N967TW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,139 hrs · 25,596 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 18D IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 50,721 hrs · 25,333 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 15D IS INOPERATIVE. REPAIRED BROKEN WIRE AT SIDEWALL CONNECTOR PER AMM 33-60-98. OPERATIONAL CHECK GOOD.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 50,662 hrs · 25,291 cycles

NR 2 CABIN AUTO PRESSURE CONTROLLER INOPERATIVE LIGHT ON. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER IAW AMM 21-32-03. OPS CHECKED GOOD.

Part: RIB — CRACKED (LE SLAT) · airframe 49,394 hrs · 24,480 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT HAND WING LEADING EDGE NR 4 SLAT TRACK RIB. REPAIRED RIB PER 57-98-06.

Part: ANGLE — CORRODED (LT MLG WW) · corrosion level 2 · airframe 49,394 hrs · 24,480 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT WHEEL WELL ANGLE ABOVE BRAKE ACCUMULATOR BETWEEN STATION 946 AND 965. REPLACED ANGLE PER SRM 57-09-00-001.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 49,394 hrs · 24,480 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND TRAPEZOID FITTING ANGLE BETWEEN STATION 826 AND 845. REPLACED FITTING ANGLE PER SRM 57-09-00-001.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,394 hrs · 24,480 cycles

AIRCRAFT IN BASE MAINTENANCE. EMERGENCY LIGHTING BATTERY PACK BETWEEN FUSELAGE STATION 800 AND 900 FAILED TEST. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. REF AALA20170216010

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,394 hrs · 24,480 cycles

AIRCRAFT IN BASE MAINTENANCE. EMERGENCY LIGHTING BATTERY PACK BETWEEN FUSELAGE STATION 800 AND 900 FAILED TEST. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. REF AALA20170214014

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,394 hrs · 24,480 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION UNDER ANTENNA INTERNAL DOUBLER ON FORWARD FASTENERS AT STRINGER 29L. INSTALLED SERVICEABLE SKIN DOUBLER AARD 53-30-00-9 REPAIR 9 AND DRAWING 5911401.

Part: LENS — DETACHED (CABIN) · airframe 49,315 hrs · 24,424 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AFT OF FORWARD GALLEY HAS A DETACHED LENS COVER. SECURED LENS COVER. OPERATIONAL CHECK GOOD.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 49,229 hrs · 24,367 cycles

AIRCRAFT WAS GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE IS DEFECTIVE. REMOVED AND REPLACED SLIDE IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: PRESSURE SWITCH — LEAKING (APU) · airframe 49,164 hrs · 24,330 cycles

AIRCRAFT WAS GROUNDED. SMOKE IN CABIN AFTER AIR CONDITIONING PACKS WERE RUNNING FOR APPROXIMATELY 20 MINUTES. REMOVED AND REPLACED AUXILIARY POWER UNIT LOW OIL PRESSURE SWITCH IAW AMM 49-90-03. OPERATIONAL AND LEAK CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 48,328 hrs · 23,797 cycles

OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 12 AND 15 WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 48,328 hrs · 23,797 cycles

AFT EMERGENCY PATH LIGHTS ARE DIM WHEN TESTING WITH PACK AB5-3. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-60-98. OPERATIONAL CHECKED NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 47,990 hrs · 23,603 cycles

ABORTED TO AT 80 KTS ACCT WHEEL NOT TURNING LIGHT ILLUMINATED. ACCOMPLISHED REJECTED TAKE OFF INSPECTION IAW MCM 05-91-27, AND PERFORMED TRANSDUCER FUNCTION CHECK IAW AMM 32-43-02-201. OPERATIONS CHECK NORMAL AND PERFORMED ANTI-SKID BITE TEST IAW AMM 32-43-00. THE AIRCRAFT WAS GROUNDED.

Part: BULLET — LEAKING (NR 1 ENGINE) · airframe 47,382 hrs · 23,239 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, OBSERVED AN EPR SPLIT BETWEEN NR 1 & 2 ENGS. FOUND PT2 LINE DISLODGED INSIDE OF BULLET ON NR 1 ENG. R & R BULLET IAW AMM 77-11-03. ACCOMPLISHED HIGH POWER ENG RUN IAW AMM 71-00-00. ALL INDICATIONS NORMAL.

