N398AN
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.
126 reports on file, 2001-05-02 – 2021-10-11.
Part: SKIN — DENTED (BS 228-246 LBL27) · airframe 79,217 hrs · 13,165 cycles
FUSELAGE SKIN, SEC 41, BETWEEN STA 228.5 TO STA 245.84, AT LBL 26.70: DURING MAINTENANCE INSPECTION, SHOP FOUND A DENT ON FUSELAGE SKIN AT STA 235.5, LBL 30.0, ABOVE THE COCKPIT. THE DENT WAS LOCATED APP. 10.0ââ FROM BUTT JOINT AT STA 246 AND 1.0ââ FROM FRAME AT STA 236.5. DENT DIMENSIONS: A=1.88ââ, Y=0.094ââ, A/Y=20. THE DENT WAS NOT COMPLYING WITH BOEING 767-300 SRM 53-10-01 ALLOWABLE DAMAGE, AND WAS REMOVED ACCORDING TO J/C MF02780R0220-01. CUT OUT DIMENSIONS: 2.50ââX1.80ââ. IN ORDER TO GAIN ACCESS TO THE DAMAGED AREA, THE COCKPIT FIRE SIELD WAS TRIMMED FROM ONE SIDE, APP. AT BL 0.0, AND DISMANTED FROM THE OTHER SIDE.
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
EXTERNAL FUSELAGE SKIN â STA 1349.5, BETWEEN S-23R AND S-24R, AND STA 1363.5, S-26R: DURING CONVERSUON AT IAI, MAINTENANCE HAVE FOUND TWO (2) EXISTING BLEND OUT ZONES IN EXTERNAL FUSELAGE SKIN AMONG FASTENER AREAS. M0383: STA 1349.5, BETWEEN S-23R AND S-24R. NDT INSPECTIONS WERE PERFORMED AND FOUND NO EVIDENCE FOR CORROSION OR CRACKS. INITIAL SKIN THICKNESS: 0.210â. MIN THICKNESS: 0.206â. BLEND OUT DIMENSION 1: L=9.29â X W=0.73â. BLEND OUT DIMENSION 2: L=10.09â X W=0.59â. SHOP REMOVED FASTENERS IN ACCORDANCE WITH SRM 51-40-02. (THREE SOLID RIVETS 1/4â, ONE HI-LOK ¼â AND ONE HI-LOK 5/16â). REMOVED MATERIAL IN BLEND OUTS IS LESS THAN 5%. M0384: STA 1363.5 STR 26R. NDT INSPECTIONS WERE PERFORMED AND FOUND NO EVIDENCE FOR CORROSION OR CRACKS. INITIAL SKIN THICKNESS: 0.162â. MIN THICKNESS: 0.157â. BLEND OUT DIMENSION: L=3.74â X W=0.47â. SHOP REMOVED A FASTENER IN ACCORDANCE WITH SRM 51-40-02 (ONE HI-LOK ¼â).
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
EXTERNAL FUSELAGE SKIN â STA 1216, COMMON TO S-31: DURING CONVERSION AT IAI, MAINTENANCE HAVE FOUND DENT IN EXTERNAL FUSELAGE SKIN, COMMON TO DOORS CUTOUTS, LAP SPLICE, BUTT SPLICE AND AMONG FASTENERS AREA. DENT A/Y RATIO EQUALS TO 26 (A=1.25, Y=0.048).
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
AFT CARGO DOOR, UPPER FWD CORNER: DURING AIRCRAFT CARGO CONVERSION, TEAR DAMAGE WAS FOUND IN DATUM LOCATION. THE DAMAGE HAS LENGTH OF 1.2ââ AND WIDTH â 0.370ââ. AFT CARGO DOOR P/N: 140T2700-7; S/N: 000721.
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
M0079: SCRATCHES IN EXTERNALS FUSELAGE SKIN AMONG FASTENERS AREA, IN STA 1354, S-29R. MAINTENANCE CLEANED DAMAGED AREA IN ACCORDANCE WITH BOEING 767-300 SRM 51-10-02, AND REMOVED AN EXISTING FASTENER IN ACCORDANCE WITH BOEING 767-300 SRM 51-40-02. NDT INSPECTIONS: 1. HFEC FOR DAMAGED AREA AND OPEN HOLE INSPECTION WERE PERFORMED WITHOUT ANY EVIDENCE FOR CRACKS OR CORROSION. 2. INITIAL SKIN THICKNESS: 0.191''. MIN. THICKNESS: 0.183''. BLENDOUT DIMENSIONS: 2.26'' X 0.68''.
