N388AA
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.
175 reports on file, 1995-04-15 – 2021-01-13.
Part: SKIN — DENTED (RUDDER) · airframe 99,028 hrs · 16,218 cycles
DURING MAINTENENCE INSPECTION FOUND A DENT ON RUDDER SKIN LEFT SIDE BETWEEN RUDDER STA 165 TO 181, 43" FROM RUDDER AFT EDGE.
Part: SKIN — DAMAGED (ZONE 100) · airframe 99,028 hrs · 16,218 cycles
DURING MAINTENENCE INSPECTION FOUND EXISTING BLENDOUT, NICKS, GOUGES AND SCRATCHES ON FUSELAGE SKIN, AFT CARGO DOOR CUTOUT, LOWER FWD CORNER.
Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 99,028 hrs · 16,218 cycles
DURING MAINTENENCE INSPECTION FOUND A CRACK ON THE EXTERNAL SKIN OF ENGINE NR 1 OUTBOARD CORE COWL, AFT EDGE SKIN, AT 10 O'CLOCK.
Part: SKIN — DEBONDED (HORIZONTAL STAB) · airframe 99,028 hrs · 16,218 cycles
THE INNER ALUMINUM SKIN FOUND DISBONDED AND SEPARATED FROM THE ALUMINUM HONEYCOMB CORE PANEL AT STAB STA 107.927 AUX SPAR STA 127.465.
Part: INLET — DENTED (NR 2) · airframe 99,028 hrs · 16,218 cycles
DURING MAINTENENCE INSPECTION FOUND A DENT WITH CREASE AT ENGINE NR 2 INLET COWL INNER BARREL.
Part: SKIN — DAMAGED (FWD CARGO) · airframe 99,028 hrs · 16,218 cycles
DURING MAINTENENCE INSPECTION FOUND EXISTING BLENDOUT, NICKS, GOUGES AND SCRATCHES ON FWD CARGO DOOR AFT CUTOUT.
Part: SKIN — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 99,028 hrs · 16,218 cycles
DURING MAINTENENCE INSPECTION FOUND CORROSION DAMAGE ON RT WING TRAILING EDGE INBOARD FLAP, REAR SPAR, UPPER CHORD, IFS 166.0.
Part: SKIN — DAMAGED (ZONE 100) · airframe 99,028 hrs · 16,218 cycles
DURING MAINTENENCE INSPECTION FOUND ON FUSELAGE SKIN, STA 1345 TO STA 1395, STR 24R TO STR 29R EXISTING BLENDOUTS, NICKS, GOUGES AND SCRATCHES.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,028 hrs · 16,218 cycles
DURING MAINTENENCE INSPECTION FOUND CORROSION ON THE UPPER SKIN OF CENTER WING, STA 955, RBL 85.0.
Earlier reports · 1995–2020 · 166 reports
2020
Part: CHILLER — ODOR (GALLEY) · airframe 98,968 hrs · 16,202 cycles
AIRCRAFT WAS GROUNDED: VERY BAD ODOR COMING FROM THE MID GALLEY CHILLER. REMOVED AND REPLACED CHILLER IAW AMM 25-33-05.
Part: COFFEEMAKER — ODOR (FWD GALLEY) · airframe 98,849 hrs · 16,168 cycles
AIRCRAFT NOT GROUNDED: ELECTRICAL BURNING ODER EMITTING FROM ONE OF THE FORWARD GALLEY COFFEE MAKERS ODER DISSIPATED AFTER COFFEE MAKERS TURNED OFF
2019
Part: FLASHLIGHT — FAULTY (MID GALLEY) · airframe 98,214 hrs · 16,015 cycles
AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT MID GALLEY LEFT HAND, AFT FLIGHT ATTENDANT SEAT NOT WORKING. MAINTENANCE REPLACED FLASHLIGHT PER AMM 25-64-00.
Part: HOUSING — LEAKING (SUMP PUMP) · airframe 98,210 hrs · 16,013 cycles
AIRCRAT WAS GROUNDED: UNWANTED FUEL TRANSFER L-WING TO CENTER TANK, HAPPENED MAINLY WITH FUEL QUANTITY < 35,000LBS AT A RATE OF ABOUT 500 LBS PER HOUR. TRANSFER STOPPED COMPLETELY WITH FUEL < 35,000 LBS. REMOVED AND REPLACED L/F AUTO SUMPING JET PUMP HOUSING ASSY IAW B767 AMM 28-22-06. OPS AND MIGRATION CHECKS PASSED. NO FAULTS NOTED.
Part: ACTUATOR — NO TEST (SLIDE DOOR) · airframe 98,024 hrs · 15,971 cycles
AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS WHILE ACCOMPLISHING JOB CARD 0012, POSTCHECK AIRCRAFT CLOSE UP THE LEFT SIDE SQUIB FAILED FOR OVERWING SLIDE TEST 1. MAINTENANCE REMOVED AND REPLACED LH SLIDE COMPT DOOR LATCH OPENING ACTUATOR IAW AMM 25-61-11. ALL OPS CHCKS NORMAL. RE-ACTIVATED SYSTEM IAW WORK 25-92-03. OK FOR SERVICE.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 97,890 hrs · 15,941 cycles
AIRCRAFT WAS NOT GROUNDED: 3L JUMP SEAT FLASHLIGHT DISCHARGED. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER AMM 25-64-00.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 97,101 hrs · 15,775 cycles
EMERGENCY LIGHT FAILED TO LIGHT FOR 10 MINUTES IAW MAINTANCE CHECK CARD 0357. REPLACED BATTERY PACK AND CHARGER TO CORRECT THE DISCREPANCY.
