N869AA

Part: WEB — CRACKED (FS 1183)

TUL - FOUND CRACK, AFT FACE OF FS 1183 PRESSURE BULKHEAD IN TAIL SKID WELL. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-2. (M)

Part: SKIN — CORRODED (FS 680-720)

TUL - FOUND CORROSION ON SKIN OUTBOARD STRINGER 26L. REPAIRED PER SRM 53-30-3 FIG 14. (M)

Part: SKIN — CORRODED (FS 680-720A)

TUL - FOUND CORROSION 60 INCHES BY 30 INCHES, ON SKIN OUTBOARD OF STRINGER 26R. REPAIRED AREA PER SRM 53-30-3 FIG 14. (M)

Part: BEAM — CORRODED (FS 265-266)

TUL - FOUND STATION 265 LBL CORROSION ON FLOORBEAM. INSTALLED REPAIR PER ESO 11697 DATED 6/25/2001. (M)

Part: STIFFENER — CORRODED (FS 244)

TUL - FOUND VERTICAL STIFFENER CORRODED OUTBOARD OF NR 2 LEADING EDGE FLAP ACTUATOR AT NR 2 TANK PRESSURE SWITCHES AT WFS 244. REPLACED STIFFENER PER SRM 51-10-1. (M)

Part: STRINGER — CORRODED (FS 683-686)

TUL - FOUND STRINGER 26L HAS HEAVY CORROSION AT STATION 683 TO 686, OUTBOARD SIDE OF STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-03. (M)

Part: STRINGER — CORRODED (FS 720B)

TUL - FOUND CORROSION 1 INCH BY 2 INCHES ON INSIDE OF STRINGER 27R. REMOVED CORROSION AND REPAIRED STRINGER PER SRM 53-10-3. (M)

Part: WEB (FS 1250)

TUL - FOUND RIGHT LOWER TORQUE BOX VERTICAL WEB ROUTED OUT AT LIGHTENING HOLE WITHOUT REPAIR. INSTALLED DOUBLER REPAIR ON WEB PER SRM 51-40-2 FIG 1, PAGE 1. (M)

Part: CONNECTOR — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 17 DIM. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — FAULTY (FUSELAGE)

IAH - FLT 1791 - EN ROUTE IAH-MIA - DETECTED LIGHT SMOKE AT FLOOR VENT NEAR ROW 27 DEF. LANDED MIA WITHOUT FURTHER INCIDENT. REPLACED GROUND VENTURI FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (AFT AIRSTAIR)

DFW - AFT STAIR OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (CABIN)

TUL - FOUND CORROSION ON FLOORBEAM AT STATION 380 BETWEEN RBL 23 AND RBL 63. INSTALLED DOUBLER ON FLOORBEAM PER SRM 53-10-08 PAGE 9B. (M)

Part: LAP JOINT — CRACKED (FUSELAGE)

TUL - FOUND LFEC SHOWS CRACK LOWER ROW OF RIVETS IN SKIN LAP STRINGER 4R AT STATION 585. INSTALLED EXTERNAL DOUBLER AT STATION 585 STRINGER 4R PER SRM 53-30-3. (M)

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON LOWER CHORD OF RBL 40.5 FRAME BETWEEN STATION 868 AND STATION 870. INSTALLED REPAIR PER SRM 51-40-4 FIG 1 SHEET 8. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - LFEC AND HFEC SHOWS CRACK IND AT LOWER ROW OF RIVETS STRINGER NR 4, STATION 451, 431, 428, 448, 427. INSTALLED REPAIR DOUBLER AT STRINGER 4 LEFT STATION 421-455 IAW SRM 53-30-3 PART 1 FIG 5. (M)

Part: SPAR — CORRODED (HORIZONTAL STAB)

TUL - FOUND RIGHT HORIZONTAL CORRODED ON TOP REAR SPAR CHORD 20 INCHES FROM INBOARD END. INSTALLED DOUBELR PER ESO 11697, DATED 6-13-2000. (M)

Part: WIRE — LOOSE (AFT AIRSTAIR)

MIA - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHTING INOPERATIVE. SECURED WIRE CONTACT ON AFT STAIR EMERGENCY EXIT LIGHTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: TRIM TAB — DEFECTIVE (RT AILERON)