Part: MOISTURE TRAP — CONTAMINATED (RT ENGINE) · airframe 46,720 hrs · 22,859 cycles

AIRCRAFT WAS GNDED. RT ENG WOULD NOT REACH TAKEOFF POWER. TAKE OFF ABORTED AT APPROX 100 KNOTS. CLEANED & PURGED THE RT ENG PT7 MANIFOLD MOISTURE TRAP. R & R THE RT ENG EPR TRANSMITTER IAW AMM 77-11-02. OPERATIONAL & LEAK CHECKED GOOD. ACCOMPLISHED MCM CARD 77-92-12 WITH NO DEFECTS NOTED. SEE ALSO AALA20160125001.

Part: COMPUTER — FAULTY (EPR) · airframe 46,723 hrs · 22,861 cycles

AIRCRAFT WAS GNDED. RT ENG WOULD NOT REACH TAKEOFF POWER. TAKEOFF ABORTED AT APPROX 100 KNOTS. CLEANED & PURGED THE RT ENG PT7 MANIFOLD MOISTURE TRAP. R & R THE RT ENG EPR COMPUTER IAW AMM 77-11-02. OPERATIONAL & LEAK CHECKED GOOD. ACCOMPLISHED MCM CARD 77-92-12 WITH NO DEFECTS NOTED. SEE ALSO AALA20160121009.

Part: FITTING — CRACKED (RT SPOILER) · airframe 45,885 hrs · 22,355 cycles

RIGHT WING GND SPOILER CASTING CRACKED, INBD & OTBD SIDE. INSTALLED NEW RT GND SPOILER CASTING IAW SRM 51-01-00.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 45,885 hrs · 22,355 cycles

E & E COMPARTMENT, 2 EACH CRACKS IN SUB-FLOOR MEMBRANE, STATION 180 APPROX 31" LT OF FLOOR CENTERLINE. INSTALLED DOUBLER IAW AARD 53-20-00-16 & EA 2545278 DATED 09 02 2015.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 45,885 hrs · 22,355 cycles

FORWARD ENTRY DOOR NR 6, BEAM IS CRACKED AT FASTENER HOLE, CTR BRACKET. STOP DRILLED CRACK & INSTALLED DOUBLER IAW AARD 52-10-00.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 45,885 hrs · 22,355 cycles

FORWARD CARGO DOOR, FWD LOWER DOOR STOP PAD CRACKED. INSTALLED NEW CARGO DOOR STOP PAD IAW AARD 51-00-01.

Part: CONTACT — DIRTY (CABIN) · airframe 45,672 hrs · 22,238 cycles

CEILING EMERGENCY LIGHTS AT SEATS 32D INOPERATIVE. CLEANED BATTERY CONTACTS FOR 32D & PERFORMED OPERATIONAL CHECK IAW MM 33-53-00. SYSTEM CHECKED NORMAL.

Part: CONTACT — DIRTY (CABIN) · airframe 45,672 hrs · 22,238 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE AT ROW 13 - 17. CLEANED BATTERY CONTACTS & PERFORMED OPERATIONAL CHECK IAW MM 33-53-00. SYSTEM CHECKED NORMAL.

Part: PROBE — OBSTRUCTED (RT ENGINE) · airframe 45,222 hrs · 21,999 cycles

DURING TAKEOFF, RT ENG WOULD NOT MAKE TAKEOFF POWER. MAXIMUM EPR WAS 1.73. TAKEOFF ABORTED AT LESS THAN 60 KNOTS. REMOVED DEBRIS FROM LT ENG PT 2 PROBED. PERFORMED ENG RUNS AT ALL POWER SETTINGS IAW AMM 71-00-00. SYS CHECKED NORMAL.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 42,455 hrs · 20,539 cycles

ORD CREW REPORTED RT HYD QTY DOWN TO ZERO DURING CLIMBOUT. GEAR MANUALLY EXTENDED. EMER DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ELEC HYD PUMP & ENG DRIVEN PUMP MPN 3029981001. SYS GND CHECKED NORMAL, OPERATIONS CLOSED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION REMOVAL ON SEAT TRACK NR 6 FROM STATIONS 824 TO 826 BEYOND LIMITS. PERFORMED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION REMOVAL ON SEAT TRACK NR 6 FROM STATIONS 836 TO 838 IS BEYOND LIMITS. PERFORMED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

