N70425

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,961 hrs · 47,471 cycles

AIRCRAFT WAS NOT GROUNDED. EGRESS FORWARD OVERWING ESCAPE HATCH LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK B5-103 PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,961 hrs · 47,471 cycles

AIRCRAFT WAS NOT GROUNDED. EGRESS AISLE FLOOD LIGHTS FROM ROWS 9 TO 16 ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS B5-101 AND B5-102 (AALA201711239011) PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,961 hrs · 47,471 cycles

AIRCRAFT WAS NOT GROUNDED. EGRESS AISLE FLOOD LIGHTS FROM ROWS 9 TO 16 ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS B5-101 (AALA201711239007) AND B5-102 PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,824 hrs · 46,749 cycles

THE AIRCRAFT WAS GROUNDED. AFTER TAKE OFF NOSE RED INDICATOR LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION. RECYCLE GEAR HANDLE PER QRH, RED LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. T/S NOSE L/G IND, SWUNG NLG PER AMM 32-60-00 COULD NOT DUPLICATE FAULT. ALL SYS OPS CKD NML.

Part: ACM — LEAKING (AC BAY) · airframe 86,410 hrs · 46,500 cycles

SHORTLY AFTER TAKE OFF FLIGHT ATTENDANT REPORTED SMELL IN CABIN. WENT THROUGH QRH, TURNED OFF A/C RECIRCULATION FAN AND PULLED C/B. SMELL WENT AWAY QUICKLY. USING MCM CARD 21-96-01 FOUND LT ACM OUT OF OIL. REPLACED ACM IAW MCM CARD 21-94-01. AFTER REPLACING ACM, NO SMELL NOTED. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 86,270 hrs · 46,406 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IN THE FORWARD CABIN FAILED TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 33-50-01. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — FAULTY (ENGINE SYNC) · airframe 85,804 hrs · 46,105 cycles

TAKEOFF ABORTED AT 82 KNOTS AT DFW. NORMAL ABORT. LEFT ENGINE ACCELERATED NORMALLY TO 1.4 EXHAUST PRESSURE RATIO BUT NEVER BEYOND 1.5. MANUALLY PUSHED THROTTLES FORWARD WITH NO RESPONSE. DISENGAGED AUTO-THROTTLES. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT ENGINE SYNCHRONIZATION ACTUATOR ASSEMBLY AND CONTROL BOX IAW AMM 76-11-02. SYNCHRONIZATION AND ACCELERATION TESTS OPERATIONAL CHECK GOOD.

Part: CONTROL BOX — FAULTY (LT ENGINE) · airframe 85,804 hrs · 46,105 cycles

TAKEOFF ABORTED AT 82 KNOTS AT DFW. NORMAL ABORT. LEFT ENGINE ACCELERATED NORMALLY TO 1.4 EXHAUST PRESSURE RATIO BUT NEVER BEYOND 1.5. MANUALLY PUSHED THROTTLES FORWARD WITH NO RESPONSE. DISENGAGED AUTO-THROTTLES. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED THE LEFT ENGINE SYNCHRONIZATION ACTUATOR ASSEMBLY AND CONTROL BOX IAW AMM 76-11-02. SYNCHRONIZATION AND ACCELERATION TESTS OPERATIONAL CHECKED GOOD.

Part: SIGN — DETACHED (CABIN) · airframe 85,764 hrs · 46,083 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY EXIT SIGN OVER WING EXIT IS DETACHED FROM CEILING MOUNT. RESECURED EXIT SIGN. OPERATIONAL CHECK GOOD.

Part: TARGET — OUT OF ADJUST (CARGO DOOR) · airframe 85,300 hrs · 45,796 cycles

DURING CLIMB THE FORWARD CARGO DOOR ANNUNICATOR LIGHT ILLUMINATED AND CAPTAIN OBSERVED CABIN WAS UNPRESSURIZED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. ADJUSTED FORWARD CARGO DOOR SENSOR TARGET AND PERFORMED BITE CHECK AT PROXIMITY BOX WITH NO FAULTS FOUND IAW AMM 52-70-02.

Part: DOOR FRAME — CRACKED (BS 1338) · airframe 84,834 hrs · 45,503 cycles

AFT STAIRS DOOR RIGHT FRAME IS CRACKED ALONG RADIUS. REPAIRED THE DOOR FRAME IAW SRM 53-01-00-001 FIGURE 2 AND EA 262287.

