N570AA

Part: BATTERY PACK — FAULTY (CABIN) · airframe 87,509 hrs · 39,830 cycles

AB5-3 EGRESS LIGHT POWER SUPPLY FAILS TO TEST WHILE PERFORMING WC 5403. R & R AB5-3 EGRESS LIGHT POWER SUPPLY BATTERY PACK IAW AMM 33-60-98. TESTED OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,509 hrs · 39,830 cycles

AFT INTERIOR OVERWING EXIT SIGNS FAILED TO TEST WHILE PERFORMING WC 0801. R & R B5-105 BATTERY PACK IAW AMM 33-53-00. TESTED OK.

Part: SPAR CAP — CRACKED (LT WING) · airframe 84,500 hrs · 38,143 cycles

CRACK INDICATION FOUND ON LT WING REAR SPAR LOWER CAP AT STATION XRS 164. INSTALLED NEW AFT SPAR & SPLICE DOUBLERS.

Part: FORMER — CRACKED (LE SLAT) · airframe 84,322 hrs · 38,043 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-06.

Part: FORMER — CRACKED (LE SLAT) · airframe 84,322 hrs · 38,043 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-05.

Part: FAN — FAULTY (ZONE 100) · airframe 83,236 hrs · 37,491 cycles

DFW CREW REPORTED A STRONG ELEC ODOR THROUGHOUT THE ENTIRE ACFT. ACCOMPLISHED SMOKE, FIRE & FUMES CHECKLIST, NO HELP. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT RECIRCULATION FAN. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: DOOR SEAL — OUT OF POSITION (CARGO DOOR) · airframe 82,339 hrs · 37,036 cycles

GDL AFT CARGO DOOR AIR LEAK. FLIGHT RETURNED GDL LANDED WITHOUT INCIDENT. REPOSITIONED AFT CARGO DOOR SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 80,329 hrs · 35,991 cycles

DFW - CREW REPORTED PRESSURIZATION PROBLEM DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CABIN PRESSURE OUTFLOW VALVE ACTUATOR AND GEARBOX. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,329 hrs · 35,991 cycles

CORROSION ON CUSP, INBOARD OF SEAT TRACK NUMBER 5 FROM STATIONS 1022 TO 1035 RIGHT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,329 hrs · 35,991 cycles

CUSP SHEET CORRODED OUTBOARD OF NUMBER 6 SEAT TRACK, FROM STATIONS 807 TO 814. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

CUSP SHEET HAS ELONGATED HOLES FROM STATIONS 1227 TO 1250. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

CUSP HAS ELONGATED HOLES FROM STATIONS 1250 TO 1309 LEFT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,329 hrs · 35,991 cycles

CORROSION ON CUSP INBOARD OF NUMBER 5 SEAT TRACK, STATIONS 1022 TO 1035 RIGHT. INSTALLED CUSP DOUBLER ON RIGHT CUSP FROM STATIONS 1022 TO 1035 PER AARD 53-20-00-16.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

DENT AT STATION 426 BELOW LONGERON 19 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-02, FIGURE 2, SHEET 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

DENT AND GOUGE IN FUSELAGE SKIN AT STATION 1304 BETWEEN LONGERONS 18 AND 19 RIGHT SIDE. INSTALLED INTERNAL REPAIR DOUBLER FOR DAMAGED AREA PER SRM 53-04-02 AND TITANIUM SCUFF PLATE REPAIR PER AARD 53-30-00-8.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,329 hrs · 35,991 cycles

INTERCOSTAL HAS CORROSION FROM STATIONS 788 TO 807, LONGERON 19 RIGHT. REMOVED AND INSTALLED SERVICEABLE INTERCOSTAL PER AARD 51-00-05-1.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

CORROSION BLEND OUT OF LIMITS UNDER LEFT ALT STATIC PORT DOUBLER. CUT OUT CORROSION AND INSTALLED FLUSH SKIN REPAIR PANEL PER SRM 53-04-00 FIGURE 12C.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