MIA - FLT 1360 - EN ROUTE MIA/DCA AT 30,000 FEET WITH AIRSPEED OF 305 KNOTS AND ECON CLIMB THERE WAS A NOTICEABLE FLUTTER IN YOKE. INSPECTED AILERON IN-FLIGHT AND NOTICED RIGHT INBOARD AILERON FLUTTER APPROXIMATELY 3 SECONDS AFTER A TURN IN EITHER DIRECTION. AIR INTERRUPTED AND LANDED MCO WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT TO MIA FOR FURTHER EVALUATION OF AILERON FLUTTER. FERRY FLIGHT TO MIA AND LANDED WITHOUT INCIDENT. REPLACED RIGHT INBOARD AILERON TRIM TAB AND ADJUSTED PER MM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - FORWARD GALLEY 36 INCH LENGTH OF SEALED EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED SECTION OF LIGHT ASSEMBLY, FOUND BROKEN WIRE (E583053872). (M)

Part: BATTERY — DIRTY (AFT AIRSTAIR)

DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CONTACTS AT BATTERY PACK AND BATTERY CHARGER FOR AFT AIRSTAIR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CORRODED (CARGO DOORWAY)

TUL - FOUND BOTTOM OF FRAME CORRODED. REMOVED CORRODED SHEAR TIE AND LEG FROM LOWER FRAME STATION 600, STRINGER 27R-28R PER SRM 53-10-4 FIG 13. FABRICATED AND INSTALLED FRAME REPAIR FOR SHEAR TIE AND LEG PER SRM 53-10-4 FIG 13. (M)

Part: FRAME — CRACKED (CARGO DOORWAY)

TUL - FORWARD FROM WEB FOR DOOR CUTOUT HAS CRACK EXTENDING ON BOTH SIDES OF FLUSH RIVET HOLE JUST ABOVE UPPER DOOR STOP CASTING. STOP DRILLED CRACKS IAW SRM 51-10-1. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-40-2 FIG 1. (M)

Part: STIFFENER — CORRODED (WS 265)

TUL - FRONT SPAR VERT STIFFENER CORRODED AT TOP JUST OUTBOARD OF FUEL PRESS SWITCHES. REMOVED AND REPLACED STIFFENER WITH 6 EACH , STEEL HI-LOCKS HL62, 7 EACH STEEL HI-LOCKS HL62 PER SRM 51-10-1 AND SAME PART NR STIFFENER. (M)

Part: LIGHT — DEFECTIVE (CABIN)

TPA - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR DOES NOT TEST. REPLACED EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACTUATOR — LEAKING (NLG)

DFW - FLT 1654 - DURING APPROACH, UNABLE TO EXTEND NOSE GEAR ON FIRST ATTEMPT BUT, EXTENDED NORMALLY ON SECOND ATTEMPT. FLIGHT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE GEAR UNLOCK ACTUATOR LEAKING. REPLACED NOSE GEAR UNLOCK ACTUATOR. LEAK AND OPERATIONS CHECKS WERE NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - EMERGENCY EXIT LIGHT IN AFT LEFT GALLEY GOES DIM AFTER LIGHT IS TURNED TO ON POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT WITH SERVICEABLE UNIT NR LIG 5192 SN ON 4307. OPERATION CHECKS NORMAL. TST: 56,854.46 HOURS. CYCLES: 35,139. (X)

Part: STRINGER — CORRODED (BS 562-564)

TUL - STR 27R CORRODED OUTBOARD FLANGE STA 562 - STA 564. STRINGER SECTION REPLACED PER 53-10-3, FIG 1. TST: 55,975 HOURS. CYCLES: 34,667. (X)

Part: FRAME — CORRODED (BS 950)

TUL - BOTTOM FORWARD LEG, 950F, FRAME CORRODED OUTBOARD SIDE STRINGER 29R, AREA PREVIOUSLY REWORKED. REPLACED SHEAR TIE PER SRM 53-10-4. (M)

Part: FLOORBEAM — CORRODED (BS 380)

TUL - FOUND CORROSION ON TOP OF FLOORBEAM STATION 380 RBL 33-38. INSTALLED DOUBLER AND FILLER PER SRM 53-10-8 PAGES C-D AT STATION 380 RBL 33-38. (M)

Part: STRINGER — BROKEN (BS 343)

TUL - FOUND STRINGER 5R BROKEN TOP AND BOTTOM FLANGE AT STATION 343. REPAIRED STRINGER 5R PER SRM 53-10-3. (M)

Part: STRINGER — CORRODED (BS 488)

TUL - INSIDE OF STRINGER 28R CORRODED AT END OF SPLICE FS 488. REPAIRED STRINGER PER SRM 53-10-3. (M)

Part: SKIN — CORRODED (BS 480-484)

TUL - FOUND STATION 480-484 INBD STRINGER 27L CORROSION BETWEEN STRINGER AND INTERCOSTAL ON CIRCUMFERENTIAL STRAP ON BILGE SKIN. REPAIRED SKIN PER SRM 53-30-3. (M)

