N7539A

Part: BATTERY PACK — UNSECURE (CABIN) · airframe 63,040 hrs · 32,922 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. SECURED BATTERY TERMINALS. OPS CHECK NORMAL.

Part: TAB — DENTED (RT WING) · airframe 62,582 hrs · 32,681 cycles

TWO DENTS WITH DELAMINATE CLOSE TOGETHER, LOCATED 12 AND 10.25 INCHES FROM OUTBOARD END OF TAB. HOT BONDED REPAIR DOUBLER PER ESO 80087 AND SRM 51-70-02.

Part: TAB — DENTED (ZONE 600) · airframe 62,582 hrs · 32,681 cycles

TWO DENTS WITH DELAMINATE CLOSE TOGETHER, LOCATED 28.5 AND 27 INCHES FROM OUTBOARD END OF TAB. INSTALLED DOUBLER PER ESO 80087 AND SRM 51-70-02.

Part: TAB — DENTED (ZONE 600) · airframe 62,582 hrs · 32,681 cycles

TWO DENTS WITH DELAMINATE CLOSE TOGETHER LOCATED AT 5.5 AND 7.5 INCHES FROM INBOARD END OF TAB. ACCOMPLISHED DOUBLER REPAIR PER ESO 80087 AND SRM 51-70-02.

Part: TAB — DENTED (ZONE 600) · airframe 62,582 hrs · 32,681 cycles

DENT WITH DELAMINATE LOCATED 19 INCHES FROM INBOARD END OF TAB. INSTALLED DOUBLER PER ESO 80087 AND SRM 51-70-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,441 hrs · 32,594 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK FOR SEAT ROWS 28 TO 30. OPS CHECKS.

Part: ENGINE — FAILED (RIGHT) · airframe 61,801 hrs · 32,246 cycles

LIT - INFLIGHT DFW-MEM. CREW REPORTED LOSS OF RIGHT ENGINE OIL PRESSURE AND QUANTITY IN FLIGHT. RIGHT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 15 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT LIT ON 03/06/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

LARGE HUCK BOLT OR HI-LOCK PROTRUDING HEAD BETWEEN STATIONS 1041 TO 1060 AND LONGERON 10 RIGHT TO LONGERON 11 RIGHT. INSTALLED DOUBLER PER EA MD80-53-010378.

Part: FRAME — BENT (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

FRAME SEGMENT AT STATION 1220 LOWER LEG WAS BENT DURING FASTNER REMOVAL. REMOVED DAMAGED FRAME SEGMENT AND INSTALLED SERVICEABLE FRAME SEGMENT PER SRM 53-30-05, SRM 51-10-03 AND EA MD80-51-010298 REV C.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

FORWARD CABIN - CRACK IN LONGERON 3 LEFT AT STATION 160. REMOVED CRACKED LONGERON 3 LEFT AND REPLACED WITH NEW LONGERON AND SPLICE. SRM 53-02-00 FIGURE 18.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

DOOR BEAM HAS CORROSION STATIONS 1155 TO 1211. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

FORWARD LOWER CORNER OF DOOR OPENING LOWER BRACKET HAS CORROSION. REPLACED FORWARD LOWER CORNER BRACKET AT STATION 1155 PER SRM 51-30-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

FORWARD CABIN CRACK IN LONGERON 2 LEFT AT STATION 160. ACCOMPLISHED LONGERON REPAIR PER SRM 53-02-00 FIGURE 18.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

CORROSION IN SUB-FLOOR AT STATION 198 LEFT BUTTLINE 6. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

SEAT TRACK CORROSION BEYOND LIMITS. INSTALLED NEW SECTION OF NUMBER 3 SEAT TRACK FROM STATIONS 895 TO 936 AND SPLICES AT STATIONS 895 AND 936 PER SRM 53-05-55 FIGURE 4F.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

CORROSION ON STRINGER G1 GALLEY TIE-DOWN FITTING AT STATION 160. INSTALLED NEW CENTER G1 GALLEY TIE-DOWN FITTING PER SRM 51-30-05.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

CRACK IN SUB FLOOR AT FASTENER HOLE AT STATIONS 201 LEFT BUTTLINE 8. INSTALLED DOUBLER IN SUB FLOOR AT STATION 201 PER AARD 53-20-00-16.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

CRACK IN SUBFLOOR AT FASTENER HOLE AT STATION 149 RIGHT BUTTLINE 8. INSTALLED DOUBLER AT SUBFLOOR STATION 149 RIGHT BUTTLINE 8 PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