LONGERON 3 LEFT, CRACKED AT FASTENER, STATION 160, OUTBOARD SIDE. ACCOMPLISHED LONGERON SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,329 hrs · 35,991 cycles

SUBFLOOR CORRODED FROM STATIONS 200 TO 218 OUTBOARD OF T-ANGLE RIGHT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

STATIC BURN FOUND AT STATION 266, LONGERON 7 RIGHT. INSTALLED INTERNAL REPAIR DOUBLER AND SKIN PLUG AS PER SRM 53-04-02 FIGURE 2, SHEET 6.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,329 hrs · 35,991 cycles

SUBFLOOR UNDER AFT GIRT BAR FITTING ON AFT SERVICE DOOR HAS CORROSION AROUND HOLE. INSTALLED TITANIUM REPAIR DOUBLER AND FILLER AT LEFT STATION 1169 PER AARD 53-20-00-16.

Part: PAN — GOUGED (CARGO DOOR) · airframe 80,329 hrs · 35,991 cycles

FORWARD CARGO DOOR, FORWARD OUTER DOOR PAN ADJACENT TO NUMBER 5 BEAM FORWARD STOP HAS FASTENER HOLE THAT IS GOUGED/ELONGATED. INSTALLED DOUBLER REPAIR PER AARD 5-2-30-00-1 AND ESO 80174.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,329 hrs · 35,991 cycles

FUSELAGE AFT LAVATORY SERVICE PANEL HAS CORROSION AROUND BOTTOM OF LAVATORY OPENING. INSTALLED REPAIR DOUBLER PER EA MD80-53-028054.

Part: PAN — CRACKED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

CRACK IN RIGHT WINDOW RING PAN AT FORWARD TOP CORNER STATION 888. INSTALLED WINDOW RING PAN DOUBLER AT STATION 888 RIGHT PER AARD 53-10-00-25.

Part: RING — CRACKED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

CRACK IN LEFT WINDOW RING AT STATION 1022. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,329 hrs · 35,991 cycles

DENT WITH GOUGE IN SKIN AT STATION 208 BELOW LONGERON 4 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-02 FIGURE 2.

Part: BATTERY — NOT SEATED (CABIN) · airframe 79,591 hrs · 35,602 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERIES BY ROW 29. OPS CHECK NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,853 hrs · 34,697 cycles

CRACK IN SKIN AT STATION 1475 CANT FRAME. STOP DRILLED ENDS OF CRACK AND INSTALLED EXTERNAL DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 77,853 hrs · 34,697 cycles

SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 LEFT. INSTALLED NEW SHEAR TIE AFT SIDE OF 1451 AFT OF LONGERON 2 LEFT PER AARD 51-10-00-5.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 76,798 hrs · 34,132 cycles

DFW - CREW REPORTED LEFT HYDRAULIC SYSTEM PRESSURE ZERO. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE HYDRAULIC PUMP THAT WAS BAD AND FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,700 hrs · 32,206 cycles

FIRST CLASS EMERGENCY LIGHTS IN GALLEY AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,700 hrs · 32,206 cycles

OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 9 TO 13 INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,519 hrs · 31,679 cycles

STL - EMERGENCY EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EGRESS LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,519 hrs · 31,679 cycles

STL - EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,519 hrs · 31,679 cycles

STL - EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,519 hrs · 31,679 cycles

STL - EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,519 hrs · 31,679 cycles

STL - EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,519 hrs · 31,679 cycles

STL - EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,519 hrs · 31,679 cycles

STL - EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,519 hrs · 31,679 cycles

STL - EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 71,378 hrs · 31,612 cycles

EMERGENCY EXIT LIGHT AT SEAT 24D INOPERATIVE. RECONNECTED SEAT TO WALL CONNECTOR AT SEAT 24D, OPS GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 70,823 hrs · 31,385 cycles

IAD - CREW REPORTED SMOKE IN AFT CABIN. EMERGENCY DECLARED RETURNED IAD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ON GROUND COULD NOT DUPLICATE. PERFORMED PNEUMATIC DUCTING BURNOUT PER MCM 21-92-12. NO DISCREPANCIES NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 70,291 hrs

SFO - MID CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR MID CABIN OVERHEAD EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,930 hrs

SFO- EMERGENCY LIGHTS FOR ROW 13 THRU ROW 17 WOULD NOT TURN OFF WHEN POWER IS SHUTDOWN. REPLACED BATTERY PACK FOR ROWS 13 THRU 17.

