N730AA

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND TOP FLANGE UPPER SURFACE FLOORBEAM 380 CORRODED RBL 11 INCHES TO RBL 63 INCHES. REMOVED CORROSION. INSTALLED DOUBLER REPAIRS PER SRM 53-10-8. (M)

Part: FLOORBEAM — MISDRILLED (FUSELAGE)

TUL - FOUND FLOORBEAM MISDRILLED AT GALLEY TRACK FASTENER HOLE STATION 360 RBL 43. INSTALLED REPAIR PER ESO 11697 DATED 11/13/00. (M)

Part: STRINGER — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON STRINGER 18A SHELF AT STATION 913 LEFT WHEEL WELL. INSTALLED DOUBLER PER ESO 11697, 11-9-2000. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON TOP FLANGE OF FLOORBEAM STATION 344 RBL 19. INSTALLED REPAIR ANGLE DOUBLER ON UPPER FLANGE OF FLOORBEAM 344, RBL 11 TO RBL 22 PER SRM 51-40-4. (M)

Part: LIGHT — SHORTED (CABIN)

DCA DURING OVERNIGHT MAINTENANCE AFT EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED AFT EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEMS GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA DURING OVERNIGHT MAINTENANCE R1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED R1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEMS GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS AT MID CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT STRIP AT SEAT 27D AND 28D. SYSTEMS GROUND CHECKED NORMAL OPERATION.

Part: ACCESSORY UNIT — DEFECTIVE (LT MLG)

DCA - FLT 1029 - EN ROUTE IAD-MIA, LEFT MAIN GEAR RED LIGHT STAYED ON AFTER GEAR RETRACTED. CYCLED GEAR, NO CHANGE. LANDED DCA WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY UNIT PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIR)

DFW DURING OVERNIGHT MAINTENANCE AIR STAIR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS IN FIRST CLASS AND FORWARD PART OF COACH INOPERATIVE. REPLACED CONNECTOR IN ROW FORWARD OF EMERGENCY OVERWING EXIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND STATION 825 RBL 55, WEB CRACKED FROM LIGHTENING HOLE TO FASTENER HOLE, OVERWING FLOORBEAM. REPAIRED WEB PER SRM 51-40-2, INSTALLED DOUBLER. (M)

Part: SKIN — CORRODED (BS 580)

TUL- CRACK STA 580, STR 27L, FUSELAGE SKIN. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 PAGE 11. TST: 72,099.47 HOURS. CYCLES: 46,542. (X)

Part: SKIN — DENTED (BS 410)

TUL - SHARP DENT FROM WITHIN IN FUSELAGE SKIN AT BS 410 BETWEEN STR 22 AND STR 23R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3, PAGE 7. TST: 72,099.47 HOURS. CYCLES: 46,524. (X)

Part: LIGHT — DEFECTIVE (AFT STAIRWAY)

DFW - DURNG OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT BOTTOM OF AFT STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — DENTED (BS 680)

TUL - LEFT SIDE BELTFRAME DENTED AND BULGED ON SIDES AT STATION 680 BETWEEN STRINGER 22L AND 23L. REMOVED DAMAGED AREA OF FRAME AT STATION 680 LEFT BETWEEN STRINGER 22L AND 23L AND INSTALLED DOUBLER PER SRM 51-40-3 PAGE 2. (M)

Part: SKIN — CORRODED (SERVICE DOOR)

TUL - RIGHT AFT SERVICE DOOR FRAME SKIN HAS HEAVY CORROSION AT APPROX 56 INCHES ABOVE FLOOR LINE. REPAIRED WITH EXTERNAL FUSELAGE DOUBLER AND TRIPLER PER ESO 11697, DATED 10/20/98. (M)

Part: FRAME — CRACKED (BS 913)

