N522ME
Registered owner: CENTER FOR EMERGENCY MEDICINE OF WESTERN PA, PA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CENTER FOR EMERGENCY MEDICINE OF WESTERN PA INC (E3MA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
Maintenance disclosures
DURING COMPLIANCE WITH THE AMOC FOR AD 2013-12-06 IT WAS NOTICED THAT THE BOLTS THAT SECURE THE AIR CONDITIONER PULLEY TO THE ROTOR BRAKE DISK WERE NOT THE CORRECT LENGTH. AFTER FURTHER INVESTIGATION IT WAS DETERMINED THAT THE BOLTS WERE THE CORRECT LENGTH & THE HOLES IN THE PULLEY WERE NOT THREADED THE ENTIRE DEPTH OF THE HOLE. THIS PREVENTED THE BOLTS, WITH THE NEW SAFETY SHEETS INSTALLED, FROM PROPERLY SECURING THE PULLEY TO THE DISK.
CRACKS FOUND EMANATING FROM LOWER 5 HI-LOK FASTENERS IN TITANIUM REINFORCEMENT LOCATED AT FRONT OF NR 1 ENGINE DECK. THIS RE-ENFORCEMENT IS ATTACHED TO THE AFT SIDE OF FRAME 5 IN THE AIRCRAFT FUSELAGE. MANUFACTURER HAS BEEN NOTIFIED AND REPAIR ORDER REQUESTED.
LEAKING FLUID FROM WEEP HOLE.
LEAKING FLUID FROM HOUSING BEYOND SERVICEABLE LIMITS.
SPHERICAL BEARING ON INPUT SHAFT, WORN.
PANEL HAD STRESS CRACK IAW SITE MECHANIC, UPON REMOVAL, PANEL SHATTERED AND MECHANIC SCRAPPED ON SITE. REPLACED WITH SERVICEABLE PANEL FROM AEC, 04/16/2004
LEAKING FLUID, AND RETRACTED ALL THE WAY INTO UNIT. REPLACED WITH SERVICABLE UNIT. 03/26/2004
LEAKING AND RETRACTED TOO FAR. REPLACED WITH SERVICABLE UNIT. 03/26/2004
UNIT LEAKING FLUID AND PLUNGER RETRACTED. ABOVE P.O. IS MEANT FOR A/C S/N 0132, BUT ONE WAS CANNED OFF OF A/C S/N 0144. PERMISSION GIVEN TO RETURN THIS UNIT. REPLACED WITH SERVICABLE UNIT. 03/24/2004
THIS UNIT'S MOTOR RUNS CONSTANTLY. REPLACED WITH SERVICABLE UNIT. 03/29/2004
EXCESSIVE LATERAL PLAY IN ACTUATOR ROD END. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/26/2004
LIGHT WAS INSTALLED ON 01/19/2004 AND FAILED 03/15/2004 FOR A TOTAL OF 80.4 FLIGHT HOURS. INTERNAL LIGHTING IS INOPERATIVE. CLOCK WAS PURCHASED OUTRIGHT ON OUR PO 2-022166-05.
MAIN ROTOR BLADE WILL NOT BALANCE. REPLACED WITH CANNED UNIT FROM A/C.
MAIN ROTOR BLADE WILL NOT BALANCE. INSTALLED CANNED UNITS OFF OF A/C.
BARO SET KNOB INOPERATIVE. REPLACED WITH SERVICEABLE UNIT. 11/11/03
BUS TIE OPEN. REPLACED WITH SERVICEABLE UNIT.
PART CRACKED AT 90 DEGREES BEND RADIUS FROM APPROX 5 O`CLOCK POS. TO THE 10 O`CLOCK POS. BEFORE IT CRACKED TO THE OUTER SURFACE WHERE IT WAS NOTICED DURING A DAILY INSPECTION. PROBABLE CAUSE MAY HAVE BEEN AN EARLIER GROUND BUMPING INCIDENT THAT CAUSED OTHER DAMAGE TO THE AIRCRAFT. RECOMMENDATIONS TO PREVENT RECURRANCE WOULD BE TO CHOSEY INSPECTION. THIS AREA AFTER ANY TAIL BUMPING INCIDENT.
FENESTRON ACTUATOR LEAKING. BOLT SPINNING IN ARM. BEARINGS WORN. REPLACED WITH SERVICEABLE UNIT.
FUEL SENSOR GIVING INTERMITTENT READINGS. ONLY HAVE ONE CORE SO FAR. REPLACED WITH SERVICEABLE UNIT.
SIGNAL COND UNIT PRODUCING IRREGULAR READINGS. REPLACED WITH SERVICEABLE UNIT.
WEATHER RADAR INOPERATIVE. REPLACED WITH SERVICEABLE UNIT.
BRAKE DISC WARPED. REPLACED WITH SERVICEABLE UNIT.
ATTITUDE INDICATOR FAILED FAR 91-411 CHECK. ALTITUDE OUT OF LIMITS. REPLACED WITH SERVICEABLE UNIT.
MAST MOMENT INOPERATIVE. REPLACED WITH SERVICEABLE UNIT.