N396AN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICAN AIRLINES, INC. (AALA) | Operator | on 2018-05-03 | Operator named in NTSB report |
Accident & incident history
Operated by American Airlines (per NTSB report)
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.
137 reports on file, 1999-06-09 – 2022-01-02.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
EXTERNAL FUSELAGE SKIN, STA 588, STR-33R: DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFECTED AREA.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
PROBLEM DESCRIPTION: SLAT NO 5 AT OSS 389.71: SHOP FOUND DENT AMONG FASTENERS AT THE EDGE OF SLAT LE SKIN ATTACHMENT COMMON TO A RIB. THE REPORTED DAMAGE WAS FOUND SMOOTH WITHOUT SHARP EDGES OR LOOSE FASTENERS.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
THE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE LEFT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR. RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTIFIED IN GROUP 3 AT STA 903.5 PER BOEING SB' 767-53A0209 REV 2' DATED JUNE 07-2013 AS MANDATED BY AD 2012-22-17, AMDT 39-17255, EFFECTIVE DECEMBER 26-2012
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
WORN CORE COWL ALUMINUM HAT FRAME â ENGINE# 1, R/H CORE COWL, HAT FRAME, NAC STA 303.75, UPPER AREA DURING THE MAINTENANCE INSPECTION AT IAI, MAINTENANCE DISCOVERED ON #1 ENGINE, R/H CORE COWL HAT CHANNEL FRAME NAC STA 303.75 UPPER SECTION WITH WORN, DAMAGE CALLED M0099. NO APPROVE DATA WAS FOUND AT SRM 54-42-01 FOR THE AFFECTED AREAS. THE FRAME IS MADE FROM 0.063" THICK CLAD AL 2219-T62.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
PROBLEM DESCRIPTION: ENGINE #2, THRUST REVERSER TRANSLATING COWL, INNER SKIN, P/N CF6-F23G019, S/N R647-129: DURING MAINTENANCE INSPECTION AT IAI A CRACKED DENT WAS FOUND IN THE INNER SKIN OF INBD THRUST REVERSE IN CLOSE PROXIMITY TO AN EXISTING REPAIR OF ENGINE #2. THE DAMAGE CANNOT BE REPAIRED IN ACCORDANCE WITH CMM 78-32-31 REPAIRS 002 AND 003 DUE TO THE DENT AND CRACK BEING WITHIN 7 INCHES OF AN EXISTING REPAIR.
Part: NONE — NONE · corrosion level 2 · airframe 78,189 hrs · 13,186 cycles
R/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 â WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE BOOST PUMP HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE.
Part: TEAR STRAP — CORRODED (BS 544 S1-4R) · corrosion level 2 · airframe 78,189 hrs · 13,186 cycles
TEAR STRAP, INNER SKIN, STA 544, S-1R AND S-4R, DOOR SURROUND ZONE: SHOP DISCOVERED DEEP CORROSION ON TEAR STRAP EDGE COMMON TO S-2R (LAP SPLICE). THE DAMAGED AREA IS LOCATED IN CONVERSION INSTALLATION ZONE.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
. DURING A/C SURVEY AT TLV, MAINTENANCE DISCOVERED EXISTING BLENDOUT AT THE EDGE OF AN EXISTING FLUSH REPAIR CUTOUT LOCATED ON THE FUSELAGE SKIN AT STA 616 BETWEEN S38L AND S39L. THE EXISTING FLUSH REPAIR WAS FOUND TO BE INSTALLED BY THE PRIOR OPERATOR, AMERICAN AIRLINES, IAW B767-300 SRM 53-00-01 REPAIR 6 AS DEFENED IN REF. 3.5. THE EXISTING BLENDOUT WAS EVALUATED PER B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1 AND IT WAS FOUND OUT OF LIMITS IN TWO AREAS. IN ADDITIONAL, BLENDOUT LS LESS THAN 2D FROM QTY 2 FASTENER LOCATION. AS ULTRASONIC THICKNESS INSPECTION OF THE REWORKED AREA WAS ACCOMPLISHED PER B767 NDT MANUAL PART 4, 51-00-10; MINIMUM REMAINING MATâL THICKNESS WAS FOUND TO BE 0.042â. ENGINEERING CONTACTED FLIGHT VEHICLE CONSULTING INC. FOR EVALUATION AND THIS ENGINEERING ORDER ACCOMPLISHES THE APPROVED WORK INSTRUCTIONS. 2. THE REPAIR OUTLINED IN THIS DOCUMENT AFFECTS FATIGUE CRITICAL STRUCTURE AND MAY REQUIRE ADDITIONAL DTA IN ACCORDANCE WITH 14CFR 121.1109 OR 129.109. REFER TO THE ANALYSIS SECTION OF THIS DOCUMENT AND THE ATTACHED APPROVAL FOR ADDITIONAL INFORMATION.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
PROBLEM DESCRIPTION: #2 ENGINE OUTBOARD THRUST REVERSER DAGMAR FAIRING DAMAGE, ASSY IDENT: 683L136613, MODEL NO. TR-CF6-F23G019, S/N R647-129: DURING MAINTENANCE INSPECTION AT IAI, MAINTENANCE DISCOVERED ELONGATED HOLES SUNK RIVETS AND GOUGES ACROSS THE FASTENERS FROM TOP TO BOTTOM BETWEEN 7 TO 9 OâCLOCK, OF #2 ENGINE THRUST REVERSER DAGMAR FAIRING. SOMETIMES THE BLOCKER DOOR LEADING EDGES INTERFACES WITH THE DAGMAR FAIRING ON THE SUPPORT ASEMBLY AND DAMAGES THE DAGMAR FAIRING.
