NTSB investigations · 2
Matched to this aircraft by N611FE and the event date: up to this one’s cancellation.
NTSB DCA97MA055Accident · Minor injuriesClass 1 · MajorFinal reportNewark, NJThe captain's overcontrol of the airplane during the landing and his failure to execute a go-around from a destabilized flare. Contributing to the accident was the captain's concern with touching down early to ensure adequate stopping distance.NTSB ANC95FA008Accident · No injuriesField investigationFinal reportAnchorage, AKThe flight crew's improper recovery from a bounced landing. Factors associated with the accident are the first officer's lack of familiarity with the airplane, his failure to stabilize the approach, and the captain's delayed remedial action.
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N611FE and the event date: up to this one’s cancellation.
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 08FDEA01662Seat Track · corrodedMAIN CARGO COMPT CENTER SEAT TRACK IS CORRODED ON THE BOTTOM AT FRAME 78. SPLICED IN A NEW SEAT TRACK SECTION IAW SRM 53-10-16; FIG 208.SDR 97FDEA00309Hydraulic Line · failed97-0096, ONE HOUR AND 30 MINUTES INTO FLIGHT, GOT HYDRAULIC 1 OFF ALERT. SYSTEM QUANTITY SHOWS 2.6 AFTER 3.5 HOURS OF FLIGHT. GOT LEVEL 2 HYDRAULIC 1 FAIL ALERT AND QUANTITY OF 1.0 GALLON. REMOVED PANEL 517CT OVER NR 1 ENGINE PYLON FOUND A .1875 HYDRAULIC PSDR 97FDEA00064Fire Detector · malfunctionedPASSING 11,000 GOT NR 1 ENG FIRE WARNING, AURAL AND BELL. DID NOT HAVE LIGHT IN HANDLE OR ANY OTHER INDICATION OF FIRE, EGT NORMAL. NO RISE IN EGT, SHUTDOWN AND RETURN TO MEMPHIS. REMOVED AND REPLACED LWR TURBINE DETECTOR ASSY.SDR 96FDEA01709Bulkhead Fitting · crackedTHE CENTER LANDING GEAR WHEEL WELL AREA HAS A CRACK AT THE RT BULKHEAD AND DRAG LINK VERTICAL SUPPORT FITTING AT STA 1453 AT X = - 31.50 CRACK MEASURES 13 AT LOWER END OF FITTING. ADDITIONALLY, VERTICAL STIFFENERS AND DIAGONAL STIFFENER HAVE DEEP GOUGES AT STSDR 96FDEA01702Tube · brokenDURING CRUISE, NR 3 HYDRAULIC SYSTEM FAILED (LOSS OF FLUID). PUMPS WERE TURNED OFF WITH 2.4 GALLONS REMAINING. REPLACED RT PUMP. CASE DRAIN REPLACED. P/N 224-9409-521. LEAK CHECKS GOOD, OK FOR SERVICE.SDR 96FDEA01541Engine · failedENGINE FAILED INSPECTION PER EA 1-7220-31511 INSP OF FIRST STAGE BOOSTER VANES.SDR 95FDEA01458Brake Assy · damageREFERENCE NR 7015 - DURING REPLACEMENT OF WORN TIRE AND WHEEL ASSY ON POS NR 3, FOUND ROTORS ON BRAKE ASSY DAMAGED. ROTORS NR 3, 4 AND 5 ARE DELAMINATED. STATORS NR 3 AND NR 5 ARE SHOWING SIGNS OF DELAMINATION, POSSIBLY DUE TO CHEMICAL CONTAMINATION, SOAPS ASDR 95FDEA00008Connector · contaminatedNRT - LANDING GEAR AURAL WARNING CAME ON AT 1500 FT ON CLIMB-OUT GEAR AND FLAP POSITIONS CONFIRMED UP NORMAL WARNING OFF WHEN GEAR WAS LOWERED FOR LANDING. FOUND CONNECTOR P1-1111 PIN S HAD BAD INSULATION BY MEGER TESTER FOR LEFT OUTBD FLAP POS XMTR T2-5 ALSOSDR 95FDEA00007Transmitter · malfunctionNRT - CONTINUOUS LANDING GEAR AURAL ALERT AT 1500 FT ON CLIMBOUT. GEAR UP INDICATIONS NORMAL, RECYCLED GEAR NO EFFECT, CONFIRMED GEAR/FLAPS UP ON CONFIG PAGE DURING GEAR RECYCLE AURAL WARNING STOPPED WHEN GEAR WAS DOWN AND LOCKED. FOUND WATER ACCUMLATION AT