N181UA
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.
391 reports on file, 1995-03-09 – 2017-08-18.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 105,703 hrs · 12,390 cycles
FOUND SEAT EEL LIGHTS DIM 33ABC-43ABC. REPLACED BATTERY PACK W6009. EFFECTED LIGHTS NOW BRIGHT. CHECKED SAFETY AND SECURITY AND VERIFIED OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 105,703 hrs · 12,390 cycles
RT UPPER DECK EMERGENCY EXIT DOOR INTERNAL AFT LIGHT INOP. RT UPPER DECK EMERGENCY EXIT DOOR INTERNAL AFT LIGHT RELAMP. OPS CHECK GOOD REF 33-51-00. CHECKED SAFETY AND SECURITY AND VERIFIED OPERATION.
Part: A/C PACK — UNKNOWN (NR 2) · airframe 105,659 hrs · 12,386 cycles
F/A REPORTED, LOUD VIBRATION FROM THE L2 DOOR THRU THE L3 DOOR. ASSOCIATED WITH ODOR, ISOLATED EACH PACK FOUND NR , A/C PACK ASSY AT FAULT, CAUSING VIBRATION. RAN THE NR 2 PACK. NO VIBRATIONS OR ODORS NOTED. NO LOOSE DUCTS FOUND. ALL PACKS EXHIBIT NORMAL FLOWS AND TEMPS. PERFORMED GROUND TEST OF RAM AIR INLETS AND EXHAUSTS, GROUND TESTS PASSED. NO CURRENT FAULTS NOTED.
Part: CHARGER — INOPERATIVE (PRESS TO TEST) · airframe 105,327 hrs · 12,355 cycles
LEFT UPPER DECK SLIDE PRESS TO TEST BULB DID NOT TEST. R & R THE BATTERY CHARGER, BATTERY CHECKED OK IAW AMM 52-23-14.
Part: BATTERY — INOPERATIVE (DOOR SLIDE) · airframe 105,327 hrs · 12,355 cycles
GREEN ARMED LIGHT AT UPPER DECK LEFT DOOR SLIDE NOT ILLUMINATING. REPLACED THE BATTERY, OPS CHECKED OK.
Part: BULB — INOPERATIVE (EMERGENCY EXIT) · airframe 105,327 hrs · 12,355 cycles
UPPER DECK LEFT EMERGENCY EXIT DOOR BATTERY CHECK LIGHT DOES NOT ILLUMINATE FOUND TEST SWITCH LIGHT BULBS OUT, REPLACED THE BULBS AND CHECKED NORMAL.
Part: LIGHT — LOOSE (R2 DOOR) · airframe 105,230 hrs · 12,346 cycles
EMERGENCY LIGHT AT THE R2 DOOR, FLOOR LEVEL IS LOOSE. SECURED THE LIGHT, OPS NORMAL.
Part: BATTERY — DISCHARGED (CABIN) · airframe 104,635 hrs · 12,287 cycles
UPPER DECK LEFT SIDE ESCAPE DOOR SLIDE LIGHT SYSTEM INOPERATIVE. INSTALLED NEW BATTERY, TEST OK INSTALLED NEW BATTERY, TEST OK. ACP INSP OF UPPER SLIDE BATTERY.
Part: FUSE — INOPERATIVE (POWER SUPPLY) · airframe 104,617 hrs · 12,285 cycles
TWO LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE FUSE IN THE POWER SUPPLY M7919 IAW WDM 33-51-42.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 104,617 hrs · 12,285 cycles
EMERGENCY LIGHT IN CEILING AT ROW 49C IS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-07.
Part: BATTERY — DISCHARGED (CABIN) · airframe 104,608 hrs · 12,284 cycles
UPPER DECK EXIT DOOR LT SIDE BATTERY LIGHT INOP. REPLACED BATTERY ASSEMBLY PER AMM 33-51-04, SYSTEM WORKS NORMALLY. LIGHT OPS CHECKS OK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 104,608 hrs · 12,284 cycles
UPPER DECK SLIDE LIGHT (RIGHT SIDE) INOPERATIVE. REPLACED FWD BATTERY, OPS CKED OK.
Part: SLIDE — UNSECURE (L5 DOOR) · airframe 104,545 hrs · 12,278 cycles
FA REPORTED SLIDE BUSTLE COVER AT DOOR 5L DETACHED, FOUND SLIDE BECAME UNPACKED BUT NOT INFLATED. REPLACED DR 5L SLIDE ASSY PER MM 25-69-01. RESECURED SLIDE BUSTLE AT DR 5L.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 104,312 hrs · 12,256 cycles
35AC 40AC SEAT EMER LT INOP. REPLACE 35AC 40AC SEAT EMER LT ASSY AND C/O OP CHK FOUND ''STATIC'' REF TO AMM 33-51-12-332-001-002 REV 87.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 104,160 hrs · 12,241 cycles
UPPER DECK LT EMERGENCY LIGHT BATTERY NOT TESTING REPLACED LT BATTERY PACK REF 52-23-14-401. OPS CK GOOD PERFORMED IDT INSPECTION PER GMM AND AMM 52-23-14-401.
Earlier reports · 1995–2016 · 376 reports
2016
Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,621 hrs · 12,185 cycles
DOOR 3 LEFT, DOOR MOUNTED SLIDE LIGHT FAILED TO ILLUMINATE DURING EMERGENCY LIGHTS TEST. REF "A" CHECK JOB CARD 74-3351-1-7105. RELAMPED AND DOOR MOUNTED EMERGENCY LIGHT TEST GOOD AT DOOR 3L PER AMM TASK 33-51-06-962-040.
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 102,625 hrs · 12,090 cycles
EMERGENCY EXIT LIGHT COMING OUT OF WALL BY LAVATORY 101. INSTALLED THE COVER, OPS GOOD
Part: POWER SUPPLY — INOPERATIVE (DOOR) · airframe 101,190 hrs · 11,951 cycles
EMERGENCY POWER SYS BATTERY WILL NOT TEST ON BOTH UPPER DECK DOORS. REPLACED LT POWER SUPPLY & RT BATTERY IAW AMM 52-23-14. BOTH LIGHTS CHECKED NORMAL.
2015
Part: WIRE — SEVERED (CABIN) · airframe 100,098 hrs · 11,847 cycles
EMERGENCY EXIT LIGHT INOPERATIVE AT 42KJH. FOUND WIRE SEVERED JUST BEFORE EEL LAMP CONNECTOR. INSTALLED NEW CONNECTOR ON 42HJK. EEL CHECKED GOOD.
Part: WIRE — SEVERED (CABIN) · airframe 100,098 hrs · 11,847 cycles
EMERGENCY EXIT LIGHT INOPERATIVE AT 42KJH. FOUND WIRE SEVERED JUST BEFORE EEL LAMP CONNECTOR. INSTALLED NEW CONNECTOR ON 42HJK. EEL CHECKED GOOD.
Part: UNKNOWN — ODOR (CABIN) · airframe 99,989 hrs · 11,834 cycles
ON THRUST REDUCTION TO SLOW SMELL, HAZE FILLED WHOLE AIRPLANE. SET OFF ALL LAVATORY SMOKE DETECTORS. AIR COND PACKS, WATER SEPARATOR, COALESCE BAGS & UPPER, LOWER RE-CIRCULATION FILTERS REPLACED IAW MM 05-51-56, ALSO PNEUMATIC SYS OIL CONTAMINATION REMOVED.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 99,547 hrs · 11,793 cycles
FUSELAGE SKIN PITTING, STATION 1700 - 1720, STRINGER 46L - 46R. REPAIRED IAW ECRA 5330-05392 REV PART 1.1.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 99,547 hrs · 11,793 cycles
CARRIED OUT REPAIR FOR LT MED NR 5 DOOR, AFT CUT OUT UPPER CORNER SKIN IAW EA5331-01798 OP 9 & ECRA 5330-05403. CREATED CF IAW ECRA 5330-05403 REV, MF6345 CREATED TO MONITOR & MF6345 ADDED TO MONITOR.
Part: SKIN — CRACKED (NR 1 PYLON) · airframe 99,547 hrs · 11,793 cycles
NUMBER 1 PYLON INBD SKIN AT 452ER DOOR CUT OUT CRACKED. PERMANENT REPAIR ACCOMPLISHED ON ECRA 5430-02049.
Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 99,547 hrs · 11,793 cycles
NUMBER 1 RT DOOR SILL UPPER WEB CRACKED. REPAIR ACP IAW ECRA 5310-06618 REV A.
Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 99,547 hrs · 11,793 cycles
NUMBER 1, LT MED DOOR UPPER SILL WEB CRACKED. REPAIR COMPLIED WITH IAW ECRA 5310-0 6618 REV A.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 97,463 hrs · 11,605 cycles
OVERWING 2 FWD EXTERIOR EEL INOPERATIVE. REPLACE POWER SUPPLY BATTERY & PICO FUSE ON LT EXTERIOR EEL 2 FWD. CHECKED GOOD IAW AMM 33-51-03.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,463 hrs · 11,605 cycles
EMERGENCY EXIT LIGHT STRIP ROW 19ABC, ROW 57HJK INOPERATIVE. REPLACE EEL STRIP ON 19ABC, 57HJK. CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,097 hrs · 11,572 cycles
G5 GALLEY RT EMER LIGHT ASSEMBLY INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPERATIONS CHECKED OK.
Part: SKIN — WORN (FUSELAGE) · airframe 97,097 hrs · 11,572 cycles
EXT FUSE SKIN BS 2280 - 2417 & 2517 - 2638 LT & RT SIDES AT VERTICAL STAB BLADE SEAL INTERFACE, WEAR DAMAGE EXCEEDS SRM LIMITS. NDT, NO CRACKS NOTED. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5330-05073.
Part: CONNECTOR — BROKEN (CABIN) · airframe 97,097 hrs · 11,572 cycles
CABIN 10AB & 10HK SEAT CABLE REMOVED FOUND EMER LIGHT PLUG BROKEN. REPLACED CABIN 10AB & 10HK SEAT CABLE PLUG. EMER LIGHT TEST FOUND PASSED IAW AMM 33-51 -00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,097 hrs · 11,572 cycles
CABIN EMER LIGHT TEST FOUND SEAT 57HK LIGHT INOPERATIVE. REPLACED CABIN EMER LIGHT & LIGHT TEST FOUND PASSED IAW AMM 33-51-00.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 97,097 hrs · 11,572 cycles
FORWARD PIT BS 560 FLOORBEAM CORROSION RBL 50 - 60 ON UPPER CHORD. REMOVED DAMAGE & INSTALLED REPAIR PARTS IAW SRM 51-40-02.
Part: LIGHT — BROKEN (CABIN) · airframe 97,038 hrs · 11,566 cycles
SEAT 45H EEL BROKEN. REPLACED EEL LIGHT. OPERATIONS CHECKED OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,038 hrs · 11,566 cycles
SEAT 48C EEL INOPERATIVE. REPLACED EEL. OPERATIONS CHECKED OK.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 97,038 hrs · 11,566 cycles
SEAT 19H EEL INOPERATIVE. SECURED EEL CONNECTOR. OPERATIONS CHECKED OK.
Part: LIGHT — UNSECURE (CABIN) · airframe 97,016 hrs · 11,564 cycles
EMERGENCY LIGHT AT 2R ON AFT LAVATORY 102 WALL IS HANGING OFF, WIRES EXPOSED. SECURED LIGHT ASSEMBLY.
2014
Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 93,340 hrs · 11,207 cycles
ROWS 51 TO 61HJK EMERGENCY LIGHTS INTERMITTENT. LIGHTS ILLUMINATE WHEN SELECTED ON, INTERMITTENT FLASH WHEN SELECTED OFF, ADJACENT LIGHTS NORMAL. IAW CH1727 REPLACED POWER SUPPLY M6012 ABOVE DOOR 5RT, EEL PATH LIGHTS ROW 51HJK TO 61HJK CHECKED OK IAW WD33-51-63.
Part: COVER — OUT OF ADJUST (LIGHT SWITCH) · airframe 93,202 hrs · 11,194 cycles
AISLE EMERGENCY GUIDANCE LIGHTS ON WHEN NOT COMMANDED TO BE ON. ROWS 54 - 60 RT SIDE ADJUSTED DOOR 1L SWITCH COVER.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,117 hrs · 11,186 cycles
EMERGENCY LIGHT STRIPS ON INTERMITTENTLY ROW 51 TO 61. REPLACED BATTERY ASSEMBLY.
Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 92,642 hrs · 11,142 cycles
CREW REPORTS EICAS NR 1 ENG LOW OIL PRESS MESSAGE.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,629 hrs · 11,140 cycles
FUSELAGE EXTERIOR SKIN WAS FOUND CORRODED ON INNER SURFACE BETWEEN STATION 480 - 500 & STRINGER 46R TO 47R, IN THE AREA COMMON TO THE TCAS ANTENNA. REPAIR WAS ACCOMPLISHED.
Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,629 hrs · 11,140 cycles
UPPER DECK LT HAND DOOR LOWER MAIN SILL STIFFENER WAS FOUND CORRODED AT STRINGER 13L FROM STATION 707 TO 714. REPAIR WAS ACCOMPLISHED IAW ECRA5310-05959.