Part: NONE — NONE · corrosion level 2 · airframe 78,189 hrs · 13,186 cycles
FUSELAGE SKIN (SEC 45), STA 999 AND STA 1043, STR-2L AND STR-2R: DURING CONVERSION PROCESS, AIRCRAFT MAINTENANCE WAS REQUIRED TO DEACTIVATE AND REMOVE THE HIGH GAIN SATCOM SYSTEM PER CUSTOMER REQUEST THAT WAS INSTALLED BY THE PREVIOUS OPERATOR. THE LARGE EXTERNAL ANTENNA IS MOUNTED TO AN ADAPTOR PLATE LOCATED BETWEEN AOOROXIMATE STATION 977 AND 1043 AND BETWEEN STRINGERS S2L AND S2R.THE FUSELAGE SKIN PANEL (P/N 145T3110 ASSY) WAS FOUND THE EXISTING ANTENNA CABLE CUT OUT, LOCATED AT APPROXIMATE STA 1038 BETWEEN STR S1L-S1R, WITH A DIAMETR OF 2.00â WAS FOUND WITH CORROSION, THE CUT OUT WAS MADE RECTANGULAR IN ORDER TO REMOVE THE DAMAGE FINAL SIZE OF THE CUT OUT 2.600X2.500 INCH, ADDITIONALY TWO AREA WAS FOUND WITH CORROSION BETWEEN STA 999 AND 1043 AND STR S1R. THE SKIN (P/N 145T3111) IS MANUFACTURED FROM 2024-T3 SKIN MACHINED AND TAPERED, 0.170â THICK AT THE CABLE CUT OUT.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
DENT DAMAGE AND AN EXISTING BLEND-OUT WAS FOUND ON THE LOWER WING SKIN PANEL (P/N 112T4702-1) COMMON TO THE OUTBOARD STRINGER L-9.5 (P/N 767-3421-7) BETWEEN WS 990.2 AND WS 1006. AN EXISTING FREEZEPLUG AND THE OUTBOARD STRINGER L-9.5 HAD BEEN INSTALLED PER SERVICE BULLETIN AP767-57-010 RVISION 6.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
PROBLEM DESCRIPTION: R/H WING LOWER SKIN SURFACE BETWEEN WS.994.7 AND WS.1001.7: SHOP FOUND TOOL MARK AMONG FASTENERS, PAINT STRIPPED AND PERFORMED NDT THICKNESS INSPECTION WAS PERFORMED .
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
EXTERNAL FUSELAGE SKIN, STA 1487, STR-21L & STA 1460, STR-29L-STR-30L: DURING THE MAINTENANCE INSPECTION AT IAI, SCRATCHES WERE FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUTS EXCEED\ THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFECTED AREA.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
EXTERNAL FUSELAGE SKIN, STA 308, STR-33L: DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS THE SRM 51-00-01, AD1, DETAIL II, THE FASTENERS ARE INSIDE THE AFFECTED AREA.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
FAN COWL SUPPORT BEAM LINK, #2 PYLON, P/N 31112522-1 DURING THE MAINTENANCE INSPECTION AT IAI, THE BORES IN THE #2 PYLON FAN COWL SUPPORT BEAM LINK PIN 311T2522-1 WERE FOUND TO BE WORN. THE BORE DIAMETERS WERE FOUND TO BE Ã.8770". THE NOMINAL DIAMETER OF THE BORES IS 0.8757"-0.8750" PER BOEING DWG 311T2522. THE LINK IS MADE FROM 7075-T73 ALUMINUM FORGING PER B767-300 SRM 54-52-90, STRUT ATTACHMENT LINK ID- CF6-80C2 ENGINE.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
NLG SUPPORT STRUCTURE, AFT VERTICAL STIFFENERS, UPPER EDGES, STA 287, L/RBL 13.10 DURING THE MAINTENANCE INSPECTION AT IAI, TWO CRACKS WERE FOUND AT DATUM LOCATIONS WITH 0.6 INCH LENGTH EACH ONE. THERE IS NO APPLICABLE DAMAGE EXISTING. VERTICAL STIFFENERS PIN: 141T2938-4/-6
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
ENGINE # 2, LH CORE COWL, HAT FRAME, NAC STA 303.75, MID LOWER AREA: DURING MAINTENANCE INSOECTION AT IAI, MAINTENANCE DISCOVERED ON #2 ENGINE, LH CORE COWL HAT CHANNEL FRAME NAC STA 303.75 MID LOWER SECTION WITH CRACK AND GOUGE. PLEASE REFER TO FIGURE 2 FOR THE DAMAGE DIMENSIONS AND LOCATIONS. NO APPROVE DATA WAS FOUND AT SRM 54-42-01 FOR THE AFFECTED AREAS. THE FRAME IS MADE FROM 0.063â THICK CLAD AL 2219-T62 AMS4096 AS PER SRM 51-00-04. CORE COWL P/N: 224-1761-513; S/N: 1832001.
Part: NONE — NONE · corrosion level 2 · airframe 78,189 hrs · 13,186 cycles
HORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR â AT RBL10.33 STR U3 TO REAR SPAR: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WAS ACCOMPLISHED. THE SKIN MADE OF 2024-T351 X 0.580 INCH ALUMINUM PLATE PER SRM 55-10-01, IDENT1.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
PROBLEM DESCRIPTION: DURING THE MAINTENANCE INSPECTION FOUND SCRATCHES ON EXTERNAL FUSELAGE SKIN AMONG FASTENERS AREA. - SHOP CLEANED DAMAGED AREA IAW SRM 51-10-02. SHOP REMOVED ONE FASTENER IAW SRM 51-40-02. PERFORMED NDT H.F.E.C. AND BOLT HOLE AND NO CORROSION OR CRACKS WERE FOUND. - NRC M0205-STA 1365 5" BELOW STR 32R. INITIAL SKIN THICKNESS IS 0.205" AND MIN THICKNESS IS 0.203". BLEND OUT SIZE L=1.75, W 1.32. - NRC M0209-CUT OUT AFT CARGO ENTRY STA 1270 BT STR 30R TO 32R. INITIAL SKIN THICKNESS IS 0.205" AND MIN THICKNESS IS 0.203". BLEND OUT SIZE L=9.53, W 2.58. - NRC M0229-CUT OUT AFT CARGO ENTRY STA 1270 2" ABOVE STR 25R INITIAL SKIN THICKNESS IS 0.202" AND MIN THICKNESS IS 0.200". BLEND OUT SIZE L=2.39, W 2.24. - NRC M0232-STA 1347 BT STR 25R TO 26R. INITIAL SKIN THICKNESS IS 0.205" AND MIN THICKNESS IS 0.202". BLEND OUT SIZE L=3.95, W 1.56.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
PROBLEM DESCRIPTION: SLAT NO. 4, OSS 579.05: SHOP FOUND A DENT ADJACENT TO A BULGE IN UPPER LE SKIN OF SLAT NO. 4. THE DAMAGED AREA LOCATED ON A RIB AND STIFFENER. SLAT: P/N 114T4104-203G; S/N 000010.
