N7521A

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,187 hrs · 32,279 cycles

CEILING EMERGENCY LIGHTS AT ROWS 19 TO 21 INOPERATIVE. REPLACED BATTERY PACK AT ROW 20. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,187 hrs · 32,279 cycles

FORWARD OVERWING EXIT EMERGENCY LIGHTS ARE AT ROW 20 INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (FUSELAGE) · airframe 62,187 hrs · 32,279 cycles

FORWARD OVERHEAD CABIN/COCKPIT EMERGENCY CEILING LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKS NORMAL.

Part: SENSOR — INOPERATIVE (RT MLG DOOR) · airframe 61,808 hrs · 32,067 cycles

ORD - CREW REPORTED YELLOW GEAR DOOR OPEN LIGHT STAYED ON AFTER TAKEOFF. CYCLED GEAR AND LIGHT REMAINED ON. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. AFTER GEAR EXTENSION FOR LANDING LIGHT WAS STILL ILLUMINATED. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT GEAR DOOR SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE — BROKEN (CATWALK) · airframe 61,637 hrs · 31,969 cycles

AFT STAIR CATWALK EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE FOR AFT STAIR CATWALK EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (PORTABLE LIGHT) · airframe 61,637 hrs · 31,969 cycles

LEFT NUMBER 1 DOOR PORTABLE LIGHT INOPERATIVE. RESEATED BATTERIES FOR LEFT NUMBER 1 DOOR PORTABLE LIGHT. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (CABIN) · airframe 61,637 hrs · 31,969 cycles

ROW 28 TO 30 CEILING EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES FOR ROW 28 TO 30 CEILING EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: PIN — LOOSE (CABIN) · airframe 59,611 hrs · 30,828 cycles

EMERGENCY AISLE LIGHT OUT AT SEAT 27D. RE-INSERTED LOOSE PIN IN SEAT 27D EMERGENCY EXIT AISLE CONNECTOR. OPS CHECKED NORMAL

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 56,966 hrs · 29,393 cycles

DFW INFLIGHT. RIGHT HYDRAULIC QUANTITY WENT TO ZERO ALONG WITH HYDRAULIC PRESSURE TO 1500 PSI WHEN SLATS WERE EXTENDED ON FINAL APPROACH. LANDING WAS NORMAL EXCEPT FOR DRAGGING DOORS ON LANDING. FOUND RIGHT SHUT OFF VALVE LEAKING. REPLACED GROUND SPOILER CONTROL VALVE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,466 hrs · 29,121 cycles

EMERGENCY BATTERY IS WEAK AT STATION 1190. REPLACED EMERGENCY LIGHT BATTERY PACK AT STATION 1190 UNDER MM 33-53-00-6.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,446 hrs · 29,121 cycles

EMERGENCY BATTERY IS WEAK AT STATION 1322. REPLACED EMERGENCY LIGHTING BATTERY PACK UNDER MM 33-53-00-6.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 56,027 hrs · 28,884 cycles

FORWARD END OF NR 4 BEAM ON AFT CARGO DOOR CORRODED. REMOVED AND REPLACED BEAM PER ESO 80174.

Part: BEAM — DAMAGED (CARGO DOOR) · corrosion level 2 · airframe 56,027 hrs · 28,884 cycles

CORROSION ON FORWARD TOP NR 4 SIDE OF DOOR BEAM. REMOVED CORROSION AND CHORD SECTION OF NR 4 BEAM AND INSTALLED NEW CHORD PER SHOP ECO 80174 AND SRM 51-20-00.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 56,028 hrs · 28,884 cycles

AFT CARGO TIE DOWN TRACK IS CORRODED AT STATION 1155. REPAIRED TIE DOWN TRACK PER AARD 53-20-00-13.

Part: WEB — GOUGED (FUSELAGE) · airframe 56,028 hrs · 28,884 cycles

SCREW GOUGE IN WEB AT STATION 1153 LONGERON 28 RIGHT. INSTALLED WEB SPLICE PER AARD 53-10-00-24.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,028 hrs · 28,884 cycles

FRAME CRACKED AT CUSP LINE. INSTALLED NEW FRAME ON RIGHT SIDE AT STATION 864 PER ECO K3290AC.

Part: ANGLE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

AFT CARGO Z-ANGLE CORRODED. INSTALLED Z-ANGLE PER SRM 50-30-01.