Part: FITTING — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
FUSELAGE STATION 980, STRINGER 38R LOWER DRAG SPLICE FITTING ONE EACH FASTENER HOLE FOUND CRACK APPROXIMATELY 0.25 LONG. FUSELAGE STATION 980, STRINGER 38R LOWER DRAG SPLICE FITTING FABRICATED & INSTALLED IAW ECRA 5310- 05960 & RI RI-53-00-10427, REV A.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,629 hrs · 11,140 cycles
MAIN DECK STATION 1295 - 1316, LBL 33 SEAT TRACK UPPER CHORD CORRODED. CORROSION BLENDED OUT BEYOND SRM LIMITS. REPAIRED UPPER CHORD IAW ECRA 5320-02202 & RI RI-53-45-10409 REV A. THE LBL 33 SEAT TRACK REPAIR INSTALLED BETWEEN BS 1265 - 1480 IAW ECRA 5320-02202.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
MAIN DECK STATION 2220 STRINGER 19R - 20R SHEAR TIE FOUND CRACK. THE FRAME REPAIRED IAW ECRA 5310-05958 & RI RI-53-62-10401, REV A, REPAIR INSTALLED.
Part: SKIN — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
CRACK REVEALED ON SKIN UNDERNEATH LOWER DRAG SPLICE FITTING ANGLE. FUSELAGE CRACKED SKIN BETWEEN BS 950 - 980 & STRINGER 37R TO 39R. REPAIRED IAW SRM 53-20-01,RPR 2,FIG 201,TABLE III. CAT B REPAIR, SUBSEQUENT INSPECTION REQUIRED IAW SRM 53-20-01, RPR 2, FIG 201 TABLE III. INSPECTION THRESHOLD AT 15000C AFTER REPAIR INSTALLATION INTERVAL 6000C, METHOD HFEC, INTERNAL DETAIL VISUAL.
Part: SKIN — CRACKED (CARGO DOOR) · airframe 92,629 hrs · 11,140 cycles
AFT CARGO DOOR FWD LOWER EXTERIOR SKIN SURFACE SCRATCHED. SCRATCH MARK SMOOTHED OUT IAW SRM51-10-02. PERFORMED HFEC, FOUND CRACKED, REPAIRED IAW SRM 52-30-01, REPAIR 2 FIG 201. SUPPLEMENTAL INSPECTION ACP IAW SRM 52-30-01, REPAIR 2, FIG. 201, TABLE III.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
FUSELAGE SKIN DAMAGE AFT OF DOOR 5R. DAMAGE CONSISTS OF FOUR SMALL GOUGES & ONE DENT. DEEPEST GOUGE IS .007, LOCATED IN DENT WITHIN SRM53-00-01 DETAIL II ALLOWABLE LIMITS. DENT DIMENSIONS ARE 3.5 X 2 .070 DEEP BEYOND SRM DETAIL III ALLOWABLE LIMITS. DAMAGE LOCATION IS AT STATION 2317 1INCH ABOVE STRINGER 22R FREE OF ANY FASTENERS OR SUBSTRUCTURE. BLENDED GOUGES SMOOTH IAW SRM53-00-01 DETAIL II PG 6. REMAINING SKIN THICKNESS .055, ACP HFEC INSPECTION NO CRACKS FOUND. TREATED, PRIMED,& PAINTED WITH DENT DOT IDENTIFIER APPLIED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,629 hrs · 11,140 cycles
MAIN DECK STATION 980, LBL 23 - LBL 110, FLOOR BEAM UPPER CHORD CORRODED. MAIN DECK FLOOR BEAM AT STATION 980, LBL23 - LBL110 UPPER CHORD REPAIRED IAW SRM 53-20-51, REPAIR 1 FIG 201.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,629 hrs · 11,140 cycles
UPPER DECK STATION 1060, RBL 16 - RBL 33 FLOOR BEAM UPPER CHORD FOUND CORRODED. UPPER DECK, FLOOR BEAM AT STATION 1060, RBL 16 - RBL 33 REPAIRED IAW SRM 53-40-51, REPAIR 3, FIG 201.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
RT BS 1120 AFT CHANNEL CRACK AT UPPER RADIUS AREA.
Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
RT BS1120 TENSION TIE ONE EACH FASTENER HOLE CRACK FOUND AT AFT CHANNEL, AT 12 & 6 O`CLOCK POSITION THROUGH THICKNESS.
Part: WEB — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
MAIN DECK A ZONE STATION 140 - 160, STRINGER 26R FLOOR WEB CRACKED.
Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,141 cycles
RT BS 1120 TENSION TIE AREA, ONE EACH HOLE FOUND CRACK AT FWD CHANNEL.
Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
MAIN DECK RT BS 1160 TENSION TIE FWD CHANNEL ONE EACH HOLE FOUND CRACKED. MAIN DECK RT BS 1160 FWD CHANNEL REPAIRED IAW SRM 53-40-30, REPAIR 1, FIG 201.
Part: WEB — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
R5 DOOR FWD CUTOUT STATION 2233 BETWEEN STRINGER 21R & 22R VERTICAL WEB CRACKED. R5 DOOR FWD CUTOUT VERTICAL WEB AT STATION 2233 BETWEEN STRINGER 21R & 22R REPAIRED IAW SRM 53-60-15, REPAIR 3, FIG 201.
Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
MAIN DECK RT BS 1160 TENSION TIE AFT CHANNEL ONE EACH HOLE FOUND CRACKED. MAIN DECK RT BS 1160 AFT CHANNEL REPAIRED IAW SRM 53-40-30, REPAIR 1, FIG 201.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
LT BS 1200 TENSION TIE AREA, THREE EACH HOLES CRACK FOUND AT FWD CHANNEL. MAIN DECK LT BS 1200 FWD CHANNEL REPAIRED IAW SRM 53-40-30, REPAIR 1, FIG 201.
Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
MAIN DECK STATION 1200 LT TENSION TIE AFT CHANNEL ONE EACH FASTENER HOLE FOUND CRACKED UPWARD WITH CRACK LENGTH APPROXIMATELY 0.040 INCHES.
Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
MAIN DECK RT BS 1160 TENSION TIE FWD CHANNEL ONE EACH HOLE FOUND CRACKED.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,629 hrs · 11,140 cycles
MAIN DECK SKIN CORROSION AT BS 1475 - 1480, STRINGER 15R - 16R.
Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
RT BS 1120 TENSION TIE, ONE EACH FASTENER HOLE CRACK FOUND AT HORIZONTAL SHEAR WEB AT 12 O'CLOCK & 6 O'CLOCK POSITION THROUGH THICKNESS. MAIN DECK RT BS 1120 HORIZONTAL SHEAR WEB CRACKED, CRACK LENGTH 0.125, REPAIRED IAW SRM53-40-30 REPAIR 4, FIG 201.
Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
RT BS 1120 TENSION TIE AREA ONE EACH FASTENER FOUND CRACK AT FAIL SAFE CHORD. MAIN DECK RT BS 1120 FRAME AFT FAIL SAFE CHORD CRACKED BETWEEN STRINGER 6R - 12R, CRACKED LENGTH 0.050, REPAIRED IAW SRM53-40-07, REPAIR 1, ITEM F.
Part: FRAME — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
MAIN DECK RT BS 1160 TENSION TIE TO FRAME ATTACHMENT AREA 4 EA HOLES FOUND CRACKED AT FRAME. MAIN DECK RT BS 1160 FRAME CRACKED AREA BETWEEN STRINGER 6R - 12R, CRACK LENGTH 0.080, REPAIR IAW SRM 53-40-07, RPR 3, FIG 201.
Part: FRAME — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
RT BS 1120 TENSION TIE AREA, SIX EACH HOLES FOUND CRACK AT FRAME. MAIN DECK RT BS 1120 FRAME CRACK LENGTH 0.040, BETWEEN STRINGER 7R - 12R. REPAIRED IAW SRM 53-40 -07, RPR 1, FIG 201.
Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
MAIN DECK RT BS 1200 TENSION TIE FWD CHANNEL FOUND ONE EACH HOLE CRACKED. MAIN DECK RT BS 1200 TENSION TIE FWD CHANNEL CRACKED, CRACK LENGTH 3-16, REPAIRED IAW SRM 53-40- 30, RPR 2 FIG 201.
Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
LT BS 1160 TENSION TIE AREA, FIVE EACH HOLES FOUND CRACK AT FWD CHANNEL. MAIN DECK LT BS 1160 TENSION TIE FWD CHANNEL CRACKED AREA REPAIRED IAW SRM53-40-30 REPAIR 2, FIG 201.
Part: FRAME — CRACKED (FUSELAGE) · airframe 92,629 hrs · 11,140 cycles
LT BS 1160 TENSION TIE AREA, ONE EACH HOLE FOUND CRACK AT FRAME. MAIN DECK LT BS 1160, R & R FRAME DOUBLER IAW SRM 53-40-07, RPR 3, FIG 201.
2013
Part: LIGHT — BROKEN (CABIN) · airframe 92,500 hrs · 11,127 cycles
ONE OF THREE SMALL EMERGENCY EXIT LIGHTS BROKEN IN MID GALLEY. RELAMPED LIGHT IAW WDM 33-00-01.
Part: ISOLATOR — DETERIORATED (APU MOUNT) · airframe 92,437 hrs · 11,121 cycles
APU RT FWD MOUNT ISOLATOR RUBBER DETERIORATED & CRACKED. REPLACED THE RT FWD MOUNT ISOLATOR. REPLACED THE APUC, NEED TO REPLACE THE APU DUE CHRONIC NO START. REMOVED & INSTALLED APU IAW TOD-49-11-01-401 UP TO TASK-764-102. DURING APU STARTING, APU SURGES & SHUTDOWN WITH BLEED AIR ON.
Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 92,321 hrs · 11,108 cycles
APU FAILED TO START, MAINT MESSAGE 49055 DISPLAYED FMU STEPPER MOTOR FAILURE, MEL COMPLIED WITH. SEE TASK FIM 49-11 TASK 856. ACP APU GROUND TEST DEFAULTED TO FMU FAILURE ITEM M3374 PART NBR 3036324.
Part: FUEL SYS — LEAKING (HORIZ STAB) · airframe 92,270 hrs · 11,102 cycles
FUEL LEAKING OUT OF STAB COMPARTMENT. FOUND FUEL SITTING BELOW STAB BOX, FWD & AFT STAB COMPARTMENT DOORS OPEN FOR ACCESS. HORIZONTAL STAB TANKS DRAINED. CLEANED STAB COMPARTMENT & FOUND FUEL UNDER LT FUEL TANK SUMP VLV.
Part: UNKNOWN — UNKNOWN (APU) · airframe 92,203 hrs · 11,096 cycles
APU ABORTS START. GROUND TEST AND OPS CHECK WITH NO FAULTS NOTED.
Part: HYDRAULIC LINE — LEAKING (RT MLG WW) · airframe 92,112 hrs · 11,088 cycles
HYD LEAK FROM "UP 2" PRESS LINE APPROXIMATELY 4 FEET FROM GROUND SPEED BRAKE VLV UNDER CLAMP. REMOVED LINE IAW IPC 27-61-67-001 ITEM 305. ACCOMPLISHED RYNGLOK REPAIR IAW GNMM 1-0-13-028. NEED TO LEAK CHECK LINE WITH HYD PRESS. LINE LOCATED IN RT WLG WW. COMPLETED LINE INSTALLATION & LEAK CHECKED NO LEAKS FOUND
Part: SKIN — CRACKED (FUSELAGE) · airframe 91,746 hrs · 11,053 cycles
ENG 3 PYLON HAS A CRACK OTBD SURFACE, CF IAW ECRA 5450-02074. INTERIM REPAIRED STOP HOLE & HST 2 LAYER APPLIED.
Part: LINE — LEAKING (FUEL SYSTEM) · airframe 91,558 hrs · 11,033 cycles
EXTREME STRONG ODOR OF FUEL IN CABIN. APPEARS TO BE CENTERED AROUND THE OVERWING AREA. REPLACED ALL HST FUEL LINES.
Part: LIGHT — DAMAGED (SEAT ROW 25C) · airframe 91,366 hrs · 11,015 cycles
EMERGENCY LIGHT DAMAGED. REPLACED EMERGENCY LIGHT IAW MM.
Part: LIGHT — LOOSE (CABIN) · airframe 90,961 hrs · 10,976 cycles
EMERGENCY LIGHT EXIT INDICATOR LIGHT AT 1 RT BASEBOARD HANGING. SECURED LOOSE EMERGENCY LIGHT.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 90,714 hrs · 10,950 cycles
EXT EMERGENCY SLIDE LT AT LT ABOVE TRAILING MOST FWD AND AFT IS INOP. RELAMPED AFT EMERGENCY LT ASSY, NO HELP. NEEDS T-S. REPLACED EMERGENCY LTS. "CHARGER UNIT" & "BATTERY PACK" (M7919) LOCATED ABOVE MAIN ENTRY DOOR 3L, OPS CK OF LT SIDE EXTERNAL FUSELAGE SLIDE EMERGENCY LIGHTS MOST FWD & AFT OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,662 hrs · 10,945 cycles
CABIN R1 DOOR MOUNT EMERGENCY LIGHT FOUND INOPERATIVE. CABIN R1 DOOR MOUNT EMERGENCY LIGHT REPLACED & TEST FOUND OK IAW 33-51-06.
Part: AILERON SYS — UNKNOWN · airframe 90,445 hrs · 10,925 cycles
ON TAXI OUT, FLT CREW OBSERVED A MISMATCH BETWEEN THE LT AND RT INBD AILERONS. OBSERVED FROM THE AILERON INDICATION ON SECONDARY EICAS. NO MESSAGES GENERATED, VISUAL INSPECTION ACCOMPLISHED FOR FULL AILERON TRAVEL IN BOTH DIRECTIONS. NO BINDING EVIDENT IN CONTROL COLUMN. AILERON POSITION INDICATION DEFERRAL APPLIED.
