N968TW

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 53,716 hrs · 27,508 cycles

AIRCRAFT WAS GROUNDED. ON THE CAPTAINS WINDSHIELD THERE IS SMOOTH CLEAR EDGE DECLAMATION WHICH EXTENDS BEYOND THE 2.0 IN LIMIT IN THE LOWER FORWARD CORNER RADIUS INTO THE CRITICAL VISION AREA REF MM 56-00-00. REPLACED CAPTAINS WINDSHIELD.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 53,716 hrs · 27,508 cycles

AIRCRAFT WAS GROUNDED. THE FIRST OFFICERS WINDSHIELD THERE IS CLEAR SMOOTH EDGE DELAMINATION WHICH EXTENDS BEYOND THE 2.0 IN LIMIT IN THE LOWER FORWARD CORNER RADIUS INTO THE CRITICAL VISION AREA. REPLACED FIRST OFFICERS WINDSHIELD.

Part: BEAM — CORRODED (BS 636-693) · corrosion level 2 · airframe 53,194 hrs · 27,148 cycles

CORROSION FOUND ON THE LOWER DOOR FRAME BEAM VERTICAL LEG BETWEEN BS 636 TO 693. INSTALLED A REPAIR DOUBLER IAW 53-10-00-3.

Part: LONGERON — CRACKED (BS 990-1003) · airframe 53,194 hrs · 27,148 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED LONGERON 20R AT STA 993 FROM EDGE TO FIRST FASTENER HOLE. REPAIRED THE LONGERON IAW SRM 53-02-00 FIGURE 22.

Part: DOOR FRAME — CORRODED (BS 1274) · corrosion level 2 · airframe 53,194 hrs · 27,148 cycles

CORROSION UNDER DOOR STOP AT DOOR CUTOUT LOWER FRAME AT BS 1274, AFT CARGO DOOR AREA. REPLACED DOOR FRAME IAW 53-10-00-3 - FIGURE 3, SHEET 1.

Part: STIFFENER — CRACKED (BS 1338) · airframe 53,194 hrs · 27,148 cycles

BS 1338 BULKHEAD VERTICAL STIFFENER AT STRINGER 1L CRACKED IN THE RADIUS. REPLACED REPAIR DOUBLER IAW SRM 53-01-00-001 - FIGURE 2, SHEET 4 AND 53-10-00-15.

Part: WEB — CRACKED (BS 180) · airframe 53,194 hrs · 27,148 cycles

CRACKED FLOOR MEMBRANE AT BS 180 APPROXIMATELY LBL 32. REPAIRED FLOOR MEMBRANE IAW 53-20-00-16.

Part: PAN — CRACKED (BS 1022) · airframe 53,194 hrs · 27,148 cycles

LEFT SIDE WINDOW RING PAN CRACKED AT BS 1022 AT UPPER AFT CORNER. INSTALLED WINDOW RING PAN REPAIR DOUBLER IAW 53-10-00-25.

Part: PAN — CRACKED (BS 1079) · airframe 53,194 hrs · 27,148 cycles

RIGHT SIDE WINDOW RING PAN CRACKED AT BS 1079 AT UPPER AFT CORNER. INSTALLED WINDOW RING PAN REPAIR DOUBLER IAW 53-10-00-25.

Part: PAN — CRACKED (ZONE 200) · airframe 53,194 hrs · 27,148 cycles

LEFT SIDE WINDOW RING PAN CRACKED AT BS 1098 AT UPPER AFT CORNER. INSTALLED WINDOW RING PAN REPAIR DOUBLER IAW 53-10-00-25.

Part: PAN — CRACKED (BS 1079) · airframe 53,194 hrs · 27,148 cycles

RIGHT SIDE WINDOW RING PAN CRACKED AT BS 1079 AT LOWER FORWARD CORNER. INSTALLED REPAIR ANGLE IAW 53-10-00-25.

Part: PAN — CRACKED (BS 1041) · airframe 53,194 hrs · 27,148 cycles

WINDOW RING PAN CRACKED AT UPPER AFT CORNER AT BS 1041. INSTALLED A RING PAN DOUBLER IAW 53-10-00-25.

Part: PAN — CRACKED (BS 1060) · airframe 53,194 hrs · 27,148 cycles

WINDOW RING PAN CRACKED IN RADIUS OF PREVIOUSLY REPAIRED ANGLE DOUBLER AT UPPER AFT CORNER AT BS 1060. INSTALLED A RING PAN REPAIR DOUBLER IAW 53-10-00-25.

