Registered owner
N499cz LLC
Owner type
LLC
Serial number
U-81
Year built
1969
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
January 13, 1992
Certificate issued
July 26, 2019
Expires
July 31, 2029
Mode S code
A631D1

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.

On this page

Airworthiness directives that may apply · 70

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

1968In forceSuperseded2026
ADs by the year they took effect: 73 ADs
19681
19691
19701
19715
19723
19741
19752
19761
19771
19784
19791
19803
19823
19831
19851
19861
19871
19881
19891
19903
19924
19941
19952
19963
19973
19981
20012
20021
20031
20042
20054
20062
20112
20121
20142
20151
20161
20211
20221
20231
20241
See all 74 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

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 · 10

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

SDR 2024F00262Fire Detector · false activationRIGHT 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 POct 23, 2024 · N499CZ · Beech 99A · Fire DetectionSDR KCQA202306070004Hose · leakingON 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 NEJun 4, 2023 · N499CZ · Beech 99A · Hydraulic System, MainSDR KCQA202306050504Hose · leakingPILOT 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 ANDJun 4, 2023 · N499CZ · Beech 99A · Master Cylinder/Brake ValveSDR KCQA20220620Attach Fitting · crackedLH 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.Jun 20, 2022 · N499CZ · Beech 99 · Main Landing GearSDR KCQA20211207Brake Assy · leakingWHILE 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 THNov 29, 2021 · N499CZ · Beech 99 · Landing Gear SystemSDR 2021F00000Drag Fitting · failedDURING LANDING RT MAIN LANDING GEAR DRAG LEG FITTING FAILED.Oct 14, 2020 · N499CZ · Beech 99A · Main Landing Gear Attach SectionSDR KCQA2018090400001Fire Detector · false activationIN 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.Sep 4, 2018 · N499CZ · Beech 99A · Fire DetectionSDR 99ZZZX1916Fire Detector · contaminatedFOUND 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.Apr 12, 1999 · N499CZ · Beech 99A · Fire DetectionSDR 98ZZZX534Rod End · defectiveENGINE 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.Jan 13, 1998 · N499CZ · Beech 99A · Fuel Controlling SystemSDR 98ZZZX2711Rod End · bindingENGIEN 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.Jan 13, 1998 · N499CZ · Beech 99A · Fuel Controlling System

STCs that may be installed · 204

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

See all 204 STCs