N652AA
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.
58 reports on file, 1995-08-18 – 2015-01-05.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,866 hrs · 24,950 cycles
EMERGENCY LIGHT IN BULLNOSE OVER SEAT 33 CEG IS INOPERATIVE. R & R LAMP IAW AMM 33-51-00. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,866 hrs · 24,950 cycles
EMERGENCY LIGHT IN BULLNOSE AT SEAT 34 ABC INOPERATIVE. R & R LAMP IAW AMM 33-51-00. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 71,866 hrs · 24,950 cycles
RIGHT MID EMER EXIT EXTERIOR LIGHT INOPERATIVE. R & R LAMP AMM 33-51-00. SYS CHECKED NORMAL.
Earlier reports · 1995–2014 · 55 reports
2014
Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,758 hrs · 24,913 cycles
EMERGENCY LIGHT AT 22D IN CURVED OVERHEAD BIN PANEL INOPERATIVE. RELAMPED AT 22D BULLNOSE EPL PANEL IAW MM 33-51-05. OPERATIONS CHECKED GOOD.
Part: SLAT — DENTED (RT WING) · airframe 70,977 hrs · 24,619 cycles
NUMBER 10 SLAT DENTED 60 INCHES FROM OTBD END & 3 INCHES BACK FROM LE. INSTALLED FILLER & DOUBLER IAW SRM 57-43-01-2R-1, EA B757-57-036117 & AARD 57-43-00-1.
Part: SKIN — CRACKED (NR 1 PYLON) · airframe 70,320 hrs · 24,380 cycles
NUMBER 1 PYLON OTBD SKIN AT LT PPS 156 CRACKED. REPAIR DOUBLER INSTALLED IAW EA B757-54-034667.
Part: STIFFENER — CORRODED (RT MLG WW) · corrosion level 2 · airframe 70,320 hrs · 24,380 cycles
RIGHT WW AFT BULKHEAD HORIZONTAL STIFFENER CORRODED AT STATION 1180. REPLACED HORIZONTAL STIFFENER.
Part: SKIN — CRACKED (NR 1 PYLON) · airframe 70,320 hrs · 24,380 cycles
NUMBER 1 PYLON OTBD SKIN & DOUBLER WERE FOUND CRACKED AT STATION 156. INSTALLED DOUBLER AT STATION 156.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,320 hrs · 24,380 cycles
RIGHT WW, KEEL BEAM TO STATION 1180 ATTACH FITTING HAD CORROSION ON UPPER SURFACE DUE TO LEVELING COMPOUND COMING LOOSE. REPLACED FITTING.
Part: FITTING — CORRODED (LT MLG WW) · corrosion level 3 · airframe 70,320 hrs · 24,380 cycles
CORROSION ON LT WW SPLICE FITTING AT STATION 1180 & LBL 2. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B757-53-034815.
2013
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,699 hrs · 23,113 cycles
RIGHT NUMBER ONE COCKPIT ENTRY AND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,699 hrs · 23,113 cycles
EMERGENCY LIGHT ON OVERHEAD BIN ON ROW 31ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ON OVERHEAD BIN ON ROW 31ABC. OPS CHECK NORMAL
Part: CONNECTOR — FAULTY · airframe 66,656 hrs · 23,097 cycles
TPA - INFLIGHT DFW-SJU. CREW REPORTED SMOKE IN COCKPIT AND CABIN, FOLLOWED BY FORWARD EQUIPMENT OVERHEAT MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED TPA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CONNECTOR AT FLOW SENSOR D1574. SYSTEM GROUND CHECK NORMAL OPERATION.
2012
Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 66,317 hrs · 22,982 cycles
MIA - CREW REPORTED LEFT ENGINE HYDRAULIC PUMP EICAS WARNING. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT ENGINE HYDRAULIC PUMP LEAKING. REPLACED ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 65,129 hrs · 22,574 cycles
UPON ARRIVAL, CREW OPENED THE LEFT NUMBER 1 DOOR AND THE DOOR ASSIST BOTTLE FIRED AND THE SLIDE FELL ONTO THE JET BRIDGE. REPLACED DOOR ASSIST BOTTLE AND LEFT NUMBER 1 DOOR SLIDE ASSEMBLY.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,885 hrs · 22,486 cycles
EXTERIOR RIGHT NUMBER 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 64,164 hrs · 22,207 cycles
SFO - CREW REPORTED ELECTRICAL HAZE VISIBLE IN REAR OF AIRCRAFT ACCOMPANIED BY ELECTRICAL FUMES SMELL. EMERGENCY DECLARED FLIGHT RETURNED SFO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ROW 30ABC POWER PORT POWER SUPPLY. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: AXLE — SHEARED (RT MLG) · airframe 62,516 hrs · 21,561 cycles
LAX - CREW REPORTED THAT AIRCRAFT MAY HAVE BLOWN A TIRE ON TAKEOFF. DEBRIS WAS REPORTED ON RUNWAY AFTER TAKEOFF FROM SDF. EMERGENCY DECLARED FLIGHT LAND LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 3 WHEEL/TIRE/BRAKE ASSEMBLY AND AXLE SEPARATED FROM RIGHT MAIN LANDING GEAR TRUCK ASSEMBLY. REPLACED RIGHT MAIN LANDING GEAR TRUCK ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SKIN — DENTED (FUSELAGE) · airframe 62,306 hrs · 21,490 cycles
SKIN DENTED ROUND PERIMETER OF FASTENER AND CREASED ON FORWARD SIDE AT APPROXIMATELY STATION 682 BETWEEN STRINGERS 1 AND 2 RIGHT. INSTALLED REPAIR DOUBLER PER EA B757-53-018188 DATED JULY 21, 2011.
Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 62,306 hrs · 21,490 cycles
NUMBER 1 CARGO DOOR NUMBER 5 LOWER STIFFENER CRACKED. REPLACED PER ESO 90114.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,306 hrs · 21,490 cycles
CORROSION ON CREASE ANGLE WEB IN CABIN LEFT SIDE BETWEEN STATIONS 1020 AND 1040. REPLACED WEB PER AARD 51-10-05-1.
Part: SKIN — SCRATCHED (CARGO DOOR) · airframe 62,306 hrs · 21,490 cycles
AFT CARGO DOOR OUTER SKIN LOWER EDGE IS SCRATCHED. INSTALLED REPAIR DOUBLER PER SRM 52-30-01-2R 4 PAGE 1.
Part: PAN — GOUGED (L4 DOOR) · airframe 62,306 hrs · 21,490 cycles
LEFT NUMBER 4 DOOR HANDLE PAN GOUGED. INSTALLED NEW HANDLE PAN PER SRM 51-40-02.
Part: BULLNOSE — DAMAGED (LT WING) · airframe 62,306 hrs · 21,490 cycles
LEFT WING BULL NOSE CRACKED. INSTALLED DOUBLER PER AARD 57-41-01-6.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 61,215 hrs · 21,091 cycles
SEAT 28D EMERGENCY LIGHT INOPERATIVE. RE-SEATED CONNECTOR AT SEAT 28D. OPS CHECK NORMAL.
2010
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,330 hrs · 20,773 cycles
EXIT SIGN AT FLIGHT DECK ENTRANCE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK. OPS CHECKED NORMAL
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,555 hrs · 20,114 cycles
EMERGENCY EXIT LIGHTS VERY DIM OR OUT FROM ROW 17 BACK. REPLACED BATTERY PACK ABOVE RIGHT AFT LAVATORY. OPS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,555 hrs · 20,114 cycles
EMERGENCY EXIT LIGHT VERY DIM OR OUT FROM ROW 17 BACK. REPLACED BATTERY PACK AT ROW 20.
2009
Part: SLAT — DAMAGED (RT WING) · airframe 57,897 hrs · 19,892 cycles
RIGHT WING NUMBER 7 SLAT LOWER TRAILING EDGE DAMAGED AND DEFORMED FROM INBOARD EDGE TO 4 FEET OUTBOARD. ACCOMPLISHED WET LAYUP REPAIR PER SRM 51-70-06-0G.
Part: DOOR — CRACKED (LE SLAT) · airframe 57,897 hrs · 19,892 cycles
RIGHT WING NUMBER 7 SLAT OUTBOARD DRIVE TRACK DOOR CRACKED. INSTALLED NEW DOOR PER AARD 51-20-00-1.
Part: SKIN — CRACKED (LE SLAT) · airframe 57,897 hrs · 19,892 cycles
NUMBER 2 SLAT BACK SIDE COVE SKIN IS CRACKED BY A FASTENER AT THE INBOARD DRIVE TRACK. INSTALLED REPAIR DOUBLER ON COVE SKIN PER AARD-57-43-00-4.
Part: SUPPORT — CRACKED (RT WING) · airframe 57,897 hrs · 19,892 cycles
RIGHT WING THERMAL ANTI-ICE DUCT ANCHOR SUPPORT AT STATION 428 IS CRACKED. INSTALLED NEW THERMAL ANTI-ICE SUPPORT PER ESO 90248.
Part: FASTENER — DAMAGED (LE SLAT) · airframe 57,897 hrs · 19,892 cycles
NUMBER 2 SLAT BLIND FASTENER HEAD DAMAGED. REMOVED DAMAGED AREA AND INSTALLED FLUSH REPAIR PER SRM-57-43-01-2R 2.