Part: SKIN — CRACKED (BS 90-100) · airframe 53,194 hrs · 27,148 cycles

CRACK FOUND ON THE SKIN BETWEEN BS 90 - 100. REPAIRED THE SKIN IAW SRM 53-05-00, FIG 158.

Part: FLOOR SUPPORT — CRACKED (BS 769-788) · airframe 53,194 hrs · 27,148 cycles

FLOOR SUPPORT CRACKED AT SEVERAL PLACES, BS 769 - 788. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1, AND DRAWING 9936580.

Part: PAN — CRACKED (BS 946-948) · airframe 53,194 hrs · 27,148 cycles

RIGHT SIDE WINDOW RING PAN CRACKED AT UPPER FORWARD CORNER BETWEEN BS 946 TO 948, STRINGER 14R TO STRINGER 15R. REPLACED THE RING PAN IAW 53-10-00-25.

Part: SHEAR TIE — CRACKED (BS 1463) · airframe 53,194 hrs · 27,148 cycles

SHEAR TIE AT BS 1463, INBOARD OF LONGERON 3R HAD A CRACK INDICATION. REPLACED THE SHEAR TIE IAW 51-00-05-1.

Part: FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 53,194 hrs · 27,148 cycles

LEFT WING OUTBOARD FLAP, THE CENTER HINGE WAS MISSING SEALANT AND CORRODED BETWEEN LOWER STUDS AND FORWARD HINGE FITTING. REPLACED STUDS AND FITTING PER AMM 57-40-01-201.

Part: PIN — PULLED (DOOR SLIDE) · airframe 53,194 hrs · 27,148 cycles

PINS PULLED ON FORWARD SERVICE DOOR SLIDE. FOUND WHEN REMOVED FOR INSPECTION.

Part: SENSOR — FAULTY (MLG) · airframe 53,128 hrs · 27,103 cycles

GEAR INDICATION MESSAGE, EMERGENCY DECLARED. AIRCRAFT LANDED IN DFW WITHOUT FURTHER INCIDENT, NOT OVERWEIGHT. NOSE GEAR UNSAFE AT HANDLE IN THE UP POSITION, NORMAL DOWN AND LOCK INDICATION. AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED NOSE GEAR UP & DOWN LOCKED SENSOR AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 32-60-05.

Part: NUT — LOOSE (SLIDING WINDOW) · airframe 52,691 hrs · 26,817 cycles

AIRCRAFT WAS NOT GROUNDED. CAPTAIN SLIDER WINDOW UPPER RIGHT CORNER BALL DOES NOT GO INTO TRACK. REPLACED AND TORQUED UPPER FORWARD SLIDER MOUNT NUT THAT WAS LOOSE REF MM 20-30-01. WINDOW OPERATIONS CHECK NORMAL REF MM 56-10-03.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 52,539 hrs · 26,716 cycles

CENTER WINDSHIELD HAS DELAMINATION EMINATING FROM THE RIGHT SIDE ASSOCIATED WITH HEATING ELEMENT. DELAMINATION APPEARED TO INCREASE IN SIZE DURING FLIGHT. REPLACED THE WINDSHIELD IAW AMM 56-10-01-201-2. AIRCRAFT WAS GROUNDED.

Part: ADC — FAULTY (ZONE 100) · airframe 52,460 hrs · 26,661 cycles

AIRCRAFT WAS GROUNDED: AT CRUISE ALTITUDE 33, WITH ALL ENGINE AND WING HEAT ON THE MACH TRIM, INOPERABLE LIGHT ILLUMINATED, AIRSPEED/MACH INDICATION. EMERGENCY WAS DECLARED INBOUND TO BNA, REMAINDER OF THE FLIGHT CONTINUED WITHOUT AUTOPILOT AND AUTOTHROTTLES USING STANDBY MACH/AIRSPEED INDICATORS. MAINTENANCE REPLACED NR 1 CENTRAL AIR DATA COMPUTER PER MM 34-16-01 AND PERFORMED SATISFACTORY OPERATIONAL CHECKS.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 52,270 hrs · 26,527 cycles

SEAT 27DEF EMERGENCY LIGHT LENS BROKEN. REPLACED THE LENS IAW AMM 25-27-03.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 52,270 hrs · 26,527 cycles

SEAT 26DEF EMERGENCY LIGHT LENS BROKEN. REPLACED THE LENS IAW AMM 25-27-03.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 52,270 hrs · 26,527 cycles

SEAT 23DEF EMERGENCY LIGHT LENS BROKEN. REPLACED LENS IAW AMM 25-27-03.

