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N354LL

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2014 Agustawestland Philadelphia AW119MKII · Pratt & Whitney Canada PT6B-37A

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Registered owners
Critical Care Services Inc DBALife Link III
Location
Blaine, MN
Owner type
Corporation
Serial number
14822
Year built
2014
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, normal
Airworthiness date
April 11, 2014
Certificate issued
June 2, 2014
Expires
June 30, 2027
Mode S code
A3F4AE
Agustawestland Philadelphia AW119MKIIAirframe model · 8 seats · 1 engine · 180 registeredTCDS H7EUAirframe · Agustawestland Philadelphia AW119MKIITCDS E21NEEngine · Pratt & Whitney Canada PT6B-37A

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 30

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2009In forceSuperseded2026
See all 38 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N354LLMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Agustawestland Philadelphia AW119MKII aircraft

FAA incident reports

No FAA accident or incident reports matched to N354LLMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Agustawestland Philadelphia AW119MKII aircraft

Service difficulty reports · 7

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 37CA202602230001Guide · departedAFTER DEPARTING ASHLAND HOSPITAL IN SUPERIOR WI, THE R/H CABIN WINDOW SLIDER DEPARTED THE AIRCRAFT.Feb 21, 2026 · N354LL · Agusta AW119MKII · Flight Compartment WindowsSDR 37CA2025/02/2601Tach Generator · defectiveN1 TACHOMETER GENERATOR ERRATIC READINGS DURING START UP CAUSING A MIS-COMPARE P CAUTION MESSAGE.Feb 20, 2025 · N354LL · Agusta AW119MKII · Engine RPM Indicating SystemSDR QMLA2019042271939Pressure Switch · failedSHORTLY AFTER DEPARTURE PILOT RECEIVED "XMSN OIL PRESSURE" WARNING LIGHT ALONG WITH AN INCREASE IN INDICATED PRESSURE. PERFORMED PRECAUTIONARY LANDING AND MAINTENANCE REPLACED THE TRANSMISSION OIL PRESSURE SWITCH. TRANSMISSION OIL PRESSURE RETURNED TO NORMAL AApr 17, 2019 · N354LL · Agusta AW119MKII · Main Rotor GearboxSDR QMLA2017110117123Mount · crackedDURING MAIN ROTOR TRANSMISSION CHANGE, FOUND THE LT AND RT AIRFRAME TRANSMISSION DECK FITTINGS CRACKED.Nov 1, 2017 · N354LL · Agusta AW119MKII · Main Rotor Transmission MountSDR QMLA2017041717038Retainer · crackedFOUND 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, AND 1 CRACK RIGHT HAND DOOR POST AFT EDGE STA 2049.5 EXTENDING FROM WL 1400.0 TO 1402.0, CRACK IS APPROXIMATELY 1.5 INCHES LONG.Apr 17, 2017 · N354LL · Agusta AW119MKII · Fuselage Miscellaneous StructureSDR QMLA2015090415082Bearing · crackedDURING A0521 NT, 100 HR TAIL ROTOR INSPECTION, WAS REMOVING THE TAIL ROTOR CROSS HEAD ASSEMBLY & FOUND THE BLADE END PC LINK BEARING CRACKED WITH A CHUNK MISSING FROM THE FLANGE AREA OF THE BEARING, THE SPHERICAL SURFACE WAS INTACT. R & R PC LINK. EXCESSIVE Sep 4, 2015 · N354LL · Agusta AW119MKII · Tail Rotor Control SystemSDR QMLA2015070915056Cowling · crackedFOUND CRACKED ENG COWLING ON PREFLIGHT, PORT SIDE OF FWD ENG COWLING AFT EDGE OF ACCESS DOOR OPENING. VERTICAL STIFFENER ALSO FOUND CRACKED WHEN INVESTIGATING FURTHER.Jul 9, 2015 · N354LL · Agusta A119 · Engine Cowling System
Reports on N354LL not matched to an aircraft · 1

They name N354LL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR QMLA2017102617117Frame · chafedFOUND EVIDENCE OF CHAFING ON LOWER EDGE OF FRAME 5, X 4692, Y 2560, Z 317, DURING PRE CLOSE INSPECTION OF AVIONIC BAY. NOTE THAT CURRENT HARDWARE IS IN LINE WITH THE GAP IN-BETWEEN FRAME 5 AND MED WALL AND ONLY CONTACTS IF TRIM IS DEFLECTED BACK WHEN PUSHING Oct 26, 2017 · N354LL · Urocop EC135P2 · Fuselage Main, Frame

STCs that may be installed · 58

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 58 STCs