N555AN

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 75,257 hrs · 39,751 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE REAR DOOR DOES NOT SHOW A FLASHING RED LIGHT. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY PER AMM 25-23-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,122 hrs · 39,662 cycles

AIRCRAFT WAS NOT GROUNDED. OVERHEAD EMERGENCY EXIT SIGN BY THE FORWARD OVERWING DOOR IS INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 75,055 hrs · 39,618 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IN THE AFT TAILCONE FORWARD LOCATION DOES NOT TURN ON OR OFF. REMOVED AND REPLACED BATTERY PACK PER AMM 25-60-00. OPERATIONAL CHECK GOOD.

Part: TOGGLE — CONTAMINATED (TAILCONE SLIDE) · airframe 75,038 hrs · 39,607 cycles

TAILCONE SLIDE LANYARD LATCH TOGGLE ON THE RIGHT SIDE IS GUMMED UP AND STICKING. CLEANED AND LUBED THE LATCH AND ACCOMPLISHED SUCCESSFUL SLIDE DEPLOYMENT. REPLACED SLIDE ASSEMBLY IAW AMM 25-62-01. OPS CHECKED GOOD.

Part: STIFFENER — CRACKED (BS 218 BULKHEAD) · airframe 75,038 hrs · 39,607 cycles

CRACK INDICATION ON THE STIFFENER LOWER END AT BS 218, BULKHEAD BETWEEN LONGERONS 23L AND 24L. REPAIRED THE STIFFENER IAW SRM 53-01-00-001, FIGURE 2.

Part: LONGERON — CRACKED (BS 160) · airframe 75,038 hrs · 39,607 cycles

CRACKED LONGERON 24L, BS 160. REPAIRED THE LONGERON IAW SRM 53-02-00-001.

Part: LONGERON — CRACKED (BS 160) · airframe 75,038 hrs · 39,607 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACKED LONGERON 25L AT BS 160. REPAIRED THE LONGERON IAW SRM 53-02-00-001.

Part: LONGERON — CRACKED (BS 200) · airframe 75,038 hrs · 39,607 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACKED LONGERON 23L AT BS 200. REPAIRED LONGERON IAW SRM 53-02-00-001.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 74,875 hrs · 39,500 cycles

CORROSION ON OUTBOARD LEFT WING FLAP CENTER HINGE FITTING AT THE AFT SPAR LOWER INBOARD BOLT. REMOVED AND REPLACED HINGE FITTING IAW AMM 57-40-01-201.

Part: OIL FILTER — CLOGGED (NR 2 ENGINE) · airframe 74,615 hrs · 39,352 cycles

THE AIRCRAFT WAS GROUNDED. RT ENGINE OIL STRAINER CLOG LIGHT CAME ON DURING APPROACH. MOVED THE RIGHT THROTTLE BACK TO IDLE AND THE LIGHT WENT OUT. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE OIL FILTER. INSPECTED AND FOUND CARBON ONLY, NO METAL IN FILTER. ACCOMPLISHED MCM 71-91-14, 71-91-11 AND 7907.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 74,547 hrs · 39,312 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT ENGINE INLET FUEL PRESSURE LOW LIGHT FLICKERS CONTINUOUSLY IN FLIGHT WITH FULL MAIN FUEL TANKS. REMOVED AND REPLACED THE LOW FUEL INLET PRESSURE CAUTION SWITCH PER AMM 73-33-01. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — DIRTY (L2 DOOR SLIDE) · airframe 74,517 hrs · 39,293 cycles

L2 DOOR GIRT BAR IS DIFFICULT TO ARM AND DISARM. CLEANED GIRT BAR. OPS CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 74,379 hrs · 39,211 cycles

EMERGENCY LIGHTS DO NOT TURN ON. REMOVED AND REPLACED BATTERY POWER SUPPLY AT OVERHEAD BIN 29 IAW AMM 33-60-98-401. OPS CHECKED GOOD, OK FOR SERVICE. THE AIRCRAFT WAS GROUNDED.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 74,379 hrs · 39,211 cycles

EMERGENCY LIGHTS DO NOT TURN ON. REPAIRED THE NR 3 WIRE IN THE OVERHEAD BIN 29, BATTERY POWER SUPPLY IAW AMM 20-31-00. OPS CHECK GOOD, OK FOR SERVICE. THE AIRCRAFT WAS GROUNDED.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 74,379 hrs · 39,211 cycles

