N7517A

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 64,357 hrs · 33,272 cycles

SHEAR TIE CRACKED AFT SIDE OF STATION 1451 AFT OF LONGERON 2 RIGHT. REPLACED SHEAR TIE PER AARD 51-10-00-5.

Part: SCHRADER VALVE — DEFECTIVE (NLG) · airframe 63,918 hrs · 33,031 cycles

DFW - CREW REPORTED NOSE GEAR WOULD NOT RETRACT. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED SCHRADER VALVE AND SERVICED NOSE STRUT TO PROPER LEVEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 63,860 hrs · 33,005 cycles

LEFT AND RIGHT AFT OVERWING DOOR UPPER EXIT SIGNS INOPERATIVE. RESEATED BATTERY PACK. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,860 hrs · 33,005 cycles

LEFT AND RIGHT FORWARD OVERWING DOOR UPPER EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,860 hrs · 33,005 cycles

FORWARD CABIN EMERGENCY SIGN ACROSS FROM FIRST CLASS LAVATORY INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY SIGN. OPS CHECKS NORMAL.

Part: SLIDE — DAMAGED (SERVICE DOOR) · airframe 61,164 hrs · 31,523 cycles

FORWARD GALLEY SERVICE DOOR SLIDE DAMAGED. REMOVED AND REPLACED SLIDE WITH SERVICEABLE SLIDE. OPS CHECK NORMAL.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,428 hrs · 31,119 cycles

AFT ACCESSORY WEB CRACKED LEFT OF RUDDER PACK AT 1485 CANT FRAME. INSTALLED DOUBLER PER AARD 53-10-00-32.

Part: RELAY — OPEN (THERMOSTAT) · airframe 56,955 hrs · 29,162 cycles

SPS - INFLIGHT COS-DFW. WHILE DESCENDING FLIGHT LOST BOTH A/C PACKS. EMERGENCY DECLARED, LANDED SPS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND OPEN COIL ON RELAY R2-279. REPLACED AIR CONDITIONING THERMOSTAT RELAY R2-279. REPLACED BOTH COALESCER BAGS IN WATER SEPARATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE — SHORTED (CABIN) · airframe 56,520 hrs · 28,933 cycles

WITH AFT BATTERY PACK SEAT DROP PLUGGED IN, AFT HALF OF SEAT EMERGENCY LIGHTS DIE. FOUND SHORTED WIRES FOR EPL IN AFT ACCESSORY, REPAIRED AND SECURED WIRES, OPERATIONAL CHECK GOOD PER WORK CARD 5703.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

CANT FRAME 1418 CRACKED AT LONGERON 2R. INSTALLED REPAIR DOUBLER ON FRAME 1418 AND SPLICE ON LONGERON 2R PER SRM 51-30-05 AND AARD 53-30-00-2.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

SUBFLOOR CORRODED BETWEEN NR 5 AND NR 6 SEAT TRACK STATION 200-218. INSTALLED SUBFLOOR DOUBLER PER SRM 51-10-3, 53-01 FIGURE 1, AND 51-30-1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,520 hrs · 28,933 cycles

AFT CARGO DOOR UPPER FORWARD STOP PAD FITTING CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174 DATED 03/23/09.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

FRAME 1418 CRACKED ON UPPER FLANGE BETWEEN LONGERON 1R AND 2R. INSTALLED DOUBLER PER EA MD80-53-005777.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON RIGHT CUSP STATION 160-175. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

LEFT CUSP SEVERELY RIPPLED STATION 769-788. INSTALLED NEW CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

HOLE IN CUSP APPROXAMATELY .375 INCH IN DIAMETER AT STATION 864 RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON RIGHT CUSP STATION 1304-1309. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

RIGHT CUSP CORRODED AT STATION 219. INSTALLED CUSP SHEET PER SRM 53-01.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

ABOVE CENTER FUEL TANK STA 927, FLOORBEAM SUPPORT CRACKED LEFT SIDE. REPLACED SUPPORT PER SRM 51-00-01.

Part: FRAME — GOUGED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

WEB GOUGED IN CANTED FRAME AT STATION 1338. INSTALLED DOUBLER PER SRM 51-70-04 FIGURE 2 SHEET 2.

