N964TW

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 52,299 hrs · 26,228 cycles

UPPER RIGHT PORTION OF FLIGHT OFFICERS WINDSHIELD STARTED ARCING DURING CRUISE. CIRCUIT BREAKER Z24 WAS PULLED IAW QRH PROCEDURE ANTI FOG SYSTEM WAS OFF. ARCING DAMAGE CONSISTS OF SNAKE 3 TO 4 INCHES LONG AT THE TOP OF THE WINDSHIELD AND DOES NOT OBSTRUCT VIEWING. THE AIRCRAFT WAS GROUNDED. REPLACED RIGHT WINDSHIELD IAW AMM 56-10-02. OPS CHECKED NORMAL.

Part: UNKNOWN — ODOR (GALLEY) · airframe 51,501 hrs · 25,711 cycles

UNUSUAL ODOR IN FORWARD GALLEY, INFLIGHT. INSPECTED THE FORWARD GALLEY COFFEEMAKERS, OVENS, CEILING LIGHTS, ELECTRICAL CONNECTORS, AND TRASH CAN. REPLACED FORWARD GALLEY BOTTOM COFFEEMAKER AS A PRECAUTION IAW AMM 25-39-02. OK FOR SERVICE.

Part: SKIN — CORRODED (BS 1304-1307) · corrosion level 2 · airframe 51,336 hrs · 25,584 cycles

CORROSION ON THE FUSELAGE SKIN INTERNAL SURFACE AROUND THE AFT LAVATORY PAN. REPAIRED THE SKIN IAW SRM 51-70-04, AND EA 281446.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 51,336 hrs · 25,584 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK IN LEFT LONGERON AT STA 993 ABOVE INBOARD FLAP TRACK. REPAIRED LONGERON PER 53-10-00-18.

Part: SLIDE — DISCONNECTED (SERVICE DOOR) · airframe 50,890 hrs · 25,303 cycles

THE AIRCRAFT WAS GROUNDED. AFT GALLEY SERVICE DOOR SLIDE HAS CABLE DISCONNECTED FROM GIRT BAR. REMOVED AND REPLACED AFT SERVICE DOOR SLIDE PER AMM 25-62-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,701 hrs · 24,556 cycles

EMERGENCY EXIT LIGHT IN THE CEILING BY THE AFT SERVICE DOOR IS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK B5-107 IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: CONNECTOR — DEFECTIVE (ZONE 200) · airframe 49,678 hrs · 24,541 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT ON THE LEFT STAIRWELL PANEL HAS WIRES PULLED FROM CONNECTOR. REMOVED AND REPLACED CONNECTOR PER WDM 33-51-15. OPERATIONAL CHECK GOOD.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,474 hrs · 24,403 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE PACK FELL OUT OF HOUSING. REINSTALLED SLIDE PER AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 49,144 hrs · 24,193 cycles

FLIGHT ATTENDANT EMERGENCY LED FLASHLIGHT AT THE AFT TAILCONE JUMPSEAT DOES NOT FLASH. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-60-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,057 hrs · 24,132 cycles

THE AIRCRAFT WAS NOT GROUNDED. COCKPIT OVERHEAD EMERGENCY LIGHTS INOP. REPLACED B5-23 EMER LIGHTS BATTERY PACK, OPER TEST NORMAL PER MM 33-53-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 48,930 hrs · 24,050 cycles

COCKPIT EMERGENCY LIGHT DOES NOT WORK WITH EMERGENCY LIGHT SWITCH ON. REMOVED & REPLACED THE FWD GALLEY OVERHEAD EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-00.

Part: WIRE — BROKEN (CABIN) · airframe 48,747 hrs · 23,927 cycles

AFT STAIRWAY LEFT SIDE EMERGENCY LIGHT HAS BROKEN WIRE. REPLACED EMERGENCY EXIT LIGHT QUICK DISCONNECT IAW WDM 33-51-13. THE AIRCRAFT WAS NOT GROUNDED.

Part: REGULATOR — FAILED (CABIN PRESSURE) · airframe 48,747 hrs · 23,927 cycles

AT 32,000 FT IN HEAVY RAIN, WITH ALL ANTI ICE SYSTEMS ON, ATC ASSIGNED MACH73, LOSS OF AIRSPEED, PUSHED THROTTLES UP POSSIBLY ABOVE CLIMB EPR. NO RED LIMITS EVER RECEIVED DURING THE 10-15 SECS OF PUSH UP ON THROTTLES, GOT A HOT SMELL IN COCKPIT. ODOR WENT AWAY ALMOST IMMEDIATELY. ACCOMPLISHED WORK CARD 21-96-01 REPLACED LT AIR CONDITIONING PILOT PRESSURE REGULATOR PER AMM 21-31-11. OPS CK OK NO LEAKS NOTED NO ODORS DETECTED AT THIS TIME. THE AIRCRAFT WAS GROUNDED.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 48,073 hrs · 23,498 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. SHEAR TIE AT AFT SIDE OF STATION 1380 FUSELAGE FRAME AND L14R IS CRACKED. REPAIRED SHEAR TIE IAW AARD 53-10-00-20.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,073 hrs · 23,498 cycles

AIRCRAFT WAS GROUNDED. FUSELAGE CANT FRAME AT STATION 1485 IS CRACKED AT L16R. REPAIRED FRAME IAW AARD 53-10-00-15 AND SRM 51-30-02.