SEAT TRACK NR 2 CORRODED AT STATION 1206. ACCOMPLISHED SEAT TRACK SPLICE REPAIR FROM STATIONS 1185 TO 1242 IAW SRM 53-05-00 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION REMOVAL ON SEAT TRACK NR 6 FROM STATIONS 894 TO 895 BEYOND LIMITS. PERFORMED SEAT TRACK PLUG REPAIR IAW AARD 53-20-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

NR 6 SEAT TRACK CORRODED FROM STATIONS 805 TO 809. INSTALLED CTR SPLICE CHANNEL FROM STATIONS 794 TO 810 & SEAT TRACK PLUG FROM STATION 805 TO 810 IAW SRM 53-05-00 FIGURE 4A.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 42,308 hrs · 20,468 cycles

FORWARD ENTRY DOOR GOUGED IN EDGE OF DOOR SKIN NEAR FWD LOWER CORNER. ROUTED OUT DAMAGE THEN INSTALLED DOUBLER IAW AARD 52-10-00-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION ON LT CUSP FROM STATIONS 840 TO 845. INSTALLED NEW SERVICEABLE LT CUSP FROM STATIONS 818 TO 845 IAW AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,308 hrs · 20,468 cycles

INTERCOSTAL CRACKED FROM STATIONS 1309 TO 1287. INSTALLED NEW INTERCOSTAL IAW SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

NUMBER 6 SEAT TRACK FROM STATIONS 590 TO 800 CORRODED. PERFORMED SEAT TRACK SPLICE REPAIR IAW AARD 51-00-05-1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

SEAT TRACK NR 6 FROM STATIONS 264 TO 590 CORRODED. PERFORMED SEAT TRACK SPLICE REPAIR FROM STATIONS 218 TO 590 IAW AARD 53-00-00-08.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION ON RT CUSP STATION 334 UNDER NR 6 SEAT TRACK. DRILLED OUT CORROSION IAW SRM 53-01-00-001 & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

FLOORBOARD SUPPORT AT STATION 1155 BETWEEN LONGERONS 29 & 28 RT CORRODED. REPLACED SUPPORT IAW SRM 51-30-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

FLOORBOARD SUPPORT FROM STATIONS 1155 TO 1145 ABOVE LONGERON 28 RT CORRODED. REPLACED SUPPORT IAW SRM 51-30-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 42,308 hrs · 20,468 cycles

LEFT CUSP SHEET CRACKED FROM STATIONS 789 TO 807. INSTALLED NEW SERVICEABLE CUSP SHEET IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION ON RT CUSP SHEET FROM STATIONS 581 TO 585. REMOVED DAMAGED SECTION & INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION ON CUSP AT STATION 857 & STRINGER 18 LT. REMOVED DAMAGED SECTION & INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION ON SEAT TRACK NR 4 FROM STATIONS 237 TO 263 RT. INSTALLED SPLICED SEAT TRACK FROM STATIONS 200 TO 265 RT IAW SRM 53-05-00-001.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 42,308 hrs · 20,468 cycles

SUBFLOOR CRACKED AT STATION 218 RT UNDER SEAT TRACK NR 4. INSTALLED SUBFLOOR DOUBLER IAW AARD 53-20-00-16.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,308 hrs · 20,468 cycles

CRACK IN WEB TANG AT STATION 207 & LONGERON 15 LT. REMOVED DAMAGE AREA & INSTALLED 7075-T6 STRAP REPAIR IAW AARD 53-10-00-11.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

WEB CORRODED INBD OF AFT CARGO DOOR CUT OUT FROM FUSELAGE STATIONS 1193 TO 1211. INSTALLED AFT CARGO DOOR BEAM WEB SPLICE IAW AARD 53-10-00-24.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION ON LT CUSP AT STATION 1177. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

RIGHT HAND CUSP CORRODED FROM STATIONS 418 TO 419. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

CORROSION ON G 2 GALLEY AFT INBD MOUNT FITTING AT STATION 218. REPLACED MOUNT FITTING IAW AARD 51-00-05-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,308 hrs · 20,468 cycles

RIGHT HAND CUSP CORRODED FROM STATION 380. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,308 hrs · 20,468 cycles

FUSELAGE SKIN CRACKED AT LT AFT NLG DOOR, AFT HINGE CUT OUT. INSTALLED DOUBLER IAW SRM 53-05-00-001.

