NTSB investigations · 1
Matched to this aircraft by N2714B and the event date: after February 21, 1974, when the previous aircraft’s registration ended, through this one’s cancellation.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N2714B and the event date: after February 21, 1974, when the previous aircraft’s registration ended, through this one’s cancellation.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HYIA20170829001Resistor · burnedIN CRUISE FLIGHT, CREW RECOGNIZED SMOKE FROM DC BUSS PANEL. THE CREW REPORTED NO CIRCUIT BREAKERS OR SWITCH BREAKERS WERE TRIPPED. DURING ISOLATION OF ELECTRICAL SYSTEMS, NO MORE SMOKE WAS NOTED. THE CREW ELECTED TO DIVERT TO KSLK AS A PRECAUTION AND LANDEDSDR HYIA201608003024Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA201608003023Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.SDR HYIA20150921001Engine · making metalJUST AFTER LIFTOFF, STILL AT TAKEOFF POWER, RT MANIFOLD PRESS WAS 36" RPM NORMAL & ROUGH RUNNING. INSPECTED THE ENG & FOUND EVIDENCE OF METAL CONTAMINATION. THE RT ENG WAS REMOVED & REPLACED, SENT FOR TEARDOWN ANALYSIS.SDR HYIA20140415073Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWSDR HYIA20140415050Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURESDR HYIA20140415026Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA2714BNLGDownlock Switch · out of adjustON APPROACH, SELECTED GEAR DOWN, NO NOSE GEAR DOWN LOCK INDICATION. BROKE OFF APPROACH, C/W GEAR WILL NOT EXTEND CHECKLIST. DECLARED EMERGENCY, CONTINUED APPROACH, LANDED WITHOUT INCIDENT. MX FOUND NOSE GEAR DOWNLOCK SWITCH OUT OF ADJUSTMENT, ADJUSTED SAME. SDR 1352714120307Adapter · failedPILOT DISCREPANCY OF RIGHT ENGINE DOES NOT SPIN ON START. AIRCRAFT WAS AT GATE IN SJU. MAINTENANCE FOUND A STARTER ADAPTER GEAR TOOTH AND ENGINE START GEAR TOOTH FAILURE. MAINTENANCE REMOVED AND REPLACED THE ENGINE.SDR HYIA070902001Master Switch · inoperativeAVIONIC MASTER SWITCH INOPERATIVE DATE CODE 0633. REMOVED AND REPLACED INOPERATIVE SWITCH WITH NEW SWITCH DATE CODED 0633.SDR 13505272714BCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH MFG DATE CODE 0527.SDR 96ZZZX5239Turbocharger · seal failedDURING PRE-OILING OF NEWLY INSTALLED TCM REBUILT ENGINE, OIL LEAKED OUT OF EXHAUST TAILPIPE. FOUND OIL POURING FROM TURBINE SHAFT LIKE SEAL WAS NOT INSTALLED.SDR 95ZZZX2901Trunnion · crackedPILOT REPORTED RT STRUT WAS RIDING LOW. MAINTENANCE DISCOVERED A CRACK APPROXIMATELY 4 INCHES LONG ALONG SIDE THE CAST MARK OR SEAM IN THE UPPER GEAR TRUNNION. DURING DISASSEMBLY, NOTED THE STRUT BARREL WAS ALSO CRACKED. PILOT REPORTED NO UNUSUAL LANDINGS A
Other aircraft with N2714B · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N2714B now.