Safety record in brief:1 NTSB accident (substantial damage, Oct 2020)2 ADs may apply10 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
A failure of the right main landing gear drag leg support fitting and angle bracket as a result of multiple areas of fatigue cracking.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA21LA021)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (99A)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; … |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (99A) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
RIGHT ENGINE T-HANDLE ILLUMINATED THEN WENT OUT FOLLOWED BY AGGRESSIVE ENGINE SURGING. EXECUTED ENGINE SHUTDOWN AND LANDED. FOUND NO EVIDENCE OF ANY FIRE ON THE RH ENGINE AND TESTED THE FIRE DETECTOR SYSTEM MORE THAN 5 DIFFERENT TIMES, COULD NOT DUPLICATE PROBLEM AND NO DEFECTS FOUND AT THIS TIME.…
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT RH HAND BRAKE INOPERATIVE. ON WO# 000101 DATED 06/05/2023 FOUND EMPTY BRAKE RESERVOIR. INSPECTED BRAKE PLUMBING AND FOUND LEAKING LOWER HOSE ON PILOT SIDE RH MASTER CYLINDER. REMOVED AND REPLACED WITH NEW HOSE AND BLED BRAKES IAW BE99 AMM 32-40-00 AND BE99 AAIP. OPS AND LEAKS CHECKS GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON TAXI THE PILOT FOUND THE RH HAND BRAKE INOPERATIVE. ON FRE/ACE WORK ORDER 000101 DATED 06/05/2023 THE AMT FOUND AN EMPTY BRAKE RESERVOIR. INSPECTED BRAKE PLUMBING AND FOUND LEAKING LOWER HOSE ON PILOT SIDE RH MASTER CYLINDER. REMOVED AND REPLACED WITH NEW HOSE PN MS28741-4-0132 SN NSN AND BLED…
From FAA Service Difficulty Reports; matched by N-number and serial number.LH MLG DRAG BRACE ATTACH FITTING PN 50-120201-1 CRACKED. REMOVED AND REPLACED COMPLETE LH DRAG BRACE SUPPORT ASSEMBLY PN 50-120202-601. WORK PERFORMED IAW SIRM 20-00-00 AND 20-50-00.
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE TAXING THE AIRCRAFT AFTER LANDING THE FLIGHT CREW NOTICED THERE WAS A LOSS OF BRAKING ON THE LH SIDE. FOUND LEAKING BRAKE FLUID OUT OF THE LH BRAKE LINE WHERE IT GOES TO THE CALIPER. TIGHTENED THE BRAKE LINE GOING INTO THE LH OUTBOARD CALIPER. BLED THE BRAKES AND LEAK CHECKED GOOD IN…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING LANDING RT MAIN LANDING GEAR DRAG LEG FITTING FAILED.
From FAA Service Difficulty Reports; matched by N-number and serial number.IN FLIGHT PILOT RECEIVE FIRE INDICATION ON NR 1 ENGINE. ENGINE SHUTDOWN IAW EMERGENCY PROCEDURES. DURING EXAMINATION OF ENGINE AND NACELLE NO EVIDENCE OF FIRE WAS PRESENT.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND FIREWALL CONNECTOR TO BE WET WITH WATER. PILOT REPORTED FLYING THROUGH SOME INTENSE SHOWERS EN ROUTE TO MILWAUKEE, WI FROM STEVENS POINT, WI. CONNECTOR WAS DRIED OUT, RE-ASSEMBLED, AND FUNCTION TESTED SATISFACTORY.
From FAA Service Difficulty Reports; matched by N-number and serial number.ENGIEN POWER WOULD NOT DECREASE DUE TO BINDING ROD END CONNECTOR CAM BOX TO FCU. TAT: 30,824 HOURS. ENG TSN: 4,295 HOURS. ENG TSO: 1,129 HOURS.
From FAA Service Difficulty Reports; matched by N-number and serial number.ENGINE POWER WOULD NOT DECREASE DUE TO TIGHT ROD END CONNECTOR FROM CAM BOX TO FCU DEFECTIVE. TAT: 30,824 HOURS. ENGINE TSN: 4,295 HOURS. ENGINE TSO: 1,129 HOURS.
From FAA Service Difficulty Reports; matched by N-number and serial number.