N323AA
Registered owner: E D SANTOS & ASSOCIATES LLC TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
50 reports on file, 1995-03-13 – 2013-05-31.
Part: O-RING — DAMAGED (NR 4 SPOILER) · airframe 102,139 hrs · 19,432 cycles
CREW REPORTED CENTER HYD QTY LOSS FOLLOWED BY CENTER HYD SYS PRESSURE EICAS MESSAGES. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND NR 4 SPOILER ACTUATOR FILTER PLUG LEAKING. REPLACED O-RING. SYS GROUND CHECK NORMAL OPS.
Earlier reports · 1995–2012 · 49 reports
2012
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,296 hrs · 18,864 cycles
FOUND CORROSION AT HINGE ATTACH POINT FOR GROUND HYDRAULICS ON RIGHT KEEL BEAM, FORWARD AND AFT HINGE POINTS. REMOVED CORROSION AND REPAIRED PER EA B767-53-025389.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,296 hrs · 18,864 cycles
SHEAR TIE AT STATION 1540 BETWEEN STRINGERS 38 AND 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.
2011
Part: SKIN — PUNCTURED (FUSELAGE) · airframe 96,450 hrs · 18,288 cycles
SKIN PUNCTURE AT STATIONS 1395 TO 1439 AT STRINGERS 31 TO 36 LEFT. ACCOMPLISHED DOUBLER REPAIR PER EA B019246.
Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 96,405 hrs · 18,278 cycles
AFT CARGO, BEAR STRAP HAS A SPOT OF CORROSION AROUND FASTENER HOLE STATION 1405 JUST OUTBOARD OF STRINGER 33 LEFT. ACCOMPLISHED DOUBLER REPAIR PER EA B767-53-019246.
Part: SENSOR — INOPERATIVE (LE SLAT) · airframe 94,512 hrs · 17,896 cycles
JFK - CREW REPORTED FLAP DISAGREE INDICATION LIGHT DURING FLIGHT. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED INBOARD SLAT RVDT SENSORS ONE AND TWO. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: ROTARY ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 94,486 hrs · 17,891 cycles
JFK - CREW REPORTED TRAILING EDGE FLAP DISAGREE MESSAGE UPON EXTENSION OF FLAPS FOR LANDING. FLIGHT LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 8 FLAP ACTUATOR OVER TORQUE INDICATOR TRIPPED. REPLACED NUMBER 8 FLAP ROTARY ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: ROTARY ACTUATOR — FAULTY (TE FLAP) · airframe 94,120 hrs · 17,816 cycles
JFK - DURING FLAP MOVEMENT FROM ONE TO FIVE DEGREES FLAP WAS STUCK AT ONE DEGREE. FLAP ASSEMETRY FAULT AND EICAS MESSAGE APPEARED. FLIGHT LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND TWO ROTARY ACTUATOR PINS POPPED ON RIGHT WING. REPLACED NUMBER 4 AND 5 FLAP ROTARY ACTUATORS. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: FITTING — DAMAGED (TE FLAP) · airframe 94,091 hrs · 17,808 cycles
FOUND TWO LOOSE BUSHINGS ON CARRIER BEAM ON THE RIGHT OUTBOARD FLAP NUMBER 1 SUPPORT. FOUND OUT-OF-ROUND CONDITION MEASURED HOLE DIAMETERS DIFERED BY A MAX OF 0.002" REAMED THE SUBJECT HOLES ON-CENTER UP TO (1.612") TO CORRECT THE CONDITION. PERFORMED SURFACE HFEC AND NO CRACKS FOUND. ROTO-PEENED THE HOLES PER SRM USING A 0.10A INTENSITY AND COVERAGE OF 2.0. HONED THE LUGS AND INSTALLED OVERSIZED BUSHING PER BAC DRAWING 113T1347 AND MAJOR EA COMP-57-014977.
Part: SWIVEL FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 94,091 hrs · 17,808 cycles
LEFT MAIN LANDING GEAR SIDE STRUT SWIVEL FITTING CORRODED. REMOVED A MAX OF 0.150" CORROSION ON THE LUG FACE PER EA B767-57-014875.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,091 hrs · 17,808 cycles
RIGHT SIDE FUSELAGE FRAME AT STATION 977 BETWEEN WATERLINES 183 TO 187 OUTER CHORDS CORRODED. ACCOMPLISHED NESTED STEEL ANGLE REPAIR PER EA B767-53-014905.
