N14551

Part: BRACKET — CRACKED (ENTRY DOOR) · airframe 64,618 hrs · 33,500 cycles

FORWARD ENTRY DOOR INTERNAL STRUCTURE BRACKET AFT OF CENTER HUB CRACKED AT LOWER FASTENER. REPLACED BRACKET.

Part: LIGHT — MISSING (CABIN) · airframe 63,572 hrs · 32,906 cycles

ESCAPE PATH LIGHT AT SEAT 22D MISSING LAMP. REPLACED LAMP FOR ESCAPE PATH LIGHT AT SEAT 22D.

Part: LENS — MISSING (CABIN) · airframe 63,572 hrs · 32,906 cycles

ESCAPE PATH LIGHT AT SEAT 22D MISSING LENS. REPLACED LENS FOR ESCAPE PATH LIGHT AT SEAT 22D. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,572 hrs · 32,906 cycles

CEILING EMERGENCY LIGHT AT SEAT 27B INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT AT SEAT 27B. OPS CHECK NORMAL.

Part: SHROUD — MISSING (CABIN) · airframe 63,572 hrs · 32,906 cycles

ESCAPE PATH LIGHT AT SEAT 29D MISSING SHROUD. REPLACED SHROUD FOR ESCAPE PATH LIGHT AT SEAT 29D. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,202 hrs · 29,328 cycles

EMERGENCY LIGHTS FOR TAIL COMPARTMENT AND CATWALK AREA INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY PACK. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,202 hrs · 29,328 cycles

EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE FROM FIRST CLASS GALLEY TO ROW 15. REPLACED ESCAPE PATH LIGHTING BATTERY PACK. OPS CHECKS NORMAL.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

LOWER SIDE OF THE FORWARD SERVICE DOOR SILL SUB FLOOR IS CORRODED STATION 160 TO STATION 180 (AS VIEWED FROM THE E&E COMPARTMENT). COMPLETED INSTALLATION DOUBLER STATION 160-200, AND OVERLAY DOUBLER STATION 160-180 PER AARD 53-20-00-16.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION ON UPPER SURFACE OF BEAM ABOVE MID CARGO DOOR CUTOUT STATION 682. FINISHED INSTALLING BEAM CHANNEL PER SRM51-30-05 ABOVE MID CARGO DOOR CUTOUT STATION 682.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION ON OUTBOARD FLANGE OF NUMBER 5 SEAT TRACK FROM STATIONS 218 TO 237. COMPLETED INSTALLATION OF NUMBER 5 SEAT TRACK FROM STATION 218 TO 237 PER SRM 53-05-00 FIGURE 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION ON SUB-FLOOR AT STATIONS 158 TO 160 AND RIGHT BUTTLINE 44. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

FUSE STATION 674 AT RIGHT SIDE CUSP SHEET IS CRACKED SEEN FROM MID CARGO. INSTALLED CUSP REPAIR PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (CABIN) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION ON G2 GALLEY MOUNT AT STATION 218 AND RIGHT BUTTLINE 11. INSTALLED G2 GALLEY MOUNT PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION ON CUSP UNDER NUMBER 6 SEAT TRACK STATION 218 TO 226. INSTALLED NEW RIGHT CUSP SHEET AT STATION 218 TO 237 PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION ON G2 GALLEY MOUNT SUPPORT, BELOW SUBFLOOR, AT STATION 218 AND RIGHT BUTTLINE 11. INSTALLED NEW INBOARD AFT G2 MOUNT SUPPORT PER SRM 51-30-05.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

SUBFLOOR HAS CORROSION JUST INBOARD OF G-1 GALLEY FORWARD INBOARD MOUNT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

NUMBER 6 SEAT TRACK IS CORRODED AT STATION 215 ON UPPER SURFACE OF OUTBOARD LOWER FLANGE. INSTALLED NEW NUMBER 6 SEAT TRACK FROM STATION 215 TO STATION 266 PER AARD 53-20-00-01 AND SRM 53-05-00.

Part: MOUNT — CORRODED (CABIN) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

G-1 GALLEY FORWARD INBOARD MOUNT HAS CORROSION. INSTALLED NEW FORWARD INBOARD GALLEY MOUNT PER SRM 51-30-02 AND SRM 51-30-05.