EMERGENCY LIGHTS DO NOT TURN ON. REMOVED AND REPLACED BATTERY POWER SUPPLY AT OVERHEAD BIN 13 IAW AMM 33-60-98-401. OPS CHECK GOOD, OK FOR SERVICE. THE AIRCRAFT WAS GROUNDED.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 74,092 hrs · 39,036 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DURING DESCENT A RAPID DEPRESSURIZATION WITH LOSS OF BOTH PACKS WAS REPORTED ACCOMPANIED BY WARNINGS FOR AUTO THROTTLES, AUTO PILOT, AIRSPEED INDICATOR AND MACH TRIM. REMOVED AND REPLACED CENTRAL AIR DATA COMPUTER NR 1 IAW AMM 34-16-01. LEAK AND OPS CHECKED IAW AMM 30-30-00, 34-11-02, 22-01-05, AND 21-32-03 SATISFACTORY.

Part: SENSOR — FAULTY (AC BAY) · airframe 73,840 hrs · 38,870 cycles

LT PACK CYCLED OFF THEN ON MULTIPLE TIMES DURING T/O. IT WAS ACCOMPANIED BY AN ODOR OF DIRTY SOCKS. DISCHARGE TEMP SENSOR REPLACED ON NON ROUTINE PER 21-31-05. OPERATED PACK PER MM 21-00-00-001 OPS CHECK GOOD. THE AIRCRAFT WAS GROUNDED.

Part: LANYARD — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 73,789 hrs · 38,837 cycles

R1 DOOR SLIDE PACK IS LOOSE. INSTALLED THE GIRT BAR LANYARD IAW AMM 25-62-00. OPERATIONAL CHECKED GOOD.

Part: LATCH — DIRTY (GIRT BAR) · airframe 73,734 hrs · 38,800 cycles

L2 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR IS DIFFICULT TO ARM AND DISARM. REMOVED DEBRIS FROM GIRT BAR LATCH IAW AMM 25-62-00. OPERATIONAL CHECKED GOOD.

Part: PIN — UNSECURE (R1 DOOR) · airframe 73,442 hrs · 38,615 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE LANYARD PIN PROTRUDING FROM PACK. SECURED THE PIN IAW AMM 25-62-00. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: RECEPTACLE — DIRTY (ZONE 800) · airframe 73,411 hrs · 38,599 cycles

AIRCRAFT NOT GROUNDED. L2 DOOR EMERGENCY EVACUATION GIRT BAR IS DIFFICULT TO ARM AND DISARM. CLEANED AND LUBRICATED GIRT BAR RECEPTACLE. OPERATIONAL CHECK GOOD.

Part: LANYARD — DETACHED (R1 DOOR) · airframe 73,355 hrs · 38,567 cycles

AIRCRAFT NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE LANYARD DETACHED FROM SLIDE. SECURED LANYARD IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,045 hrs · 38,375 cycles

EMERGENCY LIGHTS IN ROWS 28 THROUGH 32 FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK B5-107 IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: GIRT BAR — DIRTY (L2 DOOR) · airframe 73,031 hrs · 38,365 cycles

AIRCRAFT NOT GROUNDED. L2 EMERGENCY DOOR ESCAPE SLIDE GIRT BAR DIFFICULT TO ARM/DISARM. CLEANED GIRT BAR IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.

Part: INDICATOR — STICKING (NR 1 EPR) · airframe 73,297 hrs · 38,338 cycles

DURING TAKE OFF ROLL THE NR 1 ENGINE DID NOT ACCELERATE PAST 1018 EPR. TAKE OFF ABORTED AT APPROXIMATELY 25 KNOTS. MAINTENANCE REMOVED AND REPLACED THE NR 1 EPR INDICATOR AND NR 1 EPR COMPUTER ASSEMBLY AND ACCOMPLISHED SATISFACTORY ENGINE RUN IAW AMM 77-11-02-77-10-00 AND 72-00-00. SYSYTEM CHECKS NORMAL. AIRCRAFT WAS GROUNDED.

