N6823

Part: LIGHT — DEFECTIVE (L1 DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER L1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT OVER L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — TORN (BS 625)

TUL - FOUND 8 INCH DIAGONAL TEAR IN SKIN STATION 625 JUST ABOVE STRINGER 26R, THROUGH SKIN AND BEARSTRAP AT LAP SPLICE. REPAIRED WITH QUADRUPLER PER INTERIM REPAIR ESO 11697 DATED 10-21-98, REPAIRED 26R CUTOUT DAMAGE INSTALLED REPAIR SPLICE PER 51-40-4. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, RIGHT AFT CARGO DOOR EMERGENCY LIGHTS ILLUMINATED WHEN ALL POWER WAS REMOVED FROM THE AIRCRAFT. LIGHTS WENT OUT WHEN POWER WAS APPLIED. DURING TROUBLESHOOTING, COULD NOT DUPLICATE PROBLEM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: UNIT — DEFECTIVE (E/E COMPT)

DFW - FLT 885 - DURING TAKEOFF ATL-DFW WHEN LANDING GEAR RETRACTED, GEAR DID NOT RETRACT. OVERRIDE TRIGGER WAS USED AND GEAR RETRACTED NORMALLY. ABNORMAL PROCEDURES FOLLOWED FOR ENTIRE FLIGHT AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED LANDING GEAR ASSY UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CLAMP — LOOSE (NR 3 ENGINE)

MIA - FLT 0448 - AFTER TAKEOFF MIA DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. AIRCRAFT AIR INTERRUPTED MIA AND LANDED WITHOUT INCIDENT. NR 3 ENGINE BLEED CLAMPS RE-TORQUED. RAN NR 3 ENGINE AT IDLE POWER WITH NO LEAKS OR OVERHEAT INDICATIONS. RE-INSTALLED NR 3 ENGINE STRUT PANEL, RAN ENGINE AT POWER FOR 3 MINUTES. SYSTEM LEAK AND GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

RDU - DURING OVERNIGHT MAINTENANCE, FOUND THE AFT RIGHT HAND CABIN FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT SEALS BROKEN. REPLACED SEALS ON AFT RIGHT HAND CABIN FLIGHT ATTENDANT EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: DUCT — RUPTURED (AFT FUSELAGE)

RDU - FLT 0360 - EN ROUTE DFW/RDU DURING CRUISE, SLIGHT SMOKE NOTED IN CABIN WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO RDU AND LANDED WITHOUT INCIDENT. CHECK OF AIRCRAFT REVEALED STA 950 TO STA 950A LT CABIN AIR SUPPLY DUCT RUPTURED. AIRCRAFT MAINTENANCE FERRY RDU/DFW. REPLACED STA 950 TO STA 950A LT CABIN AIR SUPPLY DUCT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: STRINGER — CORRODED (BS 700-706)

TUL - STR 16L, CORROSION TOP INBOARD FLANGE, STA 700 - STA 706. REMOVED CORROSION, STRINGER REPAIR PER 53-10-03 FIG 1 SHEETS 1-4 SRM. 77,504 HOURS. CYCLES, 52,602. (X)

Part: FLOOR BEAM — CORRODED (BS 1110)

TUL - FLOOR BEAM CORRODED BL ZERO STA 1110. CUT OUT DAMAGED SECTION OF FLOOR BEAM AND INSTALLED REPAIR DOUBLER PER SRM 53-10-8. 77,504 HOURS. CYCLES, 52,602. (X)

Part: FITTING — CORRODED (BS 740)

TUL - STR 27L OUTBOARD END FITTING AT STA 740 HAS HEAVY CORROSION. FABRICATED NEW FITTING AND INSTALLED PER SRM 51-10-1. 77,504 HOURS. CYCLES, 52,602. (X)

Part: CASTING — CORRODED (BS 875)