Part: MOUNT — CORRODED (CABIN) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

G-1 GALLEY FORWARD CENTER MOUNT HAS CORROSION. INSTALLED NEW G1 GALLEY MOUNT PER SRM 51-30-05.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

CRACK IN SUBFLOOR STATION 162 AND RIGHT BUTTLINE 26. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

CORROSION ON SUBFLOOR STATION 218 AND RIGHT BUTTLINE 11 UNDER G2 GALLEY MOUNT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

SUB FLOOR HAS CORROSION FORWARD OF NUMBER 6 SEAT TRACK. INSTALLED REPAIR PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

SUB FLOOR HAS CORROSION AFT CORNER OF FORWARD SERVICE DOOR OPENING. INSTALLED REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION RIGHT CUSP STATIONS 1250 TO 1271 IS OUT OF LIMITS. INSTALLED NEW CUSP SHEET FROM STATION 1250 TO STATION 1309 PER SRM 51-30-02.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

FORWARD EMERGENCY EQUIPMENT COMPARTMENT, AFT SIDE OF STATIONS 160 TO 170, CORROSION ON BOTTOM SIDE OF CUSP. INSTALLED REPAIR PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

SUB FLOOR HAS CORROSION STATION 180 JUST INBOARD OF FORWARD SERVICE DOOR. INSTALLED REPAIR PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION ON BOTTOM OF SUBFLOOR, STATION 200, RIGHT BUTTLINE 10 TO RIGHT BUTTLINE 44. INSTALLED DOUBLER ON SUBFLOOR, STATION 200, RIGHT BUTTLINE 10 TO RIGHT BUTTLINE 44 PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

HEAVY CARGO/AFT CORROSION ON CUSP RIGHT SIDE STATION 1158. INSTALLED DOUBLER PER AARD 53-20-00-16, SRM 51-30-01, SRM 51-30-02, SRM 51-30-05, AND EA MD80-51-011812 OEM DRAWING REV A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

LEFT CUSP CORRODED BEYOND LIMITS AT STATION 1271 THRU 1274 BETWEEN SEAT TRACKS NUMBER 1 AND 2. REMOVED AND REPLACED CUSP SHEET FROM STATION 1250 TO 1309 PER AARD 53-20-00-16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

CABIN OVERWING FITTING CRACKED BELOW TRACK 4 STATION 927. INSTALLED NEW FITTING PER EA MD80-51-011812 OEM DRAWING REV C.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

LEFT TIE DOWN TRACK HAS CORROSION FROM STATION 1008 TO 1212. REMOVED TIE DOWN TRACK LEFT 1008 TO 1212. INSTALLED NEW TIE DOWN TRACK LEFT STATION 1008 TO 1212 PER SRM 51-30-01.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

HEAVY CARGO/AFT- CORROSION ON TIE DOWN TRACK LEFT SIDE STATION 1060 TO 1079. REMOVED TIE DOWN TRACK LEFT STATION 1008 TO 1212. INSTALLED NEW TIE DOWN TRACK LEFT HAND STATION 1008 TO 1212 PER SRM 51-30-01.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

REMOVED TIE DOWN TRACK LEFT 1008 TO 1212. INSTALLED NEW TIE DOWN TRACK LEFT STATION 1212 TO 1322 PER SRM 51-30-01. REMOVED AND INSTALLED NEW SPLICE STATION 1218 TO 1228 PER SRM 51-30-05.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

DENT IN FUSELAGE STATION 1305 ABOVE LONGERON 19 RIGHT. DENT FOUND TO BE WITHIN LIMITS PER SRM 53-04 FIG 38 SHEET 11 COND 1B. DYE CHECKED NO CRACKS FOUND E58 1026761 TST 49590 CYL 25123, INSTALLED TWO ROW DOUBLER AS PER BOEING DRAWING SG09530001 AND SRM 53-04-02 THIS IS A PERMANENT REPAIR.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION AT RIGHT CUSP STATION 1220 IS OUT OF LIMITS. REPLACED RIGHT CUSP FROM STATIONS 1174 TO 1250 PER AARD 53-20-00-16.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

LEFT TIE DOWN TRACK HAS CORROSION FROM STATION 1212 TO 1322. REMOVED TIE DOWN TRACK LEFT 1008 TO 1212. INSTALLED NEW TIE DOWN TRACK LEFT STATION 1212 TO 1322 PER SRM 51-30-01.