Part: COMPUTER — FAULTED (NR 1 EPR) · airframe 73,297 hrs · 38,338 cycles

DURING TAKE OFF ROLL THE NR 1 ENGINE DID NOT ACCELERATE PAST 1018 EPR. THE TAKE OFF WAS ABORTED AT APPROXIMATELY 25 KNOTS. MAINTENANCE REMOVED AND REPLACED THE NR 1 EPR INDICATOR AND NR 1 EPR COMPUTER ASSEMBLY AND ACCOMPLISHED SATISFACTORY ENGINE RUN IAW AMM 77-11-02-77-10-00 AND 72-00-00. SYSYTEM CHECKS NORMAL. AIRCRAFT WAS GROUNDED.

Part: PRBC — DAMAGED (NR 1 ENGINE) · airframe 72,993 hrs · 38,338 cycles

AIRCRAFT WAS GROUNDED. DURING TAKEOFF ROLL THE NR 1 ENGINE WOULD NOT ACCELERATE BEYOND 1.2 EPR WITH RPM INDICATING LOWER THAN RIGHT ENGINE. ABORTED TAKEOFF AT APPROXIMATELY 20 KNOTS. MAINTENANCE FOUND NR 1 ENGINE PRESSURE RATIO BLEED CONTROL(PRBC) SCREEN BLOWN OUT. REMOVED AND REPLACED PRBC ASSEMBLY IAW AMM 75-31-01. OPERATIONAL CHECKS AND ENGINE RUN AT ALL POWER SETTINGS NORMAL.

Part: GIRT BAR — DISCONNECTED (ZONE 800) · airframe 72,964 hrs · 38,319 cycles

AIRCRAFT NOT GROUNDED. FORWARD RIGHT GALLEY DOOR GIRT BAR DISCONNECTED FROM EMERGENCY EVACUATION SLIDE PACK. RECONNECTED GIRT BAR. OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,228 hrs · 37,300 cycles

THE FUSELAGE SKIN IS CRACKED AT TWO FASTENERS ALONG L22 LT, APPROX STATION 167 & 191. INSTALLED INTERIM DOUBLER REPAIR IAW DWG SRO9530219-7003. ACFT IN BASE MX.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 71,228 hrs · 37,300 cycles

FOUND MID CARGO DOOR STOP BRACKET CRACKED AT CTR FWD SIDE OF DOOR. R & R DOOR STOP FITTING AT CTR FWD SIDE OF MID CARGO DOOR IAW AARD 51-00-05-1, DWG 4920233 & 5910141. ACFT IN BASE MX.

Part: PORTABLE LIGHT — FAILED (CABIN) · airframe 70,971 hrs · 37,150 cycles

L1 DOOR PORTABLE EMER LIGHT FAILED TO TEST. LOWER LATCH COVER IS ALSO MISSING. REPLACED L1 DOOR PORTABLE EMER LIGHT ASSEMBLY IAW AMM 33-53-00. TESTED OK. THE ACFT WAS NOT GNDED.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 69,620 hrs · 36,333 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB THE TAIL COMPARTMENT TEMP HIGH WARNING ILLUMINATED. ACCOMPLISHED MCM 0930 & FOUND LT TEMP CONTROL VLV FAULTED. R & R TEMP CONTROL VLV IAW 21-61-01. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 68,052 hrs · 35,443 cycles

EMERGENCY DECLARED & LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING CLIMB RECEIVED A SLAT OVERSPEED WARNING & DISAGREE LIGHT ILLUMINATED WHILE ACCELERATING THROUGH 280 KNOTS. AUTOPILOT WOULD NOT HOLD ATTITUDE. FLIGHT CONTROLS WERE VERY HEAVY WHEN AUTOPILOT DISENGAGED. ACCOMPLISHED QRH. WHEN FLAPS MOVED TO 11 DEGREES DISAGREE LIGHT WENT OUT & TAKEOFF ILLUMINATED. PERFORMED BITE CHECK OF PROXIMITY SWITCH ELECTRONIC UNIT, CHECK OF SENSORS C & D IAW AMM 27-80-06 & CHECK OF FLAP SLAT INDICATOR IAW AMM 27-80-00-201 WITH NO FAULTS FOUND.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 67,995 hrs · 35,410 cycles

RIGHT WING NR 4 SLAT TRACK INBD RIB CRACKED. ACCOMPLISHED NESTED ANGLE REPAIR IAW EA MD80-57-037132.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

CORROSION ON NR 1 SEAT TRACK FROM STATIONS 1174 TO 1309. REPLACED NR 1 SEAT TRACK IAW SRM 53-05-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

LEFT CUSP AT STATION 1169 CORRODED. REMOVED CORROSION DAMAGE & INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

CORROSION ON NR 2 SEAT TRACK FROM STATIONS 1153 TO 1193. ACCOMPLISHED SEAT TRACK SPLICE FROM 1153 TO 1193 IAW SRM 53-05-00.