Part: CHARGER — DISCHARGED (CABIN) · airframe 97,101 hrs · 15,775 cycles
EMERGENCY LIGHT FAILED TO LIGHT FOR 10 MINUTES IAW MAINTANCE CHECK CARD 0357. REPLACED BATTERY PACK AND CHARGER TO CORRECT THE DISCREPANCY.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 97,101 hrs · 15,775 cycles
EMERGENCY LIGHT FAILED TO LIGHT FOR 10 MINUTES IAW MAINTANCE CHECK CARD 0357. REPLACED BATTERY PACK AND CHARGER TO CORRECT THE DISCREPANCY.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 97,101 hrs · 15,775 cycles
EMERGENCY LIGHT FAILED TO LIGHT FOR 10 MINUTES IAW MAINTANCE CHECK CARD 0357. REPLACED BATTERY PACK AND CHARGER TO CORRECT THE DISCREPANCY
Part: BATTERY — DISCHARGED (CABIN) · airframe 97,101 hrs · 15,775 cycles
EMERGENCY LIGHT FAILED TO LIGHT FOR 10 MINUTES IAW MAINTANCE CHECK CARD 0357. REPLACED BATTERY PACK AND CHARGER TO CORRECT THE DISCREPANCY.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 97,101 hrs · 15,775 cycles
EMERGENCY LIGHT FAILED TO LIGHT FOR 10 MINUTES IAW MAINTANCE CHECK CARD 0357. REPLACED BATTERY PACK AND CHARGER TO CORRECT THE DISCREPANCY.
Part: SHIM — CORRODED (FUSELAGE) · airframe 97,100 hrs · 15,775 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHIMS BETWEEN FUSELAGE SKIN AND STRINGER AT BS 1219 AND S37L. REPLACED SHIMS PER SRM 51-10-02-0G.
Part: SHIM — CORRODED (BS 1219) · airframe 97,100 hrs · 15,775 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHIM AT BS 1219 AND S38L. REPLACED SHIM PER SRM 51-10-02-0G.
Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 96,172 hrs · 15,588 cycles
AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS THAT DURING PDC INSPECTION FOUND P1 DOOR SLIDE PRESSURE READING ZERO. REMOVED AND REPLACED THE R1 DOOR SLIDE IAW CARD 12L80025001.
Part: SHUTOFF VALVE — STUCK (LT ENGINE) · airframe 96,004 hrs · 15,542 cycles
PILOT REPORTED A LEFT ENGINE HPSOV MESSAGE AND BLEED LIGHT ILLUMINATED DURING TAKEOFF ROLL, REGAINED PRESSURE WITH THRUST LEVER RETARDED. ICING CONDITIONS PRESENT ENTIRE TIME. DUCT PRESSURE 33 PSI. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE HPSOV DEFECTIVE AND STUCK IN THE OPEN POSITION. REMOVED AND REPLACED LEFT ENGINE HPSOV IAW AMM 36-11-07. ACCOMPLISHED OPERATIONAL TEST OF BLEED AIR SYSTEM IAW AMM 36-11-00 AND ENGINE GROUND TEST IAW AMM 71-00-00-715-066. OPS CHECKED GOOD.
Part: CONTROL UNIT — MALFUNCTIONED (RT ENGINE) · airframe 95,755 hrs · 15,493 cycles
EXPERIENCED MULTIPLE COMPRESSOR STALLS ON THE RIGHT ENGINE WHEN ADVANCING POWER FROM FLIGHT IDLE TO POWER REQUIRED FOR LEVEL FLIGHT, OCCURRED THREE TIMES. MAINTENANCE REPLACED THE RIGHT ENGINE MAIN ENGINE CONTROL IAW SIC 73-94-02 AND CIT SENSOR IAW AMM 73-21-02. MAINTENANCE ALSO PERFORMED A SATISFACTORY OPERATIONAL CHECK.
Part: SENSOR — MALFUNCTIONED (ENGINE CIT) · airframe 95,755 hrs · 15,493 cycles
RT ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS, WHEN ADVANCING POWER FROM FLIGHT IDLE TO POWER, OCCURRED THREE TIMES. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE RIGHT ENGINE, ENGINE CONTROL IAW SIC 73-94-02 AND CIT SENSOR IAW AMM 73-21-02. MAINTENANCE ALSO PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: WIRE HARNESS — BURNED (GALLEY) · airframe 95,755 hrs · 15,493 cycles
FOUND A WIRE HARNESS BURNED. MAINTENANCE REPLACED BOTH SECTIONS IAW WDM 23-32-43.
2018
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 95,552 hrs · 15,453 cycles
EMERGENCY FLASHLIGHT BY SEAT AT DOOR L1 INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE BATTERY . OPS CHECKED OK.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 95,552 hrs · 15,453 cycles
EMERGENCY FLASHLIGHT AT THE FORWARD GALLEY FLIGHT ATTENDANT SEAT WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE BATTERY. OPS OK.
Part: O-RING — LEAKING (FUEL CAP) · airframe 95,363 hrs · 15,417 cycles
APPROXIMATELY ONE HOUR INTO FLIGHT, SUSPECTED FUEL LEAK FROM THE LEFT OVERWING FUELING CAP. DECLARED AN EMERGENCY AND DIVERTED WITHOUT FURTHER INCIDENT. REPLACED THE FUEL CAP O-RING IAW AMM 28-11-04-004-001 REPLACED THE CAP, LEAK CHECKED OK.
Part: OUTFLOW VALVE — FAULTED (CABIN PRESSURE) · airframe 95,197 hrs · 15,375 cycles
DURING CLIMB OUT THROUGH 8000 TO 9000 FEET, HEARD A LOUD THUD AND AIRFLOW NOISE. AT APPROXIMATELY 13000 FEET, CABIN ALTITUDE EICAS MESSAGE DISPLAYED, FOLLOWED QRC & QRH. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT FUTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND OVERBOARD EXHAUST VALVE INADVERTENTLY DEACTIVATED IN OPEN POSITION. COMPLIED WITH AMM 21-00-00-049-047, DDG PROCEDURE 2 FOR OVERBOARD EXHAUST VALVE DEACTIVATION IN CLOSED POSITION. COMLIED WITH CABIN PRESSURE LEAKAGE TEST IAW AMM 05-51-24-782-001, LEAK RATE WELL WITHIN LIMITS.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 94,018 hrs · 15,152 cycles
AIRCRAFT IN BASE MAINTENANCE: AFT CENTER FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT FLASHED RED ON TEST (LEFTSIDE CENTER GALLEY). REPLACED BATTERIES/BATTERY PACK FOR FLASHLIGHT AT FLIGHT ATTENDANT SEAT AFT CENTER LEFT.
