N474

Part: OIL FILTER — CLOGGED (OIL SYSTEM) · airframe 75,494 hrs · 40,086 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH RT ENG OIL STRAINER CLOG LIGHT ILLUMINATED. REDUCED POWER IAW QRH & LANDED. R & R OIL FILTER IAW AMM 71-91-12. NO DEFECTS NOTED. PERFORMED LEAK CHECK, SYS CHECKED GOOD.

Part: FORMER — CRACKED (LE SLAT) · airframe 75,310 hrs · 39,973 cycles

RIGHT WING LE NR 4 SLAT TRACK LE INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 SLAT TRACK LE INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-06 & EA MD80-57-037112.

Part: FORMER — CRACKED (LE SLAT) · airframe 75,310 hrs · 39,973 cycles

LEFT WING LE NR 4 SLAT TRACK LE INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 SLAT TRACK LE INBD FORMER DOUBLER & HAT BUSHING IAW WORK CARD 57-98-05 & EA MD80-57-037112.

Part: TIRE — SEPARATED (LT MLG) · airframe 75,220 hrs · 39,915 cycles

NUMBER 1 TIRE TREAD SEPARATED & CAUSED DAMAGE TO THE LT INBD FLAP & POSSIBLE ENG INGESTION. EMER DECLARED FLIGHT REMOVED ACFT FROM SERVICE. REPLACED LT INBD FLAP MPN 5930479513 & LT ENG N1 BLADES. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 72,909 hrs · 38,588 cycles

GOUGE BELOW LT FWD LAVATORY SERVICE DOOR. FABRICATED & INSTALLED DOUBLER IAW SRM 53-04-05 & EA MD80-53-032568.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,498 hrs · 37,754 cycles

1485 CANT FRAME CRACKED BELOW STAIR RETENTION ACTUATOR. INSTALLED DOUBLER IAW AARD 53-10-00-33.

Part: CASTING — CRACKED (RT SPOILER) · airframe 71,498 hrs · 37,754 cycles

RIGHT WING GROUND SPOILER CASTING CRACKED. REPLACED CASTING IAW AARD 51-00-05-1.

Part: SHUTOFF VALVE — LEAKING (ZONE 200) · airframe 70,856 hrs · 37,383 cycles

DFW - CREW REPORTED RIGHT HYDRAULIC SYSTEM QUANTITY LOSS. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. DETERMINED A LARGE LEAK IN THE TAIL AREA. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT SYSTEM SPOILER ROTARY GROUND SHUT OFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: O-RING — DEFECTIVE (AC BAY) · airframe 70,076 hrs · 36,953 cycles

LAX - CREW REPORTED ON CLIMBOUT RIGHT PACK FAILED WITH LEFT PACK ON PLACARD FOLLOWED BY TAIL COMPARTMENT HIGH TEMPERATURE LIGHT. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED O-RING AND INSTALLED DUCT CLAMP ON RIGHT WATER SEPARATOR ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 68,422 hrs · 35,994 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT LEFT NUMBER 1 DOOR. OPS CHECKS NORMAL.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

AFT CARGO DOOR JAMB BEAM STATIONS 1155 TO 1212 CORRODED. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: DOUBLER — DEFECTIVE (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

LEFT ALTERNATE STATIC PORT HAS INTERNAL DOUBLER THAT FAILED WAVINESS INSPECTION. INSTALLED DOUBLER PER SRM 53-04-2 AND SG0953001.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

STATIONS 826 TO 845, 5/16 INCH GAP BETWEEN NUMBER 1 SEAT TRACK AND CUSP. INSTALLED NEW LEFT CUSP SHEET FROM STATIONS 807 TO 845 PER AARD 51-10-00-5.

