N867AA

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO DOOR CUTOUT, LOWER JAMB LOWER CHORD, CORROSION ON LOWER CHORD, STATION 950F PLUS 13 TO STATION 950F PLUS 19. INSTALLED REPAIR PER AARD 51-40-00-1 REPAIR 1. (M)

Part: SKIN — SCRATCHED (FUSELAGE)

TUL - FOUND LARGE SCRATCH GOING INTO DENT AT BS 993-910, BELOW STRINGER 28R TO STRINGER 25R. BURNINSHED SCRATCH, DYE CHECKED. NO CRACK FOUND. INSTALLED 8 INCH BY 9 INCH REPAIR AT DENT LOCATION REF 53-30-3. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

TUL - FOUND FORWARD SIDE AFT PRESS BULKHEAD CRACKED WL 169 RBL 25. CUT OUT DAMGE AND INSTALLED DOUBLER PER SRM 53-10-9 PAGE 1-10. (M)

Part: ANGLE — CORRODED (FUSELAGE)

TUL - FOUND HEAVY CORROSION ON ANGLE INSIDE RIGHT TORQUE BAY AT FORWARD END OF SKATE ANGLE. REMOVED CORRODED T ANGLE, FABRICATED AND INSTALLED NEW T ANGLE FROM 7075-T6 EXTRUSION, PER SRM 51-10-1. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON BOTTOM FLANGE OF 1130 FLOORBEAM APPROX RLB 3 TO LBL 40. REPAIRED FLOORBEAM PER ESO 11697 DATED 3/16/2000. (M)

Part: BATTERY PACK — INOPERATIVE (OVERWING EXIT)

TUL - FOUND RIGHT MIDDLE OVER WING EXIT LIGHT INOPERATIVE, STATION 940. INSTALLED TWO NEW LAMPS PER MM 33-50-011-2 AND INSTALLED SERVICEABLE BATTERY PACK PER MM 33-50-022-2, OPS CHECKED OK. (M)

Part: BATTERY PACK — INOPERATIVE (OVERWING EXIT)

TUL - FOUND LEFT MIDDLE OVERWING EXIT LIGHT INOPERATIVE. INSTALLED TWO NEW LAMPS PER MM 33-50-011-2 AND INSTALLED SERVICEABLE BATTERY PACK PER MM 33-50-022-2, OPS CHECKED OK. (M)

Part: CONDUCTOR — DEFECTIVE (CABIN)

MIA - AISLE EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN FIRST CLASS AND COACH INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING FLAT CONDUCTOR BETWEEN FIRST CLASS AND COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CRACKED (BS 942)

TUL - RIGHT STRINGER 18A CRACKED IN RADIUS HORIZONTAL OUTBOARD LEG, EXTENDING OUT FROM RADIUS BLOCKS AFT SIDE OF 940 CASTING. REMOVED DAMAGED SECTION SPLICED IN NEW SECTION OF RT STRINGER 18A PER SB 727-53-0172. (M)

Part: SKIN — CORRODED (BS 578-592)

TUL - FUSELAGE SKIN CORRODED FS 587-592 OUTBOARD OF STRINGER 28 LEFT. REMOVED DAMAGED SKIN. INSTALLED DOUBLER REPAIR IAW SRM 53-30-3 FIG 3. (M)

Part: STRINGER — CORRODED (BS 591)

TUL - STRINGER 28L HAS HEAVY CORROSION AT FS 591. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED SPLICE REPAIR IAW SRM 53-10-3 FIG 1. (M)

Part: SHEAR TIE — CORRODED (BS 568)

TUL - FOUND CORROSION ON SHEAR TIE BETWEEN STRINGER 26R-27R, STATION 568. REMOVED CORRODED SHEAR TIE. INSTALLED NEW SHEAR TIE PER SRM 51-10-1. (M)

Part: FRAME — CORRODED (BS 720)

TUL - LOWER FLANGE OF BELLFRAME CORRODED, FORWARD CARGO STATION 720E BETWEEN STRINGER 27L AND 28L. CORRODED SECTION REMOVED, ANGLE REPAIR INSTALLED AT SHEAR TIE PER SRM 53-10-4 PAGES 58-60. (M)

Part: ACCESSORY UNIT — DEFECTIVE (E/E COMPARTMENT)

DFW - FLT 535 - EN ROUTE TUL-DFW - DURING GEAR RETRACTION, UNABLE TO RAISE GEAR HANDLE FROM OFF TO UP WITHOUT PULLING OVERRIDE TRIGGER. LEVER LATCH CIRCUIT BREAKER ON P6-3 WAS NORMAL. GEAR EXTENSION WAS NORMAL. AL OTHER SYSTEMS NORMAL. LANDED DFW WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY UNIT. PERFORMED OPERATIONS CHECK PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (LE FLAP)

TUL - FOUND CORROSION BEHIND DATA PLATE ON NR 1 AND NR 6 L/E FLAPS. REMOVED DATA PLATE. REMOVED CORROSION AND INSTALLED DOUBLERS PER SRM 57-50-3. (M)

Part: SKIN — DAMAGED (BS 198-208)