Part: HANDLE — BROKEN (L4 DOOR) · airframe 93,980 hrs · 15,143 cycles
AIRCRAFT WAS NOT GROUNDED: DOOR 4L ASSIST HANDLE BROKE OFF. MAINTENANCE INSTALLED DOOR 4L ASSIST HANDLE PER AMM 20-11-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 93,975 hrs · 15,141 cycles
DURING FLIGHT, CABIN AND PRESSURE CONTROL INOPERATIVE, 1 AND 2. THE OXYGEN MASKS DEPLOYED BUT WERE NOT NEEDED. FLIGHT DESCENDED TO FL 100 AS A PRECAUTION. EMERGENCY DECLARED AND DIVERETED. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 1 AUTO CABIN PRESSURE CONTROLLER IAW MM 21-31-02.
Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 93,975 hrs · 15,141 cycles
DURING FLIGHT, CABIN AND PRESSURE CONTROL INOPERATIVE 1 AND 2. THE OXYGEN MASKS DEPLOYED BUT WERE NOT NEEDED. FLIGHT DESCENDED TO FL 100 AS PRECAUTION. EMERGENCY DECLARED AND DIVERTED. THE AIRCRAFT WAS GROUNDED. REPLACED CABIN PRESSURE OUTFLOW VALVE ACTUATOR IAW AMM 21-31-04.
Part: SELECTOR — FAULTY (CABIN PRESSURE) · airframe 93,975 hrs · 15,141 cycles
DURING FLIGHT, CABIN AND PRESSURE CONTROL INOPERATIVE 1 AND 2. THE OXYGEN MASKS DEPLOYED BUT WERE NOT NEEDED. FLIGHT DESCENDED TO FL 100 AS PRECAUTION. EMERGENCY DECLARED AND DIVERTED REPLACED CABIN PRESSURE SELECTOR IAW MM 21-31-01.
Part: BATTERY PACK — NO TEST (FLASHLIGHT) · airframe 93,422 hrs · 15,043 cycles
FLIGHT ATTENDANT JUMPSEAT OPPOSITE M2 LAVATORY FLASHLIGHT FAILED TO TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW MM 25-64-00. OPS CHECKED OK.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 93,422 hrs · 15,043 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT AFT CABIN RIGHT HAND SIDE FAILS TEST. REPLACED AFT RIGHT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT BATTERY PER MM 25-64-00.
Part: FLASHLIGHT — NO TEST (FWD CABIN) · airframe 93,422 hrs · 15,043 cycles
FIRST CLASS RIGHT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT FAILED TO TEST. REPLACED THE FLASHLIGHT IAW MM 25-64-00.
Part: BATTERY — NO TEST (FWD FLASHLIGHT) · airframe 93,422 hrs · 15,043 cycles
FLIGHT ATTENDANT FLASHLIGHT IN FIRST CLASS, LEFT JUMPSEAT FAILED TO TEST. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY IAW MM 25-64-00, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 93,128 hrs · 14,987 cycles
EMERGENCY LIGHTS INOPERATIVE FROM SEAT 32AB TO 41AB. REPLACED THE CHARGER CHA5031 IAW 33-51-07.
Part: STRINGER — CORRODED · corrosion level 2 · airframe 92,992 hrs · 14,950 cycles
CORROSION FOUND ON STRINGER 4R. REPAIRED THE STRINGER IAW SRM 51-70-11 AND EA 279011.
Part: UNKNOWN — FAULTY (EMERGENCY LIGHTS) · airframe 92,991 hrs · 14,950 cycles
EMERGENCY LIGHTS TURNED ON WHEN FLIGHT DECK SWITCH IS ARMED. AFTER ARMING OVERWING SLIDES, CHECKED EMERGENCY LIGHTS WITH FLIGHT DECK SWITCH. CHECKED GOOD IAW AMM 33-51-00.
Part: FITTING — CORRODED (CARGO DOOR) · airframe 92,992 hrs · 14,950 cycles
NR 3 FORWARD CARGO DOOR LATCH PIN RUSTED. REMOVED AND REPLACED THE DOOR LATCH PIN FITTING IAW AMM 52-33-00-825.
Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 92,992 hrs · 14,950 cycles
CORROSION FOUND ON TOP OF FLOORBEAM AT RBL 47 - 52. REPAIRED THE FLOORBEAM IAW SRM 53-00-51-2R-5, AND EA 278089.
Part: SEAT TRACK — CORRODED (BS 1416) · corrosion level 2 · airframe 92,992 hrs · 14,950 cycles
CORROSION FOUND ON THE SEAT TRACK AT BS 1416. REPAIRED THE SEAT TRACK IAW SRM 53-00-52.
Part: FLOORBEAM — CORRODED (BS 325) · corrosion level 2 · airframe 92,992 hrs · 14,950 cycles
CORROSION FOUND ON THE FLOORBEAM, BS 325, BL 0 TO LBL 54. REPAIRED THE FLOORBEAM IAW SRM 53-00-51-2R-1.
Part: SKIN — CORRODED (BS 1197) · airframe 92,992 hrs · 14,950 cycles
CORROSION ON INTERNAL FUSELAGE SKIN AT BS 1197 BETWEEN STRINGER 39L AND 39R, AFT SIDE OF ANTENNA MOUNT. REPAIRED THE FUSEALGE SKIN IAW EA 277870.
