FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N54350 and the event date: after August 2, 1951, 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 TWAA0010201Connector · dirtyTHE FWD CABIN LT AND RT SLIDE LIGHTS WERE INOPERATIVE. CLEANED CONNECTORS AT THE BATTERY PACK. CHECK-C 9-7-99 MCI. ---CLOSED--SDR TWAA0007102Generator · failedIN DESCENT WITH NUMBER 3 ENGINE GENERATOR PLACARD INOPERATIVE PER MEL, EXPERIENCED AC POWER LOSS WHEN NUMBER 1 AND 2 GENERATORS HAD UNDEREXCITATION AND UNDERVOLTAGE. HAPPENED AT THE SAME TIME THAT NUMBER 2 ''B'' HYD PUMP WAS TURNED ON. FIELD RESET ON NUMBER SDR TWAA0002601Light · inoperativeA SECTION OF EGRESS FLOOR LIGHTING WAS INOPERATIVE AT CABIN ROW 12. REPLACED THE STRIP. CHECK-C 1-7-00 MCI.SDR TWAA0000809Frame · crackedDURING CHECK-C MAINT, FOUND CRACK ON UPPER CORD OF VENTRAL STAIRWELL, AT STA 1273 RT SIDE. INSTALLED REPAIR ANGLE PER SSRM 53-80-211.SDR TWAA0000808Flange · corrodedDURING CHECK-C MAINT, FOUND RT AFT OVERWING EMERGENCY EXIT, PRESSURE SEAL FLANGE BOTTOM SIDE WITH CORROSION FROM 6 INCHES UP ON EACH SIDE TO BOTTOM. REMOVED CORROSION BY SANDING PER SRM 51-10-6, PAGE 147. ALODINED AND PRIMED BARE AREA PER SRM 51-10-2 PAGE 1.SDR TWAA0000807Retainer · corrodedDURING CHECK-C MAINT, FOUND THE FWD RT EMERGENCY EXIT, FWD RT EMERGENCY EXIT BOTTOM SEAL RETAINER HAD CORROSION FROM FWD BOTTOM STOP TO AFT BOTTOM STOP. REMOVED CORROSION BY SANDING PER SRM 51-16-6, PAGE 147.. ALODINED AND PRIMED PER SRM 51-16-2, PAGE 1.SDR TWAA0000412Rib · crackedDURING CHECK-C MAINT, FOUND LT WING NUMBER 3 SPOILER RIB ATTACHED TO OTBD CASTING WAS CRACKED. REPLACED PART PER SRM 57-10-1 AND 51-30-2 FASTENER INSTALLATION. -SDR TWAA9914501Power Supply · inopTHE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED POWER SUPPLY. CHECK-C 1-29-99 MCI.SDR TWAA9913801Line · rupturedDURING FLIGHT THE 'B' HYDRAULIC SYSTEM FLUID WAS LOST RESULTING IN LOSS OF THE SYSTEM HYDRAULIC PUMPS. USED PNEUMATIC BRAKES DURING LANDING. REPLACED TWO HYDRAULIC LINES, MFG AE1008787H290 AND AE3660130K0290. CHECK-C 1-29-99 MCI.SDR TWAA9723001Actuator · leakingSTL - DURING LANDING, AIRCRAFT LOST 'A' SYSTEM HYDRAULIC PRESSURE AND QUANTITY. REMOVED AND REPLACED LEAKING NR 6 FLAP ACTUATOR, MFG P/N 1U1110. OPERATIONAL CHECK NORMAL. (M)SDR 96ZZZM800Hyd Line · failedDURING TAKEOFF LEFT MAIN LANDING GEAR ACTUATOR TOP SIDE HYDRAULIC LINE FAILED. REMOVED AND REPLACED HYDRAULIC LINE, MFG P/N AE100880912030. PRESSURIZED SYSTEM, OPERATIONAL CHECK OK.SDR 95ZZZX878Skin · crackedJFK - DURING SPECIAL CHECK, FOUND A 4 INCH CRACK IN RT WING NR 5 LEADING EDGE SLAT, ON INBOARD LOWER SURFACE, RT SIDE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-50-3, FIGURE 1, PAGE 2A. AIRCRAFT TOTAL TIME: 37,178 HOURS; 24,066 CYCLES.SDR 95ZZZX1399Skin · crackedJFK - DURING SPECIAL CHECK, FOUND A 4 INCH CRACK IN RT WING NR 5 LEADING EDGE SLAT, ON INBOARD LOWER SURFACE, RT SIDE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-50-3, FIGURE 1, PAGE 2A. AIRCRAFT TOTAL TIME: 37,178 HOURS; 24,066 CYCLES.
Other aircraft with N54350 · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N54350 now.