N496AA

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 71,453 hrs · 37,431 cycles

LEFT WING NR 4 SLAT TRACK LE INBD SUPPORT RIB CRACKED. INSTALLED DOUBLER IAW CARD 57-98-04.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,887 hrs · 37,106 cycles

EMERGENCY EGRESS LIGHT BATTERY PACK AB5 - 4 INOPERATIVE. REPLACED BATTERY PACK AB5 - 4, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,887 hrs · 37,106 cycles

EMERGENCY EVACUATION LIGHTS IN TAIL COMPARTMENT SECTION FAILED TEST. REPLACED BATTERY PACK FOR EMERGENCY EVACUATION LIGHTS IN TAIL COMPARTMENT, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,887 hrs · 37,106 cycles

EMERGENCY LIGHTS FROM ROWS 11 TO 17 FAILED TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM ROWS 11 TO 17, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,887 hrs · 37,106 cycles

EMERGENCY LIGHTS FROM ROWS 27 TO 30 FAILED TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FORM ROWS 27 TO 30, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 68,537 hrs · 35,760 cycles

OVERHEAD EMERGENCY LIGHTS IN FRONT OF AFT ENTRY DOOR INOPERATIVE. RESEATED BATTERY PACK IN AFT LAVATORY. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (TAILCONE) · airframe 68,537 hrs · 35,760 cycles

AFT LT SIDE LOWER TAILCONE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR AFT LT SIDE LOWER TAILCONE LIGHT ASSY. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 68,537 hrs · 35,760 cycles

OVERHEAD EMERGENCY LIGHTS AT SEATS 15 AND 16. RESEATED BATTERY PACK AT SEAT 13DEF. OPS CHECK NORMAL.

Part: WEB — GOUGED (FUSELAGE) · airframe 67,471 hrs · 35,190 cycles

MID CARGO WEBBING IS GOUGED AT STATION 630, LONGERON 28 RIGHT, UNDER INBOARD SIDE OF TIEDOWN. INSTALLED NEW STRAP PER AARD 51-00-05-1.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,471 hrs · 35,190 cycles

MID CARGO WEBBING IS CRACKED AT STATION 693, LONGERON 28 RIGHT, UNDER INBOARD SIDE OF TIE-DOWN. SPLICED IN NEW WEB SECTION PER AARD 53-10-00-24.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,471 hrs · 35,190 cycles

AFT CARGO WEB STATION 1212 AREA HAS SEVERAL AREAS OF CORROSION. INSTALLING DOUBLER IN WEB PER SRM 51-30-05,51-30-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,471 hrs · 35,190 cycles

CORROSION ON SUBFLOOR UNDER G-1 GALLEY DRAIN PAN. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,471 hrs · 35,190 cycles

STATION 1437, LEFT SIDE, RIVETS PULLED IN SKIN AND CRACK IN SKIN, JUST BELOW VERTICAL STABILIZER SKATE ANGLE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01-00 FIGURE 2 SHEET 3 AND AARD 53-30-00-02.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,471 hrs · 35,190 cycles

CUSP CRACKED FROM STATIONS 218 TO 237. REPLACED CUSP PER AARD 51-00-05-01.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 67,471 hrs · 35,190 cycles

CRACK IN SUBFLOOR AT STATION 215 UNDER SEAT TRACK NUMBER 5. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,471 hrs · 35,190 cycles

RIGHT CUSP AT STATION 1185 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,471 hrs · 35,190 cycles

CUSP SHEET CRACKED AT STATION 842 RIGHT, UNDER HORSE COLLAR DOUBLER. ROUTED OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,471 hrs · 35,190 cycles

SUBFLOOR IS CORRODED FROM STATIONS 1170 TO 1174 FORWARD OF NUMBER 1 SEAT TRACK. INSTALLED DOUBLER PER EA MD80-53-027744.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,446 hrs · 34,589 cycles

AFT CARGO, STATION 1041, CENTER CEILING INTERCOSTAL IS CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-15.