2010
Part: LIGHT — BROKEN (CABIN) · airframe 92,218 hrs · 17,429 cycles
EMERGENCY EXIT SIGN IN BUSINESS CLASS GALLEY COVER HAS FALLEN OFF AND NEEDS TO BE RE-ATTACHED. EMERGENCY ESCAPE PATH LIGHT SYSTEM BUSINESS CLASS RIGHT SIDE LIGHT LENS BROKEN. RE-ATTACHED EMERGENCY EXIT SIGN AND REPLACED LIGHT ASSEMBLY AT BUSINESS CLASS GALLEY RIGHT SIDE. OPS CHECK NORMAL.
Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 91,027 hrs · 17,189 cycles
ORD - INFLIGHT JFK-LAX. CREW REPORTED HYDRAULIC QUANTITY LOSS IN LEFT SYSTEM. EMERGENCY DECLARED DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LINE LEAKING FROM LEFT HORIZONTAL STAB TRIM CONTROL MODULE. REPLACED FLEX LINE ON STAB TRIM. SYSTEM GROUND CHECKED NORMAL OPERATION.
2009
Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 89,338 hrs · 16,845 cycles
LEFT NUMBER ONE DOOR SLIDE HAD A BULGE IN IT PREVENTING THE DOOR BUSTLE FORM SEATING PROPERLY. REPLACED THE LEFT NUMBER ONE DOOR SLIDE.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 89,078 hrs · 16,793 cycles
JFK - LEFT NUMBER ONE DOOR OPENED BY FLIGHT CREW PRIOR TO DISARMING. DOOR HANDLE ONLY PARTIALLY OPENED. SLIDE FELL OUT OF HOUSING AND ON TO JETBRIDGE. REPLACED LEFT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (CABIN) · airframe 88,779 hrs · 16,734 cycles
BUSINESS CLASS GALLEY EMERGENCY LIGHT MISSING LENS. REPLACED ASSEMBLY FOR EMERGENCY LIGHT AT BUSINESS CLASS GALLEY.
Part: WARNING SWITCH — ACTIVATED (TE FLAP) · airframe 88,038 hrs · 16,582 cycles
JFK - TRAILING EDGE FLAP DISAGREE MESSAGE DISPLAYED AT FLAP 1 DURING APPROACH. CREW EXECUTED GO-AROUND. LANDED JFK WITHOUT INCIDENT. ACCOMPLISHED BITE OF FEEU PER FIM 27-51-00, NO FAULTS NOTED. INSPECTED ALL ROTARY ACTUATORS CHECK NORMAL. CYCLED FLAPS, ALL CHECKS OK. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: CIRCUIT BREAKER — POPPED (TE FLAP) · airframe 86,855 hrs · 16,344 cycles
LAX - INFLIGHT. CREW REPORTED FLAP DISAGREE INDICATION ON ARRIVAL. LANDED WITH FLAPS AT 20 WITHOUT INCIDENT. REPLACED CIRCUIT BREAKER C1038. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: LIGHT — INOPERATIVE (CABIN)
JFK - EMERGENCY LIGHT AT OVERWING ON LEFT SIDE FORWARD BULB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERWING ON LEFT SIDE FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
JFK - EMERGENCY LIGHT AT OVERWING ON RIGHT SIDE AFT BULB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERWING ON RIGHT SIDE AFT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: PSEU — INOPERATIVE (TE FLAPS)
JFK INFLIGHT T2/05NOV - DURING INITIAL APPROACH CREW RECEIVED LEADING EDGE SLAT ASYMMETRY. CAPTAIN EXECUTED A MISSED APPROACH AND LANDED ON SECOND APPROACH WITHOUT INCIDENT. AIRCRAFT TAXIED TO GATE. FOUND PROXIMITY SENSOR ELECTRONICS UNIT CARD FAULTED. REPLACED PROXIMITY SENSOR ELECTRONICS UNIT CARD. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: RELAY — INOPERATIVE (EVAC SLIDE)