Part: VALVE — FAILED (NR 5) · airframe 89,953 hrs · 10,875 cycles
'WAI VALVE RIGHT' EICAS ADVISORY MESSAGE DISPLAYED. RIGHT WING ANTI-ICE VALVE DISAGREES WITH COMMAND. WAI RIGHT EICAS VALVE IS STUCK IN ON POS. REPLACED VALVE IAW MM. VALVE FAILED WITH MESSAGE 30222. ORIGINAL VALVE WAS BOUND SOLID, WILL NOT MOVE, THE BA VALVE MOVES OK DURING TEST AND MESSAGE CLEARED BUT RETURN AT END OF TEST WITH MT MESSAGE 30222. REPLACED RT WAI VALVE PER MM, OPS CHECKED OKAY. NO EXISTING FAULTS NOTED.
Part: SHUTOFF VALVE — SURGES (NR 4 ENGINE) · airframe 89,750 hrs · 10,854 cycles
NR 4 ENGINE BLEED SURGES EPR AT FL 400 SURGES BETWEEN 1.17 - 1.26. ACCOMPLISHED HIGH POWER RUN AT 1.20 EPR NO FLUCTUATION IN POWER SETTING.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 89,722 hrs · 10,851 cycles
MID CABIN CROSS AISLE LIGHT OUT. REPLACED LAMP.
Part: RUB STRIP — DAMAGED (NR 4 NACELLE) · airframe 89,193 hrs · 10,794 cycles
NR 4 ENGINE INBRD CORE COWL L/E RUB STRIP DAMAGED. REMOVED AND REPLACED DAMAGED RUB STRIP.
Part: RUB STRIP — DAMAGED (NR 4 NACELLE) · airframe 89,193 hrs · 10,794 cycles
NR 4 ENGINE INBRD REV T/E RUB STRIP DAMAGED. REMOVED AND REPLACED DAMAGED RUB STRIP.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 89,098 hrs · 10,785 cycles
FLOORBEAM STIFFENER FOUND CRACKED AT STA 380 BL 0 U-DECK FLOOR. STIFFENER REPAIRED PER SRM 51-70-12 REPAIR NR 1.
2012
Part: SKIN — CRACKED (FUSELAGE) · airframe 88,710 hrs · 10,748 cycles
NLG WHEEL WELL CUTOUT AFT LEFT CORNER FUSELAGE SKIN CRACKED, STA 400 STR 44L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, INSTALLED MULTIPLE LAYER REPAIR PER COA 851431 & ECRA 5331-01658.
Part: SKIN — CRACKED (FUSELAGE) · airframe 88,710 hrs · 10,748 cycles
NLG WHEEL WELL CUTOUT AFT RT CORNER FUSELAGE SKIN CRACKED AT STA 400 STR 44R. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, INSTALLED MULTIPLE LAYER REPAIR PER COA 851432 & ECRA 5331-01658.
Part: SKIN — CRACKED (FUSELAGE) · airframe 88,710 hrs · 10,748 cycles
FUSELAGE EXTERNAL SKIN CRACKED AT BS 2370 STR 15L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE, MANUFACTURED REPAIR DOUBLER AND INSTALLED PER SRM 53-00-01 RPR 1, SOLID FASTENER RPR. HOLES NOT ZERO-TIMED. THIS IS A CATEGORY "B" REPAIR. A CF ITEM WILL BE CREATED FOR REINSPECTIONS.
Part: FRAME — DAMAGED (THRUST REVERSER) · airframe 88,710 hrs · 10,748 cycles
NR 2 ENGINE INBOARD THRUST REVERSER AFT FRAME REPAIR BETWEEN 2 O'CLOCK AND 5 O'CLOCK POSITION NEEDS REPETITIVE INSPECTION. REPLACED THE NR 2 ENG INBD TR AFT FRAME PER SRM & ECRA7831-01728.
Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 88,685 hrs · 10,745 cycles
REPORTS OF HOT ELECTRICAL ODORS VARIOUS PLACES IN CABIN AND COCKPIT. BLINKING CABIN LIGHTS AND CALL LIGHTS. F/O REPORTS BURNING RUBBER ODOR AS WELL. INSPECTED CABIN FOR OVERHEATED, DEFECTIVE COMPONENTS. CHECKED OEU'S IN AFT CABIN ZONE AND FOUND OK. INSPECTED AREAS ABOVE GALLEY & UNABLE TO IDENTIFY OVERHEATED PARTS. CHECKED POTABLE H20 COMPRESSOR. SMELL DISAPPEARS WITH NR 2 PACK TURNED OFF. PACK DEACTIVATED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,473 hrs · 10,723 cycles
EEL LIGHT BETWEEN LAVS 111 AND 112 INOPERATIVE. REPLACED EEL LAMP AND REPAIRED EEL.
Part: LIGHT — LOOSE (CABIN) · airframe 88,473 hrs · 10,723 cycles
EEL LIGHT AT SEAT 40HJK LOOSE. RELAMPED OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,473 hrs · 10,723 cycles
EEL LIGHT AT 57ABC INOPERATIVE. RELAMPED, OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,473 hrs · 10,723 cycles
EEL LIGHT AT 45ABC INOPERATIVE. RELAMPED, OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,473 hrs · 10,723 cycles
EEL LIGHT AT SEAT 45HJK INOPERATIVE. RELAMPED OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,473 hrs · 10,723 cycles
EMERGENCY LIGHT LOWER RIGHT CROSS AISLE AT DOOR 2 INOPERATIVE. RELAMPED AND REPLACED LENS OPS NORMAL.
Part: LIGHT — FAULTY (CREW REST) · airframe 88,473 hrs · 10,723 cycles
EMERGENCY CEILING LIGHT IN AT AFT CREW REST VERY DIM. REPLACED LAMPS.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 88,473 hrs · 10,723 cycles
EMERGENCY CEILING LIGHT IN FLIGHT DECK INOPERATIVE. RELAMPED, OPS NORMAL.
Part: LIGHT — BROKEN (CABIN) · airframe 88,441 hrs · 10,720 cycles
ON CM 8401 FOUND DOOR 5L EMERGENCY EXIT LIGHT BROKEN. REPLACED EMERGENCY EXIT LIGHT AND OPS CHECK OK.
Part: PANEL — DAMAGED (RT WING) · airframe 88,187 hrs · 10,696 cycles
RT WING OTBD MID INBD DEFLECTION ROLLER GUIDE TRACK BOTTOM PANEL DROPPED. PANEL ATTACHED RIVETS AND BRACKET FOUND BROKEN. INTERIM REPAIRED AND INSPECTION PER ECRA 2700-01549. PANEL INTERIM REPAIR AND SPEED TAPE 2 LAYERS APPLIED. REQUEST RECHECK INTERIM REPAIR EACH TRANSIT FOR 75 HOURS.
Part: ACTUATOR — LEAKING (NR 7 SPOILER) · airframe 87,987 hrs · 10,677 cycles
EVIDENCE OF HYDRAULIC LEAK DRIPPING FROM RIGHT WING INBOARD FLAP TRACK CANOE. FLAP HANDLE AT 25 UNITS ALT FLAP SWITCH. HYD LEAK COMING FROM NR 7 SPOILER ACTUATOR RUNNING INBOARD INTO THE FLAP TRACK CANOE. LEAKING FROM END SEAL ON ACTUATOR WHERE CHROME EXTENDS. REMOVED NR 7 SPOILER ACTUATOR. COMPLETED INSTALLATION OF NR 7 SPOILER ACT IAW MM. LEAK AND OPS CHECK NORMAL.
Part: PANEL — DELAMINATED (THRUST REVERSER) · airframe 87,987 hrs · 10,677 cycles
NR 2 LEFT REVERSER LOWER PANEL DELAMINATED. 105 TO EVALUATE AND RE-ADJUST ETR.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 87,987 hrs · 10,677 cycles
EEL INOP AT SEAT 39ABC. SECURED CONNECTOR UNDER SEAT 39C. OPS NORMAL.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 87,987 hrs · 10,677 cycles
EEL LIGHT INOP AT SEAT 45 ABC. SECURED CONNECTOR UNDER SEAT 45C. OPS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,987 hrs · 10,677 cycles
EEL LIGHT INOP CROSSAISLE RIGHT SIDE NEAR DOOR 2RT. RELAMPED, OPS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,495 hrs · 10,631 cycles
EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,495 hrs · 10,631 cycles
EMERGENCY CEILING LIGHT ABOVE ROW 46 RT INOPERATIVE. RELAMPED, OPS CHECKED NORMAL.
Part: LIGHT — UNSECURE (ROW 23RH) · airframe 87,495 hrs · 10,631 cycles
EMERGENCY LIGHT ROW 23 RT INOPERATIVE. SECURED, OPS CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,166 hrs · 10,599 cycles
EMERGENCY EXIT LIGHT INOPERATIVE, UPPER DECK CEILING JUST FORWARD OF SEAT ROW 17. RELAMPED EXIT LIGHT ON CEILING FORWARD OF ROW 17, OPS CHECK NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,166 hrs · 10,599 cycles
EMERGENCY EXIT LIGHT INOPERATIVE, AFT CREW REST CEILING. RELAMPED EXIT LIGHT AFT CREW REST CEILING, OPS CHECKED NORMAL.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 87,166 hrs · 10,599 cycles
EMERGENCY EXIT LIGHT LENS MISSING BETWEEN SEAT ROWS 7 AND 8 LEFT. REPLACED EXIT LIGHT LENS, AT SEAT ROWS 7 AND 8, OPS CHECKED NORMAL.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 87,166 hrs · 10,599 cycles
EMERGENCY EXIT LIGHT LENS MISSING UPPER DECK SEAT ROW 15AB. REPLACED EXIT LIGHT LENS, NO DEFECTS NOTED.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,166 hrs · 10,599 cycles
EMERGENCY EXIT LIGHT INOPERATIVE, UPPER DECK CEILING ROW 15. RELAMPED EMERGENCY EXIT LIGHT ON CEILING ROW 15, OPS CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,775 hrs · 10,561 cycles
R2 DOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. OPS CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,775 hrs · 10,561 cycles
CEILING EMERGENCY LIGHT ROW 13 INOPERATIVE. RELAMPED. OPS CHECKED NORMAL.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 86,775 hrs · 10,561 cycles
EMERGENCY LIGHT RT ROW 2 INOPERATIVE. REPAIRED EMERGENCY LIGHT WIRING.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 86,775 hrs · 10,561 cycles
EMERGENCY LIGHT ROW 43 LT SEAT INOPERATIVE. RESECURED EMERGENCY LIGHT CONNECTOR. OPS CHECKED NORMAL.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 86,775 hrs · 10,561 cycles
EMERGENCY SEAT LIGHT ROW 3 RT INOPERATIVE. REPAIRED WIRING.
Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 86,775 hrs · 10,561 cycles
RT OVERWING EMERGENCY LIGHT SECOND FROM TOP ONE LIGHT INOPERATIVE. REPLACED LIGHT ASSY.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,775 hrs · 10,561 cycles
EMERGENCY EXIT R1 DOOR SIGN INOPERATIVE. REPLACED LAMP.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 86,775 hrs · 10,561 cycles
EMERGENCY LIGHT SEAT 1 RT INOPERATIVE. REPAIRED EMERGENCY LIGHT WIRING.
Part: BATTERY — INOPERATIVE (EMERENCY LIGHT) · airframe 86,775 hrs · 10,561 cycles
EMERGENCY LIGHT ALONG LAV 101 RT INOP. SUPPLEMENTAL DATA UPDATE, REPLACED BATTERY AND POWER SUPPLY UNIT.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,775 hrs · 10,561 cycles
EMERGENCY LIGHT ABOVE R1 DOOR INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY ASSY.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 86,775 hrs · 10,561 cycles
EMERGENCY LIGHT ROW 4 RT INOPERATIVE. REPAIRED WIRING.
Part: WIRE — BURNED · airframe 86,639 hrs · 10,545 cycles
FOUND WIRE W268-012-1-0 AND W268-013-1-0 TERMINAL LUGS B AND C DISCOLORED AND SHOWS OFF HEAT DAMAGE DUE TO TOO MUCH HEAT. EXTERNAL POWER RECEPTICAL ONE, CONNECTOR D51J DISCONNECTED. REMOVED WIRE W268-011-1-0, W268-012-1-0 AND W268-013-1-0.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,306 hrs · 10,511 cycles
UPPER DECK CEILING LIGHT NEAR SEAT ROW 13A IS INOPERATIVE. RELAMPED. OPS CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,306 hrs · 10,511 cycles
UPPER DECK LEFT WING DOOR AFT EMERGENCY LIGHT IS INOPERATIVE. RELAMPED, OPS CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,306 hrs · 10,511 cycles
UPPER DECK CEILING LIGHT NEAR SEAT ROW 14A IS INOPERATIVE. RELAMPED. OPS CHECKED NORMAL.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 86,306 hrs · 10,511 cycles
SEAT 43 ABC EMERGENCY LIGHT IS INOPERATIVE. SECURED CONNECTION UNDER SEAT, OPS CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,306 hrs · 10,511 cycles
SEAT 40 HJK EMERGENCY LIGHT IS INOPERATIVE. RELAMPED, OPS CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,306 hrs · 10,511 cycles
LEFT OVERWING 3RD LIGHT ASSY FWD LAMP IS INOPERATIVE. RELAMPED, OPS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,306 hrs · 10,511 cycles
UPPER DECK RIGHT WING DOOR AFT EMERGENCY LIGHT IS INOPERATIVE. RELAMPED, OPS CHECKED NORMAL.
Part: SMOKE DETECTOR — FAULTED (CARGO BAY) · airframe 86,277 hrs · 10,509 cycles
FOUND FAULT IN CARGO AFT-3 LOOP-A. MESSAGE NR 26164. REPLACED SMOKE DETECTOR 3A I IN AFT PIT PER MM26-16-01 AND IPC 26-16-01-002. TEST PASS.
