Registered owner
Uas Transervices Inc
Owner type
Corporation
Serial number
U-188
Year built
1982
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
March 19, 1982
Certificate issued
August 19, 2013
Expires
August 31, 2029
Mode S code
A47916

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 28

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

1971In forceSuperseded2026
ADs by the year they took effect: 30 ADs
19715
19722
19831
19851
19871
19891
19901
19923
19961
19972
19981
20011
20031
20042
20054
20061
20211
20231
See all 30 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N388AVMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech C-99 aircraft

FAA incident reports · 2

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 JIKA2024120401Brake · low pressureTHE #2 BRAKE PEDAL LOST ALL PRESSURE DURING TAXI FOR DEPARTURE. DURING THE PRE-FLIGHT BRAKE CHECK AND THE ENGINE PERFORMANCE CHECKS THE BRAKES HELD PRESSURE NORMALLY. MAINTENANCE INSPECTED THE CAUSE OF THE FAILURE AND FOUND A LOOSE FITTING AND LOSS OF HYDRAULIDec 2, 2024 · N388AV · Beech C99 · Landing Gear Brake SystemSDR JIKA2023120512501Actuator · did not stowAFTER TAKEOFF, THE LANDING GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW PERFORMED AN AIR TURNBACK AND LANDED WITHOUT INCIDENT. DFW MAINTENANCE PERFORMED THE LANDING GEAR SHUTTLE VALVE TEST AND FOUND THAT #1 AND #2 SHUTTLE VALVES FAILED THE LEAK Nov 25, 2023 · N388AV · Beech C99 · Landing Gear Retraction/Extension SystemSDR JIKA12030901Unknown · malfunctionedACCORDING TO THE PILOT INCIDENT REPORT: LOCATION IS APPROX 10 MILES WEST OF L77. COMPLETING THE FRIDAY CHECKS, WANTED TO DO THE WEEKLY FIRE SYSTEM TEST IN FLIGHT. PULLED BOTH T-HANDLES AND WITH THAT CLOSED BOTH ENGINES DOWN. AFTER PUSHING THE HANDLES BACK Mar 9, 2012 · N388AV · Beech C99 · Engine (Turbine/Turboprop)SDR 98ZZZM635Actuator · leakingPILOT REPORTED LANDING GEAR CIRCUIT BREAKER POPPED AND GEAR WOULD NOT FULLY EXTEND. PILOT EXTENDED GEAR USING HAND PUMP, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT RETRACT ACTUATOR LEAKING. PART REMOVED.May 21, 1998 · N388AV · Beech C99 · Landing Gear ActuatorSDR 98ZZZX1617Sensor · malfunctionedAPPROXIMATELY 10 MINUTES AFTER TAKEOFF, THE RT ENGINE FIRE WARNING LIGHT CAME ON. THeRE WAS NO OTHER INDICATION OF FIRE AND THE ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO L15 WITH NO PROBLEMS. THE LIGHTS WENT OUT AFTER AIRCRAFT WAS PARKED. INVESTIGATEDApr 11, 1998 · N388AV · Beech C99 · Fire Detection

STCs that may be installed · 139

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

See all 139 STCs