N7667A
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.
62 reports on file, 1996-04-18 – 2013-06-24.
Part: MODULE — FAILED (CABIN) · airframe 65,579 hrs · 23,037 cycles
FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS, LT & RT NR ONE DOORS LOWER EMERGENCY LIGHTS INOPERATIVE. INSTALLED CHARGER MODULE. OPERATIONS CHECKED NORMAL
Part: BATTERY — DISCHARGED (CABIN) · airframe 65,579 hrs · 23,037 cycles
FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS, LT & RT NR ONE DOORS LOWER EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW BATTERY. OPERATIONS CHECKED NORMAL
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 64,479 hrs · 22,650 cycles
EQUIPMENT COOLING PUSH BUTTON SWITCH "OVERHEAT LIGHT" BURNED OUT. REPLACED LAMP FOR EQUIPMENT COOLING PUSH BUTTON SWITCH. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,479 hrs · 22,650 cycles
SEAT 22D EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 22D EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: CONNECTOR — LOOSE (ZONE 100) · airframe 64,479 hrs · 22,650 cycles
RIGHT EMERGENCY BOTTLE SQUIB CONNECTOR BACKSHELL STRAIN RELIEF LOOSE. TIGHTENED RIGHT EMERGENCY BOTTLE SQUIB PLUG BACKSHELL. OPS CHECK NORMAL.
Earlier reports · 1996–2012 · 57 reports
2012
Part: BATTERY — DEFECTIVE (CABIN) · airframe 62,914 hrs · 22,062 cycles
FIRST CLASS RIGHT SEAT MOUNTED EMERGENCY LIGHT STAY ON WITH POWER OFF. REPLACED BAD BATTERY ON BATTERY PACK. OPS CHECK NORMAL.
Part: WIRE — DAMAGED (CABIN) · airframe 62,527 hrs · 21,919 cycles
EMERGENCY LIGHTING SYSTEM FROM ROWS 26D TO 36D INOPERATIVE. REPAIRED DAMAGED WIRE AT EMERGENCY LIGHT ASSEMBLY AT RIGHT NUMBER 4 DOOR, OPS CHECK NORMAL.
Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
CORROSION WAS FOUND ON THE RIGHT INBOARD MAIN FLAP AT THE UPPER SKIN. INSTALLED DOUBLER PER EA B757-57-023402.
Part: ACTUATOR — FAILED (CABIN) · airframe 62,371 hrs · 21,861 cycles
LEFT OFF WING SLIDE PNEUMATIC DEPLOYMENT SYSTEM FAILED OPERATIONAL CHECK. REPLACED LEFT OVERWING SLIDE DOOR ACTUATOR. OPS CHECK NORMAL.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
AFT CARGO FRAME AND SHEAR TIE AT STATION 1460 LEFT BUTTLINE 3 CORRODED. INSTALLED DOUBLER PER EA B757-53-023400.
Part: HINGE FITTING — CRACKED (NR 2 PLYON) · airframe 62,371 hrs · 21,861 cycles
NUMBER 2 PYLON OUTBOARD HINGE FITTING UPPER AFT HOLE HAS TWO CRACK INDICATIONS. INSTALLED DOUBLER PER EA B757-54-023384.
Part: DOOR — WORN (CARGO BAY) · airframe 62,371 hrs · 21,861 cycles
FORWARD CARGO DOOR LOWER FLANGE HAS SEVERAL NICKS, DENTS AND CHAFED SPOT ENTIRE LENGTH OF FLANGE SECTION. REPLACED CORNER PER SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
BULK CARGO COMPARTMENT, INTERCOSTAL UPPER ANGLE CORRODED FROM BODY STATIONS 1480 TO 1500 STRINGERS 25 TO 26 RIGHT. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: SKIN — DENTED (LE SLAT) · airframe 62,371 hrs · 21,861 cycles
NUMBER 1 SLAT DENTED SEVERAL PLACES. REPAIRED DENTS BY REMOVING DAMAGE AND BONDING NEW SKINS AND DOUBLERS PER SRM 57-43-02 AND 51-70-10.