CORROSION ON BOTTOM OF SEAT TRACK FROM STATIONS 218 TO 303. REMOVED SEAT TRACK FROM STATIONS 216 TO 303 AND INSTALLED NEW SEAT TRACK FROM STATIONS 216 TO 303 AND TRACK SPLICE PER MM 53-40-01-2 AND SRM 53-05-00 FIGURE 4.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

DAMAGE TO CUSP SHEET BETWEEN SEAT TRACK 5 AND 6 STATIONS 200 TO 218. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

AFT ANGLE OF FRAME STATION 1271 LONGERON 29 LEFT AND LONGERON 29 RIGHT HAS CORROSION. INSTALLED REPAIR DOUBLER J-ANGLE PER AARD 53-10-00-17.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

CORROSION ON SUBFLOOR STATIONS 160 TO 200 APPROXIMATELY 6 INCHES INBOARD OF SERVICE DOOR JAMB. REPAIRED PER AARD 53-10-00-25.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

CUSP TO SEAT TRACK FASTENER HOLES DAMAGED AT STATION 1291 AT OUTBOARD SIDE OF NUMBER 2 SEAT TRACK. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

CORROSION ON G2 GALLEY TIE-DOWN FITTING AT STATION 218 INBOARD OF SEAT TRACK NUMBER 4. INSTALLED NEW GALLEY FITTING AT STATION 218 PER SRM 51-30-05.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

CUSP DAMAGED AT STATION 1142 NEAR LEFT NUMBER 2 DOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MOUNT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

G2 GALLEY MOUNT BRACKET UNDER SUBFLOOR STATION 218 CORRODED BEYOND LIMITS. REMOVED AND REPLACED BRACKET PER SRM 51-30-05.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

CORROSION ON SUBFLOOR AT G2 GALLEY MOUNT STATION 218. CUT OUT CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

CUSP TO SEAT TRACK FASTENER HOLES DAMAGED FROM STATIONS 1271 TO 1275 OUTBOARD OF NUMBER 2 SEAT TRACK. INSTALLED CUSP REPAIR DOUBLER FROM STATIONS 1271 TO 1275 AT OUTBOARD SIDE OF NUMBER 2 SEAT TRACK AS PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

CUSP SHEET DAMAGED AT STATION 1166. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (AILERON TAB) · airframe 56,927 hrs · 29,450 cycles

DENT ON TRAILING EDGE OF TAB 36 INCHES FROM TOP END. REMOVED 1 3/16 INCH LONG BY 1/4 INCH SKIN DAMAGE ON SIDE OF TRAILING EDGE. FABRICATED DOUBLER PER SRM / 51-70-02 PARAGRAPH 21E. HOT BONDED REPAIR PER SRM 51-70-02-PARAGRAPH 21E.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

HOLE PUNCTURED IN CUSP STATION 1236 LEFT. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

CORROSION AT RIGHT CUSP STA 934 TO 935 OUT OF LIMITS PER SRM 53-01 FIGURE 1 SHEET 3. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (G1 GALLEY) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

CORROSION ON INBOARD G1 GALLEY TIE-DOWN FITTING AT STA160. REMOVED AND REPLACED GALLEY MOUNT PER SRM 51-01-00.

Part: FITTING — WORN (LE SLAT) · airframe 56,927 hrs · 29,450 cycles

LEFT NUMBER 4 SLAT OUTBOARD KNUCKLE FITTING WORN. REMOVED OUTBOARD ATTACH FITTING, LOCATED, DRILLED, AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: SLAT — CRACKED (RT WING) · airframe 56,927 hrs · 29,450 cycles

FOUND .25 INCH CRACK INBOARD AFT CORNER OF RIB RIGHT WING ZERO LEADING EDGE SLAT. ROUTED OUT .25 INCH CRACK IN CLOSER RIB PER EA MD80-27-010250.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

CUSP SHEET DAMAGED AT STATION 546. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

WINDOW FRAME CRACKED RIGHT 39. INSTALLED DOUBLER PER AARD 53-10-00-52.

Part: RIB — CRACKED (LE SLAT) · airframe 56,927 hrs · 29,450 cycles

NUMBER 14 SLAT RIB CRACKED ON OUTBOARD SIDE RIGHT WING. REMOVED NUMBER 14 ATTACH FITTING. LOCATED, DRILLED, AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

WINDOW FRAME CRACKED RIGHT 37. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

SEAT TRACK NUMBER 3 STATIONS 1174 TO 1175 CORROSION OUT OF LIMITS. INSTALLED SEAT TRACK PLUG SRM 53-10-00.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

CABIN WINDOW FRAME CRACKED LOWER FORWARD CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: RIB — CRACKED (LE SLAT) · airframe 56,927 hrs · 29,450 cycles

NUMBER 15 SLAT RIB CRACKED AT OUTBOARD SIDE RIGHT WING. REMOVED NUMBER 15 ATTACH FITTING. LOCATED, DRILLED, AND INSTALLED NEW ATTACH FITTING PER ESO 80117.

