N385AM
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.
173 reports on file, 1995-03-30 – 2021-02-21.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 102,560 hrs · 16,713 cycles
HORIZONTAL STABILIZER CENTER SECTION UPPER SKIN, BETWEEN STR 8/11 AND RBL 13/32; MAINTENANCE FOUND CORROSION ON PREVIOUSLY BLENDED SKIN AREA LOCATED BETWEEN STR 9-10 AND ON PREVIOUSLY INSTALLED DOUBLER LOCATED BETWEEN STR 10-11 PER BOEING SR 1-1906538101 AND 1-257618371.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
EXTERNAL FUSELAGE SKIN AT STA 1417 STR 36L AND STA 1567, STR-37L, (2EA REPAIR LOCATIONS) SECTION 46. SHOP FOUND EXISTING BLENDOUTS AREAS NAMED NRC: M0086 AND M0099 AT FUSELAGE SKIN IN THE NOTED LOCATION. BLENDOUT M0086 IS LOCATED 1.1 INCHES FROM SPLICE JOUNT. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLENDOUT IS NOT APPLICABLE IN FASTENERS AREA.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
INNER FUSELAGE SKIN PANEL STA 1193 BETWEEN STR-28L AND 29L, PN 146T3252-1: AN EXISTING DEEP GOUGE WAS FOUND AND WAS BLENDED OUT AS PER SRM B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1. AFTER THE BLEND AND DRILL OUT (0.250"), THE MEASURED MINIMUM FUSELAGE SKIN THICKNESS WAS 0.052", A 26% REDUCTION FROM THE NOMINAL SKIN THICKNESS OF 0.071", WHICH IS ABOVE THE ALLOWABLE DAMAGE LIMITS OF 15% SKIN THICKNESS REDUCTION AS PER B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1. UNABLE TO PERFORM PLUG FASTENER REPAIR DUE TO REDUCTION OF THICKNESS. THE BLEND OUT IS LOCATED CLOSE TO THE HYDRAULIC SYSTEM PIPE INLET AT STA 1197 -STA1197+11 STR 27L â STR 28L, WHICH MEANS THAT BLEND OUT FALLS WITHIN THE NO REPAIR ZONE BY A FUSELAGE SKIN CUTOUT AS PER B767-300 SRM 53-00-01 REPAIR RESTRICTION, FIG 202.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 102,560 hrs · 16,713 cycles
CORROSION DAMAGE WAS FOUND TO THE RT WING UPPER INNER SPAR SKIN PANEL NR .1 OVER WING FILL PORT ADAPTER AT WS 785.2, S-15 TO S-16 LOCATION. SEE FIGURE 4 FOR EXISTING REPAIR DAMAGE DETAILS. AFTER CORROSION REMOVAL AT EACH OVER WING FILL PORT UPPER SKIN, THE AREA WAS INSPECTED: 1. NO CORROSION OR CRACKS WERE FOUND. 2. REDUCTION OF THICKNESS WAS FOUND FROM 0.250" TO 0.183" MINIMUM REMAINING THICKNESS. THICKNESS REDUCTION OF 0.077" EXCEEDS 0.025" ALLOWABLE MATERIAL LOSS ON WING UPPER SKIN BETWEEN WS 758 AND WS 945.8 PER 767-300 SRM 75-20-01 ALLOWABLE DAMAGE 1 TABLE I. 767-300 SRM 51-10-01 CALLS FOR 0.015" MAXIMAL MISS MATCH BETWEEN SURFACES IN THE AERODYNAMIC SMOOTHNESS CRITICAL AREAS FOR BETWEEN SPAR JOINTS ON THE WING.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
EXTERNAL FUSELAGE SKIN BETWEEN STA 450.5 AND STA 478, STR-26R/32R, (3EA REPAIR LOCATIONS), SECTION 43. SHOP FOUND THREE (3) EXISTING BLENDOUTS AREAS NAMED NRC : M0032, M0038 AND M00040 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZONE. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLENDOUT IS NOT APPLICABLE IN FASTENERS AREA.
Part: SKIN — DENTED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
EXTERNAL FUSELAGE SKIN â 3 BULGES AND A DENT WERE FOUND ON EXTERNAL FUSELAGE SKIN BETWEEN STA 434-456 STR 26L-28L. THE DAMAGES ARE LOCATED WITHIN THE EXTRA CRITICAL AREA AROUND THE STATIC PORT AS NOTED IN SRM 51-10-01 GENERAL FIG 3 (SHEET 3 OF 4) DETAIL IV EXTERNAL REPAIRS ARE NOT PERMITTED IN THIS AREA. THE BULGES DIMENSIONS AS REPORTED PER RFTA 02736-0041 ARE: BULGE #B1 A=0.55" Y=0.019"; BULGE #B2 A=0.71" Y=0.03"; BULGE #B3 A=1.1" Y=0.048" THE SKINS AFFECTED ARE MADE BOTH FROM ALCLAD 2024-T3 OF THICKNESSES 0.125"/0.160" CHEM-MILLED TO 0.056" MIN AND 0.140" MACHINED TO 0.056" MIN.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 102,560 hrs · 16,713 cycles
DURING MAINTENANCE INSPECTIONS AT IAI, 2 EXISTING DENTS WERE FOUND ON UNDERSIDE OF THE RT WING OUTBOARD TRAILING FLAP. THE DENTS WERE MEASURED AS HAVING WIDTHS OF 1.8" AND 1.7" AS DEPTHS OF 0.027" AND 0.029" RESPECTIVELY. THE DAMAGES WERE FOUND ABOVE LIMITS PER B767-300SRM 57-53-01, ALLOWABLE DAMAGE 1, FIGURE 101. THESE DIMENSIONS ARE WITHIN ALLOWABLE DAMAGE LIMITS AS PER SRM B767-300 SRM 57-53-01 ALLOWABLE DAMAGE 1, DETAIL IV. HOWEVER, DUE TO THE DISTANCE BETWEEN THE 2 DENTS BEING 0.85", WHICH IS LESS THAN THE MINIMUM OF 3" REQUIRED, THIS DAMAGE DOES NOT MEET ALLOWABLE DAMAGE LIMIT AS PER SRM B767-300 SRM 57-53-01 ALLOWABLE DAMAGE 1, DETAIL IV. THE LOWER PANEL OUTER SKIN IS MADE FROM 0.100, 2024-T3 CLAD ALUMINUM CHEM-MILLED TO 0.013 MIN PER 767-300 SRM 57-53-01. THE DENTS ARE COMMON TO 0.090" THICKNESS. THE STRUCTURE IS CLASSIFIED A SECONDARY STRUCTURE PER B767-300 SRM 51-00-04.
Part: SUPPORT RIB — CRACKED · airframe 102,560 hrs · 16,713 cycles
DURING MAINTENANCE INSPECTIONS AT IAI, A CRACK WAS FOUND NEAR THE RADIUS OF ACTUATOR SUPPORT RIB PN 114T2504-2. PENETRANT INSPECTION OF THE CRACK AREA WAS PERFORMED AND NO ADDITIONAL CRACKS WAS FOUND.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
REPAIR â FUSELAGE SKIN STA 1263 â 1270, STR-32R-33R & 27R-29R, SECTION 46; PN 146T3510. SHOP FOUND EXISTING BLEND OUT AREAS NAMED M0054 AND M0055 AT FUSELAGE SKIN IN THE NOTED LOCATION. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLEND OUT IS NOT APPLICABLE IN FASTENERS AREA.