Part: O-RING — BROKEN (NLG STRUT) · airframe 84,270 hrs · 45,156 cycles

AIRCRAFT WAS GNDED. DURING CLIMB, NLG WOULD NOT RETRACT & LOCK. FOUND NLG STRUT, SCHRADER VALVE O RING BROKEN. R & R O RING & VLV. ACCOMPLISHED STRUT SERVICING IAW AMM 32-21-02. ACCOMPLISHED 3 CYCLES OF NLG 5 RETRACTION & EXTENSION IAW AMM 32-21-03. SYSTEM CHECKED NORMAL.

Part: DUCT — LEAKING (ANTI-ICE SYS) · airframe 82,692 hrs · 44,238 cycles

LEFT ENG FIRE INDICATION AT APPROX 1,500 FEET ON TAKEOFF. AN EMER WAS DECLARED & THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. THE LT ENG WAS NOT SHUTDOWN. ACFT REMOVED FROM SERVICE. R & R LT ENG COWL ANTI-ICE BLEED DUCT IAW AMM 71-10-01. OPERATIONALLY CHECKED NORMAL. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 82,024 hrs · 43,826 cycles

EMERGENCY LIGHTS IN AFT TAIL CONE AREA INOPERATIVE. R & R BATTERY PACK IAW AMM 33-53-00. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 82,024 hrs · 43,826 cycles

FORWARD STRING OF ESCAPE PATH LIGHTING IS DIM & THEN FADES OUT DURING DUAL FEED CHECK WITH LIGHTS OPERATING ON CTR BATTERIES. R & R BATTERY IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 81,896 hrs · 43,754 cycles

EMERGENCY EVACUATION LIGHT BATTERY PACK B5-28 IS INOPERATIVE. R & R BATTERY PACK B5-28 IAW AMM 33-53-00. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: FUEL FILTER — FAULTY (NR 1 ENGINE) · airframe 81,213 hrs · 43,383 cycles

DURING TAKEOFF NR 1 ENG FUEL FILTER INLET PRESS LOW LIGHT ILLUMINATED. TAKEOFF ABORTED AT 40 KNOTS. R & R NR 1 ENG FUEL FILTER. PERFORMED LEAK CHECK IAW AMM 73-12-01-201. SYS CHECKED NORMAL.

Part: SUPPORT — CRACKED (LT WING) · airframe 79,661 hrs · 42,471 cycles

LEFT FWD WING SPAR PULLEY BRACKET SUPPORT CASTING CRACKED INBD OF NR 8 SLAT TRACK FROM STATIONS XHS 240 TO 253. REMOVED & INSTALLED NEW SERVICEABLE SUPPORT IAW AARD 51-00-05-1 & EA MD80-57-035547.

Part: DOME NUT — MISSING (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

ANTENNA ATTACHMENT DOME NUT ON CROWN SKIN MISSING BETWEEN STATIONS 1022 & 1041. INSTALLED ANTENNA ATTACHMENT DOME NUT IAW EA MD80-53-035371 & SRM 53-05-00 PARAGRAPH 141.

Part: ANGLE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 79,661 hrs · 42,471 cycles

LEFT WW UPPER OTBD UPPER SLANT PANEL ANGLE CORRODED. REMOVED & INSTALLED NEW SERVICEABLE ANGLE IAW AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

CRACKED INTERCOSTAL, AFT CARGO CEILING FROM STATIONS 1271 TO 1287. REMOVED & INSTALLED NEW INTERCOSTAL IAW AARD 51-00-05-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

CRACKED INTERCOSTAL, AFT CARGO CEILING AREA FROM STATIONS 1287 TO 1309. REMOVED & INSTALLED NEW INTERCOSTAL IAW AARD 51-00-05-1.

Part: PAN — CRACKED (CARGO DOOR) · airframe 79,661 hrs · 42,471 cycles

MID CARGO DOOR OUTER PAN HAS CRACK AT NR 5 BEAM AFT RADIUS BLOCK. INSTALLED DOUBLER IAW SRM 52-03-00-001 & EA MD80-52-035385.

Part: DOUBLER — WORN (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

WEAR ON EXISTING DOUBLER AT FWD SIDE OF LT FRAME STATION 1380 JUST AFT OF LT TEMPERATURE CONTROL VLV. R & R DOUBLER IAW AARD 53-10-00-28.