Part: LENS — MISSING (CABIN) · airframe 64,252 hrs · 33,374 cycles

LEFT CEILING PANEL EMERGENCY LIGHT AT ROW 28 MISSING LENS. REPLACED LENS FOR CEILING PANEL EMERGENCY LIGHT AT ROW 28. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,252 hrs · 33,374 cycles

RIGHT CEILING PANEL EMERGENCY LIGHT AT ROW 5 INOPERATIVE. REPLACED LAMP FOR RIGHT CEILING PANEL EMERGENCY LIGHT AT ROW 5. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,252 hrs · 33,374 cycles

RIGHT CEILING PANEL EMERGENCY LIGHT AT ROW 8 INOPERATIVE. REPLACED LAMP FOR RIGHT CEILING PANEL EMERGENCY LIGHT AT ROW 8. OPS CHECK NORMAL.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,001 hrs · 33,226 cycles

FORWARD CARGO DOOR PAN CRACKED AT STATION 404. COMPLETED INSTALLATION OF FASTENERS IN THE REPAIR AREA OF THE LOWER CUTOUT SECTION OF THE DOOR PAN OF THE FORWARD CARGO DOOR, AND THE TWO SPLICE DOUBLERS (ONE ON THE FORWARD SIDE AND THE OTHER ON THE AFT SIDE) PER MD-80 SRM 53-05-00 AND MD-80 AARD 53-10-00-3.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,001 hrs · 33,226 cycles

FORWARD CARGO DOOR PAN CRACKED AT STATION 358. COMPLETED INSTALLATION OF FASTENERS IN THE REPAIR AREA OF THE LOWER CUTOUT SECTION OF THE DOOR PAN OF THE FORWARD CARGO DOOR, AND THE TWO SPLICE DOUBLERS (ONE ON THE FORWARD SIDE AND THE OTHER ON THE AFT SIDE) PER MD-80 SRM 53-05-00 AND MD-80 AARD 53-10-00-3.

Part: PUMP — INOPERATIVE (NR 2 HYD SYSTEM) · airframe 58,101 hrs · 30,002 cycles

DFW - RIGHT HYDRAULIC PRESS DECLINED TO ZERO FOLLOWED BY RIGHT HYDRAULIC PRESS LOW LIGHT AND RUDDER MANUAL LIGHT CAME ON. RETURNED DFW WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 22 MISSING SHROUD. REPLACED SHROUD AT SEAT ROW 22 SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 56,290 hrs · 29,030 cycles

SHEAR TIE IS CRACKED BETWEEN LONGERON 1 AND 2 RIGHT AFT SIDE OF FRAME. REPAIRED PER ESO 80559 DATED 10/1/08.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 56,290 hrs · 29,030 cycles

RIGHT WHEEL WELL TRAP FITTING UPPER FORWARD ATTACH ANGLE HAS CORROSION AT VERTICAL ATTACH BOLTS ABOVE BRAKE ACCUMULATOR. REMOVED CORRODED ANGLE AND INSTALLED SERVICEABLE REPLACEMENT ANGLE.

Part: ANGLE — CRACKED (ZONE 100) · airframe 56,290 hrs · 29,030 cycles

LEFT TORQUE TUBE VERTICAL ANGLE CRACKED AT CENTER AREA, AFT ACCESSORY. INSTALLED SERVICEABLE ANGLE.

Part: CARGO TRACK — CORRODED (BS 1212-1231) · airframe 56,290 hrs · 29,030 cycles

CORROSION LT TIE DOWN TRACK IN AFT CARGO IN NUMEROUS PLACES. INSTALLED NEW SPLICE ON LT TIE DOWN TRACK BETWEEN STATION 1212 AND 1231 PER SRM 51-10-03.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 56,290 hrs · 29,030 cycles

NR 3 SEAT TRACK CORRODED, STATION 1295-1300. SPLICED IN NEW SEAT TRACK PER SRM 53-05-00.

Part: CUSP WEB — DAMAGED (ZONE 100) · airframe 56,290 hrs · 29,030 cycles

CABIN CUSP DAMAGED LEFT HAND SIDE. INSTALLED DOUBLER ON CUSP PER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (BS 1003-1155) · airframe 56,290 hrs · 29,030 cycles

CORROSION ON RT TIE DOWN TRACK IN AFT CARGO IN NUMEROUS PLACES. INSTALLED RT TIE DOWN TRACK FROM STATION 1003 TO 1155 PER SRM 51-01-00.

Part: SEAT TRACK — CORRODED (BS 1117-1155) · airframe 56,290 hrs · 29,030 cycles

TUL CORROSION ON FLOOR BOARD SUPPORT ZEE ANGLE ON LT TRACK IN AFT CARGO. INSTALLED NEW ZEE ANGLE ON LT TIE DOWN TRACK BETWEEN STATION 1117 AND 1155 PER SRM 51-01-00.