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
SCRATCHES IN EXTERNALS FUSELAGE SKIN AMONG FASTENERS AREA, IN STA 1368, 0.4'' ABOVE S-31R. MAINTENANCE CLEANED DAMAGED AREA IN ACCORDANCE WITH BOEING 767-300 SRM 51-10-02, AND REMOVED AN EXISTING FASTENER IN ACCORDANCE WITH BOEING 767-300 SRM 51-40-02. NDT INSPECTIONS: 1. HFEC FOR DAMAGED AREA AND OPEN HOLE INSPECTION WERE PERFORMED WITHOUT ANY EVIDENCE FOR CRACKS OR CORROSION. 2. INITIAL SKIN THICKNESS: 0.185''. MIN. THICKNESS: 0.182''. BLENDOUT DIMENSIONS: 1.13'' X 1.05''.
Part: NONE — NONE · corrosion level 2 · airframe 79,217 hrs · 13,165 cycles
SATCOM ANTENNA, STA 977 TO STA 1043, STR 2L TO STR 2R: AS PER COSTUMER REQUEST, HIGH GAIN SATCOM ANTENNA WAS REMOVED FROM THE AIRCRAFT. THE ANTENNA WAS MOUNTED TO AN ADAPTER, WHICH LOCATED BETWEEN STA 999 TO STA 1043, AND BETWEEN STR 1L TO STR 1R. ON FUSELAGE SKIN THERE IS 2.0ââ DIA. CUT OUT FOR ANTENNA CABLES, WHICH LOCATED APP. AT STA 1010, BETWEEN STR 1L TO STR 1R. CORROSION WAS FOUND AT THE CUT OUT. HENCE, CUT OUT WAS MADE RECTANGULAR (2.50ââX2.00ââ) IN ORDER TO REMOVE THE DAMAGE. ADDITIONALY, TWO (2) AREAS WERE FOUND WITH CORROSION BETWEEN STA 999 AND STA 1021, AT STR 1L. THE REMAINING SKIN THICKNEES IS COMPLYING WITH BOEING 767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1 REQUIREMENTS â ACCEPTABLE DEPTH LOSS OF 15 PERCENT MAX. THE SKIN, P/N 145T3111, IS MANUFACTURED FROM 2024-T3 CLAD ALUMINUM, MACHINED AND TAPERED, 0.170ââ THICK AT THA CABLES CUT OUT.
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
ENGINE #2, INLET COWL, PIN 242-2101-513BL, S/N 0242: DURING MAINTENANCE INSPECTION AT IAI, SEVERAL CRACKS AND EXISTING REPAIRS WERE FOUND.
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
A RECENT AIRCRAFT RECORDS REVIEW REVEALED THE PREVIOUS OPERATOR (AMERICAN AIRLINES) REPAIRED CRACK DAMAGE ON THE INBOARD SKIN PANEL (FORWARD TORQUE BOX) OF THE ENGINE STRUT #2 AT THE ACCESS PANEL OPENING LOCATED AT APPROXIMATE NAC 227/WL136.
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
DENT EXTERNAL FUSELAGE SKIN â STA 1233, COMMON TO S-27R: STA 1233, 0.14â ABOVE S-27R DENT A/Y RATIO EQUALS TO 24.6 (A=1.77, Y=0.072) GAGE: 0210â CLAD 2024-T3 (MACHINED TO 0.056â).
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
: STA 1307 - STA 1373, STR-22L - STR-26L: DURING TRIMMING OF STRINGER 25L FOR PRESSURE RELIEF VALVE INSTALLATION IN DATUM AREA AS PER DWG 371-21-30-C1104 REQUIREMENTS, EXTERNAL FUSELAGE SKIN WAS DAMAGED IN TWO LOCATIONS AS SHOWN IN RFTA 02780-0015.
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
EXTERNAL FUSELAGE SKIN â STA 1540, BETWEEN S-25R AND S-26R: MAINTENANCE HAVE FOUND SCRATCHES AT BLENDED AREA IN EXTERNAL FUSELAGE SKIN AMONG FASTENERS AREA. MAINTENANCE CLEANED DAMAGED AREA AND REMOVED AN EXISTING FASTENER WHICH INTERFERED BLEND OUT PROCEDURE. NDT INSPECTION WERE PERFORMED AND FOUND NO EVIDENCE FOR CRACKS OR CORROSION. INITIAL SKIN THICKNESS: 0.070â. MIN THICKNESS: 0.062â BLEND OUT DIMENSIONS: 3.40â X 1.13â.
Part: NONE — NONE · corrosion level 2 · airframe 79,217 hrs · 13,165 cycles
DURING MAINTENANCE INSPECTION AT IAI, PYLON #1 - NAC STA 308.00-376.20 - CORROSION DAMAGE WAS FOUND IN DATUM LOCATION. IAI HAS RECEIVED SMAL FROM BOEING TO FABRICATE P/N 313T2380-630 WEB BONDED ASSY, HOWEVER THERE IS NO CAPABILITY TO FABRICATE THE PART
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
MAINTENANCE FOUND A CRACK ON THE AFT FRAME OF ENGINE # 2 INBD CORE COWL (P/N 224-2301-521, S/N 3432001) AT 9 OâCLOCK POSITION. THE CRACK WAS FOUND BEYOND THE LIMITS OF SRM 54-45-01 REPAIR 4 NOTE C AND REPAIR 14 LIMITS.
