N889AA

Part: LIGHT — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT BETWEEN FIRST CLASS AND COACH CLASS SHORTED. REPAIRED EMERGENCY EXIT LIGHT STRIP BETWEEN FIRST CLASS AND COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT AIRSTAIRS)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT STAIRWELL INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT STAIRWELL. SYTEM GROUND NORMAL OPERATION. (M)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,265 hrs · 34,332 cycles

TUL - CORROSION ON FORWARD END OF LEFT SKATE ANGLE, STA 294. SPLICED IN NEW SECTION OF SKATE ANGLE PER SRM 51-20-4 AND ESO 11697 DATED 6-28-00 AND ESO 11697 DATED 6-9-00. (X)

Part: STRINGER — CORRODED (CARGO BAY) · airframe 57,265 hrs · 34,322 cycles

TUL - STR 29L KEELBEAM EXTENSION HAS HEAVY CORROSION AT STA 970. INSTALLED .071 INCH 301-1/2 HARD STRAP 3 INCHES BY 21 INCHES WITH HILOCKS PER ESO 11697 DATED 6-27-00. (X)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: FITTING — DAMAGED (NR 3 ENGINE)

TUL - FOUND 2 UPPER TANG 'F' HOLES ELONGATED AND GOUGED 4 HOLES ELONGATED AT NR 3 ENGINE UPPER FORWARD FITTING. TWO 'E' TAN HOLES OVERSIZED AND FASTENERS INSTALLED 4 'D' HOLES OVERSIZED AND DOUBLER AND TRIPLER INSTALLED PER ESO 11697, DATED 8-27-99 AND 8-31-99. (M)

Part: FLOORBEAM — BROKEN (BS 294)

TUL - FOUND FLOORBEAM LOWER FLANGE BROKEN COMPLETELY THROUGH THE WIRE BUNDLE STANDOFF SCREW HOLE. INSTALLED ANGLE, EQUAL LEG THICKNESS STAINLESS REPAIR PER SRM 51-40-4 PAGE 5. (M)

Part: LIGHT — INOPERATIVE (AFT AIRSTAIRS)

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

Part: STRINGER — CORRODED (BS 1010-1020)

TUL - FOUND CORROSION IN STRINGER 28LT STATION 1010-1020, CORROSION OUTBOARD STRINGER 28 LT, STATION 1010-1015. REMOVED DAMAGED STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4B DETAIL 1, 12 INCHES IN LENGTH. (M)

Part: SKIN — CORRODED (BS 1010-1015)

TUL - FOUND CORROSION ON FUSELAGE SKIN UPPER SURFACE OUTBOARD OF STRINGER 28L STATION 1010-1015 AND BELOW STRINGER 28L, STATION 1010-1015. REMOVED DAMAGED SKIN, INSTALLED REPAIR PER SRM 53-30-3 PAGE 148 FIG 3A. (M)

Part: STRINGER — CORRODED (BS 1148)

TUL - FOUND CORROSION IN STRINGER 23R STATION 1148. REMOVED STRINGER 23R FROM 1141-1155 SPLICE IN NEW SECTION AS PER SRM 53-10-3 FIG 1 SHEET 1 PAGE 3. (M)

Part: FLOORBEAM — CORRODED (BS 344)

TUL - FOUND CORROSION 42 INCHES RBL STATION 344, FLOORBEAM LOWER SURFACE. INSTALLED REPAIR AT STATION 344, RBL 12 PER ESO 11697, DATED 8/12/98. (M)

Part: SHEAR TIE — CORRODED (BS 720)

TUL - FOUND CORROSION ON SHEAR TIE STATION 720L BETWEEN 26R AND 27R. INSTALLED NEW SHEAR TIE. (M)

Part: SHEAR TIE — CORRODED (BS 580)

TUL - FOUND CORROSION ON FORWARD SIDE OF 580 FRAME OUTBOARD OF STRINGER 26L. INSTALLED NEW SHEAR TIE. (M)

Part: FRAME — DENTED (BS 720)