JFK - LEFT OVERWING SLIDE GREEN SQUIB INOPERATIVE. REPLACED RELAY FOR LEFT OVERWING SLIDE GREEN SQUIB. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CIRCUIT CARD — INOPERATIVE (PROX SENSOR)
LAX INFLIGHT T003/15AUG - ON APPROACH WHEN SELECTING FLAPS 20 DEGREES THE MASTER CAUTION LIGHT AND LEADING EDGE SLAT ASYMMETRY EICAS MESSAGE ILLUMINATED. LANDED LAX WITHOUT INCIDENT. BITE CHECK OF PROXIMITY SENSOR ELECTRONIC UNIT FOUND FAULT OF CARDS 001 AND 007. REPLACED CARDS 001 AND 007. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: SKIN PANEL — DENTED (RT WING)
MCI - RIGHT HAND WING OUTBOARD LOWER SKIN PANEL DENTED BETWEEN WING STATION 852 AND 880 AND FROM STRINGER 6 TO WING REAR SPAR. AREA OF DISCREPANCY IS TWO INCHES BY 18 INCHES WITH A DEPTH OF .125 INCH. REPAIRED PER FMR 323573C74 PER MRB 7672858. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SKIN — DENTED (FUSELAGE)
MCI - RIGHT HAND WING LOWER SKIN PANEL DENTED BETWEEN WING STATION 852 AND 880 AND FROM STRINGER 6 TO WING REAR SPAR. AREA OF DISCREPANCY IS TWO INCHES BY 18 INCHES WITH A DEPTH OF .125 INCH. REPAIRED PER FMR 323573C73 PER MRB767 2858. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: COVER — INOPERATIVE (EMERGENCY LIGHT)
JFK - EMERGENCY LIGHT COVER AT NUMBER 5 JUMPSEAT MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT NUMBER 5 JUMPSEAT FOR MISSING EMERGENCY LIGHT COVER. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: SKIN — DAMAGED (LT PYLON)
AFW - LEFT HAND PYLON STRUT SKIN ON INBOARD AND OUTBOARD SIDE HAD GOUGE CAUSED BY THRUST REVERSER SEAL RETAINER BETWEEN STATION 244 TO 250 AND WATER LINE 195. DAMAGED AREA WAS 5 INCH BY 7 INCH AND 0.053 INCH DEEP. BLENDED DAMAGE AND PERFORMED HIGH FREQUENCY EDDY CURRENT OF REWORKED AREA. VERIFIED USING NDT METHODS. ENSURE THICKNESS WITHIN LIMITS. REMOVED SOURCE OF WEAR FROM THRUST REVERSER BY PERFORMING A RIG AND SHIM OF THE THRUST REVERSER.
Part: LIGHT — INOPERATIVE (CABIN)
LAX - LEFT HAND FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING DIRECTIONAL ARROW SIGN INOPERATIVE. REPAIRED BROKEN WIRE AT SIGN ASSEMBLY FOR LEFT HAND FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING DIRECTIONAL ARROW SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BULKHEAD — CUT (FUSELAGE)
MCI - RIGHT HAND BULKHEAD WEB OUTER EDGE CUT DURING CHORD ANGLE REMOVAL. ONE HALF INCH CUT AT STATION 1809.5. REPAIRED CUT WITH TRIM OUT AND FILLER PER MRB 767 2640.
2003
Part: SPRING — MISSING (LIGHT GUARD)
SPRING FELL OFF OF OVERHEAD EMERGENCY LIGHT SWITCH GUARD. REPLACED OVERHEAD PANEL FOR THE EMERGENCY LIGHT SWITCH GUARD. SYSTEM GROUND CHECKED NORMAL OPERATION.
2002
Part: OIL COOLER — LEAKING (NR 1 ENGINE)
LEFT GEN DRIVE LIGHT AND GEN DRIVE EICAS MESSAGE DISPLAYED AFTER LANDING LIGHT WENT OUT IN LESS THAN 1 MINUTE. DID NOT DISCONNECT. T/S AND FOUND IDG OIL COOLER LEAKING IN NR 1 ENG. REMOVED AND REPLACED IDG OIL COOLER AS PER MM. RECONNECTED IDG. OPS CHECKED AND LEAK CHECKED NR 1 IDG ALL CHECKED GOOD. INSPECTED FILTERS AND POPPETS. ALL NORMAL. OK FOR SERVICE.
