N881AA

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED AT THE AFT LOWER HOLE FOR THE WIRE BUNDLE INBOARD OF THE 13TH STAGE MODULATING VALVE. STOP DRILLED CRACK AND INSTALLED DOBLER PER ESO 11697 6-2-00. (M)

Part: SKIN — CORRODED (WING)

TUL - FOUND HEAVY CORROSION ON LOWER AFT SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER AT BS 850 RBL 30. INSTALLED LOWER WING SKIN REPAIR IAW ESO 91697 DATED 6/2/00 AND SRM 51-30-3. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 26-27 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - FOUND LIGHT FAILED TO ILLUMINATE WHEN EMERGENCY EXIT LIGHT SWITCH TURNED ON. REPLACED LIGHT ASSY WITH SERVICEABLE UNIT IAW MM 33-50-01. (M)

Part: LENS — DAMAGED (CABIN)

TUL - FOUND AISLE LIGHTING IN POOR CONDITION , LENS DAMAGED. REPLACED DAMAGED SECTIONS IAW MM 33-50-01. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - FOUND OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE AT FS 1340. REMOVED AND REPLACED LIGHT ASSY AND PERFORMED OPS CHECK IAW 33-50-01. (M)

Part: LIGHT — INOPERATIVE (AFT AIRSTAIR)

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

Part: WIRE — BROKEN (CABIN)

ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROW 18 DEF THROUGH 20 DEF INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN EMERGENCY EXIT ROWS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPAR — CORRODED (HORIZ STAB)

TUL - LEFT HORIZONTAL STAB REAR SPAR UPPER CHORD CORRODED FORWARD OF NR 1 BALANCE PANEL STATION 33-34. BLENDED CORROSION PER ESO 11697, PAGES 1 AND 2, DATED 8-2-00. TREATED, PRIMED, SEALED AND PAINTED AREA. (M)

Part: STIFFENER — CORRODED (BS 920)

TUL - STATION 920 STIFFENER AT INBOARD W/W WALL CORRODED AT NUTPLATE LOWER FORWARD CORNER OF APU AIR INTLET SCREEN. REMOVED CORROSION. INSTALLED REPAIR DOUBLER PER SRM 51-40-3. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT MIDDLE OF COACH INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, MID-CABIN EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE FOR MID-CABIN EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — INOPERATIVE (AIRSTAIRS)

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

Part: WIRE — BROKEN (CABIN)

ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. SPLICED EMERGENCY EXIT FLOOR PATH LIGHTING BROKEN WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT AIR STAIRS)

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

Part: SKIN — CORRODED (BS 480-500)

TUL - FOUND CORROSION ON SKIN UNDER INTERCOSTAL AT LBL 8. INSTALLED DOUBLER REPAIR PER SRM 53-30-3. (M)

Part: FLOORBEAM — CORRODED (BS 344)

TUL - CORROSION AT FLOORBEAM AT STA 344 FROM LBL 24 TO RBL 24. INSTALLED FLOORBEAM REPAIR PER ESO 11697 AT STA 344. ESO DATED 7-28-98. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: STRINGER — CRACKED (BS 720)

TUL - STR 15R CRACKED AT END TO FIRST FASTENER AT FS 720B. REPAIRED PER SRM 53-20-3 FIG 5. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: STRINGER — CORRODED (BS 680)

TUL - STR 27R OUTBOARD LEG CORRODED AT STA 680. REMOVED STRINGER SECTION, SPLICED NEW SECTION PER SRM 53-10-3 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: STRINGER — CORRODED (BS 1076)

TUL - STR 27R CORRODED AT OUTBOARD END STA 1076. INSTALLED STRINGER REPAIR AT STA 1076 PER SRM 53-10-3 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: FRAME — CRACKED (BS 480)

TUL - BELT FRAME CRACKED 1 INCH LONG FROM RIVET TO STRINGER. CUT OUT RADIUS, STA 1180, STR 26R. INSTALLED REPAIR PER SRM 51-40-2 FIG 1 USING 7075T6 MATERIAL, .063 INCH THICKNESS WITH 2 ROWS FASTENERS, .1875 INCH HI-LOCKS, AROUND DAMAGE, .75 INCH SPACE BETWEEN FASTENERS. STOP DRILLED CRACK WITH .25 INCH. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: STRINGER — CRACKED (WS 656)