Part: CUSP WEB — PUNCTURED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

CABIN LEFT CUSP HAS A PUNCTURE AT STATION 498. INSTALLED DOUBLER PER AARD 52-20-0016.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

SHEAR TIE SUPPORT CRACKED AT STATION 1460 LEFT SIDE OF Y DUCT. INSTALLED SHEAR TIE AT STATION 1460 LONGERON 2 LEFT AND LONGERON 3 LEFT PER SRM 51-30-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

AFT ACCESSORY 1510 CANT FRAME CRACKED ABOVE AND BELOW MAINTENANCE LIGHT SWITCH. REMOVED DAMAGED SECTION OF FRAME FROM LONGERON 10 LEFT TO 30 AND INSTALLED NEW SECTION PER EA MD80-51-011812.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

DENT IN SKIN AT STATION 218 LEFT SIDE BETWEEN LONGERONS 15 LEFT AND 16 LEFT. INSTALLED CLASS 1 EXTERNAL DOUBLER PER SRM 53-04-00 FIG 12B FUSELAGE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

HEAVY CARGO/AFT- CORROSION ON DOOR CUTOUT BEAM SEVERAL PLACES STATION 1155 TO 1211. INSTALLED BEAM DOUBLER PER AARD 53-10-00-3.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CUSP TEE CORRODED BEYOND LIMITS RIGHT STATION 200. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-14.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION ON RIGHT TIE-DOWN TRACK CENTER ATTACH STATION 1145. REMOVED AND REPLACED TRACK PER SRM 51-30-01.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

LIGHTENING HOLES AT LEFT CUSP STATION 927 TO 946 FLANGES OUT OF LIMITS. INSTALLED NEW CUSP SHEET ON LEFT SIDE STATION 905 TO 946 PER AARD 53-20-00-16.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

HEAVY CARGO/AFT- CORROSION ON DOOR CUTOUT BEAM WEB STATION 1155 TO 1193. INSTALLED NEW SERVICEABLE WEB PER SRM 51-30-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

RIGHT CUSP IS CORRODED OUT OF LIMITS FROM STATION 1200 THRU 1220. REMOVED AND REPLACED CUSP SHEET FROM STATION 1174 TO 1250 PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

LEFT CUSP CRACKED AT STATION 219. REMOVED CUSP SHEET FROM STATION 218 TO 237 AND INSTALLED NEW SHEET PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

INTERCOSTAL CRACKED INBOARD OF AFT CARGO DOOR BEAM STATION 1193. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-02.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

LEFT CUSP IS CRACKED AT STATION 498. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

CABIN OVERWING FLOORBEAM CRACKED STATION 927 LONGERON 18 RIGHT. INSTALLED NEW FLOORBEAM PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

CABIN LEFT CUSP HAS CORROSION AT STATION 1174. ROUTED OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CORROSION REMOVAL OUT OF LIMITS ON RIGHT CUSP STATION 563 TO 566. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

CUSP TEE HAS CORROSION AT RIGHT STATION 200. INSTALLED REPAIR PER AARD 53-20-00-14.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

INTERCOSTAL CRACKED AT BUTTLINE O FROM STATIONS 1497 TO 1510. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW PER SRM 51-30-2.

Part: BEAM — CRACKED (PAX DOOR) · airframe 56,652 hrs · 29,007 cycles

FORWARD ENTRY PASSENGER DOOR NUMBER 2 BEAM CRACKED AT FORWARD END. FORWARD ENTRY PASSENGER DOOR INSTALLED DOUBLER ON NUMBER 2 BEAM FORWARD END PER ESO 80172.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

CRACK FOUND UNDER LEFT HORSESHOE COLLAR AT STATION 847. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

AFT CARGO - CORROSION ON THE AFT SIDE OF THE FUSELAGE FRAME AT STATION 1287 LONGERON 30 TO LONGERON 29 RIGHT. INSTALLED SHEAR TIE SPLICE PER SRM 53-30-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,652 hrs · 29,007 cycles

RIGHT CUSP STATION 870 CORROSION IS OUT OF LIMITS. INSTALLED REPAIR DOUBLER AT RIGHT CUSP SHEET OUTBOARD OF NUMBER 6 SEAT TRACK STATION 870 PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

DENT IN FUSELAGE SKIN AT STATION 237 LONGERON 18 LEFT TO 19 LEFT. INSTALLED PERMANENT REPAIR PER SRM 53-04-00 FIGURE 12B.