Part: FRAME — CRACKED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

CRACK ON RT CANT FRAME AT STATION 1474 & LONGERON 18 RT. REMOVED CRACKED SECTION OF FRAME & INSTALLED REPAIR ANGLE IAW SRM 51-70-05-001.

Part: PAN — WORN (SERVICE DOOR) · airframe 79,661 hrs · 42,471 cycles

AFT SERVICE DOOR INNER HANDLE HOUSING HAS WORN AREA. REPLACED AFT SERVICE DOOR HANDLE HOUSING IAW 51-00-05-REPAIR 1.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

SUB FLOOR IS CRACKED AT VENTURI HOLE UNDER G1 DRAIN PAN BETWEEN STATIONS 148 TO 160. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 79,661 hrs · 42,471 cycles

LEFT AFT OVERWING EXIT DOOR CRACKED UNDER THE NR 12 STOP PAD. REPAIRED WITH INTERNAL DOUBLER IAW SRM 52-05-00-001 FIGURE 51 SHEET 3.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 79,661 hrs · 42,471 cycles

RIGHT AFT OVERWING EXIT DOOR PAN IS CRACKED AT NR 12 STOP PAD. REPAIRED WITH AN INTERNAL DOUBLER IAW SRM 52-05-00-001 FIGURE 51 SHEET 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

SEAT TRACK NR 6 FROM STATIONS 281 TO 283 CORRODED. INSTALLED SEAT TRACK PLUG IAW AARD 53-20-00-10.

Part: PAN — WORN (CARGO DOOR) · airframe 79,661 hrs · 42,471 cycles

MID CARGO DOOR OUTER PAN WORN AT LOWER FWD STOP PAD. INSTALLED DOUBLER IAW AARD 52-30-00-1 FIGURE 2.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 79,661 hrs · 42,471 cycles

LEFT AFT OVERWING EXIT DOOR FRAME CRACKED UNDER NR 1 STOP PAD. REPAIRED WITH INTERNAL DOUBLER REPAIR IAW SRM 52-05-00-001 FIGURE 51 SHEET 3.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,661 hrs · 42,471 cycles

G2 GALLEY MOUNT CORRODED AT STATION 210 & RBL 12. INSTALLED G-2 GALLEY MOUNT IAW AARD 51-00-05 & DWG 9936535 & CONFIGURATION 537.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

G2 GALLEY MOUNT CORRODED AT STATION 218 & RBL 12. INSTALLED NEW GALLEY MOUNT IAW AARD 51-00-05-1 & DWG 9936535.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

CORROSION IN SUB FLOOR AROUND G2 GALLEY MOUNT HOLE AT STATION 218 & RBL 12. INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: FRAME — GOUGED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

FRAME AT STATION 636 & LONGERON 7 LT GOUGED. ACCOMPLISHED NESTED ANGLE REPAIR IAW SRM 51-70-05-001.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

CORROSION IN FITTING BELOW SUBFLOOR AT G2 MOUNT AT STATION 218 & RBL 12. INSTALLED NEW FITTING IAW AARD 51-00-05 & AARD 52-20-00.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

VERTICAL STIFFENER CRACKED AT UPPER END, ABOVE VAULT DOOR ON CTR LINE. INSTALLED NEW SERVICEABLE STIFFENER IAW AARD 51-00-05-1 & SRM 51-30-05.

Part: SKIN — BENT (CARGO DOOR) · airframe 79,661 hrs · 42,471 cycles

AFT CARGO DOOR LOWER EDGE OF OUTER SKIN BENT TO RIVET ROW. BUILT & INSTALLED DOUBLER IAW ESO 80174 PAGE 601 F.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

LEFT CUSP CRACKED FROM STATIONS 740 TO 741. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,661 hrs · 42,471 cycles

NUMBER 4 SEAT TRACK FROM STATIONS 1256 TO 1260 CORRODED. INSTALLED SEAT TRACK SPLICE IAW SRM 53-05-00 AT STATION 1222 & SEAT TRACK 4 FROM STATIONS 1222 TO 1309 IAW SRM 53-05-00-001 FIGURE 4F.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

LEFT CUSP CRACKED AT STATION 845 AT SEAT TRACK NR 1. INSTALLED NEW LT CUSP SHEET FROM STATIONS 807 TO 845 IAW SRM 51-00-05-1, SRM 53-14-03-001 FIGURE 10 & DWG 9910151.

