N571AA

Part: INDICATOR — FAULTY (COCKPIT) · airframe 86,363 hrs · 39,577 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB CREW HAD DIFFICULTY TURNING LT, AT LEVEL OFF RUDDER REQUIRED 8 UNITS OF LT TRIM. R & R RUDDER TRIM CONTROL INDICATOR & PERFORMED OPERATIONAL CHECK IAW AMM 27-10-07. SYS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 86,240 hrs · 39,512 cycles

EMERGENCY EXIT ROW LIGHT AT 32D INOPERATIVE & LENS COVER MISSING. REPLACED MISSING LENS AT 32D. EMER EXIT LIGHTS OPERATIONAL CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 86,149 hrs · 39,455 cycles

AFT EMER PATH LIGHTS VERY DIM WHEN POWERED BY MODULE AB5-1. REPLACED BATTERY FOR CONTROL MODULE AB5-1. EMER PATH LIGHTS OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 86,149 hrs · 39,455 cycles

CEILING EMER LIGHTS FROM ROW 18 - 21 INOPERATIVE. REPLACED BATTERY PACK AT B5-104, LIGHTS FROM ROW 18 - 21. EMER LIGHT OPERATIONAL CHECKED GOOD.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 83,804 hrs · 38,217 cycles

MID CARGO DOOR LOWER FWD STOP CRACKED. REPLACED STOP PAD FITTING IAW AARD 51-00-05-1.

Part: RIB — CRACKED (LT WING) · airframe 83,634 hrs · 38,122 cycles

LEFT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED LT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-05.

Part: SUPPORT RIB — CRACKED (RT WING) · airframe 83,634 hrs · 38,122 cycles

RIGHT WING NR 4 SLAT TRACK SUPPORT RIB CRACKED. INSTALLED RT WING NR 4 RIB DOUBLER.

Part: BRAKE — OVERHEATED (MLG) · airframe 83,526 hrs · 38,065 cycles

ON TAXI IN FROM LANDING, CREW REPORTED HOT BRAKES. FOUND NR 1 & 2 MLG TIRES FLAT. ACFT REMOVED FROM SERVICE. REPLACED NR 1 & 2 BRAKES & TIRES. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: MODULE — INOPERATIVE (CABIN) · airframe 83,101 hrs · 37,849 cycles

DIRECT CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 27 INOPERATIVE. REPLACED BATTERY MODULE B5-106.

Part: BATTERY — DISCHARGED (CABIN) · airframe 83,101 hrs · 37,849 cycles

ESCAPE PATH LIGHT AT FWD RT OVERWING EMERGENCY EXIT INOPERATIVE. R & R BATTERY AT AB5-3, OPERATIONS CHECKED NORMAL.

Part: CONTROL PANEL — INOPERATIVE (CABIN PRESSURE) · airframe 79,707 hrs · 36,087 cycles

DFW - CREW REPORTED UNABLE TO PRESSURIZE AIRCRAFT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED PRESSURIZATION CONTROL PANEL AND R2-258 RELAY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,707 hrs · 36,087 cycles

CORROSION ON FLOORBOAD SUPPORT UPPER FLANGE FROM STATIONS 198 TO 200, RIGHT BUTTLINE 6. INSTALLED NEW FLOORBOAD SUPPORT PER SRM 51-30-01.

Part: BELTFRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,707 hrs · 36,087 cycles

LOWER INNER FLANGE OF BELTFRAME CORRODED AT STATION 1250 BETWEEN LONGERONS 29 LEFT AND 29 RIGHT. INSTALLED FRAME DOUBLER PER AARD 53-10-00-14.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 79,707 hrs · 36,087 cycles

LEFT CUSP HAS 3 INCH CRACK AT STATION 1264. REPLACED LEFT CUSP SHEET FROM STATIONS 1250 TO 1309 PER AARD 51-00-05-1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 79,707 hrs · 36,087 cycles

CRACK IN LEFT CUSP AT STATION 843 FROM EDGE OF CUSP SHEET TO FASTENER HOLE. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 79,707 hrs · 36,087 cycles

SEVERAL ELONGATED HOLES IN SUBFLOOR UNDER G-1 GALLEY MOUNT FITTING AT STATION 160, RIGHT BUTTLINE 10. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 79,707 hrs · 36,087 cycles

DENT WITH SCRATCH AT STATION 222 ABOVE LEFT LONGERON 18. INSTALLED SKIN SPLICE REPAIR PER SRM 53-04-00 FIGURE 12 C.