Part: SKIN — DEBONDED (HORIZONTAL STAB) · airframe 102,560 hrs · 16,713 cycles
R/H HORIZONTAL STABILIZER PANEL, STAB STA 127.465 â AUX SPAR STA 157.277, 185T1001. THE INNER 7075-T6 ALUMINUM SKIN FOUND DISBONDED AND SEPARATED FROM THE ALUMINUM HONEYCOMB CORY PANEL 185T1001. IDENTIFICATION PER SRM 55-10-01 FIG. 1 (DETAIL I)
Part: SKIN — DAMAGED (EXTERIOR) · airframe 102,560 hrs · 16,713 cycles
SEVERAL SCRATCHES BLENDED OUT ON EXTERNAL FUSELAGE SKIN BETWEEN STA 1344- STA 1356 STR 28R-30R THE BLENDOUTS FALL ON RIVETED AREA AND DO NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTS
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
EXTERNAL FUSELAGE SKIN BETWEEN STA 380 AND STA 390, BELOW STR-2R, SECTION 41. SHOP FOUND 2 (2) EXISTING BLENDOUTS AREAS NAMED M0369 AND M0370 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZONE AND SPLICE JOINT ALONG S-2R. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLENDOUT IS NOT APPLICABLE IN FASTENERS AREA.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
: EXTERNAL FUSELAGE SKIN BETWEEN STA 1351 AND STA 1373, STR-22R/25R, (3EA REPAIR LOCATIONS), SECTION 46. SHOP FOUND THREE (3) EXISTING BLENDOUTS AREAS NAMED NRC :M0078, M0075 AND M00076 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZONE. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLENDOUT IS NOT APPLICABLE IN FASTENERS AREA.
Part: SKIN — DAMAGED (NR 1 INLET) · airframe 102,560 hrs · 16,713 cycles
ENGINE NR 1-INLET COWL LEADING EDGE OUTER LIP-BETWEEN 7 AND 8 O'CLOCK POSITION. SHOP FOUND AN EXISTING UNDOCUMENTED REPAIR DOUBLER AT THE DATUM LOCATION, ACCORDING TO SRM 54-15-01 REPAIR 2, THERE IS NO APPLICABILITY FOR SUCH REPAIR THEREFORE THIS REA IS MAJOR.
Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 102,560 hrs · 16,713 cycles
FUSELAGE SKIN PANEL, STA 919.5, STR 19L- STR 20L, P/N 145T3321-4, AN EXISTING AREA OF CORROSION WAS FOUND AND WAS BLENDED OUT AS PER SRM B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1. AFTER THE BLEND OUT, THE MEASURED MINIMUM FUSELAGE SKIN THICKNESS WAS 0.178", A 20% REDUCTION FROM THE NOMINAL SKIN THICKNESS OF 0.223", WHICH IS ABOVE THE ALLOWABLE DAMAGE LIMITS OF 15% SKIN THICKNESS REDUCTION AS PER B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1. THE BLEND OUT IS LOCATED CLOSE TO THE REAR OVER-WING EMERGNCY EXIT DOOR, WHICH MEANS THAT THE BLEND OUT FALLS WITHIN THE NO REPAIR ZONE BY A FUSELAGE SKIN CUTOUT AS PER B767-300 SRM 53-00-01 REPAIR, FIG 202.
Part: SKIN — DAMAGED (EXTERIOR) · airframe 120,560 hrs · 16,713 cycles
SEVERAL SCRATCHES BLENDED OUT ON EXTERNAL FUSELAGE SKIN BETWEEN STA 1345- STA 1351 STR 21R-22R THE BLENDOUTS FALL ON RIVETED AREA AND DO NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTS
Part: SKIN — CORRODED (SATCOM ANT MOUNT) · corrosion level 2 · airframe 102,560 hrs · 16,713 cycles
REPAIR â FUSELAGE SKIN (SECTION 45), BETWEEN STA 999 AND STA 1043, BETWEEN STR 2L AND STR 2R AS PER COSTUMER REQUEST SATCOM ANTENNA WAS DEACTIVATED AND DISMANTLED FROM THE AIRCRAFT. THE ANTENNA WAS MOUNTED TO AN ADAPTER PLATE AT DATUM LOCATION. UNDER ANTENNA, CORROSION WAS FOUND ON SKIN AND EXISTING COAX CABLE CUTOUT. IN ORDER TO REMOVE THE DAMAGE, CORRODED SKON WAS BLENDED AND COAX CABLE CUTOUT WAS ENLARGED (2.9" X 2.0"). ADDITIONAL REFERENCES: FVCI EO. 20517-8 REV B; JC MF02736R0215-01; B767-300 SRM 53-00-01, AD1 & IDENT; B767-300 SRM 53-00-01, REPAIR 14.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 102,560 hrs · 16,713 cycles
CORROSION DAMAGE WAS FOUND TO THE LT WING UPPER INNER SPAR SKIN PANEL NR 1 OVER WING FILL PORT ADAPTER AT WS 785.2, S-15 TO S-16 LOCATION. AFTER CORROSION REMOVAL AT EACH OVER WING FILL PORT UPPER SKIN, THE AREA WAS INSPECTED: 1. NO CORROSION OR CRACKS WERE FOUND. 2. REDUCTION OF THICKNESS WAS FOUND FROM 0.250" TO 0.208" MINIMUM REMAINING THICKNESS. THICKNESS REDUCTION OF 0.042" EXCEEDS 0.025" ALLOWABLE MATERIAL LOSS ON WING UPPER SKIN BETWEEN WS 758 AND WS 945.8 PER 767-300 SRM 75-20-01 ALLOWABLE DAMAGE 1 TABLE I. 767-300 SRM 51-10-01 CALLS FOR 0.015" MAXIMAL MISS MATCH BETWEEN SURFACES IN THE AERODYNAMIC SMOOTHNESS CRITICAL AREAS FOR BETWEEN SPAR JOINTS ON THE WING.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
EXTERNAL FUSELAGE SKIN, STA 1535, STR 20L â 22L P/N 146T3340. SHOP FOUND AN EXISTING BLENDOUT AREA NAMED M0153 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUT FALL ON ASTENERS ZONE. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLENDOUT IS NOT APPLICABLE IN FASTENERS AREA.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
FUSELAGE SKIN EXTERNAL FUSELAGE SKIN AT STA 632, STR-26R SECTION 43. SHOP FOUND BLEND OUT IN FASTENERS ZONE IN UPPER SKIN OF LAP JOINT IN FUSELAGE SKIN AT THE DATUM LOCATION. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLEND OUT IS NOT APPLICABLE IN FASTENERS AREA.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
FUSELAGE SKIN STA 1270 BETWEEN STR 29R/34R P/N 146T3510-3 AND REPAIR SCUFF PLATES, BETWEEN STA 1270 AND STA 1285, P/N 146T8051-1 AND 146T8051-3. IMPACT DAMAGE HAS BEEN FOUND ON FWD EDGE OF AFT CARGO DOOR AT STA 1270 STR 31R. THE DAMAGE SKIN IS MADE FROM 0.210" CLAD 2024-T3 MACHINED TO 0.125" MIN.
Part: SKIN — DAMAGED (EXTERIOR) · airframe 102,560 hrs · 16,713 cycles
SEVERAL SCRATCHES BLENDED OUT ON EXTERNAL FUSELAGE SKIN BELOW WING TO BODY FAIRING AT STA 698 STR 21R THE BLENDOUTS FALL ON RIVETED AREA AND DO NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTS.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
EXTERNAL FUSELAGE SKIN BETWEEN STA 1347 AND STA 1387, BETWEEN STR-28R AND STR 33R, SECTION 46. SHOP FOUND FIVE (5) EXISTING BLENDOUTS AREAS NAMED NRC: M0062, M0065, M0066, M0069 AND M0151 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZONE. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLENDOUT IS NOT APPLICABLE IN FASTENERS AREA.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
REPAIR EXTERNAL FUSELAGE SKIN BETWEEN STA 287 â STA 406, STR - 1R/4R, AND STA 266 â STA 348, STR 5R-7R, (SECTION 41). MULTIPLE BLEND OUTS AND LIGHTNING STRIKES WERE FOUND ON EXTERNAL FUSELAGE SKIN BETWEEN STA 287-406 STR 1R-4R AND STA 266 â STA 348, STR 5R-7R, (SECTION 41). THE BLEND OUT A FALL CLOSE TO RIVETED AREA (LESS THAN 2D) AND DOES NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTS. THESE BLEND OUTS AND LIGHTNING STRIKES ALSO DO NOT MEET SRM REQUIREMENT OF NO REPAIR ZONE PER SRM 53-00-01 FIG 101 ALLOWABLE DAMAGE 2. THE SKIN IS MADE FROM 0.063" 2024-T3 CLAD ALUMINUM CHEM MILLED OR MACHINED TO 0.056" MIN, THE EXISTING BLEND OUTS ARE COMMON TO DIFFERENT THICKNESS AREAS.