Part: PAN — CRACKED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

WINDOW RING PAN FROM STATIONS 1174 TO 1175 CRACKED. ACCOMPLISHED NESTED REPAIR ANGLE IAW AARD 53-10-00-25.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 79,661 hrs · 42,471 cycles

FORWARD ENTRY DOOR FRAME WEB, REPAIR DOUBLER CRACKED AT STATION 208 & LONGERON 15 LT. INSTALLED DOUBLER & FILLER IAW AARD 53-10-00-11.

Part: WEB — CRACKED (PAX DOOR) · airframe 79,661 hrs · 42,471 cycles

FORWARD PAX DOOR UPPER WEB IS CRACKED AT STATION 206. INSTALLED DOUBLER & FILLER IAW AARD 53-10-00-11.

Part: SUPPORT FITTING — CRACKED (LT SPOILER) · airframe 79,661 hrs · 42,471 cycles

LEFT GND SPOILER ACTUATOR SUPPORT FITTING CRACKED. REPLACED FITTING.

Part: RIB — CRACKED (RT WING) · airframe 79,661 hrs · 42,471 cycles

RIGHT WING LE RIB AT NR 4 SLAT TRACK INBD RIB CRACKED. REPAIRED RT WING NR 4 SLAT TRACK INBD SUPPORT RIB IAW EA MD80-57-035287.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 78,032 hrs · 41,563 cycles

OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EXIT EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,862 hrs · 41,454 cycles

INTERIOR AFT OVERWING EMERGENCY LIGHT FAILED TEST. REPLACED BATTERY PACK B5-105. OPERATIONS CHECKED NORMAL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,894 hrs · 39,781 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK AT ROW 29DEF. OPS CHECK NORMAL.

Part: COVER — MISSING (CABIN) · airframe 72,044 hrs · 38,171 cycles

EMERGENCY LIGHT COVER ON FORWARD GALLEY EMERGENCY LIGHT MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,044 hrs · 38,171 cycles

EMERGENCY PATH LIGHTS FORWARD OF THE OVERWING EXITS INOPERATIVE. REPLACED BOTH BATTERY PACKS.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 70,436 hrs · 37,279 cycles

TAIL COMPARTMENT EMERGENCY LIGHT ABOVE CATWALK INOPERATIVE. ADJUSTED POWER SUPPLY AND OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,436 hrs · 37,279 cycles

CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT, OPS CHECK NORMAL.

Part: TRACK — CORRODED (CARGO BAY) · airframe 68,032 hrs · 35,963 cycles

LEFT TIE-DOWN CORRODED OUT OF LIMITS IN AFT CARGO FROM STATIONS 1220 TO 1332. REPLACED LEFT TIE-DOWN TRACK PER SRM 51-01-00-02, SRM 51-30-01 AND SRM 51-30-05.

Part: FLOOR SUPPORT — LOOSE (FUSELAGE) · airframe 68,032 hrs · 35,963 cycles

FLOORBOARD SUPPORT BETWEEN NUMBER 3 AND 4 SEAT TRACK IS LOOSE. REPLACED FLOORBOARD SUPPORT BETWEEN SEAT TRACK NUMBER 3 AND 4 PER SRM 51-10-1.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,032 hrs · 35,963 cycles

HEAVY CARGO/AFT - CORROSION ON FRAME LOWER FLANGE STATION 1271 LONGERON 28 LEFT TO LONGERON 28 RIGHT. BLENDED AND REMOVED CORROSION PER SRM 51-10-03 FOUND TO BE OUT OF LIMITS PER SRM 53-01. TREATED AND PRIMED AREA PER SRM 51-10-3. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-14 AND SRM 51-30-5.

Part: FITTING — CORRODED (GALLEY) · airframe 68,032 hrs · 35,963 cycles

CORROSION G1 OUTBOARD TIE DOWN STATION 160. INSTALLED NEW G-1 GALLEY TIE DOWN FITTING PER SRM 51-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,032 hrs · 35,963 cycles

CORROSION BELOW AFT GIRT BAR SUPPORT AT AFT SERVICE DOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STRUCTURE — MISREPAIRED (SERVICE DOOR) · airframe 68,032 hrs · 35,963 cycles

IMPROPER REPAIR AT AFT SERVICE DOOR HOLD OPEN HOOK AREA. REMOVED IMPROPER DOUBLER, DRILLED NEW DOUBLER TO FIT AND INSTALLED NEW DOUBLER ON AFT SERVICE DOOR PER SRM 52-05-00, FIG 54.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 68,032 hrs · 35,963 cycles