Part: SCANNER — MALFUNCTIONED (WEATHER RADAR) · airframe 85,800 hrs · 10,463 cycles
LOST WX RADAR, RTFL (2X) REPLACED WEATHER RADAR ANTENNA PER MM. DUE TO REPEAT FAULT OF WX RADAR CLUTTER IN FLIGHT. NEED TO REPLACE ANTENNA DRIVE WITH A NEW ANTENNA PLATE. CONCURRED. PCN 580-9031 AND PCN 582-0031. PLEASE VERIFY WITH ONLINE IPC. USE MM 34-43-03. 401. REPLACED BOTH SCANNER ASSY AND PLATE ASSY.
Part: STRUCTURE — CRACKED (K FLAP) · airframe 85,746 hrs · 10,455 cycles
KRUEGER FLAP 16 HAS CRACK APPROX 6 IN AT UPPER OTBD CORNER. REMOVED KRUEGER FLAP PER MM. ACCOMPLISHED PRE-INSTALLATION INSPECTION OF NR 16 KRUEGER FLAP ATTACH POINTS ON ACFT. INSTALLED FLAP AND TORQUED BOLTS UP TO STEP 3.E.(9) PG 406 MM. COMPLETED INSTALLATION OF NR 16 L/E FLAP FROM ITEM 3(E)9.
Part: LIGHT — BROKEN (CABIN) · airframe 85,314 hrs · 10,412 cycles
SEAT MOUNTED EEL BROKEN. REPLACED SEAT MOUNTED EEL AT SEAT 46C, OPS CKD OKAY.
Part: LAMP — INOPERATIVE (L5 DOOR SLIDE) · airframe 85,180 hrs · 10,400 cycles
EMERGENCY EXIT LIGHT INOPERATIVE AT L5 DOOR SLIDE LIGHT. REPLACED LAMP, CHECKED OKAY.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,180 hrs · 10,400 cycles
EMERGENCY EXIT LIGHT INOPERATIVE AT UPPER DECK CEILING BETWEEN DOORS AFT LIGHT. RELAMPED, OPS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,180 hrs · 10,400 cycles
EMERGENCY EXIT LIGHT INOPERATIVE AT CEILING SEAT ROW 57 LEFT. RELAMPED, OPS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,180 hrs · 10,400 cycles
EMERGENCY EXIT LIGHT INOPERATIVE AT LOWER WALL ACROSS DOOR 3 RIGHT. RELAMPED, OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,180 hrs · 10,400 cycles
EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING JUST FWD OF SEAT ROW 17. RELAMPED, OPS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,180 hrs · 10,400 cycles
EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED, OPS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,180 hrs · 10,400 cycles
EMERGENCY EXIT LIGHT INOPERATIVE AT UPPER DECK CEILING SEAT ROW 15. RELAMPED, OPS NORMAL.
Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 85,180 hrs · 10,400 cycles
EMERGENCY EXIT LIGHTS VERY DIM AT SEATS 33 THRU 43 RIGHT. REPLACED BATTERY PACK, OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,180 hrs · 10,400 cycles
EMERGENCY EXIT LIGHT INOP DOOR 2 GALLEY AREA LOWER RIGHT WALL. RELAMPED, OPS NORMAL.
2011
Part: CONTAINER — TORN (LIFE VEST) · airframe 84,841 hrs · 10,366 cycles
THE 20E LIFE VEST POUCH TORN. REPLACED LIFE VEST.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,634 hrs · 10,346 cycles
SEAT 40R EEL LIGHT INOPERATIVE. REPLACED EEL LIGHT ASSY, OPS CHECK OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,634 hrs · 10,346 cycles
SEAT 16L EEL LIGHT INOPERATIVE. RELAMPED, OPS CHECK OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,634 hrs · 10,346 cycles
SEAT 15L EEL LIGHT INOPERATIVE. RELAMPED, OPS CHECK OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,634 hrs · 10,346 cycles
EEL LIGHT INOP BETWEEN DOORS 2L AND 2R LEFT SIDE. RELAMPED, OPS CHECK OKAY.
Part: FAN — FAULTY (GALLEY) · airframe 84,578 hrs · 10,340 cycles
PRE-FLT CHECK FOUND STATUS MSG-LAV GALLEY FAN. REPLACED LAV-GALLEY VENT FAN AS PER MM AND OPS CHECK OK, NIL STATUS MSG DISPLAYED. PART REPLACED, P/N 4100149C, S/N 1350A. NON-POOL PART, RETURN IN SEVEN DAYS.
Part: SKIN — CRACKED (FUSELAGE) · airframe 84,448 hrs · 10,326 cycles
RIGHT FUSELAGE SKIN AROUND LAV BLOWER HOLE VENT HAS SMALL CRACK AND METAL PUSHED OUTWARD. REMOVED DAMAGE, ACP HFEC INSPECTION SEE AMIS #4482033, MANUFACTURED RPR PARTS, AND PREPPED FOR INSTALLATION REF SRM 53-60-01-201 RPR #5. REPAIRED AREA AROUND RT SIDE FUSELAGE LAV BLOWER HOLE VENT PER SRM, REPAIR 5.
Part: TUBE — LEAKING (HYD SYSTEM) · airframe 84,104 hrs · 10,287 cycles
HYD FLUID LEAK INSIDE NR 1 ENGINE PYLON. FOUND PIN HOLE AT TUBE ASSY RETURN SYS 1. REPLACED NEW TUBE ASSY & PER MM PRESSURE CHECKED. NO LEAK FOUND, FLIGHT CONTROL SURFACE OPERATION CHECKED NORMAL.
Part: TRUNNION — WORN (NLG) · airframe 84,042 hrs · 10,280 cycles
FOUND AFT RT NOSE GEAR DOOR LOOSE, METAL TRIANGLE CASTING BOLTED TO RT TRUNNION AREA OF GEAR IS WORN. FOUND SPACER MISSING NOSE GEAR TRUNNION CRANK, REMOVED RIGHT TRUNNION DRIVE CRANK. RT TRUNNION DRIVE CRANK NEEDS INSTALLATION. INSTALLED TRUNNION DRIVE CRANK. NO ADJUSTMENT TO DOOR OPERATOR RODS OR LINKAGE MADE.
Part: LIGHT — SHORTED (CABIN) · airframe 84,042 hrs · 10,280 cycles
SEATS 45ABC-53ABC EMERGENCY LIGHTS IS INOP. FOUNDED SEAT 45ABC SHORTED. REPLACED EMERGENCY LAMP, CHECKS NORMAL.
Part: LEAD — DISCONNECTED (EMERGENCY LIGHT) · airframe 84,042 hrs · 10,280 cycles
MID LAV LOWER SIDEWALL EMERGENCY LIGHT IS INOP. RECONNECT LAMP LEAD, OP CHECK NORMAL.
Part: LIGHT — DISCONNECTED (CABIN) · airframe 84,042 hrs · 10,280 cycles
AFT GALLEY LOWER SIDEWALL EMERGENCY LIGHTS IS INOPERATIVE. FOUND DISCONNECTED. RECONNECTED, CHECKS NORMAL.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 84,042 hrs · 10,280 cycles
SEAT ROW 40HJK EMERGENCY LIGHT IS INOP. RESECURED LIGHT CONNECTION, OP CHECK NORMAL.
Part: WIRE — CHAFED (NR 4 ENGINE) · airframe 84,042 hrs · 10,280 cycles
NR 4 ENG OTBD SIDE JUST ABOVE THE FUEL FLOW TRANSMITTER. WIRE BUNDLE HAS SEVERAL EXPOSED WIRES DUE TO CLAMP CHAFING. CLAMP REMOVED. REPAIRED THE WIRES.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,042 hrs · 10,280 cycles
UPPER DECK CEILING EMERGENCY LIGHT IS INOP NEAR 15AB. RELAMPED, OP CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,042 hrs · 10,280 cycles
UPPER DECK CEILING EMERGENCY LIGHT IS INOP NEAR 13AB. RELAMPED, OP CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,042 hrs · 10,280 cycles
UPPER DECK CEILING EMERGENCY LIGHT INOP NEAR 16AB. RELAMPED, OP CHECK NORMAL.
Part: LIGHT — DISCONNECTED (CABIN) · airframe 84,042 hrs · 10,280 cycles
DOOR 5R AREA LOWER SIDEWALL EMERGENCY LIGHT IS INOP. FOUND DISCONNECTED; RECONNECTED. CHECKS NORMAL.
Part: LEAD — FAULTY (EMERGENCY LIGHT) · airframe 84,042 hrs · 10,280 cycles
DOOR 3 RIGHT MID LAV LOWER SIDEWALL EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT LEAD, OP CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,042 hrs · 10,280 cycles
DOOR 2L LOWER SIDEWALL EMERGENCY LIGHT IS INOP. RELAMPED, OP CHECK NORMAL.
Part: LIGHT — DAMAGED (CABIN) · airframe 83,809 hrs · 10,256 cycles
PER LOW TECH SEAT MOUNTED EEL DAMAGED AT SEAT 45C. REPLACED SEAT MOUNTED EEL STRIP. OPS NORMAL.
Part: WIRE — LOOSE (ESCAPE REEL) · airframe 83,735 hrs · 10,248 cycles
ESCAPE REEL WIRE LOOSE. REEL REMOVED PER MEL. REPLACED REEL OPERATES NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,620 hrs · 10,234 cycles
EMERGENCY LIGHT INOPERATIVE. RELAMPED. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,620 hrs · 10,234 cycles
EEL LIGHT AT SEAT 40 HJK INOP. RELAMPED EMERGENCY LIGHT.
Part: LAMP — INOPERATIVE (CABIN) · airframe 83,620 hrs · 10,234 cycles
LEFT SIDE SECOND FROM BOTTOM SLIDE LIGHT ASSY EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,026 hrs · 10,169 cycles
DOOR 1R SLIDE EMERGENCY LIGHT IS INOP. RELAMPED, CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,026 hrs · 10,169 cycles
LEFT OVERWING EMERGENCY 3RD ASSY FWD LAMP IS INOP. LEFT OVERWING EMERGENCY 3RD ASSY FWD LAMP IS INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,026 hrs · 10,169 cycles
FLIGHT DECK CEILING EMERGENCY LIGHT IS INOP. RELAMPED, CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,026 hrs · 10,169 cycles
DOOR 5R FWD SILL EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 83,026 hrs · 10,169 cycles
DOOR 5R CROSS AISLE LOWER WALL EMERGENCY IS INOP. SECURED CONNECTION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,026 hrs · 10,169 cycles
MID GALLEY 2 EA LOWER WALL EMERGENCY LIGHTS CROSS AISLE IS INOP. RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,026 hrs · 10,169 cycles
ZONE C CEILING BOTH SIDES IS INOP. RELAMPED CEILING LIGHTS.
Part: BUSHING — MISMANUFACTURED (NR 7 FLAP TRACK) · airframe 82,330 hrs · 10,088 cycles
NR 7 FLAP TRACK NEW SEQUENCE CARRIAGE FWD END TOGGLE ROLLER BUSHINGS ARE NOT REAMED. REPLACED SEQ CARRIAGE ROLLER BUSHINGS & FITTING, PUT NEW BUSHINGS IN THE PARTS BIN ABOVE DOOR 2 LT.
Part: FLAP — DAMAGED (RT WING) · airframe 82,330 hrs · 10,088 cycles
RIGHT OUTBD L/E MID FLAP AT INBD LOC OF NR 8 ARM FITTING. DMG IS A 4'X3' CUTOUT W- INBD L/E RIB CRACKED 1.5' FROM L/E. RT OB FOREFLAP LE IS DELAMINATED, 10" AREA MIDWAY ON FLAP. DAMAGE IS 10" X .75" 10 FEET FROM INBD END. ACTUAL DELAMINATED AREA IS 4"X.75". AREA WAS CLEANED AND SPEED TAPED. WITHIN ALLOWABLE LIMITS. REPLACED THE FOREFLAP PER AMM.
Part: ROLLER — OUT OF TOLERANCE (NR 7 FLAP) · airframe 82,330 hrs · 10,088 cycles
NR 7 FLAP TRACK SEQUENCE CARRIAGE, INBD ROLLER IS MISSING AND THE O-B ROLLER IS INSTALLED BACKWARDS. REPLACED PER MM.
Part: LEVER — BENT (RT WING TE FLAP) · airframe 82,330 hrs · 10,088 cycles
RT OTBD FLAP, INBD ATTACH LEVER IS BENT. REPLACED RT OTBD FLAP INBD ATTACH LEVER WITH SERVICEABLE PART.
Part: BUSHING — MISSING (NR 8 FLAP) · airframe 82,330 hrs · 10,088 cycles
NR 8 FLAP CARRIAGE UPPER SEQ. CARRIAGE STOP IS MISSING THE O-B BUSHING. REINSTALLED NEW BUSHING.
Part: ATTACH FITTING — GOUGED (TE FLAP XMSN) · airframe 82,330 hrs · 10,088 cycles
NR 7 FLAP TRANSMISSION LOWER ATTACH FITTING HAS 4 GOUGES.1- .5 INCHES LONG X .10" DEEP & MAX. .20" WIDE. 2 = .6" LONG X .150" DEEP & MAX DEPTH .20".3= .9" LONG X .150" DEEP & MAX WIDE= .20". 4 = 1.1" LONG X MAX. DEPTH .20" & MAX. WIDE= . 450". ACP HFEC OF AREA PER NDT MM, NO CRACKS. REPLACED TRANSMISSION PER MM.