Part: SLIDE — CONTAMINATED (TAILCONE) · airframe 52,081 hrs · 26,410 cycles

TAILCONE EVACUATION SLIDE CONTAMINATED WITH SKYDROL. AIRCRAFT WAS GROUNDED. REPLACED TAIL CONE SLIDE PER WORK CARD 25-94-15.

Part: LANYARD — CONTAMINATED (TAILCONE SLIDE) · airframe 52,081 hrs · 26,410 cycles

AFT ASSY TAIL CONE SLIDE LANYARD CONTAMINATED WITH HYDRAULIC FLUID. AIRCRAFT WAS GROUNDED. REPLACED SLIDE LANYARD IAW WORK CARD 25-94-15.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 51,028 hrs · 25,700 cycles

AIRCRAFT WAS GROUNDED. CABIN CENTER FLOOR PANEL AT ROW 23 IS SOFT. ACCOMPLISHED TIME LIMITED REPAIR TO FLOOR PANEL PER EA 272392.

Part: PUMP — FAULTED (FUEL BOOST) · airframe 50,876 hrs · 25,594 cycles

DURING CLIMB THE CENTER FUEL BOOST PUMP CIRCUIT BREAKER J-21 TRIPPED. EMERGENCY DECLARED. FLIGHT DIVERTED, LANDING UNEVENTFUL. REMOVED AND REPLACED CENTER AFT FUEL BOOST PUMP IAW AMM 28-20-07. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SLIDE — PARTIAL DEPLOY (R1 DOOR) · airframe 50,519 hrs · 25,375 cycles

FOUND THE R1 SLIDE PARTIALLY DEPLOYED. REPLACED THE SLIDE IAW AMM 25-62-00.

Part: SCREW — MISSING (FLASHLIGHT) · airframe 50,309 hrs · 25,224 cycles

FLASHLIGHT ASSY IS DAMAGED. REPLACED FLASHLIGHT ASSY WITH TWO SCREWS. OPS CHECK NORMAL. OKAY FOR SERVICE. THE AIRCRAFT WAS NOT GROUNDED.

Part: LANYARD — DETACHED (R1 DOOR) · airframe 50,276 hrs · 25,203 cycles

THE 1R DOOR SLIDE LANYARD IS DETACHED FROM GIRT BAR. RE INSTALLED GIRT BAR RELEASE LANYARD IAW AMM 25-62-00. THE AIRCRAFT WAS NOT GROUNDED.

Part: PORTABLE LIGHT — DIM (CABIN) · airframe 49,841 hrs · 24,934 cycles

AIRCRAFT IN BASE MAINTENANCE. PORTABLE EMERGENCY LIGHT VERY DIM. REPLACED LIGHT AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 49,841 hrs · 24,934 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT HAND FORWARD DOUBLER BETWEEN STRINGER 1R AND 2R. INSTALLED SKIN DOUBLER PER SRM 53-05-00-001 AND EA 267054.

Part: HINGE FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 49,841 hrs · 24,934 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND WING OUTBOARD FLAP CENTER HINGE FITTING. REPLACED HINGE FITTING PER CMM 27-50-02.

Part: CASTING — CRACKED (RT SPOILER) · airframe 49,841 hrs · 24,934 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT HAND WING GROUND SPOILER CASTING. REPLACED CASTING PER SRM 57-01-00 AND SB MD80-57-180.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,841 hrs · 24,934 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LOWER FORWARD DOOR STOP FITTING ON FORWARD CARGO DOOR. REPLACED FITTING PER AARD 51-00-05-1 AND IPC 52-30-01-02B DRAWING 5910141.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,841 hrs · 24,934 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON UPPER FORWARD DOOR STOP FITTING ON FORWARD CARGO DOOR. REPLACED FITTING PER IPC 52-30-01-02B DRAWING 5910141, DRAWING CDK2345 AND AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,841 hrs · 24,934 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON CENTER FORWARD DOOR STOP FITTING ON FORWARD CARGO DOOR. REPLACED FITTING PER IPC 52-30-01-02B DRAWING 5910141, DRAWING CDK2345 AND AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 49,841 hrs · 24,934 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON UPPER AFT DOOR STOP FITTING ON MID CARGO DOOR. REPLACED FITTING PER IPC 52-30-01-02B DRAWING 5910141, DRAWING CDK2345 AND AARD 51-00-05-1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,841 hrs · 24,934 cycles

