N679AN
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.
78 reports on file, 1999-02-27 – 2018-11-15.
Part: FLAP — CORRODED (RT WING) · airframe 56,225 hrs · 19,954 cycles
RT O/B MAIN FLAP HAS INTERNAL CORROSION AROUND FASTENERS HOLE APPROX WBL 493.
Part: FLAP — CORRODED (LT WING) · airframe 56,225 hrs · 19,954 cycles
LT O/B MAIN FLAP HAS INTERNAL CORROSION ON FWD LOWER FLANGE AND AROUND FASTENER HOLES APPX WBL493.
Part: STRAP — CRACKED (FUSELAGE) · airframe 56,225 hrs · 19,954 cycles
BS 377 LBL 45.5 STABILIZATION STRAP IS CRACKED.
Part: SKIN — GOUGED (HORIZ STAB) · airframe 56,225 hrs · 19,954 cycles
DENT WITH GOUGES FOUND ON LOWER SURFACE OF HORIZONTAL STABILIZER, 9" AFT OF AUX SPAR, AND 24" FROM IB END.
Part: SKIN — DENTED (FUSELAGE) · airframe 56,225 hrs · 19,954 cycles
(2) DENTS FOUND IN CLOSE PROXIMITY TO EACH OTHER ON FUSELAGE SKIN AT APPROX STA 520-540 STR 27L-28L.
Part: SKIN — DENTED (CARGO DOOR) · airframe 56,225 hrs · 19,954 cycles
DENTED AREA FOUND ON EXTERIOR SKIN OF C-2 DOOR, FORWARD LOWER CORNER.
Earlier reports · 1999–2017 · 72 reports
2017
Part: GUARD — BROKEN (CABIN) · airframe 56,036 hrs · 19,844 cycles
THE AIRCRAFT WAS NOT GROUNDED. L1 FWD LEFT ENTRY DOOR GUARDED EMERGENCY LIGHT SWITCH INOP. THE GUARD IS BROKEN. REPLACED LI FWD ENTRY DOOR EMERGENCY LIGHT SWITCH GUARD ON F/A PANEL AS REQUIRED. OP CHK GOOD.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 55,867 hrs · 19,802 cycles
EMERGENCY LIGHT AT SEAT 33D IS INOPERATIVE. SECURED THE CONNECTOR. OPS CHECKED GOOD IAW AMM 33-51-00.
Part: GIRT BAR — DIRTY (R1 DOOR SLIDE) · airframe 55,665 hrs · 19,700 cycles
FLIGHT ATTENDANT REPORTED THE R1 DOOR WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR TRACK. OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,654 hrs · 19,694 cycles
EMERGENCY EXIT LIGHTS AT SEATS 1E TO 6E ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK AT M10798 IAW AMM 33-51-00. OPERATIONAL CHECKED GOOD.
Part: GIRT BAR — OUT OF POSITION (R4 DOOR) · airframe 55,501 hrs · 19,625 cycles
AIRCRAFT WAS GROUNDED. WHILE OPENING DOOR 4R THE SLIDE AND GIRT BAR FELL OUT AND PULLED THE SLIDE OUT OF ITS CONTAINER. REPLACED ESCAPE SLIDE ASSEMBLY PER MCM 25-94-34.
Part: GIRT BAR — OUT OF POSITION (ZONE 800) · airframe 55,497 hrs · 19,623 cycles
AIRCRAFT WAS GROUNDED. R3 DOOR ARMED LIGHT DOES NOT ILLUMINATE WITH DOOR ARMED. REINSTALLED R3 DOOR GIRT BAR AND SLIDE COVER IAW AMM 52-11-25. SYSTEM CHECKS NORMAL.
Part: LINER — OUT OF POSITION (L3 DOOR) · airframe 55,493 hrs · 19,622 cycles
L3 DOOR ARM LINKAGE FROM LATCH TO BUTTON IS STUCK IN THE RETRACTED POSITION. REPOSITIONED LOWER DOOR LINER IAW AMM 52-11-00. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: COVER — OUT OF POSITION (L4 DOOR) · airframe 55,470 hrs · 19,612 cycles
AIRCRAFT WAS NOT GROUNDED. L4 DOOR EMERGENCY EVACUATION SLIDE COVER HITS THE DOOR CUTOUT. ADJUSTED COVER PER AMM 52-11-01. OPERATIONAL CHECK GOOD.