G2 GALLEY MOUNT CORRODED OUT OF LIMITS AT STATION 210 INBOARD OF SEAT TRACK NUMBER 4. REPLACED G2 GALLEY MOUNT PER SRM 51-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,032 hrs · 35,963 cycles

LEFT CUSP CORRODED OUT OF LIMITS AT STATION 714 TO 716 LEFT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,032 hrs · 35,963 cycles

CORROSION OUT OF LIMITS ON DOUBLER AT CENTER OF 1138 BULKHEAD AT LONGERON 30. INSTALLED DELTA PLATE DOUBLER PER SRM 51-30-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,032 hrs · 35,963 cycles

AFT ACCESSORY CANT FRAME CRACKED AT STATION 1497 BELOW RIGHT LOUVER BOX. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-15 AND SRM 51-01-00.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,032 hrs · 35,963 cycles

ANGLE STATION 1212 CORRODED BEYOND LIMITS. REPLACED ANGLE.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,032 hrs · 35,963 cycles

CORROSION ON CUSP OUTBOARD OF SEAT TRACK NUMBER 1 AT STATION 852 TO STATION 859. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: ATTACH FITTING — CRACKED (LE SLAT) · airframe 68,032 hrs · 35,963 cycles

HIGHT FREQUENCY EDDY CURRENT INDICATES CRACK ON LEFT WING LEADING EDGE NUMBER 5 SLAT AT 2ND FROM OUTBOARD RIB, INBOARD LEG. REMOVED 2ND FROM OUTBOARD ATTACH FITTING; LOCATED, DRILLED, AND INSTALLED NEW ATTACH FITTING PER / ESO 80117. CLEARANCE TO INSTALL LOWER SKIN. INSTALLED LOWER OUTBOARD SKIN PER ESO 80117.

Part: RIB — CRACKED (LE SLAT) · airframe 68,032 hrs · 35,963 cycles

HIGH FREQUENCY EDDY CURRENT INDICATES CRACK ON RIGHT WING LEADING EDGE NUMBER 5 SLAT AT OUTBOARD RIB INBOARD LEG MARKED. REMOVED AND REPLACED RIB PER SRM 57-50-13.

Part: SKIN — DAMAGED (FLAP VANE) · airframe 68,032 hrs · 35,963 cycles

RIGHT WING FLAPS NUMBER 3 FLAP VANE HAS WEAR MARK ON LEADING EDGE. HOT BOND METAL DOUBLER PER SRM 51-70-02.

Part: PAN — CRACKED (FUSELAGE) · airframe 68,032 hrs · 35,963 cycles

TOP AFT CORNER OF RIGHT WINDOW PAN AT STATION 1136 IS CRACKED. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 68,032 hrs · 35,963 cycles

LEFT UPPER AFT WINDOW PAN TAB STATION 1041 CRACKED AT FASTENER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 68,032 hrs · 35,963 cycles

LEFT UPPER AFT WINDOW PAN TAB STATION 1060 CRACKED AT RADIUS. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,324 hrs · 35,568 cycles

EMERGENCY LIGHT INOPERATIVE BETWEEN AFT CABIN LAVATORY. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT CABIN LAVATORY. OPS CHECKS NORMAL.

Part: BATTERY — LOOSE (EMERGENCY LIGHTS) · airframe 63,357 hrs

LGA - EMERGENCY LIGHTS AT AFT LAVATORIES INOPERATIVE. RESEATED BATTERIES IN BATTERY PACKS FOR EMERGENCY LIGHT AT AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - OVERHEAD EMERGENCY LIGHTS AT SEATS 6B TO 7B INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT SEATS 6B TO 7B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (LANDING GEAR)

TUL INFLIGHT - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. SERVICED NOSE LANDING GEAR STRUT PER MAINTENANCE MANUAL 32 21 02 3. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 11D HAS LAMPS MISSING. RELAMPED EMERGENCY LIGHTS AT SEAT 11D SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 11D HAS LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT OVERWING EXIT SIGN INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - LOWER OVERWING EXIT SIGN AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR LOWER OVERWING EMERGENCY EXIT SIGN AT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - LOWER EMERGENCY EXIT SIGN AT 2L DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT 2L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 9D, 14D, AND 26D INOPERATIVE. REPLACED EMERGENCY PATH LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 9D, 14D, AND 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

