/ad/2021-03-15): Tail Rotor System · Leonardo A119 and AW119 MKII. Effective Apr 1, 2021 - [AD 2020-26-10](https://openairdocs.org/ad/2020-26-10): Placards and markings · Leonardo A119 and AW119 MKII. Effective Feb 1, 2021 - [AD 2020-21-21](https://openairdocs.org/ad/2020-21-21): Main Rotor Head · Leonardo A109E, A109S, A119 and 2 more. Effective Nov 24, 2020 - [AD 2020-15-16](https://openairdocs.org/ad/2020-15-16): Tail Rotor Drive System · Leonardo A109E, A109K2, A109S and 3 more. Effective Aug 27, 2020 - [AD 2018-06-51](https://openairdocs.org/ad/2018-06-51): Main Rotor Mast/Swashplate · Agusta A109A, A109A II, A109C and 6 more. Effective Jun 7, 2018 - [AD 2018-07-02](https://openairdocs.org/ad/2018-07-02): Main Rotor Blades · Agusta A109E, A109S, A119 and 2 more. Effective Apr 13, 2018 - [AD 2015-05-52](https://openairdocs.org/ad/2015-05-52): Tail Rotor Controls · Agusta A109, A109A, A109A II and 7 more. Effective Apr 29, 2015 - [AD 2015-05-05](https://openairdocs.org/ad/2015-05-05): Main Rotor System · Agusta A109S, A119, AW109SP and 1 more. Effective Apr 23, 2015 - [AD 2014-23-02](https://openairdocs.org/ad/2014-23-02): Main Rotor Gearbox · Agusta A109E, A109K2, A119 and 1 more. Effective Dec 26, 2014 - [AD 2014-11-07](https://openairdocs.org/ad/2014-11-07): Main Rotor System · Agusta A109A, A109A II, A109C and 6 more. Effective Jun 18, 2014 - [AD 2013-20-51](https://openairdocs.org/ad/2013-20-51): Tail rotor system · Agusta A109A, A109A II, A109C and 6 more. Effective Oct 25, 2013 - [AD 2013-19-01](https://openairdocs.org/ad/2013-19-01): Flight Compartment Windows · Agusta A119 and AW119 MKII. Effective Oct 25, 2013 - [AD 2013-09-06](https://openairdocs.org/ad/2013-09-06): Rotors Flight Control · Agusta A119 and AW119 MKII. Effective Jun 20, 2013 - [AD 2010-12-51](https://openairdocs.org/ad/2010-12-51): Tail Rotor Gearbox · Agusta A119 and AW119 MKII. Effective Sep 17, 2010 - [AD 2009-12-07](https://openairdocs.org/ad/2009-12-07): Cargo hook lever · Agusta A109E, A109S, A119 and 1 more. Effective Jul 17, 2009 Historical (superseded or no longer in force): AD 2021-22-05, AD 2021-23-13, AD 2020-19-11, AD 2020-13-02, AD 2018-07-08, AD 2014-04-14, AD 2010-15-51 ## ADs matched by engine (Pratt & Whitney Canada PT6B-37A) (OpenAirDocs) - [AD 2020-18-05](https://openairdocs.org/ad/2020-18-05): Fuel Control/Turbine Engines · Pratt & Whitney Canada PT6B-37A. Effective Oct 7, 2020 - [AD 2019-22-03](https://openairdocs.org/ad/2019-22-03): Turbine Engine Reduction Gear · Pratt & Whitney Canada PT6B-37A. Effective Dec 24, 2019 Historical (superseded or no longer in force): AD 2015-20-04 ## Information bulletins (advisory) - [SAIB SW-18-13](https://openairdocs.org/saib/SW-18-13): Main Transmission Plate Fitting - [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System ## Service difficulty reports (3) - [SDR QMLA2018061418071](https://openairdocs.org/sdr/QMLA2018061418071), Jun 14, 2018: DAMPER. DURING INSPECTION, FOUND THE MAIN ROTOR DAMPER ON THE YELLOW BLADE WAS CRACKED ALONG INBOARD MOUNTING FLANGE, COMPLETELY THROUGH THE UPPER FORK AND STARTING ON - [SDR QMLA2018052918064](https://openairdocs.org/sdr/QMLA2018052918064), May 21, 2018: FITTING. FOUND A CRACKED RT TRANSMISSION FITTING DURING AN EDDY CURRENT INSPECTION IAW EO 49-5300-EO-2335. - [SDR QMLA2017041717039](https://openairdocs.org/sdr/QMLA2017041717039), Apr 17, 2017: RETAINER. FOUND 2 EACH CRACKS AT STA 2049.5, BL 480 LT AND BL 480 RT. RETAINER AND 2 EACH CRACKS AT FASTENER STA 2049.5 LEFT/RIGHT WL 1150.0. --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.