Part: TEE FITTING — DAMAGED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

AT APPROXIMATE STATION 836, LEFT CUSP TEE HORIZONTAL FLANGE BENT AT CUSP SHEET TO CUSP TEE FASTENER HOLE. INSTALLED NEW SECTION OF LEFT CUSP TEE STATIONS 826 TO 845 AARD 51-10-00-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

OUTBOARD SIDE OF LONGERON IS CRACKED AT STATION 160 LONGERON 2 LEFT. REPAIRED LONGERON PER SRM 53-02-00 FIGURE 18.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

AFT CARGO, LOWER DOOR BEAM VERTICAL AND HORIZONTAL LEG HAS CORROSION, STATIONS 1155 TO 1212. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR AS PER AARD 53-10-00-3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

RIGHT SIDE SHEAR TIE IS CRACKED FORWARD SIDE OF FRAME 1380 ABOVE LONGERON 14 RIGHT. INSTALLED DOUBLER ON SHEAR TIE AT STATION 1380 LONGERON 14 RIGHT PER AARD 53-10-00-20.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

GALLEY MOUNT CORROSION AT STATION 160 RIGHT BUTTLINE 11. REPLACED MOUNT PER AARD 51-10-00-5.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

CORROSION ON SUB-FLOOR AT STATION 199, 4 INCHES INBOARD OF FORWARD SERVICE DOOR JAMB. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

CORROSION ON CUSP UNDER NUMBER 6 SEAT TRACK AT STATIONS 237 TO 242. REPAIRED CUSP PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

FORWARD OUTBOARD G2 GALLEY MOUNT CORRODED AT STATION 215 RIGHT BUTTLINE 56. INSTALLED NEW MOUNT PER AARD 51-10-00-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

INTERCOSTAL BETWEEN LONGERONS 28 AND 27 RIGHT AT STATIONS 237 TO 218 IS CRACKED. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-5.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

FORWARD LEFT SUBFLOOR HAS DAMAGED HOLES BELOW FLOORBOARD SUPPORT STATIONS 162 TO 196 LEFT BUTTLINE 55. REPAIRED SUBFLOOR PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

GALLEY MOUNT HAS CORROSION AT STATION 160 RIGHT BUTTLINE 11. INSTALLED NEW MOUNT PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

CORROSION ON CUSP UNDER NUMBER 6 SEAT TRACK AT STATION 256. REPAIRED CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

CUSP SHEET ON LEFT AROUND STATION 840 IS CORRODED. REPAIRED CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

RIGHT CUSP AT STATION 163 RIGHT BUTTLINE 12 DAMAGED. REPAIRED CUSP PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

CORROSION ON SUB-FLOOR AT STATION 200, 2 INCHES INBOARD OF FORWARD SERVICE DOOR JAMB. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-14.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

CORROSION ON CUSP TEE STATION 200, INBOARD OF FORWARD SERVICE DOOR. REPAIRED CUSP TEE PER AARD 53-20-00-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

NUMBER 6 SEAT TRACK CORRODED AT STATIONS 214 TO 227. REPAIRED SEAT TRACK PER SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

CRACK ON LEFT CUSP AT STATION 220 AT LIGHTENING HOLE EXTENDING INBOARD. INSTALLED NEW LEFT CUSP FROM STATIONS 218 TO 237 PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,847 hrs · 35,682 cycles

CABIN HAS BULGE IN RIGHT CUSP AT STATION 1308. INSTALLED NEW RIGHT CUSP SHEET STATIONS 1250 TO 1309 PER AARD 51-10-00-5.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

CORROSION ON SUBFLOOR UNDER G-1 GALLEY DRAIN PAN. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — BENT (CARGO DOOR) · airframe 67,847 hrs · 35,682 cycles

AFT CARGO DOOR UPPER EDGE OF DOOR SKIN BENT. INSTALLED REPAIR DOUBLER ON UPPER EDGE OF DOOR SKIN PER ESO 80186.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

WINDOW FRAME, TOP FORWARD TAB HAS CRACK AT STATION 886 ON RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 67,847 hrs · 35,682 cycles

WINDOW FRAME, FORWARD BOTTOM TAB HAS CRACK AT STATION 1098 ON RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,448 hrs · 34,834 cycles

RIGHT CUSP IS CORRODED STATION 559. INSTALLED RIGHT CUSP SHEET STATIONS 503 TO 598 PER AARD 51-10-00-5.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,011 hrs · 32,888 cycles

FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 60,027 hrs · 31,275 cycles

SHEAR TIE CRACKED AT STATION 1451 FRAME AT LONGERON 2 RIGHT. INSTALLED A SERVICEABLE SHEAR TIE PER SRM 53-01.