Part: SUPPORT — CRACKED (NLG DOOR) · airframe 69,155 hrs · 30,709 cycles

CRACK FOUND ON LEFT NOSE LANDING GEAR DOOR FORWARD HINGE SUPPORT ARM. CRACK LENGTH IS .025 INCH. REPLACED SUPPORT ARM AND DOOR RIGGED IN ACCORDANCE WITH MM 32 22 01 2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION ON CUSP ANGLE TANG AT STATION 168. AREA OF DISCREPANCY IS 10 INCHES BY 5 INCHES. REPAIRED CUSP ANGLE IN ACCORDANCE WITH ESO 80559 DATED 03 OCTOBER 2008.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON HORIZONTAL STABILIZER RIGHT OUTBOARD INBOARD HINGE PLATE LUG NUMBER 3. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED RIGHT OUTBOARD INBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON SUB FLOOR INBOARD OF FORWARD SERVICE DOOR. AREA OF DISCREPANCY IS 10 INCHES BY 10 INCHES. REMOVED DAMAGE AND INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53 20 00 16.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON BALL FRAME AT STATION 1309 LONGERON 30. AREA OF DISCREPANCY WAS 12 INCHES BY 2 INCHES. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53 10 00 17 AND ESO 80559 DATED 01 OCT 2008.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON HORIZONTAL STABILIZER LEFT OUTBOARD HINGE PLATE LUG NUMBER 1. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED LEFT OUTBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON HORIZONTAL STABILIZER RIGHT OUTBOARD HINGE PLATE LUG NUMBER 4. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED RIGHT OUTBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON HORIZONTAL STABILIZER LEFT OUTBOARD INBOARD HINGE PLATE LUG NUMBER 2. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED LEFT OUTBOARD INBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON HORIZONTAL STABILIZER LEFT INBOARD OUTBOARD HINGE PLATE LUG NUMBER 3. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED LEFT INBOARD OUTBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,155 hrs · 30,709 cycles

CRACK FOUND ON LONGERON 4 LEFT BETWEEN STATIONS 170 AND 228. CRACK LENGTH WAS 60 INCHES. ACCOMPLISHED SPLICE REPAIR IN ACCORDANCE WITH SRM 53 02 00.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON HORIZONTAL STABILIZER RIGHT INBOARD OUTBOARD HINGE PLATE LUG NUMBER 2. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED RIGHT INBOARD OUTBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON HORIZONTAL STABILIZER LEFT INBOARD HINGE PLATE LUG NUMBER 4. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED LEFT INBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON RIGHT TIE DOWN TRACK IN AFT CARGO. AREA OF DISCREPANCY IS 3 INCHES BY 111 INCHES. REPLACED RIGHT TIE DOWN TRACK IN ACCORDANCE WITH SRM 51 10 3.

Part: HINGE FITTING — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON HORIZONTAL STABILIZER RIGHT INBOARD HINGE PLATE LUG NUMBER 1. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED RIGHT INBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05.

Part: LONGERON — CRACKED (ZONE 200) · airframe 69,155 hrs · 30,709 cycles

CRACK FOUND ON LONGERON 2 LEFT AT STATION 160. CRACK LENGTH WAS 1 INCH. REPLACED LONGERON SECTION BETWEEN STATIONS 148 AND 170 IN ACCORDANCE WITH SRM 53-02-00.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION ON LEFT TIE DOWN TRACK SPLICE AT AFT CARGO. AREA OF DISCREPANCY IS 1 INCH BY 6 INCHES. REPLACED LEFT TIE DOWN TRACK SPLICE IN ACCORDANCE WITH SRM 51 10 1.