Part: NONE — NONE · corrosion level 2 · airframe 78,189 hrs · 13,186 cycles
L/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 â WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE BOOST PUMP HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE.
Part: NONE — NONE · corrosion level 2 · airframe 78,189 hrs · 13,186 cycles
HORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR â AT LBL10.83 STR U3 TO U2 AND LBL 11.83 STR U2 TO U1: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE CORROSION WAS REMOVED AS PER SRM 51-20-01.THE SKIN REMAINING MATERIAL THICKNESS WAS ACCOMPLISHED. THE SKIN MADE OF 2024-T351 X 0.580 INCH ALUMINUM PLATE PER SRM 55-10-01, IDENT1.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
ENGINE #1 OUTBD CORE COWL HAT FRAME NAC STA 303.75, LOWER AREA: DURING THE MAINTENANCE INSPECTION AT IAI, CRACK WAS FOUND AT DATUM LOCATION WITH 1.5 INCH LENGTH.
Part: NONE — NONE · airframe 78,189 hrs · 13,186 cycles
THE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE RIGHT SIDE OF B767-300 AIRCRAFT THAT HAVE TYPE III OVER WING EXIT DOOR. RHE REPAIRS ARE DEFINED FOR THE AIRPLANES IDENTIFIED IN GROUP 3 AT STA 903.5 PER BOEING SB' 767-53A0209 REV 2' DATED JUNE 07-2013 AS MANDATED BY AD 2012-22-17, AMDT 39-17255, EFFECTIVE DECEMBER 26-2012
Earlier reports · 1999–2020 · 113 reports
2020
Part: CLUTCH — STICKING (THROTTLE) · airframe 77,958 hrs · 13,125 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT THROTTLE STICKING AUTO AND MANUAL OPERATION DOES NOT KEEP UP WITH RIGHT THROTTLE IN AUTO MODE. REPLACED AUTO THROTTLE CLUTCH PACK PER AMM 22-32-05.
2019
Part: LIGHT — INOPERATIVE (SEAT 7A)
7A SEAT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-10. OPS CHECK GOOD.
Part: ACCESS PANEL — DAMAGED (CABIN FLOOR) · airframe 76,722 hrs · 12,830 cycles
AIRCRAFT WAS GROUNDED: CABIN FLOOR ACCESS PANEL FOR E&E COMPARTMENT BOARD SOFT. REPLACED ACCESS PANEL PER AMM 52-48-05.
Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 75,597 hrs · 12,615 cycles
AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS L1 DOOR SLIDE DOES NOT SHOW NEEDLE SHADOW IN GREEN BAND AND IS OUT OF LIMITS FOR PRESSURE GAUGE ON LOW SIDE. REMOVED AND REPLACED SLIDE ASSY IAW AMM 25-66-01. ALL CHECKS NORMAL.
Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,416 hrs · 12,566 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SUPPORT FITTING AT BS 1570 ON THE LAVATORY DUMP CRANK TOWER. REPLACED SUPPORT FITTING PER SRM 51-40-02.
Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,416 hrs · 12,566 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHEAR TIE AT BS 1562 AND BL 0. REPLACED SHEAR TIE PER SRM 51-10-02-0G
Part: FUEL FILTER — DIRTY (RT ENGINE FUEL) · airframe 74,976 hrs · 12,468 cycles
DURING CLIMB, THE RIGHT ENGINE FUEL FILTER LIGHT ILLUMINATED. REFERRED TO THE QRH, ADVISED TO LAND AS SOON AS POSSIBLE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ACCOMPLISHED MCM 4918. RT FUEL FILTER ELEMENTS REMOVED AND REPLACED. NO STATUS MESSAGE AFTER . ACFT OK FOR SERVICE.
2018
Part: FLASHLIGHT — NO TEST (JUMP SEAT) · airframe 74,018 hrs · 12,231 cycles
EMERGENCY FLASHLIGHTS AT THE FLIGHT ATTENDANTS JUMPSEAT, DID NOT TEST. REPLACED THE FLASHLIGHT AND TESTED GOOD IAW FIM 25-60-05.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 73,943 hrs · 12,212 cycles
MID CABIN, LEFT SIDE ,AFT FLIGHT ATTENDANT SEAT FLASHLIGHT WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLASHLIGHT BATTERY IAW GPM 05-01-07. OPS CHECKED GOOD.
Part: CONTROL PANEL — FAILED (WX RADAR) · airframe 73,749 hrs · 12,174 cycles
WEATHER RADAR FAILED DURING FLIGHT. AN EMERGENCY WAS DECLARED, RETURNED TO DEPARTURE, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED TROUBLESHOOTING IAW FIM 34-43-00, FOUND THE WEATHER RADAR PANEL AND ANTENNA AT FAULT. REPLACED IAW MM 34-43-2 AND MM 34-43-05. TESTED OKAY, NO FAULTS NOTED.