Part: PLACARD — MISSING (TAILCONE) · airframe 58,505 hrs

LGA - PLACARD AT TAIL CONE OUTER LT EMERGENCY EXIT MISSING. REPLACED PLACARD FOR AT TAIL CONE OUTER LT EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: PLACARD — WORN (TAILCONE) · airframe 58,505 hrs

LGA - PLACARD AT TAIL CONE OUTER EMERGENCY EXIT WORN. REPLACED PLACARD FOR AT TAIL CONE EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 57,530 hrs

MSP - EMERGENCY LIGHT AT SEAT ROW 13 MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,530 hrs

MSP - EMERGENCY LIGHT AT SEAT ROW 10 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,530 hrs

MSP - EMERGENCY LIGHT AT SEAT ROW 13 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 57,530 hrs

MSP - EMERGENCY LIGHT AT SEAT ROW 10 MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (NLG)

ORD INFLIGHT T1349/05FEB - NOSE GEAR RED UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF DURING GEAR RETRACTION. CYCLED LANDING GEAR WITH NO CHANGE. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. PERFORMED NOSE LANDING GEAR STRUT INSPECTION AND SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHT ON CEILING AT LEFT AND RIGHT NUMBER ONE DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT ON CEILING AT LEFT AND RIGHT NUMBER ONE DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 24 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 24 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - FORWARD MOST BLOCK OF CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK NEXT TO FORWARD LAVATORY FOR FORWARD MOST BLOCK OF CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

DEN AFT EMERGENCY LIGHTS IN TAIL INOPERATIVE. REPLACED BATTERY PACK FOR TAIL CONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

SEA - INSEAT EMERGENCY LIGHTS AT OVERWING EXIT INOPERATIVE. REPAIRED WIRING IN AFT TAIL COMPARTMENT FOR INSEAT EMERGENCY LIGHTS AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY IN TAIL CONE INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY FOR TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. REATTACHED EMERGENCY EXIT LIGHT BATTERY FOR TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT ROWS 18 AND 19 INOPERATIVE. REPLACED BATTERY PACK AT BS 104. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DAMAGED (FUSELAGE)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND LEFT SIDE FUSELAGE SKIN DAMAGED BETWEEN STATIC PORTS. REQUIRED MAJOR REPAIR OF AREA BETWEEN CABIN PRESSURE RELIEF VALVES. REPLACED DAMAGE SKIN, ACCOMPLISHED FLUSH REPAIR WITH DOUBLERS. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M)

Part: DUCT — DEFECTIVE (TAIL)

BOS - FLT 1229 - BOS-ORD - AFTER TAKEOFF, TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED. LANDED BOS WITHOUT INCIDENT. REPLACED RUPTURED DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHTS WERE INOPERATIVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS ROWS 12 THROUGH 16 INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (APU BAY)

EWR - FLT 1643 - EN ROUTE LGA-HOU, SHORTLY AFTER TAKEOFF DETECTED SMOKE IN CABIN AND COCKPIT. DIVERTED EWR AND LANDED WITHOUT FURTHER INCIDENT. REPLACED APU. SYSTEM GROUND CHECKS NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: PUMP — FAILED (NR 1 ENGINE)

DFW - FLT 1431 - EN ROUTE DFW-ONT, DETECTED NR 1 ENGINE HYDRAULIC PUMP FAILURE. AIR INTERRUPTED, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 SIDE ENGINE HYDRAULIC PUMP. ACCOMPLISHED LEAK CHECK. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (DOOR WARNING SYS)