Part: SKIN — CRACKED (PAX DOOR) · airframe 56,927 hrs · 29,450 cycles

DAMAGE TO OUTER SKIN DOUBLER AT HOLD-OPEN HOOK ENTRY. DAMAGED OUTER SKIN DOUBLER AT HOLD-OPEN HOOK ENTRY REPLACED PER SRM 52-05-00 FIGURE 20A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,927 hrs · 29,450 cycles

CORROSION ON LEFT CUSP SHEET AT STATION 456 OUT OF LIMITS PER SRM 53-01 FIGURE 1 SHEET 3. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

AFT ACCS SHEAR TIE CRACKED AT STATION 1451 FRAME AFT OF LONGERON 2L. INSTALLED NEW SHEAR TIE PER SRM 51-30-05.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

WRONG REPAIR ANGLE INSTALLED AT LOWER FORWARD CORNER OF NUMBER R32 WINDOW AT STATION 807. INSTALLED PROPER REPAIR ANGLE DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,927 hrs · 29,450 cycles

WINDOW PAN CRACKED AT UPPER FORWARD CORNER OF NUMBER R32 WINDOW. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

DENT WITH DEEP GOUGES ON FUSE SKIN LONGERON 15 LEFT STATION 365. INSTALLED PERMANENT REPAIR PER SRM 53-04-00 FIGURE 12B.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,927 hrs · 29,450 cycles

FUSELAGE EXTERIOR SKIN CRACKED STATION 1418 AT SHEAR TIE FASTENER LONGERON 2 LEFT TO 3 LEFT. INSTALLED REPAIR PER SRM 53-04-00 FIGURE 40 SHEET 1.

Part: CASTING — CRACKED (SPOILER) · airframe 56,927 hrs · 29,450 cycles

GROUND SPOILER FITTING CASTING HAS CRACKS. SPOILER CASTING REPLACED PER EA MD80 51-010298 REV C, BOEING DRAWING SR095700010, AARD 57-20-00-13.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,332 hrs · 28,559 cycles

OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,094 hrs · 28,423 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT FORWARD CABIN. OPS, NORMAL.

Part: BATTERY PACK — UNSECURE (CABIN) · airframe 55,094 hrs · 28,423 cycles

CABIN OVERHEAD EMERGENCY LIGHT ROW 27-30 INOPERATIVE. REPOSITIONED AND SECURED BATTERY PACK AT MID CABIN. OPS NORMAL.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 55,094 hrs · 28,423 cycles

FORWARD UPPER FLASHLIGHT SAFETY STRAP MISSING. REPLACED SAFETY STRAP FOR FORWARD UPPER FLASHLIGHT.

Part: CASTING — CRACKED (RT SPOILER) · airframe 53,318 hrs · 27,439 cycles

RIGHT GROUND SPOILER CASTING CRACKED. INSTALLED DOUBLER OF 17-7 PH 0.100 THICK, (FULL LENGTH), AARD 57-20-00-15.

Part: BEAM — CRACKED (ZONE 100) · airframe 53,318 hrs · 27,439 cycles

NOSE WHEEL WELL, LEFT J BEAM REPAIR DOUBLER CRACKED AT LOCK FASTENER AT UPPER AFT SIDE. REMOVED AND REPLACED DOUBLER PER AARD 53-10-00-4.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 52,054 hrs

LGA - EXTERNAL EMERGENCY LIGHT AT RT AFT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT RT AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: COVER — INOPERATIVE (L2 DOOR SLIDE)

ORD - LEFT NUMBER TWO DOOR SLIDE MANUAL INFLATION HANDLE COVER DOES NOT HOLD. REPLACED LEFT NUMBER TWO DOOR SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT SIGN LIGHT AT BOTH FORWARD OVERWING EXITS INOPERATIVE. RESEATED BATTERIES AND TIGHTENED CONNECTOR ON OVERHEAD BIN BATTERY PACK AT ROW 20 OR EMERGENCY EXIT SIGN LIGHT AT BOTH FORWARD OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — LOOSE (CABIN)

LGA - TWO OVERHEAD EMERGENCY LIGHTS IN TAIL CONE INOPERATIVE. SECURED LOOSE BATTERY PACKS FOR TWO OVERHEAD EMERGENCY LIGHTS IN TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

