N671AA
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.
44 reports on file, 1997-04-29 – 2012-06-21.
Part: LENS — DAMAGED (CABIN) · airframe 63,231 hrs · 22,166 cycles
ROW 9DEF EMERGENCY LIGHT LENS DAMAGED. REPLACED LENS FOR ROW 9DEF EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,231 hrs · 22,166 cycles
BULLNOSE EMERGENCY LIGHT AT 5EF INOPERATIVE. REPLACED LAMP FOR BULLNOSE EMERGENCY LIGHT AT 5EF. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,231 hrs · 22,166 cycles
ROW 36DEF EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR ROW 36DEF EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,231 hrs · 22,166 cycles
RIGHT NUMBER 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,828 hrs · 22,023 cycles
21D SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR 21D SEAT MOUNTED EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: BUSHING — CORRODED (RT MLG TRUNNION) · airframe 61,851 hrs · 21,670 cycles
RIGHT MAIN LANDING GEAR TRUNNION SUPPORT ASSEMBLY CORRODED. REPLACED BUSHING PER EA B757-57-021178.
Earlier reports · 1997–2011 · 38 reports
2011
Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,715 hrs · 21,239 cycles
DUE TO MULTIPLE AREAS OF CORROSION AND MULTIPLE REPAIRS, THE AFT DECK PLATE FROM STATIONS 1681 TO 1720 WILL REQUIRE REPLACEMENT. INSTALLED NEW DECK PLATE PER AARD 51-10-05-1.
Part: LENS — MISSING (CABIN) · airframe 59,047 hrs · 20,628 cycles
EMERGENCY LIGHT ON ROW 24 MISSING LENS. INSTALLED LENS ON ROW 24 EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LENS — MISSING (CABIN) · airframe 59,047 hrs · 20,628 cycles
EMERGENCY LIGHT ON ROW 27 MISSING LENS. INSTALLED LENS ON ROW 27 EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 58,971 hrs · 20,600 cycles
BELOW THE CABIN FLOOR IN THE AFT CARGO STATIONS 1580 TO 1600 AT BUTTLINE 0 THE INTERCOSTALS TOP L-ANGLE IS CRACKED BY THE FORWARD NUT PLATE. REMOVED AND INSTALLED NEW UPPER "L" ANGLE ON WEB STATIONS 1580 TO 1600 BUTTLINE 0 IAW SRM 52-10-02-0G.
2010
Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 58,376 hrs · 20,383 cycles
CABIN, STATIONS 324 TO 345, LEFT BUTTLINE 40, FLOORBOARD SUPPORT HAS HOLE IN IT. REMOVED AND REPLACED FLOORBOARD SUPPORT PER AARD 51-10-05-1 REPAIR 1.
Part: GOVERNOR — LEAKING (LT ENGINE) · airframe 57,694 hrs · 20,142 cycles
SJU - DURING CLIMBOUT LEFT ENGINE OIL PRESSURE LIGHT ILLUMINATED. CAPTAIN SHUT DOWN LEFT ENGINE. SINGLE ENGINE TIME 10 MINUTES. EMERGENCY DECLARED, RETURNED SJU LANDED WITHOUT INCIDENT. FOUND FUEL GOVERNOR LEAKING. REPLACED FUEL FLOW GOVERNOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2009
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 55,581 hrs · 19,393 cycles
EMERGENCY BULL NOSE LENS COVER AT SEAT ROW 21 RIGHT SIDE MISSING. REPLACED MISSING BULL NOSE LIGHT COVER.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 55,190 hrs · 19,260 cycles
LEFT DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,190 hrs · 19,260 cycles
EMERGENCY LIGHT AT SET 36D INOPERATIVE. REPLACED LAMP, OPS CHECKS GOOD.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 55,190 hrs · 19,260 cycles
FOUND CONNECTOR FOR BATTERY PACK AT STATION 1243 (M735) DISCONNECTED, EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND RECONNECTED CONNECTOR. OPS CHECKS GOOD.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 55,190 hrs · 19,260 cycles
FOUND CONNECTOR DISCONNECTED AT BATTERY PACK STATION 1678. EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW BATTERY PACK AT STATION 1678 LEFT. RECONNECTED CONNECTOR AND OPS CHECKED GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,190 hrs · 19,260 cycles
FOUND CONNECTOR DISCONNECTED AT BATTERY PACK STATION 1678 RIGHT. EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW BATTERY PACK AT STATION 1678 RIGHT AND OPS CHECKED GOOD.