Part: RIB — CRACKED (LE SLAT) · airframe 56,652 hrs · 29,007 cycles

RIGHT WING NUMBER 5 SLAT: HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES A CRACK ON NUMBER 15 SLAT RIB MOST OUTBOARD RIB. REPLACED CRACKED RIB OUTBOARD MOST NUMBER 15 POSITION RIGHT SLAT PER ESO 80117.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

DENT IN SKIN OUT OF LIMITS. INSTALLED DOUBLER PER SRM 53-04-00.

Part: RIB — CRACKED (LE SLAT) · airframe 56,652 hrs · 29,007 cycles

RIGHT WING NUMBER 5 SLAT: HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES A CRACK ON NUMBER 14 SLAT RIB 2ND FROM OUTBOARD. REPLACED CRACKED RIB 2ND FROM OUTBOARD NUMBER 14 POSITION RIGHT NUMBER 5 SLAT PER ESO 80117.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 56,652 hrs · 29,007 cycles

CRACK IN LEFT WINDOW FRAME STATION 946 LOWER FORWARD CLIP. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — DAMAGED (WINDOW) · airframe 56,652 hrs · 29,007 cycles

WINDOW PAN DAMAGED AT STATION 1098. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — DAMAGED (WINDOW) · airframe 56,652 hrs · 29,007 cycles

WINDOW PAN DAMAGED AT STATION 1060. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 56,652 hrs · 29,007 cycles

WINDOW PAN CRACKED AT STATION 1174. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — DAMAGED (WINDOW) · airframe 56,652 hrs · 29,007 cycles

WINDOW PAN DAMAGED AT STATION 1041. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 56,652 hrs · 29,007 cycles

CRACK IN LEFT UPPER AFT WINDOW FRAME CLIP STATION 1022. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: PAN — DAMAGED (WINDOW) · airframe 56,652 hrs · 29,007 cycles

WINDOW PAN DAMAGED AT STATION 1078. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 56,652 hrs · 29,007 cycles

DENT IN FUSELAGE STATION 1305 ABOVE LONGERON 19 RIGHT. INSTALLED TWO ROW DOUBLER AS PER BOEING DRAWING SG09530001 AND SRM 53-04-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,355 hrs · 28,847 cycles

LEFT NUMBER 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AT LEFT NUMBER 2 DOOR FOR EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: ANTI-ICE VALVE — INOPERATIVE (RT ENGINE) · airframe 55,486 hrs · 28,379 cycles

AUS - INFLIGHT FLL-DFW. CREW TURNED ON ENGINE ANTI-ICE IN CRUISE AND DISAGREE LIGHT ILLUMINATED. NO CIRCUIT BREAKER POPPED OR OTHER INDICATIONS. FLIGHT DIVERTED AUS LANDED WITHOUT INCIDENT. FOUND COWL ANTI ICE VALVE INOPERATIVE. REPLACED RIGHT ENGINE COWL ANTI ICE VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,208 hrs · 27,657 cycles

FORWARD FEED, FORWARD SECTION OF EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED AB5-1 BATTERY PACK. FORWARD FEED NOW OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,208 hrs · 27,657 cycles

EMERGENCY LIGHTS AFT OF ROW 20 INOPERATIVE. FOUND AB5-3 BATTERY PACK DEFECTIVE. REPLACED BATTERY PACK. EMERGENCY LIGHTS NOW GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,208 hrs · 27,657 cycles

EMERGENCY LIGHTS AFT OF ROW 20 INOPERATIVE. FOUND AB5-4 BATTERY PACK DEFECTIVE. REPLACED BATTERY PACK. EMERGENCY LIGHTS NOW GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,957 hrs · 27,523 cycles

FORWARD OVERWING EMERGENCY LIGHT SIGNS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR FORWARD OVERWING EMERGENCY LIGHT SIGN. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,626 hrs

LGA - AFT LAVATORY EMERGENCY BATTERY DEPLETED. REPLACED BATTERY PACK FOR AFT LAVATORY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,062 hrs · 27,028 cycles

