N868AA

Part: LIGHT — INOPERATIVE (AFT STAIRWELL)

DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWELL EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIRWELL EMERGENCY LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIR)

IAH - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (BS 480)

TUL - SKIN AT SKIN LAP BULGED AND 2 RIVET HEADS SHEARED STATION 480 STRINGER 26R. REMOVED CORRODED SECTION OF STRINGER. INSTALLED NEW SECTION OF STRINGER AND SPLICED. INSTALLED ALL FASTENERS PER SRM 53-10-3 FIG 1. (M)

Part: FRAME — CRACKED (BS 480)

TUL - STATION 480 FRAME CRACKED AT STRINGER 26R, CRACK IN STRINGER CUT OUT RADIUS. INSTALLED .063 INCH 7075-T6 DOUBLER 9 INCHES LONG USING TOTAL OF 34 FASTENERS PER SRM 51-40-3. (M)

Part: STRINGER — CRACKED (BS 480)

TUL - FOUND STRINGER 25 RIGHT, 6 INCHES AFT OF STATION 480 CRACKED. REPAIRED STRINGER 25 RIGHT STATION 480 PER SRM 53-10-3 FIGURE 2 DETAIL II. (M)

Part: BEAM — CORRODED (HORIZ STAB)

TUL - FOUND CORROSION ON TOP OF T/E BEAM RIGHT HORIZ STAB 2ND FROM OUTBOARD ELEV HINGE. INSTALLED DOUBLER REPAIR PER ESO 11697, DATED 2-14-00. (M)

Part: SHEAR TIE — CORRODED (BS 1148)

TUL - FOUND CORRODED SHEAR TIE STATION 1148 STRIGNER 26L. REPLACED SHEAR TIE. (M)

Part: PANEL — CORRODED (BS 1166-1183)

TUL - AFT LAVATORY SERVICE PANEL BULGING AT BOTTOM. REPAIRED SECTION OF SKIN DOUBLER PER SRM 53-30-3. INSTALLED NEW LAVATORY PAN TRIPLER. REINSTALLED LAVATORY PAN DUMP LINE, FILL LINES AND CABLES. (M)

Part: STRINGER — CORRODED (BS 525)

TUL - FOUND CORROSION ON STRINGER 28L AT BS 525, REMOVED CORROSION MADE STRINGER OUT OF LIMITS. INSTALLED STRINGER REPAIR AS PER SRM 53-10-3 FIG 1. (M)

Part: NLG — LACK OF LUBE (NLG)

DFW - FLT 1607 - DURING APPROACH DFW, NOSE LANDING GEAR HUNG UP MOMENTARILY BEFORE EXTENDING NORMALLY. FLIGHT LANDED DFW WITHOUT FURTHER INCIDENT. NOSE LANDING GEAR WAS INSPECTED, LUBRICATED, AND SWUNG SEVERAL TIMES WITH NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAL — STUCK (NLG DOOR)

ORD - FLT 1523 - DURING APPROACH, WHEN GEAR HANDLE MOVED TO DOWN POSITION BOTH MAIN LANDING GEARS EXTENDED NORMALLY. NOSE GEAR REMAINED RETRACTED FOR SEVERAL SECONDS MORE FOLLOWED BY A LOUD BANG AND THEN NORMAL NOSE GEAR EXTENSION. LANDED ORD WITHOUT INCIDENT. REMOVED EXCESSIVE PAINT ON NOSE GEAR DOOR SEAL. REPAINTED DOOR SEAL, DOES'NT RUB. LUBED NOSE GEAR STRUT AND ACCOMPLISHED RETRACTION AND EXTENSION CHECK PER MM. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 1070)

TUL - FOUND CORROSION ON CABIN FLOORBEAM LOWER FLANGE, WHERE CEILING PANEL OF CARGO COMP IS SECURED. REMOVED CORROSION, ALODINED AND PAINTED, INSTALLED SUPPORT ANGLES AND STRAP PER SRM 53-10-8 ON LOWER FLOORBEAM AT STATION 1070, BL 0 TO LBL 48. (M)

Part: SWITCH — DEFECTIVE (NLG)

DFW - FLT 781 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR INDICATED UNSAFE WITH NORMAL NOSE GEAR DOOR INDICATION. RECYCLED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT LANDED DFW WITHOUT INCIDENT. LUBRICATED LANDING GEAR AND REPLACED NOSE LANDING GEAR OVERCENTER LOCK SWITCH. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANGLE — CORRODED (NR 5 LE SLAT)

