FAA incident reports · 5
FAA accident and incident reports matched to this aircraft by N6811 and the event date: after March 26, 1930, when the previous aircraft’s registration ended, through this one’s cancellation.
Incident 19900829049349IForced/Precautionary Landing · Austin, TXLower aft body overheat warning. Returned. Evacuated via slides. Duct supply v band clamp had failed.Incident 19800717061069IClimb · Dallas, TXService cart injured flight attendant's heel.Incident 19800711060349ITo Init Climb(1st Pwr Reduct) · Chicago, ILFlight returned when main gear door light remained on. Found exposed wire causing ground.Incident 19790510200359IDescent · Little Rock, ARInfant received possible injuries because it was left on floor during turbulence, despite captain's warnings.Incident 19780518033839IClimb · Dallas, TXOverheat warning light on #1 strut illuminated during climb. Loose clamp on pneumatic duct.
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR GAIA00689Switch · inoperativeDFW/FWA - FLT 1733 - DURING CLIMB AT FLAPS 2 DEGREES, THE NR 1 LE FLAP SHOWED AMBER LIGHT ON FRONT PANEL INDICATOR. THE CREW DECLARED AN EMERGENCY, RETURNED TO DFW. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED, REPLACED THE LE FLAP INDICATOR SWITCH. OPS CHESDR GAIA00505Accessory Unit · failedFLT 1736 - BNA-CLT - DURING DESCENT 20 MILES OUT OF CLT. THE WHEEL WELL WARNING LIGHT CAME ON. THERE WAS NO FIRE BELL. ACCOMPLISHED EMERGENCY CHECK LIST AND LANDED SAFELY. MAINTENANCE PERFORMED A DETAIL INSPECTION OF THE WHEEL WELL FIRE LOOP. NO CHAFING OSDR GAIA99163Anti-Ice Valve · looseDEN/MHR - FLT 2015 - FOUR MINUTES AFTER TAKEOFF DURING CLIMB-OUT PASSING THROUGH 10,000 FEET, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED WITH 42 PSI DUCT PRESSURE. RAN ABNORMAL CHECKLIST AND LIGHT REMAINED EXTINGUISHED AT CRUISE THRUST. THE AIRCRAFT COSDR GAIA99065Actuator · leakingAFTER TAKEOFF OF SCHEDULED FLIGHT NUMBER 302 FROM SEA TO DFW, THE CREW SELECTED THE GEAR UP. THE LEFT GEAR WOULD NOT RETRACT. THE CREW RECYCLED THE LANDING GEAR, AND THE LEFT MAIN GEAR REMAINED EXTENDED. THE CREW ELECTED TO RETURN TO SEA. THE AIRCRAFT LANDSDR GAIA99025Circuit Breaker · failedWHILE EN ROUTE TO YIP FROM IND, THE FLIGHT ENGINEER FOUND THE NR 1 ENGINE FIRE DETECTION CIRCUIT BREAKER HAD TRIPPED. ATTEMPTED ONE RESET, BUT THE CIRCUIT BREAKER WOULD NOT RESET. THERE WAS A BUNRING RUBBER SMELL NOTED IN THE COCKPIT. DECLARED AN EMERGENCY SDR GAIA9919Frame · misdrilledDURING SCHEDULED PHASE IN C-CHECK, ELONGATED HOLES ON THE RBL 45 UPPER CHORD AT FUSELAGE FRAME STATIONS 480 TO 680. HOLES WERE DRILLED AND REAMED TO .03125 OVERSIZE. THE HOLES WERE DEBURRED, AND FASTENERS WERE INSTALLED AS CALLED OUT IN AIA EDR B2-06354. RESDR GAIA9918Frame · misdrilledDURING SCHEDULED PHASE IN C-CHECK, A MISDRILLED HOLE ON FRAME STATION 500 BETWEEN S-10L AND S14L. HOLES WERE REAMED AND DEBURRED. NAS1097AD6-XX RIVETS WERE INSTALLED. REPAIR ACCOMPLISHED IAW AIA EDR B206359. NON ROUTINE 52142. (M)SDR GAIA9917Tip · unserviceableDURING SCHEDULED PHASE IN C-CHECK, A INCORRECT STATIC WICK BASE WAS FOUND INSTALLED ON THE LEFT WING TIP. DURING REMOVAL FOUR .1875 INCH FASTENERS HOLES WERE LEFT. THE DAMAGED AREA WAS REMOVED A FILLER WAS FABRICATED USING SAME MATERIAL AS REMOVED. THE FILLSDR GAIA9916Web · crackedDURING SCHEDULED PHASE IN C-CHECK, THE WEB LOCATED AB BS 1110 TO 1130 AT RBL 60 WAS FOUND CRACKED. A REPLACEMENT PANEL WAS FABRICATED FROM .050 INCH THICK 7075-0 HT TO T6 AFTER IT WAS FORMED. STIFFENERS ANGLES FORMED FROM 7075-T6 BY .050 IN LIEU OF WELDED BESDR GAIA99022Bulkhead · corrodedDURING SCHEDULED PHASE IN C-CHECK, CORROSION WAS FOUND ALONG THE HORIZONTAL FLANGE, AT FS 740 BULKHEAD. THE DAMAGED AREA TO THE BULKHEAD WAS REPAIRED AS EPR B727 SRM 53-10-1 FIG 1 DETAIL 1, AND AIA EDR B2-06357. REPAIR DOCUMENTED ON AIA NON-ROUTINE 1710. (MSDR GAIA99021Floorbeam · corrodedDURING SCHEDULED PHASE IN C-CHECK, CORROSION ON FLOORBEAM UPPER CHORD AT RBL 15 TO 44, FS 1130. AFTER CORROSION REMOVAL THE UPPER CHORD WAS FOUND BEYOND LIMITS. THE DAMAGED AREA TO THE FLOORBEAM WAS REPAIRED AS PE AIA EDR B2-06351, AIA/E/2922 REV ORIG. REPASDR GAIA99020Skin · crackedDURING SCHEDULED PHASE IN C-CHECK, A SMALL CRACK WAS FOUND IN THE SKIN LOCATED AT BS 352 STRINGER 27 RT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED USING AIA EDR B2-06360 OVER THE DAMAGED AREA. REPAIR DOCUMENTED ON AIA NON-ROUTINE 51817. (M)SDR CKSA96194Stringer · corrodedDURING B-CHECK INSPECTION, FOUND STRINGER 29R CORRODED STA 680. REPAIRED AS PER 727 BOEING SRM 53-10-3 FIGURE NR 1. AD 90-25-03, CORROSION CARD NR C53-113-01 PART 1 OF 2, NON-ROUTINE WORK CARD NR 61464.SDR AALA951935Eel Wire · brokenMIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT TRACK LIGHTING IN FIRST CLASS ON THE RIGHT SIDE INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)
Other aircraft with N6811 · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N6811 is registered now to the first aircraft listed.