Part: FITTING — CRACKED (RT SPOILER) · airframe 48,073 hrs · 23,498 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. RIGHT WING GROUND SPOILER FITTING IS CRACKED. REMOVED AND REPLACE FITTING IAW SRM 51-30-02-001 AND SRM 51-30-05-001.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 48,073 hrs · 23,498 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. RIGHT WING #4 SLAT TRACK INBOARD SUPPORT RIB IS CRACKED. REPAIRED RIB IAW MCM 57-98-06 AND EA 266888.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,073 hrs · 23,498 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. FUSELAGE FRAME AT STATION 1401 IS CRACKED AT K1. REPAIRED FRAME IAW AARD 53-10-00-15.

Part: PIN — OUT OF POSITION (EVAC SLIDE) · airframe 47,583 hrs · 23,176 cycles

AIRCRAFT WAS GROUNDED. R2 DOOR SLIDE PACK HAS PINS NOT IN CORRECT LOCATION. REMOVED AND REPLACED SLIDE PACK IAW AMM 25-62-00.

Part: BEARING — FAILED (NLG) · airframe 47,043 hrs · 22,847 cycles

WHILE CLEARING THE RUNWAY AFTER LANDING, THERE WAS A VIBRATION AND NOISE IN THE NOSE WHEEL AREA. AIRCRAFT STOPPED ON TAXIWAY. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE RIGHT NOSE WHEEL BEARING FAILED RESULTING IN DAMAGE TO THE NOSE LANDING GEAR RIGHT AXLE, THE RIGHT SPRAY DEFECTOR AND BOTH NOSE WHEEL ASSEMBLIES. REMOVED AND REPLACED RIGHT AND LEFT NOSE WHEEL ASSEMBLIES, RIGHT SPRAY DEFLECTOR AND THE NOSE GEAR CYLINDER, PISTON AND AXLE IAW AMM 32-21-02. SYSTEM CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,018 hrs · 22,828 cycles

OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 22 AND 26 FAIL TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-53-00. OPS CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,018 hrs · 22,828 cycles

OVERHEAD EMERGENCY LIGHTS AT AFT CABIN DOOR FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-53-00. OPS CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,018 hrs · 22,828 cycles

TAIL COMPARTMENT EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW AMM 33-53-00. OPS CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,018 hrs · 22,828 cycles

FORWARD EMERGENCY LIGHTS FAILED TO TEST WHEN CHECKED WITH BATTERY PACK AB5-1 IAW "B" CHECK CARD. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-60-98. OPS CHECKED NORMAL.

Part: SWITCH — LEAKING (APU) · airframe 46,963 hrs · 22,791 cycles

AT GATE AN ACRID ODOR WAS REPORTED WITH APU SUPPLYING THE LEFT PACK. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE APU OIL SEQUENCING SWITCH LEAKING. REMOVED AND REPLACED SWITCH. SYSTEM CHECKED NORMAL.

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 46,842 hrs · 22,714 cycles

DURING CLIMB, CREW REPORTED A BIRDSTRIKE ACCOMPANIED BY A BURNING ODOR IN AIRCRAFT. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. NR 2 ENGINE INSPECTION REVEALED DAMAGED FAN BLADES. REMOVED AND REPLACED 2 PAIRS OF FAN BLADES IAW WORKCARD 72-91-11. OPS AND LEAK CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,836 hrs · 22,133 cycles

OVERHEAD EMER LIGHTS AT ROWS 23 - 25 WON`T TEST. REPLACED EMER LIGHTS BATTERY PACK FOR ROWS 23 - 25 IAW AMM 33-53-00. OPERATIONS CHECKS NORMAL. THE ACFT WAS NOT GNDED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,836 hrs · 22,133 cycles

AFT EPL LIGHTS WON`T TEST WHEN USING PACKS AB5-2 & AB5-3. REPLACED BATTERY FOR AFT EPL LIGHTS AB5-3 IAW MM 33-60-00. OPERATIONS CHECKS NORMAL. THE ACFT WAS NOT GNDED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,836 hrs · 22,133 cycles

TAIL COMPARTMENT EMER LIGHTS WON`T TEST. REPLACED TAIL COMPARTMENT EMER LIGHTS BATTERY PACK IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL. THE ACFT WAS NOT GNDED.