Part: RIB — CRACKED (LT WING) · airframe 42,308 hrs · 20,468 cycles

LEFT WING LE INBD FORMER IS CRACKED AT NR 4 ST. REPAIRED FORMER IAW MCM 57-98-05 & EA MD80-57-034517.

Part: BATTERY — NOT SEATED (CABIN) · airframe 39,028 hrs · 18,660 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RE-SEATED BATTERIES. OPS CHECK GOOD.

Part: BATTERY — NOT SEATED (CABIN) · airframe 39,028 hrs · 18,660 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 13 TO 16 INOPERATIVE. RE-SEATED BATTERIES. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 34,706 hrs · 16,462 cycles

DFW - CREW REPORTED NAVIGATION SYSTEM ISSUES DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. REPLACED NUMBERS ONE AND TWO DIGITAL FLIGHT GUIDANCE COMPUTERS AND NUMBERS ONE AND TWO INERTIAL REFERENCE UNIT COMPUTERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 34,183 hrs · 16,198 cycles

SHEAR-TIE CRACKED, AFT SIDE OF STATION 1451 LONGERON 2 LEFT. REPLACED SHEAR TIE PER SRM 53-01-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,392 hrs · 15,814 cycles

SEVERAL CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMPS FOR CEILING EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 33,392 hrs · 15,814 cycles

ALL SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. RE-SEATED CONNECTOR ON SEAT POWER SUPPLY MID CABIN. OPS CHECK NORMAL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,055 hrs · 14,269 cycles

CORROSION AT FRAME STATION 1309. INSTALLED FRAME SPLICE PER SRM 53-03-0.

Part: LONGERON — CORRODED (E&E BAY) · corrosion level 2 · airframe 30,055 hrs · 14,269 cycles

ELECTRICAL COMPARTMENT LONGERON 30 IS CORRODED AT STATION 20 TO 170. INSTALLED SPLICE SECTION PER AARD 53-00-00-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,055 hrs · 14,269 cycles

FOUND CRACK AT FRAME STATION 1418, LONGERON 2 RIGHT. INSTALLED DOUBLER AND STRAP PER SRM 53-03-00 FIG 31A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 30,055 hrs · 14,269 cycles

LONGERON 2 RIGHT CRACKED AFT OF STATION 1418. INSTALLED NEW SECTION OF LONGERON AND LONGERON SPLICE PER AARD 53-30-00-2.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,055 hrs · 14,269 cycles

MID CARGO DOOR BEAM HAS CORROSION AT STATION 636 TO 693. INSTALLED DOUBLER PER AARD 53-10-00-3

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,055 hrs · 14,269 cycles

CORROSION ON RIGHT CUSP STATION 733 TO 734. INSTALLED CUSP DOUBLER PER 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,055 hrs · 14,269 cycles

DENT IN SKIN AT STATION 237 BETWEEN STRINGER 17L AND 18L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,055 hrs · 14,269 cycles

UPPER AND LOWER LEGS ON DOOR BEAM HAVE CORROSION AT STATION 1155 TO 1211. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,055 hrs · 14,269 cycles

CORROSION ON RIGHT CUSP AT STATION 716 TO 718. INSTALLED CUSP DOUBLER PER AARD 53-20-0-176.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 30,055 hrs · 14,269 cycles

STATION 905 CUSP FASTENER HOLE CRACKED. INSTALLED DOUBLER.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,055 hrs · 14,269 cycles

DENT AT STATION 237 BETWEEN LONGERON 17 LEFT AND 18 LEFT. ACCOMPLISHED EXTERNAL DOUBLER REPAIR UNDER SRM 53-04 FIG 12B.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 30,055 hrs · 14,269 cycles

J-ANGLE DOUBLER CRACKED IN LEFT SIDE OF NOSE WHEEL WELL AREA. INSTALLED DOUBLER PER AARD 53-10-00-4.