Part: LONGERON — CRACKED (ZONE 200) · airframe 69,155 hrs · 30,709 cycles

CRACK FOUND ON LONGERON 3 LEFT AT STATION 160. LENGTH OF CRACK WAS .025 INCH. REPLACED APPROXIMATELY A 22 INCH SECTION OF LONGERON FROM STATION 148 TO 170 IN ACCORDANCE WITH SRM 53-02-00 FIGURE 18.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON MID CARGO DOOR BEAM. AREA OF DISCREPANCY IS 3 INCHES BY 12 INCHES WITH AT DEPTH OF .112 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53 10 00 3.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON MID CARGO DOOR BEAM. AREA OF DISCREPANCY WAS 3 INCHES BY 12 INCHES WITH A DEPTH OF .113 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 51 10 00 5.

Part: CUSP WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON BOTTOM SIDE OF RIGHT CUSP AT MID CARGO. AREA OF DISCREPANCY WAS 11.5 INCHES BY 3.5 INCHES. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-20-00-16.

Part: SKIN — CRACKED (BS 1380) · airframe 69,155 hrs · 30,709 cycles

CRACK FOUND IN AIRCRAFT SKIN ABOVE LEFT ENGINE PYLON. CRACK LENGTH 2/32 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-30-00-02.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON LEFT FLOOR TIE DOWN TRACK IN AFT CARGO. AREA OF DISCREPANCY WAS 8 FEET BY 4 INCHES. REPLACED LEFT TIE DOWN TRACK IN ACCORDANCE WITH SRM 51-10-1.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON AFT CARGO FLOORBOARD SUPPORT AT TOP. AREA OF DISCREPANCY WAS 57 INCHES BY 2 INCHES. REPLACED FLOORBOARD SUPPORT IN ACCORDANCE WITH SRM 51-10-1.

Part: CUSP WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON RIGHT CUSP MEMBRANE BETWEEN STATIONS 484 AND 503. AREA OF DISCREPANCY WAS 3 INCHES BY 15 INCHES. INSTALLED DOUBLER REPAIR ON RIGHT CUSP AT STATION 495 TO 502 IN ACCORDANCE WITH AARD 53-20-00-16.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON INTERCOSTAL BETWEEN LEFT STATIONS 1309 AND 1322. AREA OF DISCREPANCY IS 12 INCHES BY 6 INCHES. REPLACED INTERCOSTAL IN ACCORDANCE WITH SRM 51-10-1.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON SEAT TRACK 4. REPAIRED SEAT TRACK 4 PER AARD 53-20-00-10.

Part: FITTING — CORRODED (ZONE 900) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON GALLEY NUMBER TWO TIE DOWN FITTING INBOARD OF SEAT TRACK NR 4. AREA OF DISCREPANCY WAS 3 INCHES BY 1 INCH. REPLACED TIE DOWN FITTING IN ACCORDANCE WITH SRM 51-01.

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON FORWARD GIRT BAR SUPPORT BRACKET AT AFT SERVICE DOOR AT LONGERON 18 LEFT. AREA OF DISCREPANCY WAS THREE INCHES BY THREE INCHES. INSTALLED NEW FITTING IN ACCORDANCE WITH SRM 51-01.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON MOUNT AT GALLEY NUMBER TWO. AREA OF DISCREPANCY IS 1.5 INCHES WIDE BY 5 INCHES LONG. INSTALLED MOUNT IN ACCORDANCE WITH SRM 51-01.

Part: BRACKET — CORRODED (GIRT BAR) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION ON AFT GIRT BAR SUPPORT AT AFT SERVICE DOOR. INSTALLED NEW FITTING IN ACCORDANCE WITH SRM 51 01.