STATION 1485 CANTED FRAME LEFT UPPER WEB IS CRACKED. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-32.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,062 hrs · 27,028 cycles

STATION 1510 CANTED FRAME IS CRACKED AT LEFT LOWER ALIGNMENT PIN. INSTALLED DOUBLER PER EA MD80-53-005724 DATED 03/16/09.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,960 hrs

LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 6 TO 9 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN 6F FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,960 hrs

LGA EMERGENCY LIGHTS AT OVERHEAD COCKPIT INOPERATIVE. REPLACED BATTERY PACK AT FIRST CLASS OVERHEAD ELECTRICAL BAY FOR EMERGENCY LIGHTS AT OVERHEAD COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: DOOR — SEPARATED (RT MLG) · 51,910 cycles

INFLIGHT T376/30SEP. CREW REPORTED RT GEAR DOOR OPEN LIGHT REMAINED ON AFTER RETRACTION. RAN CHECKLIST AND LIGHTS WENT OUT. NO OTHER ABNORMAL INDICATIONS REPORTED. LANDED DFW WITHOUT INCIDENT AND FOUND RLG STRUT DOOR MISSING WITH HINGE STILL ATTACHED TO ACFT. BOTH SUPPORT RODS HAND THE ENDS THAT ATTACHED TO THE DOOR BROKEN OFF AND MISSING. REMOVED DAMAGED HINGE AND REPLACED RLG DOOR ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,204 hrs

LGA - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,204 hrs

LGA - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 50,204 hrs

LGA - EMERGENCY FLASHLIGHT AT FORWARD JUMPSEAT HAS BROKEN SAFETY STRAP. REPLACED SAFETY STRAP FOR EMERGENCY FLASHLIGHT AT FORWARD JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — DISCHARGED (NLG) · airframe 49,730 hrs

ORD INFLIGHT T1447/21DEC - AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND STRUT FLAT. PERFORMED STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 9D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — CRACKED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT LEFT AFT OVERWING EMERGENCY EXIT SIGN COVER IS CRACKED. REPLACED COVER FOR EMERGENCY LIGHT AT LEFT AFT OVERWING EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT CEILING TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK AT B5 28 FOR EMERGENCY LIGHTS AT CEILING TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT MID CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK B5 104 FOR EMERGENCY LIGHTS AT MID CABIN CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 12D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT FORWARD RIGHT HAND OVERHEAD SIGN INOPERATIVE. RELAMPED EMERGENCY LIGHT AT FORWARD RIGHT HAND OVERHEAD SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — LOOSE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AFT CABIN AND STAIRWAY INOPERATIVE. RESEATED BATTERIES AND CYCLED POWER FOR EMERGENCY LIGHTS AT AFT CABIN AND STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY CEILING LIGHTS AT ROWS 3 TO 6 AND 23 TO 26 INOPERATIVE. REPLACED BATTERY PACKS AT ROWS 6 AND 25 FOR EMERGENCY CEILING LIGHTS AT ROWS 3 TO 6 AND 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING AT 12D INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - ENTRY AISLE AND FORWARD GALLEY CEILING EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK AT B523 FOR OVERHEAD ENTRY AISLE AND FORWARD GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — FAILED (R1 DOOR)

PHL - WHEN GROUND CREW WAS PREPARING TO TOW AIRCRAFT TO THE GATE THE RIGHT 1 GALLEY DOOR WAS OPENED BY GROUND CREW FROM THE INSIDE AND THE SLIDE FELL OUT. SLIDE DEPLOYED BY ONLY PARTIALLY INFLATING. FERRIED AIRCRAFT TO DFW FOR SLIDE REPLACEMENT. REPLACED R1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - AFT OVERHEAD EMERGENCY EXIT DOOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5-105 FOR AFT OVERHEAD EMERGENCY EXIT DOOR LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - AFT ACCESSORY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5-28 FOR AFT ACCESSORY OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RELAY — FAILED (CABIN)