Part: ANTENNA — FAULTED (WX RADAR) · airframe 73,749 hrs · 12,174 cycles
WEATHER RADAR FAILED DURING FLIGHT. ACCOMPLISHED TROUBLESHOOTING IAW FIM 34-43-00, FOUND WEATHER RADAR PANEL AND ANTENNA AT FAULT. AN EMERGENCY WAS DECLARED, RETURNED TO DEPARTURE, AND AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED IAW MM 34-43-2, AND MM 34-43-05. TESTED OKAY, NO FAULTS NOTED.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 73,250 hrs · 12,077 cycles
MID GALLEY LEFT SIDE LOWER ACCESS DOOR DETACHABLE FLASHLIGHT BATTERY INOPERATIVE. REPLACED THE BATTERY. CHECKED NPRMAL.
Part: LIGHT — INOPERATIVE (SEAT 3J) · airframe 72,405 hrs · 11,905 cycles
SEAT 3J MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED 3J SEAT MOUNTED EMERGENCY LIGHT ASSY IAW AMM 33-51-10. OPS CHECKED NORMAL. AIRCRAFT WAS GROUNDED.
Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 71,924 hrs · 11,811 cycles
FLASHLIGHT AT THE JUMPSEAT REAR LEFT FLIGHT COMPARTMENT BATTERY WILL NOT TEST. REPLACED THE BATTERY IAW AMM 25-64-00.
2017
Part: THRESHOLD — LOOSE (LAVATORY DOOR) · airframe 71,672 hrs · 11,765 cycles
FIRST CLASS FORWARD LAVATORY DOOR STICKING AT THRESHOLD BASE. TIGHTENED THRESHOLD SCREWS. CHECKED NORMAL.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,548 hrs · 11,742 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER ON FORWARD SIDE OF FRAME 246 AT LBL26. INSTALLED ANGLE STIFFENER PER SRM 53-10-51-2R3.
Part: STIFFENER — CRACKED (BS 246) · airframe 71,548 hrs · 11,742 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENERS ON STA. 246 AT LEFT BUTTLINE 0 TO LEFT BUTTLINE 4. REPLACED STIFFENERS ON STA. 246 AT LEFT BUTTLINE 0 TO LEFT BUTTLINE 4 PER SRM 53-10-51-2R3.
Part: STIFFENER — CRACKED (BS 246) · airframe 71,548 hrs · 11,742 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER AT STA. 246 LEFT BUTTLINE 2 AND LEFT BUTTLINE 6. REPLACED STIFFENER AT STA. 246 LEFT BUTTLINE 2 AND LEFT BUTTLINE 6 PER SRM 53-10-51-2R3.
Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 70,917 hrs · 11,633 cycles
THE AIRCRAFT WAS NOT GROUNDED. PASSENGER SMOKING IN LAV A5. SMOKE DETECTION SYSTEM DID NOT INDICATE ANY SMOKE. LAV A5 SMOKE DETECTOR OPS CHECK PERF IAW AMM 26-13-00-715-090, TEST OK. THERMAL STICKER IN WASTE BIN CHECKED FOR SIGNS OF HEAT, NIL EVIDENT. A/C OK FOR SERVICE.
Part: PUMP — FAILED (FUEL BOOST) · airframe 70,577 hrs · 11,566 cycles
DURING FLIGHT LEFT FWD BOOST PUMP WOULD NOT WORK AFTER BALANCING FUEL. CIRCUIT BREAKER DISCOVERED TRIPPED. REMOVED AND REPLACED LEFT FWD BOOST PUMP IAW AMM 28-22-03. OPS CHECKED AND LEAK CHECKED GOOD.
Part: LENS — DETACHED (CABIN) · airframe 70,348 hrs · 11,517 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE L1 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER IAW AMM 33-51-03. OPERATIONAL CHECK GOOD.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,324 hrs · 11,509 cycles
EMERGENCY EXIT CEILING LIGHT NEAR SEATS 26G AND 25H HAS A MISSING LENS. REPLACED THE LENS IAW AMM 33-51-04. OPS CHECKED GOOD.
Part: ATTACH ANGLE — CORRODED (LT NOSE COWL) · airframe 70,102 hrs · 11,472 cycles
LEFT ENGINE FAN CASE NOSE COWL ATTACH ANGLE HAS EVIDENCE OF CORROSION AT THE 4 O'CLOCK AND 5'OCLOCK POSITIONS. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT ENGINE IAW MCM 71-93-01, 71-95-22, 71-94-45, 71-94-03, AND 71-94-43. OPERATIONAL CHECK GOOD.
Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 69,785 hrs · 11,410 cycles
SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 22 TO 28HJ FAILED TO TEST. REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY AT M732 IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,785 hrs · 11,410 cycles
SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 22 TO 28HJ FAILED TEST. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY AT M732 IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: CONNECTOR — BROKEN (CABIN) · airframe 69,679 hrs · 11,393 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 39H HAS A BROKEN CONNECTOR. REMOVED AND REPLACED CONNECTOR IAW SWPM 20-64-17. OPERATIONAL CHECK IAW AMM 33-51-00 GOOD.
Part: BPCU — FAULTY (ELECTRICAL SYS) · airframe 68,925 hrs · 11,240 cycles
AIRCRAFT WAS GROUNDED. JFK-ZRH FLIGHT RETURNED TO JFK. OVERWEIGHT LANDING UNEVENTFUL. DURING CRUISE, THE CREW REPORTED ELECTRICAL BUS AND CIRCUIT BREAKER PROBLEMS. REMOVED AND REPLACED THE BUS POWER CONTROL UNIT IAW AMM 24-41-03. OPERATIONAL CHECK GOOD.
Part: LENS — DETACHED (EXIT SIGN) · airframe 68,914 hrs · 11,237 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN MID GALLEY AFTER ROW 17 RIGHT SIDE HAS A DETACHED LENS COVER. RE-ATTACHED LENS COVER. OPERATIONAL CHECK GOOD.