AIRCRAFT IN BASE MAINTENANCE. EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — MALFUNCTIONED (AUTOTHROTTLE SYS) · airframe 49,694 hrs · 24,822 cycles

AIRCRAFT NOT GROUNDED. DFW-TUL FLIGHT. ABORTED TAKEOFF AT 60 KNOTS ACCOUNT AUTOTHROTTLES WOULD NOT ENGAGE. PERFORMED RETURN TO SERVICE IAW AMM 22-01-05. NO FAULTS NOTED. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 49,098 hrs · 24,459 cycles

THE EMERGENCY PATH LIGHT OPERATED BY BATTERY PACK AB5-4 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 49,098 hrs · 24,459 cycles

THE EMERGENCY LIGHT OPERATED BY BATTERY PACK AB5-3 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 49,098 hrs · 24,459 cycles

THE EMERGENCY PATH LIGHT OPERATED BY BATTERY PACK AB5-2 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: STRUT — LOW (LT MLG) · airframe 47,885 hrs · 23,698 cycles

AIRCRAFT WAS GNDED. FLIGHT CREW REPORTS THAT LT WING RAISES UP AT TOUCH DOWN WITH NO CONTROL INPUT. MX CONFIRMS NO FLIGHT ABNORMALITIES. SUSPECT STRUTS NEED SERVICING. ACCOMPLISHED STRUT SERVICING IAW AMM 32-11-02.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 46,180 hrs · 22,664 cycles

E & E COMPARTMENT, CABIN FLOOR MEMBRANE, SUB-FLOOR CRACKED, STATION 180 AT APPROX LBL 32. INSTALLED REPAIR DOUBLER IAW 53-20-00-16.

Part: PAN — CORRODED (FUSELAGE) · airframe 46,180 hrs · 22,664 cycles

FORWARD CARGO THRESHOLD PAN IS CORRODED BETWEEN STATIONS 375 & 425. REMOVED CORROSION & INSTALLED FILLER & STRAP DOUBLER IAW EA 253813.

Part: BEAM — CRACKED (PAX DOORWAY) · corrosion level 2 · airframe 46,180 hrs · 22,664 cycles

FORWARD ENTRY DOOR BEAM NR 6 CRACKED, CTR LOWER AREA BELOW BRACKET AT ATTACHMENT BOLT. INSTALLED REPAIR ANGLE DOUBLER IAW 52-10-00-3.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 45,818 hrs · 22,449 cycles

FORWARD ENTRY EMER LIGHT ILLUMINATED WITH BATTERY SHUTOFF. R & R BATTERY PACK AT LOCATION B5-23.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,568 hrs · 22,316 cycles

EMERGENCY CEILING LIGHTS FROM ROW 4 - 6 INOPERATIVE. R & R BATTERY PACK B5-100. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 45,568 hrs · 22,316 cycles

FORWARD PORTABLE EMER LIGHT NEON LAMP INOPERATIVE. R & R FWD PORTABLE EMER LIGHT ASSEMBLY. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 42,747 hrs · 20,775 cycles

SYR INFLIGHT DFW EWR. CAPTAIN`S PRIMARY FLIGHT DISPLAY & FLIGHT MODE ANNUNCIATOR BLANKED OUT ON APPROACH. EMERGENCY DECLARED FLIGHT DIVERTED SYR LANDED WITHOUT INCIDENT. REPLACED NR 1 DIGITAL FLIGHT GUIDANCE COMPUTER & SYMBOL GENERATOR. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

CORROSION FOUND AT STATION 1111 & LONGERONS 27 & 28 RT. CUT OUT CORROSION & INSTALLED DOUBLER, TRIPLER & FILLER IAW SRM 53-04-00 PARAGRAPH 57.

Part: SKIN — DENTED (CARGO DOOR) · airframe 42,646 hrs · 20,733 cycles

MID CARGO DOOR SKIN DENTED BETWEEN NR 1 & 2 FRAME ON AFT EDGE. INSTALLED DOUBLER IAW EA MD80-52-034408.

Part: FITTING — LEAKING (ZONE 500) · airframe 42,646 hrs · 20,733 cycles

CENTER WING FUEL LEAK AT BATHTUB FITTING LOWER LT SIDE OF CTR FUEL TANK JUST ABOVE KEEL BEAM. INSTALLED NEW BATHTUB FITTING IAW AARD 51-00-05-1 & DWG 5930569.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

SEAT TRACK NR 6 CORRODED AT SIDEWALL SUPPORT ATTACHING HOLE FROM STATIONS 1162 & 1172. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-13.