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 67,995 hrs · 35,410 cycles

LEFT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. ACCOMPLISHED NESTED ANGLE REPAIR IAW EA MD80-57-037132.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

SUBFLOOR SUPPORT ANGLE CRACKED AT STATION 185 & RBL 26, BOTTOM SIDE OF SUBFLOOR. REMOVED CRACKED ANGLE & INSTALLED NEW SERVICEABLE FABRICATED ANGLE IAW SRMS 51-00-00-1, 51-10-09 & DWG 9936534.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

CORROSION ON CUSP SHEET FROM STATIONS 1250 TO 1309. REPLACED LT CUSP SHEET IAW AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

NUMBER 6 SEAT TRACK CORRODED FROM STATIONS 216 TO 302. REPLACED NR 6 SEAT TRACK IAW SRM 53-05-00.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

DOOR STOP SUPPORT CASTING CRACKED. REPLACED SUPPORT.

Part: PAN — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

AFT ENTRY DOOR WEB 5917579-239 & PAN CRACKED. REPAIRED WITH NESTED ANGLE DOUBLERS ON PAN & DOUBLER ON WEB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

CANTED FRAME 1485 CRACKED AT THE AFT AIRSTAIR MOUNT RT SIDE. ACCOMPLISHED REPAIR SPLICE IAW AARD 53-10-0033.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

DENTS IN SKIN AT STATION 1354 BETWEEN LONGERONS 8 TO 9 LT. INSTALLED DOUBLER IAW SRM 53-01-00 FIGURE 2 SHEET 3.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

RIGHT CUSP CRACKED AT STATION 247. INSTALLED DOUBLER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

RIGHT SEAT TRACK FROM STATIONS 324 TO 326 CORRODED. INSTALLED PLUG REPAIR IAW SRM 53-05-00-001 & 53-20-00-10.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 67,995 hrs · 35,410 cycles

CORROSION ON RT TIE DOWN TRACK FROM STATIONS 1220 TO 1322 AFT CARGO. R & R TRACK.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

CRACKED LT ANGLE INSIDE & BELOW RAM AIR INTAKE 5912188-49. R & R ANGLE 5912188-49.

Part: WEB — WORN (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

AFT ACCESSORY TEMPERATURE CONTROL VLV HAS WORN INTO WEB ON FRAME 1380 LT SIDE BELOW LONGERON 4 LT. INSTALLED DOUBLER IAW 53-10-00-28.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

CRACK IN LT TIE-DOWN TRACK INTERCOSTAL BETWEEN FUSELAGE STATIONS 1322 & 1309. R & R INTERCOSTAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,995 hrs · 35,410 cycles

CORROSION ON LT CUSP BETWEEN FUSELAGE STATIONS 218 & 237. REPAIRED CUSP IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,995 hrs · 35,410 cycles

CORROSION ON RT CUSP BETWEEN FUSELAGE STATIONS 807 & 845. R & R RT CUSP IAW AARD 51-00-05-1.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

TEMPORARY DOUBLER INSTALLED AT STATION 1309 & LONGERON 7 LT. INSTALLED CLASS 1 PERMANENT REPAIR DOUBLER IAW SRM 55-04-02 FIGURE 2 SHEET 29.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

FUSELAGE SKIN CRACKED, CANTED FRAME STATION 1474, RT SIDE 15 INCHES DOWN FROM GUTTER. DAMAGE CUT OUT & INSTALLED EXTERNAL DOUBLER IAW SRM 53-01-00-001.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 67,995 hrs · 35,410 cycles

CORROSION ON INBD G1 MOUNT AT STATION 160 & RBL 12. REPLACED MOUNT & FITTING IAW SRMS 51-30-02 & 51-30-05.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