LAX) EMERGENCY LIGHTS POWERED BY POWER SUPPLY B5-107 INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY B5-107 BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SAT ALL EMERGENCY LIGHTS INOPERATIVE DUE TO COCKPIT EMERGENCY LIGHTS SWITCH LEFT IN ON POSITION OVERNIGHT. REPLACED ALL EMERGENCY BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — MALFUNCTIONED (RIGHT)

ATL T1679/29 EN ROUTE ATL-MIA RIGHT HAND ENGINE LOW OIL PRESSURE. RETURNED ATL WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: BATTERY PACK — DISCHARGED (CABIN)

RDU VENTRAL STAIRS SIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR VENTRAL STAIRS SIDE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROWS 24-26 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY FOR ROWS 24-26. SYTSEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION AROUND MOUNT HOLE FOR G-4 GALLEY IN NR 1 SEAT TRACK, STATION 1174. REMOVED CORRODED TRACK. INSTALLED NEW TRACK, STATION 1174 TO 1309 PER SRM 51-00. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND INDICATION OF CRACK IN LONGERON 16L STATION 1437. INSTALLED LONGERON REPAIR PER SRM 53-02-00. REINSTALLED SERVICEABLE SHELF INTERCOSTAL PER ESO 80559. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND SKIN GOUGED AT STATION 863 L9R. BLENDED DAMAGE PER SRM 53-04, ALODINED PER SRM 51-10-3, INSTALLED REPAIR DOUBLER PER SRM 53-04-00. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK INBOARD FLANGE AT CLIP NUTS STATION 1190-1205. BLENDED CORROSION PER SRM 53-01. INSTALLED DOUBLER STRAP PER AARD 53-22-00-13. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND DAMAGED FASTENER HOLE ON LEFT CUSP AT STATION 1250. DOUBLER INSTALLED AT LEFT CUSP STATION 1240-1250, AND SEALED PER SRM 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FLOOR PAN CUSP, BETWEEN SEAT TRACK 1 AND 2. REMOVED CORROSION AND INSTALLED NEW SECTION OF CUSP STATION 1250-1309 AS PER SRM 53-05. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION LOWER SIDE OF RIGHT CUSP STATION 1160. REMOVED CORROSION AND INSTALLED DOUBLER AS PER AARD 53-00-00-02. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED FROM FASTENER HOLE AT STATION 1380 ABOVE L14L. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-04. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED AT FASTENER HOLE STATION 1380 ABOVE LONGERON 14R. INSTALLED DOUBLER PER SRM 53-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 5 SEAT TRACK HAS EXFOLIATED CORROSION BETWEEN STATION 200-207. REPLACED SEAT TRACK NR 5 FROM STATION 200-245 AS PER SRM 53-05 SHEET 1. (M)

Part: WEB — TORN (FUSELAGE)

TUL - FOUND STRUCTURE UNDER FLOORING AT STATION 218, RIGHT INBOARD TORN. REPLACED STRUCTURE CUSP AT STATION 218-237 PER SRM 51-01 PAGE 1. (M)

Part: STRINGER — CRACKED (FUSELAGE)

TUL - FOUND STRINGER 4 LEFT CRACKED LOWER FLANGE AT STATION 160. INSTALLED REPAIR SPLICE PER SRM 53-00. (M)

Part: ANGLE — CRACKED (FUSELAGE)

TUL - FOUND HORIZONTAL ANGLE CRACKED IN RADIUS LOCATED BELOW F/O BRIEFCASE SHELF FORWARD SIDE OF FRAME STATION 120 RBL 49. REMOVED ANGLE AND REPLACED WITH NEW SRM 51-01. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND WINDOW FRAME CRACKED LOWER FORWARD LEG STATION 984 AT LONGERON 15R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-00-25. (M)

Part: WINDOW FRAME — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN LOWER FORWARD WINDOW FRAME STATION 807R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-00-29. (M)

Part: WIRE — DAMAGED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20DEF INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SCHRADER VALVE — MALFUNCTION (NLG STRUT)

DFW - FLT 1718 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR STRUT AND REPLACED SCHRADER VALVE. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

ORD - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AFT OF PAX SEAT ROW 21F INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 21F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — DEFECTIVE (LT POWER LEVER)

DFW - FLT 2093 - AFTER TAKEOFF PBI DURING CLIMB, RED GEAR LIGHT ILLUMINATED WITH GEAR HANDLE UP AND POWER LEVERS AT CLIMB POWER. ACCOMPLISHED QRH PROCEDURE AND AIRCRAFT PROCEEDED TO DFW, LANDING WITHOUT INCIDENT. REPLACED LEFT POWER LEVER SWITCH UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)