Part: UFI — MALFUNCTIONED (FUEL SYSTEM) · airframe 45,321 hrs · 21,801 cycles

CENTER PUMP LOW LIGHT CLIMBING THROUGH 5,000. ACCOMPLISHED QRH PROCEDURE & DIVERTED. NO EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS GNDED. PLACED THE CTR TANK FUEL BOOST PUMP ON MEL DEFERRAL. R & R BOTH CTR PUMP UFI`S & TESTED IAW 28-20-28. TEST PASSED. REMOVED PLACARD & CLEARED MEL. SEE ALSO SDR AALA20160512002.

Part: UFI — FAULTY (FUEL SYSTEM) · airframe 45,321 hrs · 21,801 cycles

CENTER PUMP LOW LIGHT CLIMBING THROUGH 5,000. ACCOMPLISHED QRH PROCEDURE & DIVERTED. NO EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS GNDED. PLACED THE CTR TANK FUEL BOOST PUMP ON MEL DEFERRAL. R & R BOTH CTR PUMP UFI`S & TESTED IAW 28-20-28. TEST PASSED. REMOVED PLACARD & CLEARED MEL. SEE ALSO SDR AALA 20151221008.

Part: RELAY — MALFUNCTIONED (FUEL SYSTEM) · airframe 44,992 hrs · 21,613 cycles

AIRCRAFT AIR INTERRUPT DUE TO CTR FUEL NOT FEEDING. AN EMERGENCY WAS DECLARED & THE FLIGHT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R RELAYS M09901 T0990 IAW AMM 28-20-28, OPS CHECKED NORMAL.

Part: MODULE — ACTIVATED (COCKPIT) · airframe 44,856 hrs · 21,528 cycles

ON ROTATION CTR FUEL PRESS LOW LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE WHICH INDICATED TRAPPED FUEL IN CTR TANK. FLIGHT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. LANDED AT 126,600 LBS. INDICATED CTR FUEL 8800 LBS. ACFT REMOVED FROM SERVICE. R & R FUEL QTY SEM UNIT IAW AMM 28-40-00 & GROUND OPS TESTED NORMAL.

Part: MODULE — FAULTED (FUEL SYSTEM) · airframe 44,852 hrs · 21,524 cycles

RIGHT WING FUEL QTY FLUCTUATES PLUS OR MINUS 2000 POUNDS. AN EMERGENCY WAS DECLARED & ACFT LANDED WITHOUT FURTHER INCIDENT. R & R FUEL QTY SEM UNIT IAW AMM 28-40-00 & GND OPERATIONS TESTED NORMAL.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 44,773 hrs · 21,480 cycles

DURING CLIMB CREW NOTED FUEL MIGRATING INTO THE CTR TANK & WOULD NOT TRANSFER OUT. ACCOMPANIED BY A CTR LOW PRESSURE LOW LIGHT INDICATION. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL. R & R CTR TANK FWD & AFT UFIS. PERFORMED OPERATIONAL CHECK IAW AMM 28-20-28. SEE ALSO AALA20150917008 FOR FWD UNIT.

Part: UNKNOWN — FAULTY (FUEL SYSTEM) · airframe 44,773 hrs · 21,480 cycles

AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB CREW NOTED FUEL MIGRATING INTO THE CTR TANK & WOULD NOT TRANSFER OUT. ACCOMPANIED BY A CTR LOW PRESS LOW LIGHT INDICATION. R & R CTR TANK, FWD & AFT UFIS. PERFORMED OPERATIONAL CHECK IAW AMM 28-20-28. SEE ALSO AALA20150909014 FOR AFT UNIT.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 44,758 hrs · 21,471 cycles

AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB THE CTR FUEL PRESS LOW LIGHT ILLUMINATED. BOTH CTR FUEL PUMPS INOPERATIVE. R & R FWD CTR FUEL BOOST PUMP IAW AMM 28-20-07-201 & AMM 57-30-03-401. OPERATIONAL & LEAK CHECKS GOOD. SEE ALSO AALA20150903015.

Part: PUMP — FAULTY (FUEL SYSTEM) · airframe 44,758 hrs · 21,471 cycles

AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB THE CTR FUEL PRESS LOW LIGHT ILLUMINATED. BOTH CTR FUEL PUMPS INOPERATIVE. R & R AFT CTR FUEL BOOST PUMP IAW AMM 28-20-07-201 & AMM 57-30-03-401. OPERATIONAL & LEAK CHECKS GOOD. SEE ALSO AALA20150908019.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 44,683 hrs · 21,425 cycles

TAIL UPPER VERTICAL LE HAS 1 EACH 1/4" FASTENER HOLE CRACKED & DAMAGED ABOVE ZFS=52.267 SPLICE, LT SIDE, 14TH FASTENER HOLE. INSTALLED DOUBLER REPAIR IAW SRM 55-03-00 FIG 30.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

FUSELAGE SKIN CRACKED AT STATION 1380 BELOW L13L. INSTALLED DOUBLER REPAIR IAW SRM53-01-00-001 FIG 2 & AARD 51-00-00-014.

