N352LL

AGUSTAWESTLAND PHILADELPHIA CO AW119MKII · 2014 · Rotorcraft · 1 engine · 8 seats · Valid Registration

Registered owner: CRITICAL CARE SERVICES INC DBA, MN (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
CRITICAL CARE SERVICES INC (37CA)Certificate holderMatched by certificate designator
CRITICAL CARE SERVICES INC (37CA)Operatoron 2021-02-13Operator named in NTSB report

Accident & incident history

Accident · 2021-02-13 Operator named in NTSB report
AGUSTAWESTLAND PHILADELPHIA CO AW119MKII No injuries Part 135CRITICAL CARE SERVICES INC

Operated by CRITICAL CARE SERVICES INC DBA (per NTSB report)

Source: NTSB case CEN21LA128

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

5 reports on file, 2017-04-17 – 2026-07-09.

OTHER · 2026-07-09 Matched by certificate designator
ATA 3243

Part: SKID — CORRODED (ZONE 700) · airframe 5,214 hrs

CORROSION WAS IDENTIFIED IN THE SKID TUBE BUSHING AREA WHERE SKID SHOE THROUGH BOLTS ATTACH.

Source: SDR 37CA2026070900144
SMOKE/FUMES/ODORS/SPARKS · 2022-09-29 Matched by certificate designator
ATA 2460

Part: MAGNETOMETER — FAILED (ALTITUDE IND) · airframe 3,440 hrs · 11,069 cycles

AIRCRAFT HAS BURNT ELECTRICAL SMELL THROUGHOUT COCKPIT AND CABIN. AIRCRAFT WAS AT 3500 FT MSL STARTED DECENT, SMELL GOT STRONGER. DECIDED TO LAND IN FIELD, ON THE WAY DOWN LOST STANDBY ATTITUDE INDICATOR, #3 VHF RADIO, HSI INDICATIONS ON PFD AND SYNTHETIC VISION ON PFD. UPON SHUT DOWN DISCOVERED STANDBY ATTITUDE INDICATOR CIRCUIT BREAKER POPPED. MAGNETOMETER WAS DETERMINED TO BE THE FAULT, WHICH CAUSED THE FAILURE OF THE CIRCUIT BREAKER WHICH CAUSED THE SMELL.

Source: SDR 2022F00381
F.O.D. · 2021-02-13 Matched by certificate designator
ATA 6210

Part: BLADE — DAMAGED (MAIN ROTOR) · airframe 2,632 hrs · 8,660 cycles

MAIN ROTOR BLADE DAMAGE. DURING CLIMB EXPERIENCED LOUD THUD PERFORMED PER-CAUTIONARY TO BASE LANDING FOUND HOLE THROUGH BLUE MAIN ROTOR BLADE AND LEADING EDGE DAMAGE. NO FLIGHT CONTROL DEFICIENCIES NOTED. HOLE AND DAMAGE IS LOCATED AT APROX 165 MM FROM ROOT OF BLADE.

Source: SDR 2021FA0000048
OTHER · 2018-05-18 Matched by certificate designator
ATA 6330

Part: FITTING — CRACKED (TRANSMISSION) · airframe 1,781 hrs · 5,955 cycles

FOUND A CRACKED LT TRANSMISSION FITTING, FOUND DURING AN EDDY CURRENT INSPECTION IAW EO 49-5300-EO-2335.

Source: SDR QMLA2018052988065
OTHER · 2017-04-17 Matched by certificate designator
ATA 5320

Part: RETAINER — CORRODED (FUSELAGE) · airframe 1,323 hrs · 4,406 cycles

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.

Source: SDR QMLA2017041717036