TUL - FOUND FORWARD CARGO FRAME 720A DENTED ABOVE STRINGER 24R. REMOVED DAMAGED SECTION, INSTALLED DOUBLER 8 INCH OF 7075-T6 .063 INCH, TWENTY MS2047DD FASTENERS, THREE ROWS OF FASTENERS, THREE PAST DAMAGE EACH SIDE PER SRM 51-40-3 FIG 1 PAGE 3. (M)

Part: STRINGER — CRACKED (BS 720)

TUL - FOUND STRINGER 15L CRACK JUST FORWARD OF ICE LIGHT HOUSING. REMOVED CRACK AREA OF STRINGER, REPAIRED PER SRM 53-10-3 FIG 5. (M)

Part: FRAME — CRACKED (BS 804)

TUL - FOUND CRACK STATION 804.95 STRINGER 14R. REMOVED AND REPLACED CRACKED BELL FRAME REINFORCEMENT ANGLE STATION 804.95, STRINGER 14R PER SRM 51-10-1 PAGE 4. (M)

Part: WEB — CRACKED (CENTER TANK)

TUL - FOUND 1.5 INCH CRACK IN WEB BETWEEN 2ND AND 3RD BAY CENTER TANK LBL 13.19 3 INCHES DOWN FROM TOP OF TANK. INSTALLED DOUBLER PER SRM 51-40-2. (M)

Part: FRAME — CRACKED (BS 930)

TUL - FOUND CRACK ON FRAME AT FS 930 AND STRINGER 14R. INSTALLED DOUBLER AT FS 930 AND STRINGER 14R PER SRM 53-10-2 PAGE 28 E, F, AND G. (M)

Part: FRAME — CRACKED (BS 500)

TUL - FOUND FUSELAGE FRAME DENTED ABOVE STRINGER 23L, FS 500. INSTALLED BELL FRAME DOUBELR REPAIR PER SRM 51-40-3 PAGE 1 USING 7075T6, .071 THICK 11 INCHES LONG, .375 INCH FASTENER AND 24MS204700 RIVETS, 2 ROWS ON BOTTOM AND ONE ON TOP, 3 RIVETS EACH END. (M)

Part: FRAME — DENTED (BS 600)

TUL - FUSELAGE BELL FRAME DENTED ABOVE STRINGER 24L AT FS 600. INSTALLED BELL FRAME DOUBLER PER SRM 51-40-3 PAGE 1 USING 7075-T6, .071 INCH THICK, 7 INCHES LONG, .375 INCH AND .25 INCH FASTENERS AND 20 MS 20470D RIVETS, TWO ROWS ON BOTTOM AND ONE RAN ON TOP, THREE RIVETS EACH END. (M)

Part: SKIN — CRACKED (BS 1098)

TUL - FOUND CRACK COMING FROM FASTENER 12 INCHES FORWARD OF STATION 1110 AT NR 2 ENGINE INTAKE DOG HOUSE STRINGER NR 1. CUT OUT DAMAGE SKIN PER SRM 53-30-3 PAGE 12 AND INSTALLED DOUBLER PER BOEING S/B 727-53AD204. (M)

Part: SKIN — CORRODED (BS 680-686)

TUL - FOUND CORROSION ON SKIN UNDER LEVELING COMPOUND STATION 680-686, STRINGER 26L. REMOVED DAMAGED AREA 1 INCH BY 1 INCH AND INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: FRAME — MISDRILLED (BS 1130)

TUL - FOUND BELL FRAME HEAVY DAMAGE, OVERSIZE FIG 8 HOLE, RIVET TO SMALL, TAILS BENT HOLE GROUND THROUGH BELL FRAME. CUT OUT DAMAGED SECTION ANGLE, INSTALLED ANGLE REPAIR SRM 51-40-3. INSTALLED DOUBLER SRM 51-40-2 AND REPLACED BAD FASTENERS. (M)

Part: STIFFENER — CRACKED (BS 1183)

TUL - FOUND CRACK IN VERTICLE STIFFENER FS 1183, RBL 38 WL 239 OUTBOARD SIDE OF STIFFENER. INSTALLED REPAIR DOUBLER PER BOEING S/B 727-53-0192 AND BOEING DRAWING NR 65C34406. (M)

Part: FRAME — DENTED (BS 660)