Part: SKIN — SCRATCHED (EXTERIOR) · airframe 102,560 hrs · 16,713 cycles
SEVERAL SCRATCHES BLENDED OUT ON EXTERNAL FUSLAGE SKIN AT STA 1417 STR 29L-31L THE BLENDOUTS FALL ON RIVETED AREA AND DO NOT MEET SRM ALLOWABLE DAMAGE REQUIREMENTS.
Part: SKIN — DENTED (ACCESS DOOR) · airframe 102,560 hrs · 16,713 cycles
ELEC/ELEX ACCESS DOOR INNER SKIN. DURING CONVERSION AT IAI FACILITIES, MAINTENANCE HAS FOUND AT SERVICE DOOR ELEC/ELEX 2 DENTS ON INNER SKIN AND GOUGED WEB. THE DENTS WERE FOUND WITH CREASE AND ARE OUT OF ALLOWABLE DAMAGE PER SRM 52-40-01 AD5. THE INNER SKIN IS MADE FROM 0.032" THICK ALCLAD 2024-T3 AND THE WEB FROM 0.063" THICK ALCLAD 2024-0 HT TO-T42.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
EXTERNAL FUSELAGE SKIN BETWEEN STA 343 AND STA 350, STR-22R, SECTION 41. SHOP FOUND FORE (4) EXISTING BLENDOUTS AREAS NAMED NRC : M0048 AT FUSELAGE SKIN IN THE NOTED LOCATION. THE BLENDOUTS FALL ON FASTENERS ZONE. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLENDOUT IS NOT APPLICABLE IN FASTENERS AREA.
Part: SKIN — DENTED (NO 1 ENGINE) · airframe 102,560 hrs · 16,713 cycles
PRIMARY EXHAUST NOZZLE OUTER SLEEVE SKIN, NR 1 ENGINE, AT 3 O'CLOCK. DURING CONVERSION AT IAI FACILITIES, MAINTENANCE HAS FOUND TWO (2) DENTS ON THE NR 1 ENGINE EXHAUST'S AFT EDGE AT 3 O'CLOCK. THE DENTS ARE OUT OF TOLERANCE DUE TO THEIR AY/Y RATIO AND ALSO BECAUSE OF THEIR DISTANCE FROM THE AFT EDGE OF THE NOZZLE AS REPORTED IN RFTA 02736-0256. THE OUTER SLEEVE SKIN IS MADE FROM 0.050" INCONEL ALLOY 625 CHEM MILLED TO 0.032" MIN.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 102,560 hrs · 16,713 cycles
EXTERNAL FUSELAGE SKIN AT STA 1417, BETWEEN STR-31L/33L, SECTION 46. SHOP FOUND 9 BLEND OUTS IN FASTENERS ZONE IN FUSELAGE SKIN AT THE DATUM LOCATION. ACCORDING TO SRM 53-00-01 ALLOWABLE DAMAGE 1, BLEND OUT IS NOT APPLICABLE IN FASTENERS AREA.
Earlier reports · 1995–2019 · 144 reports
2019
Part: PROXIMITY SWITCH — FAULTY (LE SLAT) · airframe 101,517 hrs · 16,475 cycles
AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO MIA ON ACCOUNT OF LEADING EDGE SLAT DISAGREE. NO EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED PSEU UNIT IAW AMM 32-09-04, OPS CHECKED NORMAL. NO FAULTS NOTED.
Part: O-RING — LEAKING (FUEL SYS) · airframe 101,421 hrs · 16,450 cycles
AIRCRAFT WAS GROUNDED: PILOT REPORTS AFTER BOARDING, CAPT WAS NOTIFYING A/C HAS UNCONTROLLED FUEL PUMPING OVERBOARD, CAPT WAS ADVISED TO DEPLAIN/EVACUATE A/C SUCCESSFULL EVACUATED FROM DOOR 2L. MAINTENANCE REMOVED & REPLACED IMBOARD REFUELING POPPET ASSEMBLY O-RING IAW AMM 28-21-01, NO LEAKS NOTED IAW AMM 28-21-01.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 101,007 hrs · 16,359 cycles
AIRCRAFT WAS GROUNDED: FORWARD, RIGHTHAND SIDE, OVERWING, EMERGENCY EXIT LIGHT WAS INOPERABLE DURING TEST. MAINTENANCE RELAMPED OVERWING EMERGENCY LIGHT PER AMM 33-51-06.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 100,513 hrs · 16,273 cycles
AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED FLIGHT DECK EMERGENCY LIGHT AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 99,361 hrs · 16,007 cycles
EMERGENCY LIGHT AT SEAT 37H WAS INOPERATIVE. MAINTENANCE FOUND A LOOSE CONECTION AT SEAT 37H, SECURED THE CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 99,361 hrs · 16,007 cycles
EMERGENCY LIGHT AT SEAT 38H WAS INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR AT 38H, SECURED THE CONNECTOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.
2018
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 99,072 hrs · 15,931 cycles
AIRCRAFT WAS NOT GROUNDED: FLOOR WAS SPONGY 5 FEET INSIDE L1 DOOR. MAINTENANCE REPLACED ELECTRONIC EQUIPMENT BAY MAIN DECK ACCESS PANEL PER AMM 52-48-05 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: STRINGER — CORRODED (BS 1219) · corrosion level 2 · airframe 98,576 hrs · 15,826 cycles
CORROSION ON STRINGER 38, BS 1219. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-2, AND EA285161.
Part: SKIN — CORRODED (BS 1554) · corrosion level 2 · airframe 98,576 hrs · 15,826 cycles
CORROSION FOUND ON THE EXTERIOR FUSELAGE SKIN AT BS 1554, BETWEEN STRINGERS 23L AND 24L. REPAIRED THE SKIN IAW SRM 53-60-01-2R.
Part: CONNECTOR — DAMAGED (SLAT SYSTEM) · airframe 98,358 hrs · 15,782 cycles
AT FL 350, AN L/E SLAT ASSEMBLY EICAS MESSAGE WAS INTERMITTENT, FLAP INDICATION NEEDLE ERRATIC, LEADING EDGE WARNING LIGHT INTERMITTENT, CLICKING NOISE IN THE OVERHEAD CIRCUIT BREAKER PANEL. AN EMERGENCY WAS DECLARED, FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. FOUND PUSHED BACK PIN 18 ON CONNECTOR D4378P. REPLACED THE CONNECTOR IAW AMM 27-58-00.
Part: FLASHLIGHT — DISLODGED (CABIN) · airframe 97,844 hrs · 15,682 cycles
ROW 17 AB FLIGHT ATTENDANT FLASHLIGHT WAS INOPERATIVE. RESEATED THE FLASHLIGHT IAW AMM 33-00-00.
Part: INTEGRATOR — FAULTY (RT WING SLIDE) · airframe 97,603 hrs · 15,642 cycles
RIGHT OUTWARD SLIDE ESCAPE SYSTEM INTEGRATOR INOPERATIVE, WOULD NOT ADJUST. REPLACED RIGHT WING OUTWARD SLIDE ESCAPE SYSTEM INTEGRATOR IAW AMM 25-65-12. OPS CHECKED OK. AIRCRAFT WAS GROUNDED.
Part: SWITCH — FAULTY (RT OVRWG SLIDE) · airframe 97,603 hrs · 15,642 cycles
RIGHT OVERWING SLIDE, AFT HATCH FOWARD SWITCH FAULTY. MAINTENANCE REPLACED THE SWITCH S621 IAW MM 25-65-15, AND PERFORMED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.