Part: SKIN — CORRODED (BS 950)

TUL - FOUND CORROSION COMING OUT OF THE SEALANT RIGHT SIDE STRINGER 30 STATION 950E PLUS 2, STRINGER AND SKIN CORRODED. INSTALLED REPAIR IAW SRM 53-30-3 PAGE 13-14A. (M)

Part: SHEAR TIE — CORRODED (BS 700)

TUL - SHEAR TIES ON BOTH SIDES OF BELT FRAME STA 700 OUTBOARD STR 28R CORRODED. REMOVED AND REPLACED SHEAR TIE. TST: 55,973 HOURS. CYCLES: 34,656. (X)

Part: STRINGER — CORRODED (BS 720)

TUL - FOUND CORROSION ON OUTBOARD SIDE OF STRINGER 26R AFT SIDE OF STATION 720D. CUT OUT DAMAGED SECTION OF STRINGER FABRICATED NEW SECTION AND INSTALLED REPAIR SPLICES PER SRM 53-10-3 FIG 1 DETAIL 1. (M)

Part: ANGLE — CORRODED (BS 1212)

TUL - FOUND CORROSION ON CHORD ANGLE AND SPLICE RIGHT SIDE UNDER STEP 5 FROM TOP STATION 1212. REMOVED CORROSION ON CHORD ANGLE AND REMOVED AND INSTALLED FABRICATED ANGLE SPLICE RIGHT PER SRM 51-10-1. (M)

Part: SKIN — CORRODED (BS 480-484)

TUL - FOUND STATION 480-484 CORRODED BETWEEN STRINGER 28L AND INTERCOSTAL, ON BILGE SKIN AND ON CIRCUMFERENTIAL STRAP. CUT OUT CORRODED SKIN AND INSTALLED REPAIR PER SRM 53-30-3. (M)

Part: STRINGER — CORRODED (BS 560)

TUL - FOUND CORROSION ON STRINGE R27R AND STRINGER TIE CLIP AT STATION 560 FORWARD SIDE. REPLACED STRINGER SECTION PER SRM 53-10-3. INSTALLED NEW STRINGER TIE CLIP. (M)

Part: SKIN — FUEL LEAK (WS 810)

TUL - FUEL LEAKING AT FASTENER IN REPAIR ABOVE THE LEFT AFT HEAT EXCHANGER STATION 810 ACM DOOR 32156. REMOVED FASTENER AND OVERSIZED TO ESO 11697 DTD 8-11-97 INSTALLED NEW FASTENER. (M)

Part: STRINGER — CORRODED (BS 700-720)

TUL - FOUND STRINGER 27R CORRODED INSIDE STATION 700-720. INSTALLED NEW SECTION OF STRINGER AND SPLICE PER SRM 53-10-3 FIG 1. (M)

Part: ANGLE — CORRODED (BS 950)

TUL - STATION 950 CHORD ANGLE HAS HEAVY CORROSION JUST OUTBOARD OF RT STRINGER 29 KEEL BEAM EXT. REMOVED AND REPLACED RIGHT STATION 950 LOWER CHORD ANGLE PER SRM 51-10-1 PAGE 4. (M)

Part: STRINGER — CORRODED (BS 700)

TUL - FOUND CORROSION UNDER NUT PLATE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-3 FIG PG 3-4B. (M)

Part: SKIN — CORRODED (BS 700)

TUL - FOUND SKIN BULGED, RIVET HEADS DISHED. REMOVED AND REPLACED SHEAR TIE. (M)

Part: STRINGER — CORRODED (BS 950)

TUL - CORROSION ON STR 29L, STA 950. TREATED AND PRIMED BLENDED AREA, INSTALLED REPAIR STRAP PER ESO 11697. TST: 55,973 HOURS. CYCLES: 34,656. (X)

Part: SKIN — CORRODED (BS 480)

TUL - SKIN CORRODED BETWEEN STA 480 AND STA 500 BETWEEN STR 27R AND STR 28R. REPAIRED SKIN PER SRM 53-30-3. TST: 55,973 HOURS. CYCLES: 34,656. (X)

Part: SHEAR TIE — CORRODED (BS 500)

TUL - OUTBOARD OF STRINGER 28L STATION 500 SHEAR TIE ON FWD SIDE OF FRAME CORRODED FROM STRINGER 28L AND STRIGNER 27L. REPAIRED SHEAR TIE PER SRM 53-10-4. (M)

Part: BEAM — CORRODED (BS 1176)

TUL - INTERGRANULAR CORROSION ON 1176 CHORD ANGLE RIGHT AFT LAV FLOOR AT CABLE TIE DOWN RB46. REPAIRED CHORD ANGLE 1176 PER ESO 11697 DATED 8/11/97 AT RBL 46. (M)