2016
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 68,287 hrs · 11,133 cycles
L1 DOOR EMERGENCY EXIT SIGN NEAR FLOOR HAS DETACHED LENS COVER. REPLACED LENS. OPERATIONAL CHECKED GOOD.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 68,287 hrs · 11,133 cycles
R1 DOOR EMERGENCY EXIT SIGN NEAR FLOOR HAS DETACHED LENS COVER. REPLACED LENS. OPERATIONAL CHECK GOOD.
Part: LENS — DETACHED (EXIT SIGN) · airframe 68,138 hrs · 11,107 cycles
AIRCRAFT NOT GROUNDED. BOTH OVERWING EMERGENCY EXIT SIGN LENS COVERS FELL OFF ON LANDING. REATTACHED BOTH EXIT SIGNS IAW AMM 25-64-00. OPERATIONAL CHECK GOOD. REF AALA20161102002.
Part: LENS — DETACHED (EXIT SIGN) · airframe 68,138 hrs · 11,107 cycles
AIRCRAFT NOT GROUNDED. BOTH OVERWING EMERGENCY EXIT SIGN LENS COVERS FELL OFF ON LANDING. REATTACHED BOTH EXIT SIGNS IAW AMM 25-64-00. OPERATIONAL CHECK GOOD. REF AALA20161102003.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,225 hrs · 10,775 cycles
AIRCRAFT WAS IN BASE MX. LT AFT FLIGHT ATTENDANTS EMER LIGHT & EMER LIGHTS ON SEATS 29B - 41B ARE INOPERATIVE. R & R BATTERY CHARGER M739 & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-07.
Part: MEC — MALFUNCTIONED (RT ENGINE) · airframe 66,144 hrs · 10,756 cycles
DURING TAKEOFF, ACFT EXPERIENCED 3 COMPRESSOR STALLS BELOW 800 FEET ON THE RT ENG WITH LOSS OF POWER. WHEN THE RT ENG THROTTLE WAS REDUCED, THE ENG RAN NORMALLY, NO OTHER INDICATIONS. THE FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. TROUBLE SHOT IAW FIM 71-05-00. ACCOMPLISHED BORESCOPE INSPECTION IAW MCM 71-96-01. REPLACED MEC IAW SIC 73-94-02. ACCOMPLISHED CIT CHECK IAW 73-21-02. ENG OPERATIONS CHECKED GOOD. THE ACFT WAS GNDED.
2015
Part: BATTERY — DISCHARGED (CABIN) · airframe 63,873 hrs · 10,359 cycles
SEAT MOUNTED & CEILING EMER LIGHTS ARE INOPERATIVE FROM SEAT 2A - 6A. R & R EMER LIGHT BATTERY FOR 2A - 6A IAW AMM 33-51-07. ACCOMPLISHED OPERATIONAL CHECKS IAW AMM 33-51-05 & AMM 33-51-04. SYS CHECKED NORMAL.
Part: LIGHT — BROKEN (ZONE 200) · airframe 63,049 hrs · 10,223 cycles
EMERGENCY LIGHT AT FWD GALLEY BROKEN. R & R EMERGENCY LIGHT IAW AMM 33-51-01 WITH GOOD OPERATIONAL CHECK.
Part: LIGHT — BROKEN (GALLEY) · airframe 63,049 hrs · 10,223 cycles
FOUND EMERGENCY LIGHT AT FWD GALLEY BROKEN. R & R FORWARD GALLEY EMERGENCY LIGHT IAW AMM 33-51-01. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,864 hrs · 10,195 cycles
RIGHT FUSELAGE EXTERNAL EMER LIGHT 2ND AFT OF WING BODY FAIRING IS INOPERATIVE. RELAMPED RT FUSELAGE EXTERNAL EMER LIGHT 2ND AFT OF WING BODY FAIRING IAW AMM 33-51-06. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,864 hrs · 10,195 cycles
L1 EXTERNAL EMER LIGHT IS INOPERATIVE. RELAMPED L1 DOOR EXTERNAL EMER LIGHT IAW MM 33-51-06. OPERATIONS CHECKED NORMAL.
Part: BATTERY — DISCHARGED (CABIN) · airframe 62,579 hrs · 10,150 cycles
FORWARD ENTRY DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. CHARGED BATTERY, PERFORMED GOOD FUNCTIONAL CHECK IAW AMM 33-51-902-082 & AMM 33-51-07-612 056. SYS CHECKED NORMAL.
Part: BATTERY — DISCHARGED (CABIN) · airframe 62,579 hrs · 10,150 cycles
RIGHT WING SLIDE GND ILLUMINATION LIGHT L391 INOPERATIVE. CHARGED BATTERY & PERFORMED GOOD FUNCTIONAL CHECK IAW AMM 33-51-06-902-082 & AMM 33-51-07-612-056. SYS CHECKED NORMAL.
Part: FUSE — BLOWN (CABIN) · airframe 62,579 hrs · 10,150 cycles
RIGHT EMER LIGHTS BETWEEN SEATS 7 & 21 INOPERATIVE. R & R F3 FUSE. SYS CHECKED NORMAL.
2014
Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,660 hrs · 9,979 cycles
FUSELAGE CROWN SKIN LIGHTNING STRIKE DAMAGE REPAIR RE-EVALUATION AT FUSELAGE STATION 522 & STRINGER 4 LT. MRT 051854, NON-ROUTINE 2694940. COMPLETED DOUBLER INSTALLATION WITHOUT DEVIATION IAW ENGINEERING AUTHORIZATION B767-53-037240 DATED 11-03-2014.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,660 hrs · 9,979 cycles
AFT CARGO INTERCOSTAL CRACKED AT STATION 1300 BETWEEN CHANNELS 4 & 5. INSTALLED NEW INTERCOSTAL AT STATION 1300 BETWEEN CHANNELS 4 & 5 IAW AARD 53-60-53-1.