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
PROBLEM DESCRIPTION: EXTERNAL FUSELAGE SKIN â STA 1417 â STA 1426, S-29L â S-34L: DURING CONVERSION AT IAI, MAINTENANCE HAVE FOUND SCRATCHES AT BLENDED AREA IN EXTERNAL FUSELAGE SKIN, AMONG FASTENERS AREA. THE DAMAGED AREA IS LOCATED IN THE FOLLOWING LOCATION: M0098: STA 1417.6, COMMON TO S-29L. BLEND OUT SIZE: 2.0''X0.64''(FWD BLEND), 0.94''X0.80'' (AFT BLEND). INITIAL SKIN THICKNESS: 0.185''. MIN. THICKNESS: 0.182''. M0102: STA 1423, COMMON TO S-33L. BLEND OUT SIZE: 1.35''X0.67''. MAX. SKIN THICKNESS: 0.188''. MIN. THICKNESS: 0.185''. M0103: STA 1426, ABOVE S-33L. BLEND OUT SIZE: 1.24''X0.56''. MAX. SKIN THICKNESS: 0.194''. MIN. THICKNESS: 0.192''. M0104: STA 1426, BELOW S-33L. BLEN DOUT SIZE: 2.38''X0.55''. MAX. SKIN THICKNESS: 0.194''. MIN. THICKNESS: 0.186''. MAINTENANCE CLEANED DAMAGED AREAS IN ACCORDANCE WITH BOEING 767-300 SRM 51-10-02, AND REMOVED EXISTING FASTENERS IN ACCORDANCE WITH BOEING 767-300 SRM 51-40-02. NDT INSPECTIONS: HFEC FOR DAMAGED AREA AND OPEN HOLE INSPECTION WERE PERFORMED WITHOUT ANY EVIDENCE FOR CRACKS OR CORROSION.
Part: NONE — NONE · airframe 79,217 hrs · 13,165 cycles
DENT WITH CREASE BEYOND SRM LIMITS IN EXTERNAL FUSELAGE SKIN AT STA 1373, 3.5â ABOVE S-29R. THE DAMAGE IS COMMON TO CUTOUT AND IS LOCATED IN FASTENERS AREA. DENT A/Y=25. MAINTENANCE ALSO FOUND AN NON-STANDARD SHEAR TIE INSTALLED IN THE INNER SKIN SIDE OF THE DENTED AREA.
Earlier reports · 2001–2020 · 110 reports
2020
Part: SIGN — UNSECURE (CABIN) · airframe 79,092 hrs · 13,131 cycles
AIRCRAFT WAS NOT GROUNDED: 1L DOOR EXIT SIGN NEEDED TO BE SECURED. MAINTENANCE REPLACED DOOR EXIT SIGN ASSEMBLY PER AMM 33-51-09.
Part: OVEN — SMOKE (GALLEY) · airframe 79,052 hrs · 13,120 cycles
AIRCRAFT WAS GROUNDED: FORWARD GALLEY #2 OVEN SMOKING. **SUPPLEMENTAL REPORT: REPLACED OVEN PER AMM 25-33-05** (CLOSED)
2019
Part: INDICATOR — LEAKING (HYD SYSTEM) · airframe 77,056 hrs · 12,678 cycles
AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF CENTER HYDRAULIC PRESSURE AND QUANTITY LOSS. MAINTENANCE REPORTS UPON TROUBLE SHOOTING FOUND SYSTEM DEPLETED DUE TO ADP MODULE DPI SWITCH LAKING, REPLACED ADP DPI, SERVICED OPS CHECK AND LEAK CHECK GOOD. PRESSURE NORMAL IAW AMM 29-11-19.
Part: BRACE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,886 hrs · 12,641 cycles
AIRCRAFT IN BASE MAINTENANCE: KEELBEAM CROSS BRACE AT BS 830 AT BL 0. REPLACED CROSS BRACE PER SRM 51-10-02.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 76,424 hrs · 12,552 cycles
AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT AT 2L AFT WAS DEAD. MAINTENANCE REPLACED EMERGENCY BATTERY FOR FLASHLIGHT PER AMM 25-60-00.
Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 76,072 hrs · 12,474 cycles
AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT AT 4R FAILED TEST. MAINTENANCE REPLACED FLASHLIGHT BATTERY AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 25-64-00.
Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 75,387 hrs · 12,313 cycles
EMERGENCY FLASHLIGHT FOUND TO HAVE AN INOPERATIVE BATTERY. MAINTENANCE REPLACED THE BATTERY IAW AMM 25-64-00, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.