Part: RIB — DAMAGED (RT WING) · airframe 82,330 hrs · 10,088 cycles
RIGHT O/B MIDFLAP IS DAMAGED THE O/B FOREARM ATTACH CUTOUT AREA. NOSE RIB (65B39154-24) WAS DAMAGED. DAMAGED AREA WAS REMOVED INSTALLED STRAP REPAIR PICKING UP 2 FASTENERS EITHER SIDE OF DAMAGE, FIBERGLASS CLOSURE PANEL CRACK REMOVED RE-INSTALLED AND SPEED TAPED.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 82,330 hrs · 10,088 cycles
RIGHT O/B FOREFLAP L/E IS DELAMINATED, 10 INCH AREA MIDWAY ON FLAP. REFER TO SRM FOR ALLOWABLE DAMAGE. DAMAGE IS 10" X .75" 10 FEET FROM INBOAD END. ACTUAL DELAMINATED AREA IS 4"X .75". AREA WAS CLEANED AND SPEED TAPED.
Part: COTTER PIN — MISSING (FLAP TRACK) · airframe 82,330 hrs · 10,088 cycles
RIGHT O/B FOREFLAP ATTACH POINT TO NR 8 FLAP TRACK, FOUND COTTER PIN MISSING FOR THE ATTACH NUT. NUT TIGHTENED AND PIN INSTALLED BY MECH.
Part: ARM — BENT (TE FLAP) · airframe 82,330 hrs · 10,088 cycles
NR 7 FLAP TRACK O-B GUIDE ARM IS BENT. REPLACED GUIDE ARM.
Part: TRANSMISSION — DAMAGED (TE FLAP SYS) · airframe 82,330 hrs · 10,088 cycles
RT FWD FLAP AND NR 7 FLAP CARRIAGE ASSY DAMAGED. TRANSMISSION NR 7 HAS DEEP GOUGES & MID FLAP OUTBOARD CUTOUT HAS DAMAGE TO ASSESS. ACCOMPLISHED HFEC OF AREA PER NDT, NO CRACKS. REPLACED TRANSMISSION PER MM.
Part: ENGINE — SURGES (NR 2) · airframe 82,260 hrs · 10,079 cycles
SILENT SURGE FOUND 2.5 BLEED RING DRIVE ATTACK LINK SHEARED. NEEDS ENGINE CHANGE. ENG OFF, UNDER FW INSP. ENGINE REPLACED.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 82,223 hrs · 10,074 cycles
LT EEL LIGHT INOP FROM SEATS 45 TO 53. TROUBLESHOT AND FOUND BAD CONNECTION AT B9129 CONNECTOR. RESEATED CONNECTOR AND OPS CHECKS FINE PER AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,773 hrs · 5,932 cycles
EMERGENCY EXIT EEL LIGHT INOP LOWER WALL ACROSS LAV 100. REPLACED LIGHT ASSY. OPS CKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,773 hrs · 5,932 cycles
EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING AT DOORS FWD. LIGHT ASSY. RELAMPED, CKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,773 hrs · 5,932 cycles
EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING ROW 13. RELAMPED, CKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,223 hrs · 10,074 cycles
EMERGENCY LIGHT AT DOOR 4L INOP. RELAMPED EMERGENCY LIGHTS AT DOR 4L, OPS CHECK GOOD PER AMM ON PEMCO NR 2519N00007.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,223 hrs · 10,074 cycles
EMERGENCY LITES DOOR 4R INOP. RELAMPED EMERGENCY LITES AT DOOR 4R, OPS CHECK GOOD PER AMM ON PEMCO NR 2519N00008.
Part: ELECTRONIC UNIT — MALFUNCTIONED (CABIN) · airframe 82,115 hrs · 10,061 cycles
LIGHT BALLAST SMELL NEAR ROW 1. ALSO SIDEWALL LIGHT AT 1A CAME ON UNCOMMANDED, WONT GO OFF. T-S FOUND TWO BALLAST (CEILING, SIDEWALL) ARE BAD AND DISCONNECTED PLUGS FROM AFFECTED BALLAST THAT LOCATED CEILING ABOVE 2A SEAT. SMELL IS GONE AND REMAINING LIGHTING IS SUFFICIENT TO PERFORM DUTIES. CONFIRMED BURNING SMELL FROM CIRCUIT CARD OEU ROW 2A. REPLACED OEU AT 2A, SECURED BALLAST CONNECTORS, LIGHTING, CHECKS OKAY.
Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 82,082 hrs · 10,057 cycles
CREW REPORT: L1 WINDSHIELD CLOUDY DELAMS LEFT-TOP. SAMC TEXT: PICTURES ON RVI SITE, WINDOW DELAMINATED WITH EVIDENCE OF MOISTURE INGRESSION ON EDGES. REPLACED L1 WINDSHIELD PER MM AND CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,898 hrs · 10,037 cycles
SEAT 40R EEL LT INOPERATIVE. RELAMPED, CHECKS OKAY.
Part: CABLE — SATURATED (CABIN) · airframe 81,898 hrs · 10,037 cycles
REOCCURRING PROBLEM EEL LIGHTS AFT GALLEY FWD LEFT WALL LTS, SEATS 45L TO 53L, DOOR 4L FWD EXIT, DOOR 5L AFT EXIT. CLEANED WATER FROM AREA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,898 hrs · 10,037 cycles
CEILING EEL LT INOP AT ROW 52R. RELAMPED, CHECKS OKAY.
Part: FILTER — DIRTY (CABIN) · airframe 81,728 hrs · 10,019 cycles
IN COACH CABIN, THE CABIN TEMPERATURES FLUCTUATE WILDLY BETWEEN TOO HOT AND TOO COLD. CLEANED CABIN FILTERS. SYSTEM TESTED GOOD.
Part: LINE — LEAKING (APU FUEL) · airframe 81,480 hrs · 9,993 cycles
APU FUEL LINE SHROUD LEAKING FUEL. DRAINED APPROX 1 GAL OF FUEL FROM FUEL LINE SHROUD, WAITED 10 MIN FUEL CAME OUT OF DRAIN IN A STREAM DRAINED APPROX 4 OZ OF FUEL, WAITED 2 HRS DRAINED APPROX 1 PT OF FUEL FROM LINE, FUEL LEAK RATE EXCEEDS 1 DROP IAW MIN REF MM. REPLACED LEAKING LINE (180-0105) REF MM. LEAK CHECKED GOOD. NO FURTHER DEFECT NOTED.
Part: LAMP — INOPERATIVE (SEAT ROW 53HJK) · airframe 81,480 hrs · 9,993 cycles
SEAT ROW 53HJK EMERGENCY LIGHT INOP. RELAMPED SEAT ROW 53HJK EMERGENCY LIGHT. CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,480 hrs · 9,993 cycles
R2 DOOR AFT SILL EMERGENCY LIGHT IS INOP. RELAMPED DOOR 2R AFT SILL EMERGENCY LIGHT. CHECKED NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,480 hrs · 9,993 cycles
NEAR SEAT ROW 38HJK CEILING LIGHT IS INOPERATIVE. RELAMPED LIGHT, OPS CHECKED OK.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,480 hrs · 9,993 cycles
NEAR SEAT ROW 43ABC CEILING LIGHT INOP. RELAMPED LIGHT, OPS CHECKED OK.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,480 hrs · 9,993 cycles
R2 DOOR LOWER FLOOR EMERGENCY LIGHT IS INOP. RELAMPED DOOR 2R LOWER FLOOR EMERGENCY LIGHT. CHECKED NORMAL.
Part: CONNECTOR — DAMAGED · airframe 81,453 hrs · 9,989 cycles
PIGTAIL CORDS AT 401 AND 402 WIRES EXPOSED. SECURED RUBBER BACKSHELL COVER ON CONNECTORS, OPS NORMAL.
Part: WIRE — SHORTED (FUEL CELL PROBE) · airframe 81,431 hrs · 9,987 cycles
GROUND TEST MESSAGE REPORT SHOWS TANK WIRING-MAIN 3, PROBE 4, SHORT LO-Z GROUND. REMOVED NR 4 PROBE FROM NR 3 MAIN F138. REPLACED 3 MAIN TANK UNIT F138. REMOVED FUEL PLATE 645AB. INSTALLED 3 MAIN FUEL PLATE 645AB, CLEARED AND CLOSED.
Part: WIRE — FAULTY (SPEAKER) · airframe 81,431 hrs · 9,987 cycles
SPEAKER AT ROW 15AB IS NOT MUTE WHEN USE PA FOR UPPER DECK ONLY (CODE 44). REPLACED CABLE FSW443118126 BETWEEN D6984J AND IOEU UL-2 IAW WDM. PA OPS NORMAL.
2010
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,029 hrs · 9,939 cycles
SEAT 56R EMERGENCY LIGHT INOPERATIVE. RELAMPED, CHECKS OK.
Part: CART — ODOR (GALLEY) · airframe 80,652 hrs · 9,893 cycles
CART 404 HAS BURNING ODOR. UNPLUGGED. NO EVIDENCE OF BURNING MARK. . CB PULLED AND COLLARED PER MEL. FOUND CABLE AND CONTROLLER OPS CHECKED OKAY, REPLACED THE FOOD CART.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,975 hrs · 9,817 cycles
EMERGENCY LIGHT ROW 45 THROUGH 53 INOP. REPAIRED DAMAGED EMERGENCY LIGHT BELOW GALLEY AT DR 4L, OPS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,975 hrs · 9,817 cycles
OVERWING LT EMERGENCY LIGHT 2ND FROM BOTTOM INOP. RELAMPED, OPS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,975 hrs · 9,817 cycles
EMERGENCY LIGHT RT WALL DR2 GALLEY FWD INOP. RELAMPED OPS NORMAL.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 79,975 hrs · 9,817 cycles
EMERGENCY LIGHT CEILING LIGHT ABOVE ROW 47 INOP. SECURED LOOSE CONNECTOR ON CEILING PANEL, OPS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,975 hrs · 9,817 cycles
EMERGENCY LIGHT CEILING LIGHT ABOVE ROW 57 LT INOP. RELAMPED OPS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,975 hrs · 9,817 cycles
EMERGENCY LIGHT DR4 GALLEY LT INOP. REPAIRED EMERGENCY LIGHT AT DR 4L, OPS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,951 hrs · 9,814 cycles
UPPER DECK BETWEEN EMERGENCY EXITS LIGHT INOP. RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (SEAT ROW 52) · airframe 79,951 hrs · 9,814 cycles
SEAT ROW 52 EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP, OP CHECKS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,951 hrs · 9,814 cycles
SEAT ROW 48HJK EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP, OP CHECKS GOOD.
Part: CONTROLLER — FAULTY (NR 1 A/C PACK) · airframe 79,824 hrs · 9,798 cycles
15 MIN AFTER TAKEOFF COCKPIT 91F POOR QUALITY AIRFLOW 20 MIN AFTER TAKEOFF COCKPIT & REAR CABIN 90F UNIFORM SOAKED WITH SWEAT CALL ABOUT OVERHEATED COCKPIT NO ANSWER 30 MIN AFTER TAKEOFF. REAR CABIN 88F COCKPIT 88F AT PILOT SEAT. FOUND NR1 PACK PTC-A FAIL BY GRD TEST. REPLACED PTC-A IAW MM. ALL PACK SYS AND ZONE TRIM SYS OPS CKD OK.
Part: FAIRING — DAMAGED (FUSELAGE) · airframe 79,617 hrs · 9,775 cycles
WING-BODY FAIRING 193CL HAS DAMAGE DUE TO TIRE TREAD THROWN ON TAKEOFF. ROUTED PANELS TO SHOP 273. REMOVED AND REPLACED R21009-R21012. DRILLED, FITTED AND INSTALLED NEW BODY FAIRING PANEL 193CL.
Part: TIRE — SEPARATED (MLG) · airframe 79,617 hrs · 9,775 cycles
WING-BODY PANEL 193FL HAS DELAMINATION DUE TO TIRE TREAD THROWN ON TAKEOFF. ROUTED PANELS TO SHOP 273. REMOVED AND REPLACED R21009-R21012. SECURED IN PLACE.
Part: PANEL — DAMAGED (WING-BODY) · airframe 79,617 hrs · 9,775 cycles
WING-BODY PANEL 193DL HAS DELAMINATION DUE TO TIRE TREAD THROWN ON TAKEOFF. ROUTED PANELS TO SHOP 273. REMOVED AND REPLACED R21009-R21012. INSTALLED PANEL.
Part: PANEL — DAMAGED (WING-BODY) · airframe 79,617 hrs · 9,775 cycles
WING-BODY FAIRING 193BL IS DELAMINATED DUE TO TIRE TREAD DURING TAKEOFF. ROUTED PANELS TO SHOP 273. REMOVED AND REPLACED R21009-R21012. SECURED PANEL.
Part: COMPUTER — FAULTY (BRAKE SYSTEM) · airframe 79,519 hrs · 9,765 cycles
ABORTED TAKEOFF AT 100 KNOTS DUE TO AIRSPEED INDICATION. ACP HIGH ENERGY STOP HEAT INSP. PER AMM. EICAS BRAKE TEMP MAX ON DISPLAY WAS 2, COOLING TIME 40 MIN PER AMM. ALL BRAKING AND TIRES NORMAL. ON ARRIVAL NO FAULTS FOUND, ADC R & LEFT GROUND TESTS OK. NO HISTORY. PER CAPTAINS REQUEST REPLACED RIGHT ADC, ACP GROUND TEST PASSED. PITOT STATIC CONNECTIONS GOOD.