Part: LIGHT — BROKEN (EXTERIOR) · airframe 61,660 hrs · 9,979 cycles
EXTERIOR EMER LIGHT FWD OF MAIN AFT CARGO DOOR DID NOT ILLUMINATE DURING TEST. REPLACED BROKEN LAMP. OPERATIONS CHECKED NORMAL.
Part: SKIN — DENTED (FUSELAGE) · airframe 61,660 hrs · 9,979 cycles
DENTS AT FUSELAGE STATION 1197 + 122 WITHIN ADJACENT FRAME STRINGER BAYS, FROM STRINGER 36 RT TO 39 LT. REPAIRED IAW EA B767-53-037232 DATED 11/3/2014.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,861 hrs · 9,709 cycles
SEAT 28H EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 28H EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,861 hrs · 9,709 cycles
LEFT NR 4 DOOR, UPPER AFT EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR UPPER AFT EMERGENCY EXIT SIGN AT LT NR 4 DOOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,861 hrs · 9,709 cycles
RIGHT AFT OVERWING EXIT, LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LOWER EMERGENCY LIGHT AT RT AFT OVERWING EXIT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,861 hrs · 9,709 cycles
RIGHT NR 4 DOOR, UPPER AFT EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR UPPER AFT EMERGENCY EXIT SIGN AT RT NR 4 DOOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,861 hrs · 9,709 cycles
LEFT NR 4 EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED LAMP FOR LT NR 4 EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,861 hrs · 9,709 cycles
LEFT AFT OVERWING EXIT, LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LOWER EMERGENCY LIGHT AT LT OVERWING EXIT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,861 hrs · 9,709 cycles
RIGHT NR 1 DOOR, UPPER FWD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR UPPER FWD EMERGENCY EXIT SIGN AT NR NR 1 DOOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,861 hrs · 9,709 cycles
RIGHT FWD OVERWING EXIT, LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LOWER EMERGENCY LIGHT AT RT OVERWING EXIT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,136 hrs · 9,593 cycles
20AB EMERGENCY EXIT SIGN LOWER LAMPS INOPERATIVE. REPLACED LAMPS FOR 20AB EMERGENCY EXIT SIGN, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,136 hrs · 9,593 cycles
21HJ LOWER EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR 21HJ LOWER EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,136 hrs · 9,593 cycles
LEFT NR 2 DOOR LOWER PORTION OF EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMPS FOR LT NR 2 DOOR LOWER PORTION OF EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,136 hrs · 9,593 cycles
21AB EMERGENCY EXIT SIGN LOWER LAMPS INOPERATIVE. REPLACED LAMPS FOR 21AB EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,136 hrs · 9,593 cycles
RIGHT NR 1 DOOR FWD EMERGENCY LIGHT IN DOOR SILL INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR SILL EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,136 hrs · 9,593 cycles
RIGHT NR 1 DOOR FWD EMERGENCY EXIT LIGHT LOWER PORTION LAMPS INOPERATIVE. REPLACED LAMPS FOR RT NR 1 DOOR LOWER PORTION OF FWD EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 59,136 hrs · 9,593 cycles
20HJ LOWER EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LAMP FOR 20HJ LOWER EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 58,964 hrs · 9,565 cycles
LT NR 2 DOOR UPPER EMERGENCY EXIT SIGN LOWER LIGHT LAMP INOPERATIVE. REPLACED LAMP, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 58,964 hrs · 9,565 cycles
RT NR 2 DOOR UPPER EMERGENCY EXIT LIGHT LAMP INOPERATIVE. REPLACED LAMP, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,569 hrs · 9,492 cycles
LT NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,617 hrs · 9,345 cycles
RT NR 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR RT NR 1 DOOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 57,617 hrs · 9,345 cycles
LT SIDE AFT DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT SIDE AFT DOOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,617 hrs · 9,345 cycles
LT NR 2 DOOR HANDLE LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR HANDLE LIGHT. OPERATIONS CHECKED NORMAL.
Part: CONNECTOR — LOOSE (CABIN) · airframe 57,208 hrs · 9,277 cycles
SEAT 6H EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE CONNECTOR UNDERNEATH THE SEAT. RECONNECTED LOOSE CONNECTOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,910 hrs · 9,085 cycles
EMERGENCY AISLE LIGHT AT RT ROW 20 INOPERATIVE. REPLACED LAMP FOR EMERGENCY AISLE LIGHT AT RT ROW 20. OPS CHECK NORMAL.
Part: PCA — LEAKING (SPOILER) · airframe 55,106 hrs · 8,950 cycles
GYE - INFIGHT LIM-MIA CREW REPORTED CENTER HYDRAULIC SYSTEM FLUID LOSS. EMERGENCY DECLARED FLIGTH DIVERTED GYE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER FOUR SPOILER POWER CONTROL ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
2012
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,278 hrs · 8,820 cycles
LEFT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 54,278 hrs · 8,820 cycles
RIGHT NUMBER 1 DOOR EMERGENCY EXIT SIGN LOWER LIGHTS INOPERATIVE. REPLACED LAMP FOR RIGHT NUBMER 1 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 54,278 hrs · 8,820 cycles
RIGHT NUMBER 2 DOOR EMERGENCY EXIT SIGN LOWER LIGHTS INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 54,278 hrs · 8,820 cycles
LEFT NUMBER 2 DOOR EMERGENCY EXIT SIGN LOWER LIGHTS INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 2 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.