Part: SKIN — CRACKED (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

LEFT AFT NLG, AFT DOOR HINGE CUT OUT SKIN CRACKED AT L26L BETWEEN STATIONS 83 & 110. REPAIR INSTALLED IAW SRM 53-05-00.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,683 hrs · 21,425 cycles

AFT CARGO COMPARTMENT, LT TIE DOWN TRACK AT L27L IS CORRODED IN SEVERAL PLACES BETWEEN STATIONS 1212 & 1322. REMOVED OLD & INSTALLED NEW TRACK IAW SRM 51-30-01 & 51-30-05.

Part: CUSP WEB — CORRODED (BS 712-788) · airframe 44,683 hrs · 21,425 cycles

LEFT CUSP WEB CORRODED OUT OF LIMITS BETWEEN BS 712 & 788. R & R CUSP WEB BETWEEN BS 712 & 788 IAW 51-00-05-1 & DWG 9930538.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,683 hrs · 21,425 cycles

SEAT TRACK NR 6 CORRODED OUT OF LIMITS AT STATION 383. INSTALLED SEAT TRACK PLUG IAW AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

HEAVY CORROSION ON RT CUSP BETWEEN STATIONS 288 & 292. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,683 hrs · 21,425 cycles

SEAT TRACK CORRODED OUT OF LIMITS AT STATION 598. INSTALLED SEAT TRACK PLUG IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,683 hrs · 21,425 cycles

SEAT TRACK NR 6 CORRODED OUT OF LIMITS BETWEEN STATIONS 344 & 34. INSTALLED SEAT TRACK PLUG IAW AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

LEFT CUSP CORRODED BETWEEN STATIONS 1009 & 1011. R & R CUSP SHEET SECTION BETWEEN STATIONS 1003 & 1022 IAW SRM 51-01-00-001 & DWG 9930612.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

LEFT CUSP CORRODED BETWEEN STATIONS 842 & 845. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

LEFT CUSP IS CORRODED BETWEEN STATIONS 857 & 858. INSTALLED DOUBLER REPAIR IAW SRM 53-05-00-001 FIGURE 131A-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,683 hrs · 21,425 cycles

SEAT TRACK NR 6 CORRODED OUT OF LIMITS BETWEEN STATIONS 364 & 365. INSTALLED SEAT TRACK PLUG IAW AARD 53-20-00-10.

Part: DIAPHRAGM — CRACKED (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

CRACK IN SUBFLOOR DIAPHRAGM AT FS 170 LT, 30 INCHES INBD OF FWD ENTRY DOOR. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: STRUCTURE — WORN (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

APU ENCLOSURE HAS DEEP WEAR SPOT ON TOP, AFT OVER 2ND RIB INBD, INSIDE OF ENCLOSURE. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-11.

Part: FORMER — CRACKED (LT WING) · airframe 44,683 hrs · 21,425 cycles

LEFT WING LEADING EDGE NUMBER 4 SLAT TRACK INBOARD FORMER IS CRACKED. INSTALLED LEFT WING NUMBER 4 SLAT INBOARD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

LEFT CUSP CRACKED AT STATION 803. R & R CUSP SECTION BETWEEN STATIONS 788 & 807 IAW AARD 51-00-05-1, DWG 9910151 CONF 513 & DWG EDK 3238.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,683 hrs · 21,425 cycles

LEFT CUSP IS CORRODED AT STATION 638. ACCOMPLISHED DOUBLER REPAIR IAW ARRD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,683 hrs · 21,425 cycles

SEAT TRACK NR 4 CORRODED OUT OF LIMITS BETWEEN STATION 1240 & 1309. NEW SECTION OF SEAT TRACK WAS SPLICED & INSTALLED BETWEEN STATIONS 1240 & 1309 IAW SRM 53-05-00-001 FIG 4F.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 44,683 hrs · 21,425 cycles

STIFFENER CRACKED ON STATION 1338 AFT BULKHEAD, ABOVE AFT ENTRY & VAULT DOOR. REMOVED DAMAGED STIFFENER & INSTALLED NEW SERVICEABLE STIFFENER IAW AARD 51-00-05-1 & DWG 595760 EF 53614.

Part: OIL FILTER — CLOGGED (ZONE 400) · airframe 44,468 hrs · 21,291 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT THE RT ENG OIL STRAINER CLOG LIGHT ILLUMINATED. R & R RT MAIN ENG OIL FILTER IAW AMM 79-20-06 P 201 CON 2. PERFORMED LEAK & OPERATIONAL CHECKS. SYSTEM CHECKED NORMAL.