2018
Part: WINDOW SHADE — DAMAGED (CABIN) · airframe 74,466 hrs · 12,132 cycles
PHL - THE AIRCRAFT WAS NOT GROUNDED. OVERWING WINDOW SHADE AT SEAT 21A EMERGENCY EXIT IS DAMAGED. MAINTENANCE R&R WINDOW SHADE AT SEAT 21A AS PER AMM 25-21-00, OPS CKS GOOD.
Part: SEAL — BROKEN (FLASHLIGHT) · airframe 74,436 hrs · 12,128 cycles
FOUND THE EMERGENCY FLASHLIGHT TAMPER SEAL BROKEN AND FLASHLIGHT NOT PROPERLY STOWED WITH DISCHARGED BATTERIES. INSTALLED THE FLASHLIGHT WITH A NEW TAMPER SEAL IAW AMM 25-64-00.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 74,436 hrs · 12,128 cycles
FOUND FLASHLIGHT TAMPER SEAL BROKEN AND FLASHLIGHT NOT PROPERLY STOWED, AND WITH DEAD BATTERIES. REPLACED THE BATTERIES IAW AMM 25-64-00.
Part: TEST PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 74,342 hrs · 12,111 cycles
NR 1 TEST DOES NOT ILLUMINATE BOTH LEFT AND RIGHT EMERGENCY LIGHTS. NR 2 TEST DOES TEST CORRECTLY (SQUIB TEST). THE AIRCRAFT WAS GROUNDED. REPLACED SQUIB TEST PANEL IAW MM 26-21-04. TEST CHECKED OK.
Part: WINDOW SHADE — DAMAGED (CABIN) · airframe 74,260 hrs · 12,098 cycles
MIA - THE AIRCRAFT WAS NOT GROUNDED. OVER WING WINDOW SHADE AT SEAT 21A EMERGENCY EXIT IS DAMAGED. MAINTENANCE R&R COACH SEAT WINDOW SHADE AT 21A EMERGENCY EXIT PER AMM 52-21-01-402-202 AND AMM 25-21-00-004-001.
Part: MEC — FAILED (LT ENGINE) · airframe 73,708 hrs · 11,993 cycles
LEFT ENGINE UNABLE TO CONTROL N1 WITH AUTO THROTTLES OFF. ABOVE IDLE ALL ENGINE INDICATIONS INCREASED WITH N1 INCREASE FROM AND EGT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. AFTER TEST FLIGHT AND FUNCTIONAL CHECKS, THE ENGINE FAILED AGAIN. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE MEC ASSY IAW 73-94-02, AND ENGINE RUN UP AFTER MEC CHANGE 71-95-20. SYSTEM CHECKED OK.
Part: WINDOW — SEPARATED (COCKPIT) · airframe 73,272 hrs · 11,909 cycles
LOUD SQUEAL COMING FROM THE CAPTAIN`S SIDE WINDOW. IT STARTED DURING CLIMB, PASSING THORUGH 21,000 FT, CABIN ALTTITUDE OF 5,000 FT APPROXIMATELY. STOPPED DURING DESCENT BELOW 13,700 FT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND SEPARATION OF THE WINDOW CAUSED THE LOUD SQUEL. REMOVED AND REPLACED THE L2 WINDOW AND L2 WINDOW SEAL IAW AMM 56-11-02, AND 56-11-11. OPS AND LEAK CHECKED GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 73,210 hrs · 11,897 cycles
ONE FLASHLIGHT AT THE FLIGHT ATTEND MID SECTION, BESIDE SEAT 17B ON EMERGENCY PANEL BATTERY DISCHARGED. REPLACED THE BATTERY IAW STANDARD PRACTICE. OPS CHECKED OK FOR CONTINUED SERVICE.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 72,413 hrs · 11,750 cycles
AIRCRAFT WAS NOT GROUNDED. 2L FLASHLIGHT INOPERABLE. REPLACED FLASHLIGHT BATTERY. OPERATIONS CHECK GOOD.
Part: FRAME — CRACKED (LT NACELLE) · airframe 72,260 hrs · 11,715 cycles
LEFT PYLON OUTBOARD SIDE FRAME AT NAC STA 285.450 IS CRACKED ON THE LOWER END AT INBOARD FASTENER LOCATION. REPLACED IAW 51-00-05-1.
Part: SUPPORT — CRACKED (LT NACELLE) · airframe 72,260 hrs · 11,715 cycles
LEFT PYLON INBOARD VERTICAL SUPPORT BELOW AFT UPPER DRAIN BOX IS CRACKED AND BROKEN. INSTALLED A NEW SUPPORT IAW 51-00-05-1 AND DRAWING 311T2400.