Part: CARGO TRACK — CORRODED (BS 1003-1221) · airframe 56,290 hrs · 29,030 cycles

CORROSION ON LT TIE DOWN TRACK IN AFT CARGO NUMEROUS PLACES. INSTALLED TIE DOWN TRACK SINGLE PIECE FROM STATION 1003 TO 1221 PER SRM 51-01-00.

Part: LONGERON — CRACKED (BS 1418) · airframe 56,290 hrs · 29,030 cycles

LONGERON 2 RT IS CRACKED AT FLANGE. ACCOMPLISHED REPAIR SPLICE PER AARD 53-30-00-2.

Part: SKIN — CRACKED (BS 1437) · airframe 56,290 hrs · 29,030 cycles

TUL CRACKS IN FUSELAGE SKIN AT STATION 1437 ABOVE AND BELOW LONGERON 3R. AREA OF DISCREPANCY IS 8 INCHES BY 4 INCHES. INSTALLED REPAIR DOUBLER PER SRM 51-01-00.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,290 hrs · 29,030 cycles

CORROSION ON ANGLE AFT SIDE OF DOOR JAMB IN AFT CARGO AT STATION 1155 RT LONGERON 27 IS BEYOND LIMITS. AREA OF DISCREPANCY IS 4 INCHES BY 10 INCHES. INSTALLED NEW ANGLE PER SRM 51-01-00.

Part: BEAM — CORRODED (FUSELAGE) · airframe 56,290 hrs · 29,030 cycles

CORROSION IN SEVERAL LOCATIONS OF CARGO DOOR BEAM IN AFT CARGO AT STATION 1155 TO 1211. AREA OF DISCREPANCY IS 1 INCHES BY 48 INCHES. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,290 hrs · 29,030 cycles

CORROSION ON LOWER SURFACE OF RT HAND CUSP AT AFT CABIN BETWEEN STATIONS 1287 AND 1309 IS BEYOND SRM LIMITS. INSTALLED NEW CUSP PER SRM 53-05-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,290 hrs · 29,030 cycles

CORROSION ON LOWER SURFACE OF LT HAND CUSP AT AFT CABIN BETWEEN STATIONS 1287 AND 1309 IS BEYOND SRM LIMITS. INSTALLED NEW CUSP PER SRM 53-05-00.

Part: CUSP WEB — CRACKED (BS 1211) · airframe 56,290 hrs · 29,030 cycles

LT CUSP SHEET CRACKED AT STATION 1211 UNDER NR 2 SEAT TRACK. AREA OF DISCREPANCY IS 2 INCHES BY 3 INCHES. CRACK LENGTH IS 1 INCH. REMOVED DAMAGED AREA AND INSTALLED CUSP SHEET REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (BS 218) · airframe 56,290 hrs · 29,030 cycles

TUL-LT CUSP CRACKED AT STATION 218 UNDER NR 2 SEAT TRACK. AREA OF DISCREPANCY IS 3 INCHES BY 3 INCHES WITH A CRACK LENGTH OF 2 INCHES. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 56,290 hrs · 29,030 cycles

TUL-CORROSION ON NR 2 GALLEY TIE DOWN SUPPORT FITTING. REPLACED NR 2 GALLEY SUPPORT FITTING PER SRM 51-01-00.

Part: GALLEY TRACK — CORRODED (BS 218) · airframe 56,290 hrs · 29,030 cycles

TUL, GALLEY TIE DOWN SUPPORT AT CABIN SUBFLOOR CORRODED BEYOND SRM LIMITS. INSTALLED NEW GALLEY TIE DOWN SUPPORT PER SRM 51-01-00.

Part: FLOOR SUPPORT — CRACKED (BS 176) · airframe 56,290 hrs · 29,030 cycles

TUL FLOORBOARD SUPPORT IS WORN AND CRACKED AT STATION 176. AREA OF DISCREPANCY IS 2 INCHES BY 26 INCHES WITH A DEPTH OF 20 PERCENT PLUS. CRACK LENGTH OF 1 INCH. REPLACED FLOORBOARD SUPPORT PER SRM 51-01-00.