Part: SKIN — DAMAGED (SERVICE DOOR) · airframe 42,646 hrs · 20,733 cycles

FORWARD SERVICE DOOR HAS SEVERAL LIGHTNING STRIKES ALONG LOWER EDGE OF OUTER SKIN. ACCOMPLISHED SPLICE REPAIR OF FWD SERVICE DOOR IAW SRM 52-05-00-001FIGURE 64.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,646 hrs · 20,733 cycles

RIGHT CUSP CRACKED AT STATION 1162 INBD EDGE UNDER SEAT TRACK NR 5. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

CORROSION ON RT CUSP FROM STATIONS 1174 TO 1250. REPLACED CUSP SHEET IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,646 hrs · 20,733 cycles

CORROSION AT CLIP NUTS, REPLACED TRACK.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

LEFT CUSP CORRODED FROM STATIONS 547 TO 552. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

G 2 GALLEY OTBD MOUNT IN END OF SEAT TRACK NR 6 CORRODED. INSTALLED NEW SERVICEABLE G 2 GALLEY OTBD TIE DOWN MOUNT FITTING AT FWD END OF NR 6 SEAT TRACK IAW AARD 51-00-05-1, DWG 5930547 & IPC 53-40-00-06 Q ITEM 382 CONF 525.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,646 hrs · 20,733 cycles

SUPPORT CRACKED BELOW NR 4 SEAT TRACK AT STATION 845, JUST ABOVE FUEL TANK. INSTALLED NEW SUPPORT BRACKET IAW AARD 51-00-05-1 & DWG 3925816-502 & 9936634.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

LEFT CUSP CORRODED FROM STATIONS 567 TO 571. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

FORWARD CABIN CORROSION IN THE OTBD G1 GALLEY MOUNT BORE AT STATION 160 AT THE INBD SIDE OF THE GALLEY DRAIN PAN. INSTALLED NEW SERVICEABLE G1 GALLEY MOUNT IAW AARD 51-00-05-01 & DWG 9936534.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

CORROSION UNDER SEAT TRACK NR 6 AT STATION 218 ON RT CUSP. INSTALLED NEW CUSP SHEET IAW AARD 51-00-05-1.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

CORROSION ON THE OTBD G1 GALLEY MOUNT SURFACE & IN THE BORE AT STATION 160 AT THE OTBD SIDE OF THE GALLEY DRAIN PAN. INSTALLED NEW SERVICEABLE G1 GALLEY MOUNT IAW AARD 51-00-05-01 & DWG 9936534.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

SEAT TRACK NR 2 CORRODED FROM STATIONS 1088 TO 1145. INSTALL SEAT TRACK SPLICE IAW SRMS 53-05-00, 51-30-05 & AMM 53-40-01-2.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 42,646 hrs · 20,733 cycles

BELL FRAME CORRODED, INSTALLED DOUBLER.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

CORROSION TO SUBFLOOR FROM STATIONS 148 TO 160. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

CORROSION ON THE BOTTOM OF THE RT CUSP AT STATION 565. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

CORROSION ON AFT CARGO LT TIE DOWN TRACK. INSTALLED NEW TRACK IAW AARD 51-00-05-1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 42,646 hrs · 20,733 cycles

SEAT TRACK NR 4 FROM STATIONS 798 TO 1011 DAMAGED. INSTALLED NEW NR 4 SEAT TRACK IAW AMM 53-40-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

LEFT CUSP FROM STATIONS 611 TO 615 CORRODED. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,646 hrs · 20,733 cycles

RIGHT CUSP CRACKED AT STATION 886. INSTALLED DOUBLER AT STATION 886 RT SIDE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

SEAT TRACK NR 6 PLUG IS CORRODED AT STATION 408. INSTALLED NEW SEAT TRACK PLUG IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

SEAT TRACK NR 6 CORRODED FROM STATIONS 367 TO 370. INSTALLED NEW PLUG AT SEAT TRACK NR 6 IAW AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

RIGHT CUSP FROM STATIONS 643 TO 646 CORRODED. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

LEFT CUSP FROM STATIONS 719 TO 724 CORRODED. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

SEAT TRACK NR 6 FROM STATIONS 263 TO 265 CORRODED. REMOVED CORROSION & INSTALLED PLUG DDK2704 & CHANNEL 752952 FOR PLUG REPAIR IAW SRM 53-05-00 FIGURE 4A.

