N890AA

Part: CHANNEL — DAMAGED (SPOILER)

TUL - FOUND ELONGATED HOLE IN VERTICAL CHANNEL AT OUTBOARD HINGE OF NR 2 SPOILER. REMOVED VERTICAL CHANNEL AND INSTALLED NEW PART USING FIRST OVERSIZE HI-LOCKS SRM 51-10-1 PAGE 4. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD CENTER CEILING INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT FORWARD CENTER CEILING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIR)

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

Part: CONNECTOR — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 17D, 20D, AND 24D INOPERATIVE. REPLACED CONNECTORS TO EMERGENCY EXIT FLOOR PATH LIGHTS STRIPS AT SEATS 17D, 20D, AND 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (BS 720)

TUL - FOUND CORROSION AROUND INNER SKIN AROUND ICE LIGHT HOUSING LANDING AT BS 720B-720C AND STRINGER 14L-16L. REPAIRED PER SRM 53-30-3 AREA AROUND ICE LIGHT HOUSING, AND ESO 11697 (PAN HEAD HI-LOCKS) 2 EACH, 4-9-99. (M)

Part: FRAME — CORRODED (BS 620)

TUL - FOUND OUTBOARD SIDE STRINGER 26R AFT SIDE 620 FRAME LOWER CHORD ANGLE CORRODED. REPAIRED CHORD ANGLE PER SRM 51-40-3. (M)

Part: BEAM — CORRODED (BS 786-790)

TUL - FOUND CORROSION ON LIGHTENING HOLE ON BOTTOM OF DELTA BEAM AT STATION 786 TO 790. REPAIRED WITH DOUBLER IAW SRM 51-40-2 AND 51-20-0. (M)

Part: STRINGER — CRACKED (BS 720)

TUL - REF E58 NR 3150893, STRINGER 15L CRACKED AT BS 720B PLUS 15 INCHES AT AFT EDGE OF ICE LIGHT HOUSING. REPAIR STRINGER 15L BS 720B PLUS 15 INCHES AT AFT EDGE OF ICE LIGHT PER SRM 53-10-3. (M)

Part: SPAR — CORRODED (HORIZ STAB)

TUL - FOUND LEFT HORIZ STAB REAR SPAR CHORD UPPER END HAS 1 INCH AREA OF CORROSION BETWEEN NR 6 AND NR 7 ELEV HINGE BEARING. REPAIRED AREA OF CORROSION REMOVAL PER ESO 11697, DATED 3/30/99. (M)

Part: FRAME — DENTED (BS 1110)

TUL - FOUND BELL FRAME FLANGE DENTED STATION 1110, STRINGER 27 AND 25R. INSTALLED DOUBLER PER SRM 51-40-3. (M)

Part: ANGLE — CORRODED (BS 620)

TUL - FOUND OUTBOARD SIDE STRINGER 26R AFT SIDE 620 FRAME LOWER CHORD ANGLE CORRODED. REPAIRED CHORD ANGLE PER SRM 51-40-3 DOUBLER 17-7 MATERIAL .063 THICK 2.5 INCH BY 2.5 INCH BY 15 INCH WITH BAC30FQ6 FASTENERS AND 44 BACC30MB COLLARS. (M)

Part: STRAP — CORRODED (BS 620)

TUL - FOUD STRINGER 614-619 ABOVE STRINGER 26R UPPER CHORD ANGLE LOWER TAPERED STRAP DOUBLER CORRODED AROUND 3 NUT PLATES. REMOVED AND REPLACED TAPERED STRAP. (M)

Part: FRAME — BENT (BS 1030)

TUL - FOUND STATION 1030 BELL FRAME BENT (FLANGE/WEB) STRINGER 26-25 LEFT. REMOVED DAMGED SECTIONS, 1 INCH BY 2.8125 INCH BY 1 INCH BY 1.3125 INCH FROM BELL FRAME FLANGE, DYE CHECKED FOR CRACKS, NONE FOUND. INSTALLED DOUBLER PER SRM 51-40-3. (M)

Part: FLOORBEAM — CORRODED (BS 1130)

TUL - FOUND CORROSION AT FASTENER HOLES FOR CEILIG PANEL ATTACHMENT. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATED 4-9-99 USING 7075T6 .080 1 INCY BY 16.5 INCH OAL. (M)

Part: SPAR — CORRODED (WS 213-216)