Part: LATCH — FAULTY (RT WING SLIDE) · airframe 97,603 hrs · 15,642 cycles
ACTUATOR LATCH (3125400-10) BAD AT RIGHT WING SLIDE IAW AMM 25-65-11. REPLACED ACTUATOR LATCH IAW AMM 25-65-11 STEP E (1). AIRCRAFT WAS GROUNDED.
Part: ACTUATOR — FAULTY (RT WING SLIDE) · airframe 97,603 hrs · 15,642 cycles
AFT SLIDE ACTUATOR BAD AT RIGHT WING SLIDE IAW AMM 25-65-10 G (1) AND (2). REPLACED AFT SLIDE ACTUATOR FOR RIGHT SLIDE IAW AMM 25-65-10. AIRCRAFT WAS GROUNDED.
Part: ACTUATOR — FAULTY (RT WING SLIDE) · airframe 97,603 hrs · 15,642 cycles
FORWARD SLIDE ACTUATOR BAD AT THE RIGHT WING SLIDE IAW AMM 25-65-10 G (1) AND (2). REPLACED FORWARD SLIDE ACTUATOR IAW AMM 25-65-10 CONT G (1) AND G (2). AIRCRAFT WAS GROUNDED.
Part: CABLE — FAULTY (RT OVRWG SLIDE) · airframe 97,603 hrs · 15,642 cycles
RIGHT OVERWING SLIDE CABLE FROM BOTTLE TO SLIDE FAULTY. REPLACED THE SLIDE INFLATION CABLE IAW AMM 25-65-04. AIRCRAFT WAS GROUNDED.
Part: DISPLAY — FAULTY (COCKPIT) · airframe 97,158 hrs · 15,563 cycles
AIRCRAFT WAS GROUNDED: ON FLAP RETRACTION AT FLAPS UP HANDLE POSITION, THE LEADING EDGE FLAP DISAGREE WARNING ILLUMINATED. EMERGENCY DECLARED, AIR RETURN TO DEPARTURE, FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CENTRALIZED FAULT DISPLAY INTERFACE (CFDIU) AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW MM 309-04.
Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 96,588 hrs · 15,462 cycles
AFT LAVATORY SMOKE DETECTOR WENT OFF. FALSE ALARM. REPLACED LAVATORY SMOKE DETECTOR IAW AMM 26-13-01. SYSTEM CHECKED NORMAL.
Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 96,490 hrs · 15,444 cycles
R4 DOOR FLASHLIGHT UNDER FLIGHT ATTENDANT SEAT FAILED TO OPERATE DURING TEST. REPLACED THE FLASHLIGHT BATTERY IAW AMM 25-60-00.
Part: FLASHLIGHT — UNSECURE (CABIN) · airframe 96,490 hrs · 15,444 cycles
FLASHLIGHT UNDER AFT GALLEY RIGHT FLIGHT ATTENDANT SEAT FAILED AN OPS CHECK. FLASHLIGHT SECURED IN CRADLE IAW AMM 25-60-00.
2017
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 96,034 hrs · 15,364 cycles
AIRCRAFT WAS NOT GROUNDED. LAVATORY M1 SMOKE DETECTOR ALARM WENT OFF AGAIN DURING FLIGHT, NO SMOKE DETECTED. REMOVED AND REPLACED SMOKE DETECTOR ASSEMBLY PER AMM 26-13-01. OPERATIONAL CHECK GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 96,018 hrs · 15,362 cycles
SMOKE DETECTOR IN THE LEFT AFT LAVATORY WENT OFF SEVERAL TIMES WITH NO SMOKE EVIDENT. ACCOMPLISHED LAVATORY SMOKE DETECTOR TEST IAW AMM 26-13-00. OPS CHECKED GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 96,018 hrs · 15,362 cycles
SMOKE DETECTOR IN THE LEFT MID LAVATORY WENT OFF SEVERAL TIMES WITH NO SMOKE EVIDENT. ACCOMPLISHED A LAVATORY SMOKE DETECTOR TEST IAW AMM 26-13-00. OPS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 95,950 hrs · 15,352 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE AT FORWARD FACING SEAT LEFT HAND SIDE FLIGHT ATTENDANT JUMP SEAT BY MID GALLEY. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY AT FORWARD FACING SEAT LEFT HAND SIDE FLIGHT ATTENDANT JUMP SEAT BY MID GALLEY IAW 25-64-00.
Part: SOCKET — INOPERATIVE (EXTERIOR) · airframe 95,846 hrs · 15,334 cycles
AIRCRAFT WAS NOT GROUNDED. EXTERIOR EMERGENCY EXIT LIGHT AT THE LEFT AFT ENTRY DOOR IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY (SOCKET) AT L397 PER AMM 33-51-06. OPERATIONAL CHECK GOOD.
Part: ELECTRONIC UNIT — MALFUNCTIONED (SLAT/FLAP SYS) · airframe 95,731 hrs · 15,316 cycles
LEADING EDGE FLAPS DISAGREE INDICATION. EMERGENCY DECLARED. RETURNED TO DEPARTURE, LANDING UNEVENTFUL. REMOVED AND REPLACED FLAP/SLAT ELECTRONICS UNIT IAW AMM 27-51-01. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 95,666 hrs · 15,301 cycles
FORWARD GALLEY FLIGHT ATTENDANT FLASHLIGHT WAS INOPERATIVE. THE BATTERY WAS REPLACED IAW AMM 25-61-00.
Part: SMOKE DETECTOR — FALSE INDICATION (MID LAVATORY) · airframe 95,460 hrs · 15,267 cycles
THE SMOKE DETECTOR IN THE M1 MID LAVATORY LEFT SIDE, HAD AN ALERT INFLIGHT AND REPEATED AFTER LANDING. NO EVIDENCE OF SMOKE. ACCOMPLISHED FIM 26-13-00-815-806. CLEANED THE SMOKE DETECTOR AS A PRECAUTION IAW AMM 26-13-01. OPS CHECKED GOOD.
Part: SHROUD — MISSING (CABIN) · airframe 95,396 hrs · 15,259 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 21H HAS A MISSING LENS AND SHROUD. INSTALLED LENS (AALA201709129007) AND SHROUD PER AMM 33-60-98. OPERATIONAL CHECK GOOD.
Part: LENS — MISSING (CABIN) · airframe 95,396 hrs · 15,259 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 21H HAS A MISSING LENS AND SHROUD. INSTALLED LENS AND SHROUD (AALA201709129030) PER AMM 33-60-98. OPERATIONAL CHECK GOOD.
Part: WINDOW SHADE — BROKEN (CABIN) · airframe 95,244 hrs · 15,227 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SEAT 21A WINDOW SHADE IS BROKEN. REMOVED AND REPLACED WINDOW SHADE ASSEMBLY PER AMM 52-21-01 AND AMM 25-21-10. OPERATIONAL CHECK GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 94,895 hrs · 15,163 cycles
AIRCRAFT WAS NOT GROUNDED. AFT LAVATORY SMOKE DETECTOR ACTIVATED. NO SMOKE OBSERVED. RESET SMOKE DETECTOR PER AMM 26-13-00. OPERATIONAL CHECK GOOD.
Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 94,386 hrs · 15,068 cycles
EMERGENCY EXIT SIGN AT SEAT 20H IS MISSING. REPLACED EXIT SIGN. OPERATIONAL CHECKED GOOD.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 94,357 hrs · 15,062 cycles
OVERHEAD EMERGENCY EXIT LIGHT RIGHT SIDE NEAR ROW 20 HAS A MISSING LENS. REPLACED THE LENS. OPERATIONAL CHECKED GOOD.
Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 94,267 hrs · 15,050 cycles
EMERGENCY EXIT SIGN AT SEAT 20D IS NOT SECURE. INSTALLED EXIT SIGN LENS. OPERATIONAL CHECKED GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 94,242 hrs · 15,045 cycles
AIRCRAFT WAS NOT GROUNDED. SMOKE DETECTOR ALARM IN AFT LAVATORY A5 INITIATED WITHOUT SMOKE DETECTED. ACCOMPLISHED LAVATORY SMOKE DETECTION CHECK IAW AMM 26-13-00. OPERATIONAL CHECK GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 94,242 hrs · 15,045 cycles
AIRCRAFT WAS NOT GROUNDED. SMOKE DETECTOR ALARM IN MID LAVATORY M1 INITIATED WITHOUT SMOKE DETECTED. ACCOMPLISHED LAVATORY SMOKE DETECTION CHECK IAW AMM 26-13-00. OPERATIONAL CHECK GOOD.
Part: INDICATOR — FAILED (COCKPIT) · airframe 94,058 hrs · 15,011 cycles
AIRCRAFT WAS GROUNDED. MIA-DFW FLIGHT ABORTED TAKE-OFF AT 90 KNOTS DUE TO CAPTAIN AIRSPEED INDICATOR FAILED. ACCOMPLISHED INERTIAL REFERENCE SYSTEM CHECK IAW AMM 34-21-00, AIR DATA COMPUTING SYSTEM CHECK IAW AMM 34-12-00, AND CAPTAIN/FIRST OFFICER AIRSPEED CHECK IAW AMM 34-11-00. ALL OPERATIONAL CHECKS GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,868 hrs · 14,980 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. LEFT EXTERIOR EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY AT M736 IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,868 hrs · 14,980 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS AT SEATS 20HJ AND 21HJ AND OVERWING EXIT SIGNS FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY AT M1209 IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 93,868 hrs · 14,980 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO INTERCOSTAL CORRODED ON TOP FLANGE AROUND THE NUTPLATE AT FUSELAGE STATION 527 RBL11. REMOVED AND REPLACED INTERCOSTAL BETWEEN FUSELAGE STATIONS 522 AND 544 IAW AARD 51-00-05-1 AND DRAWINGS 143T5010 AND 451T2601.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,868 hrs · 14,980 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. AFT CARGO COMPARTMENT WEB AT FUSELAGE STATION 1280 LBL19 IS CORRODED. REMOVED AND REPLACED WEB IAW AARD 53-60-53-01.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,868 hrs · 14,980 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. FORWARD CARGO INTERCOSTAL CORRODED ON TOP FLANGE AROUND THE NUTPLATE AT FUSELAGE STATION 505 RBL11. REMOVED AND REPLACED INTERCOSTAL BETWEEN FUSELAGE STATIONS 505 AND 522 IAW AARD 51-00-05-1 AND DRAWINGS 143T5010 AND 451T2601.
Part: INTERCOSTAL — CRACKED (BS 327-347) · airframe 93,868 hrs · 14,980 cycles
CRACKED INTERCOSTAL BS 327 & 347, 49 INCHES INBOARD OF L1 DOOR. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02.
Part: INTERCOSTAL — CRACKED (BS 390-412) · airframe 93,868 hrs · 14,980 cycles
CRACKED INTERCOSTAL BS 390 & 412, RIGHT SIDE INBOARD OF RBL 45.5. REMOVED AND REPLACED INTERCOSTAL ANGLE IAW SRM 51-10-02.
Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 93,868 hrs · 14,980 cycles
CORROSION ON FLOORBEAM UPPER ANGLE AT BS 1480 BETWEEN RBL 68 TO RBL 78. REPLACED UPPER ANGLE IAW SRM 53-00-51-2R.
Part: LENS — DETACHED (CABIN) · airframe 93,722 hrs · 14,955 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT R4 DOOR FLOOR LEVEL HAS A DETACHED LENS COVER. SECURED LENS COVER IAW AMM 33-51-09. OPERATIONAL CHECK GOOD.
Part: FLASHLIGHT — UNSERVICEABLE (CABIN) · airframe 93,599 hrs · 14,933 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MID GALLEY LEFT SIDE AFT FACING REQUIRES REPLACEMENT. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 25-25-03. OPERATIONAL CHECK GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 93,353 hrs · 14,884 cycles
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DURING FLIGHT AN EICAS AMBER ANTISKID MESSAGED GENERATED ACCOMPANIED BY ILLUMINATION OF THE OVERHEAD AMBER ANTISKID LIGHT. ACCOMPLISHED WIRING CHECK OF NR 6 AND NR 7 WHEEL TRANSDUCER TO ANTISKID/AUTOBRAKE CONTROLLER IAW WDM 32-42-11 AND ANTISKID SYSTEM OPERATIONAL TEST IAW AMM 32-42-00-715-001. NO FAULTS FOUND. SYSTEM CHECKS NORMAL.
2016
Part: PANEL — LOOSE (CABIN) · airframe 92,767 hrs · 14,782 cycles
EMERGENCY EXIT SIGN PANEL ABOVE SEAT 21A LOOSE. SECURED PANEL IAW AMM 25-65-00. OPERATIONAL CHECK GOOD.
Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 92,629 hrs · 14,759 cycles
AIRCRAFT NOT GROUNDED. DURING DESCENT THE AFT RIGHT LAVATORY SMOKE DETECTOR AURAL WARNING SOUNDED UNTIL MANUALLY DISABLED. NO EVIDENCE OF SMOKE. REMOVED AND REPLACED SMOKE DETECTOR IAW AMM 26-13-01. OPERATIONAL CHECK GOOD.
Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 92,027 hrs · 14,675 cycles
BOTH WEATHER RADAR FAILED IN FLIGHT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DESTINATION WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED WEATHER RADAR TRANSCEIVER IAW MM 34-43-01, ALL TESTS NORMAL.
Part: COMPRESSOR — LEAKING (RT ENGINE) · airframe 89,972 hrs · 14,299 cycles
AFTER TAKEOFF, ACFT BLEED AIR PACK GAVE OFF ACRID & DIRTY SOCK ODOR. THE FLIGHT CONTINUED & LANDED WITHOUT FURTHER INCIDENT. NO EMER WAS DECLARED. ENG RUNS DETERMINED ODOR COMING FROM RT ENG. ACCOMPLISHED A BORESCOPE OF RT ENG & FOUND OIL IN 8TH STAGE COMPRESSOR SECTION. CHANGING RT ENG. THE ACFT WAS GNDED. REPLACED NR 2 ENG IAW MCM & AMM 71-93-61. ACCOMPLISHED PACK BURN IAW AMM 21-00-21 & CARD 05-96-40. NO ODOR NOTED.
2015
Part: ANTENNA — FAULTY (WEATHER RADAR) · airframe 89,418 hrs · 14,194 cycles
AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. ACFT WAS GNDED. DURING CLIMB WEATHER RADAR FAILED. R & R WEATHER RADAR ANTENNA ASSEMBLY IAW AMM 34-43-05. SYS CHECKED NORMAL.
Part: LIGHT — BROKEN (CABIN) · airframe 89,256 hrs · 14,160 cycles
32B SEAT MOUNTED EMER LIGHT IS BROKEN. R & R SEAT MOUNTED EMER LIGHT AT 32B IAW 33-51-10. SYS CHECKED NORMAL.
Part: WEB — DAMAGED (FUSELAGE) · airframe 88,882 hrs · 14,105 cycles
FOUND DAMAGE TO THE WEB IN AFT CARGO, AT STATION 1300, RBL 12. INSTALLED WEB REPAIR IAW EA 254861 & SRM 51-70-13-0G.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 88,882 hrs · 14,105 cycles
INTERCOSTAL CRACKED AT STATION 1300. R & R INTERCOSTAL IAW AARD 53-60-53-1.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 88,882 hrs · 14,105 cycles
FLIGHT DECK DOOR EMER LIGHT DID NOT STAY ILLUMINATED FOR 10 MINUTES IAW WC 0357. REPLACED LIGHT ASSEMBLY.