Part: ANGLE — CRACKED (BS 236) · airframe 42,646 hrs · 20,733 cycles

ANGLE AT BS 236 OTBD OF LONGERON 28 RT CRACKED. INSTALLED NEW ANGLE IAW AARD 51-0-05-1.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 42,646 hrs · 20,733 cycles

SUPPORT BELOW NR 3 SEAT TRACK AT BS 926, JUST ABOVE FUEL TANK CRACKED. INSTALLED NEW SUPPORT IAW SRM 53-14-03 FIGURE 10, PRINT 5930561-505 & DWG 9936634-1.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,646 hrs · 20,733 cycles

CORROSION ON SUBFLOOR UNDER NR 6 SEAT TRACK AT STATION 214 RT SIDE. CUT OUT CORROSION & INSTALLED DOUBLER FROM STATION 200 TO 218 & RBL 49 TO 57 IAW AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,228 hrs · 18,924 cycles

CRACK IN RIGHT AFT FUSELAGE SKIN CANT FRAME AT STATION 1474. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,228 hrs · 18,924 cycles

CRACK IN LEFT AFT FUSELAGE SKIN CANT FRAME AT STATION 1474. INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: CONNECTOR — MISSING (CABIN) · airframe 38,732 hrs · 18,667 cycles

LOOSE WIRE UNDERNEATH THE FRONT OF SEAT 7F AT SIDEWALL. INSTALLED NEW CONNECTOR ON EMERGENCY LIGHTING WIRES AT SEAT 7F. OPS CHECK NORMAL.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 38,722 hrs · 18,661 cycles

OKC - INFLIGHT MSP-DFW. CREW REPORTED FUEL LEVEL LOW LIGHT ILLUMINATED. FLIGHT DIVERTED OKC LANDED WITHOUT INCIDENT. PLACARD FUEL LEVEL LOW LIGHT SYSTEM INOPERATIVE PER MEL. FLIGHT CONTINUED TO DESTINATION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,235 hrs · 18,405 cycles

CEILING EMERGENCY LIGHTS FOR ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FOR ROWS 3 TO 6. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 38,235 hrs · 18,405 cycles

ESCAPE PATH LIGHT AT SEAT 26D INOPERATIVE. RE-SEATED CONNECTOR AT SIDEWALL FOR ESCAPE PATH LIGHT ST SEAT 26D. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,235 hrs · 18,405 cycles

CEILING EMERGENCY LIGHTS FOR ROWS 21 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FOR ROWS 21 TO 27. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,235 hrs · 18,405 cycles

CEILING EMERGENCY LIGHTS FOR ROWS 13 TO 18 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FOR ROWS 13 TO 18. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 38,235 hrs · 18,405 cycles

CEILING EMERGENCY LIGHTS FOR ROWS 7 TO 11 INOPERATIVE. RESEATED EMERGENCY BATTERY CELLS IN CHARGER. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,235 hrs · 18,405 cycles

LEFT AND RIGHT FORWARD OVERWING UPPER EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT FORWARD OVERWING UPPER EXIT SIGNS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,235 hrs · 18,405 cycles

LEFT AND RIGHT HAND AFT OVERWING UPPER EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AND RIGHT AFT OVERWING FOOR UPPER EXIT SIGNS. OPS CHECK NORMAL.

Part: SKIN — DAMAGED (AILERONS) · airframe 37,196 hrs · 17,862 cycles

AILERON HAS DAMAGED & DISBONDED UPPER SKIN. REMOVED DAMAGED & DELAMINATED SKIN AT 11 EACH AREAS, POTTED EXPOSED CORE AND APPLIED WET LAY-UP PERMANENT REPAIRS PER SRM 51-70-01A PARAGRAPH 14.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,512 hrs · 17,499 cycles

RIGHT AND LEFT AFT OVERWING DOOR UPPER EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK BY OVERHEAD BIN 19DEF. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,512 hrs · 17,499 cycles

CEILING EMERGENCY LIGHT BY FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK BY CEILING PANEL NEAR FORWARD LAVATORY. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,512 hrs · 17,499 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK IN OVERHEAD BIN 28 DEF. OPS CHECK NORMAL.