2017
Part: RECEIVER — FAILED (WEATHER RADAR) · airframe 70,931 hrs · 11,475 cycles
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. RETURNED TO DFW DUE TO MESSAGE WEATHER RADAR FAIL (*WXR FAIL*) MESSAGE. WEATHER RADAR INOPERABLE. MAINTENANCE PERFORMED TROUBLESHOOTING PER FIM 34-43-00-815-805 AND REPLACED RECEIVER PER MM 34-43-03. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 70,579 hrs · 11,407 cycles
EMERGENCY EXIT AISLE LIGHT BY SEAT 22B IS INOPERATIVE. SECURED THE CONNECTOR PLUG IAW ESO 11757. OPERATIONAL CHECKED GOOD.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,459 hrs · 11,389 cycles
OVERHEAD EMERGENCY LIGHT AT 8A, MISSING THE LENS. REPLACED THE LENS IAW AMM 33-51-04.
Part: CHARGER — NO TEST (EMERGENCY LIGHT) · airframe 87,591 hrs · 14,113 cycles
L2 DOOR SLIDE LIGHT IS INOPERATIVE. REMOVED AND REPLACED AFT CABIN BATTERY ASSEMBLY AND CHARGER IAW AMM 33-51-00. OPS CHECKED GOOD.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 70,334 hrs · 11,362 cycles
L2 DOOR EMERGENCY EVACUATION SLIDE LIGHT IS INOPERATIVE. REMOVED AND REPLACED AFT CABIN BATTERY ASSEMBLY AND CHARGER IAW AMM 33-51-00. OPS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 70,168 hrs · 11,338 cycles
FLIGHT ATTENDANT FLASHLIGHT NEXT TO M2 LAVATORY IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY IAW AMM 25-64-00. OPERATIONAL CHECKED GOOD.
Part: LIGHT — INOPERATIVE (SEAT 5J) · airframe 70,168 hrs · 11,338 cycles
SEAT MOUNTED EMERGENCY LIGHT AT SEAT 5J IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-51-05. OPERATIONAL CHECKED GOOD.
Part: FLASHLIGHT — FAILED (CABIN) · airframe 69,754 hrs · 11,273 cycles
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT L1 JUMP SEAT FAILED TEST. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 25-64-01. OPERATIONAL CHECKED GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,431 hrs · 11,215 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BY L4 DOOR FAILED TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.
2016
Part: FUEL CONTROL — FAULTY (LT ENGINE) · airframe 68,818 hrs · 11,095 cycles
LEFT ENGINE WOULD NOT SHUT DOWN WITH FUEL CONTROL IN OFF POSITION. CYCLED SWITCH AND ENGINE SHUT DOWN. ENGINE VALVE LIGHT REMAINED ON. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT MAIN ENGINE CONTROL IAW WC 73-94-02 AND 71-95-20. OPERATIONAL CHECKED GOOD.
Part: SWITCH — FAULTY (LT ENGINE) · airframe 68,500 hrs · 11,042 cycles
LEFT ENGINE WOULD NOT SHUT DOWN FOR ONE MINUTE WITH CUTOFF SWITCH IN THE OFF POSITION. REMOVED AND REPLACED FUEL CUTOFF SWITCH IAW AMM 76-11-09. OPERATIONAL CHECK GOOD. AIRCRAFT GROUNDED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,341 hrs · 10,861 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. CABIN SEAT TRACK NR 1 IS CORRODED BETWEEN FUSELAGE STA 801 AND 1098. R & R SEAT TRACK SECTION BETWEEN STA 801 AND 1098 IAW SRM 53-00-52-2R-3 AND EA 261528.
Part: FLOORBEAM — WORN (FUSELAGE) · airframe 67,341 hrs · 10,861 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. CABIN FLOORBEAM AT FUSELAGE STA 325 IS WORN AROUND FLOOR PANEL HOLES BETWEEN LBL 48 AND LBL 27. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 67,341 hrs · 10,861 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. FLOORBEAM AT FUSELAGE STATION 764 HAS 4 ELONGATED HOLES AT APPROXIMATELY RBL 30. REPAIRED FLOORBEAM BETWEEN RBL 18 AND RBL 44 IAW SRM 53-00-51-2R-1.
Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 67,226 hrs · 10,842 cycles
AIRCRAFT WAS GNDED, AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CRUISE BOTH WEATHER RADAR UNITS BECAME INOPERATIVE. ACCOMPLISHED BITE PROCEDURE IAW FIM 34-43-00-815-805, WXP FAIL WEAK, WOULD SHOW INTERMITTENT. R & R WEATHER RADAR TRANSCEIVER ASSEMBLY & PERFORMED OPERATIONAL TEST IAW AMM 34-43-01. SYS CHECKED NORMAL.
Part: CONNECTOR — SHORTED (CABIN) · airframe 66,497 hrs · 10,703 cycles
EMERGENCY LIGHT AT 32B SEAT IS INOPERATIVE. INSTALLED NEW PIN AT CONNECTOR 32B IAW SWPM 20-42-01. OPERATIONS CHECKED NORMAL IAW AMM 33-51-00. THE ACFT WAS NOT GNDED.