Part: INTERCOSTAL — GOUGED (FUSELAGE) · airframe 56,028 hrs · 28,884 cycles

INTERCOSTAL HAS GOUGE AT STATION 1318 BETWEEN LONGERON 26 LEFT AND 27 LEFT. INSTALLED NEW INTERCOSTAL PER SRM 51-30-05.

Part: STRAP — GOUGED (FUSELAGE) · airframe 56,028 hrs · 28,884 cycles

SCREW GOUGE IN STRAP AT STATION 1148 AND LONGERON 28 RIGHT UNDER TIE DOWN TRACK. REPLACED STRAP PER AARD 51-00-012 AND SRM 53-01-00.

Part: WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

CRACK IN WEB AT FASTENER HOLE AND CORROSION AT SAME AREA ON WEB AT FASTENER HOLE RIGHT STATION 433 BETWEEN LONGERON 25 AND 26 RIGHT. INSTALLED DOUBLER RIGHT STATION 433 PER AARD 53-10-00-24 FIGURE 1 SHEET 3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

SHEAR TIE CORRODED FROM LONGERON 29 LEFT TO LONGERON 29 RIGHT. SPLICED IN NEW SECTION OF SHEAR TIE AT STATION 1287 BETWEEN LONGERON 29 LEFT TO LONGERON 29 RIGHT PER SRM 53-03-00 FIGURE 3.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

CORROSION IN CARGO ON LOWER DOOR BEAM. DOUBLER WAS INSTALLED PER AARD 53-10-00-03.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

AFT CARGO CORROSION ON LOWER SIDE OF LEFT CUSP AT STATION 1090. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

RIGHT CUSP CORRODED STATION 639 TO 643. INSTALLED DOUBLER PER AARD 53-20-00-16, MATERIAL 7075-T6 .032 AFTER CORROSION REMOVAL.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

CORROSION IN AFT CARGO LONGERON 29 LEFT. COMPLETED U-CHANNEL REPAIR PER SRM 53-02-00.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

CORROSION AT STATION 1288 TO 1295 ON LONGERON 30. INSTALLED LONGERON REPAIR PER SRM 53-02-00.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 56,027 hrs · 28,884 cycles

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

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,028 hrs · 28,884 cycles

MULTIPLE DAMAGE IN AREA STATION 229 TO 256 LONGERON 18 LEFT TO LONGERON 20 LEFT. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED CLASS ONE DOUBLER IN ACCORDANCE WITH SRM 53-04 FIG 12B, SHEET 34.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

CORROSION IN AFT CARGO TIE DOWN TRACK. REPAIRED PER SRM 51-30-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,028 hrs · 28,884 cycles

TWO CRACKS IN CUSP OUTBOARD NR 5 & NR 6 SEAT TRACKS. NEW CUSP WAS INSTALLED PER SRM 51-01-00, SRM 51-30-02, SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,028 hrs · 28,884 cycles

CRACK IN LEFT CUSP. REMOVED AND REPLACED CUSP SHEET PER SRM 53-01 FIG 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

CORROSION IN AFT CARGO LOWER RT SIDE CUSP. REMOVED CORROSION AND INSTALLED DOUBLER WAS INSTALLED PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,027 hrs · 28,884 cycles

SHARP DENT IN FUSELAGE BETWEEN L17L-L18L. DRILLED OUT DAMAGED AREA, INSTALLED FLUSH PLUG RIVET PER SRM 53-04 FIG 38 SHEET 13.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

CORROSION ON ANGLE BRACKET AT LOWER CORNER OF CARGO DOOR CUTOUT. REMOVED AND REPLACED BRACKET PER SRM 51-30-05.

Part: MOUNT — CORRODED (G1 GALLEY) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

G1 GALLEY FORWARD INBOARD TIE DOWN FITTING CORRODED. REMOVED AND REPLACED GALLEY MOUNT PER SRM 51-01.