Part: ANGLE — CORRODED (RT WING) · corrosion level 2 · airframe 30,826 hrs · 14,698 cycles

FOUND CORROSION ON ANGLE IN RIGHT WHEEL WELL. REMOVED AND REPLACED ANGLE UNDER 57-10-00-13A.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

CORROSION BETWEEN SKIN AND AFT LAVATORY SERVICE PANEL AT FORWARD CORNER. INSTALLED TITANIUM DOUBLER PER EA MD80-53-008593.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 30,827 hrs · 14,698 cycles

AFT ACCESSORY STIFFENER BRACE CRACKED BELOW AFT STAIR UPLOCK ACTUATOR AT LEFT CANT FRAME BETWEEN STATION 1485 AND 1497. INSTALLED STIFFENER DOUBLER PER SRM 51-01-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

OUTBOARD END OF CUSP FOUND CORRODED OUT OF LIMITS AT STATION 481 RIGHT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

AFT CARGO LEFT TIE DOWN TRACK SPLICE CORRODED. REMOVED AND REPLACED TIE DOWN TRACK SPLICE.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

LONGERON 29 RIGHT CORRODED AT STATION 1289 TO 1293. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 53-02-00.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

AFT CARGO HAS CORROSION AT RIGHT TIE DOWN TRACK AT FASTENERS STATION 1212 TO 1322. INSTALLED RIGHT TIE DOWN TRACK PER SRM 51-30-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

NUMBER 1 SEAT TRACK CORRODED OUT OF LIMITS BETWEEN STATION 1174 AND 1309. REPLACED SECTION OF SEAT TRACK PER SRM 51-01 MPN AA74-A-12.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

CORROSION FOUND ON CUSP UNDER T-ANGLE AT RIGHT STATION 522 TO 541. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,827 hrs · 14,698 cycles

DENT AT STATION 329 AT LONGERON 23 LEFT MEASURES 1.0 X .75 X .035 DEEP. DAMAGED AREA CUTOUT AND DOUBLER INSTALLED PER SRM 53-04 FIG 12B.

Part: TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

CORROSION FOUND ON AFT CARGO LEFT TIE DOWN TRACK AROUND FASTENER HOLES BETWEEN STATION 1212 AND 1322. REPLACE AFT CARGO TIE DOWN TRACK PER SRM 51-30-01 AND 51-30-05.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

CORROSION BETWEEN SKIN AND AFT LAVATORY SERVICE PANEL FORWARD LOWER CORNER. INSTALLED DOUBLER PER SRM 53-04 FIGURE 38.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 30,827 hrs · 14,698 cycles

CABIN SUB FLOOR CRACKED AT STATION 219, OUTBOARD OF SEAT TRACK 5. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

NUMBER 2 SEAT TRACK CORROSION REMOVAL OUT OF LIMITS AT STATION 1206. INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-05 FIG 4A.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

CORROSION ON FRAME STATION 1250 AT LONGERON 30. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-17.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,827 hrs · 14,698 cycles

CORROSION FOUND OUT OF LIMITS AT RIGHT CUSP AT STATION 858. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,583 hrs

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,583 hrs

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT SEAT 25B INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — CORRODED (LT MLG)

TUL - LEFT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE HAS CORROSION IN LARGE BORE. AREA IS 1.75 INCHES BY 2.2515 INCHES. FINAL MEASUREMENT IS 2.253 INCHES IN 1.75 INCH BUSHING AREA. LOCAL BLEND WHERE BUSHING DOES NOT CONTACT FROM SMALL BORE TO 1.98 INCH FROM FACE. DIMENSION DEPTH 2.270 AND .75 INCH IN DIAMETER. LEFT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE AREA REWORKED IN ACCORDANCE WITH ESO 80559 DATED NOVEMBER 22 2005.

Part: ACTUATOR — CORRODED (RT MLG)

TUL - RIGHT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE HAS CORROSION. AREA IS 1.75 INCHES BY 2.2515 INCHES. RIGHT HAND MAIN LANDING GEAR SUPPORT FITTING ASSEMBLY RETRACT ACTUATOR FITTING BORE REWORKED IN ACCORDANCE WITH ESO 80559 DATED NOVEMBER 17 2005.

Part: BUSHING — CORRODED (MLG SUPPORT BEAM)

TUL - MAIN LANDING GEAR SUPPORT BEAM RIGHT HAND RETRACT BUSHING INBOARD BUSHING OUTBOARD FACE HAS MINOR CORROSION. AREA IS 2.13 INCHES BY 2.13 INCHES WITH A DEPTH OF .025. ORIGINAL THICKNESS 1.235 INCHES. FINAL THICKNESS 1.210 INCHES. RIGHT HAND MAIN LANDING GEAR RETRACT BUSHING AREA REWORKED IN ACCORDANCE WITH ESO 80559 DATED NOVEMBER 17 2005.