TUL - NR 5 SLAT ACTUATOR INBOARD AND OUTBOARD ATTACH ANGLES CORRODED. REMOVED AND REPLACED BOTH ANGLES. TST: 55,431 HOURS. CYCLES: 34,330. (X)

Part: STRINGER — CORRODED (BS 562)

TUL - STA 562 INSIDE STR 27L CORRODED. INSTALLED STRINGER REPAIR PER SRM 53-10-3, FIG 1. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: SKIN — DENTED (BS 360)

TUL - .5 INCH BY .042 INCH DENT AT FS 360 BETWEEN STR 5 AND STR 6 RIGHT ABOVE AND AFT OF FORWARD ENTRY DOOR. INSTALLED PERMANENT REPAIR PER SRM 53-30-3, FIG 1. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: GEAR BEAM — CORRODED (RT MLG WW)

TUL - CORROSION ON AFT SIDE OF GEAR BEAM AFT BORE AT THE H-LINK ATTACH PIN HOLE. LOCALLY BLENDED HOLE, REMOVED CORROSION, COUNTERSUNK THE BORE AND MF6D BUSHING. INSTALLED WET PER ESO 11697 STD 5-29-97 AND BOEING M56 AAL TUL 93-0603TR AND 0660RR. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: TRUNNION SLEEVE — CORRODED (LT/RT MLG)

TUL - LEFT AND RIGHT GEAR AFT TRUNNION SLEEVES CORRODED. REMOVED BOTH SLEEVES, CLEANED AND TREATED THE GEAR BEAM BORES, AND INSTALLED NEW SLEEVES PER AAMPSM PAGES 16-21 AND PAGES 33 AND 34. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: STIFFENER — CRACKED (WS 686.50 LT)

TUL - UPPER SPAR STIFFENER NR 9 CRACKED, STA 656.50, LEFT WING. CRACK ENDED IN FASTENER HOLE. INSTALLED REPAIR PER BOEING SB 727-57A 159. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: FLAP TRACK — PITTED (NR 4 TE FLAP)

TUL - NR 4 FLAP TRACK PITTED OUTBOARD SIDE UNDER THE TOP ROLLER INBOARD RADIUS. REMOVED AND REPLACED TRACK PER PATTERN CARD 8703. TST: 55,431 HOURS. CYCLES: 34,330. (X)

Part: BULKHEAD BEAM — CRACKED (BS 1183)

TUL - RIGHT AFT PRESSURE BULKHEAD CENTER SUPPORT BEAM CRACKED AT THE FASTENER HOLES 28 INCHES ABOVE THE FLOOR. STOP DRILLED THE CRACKS AND INSTALLED DOUBLER KIT PER SB 727-53-0192, IT NR 65C34406-13. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: CASTING — CORRODED (AILERON)

TUL - WEB BULGING INBOARD OF INBOARD AILERON QUADRANT ATTACH CASTING. REMOVED AND INSTALLED SERVICEABLE AILERON QUAD CASTING. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: STRINGER — CRACKED (WS 629)

TUL - NR 1 TANK STRINGER CRACKED WS 629 TOP SECOND FROM AFT WEB. NR 1 TANK STRINGER CRACKED WS 629 THIRD FROM AFT WEB. STOP DRILLED CRACK AND INSTALLED REPAIR PER SB 727-57A159. CRACK ENDED AT FASTENER HOLE. INSTALLED REPAIR PER SB 727-57A159. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: FLOOR BEAM — CORRODED (BS 1130)

TUL - FLOOR BEAM CORRODED BETWEEN LT INBOARD AND CENTER GALLEY TRACKS AT STA 1130 TOP LAND OF BEAM, FORWARD LIP. ACCOMPLISHED FLOOR BEAM REPAIR PER SRM 53-10-8. TST: 66,431. CYCLES: 34,330. (X)

Part: SKIN — CRACKED (BS 1097)

TUL - SKIN CRACKED AT FS 1097 LT AND RT RIVETS STR 1. CUT OUT DAMAGED SKIN AND REPAIRED PER SB 727-53A0204. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: SHEAR TIE — CORRODED (BS 700)

TUL - SHEAR TIE CORRODED STA 700 BETWEEN STR 25L AND STR 26L. REMOVED AND REPLACED SHEAR TIE PER 53-10-4. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: FLOOR BEAM — CORRODED (BS 380)

