FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N705S and the event date: up to this one’s cancellation.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SPAA0000025Light · defectiveDURING SCHEDULED CHECK, THE COCKPIT EMERGENCY EXIT LIGHT WAS FOUND DIMLY ILLUMINATING. THE LIGHT ASSEMBLY WAS REPLACED. SUBSEQUENT SYSTEM CHECK WAS SATISFACTORY PER MM 33-51-01.SDR SPAA0000024Intermed Gearbox · leakingFLT 214 FROM IFP TO DTW: NR 2 ENGINE WAS SHUT DOWN IN FLIGHT FOR LOSS OF OIL QUANTITY AND PRESSURE. THE AIRCRAFT DIVERTED TO ABQ. INVESTIGATION REVEALED THAT THE LP5 PORT FITTING ON THE NR 2 ENGINE ACCESSORY GEARBOX WAS LOOSE DUE TO DAMAGED INTERNAL THREADS TSDR SPAA0000023Control Unit · malfunctionedON DESCENT INTO IFP, AIRCRAFT HAD UNCONTROLLED, MILD DUTCH ROLLING (LATER DESCRIBED AS FISH-TAILING) WITH AUTO-PILOT DISENGAGED. EXTENSIVE TROUBLESHOOTING REVEALED AN ANOMALY WITH THE MAIN RUDDER PCU YAW DAMPER SERVO CONTROL AS INDICATED THROUGH THE YAW DAMPERSDR SPAA0000022Stringer · corrodedDURING COMPLIANCE WITH CPCP TASK C53-202-04, AD 90-25-01, STRINGER 27L AT BS 947.6 WAS FOUND CORRODED. THE DAMAGE WAS REPAIRED IN ACCORDANCE WITH THE 737-200 SRM 53-10-3, FIGURE 1.SDR SPAA0000021Power Supply · inoperativeDURING SCHEDULED CHECK, THE LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE ASSOCIATED SYSTEM POWER SUPPLY WAS REPLACED PER MM 33-51-31. SUBSEQUENT SYSTEM TEST WAS SATISFACTORY.SDR SPAA0000018Actuator · crackedFLIGHT 214 IFP-SAT AFTER LANDING, DURING TAXI TO GATE, AIRCRAFT EXPERIENCED LOSS OF HYDRAULIC FLUID. IT WAS DETERMINED THAT THE NR 8 GROUND SPOILER ACTUATOR HOUSING HAD CRACKED AT THE PISTON END. THE ACTUATOR WAS REPLACED PER BOEING MM 27-62-101. HYDRAUL
Other aircraft with N705S · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N705S now.