Part: MOUNT — WORN (G1 GALLEY) · airframe 56,028 hrs · 28,884 cycles

G1 GALLEY FORWARD OUTBOARD MOUNT WORN. REMOVED AND REPLACED GALLEY MOUNT PER SRM 51-01.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 56,028 hrs · 28,884 cycles

CRACK IN MID CARGO LOWER OUTBOARD T-ANGLE. REMOVED CRACKED T-ANGLE AND INSTALLED NEW T-ANGLE PER ESO 80174 IN SHOP.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,028 hrs · 28,884 cycles

WINDOW PAN IS CRACKED AT LOWER FORWARD CORNER LEFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,027 hrs · 28,884 cycles

SEAT TRACK NR 5 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-40-01-2

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,028 hrs · 28,884 cycles

CORROSION ON CUSP UNDER GIRT BAR FITTING AT AFT DOOR SERVICE FORWARD FITTING. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,027 hrs · 28,884 cycles

HEAVY CABIN CORROSION ON CUSP UNDER GIRT BAR FITTING AT AFT SERVICE DOOR AFT FITTING. REMOVED CORROSION PER SRM 51-10-3, INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,027 hrs · 28,884 cycles

RIGHT CUSP CORRODED. INSTALLED DOUBLER PER SRM 53-20-00-16.

Part: HYDRAULIC SYSTEM — CONTAMINATED (LEFT & RIGHT) · airframe 55,525 hrs · 28,606 cycles

OKC - INFLIGHT FAT-DFW. CREW REPORTED A RIGHT HYDRAULIC SYSTEM LOSS. EMERGENCY DECLARED, LANDED OKC WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AIRCRAFT FOR POSSIBLE LEAKS, NO INDICATION OF LEAK. BLED AIR FROM LEFT AND RIGHT RESERVOIRS AND SERVICED LEFT AND RIGHT HYDRAULICS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,106 hrs

LGA- TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ON TAIL CONE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,858 hrs

MSP - EMERGENCY LIGHTS IN MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 14. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,858 hrs

MSP - EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT MISSING LENS. REPLACED LENS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 54,858 hrs

MSP - OVERHEAD EMERGENCY LIGHTS AT RIGHT AND LEFT EMERGENCY EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK AT EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (NOSE GEAR) · airframe 52,101 hrs

ORD INFLIGHT T755/05DEC - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. ACCOMPLISHED NOSE STRUT REPACK AND REPLACED SCHRADER VALVE AND SERVICED WITH DRY NITROGEN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT ROW 10D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 10D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

LGA - EMERGENCY EXIT LIGHTS AT FORWARD LEFT AND RIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHTS AT FORWARD LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TOWERSHAFT — BROKEN (LT ENGINE)

RDU - LEFT ENGINE FAILED ON TAKEOFF. NO OTHER INDICATIONS. RETURNED TO RDU AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. EVALUATION INDICATES BROKEN TOWER SHAFT. GEARBOX DECOUPLED. STARTER SPINS ENGINE 50 PERCENT. REPLACED NUMBER ONE ENGINE ON 27 NOV 2006 AT RDU. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTACT — DIRTY (BATTERY PACK)

RDU - OVERHEAD EMERGENCY LIGHTS AT ROW 29 INOPERATIVE. CLEANED CONTACTS ON EMERGENCY LIGHT BATTERY PACKS FOR OVERHEAD EMERGENY LIGHTS AT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (SEAT 28)

SFO - CEILING EMERGENCY LIGHTS AFT OF SEAT 28 INOPERATIVE. CHARGED CEILING EMERGENCY LIGHTS AFT OF SEAT 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - OVERHEAD EMERGENCY LIGHTS AT SEATS 13 THROUGH 16 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY OVERHEAD LIGHTS AT ROWS 13 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FORWARD EMERGENCY LIGHT AT COCKPIT OVERHEAD INOPERATIVE. REPLACED BATTERY PACK ASSEMBLY FOR FORWARD EMERGENCY LIGHT AT COCKPIT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DIRTY (CABIN)

DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS BETWEEN SEATS 8F AND 12F INTERMITTENT. CLEANED AND SECURED EMERGENCY EXIT LIGHT GROUND WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTACTOR — DIRTY (LIGHT BATTERY)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS BETWEEN ROW 13-16 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHTS BATTERY CONTACTS. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OATH LIGHTS OF BOTH AFT OVERWING DOORS INOPERATIVE. REPLACED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FLOORBEAMS AROUND NUTPLATE HOLES. REMOVED CORROSION BY REAMING HOLES AND INSTALLING FREEZE PLUGS PER ESO80559 DATED 6-27-2001. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CUSP CRACKED OUTBOARD OF NR 5 SEAT TRACK STATION 248. INSTALLED REPAIR STRIP (DOUBLER) PER ESO 80559 DATED 6/27/2001. (M)

Part: SKIN — DENTED (FS 218)