Part: CONTROLLER — FAILED (ZONE 400) · airframe 66,432 hrs · 10,688 cycles
AIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, RT ENG HPSOV, EICAS MSG DISPLAYED & BLEED LIGHT REMAINED ILLUMINATED. ACCOMPLISHED PNEUMATIC SYS HEALTH CHECK IAW AMM 36-00-21 WITH RT HIGH PRESSURE CONTROLLER FOUND FAULTED. R & R CONTROLLER IAW AMM 36-11-05. PASSED HEALTH CHECK & LEAK CHECK.
Part: GCU — FAULTY (ZONE 100) · airframe 66,137 hrs · 10,642 cycles
AIRCRAFT WAS NOT GNDED, AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING FLIGHT RT ENG IDG OFF LIGHT ILLUMINATED. IDG WOULD NOT RESET. R & R RT GCU IAW AMM 24-22-02-004-001. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.
2015
Part: CHARGER — FAULTY (ZONE 100) · airframe 63,422 hrs · 10,214 cycles
SEAT MOUNTED EMERGENCY LIGHTS FROM 7J TO 21H INOPERATIVE. R & R BATTERY CHARGER & BATTERY . PERFORMED OPS CHECKED IAW AMM 33-21-00. SYS CHECKED NORMAL.
Part: CABLE — DETACHED (EVAC SLIDE) · airframe 62,858 hrs · 10,126 cycles
CABLE AT FWD END OF R4 DOOR GIRT BAR DETACHED FROM SLIDE. REPLACED DOOR SLIDE AT R4 DOOR IAW MM 25-66-01. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,619 hrs · 10,088 cycles
EXTERIOR EMER LIGHT JUST AFT OF THE RT WING IS INOPERATIVE. R & R EMER LIGHT LAMP. PERFORMED OPERATIONAL IAW AMM 33-51-06-902-082. SYS CHECKED NORMAL.
2014
Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,441 hrs · 10,053 cycles
FORWARD PAX L1 DOOR FRAME WEB CORRODED JUST FWD OF FWD GIRT BAR FLOOR FITTING, APPROX STATION 300, STRINGER 20L. COMPLIED WITH REPAIR OF CORRODED FRAME & WEB IAW EA 53-037915 DATED 12/23/14.
Part: DOOR SILL — DENTED (FUSELAGE) · airframe 62,441 hrs · 10,053 cycles
DENT ON AFT CARGO DOOR CUT OUT LOWER SILL WEB APPROX 38 INCHES FROM FWD END OF CUT OUT. REPAIRED SILL IAW EA B767-53-037618 DATED 11/28/1014 & SRM 51-70-13-0G.
Part: SLIDE — DAMAGED (OVERWING EXIT) · airframe 62,441 hrs · 10,053 cycles
LEFT OFF WING SLIDE GIRT BAR HAS BROKEN LOOSE & IS LAYING IN THE CAVITY. R & R LT OVERWING SLIDE IAW AMM 25-65-01-424-060-001.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,441 hrs · 10,053 cycles
RIGHT FUSELAGE EXTERIOR EMER LIGHTS INOPERATIVE. FOUND LOW CHARGE ON TWO BATTERY PACKS M731. REPLACED BATTERY & CHARGER AT M731. SYS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,441 hrs · 10,053 cycles
RIGHT FUSELAGE EXTERIOR EMER LIGHTS INOPERATIVE. FOUND LOW CHARGE ON TWO BATTERY PACKS M733. REPLACED BATTERY AT M733. SYS CHECKED NORMAL.
Part: LIGHT — BROKEN (CABIN) · airframe 62,230 hrs · 10,016 cycles
L972 RT NR 1 DOOR LOWER FWD ESCAPE PATH LIGHT ASSEMBLY BROKEN. R & R L972 ESCAPE PATH LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.
Part: LENS — BROKEN (CABIN) · airframe 62,230 hrs · 10,016 cycles
L973 FWD RT OVERWING ESCAPE PATH LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY L973. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,502 hrs · 9,909 cycles
LEFT WING AFT EMER SLIDE LIGHT AFT INOPERATIVE. REPLACED LAMP FOR LT WING AFT EMER SLIDE LIGHT. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,502 hrs · 9,909 cycles
LEFT LOWER AFT EMER SLIDE LIGHT INOPERATIVE. REPLACED CHARGER & BATTERY PACK FOR LT LOWER AFT EMER SLIDE LIGHT. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,502 hrs · 9,909 cycles
LOWER FWD EMER SLIDE LIGHT INOPERATIVE. REPLACED CHARGER & BATTERY PACK FOR LOWER FWD EMER SLIDE LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,502 hrs · 9,909 cycles
FORWARD WING SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR FWD WING SLIDE LIGHT. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,502 hrs · 9,909 cycles
LEFT NR 2 DOOR EXTERNAL EMER LIGHT INOPERATIVE. REPLACED CHARGER & BATTERY PACK FOR LT NR 2 DOOR EXTERNAL EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,078 hrs · 9,844 cycles
EMERGENCY LIGHT AT SEAT 35B INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 35B. OPERATIONS CHECKED NORMAL.