Part: LIGHT — LOOSE (CABIN) · airframe 79,426 hrs · 9,754 cycles
DOOR 2R 662 ACROSS FROM JS250 EXIT LIGHTING LOOSE ON WALL. SECURED EMERGENCY LIGHT AT DOOR 2R. ILLUMINATE TEST OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,394 hrs · 9,751 cycles
EMERGENCY WALL EEL INOP DOOR 5 LT AFT CROSS AISLE. REPLACED LAMP ASSY, OPS CHECK OK.
Part: HOSE — LEAKING (FUEL SYSTEM) · airframe 79,394 hrs · 9,751 cycles
FUEL COMING OUT OF DRAIN MAST FOR HORIZ STAB TRANSFER LINE. ALSO FUEL IN APU SHROUD DRAIN LINE. FUEL LEAK FROM HST TRANSFER LINE, LINE IS DRAINED AND HST SYSTEM INOP.
Part: LIGHT — EXPOSED (LAVATORY) · airframe 79,108 hrs · 9,720 cycles
EMERGENCY LIGHT LOCATED ON BOTTOM OF LAV 102 IS COMING OFF..WIRES EXPOSED. SECURED EMERGENCY LIGHT AT LAV 102 CORNER. ILLUMINATION TEST OKAY.
Part: CONNECTOR — SATURATED (EMERGENCY LIGHTS) · airframe 78,823 hrs · 9,687 cycles
EMERGENCY EXIT LIGHTS INOP. SEAT ROWS 45 THRU 53 LT, DOOR 4 LT FWD EXIT SIGN, DOOR 4 RT AFT. EXIT SIGN, LOWER WALL EMERGENCY LIGHT ACROSS DOOR 4 LT, AND DOOR 4 GALLEY AREA LOWER WALL EMERGENCY LIGHT. THIS IS A REPETITIVE PROBLEM IN THIS SPECIFIC AREA ON 84XX ACFT. FOUND WATER PUDDLING IN GALLEY AREA UNDER GALLEY MAT AT EMERGENCY LIGHT CONNECTOR, SHORTING LIGHTS. DRIED AREA OF WATER, EMERGENCY LIGHTS OPS CK NORMAL AT THIS TIME.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,823 hrs · 9,687 cycles
EMERGENCY EXIT LIGHTS INOP DOOR 5 RT FWD AND AFT SILL. RELAMPED. OPS, CKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,252 hrs · 9,621 cycles
DOOR 5 RT BOTH UPPER DOOR SILL EMERGENCY LIGHTS INOP, ABOVE DOOR EXIT SIGN INOPERATIVE. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,252 hrs · 9,621 cycles
UPPER DECK CEILING EMERGENCY LIGHT ROW 17 INOPERATIVE. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,252 hrs · 9,621 cycles
SEAT ROW 25 EMERGENCY SEAT LIGHT INOP RT HJK. RELAMPED, CHECKS OKAY.
Part: FEEDER CABLE — FAULTY (CABIN) · airframe 78,252 hrs · 9,621 cycles
SEAT ROWS 45-53 EMERGENCY LIGHTS STRIPS INOP, DOORS 4 LT AND 4 RT EXIT SIGN INOP, AFT GALLEY EMERGENCY LIGHTS STRIPS INOPERATIVE. REPLACED FEED IN JUMPER POWER CABLE FROM SEAT ROW TO GALLEY, OP CHECKS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,252 hrs · 9,621 cycles
SEAT ROW 21 HJK EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED SEAT ROW 21HJK EMERGENCY LIGHT STRIP, OP CHECKS GOOD ON GROUND.
Part: FIRE LOOP — FAULTY (NR 1 NACELLE) · airframe 78,252 hrs · 9,621 cycles
'ENG 1 FIRE LP B' EICAS STATUS MSG DISPLAYED. ENG 1 FIRE LOOP B FIRE OR FAULT OUTPUT. FAULT HAS OCCURED IN CRUISE, SUSPECT WIRING CHAFED. CHK NR1 ENG FIRE LP -B- WIRING UNDER EA-CLAMP FOR CHAFING, RING OUT FOR SHORTS-GND & RESIST REF FIM 26-11TSK852, REPAIR AS REQUIRED. PERFORMED INSP, CKD IAW MM. FOUND DETECTOR RESPONDER'S CERAMIC HSG AT LOWER FWD TS683 IS BROKEN. PART NEEDS TO BE REPLACED AS PART BECOMES AVAILABLE.
Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 78,252 hrs · 9,621 cycles
LT WING BODY EMERGENCY SLIDE LIGHT HAS ONLY ONE LAMP NR 3 LIGHT ASSY. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,044 hrs · 9,596 cycles
THE 16B SEAT LIGHTING INOPERATIVE. SEAT LIGHT BULB REPLACED & CHECKED OKAY.
Part: TENSION TIE — DAMAGED (FUSELAGE) · airframe 78,030 hrs · 9,595 cycles
RT TENSION TIE AT BS 1180 HAS DAMAGE. ACCMP'D CATEGORY 'B' REPAIR IAW SRM. PERFORM SUPPLEMENTAL INSPECTIONS AS GIVEN IN SRM. INSPECTION THRESHOLD AT 20,000 FLIGHT CYCLES AFTER AIRPLANE DELIVERY AND EVERY 3000 CYCLES THEREAFTER. CURRENT PTC:9595. ** MF5627 CREATED TO MONITOR **
Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 78,030 hrs · 9,595 cycles
STA 1120 RT SLOPING SHEAR WEB IS CRACKED IN 2 LOCATIONS. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR PARTS PER TMA 52593 CANTED SHEAR WEB REPAIR.
Part: FRAME — CRACKED (FUSELAGE) · airframe 78,030 hrs · 9,595 cycles
STA 1200 RT OUTBOARD OF TENSION CIRCUM FRAME CRACKED. INSTALL FRAME REPAIR PER SRM REPAIR 6.
Part: FRAME — CRACKED (FUSELAGE) · airframe 78,030 hrs · 9,595 cycles
STA 1200 RT FRAME IN CROWN NEAR TENSION TIE CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME ON DOCK WU K7642C PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 78,030 hrs · 9,595 cycles
STA 1140 LT FRAME AT STR 10A IS CRACKED AT CUTOUT LOWER RADIUS. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 78,030 hrs · 9,595 cycles
STA FRAME 1160 FWD FACE STR 9L CUT OUT LWR RADIUS IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER MM.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 78,030 hrs · 9,595 cycles
STA FRAME 1140, STR 10L AND 10A CUTOUT CRACKED AT LWR RADIUS. ACP REPAIR PER SRM REPAIR NR 7. REF SFOOV WRITE UPS L1059M & L1058M.
Part: FRAME — CRACKED (FUSELAGE) · airframe 78,030 hrs · 9,595 cycles
STA 1140 FRAME AT STR 9R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT THE DAMAGE AND INSTALLED FILLER AND A DOUBLER REPAIR.
Part: CDU — FAULTY (COCKPIT) · airframe 77,926 hrs · 9,580 cycles
R CDU BLANK, FLIGHT DIVERTED. MSG 34835 ACTIVE HARD. REPLACED RT MULTI PURPOSE CDU, CHECKS OKAY.
2009
Part: PSU — LEAKING (OXYGEN SYS) · airframe 77,383 hrs · 9,513 cycles
CREW O2 PRESSURE LOW, SUSPECT LEAK. PRESSURE DROP FROM 1500PSI TO 1370PSI. SUPPLEMENTAL DATA UPDATE SERVICED CREW 02 QTY TO 1810 PSI, AND WITHIN 30 MIN PRESSURE DROPPED TO 1730 PSI, AND IS CONTINUING TO DROP. 1ST OBS O2 BOX AND MASK REPLACED. LEAK CHECKS GOOD. SYSTEM HELD PRESSURE.
Part: FEEDER CABLE — CONTAMINATED (CABIN) · airframe 76,659 hrs · 9,429 cycles
EMERGENCY LIGHTS AT SEATS 57 KJH AND 49 KJH INOPERATIVE. FOUND FEEDER CABLE GOING TO GALLEY SIDEWALL LIGHTS FULL OF WATER. REPLACED FEEDER CABLE AND GRD CHECKED OK.
Part: CONNECTOR — CONTAMINATED (CABIN) · airframe 76,659 hrs · 9,429 cycles
TWO (2) GALLEY EMERGENCY CROSS AISLE LIGHTS INOP BETWEEN DOOR 2L AND 2R. FOUND CONNECTOR BY GALLEY WET AND REPLACED FEEDER CABLE. OPS CHECK OKAY.
Part: CABLE — DEFECTIVE (CABIN) · airframe 76,659 hrs · 9,429 cycles
DOOR 3L EMERGENCY EXIT LIGHT FORWARD INOP. FOUND CABLE BAD ON FLOOR, REPLACED AND GRD CHECKED OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,659 hrs · 9,429 cycles
EMERGENCY CEILING LIGHT INOP AT ROW 12. RELAMPED AND GRD CHECKED OKAY.
Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 76,393 hrs · 9,399 cycles
UPPER DECK DOOR EMERGENCY LIGHT TEST INOPERATIVE. FOUND EMERGENCY POWER BATTERY WEAK. REPLACED POWER BATTERY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT EEL LIGHT INOP, SEAT ROW 56 LEFT. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT LIGHT INOP, UPPER DECK CEILING ROW 15. RELAMPED, CHECKS OKAY.
Part: WIRE — LOOSE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT EEL LIGHT INOP, ACROSS LAV 100 LOWER WALL. FOUND LOOSE WIRE AT POWER SUPPLY. SECURED SAME.
Part: FEEDER CABLE — DAMAGED (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT EEL LIGHTS INOP, SEAT ROWS 45 THRU 53 LEFT, DOOR 4 LEFT FWD EXIT SIGN, DOOR 4 RIGHT AFT EXIT SIGN, LOWER WALL EEL ACROSS DOOR 4 LEFT, AND DOOR 4 GALLEY AREA LOWER WALL EEL. FOUND WATER UNDER GALLEY MAT SHORTING POWER FEEDER CABLE. DRIED AREA, REPLACED POWER FEEDER CABLE. ALL LIGHTS OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT LIGHT INOP, FWD STAIRS ILLUMINATION LIGHT AFT BULB. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT LIGHT INOP, UPPER DECK CEILING ROW 13. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT EEL LIGHT INOP, SEAT ROW 43 LEFT. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT EEL LIGHT INOP, SEAT ROW 41 LEFT. RELAMPED, CHECKS OKAY.
Part: BATTERY — DISCHARGED (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT LIGHT INOP, DOOR 5 RIGHT BUSTLE LIGHT. RECHARGED BATTERIES, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT LIGHT INOP, LEFT EXTERIOR OVERWING 2ND FROM AFT LIGHT ASSY. RELAMPED, OPS CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT EEL LIGHT INOP, SEAT ROW 57 RIGHT. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT EEL LIGHT INOP, SEAT ROW 53 RIGHT. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,135 hrs · 9,371 cycles
EMERGENCY EXIT LIGHT INOP, DOOR 4 LEFT FWD SILL LIGHT. RELAMPED, CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,411 hrs · 9,291 cycles
NR1 RT DOOR CEILING EMERGENCY LIGHT NOT ON. REPLACED LAMP. OPS CHECKS GOOD.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 75,411 hrs · 9,291 cycles
EEL INOP AT 45C-53C AND 56C. RECONNECTED EEL CONNECTOR. OP CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,038 hrs · 9,250 cycles
EEL INOP SEAT ROW 49 RT. REPLACED LAMP.
Part: LIGHT — CONTAMINATED (CABIN) · airframe 75,038 hrs · 9,250 cycles
EMERGENCY EXIT EEL LIGHTS INOP SEATS 45-53 RT, DOOR 4L FWD EXIT SIGN, DOOR 4R AFT EXIT SIGN, LWR WALL EEL ACROSS FROM DOOR 4L AND DOOR 4 GLY LWR WALL. OPENED GALLEY FLOOR MAT AND DRIED AREA OF WATER AND OTHER QUESTIONABLE LIQUIDS FROM AREA, OPS CHECKS NORMAL CURRENTLY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,038 hrs · 9,250 cycles
EMERGENCY LIGHT INOP CEILING ROW 3L. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL.
Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 75,038 hrs · 9,250 cycles
AFT CARGO DOOR LOWER FWD CORNER DAMAGED. NO CRACK INDICATION FOUND. MFG'D & INSTALLED DOUBLER/TRIPLER & FILLER REPAIR FOR AFT CARGO DOOR. TRIMMED AND PRIMED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,038 hrs · 9,250 cycles
EEL INOP SEAT ROW 56L. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,038 hrs · 9,250 cycles
EMERGENCY LIGHTS INOP LT OVERWING 3RD ASSY AFT, BOTH LAMPS. REPLACED LAMPS, CHECKS OKAY.
Part: CABLE — SHORTED (CABIN) · airframe 74,524 hrs · 9,186 cycles
EMERGENCY LIGHTS INOP AT DOOR 4 RT EXIT AND SEAT ROW 45 THRU 53. REPETITIVE PROBLEM WITH 84XX AIRCRAFT. REPAIRED SHORTS TO CABLE UNDER FLOOR MAT AND CARPETS NEAR LEFT CORNER OF GALLEY. OPS CHECKS NORMAL.
2008
Part: LIGHT — UNSECURE (LAVATORY) · airframe 73,740 hrs · 9,100 cycles
DOOR 1R LAV EMERGENCY LIGHT NEEDS TO BE SECURED. FOUND SCREW MISSING, SECURED WITH SCREW, OPS OK.