WEB IS CRACKED AT STATION 207 & INTERCOSTAL 11 LT. INSTALLED DOUBLER IAW AARD 53-10-00-11.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 67,995 hrs · 35,410 cycles

OUTBOARD G1 GALLEY MOUNT CORRODED. REPLACED CORRODED MOUNT.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 67,995 hrs · 35,410 cycles

SUBFLOOR BULGED & CRACKED FROM STATIONS 160 TO 180 AT RBL 48. INSTALLED NEW SUBFLOOR SECTION & STIFFENER IAW 53-20-00-16.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 67,995 hrs · 35,410 cycles

CORROSION ON NR 1 GALLEY CTR TIE DOWN FITTING AT STATION 160 & RBL 45. REMOVED CORRODED FITTING & INSTALLED NEW FITTING.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 67,995 hrs · 35,410 cycles

G2 GALLEY MOUNT UNDER SUBFLOOR CORRODED. REPLACED MOUNT IAW AARD 51-00-05-1.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 67,995 hrs · 35,410 cycles

CORROSION ON SUBFLOOR MEMBRANE. CUT OUT CORROSIONS & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

FLOOR SUPPORT CRACKED BELOW NR 4 SEAT TRACK & ABOVE CTR FUEL TANK AT STATION 864. INSTALLED NEW SERVICEABLE SUPPORT AT STATION 864.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,995 hrs · 35,410 cycles

G2 GALLEY MOUNT AT FWD END OF NR 6 SEAT TRACK CORRODED. INSTALLED NEW G2 GALLEY MOUNT IAW AARD 51-00-05-1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 67,995 hrs · 35,410 cycles

FLOOR SUPPORT CRACKED BELOW NR 4 SEAT TRACK & ABOVE CTR FUEL TANK AT STATION 826. INSTALLED NEW SERVICEABLE SUPPORT STATION 826.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,995 hrs · 35,410 cycles

G2 GALLEY INBD TIE DOWN MOUNT CORRODED. REMOVED CORRODED MOUNT & INSTALLED NEW SERVICEABLE MOUNT IAW 51-00-05-1 & DWG 9936535.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,712 hrs · 33,516 cycles

EXTERNAL LONGERON 20 RT HAND CRACKED AFT OF WHEEL WELL. STOP DRILLED CRACK & INSTALLED DOUBLER IAW AARD 53-10-00-18.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,145 hrs · 32,643 cycles

LEFT NUMBER 1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: PROXIMITY SENSOR — OBSTRUCTED (LE SLAT) · airframe 61,189 hrs · 31,534 cycles

DFW - CREW REPORTED SLAT DISAGREE LIGHT WOULD NOT EXTINGUISH. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PROXIMITY BOX SHOWED FAULT FOR D SENSOR RIGHT WING. INSPECTED SENSOR AND FOUND DEBRIS STUCK IN PLUNGER ARM FOR SENSOR TARGET. CLEANED AREA. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,811 hrs · 31,326 cycles

FUSELAGE FRAME AT STATION 1510 HAS SMALL CRACK. STOP DRILLED CRACK AND INSTALLED DOUBLER.

Part: WARNING SYSTEM — MALFUNCTIONED (LE SLAT) · airframe 60,547 hrs · 31,179 cycles

CREW REPORTED SLAT DISAGREE INDICATION. FLIGHT RETURNED AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PROXIMITY BOX AS A PRECAUTION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — DIRTY (OIL SYSTEM) · airframe 59,601 hrs · 30,615 cycles

PHL - CREW REPORTED HIGH OIL TEMPERATURE ON NUMBER 1 ENGINE INDICATION AND FUEL TEMPERATURE ALSO HIGH. EMERGENCY DECLARED FLIGHT RETURNED PHL LANDED WITHOUT INCIDENT. CLEANED OIL TEMPERATURE CONNECTOR ON NUMBER 1 ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE — CHAFED (AC BAY) · airframe 58,655 hrs · 30,081 cycles