Part: SKIN — DENTED (CARGO DOOR) · airframe 79,707 hrs · 36,087 cycles

FORWARD CARGO DOOR HAS SEVERAL DENTS IN OUTER SKIN AT UPPER CENTER OF DOOR. INSTALLED NEW SKIN PER ESO 80174.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,707 hrs · 36,087 cycles

LONGERON 17 LEFT CRACKED AT STATION 1309. INSTALLED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,707 hrs · 36,087 cycles

CORROSION ON SUBFLOOR UNDER G-1 GALLEY. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 79,707 hrs · 36,087 cycles

DENT IN FUSELAGE SKIN AT FRAME STATION 484 BETWEEN LONGERON 27 AND 28 RIGHT. INSTALLED CLASS 1 EXTERNAL DOUBLER WITH INTERNAL FINGER DOUBLERS PER SRM 53-04-03 FIG 8 SHT 8.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 79,235 hrs · 35,857 cycles

DFW - CREW REPORTED DIGITAL FLIGHT GUIDANCE COMPUTERS FAILED, LOST ALL NAVIGATION AND AUTOPILOT AND AUTO THROTTLES DISCONNECTED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBERS ONE AND TWO DIGITAL FLIGHT GUIDANCE COMPUTER MODE CONTROL PANELS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSE LINE — LOOSE (ZONE 200) · airframe 77,452 hrs · 34,902 cycles

TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. FOUND AUGMENTATION VALVE SENSE LINES LOOSE ON VALVE. TIGHTENED LINES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DEFECTIVE (ZONE 200) · airframe 76,028 hrs · 34,185 cycles

DFW - CREW REPORTED DURING CLIMBOUT LOST ALL INFO ON NAVIGATION DISPLAY. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 COMPASS RACK CONNECTOR THAT WAS BAD. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,232 hrs · 32,800 cycles

THE 1497 CANT FRAME CRACKED BELOW RIGHT LOUVER BOX. DOUBLER WAS INSTALLED PER EA NUMBER MD80-53-009647.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 71,437 hrs · 32,029 cycles

DFW - LEFT ENGINE OIL PRESSURE LIGHT CAME ON WITH PRESSURE SHOWING ZERO. CREW SHUT DOWN LEFT ENGINE. SINGLE ENGINE TIME 10 MINUTES. EMERGENCY DECLARED RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE DUE TO OIL PRESSURE OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DUCT — LEAKING (AIR CON) · airframe 68,785 hrs

LAX INFLIGHT DFW TO PDX - TAIL COMPARTMENT HIGH TEMPERATURE INDICATION IN FLIGHT. CREW SHUT DOWN LEFT AIR CONDITIONING PACK AND LIGHT EXTINGUISHED. LANDED LAX WITHOUT INCIDENT. REPLACED BROKEN LEFT AIR CONDITIONING PACK DUCT CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (BS 1437) · airframe 68,753 hrs · 30,886 cycles

CRACK FOUND ON AFT FUSELAGE SKIN AT STATION 1437 BETWEEN LONGERONS 2 RT AND 3 RT. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-30-00-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,753 hrs · 30,886 cycles

3 CRACKS FOUND ON AFT FUSELAGE SKIN AT STATION 1437 BETWEEN LONGERONS 3 RT AND 4 RT. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-30-00-02.

Part: BEAM — CRACKED (FUSELAGE) · airframe 68,753 hrs · 30,886 cycles

CRACK FOUND ON LT J BEAM REPAIR DOUBLER IN NG WW. REPLACED REPAIR DOUBLER IN ACCORDANCE WITH AARD 53-10-00-04.

Part: BRACKET — CORRODED (BS 211) · airframe 68,753 hrs · 30,886 cycles

TUL GALLEY INBD TIE DOWN BRACKET CORRODED BEYOND LIMITS AT STATION 211. REPLACED TIE DOWN BRACKET IN ACCORDANCE WITH AARD 53-20-00-16.

Part: SKIN — CRACKED (BS 1474) · airframe 68,753 hrs · 30,886 cycles

SKIN CRACKED AT CANTED FRAME AT STATION 1474. INSTALLED DOUBLER IN ACCORDANCE WITH SRM 53-01-00.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 68,753 hrs · 30,886 cycles

RT VERTICAL STABILIZER FORWARD SPAR TANG CRACKED ON AFT SIDE OF CANTED FRAME AT STATION 1388. INSTALLED REPAIR ANGLE IN ACCORDANCE WITH AARD 55-30-00-08.

Part: BRACKET — CORRODED (GALLEY TIE DOWN) · airframe 68,753 hrs · 30,886 cycles

TUL GALLEY INBD TIE DOWN BRACKET CORRODED BEYOND LIMITS AT STATION 217. REPLACED TIE DOWN BRACKET IN ACCORDANCE WITH AARD 53-20-00-16.

Part: INTERCOSTAL — CORRODED (BS 769-786) · airframe 68,753 hrs · 30,886 cycles

INTERCOSTAL CRACKED IN MID CARGO CEILING AT STATION 769 TO 786. CRACK LENGTH IS 2 INCHES. REPLACED INTERCOSTAL IN ACCORDANCE WITH AARD 53-20-00-16.