OVERHEAD EMERGENCY EXIT PATH LIGHTING AT ROWS 28-29 INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT PATH LIGHTING BATTERY AT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DFW TAIL CONE EMERGENCY LIGHTS INOPERATIVE. CLEANED BATTERY CONTACTS B5-28 FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT 22D EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT ASSEMBLY ON SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 18 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 18. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CHAFED (FUSELAGE)

TUL - FOUND STATION 1388 CANT HAS HEAVY CHAFING AT 12:00 POSITION. BLENDED CHAFING AND INSTALLED DOUBLER/TRIPLER. REPAIR PER ESO 80559 DATED 4/25/01. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DFW- DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 8, 9, AND 10 DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY AT SEAT 8, 9 AND 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (TAILCONE)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER TAIL CONE HANDLE INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT ASSEMBLY OVER TAIL CONE HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: SWITCH — DEFECTIVE (E/E COMPT)

DFW - FLT 1946 - DURING CRUISE AT FL370, BOTH PACKS FAILED AT THE SAME TIME. CREW INITIATED AN EMERGENCY DESCENT AND DEPLOYED OXYGEN MASKS. AT FL100 THE AIRCRAFT LEVELED OFF AND THE RIGHT PACK STARTED WORKING AGAIN. LEFT PACK WAS CYCLED AND STARTED TO WORK AGAIN. FLIGHT REMAINED AT FL100 FOR THE REMAINDER OF THE FLIGHT WITH PACKS OPERATING NORMALLY. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT AND LEFT PACK AUTO SHUTOFF RELAYS TO BE FAULTY. REPLACED RIGHT AND LEFT PACK AUTO SHUTOFF RELAYS AND AS A PRECAUTIONARY, REPLACED ENGINE DIFFERENTIAL PRESSURE SWITCHES. AIRCRAFT WAS FLOW ON A FUNCTIONAL FLIGHT TEST AND THE SYSTEM OPERATED NORMALLY. SYSTEM GROUND CHECKED NORMALY OPERATION.

Part: VALVE — LEAKING (RUDDER)

SJC - FLT 1041 - DURING APPROACH TO SJC, HAD HYDRAULIC FLUID LOSS ON RIGHT HAND SYSTEM. THE LANDING GEAR WAS EXTENDED AND BACKED UP WITH THE ALTERNATE GEAR EXTENSION. PRESSURE AND QUANTITY WENT TO ZERO. CREW FOLLOWED THE CHECKLIST AND LANDED AT SJC WITH GEAR DOORS DOWN (WOULD NOT RETRACT). REPLACED PACKING ON RUDDER HYDRAULIC POWER SHUT OFF VALVE. SERVICED RIGHT HAND HYDRAULIC SYSTEM. RAN RIGHT HAND ENGINE AND PERFORMED LEAK CHECK. RUDDER HYDRAULIC SHUT OFF VALVE CHECKS NORMAL FOR SERVICE. CHECKED GEAR DOORS FOR DAMAGE, NO DAMAGE NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SEAT TRACK — CORRODED (BS 1304)

TUL - FOUND CORROSION IN NR 2 SEAT TRACK AT STATION 1304. CORROSION REMOVAL WENT BEYOND LIMITS. REPLACED SEAT TRACK NR 2 FROM STATION 1260 TO 1309 AND SPLICE PER SRM 53-05 FIG 4F. (M)

Part: FRAME — CORRODED (BS 168)

TUL - CUSP FRAME AT STATION 168 HAS CORROSION, JUST FORWARD OF FORWARD SERVICE DOOR AT CABIN FLOOR LEVEL. REMOVED CORROSION PER SRM 53-10-3. INSTALLED DOUBLER AFTER TREATING AND PRIMING PER SRM 53-20-00-14. (M)

Part: CUSP — CORRODED (BS 598-693)

TUL - FOUND CORROSION ON CUSP AT STATIONS 598 TO STATION 693, REF E58-4, NR 75480, 75481, 75482 AND 75483. DOUBLER REPAIR INSTALLED IAW ESO 80559, DATED 2-3-97. (M)

Part: B-NUT — LOOSE (RUDDER ACTUATOR)

DFW - FLT 1532 - AFTER TAKEOFF ABQ, DURING INITIAL CLIMB-OUT, STRONG BURNING ODOR BRIEFLY NOTED IN CABIN. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED DFW, LANDING WITHOUT INCIDENT. RESECURED B-NUT FOUND LEAKING ON RUDDER ACTUATOR. REPLACED ALL AIR CYCLE MACHINE COALESCER BAGS AND ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. (M)