Part: PORTABLE LIGHT — WEAK (CABIN) · airframe 41,928 hrs · 19,870 cycles

PORTABLE EMER LIGHT B5-29 IS WEAK. R & R PORTABLE EMER LIGHT B5-29. OPERATIONS CHECKED NORMAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 41,928 hrs · 19,870 cycles

STOP CRACKED ON MID CARGO DOOR. R & R STOP IAW AARD 51-00-05-1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,848 hrs · 19,826 cycles

EMERGENCY LIGHTS BATTERY PACK B5-106 INOPERATIVE. R & R BATTERY PACK B5-106. OPERATIONS CHECKED NORMAL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,842 hrs · 18,756 cycles

NR 5 SEAT TRACK FROM STATIONS 200 TO 246 CORRODED. REPAIRED IAW SRM 53-05-00 FIGURE 4F.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FS SKIN WRINKLED FROM STATIONS 588 - 742.5 & LONGERON 18 - 26 RT. INSTALLED NEW INTERNAL DOUBLER IAW SRM 51-30-02 & EA MD80-51-029388.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FOUND INNER SKIN DOUBLER DAMAGED TOP AFT END TO CARGO DOOR CUT OUT & INNER DOUBLER HAS CRACK AT TOP INNER DOUBLER TOP ABOVE CENTER CARGO DOOR CUT OUT. REPLACED INTERNAL DOUBLER AROUND MID CARGO DOOR IAW AARD 51-00-00-1.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FS SKIN WRINKLED FROM STATIONS 693 - 703 AT UPPER AFT CORNER OF MID CARGO DOOR. REPLACED EXTERNAL DOUBLER ABOVE MID CARGO DOOR IAW AARD 51-00-00-1.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FS SKIN WRINKLED FROM STATIONS 588 - 742.5 & LONGERON 18 - 26 RIGHT. REPLACED FS IAW SRM 53-04-00 FIGURE 13C & EA MD80-53-029388.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FS SKIN WRINKLED FROM STATIONS 664 - 740.5 FROM LONGERONS 18 TO 26 LT. INSTALLED DOUBLER REPAIR IAW SRM 53-04 FIGURE 12C.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FS SKIN WRINKLED FROM STATIONS 664 - 760 FROM LONGERONS 26 LT & RT. INSTALLED NEW SKIN ECTION & SPLICE DOUBLERS IAW SRM 53-04-00 FIGURE 12C.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FS SKIN WRINKLED FROM STATIONS 588 TO 513 AND LONGERONS 18 - 26 RIGHT. INSTALLED NEW SKIN SECTION & SPLICED DOUBLERS IAW SRM 53-04-00 FIGURE 12C & EA MD80-51-029388.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

INNER SKIN DOUBLER FORWARD EDGE CRACKED AT FORWARD SIDE OF 3RD FROM FORWARD BELLY SKIN GOING AFT RADIO ALTIMMER ANTENNA CUTOUT. INSTALLED DOUBLER REPAIR IAW EA MD-80-53-030752.

Part: SKATE ANGLE — CRACKED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

TAIL VERTICAL STABILIZER SKATE ANGLE IS CRACKED ON LT SIDE OF FS 1463. INSTALLED SKATE ANGLE REPAIR DOUBLER IAW EA.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FUSELAGE SKIN WRINKLED FROM STATIONS 1088 - 1183 & LONGERONS 26 TO 18 RIGHT. REPAIRED IAW SRM 53-04 FIGURE 12C.(REPAIR REFERENCE 4A) & EA MD 80-51-029387. INSTALLED FASTENERS IN SKIN & DOUBLER IAW SRM 53-05-00 FIGURE 117 & AARD 51-00-00-1.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

OUTER SKIN WRINKLED FROM STATIONS 1202 - 1222 BETWEEN LONGERONS 22 & 23 LT. INSTALLED NEW SECTION OF SKIN IAW SRM 53-04-FIGURE 12 C.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,571 hrs · 18,598 cycles

CORROSION ON BOTTOM OF LT HAND CUSP FROM STATIONS 712 - 731. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FUSELAGE SKIN WRINKLED FROM STATIONS 512 TO 588 AND LONGERONS 18 TO 26 LT. INSTALLED NEW SERVICABLE SKIN FROM STATIONS 512 TO 588 IAW SRM 53-04-00, FIG 12C.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

FUSELAGE SKIN WRINKLED FROM STATIONS 1088 TO 1202 BETWEEN LONGERONS 21 AND 22 LEFT. INSTALLED NEW SKIN SECTION AND INTERNAL DOUBLERS FROM STATIONS 1088 TO 1202 IAW SRM 53-04-00, FIG 12C.