Part: STIFFENER — WORN (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

STIFFENER WORN ON CANTED FRAME AT STATION 1338. REMOVED AND REPLACED STIFFENER PER SRM 51-30-05.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON FRAME 1250 LOWER FLANGE LONGERON 29L-29R IN AFT CARGO. INSTALLED REPAIR SPLICE PER SRM 53-03-02A SHEET 5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

CRACK IN LIGHTNING HOLE ON CUSP MEMBRANE AT STATION 451 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

LEFT CUSP CORRODED STATION 1163-1168 AT AFT SERVICE DOOR. REPAIRED PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON BOTTOM OF RIGHT CUSP AT STATION 1219. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

AFT SERVICE DOOR, FORWARD GIRT BAR FITTING CORRODED ON TOP AT STATION 1142. REMOVED AND REPLACED FORWARD GIRT BAR FITTING PER SRM 51-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON BOTTOM OF LEFT CUSP BETWEEN STATIONS 712-731. INSTALLED NEW CUSP SHEET FROM STATION 712-788 PER SRM 51-10-3 AND 53-01 FIGURE 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON LEFT CUSP AT STATION 480. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON TOP OF LEFT CUSP STATION 503-522. INSTALLED DOUBLER PER SRM 53-20-00-16.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CUSP T-ANGLE TANG AT STATION 200 RIGHT SIDE CORRODED. INSTALLED CUSP ANGLE SPLICE REPAIR PER SRM 53-05-00 FIGURE 55 SHEET 2.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

NR 6 SEAT TRACK WORN BEYOND LIMITS. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

LEFT PAN CRACKED TOP FORWARD CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

LONGERON 2R CRACKED OUTBOARD SIDE JUST AFT OF FRAME AT STATION 1418. INSTALLED REPLACEMENT LONGERON AND SPLICE DOUBLER PER AARD 53-30-00-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON BOTTOM SIDE OF CUSP RIGHT SIDE STATION 636-655. REPLACED CUSP SHEET PER AARD 53-20-00-16.

Part: CASTING — CRACKED (SPOILER ACTUATOR) · airframe 56,520 hrs · 28,933 cycles

GROUND SPOILER CASTING CRACKED IN RADIUS ABOVE FORWARD END OF ACTUATOR, OUTBOARD SIDE. REPLACED SPOILER CASTING PER SRM 51-30.

Part: PAN — CRACKED (FUSELAGE) · airframe 52,520 hrs · 28,933 cycles

TOP AFT TANG CRACKED ON RIGHT WINDOW PAN AT STATION 1042. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON BOTTOM SIDE OF RIGHT CUSP STATION 1174-1193. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

DENT AT STATION 1380 LONGERON 8L. INSTALLED DOUBLER PER SRM 53-01 FIGURE 2 SHEET 3.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

LONGERON 4L CRACKED AT OUTBOARD FASTENER STATION 200. INSTALLED NEW LONGERON PER SRM 53-02.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

WINDOW PAN CRACKED RIGHT SIDE STATION 1041. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SUPPORT BRACKET — DAMAGED (GIRT BAR) · airframe 56,520 hrs · 28,933 cycles

FWD GIRT BAR SUPPORT BRACKET WAS DAMAGED DURING REMOVAL FOR OTHER MAINTENANCE (CUSP REPAIR). INSTALLED NEW BRACKET AT STATION 1143 LEFT SIDE PER SRM 51-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON LEFT HAND TIE DOWN TRACK IN AFT CARGO STATION 1022-1212. REMOVED AND REPLACED TIE DOWN TRACK PER AARD 51-00-00-012.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

LEFT CUSP CORRODED STATION 1163-1168. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

AFT SERVICE DOOR, AFT GIRT BAR FITTING CORRODED. INSTALLED NEW GIRT BAR FITTING PER SRM 53-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON TOP OF LEFT CUSP STATION 570-579. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

HEAVY CORROSION ON TOP OF LEFT CUSP STATION 826-845. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CUSP CORRODED LEFT SIDE UNDER GIRT BAR FITTING AT STATION 1143. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

HEAVY CORROSION ON TOP OF LEFT CUSP STATION 826-845. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

UPPER HORIZONTAL FLANGE OF FRAME DAMAGED WHERE 2 FASTENERS ATTACH TO LONGERON 4L. INSTALLED J-ANGLE DOUBLER AND FILLER PER AARD 53-10-00-17.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

RIGHT FUSELAGE SKIN CRACKED AT STATION 1380 LONGERON 12R. INSTALLED DOUBLER PER AARD 53-30-00-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON BOTTOM SIDE OF LEFT CUSP BETWEEN STATIONS 636-655. INSTALLED NEW LEFT CUSP SECTION FROM STATION 598-710 PER SRM 51-30.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

GOUGE IN STRAP AT STATION 630 IN MID CARGO. REPLACED STRAP PER AARD 51-00-00-12.

