N90PB
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| PROVINCETOWN B | Operator | on 1975-02-23 | Operator named in NTSB report |
Accident & incident history
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.
8 reports on file, 1997-12-14 – 2004-10-19.
Part: LINE — SPLIT (OUTFLOW VALVE) · airframe 13,795 hrs · 9,299 cycles
ON 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.
Part: BULKHEAD — CRACKED (RT NACELLE) · airframe 12,272 hrs · 8,399 cycles
RT NACELLE WAS WEARING AND CRACKING WITH RT AFT LOWER COWL. REPLACED BULKHEAD
Part: BULKHEAD — CRACKED (RT NACELLE) · airframe 12,272 hrs · 8,399 cycles
RT NACELLE WAS WEARING AND CRACKING AT CONTACT WITH RT AFT LOWER COWL. REPLACED BULKHEAD
Part: BULKHEAD — CRACKED (RT NACELLE) · airframe 12,272 hrs · 8,399 cycles
RT NACELLE WAS WEARING AND CRACKING AT CONTACT WITH RT AFT LOWER COWL. REPLACED BULKHEAD.
Part: FUEL CONTROL — MALFUNCTIONED (RT ENGINE)
DURING 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 REPLACED WITH (0) TSO UNIT. AS A PRECAUTIONARY MEASURE THE HI PRESS PUMP WAS REPLACED WITH (0) TSO COMPONENT. THE AIRCRAFT WAS GROUND RUN AND ENGINE TRIM ADJUSTED. NO FURTHER ENGINE OPERATIONAL PROBLEMS WERE INCOUNTERED, ENGINE GROUND RUN-UP CHECKS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. TTSO ON FAULTED FUEL CONTROL UNIT 3276.7.
Part: FUEL CONTROL — INOPERATIVE (ENGINE)
RT 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.
Part: FUEL CONTROL — MALFUNCTIONED (ENGINE)
DURING 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 FCU INTERNAL MALFUNCTION. THE FCU WAS REPLACED WITH '0' TSO UNIT. AS A FURTHER PRECAUTION THE HIGH PRESSURE PUMP WAS ALSO REPLACED WITH '0' TSO COMPONENT. THE AIRCRAFT WAS GROUND RUN AND ENGINE TRIM ADJUSTED. NO FURTHER ENGINE OPERATIONAL PROBLEMS WRE ENCOUNTERED, ENGINE RUN-UP CHECKS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: FILTER HOUSING — CRACKED (ASSORY GEARBOX)
PILOT NOTICED OIL PRESSURE DROPPED AFTER 1:30 HOURS INTO FILIGHT. FOUND OIL FILTER HOUSING CRACKED.