Part: FLOORBEAM — CORRODED (BS 347) · corrosion level 2 · airframe 92,992 hrs · 14,950 cycles
CORROSION FOUND ON THE LOWER SURFACE OF THE FORWARD FLANGE AROUND NUT CLIP HOLES OF THE FLOORBEAM AT BS 347, BETWEEN RBL 26 AND RBL 42. REPAIRED THE FLOORBEAM IAW SRM 53-00-51-2R-1.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,992 hrs · 14,950 cycles
ALL THE OVERHEAD EXIT SIGNS IN COACH ARE NOT WORKING. REPLACED THE BATTERY PACKS.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 92,992 hrs · 14,950 cycles
EMERGENCY LIGHTS ON THE SIDE OF SEATS 32H THROUGH 41H ARE NOT WORKING. REPLACED THE BATTERY PACKS.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 92,992 hrs · 14,950 cycles
THE EMERGENCY LIGHTS ON THE SIDE OF SEATS OF 20H WAS NOT WORKING. REPLACED BATTERY AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,992 hrs · 14,950 cycles
THE EMERGENCY LIGHTS ON THE SIDE OF SEATS AT ROWS 20AB - 24AB WERE NOT WORKING. REPLACED THE BATTERY PACK AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,992 hrs · 14,950 cycles
THE OVERHEAD EXIT SIGN AT THE FRONT OF THE LEFT ROW IN FIRST CLASS IS NOT WORKING. REPLACED ALL THE BATTERY PACKS.
2017
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,992 hrs · 14,950 cycles
THE EMERGENCY LIGHT ON THE SIDE OF SEAT 21H IS NOT WORKING. REPLACED THE BATTERY PACKS IAW AMM 33-51-00.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,992 hrs · 14,950 cycles
EMERGENCY LIGHTS ON THE SIDE OF SEATS 32AB THROUGH 41AB ARE NOT WORKING. REPLACED ALL THE BATTERY PACKS IAW AMM 33-51-00.
Part: FLASHLIGHT — INOPERATIVE (MID CABIN) · airframe 92,831 hrs · 14,915 cycles
AFT MID CABIN FLIGHT ATTENDANT ON LEFT SIDE HAS AN INOPERATIVE EMERGENCY FLASHLIGHT. REPLACED THE FLASHLIGHT IN MID GALLEY IAW AMM 25-60-00.
Part: COMPUTER — FAULTY (ZONE 200) · airframe 92,707 hrs · 14,893 cycles
AIRCRAFT WAS GROUNDED: AFTER TAKEOFF, RECEIVED ELEVATOR FEEL STATUS MESSAGE. RETURNED TO JFK PER TECHNICIAN. REPLACED ELEVATOR FEEL COMPUTER PER AMM 27-31-19 AND SUCCESSFULLY COMPLETED ALL OPERATIONS AND LEAKS CHECKS.
Part: HANDLE — LACK OF LUBE (ZONE 800) · airframe 92,526 hrs · 14,863 cycles
THE AIRCRAFT WAS NOT GROUNDED. LEFT FORWARD ENTRY DOOR COULD NOT BE OPENED FROM THE OUTSIDE UPON ARRIVAL INTO DFW. LUBRICATED HANDLE AND DOOR TRACK. OPS CHECK NORMAL. OK FOR SERVICE.
Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 92,470 hrs · 14,853 cycles
AIRCRAFT WAS NOT GROUNDED. COCKPIT PORTABLE EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: WARNING MESSAGE — FALSE INDICATION (STANDY INVERTER) · airframe 92,197 hrs · 14,804 cycles
STANDBY INVERTER STATUS MESSAGE. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. LANDING UNEVENTFUL. MAINTENANCE COULD NOT DUPLICATE FAULT MESSAGE. REMOVED AND REPLACED STATIC INVERTER AS PRECAUTION IAW AMM 24-33-03. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: LENS — LOOSE (EXIT SIGN) · airframe 91,736 hrs · 14,714 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN BY SEAT 21 RIGHT HAS A LOOSE LENS COVER. RESECURED LENS COVER. OPERATIONAL CHECK GOOD.
Part: LENS — MISSING (CABIN) · airframe 91,513 hrs · 14,667 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 33B HAS A MISSING LENS COVER. REPLACED LENS COVER PER AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: LENS — DETACHED (ZONE 200 - FUSE) · airframe 91,188 hrs · 14,608 cycles
EMERGENCY EXIT LIGHT BY SEAT 20A HAS A DETACHED LENS. SECURED THE LENS IAW AMM 33-51-01. OPS CHECKED GOOD.
Part: WASTE TANK — BLOCKED (ZONE 100 - FUSE) · airframe 91,002 hrs · 14,577 cycles
EMERGENCY DECLARED. FLIGHT DIVERTED DUE TO 4 OF 6 LAVATORIES READING FULL. LANDING UNEVENTFUL. ACCOMPLISHED LAVATORY LEVEL SENSOR AND CONTROLLER RESET IAW AMM 38-33-00. ISSUE REPEATED ON LAVATORIES FS3, M2, AND A5 FIVE HOURS INTO CONTINUED FLIGHT. REMOVED FORWARD WASTE TANK BLOCKAGE. OPERATIONAL CHECK IAW AMM 38-32-00 GOOD. AIRCRAFT WAS GROUNDED.
Part: SIGN — UNSECURE (EMERGENCY LIGHT) · airframe 90,790 hrs · 14,534 cycles
EMERGENCY EXIT ARROW SIGN ON THE LOWER LAVATORY HAS PROTRUDING METAL. SECURED THE SIGN. OPERATIONAL CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 90,719 hrs · 14,518 cycles
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MID GALLEY FORWARD LEFT SEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,992 hrs · 14,950 cycles
THE EMERGENCY LIGHTS ON THE SIDE OF THE SEATS 2AB THROUGH 5AB ARE NOT WORKING. ALL THE BATTERY PACKS WERE REPLACED.
2016
Part: LENS — MISSING (EXIT SIGN) · airframe 89,109 hrs · 14,201 cycles
AIRCRAFT NOT GROUNDED. EMERGENCY EXIT SIGN LENS COVER MISSING AT SEAT 21AB. RE-ATTACHED LENS COVER IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 88,214 hrs · 14,047 cycles
DURING CRUISE, RIGHT HYDRAULIC QUANTITIY STATUS MESSAGE DISPLAYED. QUANTITY DROPPED TO ZERO, RIGHT PRIMARY HYDRAULIC PUMP WARNING ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND LEAK AT RIGHT PUMP FILTER MODULE. REMOVED AND REPLACED MODULE IAW AMM 29-11-17. DURING TAXI OUT FOR NEXT FLIGHT EVENT REPEATED. MAINTENANCE FOUND RIGHT HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED PUMP IAW AMM 29-11-05.