Part: SKIN — DENTED (TE FLAP) · airframe 62,371 hrs · 21,861 cycles
RIGHT WING INBOARD MID FLAP UPPER SURFACE DENTED CLUSTER IN THE CENTER. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
BULK CARGO COMPARTMENT INTERCOSTAL CORRODED AT BODY STATIONS 1600 TO 1620, STRINGER 29 TO 30 RIGHT. REPLACED INTERCOSTAL PER SRM 51-40-02 AND BAC DWG 146N5451.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
BULK CARGO COMPARTMENT, INTERCOSTAL CORRODED FROM BODY STATIONS 1600 TO 1620, STRINGERS 29 TO 30 LEFT. REMOVED CORROSION AND REPLACED INTERCOSTAL PER SRM 51-40-02 AND BAC DWG 146N5451.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
AFT CARGO COMPARTMENT LEFT INTERCOSTAL FROM BODY STATION 1480 TO 1500, STRINGER 26 LEFT HAS CORROSION. REMOVED AND REPLACED CHORD PER SRM 51-40-02.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
NUMBER 3 SLAT LEADING EDGE SKIN SIX FEET FROM THE OUTBOARD END IS CORRODED. REMOVED DAMAGE AND FABRICATED A FLUSH REPAIR PER AARD 57-43-01-2.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
MAIN CABIN FLOOR SUPPORT ANGLE AND SILL SUPPORT PLATE CORRODED UNDER DOOR DRAIN PLATE FROM BODY STATIONS 676 TO 740, RIGHT BUTTLINES 62 TO 65. REMOVED AND REPLACED SILL SUPPORT PER DWG 143N8322.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
MAIN CABIN FLOORBOARD ATTACH ANGLE CORRODED FROM BODY STATIONS 1597 TO 1600 LEFT BUTTLINE 63. REMOVED AND REPLACED DAMAGE ATTACHED ANGLE PER AARD 53-60-73-1.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,371 hrs · 21,861 cycles
MAIN CABIN FLOOR SUPPORT ANGLE AND SILL SUPPORT STRUCTURE CORRODED UNDER DRAIN PLATE FROM BODY STATIONS 676 TO 740, LEFT BUTTLINES 61 TO 64. REMOVED AND REPLACED MAIN CABIN FLOOR SUPPORT SILL PER BAC DWG 143N8322.
Part: ENGINE — FAILED (LEFT) · airframe 62,133 hrs · 21,766 cycles
CREW REPORTED ON INITIAL DESCENT WHEN THROTTLES STARTED BACK THEY FELT A THUMP AND SAW THE LEFT ENGINE HAD FLAMED OUT. UNCOMMANDED ENGINE SHUTDOWN (SINGLE ENGINE TIME 20 MINS). NO ATTEMPT WAS MADE TO RESTART. CREW ALSO HAD A EICAS STATUS MESSAGE: "L ENG LP PUMP". EMERGENCY DECLARED FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL.
2011
Part: PROBE — DEFECTIVE (RT ENGINE) · airframe 60,505 hrs · 21,167 cycles
BDA - CREW REPORTED RIGHT ENGINE PRESSURE RATIO INDICATION FAULT. EMERGENCY DECLARED FLIGHT RETURNED BDA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACE P1 PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,031 hrs · 20,613 cycles
CORROSION ON G1 FLOOR FITTING. REMOVED AND REPLACED FLOOR FITTING.
Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 59,031 hrs · 20,613 cycles
DENT IN LEFT SKIN PANEL, JUST AFT OF RADOME. CUT OUT DAMAGE AND REPAIRED IAW EA B757-53-014838 AND SRM 53-00-011-2R3.
2010
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,498 hrs · 20,413 cycles
LEFT AFT OFF WING LIGHT L568 INOPERATIVE. REPLACED M735 POWER SUPPLY ASSEMBLY. OPS CHECKS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,477 hrs · 20,405 cycles
SEAT 33D ESCAPE PATH LIGHT LAMP INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT SEAT 33D. OPS CHECK NORMAL.