TUL - LANDING GEAR PRESSURE DECK GEARING CASTING HAS CORROSION ON BOTTOM SIDE. LANDING GEAR PRESSURE DECK GEARINGS MOUNT CASTING REPAIRED PER ESO 11697 DATED 4-2-97. 77,504 HOURS. CYCLES, 52,602. (X)

Part: BELL FRAME — CRACKED (BS 930)

TUL - CRACK AT RIVET IN BELL FRAME BS 930 ABOVE STR 13R. INSTALLED DOUBLER IN BELL FRAME BS 930 PER SRM 53-10-4. STOP DRILLED CRACK. 77,504 HOURS. CYCLES, 52,602. (X)

Part: SKIN — CRACKED (FWD FUSELAGE)

TUL - .50 INCH CRACK IN FUSELAGE SKIN AT THE NR 5 FIRST OFFICER'S WINDOW UPPER AFT CORNER EXTENDING FROM SCREW HOLE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 8. 77,504 HOURS. CYCLES, 52,602. (X)

Part: STRINGER — CORRODED (BS 720)

TUL - CORROSION ON STR 28R OUTBOARD AREA. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATED 4-1-97. 77,504 HOURS. CYCLES, 52,602. (X)

Part: SKIN — CORRODED (BS 440-460)

TUL - CORROSION ON INSIDE OF FUSELAGE SKIN BEHIND AND ABOVE STR 19R. CUT OUT CORROSION I SKIN. INSTALLED FILLER AND DOUBLER AT LA SPLICE PER SRM 53-30-30. 77,504 HOURS. CYCLES, 52,602. (X)

Part: STIFFENERS — CRACKED (BS 178)

TUL - THREE EACH HORIZONTAL STIFFENERS CRACKED, STA 178 UNDER RADAR DISH. WEB CRACKED AT STA 178 BETWEEN STIFFENERS. REPLACED STIFFENERS AND INSTALLED DOUBLER OVER WEB CRACK PER SRM 53-10-09, PAGES 10 AND 11. 77,504 HOURS. CYCLES, 52,602. (X)

Part: STRINGER — CRACKED (BS 720)

TUL - STR 15R CRACKED AT END, FORWARD SIDE OF WING ICE LIGHT BS 720B. REPAIRED CRACKED SECTION OF STR 15R AND INSTALLED STRINGER SPLICE PER SRM 53-10-3 PAGE 4B FIG 1. 77,504 HOURS. CYCLES, 52,602. (X)

Part: STRINGER — CORRODED (BS 720)

TUL - STR 26R HAS HEAVY CORROSION ON OUTBOARD VERTICAL FLANGE AT STA 720D PLUS 10 INCHES. REPLACED DAMAGED AREA WITH SPLICE PER SRM 51-40-4. 77,504 HOURS. CYCLES, 52,602. (X)

Part: ANGLE — CRACKED (BS 1348)

TUL - UPPER CHORD ANGLE IN LEFT NR 2 STRUT IS CRACKED AT STA 1348. REPAIRED CHORD ANGLE PER SRM 51-40-3 PAGES 1 AND 2. 77,504 HOURS. CYCLES, 52,602. (X)

Part: FLOOR BEAM — CRACKED (BS 294.5)

TUL - STA 294.5 FRAME (FLOOR BEAM) CRACKED 12 INCHES INBOARD FROM LEFT OUTBOARD SKIN TOP SIDE. REMOVED CRACKED SECTION OF EXTRUDED ANGLE AND SPLICED IN NEW SECTION PER SRM 51-40-4. 77,504 HOURS. CYCLES, 52,602. (X)

Part: SUPPORT — CRACKED (BS 592)

TUL - STA 592 BL ZERO INBOARD LEG TOP FLANGE OF FLOOR SUPPORT BEAM, CRACKED AT FASTENER HOLE. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 51-40-4 FIG 1. 77,504 HOURS. CYCLES, 52,602. (X)

Part: SUPPORT — CORRODED (BS 351)