2013
Part: TRU — MALFUNCTIONED (ZONE 200) · airframe 59,287 hrs · 9,525 cycles
PHX INFLIGHT MIA-LAX. CREW REPORTED ELECTRICAL ODOR IN THE CABIN. EMERGENCY DECLARED FLIGHT DIVERTED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT TRANSFORMER RECTIFIER UNIT. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.
Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 57,438 hrs · 9,212 cycles
SMOKE IN THE MID GALLEY & FORWARD, MID LAVATORY SMOKE ALARMS WENT OFF. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. ACFT FERRIED TO TUL FOR FURTHER MX. REPLACED RT ENGINE AT TUL. SYSTEM GROUND CHECKED NORMAL.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 56,968 hrs · 9,142 cycles
LEFT NR 4 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.
2012
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 53,854 hrs · 8,638 cycles
LEFT NUMBER 4 DOOR EMERGENCY EXIT SIGN LOWER PORTION INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.
Part: SOCKET — OUT OF ADJUST (EXTERIOR) · airframe 53,854 hrs · 8,638 cycles
LEFT NUMBER 4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. ADJUSTED SOCKET FOR LEFT NUMBER 4 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: SOCKET — OUT OF ADJUST (EXTERIOR) · airframe 53,854 hrs · 8,638 cycles
EXTERIOR EMERGENCY LIGHT AFT OF RIGHT INBOARD FLAP INOPERATIVE. ADJUSTED SOCKET FOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,854 hrs · 8,638 cycles
OVERHEAD EMERGENCY LIGHT ON RIGHT SIDE BEHIND AFT CABIN DIVIDER INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT ON RIGHT SIDE BEHIND AFT CABIN DIVIDER. OPS CHECK NORMAL.
2011
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,809 hrs · 8,299 cycles
INTERIOR EMERGENCY LIGHTS AT SEAT ROWS 10AB TO 17AB INOPERATIVE. REPLACED BATTERY PACK M1505. OPS CHECK NORMAL.
Part: TRANSMITTER — INOPERATIVE (TE FLAP) · airframe 51,237 hrs · 8,223 cycles
DFW - CREW REPORTED FLAP INDICATION SPLIT 1 DEGREE FROM RIGHT TO LEFT. NO EICAS MESSAGE INDICATED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 FLAP POSITION TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: DETECTOR — INOPERATIVE (LT ENGINE) · airframe 50,239 hrs · 8,068 cycles
SDQ - INFLIGHT MIA-POS. CREW REPORTED STATUS MESSAGE FOR LEFT ENGINE FIRE LOOP 2, WITH LEFT ENGINE FIRE LOOP 1 ALREADY ON PLACARD. ACCOMPLISHED QRH AND LEFT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 20 MINS). EMERGENCY DECLARED FLIGHT DIVERTED SDQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NO EVIDENCE OF FIRE OR OVERHEAT. REPLACED LOWER FORWARD DETECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.
2009
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 40,513 hrs
MIA - EMERGENCY LIGHT AT SEAT 15H INOPERATIVE. REPLACED LAMP AT 15H.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 40,513 hrs
MIA - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP AT 20C.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 40,513 hrs
MIA - EMERGENCY LIGHT AT SEAT 3B INOPERATIVE. REPLACED LAMP AT 3B.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 40,513 hrs
MIA - LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AT LEFT OVERWING.