2008
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. SECURED LOOSE CONNECTOR AS SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: RELIEF VALVE — POPPED (RT WING) · airframe 50,154 hrs
JFK INFLIGHT T1375/21MAR BDL TO SJU - TOWER REPORTED FUEL LEAKING FROM RIGHT WING. LANDED JFK WITHOUT INCIDENT. FOUND PRESSURE RELIEF VALVE POPPED IN PANEL NUMBER SIX POSITION FROM OUTBOARD. RELOCATED PRESSURE RELIEF VALVE TO NUMBER FIVE POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,735 hrs
DFW - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: TRANSMISSION — TRIPPED (TE FLAP)
AUA INFLIGHT T1013/02NOV - TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED ON APPROACH. LANDED AUA WITHOUT INCIDENT. FOUND LEFT INBOARD TRAILING EDGE FLAP TRANSMISSION TRIPPED. RESET AND LUBED FLAP ROLLERS AND JACK SCREW. SYSTEM CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHTS)
DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11D MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — MISSING (EMERGENCY LIGHTS)
DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11D MISSING LAMP. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK M10801 FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY AISLE LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY AISLE LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: CONNECTOR — DISCONNECTED (CABIN)
ORD - EMERGENCY PATH LIGHT AT SEAT ROW 34D RIGHT SIDE INOPERATIVE. FOUND PLUG AT WALL DISCONNECTED. CONNECTED EMERGENCY LIGHT PLUG AT ROW 36. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
ORD - EMERGENCY LIGHTS ABOVE ROW 34ABC INOPERATIVE. RELAMPED EMERGENCY LIGHTS ABOVE ROW 34ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — UNSECURE (CABIN)
TUL - CEILING EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. SECURED BATTERY PACK AND CHARGER TRAY TO CEILING PANEL FOR CEILING EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: CONTROLLER — ARCED (WINDSHIELD HEAT)
LIM - INFLIGHT T0947 RIGHT FORWARD WINDSHIELD ARCHED AND SMALL FIRE OCURRED AT BASE OF WINDSHIELD. TURNED RIGHT WINDOW HEAT SWITCH OFF TO STOP ARCING. REPLACED WINDOW AND WINDOW HEAT CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LINE — LEAKING (ZONE 600)
ORD T2095/11 CARGO REPORTED EVIDENCE OF FLUID LEAK FROM THE RIGHT HAND ENGINE UPON ARRIVAL AT GATE. INVESTIGATION REVEALED LP FUEL PUMP LINE HAD CHAFED AGAINST THE HYDRAULIC LINE CAUSING A HOLE IN THE FUEL PUMP LINE. REPLACED FUEL LINE ON NR 2 ENGINE. LEAK CHECK GOOD ON ENGINE RUN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LINE — CHAFED (FUEL DISTRIB) · airframe 37,466 hrs · 13,017 cycles
ENGINE HYDRAULIC LINES WERE RUBBING ON FUEL LINE. HYDRAULIC PRESSURE LINE WORE A HOLE IN THE LOW PRESSURE FUEL LINE. SHOULD HAVE STANDOFF FOR HYDRAULIC LINES AND OR MORE FREQUENT INSPECTION.
2003
Part: TRANSMITTER — INOPERATIVE (LT HYD QTY)
EN ROUTE LT HYD QTY LIGHT ILLUMINATED. LANDED ORD WITHOUT INCIDENT. REPLACED LT HYD QTY TRANSMITTER PER MM 29-33-01-4. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: OVEN — INOPERATIVE (GALLEY)
FLIGHT ATTENDANTS REPORTED SMOKE AND A BURNING SMELL FROM FORWARD GALLEY OVEN. RETURNED AND LANDED JFK WITHOUT INCIDENT. REMOVED DEBRIS FROM FIRT CLASS OVEN. SYTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: FLOOR BEAM — CORRODED (BS 1640)
AFW - FLOOR BEAM AT STA 1640 HAS SEVERAL AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. REF E 58 NR'S 1697035, 1697033, 1697032, 1697036, AND 1697034. TST: 15,561.43 HOURS. CYCLES: 5,712. (X)
Part: ANGLE — CORRODED (L1 DOORWAY)
AFW - ANGLE BY L-1 DOOR OPENING HAS CORROSION REMOVAL MATERIAL REMAINING AND IS BEYOND SRM LIMITS. REF E 58 NR 1697136. TST: 15,516.36 HOURS. CYCLES: 5,712. (X)
Part: SEAT TRACK — CORRODED (BS 377)
AFW - SEAT TRACK AT STA 377, LBL 45, HAS CORROSION REMOVAL MATERIAL REMAINING BEYOND SRMS LIMITS. REF E 58 NR 1697043. TST: 15,516.36 HOURS. CYCLES: 5,712. (X)
Part: RIB — CORRODED (AILERON)
AFW - AILERON ATTACH RIB NR 1 HAS CORROSION REMOVAL AROUND GROUNDING ATTACH BOLT HOLE. MATERIAL REMAINING IS BEYOND SRM LIMITS. REF: E 58 NR 1697121. TST: 15,516.36 HOURS. CYCLES: 5,712. (X)
Part: DECK PLATE — CORRODED (BS 1660)
AFW - DECK PLATE HAD CORROSION BLENDED BEYOND SRM LIMITS. REF E 58 NR'S 9037033 AND 9037052. (X)
Part: PAN — GOUGED (R1 DOOR)
AFW - R1 DOOR PAN HAS GOUGE THAT IS BEYOND SRM LIMITS. REF E 58 NR 1696987. TST: 15,516.43 HOURS. CYCLES: 5,712. (X)
Part: FLOOR BEAM — CORRODED (BS 377)
AFW - FLOOR BEAM AT STA 377 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. REF E 58 NR'S 1697054 AND 1697062. TST: 15,561.43 HOURS. CYCLES: 5,712. (X)
Part: FLOOR BEAM — CORRODED (BS 324)
AFW - FLOOR BEAM AT STA 324 HAS CORROSION REMOVAL ON UPPER SURFACE MATERIAL REMAINING IS BEYOND SRM LIMITS. REF E 58 NR'S 1697049 AND 1697047. TST: 15,561.43 HOURS. CYCLES: 5,712. (X)
Part: FLOOR BEAM — CORRODED (BS 365)
AFW - FLOOR BEAM AT STA 365 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRMS LIMITS. REF E 58 NR 1697052. TST: 15,561.43 HOURS. CYCLES: 5,712. (X)
Part: STRUCTURE — CORRODED (41 SECTION)
AFW - FLOOR SUPPORT STRUCTURE SEC 41 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING BEYOND SRM LIMITS REF E 58 NR'S 1697045, 1697051, 1697057, 1697058, 1697139. TST: 15,561.43 HOURS. CYCLES: 5,712. (X)