TUL - FOUND CRACK IN RADIUS AT OUTER FLANGE OF LEFT STATION 913.5 FRAME. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 53-10-2 FIG 3. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ABOVE AIR STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY ABOVE AIR STAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - AFT AIRSTAIR EMERGENCY LIGHT ASSY INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. TST: 67,414.53 HOURS. CYCLES: 44,081. (X)

Part: STRINGER — CRACKED (BS 720)

TUL - STRINGER 15R CRACKED IN U-CHANNEL FROM WING ICE LIGHT END TO FIRST FASTENER STATION 720B. REPAIRED STRINGER PER SRM 53-10-03 FIG 1 SHEET 4, DETAIL 2. (M)

Part: ANGLE — CORRODED (BS 957)

TUL - BOLTS AND ANGLES CORRODED AT THE LEFT SIDE OF KEEL BEAM AT THE EXTENSION FITTING AT BS 957. BLENDED OUT ALL CORROSION, REPLACED ANGLE WITH NEW ONE. RE-INSTALLED ALL BOLTS ON KEEL BEAM, TREATED AND PRIMED PER MM 51-20-0. (M)

Part: STRINGER — CRACKED (BS 740)

TUL - FOUND STRINGER 27R CORRODED AND CRACKED STATION 740. CUT OUT DAMAGED AREA OF STRINGER. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-10-3. (M)

Part: SKIN — CORRODED (BS 320-325)

TUL - BULDGING SKIN AT LOWER FLANGE OF THE FORWARD LAV SERVICE PANEL BS 370-325 AND STRINGER 20R. CUT OUT CORRODED SKIN BELOW FORWARD LAVATORY SERVICE PANEL AND INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: STRINGER — CRACKED (BS 720)

TUL - STRINGER 15R CRACKED IN U-CHANNEL FROM WING ICE LIGHT END TO FIRST FASTENER AT STATION 720C. REPAIRED STRINGER PER SRM 53-10-03 FIG 1 SHEET 4 DETAIL 2. (M)

Part: SKIN — CORRODED (BS 940-950)

TUL - FOUND CORROSION AT FORWARD EDGE OF JOINT BETWEEN STRINGER 18A AND STATION 950 CASTING RT WHEEL WELL. REMOVED 3 SECTIONS OF CORRODED SKIN BETWEEN STATIONS 940 AND 950 AND INSTALLED FILLERS AND DOUBLERS PER ESO 11697 DATED 9-29-97. (M)

Part: SKIN — CORRODED (BS 281-286)

TUL - CRACKS EXTENDING FROM RIVETS AT STATION 9L STATION 281-286. REMOVED CRACKED AREA OF SKIN AND INSTALL FILLER AND REPAIR DOUBLER PER SRM 53-70-3, FIGURE 3. (M)

Part: SKIN — CORRODED (BS 320-325)

TUL - BULDGING SKIN AT LOWER FLANGE OF THE FORWARD LAV SERVICE PANEL, BS 320-325 AT STRINGER 20R. CUT OUT CORRODED SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: SPAR CHORD — CORRODED (BS 560-563)

TUL - LEFT WING FORWARD SPAR LOWER L/E CHORD HAS CORROSION ON LOWER LAND. REMOVED CORROSION TREATED AND PRIMED AREA APPLIED DOUBLER PER AARD 57-30-00-2. (M)

Part: FRAME — DENTED (BS 950)

TUL - BELT FRAME DENTED ABOVE STRINGER 26L STATION 950C. REMOVED DAMAGED AREA OF BELT FRAME FAB REPAIR PIECE ASSY PER SRM CH 53-10-4 PAGE 1-6. (M)

Part: BULKHEAD WEB — CORRODED (BS 1183)

TUL - FOUND CORROSION UNDER STIFFENER ON 1183 BULKHEAD RBL 18 INCHES, 22 INCHES UP. REPAIRED WEB WITH DOUBLER SRM PER 53-10-9, PAGE 11 FIG 4. (M)

Part: FRAME — DENTED (BS 1030)