Part: CONNECTOR — LOOSE (CABIN) · airframe 73,438 hrs · 9,067 cycles
ZONE-D RIGHT SIDE SEAT EMERGENCY LIGHTS INOP (SEATS 33 - 43). RESECURED EMERGENCY LIGHT CONNECTOR, OP CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,438 hrs · 9,067 cycles
EMERGENCY LIGHT ROW 41 RT INOP. FOUND LIGHT INOP. REPLACED SEAT 41 RIGHT EMERGENCY LIGHT. OPS CHECKED GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 73,438 hrs · 9,067 cycles
ROWS 45 - 55 LEFT SEAT EEL LIGHT INOP. REPLACED BATTERY. CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,438 hrs · 9,067 cycles
DOOR 4 RIGHT AFT SILL LIGHT INOP. RELAMPED, OP CHECK NORMAL.
Part: FUSE — FAULTY (CHARGER) · airframe 73,438 hrs · 9,067 cycles
DOOR 1 RIGHT BOTH SILL LIGHTS INOP AND OVER DOOR EXIT SIGN INOP. REPLACED FUSE IN CHARGER. CHECKS OK.
Part: FEEDER CABLE — DEFECTIVE (CABIN) · airframe 73,438 hrs · 9,067 cycles
AFT GALLEY FWD AND LEFT EMERGENCY LIGHTS INOP. REPLACED FEEDER CABLE. CHECKS OKAY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,438 hrs · 9,067 cycles
SEAT 20 RIGHT EMERGENCY LIGHT INOP. FOUND LIGHT INOP. REPLACED SEAT 20 RIGHT EMERGENCY LIGHT. OPS CHECKED GOOD.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 73,167 hrs · 9,034 cycles
FOUND AFT GALLEY EMERGENCY LIGHT WIRE BROKEN. REPLACED AFT GALLEY LOWER SIDE WALL EMERGENCY LIGHT AND SECURED RIBBON CABLE. EMERGENCY EMERGENCY LIGHTS OP CHECKS NORMAL.
Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,298 hrs · 8,931 cycles
EMERGENCY LIGHT INOP: LT OVERWING 2 FWD ASSY'S. *S/D* FOUND FAULTY FUSE. REPLACED FUSE, OP CHECK GOOD. AC OK FOR SERVICE.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 72,298 hrs · 8,931 cycles
EMERGENCY LIGHT INOP: DOOR 5R SLIDE ILLUM. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 72,298 hrs · 8,931 cycles
EMERG LIGHT INOP: LT OVERWING 3RD ASSY AFT BULB. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,298 hrs · 8,931 cycles
WALL EEL INOP: LWR WALL BETWEEN MID LAVS. *S/D* FOUND BURNED OUT LIGHT ASSEMBLY. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,298 hrs · 8,931 cycles
EMERGENCY LIGHT INOP: DOOR 4L AFT SILL. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 71,764 hrs · 8,868 cycles
UPPER DECK FLOORBEAM UPPER CHORD AT BS 860 & 880, LBL 7 1.5, TOTAL OF 3 FASTENER HOLES MISDRILLED. PLUGGED FASTENER HOLES REF SRM 51-40-02. AC OK FOR SERVICE.
Part: SWITCH — INOPERATIVE (FIRE SWITCH) · airframe 71,748 hrs · 8,866 cycles
FWD CARGO FIRE ARM SWITCH INTERNAL LIGHT IS INOP, RELAMP NO HELP. SUSPECT FAULTY SWITCH. REPLACED LIGHTED SWITCH. AC OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,748 hrs · 8,866 cycles
EMERGENCY LIGHT ROW 3A AFT INOP. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.
Part: CONNECTOR — LOOSE (CABIN) · airframe 71,748 hrs · 8,866 cycles
EMERGENCY LIGHT ROW 4F AFT INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
EMERGENCY CEILING LIGHTS ROW 16-17 INOPERATIVE. SUPPLEMENTAL DATA UPDATE, SUSPECT FAULTY POWER SUPPLY. REPLACED POWER SUPPLY ASSEMBLY, OPS CHECKES NORMAL. A/C OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,748 hrs · 8,866 cycles
EMERGENCY LIGHT DR 4L SLIDE LIGHT INOP. SUSPECT LIGHT ASSEMBLY FAULTY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE.
Part: OXYGEN SYSTEM — READS LOW (PASSENGER) · airframe 71,476 hrs · 8,836 cycles
PASSENGER O2 SHOWS 1520. SERVICED O2 SYSTEM TO FULL. AC OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (SEAT 3A) · airframe 71,283 hrs · 8,818 cycles
EEL LIGHT INOP AT SEAT 3A. SUPPLEMENTAL DATA UPDATE, REPLACED LIGHT ASSY.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,283 hrs · 8,818 cycles
EEL LIGHT INOP AT SEAT 58 ABC. SUPPLEMENTAL DATA UPDATE, RELAMPED.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,283 hrs · 8,818 cycles
EEL LIGHT INOP AT SEAT 48 ABC. SUPPLEMENTAL DATA UPDATE, RELAMPED.
Part: B-NUT — LEAKING (PAX OXYGEN) · airframe 71,215 hrs · 8,809 cycles
PAX O2 READS 1460 PSI FROM COCKPIT EICAS. AFTER EXTENSIVE TROUBLE SHOOTING FOUND LEAK IN OXYGEN LINE B-NUT. TIGHTENED B-NUT SERVICED OXYGEN SYSTEM. AC OK FOR SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,835 hrs · 8,766 cycles
RIGHT EXTERIOR EMERGENCY LIGHT ASSY NR 3 FROM TOP HAS ONE LAMP INOP, RELAMPED.
Part: LIGHT — INOPERATIVE (SEAT 58 HJK) · airframe 70,835 hrs · 8,766 cycles
EMERGENCY LIGHT INOP AT 58 HJK. REPLACED LIGHT ASSEMBLY.
Part: FIRE DETECTOR — INTERMITTENT (AFT CARGO BAY) · airframe 70,229 hrs · 8,699 cycles
THE 'FIRE CARGO AFT' EICAS WARNING MESSAGE DISPLAYED. REPLACED DETECTOR PER MM26-16-01-401, OPS NORMAL. AC OK FOR SERVICE.
2007
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,908 hrs · 8,665 cycles
DOOR 4 LEFT EMERGENCY CROSS AISLE LIGHT IS INOP. RELAMPED.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,908 hrs · 8,665 cycles
SEAT 2J AFT EMERGENCY LIGHT IS INOPERATIVE. RELAMPED.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,908 hrs · 8,665 cycles
EMERGENCY LIGHT NEAR ROW 17 RIGHT IS INOP. RELAMPED.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,908 hrs · 8,665 cycles
DOOR 3 RIGHT LOWER WALL EMERGENCY LIGHT IS INOP. RELAMPED.
Part: FRAME — CRACKED (FUSELAGE) · airframe 69,436 hrs · 8,619 cycles
DOORWAY 5L FWD FRAME TORQUE TUBE COVER FRAME CRACKED AT STR 23L-25L. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME SECTION.
Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHTS) · airframe 69,436 hrs · 8,619 cycles
DOOR 1L EMERGENCY EXIT LIGHT INTERMITTENT. REPLACED BATTERY PACK.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,436 hrs · 8,619 cycles
DOOR 5L EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK.
Part: SKIN — DENTED (FUSELAGE) · airframe 69,436 hrs · 8,619 cycles
EXTERNAL FUSELAGE IS DENTED. INSTALLED EXTERNAL DOUBLER REF SRM 53-00-01 FIG 201. AC OK FOR SERVICE.
Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHTS) · airframe 69,436 hrs · 8,619 cycles
THE E-ZONE RT FWD EEL STRIP INTERMITTENT. REPLACED BATTERY PACK. OP CHECKED OK.
Part: SKIN — CRACKED (FUSELAGE) · airframe 69,436 hrs · 8,619 cycles
AFT CARGO DOOR CUTOUT UPPER FWD CORNER, 1 EACH FASTENER HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER, TRIPLER & QUADRUPLER REPAIRS.
Part: STRUCTURE — CORRODED (AFT CARGO DOOR) · airframe 69,436 hrs · 8,619 cycles
MAJOR REPAIR: AFT CARGO DOOR INSIDE LWR AFT AREA CORROSION, 6 PLACES. INSTALLED DOUBLER REF SRM 51-70-13 FIG 201. AC OK FOR SERVICE.
Part: LAMP — FAULTY (EMERGENCY LIGHTS) · airframe 69,436 hrs · 8,619 cycles
DOOR 4L DOOR MOUNTED EMERGENCY EXIT LIGHT DIM. RELAMPED.
Part: DOOR FRAME — CRACKED (L5 DOOR) · airframe 69,436 hrs · 8,619 cycles
NR 5 LT MED UPPER FRAME CRACKED AT CENTER UPPER GATE HINGE ATTACH HOLE. REPAIRED CRACK PER IAW SRM 80-52-10-08-JD PG 15 & SRM 51-70-11.
Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 69,436 hrs · 8,619 cycles
NR 1 RIGHT MED UPPER FRAME CRACKED AT CENTER UPPER GATE HINGE ATTACH HOLE. REPAIRED CRACK PER IAW FRR UAL-744-0317.
Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 69,436 hrs · 8,619 cycles
NR 1 LEFT MED UPPER FRAME CRACKED AT CENTER UPPER GATE HINGE ATTACH HOLE. REPAIRED CRACK PER IAW FRR UAL-744-0317.
Part: FRAME — CRACKED (BS 1265) · airframe 69,436 hrs · 8,619 cycles
BS 1265 LEFT FRAME WEB CRACKED AT NR 1 FASTENER HOLE. REPAIRED FRAME WEB ACCOMPLISHED COA 897887102. AC OK FOR SERVICE.
Part: DOOR — DAMAGED (R1) · airframe 69,436 hrs · 8,619 cycles
NR 1 LT & 1 RT PAX DOORS HAVE DAMAGE. REPAIRED.
Part: SKIN — DAMAGED (LT TE FLAP) · airframe 69,431 hrs · 8,617 cycles
ON ARRIVAL FOUND DAMAGE AT LEFT INBOARD T/E FLAP LOWER SKIN BY 2.5 INCH X 1 INCH DENT AND 2.5 U-SHAPE CRACK AND 1.25 INCH IN SIDE DENT. DENT IS 5 INCHES FROM T/E SIDE FASTENER AND 11 INCHES FROM L/E FASTENER. ALSO, 17.5 INCH FROM FLAP L/E AND 20 INCHES FROM T/E. REPAIRED FLAP PER SRM 51-70-10 REPAIR 4 PG 201. AC OK FOR SERVICE.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,205 hrs · 8,596 cycles
RIGHT OVERWING AFT TWO EMERGENCY LIGHT ASSY IS INOP. 10-19-07 REPLACED BATTERY CHARGER UNIT. OP CHECKS NORMALLY.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,771 hrs · 8,552 cycles
EMERGENCY LIGHT INOPERATIVE AT 3A AFT. 08-31-07 REPLACED LAMP ASSY. OP CHECKED OK.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,771 hrs · 8,552 cycles
CEILING EMERGENCY LIGHTS INOP AT ROWS 13, 17 & 48R. 08-31-07 RELAMPED ALL THREE POSITIONS. ALL OP CHECKOK FOR SERVICE.
Part: ASPIRATOR — LEAKING (SLIDE RAFT)
ASPIRATOR LEAKS FROM THE FLAP VALVES. REPLACED ASPIRATOR, CAUSE UNKNOWN. 08-31-07 SUSPECT IMPROPER ASSY OF JET PLATE ASSY DURING RESTORATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,329 hrs · 8,500 cycles
EEL AT 5E AFT & 52ABC ARE INOPERATIVE. RELAMPED.
Part: FUSE — BLOWN (POWER SUPPLY) · airframe 86,329 hrs · 8,500 cycles
EMERGENCY LIGHTS INOP RIGHT OVERWING BODY FAIRING TWO AFT ASSEMBLIES. REPLACED FUSE IN POWER SUPPLY.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,329 hrs · 8,500 cycles
EMERGENCY LIGHT INOP AT DOOR 5L FWD & AFT SILL. REPLACED POWER SUPPLY.
Part: FEEDER CABLE — FAULTY (EMERGENCY LIGHT) · airframe 86,329 hrs · 8,500 cycles
EEL AT DOOR 5R XAISLE INOP. REPLACED FLOOR RIBBON CABLE AT DOOR 5 RIGHT. CHECKS NORMAL.
Part: SLIDE — FAULTY (DOOR 3R) · airframe 68,229 hrs · 8,486 cycles
AFTER POWER UP THE ACFT FOUND DOOR 3R INDICATOR SHOW DOOR OPENED. AFTER CHECK FOUND SLIDE RAFT WAS LAID DOWN ON THE FLOOR NEAR BY DOOR 3R. [08-07-07] REPLACED 3R SLIDE RAFT ASSY PER MM 25-65-16. CHKD OK. -INSPECTED INSTALLATION OF DR-3R SLIDE RAFT ASSY PER MM 25-65-16. NO DEFECTS NOTED. AFTER INSTALLATION, DISCOVERED AFT RELEASE HANDLE OF RAFT COVER CAME OFF. MADE INTERIM REPAIR BY BOLTING INTO HINGE OF BUSSLE.
Part: LIGHT — INOPERATIVE (SEAT 5E AFT) · airframe 67,901 hrs · 8,451 cycles
SEAT 5E AFT EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 67,901 hrs · 8,451 cycles
DOOR 5R CROSS AISLE & SEAT 50 HJK EMERGENCY LIGHTS ARE INOP. *S/D* SECURED CONNECTION.
Part: CARGO TRACK — CRACKED (BS 1850) · airframe 67,585 hrs · 8,417 cycles
AFT CARGO PIT STA 1850 2ND CARGO TRACK FROM ENTRANCE HAS 10 INCH CRACK AT PALLET LOCKDOWN AREA. [SUP 05-29-07] MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW TRACK SECTION FROM AFT END TO EXISTING SPLICE SECTION IN AFT PIT.