Part: SHEAR TIE — BENT (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

SHEAR TIE BENT AT STA 484 BETWEEN LONGERONS 28 AND 27 RT. INSTALLED SHEAR TIE IAW SRM 53-03-00 AND SRM 51-60-00.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

SHEAR TIE BENT AT STA 484 BETWEEN LONGERONS 29 AND 28 RT. INSTALLED SHEAR TIE IAW SRM 53-03-00 AND SRM 51-60-00.

Part: SHEAR TIE — BENT (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

SHEAR TIE BENT AT STA 503 BETWEEN LONGERONS 29 AND 28 RT. INSTALLED SHEAR-TIE IAW SRM 53-03-00 AND SRM 51-60-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,285 hrs · 18,441 cycles

FUSELAGE SKIN FROM STATIONS 1060 TO 1088 AND LONGERON 17 TO 18 LEFT DAMAGED. INSTALLED NEW SECTION OF SKIN AND REPAIR DOUBLERS BETWEEN LONGERON 15 AND 18 AND FROM STATIONS 1050 TO 1088 PER SRM 53-04-00 FIGURE 12C.

Part: TEE FITTING — BENT (FUSELAGE) · airframe 39,571 hrs · 18,598 cycles

RT HAND CUSP TEE, UPPER VERTICAL LEG & HORIZONTAL LEG BENT AT STATION 1190. INSTALLED REINFORCING DOUBLER REPAIR IAW EA MD80-53-030384.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 39,285 hrs · 18,441 cycles

RIGHT FUSELAGE SKIN WRINKLED AND BULGED BETWEEN STATIONS 1231 TO 1250 AND LONGERONS 25 AND 26. REPLACED SKIN SECTION PER SRM 53-04-00 FIGURE 12C.

Part: PSEU — INOPERATIVE (LANDING GEAR) · airframe 39,285 hrs · 18,441 cycles

DFW - CREW REPORTED GEAR UNSAFE ILLUMINATED DURING GEAR RETRACTION. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PROXIMITY SENSOR ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 35,195 hrs · 16,413 cycles

SHEAR CLIP CRACKED AT STATION 1437 LONGERONS 2 TO 3 RIGHT. INSTALLED NEW SHEAR TIE CLIP WITH HI-LOKS PER SRM 51-30-05.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,195 hrs · 16,413 cycles

MID CARGO CORROSION ON DOOR BEAM UPPER AND LOWER LEGS STATIONS 636 TO 693 LONGERON 28 RIGHT. INSTALLED BEAM DOUBLER PER AARD 53-10-00-3.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,195 hrs · 16,413 cycles

CORROSION ON WEBBING, STATION 1200 BETWEEN LONGERONS 28 TO 29 RIGHT. INSTALLED NEW SECTION OF WEB PER AARD53-10-00-24.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,195 hrs · 16,413 cycles

CORROSION ON VERTICAL AND HORIZONTAL LEGS LOWER CARGO DOOR JAMB, STATIONS 1212 TO 1174. INSTALLED FULL LENGTH BEAM DOUBLER FROM STATIONS 1155 TO 1212 PER AARD 53-10-00-3.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,195 hrs · 16,413 cycles

CRACK ON SEAT TRACK SUPPORT VERTICAL FITTING BELOW NUMBER 3 SEAT TRACK AT STATION 886. INSTALLED NEW FITTING, BELOW NUMBER 3 SEAT TRACK AT STATION 886 PER AARD 51-10-00-5 AND EA NUMBER MD-80-53-018451.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,195 hrs · 16,413 cycles

AFT CARGO HAS CORROSION ON FRAME 1322 NEAR LONGERON 30. CUT OUT CORRODED FRAME ABOVE LONGERON 28 RIGHT TO LONGERON 28 LEFT. SPLICED IN NEW SECTION OF FRAME PER SRM 53-03-00 FIGURE 2A.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,195 hrs · 16,413 cycles

MID - CX CORROSION ON RIGHT TIEDOWN TRACK SUPPORT INTERCOSTAL STATIONS 769 TO 786 BETWEEN LONGERONS 27 TO 28 LEFT. INSTALLED SERVICEABLE NEW INTERCOSTAL PER AARD 51-10-00-5.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,195 hrs · 16,413 cycles

STATION 1112 THRESHOLD CORNER SUPPORT ANGLE CORRODED. INSTALLED SERVICABLE NEW SUPPORT ANGLE PER AARD 51-10-00-5.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,195 hrs · 16,413 cycles

SHEAR CLIP CRACKED AT STATION 1437, LONGERONS 2 TO 3 RIGHT. INSTALLED NEW SHEAR TIE CLIP WITH HI-LOKS PER SRM 51-30-05.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,195 hrs · 16,413 cycles

STATION 1155 THRESHOLD CORNER SUPPORT ANGLE CORRODED. INSTALLED SERVICEABLE NEW SUPPORT ANGLE PER AARD 51-10-00-5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,195 hrs · 16,413 cycles

CORROSION ON TIEDOWN TRACK SUPPORT INTERCOSTAL STATION 769 TO 786 BETWEEN LONGERONS 27 AND LONGERON 28 RIGHT. INSTALLED INTERCOSTAL PER SRM 51-10-3, 53-01-00 AND AARD 51-10-00-5.