Part: FAN — FAULTY (E&E BAY) · airframe 53,255 hrs · 8,668 cycles
LHR - CREW REPORTED FORWARD EQUIPMENT EXHAUST FAN CAME ON FOLLOWED BY ELECTRICAL BURNING ODOR FOR BRIEF TIME. FLIGHT LANDED LHR WITHOUT INCIDENT. FORWARD EQUIPMENT EXHAUST FAN DEFERRED PER MEL. REPLACED FORWARD EQUIPMENT EXHAUST FAN AT MIA ON 09/11/2012. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,809 hrs · 8,595 cycles
LEFT NUMBER 1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: PROXIMITY SENSOR — FAULTY (LANDING GEAR) · airframe 52,113 hrs · 8,486 cycles
LAX - CREW REPORTED AFTER GEAR HANDLE MOVED TO "DOWN" POSITION AND ALL GREEN GEAR POSITION LIGHTS ILLUMINATED, THE AMBER "DOORS" LIGHT STAYED ILLUMINATED FOLLOWED BY AMBER CAUTION "GEAR DOWN" EICAS MESSAGE. FLIGHT LANDED LAX WITHOUT INCIDENT. REPLACED PROXIMITY BOX. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
LIGHTNING STRIKE TO UPPER FUSELAGE SKIN STATIONS 518 TO 524 AT STRINGERS 3 TO 5 LEFT. REMOVED DAMAGE BY CUTTING OUT A SECTION OF SKIN AND INSTALLED AN EXTERNAL SKIN DOUBLER REPAIR PER SRM 53-00-01 REPAIR 1 AND EA B767-53-020505.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
LIGHTNING STRIKE TO UPPER FUSELAGE SKIN STATIONS 454 TO 4555 5 INCHES BELOW STRINGER 4 LEFT. REMOVED DAMAGE WITH 3/16 HOLE AND PLUGGED WITH SOLID RIVET PER SRM 53-00-01 REPAIR 8 AND EA B767-53-020505.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
LIGHTNING STRIKE TO UPPER FUSELAGE SKIN STATIONS 476 TO 477 2 INCHES BELOW STRINGER 4 LEFT. REMOVED DAMAGE WITH 3/16 HOLE AND PLUGGED WITH SOLID RIVET PER SRM 53-00-01 REPAIR 8 AND EA B767-53-020505.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
LIGHTNING STRIKE TO UPPER FUSELAGE SKIN STATIONS 576 TO 585. REMOVED DAMAGE BY CUTTING OUT A SECTION OF SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR PER SRM 53-00-01 REPAIR 1 AND EA B767-53-020505.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
LIGHTNING STRIKE TO UPPER FUSELAGE SKIN STATION 694, 4 INCHES BELOW STRINGER 2 LEFT. REMOVED DAMAGE WITH 3/16, HOLE AND PLUGGED WITH SOLID RIVET PER SRM 53-00-01 REPAIR 8 AND EA B767-53-020587.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
LIGHTNING STRIKE TO UPPER FUSELAGE SKIN STATION 676, 2 INCHES BELOW STRINGER 2 LEFT. REMOVED DAMAGE BY CUTTING OUT A SECTION OF SKIN AND TEAR STRAP AND INSTALLED AN EXTERNAL SKIN DOUBLER REPAIR PER SRM-00-01 REPAIR 14 AND EA B767-53-020587.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
LIGHTNING STRIKE TO UPPER FUSELAGE SKIN STATIONS 546 TO 552 6 INCHES BELOW STRINGER 3 LEFT. REMOVED DAMAGE BY CUTTING A 1 INCH HOLE AND INSTALLED AN INTERNAL FLUSH REPAIR PER B767 SRM 53-00-01 REPAIR 6 AND EA B767-53-020505.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
LIGHTNING STRIKE TO UPPER FUSELAGE SKIN STATION 665 BETWEEN STRINGERS 2 AND 3 LEFT. REMOVED DAMAGE BY CUTTING A 1 INCH HOLE AND INSTALLED AN INTERNAL FLUSH REPAIR PER SRM 53-00-01 REPAIR 6 AND EA B767-53-020587.
Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
ACCIDENTAL IMPACT TO STATION 610 STRINGER 39 LEFT. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-00-01-2R 6.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,411 hrs · 8,188 cycles
INTERCOSTAL CRACKED FROM STATION 742 TO 764 AT RIGHT BUTTLINE 40. REPLACED INTERCOSTAL PER AARD 53-30-00-1.
Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 48,624 hrs · 7,907 cycles
DURING OVERNIGHT A CHECK INSPECTION, THE RIGHT NUMBER 2 DOOR SLIDE WAS FOUND TO BE UNRAVELLING (LACING COMING LOOSE). REPLACED RIGHT NUMBER 2 DOOR SLIDE.
Part: CONNECTOR — BROKEN (CABIN) · airframe 48,624 hrs · 7,907 cycles
RED EMERGENCY LIGHT AFT OF SEAT 17AB INOPERATIVE. REPLACED A BROKEN CONNECTOR AT SEAT 17AB AREA. OPS CHECK NORMAL.
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 48,100 hrs · 7,825 cycles
CREW REPORTED ON DESCENT F1 LAVATORY SMOKE WARNING. DETECTOR WAS RESET THEN REPEATED ON TAXI IN. REPLACED SMOKE DETECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 46,249 hrs · 7,518 cycles
CDG - CREW REPORTED LAVATORY SMOKE DETECTOR IN LAV FS3 WENT OFF. FLIGHT ATTENDANT RESET DETECTOR AND WORKED NORMAL THE REMINDER OF FLIGHT. NO SMOKE REPORTED IN LAVATORY. SMOKE DETECTOR CAME ON AGAIN AFTER TOUCHDOWN. FLIGHT LANDED CDG WITHOUT INCIDENT. REPLACED LAVATORY FS3 SMOKE DETECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,583 hrs · 7,215 cycles
CORROSION WAS FOUND ON STATION 303 FLOORBEAM AT RIGHT BUTTLINE 20. INSTALLED REPAIR STRAP.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,583 hrs · 7,215 cycles
CORROSION WAS FOUND ON STATION 325 FLOORBEAM BETWEEN LEFT BUTTLINE 17 AND RIGHT BUTTLINE 26. INSTALLED REPAIR STRAP.