DFW - CREW REPORTED ON CLIMBOUT C17 DIGITAL GUIDANCE COMPUTER CIRCUIT BREAKER POPPED. TOTAL LOSS OF DIGITAL FLIGHT GUIDANCE SYSTEM, 1 AND 2 YAW DAMPER, MACH TRIM, AUTO THROTTLE AND AUTO PILOT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND 1C610R20RD WIRE TO LEFT ELEVATOR POSITION SENSOR IN AFT TAIL COMPARTMENT CHAFED. REPAIRED WIRE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PAN — CRACKED (WINDOW) · airframe 57,277 hrs · 29,309 cycles

CRACK IN LOWER FORWARD CORNER OF WINDOW PAN AT STATION 1041 LEFT SIDE. INSTALLED REPAIR DOUBLER PER AARD 53010300325.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,023 hrs · 29,165 cycles

CRACK FRAME STATION 1418 AND LONGERON 2 LEFT. INSTALLED DOUBLER PER SRM 53-03-00 FIG 31.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

CORROSION ON SHEAR TIE STATION 1117 LONGERON 29 TO 30 LEFT. INSTALLED DOUBLER PER SRM 51-30-05 AND SRM 53-03-00.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

STRAP BETWEEN LONGERON 28 RIGHT AND 29 RIGHT STATION 1174 IS CORRODED. REMOVED AND REPLACED STRAP PER IPC 53-14-03 AND SRM 53-30-05.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

CORROSION AT DOOR THRESHOLD AT FORWARD CARGO. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-05-00 FIG 44 SHEET 8.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

RIGHT CUSP STATION 598 TO 712 CORROSION OUT OF LIMITS. REMOVED AND REPLACED CUSP SHEET PER AARD 53-20-00-16.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

CORROSION ON AFT SIDE OF SHEAR TIE AT STATION 1231 ABOVE LONGERON 29 LEFT. RE-INSTALLED SHEAR TIE AND INSTALLED DOUBLER ON LEFT SIDE OF SHEAR TIE AT STATION 1231 FROM LONGERON 28 LEFT TO LONGERON 30. WORK ACCOMPLISHED AS PER SRM 53-03-00 / FIGURE 3 SHEET 1.

Part: RIVET — MISSING (SHEAR TIE) · airframe 57,023 hrs · 29,165 cycles

FASTENER MISSING AT SHEAR TIE AFT SIDE OF STATION 1437 AFT OF LONGERON 2 RIGHT. INSTALLED REPAIR FASTENER PER SRM 53-05-00 FIGURE 99.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,023 hrs · 29,165 cycles

AFT CARGO HAS CORROSION IN SHEAR TIE AT STATION 1250 NEAR LONGERON 28 RIGHT. INSTALLED SHEAR TIE SPLICE REPAIR PER SRM 53-03-00 FIG 3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

RIGHT CUSP IS CORRODED BETWEEN STATION 579 AND 598. REPAIRED CUSP PER AARD 53-20-00-16.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

SHEAR TIE CORRODED BETWEEN LONGERON 30 AND 29 LEFT AT STATION 1117. INSTALLED REPAIR SHEAR TIE PER SRM 53-03-00 FIGURE 3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

RIGHT CUSP IS CORRODED BETWEEN STATION 522 AND 541. REPAIRED CUSP PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

CORROSION ON NUMBER 6 SEAT TRACK STATION 216. INSTALLED SERVICEABLE SECTION FROM 216-303 PER SRM 53-05-00 FIG 4F.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

RIGHT CUSP SHEET CORROSION OUT OF LIMITS STATION 1250 TO 1309. INSTALLED NEW CUSP SHEET FROM STATION 1250 TO 1309 RIGHT PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

CORROSION ON G1 GALLEY OUTBOARD MOUNT. INSTALLED SERVICEABLE GALLEY MOUNT ON G1 PER SRM 51-01-00.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

G2 GALLEY MOUNT FORWARD OF NUMBER 6 SEAT TRACK CORRODED. REMOVED AND REPLACED G2 GALLEY MOUNT.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,023 hrs · 29,165 cycles

CRACK IN LEFT CUSP AT STATION 226 OUTBOARD OF NUMBER 1 SEAT TRACK. INSTALLED DOUBLER AT STATION 226 LEFT CUSP PER AARD 53-20-00-16.