TUL - RIGHT WING FSS 213-216 LOWER CHORD ANGEL LOWER LEFT HAS EXFOLIATING CORROSION, UPPER SURFACE AROUND AND UNDER STRUT ROD MOUNT BRACKET. REMOVED AND BLENDED CORROSION PER SRM 57-10-1. REPAIRED PER AARD 57-30-00-2. (M)

Part: FRAME — BENT (BS 1130)

FOUND BELL FRAME BENT IN WEB STATION 1130, STRINGER 26R TO STRINGER 25R. CUT OUT DAMGED AREA AND INSTALLED DOUBLER REPAIR PER 51-40-5 (AARD 53-10-07-3). (M)

Part: FRAME — BENT (BS 1030)

TUL - FOUND BELL FRAME BENT FLANGE AND WEB STATION 1030 STRINGER 26R TO STRINGER 25R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLERS PER SRM 51-40-3. (M)

Part: SHEAR TIE — CORRODED (BS 1130)

TUL - FOUND CORROSION ON SHEAR TIE AFT SIDE FS 1130, STRINGER 28 LEFT OUTBOARD. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIG FASTENER LOCATIONS. FASTENERS THROUGH FRAME .1875 INCH HI-LOCKS. FASTENERS THROUGH SKIN RIVET ORIGINAL SIZE AND TYPE. (M)

Part: SPLICE — CRACKED (BS 1030)

TUL - FOUND BELL FRAME (SPLICE) STRAP CRACKED STATION 1030 BETWEEN STRINGER 24L AND 25L. REPLACED (SPLICE) STRAP PER 51-10-1. (M)

Part: SHEAR TIE — CORRODED (BS 1130)

TUL - FOUND CORROSION ON SHEAR TIE FS 1130 AT STRINGER 30. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIGINAL FASTENER LOCATIONS. FASTENERS THROUGH FRAME .1875 INCH HI-LOCKS. FASTENERS THROUGH SKIN ORIGINAL SIZE AND TYPE REF 51-10-1. (M)

Part: SHEAR TIE — CORRODED (BS 1130)

TUL - FOUND CORROSION ON SHEAR TIE AFT OF FS 1130 AT STRINGER 29 LEFT. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE USING ORIGINAL FASTENER LOCATIONS. FASTENER THROUGH FRAME .1875 HI-LOCKS. FASTENERS THROUGH SKIN ORIGINAL SIZE ADN TYPE REF 51-10-1. (M)

Part: FRAME — BENT (BS 1050)

TUL - FOUND STATION 1050 BELLFRAME FLANGE 8 WEB BENT STATION 1050, STRINGER 26 AND 25 LEFT. REPAIRED BELLFRAME PER SRM 51-40-3. (M)

Part: FRAME — CORRODED (BS 1070)

TUL - FOUND STATION 1070 BELLFRAME FLANGE AND WEB STRINGER 26 AND 25 LEFT. INSTALLED DOUBLER PER SRM 51-40-3. (M)

Part: STRINGER — CRACKED (BS 720)

TUL - CUT OUT CRACK AND REPAIRED STRINGER 15R FORWARD SIDE OF WING SCANNING LIGHT. MATERIAL PER SRM 53-10-3 FIG 5. FASTENERS SIX .1875 HI-LOCKS THROUGH SKIN AND STRINGER THREE .1875 HI-LOCKS THROUGH SIDE OF U-CHANNEL PER SIDE, TWO .15625 HI-LOCKS THROUGH STRINGER CLIP AND STRINGER PER SIDE. (M)

Part: STRINGER — DAMAGED (BS 720)

TUL - CUT OUT DAMAGE AT FS 720A PLUS 10 INCHES SPLICED IN NEW STRINGER. MATERIAL PER SRM 53-10-3 FIG 5. FASTENERS THROUGH SKIN FOUR .1875 HI-LOCKS PER SIDE OF SPLICE ALSO THROUGH LIP OF STRINGER. FOUR .15625 HI-LOCKS THROUGH SIDE OF 'J' CHANNEL PER SIDE, EACH SIDE OF SPLICE. (M)

Part: FRAME — BENT (BS 1010)

TUL - FOUND BELL FRAME FLANGE/WEB BENT. INSTALLED DOUBLER PER SRM 51-40-3. (M)

Part: STRINGER — CORRODED (BS 1177)