2008
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,056 hrs
JFK - EMERGENCY EXIT SIGN LIGHT AT SEAT 17B INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 17B. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,056 hrs
JFK - EMERGENCY EXIT SIGN LIGHT AT SEAT 17H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 17H. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,335 hrs
MIA - EMERGENCY LIGHT AT SEAT 3B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,604 hrs
ORD - EMERGENCY LIGHT AT RIGHT OVERHEAD SEAT ROW 17 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT OVERHEAD SEAT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,604 hrs
ORD - EMERGENCY LIGHT AT RIGHT OVERHEAD SEAT ROW 37 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT OVERHEAD SEAT ROW 37. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
JFK - EMERGENCY LIGHT AT OVERHEAD SEAT 6B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 6B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)
JFK - EMERGENCY LIGHT AT FIRST CLASS GALLEY OVERHEAD RIGHT CENTER AISLE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FIRST CLASS GALLEY OVERHEAD RIGHT CENTER AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHTS AT SEAT MOUNTED LEFT SEAT ROWS 10 TO 17 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT MOUNTED LEFT SEAT ROWS 10 TO 17. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EXTERIOR EMERGENCY LIGHT AT RIGHT OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGHT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EXTERIOR EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHT AT AFT LEFT ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT LEFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHTS AT SEAT ROWS 10 TO 13A INOPERATIVE. RESET CABIN AND FLIGHT DECK SWITCHES FOR EMERGENCY LIGHTS AT SEAT ROWS 10 TO 13A. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHT AT LEFT FORWARD ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
JFK - EMERGENCY LIGHTS AT SEAT ROWS 10 TO 13 LEFT SIDE INOPERATIVE. REPLACED BATTERY PACK M1208 FOR EMERGENCY LIGHTS AT SEAT ROWS 10 TO 134 LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
JFK - EMERGENCY LIGHT AT SEAT ROWS 10B TO 12B INOPERATIVE. SECURED CONNECTOR AT SEAT ROW 10B FOR EMERGENCY LIGHT AT SEAT ROWS 10B TO 12B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SFO - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)
SFO - EMERGENCY LIGHT AT SEAT 22B INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY EXIT LIGHT AT LEFT NR ONE DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE HARNESS — LOOSE (CABIN)
SFO - EMERGENCY LIGHT AT SEAT 22B INOPERATIVE. SECURED HARNESS FOR EMERGENCY LIGHT AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT AT LEFT LIGHT 645 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT LIGHT 645. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT AT SEAT 22B INOPERATIVE. REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT AT FORWARD MOST LEFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT M736 FOR EMERGENCY LIGHT AT 788 FORWARD MOST LEFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT AT RIGHT FORWARD LIGHT 644 INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT FORWARD LIGHT 644. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
MIA - EMERGENCY ESCAPE PATH LIGHT AT FORWARD LAVATORY WILL NOT TURN ON FROM FLIGHT DECK. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT UNARMED LIGHT AT OVERHEAD INOPERATIVE. RELAMPED EMERGENCY LIGHT UNARMED LIGHT AT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN)
SFO - EMERGENCY LIGHTS ON AFT CABIN EXTERIOR RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK AT M733 FOR INOPERATIVE EMERGENCY LIGHTS ON AFT CABIN OUTBOARD RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)
SFO - SEAT MOUNTED EMERGENCY LIGHTS AT 30AB INOPERATIVE. SECURED CONNECTOR AT SEAT 30AB FOR SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHTS AT SEAT 33D INOPERATIVE. SECURED CONNECTOR UNDER SEAT FOR EMERGENCY LIGHTS AT SEAT 33D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT SEAT 6B INOPERATIVE. REPLACED EMERGENCY LIGHT AT SEAT 6B. SYSTEM GROUND CHECKED NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT SEAT 20H INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 20H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — DISCONNECTED (CABIN)
GRU - EMERGENCY AISLE LIGHTING AT SEAT ROWS 30H THROUGH 32H INOPERATIVE. FOUND CONNECTOR UNDER SEAT 29J DISCONNECTED. RECONNECTED EMERGENCY AISLE LIGHTING CONNECTOR AT SEAT 29J FOR EMERGENCY AISLE LIGHTING AT ROWS 30H THROUGH 32H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WARNING LIGHT — ILLUMINATED (RT ENGINE)
GRU - RIGHT PACK OFF LIGHT ILLUMINATED AND RIGHT ENGINE BLEED OFF LIGHT ILLUMINATED. ACCOMPLISHED BYTE CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — LOOSE (EMERGENCY LIGHTS)
SFO EMERGENCLY LIGHTS AT SEATS 22A THROUGH 36A INOPERATIVE. REPAIRED LOOSE CONNECTION FOR EMERGENCY LIGHTS AT SEATS 22A THROUGH 36A. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: BATTERY PACK — DISCHARGED (CABIN)
LAX SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 24B THROUGH 35B INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 24B THROUGH 35B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT)
MIA - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT SEAT 32H. SECURED ELECTRICAL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DAMAGED (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT SEAT ROWS 24 THROUGH 36. REPLACED BATTERY PACK AND REPAIRED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)
AFT GALLEY EMERGENCY LIGHT CROSSOVER WAS INOPERATIVE. BATTERY PACK FAILED DUAL FEED CHECK. SECURED WIRING AND REPLACED THE LENS COVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21A INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 21A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: BATTERY PACK — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)
2001
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32H INOPERATIVE. RE-SECURED EMERGENCY EXIT LGHT CONNECTOR AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 3H DIM. RELAMPED AFT EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 3H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: TELEPRINTER — OVERHEATED (COCKPIT)
CDG - FLT 62 - EN ROUTE MIA-CDG, DETECTED MALFUNCTION AND OVERHEAT AT ACARS PRINTER. PULLED AND COLLARED ACARS PRINTER CIRCUIT BREAKER. LANDED CDG WITHOUT FURTHER INCIDENT. REPLACED ACARS PRINTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)