Part: FITTING — CRACKED (SPOILER ACTUATOR) · airframe 35,195 hrs · 16,413 cycles

CRACK IN OUTBOARD, FORWARD RADIUS OF LEFT GROUND SPOILER CASTING. REMOVED AND REPLACED GROUND SPOILER ACTUATOR FITTING PER SRM 51-30-05.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 35,195 hrs · 16,413 cycles

WEB CRACKED AT AFT OF FORWARD ENTRY DOOR JAMB STATION 209 LONGERON 15 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: SKIN — GOUGED (FUSELAGE) · airframe 35,195 hrs · 16,413 cycles

DENT WITH DEEP GOUGES AT STATION 200, BETWEEN LONGERONS 4 AND 5 LEFT FUSELAGE SKIN. REPAIRED BY INSTALLING INTERNAL DOUBLER PER DWG SG09530001.

Part: RIB — CRACKED (LE SLAT) · airframe 35,195 hrs · 16,413 cycles

RIGHT OUTBOARD SLAT OUTBOARD RIB IS CRACKED. REPLACED DAMAGED OUTBOARD RIB WITH NEW RIB PER ESO 80117 CHAPTER 27-80-1.

Part: PAN — CRACKED (WINDOW) · airframe 35,195 hrs · 16,413 cycles

RIGHT STATION 788 UPPER FORWARD WINDOW PAN EAR IS CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 35,195 hrs · 16,413 cycles

RIGHT STATION 769 LOWER FORWARD WINDOW PAN EAR IS CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 35,195 hrs · 16,413 cycles

LEFT STATION 1060 UPPER AFT WINDOW PAN EAR IS CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: FRAME — BROKEN (FUSELAGE) · airframe 35,188 hrs · 16,409 cycles

AIRCRAFT STRUCK BY LAVATORY SERVICE CART. FRAME AND FORMERS WERE DAMAGED UNDER SKIN. REPAIRED FRAME AND FORMERS PER SRM AND EA MD-80-53-018225.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 35,188 hrs · 16,409 cycles

AIRCRAFT WAS STRUCK BY LAVATORY CART. FUSELAGE WAS DAMAGED BETWEEN STATIONS 120 AND 134. ACCOMPLISHED REPAIR PER SRM AND EA MD80-53-018224.

Part: COMPUTER — FAULTED (NR 2) · airframe 32,912 hrs · 15,292 cycles

EWR - CAPTAIN REPORTED SLAT DISAGREE LIGHT REMAINING ILLUMINATED AFTER SLAT RETRACTION. EMERGENCY DECLARED RETURNED EWR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DIRECT FLIGHT GUIDANCE COMPUTER NUMBER 2 THAT WAS AT FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: IRU — FAILED (COCKPIT) · airframe 29,874 hrs · 13,955 cycles

DFW - INERTIAL REFERENCE UNIT FAILED IN FLIGHT. RETURNED DFW WITHOUT INCIDENT. REPLACED INERTIAL REFERENCE UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — FAILED (RT ENGINE) · airframe 29,850 hrs · 13,941 cycles

DFW - ON DESCENT PASSING ABOUT FL310 RUDDER CONTROL MANUAL LIGHT ILLUMINATED FOLLOWED BY RIGHT HYDRAULIC PRESS LOW LIGHT. RIGHT HYDRAULIC PRESSURE INDICATED 500 PSI, FOLLOWED CHECKLIST RIGHT PRESS REMAINED AT 500 PSI, LEFT PRESS WAS NORMAL. AT APPROX 10,000 FT RIGHT PRESS RETURNED TO NORMAL. REPLACING RIGHT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 27,700 hrs

LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CABLE — DISCONNECTED (SEAT 5EF)

MEM INFLIGHT T482/18OCT DFW TO IND, SMOKE REPORTED COMING FROM AREA BELOW SEATS 5EF AN 6EF. LANDED MEM WITHOUT INCIDENT. SMOKE DISSIPATED PRIOR TO ARRIVAL AT GATE. FOUND TWO WIRES TO SEAT 5EF POWERPORT DISCONNECTED BUT NO ARCING WAS EVIDENT. INSPECTED CARGO AREA WITH NO DAMAGED NOTED. REATTACHED POWERPORT CABLE AT SEAT 5EF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (RIGHT)

SAN INFLIGHT - RIGHT HYDRAULIC PRESSURE WENT TO ZERO. USED ALTERNATE GEAR EXTENSION LEVER. LANDED SAN WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC DRIVEN PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