Part: FILTER — DIRTY (CABIN) · airframe 43,660 hrs · 7,033 cycles
MIA - FLIGHT ATTENDANTS REPORTED STRONG ELETRICAL SMELL IN CABIN. EMERGENCY DECLARED RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INSPECTED ENGINES AND AUXILIARY POWER UNIT FOR OIL LEAKS AND NONE FOUND. OPERATED ALL GALLEY OVENS NO ABNORMAL ODORS NOTED. ACCOMPLISHED PACK BURN NO SMELL OF SMOKE OR OIL NOTED IN CABIN. REPLACED FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 43,297 hrs · 6,967 cycles
LHR - INFLIGHT FCO-JFK. CREW REPORTED CABIN AUTO INOPERATIVE EICAS MESSAGE. UNABLE TO CONTROL CABIN CLIMB OR DESCENT IN MANUAL MODE DUE TO POSSIBLE LIGHTNING STRIKE. EMERGENCY DECLARED DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CABIN PRESSURE CONTROLLERS AND ACCOMPLISHED LIGHTNING STRIKE CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2009
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,532 hrs · 6,814 cycles
EXTERIOR EMERGENCY EXIT LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP.
2008
Part: HOUSING — BROKEN (CABIN)
MIA - EMERGENCY FLOOD LIGHT AT RIGHT FIRST CLASS GALLEY HAS BROKEN HOUSING ASSEMBLY. REPLACED HOUSING ASSEMBLY FOR EMERGENCY FLOOD LIGHT AT RIGHT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EXTERNAL EMERGENCY EXIT LIGHTS AT RIGHT FUSELAGE INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY EXIT LIGHT AT RIGHT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: SIGN — BROKEN (CABIN)
MIA - EMERGENCY EXIT LIGHT ARROW AT LEFT FIRST CLASS LAVATORY HAS PLASTIC BASE BROKEN. REPLACED PLASTIC BASE FOR EMERGENCY EXIT LIGHT ARROW AT LEFT FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHT LEFT SIDE AFT OF FLAP INOPERATIVE. RELAMPED EMERGENCY LIGHT LEFT SIDE AFT OF FLAP. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — LOOSE (CABIN)
JFK - EMERGENCY LIGHTS AT ROW 29AB TO 36AB INOPERATIVE. FOUND LOOSE CONNECTION AT SEAT 36AB. RESECURED CONNECTION FOR EMERGENCY LIGHTS AT ROWS 29AT TO 36AB. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: OXYGEN MASK — INOPERATIVE (COCKPIT)
AFW - SECOND OBSERVER OXYGEN MASK REGULATOR INOPERATIVE. REPLACED SECOND OBSERVER OXYGEN MASK. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
LAX - EMERGENCY LIGHT AT LEFT SIDE OF STORAGE COMPARTMENT FORWARD OF SEAT 20B INOPERATIVE. FOUND LOOSE CONNECTOR AT SIDEWALL. SECURED LOOSE CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT LEFT SIDE OF STORAGE COMPARTMENT FORWARD OF SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)
EMERGENCY LIGHTS AT SEAT ROWS 28, 29, AND 30AB INOPERATIVE. RESECURED CONNECTOR AT SEAT 28AB FOR EMERGENCY LIGHTS AT SEAT ROWS 28 THROUGH 30AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
2003
Part: RELAY — FAILED (ELECTRICAL)
LAX - FLT 217 - EN ROUTE ORD-OGG, THREE HOURS INTO FLIGHT, RECEIVED LEADING EDGE SLAT ASYMMETRY EICAS CAUTION AND STANDBY BUS OFF CONDTIONS. DC STANDBY CIRCUIT BREAKER POPPED. EMERGENCY DECLARED AND LANDED AT LAX WITHOUT FURTHER INCIDENT. REPLACED DC STANDBY CIRCUIT BREAKER AND K109 RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: LIGHT — INOPERATIVE (EXTERIOR)
AFW - FOUND EXTERIOR EMERGENCY LIGHT FORWARD OF AFT CARGO DOOR INOPERATIVE. REPLACED AND RESEATED LAMP, OPS CHECKS GOOD. (M)
Part: CONNECTOR — DISCONNECTED (CABIN)
DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 3B INOPERATIVE. RECONNECTED EMERGENCY ESCAPE PATH LIGHTING CONNECTOR AT SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATIONS.
Part: CONNECTOR — DAMAGED (CABIN)
DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE LIGHTING INOPERATIVE AT SEAT 2B. REPAIRED EMERGENCY ESCAPE LIGHTING CANNON PLUG SOCKET AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — DISCONNECTED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING ROWS 19B, 20B, 21B AND 22B INOPERATIVE. REINSTALLED CANNON PLUG AT SEATS 19B, 20B, 21B, AND 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: GENERATOR — INOPERATIVE (RIGHT)
BOS - FLT 147 - RT GENERATOR OFF LIGHT IN CRUISE. GENERATOR WOULD NOT RESET. REPLACED RIGHT GENERATOR PER MM. ACCOMPLISHED REQUIRED TESTS. ALSO, REPLACED GCU PER MM. ALL CHECKS OK. (M)
2000
Part: CLAMP — LOOSE (NR 1 ENGINE)
LHR - FLT 45 - EN ROUTE CDG-JFK, DURING FILGHT LEFT SIDE BLEED DUCT LIGHT ILLUMINATED. PROCEEDED TO SHUTOFF LEFT SIDE ENGINE BLEED AND LEFT SIDE PACK. LEFT SIDE INDICATION TURNED OFF. DIVERTED LHR AND LANDED WITHOUT FURTHER INCIDENT. REPOSITIONED LEFT SIDE ISOLATION VALVE CLAMP. ACCOMPLISHED PACK BURNOUT PER THE MM. PERFORMED ENGINE RUN ON BOTH ENGINES. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: CONNECTOR — LOOSE (ROWS 26-30)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 25B THROUGH 30B INOPERATIVE. RE-SECURED CONNECTOR AT SEAT 25A. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)