TUL - FOUND STRINGER 30 CORRODED AT STATION 1177. INSTALLED NEW SECTION OF STRINGER STATION 1156-1183 WITH NEW SPLICE BETWEEN STATION 1148 AND 1166 PER SRM 51-10-3 PAGE 3, NEW END FITTING INSTALLED AT 1183 ALODINED AND PRIMERED ALL PARTS. (M)

Part: FRAME — DAMAGED (BS 375)

TUL - REMOVED DAMAGE BY CUTTING OUT. INSTALLED DOBULER AND FILLER SRM 51-40-3 DOUBLER MATERIAL 7075-T6 .063 INCH THICK FILLER .050 INCH 7075-T6 FASTENERS (10 EACH) .1875 PROTRUDING HD HI-LOCKS (4) .1875 100 DEGREES COUNTERSUNK HD HI-LOCKS WITH TOTAL 14 INCH THIN ALUM WASHERS CPN 592217. (M)

Part: STRINGER — CORRODED (BS 950)

TUL - FOUND STRINGER 29L CORRODED AROUND FASTENER, OUTBOARD LEG AFT OF STATION 950B TO 950B PLUS 1 INCH. REPAIRED PER ESO 11697 DATED 4-1-99 USING GENERAL GUIDE LINES OF SRM 51-40-4. INSTALLED STRAP REPAIR. (M)

Part: SILL — CORRODED (BS 970)

TUL - FOUND STATION 970 STRINGER 27 RIGHT DOOR CUT OUT CORRODED CHORD ANGLE, SILL PLATE LOWER. BLENDED CORROSION, HFEC FASTENER HOLES. LIGHTLY SPOTFACED FASTENERS HOLES, AND FLAP PEENDED REWORK AREA PER ESO11697, DATED 3/29/99. (M)

Part: FRAME — DENTED (BS 560)

TUL - FOUND STATION 560 BELLFRAME DENTED IN BETWEEN STRINGERS 24L AND 25L. CUT OUT DAMAGE 1 INCH BY 1.25 INCH AND INSTALLED DOUBLER PER SRM 51-40-3 PAGE 1-5. MATERIAL .063 INCH 7075T-6, 9 INCH LONG USING 27MS20470D, .1875 INCH RIVETS, 3 ROWS PAST DAMAGE, 1 ON TOP. (M)

Part: FRAME — BENT (BS 1070)

TUL - FOUND STATION 1070 BETWEEN STRINGER 26R-25R, BELLFRAME BENT IN WEB. REMOVED 3.5 INCH BY 1.25 INCH DAMAGED AREA. INSTALLED .071 T6 DOUBLER PER SRM 51-40-3. INSTALLED DOUBLER WITH 11BACB30FP8-4, 11 BACC30M8, 11 BACBB30FP6-3, 19 BACC30M6, 8 BACB30F06-3 HI-LOCKS. (M)

Part: FRAME — BENT (BS 950)

TUL - BELT FRAME, BENT FLANGE AND WEB STATION 950F BETWEEN 26L AND 25L. INSTALLED DOUBLER ON BELT FRAME AT STATION 950F BETWEEN STRINGER 25L AND 26L IAW AARD 53-10-07-3. DAMAGED AREA OF FREE FLANGE AT WEB CUT OUT WAS 1 INCH BY 1.5 INCH. DOUBLER USED WAS 2024 T4 .071 THICK. INSTALLED ONE ROW OF .1875 INCH BOEING HEAD SCREWS (NAS 8603-2) IN FREE FLANGE OF DOUBLER. INSTALLED TWO ROWS OF 1ST OVER HI-LOKS IN FRONT SIDE OF DOUBLER WEB. HI-LOKS WERE BACBB30FN6. (M)

Part: FRAME — DAMAGED (BS 950)

TUL - STATION 950A STIRNGER 19R, BELT FRAME HAS DEEP WEAR FROM CEILING PANEL, DAMAGE ON FREE FLANGE. INSTALLED DOUBLER PER 51-40-3. NO CUT OUT REQUIRED. DOUBLER PUT ON TOP OF FREE FLANGE AND WEB WAS .063 7075 MATERIAL 5.5 INCH LONG. 1 ROW OF 6 HI-LOCKS BACB30FN6-4 IN FREE FLANGE. WEB HAD 2 ROWS OF HI-LOCKS 1ST OVERSIZED. 1ST ROW WAS .1875 INCH BACB30FP6-4, 2ND ROW WAS .1875 INCH BACB30FP6-3. (M)