Part: LIGHT — INOPERATIVE (SEAT 5E AFT) · airframe 67,437 hrs · 8,401 cycles
EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5E AFT ASSY. [SUP 06-01-07] SECURED LT ASSY OPS NORMAL.
Part: FEEDER CABLE — FAULTY (EMERGENCY LIGHTS) · airframe 67,437 hrs · 8,401 cycles
EMERGENCY EEL LIGHT INOP ACROSS DOOR 4R LOWER WALL. [SUP 06-01-07] REPLACED FEEDER CABLE OPS NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,437 hrs · 8,401 cycles
EMERGENCY EXIT SILL LIGHTS BOTH FWD AND AFT INOPERATIVE AT DOOR 5L. [SUP 06-06-07] REPLACED BATTERY PACK . OP CHECKS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,437 hrs · 8,401 cycles
EMERGENCY EXIT SIGN INOP AT AFT CREW REST AREA. [SUP 06-06-07] RELAMPED NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,437 hrs · 8,401 cycles
EMERGENCY EXIT SIGN INOPERATIVE ABOVE DOOR 5L & JUST AFT OF ROW 61L. [SUP 06-06-07] REPLACED BATTERY PACK . OP CHECKS NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,437 hrs · 8,401 cycles
EMERGENCY EXIT CEILING ENTRY LIGHT INOP AT DOOR 5L. [SUP 06-06-07] REPLACED BATTERY PACK . OP CHECKS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,437 hrs · 8,401 cycles
EMERGENCY EXIT CEILING LIGHT AT UPPER DECK ROW 12 & ENTRY LIGHT AT DOOR 2R ARE INOPERATIVE. [SUP 06-01-07] RELAMPED NORMAL.
Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 67,437 hrs · 8,401 cycles
EMERGENCY EXIT LIGHT VERY DIM AT DOOR 1L BUSTLE. [SUP 06-06-07] RECHARGED BATTERY PACK OPS NORMAL
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,437 hrs · 8,401 cycles
OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP, RIGHT SIDE 2 AFT LIGHT ASSEMBLIES. [SUP 06-06-07] REPLACED BATTERY PACK. OP CHECKS NORMAL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,976 hrs · 8,353 cycles
EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5A AFT. *S/D* RELAMPED EEL.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,976 hrs · 8,353 cycles
EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5A AFT. *S/D* 4-17-07 RELAMPED. OP CHECKED NORMALLY.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 66,976 hrs · 8,353 cycles
EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 1J AFT. SECURED CONNECTOR. OPS CHECKS NORMAL.
Part: SKIN — DENTED (CARGO DOOR) · airframe 66,063 hrs · 8,257 cycles
AFT MANUAL PIT DOOR, TWO DEEP DENTS APPROX 8" AFT OF FWD EDGE AT MID POINT IN DOOR. INSTALLED EXTERNAL DOUBLER REF SRM. CREATED MF5469 TO MONITOR & CALL-OUT VISUAL RECHECK EVERY 250 CYCLES, EDDY CURRENT RECHECK EVERY 1500 CYCLES. & REPAIR NEXT SCHEDULED MAJOR MAINT CHECK. SUSPECT IMPACT WITH GROUND EQUIPMENT.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,063 hrs · 8,257 cycles
LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. RELAMPED BOTH SIDES; OP CHECKED OK.
Part: LAMP — FAULTY (EMERGENCY LIGHT) · airframe 66,063 hrs · 8,257 cycles
EEL'S INOP ON CEILING AT SEAT ROW 56R. EEL BROKEN AT SEAT 1J. RELAMPED BOTH POSITIONS; OP CHECKED OK.
2006
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 65,321 hrs · 8,179 cycles
EEL INOP AT 2J AFT AND 43H. RELAMPED, OP CHECKS OK.
Part: FLOORBOARD — DAMAGED (BS 1670) · airframe 65,064 hrs · 8,150 cycles
RAMP REPORTED AFT CARGO PIT FLOOR DAMAGED IN FLOOR, TWO AREAS. TORQUE BOX PANEL PUNCTURED AT STA 1670,4 FT AND 5 FT RT OF CL APPROX 2" AND 4" HOLES. ACCOMPLISHED INTERIM DOUBLER REPAIR WITH HI-SPEED TAPE PER UA-EVA-60652.ACCOMPLISHED REPAIR PER SRM. SUSPECT CARGO LOADING DAMAGE CAUSED BY IMPACT OR FLIGHT IMPOSED LOADS.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,391 hrs · 8,075 cycles
LEFT OVERWING EMERGENCY LIGHT 2ND BOTTOM INOPERATIVE. REPLACED BATTERY CHARGER. OP CHECKS OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,391 hrs · 8,075 cycles
F-D & ABOVE ROW 13 EMERGENCY CEILING LIGHTS INOPERATIVE. RELAMPED. OP CHECKS OK.
Part: ENGINE — VIBRATION (NR 3) · airframe 63,128 hrs · 7,931 cycles
AT FL320, NR 3 ENG HIGH EGT, HIGH VIBES AND HIGH OIL PRESS PER CREW. EGT REACHED 670C. AFTER SHUTDOWN, ENG WINDMILLING, VIBES FELT IN AIRFRAME AND OIL PRESS INDICATES ZERO. SHOP TEARDOWN SHOWED THE ROOT CAUSE TO BE FAILURE OF A STAGE-2 HIGH PRESSURE TURBINE BLADE. THE BLADE HAD FAILED UNDER THE PLATFORM DUE TO STRESS CORROSION CRACKING (SCC). FOUR ADJACENT BLADES SUBSEQUENTLY FRACTURED AT THE PLATFORM CAUSING THE HEAVY VIBRATION. THE STAGE-1 HUB, BLADES, AND ROTATING AIRSEAL HAD TO BE SCRAPPED DUE TO HEAVY RUB. THE SCC FAILED BLADE HAD 19733 HOURS SINCE NEW. INCORPORATING PRATT & WHITNEY SERVICE BULLETIN PW4ENG 712-263.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,021 hrs · 7,918 cycles
EEL BETWEEN ROWS 1 AND 5 LT INOP.
Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 63,021 hrs · 7,918 cycles
EEL AT ROWS 4E AND 5E LT INOP. REPAIRED AND TIGHTENED CONNECTORS. OP CHECKS OK.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 63,021 hrs · 7,918 cycles
FOUND EMERGENCY LIGHT AT DR 1R FWD THRESHOLD INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,021 hrs · 7,918 cycles
EEL LIGHT INOP AT AISLE BETWEEN AFT GALLEY AND DR 4R.
Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 62,292 hrs · 7,840 cycles
FOUND EMERGENCY LIGHTS FLASHING AROUND DOOR 5.
2005
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,636 hrs · 7,761 cycles
EMERGENCY LIGHT AT ROW 23 LT CEILING INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,636 hrs · 7,761 cycles
EEL AT SEAT 5E AFT, 3J AFT, 5J AFT INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,636 hrs · 7,761 cycles
DOOR 2R BUSTLE EMERGENCY LT INOP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,636 hrs · 7,761 cycles
EMERGENCY LIGHT ASSY AT RT BODY FAIRING INOP, 2ND ROW FROM FWD AND AT RT BODY FAIRING 2ND ASSY FROM AFT.
Part: TIRE — FAILED (MLG) · airframe 60,926 hrs · 7,681 cycles
TWO LEFT MAIN TIRES BLEW. TWO LEFT REAR BODY GEAR TIRES BLOWN DURING TAKEOFF ROLL. DAMAGE TO BODY GEAR STEERING AND FAIRING. REPLACED BOTH TIRE ASSEMBLIES AND REPAIRED DAMAGE.
2004
Part: HANDLE — MALFUNCTIONED (DOOR ASSIST) · airframe 56,963 hrs · 7,199 cycles
UPPER DECK DOOR LEFTSIDE ASSIST STRAP NEEDS TO BE ON FORWARD HANDLE NOT AFT. PREVIOUS MAINTENANCE WORK PERFORMED WAS NOT IN ACCORDANCE WITH INSTRUCTIONS IN 747 AIRCRAFT MAINTENANCE MANUAL AND ILLUSTRATED PARTS CATALOG, CAUSING DISCREPANT CONFIGURATION. MIS-LOCATED STRAP WAS REMOVED AND INSTALLED IN PROPER LOCATION.
Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 53,860 hrs · 6,799 cycles
LIGHTNING STRIKE BLENDED OUT OF LIMIT AT STA 190 AND STRINGER 28AL (LEFT). MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED EXTERNAL SKIN DOUBLER.
2003
Part: FAN — ODOR (CABIN) · airframe 52,998 hrs · 6,684 cycles
ELECTRICAL BURNING ODOR WITH ASSOCIATED STATUS MESSAGE RECIRC FAN UPPER L DISPLAYED. THE UPPER RIGHT RECIRCULATION FAM MOTOR BEARINGS FAILED.THE RECIRCULATION FAN WAS REPLACED.
Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 52,689 hrs · 6,645 cycles
LIGHTNING STRIKE DAMAGE AT STA 134.75 AND STR 45R. MAJOR REPAIR ACCOMPLISHED. EXTERNAL DOUBLER REPAIR.
2002
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,583 hrs · 5,890 cycles
AT SEAT 5A, AFT EEL LIGHT IS INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,583 hrs · 5,890 cycles
AT SEAT 5J, AFT EEL LIGHT IS INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,583 hrs · 5,890 cycles
AT DOOR 5 RIGHT HAND SIDE, THE FORWARD EEL SILL LIGHT IS INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,583 hrs · 5,890 cycles
AT SEAT 3J, AFT EEL LIGHT IS INOP. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,583 hrs · 5,890 cycles
CEILING EEL LIGHT IS INOP AT ROW 16. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,583 hrs · 5,890 cycles
AT DOOR 5 RIGHT HAND SIDE THE FORWARD EEL SILL LIGHT IS INOP. REPLACED LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,583 hrs · 5,890 cycles
ON LEFT SIDE OF AIRCRAFT, THE SECOND ASSEMBLY BACK FROM THE FRONT, THE FORWARD BULB IS INOP ON THE OVERWING EEL. RELAMPED.
2001
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 46,692 hrs · 5,756 cycles
STATION 1700 FLOORBEAM UPPER CHORD HAS EXCESSIVE MATERIAL AT RBL 44. ANGLES AND STIFFENERS ANGLES INSTALLED.
Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 46,692 hrs · 5,756 cycles
NR 2 RIGHT HAND MED UPPER DOOR FRAME AT GATE HAS CRACK ATTACH HOLE. DOOR SHOP ACCOMPLISHED REPAIR.
Part: FRAME — PUNCTURED (FUSELAGE) · airframe 46,692 hrs · 5,756 cycles
FORWARD PIT FRAME WEB AT STATION 620 RBL 40 PUNCTURED. MAJOR REPAIR ACCOMPLISHED TO FORWARD PIT WEB AT STATION 620 RBL 40.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,692 hrs · 5,756 cycles
BS 520 FLOORBEAM UPPER CHORD EXCESSIVELY CORRODED. BLENDED BEYOND LIMITS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,324 hrs · 5,702 cycles
EMERGENCY EXIT SIGN AT ROW 22B HAS SOME LAMPS INOP.
Part: WINDOW — FAILED (COCKPIT) · airframe 44,294 hrs · 5,430 cycles
NUMBER THREE COCKPIT LEFT WINDOW INNER PANE SHATTERED INFLIGHT. CREW NOTED PRIOR TO WINDSHIELD FAILURE WINDOW WAS FROSTED OVER AND NOT DEFOGGING. REMOVED WINDOW AND FOUND CORROSION ON UPPER AND AFT LOWER SIDES.
2000
Part: GASPER FAN — FAILED (CABIN) · airframe 40,613 hrs · 5,011 cycles
REPORT OF BURNING SMELL IN COACH CABIN. TURNED OFF RECIRCULATING FANS AND SMELL WENT AWAY. *S/D* GASPER FAN REPLACED. NO FURTHER PROBLEMS.
1998
Part: BRACE — GOUGED (NR 1 PYLON)
A .060 INCH DEEP GOUGE IN PYLON NUMBER ONE DIAGONAL BRACE. THE GOUGE IS 40 INCHES FORWARD OF AFT END OF DIAGONAL BRACE AND 1.74 INCHES LONG BY .5 INCH WIDE. CAUSED BY CONTACT WITH STEEL PNEUMATIC LINE. PYLON NUMBER ONE DIAGONAL BRACE REPLACED BEFORE FURTHER FLIGHT. NO SUCH CONDITION DETECTED ON THE OTHER THREE PYLON DIAGONAL BRACES. UAL ACFT WITH SIMILAR CONFIGURATION TO BE CHECKED FOR DAMAGE.
1996
Part: WIRE — BROKEN (CABIN)
EMERGENCY EXIT LIGHT AT CROSS AISLE IN FORWARD GALLEY INOP. BROKEN EMERGENCY EXIT LIGHT CABLE, REPAIRED CABLE.
Part: ENGINE — BIRDSTRIKE (NR 3)
SHORTLY AFTER TAKEOFF, INGESTED NUMEROUS BIRDS INTO NUMBER THREE ENGINE, ENGINE STALLED AND CREW WAS UNABLE TO RESTART. ACFT RETURNED TO SYD. *S/D* BIRD STRIKE IN NR 3 ENGINE. REPLACED ENGINE AND FAN BLADES.
1995
Part: EEL — INOPERATIVE (CABIN)
EEL IS INOP FROM ROW 35 TO ROW 45 ON RIGHT SIDE OF AIRCRAFT. FEEDER STRIP REINSTALLED PER WIRING DIAGRAM.