Part: UNKNOWN — ODOR (COCKPIT) · airframe 88,685 hrs · 14,068 cycles
EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT, CREW DETECTED A RUBBERY SMOKE SMELL IN THE COCKPIT ONLY. THE SMOKE SMELL DISSIPATED AFTER A FEW MINUTES. PERFORMED INSPECTION IAW CARD 05-96-70 & AMM TASK 05-51-56-20 2-001. NO ABNORMALITIES OR ODOR OBSERVED. ALSO CHECKED FWD EQUIPMENT COOLING FANS, EXHAUST FAN & SUPPLEMENTAL HEATING. SYS CHECKED NORMAL.
Part: HOLDER — INOPERATIVE (EXTERIOR LIGHT) · airframe 88,499 hrs · 14,041 cycles
2ND EXTERNAL EMER LIGHT AFT OF LT WING IS INOPERATIVE. R & R LAMP HOLDER ASSEMBLY IAW 33-51-06. SYS CHECKED NORMAL.
Part: NUT PLATE — BROKEN (ZONE 100) · airframe 88,882 hrs · 14,105 cycles
AIRCRAFT RECEIVED WITH FMR FOR MISSING FASTENER FOR EMER LIGHT LENS SPEED TAPE APPLIED. FOUND BROKEN NUTPLATE FOR LENS, REPLACED LIGHT AT LC.
Part: ANTI-ICE VALVE — FAULTY (RIGHT) · airframe 87,376 hrs · 13,867 cycles
RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED WITH EICAS MSG WHEN SELECTED ON. EMERGENCY DECLARED & FLIGHT LANDED WITHOUT INCIDENT. R & R RT ENG OUTLET TAI VALVE IAW AMM 30-21-03. GOOD LEAK & OPERATIONAL CHECK.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 86,831 hrs · 13,774 cycles
SEAT MOUNTED EMER PATH LIGHTS INOPERATIVE AT SEATS 32AB & 33AB. SECURED SEAT 32 & 33AB EMER LIGHTS CONNECTOR. PERFORMED OPERATIONAL CHECK SEAT 32 & 33AB IAW AMM 33-51-10. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,596 hrs · 13,737 cycles
21H SEAT MOUNTED RED EMER LIGHT HAS 1 BULB INOPERATIVE. RELAMPED SEAT MOUNTED EMER LIGHT AT SEAT 21H IAW AMM 33-51-10. OPERATIONS CHECKED NORMAL.
Part: LENS — LOOSE (EXIT SIGN) · airframe 86,596 hrs · 13,737 cycles
20G AISLE OVERHEAD EXIT SIGN LENS IS LOOSE. SECURED IN PLACE. OPERATIONS CHECKED NORMAL IAW AMM 33-51-01.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 86,596 hrs · 13,737 cycles
L4 DOOR EMER EXIT LIGHT OUTSIDE INOPERATIVE. RELAMPED L4 DOOR EMER EXIT LIGHT. TESTED IAW AMM 33-51-06. OPERATIONS CHECKED OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,596 hrs · 13,737 cycles
27H SEAT MOUNTED EMER LIGHT HAS 1 BULB INOPERATIVE. RELAMPED SEAT MOUNTED EMER LIGHT AT SEAT 27H IAW AMM 33-51-10. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,596 hrs · 13,737 cycles
21H SEAT MOUNTED EMER LIGHT HAS 1 BULB INOPERATIVE. RELAMPED SEAT MOUNTED EMER LIGHT AT SEAT 21H IAW AMM 33-51-10. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,596 hrs · 13,737 cycles
ONE LAMP OUT AT SEAT MOUNTED EMER PATH LIGHT, SEAT 37B. REPLACED LIGHT ASSEMBLY & TESTED IAW AMM 33-51-10. OPERATIONS CHECKED OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,596 hrs · 13,737 cycles
26H SEAT MOUNTED EMER LIGHT HAS 1 BULB INOPERATIVE. RELAMPED SEAT MOUNTED EMER LIGHT AT 26H IAW AMM 33-51-10. OPERATIONS CHECKED NORMAL.
Part: LENS — LOOSE (CABIN) · airframe 86,596 hrs · 13,737 cycles
1R EMER LIGHT IN DOOR JAM, LENS IS LOOSE. SECURED IN PLACE. OPERATIONS CHECKED NORMAL IAW AMM 33-51-03.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,596 hrs · 13,737 cycles
M1 LAVATORY AISLE EMER LIGHT AT FLOOR LEVEL HAS 1 BULB INOPERATIVE. RELAMPED M1 LAVATORY AISLE EMER LIGHT IAW AMM 33-51-10. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 86,596 hrs · 13,737 cycles
LEFT FWD OVERWING EXIT IDENTIFIER SIGN HAS 1 BULB INOPERATIVE. RELAMPED LT FWD OVERWING EXIT IDENTIFIER SIGN IAW AMM 33-51-09. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,596 hrs · 13,737 cycles
36B SEAT MOUNTED EMER LIGHT HAS 1 BULB INOPERATIVE. RELAMPED SEAT MOUNTED EMER LIGHT AT SEAT 36B IAW AMM 33-51-10. OPERATIONS CHECKED NORMAL.
Part: LENS — LOOSE (CABIN) · airframe 86,596 hrs · 13,737 cycles
1L DOOR EXIT HANDLE LENS IS LOOS. SECURED LENS IN PLACE. OPERATIONS CHECKED NORMAL IAW AMM 33-51-10.
2014
Part: SKIN — CORRODED (FUSELAGE) · airframe 84,306 hrs · 13,355 cycles
CORROSION ON INNER SKIN AT STATION 1090 BETWEEN STRINGERS 38 & 39 LT. INNER SKIN WAS REPAIRED IAW EA B767-53-035186.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 84,306 hrs · 13,355 cycles
LEFT WING UPPER WING TO BODY SKIN, LOCATED APPROX 15 INCHES AFT OF AFT OVERWING EXIT DOOR CUT OUT HAS LIGHT CORROSION. ACCOMPLISHED REPAIR IAW EA B767-57-035117.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 84,306 hrs · 13,355 cycles
LEFT WING UPPER SKIN HAS AREA OF CORROSION OTBD OF WING TO BODY CHORD FWD OF REAR SPAR, APPROX 27 INCHES AFT OF AFT EMER EXIT. ACCOMPLISHED REPAIR IAW EA B767-57-035117.
Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 84,306 hrs · 13,355 cycles
FLOOR PANEL JUST INSIDE & UNDER SILL PLATE HAS AREAS OF CORROSION. INSTALLED NEW FLOOR PANEL INSIDE & JUST UNDER BULK CARGO DOOR THRESHOLD IAW AARD 51-00-05-1.
Part: ANGLE — CORRODED (BS 1420-1424) · corrosion level 2 · airframe 84,306 hrs · 13,355 cycles
BULK CARGO DOOR LOWER THRESHOLD INSIDE THE FWD LIGHTNING HOLE, L ANGLE ON THE INBD SIDE TOP EDGE IS CORRODED THROUGH, 4 INCHES LONG BETWEEN BS 1420 & 1424. INSTALLED NEW ANGLE IAW AARD 51-00-05-1.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 84,306 hrs · 13,355 cycles
EXTERIOR EMERGENCY LIGHT AT RT NR 4 DOOR FAILED TO ILLUMINATE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR 4 DOOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 84,306 hrs · 13,355 cycles
EXTERIOR EMERGENCY LIGHT AT LT NR 1 DOOR FAILED TO ILLUMINATE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR 1 DOOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,306 hrs · 13,355 cycles
OVERHEAD EMERGENCY LIGHT ABOVE LT FLIGHT ATTENDANTS SEAT IN AFT GALLEY FAILED TO ILLUMINATE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT ABOVE LT FLIGHT ATTENDANTS SEAT IN AFT GALLEY. OPERATIONS CHECKED NORMAL.