Part: MODULE — LEAKING (HYD SYSTEM) · airframe 88,214 hrs · 14,047 cycles
DURING CRUISE RIGHT HYDRAULIC QUANTITIY STATUS MESSAGE DISPLAYED. QUANTITY DROPPED TO ZERO, RIGHT PRIMARY HYDRAULIC PUMP WARNING ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND LEAK AT RIGHT PUMP FILTER MODULE. REMOVED AND REPLACED MODULE IAW AMM 29-11-17. DURING TAXI OUT FOR NEXT FLIGHT EVENT REPEATED. MAINTENANCE FOUND RIGHT HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED PUMP IAW AMM 29-11-05.
Part: BATTERY — DISCHARGED (CABIN) · airframe 87,478 hrs · 13,900 cycles
AIRCRAFT WAS IN BASE MX. R1 DOOR EMER SLIDE LIGHT IS INOPERATIVE. R & R BATTERY ASSEMBLY IAW AMM 33-51-00.
Part: PIN — NOT SEATED (CABIN) · airframe 87,478 hrs · 13,900 cycles
AIRCRAFT WAS IN BASE MX. RED EMER LIGHT ON RT DIVIDER FWD OF SEAT 20H IS INOPERATIVE. FOUND A PIN IN THE CONNECTOR BEHIND THE DIVIDER PUSHED BACK. RE-SEATED PIN IAW SWPM 20-42-01. OPERATIONAL CHECKED GOOD IAW AMM 33-60-98.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 87,462 hrs · 13,897 cycles
AIRCRAFT WAS NOT GNDED. MID CABIN LT SIDE EMER FLASHLIGHT IS INOPERATIVE. R & R FLASHLIGHT BATTERY IAW AMM 25-20-01. OPERATIONAL CHECK NORMAL.
2015
Part: MOTOR — FAILED (RECIRC FAN) · airframe 85,895 hrs · 13,608 cycles
AT GATE, SUDDEN ELEC SMELL THROUGHOUT ACFT CABIN & RT RECIRCULATION FAN INOPERATIVE LIGHT ILLUMINATED. SMELL STOPPED WITH RT RECIRCULATION FAN TURNED OFF. INSPECTED FAN & CONFIRMED FAULTY MOTOR. DEACTIVATED FAN. R & R RT RECIRCULATION FAN IAW AMM 21-25-01. OPERATIONAL CHECKED GOOD. NO SMELL NOTED.
Part: WIRE — BROKEN (CABIN) · airframe 85,644 hrs · 13,571 cycles
36B SEAT MOUNTED EMER LIGHT IS INOPERATIVE, DUE TO BROKEN WIRES. R & R SEAT MOUNTED 36B EMER LIGHT ASSEMBLY IAW AMM 33-51-10. OPERATIONS CHECKED NORMAL.
Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 83,235 hrs · 13,202 cycles
AIR INTERRUPT, DIVERTED & AN EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE BOTH AUTO PRESSURIZATION CONTROLLERS FAILED. CREW RESET PRESSURIZATION CONTROLLERS. CABIN PRESS CONTROLLER BITE PROCEDURE ACCOMPLISHED IAW FIM 21-31-00-815-803. SYS CHECKED NORMAL.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,801 hrs · 13,122 cycles
FORWARD CARGO DOOR SILL FAIL SAFE STRAP CORRODED AROUND BOLT HOLES AT FS 568 & RBL 44.4 AT WL 122.86. R & R FAIL SAFE STRAP AT FWD CARGO DOOR SILL IAW AARD 53-34-00-1 & DWG 143T8513.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 82,801 hrs · 13,122 cycles
RIGHT WING UPPER SURFACE SKIN AT FS 936 BY WING STRINGER 3 IS CORRODED. REPAIRED SKIN IAW EA B767-57-037902 DATED 12/22/2014.
2014
Part: SLIDE — BROKEN (CABIN) · airframe 82,801 hrs · 13,122 cycles
RIGHT OVERWING SLIDE HAS GIRT BAR BROKEN LOOSE FROM MOUNTS. REPLACED RT OVERWING SLIDE PACK ASSEMBLY IAW AMM 25-65-01-424-060-001.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 82,801 hrs · 13,122 cycles
FORWARD CARGO COMPARTMENT INTERCOSTAL LOCATED BELOW FWD ROLL OUT STOP AT FS 500 & RBL 10 IS CRACKED. R & R INTERCOSTAL IAW AARD 53-60-53.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 82,306 hrs · 13,041 cycles
FUSELAGE MOUNTED EMER ESCAPE LIGHT FWD OF LT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR FUSELAGE MOUNTED EMER ESCAPE PATH LIGHT FWD OF LT NR 4 DOOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,409 hrs · 12,903 cycles
EMERGENCY LIGHT AT SEAT 21B INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 21B. OPERATIONS CHECKED NORMAL.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 81,409 hrs · 12,903 cycles
LEFT NR 2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED CHARGER & BATTERY PACK M738 FOR LT NR 2 DOOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,409 hrs · 12,903 cycles
RIGHT NR 1 DOORWAY EMER LIGHT INOPERATIVE L288. REPLACED LAMP FOR RT NR 1 DOORWAY EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 81,409 hrs · 12,903 cycles
LEFT FWD EXTERIOR EMER LIGHT ASSEMBLY OVERWING SLIDE EGRESS INOPERATIVE. REPLACED LAMP FOR LT FWD EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,409 hrs · 12,903 cycles
EMERGENCY LIGHT AT SEAT 13H INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 13H. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,409 hrs · 12,903 cycles
AFT GALLEY LT FLOOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR AFT GALLEY LT FLOOR EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 80,936 hrs · 12,830 cycles
LEFT AFT INTERIOR OVERWING LOWER EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT AFT INTERIOR LOWER EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,936 hrs · 12,830 cycles
RIGHT NR 1 DOORWAY EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOORWAY EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,936 hrs · 12,830 cycles
EMERGENCY LIGHT AT SEAT 28H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 28H. OPERATIONS CHECKED NORMAL.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 79,616 hrs · 12,621 cycles
F1 LAVATORY SMOKE DETECTOR FALSE ACTIVATION. CHECKED HEAT STICKER IN F1 LAVATORY TRASH & FOUND OK. PERFORMED OPERATIONAL TEST OF SMOKE DETECTOR IAW AMM 26-13-00.
