N220CF

EUROCOPTER AS 350 B2 · 2001 · Rotorcraft · 1 engine · 6 seats · Valid Registration

Registered owner: MERCY AIR HELICOPTER INC, FL (owner ≠ operator)

Operators of this aircraft

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

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

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.

11 reports on file, 2001-12-12 – 2013-02-28.

FLT CONT AFFECTED · 2013-02-28 Matched by certificate designator
ATA 6710

Part: BEARING — ROUGH (CYCLIC) · airframe 5,267 hrs · 14,805 cycles

ON APPROACH TO LANDING PILOT REPORTED BINDING IN CYCLIC CONTROL IN THE AFT QUADRANT. MX INVESTIGATION REVEALED 2 BEARINGS IN CYCLIC CONTROL SYS WITH ROUGH SPOTS. REPLACED 1 EA PN ASNA0136-35E2 BEARING AND 1 EA ASNA0137-35E2 BEARING IN CYCLIC CONTROL TORQUE SHAFT.

Source: SDR QMLA2013022813031
OTHER · 2012-11-09 Matched by certificate designator
ATA 6220

Part: FREQ ADAPTER — DISTORTED (MAIN ROTOR) · airframe 1,220 hrs · 4,293 cycles

DURING 600HR AAIP AIRFRAME INSPECTION, FOUND 3 OF 3 FREQUENCY ADAPTERS ON MAIN ROTOR HEAD HAD SIGNIFICANT DISTORTION IN THE AREA WHERE THEY ATTACH TO MAIN ROTOR SLEEVES. DISTORTION WAS LIMITED TO THE T/E UPPER AND LOWER SIDES OF THE FREQUENCY ADAPTERS. MAIN ROTOR SLEEVES APPEARED TO BE TORQUED CORRECTLY UPON DISASSEMBLY. SN'S AFFECTED ARE 00085, 00094, AND 00097.

Source: SDR QMLA2012110912176
OTHER · 2012-04-02 Matched by certificate designator
ATA 3110

Part: TRAY — CRACKED (INSTRUMENT PANEL) · airframe 4,972 hrs · 13,124 cycles

DURING SCHEDULED INSPECTION, FOUND INSTRUMENT PANEL SUPPORT TRAY CRACKED IN THREE LOCATIONS.

Source: SDR QMLA2012040212050
OTHER · 2012-03-08 Matched by certificate designator
ATA 6710

Part: CYCLIC STICK — LOOSE (PILOT SEAT) · airframe 4,963 hrs · 13,064 cycles

PLAY IS FELT IN THE CYCLIC STICK - FORE AND AFT AXIS: DISCOVERED THE CYCLIC PITCH STICK STAND WAS SLIDING BACK AND FORTH ON THE BUSHING THAT WAS SUPPOSE TO BE PRESS FITTED TO THE CYCLIC PITCH STICK STAND.

Source: SDR QMLA2012030812053
OTHER · 2002-07-18 Unresolved
ATA 3457

Part: GPS — INOPERATIVE (COCKPIT)

POOR GPS COVERAGE ON SCREEN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR R7MR35536
NO TEST · 2002-04-03 Unresolved
ATA 3444

Part: INDICATOR — INOPERATIVE (RADAR ALTIMETER)

KNI416 - RADAR ALTIMETER INDICATOR INOPERATIVE. NO DH WARNINGS. REPLACED WITH LOANER UNIT CORRECTED PROBLEM.

Source: SDR R7M2002F00004
OTHER · 2002-03-29 Unresolved
ATA 3421

Part: INDICATOR — INOPERATIVE (COCKPIT)

HORIZON REFERENCE INDICATOR INOPERATIVE. DRIFTS 10 DEGREES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR R7M2002F00003
OTHER · 2002-03-13 Unresolved
ATA 3120

Part: CLOCK — INOPERATIVE (COCKPIT)

CLOCK INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR R7M2002F00007
NO TEST · 2002-03-06 Unresolved
ATA 2312

Part: TRANSCEIVER — MALFUNCTIONED (VHF SYSTEM)

UHF/VHF/LOW/HI BAND TRANSCEIVER UNIT INOPERATIVE. ON ANY FREQUENCY, THE TRANSMISSION FADES OUT AFTER 6.7 SECONDS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR R7M2002F00005
WARNING INDICATION · 2002-01-18 Unresolved
ATA 2913

Part: PUMP — FAILED (HYDRAULIC SYS)

HYDRAULIC PUMP UNIT INOPERATIVE. AIRCRAFT EXPERIENCED HYDRAULIC FAILURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR R7M2002F00006
OTHER · 2001-12-12 Unresolved
ATA 2422

Part: INVERTER — INOPERATIVE (ELECTRICAL)

STATIC INVERTER 1200VA DC TO 60HZ 1 PHASE, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR R7MR34347