Part: BUSHING — CORRODED (LT MLG)

TUL - LEFT HAND MAIN LANDING GEAR SUPPORT BEAM RETRACT BUSHING AREA INBOARD BUSHING OUTBOARD FACE HAS MINOR CORROSION. AREA IS 2.13 INCHES BY 2.13 INCHES. ORIGINAL THICKNESS .033 AND FINAL MEASUREMENT IS 1.202 REMAINING THICKNESS. LEFT HAND MAIN LANDING GEAR RETRACT BUSHING AREA REWORKED IN ACCORDANCE WITH ESO 80559 DATED NOVEMBER 22 2005.

Part: BATTERY PACK — INOPERATIVE (CABIN)

ORD - EMERGENCY LIGHTS AT OVERHEAD ROWS 19 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD ROWS 19 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DTW - LOWER EMERGENCY EXIT LIGHT AT LEFT OVERWING EMERGENCY EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT OVERWING EMERGENCY EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LANDING GEAR — MALFUNCTIONED (NLG)

ORD - EN ROUTE PSP AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT COMPLETELY. RED NOSE GEAR LIGHT REMAINED ON AND GREEN NOSE GEAR WENT OUT. RETURNED ORD AND LANDED WITHOUT INCIDENT. JACKED AIRCRAFT PER MM 7-12-00-2, PERFORMED INSPECTION OF NOSE GEAR. NO FAULTS NOTED. DROP CHECKED NOSE GEAR THREE TIMES, NO FAULTS. GREASED NOSE GEAR WITH WTR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (TAILCONE)

DFW AFT TAIL CONE COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT TAIL CONE COMPARTMENT BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLEED VALVE — DAMAGED (NR 1 ENGINE)

AIRCRAFT EN ROUTE ENCOUNTERED TWO LARGE VIBRATIONS THROUGHT OUT THE ENTIRE AIRCRAFT, PRESSURE FLOW LIGHT WENT ON WITH CABIN CLIMBING AT 1500 FT PER MINUTE. ANTI-ICE WAS IN THE ON POSITION. APPEARED TO BE COMPRESSOR STALL ON ENGINE NR 1. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS NOT OVERWEIGHT. REPLACED THE PRBS VALVES AND ACCOMPLISHED BLEED LUBE. LEAK AND SYSTEM GROUND CHECKED NORMAL. (M)

Part: FIRE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 6,446 hrs · 3,404 cycles

THE AFT CARGO FIRE DETECTOR WARNING SOUNDED. FIRED BOTTLE AND MADE UNSCHEDULED LANDING AT PIT. PLACARDED FIRE DETECTION SYSTEM INOPERATIVE PER MEL AND OPERATED TO STL. REPLACED THE AFT CARGO FIRE PROTECTION CEU CONNECTOR ACCOUNT CONTAMINATED.

Part: BATTERY — DISCHARGED (MID CABIN) · airframe 4,165 hrs · 2,254 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 18 TO 21. REPLACED THE BATTERIES. CHECK-C 7-1-00 STL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,811 hrs · 2,062 cycles

THE EMERGENCY LIGHT AT THE FWD LT ENTRANCE DOOR WAS INOPERATIVE, AND THE EGRESS LIGHTS AT ROWS 22 AND 23. REPLACED THE LAMP (P/N PR2) AT THE ENTRANCE DOOR, AND THE LAMP MODULE (P/N 0105606-002) FOR THE EGRESS LIGHTS. CHECK-C 7-1-00 STL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 3,593 hrs · 1,946 cycles

THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT ROWS 29 TO 31, AND THE LEFT AND RIGHT AFT EMERGENCY EXIT DOOR LIGHTS WERE INOPERATIVE. RECONNECTED WIRES AT ROW 31 FOR THE EGRESS LIGHTS, AND REPLACED THE BATTERY PACK, (P/N 408822-101), AND POWER SUPPLY FOR THE EXIT LIGHTS. CHECK-C 7-1-00 STL.

Part: MODULE — WORN (CABIN) · airframe 2,756 hrs · 1,483 cycles

THE EGRESS LIGHT AT ROW 33 END LIGHT WAS INOPERATIVE. REPLACED THE LIGHT MODULE.

Part: LENS — BROKEN (CABIN) · airframe 2,718 hrs · 1,463 cycles

DURING LANDING IT WAS NOTED THAT THE EGRESS LIGHT COVER WAS BROKEN AT ROWS 18DEF. REPLACED LENS. AC04 4-12-00 DFW.

Part: MODULE — FAILED (ROW 21)

TWO EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROW 21. REPLACED THE LAMP MODULE.