Part: TAB — CRACKED (DOOR FRAME) · airframe 69,155 hrs · 30,709 cycles

CRACK FOUND ON TAB ON FORWARD ENTRY DOOR JAMB STRAP AT LONGERON 11 LEFT. AREA OF DISCREPANCY IS ONE INCH BY ONE INCH. CRACK LENGTH IS 0.5 INCH. INSTALLED REPAIR STRAP OVER CUT OUT OF DAMAGED TAB IN ACCORDANCE WITH AARD 53-10-00-11.

Part: PAN — CRACKED (ZONE 200) · airframe 69,155 hrs · 30,709 cycles

FOUND WINDOW CRACKED AT FORWARD LOWER WINDOW AT RIGHT STATION 845. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH AARD 53 10 00 25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,155 hrs · 30,709 cycles

CORROSION FOUND ON NR 5 SEAT TRACK. AREA OF DISCREPANCY WAS 3 INCHES BY 2 INCHES. INSTALLED SEAT TRACK PLUG IAW SRM 53-05-00 FIGURE 4A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

ATL - EMERGENCY LIGHTS IN COCKPIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 4E INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 14 TO 17 INOPERATIVE. REPLACED BATTERY PACK AT STATION 515 FOR INOPERATIVE OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 14 TO 17. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT LIGHT IN OVERHEAD TAILCONE INOPERATIVE. REPLACED BATTERIES AND BULBS FOR EMERGENCY EXIT LIGHT IN OVERHEAD TAILCONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - OVERHEAD EMERGENCY EXIT LIGHT IN AFT CABIN BETWEEN LAVATORIES INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR OVERHEAD EMERGENCY EXIT LIGHT IN AFT CABIN BETWEEN LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - MOST EMERGENCY ESCAPE PATH LIGHTS IN CABIN INOPERATIVE. REPLACED FORWARD AND MID BATTERY PACKS FOR EMERGENCY ESCAPE PATH LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

BOS - DURING CHECK FOUND EMERGENCY LIGHTS FROM FIRST CLASS BACK TO ROW 24 INOPERATIVE. REPLACED FIRST CLASS CHARGER AND THREE BATTERY PACKS FOR EMERGENCY LIGHTS FROM FIRST CLASS BACK TO ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

ORD - FORWARD PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD PORTABLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

TPA EMERGENCY CEILING LIGHT BETWEEN AFT LAVATORY AND EMERGENCY LIGHT AT TAIL CONE INOPERATIVE. REPLACED BATTERY PACK B5 THROUGH 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

BOS LT AFT STAIRWELL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR LEFT AFT STAIRWELL EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

MAINTENANCE OBSERVED SEAT MOUNTED ESCAPE PATH LIGHT INOPERATIVE AT SEAT 18D. REPLACED WIRE HARNESS AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT)

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

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING OVERNIGHT MAINTENANCE, FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD OVERWING EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: CONTACTOR — DIRTY (BATTERY)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 18B, 20B, AND 20D INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN SEAT TRACK SUPPORT AFT NR 4 TRACK FS 927. REMOVED CRACKED SEAT TRACK SUPPORT AND INSTALLED NEW SUPPORT SRM 51-01 PAGE 1. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP CORRODED RIGHT STATION 1080. CUT OUT CORROSION, CUSP DOUBLER INSTALLED AS PER SRM 53-01 FIG 4 SHT 3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP CORRODED RIGHT STATION 635. INSTALLED DOUBLER PER SRM 53-01. (M)

Part: LONGERON — DAMAGED (FUSELAGE)

TUL - FOUND LONGERON 28R AT STATION 320 IS DAMAGED INBOARD SIDE OF LONGERON CHANNEL IS BENT DOWNWARD. REPAIRED AREA PER SRM 53-02 PAGE 48-53, FIG 18 SHEET 1. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND SEAT TRACK NR 5 CORRODED AT STATION 237. REMOVED SECTION AND INSTALLED NEW SECTION WITH SPLICE PER SRM 53-05 PART 1 FIG 4F. (M)