Part: LENS — BROKEN (CABIN) · airframe 55,111 hrs · 19,468 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 30DEF HAS A BROKEN LENS COVER. REMOVED AND REPLACED LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: WIRE — DAMAGED (CABIN) · airframe 55,111 hrs · 19,468 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH AISLE LIGHT AT SEAT 33DEF IS INOPERATIVE. REPAIRED WIRE IAW AMM 20-10-06. OPERATIONAL CHECK GOOD.
Part: WIRE — DAMAGED (CABIN) · airframe 55,111 hrs · 19,468 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH AISLE LIGHT AT SEAT 31DEF IS INOPERATIVE. REPAIRED WIRE IAW AMM 20-10-06. OPERATIONAL CHECK GOOD.
Part: COVER — DETACHED (R4 DOOR) · airframe 54,976 hrs · 19,408 cycles
AIRCRAFT WAS NOT GROUNDED. R4 DOOR ARM/DISARM LEVER HINGED COVER IS DETACHED. REPLACED COVER IAW AMM 52-11-02. OPERATIONAL CHECK GOOD.
Part: SEAL — LOOSE (L1 DOOR) · airframe 54,688 hrs · 19,281 cycles
AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE COVER LOWER CONNECTION POINTS DETACHED. REINSTALLED LOOSE L1 DOOR BULB SEAL. OPERATIONAL CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,688 hrs · 19,281 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 24D IS INOPERATIVE. INSTALLED LIGHT ASSEMBLY IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,382 hrs · 19,159 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT AT 21DEF INOPERABLE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 21DEF PER AMM 33-51-11.
2016
Part: LANYARD — UNSECURE (EVAC SLIDE) · airframe 54,012 hrs · 19,007 cycles
AIRCRAFT NOT GROUNDED. L4 DOOR EMERGENCY EVACUATION SLIDE HAS LANYARD PROTRUDING FROM DOOR. REMOVED AND REPLACED SLIDE IAW SIC 25-94-34. OPERATIONAL CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,875 hrs · 18,949 cycles
AIRCRAFT NOT GROUNDED. ESCAPE PATH LIGHTING DIM FROM ROW 26 BACK, FUSELAGE STATIONS 1470 TO 1678. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW 33-51-11. OPERATIONAL CHECK GOOD. REF AALA20161101002.
Part: CONTROL MODULE — FAULTY (CABIN) · airframe 53,875 hrs · 18,949 cycles
AIRCRAFT NOT GROUNDED. ESCAPE PATH LIGHTING DIM FROM ROW 26 BACK, FUSELAGE STATIONS 1470 TO 1678. REMOVED AND REPLACED AISLE PATH LIGHTING CONTROL MODULE IAW 33-51-11. OPERATIONAL CHECK GOOD. REF AALA20161029003.
Part: HANDLE — BROKEN (RT OVERWING EXIT) · airframe 53,842 hrs · 18,934 cycles
RIGHT OFF WING SLIDE COMPARTMENT CRANK HANDLE RELEASE TRIGGER IS BROKEN. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED HANDLE IAW AMM 25-65-12.
Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 53,781 hrs · 18,907 cycles
L4 DOOR EXIT SIGN COVER BROKEN. REMOVED AND REPLACED SIGN AND ACCOMPLISHED AN OPS CHECK IAW 33-00-00.
Part: FAN — OVERHEATED (COCKPIT) · airframe 53,576 hrs · 18,837 cycles
DURING CRUISE, AN ELECTRICAL ODOR WAS REPORTED IN THE CABIN AND FLIGHT DECK. ODOR DISSIPATED AFTER TURNING OFF THE RIGHT RECIRCULATION FAN. MAINTENANCE REMOVED AND REPLACED THE RIGHT CABIN RECIRCULATION FAN IAW AMM 21-25-01. OPERATIONAL CHECK GOOD.
Part: ENGINE — POWER LOSS (NR 2) · airframe 53,267 hrs · 18,715 cycles
AT FL380, THE RIGHT PACK OFF LIGHT ILLUMINATED ACCOMPANIED BY EICAS MESSAGE. UNCOMMANDED REDUCTION IN AIRSPEED AND NR 2 ENGINE POWER OCCURRED. MANUAL THROTTLE MOVEMENT INEFFECTIVE. EMERGENCY DECLARED. FLIGHT DESCENDED TO FL280. ENGINES AND PACKS RETURNED TO NORMAL. EMERGENCY CANCELLED. AIRCRAFT GROUNDED. TROUBLESHOT NR 2 ENGINE TPU, BVCU AND EEC, BOTH PACK CONTROLLERS, THE MCDP AND PLA ALL WITH NO FAULTS FOUNDED. ACCOMPLISHED RUN OF BOTH ENGINES IAW AMM 71-00-00 WITH NO ANOMALIES NOTED. FDR SHOWED NO INDICATION OF NR 2 ENGINE ROLL BACK.