ORD - EMERGENCY LIGHTS IN AISLE SEAT ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AISLE SEAT ROWS 22 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

ALL SEAT MOUNTED AND FIRST CLASS GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT CONTROL MODULE AB5 1 AND AB5 3 FOR SEAT MOUNTED EMERGENCY LIGHTS. INSERTED LOOSE WIRES AT SEAT 17D AND CHARGED BATTERY FOR FIRST CLASS GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

MIA EMERGENCY LIGHT AT SEAT 8D INOPERATIVE. FOUND LOOSE WIRING. SECURED WIRING FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY B5-27 AND B5-28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE FOUND ALL SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED 4 STRIP LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND AFT RIGHT AND LEFT SIDE OVERWING DOOR EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD RIGHT AND LEFT OVERWING DOOR EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CHARGER — INOPERATIVE (COCKPIT)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY B5-23. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MCI - FOUND CORROSION ON CARGO FLOOR SUPPORT AT STATION 1212, 6 INCHES RBL TO 10 INCHES LBL TOP SIDE AND BOTTOM SIDE. REPLACED WITH NEW MPN 5936597-509, RIVETS WERE INSTALLED PER SRM 51-30-02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MCI - FOUND CORROSION ON CARGO FLOOR SUPPORT STATION 1155 TO 1212, 7 INCHES RBL TOP SIDE AND BOTTOM SIDE. REPLACED WITH NEW MPN 5936660-171, RIVETS WERE INSTALLED PER SRM 51-30-02. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

MCI - FOUND CORROSION ON CARGO FLOOR SUPPORT AT STATION 1155 10 INCHES RBL TOPSIDE AND LOWER SIDE. CORRODED FLOOR SUPPORT WAS REPLACED WITH NEW MPH 5936660-63, PART WAS PRIMED, PAINTED WHITE AND HI-LOCKS WERE INSTALLED PER SRM 51-31-05. (M)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,906 hrs · 5,789 cycles

THE EGRESS LIGHT WAS INOPERATIVE AT ROW 22. RESEATED THE LAMP. CHECK-C 5-25-2002.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 10,571 hrs · 5,598 cycles

THE EMERGENCY CEILING LIGHTS WERE INOPERATIVE AT ROWS 28 AND 29, AND THE EGRESS FLOOR LIGHT WAS INOPERATIVE AT ROW 21. REPLACED THE BATTERIES IN B5-107 BATTERY PACK, PN 408822-101, FOR THE CEILING LIGHTS, AND RESEATED THE LAMP INTO THE SOCKET FOR THE EGRESS LIGHT. CHECK-C 5-25-02 STL.

Part: LAMP · airframe 10,392 hrs · 5,502 cycles

THE CABIN EGRESS LIGHTING WAS INOPERATIVE FROM ROW 26 TO 31. REPLACED LAMP AND SECURED LIGHTS. CHECK-C 5-25-02 STL. --CLOSED--

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 5,686 hrs · 2,872 cycles

THE EMERGENCY EXIT LIGHTS OVER THE LT AND RT FWD OVERWING EXIT DOORS WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 5-6-00 STL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 5,343 hrs · 2,715 cycles

THE LIGHTS OVER LT FWD AND RT FWD OVERWING EMERGENCY EXITS WERE INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 5-6-00 STL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 5,062 hrs · 2,587 cycles

THE FWD LT AND RT OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 5-6-00 STL.

Part: SOCKET — WORN (ROW 31) · airframe 4,419 hrs · 2,275 cycles

THE EGRESS LIGHTING AT ROW 30 AND 31 WERE INOPERATIVE. REPLACED THE LIGHT SOCKET AT ROW 31. CHECK-C 5-6-00 STL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,812 hrs · 1,985 cycles

THE HAND HELD PORTABLE EMERGENCY LIGHT AT THE LEFT SIDE MOST FORWARD CABIN DOOR WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. CHECK-C 5-6-00 STL.

Part: AIR DIST — SMOKING (CABIN)

IN CRUISE CABIN GRADUALLY FILLED WITH BLUE SMOKE AND OIL SMELL. CABIN TEMP WAS TURNED DOWN AND ANTI ICE TURNED OFF. RT PACK PRESSURE WAS 10 PSI WHEN SMOKE APPEARED BUT RETURNED TO NORMAL WHEN ENG ANTI ICE TURNED OFF. BLUE SMOKE AND OIL SMELL GRADUALLY DISIPATED. INSPECTED RT ENG 13TH AND 8TH STAGE END CAPS FOR SIGNS OF OIL CONTAMINATION. NO OIL NOTICED. INSPECTED INLET FOR SIGN OF OIL LEAKAGE BUT NO LEAKS NOTED. ENG OIL QTY FULL. PERFORMED OP CHECK OF RH PACK IN AUTO AND MANUAL FULL HOT AND COLD AND NO DEFECTS NOTED.