Part: FLOOR SUPPORT — CRACKED (BS 176) · airframe 56,290 hrs · 29,030 cycles

TUL FLOORBOARD SUPPORT IS WORN AND CRACKED AT STATION 176. AREA OF DISCREPANCY IS 2 INCHES BY 26 INCHES WITH A DEPTH OF 20 PERCENT PLUS. CRACK LENGTH OF 1 INCH. REPLACED FLOORBOARD SUPPORT PER SRM 51-01-00.

Part: ANGLE — CORRODED (BS 1155-1211) · airframe 56,290 hrs · 29,030 cycles

TUL, TEE ANGLE IN AFT CARGO AT RT LONGERON 27 AT STATION 1155 TO 1211 CORRODED BEYOND SRM LIMITS. INSTALLED NEW T ANGLE IN AFT CARGO AT RT LONGERON 27 AT STATION 1155 TO 1211 PER SRM 51-10-03.

Part: SUPPORT BRACKET — CORRODED (GIRT BAR) · airframe 56,290 hrs · 29,030 cycles

TUL AFT SERVICE DOOR GIRT BAR AFT SUPPORT FITTING AT STATION 1165 CORRODED. AREA OF DISCREPANCY IS 4 INCHES BY 5 INCHES. INSTALLED NEW AFT SERVICE DOOR GIRT BAR BRACKET PER SRM 51-01-00.

Part: WEB — CRACKED (BS 1060) · airframe 56,290 hrs · 29,030 cycles

LT LOWER FORWARD WINDOW WEB (RING PAN) CRACKED AT FASTENER HOLE. INSTALLED REPAIR DOUBLER PER SRM 53-10-00-25.

Part: WEB — CRACKED (BS 886) · airframe 56,290 hrs · 29,030 cycles

LT UPPER FORWARD WINDOW WEB (RING PAN) CRACKED. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25.

Part: LONGERON SPLICE — CRACKED (BS 1297 L25L) · airframe 56,290 hrs · 29,030 cycles

CRACK IN LONGERON PRODUCTION SPLICE IN AFT CARGO AT STATIONS 1297 LONGERON 25 LT. AREA OF DISCREPANCY IS 2 INCHES BY 6 INCHES. CRACK LENGTH IS 2 INCHES. INSTALLED NEW LONGERON SPLICE PER SRM 51-30-00.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 55,516 hrs

LGA - FORWARD LOWER EMERGENCY FLASHLIGHT MISSING SAFETY STRAP. REPLACED SAFETY STRAP FOR FORWARD LOWER EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY — LOOSE (EMERGENCY LIGHT) · airframe 55,516 hrs

LGA - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROW 21 TO AFT CABIN INOPERATIVE. RESECURED LOOSE BATTERY FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROW 21 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,313 hrs

LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,313 hrs

LGA - EMERGENCY LIGHT AT SEAT ROW 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,313 hrs

LGA - EMERGENCY LIGHT AT SEAT ROW 25DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,313 hrs

LGA - EMERGENCY LIGHT AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT B523 FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AB51 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

SFO COCKPIT EGRESS LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR COCKPIT EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR COCKPIT EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FORWARD NR 1 SPOT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR FORWARD NR 1 SPOT OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FORWARD NR 1 GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR FORWARD NR 1 GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23 FOR FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED.

Part: PUMP — INOPERATIVE (HYD SYSTEM)

ORD T702/23 EN ROUTE DEN-ORD RIGHT HYDRAULIC QUANTITY DECREASED TO 4 QUARTS. RIGHT QUANTITY WENT TO ZERO AFTER GEAR WAS EXTENDED. LANDED ORD WITHOUT INCIDENT. REPLACED RIGHT HAND ELECTRIC AUXILIARY HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

TPA - DURING OVERNIGHT MAINTENANCE, FOUND E LIGHT INOPERATIVE IN FIRST CLASS. INSTALLED NEW BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACM — LACK OF LUBE (A/C BAY)

SAN - FLT 736 - EN ROUTE SAN-DFW, IMMEDIATELY AFTER TAKEOFF CABIN BEGAN TO FILL UP WITH A BLUE HAZE/SMOKE. RAN EMERGENCY PROCEDURES AND RETURNED TO SAN. SMOKE FINALLY BEGAN TO DISSIPATE JUST PRIOR TO LANDING. SERVICED ACMS TO PROPER LEVEL. ACCOMPLISHED PACK BURN PER MM. NO SMOKE IN CABIN DURING PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM 20D AFT, EXITS AND SEATS, ARE INTERMITTENT. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (TAIL)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT AT TAIL COMPARTMENT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PLATE — CORRODED (FUSELAGE)

