FAA incident reports · 5
FAA accident and incident reports matched to this aircraft by N8909E and the event date: up to this one’s cancellation.
Incident 19991219042079IIdling Engines · Detroit, MI(-23) At 2123 local on 12/19/99, nwa flight 1408, a DC-9 N8909E, located in the alley way between concourse c and d on spot "4" was struck from behind by an unmanned fuel truck. With both engines running, the crew was completing their checklist prior to taxi…Incident 19910514026869ITo Aborted (Fixed Wing) · Covington - Cin, OHAborted takeoff due to fuel imbalance. Continued after fuel balance obtained.Incident 19820920065479ITo Init Climb(1st Pwr Reduct) · Milwaukee, WIRight engine experienced partial loss of power on takeoff. Shut down engine, returned. Fuel control pump replaced.Incident 19820304006979IInitial Approach-IFR · Memphis, TNArrived with one engine shut down. Replaced pressure ratio control valve and pressure and dump valve.Incident 19790122003299INormal Cruise · Indianapolis, INFlight had cabin pressurization loss at FL 330. No cause found.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 0301029151Seal · leakingCLIMBING THROUGH FL 270 THE "CABIN PRESSURE" WARNING ILLUMINATED. CABIN WAS AT 10,000 AND 4.2 PSI DIFFERENTIAL WITH OUTFLOW VALVE FULLY CLOSED. BOTH PACKS WERE INDICATING NORMAL PRESSURE. CREW INITIATED AN EMERGENCY DESCENT WITH POWER ON TO FL 170 UNTIL CABIN SDR 0202869151Controller · malfunctionedLOST PRESSURIZATION AT FL290, CABIN ALTITUDE WENT TO 12,000 FEET. CREW INITIATED A RAPID DESCENT TO 10,000 FEET. MASKS DID NOT DEPLOY. AUTO PRESSURE CONTROLLER RESTORED CABIN PRESSURE CONTROL BUT CONTINUED TO OPERATE ERRATICALLY IN AUTO. AIRCRAFT LANDED SASDR 0201309151Door · crackedDuring shop visit in ATL, the 2 aft cargo door assy webs were found cracked at aft end. Repaired per EA 99-189648.SDR 0103829151Duct · crackedDuring an aircraft overnight in MSP at gate G7, The electrical compartment exhaust duct outlet, common to the fuselage skin was found with a crack. The crack length is approximately 1.00" and is in the lower transition from the skin contour to the duct exhaustSDR 0000669151Skin · crackedVERTICAL STABILIZER SKIN CRACKED AT FASTENER HOLE LOWER LT SIDE OF STAB FS 900 AT ACCESS PANEL NR 5912188 ATTACH POINT LOG PAGE 1419162.SDR 9809519151Radar · failedWEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RADAR TRANSCEIVER AND ANTENNA, OPERATIONAL CHECK NORMAL.SDR 9800789151Anti-Ice Light · malfunctionedWING ANTI-ICE BLUE LIGHT DID NOT ILLUMINATE WITH AIRFOIL ANTI-ICE SELECTED. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY ON GROUND.SDR 9721929151Power Pack · inoperativeDURING LINE CHECK, FOUND TWO EMERGENCY LIGHTS INOPERATIVE AT CENTER AISLE SEAT ROWS 6 AND 8. MAINTENANCE REPLACED POWER PACK AT SEAT ROW 7, OPERATIONAL CHECK OK.SDR 9605209151Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE CUSP T-FITTING AFT OF THE RIGHT SIDE SERVICE DOOR CUTOUT FS 200. REPLACED FITTING PER SRM 51-30-1, 30-5.SDR 9601909151Epr Indicator · failedNR 2 ENGINE EPR INDICATION WAS LOW ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT.SDR 9601199151Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ABOVE TAILCONE SLIDE INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL.SDR 9511519150Epr Ind · malfunctionedNR 1 ENGINE EPR INDICATION WAS BELOW NORMAL ON TAKEOFF, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER, CHECKED THE PT7 SYSTEM FOR LEAKS AND THE INDICATOR FOR ACCURACY. SYSTEM OPERATION WAS NORMAL ON RUNUP. SDR 9511509150Epr Ind · malfunctionedNR 1 ENGINE EPR INDICATION WENT TO ZERO ON TAKEOFF ROLL, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR. THE SYSTEM CHECKED OK, AIRCRAFT RETURNED TO SERVICE.SDR 9511199151Shutoff Vlv · leakingDURING INITIAL CLIMB, EXPERIENCED RIGHT HYDRAULIC SYSTEM FLUID AND PRESSURE LOSS. FLIGHT RETURNED TO ORIGIN WITHOUT FURTHER INCIDENT. THERE WAS NO FURTHER LOSS WITH GEAR EXTENDED. FOUND RUDDER HYDRAULIC POWER SHUTOFF VALVE LEAKING FROM VALVE BODY. REPLACEDSDR 9505579151Adc · malfunctionedCAPTAIN'S ALTIMETER AND ALTITUDE ALERTER FLAGGED DURING CLIMBOUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S AIR DATA COMPUTER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.