2013
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 79,151 hrs · 12,551 cycles
LT NR 4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 78,977 hrs · 12,523 cycles
A5 AFT LAVATORY SMOKE DETECTOR ALARM SOUNDED. PERFORMED A5 SMOKE DETECTOR TEST IAW AMM 26-13-00 TESTED OK. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,660 hrs · 12,477 cycles
LT EXTERIOR FS MOUNTED NR 7 EMERGENCY EXIT ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR LT SIDE EXTERIOR FS MOUNTED NR 7 EMERGENCY EXIT ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 78,660 hrs · 12,477 cycles
AFT GALLEY BULKHEAD DIVIDER RT LOWER EXIT MARKER SIGN LIGHT SEGMENT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT SIGN AT AFT BULKHEAD. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,660 hrs · 12,477 cycles
FORWARD OF SEAT 20G LOWER BULKHEAD MOUNTED ESCAPE PATH LIGHT SEGMENTS INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT IN FRONT OF SEAT 20G. OPERATIONS CHECKED NORMAL.
Part: SIGN — LOOSE (CABIN) · airframe 78,660 hrs · 12,477 cycles
INTERIOR RT AFT OVERWING DOOR UPPER EXIT SIGN ASSEMBLY NOT PROPERLY MOUNTED TO SIDEWALL. REATTACHED RT AFT OVERWING DOOR EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,229 hrs · 12,405 cycles
EXTERIOR EMERGENCY LIGHT AT RT OVERWING FWD BETWEEN HATCHES INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,229 hrs · 12,405 cycles
EXTERIOR EMERGENCY FS LIGHT AT LT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 78,160 hrs · 12,389 cycles
EXTERIOR LIGHT BY LT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR LT NR 4 DOOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: PIN — BACKED OUT (LG WARNING) · airframe 76,042 hrs · 12,062 cycles
MIA - CREW REPORTED NOSE AIR TO GROUND DISAGREE EICAS WARNING MESSAGE. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND PIN NUMBER TWO AT D1756J PUSHED BACK. REPOSITIONED AND SECURED PIN NUMBER TWO AT D1756J. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 75,892 hrs · 12,042 cycles
AFT LAVATORY A6 SMOKE DETECTOR ALERTED IN FLIGHT WITH LAVATORY UNOCCUPIED. PERFORMED TEST PER AMM 26-13-00-501 WITH NO FAULTS FOUND.
2012
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,152 hrs · 11,451 cycles
CABIN FLOORBEAM STATION 347 FROM LEFT BUTTLINE 37 TO RIGHT BUTTLINE 44 HAS CORROSION AND WEAR FROM NUT CLIPS. INSTALLED REPAIR STRAP PER EA B767-53-021477.
Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,152 hrs · 11,451 cycles
FAILSAFE STRAP AT LOWER DOOR CUTOUT HAS AREA OF CORROSION AT BOTTOM SIDE AT STATION 591. INSTALLED FREEZE PLUGS PER EA B767-53-021440.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
LIGHTNING STRIKE BETWEEN STRINGERS 3 AND 4 RIGHT FROM STATIONS 1480 TO 1502. ACCOMPLISHED HFEC WITH NO CRACKS INDICATED. REMOVED DAMAGE ON PER EA B767-53-021517.
Part: FRAME — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
CRACK FOUND AT STATION 903.5 LEFT BUTTLINE 88.5. ACCOMPLISHED DOUBLER REPAIR PER ECO C3214.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,152 hrs · 11,451 cycles
STRINGER 39 RIGHT FROM STATIONS 645 TO 665 CORRODED. ACCOMPLISHED SPLICE REPAIR PER SRM 53-30-03-2R REPAIR 1 AND EA B767-53-021409.
Part: SPAR — CRACKED (LT PYLON) · airframe 72,152 hrs · 11,451 cycles
LEFT PYLON STRUT TORQUE BOX FORWARD SPAR WEB HAS A CRACK AT THE CUTOUT FOR THE FEEDER CABLE. ACCOMPLISHED DOUBLER REPAIR PER EA B767-54-021366.
Part: FITTING — GOUGED (SPOILER) · airframe 72,152 hrs · 11,451 cycles
NUMBER 8 SPOILER INBOARD PCA ATTACH LUG IS GOUGED. ROTO-PEENED NUMBER 8 SPOILER INBOARD PCA LUG PER EA COMP-57-021436 AND SRM 51-20-06.
Part: ROLLER TRAY — CRACKED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO F4 ROLLER TRAY CRACKED. REPLACED F4 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO A2 ROLLER TRAY DAMAGED. REPLACED A2 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO D3 ROLLER TRAY DAMAGED. REPLACED D3 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO C2 ROLLER TRAY DAMAGED. REPLACED C2 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO D1 ROLLER TRAY DAMAGED. REPLACED D1 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO F2 ROLLER TRAY DAMAGED. REPLACED F2 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO E4 ROLLER TRAY DAMAGED. REPLACED E4 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO D2 ROLLER TRAY DAMAGED. REPLACED D2 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO A1 ROLLER TRAY DAMAGED. REPLACED A1 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO B2 ROLLER TRAY DAMAGED. REPLACED B2 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO E3 ROLLER TRAY DAMAGED. REPLACED E3 ROLLER TRAY PER SRM 51-40-02.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO C1 ROLLER TRAY DAMAGED. REPLACED C1 ROLLER TRAY PER SRM 51-40-02.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,152 hrs · 11,451 cycles
STRINGER SPLICE FOR STRINGER 39 LEFT AFT OF STATION 1219 CORRODED. INSTALLED STRINGER SPLICE PER EA B767-53-021424.