Part: CASTING — CRACKED (SPOILER) · airframe 57,023 hrs · 29,165 cycles

LEFT WING GROUND SPOILER CASTING HAS CRACK INBOARD SIDE. NEW SPOILER CASTING ON LEFT WING WAS INSTALLED PER SRM 51-30-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

CORROSION ON SEAT TRACK NUMBER 5 STATION 200 TO 218. INSTALLED SERVICEABLE TRACK NUMBER 5 STATION 200 TO 218 PER SRM 53-05-00 FIGURE 4F.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

CORROSION ON G-2 GALLEY MOUNT INBOARD OF SEAT TRACK NUMBER 4 AT STATION 218. INSTALLED REPLACEMENT GALLEY MOUNT PER SRM 51-01-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

SEAT TRACK NUMBER 6 CORROSION BLEND OUT, OUT OF LIMITS AT STATION 283. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: DOUBLER — DAMAGED (WINDOW PAN) · airframe 57,023 hrs · 29,165 cycles

NO EDGE DISTANCE ON AFT FASTENER ON WINDOW PAN REPAIR STATION 1231 UPPER CORNER. REMOVED DEFECTIVE DOUBLER AND INSTALLED NEW DOUBLER PER AARD 53-10-00-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,023 hrs · 29,165 cycles

SEAT TRACK NUMBER 6 CORROSION BLEND OUT, OUT OF LIMITS AND TANG BROKE OFF AT STATION 264. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: PAN — DAMAGED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

NO EDGE DISTANCE ON AFT FASTENER ON WINDOW PAN REPAIR STATION 1250 LEFT UPPER CORNER. INSTALLED WINDOW PAN REPAIR STATION 1250 LEFT UPPER CORNER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

RIGHT SIDE AFT UPPER CORNER STATION 1022 WINDOW PAN CRACKED. INSTALLED DOUBLER CDK 3488-1 PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

LEFT FUSE-WINDOW RING PAN CRACKED AT THE UPPER AFT CORNER STATION 1060. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25 MRT-027568.

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

WINDOW PAN CRACKED STATION 927 FORWARD UPPER CORNER. DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

WINDOW PAN CRACKED STATION 946 FORWARD UPPER CORNER. DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

LEFT FUSELAGE WINDOW RINGPAN CRACKED AT THE AFT UPPER CORNER STATION 1041. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. MRT-027567

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

RIGHT SIDE FORWARD UPPER CORNER STATION 846 WINDOW PAN CRACKED. INSTALLED DOUBLER CDK 3488-2 PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

WINDOW PAN CRACKED STATION 1022 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

WINDOW PAN CRACKED AT LOWER AFT CORNER STATION 598 LEFT. REPAIRED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

WINDOW PAN CRACKED STATION 1022 AFT UPPER CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 57,023 hrs · 29,165 cycles

RIGHT SIDE UPPER AFT CORNER STATION 1155 WINDOW PAN CRACKED. INSTALLED ANGLE DOUBLER CDK 3488-1 PER AARD-53-10-00-25.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,397 hrs · 27,184 cycles

AFT ACCESSORY, LONGERON 3L SHEAR TIE CRACKED, STATION 1451. INSTALLED A SERVICEABLE SHEAR TIE INBOARD SIDE OF LONGERON 3L PER SRM 51-10-0.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 53,397 hrs · 27,184 cycles

AFT ACCESSORY, STATION 1451 SHEAR TIE CRACKED, LONGERON 3R. INSTALLED A SERVICEABLE SHEAR TIE PER SRM 51-10-0.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 53,397 hrs · 27,184 cycles

AFT CARGO DOOR, T-ANGLE UPPER AFT CRACKED. INSTALLED NEW T-ANGLE PER ESO 80174.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,397 hrs · 27,184 cycles

AFT ACCESSORY LONGERON 3L, CLIP CRACKED STATION 1451. INSTALLED A SERVICEABLE CLIP AT IN BOARD OF LONGERON 3L STATION 1451 PER SRM 51-10-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,397 hrs · 27,184 cycles

LONGERON CRACKED, AFT ACCESSORY, STATION 1451. INSTALLED DOUBLER PER SRM 53-01-00, LONGERON 1 STATION 1451.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,397 hrs · 27,184 cycles

AFT ACCESSORY, LONGERON 3R CRACKED STATION 1451. INSTALLED DOUBLER PER SRM 53-01-00.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 53,397 hrs · 27,184 cycles

AFT CARGO DOOR, T-ANGLE SKIN SIDE LOWER FORWARD CRACKED AROUND FASTENER HOLE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,017 hrs

LGA FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY EMERGENCY LIGHTS.