Part: FRAME — DENTED (BS 580)

TUL - FOUND STATION 580 BELLFRAME DENTED FROM STRINGER 24L TO 22L. REMOVED AND CUTOUT 3 DAMAGED AREAS (SIZES NOTED ABOVE). INSTALLED .063 DOUBLER, 7075-T6, 20 INCH LONG. INSTALLED 55-MS20470D, .1875 RIVETS AND 4 MS20470D, .25 INCH RIVETS, 3 ROWS TOTAL PER SRM 51-40-3, FIG 1. (M)

Part: SKIN — CORRODED (CENTER WING)

TUL - HEAVY CORROSION ON OUTER SKIN OF NR 2 FUEL CELL AT STATION 847, LBL 28, WING CENTER SECTION. REMOVED 4 FASTENERS, BLENDED CORROSION. REMOVED .051 THICKNESS. REAMED HOLES 2ND OVER, COLD WORKED HOLES. INSTALLED 4 4 EACH 2ND OVERSIZE HI-LOCKS (SEALER) TREATED AND PRIMED. (M)

Part: FRAME — DENTED (BS 990)

TUL - FOUND STATION 990 BELL FRAME FLANGE AND WEB BENT LEFT STRINGER 25-27. CUT OUT 6.75 INCH BY 1.25 INCH DAMAGED AREAS. INSTALLED .071 T-6 DOUBLER PER SRM 51-40-3, 25 MS20470, 25MS 20470 D6-6 (RIVETS), 16 BACR15CE6D6 RIVETS, 3 BACB30FP6-3 (RIVETS), 3BAC30M6 COLLARS. (M)

Part: ANGLE — CRACKED (BS 804.3)

TUL - FOUND ANGLE ON FRAME CRACKED AT FASTENER HOLE AT ATTACH POINT TO STRINGER 14R. REMOVED CRACKED PART AND INSTALLED NEW PART WITH HI-LOCKS. (M)

Part: FRAME — BENT (BS 680)

TUL - FOUND STATION 680 BELLFRAME BENT BETWEEN STRINGER 24L AND 23L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3. (M)

Part: FLOORBEAM — CORRODED (BS 380)

TUL - FOUND TOP OF FLOORBEAM AT BS 380 IS CORRODED FROM RBL 48 TO 64 RBL. FLOORBEAM REPAIR COMPLETE AFT FLANGE OF UPPER CHORD STATION 380 RBL 48 TO 65 AS PER AARD 53-10-07-02 PAGE 1-3 FIG 1. (M)

Part: FRAME — DENTED (BS 660)

TUL - FOUND FRAME 660 DENTED FROM STATION 24L TO 23L. REMOVED TWO DAMAGED AREAS, .75 INCH BY 6.5 INCH, .75 INCH BY .75 INCH. INSTALLED DOUBLER (7075 T-6, .063) 18 INCHES LONG, WITH 3 ROWS OF RIVETS, 1 ROW ON TOP, 2 ROWS ON SIDE WITH 41 .1875 D-RIVETS AND FOUR .25 INCH D-RIVETS. (M)

Part: FRAME — DENTED (BS 520)

TUL - FOUND BELLFRAME DENTED BETWEEN STRINGERS 24L AND 22L AT STATION 520. REMOVED DAMAGED AREA OF BELTFRAME AT STRIGNER 23L AND REPAIRED PER SRM 51-40-2 PAGE 1-5 SHEET 3. DENTS AT 22L AND 24L FOUND TO BE WITHIN LIMITS. (M)

Part: FRAME — DENTED (BS 720)

TUL - FOUND FRAME 720 DENTED BETWEEN STRINGER 25L AND 24L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3. (M)

Part: FRAME — DENTED (BS 680)

TUL - FRAME 680 DENTED BETWEEN STRINGER 23R AND 24R. INSTALLED BELT FRAME DOUBLER PER SRM 51-40-3. (M)

Part: FRAME — DENTED (BS 970)

TUL - BELLFRAME FLANGE AND WEB BENT STATION 970 BETWEEN 25 AND 26, STRINGER LEFT. CUT OUT DAMAGE 5.75 BY 1.25. REPAIRED BELL FRAME STATION 970 BETWEEN 25 AND 26 STRINGER LEFT PER 51-40-3, DOUBLER .71 MATERIAL 13BACB30MB6-3 HI-LOCKS, 13 BACC30M8 COLLARS, 7NAS8603-3 SCREWS, 2 ROWS ON SIDE, 1 ONT TOP. (M)