Part: BEAM — DAMAGED (LT WING) · airframe 84,306 hrs · 13,355 cycles
LEADING EDGE NOSE BEAM STIFFENER OF FIXED LE JUST INBD OF RIB 36 DAMAGED WHEN WING TIP STRUCK BLAST FENCE. NOSE BEAM REPLACED WITH NEW MANUFACTURED PART IAW AARD 51-00-05-1, DWG 114T2300 & SRM 51-20-01.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 84,100 hrs · 13,320 cycles
EMERGENCY LIGHT AT SEAT 23H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 23H, OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 84,100 hrs · 13,320 cycles
EMERGENCY LIGHT AT SEAT 22H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 22H, OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 84,100 hrs · 13,320 cycles
EMERGENCY LIGHT AT SEAT 24H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 24H, OPERATIONS CHECKED NORMAL.
Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 83,767 hrs · 13,255 cycles
DFW CREW REPORTED WX RADAR FAILED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WX RADAR TRANSCEIVER. SYS GND CHECKED NORMAL OPERATION CLOSED.
2013
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 83,170 hrs · 13,163 cycles
LT SIDE EXTERIOR NR 7 FUSELAGE MOUNTED EMERGENCY EXIT ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR LT SIDE EXTERIOR NR 7 FUSELAGE MOUNTED EMERGENCY EXIT ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 83,170 hrs · 13,163 cycles
RT SIDE EXTERIOR NR 7 FUSELAGE MOUNTED EMERGENCY EXIT ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR RT SIDE EXTERIOR NR 7 FUSELAGE MOUNTED EMERGENCY EXIT ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.
Part: SENSOR — INOPERATIVE (LT ENGINE) · airframe 81,681 hrs · 12,901 cycles
CREW REPORTED LT ENGINE EXCEEDED THROTTLE SPLIT. REPLACED T2 SENSOR. SYSTEM GROUND CHECKED NORMAL.
2012
Part: SKIN — DEBONDED (TE FLAP) · airframe 78,715 hrs · 12,430 cycles
LEFT OUTBOARD FLAP LOWER SURFACE DISBONDED. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.
Part: ACTUATOR — LEAKING (SPOILER) · airframe 78,629 hrs · 12,414 cycles
LAX - CREW REPORTED DURING CLIMBOUT, CENTER HYDRAULIC SYSTEM PRESSURE EICAS MESSAGE AND LIGHT. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER NINE SPOILER ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: PORTABLE LIGHT — INOPERATIVE (COCKPIT) · airframe 76,942 hrs · 12,161 cycles
COCKPIT PORTABLE EMERGENCY LIGHT INOPERTAIVE. REPLACED LAMP FOR COCKPIT PORTABLE EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,942 hrs · 12,161 cycles
RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,947 hrs · 12,009 cycles
OVERHEAD EMERGENCY LIGHT BY SEAT 40G INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT BY SEAT 40G. OPS CHECK NORMAL.
Part: CONNECTOR — LOOSE (CABIN) · airframe 75,947 hrs · 12,009 cycles
SEAT 5H EMERGENCY LIGHT INOPERATIVE. SECURED LOOSE CONNECTOR FOR SEAT 5H EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LENS — MISSING (CABIN) · airframe 75,947 hrs · 12,009 cycles
OVERHEAD EMERGENCY LIGHT AT ROW 26G MISSING LENS. REPLACED LENS FOR OVERHEAD EMERGENCY LIGHT AT ROW 26G. OPS CHECK NORMAL.
Part: WIRE — DAMAGED (LE SLAT) · airframe 75,437 hrs · 11,930 cycles
MIA - CREW REPORTED SLATS WOULD NOT RETRACT. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPAIRED WIRE AT 5303 RIGHT OUTBOARD SLAT NUMBER 9 INBOARD PROXIMITY SWITCH STATION 581. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 75,138 hrs · 11,882 cycles
ORD - CREW REPORTED LEADING EDGE SLAT DISAGREE ON EICAS. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONICS UNIT AS A PRECAUTION. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 72,815 hrs · 11,543 cycles
CORROSION ON HORIZONTAL STABILIZER CENTER SECTION UPPER SKIN AT 3 LOCATIONS BETWEEN STRINGERS 11 AND 8 AND RIGHT BUTTLINES 13 AND 32. INSTALLED TWO EXTERNAL DOUBLERS PER EA B767-55-017172.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 72,815 hrs · 11,543 cycles
CORROSION WAS FOUND ON THE FORWARD CARGO DOOR LOWER SILL OUTER CHORD VERTICAL LEG AT STATION 568. REMOVED CORROSION BY BLENDING AND ACCOMPLISHED HFEC INSPECTION, APPLIED ALODINE, TWO COATS OF PRIMER TO THE REPAIR AREA PER 767-300 SRM. APPLIED CIC TO REPAIR AREA PER EA B767-53-017173.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 72,815 hrs · 11,543 cycles
CORROSION WAS FOUND AT STATION 325 FLOORBEAM UPPER CAP HORIZONTAL FLANGE UPPER SURFACE. THE AREAS OUT OF LIMITS WERE AT LEFT BUTTLINES 8.75, 17, 21.5 AND RIGHT BUTTLINES 17.25, 22.5, AND 26.5. REMOVED ALL CORROSION PER 767-300 SRM AND FABRICATED REPAIR STRAPS PER EA B767-53-017250.
Part: ACTUATOR — LEAKING (SPOILER) · airframe 71,883 hrs · 11,400 cycles
SDQ - INFLIGHT PAP-MIA. CREW REPORTED CENTER HYDRAULIC SYSTEM FAILED INFLIGHT. FLAPS WOULD ONLY EXTEND TO 1 DEGREE. EMERGENCY DECLARED FLIGHT DIVERTED SDQ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 9 SPOILER ACTUATOR LEAKING AT BLUE PLUG WITH O-RING STICKING OUT. REPLACED SPOILER ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SHUTOFF VALVE — LEAKING (RT WING) · airframe 71,830 hrs · 11,389 cycles
MIA - CREW REPORTED LOW CENTER HYDRAULIC FLUID QUANTITY. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK COMING FROM THE RIGHT WING FLAP/SLAT SHUTOFF VALVE MODULE LOCATED AT THE REAR WHEEL WELL INBOARD SIDE. REPLACED MODULE. SYSTEM GROUND CHECK NORMAL OPERATION.
2009
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 66,552 hrs · 10,482 cycles
RIGHT CENTER AISLE FLIGHT ATTENDANT FLASHLIGHT HAS BROKEN STRAP. REPLACED FLASHLIGHT BATTERY AND SECURED STRAP.
2008
Part: LIGHT — DAMAGED (CABIN) · airframe 63,136 hrs
EMERGENCY LIGHT AT SEAT 27H DAMAGED. REPLACED LIGHT ASSEMBLY AT SEAT 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
Part: LIGHT — DAMAGED (SEAT 2B) · airframe 61,724 hrs
JFK EMERGENCY LIGHT AT SEAT 2B DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
Part: LENS — MISSING (CABIN) · airframe 83,805 hrs
DFW EMERGENCY LIGHT AT RT HAND AFT OVERWING MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RT HAND AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)
Part: LENS — MISSING (CABIN) · airframe 83,805 hrs
DFW EMERGENCY LIGHT AT SEAT 21B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,805 hrs
DFW EMERGENCY LIGHT AT SEAT 21B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)
Part: LIGHT — WRONG PART (CABIN)
DFW - EMERGENCY LIGHT AT SEAT 5B HAS WRONG LIGHT. REPLACED LED LIGHT FOR EMERGENCY LIGHT AT SEAT 5B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 59,903 hrs
CDG - EMERGENCY LIGHT ASSEMBLY AT SEAT 5B BROKEN OFF. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT ASSEMBLY AT SEAT 5B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS)
ORD - EMERGENCY EXIT LIGHT OVERHEAD COCKPIT DOOR INOPERATIVE. REPLACED LIGHT SWITCH PANEL FOR EMERGENCY EXIT LIGHT OVERHEAD COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: MOUNT — INOPERATIVE (EMERGENCY LIGHT)
ORD - EMERGENCY EXIT LIGHT OVERHEAD COCKPIT DOOR INOPERATIVE. REPLACED EXIT SIGN BASE PLATE FOR EMERGENCY EXIT LIGHT OVERHEAD COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: VALVE — OUT OF RIG (RT MLG)
MIA INFLIGHT T69/11JUN - RIGHT MAIN GEAR UNSAFE INDICATION ON APPROACH. PERFORMED GEAR CHECKLIST AND RECEIVED THREE GREEN GEAR INDICATIONS. LANDED MIA WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. FOUND RIGHT GEAR OPERATED SEQUENCE VALVE OUT OF RIG. ADJUSTED RIGHT GEAR OPERATED SEQUENCE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: PIN — BACKED OUT (LIGHT CONNECTOR)
SFO - EMERGENCY AISLE LIGHT AT SEAT ROW 34HJ INOPERATIVE. SECURED PUSHED BACK PINS AT EMERGENCY LIGHT SEAT CONNECTOR AT SEAT ROW 34HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: FAILSAFE — CORRODED (FUSELAGE)
AFW - FOUND CORROSION ON THE LOWER SURFACE OF THE LOWER MAIN SILL FAIL SAFE STRAP IN THE FORWARD CARGO AREA AT STATION 566. CORROSION WAS 2 INCHES BY 4 INCHES. BLENDED CORROSION AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION OF THE BLENDED AREA TO ENSURE IT WAS CRACK-FREE. PERFORMED OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION OF ALL FASTENER HOLES IN BLENDED AREA AND REFINISHED BLENDED AREA. REINSTALL NON-ALUMINUM FASTENERS WITH BMS595 SEALANT. RETURNED TO SERVICE WITH NOTED CONDITION.