Part: LENS — BROKEN (EMERGENCY LIGHTS)

LAX - EMERGENCY LIGHT AT SEAT ROW 29D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BROKEN (EMERGENCY LIGHTS)

LAX - EMERGENCY LIGHT AT SEAT ROW 16D BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHTS)

LAX - EMERGENCY LIGHT AT SEAT ROW 16D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BROKEN (EMERGENCY LIGHTS)

LAX - EMERGENCY LIGHT AT SEAT ROW 29D BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - CEILING EMERGENCY LIGHTS THROUGHOUT CABIN INOPERATIVE. REPLACED BATTERY PACKS B527, B528, B5106, AND B5107 FOR INOPERATIVE CEILING EMERGENCY LIGHTS THROUGHOUT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT IN COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — LEAKING

JFK - INFLIGHT LGA TO DFW, AFTER TAKE OFF STRONG BURNING FLUID SMELL WAS NOTED IN COCKPIT. F/A REPORTED SMOKE IN CABIN. AIR INTERRUPTED TO JFK AND LANDED WITHOUT INCIDENT. FOUND INTERNAL AND EXTERNAL OIL LEAK ON AUXILLARY POWER UNIT. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

CEILING EMERGENCY LIGHTS FROM 8DEF TO 16DEF AND ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK B5101, B5102, AND B5106 FOR CEILING EMERGENCY LIGHTS FROM 8DEF TO 16DEF AND ROWS 22 TO 26. SYSTEM GROUND CHECKED. NORMAL OPERATION.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHT)

DFW - FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RE-RACKED BATTERY PACK IN ASSEMBLY FOR FORWARD OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — SHORTED (CABIN)

DFW - EMERGENCY SEAT MOUNTED AND LEFT AND RIGHT HAND OVERWING EXIT LIGHTS AT ROW 20 TO TAIL CONE INOPERATIVE. REPAIRED SHORTED WIRE FOR EMERGENCY SEAT MOUNTED AND LEFT AND RIGHT HAND OVERWING EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - AFT GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR AFT GALLEY EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SAN FORWARD EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED CONTROL MODULE AND REPAIRED SEAT WIRING FOR FORWARD EMERGENCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (SEAT 3-20)

SAT EMERGENCY LIGHTS AT SEATS 3 THROUGH 20 INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK FOR ROWS 3 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK. REPLACED NR 2 TRACK SECTION PER SRM 53-05 FIG 4. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L245-L246 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 21-31 INOPERATIVE. RESEATED PUSH PIN AT AFT STAIRS EMERGENCY EXIT SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT EMERGENCY PATH LIGHTING AFT HALF OF AIRCRAFT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT HALF OF CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PHX - DURING OVERNIGHT MAINTENANCE, AFT ROW SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK FOR AFT EMEREGNCY PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEATS 4D, 8D, 11D, AND 21D, DIM. REPLACED EMERGENCY EXIT LIGHT AT 4D, 8D, 11D, AND 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHT DIM. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. M)

Part: SOCKET — BROKEN (LT EMER EXIT)

DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT LIGHT AT LEFT FORWARD OVERWING EXIT INOPERATIVE. REPAIRED LIGHT ASSEMBLY SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS INOPERATIVE AT ROWS 12, 17 AND 33. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIPS AT PASSENGER SEAT ROWS 12, 17 AND 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

PHX - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHTS AT FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

RDU - DURING OVERNIGHT MAINTENANCE, FOUND THE AFT CABIN FLIGHT ATTENDANT EMERGENCY FLASHLIGHT SEALS BROKEN. REPLACED SEALS ON AFT CABIN FLIGHT ATTENDANT EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: ACTUATOR — DEFECTIVE (NLG)

ORD - FLT 386 - AFTER TAKEOFF ORD, WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. RECYCLED LANDING GEAR WITH SAME RESULTS. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO ORD, LANDING WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR RETRACT CYLINDER. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 2D AND 12D FLICKERED. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PASSENGER SEAT ROW 2D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)