N842CA
Registered owner: RICH VALLEY LLC, MA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
16 reports on file, 1996-01-12 – 2001-04-09.
Part: SWITCH — OUT OF RIG (PAX DOOR)
BOTH CAM LATCH SWITCHES WERE NOT RIGGED CORRECTLY IN RELATION TO ANNUNICATOR OPERATION.
Part: HANDLE — OBSTRUCTED (PAX DOOR)
DOOR HANDLE HAD TO BE FORCED TO THE LOCK POSITION AS A RESULT OF RESTRICTION BETWEEN DOOR WELD AND BUSHING AT CENTER DOOR HANDLE.
Part: DOOR — OPEN (PAX DOOR)
DURING DECENT AT APPROX 3000 FT, THE FORWARD CABIN ENTRANCE DOOR OPENED. EMERGENCY WAS DECLARED AND THE AIRCRAFT MADE AN UNEVENTFUL LANDING. UPON INSPECTION OF DOOR AND ANNUNICATOR SYSTEM THE FOLLOWING DEFECTS WERE FOUND: 1/ BOTH DOOR HANDLE ANNUNICATOR SWITCHES WERE STUCK CLOSED AND HAD EVIDENCE OF CORROSION AT WIRE ATTACHMENT POINTS.
Part: NUT — LOOSE (ACTUATING ROD)
TWO (2) LOCKING NUTS ON ACTUATING RODS WERE LOOSE AND WERE BACKED OFF.
Part: SWITCH — CORRODED (PAX DOOR)
BOTH DOOR HANDLE ANNUNCATOR SWITCHES WERE STUCK CLOSED AND HAD EVIDENCE OF CORROSION AT WIRE ATTACHMENT POINT.
Part: WIRE ROPE — FRAYED (DOOR LATCH)
DOOR LATCHING CABLE WAS FOUND FRAYED DUE TO CONTACT WITH CABLE GUIDE. CABLE PULLEY HAD A FOREIGN MATERIAL IN GROOVE CAUSING CABLE TO BE FORCED INTO CABLE GUIDE.
Part: WIRE ROPE — OUT OF ADJ (DOOR LATCH)
DOOR LATCHING CABLES WERE BELOW RECOMMENDED TENSION.
Earlier reports · 1996–1999 · 9 reports
1999
Part: PUMP — LEAKING (RT ENGINE)
FUEL LEAK RIGHT ENGINE NACELLE. FOUND LOW PRESSURE FUEL PUMP LEAKING. REMOVED AND REPLACED UNIT, SYSTEM LEAK AND OPS CHECK SATISFACTORY.
Part: PUMP — LEAKING (RT ENGINE)
RIGHT ENGINE LOWER PRESSURE FUEL PUMP LEAKING. UNIT REPLACED. (M)
Part: PUMP — LEAKING (LT ENGINE)
LEFT ENGINE LOW PRESSURE FUEL PUMP LEAKING. UNIT REPLACED. (M)
Part: GEARBOX — STRIPPED (TE FLAPS)
FLAPS FAILED TO RETRACT, FLAP MOTOR GEAR BOX FAILURE. REPLACED FLAP MOTOR/GEAR BOX ASSEMBLY IAW RAYTHEON MM CHAPTER 27. (M)
1998
Part: ACM — FAILED (FUSELAGE)
AIRCRAFT WILL NOT COOL. REPLACED AIR CYCLE MACHINE AND HEAT EXCHANGER. (M)
Part: RELAY — SHORTED (COCKPIT)
ELECTRICAL ODOR FROM BEHIND INSTRUMENT PANEL DURING DESCENT FROM 4000 FEET. FOUND RELAY K119 WINDSHIELD HEAT SHORTED.
1997
Part: EADI — SHORTED (COCKPIT)
CAPTAIN'S EADI INOPERATIVE.
Part: SERVICE VALVE — SHORTED (LT MLG)
LANDING GEAR FAILED TO RETRACT. REPLACED SERVICE VALVE ON LT INBD MLG.
1996
Part: RIVETS — LOOSE (VERT STAB)
DURING SCHEDULED INSPECTIONS LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTHER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAFT RECOMMENDED PROCEDURE.