Part: PAN — CRACKED (FUSELAGE) · airframe 30,055 hrs · 14,269 cycles

RIGHT WINDOW RING PAN LOWER AFT CORNER AT STATION 1098 CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,055 hrs · 14,269 cycles

CORROSION FOUND ON SUB FLOOR WEBBING IN FORWARD CABIN AREA BETWEEN STATION 200 TO 212, OUTBOARD OF SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (FUSELAGE) · airframe 30,055 hrs · 14,269 cycles

RIGHT WINDOW PAN AT STATION 1174 TO 1193 UPPER AFT CORNER HAS CRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WEB — CRACKED (FUSELAGE) · airframe 30,055 hrs · 14,269 cycles

FORWARD CABIN AREA HAS CRACK IN SUBFLOOR WEBBING AT STATION 218 OUTBOARD OF NUMBER 5 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SHROUD — BROKEN (CABIN)

EMERGENCY LIGHT AT SEAT 13D HAS BROKEN SHROUD. REPLACED SHROUD AND LENS.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 28,892 hrs

LGA - FORWARD EMERGENCY FLASHLIGHT SAFETY STRAP MISSING. REPLACED SAFETY STRAP FOR FORWARD EMERGENCY FLASHLIGHT.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 27,154 hrs

EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. SECURED CONNECTOR AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 27,154 hrs

EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. SECURED CONNECTOR AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 27,154 hrs

LGA EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. SECURED CONNECTOR AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 27,125 hrs

LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT LAVATORY HAS BROKEN SAFETY STRAP. REPLACED STRAP FOR FLASHLIGHT AT AFT RIGHT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PISTON — BENT (NLG) · airframe 25,622 hrs

ONT - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED BENT PISTON. REPLACED CYLINDER SHOCK STRUT, SEALS AND UPPER AND LOWER TORQUE LINKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT)

SEA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. SECURED LOOSE WIRE FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY ESCAPE PATH SEAT LIGHT IN FORWARD SECTION OF CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5-2 FOR EMERGENCY ESCAPE PATH SEAT LIGHT IN FORWARD SECTION OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - FOUND EMERGENCY ESCAPE PATH SEAT LIGHTS IN AFT CABIN SECTION INOPERATIVE. REPLACED BATTERY PACK AT AB53 FOR EMERGENCY ESCAPE PATH SEAT LIGHTS IN AFT CABIN SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT)

LGA - EMERGENCY FLASHLIGHT FORWARD STRAP BROKEN. REPLACED EMERGENCY FLASHLIGHT FORWARD STRAP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY EXIT LIGHT AT RIGHT HAND OVERWING FORWARD HATCH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT RIGHT HAND OVERWING FORWARD HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHTS AT SEAT 11D, 13D, AND 32D INOPERATIVE. REPLACED SEAT CONNECTOR AT SEAT 11D AND RECONNECTED SEATS 13D AND 32D TO LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

OVERHEAD EMERGENCY EXIT LIGHTS IN VENTRAL STAIRWAY INOPERATIVE. REPLACED BATTERY PACK B528 FOR OVERHEAD EMERGENCY EXIT LIGHTS IN VENTRAL STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 9,956 hrs · 5,464 cycles

AT STA 169, THE FRAME FOOT WAS DAMAGED AT LONGERON 19R TO 20R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 9,946 hrs · 5,464 cycles

LONGERON 19R AT STA 160 TO 154 WAS DAMAGED. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 9,946 hrs · 5,464 cycles

AT STA 160 THE FRAME WAS DAMAGED AT LONGERON 19R TO 22R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 9,946 hrs · 5,464 cycles

THE FUSELAGE SKIN WAS DAMAGED AT STA 154 TO 160. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL.

Part: SKIN — DENTED (FUSELAGE) · airframe 9,946 hrs · 5,464 cycles

FOUND DENT IN FUSELAGE SKIN AT STA 167, ABOVE LONGERON 20R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 9,946 hrs · 5,464 cycles

LONGERON 20R AT STA 160 TO 154 WAS DAMAGED. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 9,946 hrs · 5,464 cycles

AT STA 160 THE FRAME FOOT WAS DAMAGED AT LONGERON 20R TO LONGERON 18R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL.