TUL - FOUND CRACK IN STRINGER NR 8 AT RIB ATTACHMENT TOP OF RIB. INSTALLED STRINGER REPAIR PER SB 727-57A159. (M)

Part: STRINGER — CORRODED (BS 595)

TUL - CORROSION ON STR 28R OUTBOARD SIDE STA 595. INSTALLED STRINGER SPLICE SECTION REPAIR PER SRM 53-10-3 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: STRINGER — CRACKED (BS 720)

TUL - STR 15L CRACKED AT END TO FIRST FASTENER FORWARD 4 INCHES OF FS 720C. REPAIRED PER SRM 53-10-3 FIG 5. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: FRAME — DENTED (BS 580)

TUL - BELT FRAME STA 580 UPPER LIP DENTED BETWEEN STR 24L AND STR 23L (DISTORTED WEB). REPAIRED PER SRM 53-10-4 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: SKIN — CORRODED (FUSELAGE)

TUL - SKIN UNDER INTERCOSTAL CORRODED JUST OUTBOARD OF FORWARD CARGO. INSTALLED REPAIR PER SRM 53-30-3 FIG 3. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: SKIN — CORRODED (BS 1075-1086)

TUL - BELLY SKIN CORROSION UNDER STR 27R, STA 1075 - STA 1086. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: FRAME — CRACKED (BS 380)

TUL - BELL FRAME CRACKED STA 380 BETWEEN STR'S 7-8, RT SIDE. REPAIRED FRAME PER SRM 53-10-4 FIG 2. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: STRINGER — CORRODED (BS 720-740)

TUL - STR 27R CORRODED STA 720F + 4 INCHES TO STA 740. INSTALLED STRINGER SPLICE PER SRM 53-10-3 PG HB FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: STRINGER — CORRODED (BS 663)

TUL - STR 27R OUTBOARD LEG CORRODED TOP EDGE STA 663. REPAIRED PER SRM 53-10-3 FIG 2. TST: 53,245 HOURS. CYCLES: 32,117. (X)

Part: SPAR — CORRODED (WS 300-305)

TUL - FRONT SPAR LOWER CHORD CORRODED BELOW NR 1 KRUGER FLAP ACTUATOR FS 300 TO 305. INSTALLED REPAIR PER AARD 57-30-00-2 PAGE 1-3. (M)

Part: SKIN — CORRODED (BS 580-600)

TUL - FOUND CORROSION ON FUSELAGE SKIN UNDER INTERCOSTAL AT STRINGER 28R, STATION 580 - STATION 600. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. (M)

Part: STRINGER — CRACKED (BS 344)

TUL - FOUND STATION 344 STRINGER 5 RT BACKSIDE OF STRINGER CRACKED TWO PLACES UPPER AND LOWER. CUTOUT DAMAGED AREA. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 3 THROUGH 4B. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT SECTION OF COACH EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN AFT COACH SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT COACH INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LGHT STRIP IN AFT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — NOT REMOVED (NLG)

DTW - FLT 1765 - AFTER TAKEOFF FROM DTW, NOSE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REMOVED NOSE GEAR PIN THAT WAS STILL INSTALLED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FLAP TRACK — OVERSIZED HOLE (TE FLAP)

AFW - FLAP TRACK NR 4 BOLT HOLE REAMED TO .689. BUSHINGS CAP PLATED WITHOUT NICKLE STRIKE. REQUEST ENGINEERING APPROVAL. REPAIRED PER MRB 727-0028. (M)

Part: STRINGER — CORRODED (BS 1018)

AFW - FOUND STRINGER 29R AT APPROX STATION 1018 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 727-0027. (M)

Part: STRINGER — CORRODED (BS 525)

AFW - FOUND CORROSION ON STRINGER. INSTALLED REPAIR PER SRM 53-10-3. (M)

Part: SKIN — CORRODED (BS 580)

AFW - FOUND BULGE IN SKIN AT FUSELAGE. INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: STRINGER — CORRODED (BS 720)