TUL - FOUND RIGHT OUTBOARD INBOARD PLATE COMMON TO VERTICAL STABILIZER HAS CORROSION. REPLACED RIGHT OUTBOARD INBOARD LUG PLATE PER DOUGLAS DWG 9911834 AND SRM 51-30-5. (M)

Part: PLATE — CORRODED (FUSELAGE)

TUL - FOUND LEFT INBOARD, INBOARD LUG PLATE COMMON TO VERTICAL STABILIZER HAS CORROSION. REPLACED LEFT INBOARD, INBOARD LUG PLATE PER DOUGLAS DWG 9911834 AND SRM 51-30-5. (M)

Part: PLATE — CORRODED (FUSELAGE)

TUL - FOUND RIGHT INBOARD PLATE COMMON TO VERTICAL STABILIZER HAS CORROSION. REPLACED RIGHT INBOARD LUG PLATE PER DOUGLAS DWG 9911834 AND SRM 57-30-5. (M)

Part: PLATE — CORRODED (FUSELAGE)

TUL - FOUND RIGHT INBOARD LUG PLATE COMMON TO VERTICAL STABILIZER HAS CORROSION. REPLACED RIGHT INBOARD OUTBOARD LUG PLATE PER DOUGLAS DWG 9911834 AND SRM 51-30-5. (M)

Part: PLATE — CORRODED (FUSELAGE)

TUL - LEFT INBOARD OUTBOARD PLATE COMMON VERTICAL STABILIZER HAS CORROSION. REPLACED LEFT INBOARD OTUBOARD LUG PLATE PER DOUGLAS DWG 9911834 AND SRM 51-30-5. (M)

Part: FITTING — TOOL DAMAGE (FUSELAGE)

TUL - FOUND FITTING HAS TOOLING MARKS IN LEFT AND RIGHT BORES. REPLACED FITTING PER DOUGLAS DWG 9911834 AND SRM 51-30-5. (M)

Part: PLATE — CORRODED (FUSELAGE)

TUL - FOUND COMMON TO VERTICAL STABILIZER RIGHT OUTBOARD LUG OUTBOARD PLATE IS CORRODED AND OUTBOARD SURFACE WORN. REPLACED RIGHT OUTBOARD LUG OUTBOARD PLATE PER DOUGLAS DWG 9911834 AND SRM 51-30-5. (M)

Part: PLATE — CORRODED (FUSELAGE)

TUL - FOUND LEFT OUTBOARD LUG OUTBOARD PLATE CORRODED COMMON TO VERTICAL STABILIZER PLATE HAS INTERFERENCE WEAR 2 INCHES BELOW BORE. REPLACED LEFT OUTBOARD LUG OUTBOARD PLATE PER DOUGLAS DWG 9911834 AND SRM 51-30-5. (M)

Part: PLATE — CORRODED (FUSELAGE)

TUL - FOUND COMMON TO VERTICAL STABILIZER LEFT OUTBOARD LUG INBOARD PLATE CORRODED IN BORE AND INBOARD SURFACE. REPLACED LEFT OUTBOARD LUG INBOARD PLATE PER DOUGLAS DWG 9911834 AND SRM 51-30-5. (M)

Part: FRAME — CRACKED (WINDOW)

TUL - FOUND CRACK IN BOTTOM FORWARD CORNER OF WINDOW FRAME RIGHT SIDE STATINO 1060. INSTALLED REPAIR PER AARD 53-10-00-25. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK CORRODED. INSTALLED PLUG PER SRM 53-05 FIG 4A. (M)

Part: FRAME — CRACKED (WINDOW)

TUL - FOUND CRACK IN TOP AFT CORNER OF WINDOW FRAME RIGHT SIDE STATION 1060. INSTALLED REPAIR PE AARD 53-10-00-25. (M)

Part: TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 TRACK CORRODED. INSTALLED PLUG PER SRM 53-05 FIG 4A. (M)

Part: FRAME — CRACKED (WINDOW)

TUL - FOUND CRACK IN TOP AFT CORNER OF WINDOW FRAME RIGHT SIDE STATION 1022. INSTALLED REPAIR PER AARD 53-10-00-25. (M)