Part: STRAP — DAMAGED (CARGO BAY) · airframe 56,520 hrs · 28,933 cycles

SCREW GOUGE IN STRAP BELOW Z-ANGLE INBOARD SIDE AT STATION 698 IN MID CARGO. REMOVED AND REPLACED STRAP PER AARD 51-00-00-12.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

MID CARGO DOOR BEAM CORRODED BETWEEN STATION 636 AND 693. REPAIRED PER EA MD80 53-005707 DATED 03/12/09.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CARGO ON BOTTOM OF CUSP RIGHT SIDE FROM STATION 1193-1212. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON AFT CARGO DOOR BEAM VERTICAL LEG STATION 1155 TO 1211. REPAIRED DOOR BEAM PER AARD 53-10-00-3 AND EA MD80-53-005703.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

OVERWING FRAME CRACKED IN UPPER RADIUS AT LEFT SIDE STATION 886. REPLACED STATION 886 FRAME PER SERVICE REWORK DRAWING SRO 9530282.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON TOP OF LEFT CUSP AT STATION 219. REPLACED CUSP SHEET FROM STATION 218 TO 237 PER AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

CRACK IN RADIUS OF CANTED FRAME 1463, LONGERON 18L. REPAIRED PER SRM 53-01-00 FIGURE 2 SHEET 4.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

CRACK IN REPAIR DOUBLER AT CANTED FRAME 1485 LEFT SIDE BELOW AIRSTAIR RETRACT ACTUATOR. INSTALLED NEW DOUBLER PER AARD 53-10-00-33.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

CORROSION ON LOWER FLANGE OF FRAME AT STATION 1309, LONGERON 30. INSTALLED J-ANGLE DOUBLER PER AARD 53-10-00-17.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

INTERCOSTAL CRACKED IN CEILING OF AFT CARGO AT STATION 1309. INSTALLED DOUBLER PER EA MD80 53-005713 DATED 03/13/09.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

SHELF BRACKET JUST FORWARD OF THE LEFT GEAR DOOR ACTUATOR UPPER MOUNT IS CRACKED AT THE AFT SIDE OF THE RADIUS. REMOVED AND REPLACED LEFT DOOR ACTUATOR BRACKET PER SRM 51-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

CRACK IN LEFT CUSP AT STATION 245. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

SHELF BRACKET JUST FORWARD OF RIGHT DOOR ACTUATOR UPPER MOUNT IS CRACKED AT THE AFT SIDE. REMOVED AND REPLACED DOOR ACTUATOR BRACKET PER SRM 51-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

RIGHT CUSP CRACKED AT STATION 1264. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

RIGHT CUSP CRACKED AT STATION 992. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CASTING — CRACKED (SPOILER ACTUATOR) · airframe 56,520 hrs · 28,933 cycles

LEFT WING GROUND SPOILER ACTUATOR CASTING CRACKED IN RADIUS ABOVE FORWARD END OF ACTUATOR, INBOARD SIDE. INSTALLED NEW SPOILER CASTING PER SRM 51-30.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,520 hrs · 28,933 cycles

RIGHT CUSP CORRODED AT STATION 602. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,520 hrs · 28,933 cycles

AFT CARGO DOOR UPPER FORWARD STOP PAD FITTING CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

DENT IN FUSELAGE LEFT SIDE STATION 237, LONGERON 17L TO 18L. INSTALLED DOUBLER PER SRM 53-04 FIGURE 12B.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

TOP AFT FLANGE CRACKED ON LEFT WINDOW PAN AT STATION 1079. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

FORWARD ENTRY DOOR CUTOUT AFT FRAME WEB TANG IS CRACKED AT LONGERON 11L STATION 208. REPLACED WEB TANG DOUBLER PER AARD 53-10-00-11.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

FORWARD UPPER FLANGE ON LEFT WINDOW PAN CRACKED AT STATION 1212. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SKATE ANGLE — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

RIGHT SKATE ANGLE CRACKED. INSTALLED DOUBLER AND FILLER PER AARD 53-10-00-2.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,520 hrs · 28,933 cycles

FORWARD UPPER TANG CRACKED ON LEFT WINDOW PAN AT STATION 1098. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,134 hrs

LGA- CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACE BATTERY PACK FOR CEILING EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 56,134 hrs

LGA - AFT EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT AFT EXIT.

Part: BATTERY PACK — DISCHARGED (CABIN) · 54,875 cycles

LGA EMERGENCY LIGHTS AT OVERWING INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD ROW 24 FOR INOPERATIVE EMERGENCY LIGHTS AT OVERWING. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SHROUD — BROKEN (CABIN) · airframe 54,547 hrs

DFW - EMERGENCY LIGHT AT SEAT AT 13D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: SHROUD — BROKEN (CABIN) · airframe 54,547 hrs

DFW - EMERGENCY LIGHT AT SEAT 15D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,743 hrs

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

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - PORTABLE EMERGENCY LIGHT AT LEFT ONE DOOR AND EXTERIOR OVERWING EMERGENCY LIGHTS ON LEFT AND RIGHT SIDE INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT LEFT ONE DOOR AND REPLACED BATTERY PACK FOR EXTERIOR OVERWING EMERGENCY LIGHTS ON LEFT AND RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT TAIL CONE SIDE WALL INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHTS AT TAIL CONE SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WINDOW — DEBONDED (PAX CABIN)