AFW - FOUND CORROSION IN STRINGER FORWARD CARGO STRINGER 27R. INSTALLED STRINGER SPLICE PER SRM 53-10-3. (M)

Part: FAN — DEFECTIVE (CABIN)

DFW - FLT 942 - EN ROUTE MAI/DFW DURING CRUISE, SLIGHT SULPHUR ODOR NOTED FROM GASPER. ACCOMPLISHED ABNORMAL PROCEDURE. WHEN BUS TIE BREAKERS TO GASPER TRIPPED, ODOR DISSIPATED. AIRCRAFT PROCEEDED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED GASPER FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (BS 344)

TUL - FOUND STATION 344, RIGHT INBOARD SEAT TRACK HAS CORROSION AT ATTACH POINT TO FLOOR BEAM UPPER FLANGE OF TRACK, INBOARD AND OUTBOARD SIDES. REMOVED CORRODED SECTION. SPLICED IN NEW SECTION SRM 53-10-5, FIG 7. (M)

Part: SUPPORT — CORRODED (BS 364-380)

TUL - FOUND STATION 364 TO 380 RBL 12 FLOOR BOARD SUPPORT BEAM CORRODED ON UPPER FLANGE. REMOVED FLOOR SUPPORT BEAM, INSTALLED NEW FLOOR SUPPORT BEAM. (M)

Part: STOP — CORRODED (BS 420)

TUL - FOUND STATION 420 RIGHT SIDE OF CABIN SEAT TRACK STOP BLOCK CORRODED ON INBOARD AND OUTBOARD FLANGES IN FRONT OF THE SHORT 40 INCHES SECTION OF SEAT TRACK JUST INBOARD OF CREASE ANGLE. REMOVED AND DELETED SEAT TRACK STOP BLOCK PER SRM 53-10-2 PG 44N (A). (M)

Part: SEAT TRACK — CORRODED (BS 360)

TUL - FOUND STATION 360 RBL 55 SEAT TRACK CORRODED ON INBOARD FLANGE TOP SIDE. INSTALLED NEW SEAT TRACK FROM STATION 344-380, RT RBL 55. (M)

Part: SEAT TRACK — CORRODED (BS 420-460)

TUL - FOUND STATION 420 TO 460, RIGHT SIDE OF CABIN 40 INCHES SHORT SECTION OF SEAT TRACK CORRODING INSIDE CHANNEL, ENTIRE LENGTH. REMOVED AND DELECTED SEAT TRACK FROM STATION 420 TO 460 RT PER SRM 53-10-2 PG 44. (M)

Part: SUPPORT — CORRODED (BS 418)

TUL - FOUND STATION 418 FLOOR SUPPORT CORRODED FROM OUTBOARD SIDE OF OUTBOARD SEAT TRACK TO CREASE ANGLE. REMOVED FLOOR SUPPORT AND INSTALL NEW SUPPORT. (M)

Part: SKIN — CORRODED (WS 474-494)

TUL - FOUND CORROSION ON LOWER LE WING SKIN EXTENSION LFSS 474-LFSS 494. REMOVED CORROSION, TREAT, PRIME AND INSTALLED REPAIR DOUBLER PER AARD 5730 00 2 PAGE 1 FIG 1. (M)

Part: FLOOR BEAM — CORRODED (BS 380)

TUL - FOUND STATION 380 FLOOR BEAM HAS CORROSION AT RBL 55-60 (TOP FLANGE). REMOVED CORRODED SECTION. INSTALLED FILLER AND DOUBLER PAINTED AND TREATED SRM 53-10-8 PG 9 C, D, E. (M)

Part: SEAT TRACK — CORRODED (BS 1110-1130)

TUL - FOUND CORROSION ON SEAT TRACK STATION 1110 TO 1130 LEFT OUTBOARD. REPLACED SEAT TRACK, LEFT OUTBOARD STATION 1110 TO 1130. (M)

Part: FLOOR BEAM — CORRODED (BS 380)

TUL - FOUND STATION 380 FLOOR BEAM HAS CORROSION AT RBL 32-37. CUT OUT CORRODED SECTION. INSTALLED NEW SECTION SRM 53-10-8 PAGE 9C-E. (M)