N7203C

BEECH 1900C · 1985 · Fixed-wing multi-engine · 2 engines · 19 seats · Valid Registration

Registered owner: UAS TRANSERVICES INC, FL (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Ameriflight, LLC (JIKA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

7 reports on file, 1996-03-01 – 2026-04-07.

WARNING INDICATION · 2026-04-07 Matched by certificate designator
ATA 3230

Part: LANDING GEAR — INOPERATIVE (ZONE 700) · airframe 38,144 hrs · 58,521 cycles

THE LANDING GEAR DID NOT EXTEND NORMALLY WHEN SELECTED FOR LANDING BY THE FLIGHT CREW. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE LANDING GEAR CONTROL RELAY WAS STUCK AND WAS ABLE TO RESET THE RELAY. MULTIPLE RETRACTION AND EXTENSION CHECKS WERE PERFORMED ON AIRCRAFT JACKS, AND THE DISCREPANCY WAS NOT DUPLICATED. THE AIRCRAFT HAS BEEN RELEASED BACK TO SERVICE, AND NO FURTHER REPORTS OF LANDING GEAR FAILURE HAS BEEN REPORTED.

Source: SDR JIKA2026041301
OTHER · 2025-04-14 Matched by certificate designator
ATA 3297

Part: WIRE — BROKEN (ZONE 200) · airframe 37,764 hrs · 57,905 cycles

THE FLIGHT CREW PERFORMED AN EMERGENCY LANDING GEAR EXTENSION. WHEN ATTEMPTING TO EXTEND THE LANDING GEAR THE LANDING GEAR HANDLE WAS UN-RESPONSIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE TO THE LANDING GEAR HYDRAULIC POWER PACK PRESSURE SWITCH AND OPERATIONAL CHECKS ON JACKS WERE SUCCESSFUL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Source: SDR JIKA2025041501
FLUID LOSS; WARNING INDICATION · 2023-01-10 Matched by certificate designator
ATA 7261

Part: SEAL — LEAKING (SCAV PUMP) · airframe 36,670 hrs · 56,607 cycles

PILOT REPORTED THAT UPON APPROACH TO KRDM THE RT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED. PILOT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM TO A LEAK COMING FROM RH ENGINE OIL SCAVENGE PUMP. MAINTENANCE REMOVED AND REPLACED THE RH ENGINE OIL SCAVENGE PUMP SEAL PN 3022375. ALL ENGINE OPERATIONS AND LEAK CHECKS WERE GOOD..

Source: SDR JIKA20230116001
SMOKE/FUMES/ODORS/SPARKS · 2021-12-18 Matched by certificate designator
ATA 2121

Part: BLOWER — FAILED (VENTING) · airframe 36,212 hrs · 55,899 cycles

WHILE IN FLIGHT, THE FLIGHT CREW NOTED A BURNING SMELL. THE VENT WAS SHUT OFF AND THE SMELL DISSIPATED. BFI MAINTENANCE INSPECTED AND FOUND THAT VENT BLOWER WAS DEFECTIVE. DEFERRED, VENT BLOWER ON ORDER.

Source: SDR 2021FA0000421
NO WARNING INDICATION · 2021-07-07 Matched by certificate designator
ATA 3260

Part: BULB — INOPERATIVE (MLG INDICATOR) · airframe 36,054 hrs · 55,628 cycles

RIGHT LANDING GEAR DID NOT ILLUMINATE IN FLIGHT. MAINTENANCE FOUND UPON INSPECTION THE RIGHT MLG INDICATION BULB TO BE INOP. REMOVED AND REPLACED BULB.

Source: SDR JIKA20210701
WARNING INDICATION · 2020-09-28 Matched by certificate designator
ATA 7321

Part: FUEL CONTROL — BROKEN (ENGINE) · airframe 35,719 hrs · 55,127 cycles

WHILE IN ROUTE TO KPDX, THE FLIGHT CREW REPORTED LEFT ENGINE TORQUE AND N1 INDICATIONS DROPPED. CHECKLIST ITEMS WERE FOLLOWED AND THE LEFT ENGINE WAS SHUT DOWN. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT DIVERTED TO KDLS AND LANDED WITHOUT INCIDENT. PDX MAINTENANCE TRAVELED TO KDLS. REMOVED AND REPLACED LT ENGINE FCU WITH SERVICEABLE UNIT, PER P&W PT6A-65 EMM 73-20-00 PARA 5A&B. OPERATIONAL AND LEAK CHECK NORMAL.

Source: SDR JIKA2020092801
SMOKE/FUMES/ODORS/SPARKS · 1996-03-01 Matched by certificate designator
ATA 2210

Part: COMPUTER — FAILED (YAW DAMP SYSTEM)

FLT NR 4356 - ALB-BOS - AFTER TAKEOFF, FUMES AND SMOKE APPEARED IN THE CABIN AND COCKPIT. CREW DECLEARED AN EMERGENCY, DEPLOYED THE OXYGEN MASKS AND RETUREND TO ALB LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE YAW DAMP CIRCUIT BREAKERS HAD POPPED. INVESTIGATION FOUND THE YAW DAMP COMPUTER HAD SHORTED INTERNALLY. THE YAW DAMP SYSTEM WAS DEFERRED AND THE AIRCRAFT RETURNED TO SERVICE. (M)

Source: SDR PLG3196E1