Part: LENS — MISSING (CABIN) · airframe 58,477 hrs · 20,405 cycles
SEAT 26D ESCAPE PATH LIGHT LENS MISSING. REPLACED LENS FOR ESCAPE PATH LIGHT AT 26D. OPS CHECK NORMAL.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,228 hrs · 19,287 cycles
RIGHT NUMBER 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY AT RIGHT NUMBER 2 DOOR. OPS CHECK OK.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 55,228 hrs · 19,287 cycles
PATHWAY EMERGENCY LIGHT FROM SEAT ROWS 9D TO 16D INOPERATIVE. REPLACED BATTERY PACK AND MODULE CHARGER.
Part: VALVE — FAILED (PARKING BRAKE) · airframe 55,201 hrs · 19,273 cycles
TWO HOURS INTO THE FLIGHT THE PARKING BRAKE LIGHT WITH THE ASSOCIATED EICAS MESSAGE ILLUMINATED. LANDED LAX WITHOUT INCIDENT. REPLACED PARKING BRAKE VALVE.
Part: MODULE — INOPERATIVE (CABIN) · airframe 55,088 hrs · 19,232 cycles
FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED MODULE FOR SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS. OPS CHECK OK.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,090 hrs · 18,868 cycles
ELEVATOR SYMETRY STATUS MESSAGE DURING CLIMBOUT. RETURNED ORD WITHOUT INCIDENT. RESET FAULT BALL AND PERFORMED THE REST OF THA SAM BITE PROCEDURE AND THE SYSTEM CHECKS OK. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)
2008
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 52,713 hrs
EMERGENCY LIGHT AT OVERHEAD SEAT ROW 11D INOPERATIVE. FOUND LOOSE CONNECTOR AND SECURED CONNECTOR AT OVERHEAD SEAT ROW 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 52,329 hrs
MIA - EMERGENCY LIGHT AT SEAT ROW 5 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 5. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: LIGHT — BROKEN (CABIN)
MIA - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SLIDE — DISLODGED (L1 DOOR)
SXM - EMERGENCY SLIDE AT LEFT NUMBER ONE DOOR DISLODGED FROM SLIDE STORAGE PACK AND WAS SUPPORTED BY JETBRIDGE NOT ACTIVATING INFLATION SEQUENCE. SLIDE DID NOT DEPLOY. REPLACED EMERGENCY SLIDE AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - EMERGENCY EXIT LIGHT AT SEAT 14D INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHTS AT ROW 17D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT ROW 17D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHTS AT ROWS 17 THROUGH 25 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AND CHARGER FOR INOPERATIVE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 25. SYSTEM GROUND CHECKED NORMAL OPERATION.
2002
Part: CIRCUIT BREAKER — DAMAGED (COCKPIT)
MIA - EMERGENCY ESCAPE SLIDE SQUIB TEST INOPERATIVE. FOUND LEFT GENERATOR CIRCUIT BREAKER WITH BROKEN 'A' PHASE TERMINAL. REPLACED CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)
Part: SLIDE — DEPLOYED (OVERWING)
TUL - FLT 9603 - EN ROUTE TUL-DFW - AFTER TAKEOFF, RECEIVED EICAS MESSAGE FOR LEFT WING SLIDE PROBLEM. DURING LANDING, AIRCRAFT REQUIRED QUARTER WHEEL DEFLECTION FOR CONTROLLED FLIGHT. RETURNED TUL AND LANDED WITHOUT INCIDENT. REMOVED DEPLOYED OVERWING SLIDE THAT CAUSED AIRCRAFT BUFFETING AND WHEEL DEFLECTION AND REPLACED WITH SERVICEABLE UNIT. FOUND FOUR HOLES IN FILET PANEL WHICH WERE REPAIRED PER SRM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: RECEIVER — INOPERATIVE (WEATHER RADAR)