DFW - DURING OVERWING EMERGENCY LIGHTS INOPERATIVE FROM FLIGHT ATTENDANT SWITCH. REPLACED RELAY R2 271. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH FORWARD RED LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT SEAT PATH LIGHT. SYSTEM GORUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS ROW 23-26 INOPERATIVE. REATTACHED EMERGENCY EXIT LIGHT BATTERY AT SEAT 23-26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRUCTURE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION STATION 1149-1212. REMOVED CORROSION, INSTALLED DOUBLER PER ESO 80559. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

TUL - FOUND AFT EDGE OF FLOORBOARD CORRODED UNDER F/O'S SEAT. REPLACED FLOORBOARD TOP SKIN SHEET AND INSTALLED FLOORBOARD PER SRM 51-01. (M)

Part: BRACKET — CORRODED (FUSELAGE)

TUL - FOUND CORROSION FORWARD LOWER DOOR CORNER CUTOUT BRACKET. INSTALLED NEW SERVICEABLE FORWARD LOWER DOOR CORNER CASTING AT STATION 1145-1146. (M)

Part: LAMP — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21D TOO BRIGHT. REPLACED EMERGENCY EXIT LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — MALFUNCTIONED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 13D DIM. REPLACED EMERGENCY EXIT LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — ARCED (CABIN)

LGA - DURING OVERNIGHT MAINTENANCE WHILE IN HANGAR UPPER SIDEWALL FLOURESCENT LIGHT STARTED ARCING. SMOKE ACCUMULATED IN CABIN. LIGHT FIXTURE OVER SEAT 25AB BURNED. REPLACED BAD LIGHT SOCKET. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: VALVE — DEFECTIVE (NLG)

DFW - FLT 1760 - AFTER TAKEOFF DFW EN ROUTE MCO, NOSE GEAR WOULD NOT RETRACT. AIR INTERRUPTED BACK DFW AND LANDED WITHOUT INCIDENT. REPLACED SHRADER VALVE AND SERVICED NOSE GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CORRODED (BS 370-427)

TUL - FOUND CORROSION ON DOOR JAMB FORWARD EDGE TO AFT EDGE, LOWER END. REMOVED AND REPLACED LOWER DOOR JAMB PER SRM 53-05. (M)

Part: APU — LEAKING (APU COMPARTMENT)

BOS - FLT 0487 - AFTER TAKEOFF EN ROUTE BOS/MIA - CREW NOTED VISIBLE SMOKE IN CABIN. SMOKE WAS CLEARLY VISIBLE AS THICK AS FOG, DECLARED AN EMERGENCY AND AIR INTERRUPTED. LANDED BOS WITHOUT INCIDENT. REPLACED APU DUE TO LEAKING OIL. REPLACED BOTH COALESCER BAGS PER MM. ACCOMPLISHED APU BURN-OUT. SYSTEM GROUND CHECKED NORMAL. (X)

Part: ACM — DEFECTIVE (RT ACM BAY)

DFW - FLT 1935 - AFTER TAKEOFF DFW, CREW REPORTED STRONG ACRID SMELL AND SMOKE IN REAR OF CABIN. AIRCRAFT RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED RIGHT HAND AIR CYCLE MACHINE AND BOTH COALESCER BAGS. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. PERFORMED PACK BURN-OUT PROCEDURE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - FLT 867 - DURING OVERNIGHT CHECK, FOUND THE FORWARD EMERGENCY ARM LIGHT ASSEMBLY INOPERATIVE. REPLACED FORWARD EMERGENCY ARM LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT AT AFT VENTRAL STAIR WALL BROKEN. REPLACED EMERGENCY LIGHT AT AFT VENTRAL STAIR WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FUEL PUMP — DEFECTIVE (RT ENGINE)

ORD - FLT 1236 - AFTER TAKEOFF ORD DURING INITIAL CLIMB, RIGHT ENGINE EXPERIENCED FLAME OUT. ACCOMPLISHED ENGINE SHUTDOWN PROCEDURE AND AIRCRAFT RETURNED TO ORD, LANDING WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL PUMP AND FUEL CONTROL. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 20 AND AFT INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR AT AFT END OF MAIN CABIN SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LATCH — OUT OF ADJUST (AFT FUSELAGE)

TUL - FLT 746 - AFTER TAKEOFF TUL DURING CLIMB-OUT, TAILCONE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO TUL AND LANDED WITHOUT INCIDENT. ADJUSTED TAILCONE LATCH. PRECAUTIONARY CHECKED TAILCONE RIGGING WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)