TUL - FOUND DENT ON LEFT SIDE OF AIRCRAFT BELOW FIRST PLUGGED WINDOW, APPROX 3 FEET BELOW RED STRIPE. CUT OUT ONE INCH HOLE TO REMOVE DAMAGE AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: FRAME — CRACKED (FS 1485)

TUL - FOUND FRAME 1485 IS CRACKED ON RIGHT SIDE OF STAIRS CUTOUT AT STAIR ACT CASTING. CUT OUT DAMAGED SECTION OF FRAME. INSTALLED REPAIR AS PER AARD 53-10-00-33. (M)

Part: SKIN — GOUGED (FS 237)

TUL - FOUND FUSELAGE SKIN GOUGED STATION 237 LONGERON 20L. CUT OUT 1 INCH HOLE TOO REMOVE DAMAGE AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND FLOORBEAM HAS CORROSION IN LAVATORY PAN HOLES STATION 1322 RIGHT AFT LAVATORY. REMOVED CORROSION PER SRM 51-10-3. INSTALLED REPAIR PER ESO 80559 DATED 6-22-2001. (M)

Part: BEAM — CORRODED (CARGO DOOR)

TUL - FOUND AFT CARGO DOOR BEAM CORRODED, STATION 1160-1205. INSTALLED NEW DOOR BEAM SRM 51-30-5 FIG 2. (M)

Part: SHEAR TIE — CRACKED (FS 1456)

TUL - FOUND SHEAR TIE CRACKED LBL 10 INCHES STATION 1456 ABOVE 'Y' DUCT. INSTALLED NEW SHEAR TIE PER SRM 51-01. (M)

Part: LONGERON — CRACKED (FS 160)

TUL - FOUND L4L HAS A CRACK AROUND FASTENERS AT STATION 160. INSTALLED NEW LONGERON AND LONGERON SPLICE PER SRM 53-02 FIG 18. (M)

Part: SKIN — DAMAGED (FS 218)

TUL - FOUND FUSELAGE SKIN DAMAGED WITH TEMPORARY REPAIR AT STATION 218 BETWEEN LONGERON 21L AND 23L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B SHEET 3. (M)

Part: SHEAR TIE — CRACKED (FS 1456)

TUL - FOUND SHEAR TIE CRACKED AT STATION 1456 BETWEEN LONGERON 1/2 RIGHT. INSTALLED NEW SHEAR TIE PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (BS 1174-1308)

TUL - FOUND CORROSION ON SEAT TRACK NR 3. REMOVED CORRODED SEAT TRACK NR 3 AND INSTALLED NEW TRACK FROM FS 1164 THRU 1308 SRM 53-05. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND THREE SCRATCHES FLOOR MEMBRANE BETWEEN FLOOR TRACK 1/2 STATION 1216-1217. CUTOUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: SKIN — DENTED (FS 242)

TUL - FOUND DENT RIGHT FUSELAGE 5 FEET AFT OF SERVICE DOOR. INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M)

Part: SHEAR TIE — CRACKED (FS 1437)

TUL - FOUND SHEAR TIE CRACKED STATION 1437 BETWEEN LONGERON 3 LEFT AND 4 LEFT. REMOVED AND REPLACED SHEAR TIE PER SRM 51-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND LOWER SIDE OF RIGHT CUSP CORRODED AT STATION 526. REMOVED CORROSION, INSTALLED CUSP DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: SEAT TRACK — CORRODED (FS 1174-1308)

TUL - FOUND CORROSION ON SEAT TRACK NR 1. REMOVED CORRODED SEAT TRACK NR 1 AND INSTALLED NEW SEAT TRACK NR 1 FROM FS 1174-1308 SRM 51-01. (M)

Part: LIGHT — INOPERATIVE (AFT GALLEY)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (SERVICE DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT SERVICE DOOR FLOOR EMERGENCY EXIT MARKER INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECTOR ON BATTERY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — FAILED (CABIN)

DFW - DURING MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH FLAT JUMPER WIRE AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

DFW - FLT 352 - EN ROUTE SAN/DFW DURING CRUISE, EMERGENCY FLOOR LIGHTS AT MID-CABIN (ROWS 21 THROUGH 33) ILLUMINATED AND COULD NOT BE EXTINGUISHED FROM F/A SWITCH OR COCKPIT SWITCH. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPAIRED SHORTED WIRE IN EMERGENCY FLOOR LIGHT FEEDER HARNESS AT MID-CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)