MIA - FLT 860 - EN ROUTE MIA-LGA, AIRCRAFT INTERRUPTED BACK TO MIA DUE TO WEATHER RADAR INOPERATIVE. REPLACED WEATHER RECEIVER PER MM. ACCOMPLISHED ADJUSTMENT AND TEST PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: WIRE — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD SIDEWALL EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: CONNECTOR — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 1E AND FORWARD OF 9E INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTORS AT 1E AND 9E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — DAMAGED (ROWS 1 AND 6)
TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT ROWS 1E AND 6E INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT ROW 1E. SYSTEM GROUND CHECKED, NORMAL OPERRATION. (X)
1998
Part: CONNECTOR — DIRTY (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MOST FORWARD CABIN CENTER POSITION INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT ASSEMBLY CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: STRUCTURE — CORRODED (BS 373)
AFW - FLOOR STRUCTURE AT STATION 373 RBL 60 HAD CORROSION BLENDED BEYOND SRM LIMITS, E58 NR 1668876. REPAIRED PER MRB NR 757-1103. (M)
Part: STRUCTURE — CORRODED (BS 404)
AFW - FLOOR STRUCTURE AT STATION 404 RBL 55 HAD CORROSION BLENDED BEYOND SRM LIMITS E58 NR 1668873. REPAIRED PER MRB NR 757-1100. (M)
Part: STRUCTURE — CORRODED (BS 407)
AFW - FLOOR STRUCTURE AT STATION 407 RBL 60 HAD CORROSION BLENDED BEYOND SRM LIMITS E58 NR 1668872. REPAIRED PER MRB NR 757-1109. (M)
Part: STRUCTURE — CORRODED (BS 393)
AFW - FLOOR STRUCTURE AT STATION 393 RBL 60 HAD CORROSION BLENDED BEYOND SRM LIMITS, E58 NR 1668875. REPAIRED PER MRB NR 757-1102. (M)
Part: FLOORBEAM — CORRODED (BS 365)
AFW - FLOORBEAM AT STATION 365 LBL 60 AND RBL 60 HAD CORROSION BLENDED BEYOND SRM LIMITS E58 NR 1668888 AND 1669025. REPAIRED PER MRB NR 757-110. (M)
Part: FLOORBEAM — CORRODED (BS 395)
AFW - FLOORBEAM AT STATION 395 RBL 60 HAD CORROSION BLENDED BEYOND SRM LIMITS, E58 NR 1668874. REPAIRED PER MRB NR 757-1106. (M)
Part: FLOORBEAM — CORRODED (BS 377)
AFW - FLOORBEAM AT STATION 377 RBL 60 HAD CORROSION BLENDED BEYOND SRM LIMITS, E58 NR 1668877. REPAIRED PER MRB NR 757-1104. (M)
Part: SEAT TRACK — CORRODED (BS 377)
AFW - SEAT TRACK AT STATION 377 LBL 45 HAD CORROSION BLENDED BEYOND SRM LIMITS E58 NR 1668871. REPAIRED PER MRB NR 757-1108. (M)
Part: PAN — GOUGED (R-4 DOOR)
AFW - R-4 DOOR HANDLE PAN HAS GOUGE BEYOND SRM LIMITS, E58 1668902. REPAIRED PER MRB NR 757-1110. (M)
Part: STRUCTURE — CORRODED (BS 332)
AFW - FLOOR STRUCTURE AT STATION 332 RBL 3 HAD CORROSION BLENDED BEYOND SRM LIMITS E58 NR 1668880. REPAIRED PER MRB NR 757-1105. (M)
Part: FLOORBEAM — CORRODED (BS324 RBL 61)
AFW - FLOORBEAM AT STATIO 324, RBL 61 HAD CORROSION BLENDED BEYOND SRM LIMITS E58NR 1668879. REPAIRED PER MRB NR 757-1107. (M)
1996
Part: FLOOR BEAM — CORRODED (BS 1640)
AFW - FOUND SEVERAL AREAS OF CORROSION BLENDED BEYOND SRM LIMITS ON FLOOR BEAM AT STATION 1640. PER MRB 757-954. (M)
Part: WIRE — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, SHORT SECTION OF EMERGENCY FLOOR LIGHT AT MID-CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE AT MID-CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)