Part: SKIN — DENTED (FUSELAGE) · airframe 9,946 hrs · 5,464 cycles

SKIN AT STA 181 ABOVE LONGERON 20R WAS DENTED. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 9,946 hrs · 5,464 cycles

AT STA 169 THE FRAME WAS DAMAGED AT LONGERON 19R TO 20R. REPAIRED PER ARA 18469. CHECK-C 1-22-03 STL.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 9,131 hrs · 5,015 cycles

STRONG ELECTRICAL SMELL WAS NOTICED IN COCKPIT AND FORWARD GALLEY. SHUT OFF GALLEY POWER AND SMELL DISSIPATED. REPLACED THE NUMBER 2 GALLEY OVEN.

Part: HYDRAULIC SYSTEM — LEAKING (APU BAY) · airframe 8,600 hrs · 4,682 cycles

HYD FLUID LEAK INTO APU INLET RESULTING IN SMOKE IN THE CABIN. RETURNED AIRCRAFT TO THE GATE. CHANGED WATER SEPARATORS AND PERFORMED MD9-49-06. PAC BURNOUT OP CHECK.

Part: BATTERY — OUT OF POSITION (CABIN) · airframe 8,167 hrs · 4,425 cycles

THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 14 THROUGH 19. REPOSITIONED THE BATTERY PACK BATTERIES.

Part: BULB · airframe 8,142 hrs · 4,409 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 21D TO 27D. REPLACED POWER SUPPLY, PN 60-0304-51, AND ALL THE BULBS. CHECK-C 5-26-01 STL. --CLOSED--

Part: SIGN — INOPERATIVE (CABIN) · airframe 8,151 hrs · 4,415 cycles

THE LOWER OVERWING EXIT SIGN WAS INOPERATIVE. REPLACED THE SIGN.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 7,717 hrs · 4,168 cycles

DURING CHECK-C MAINT FOUND CORROSION AROUND E/E COMPARTMENT DOOR FRAME. REMOVED AND REPLACED DOOR PAN STRUCTURE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 7,717 hrs · 4,168 cycles

DURING CHECK-C MAINTENANCE FOUND CORROSION FROM LONGERON 29L TO 29R, STA 160 TO 218. REPLACED SKIN FROM STA 110 TO 229, STRINGER 26L TO 26R, PER SPM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 7,717 hrs · 4,168 cycles

DURING CHECK-C MAINT THE FWD CARGO COMPT BELLY SKIN HAD CORROSION AT STA 218 TO 229, LONGERON 29L TO 29R. INSTALLED NEW SKIN PER DRAWING 5911401.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 7,717 hrs · 4,168 cycles

DURING CHECK-C FOUND AFT ACCY COMPARTMENT BRACKET CRACKED ABOVE RT VENT BOX FWD OF RUDDER TRIM DRUM. DOUBLER FABRICATED PER SRM 53-01, FIG 3 AND 4, PAGE 18.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 7,717 hrs · 4,168 cycles

DURING CHECK-C MAINT THE LT SIDE VENT BOX UPPER FORWARD STRUCTURAL TIE CLIP WAS FOUND BROKEN.

Part: TIE CLIP — BROKEN (FUSELAGE) · airframe 7,717 hrs · 4,168 cycles

DURING CHECK-C MAINT THE UPPER FWD CORNER OF THE RT VENT BOX STRUCTURAL TIE CLIP WAS BROKEN. FABRICATED NEW CLIP AND INSTALLED PER SRM 51-30-6 AND SPM 6-30-07.

Part: LIGHT — INOPERATIVE (ROWS 12 - 22) · airframe 4,099 hrs · 2,220 cycles

BOTH FWD EMERGENCY EXIT SIDE WALL SIGNS, THE FLOOR EGRESS LIGHTS FROM ROWS 12 TO 22, AND THE CEILING EMERGENCY LIGHTS FROM ROWS 7 THRU 11 WERE INOPERATIVE. REPLACED THE BATTERIES (P/N 408822-101) FOR THE EMERGENCY EXIT SIGNS, REPLACED THE MODULE (P/N 0105606-003) FOR THE EGRESS LIGHTS, AND THE BATTERIES (P/N 408822-102) FOR THE CEILING LIGHTS. CHECK-C 7-15-00 JFK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,757 hrs · 1,517 cycles

THE FORWARD PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LIGHT, NO CHECK-C.