ATL - FLT 1572 - DURING APPROACH, SLAT/FLAP HANDLE MOVED TO ZERO DEGREE/EXTERNAL. DISAGREE LIGHT CAME ON. RECYCLED HANDLE AND BOTH SLATS AND LIGHTS NORMAL. LANDED ATL WITHOUT INCIDENT. DURING REFUELING OPERATION, PERSON FUELING NOTICED SPARKS COMING FROM A WIRE BUNDLE OUTBOARD OF FUELING PANEL. REFUEL DOOR HODL OPEN ROD SHORTING SLAT/FLAP WIRES BUNDLE. REPAIRED AND REPOSITIONED BURNED WIRES IN BUNDLE AT REFUEL DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SEAT TRACK — GOUGED (BS 1155)

TUL - NR 4 SEAT TRACK DEEP GOUGE STATION 1155. ROUTED OUT AREA DAMAGED, INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A. (M)

Part: FITTING — WORN (LE FLAP)

TUL - SUPPORT ATTACH FITTING ON OUTBOARD END OF NR 4 LEADING EDGE SLAT HAS EXCESSIVE PLAY. INSTALLED NEW RIB PER SHOP ESO 80117. (M)

Part: SEAT TRACK — CORRODED (BS 1037-1087)

TUL - PITTING CORROSION NR 1 SEAT TRACK, STATION 1054-1056, STATION 1037-1039. INSTALLED NEW SEAT TRACK NR 1 FROM STATION 1032-1087 SRM 53-05 PAGE 4B. (M)

Part: SEAT TRACK — CORRODED (BS 700-793)

TUL - FOUND CORROSION SPOTS STATION 700-793. REPLACED SEAT TRACK FROM STATION 645-797 WITH SPLICE AT STATION 645 PER SRM 53-05 FIG 4F. (M)

Part: SKIN — DAMAGED (BS 351)

TUL - DENT WITH CREASE STATION 351 BELOW L23R. CUT DAMAGED AREA OUT. INSTALLED DOUBLER PER SRM 53-04. (M)

Part: SKIN — DAMAGED (BS 360)

TUL - AIRCRAFT DAMAGE RIGHT FUSELAGE STATION 351-370 FORWARD CARGO DOOR, BETWEEN L22R-L23R. REMOVED OLD TEMP, INSTALLED NEW DOUBLER PER SRM 53-04 FIG 12B NR 8. (M)

Part: SKIN — DENTED (BS 446)

TUL - DENT 3 INCH BY 1.5 INCH FORWARD LEFT ALT STATIC PORT 4.5 INCHES BELOW AND 10 INCHES FORWARD ALT PORT STATION 446 BETWEEN LONGER 23L AND 24L. REWORKED DENT, INSTALLED DOUBLER SRM 53-04, FIG 12B NR 8. (M)

Part: WEB — CORRODED (BS 1155)

TUL - LEFT FLOOR CUSP HAS SMALL AREA OF CORROSION AROUND NUT PLATE, 12 INCHES INBOARD FROM AFT GALLEY DOOR SILL. INSTALLED DOUBLER ON CUSP PER SRM 53-01. (M)

Part: SEAT TRACK — CORRODED (BS 823-1022)

TUL - PITTING CORROSION IN NR 1 SEAT TRACK INSIDE AND FLANGES AT BS 823-826, 892-896, 910-914, 994-995, AND 1022-1023. INSTALLED NEW SEAT TRACK NR 1 FROM STATION 823 TO STATION 1022 SRM 53-05 PAGE 4B. (M)

Part: SEAT TRACK — CORRODED (BS 1202-1204)

TUL - PITTING CORROSION ON NR 3 SEAT TRACK INSIDE AND ON FLANGES, STATION 1202-1204. REMOVED SECTION OF SEAT TRACK FROM STATION 1170 TO 1221 AND INSTALLED NEW SECTION PER SRM 53-05 FIG 4 PAGE 5. (M)