Part: CONNECTOR — DAMAGED (CABIN) · airframe 52,986 hrs · 18,597 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHT AT SEAT 29D IS INOPERATIVE. LIGHT ASSEMBLY WAS FOUND TO HAVE A BROKEN CONNECTOR. R & R LIGHT ASSY IAW AMM 33-51-11. OPS CHECK NORMAL.
Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 52,052 hrs · 18,242 cycles
RELAMPED EMER LIGHT AT DEF SEAT 17, STILL INOPERATIVE. REPLACED SEAT 17 DEF HARNESS CONNECTOR NEAR WALL & ACCOMPLISHED OPERATIONAL CHECKS IAW 33-51-11. ALL CHECKED NORMAL. THE ACFT WAS NOT GNDED.
2015
Part: BULKHEAD — CRACKED (RT PYLON) · airframe 51,569 hrs · 18,062 cycles
RIGHT ENG PYLON AFT BULKHEAD VERTICAL LEG FASTENER HOLE NR 3, LEG SHOWS CRACK INDICATION IN ALUMINUM DURING HOLE PROBE HFEC 757 ET-22. REPAIRED CRACKED HOLE IAW EA 255714.
Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 51,569 hrs · 18,062 cycles
AFT CARGO COMPARTMENT RT TRANSITION PANEL CORRODED, BETWEEN STATIONS 1530 & 1640. R & R TRANSITION PANEL IAW SRM 51-10-02.
Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 51,442 hrs · 18,012 cycles
STRONG SMELL, ELECTRICAL, THROUGH COCKPIT & CABIN. RAN QRM, ODOR DISSIPATED WITH BOTH UTILITY BUSES OFF. FLIGHT DECLARED AN EMER & LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. RAN ALL SYSTEMS AS REQUIRED, PACKS, FAN, AUDIO & VIDEO SYS & ENG BLEEDS, UNABLE TO DUPLICATE. NO PROBLEMS NOTED IAW AMM 05-51-56.
2014
Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,277 hrs · 17,204 cycles
SEAT MOUNTED EMER LIGHT AT 28D BURNT OUT. R & R LAMP IAW AMM 38-51-11. SYS CHECKED GOOD.
Part: LENS — UNSECURE (EXIT SIGN) · airframe 49,080 hrs · 17,131 cycles
L3 DOOR FWD EMER LIGHT LENS FELL OFF. R & R L3 DOOR EMER EXIT IDENTIFIER SIGN IAW AMM 33-51-10. SYSTEMS CHECKED NORMAL.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 48,757 hrs · 17,007 cycles
DURING CLIMB OUT THE CAPTAINS WINDOW SHATTERED. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 1 WINDSHIELD HEAT CONTROLLER & LT NR 1 WINDSHIELD. SYS GND CHECKED NORMAL OPERATION CLOSED.
Part: LENS — MISSING (CABIN) · airframe 46,938 hrs · 16,328 cycles
ROW 9 FWD SEAT MOUNTED EMERGENCY LIGHT MISSING RED LENS. REPLACED RED LENS FOR FWD SEAT MOUNTED EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: CONNECTOR — LOOSE (CABIN) · airframe 46,938 hrs · 16,328 cycles
ROW 16DEF EMERGENCY LIGHTS INOPERATIVE. RESET LOOSE SIDEWALL CONNECTOR, OPERATIONS CHECKED NORMAL.
Part: RETAINING CLIP — BROKEN (EMERGENCY LIGHT) · airframe 46,864 hrs · 16,306 cycles
EMERGENCY EXIT LIGHT AT SEAT 18F LENS RETAINER CLIP BROKEN. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT SEAT 18F, OPERATIONS CHECKED NORMAL.
Part: RETAINING CLIP — BROKEN (EMERGENCY LIGHT) · airframe 46,864 hrs · 16,306 cycles
EMERGENCY EXIT LIGHT AT SEAT 17F LENS RETAINER CLIP BROKEN. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT SEAT 17F, OPERATIONS CHECKED NORMAL.