Part: SKIN — DAMAGED (LE SLAT) · airframe 57,897 hrs · 19,892 cycles
LEFT WING NUMBER 3 SLAT LOWER SKIN TRAILING EDGE GOUGED ABOVE INBOARD DRIVE TRACK. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER PER SRM 51-70-10 2R 4 ON TRAILING EDGE ABOVE INBOARD DRIVE TRACK.
Part: SKIN — DAMAGED (LE SLAT) · airframe 57,897 hrs · 19,892 cycles
NUMBER NINE RIGHT OUTBOARD SLAT PLATING SEPARATING ON LEADING EDGE SKIN 26 INCHES OF OUTBOARD EDGE. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER AARD 57-43-00-01.
Part: SKIN — CRACKED (LE SLAT) · airframe 57,897 hrs · 19,892 cycles
NUMBER NINE RIGHT OUTBOARD SLAT INNER SKIN CRACKED INBOARD OF INBOARD DRIVE ATTACH. INSTALLED DOUBLER ON SKIN PER AARD 57-43-00-4.
Part: LIGHT — INOPERATIVE (CABIN)
LAX EMERGENCY PATH LIGHTS AT SEAT 18D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY PATH LIGHTS AT SEAT 18D.
2008
Part: LENS — DAMAGED (EMERGENCY LIGHT)
DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR HAS DAMAGED LENS. REPLACED LENS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 53,466 hrs
MIA - EMERGENCY LIGHT AT OVERHEAD CABIN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,149 hrs
DFW - EMERGENCY EXIT LIGHT AT SEAT 17A INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT SEAT 17A. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN)
JFK - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: LINE — RUPTURED (HYD SYSTEM)
BOS INFLIGHT T1752/21AUG - ON FINAL APPROACH, AIRCRAFT UNABLE TO EXTEND RIGHT MAIN GEAR. EXENDED GEAR THROUGH EMERGENCY PROCEDURE AND LANDED WITHOUT INCIDENT. FOUND FLEX LINE AT RIGHT GEAR DOWNLOCK ACTUATOR RUPTURED. REPLACED BOTH FLEX LINES. AIRCRAFT MAINTENANCE FERRIED TO JFK FOR GEAR RETRACTION CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - RIGHT AFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK/CHARGER ASSEMBLY FOR RIGHT AFT EXTERIOR OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)
ATL - FOUND EMERGENCY ESCAPE FLASHLIGHT INOPERATIVE AT THE AFT FLIGHT ATTENDANT LOCATION. REPLACED BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - FOUND EMERGENCY EXIT SIGN AT LEFT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR LEFT OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
JFK - EMERGENCY EXIT LIGHT BELOW OVERHEAD BIN 12 ABC IS OUT. REMOVED AND REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FRONT OF FIRST ROW OF SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS IN FORWARD END OF COACH INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE FLOOR PATH LIGHT STRIP IN FORWARD END OF COACH. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1997
Part: BOTTLE — LOW PRESSURE (R3 DOOR)
ORD - DURING OVERNIGHT CHECK, R3 OVERWING SLIDE WOULD NOT PRESS-TO-TEST. REPLACED LOW NITROGEN BOTTLE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: LIGHT PANEL — BROKEN (COCKPIT)
JFK - DURING OVERNIGHT CHECK, EMERGENCY LIGHT SWITCH IN COCKPIT BROKEN/INOPERATIVE. REPLACED EMERGENCY LIGHT PANEL ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: FRAME — CRACKED (BS 524)
AFW - FOUND FUSELAGE FRAME CRACKED AT 524R. REPAIRED PER MRB 757-872. (M)
Part: STUB FRAME — GOUGED (PAX DOOR)
AFW - FOUND NR 1 ENTRY DOOR HAS GOUGE BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-875. (M)
Part: DECK PLATE — CORRODED (BS 1681)
AFW - FOUND DECK PLATE CORROSION BEYOND SRM LIMITS. REPAIR PER MRB 757-871. (M)
Part: FLOOR BEAM — CORRODED (BS 377)
AFW - FOUND FLOOR BEAM AT STATION 377 CORROSION BEYOND SRM LIMITS. REPAIR PER MRB 757-867. (M)
Part: DOOR SILL — CORRODED (CARGO COMPT)
AFW - FOUND CORRODED LOWER SILL BEYOND SRM LIMITS. REPAIRED PER MRB 757-865. (M)
Part: FLOOR BEAM — CORRODED (BS 365)
AFW - FOUND FLOOR BEAM CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-868. (M)
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 10 THROUGH 18 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: EEL CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT AFT OF CENTER GALLEY FOUND INOPERATIVE. RESECURED LOOSE CONNECTOR AFT OF CENTER GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)