Part: SEAT TRACK — GOUGED (BS 1155)

TUL - FOUND NR 4 SEAT TRACK DEEP GOUGE STATION 1155. ROUTED OUT DAMAGED AREA AND INSTALLED SEAT TRACK PLUG PER SRM 53-05-08 FIG 4A. (M)

Part: GALLEY TRACK — CORRODED (BS 218)

TUL - GALLEY TIE DOWN FLOOR FITTING CORRODED BELOW SUBFLOOR. REMOVED AND REPLACED GALLEY TIE DOWN FITTING PER SRM 51-01. (M)

Part: SKIN — CRACKED (BS 380)

TUL - TWO CRACKS IN FUSELAGE SKIN AT STATION 380 ANTENNA ATTACHMENT AT 6 O'CLOCK POSITION, STRINGER 30, STATION 380. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-04. (M)

Part: COFFEE MAKER — ODOR (GALLEY)

LIT - FLT 0826 - EN ROUTE IAH/ORD DURING CRUISE, FLIGHT ATTENDANT NOTED AN ELECTRICAL SMELL IN THE FIRST CLASS GALLEY AREA. AIRCRAFT LANDED LIT WITHOUT INCIDENT. GALLEY COFFEE MAKERS AND OVENS WERE PLACARDED AND THE AIRCRAFT FERRIED TO ORD FOR FURTHER EVALUATION. MAINTENANCE OPERATED FIRST CLASS OVENS AND COFFEE MAKERS FOR ONE HOUR UNABLE TO DUPLICATE ELECTRICAL SMELL. AS A PRECAUTION, BOTH COFFEE MAKERS WERE CHANGED. SYSTEM GROUND CHECKED, NORMAL OPERATION WITH NO SMOKE NOTED. (X)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 3 AND 6 INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 3 AND 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DFG CONTROL PNL — DEFECTIVE (COCKPIT)

MIA - FLT 214 - WHILE CLIMBING THROUGH 29,000 FEET AT MACH .74. AIRCRAFT YAWED LEFT THEN RIGHT DUTCH ROLL. AUTO THROTTLE AND AUTO PILOT TRIPPED OFF. MANUALLY FLY REQUIRED IMMEDIATE INPUT OF 3 TO 4 DEGREE LEFT RUDDER TRIM WAS REQUIRED. ALTITUDE SET WINDOW BLANK, ACCOMPLISHED CHECKLIST, FOUND DIGITAL FLIGHT GUIDANCE C-17 CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER, NO CHANGE. LANDED MIA WITHOUT FURTHER INCIDENT. PERFORMED FLIGHT FAULT REVIEW, TROUBLE SHOT TO DFW CONTROL PANEL. REPLACED DFG CONTROL PANEL SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ENGINE — DEFECTIVE (RIGHT)

IAD - FLT 217 - ON TAKEOFF FROM DCA, RIGHT ENGINE EGT INCREASED GRADUALLY TO APPROXIMATELY 40 DEGREES CENTIGRADE HIGHER THAN LEFT ENGINE WITH ALL OTHER ENGINE PARAMETERS NORMAL. DURING CLIMB-OUT, TRAILING AIRCRAFT REPORTED NOTING SPARKS IN EXHAUST FROM RIGHT ENGINE. FLIGHT CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO IAD WITH RIGHT ENGINE STILL OPERATING. AIRCRAFT LANDED IAD WITHOUT INCIDENT. REPLACED RIGHT ENGINE. ACCOMPLISHED LEAK CHECKS AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

MIA - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPAIRED SPLICE IN EMERGENCY EXIT FLOOR PATH LIGHTING WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL WIRE — CORRODED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE BY FORWARD LAVATORY. REPLACED CORRODED SECTION OF WIRING HARNESS. SYSTEM GROUND CHECKED NORMAL. (M)