TUL - CORROSION ON FLOOR BEAM STA 380 RBL 14 TO RBL 64. REMOVED CORROSION, INSTALLED REPAIR PER SRM 53-10-8. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: FIREWALL — CRACKED (NR 3 PYLON)

TUL - FIREWALL CRACKED 2 INCHES LONG FORWARD FLANGE FORWARD ENGINE MOUNT. INSTALLED REPAIR PER ESO 11697 DATED 5-22-97. TST: 55,431 HOURS. 34,330. (X)

Part: STRINGER — CORRODED (BS 488)

TUL - STA 488 INSIDE STR 28L CORRODED. REMOVED CORROSION PER 51-10-1 (OUT OF LIMITS). INSTALLED DOUBLER PER SRM 53-10-3. (X)

Part: SKIN — CORRODED (BS 500-510)

TUL - SKIN CORRODED ALONG THE INTERCOSTAL WHERE THE SEALING COMPOUND WAS REMOVED. INSTALLED DOUBLER PER SRM 53-30-3, FIG 24. TST: 55,431 HOURS. CYCLES: 34,330. (X)

Part: SKIN — CORRODED (BS 480-500)

TUL - SKIN CORRODED FROM STA 480 TO STA 500 UNDER AND OUTBOARD OF STR 28L. INSTALLED DOUBLER PER SRM 53-30-3, FIG 3A. TST: 55,431 HOURS. CYCLES, 34,330. (X)

Part: SKIN — CORRODED (BS 663)

AFW - FOUND CORROSION ON SKIN, UNDER PODDING COMP. REMOVED CORROSION, INSTALLED DOUBLER AS PER SRM 53-30-3. (M)

Part: FLAP TRACK — RUSTED (RT TE FLAP)

AFW - RUST AT MOUNTING POINTS. REPLACED WITH SHOP TRACK. (M)

Part: FLAP TRACK — CORRODED (TE FLAP)

AFW - FOUND CORROSION AT MOUNTS. REMOVED AND REPLACED TRACK WITH SERVICEABLE TRACK. (M)

Part: STRINGER — CORRODED (BS 577)

AFW - FOUND CORROSION ON STRINGER 27L. INSTALLED REPAIR IAW SRM 53-10-3. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ATL - DURING OVERNIGHT MAINTENANCE, FOUND THE FORWARD LEFT EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED THE M982 MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (BS 380)

TUL - FOUND SKIN BULGED, CRACKED AT FASTENER HOLE STATION 380 STRINGER 21 TO 22R. REMOVED CRACKED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 5-8. (M)

Part: SKIN — CRACKED (BS 305)

TUL - FOUND FUSELAGE SKIN HAS .5 INCH CRACK AT FORWARD END OF FUEL ENTRY DOOR LOWER HINGE CUTOUT. ROUTED OUT CRACK, INSTALLED DOUBLER PER SB 727-53-0198. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (COCKPIT DOR)

BWI - FLT NR 1736 - DURING OVERNIGHT CHECK, COCKPIT DOOR EMERGENCY EXIT SIGN/LIGHT INOPERATIVE. REPLACED COCKPIT DOOR EMERGENCY EXIT SIGN/LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SCREW — LOOSE (NR 3 FUEL TANK)

IAD - FLT 1161 - DURING CLIMB-OUT, EN ROUTE DCA-RDU, FUEL LEAKING FROM RIGHT WING POURING OVER OUTBOARD FLAPS. AIR INTERRUPTED AND LANDED IAD WITHOUT INCIDENT. TIGHTENED NR 15 AND 16 FUEL ACCESS PANEL SCREWS ON NR 3 TANK. INSTALLED TWO MISSING SCREWS ONE ON EACH PANEL. ACCOMPLISHED FCF, SYSTEM CHECKED NORMAL OPERATION. (W)

Part: SLIDE — DEFECTIVE (CABIN DOOR)

ORD - DURING SHOP VISIT, FOUND HOLE IN EMERGENCY EVACUATION SLIDE AT LT BOTTOM CENTER AIR TUBE. SLIDE INTRODUCED TO SHOP FOR REPAIR. (W)

Part: SLIDE — DEFECTIVE (PAX DOOR)

ODR - DURING SHOP VISIT, FOUND 3 INCH SEAM SEPARATION AT BOTTOM LT CENTER OF EMERGENCY EVACUATION SLIDE. ROUTED FOR REPAIR. (W)