NTSB investigations · 1
Matched to this aircraft by N285F and the event date: up to this one’s cancellation.
FAA incident reports · 4
FAA accident and incident reports matched to this aircraft by N285F and the event date: up to this one’s cancellation.
Incident 19950303009539IFcd/Prec Ldg From Cruise · Baltimore, MDNarrative: during climb out from bwi, aircraft did not pressurize. Door warning lights & indications were normal. Continued flight below 10,000 ft to ewr. At ewr, discovered right hand over wing exit missing.Incident 19941102040619IGround Taxi, Other Airplane · Austin, TXLanded at alternate due weather. New to aus and dark taxied off taxiway into soft ground. Was towed out by a tug.Incident 19860513025079INormal Cruise · Memphis, TNEngine shutdown en route due to low oil pressure. Safe landing. Aircraft ferried for repair.Incident 19801229083849IFinal Approach · Warner Robins, GACrew had to use force to move gear selector handle. Found stop cable interfering with handle.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR LR7A9804Compressor · wornNR 3 ENGINE AUTO FEATHERED ON T/O. PULLED EMERGENCY SHUTDOWN HANDLE AT 0038Z. REPLACED NR 3 SPEED SENSE VALVE IAW MM75-10-1, NO HELP. INSPECTED COMPRESSOR THROUGH 5TH AND 10TH STAGE BLEED VALVES AND FOUND COMPRESSOR WORN.SDR LR7A9731Engine · failedNR 1 ENGINE UNCONTROLLABLE LOSS IN OIL PRESSURE. SHUTDOWN ENGINE AT 0930Z. REPLACED NR 1 ENGINE PER ONE-120.SDR LR7A9727Valve · failedNR 3 ENGINE SHUTDOWN ON TAKEOFF AT 1633Z DUE TO RAPID FLUCTUATIONS IN TIT AND ENGINE RPM. REMOVED AND REPLACED NR 3 SPEED SENSE VALVE IAW N75-02, OPS NORMAL.SDR LR7A9728Oil Pump · failedNR 1 ENG SHUTDOWN ON ROLL-OUT IN PANC DUE TO ZERO ENG OIL PRESSURE AT 2358. REMOVED AND REPLACED POWER SECTION PRESSURE AND SCANVANGE PUMP PER 72-2-1, OPS OK.SDR LR7A9725Wire · chafedON SHUTDOWN NR 4 FIRE WARNING ILLUMINATED, PULLED EMERGENCY HANDLE AND DISCHARGED BOTTLE AT 1756Z. REPAIRED AND SECURED CHAFED WIRE AT ZONE 2 OF FIRE LOOP, TESTED PER LAC MM 26-1-0 CHECKS NORMALSDR LR7A25Wire · chafedON SHUTDOWN NR 4 FIRE WARNING ILLUMINATED. PULLED EMERGENCY HANDLE AND DISCHARGED BOTTLE AT 1756Z. REPAIRED AND SECURED CHAFED WIRE AT ZONE 2 OF FIRE LOOP, TESTED PER LAC MM 26-1-0 CHECKS NORMAL.SDR LR7A9707RSelector Valve · failedLANDING GEAR RELEASED IN FLIGHT, RECYCLED GEAR WOULD'NT STAY LOCKED UP. RETURNED TO PANC FOR UNEVENTFUL LANDING. REPLACED LANDING GEAR SELECTOR VALVE, LEAK CHECKED AND OPS CHECKED NORMAL PER MM. AIRCRAFT RELEASED FOR TEST FLIGHT ONLY. VENDER REPORTED ERRATSDR 97ZZZM873Selector Vlv · failedLANDING GEAR RELEASED INFLIGHT, RECYCLED GEAR WOULD NOT STAY LOCKED UP. RETURNED TO PANC FOR UNEVENTFUL LANDING. REPLACED LANDING GEAR SELECTOR VALVE, LEAK CHECKED AND OPS CHECKED NORMAL PER MM. AIRCRAFT RELEASED FOR TEST FLIGHT ONLY. (M)SDR ZIAA96009Skin · crackedYIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 620 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR 96ZZZX2335, NR 96ZZZX2336, NR 96ZZZX2337, AND NR 96ZZZX2338. (X)SDR 96ZZZX2338Skin · crackedYIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 620 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR ZIAA96009, 96ZZZX2335, NR 96ZZZX2336, AND NR 96ZZZX2337.SDR 96ZZZX2337Skin · crackedYIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 620 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR ZIAA96009, 96ZZZX2335, NR 96ZZZX2336, AND NR 96ZZZX2338.SDR 96ZZZX2336Skin · crackedYIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 620 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR ZIAA96009, 96ZZZX2335, NR 96ZZZX2337, AND NR 96ZZZX2338.SDR 96ZZZX2335Skin · crackedYIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 620 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR ZIAA96009, 96ZZZX2336, NR 96ZZZX2337, AND NR 96ZZZX2338.