Part: SWITCH — FAILED (LT ENGINE)
JFK - FLT 133 - EN ROUTE JFK-LAX - JUST AFTER TAKEOFF, LEFT ENGNE REVERSER UNLOCK LIGHT ILLUMINATED. NO ADVERSE YAW NOTED. RETURNED JFK AND LANDED WITHOUT INCIDENT. REPLACED MICRO SWITCH PACK TO LEFT ENGINE REVERSER PER MM. ALL OPERATIONAL CHECKS NORMAL. (M)
2001
Part: PIN — BROKEN (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 25B INOPERATIVE. REPLACED BROKEN PIN AT SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT INOPERATIVE AT SEAT 28B. RECONNECTED CONNECTOR FOR EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: OVEN — DIRTY (GALLEY)
GLA - FLT 53 - EN ROUTE GLA-ORD, DETECTED ELECTRICAL SMELL AT FIRST CLASS OVEN. TURNED OFF OVEN. LANDED ORD WITHOUT FURTHER INCIDENT. CLEANED FIRST CLASS OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: CONNECTOR — LOOSE (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 10AB INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT ROW 10 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: UNKNOWN — ODOR (COCKPIT)
LHR - FLT 104 - DURING DESCENT, SMELL ODOR, BURNING RUBBER IN COCKPIT, NO WARNING INDICATIONS IN COCKPIT SMELL DISSIPATED ON FINAL APPROACH. RIGHT AND LEFT PACK OPS CHECK DURING APU AND ENGINE OPERATION NO UNUSUAL OR STRANGE SMELLS NOTED. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: TIRE — FAILED (NR 8 WHEEL)
JFK - FLT 0003 - DURING TAKEOFF, LOST NR 8 MAIN WHEEL ON CLIMB-OUT. RETURNED AND LANDED JFK WITHOUT INCIDENT. (M)
Part: LIGHT — BROKEN (CABIN)
JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT NEAR RIGHT AFT LAV INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT NEAR RIGHT AFT LAV. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: LIGHT — INOPERATIVE (COCKPIT)
ORD - FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPLACED FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT, MAINTENANCE L2 DOORWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT L2 DOORWAY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: WIRE — LOOSE (CABIN)
SFO - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FLIGHT ATENDANT JUMP SEATS 3RC AND 3LC INOPERATIVE. SECURED WIRING TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1998
Part: LIGHT — INOPERATIVE (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: TRUNNION — CORRODED (LT MLG)
AFW - FOUND SMALL AREA OF CORROSION IN THE LT MLG SUPPORT BEAM AFT TRUNNION BEARING BORE. REMOVED PITTING AND GOUGING BY BLENDING THE AREA. (M)
Part: IDG — FAILED (RT ENGINE)
RT GEN DRIVE LIGHT FLICKERED FOR 25 MINUTES. DRIVE LIGHT THEN CAME ON STEADY ENOUGH TO GIVE ICAS R GEN DRIVE INDICATION STEADY. RT IDG SHUT DOWN PER OPERATION MANUAL PROCEDURE APU STARTED, AT 41,000 FT, CARRIED TO RT BUS. INSPECTED FOUND DEBRIS IDG FILL COUPLING SEAT. REMOVED DEBRIS SERVICED IDG. RAN UP ENG, LEAK CHECK GOOD OP CHECK GOOD. DELAY INCURRED DUE RT GEN DRIVE LIGHT ILLUMINATED. IDG WAS DISCONNECTED. (M)
1997
Part: CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 10B, 10H, AND 7H FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTORS AT PASSENGER SETS 10B, 10H, AND 7H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1996
Part: ACM — DEFECTIVE (AFT FUSELAGE)
RDU - FLT 174 - AFTER TAKEOFF RDU, FUMES SIMILAR TO ELECTRICAL OVERHEATING ODOR NOTED THROUGHOUT AIRCRAFT. ODOR BEGAN DISSIPATING ON CLIMB-OUT, BUT INCREASED DURING DESCENT TO RDU. AIRCRAFT LANDED RDU WITHOUT FURTHER INCIDENT. ACCOMPLISHED ENGINE RUN-UP AND NOTED FUMES COMING FROM RIGHT PACK. RIGHT PACK PLACARDED 'DO NOT OPERATE'. AIRCRAFT MAINTENANCE FERRY RDU/AFW LANDED WITHOUT INCIDENT. REPLACED ACM, BOTH HEAT EXCHANGERS, CATALYTIC CONVERTER AND REMOVED, CLEANED, AND REINSTALLED PNEUMATIC DUCTS IN RIGHT PACK BAY. ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: EEL CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 24H INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL WIRE — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT AFT CABIN CROSS-AISLE INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT AFT CABIN CROSS-AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)
Part: EEL WIRE — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, FLIGHT ATTENDANT SEAT CONTROL EMERGENCY LIGHT TRACK HAS BROKEN WIRE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)