Registered owner
Bald 3 LLC
Owner type
LLC
Serial number
750-0051
Year built
1998
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
August 14, 1998
Certificate issued
May 20, 2021
Expires
May 31, 2028
Mode S code
A04F25

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Allison AE3007C model are included below.

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Airworthiness directives that may apply · 24

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

1998In forceSuperseded2026
ADs by the year they took effect: 30 ADs
19983
19991
20004
20013
20022
20031
20051
20063
20071
20081
20091
20101
20111
20121
20131
20151
20171
20181
20231
20261
See all 30 ADs

Information bulletins that may apply · 6

Advisory, not mandatory.

Historical bulletins · 3

NTSB investigations · 1

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

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 5

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

SDR 5JHA2025030700160Overheat Sensor · false indicationTHE LH AND RH HYDRAULIC TEMP SENSORS GIVE FALSE INDICATIONS. WE HAVE REPLACED 5 SENSORS IN THE LAST FEW YEARS AND THE LATEST ONE THAT IS BRAND NEW FAILED AFTER TWO WEEKS IN SERVICE.Mar 7, 2025 · N119RM · Cessna 750 · Overheat DetectionSDR 2022F00334None · noneON TAKEOFF THE CREW SAW THE MAIN CABIN DOOR CAS MESSAGE ILLUMINATE AS WELL AS THE CABIN VENT DOOR CAS MESSAGE. BOTH CAME ON AT 11,000 FEET WHILE DEPARTING ASPEN. THEY RETURNED TO ASPEN AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE INTERIOR CABIN DOOR HAug 20, 2022 · N119RM · Cessna 120 · Fuselage Structure (General)SDR 9JLA2018080919551Position Sensor · defectiveDURING FLIGHT CONTROL CHECKS, PRIOR TO FLIGHT, IT WAS DISCOVERED THAT THE UPPER RUDDER CHANNEL B FAILED THE PRE-FLIGHT CHECKS. THE UPPER RUDDER POSITION WOULD STAY FULLY DEFLECTED UNTIL RESET. THE MAINTENANCE FOUND THE CHANNEL B RUDDER POSITION SENSOR DEFECTIJul 15, 2018 · N119RM · Cessna 750 · Rudder Control SystemSDR 9JLA2018042711498Hydraulic Line · chafedDURING POST FLIGHT INSPECTIONS, THE RT THRUST REVERSER PRESSURE HYDRAULIC LINE WAS FOUND TO BE CHAFED BY NEARBY B-NUT CAUSING A HYDRAULIC LEAK. . THE LOCATION OF THE CHAFED HYDRAULIC LINE WAS WITHIN THE AFT MAINTENANCE BAY ON THE RT SIDE OF THE COMPARTMENT JUSApr 23, 2018 · N119RM · Cessna 750 · Hydraulic System, MainSDR 9JLA2018021911496Seal · leakingWHILE WAITING FOR PASSENGERS WITH THE APU RUNNING AND THE AIR CONDITIONING OPERATING, THE CREW REPORTED THAT VISIBLE SMOKE WAS SEEN IN THE COCKPIT WITH THE ODORS OF SOMETHING GETTING HOT, WERE UNABLE TO CONTROL THE COCKPIT TEMP. THE CREW SHUTOFF THE COCKPIT AIFeb 15, 2018 · N119RM · Cessna 750 · Cabin Cooling System

STCs that may be installed · 73

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

See all 73 STCs