Part: ROLLER TRAY — DAMAGED (CARGO BAY) · airframe 72,152 hrs · 11,451 cycles
AFT CARGO B3 ROLLER TRAY DAMAGED. REPLACED B3 ROLLER TRAY PER SRM 51-40-02.
Part: FRAME — DAMAGED (RT PYLON) · airframe 72,152 hrs · 11,451 cycles
RIGHT PYLON INBOARD SIDE FRAME CHORD DAMAGED AT UPPER CLIP ATTACH POINT AT STATION 285.45. REPAIR DOUBLER INSTALLED PER AARD 54-52-02.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,152 hrs · 11,451 cycles
J-CAP STATION 1197+132 CORRODED. INSTALLED NEW J-CAP PER SRM 51-40-02.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,152 hrs · 11,451 cycles
J-CAP AT STATION 1175 CORRODED. INSTALLED REPAIR STRAPS AT STATION 1175 PER SRM 53-00-07.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
FORWARD CARGO AREA INTERCOSTAL IN CEILING BETWEEN STATIONS 742 TO 764 RIGHT BUTTLINE 40 CRACKED. INSTALLED NEW SERVICEABLE INTERCOSTAL ANGLE PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
INTERCOSTAL AT STATION 1197 RIGHT BUTTLINE 40 CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
INTERCOSTAL FROM STATIONS 368 TO 390 AT LEFT BUTTLINE 40 CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
INTERCOSTAL ANGLE AT CEILING AREA IN FORWARD CARGO BETWEEN STATIONS 566 TO 588 AT LEFT BUTTLINE 40 HAS 3 EACH CRACKS. REPLACED INTERCOSTAL PER SRM 53-00-07.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
INTERCOSTAL FROM STATIONS 346 TO 368 AT LEFT BUTTLINE 43 CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
FRAME STATIONS 325 TO 347 AT LEFT BUTTLINE 39 CRACKED. REPLACE INTERCOSTAL PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
INTERCOSTAL ANGLE AT CEILING IN AFT CARGO BETWEEN STATIONS 1197.22 TO 1197.44 AT LEFT BUTTLINE 40 CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,152 hrs · 11,451 cycles
J-CAP AT STATION 1197 HAS CORROSION AT RIGHT BUTTLINE 38 BOTTOM SIDE. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-07-2R-4.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
INTERCOSTAL FROM STATIONS 1087 TO 1109 AT RIGHT BUTTLINE 40 CRACKED. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 72,152 hrs · 11,451 cycles
INTERCOSTAL ANGLE AT CEILING AREA IN FORWARD CARGO BETWEEN STATIONS 654.55 TO 654.88 AT LEFT BUTTLINE 40 CRACKED. REPLACED INTERCOSTAL ANGLE PER SRM 53-00-07.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,152 hrs · 11,451 cycles
J-CAP AT STATION 1197 LEFT BUTTLINE 13 CORRODED. ACCOMPLISHED NESTED ANGLE REPAIR PER SRM 53-00-07.
2011
Part: TRANSCEIVER — INOPERATIVE (WEATHER RADAR) · airframe 70,743 hrs · 11,240 cycles
MIA - CREW REPORTED WEATHER RADAR FAILED DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LEVER — OUT OF POSITION (COCKPIT) · airframe 68,701 hrs · 10,915 cycles
MIA - CREW REPORTED LEADING EDGE SLAT DISAGREE ON LANDING. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. FOUND FLAP LEVER SLIGHTLY OUT OF 25 DEGREE DETENT. FSEU ALSO DISPLAYED FLAP LEVER RVDT FAULT. CYCLED FLAP/SLAT SYSTEM AND ALL FAULTS CLEARED. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: VIDEO MONITOR — MALFUNCTIONED (CABIN) · airframe 68,604 hrs · 10,898 cycles
MIA - CREW REPORTED ELECTRICAL ODOR IN CABIN NEAR 2H-J SEATS. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED VIDEO MONITOR IN FRONT OF SEATS 2H-J. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,768 hrs · 10,415 cycles
SEAT 27B EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED SEAT 27B LIGHT ASSEMBLY FOR EGRESS LIGHTS. OPS CHECKED NORMAL.
Part: LIGHT — BROKEN (CABIN) · airframe 64,939 hrs · 10,272 cycles
AISLE FACING EGRESS PATH LIGHT ACROSS FROM LEFT NUMBER LAVATORY BROKEN. REPLACED LIGHT ASSEMBLY FOR EGRESS PATH LIGHT ACROSS FROM LEFT NUMBER 4 LAVATORY. OPS CHECKS NORMAL.