TUL - DENT IN FRAME ABOVE STRINGER 24R AT FS 660. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER 51-40-3 FIG 1 PAGE 3, 8 INCH DOUBLER OF .063 INCH 7075-T6, 20.375 MS2047DD RIVETS, THREE ROWS. (M)

Part: FLOORBEAM — CORRODED (BS 380)

TUL - FOUND CORROSION ON FLOORBEAM OF FS 380 AND RBL 47 INCHES. INSTALLED REPAIR STRAP PER SRM 53-10-07-2 FIG 1 ON FORWARD SIDE OF FLOORBEAM. (M)

Part: FRAME — DENTED (BS 660)

TUL - FOUND DENT IN FRAME AT FS 600 ABOVE STRINGER 23R. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER 51-40-3 FIG 1 PAGE 3, 8 INCH DOUBLER OF .063 INCH 7075-T6, 20.375 INCH RIVETS MS2047DD, THREE ROWS. (M)

Part: FLOORBEAM — CORRODED (BS 344)

TUL - FOUND CORROSION 18 INCHES RBL AT STATION 344 BELOW BEAM. REPAIRED TOP OF FLOORBEAM LOWER SIDE BY INSTALLING STRAP PER AAR 53-10-7-2 PAGE 1-3. (M)

Part: FRAME — DENTED (BS 950)

TUL - BELL FRAME DENTED AT STRINGER 26 LT AND 5 INCH ABOVE STRINGER 26 LT. INSTALLED DOUBLER .080 7075-T6 OVER DAMAGE AREA PER SRM 51-40-3. BELL FRAME DOUBLER 13.5 INCH IN LENGTH. (M)

Part: SKIN — CORRODED (BS 720)

TUL - FOUND CORROSION EMITTING FROM UNDER ICE LIGHT HOUSING, FUSELAGE SKIN CUTOUT. FABRICATED DOUBLER, FILLER DRILLED HOLES, COUNTERSANK HOLES, ALODINED, PRIMED, APPLIED SEALANT AND INSTALLED DOUBLER FILLER AND ICE LIGHT PER SRM 53-30-3 FIG 22 PAGE 137. (M)

Part: FRAME — DENTED (BS 990)

TUL - FOUND BELL FRAME DENTED. FABRICATED DOUBLER, DRILLED HOLES, TREATED AND PRIMED PER SRM 51-10-2. (M)

Part: FLOORBEAM — CORRODED (BS 344)

TUL - FOUND CORROSION ON TOP CHORD OF FLOORBEAM FS 344 RBL 20 TO LBL 40. REPAIRED DAMAGED AREA OF TOP CHORD FLOORBEAM WITH SPLICE AND REPAIR ANGLES PER SRM 53-10-8 PAGE 49-53. (M)

Part: STIFFENER — CRACKED (BS 1183)

TUL - FOUND CRACK ON RIGHT SIDE OF VERTICLE STIFFENER STATION 1183, RBL 38 WL 239 (INBOARD SIDE OF STIFFENER). INSTALLED REPAIR DOUBLER PER BOEING S/B 727-53-0192 AND DRAWING 65C34406. (M)

Part: FRAME — DENTED (BS 990)

TUL - BELL FRAME DENTED. SRM 51-40-3, TREATED AND PRIMED SRM 51-10-2. (M)

Part: STRINGER — CRACKED (BS 720)

TUL - FOUND STRINGER 15L CRACKED JUST AFT OF ICE LIGHT. REMOVED CRACK AREA OF STRINGER AND REPAIRED PER SRM 53-10-3 FIG 5. (M)

Part: FRAME — DENTED (BS 1010)

TUL - FOUND BELL FRAME DENTED STATION 1010, BETWEEN STRINGER 26 LT AND 25 LT. INSTALLED BELL FRAME DOUBLER AT STATION 1010, BETWEEN STRINGER 26 LT AND 26 RT PER SRM 51-40-3. (M)

Part: SHEAR TIE — CORRODED (BS 950)

TUL - FOUND CORROSION ON SHEAR TIE STATION 950B BETWEEN STRINGER 28RT AND 29 RT. REMOVED DAMAGED SHEAR TIE AND REPAIRED PER SRM 53-10-4. (M)