Part: FRAME — DENTED (BS 700)

TUL - FRAME DENTED BETWEEN STRINGER 25L AND 24L AT FS 700. REMOVED DAMAGED AREA. INSTALLED DOUBLER 7075T6, .063 FIVE INCHES LONG WITH FOURTEEN MS20470D, .1875 INCH AND FOUR MS20470D .25 INCH RIVETS, THREE ROWS TOTAL. (M)

Part: SKIN — DENTED (BS 1301)

TUL - DENT IN FUSELAGE AT STATION 1303, STRINGER 23R. FABRICATED DOUBLER 2024T3, .063 THICK 9 INCH BY 7.5 INCH, ATTACHED WITH (63 EACH) BACR15CE5 RIVETS AND (12 EACH) BACR15CE SIX RIVETS. (M)

Part: FRAME — CORRODED (BS 720)

TUL - FOUND CORROSION ON BELT FRAME AT BS 720B FROM STRINGER 5R-6R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-10-4 USING .071 7075T6 MATERIAL AND .1875 '0' HI-LOCKS. (M)

Part: SKIN — CORRODED (BS 383-391)

TUL - PREVIOUSLY WORKED GOUGES IN SKIN HAVE CORROSION AT STATION 383 TO 391, STRINGER 7L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 USING .050 2024T3 MATERIAL. (M)

Part: FRAME — DENTED (BS 600)

TUL - FRAME 600 LEFT STRINGER 22L TO STRINGER 24L, 3 EACH DENTS IN UPPER LIP OF FRAME 2 EACH CUT OUT APPROX 2.25 INCH, ONE CUT OUT APPROX 3 INCHES. REPAIRED AREA. (M)

Part: FRAME — CORRODED (BS 1161)

TUL - FOUND BELL FRAME CORRODED, STATION 1166, STRINGER 26L TO 27L. INSTALLED DOUBLER ON BELL FRAME AS PER SRM 53-10-4. (M)

Part: SKIN — CORRODED (BS 720)

TUL - CORROSION AROUND RAM AIR DOOR ACTUATOR CUT-OUT. INSTALLED DOUBLER REPAIR PER ESO 11697 DATED 3-23-98. TST: 49,306 HOURS. CYCLES: 26,738. (X)

Part: SPLICE — CORRODED (BS 1149-1156)

TUL - STR 30 SPLICE ANGLE CORRODED. RT FLANGE STA 1149 - STA 1156. REMOVED CORRODED STR 30 SPLICE ANGLE STA 1149 - STA 1156. INSTALLED NEW SPLICE ANGLE PER SRM 53-10-3. TST: 49,306 HOURS. CYCLES: 26,738. (X)

Part: SKIN — CORRODED (BS 835)

AFW - CORROSION ON CENTER WING FUEL TANK SKIN AT STA 835 AT STIFFENER S-5, LBL 25. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 57-30-3. TST: 47,396:15 HOURS. CYCLES: 25,819. (X)

Part: BEAM — CORRODED (BS 848.95)

AFW - LEFT DELTA BEAM CORRODED AND CRACKED AT STA 848.95. REMOVED DAMAGED T-ANGLE AND SPLICED IN NEW SECTION PER SRM 53-10-6. TST: 47,396:15 HOURS. CYCLES: 25,819. (X)

Part: SKIN — CORRODED (BS 848)

AFW - CORROSION ON CENTER WING FUEL TANK LOWER SKIN AT STR 848, RBL 26. REMOVED CORROSION AND INSTALLED EXTERNAL DOUBLERS PER SRM 57-30-5 AND SRM 57-30-3. TST: 47,396:15 HOURS. CYCLES: 25,819. (X)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 12 INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PAX SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (BS 680-685)

FOUND CORROSION ON STRINGER 27R AND FUSELAGE SKIN AT STATION 680-685. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND STRINGER PER SRM 53-30-3 PG 3C. (M)

Part: SKIN — CORRODED (BS 580-585)

FOUND SKIN CORROSION BEYOND LIMITS ON FUSELAGE. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1, PG 1-4. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 10D AND 16D FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 10D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)