2007
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,093 hrs
SFO - EMERGENCY LIGHT AT LEFT AFT CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AT LEFT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHT AT OVERHEAD COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT OVERHEAD COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHT AT SEAT 38B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 38B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: SOCKET — DEFECTIVE (CABIN)
LAX - EMERGENCY ESCAPE PATH LIGHT AT SEAT 31H INOPERATIVE. REPLACED LIGHT FIXTURE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — BROKEN (EMERGENCY LIGHTS)
LAX - EMERGENCY LIGHT AT LEFT SIDE WALL FORWARD OF SEAT 20B INOPERATIVE. FOUND BROKEN WIRE AT SIDE WALL CONNECTOR. REPLACED PIN ON WIRE CONNECTOR FOR EMERGENCY LIGHT AT LEFT SIDE WALL FORWARD OF SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: LIGHT — LOOSE (CABIN)
MIA - EMERGENCY LIGHT AT RIGHT FOUR DOOR INOPERATIVE. FOUND BAD CONTACT AT LIGHT ASSEMBLY. SECURED CONTACT FOR EMERGENCY LIGHT ASEMBLY AT RIGHT FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (COCKPIT)
DFW - EMERGENCY LIGHT IN COCKPIT OVER COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT IN COCKPIT OVER COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY PACK — DISCHARGED (CABIN)
MIA - LEFT AFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED LEFT AFT OVERWING EMERGENCY EXIT SIGN BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN)
MIA - RIGHT AFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR RIGHT AFT OVERWING EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BRAKE — FAILED (NR 5 MLG)
MAN - DURING ROLLOUT, NR 5 MAIN LANDING GEAR WHEEL DEFAULTED. INSPECTION REVEALED NR 5 BRAKE REACTION PLATE SHEAR PINS FAILED AND CAUSED DAMAGE TO BRAKE AND WHEEL ASSEMBLY, INCLUDING THERMAL RELIEF PLUG CAUSING DEFLATION. REPLACED NR 5 BRAKE AND NR 5 AND NR 6 WHEELS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: LIGHT — INOPERATIVE (CABIN)
MAINTENANCE OBSERVED EMERGENCY LIGHT IN FRONT OF SEAT 21C INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT 34B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 2F INOPERATIVE. REPLACED FORWARD SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: WIRE — DISCONNECTED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22B INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: SLIDE — MALFUNCTIONED (PAX DOOR)
EZE - WHILE ON GROUND, R1 DOOR SLIDE WAS UNSUCCESSFULLY INADVERTENTLY DEPLOYED. INSTALLED SLIDE AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: LIGHT — BROKEN (G4 GALLEY)
DFW - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE G4 GALLEY EMERGENCY EXIT FLOODLIGHT INOPERATIVE. REPLACED RIGHT SIDE G4 GALLEY EMERGENCY EXIT FLOOD LIST. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: SOCKET — DEFECTIVE (ROW 33H)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 33H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 33H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: SWITCH — FAILED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT IN CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONTROL SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: WIRE — BROKEN (CABIN)
LHR - DURING MAINTENANCE, EMERGENCY PATH LIGHT AT SEAT 21B INOPERATIVE. REPLACED EMERGENCY PATH LIGHT CABLE ASSEMBLY AT SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SOCKET — CORRODED (FUSELAGE)
SFO - DURING OVERNIGHT MAINTENANCE, AFT SLIDE GROUND EMERGENCY EXIT LIGHT ON LEFT FUSELAGE WAS INOPERATIVE. CLEANED CORRODED LIGHT SOCKET AND RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
SFO - DURING MAINTENANCE, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 28HJ INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY EXIT LIGHT CONNECTOR PASSENGER SEAT 28HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: FLOOR BEAM — CORRODED (BS 799)
AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE AT THE MAIN CABIN FLOOR BEAM. THE BLEND-OUT EXCEEDS SRM MAX LIMITS. ROTOPEENED AND REFINISHED BLEACHED AREA. FILLED BLENDOUTS WITH BM 5-95 SEALANT AS NECESSARY. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1548. TST: 13,573.08 HOURS. CYCLES: 2,177. (X)
Part: RADAR — FAILED (E/E COMPT)
SCL - FLT 2101 - ON CLIMB-OUT, WX RADAR FAILED ON BOTH SIDES. TESTS STILL SHOWED OK. CIRCUIT BREAKER F2 WAS CYCLED WITH NO RESULT. RETURNED AND LANDED MIA PER MEL. T/S WX RADAR SYSTEM PER MM. REMOVED AND REPLACED WX RADAR ANT AND TRANCIEVER PER MM. SYSTEM OPS CHECKS NORMAL PER MM ON GROUND. NO FAILURES DETECTED. BOTH SIDES CHECK NORMAL. OK FOR SERVICE. AIRCRAFT LMP STATUS UNCHANGED. (M)
Part: WIRE — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 31H INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT CONNECTOR FOR PAX SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: IDG — FAILED (RIGHT)
MIA - FLT 912 - RIGHT GEN DRIVE LIGHT FLICKERED THEN CAME ON STEADY DISCONNECTED IDG IAW PROCEDURES. PLACARDED RIGHT ENG GEN INOP PER MEL 2401 8-501DC-B CHECKED ALL OTHER GEN SERVICING ENTERED IN MIC. REMOVED AND REPLACED RIGHT ENG IDG PER MM, GROUND OPS CHECKED GOOD REMOVED MEL 24-01/8-501DC-B CLEARED MIC SHEET. (M)
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 28H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT AT PAX SEAT 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: GEAR INDICATION — MALFUNCTIONED (LT MLG)
MIA - FLT 26 - ON APPROACH TO MIA DURING NORMAL GEAR EXTENSION, THE LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. PERFORMED ALTERNATE GEAR EXTENSION, LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. PUT ADP TO ON POSITION AND RETURNED ALTERNATE GEAR SWITCH TO OFF POSITION, THIS GAVE A DOWN AND LOCKED INDICATION. LANDED MIA WITHOUT INCIDENT. TROUBLESHOT LANDING GEAR SYSTEM BY SWINGING GEAR SEVERAL TIMES. ALSO, CHECKED ALTERNATE GEAR EXTENSION SYSTEM. PERFORMED LEAK CHECK. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. AIRCRAFT RELEASED FOR SERVICE. (M)
Part: CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 33B FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 33B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1995
Part: WIRE — CHAFED (CABIN)
JFK - DURING OVERNIGHT CHECK, CIRCUIT BREAKER FOR EMERGENCY LIGHTS STANDBY B1-905 POPPING. REPAIRED CHAFED WIRE (L2712L12) AT OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY LIGHT SYSTEM FAILED TEST IN COCKPIT. RESECURED LOOSE CANNON PLUG P1-2068 AT MID CABIN EMERGENCY POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL ASSY — INTERMITTENT (CABIN)
SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHT AT PASSENGER SEAT ROW 40B INTERMITTENT. REPLACED EMERGENCY FLOOR LIGHT AT PASSENGER SEAT ROW 40B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)