2013
Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,093 hrs · 15,317 cycles
FLOOR STRUCTURE CORRODED FROM FRAME STATIONS 1715 TO 1720 AND RIGHT BUTTLINES 45 TO 54. REMOVED CORROSION AND REPAIRED DECK PLATE PER SRM 53-00-51-2R AND EA B757-53-029004.
2012
Part: PLUG — LOOSE (P1 DRAIN) · airframe 41,472 hrs · 14,338 cycles
IAD - INFLIGHT MIA-BOS CREW REPORTED LEFT ENGINE LOW POWER. EMERGENCY DECLARED LIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RE-SECURED P1 DRAIN PLUG THAT WAS LOOSE. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 39,921 hrs · 13,741 cycles
CLO - INFLIGHT LIM-MIA. CREW REPORTED WEATHER RADAR FAILED. EMERGENCY DECLARED FLIGHT DIVERTED CLO LANDED WITHOUT INCIDENT. WEATHER RADAR PLACARD PER MEL. REPLACED WEATHER RADAR CONTROL PANEL AT DFW ON 07/24/2011. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,185 hrs · 13,111 cycles
OVERHEAD BIN EMERGENCY LIGHT AT SEAT 25D INOP. RELAMPED OVERHEAD BIN EMERGENCY LIGHT AT SEAT 25D. OPS CHECK GOOD.
2010
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,496 hrs · 12,162 cycles
FLOORBEAM CRACKED AT STATION 700 LEFT BUTTLINE 48. REPAIRED PER WORKCARD 53-98-01 AND SRM 53-00-51-2R 3.
Part: PANEL — CORRODED (TE FLAP) · corrosion level 2 · airframe 35,496 hrs · 12,162 cycles
TEMPORARY REPAIR DOUBLER ON TOP INBOARD PANEL ON FORWARD INBOARD PANEL. REMOVED OLD DOUBLER AND REPAIRED AREA PER EA NUMBER B575-57-009242 REV B DATED 2-25-10.
Part: PANEL — CORRODED (TE FLAP) · corrosion level 2 · airframe 35,496 hrs · 12,162 cycles
PREVIOUSLY BLENDED AREA ON TOP INBOARD PANEL ALONG ROW OF RIVETS AFT EDGE. INSTALLED DOUBLER PER EA B757-57-009242 DATED 2/25/10.
Part: PANEL — CORRODED (TE FLAP) · corrosion level 2 · airframe 35,496 hrs · 12,162 cycles
SEVERAL AREAS OF CORROSION ON TOP INBOARD PANEL AT RIVET HEADS ALONG PANEL LEADING EDGE AND RIB LOCATED 18 INCHES FROM INBOARD. INSTALLED DOUBLER PER EA B 757-57-009242 REV B.
Part: SKIN — CRACKED (LE SLAT) · airframe 35,496 hrs · 12,162 cycles
THE NUMBER 8 SLAT BESIDE COVE SKIN IS CRACKED AT THE INBOARD DRIVE TRACK FITTING AREA. INSTALLED EXTERNAL DOUBLER ON NUMBER 8 SLAT INBOARD COVE SKIN PER 57-43-00-04.
Part: SLAT TRACK — GOUGED (EL SLAT) · airframe 35,496 hrs · 12,162 cycles
GOUGE ON INSIDE OF NUMBER 8 SLAT TRACK. INSTALLED DOUBLER ON NUMBER 8 SLAT TRAILING EDGE WEDGE INBOARD TRACK AREA PER SRM 51-70-10-2R.
Part: SKIN — CRACKED (LE SLAT) · airframe 35,496 hrs · 12,162 cycles
CRACK AT NUMBER 8 SLAT PANEL BOTTOM OF INBOARD SLAT TRACK. INSTALLED EXTERNAL DOUBLER ON NUMBER 8 SLAT INBOARD COVE SKIN PER 57-43-00-04.
Part: PAN — GOUGED (L1 DOOR) · airframe 35,496 hrs · 12,162 cycles
LEFT NUMBER 1 DOOR HANDLE PAN WORN. REMOVED AND REPLACED LEFT NUMBER 1 DOOR OUTER HANDLE PAN PER ESO90283.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,973 hrs · 11,966 cycles
EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR EMERGENCY EXIT SIGN HAS MULTIPLE LIGHTS INOPERATIVE. RELAMPED 6 EACH LAMPS IN RIGHT NUMBER FOUR EMERGENCY EXIT SIGN.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 34,973 hrs · 11,966 cycles
COCKPIT EMERGENCY LIGHT INOPERATIVE. RELAMPED COCKPIT EMERGENCY LIGHT.
Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 34,835 hrs · 11,912 cycles
EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. FOUND WIRE BROKEN AT SEAT CONNECTOR. REPINNED CONNECTOR AT SEAT 27D.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 34,835 hrs · 11,912 cycles
EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPLACED LAMP.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 34,835 hrs · 11,912 cycles
SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS ARE DIM. REPLACED BATTERY PACK.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 34,835 hrs · 11,912 cycles
EXTERNAL EMERGENCY LIGHT AT RIGHT NR 1 DOOR INOPERATIVE. REPLACED LAMP.
Part: WINDOW — DELAMINATED (CABIN) · airframe 34,641 hrs · 11,843 cycles
SHORTLY BEFORE LEVEL OFF AT FLIGHT LEVEL 380 THE RIGHT CABIN WINDOW AT SEAT ROW 12 DELAMINATED. DESCENDED TO LOWER ALTITUDE. LANDED MIA WITHOUT INCIDENT. REPLACED WINDOW.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 32,856 hrs
MIA - EMERGENCY LIGHT AT ROW 27 INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 27D.
Part: SKIN — DAMAGED (TE FLAP) · airframe 32,089 hrs · 10,947 cycles
FLAP SKIN HAS DAMAGE. REPAIRED IAW EA B757-57-005192.
2008
Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,772 hrs
DFW - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT DOOR FORWARD HATCH HANDLE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT DOOR FORWARD HATCH HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — WORN (CABIN)
DFW - EMERGENCY LIGHT AT FLIGHT DECK ENTRY AREA EXIT SIGN DOUBLE ARROW LENS HAD WRITING WORN OFF. REPLACED LENS FOR EMERGENCY LIGHT AT FLIGHT DECK ENTRY AREA EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)
SFO - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. REPAIRED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: CONNECTOR — FIRE (COCKPIT)
MIA INFLIGHT T2274/11 MAR CAPTAINS SLIDING WINDOW HEAT CONNECTORS CAUGHT ON FIRE AND MELTED CONNECTIONS. WINDOW HEAT WAS SHUT OFF AND FLAMES STOPPED. LANDED MIA WITHOUT INCIDENT. REPLACED CAPTAINS SLIDING WINDOW AND HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)
MIA AFT EMERGENCY PATH LIGHT AT ROW 25 INOPERATIVE. REPLACED BATTERY FOR AFT EMERGENCY PATH LIGHT FOR ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
MIA EMERGENCY PATH LIGHT AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK OR FIRST CLASS EMERGENCY PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: SPRING — DAMAGED (GIRT BAR)
JFK - DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT SPRINGS NEEDING REPLACED. REPLACED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: LIGHT — INOPERATIVE (CABIN)
DFW - A FLOOR MOUNTED EMERGENCY LIGHT IN MID GALLEY INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)
2001
Part: LIGHT — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY ESCAPE PATH LIGHTS LAST ROW INOPERATIVE. REPLACED LIGHTS TO FIRST CLASS, LAST ROW EMERGENCY ESCAPE PATH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FUEL CONTROL — DEFECTIVE (RT ENGINE)
LAX - FLT 207 - EN ROUTE MIA-LAX, RIGHT ENGINE STAGNATION AT 35,000 FT FUEL FLOW 1.5 TO 1.7 MAX EGT 400. UNABLE TO CONTROL EPR OR FUEL FLOW WITH THROTTLE MOVEMENT. LANDED LAX WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL FLOW GOVERNOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: WIRE — DAMAGED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS BETWEEN ROW 1 AND ROW 3 INOPERATIVE. REPAIRED WIRE BETWEEN ROW 1 AND ROW 3. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - FLT DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 2R DOOR INOPERATIVE. SECURED LOOSE CONNECTOR AT 2R DOOR PATCH STRIP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: WIRE — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AISLE EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 12-18D INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION.. (M)
Part: CONNECTOR — BROKEN (CABIN)
BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS SECTION INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT MID GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — FAILED (ROWS 18-26)
DFW - FLIGHT CREW FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE BETWEEN SEAT ROWS 18 AND 26. REPAIRED WIRE SPLICE AT SEAT ROW 22. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)