Part: FRAME — DENTED (BS 700)

TUL - FRAME STATION 700 DENTED ABOVE STRINGER 24R. REMOVED DAMAGE, REPAIRED DOUBLER SRM 51-40-3, FIG 1 SHEET 3 7075-T6, .063 INCH, 10 INCH DOUBLER, .375 AND .25 FASTENERS 20 EACH MS204700 RIVETS 2 ROWS ON SIDE, 1 ROW ON TOP. (M)

Part: SKIN — CORRODED (BS 1010-1015)

TUL - FOUND CORROSION ON FUSELAGE BELLY SKIN UPPER SURFACE OUTBOARD OF STRINGER 28 LT STATION 1010-1015, EXTENDING BELOW STRINGER 28 LT. REMOVED DAMAGED SKIN, INSTALLED FUSELAGE SKIN EXTERNAL REPAIR PER SRM 53-30-3 PAGE 14 FIG 3A, 8 INCHES BY 10 INCHES 7075 T-6 .080. (M)

Part: FRAME — DENTED (BS 520)

TUL - FRAME AT STATION 520 DENTED ABOVE STRINGER 23R. INSTALLED FRAME REPAIR PER SRM 51-40-3. REMOVED DAMAGE AREA, INSTALLED 13 INCH DOUBLER OF .073 7075-T6 WITH THIRTY FOUR .375 D-RIVETS AND FOUR .25 INCH D-RIVETS, TWO .375 INCH SCREWS AND SIX .375 INCH BOLTS. (M)

Part: FRAME — DENTED (BS 700)

TUL - BELL FRAME DENTED ABOVE STRINGER 24R AT FS 700. INSTALLED DOUBLER REPAIR PER SRM 51-40-3 FIG 1 SHEET 3 USING 7075 T6, .063 INCH, 10 INCH DOUBLER, .375 FASTENERS AND .25 INCH FASTENER, 20 MS2047AA RIVETS, TWO ROWS ON TOP SIDE AND ONE ROW ON TOP.

Part: FRAME — DENTED (BS 1110)

TUL - BELL FRAME DENTED STATION 1110, ABOVE STRINGER 26 RT. INSTALLED .080 7075-T6 DOUBLER OVER 1 INCH CUTOUT, TWO ROWS ON SIDE, ONE ROW ON TOP FLANGE DOUBLER 7.5 INCH BY 2.5 INCH. .375 AND .25 470DD RIVETS PER SRM 51-40-3 PAGE 1-4. (M)

Part: FRAME — DENTED (BS 680)

TUL - FUSELAGE BELL FRAME DENTED ABOVE STRINGER 23-24R AT FS 680. INSTALLED REPAIR DOUBLER PER SRM 51-4-3 FIG 1 PAGE 3 USING 7075-T6, .063 INCH THICK, 8 INCH DOUBLER, 21 MS20470D06 RIVETS TWO ROWS PAST DAMAGE AND ONE ROW ON TOP WITH 3 RIVETS AT EACH END. (M)

Part: FRAME — BENT (BS 580)

TUL - FRAME 580 BENT STRINGER 23L-25L. REMOVED DAMAGE, MADE DOUBLER AND INSTALLED PER SRM 51-40-3 PAGE 3 FIG 1 DOUBLER IS .5 INCH LONG. 7075-T6, .063 T, .375 AND .25 MS2407DD RIVETS, 31 TOTAL, 4.25 INCHES AT TWO ROWS AND ONE ROW ON TOP. (M)

Part: SHEAR TIE — CRACKED (BS 540)

TUL - SHEAR TIE CRACKED AT STATION 540 BETWEEN STRINGER 17L AND 16L. REMOVED AND REPLACED SHEAR TIE AT FS 540 BETWEEN STRINGER 17L AND 16L PER SRM 51-10-1. (M)

Part: ANGLE — CORRODED (WS 442)