Part: FRAME — CRACKED (WINDOW)

TUL - FOUND CRACK IN TOP AFT CORNER OF WINDOW FRAME RIGHT SIDE STATION 1098. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: FRAME — CRACKED (WINDOW)

TUL - FOUND WINDOW FRAME CRACKED AT FASTENER FORWARD TOP CORNER LEFT SIDE AT STAITON 946. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER AARD 53-10-00-25. (M)

Part: FRAME — CRACKED (WINDOW)

TUL - FOUND CRACK IN BOTTOM FORWARD CORNER OF WINDOW FRAME RIGHT SIDE STATION 1022. INSTALLED REPAIR PER AARD 53-10-00-25. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND CRACK AT FASTENER LONGERON NR 4 LEFT AT STATION 160 LEFT. INSTALLED LONGERON REPAIR AND SPLICE PER SRM 53-02 PAGE 48-53. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK CORRODED STATION 247. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 212 TO STATION 798 PER SRM 53-05 FIG 4F. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND LARGE CREASE AND SCRATCH IN FUSE STATION 440 TO 456 LONGERON 21R. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 12R SHEET 4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION BEYOND LIMITS. INSTALLED NEW SEAT TRACK SRM 51-01. (M)

Part: WEB — BUCKLED (FUSELAGE)

TUL - FOUND CUSP BUCKLED ON RIGHT SIDE, BETWEEN STATION 335 AND 338 ON OUTBOARD ROW OF RIVITS. FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 2 AT THE FOLLOWING STATIONS 1300-1303, 1200-1202, 1205-1207, 1196, 1266, 1225, 1171, 1259, 1286, 1177, 1167, 1190, 1276, 1280 AND 1201. REPLACED NR 2 SEAT TRACK FROM STATION 1165 TO 1307 PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 6 AT THE FOLLOWING STATIONS 484, 625, 687, 717, 748, 765, 779 AND 795. REPLACED SEAT TRACK NR 6 FROM STATION 302-798 PER SRM 51-01. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND CLASS III REPAIR INSTALLED AT STATION 195 LONGERON 23L. INSTALLED CLASS II REPAIR PER SRM 53-04. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LEFT CUSP CORRODED AT NUT PLATE STATION 1306. CUT OUT CORRODED AREA. INSTALLED FILLER PER ESO 80559 DATED 8/30/00. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP AROUND FASTENERS STATION 519-529 RIGHT SIDE. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK CORROSION STATION 639. INSTALLED PLUG NR 6 SEAT TRACK AT STATION 639 PER SRM 53-05 FIG 4A. (M)

Part: WEB — GOUGED (FUSELAGE)

TUL - FOUND GOUGE AT LEFT CUSP AT STATION 746. FABRICATED DOUBLER, TREATED AND PRIMED AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK CORRODED STATION 446-465. ROUTED OUT DAMAGE AREA AND INSTALLED PLUG AT NR 6 SEAT TRACK STATION 450-454 PER SRM 53-05 FIG 4A. (M)

Part: SKIN — BULGED (FUSELAGE)

TUL - FOUND SKIN BULGING AROUND FASTENERS FROM PREVIOUS REPAIR AT STATION 277 TO 288 STRINGER 17R. CUT OUT DAMGE AREA, INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M)

Part: WIRE — BROKEN (AFT AIRSTAIRS)

IAH - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIRS INOPERATIVE. REPAIRED WIRE TO EMERGENCY LIGHT AT AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT ROW 30 FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIPS AT PASSENGER ROW 30. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: COALESCER BAG — DIRTY (CABIN)

ORD - FLT 435 - AFTER TAKEOFF ORD DURING CLIMB-OUT, FOUL ODOR ENTERED COCKPIT AND ODOR/SMOKE NOTED IN CABIN. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. CHECKED BOTH ENGINES AND NOTED POSSIBLE BIRD STRIKE TO RIGHT ENGINE. ACCOMPLISHED BORESCOPE OF RIGHT ENGINE WITH NO DEFECTS FOUND. REPLACED LEFT AND RIGHT COALESCER BAGS AND ACCOMPLISHED GRUOND RUN OF BOTH ENGINES, APUT AND BOTH PACKS WITH NO DEFECTS, SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION AND AIRCRAFT RETURNED TO SERVICE. (M)