Part: LONGERON — DAMAGED (FUSELAGE)

TUL - FOUND LONGERON 29R AT STATION 320 IS DAMAGED, INBOARD SIDE OF LONGERON CHANNEL IS BENT DOWNWARD. REPAIRED AREA PER SRM 53-02, PAGES 48-53, FIG 18, SHT V. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON ABOVE FORWARD ENTRY DOOR STATION 168 CRACKED. REPAIRED LONGERON PER SRM 53-02, PAGE 48, FIG 18 SHEET 1. (M)

Part: CARGO TRACK — CORRODED (AFT CARGO BAY)

TUL - FOUND LIGHT CORROSION ON RIGHT CARGO TIE DOWN TRACK STATION 1250-1287, AROUND ALL FASTENERS LENGTH OF TRACK. INSTALLED NEW TIE DOWN TRACK PER SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP CORRODED TOP SIDE, STATION 522-528. REPAIRED CORROSION AREA PER AARD 53-00-00-02. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CUSP PANEL CORRODED JUST ABOVE MID CX DOOR AFT HINGE BRACKETS AT STATION 674 AND 686 RIGHT SIDE. REPAIRED PER SRM 53-01, INSTALLED DOUBLER. (M)

Part: WIRE — BROKEN (AFT AIRSTAIR)

DFW - DURING OVER-NIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON AFT AIRSTAIR INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

DFW - FLT 2323 - AFTER NORMAL GEAR RETRACTION ON CLIMB-OUT PASSING THROUGH APPROXIMATELY FL 180 AFTER INITIALLY CONFIRMED NOSE RED LIGHT OUT, NOTICED NOSE GEAR RED LIGHT ON WITH HYDRAULIC PUMPS IN LOW. RAN ABNORMAL PROCEDURE AND LIGHT SENT OUT. EXTENSION AND ALL ASSOCIATED LIGHTS WERE NORMAL ON APPROACH. LANDED DFW WITHOUT INCIDENT. RETRACTED NOSE GEAR AND DEPRESSURIZED HYDRAULIC SYSTEM FOR APPROXIMATELY ONE-HALF HOUR. NOSE GEAR RED LIGHT REMAINED OUT, BOTH NOSE GEAR PROXIMITY SENSORS NORMAL AT PSEU DURING GEAR SWING. NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: BRACKET — CRACKED (MLG PROX SENSOR)

ORD - FT 1560 - AMBER GEAR DOOR OPEN LIGHT ILLUMINATED DURING HIGH SPEED DESCENT. RED GEAR UNSAFE LIGHTS ALSO ILLUMINATED. SLOWED AIRCRAFT BOTH LIGHTS EXTINGUISHED. LANDED ORD WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR AND BRACKET ON LEFT GEAR DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND NR 1 SEAT TRACK CORRODED AND GOUGED STATION 671-673. INSTALLED PLUG REPAIR PER SRM 53-05 PART 1 FIG 4A. (M)

Part: CONNECTOR — LOOSE (TAIL COMPARTMENT)

ORD - DURING OVERNIGHT MAINTENANCE, WARNING LIGHT ON OVERHEAD PANEL IN COCKPIT FAILED TO ILLUMINATE DURING TAIL CONE JETTISION CHECK. RESEATED CONNECTORS ON TAIL CONE SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOUBLER — CORRODED (BS 1155-1210)

TUL - FOUND CORROSION ON SILL/PLATE ON BOTTOM OF AFT CARGO DOOR FRAME. INSTALLED DOUBLER IAW AARD 53-10-00-3. (M)

Part: TRACK — CORRODED (BS 1119)

TUL - FOUND CORROSION AROUND FASTENERS ON TIE DOWN TRACK AT STATION 1119 BETWEEN L27R TO L28R, (RT TIE DOWN TRACK). INSTALLED NEW TIE DOWN TRACK PER SRM 51. (M)