TUL - THREE INCH CORROSION SPOT LOWER CHORD BOTTOM SIDE SURFACE AT NR 8 FLAP TRACK ATTACH AREA REAR SPAR. REMOVED CORROSION, ALODINED AND PRIMED. INSTALLED 2024 T-3 .071 THICK DOUBLER USING EXISTING PATTERN, THREE ROWS HIGH LOCKS .375 AROUND BLEND AREA, REF ESO 11697, DATED 8/10/98. (M)

Part: ANGLE — CORRODED (BS 990)

TUL - AFT CARGO DOOR LOWR CUTOUT CHORD ANGLE CORRODED AT STATION 990. REMOVED CORROSION, INSTALLED DOUBLER IAW ESO 11697, 2/13/98 AND SRM 51-40-4 PAGE 1 AND 2. (M)

Part: ANGLE — CORRODED (BS 950)

TUL - AFT CARGO DOOR LOWER CUTOUT CHORD ANGLE CORRODED AT STATION 950E. REMOVED CORROSION, INSTALLED DOUBLER IAW ESO 11697, 8/13/98 AND SRM 51-40-4 PAGE 1 AND 2. (M)

Part: STRINGER — CORRODED (BS 1148)

TUL - FOUND CORROSION IN STRINGER 23 RT, AT STATION 1148. REMOVED STRINGER 23R, STATION 1141-1155, SPLICED IN NEW SECTION PER SRM 53-10-3 FIG 1 SHEET 1 PAGE 3. (M)

Part: SENSOR — DEFECTIVE (RT MLG)

MIA - FLT 1193 - AFTER GEAR RETRACTION, THE RIGHT GEAR RED AND GREEN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOWNLOCK SENSOR. PERFORMED GEAR RETRACTION WITH NO DEFECTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

RDU - DURING OVERNIGHT CHECK, AFT AIRSTAIR EMERGENCY LIGHT DID NOT ILLUMINATE. REPLACED AFT AIRSTAIR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

TUL - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS DIM AND INTERMITTENT IN MAIN CABIN. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP JUMPER WIRE AT FIRST CLASS/MAIN CABIN DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (BS 950)

TUL - STRINGER 29 LEFT, OUTBOARD LEG OF STRINGER IS CORRODED AT STATION 950E PLUS 2 INCHES, AND 950 E PLUS 18 INCHES, AT FASTENERS EACH END BAY. REMOVED CORROSION, REMOVED ALL FASTENER STATION 950E TO 950F. INSTALLED STRAP 7075-T6 BY .063 THICK WET WITH SEALER. REINSTALLED 1ST O/S HI-LOKS. ALL FASTENER HOLES, SEALED AROUND EDGES. REF ESO 11697 DATED 2-26-97. (M)

Part: SKIN — CORRODED (BS 700-720)

TUL - FOUND CORROSION ON BOTTOM OF FUSELAGE SKIN BETWEEN STATION 700 PLUS 720. REMOVED CORROSION, ALODINED AND PRIMED, THEN INSTALLED SKIN DOUBLER FROM STATION 680 TO 720 (INCORPORATED PREVIOUSLY INSTALLED DOUBLER) IAW SRM 53-30-3. (M)

Part: FLOOR BEAM — CORRODED (BS 1130)

TUL - FOUND TOP OF FLOOR BEAM CORRODED, RBL 20 INCHES TO WS 70. INSTALLED REPAIR STRAPS PER 53-10-7-1 PG 1 3727 AARD/MS/MG. (M)

Part: STRUT — NEEDED REPACK (NLG)

DFW - FLRN NR 1310 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, THE DOORS LIGHT ABOVE THE LANDING GEAR HANDLE REMAINED ILLUMINATED WITH CORRESPONDING NOSE LANDING GEAR DOOR LIGHT ILLUMINATED ON F/E PANEL. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO DFW, LANDING WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR STRUT AND REPLACED UPPER GLAND NUT. SERVICED NOSE LANDING GEAR STRUT WITH OIL AND NITROGEN. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAM — SEPARATING (SLIDE)

ORD - DURING SLIDE SHOP RECEIVING INSPECTION, EMERGENCY EVACUATION SLIDE, P/N 31073105, SEAMS AT BOTTLE HOLDER FOUND SEPARATING. REGLUED AND PATCHED BOTTLE HOLDER SEAMS DURING SHOP REPAIR PROCESS. (M)