TUL - CORROSION UNDER AFT TWO FASTENERS' LT AND RT SIDE NLG DRAG BRACE SUPPORT LOWER SIDE. INSTALLED NEW DRAG BRACE SHELF PER 51-10-1. 77,504 HOURS. CYCLES, 52,602. (X)

Part: STRINGER — CORRODED (BS 1166)

TUL - HEAVY CORROSION STR 23R STA 1166. REPLACED STR 23R STA 1148 - STA 1166 AND STRINGER SPLICE PER 53-10-3. 77,504 HOURS. CYCLES, 52,602. (X)

Part: SKIN — GOUGED (BS 990)

TUL - GOUGE IN SKIN. REPAIRED PER SRM 53-30-3. TST: 77,504 HOURS. CYCLES, 52,602. (X)

Part: ANGLE — CORRODED (BS 340)

TUL - CORROSION ON SKATE ANGLE. REMOVED RIGHT SKATE ANGLE AND REPLACED WITH NEW SKATE ANGLE 65-19861-8. TST: 77,504 HOURS. CYCLES, 52,602. (X)

Part: FITTING — CORRODED (BS 351.2)

TUL - LEFT FWD SUPPORT FITTING FOR SHELF BELOW NLG DRAG BRACE CORRODED. REMOVED AND REPLACED WITH SERVICEABLE PART PER SRM 51-10-1. 77,504 HOURS. CYCLES, 52,602. (X)

Part: SKIN — CRACKED (WS 465)

TUL - 3 INCH - 4 INCH CRACK ON RIVETED SKIN PANEL JUST FWD OF NR 5 SPOILER, .50 INCH CRACK JUST FWD OF OUTBOARD SIDE NR 5 SPOILER ON RIVETED SKIN PANEL. STOP DRILLED CRACKS. INSTALLED DOUBLER OVER BOTH CRACKS PER 57-30-04. 77,504 HOURS. CYCLES, 52,602. (X)

Part: SPAR — CORRODED (BS 740)

TUL - FRONT WING SPAR CHORD ANGLE AND WEB CORRODED LOWER AREA AT THIS SEAL RETAINER. CUT OUT CORRODED WEB, BLENDED OUT CHORD ANGLE CORROSION PER SRM 57-10-1. INSTALLED WEB AND CHORD ANGLE. REPAIR PER ESO 11697 DATED 4-4-97. 77,504 HOURS. CYCLES, 52,602. (X)

Part: RELAY — DEFECTIVE (CABIN)

DFW - FLT 548 - AFTER GATE DEPARTURE DURING TAXI-OUT, EMERGENCY EXIT LIGHTS ILLUMINATED INTERMITTENTLY WITH SWITCH IN ARMED POSITION. AIRCRAFT RETURNED TO GATE. REPLACED EMERGENCY EXIT LIGHT RELAY R-70. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SIDE WALL — CRACKED (BS 260-285)

TUL - NOSE WHEELWELL, LEFT SIDE WALL, CRACKED IN 4 PLACES BELOW AND AFT OF THE AFT ACCESS PANEL. STOP DRILLED 2 CRACKS, CUT OUT 2 DAMAGED AREAS, INSTALLED FILLERS, DOUBLER, AND TRIPLER PER SRM 51-40-2, FIGURE 1, PAGE 1. TST: 74,632 HRS. CYCLES, 51,110. (X)

Part: SKIN — CORRODED (BS 1125-1126)

TUL - BELLY SKIN AT STR 30, BS 1125-1126, IS CORRODED THROUGH SKIN. INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 3. TST: 74,632 HRS. CYCLES, 51,110. (X)

Part: RIB — CRACKED (WS 656.5)

TUL - LEFT 656.5 RIB CRACKED AT LOWER NR 8 STRINGER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-10-5, PAGE 6. TST: 74,632 HRS. CYCLES, 51,110. (X)