TUL - A/C SUSTAINED DAMAGED TO RADOM AND WRINKLES TO LEFT FUSELAGE STATION 178 TO 208, STRINGER 17L TO 24L, SUSPECT AFT AIR STAIRS OUT OF RIG. REPLACED RADOME, FUSE DAMAGE REPAIRED PER SRM 53-30-3. RIGGED AND ADJUSTED STAIRS PER MM. ALL WORK ACCOMPLISHED ON TUL DROP IN BOW NR 320, DATED 7-1-98. (M)

Part: STRUCTURE — DAMAGED (BS 178-209)

TUL - AIRCRAFT SUSTAINED DAMAGE TO RADOME AND WRINKLES TO LT FUSELAGE. STA 178 TO STA 208, STR 17L TO STR 24L. SUSPECT AFT AIRSTAIR OUT OF RIG. REPAIRED RADOME, FUSELAGE DAMAGE. REPAIRED PER SRM 53-30-3. RIGGED AND ADJUSTED VENTRICAL STAIR PER MM. ALL WORK ACCOMPLISHED ON W.O. NR 320 DATED 7-1-98. TULSA BOW 320-71-98. REF: OPERATOR CONTROL NR AALA981360.

Part: SKIN — CORRODED (BS 178-209)

TUL - AIRCRAFT SUSTAINED DAMAGE TO RADOME AND WRINKLES TO LT FUSELAGE. STA 178 TO STA 208, STR 17L TO STR 24L. SUSPECT AFT AIRSTAIR OUT OF RIG. REPAIRED RADOME, FUSELAGE DAMAGE. REPAIRED PER SRM 53-30-3. RIGGED AND ADJUSTED VENTRICAL STAIR PER MM. ALL WORK ACCOMPLISHED ON W.O. NR 320 DATED 7-1-98. TULSA BOW 320-71-98. REF: OPERATOR CONTROL NR 98ZZZX3702. (X)

Part: STRINGER — CORRODED (BS 1155)

TUL - FOUND STRINGER 30 CORRODED NEXT TO DRAIN MAST ATTACHMENT STATION 1155. REPAIRED STRINGER 30 WITH SPLICE REPAIR, SRM 53-10-3 FIG 1, PAGE 1-11. (M)

Part: KICK WEB — CORRODED (BS 1176)

TUL - FOUND CORROSION ON LEFT LAV KICK WEB AT STATION 1176 AT ATTACH LUGS, OUTBOARD END. REMOVED AND REPLACED LEFT AFT LAV KICK WEB PER SRM 51-10-1 PAGE 4. (M)

Part: FITTING — CORRODED (VERT STABILIZER)

TUL - VERT STABILIZER CLOSURE RIB HORIZ FLANGE HAS .058 BLENDOUT AT LEFT TENSION TIE ATTACH BOLTHOLE, UNDER SIDE OF FLANGE IRREGULAR SURFACE WILL NOT ALLOW SEATING OF NUT AND WASHER. ACCOMPLISHED REPAIR PER ESO 11687 DATED 7/15/97. (M)

Part: STRINGER — CORRODED (BS 1183-1148)

TUL - RIVET HEADS POPPED AND DISHED IN FUSELAGE SKIN, STRINGER 29L FORWARD OF STATION 1183. CUTOUT CORRODED SECTION OF STRINGER 29L AND SPLICED IN NEW 25 INCH SECTION FROM APPROX STATION 1158-1183. (M)

Part: SKIN — CORRODED (BS 660)

TUL - FOUND FUSELAGE SKIN CORROSION BEYOND LIMITS UNDER SHEAR TIE. INSTALLED DOUBLER PER SRM 53-30-03-3. (M)

Part: FRAME — CORRODED (BS 660)

TUL - FOUND CORROSION ON BOTTOM OF FRAME STATION 660 BETWEEN 28R AND 28L. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER PER SRM 53-10-4 FIG 11. (M)

Part: SKIN — CORRODED (BS 720)

TUL - FOUND CORROSION AROUND RIGHT WING FUSE MOUNTED LIGHT ASSY. REMOVED LIGHTS ASSY BLENDED AREA TREAT PRIME AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3 PAGE 137 AND 51-10-2 PAGE 12 AND REINSTALLED LIGHT ASSY. (M)

Part: VERT BEAM — CRACKED (BS 1183)

TUL - FOUND .5 INCH CRACK IN OUTBOARD RADIUS OF 1183 VERTICAL BEAM RBL 36 AT WL 238. STOP DRILLED CRACK AND INSTALLED DOUBLER PR SB 727-53-0192 DATED 2-22-93 DRAWING 65C34406. (M)

Part: FITTING — CORRODED (BS 277)

TUL - FOUND CORROSION ON NLG DRAG BRACE CASTING MAIN PIVOT LEFT SIDE. INSTALLED NEW NLG DRAG BRACE ATTACH FITTING. (M)

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 8D AND 10D INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PASSENGER SEAT ROW 8D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (BS 680-686)

TULE - FOUND STRINGER 26 RIGHT CORRODED, STATION 680-686. CUT OUT CORROSION AND INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)

Part: STRINGER — CORRODED (BS 682)

FOUND STRINGER 27 RIGHT CORRODED. REMOVED CORRODED AREA, INSTALLED SPLICE PER SRM 53-10-3 FIG 1. (M)

Part: SKIN — CORRODED (BS 706)

TUL - FOUND BULGE IN FUSELAGE SKIN. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 5. (M)