Part: FRAME — CORRODED (BS 950)

TUL - FRAME BENT DOWN AND BULGED OUT FORE AND AFT SIDES. CUT OUT DAMAGED AREA FABRICATED REPAIR DOULER IAW SRM 53-10-4 PAGE 3-6. (M)

Part: SHEAR TIE — CORRODED (BS 500)

TUL - FOUND CORROSION ON SHEAR TIE STATION 500, FORWARD SIDE OF FRAME OUTBOARD OF STRINGER 28R TO 27R. SHEAR TIE REPAIRED PER SRM 53-10-4. (M)

Part: STRAP — CORRODED (BS 480)

TUL - CORROSION ON CIRCUMFERENTIAL STRAP AT FS 480 AFT SIDE FROM STATION 28L. REPAIRED CIRCUMFERENTIAL STRAP PER ESO 11697 DATED 8/14/97. (M)

Part: STRINGER — CORRODED (BS 950)

TUL - FOUND CORROSION REPAIR STRINGER 29R CORRODED OUTBOARD LEFT FROM STATION 950D PLUS 17 TO 950E PLUS 3. ROUND OUT CORROSION MANUFACTURED DOUBLER IAW ESO 11697. (M)

Part: KEEL BEAM — CORRODED (BS 950)

TUL - OUTBOARD STRINGER 29L AT STATION 950A PLUS 3 CORRODED. INSTALLED REPAIR IAW BOEING SB 727-53-0179 DATED JULY 13, 1989 NOTE PAGE 45. (M)

Part: SKIN — CORRODED (BS 660)

TUL - FOUND CORROSION ON LOWER BELLY SKIN AT STATION 660-666 BETWEEN STATION 28R AND 28L. REMOVED SECTION OF SKIN AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3 FIG 1. (M)

Part: FRAME — CORRODED (BS 500)

TUL - FOUND STATION 500 FORWARD SIDE OF FRAME BETWEEN STRINGER 27L AND 28L FRAME CORRODED, ALSO CORROSION BETWEEN STRINGER 27L AND INTERCOSTAL BETWEEN STR 27L AND 28L. REPAIRED FRAME STATION 500 FWD, STRINGER 27L - 28L PER SRM 53-10-4, REPAIRED SKIN AT INTERCOSTAL PER SRM 53-30-3. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD PART OF MAIN CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT FRONT OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — FAILED (SYS B NR 1)

DFW - FLT 440 - AFTER TAKEOFF DFW, DURING INITIAL CLIMB-OUT, LOST HYDRAULIC SYSTEM B. ACCOMPLISHED ABNORMAL PROCEDURES FOR LOSS OF SYSTEM B-HYDRAULICS AND DUMPED FUEL. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED HYDRAULIC SYSTEM B NR 1 PUMP. SERVICED HYDRAULIC SYSTEM. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. HYDRAULIC PUMP REPLACED DUE SPLIT CASE AND THREE NUTS AND STUDS MISSING. (M)

Part: LIGHT — DEFECTIVE (CABIN)

JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIGN OVER AFT GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY OVER AFT GALLEY DOOR. SYSETM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACTUATOR — DEFECTIVE (NLG)

TUL - FLT 1923 - AFTER TAKEOFF TUL DURING GEAR RETRACTION, THE GEAR DOOR LIGHT STAYED ON AS WELL AS THE RED NOSE GEAR LIGHT. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR RETRACT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: SKIN — CORRODED (VERT STAB)

TUL - FOUND 1 INCH CRACK IN LEFT SIDE OF VERTICAL STABILIZER SKIN EXTENDING FROM FASTENER HOLE, FS 1212. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO11697 DATED 6-23-95. (M)

Part: FLOOR BEAM — CORRODED (FS 380)

TULE - FOUND CORROSION ON UPPER FLANGE OF FLOOR BEAM STATION 380 RIGHT SIDE, APPROX 12 INCHES INBOARD OF INBOARD SEAT TRACK OUTBOARD TO THE DOOR CUTOUT. REPAIRED FLOOR BEAM PER SRM 53-10-8 AT STATION 380 RIGHT SIDE. (M)

Part: SKIN — CORRODED (FS 836)

TUL - FOUND CORROSION ON LOWER SKIN OF CENTER WING SECTION ABOVE LEFT PRIMARY HEAT EXCHANGER FS 836 AND LBL 31. SMOOTH BLEND CORROSION, EDDY CURRENT THICKNESS CHECK, FLAP/SHOT PEN, ALODINE, LPS-3/AV8 PER ESO 11697 DATED 12/5/95. (M)