TUL - BELT FRAME DENTED AT STATION 1030 BETWEEN STRINGER 27 AND 26R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-10-4 PAGE 1-6. (M)

Part: FLOORBEAM — CORRODED (BS 344)

TUL - FOUND CORROSION TOP AND BOTTOM OF FORWARD UPPER CHORD OF STATION 344 FLOORBEAM FROM LBL 12 INCHES - RBL 12 INCHES. REMOVED CORROSION, INSTALLED REPAIR PER SRM 53-10-8 FIG 7 AND ESO 11697, DATED 10-6-97. (M)

Part: CHORD — CORROSION (BS 640-643)

TUL - LOWER LEADING EDGE CHORD EXTRUSION HAS CORROSION AT LE STATION 640 TO 643. FABRICATED DOUBLER AND INSTALLED PER AARD 57-30-0-2 AFTER CORROSION REMOVAL TREATED AND PRIMED AREA AND DOUBLER. (M)

Part: SKIN — GOUGED (BS 1315)

TUL - LOWER RIGHT TORQUE BOX STATION 1315 OUTBOARD OF INBOARD LOWER CHORD ANGLE INNER FUSE SKIN HAS SEVERAL DEEP GOUGES. REMOVED DAMAGED AREA AND INSTALLED EXTERNAL SKIN PATCH PER SRM 53-30-3 FIG 1 PAGE 5. (M)

Part: DITCHING PANEL — CORRODED (BS 1068)

TUL - DITCHING PANEL CORRODED ON LOWER SIDE AT STATON 1068 BELOW 3 ANGLE FOR LEFT AFT SERVICE DOOR AT F/B SUPPORT ANGLE ATTACH. INSTALLED NEW DITCHING PANEL PER SRM 51-10-1 PAGE 4 DITCHING PANEL WAS TREATED AND PRIMED PER SRM 51-10-2 BEFORE INSTALLATION. (M)

Part: DOWNLOCK — JAMMED (LT MLG)

TUL - FLT 9650 - DURING POST C-CHECK FUNCTIONAL CHECK FLIGHT WHEN LANDING GEAR EXTENDED DURING APPROACH, LT MAIN LANDING GEAR INDICATED UNSAFE. RECYCLED LANDING GEAR WITH SAME RESULTS. ACCOMPLISHED MANUAL LANDING GEAR EXTENSION WITH SAME RESULTS. FLIGHT CREW DECLARED EMERGENCY AND AIRCRAFT LANDED TUL WITHOUT INCIDENT. INSTALLED GEAR PINS AND AIRCRAFT TOWED TO HANGAR. REMOVED ALUMINUM PIECE OF BARSTOCK FROM LT MLG SIDE BRACE UPPER SEGMENT DOWNLOCK MECHANISM. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (X)

Part: LIGHT — DEFECTIVE (AFT STAIRS)

DFW - DURING OVERNIGHT CHECK, OVERHEAD EMERGENCY EXIT LIGHT AT AFT STAIRWAY INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT AT AFT STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

RDU - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT IN AFT STAIRWELL INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN AFT STAIRWELL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXITLIGHT BY FORWARD ENTRY DOOR INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BY FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BEAM — CORRODED (LT MLG)

TUL - FOUND CORROSION ON LOWER SIDE OF LMG BEAM OUTBOARD OF NR 4 FLAP TRACK. REMOVED CORROSION AND WORK AREA PER ESO 11697, DATED 12/4/96. (M)

Part: S-DUCT — CORRODED (BS 1210)

TUL - FOUND CORROSION AT LOWER SIDE OF MATE POINTS FOR UPPER AND LOWER S-DUCTS (WORN DUCTS) 6 O'CLOCK ON DUCT OUTSIDE DIAMETER. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697, DATED 11-26-96. (M)

Part: EEL WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN AND FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN/SHORTED EMERGENCY FLOOR LIGHT WIRE FOR EXIT LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)