Part: DOOR FRAME — CORRODED (FUSELAGE)
AFW - FORWARD CARGO DOOR CUTOUT LOWER OUTER CHORD HAD CORROSION BLENDED FROM VERTICAL LEG AT STATION 569. BLEND IS IN AREA OF 2.3 INCHES BY 1.1 INCH AND 0.021 INCH DEEP. BLEND OUT CORROSION AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION TO ENSURE BLENDED AREA AND FASTENER HOLES ARE CRACK-FREE. INSTALLED FREEZE PLUG DIAMETER 0.0437 INCH IN FORWARD HOLE. REFINISH THE BLENDED AREA AND ENSURE SURFACE IS FLAT FOR PROPER FASTENER INSTALLATION. REINSTALL NON-ALUMINUM FASTENERS WET WITH BMS595 SEALANT. RETURNED TO SERVICE WITH THE NOTED CONDITION.
Part: REFLECTOR — INOPERATIVE (EMERGENCY LIGHT)
DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LIGHT REFLECTOR ASSEMBLY FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: LIGHT — INOPERATIVE (CABIN)
LAX - EMERGENCY ESCAPE PATH LIGHTING AT SEAT 39H INOPERATIVE. REPLACED LAMP HOLDER ASSEMBLY FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: WIRE — LOOSE (CABIN)
SFO EMERGENCY LIGHTS AT SEATS 5HJ INOPERATIVE. REINSTALLED LOOSE WIRE FOR EMERGENCY LIGHTS AT SEATS 5HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED
Part: CONNECTOR — LOOSE (CABIN)
SFO FORWARD EMERGENCY LIGHT AT SEAT 5H INOPERATIVE. RECONNECTED LOOSE FORWARD EMERGENCY LIGHT CONNECTOR AT SEAT 5H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: O-RING — CUT (RT MLG WW)
AFT APPROX 1 HOUR OF FLIGHT CENTER HYD QTY EICAS MSG DISPLAYED. PUMPS SELECTED OFF IAW PROCEDURE STOPPED FLUID LOSS AT .40. UPON INSPECTION, FOUND DPI FOR ADP PRESS MODULE LOOSE WITH A CUT O-RING. REPLACED O-RING, NO LEAKS NOTED. SERVICED CTR HYDRAULIC QUANTITY TO FULL. (M)
2002
Part: GCU — FAILED (E/E COMPT)
MIA - FLT 68 - STARTED CYCLING ON AND OFF PRIOR TO OCEANIC ENTRY POINT AND CONTINUED FOR REMAINDER OF FLIGHT DIVERT TO MIA. REMOVED AND REPLACED LGCB AND RGBC. CHECKED GROUNDS AND GROUND WIRE BACK TO BPCU, CHECKS NORMAL. RAN ENGINES, STILL NO HELP. REMOVED AND REPLACED LT AND RT GENERATOR CONTROL UNITS PRECAUTIONARY. ACCOMPLISHED BITE OF BPCU, CHECK OK. REPLACED K10109 RELAY. RAN ENGINE, GND CHECK OK. REMOVED AND REPLACED LT GENERATOR CB AND RT GENERATOR CB. REPLACED LT AND RT GENERATOR CONTROL UNITS, REF E58 9139260 AND 9139258. (M)
Part: IDG — FAILED (LT ENGINE)
JFK - LEFT GENERATOR DRIVE LIGHT ILLUMINATED ON FINAL APPROACH TO JFK, LT GENERATOR DISCONNECTED PER FM VOL 1. RECONNECTED AND SERVICED LEFT IDG AS PER MM PERFORMED GENERATOR DRIVE SYSTEM ADJUST/TEST AS PER 24-11-00-5. OPERATIONAL CHECK NORMAL WITH NO FAULTS INDICATED. (M)
2001
Part: WIRE — INOPERATIVE (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: PIN — DAMAGED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 8A AND 8B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR PINS AT SEAT 8A AND 8B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 38A AND B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 38A AND B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - FLT 95 - BEFORE FLIGHT LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. ACCOMPLISHED INSPECTION AND TEST. UNABLE TO DUPLICATE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: CONNECTOR — DEFECTIVE (ROW 25H)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTS AT SEAT ROW 25H INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT SEAT CONNECTOR AT SEAT ROW 25H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1998
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 11H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT 11H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEATS 39A/B AND 40A/B FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 39A/B AND 40A/B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 26B FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 26B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: WIRE — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 26AB AND 29HJ INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY EXIT LIGHT CONNECTORS ON BOTH PAX SEATS 26AB AND 29HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 25H INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 25H. SYSTEM GROUND CHECKED NORMAL. (M)
1996
Part: BUS CONTL UNIT — FAILED (LT/RT ENGINE)
MIA - FLT 0911 - BOTH UTILITY BUSSES CYCLE OFF THEN ON AT ABOUT 1 MINUTE INTERVALS. TURNED OFF ALL GALLEY OVENS AND BOTH RECIRC FANS AND PROBLEM CONTINUED. TRIED USING ONE UTILITY BUS. PROBLEM CONTINUED. BOTH BUSSES TURNED OFF REMAINDER OF FLIGHT. REPLACED THE BUS CONTROL UNIT. ACCOMPLISHED ENGINES 1 AND 2 RUN-UP. LOADED LT AND RT UTILITY BUSSES, ALL CK'D NORMAL. COULD NOT DUPLICATE FAULT. PLEASE OBSERVE AND ADVISE. (X)
Part: PIN — BROKEN (PAX SEAT)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 30B INOPERATIVE. REPLACED TWO BROKEN PINS AT PASSENGER SEAT 30B EMERGENCY EXIT LIGHT CANNON PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGNCY EXIT LIGHT AT PAX SEAT 26B INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT AT PAX SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: EEL CONTACT PIN — OUT OF POSITION (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 25B INOPERATIVE. REPOSITIONED CONTACT PIN FOR PASSENGER SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL FUSE — DEFECTIVE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 20H AND 21H INOPERATIVE. REPLACED FUSE AT EMERGENCY EXIT LIGHT POWER PACK FOR PASSENGERS SEATS 20H AND 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL WIRE — LOOSE GROUND (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 32-41 INOPERATIVE. TIGHTENED LOOSE GROUND AT M734 BATTERY PACK. SYSTEM GROUND CHECKS NORMAL OPERATION. (W)
Part: EEL CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 4H INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 4H. SYSTEM GROUND CHECKS NORMAL OPERATION. (W)