PHX - INFLIGHT T517/20 DFW TO LAX PASSENGER WINGOW AT SEAT 19A OUTER PANE DISBONDED. LANDED PHX WITHOUT INCIDENT. EVALUATION IN PROGRESS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT CABIN. BATTERY PACK FAILED DUAL FEED CHECK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — NOT SEATED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT REAR FLOOD EMERGENCY EXIT LIGHT INOPERATIVE. SEATED AFT REAR FLOOD EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION BEYOND LIMITS. INSTALLED WEB REPAIR PER AARD 53-00-00-2. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RT CUSP, STATION 617 TO STATION 674, HEAVY AT FRAME CUTOUTS AND STATION 660. REMOVED CORROSION, CUT OUT SMALL SECTION, TREATED AND PAINTED. INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M)

Part: CASTING — CORRODED (HORIZ STAB)

TUL - FOUND HORIZONTAL STABILIZER SPREADER CASTING IS CORRODED BEYOND LIMITS, YV 222.4321. REMOVED AND REPLACED HORIZONTAL STABILIZER SPREADER CASTING PER SRM 51-01. (M)

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: CONNECTOR — MISWIRED (CABIN)

DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY DOOR EXIT MARKER INOPERATIVE. REVERSED CONNECTOR IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (ROW 20)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 20 INOPERATIVE. REPLACED SPLICE CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. RESEATED EMERGENCY FLOOR PATH LIGHT WIRE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHTS IN AFT COACH CLASS WERE INOPERATIVE. REPAIRED BROKEN WIRE AT OVERHEAD BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT OVERWING EXITS WERE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. RESEATED EMERGENCY FLOOR PATH LIGHT WIRE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FORWARD OF FIRST CLASS SEATS INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FUEL CONTROL — FAILED (RT ENGINE)

LAX - FLT 7 - DURING FINAL APPROACH LAX AT 5,000 FEET, THROTTLES WERE RETARDED AND RIGHT ENGINE SHUT DOWN IN FLT. FLIGHT CREW ACCOMPLISHED ENGINE OUT PROCEDURES AND LANDED LAX WITHOUT FURTHER INCIDENT. REPLACED RIGHT ENGINE FUEL CONTROL UNIT AND AS A PRECAUTIONARY, REPLACED RIGHT ENGINE FUEL PUMP. RIGGED RIGHT ENGINE FUEL CONTROL UNIT PER PROCEDURES. RIGHT ENGINE WAS GROUND RUN AT VARIOUS POWER SETTINGS WITH NO LEAKS OR UNCOMMANDED SHUT DOWNS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: AIR DISTRIBUTION — ODOR (CABIN)

DFW - FLT 2073 - DURING DESCENT INTO DFW, STRONG SMELL OF FOREIGN ODOR NOTED IN MIDDLE OF AFT CABIN. EMERGENCY DECLARED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. ODOR DIMINISHED AFTER LANDING. CHECKED OVERHEAD BINS FOR EVIDENCE OF SPILLAGE WITH NO DEFECTS FOUND. AIRED OUT AFT CARGO COMPARTMENT AND THEN OPERATED AIR CYCLED MACHINE FROM COLD TO HOT TO ENSURE NO RESIDUAL ODOR. SYSTEMS GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHTS — MALFUNCTIONED (CABIN)

MIA - FLT 1460 - DURING TAKEOFF IAH, EMERGENCY FLOOR LIGHTS AFT OF PAX SEAT ROW 18 ILLUMINATED. DURING CRUISE EMERGENCY FLOOR LIGHTS AFT OF PAX SEAT ROW 18 EXTINGUISHED. AIRCRAFT PROCEEDED TO MIA. DURING LANDING ROLL OUT, EMERGENCY FLOOR LIGHTS AFT OF PAX SEAT ROW 18 WERE FLASHING ON AND OFF. ACCOMPLISHED TEST OF EMERGENCY FLOOR LIGHTS PER MAINTENANCE MANUAL. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

IAH - FLT 1107 - AT THE GATE AFTER ARRIVAL, EMERGENCY FLOOR LIGHT STRIPS ILLUMINATED AT ALL TIMES WITH THE EMERGENCY EXIT LIGHT SWITCH IN OFF POSITION. FOUND EMERGENCY EXIT LIGHT ASSEMBLY SHORTED TO GROUND IN AFT AIR STAIR. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL STRIP — CORRODED (CABIN)

ORD - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS VERY DIM. FURTHER INVESTIGATION FOUND CORRODED STRIPS AT FWD GALLEY. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z)