N90PB

Cancelled 2022

Deregistered aircraft · 1976 Beech 200 · Pratt & Whitney PT6A series

Cancelled
October 1, 2022
Status when cancelled
Registration expired, pending cancellation
Serial number
BB125
Year built
1976
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
February 28, 1997
Certificate issued
June 27, 2019
Last registry action
June 27, 2019
Mode S code
AC6E1A
Owner when cancelled
Grant Aviation Inc
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N90PB and the event date: after July 16, 1990, when the previous aircraft’s registration ended, through this one’s cancellation.

Service difficulty reports · 8

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

SDR ENHA200420001Line · splitON TAKEOFF, PILOT UNABLE TO CONTROL CABIN PRESSURIZATION, RETURN TO AIRPORT OF DEPARTURE. FOUND SPLIT PRESSURIZATION LINE AT OUTFLOW VALVE, REPAIRED IAW BEECH 200 MM20-06-00 PG 201. AIRCRAFT TEST FLOWN. PRESSURIZATION SYSTEM FUNCTION NORMAL.Oct 19, 2004 · N90PB · Beech 200BEECH · Pressure Regulator/Outflow ValveSDR ENHA20032002BBulkhead · crackedRT NACELLE WAS WEARING AND CRACKING WITH RT AFT LOWER COWL. REPLACED BULKHEADDec 17, 2003 · N90PB · Beech 200BEECH · Nacelle/Pylon, Bulkhead/FirewallSDR ENHA20032002ABulkhead · crackedRT NACELLE WAS WEARING AND CRACKING AT CONTACT WITH RT AFT LOWER COWL. REPLACED BULKHEADDec 17, 2003 · N90PB · Beech 200BEECH · Nacelle/Pylon, Bulkhead/FirewallSDR ENHA200320002Bulkhead · crackedRT NACELLE WAS WEARING AND CRACKING AT CONTACT WITH RT AFT LOWER COWL. REPLACED BULKHEAD.Dec 12, 2003 · N90PB · Beech 200BEECH · Nacelle/Pylon, Bulkhead/FirewallSDR GSB2006DEC02Fuel Control · malfunctionedDURING CRUISE FLIGHT RIGHT ENGINE WOULD NOT DEVELOPE POWER, THE ENGINE WAS SHUTDOWN, THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE CAUSE OF THE ENGINE POWER LOSS WAS DETERMINED TO BE POSSIBLE (FUEL CONTROL UNIT) INTERNAL MALFUNCTION. THE FCU WAS REPLACEDDec 16, 2002 · N90PB · Beech 200BEECH · Fuel Control/Turbine EnginesSDR 2004F00258Fuel Control · malfunctionedDURING CRUISE FLIGHT, WOULD NOT DEVELOP POWER, THE ENGINE WAS SHUTDOWN AND SECURED PER PUBLISHED EMERGENCY PROCEDURE. THE AIRCRAFT LANDED AT ANCHORAGE INTERNATIONAL AIRPORT WITHOUT FURTHER INCIDENT. THE CAUSE OF THE POWER LOSS WAS DETERMINED TO BE POSSIBLE FDec 6, 2002 · N90PB · Beech 200BEECH · Fuel Controlling SystemSDR ENH2003F00000Fuel Control · inoperativeRT ENGINE NO DEVELOPING POWER (SHUT DOWN RIGHT ENGINE) REPLACED FCU AND HIGH PRESSURE FUEL PUMP W/OVERHAULED UNIT. WO NR 5352856 DATED MARCH 6, 02 (PUMP) 5284375 DATED 22 AUG O2 (FCU) GROUND RAN AND LEAK CHECKED GOOD. ADJUSTED IDLE SPEED TO 52 PERCENT.Dec 6, 2002 · N90PB · Beech 200BEECH · Fuel Control/Turbine EnginesSDR 98ZZZX1372Filter Housing · crackedPILOT NOTICED OIL PRESSURE DROPPED AFTER 1:30 HOURS INTO FILIGHT. FOUND OIL FILTER HOUSING CRACKED.Dec 14, 1997 · N90PB · Beech 200BEECH · Turbine Engine Oil System

Other aircraft with N90PB · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N90PB now.