Part: PAN — CORRODED (BS 370-427) · airframe 68,753 hrs · 30,886 cycles

DOOR PAN AT FORWARD CARGO HAS CORROSION OUT OF LIMITS AT STATION 370 TO 427. AREA OF DISCREPANCY IS 3 INCHES BY 4 INCHES. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 18 SEP 2008.

Part: SUPPORT BRACKET — CRACKED (MLG) · airframe 68,753 hrs · 30,886 cycles

TUL RT DOOR STRUT SUPPORT BRACKET CRACKED 12 INCHES ABOVE HINGE IN WW AT STATION 101. REPLACED RT STRUT SUPPORT IN ACCORDANCE WITH SRM 51-30-05.

Part: BULKHEAD — CRACKED (BS 110) · airframe 68,753 hrs · 30,886 cycles

RT LOWER SIDE PRESSURE BULKHEAD CRACKED AT STATION 110. CRACK LENGTH IS .5 INCH. INSTALLED DOUBLER WITH FINGERS IN ACCORDANCE ESO 80559 DATED 19 SEP 2008.

Part: FRAME — CORRODED (BS 1231) · airframe 68,753 hrs · 30,886 cycles

TUL CORROSION FOUND ON BELL FRAME AT STATION 1231. AREA OF DISCREPANCY IS 2 INCHES BY 1 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH SRM 51-70-05.

Part: CARGO TRACK — CORRODED (BS 1212-1320) · airframe 68,753 hrs · 30,886 cycles

TUL CORROSION FOUND ON RT TIE DOWN TRACK AT STATION 1212 TO 1320. AREA OF DISCREPANCY IS 108 INCHES BY 2 INCHES. REPLACED RT TIE DOWN TRACK AT STATION 1212 TO 1320 IN ACCORDANCE WITH SRM 51-10-03 AND 51-30-01.

Part: CARGO TRACK — CORRODED (BS 1212) · airframe 68,753 hrs · 30,886 cycles

TUL CORROSION FOUND ON RT TIE DOWN TRACK SPLICE AT STATION 1212. AREA OF DISCREPANCY IS 6 INCHES BY 2 INCHES. REPLACED SPLICE AT STATION 1212 IN ACCORDANCE WITH SRM 51-10-01.

Part: BRACKET — CORRODED (GALLEY MOUNT) · airframe 68,753 hrs · 30,886 cycles

TUL RT GALLEY MOUNT BRACKET CORRODED AT STATION 160. AREA OF DISCREPANCY IS 1 INCH BY 1 INCH. REPLACED RT GALLEY MOUNT BRACKET IN ACCORDANCE WITH SRM 51-10.

Part: ANGLE — CRACKED (BS 826) · airframe 68,753 hrs · 30,886 cycles

RT ANGLE CRACKED AT TOP OF CENTER AUXILIARY FUEL TANK AT STATION 826. INSTALLED STACK DOUBLERS IN ACCORDANCE WITH ESO 80559 DATED 24 SEP 2008.

Part: FRAME — CORRODED (BS 1231) · airframe 68,753 hrs · 30,886 cycles

TUL CORROSION FOUND ON BELL FRAME AT STATION 1231. AREA OF DISCREPANCY IS 2 INCHES BY 1 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH SRM 51-70-05.

Part: STRUCTURE — CORRODED (BS 180) · airframe 68,753 hrs · 30,886 cycles

TUL RT SUBFLOOR CORRODED AT STATION 180. AREA OF DISCREPANCY IS 2 INCHES BY 2 INCHES. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-20-00-16.

Part: ANGLE — CRACKED (BS 826) · airframe 68,753 hrs · 30,886 cycles

LT ANGLE CRACKED AT TOP OF CENTER AUXILIARY FUEL TANK BELOW SEAT TRACK NR 5 AT STATION 826. INSTALLED STACK DOUBLERS IN ACCORDANCE WITH ESO 80559 DATED 24 SEP 2008.

Part: CUSP WEB — CORRODED (BS 616-619) · airframe 68,753 hrs · 30,886 cycles

TUL-CORROSION FOUND ON LT CUSP AT STATION 616 TO 619. AREA OF DISCREPANCY IS 3 INCHES BY 2 INCHES. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-20-00-16.

Part: LONGERON — CRACKED (BS 200 L2L) · airframe 68,753 hrs · 30,886 cycles

LONGERON 2 LT WAS CRACKED AT INBD SIDE AT STATION 200. CRACK LENGTH IS 1/4 INCH. INSTALLED SPLICE REPAIR IN ACCORDANCE WITH SRM 53-02-00 FIGURE 18.

Part: LONGERON — CRACKED (BS 160 L2L) · airframe 68,753 hrs · 30,886 cycles

LONGERON 2 LT WAS CRACKED AT INBD SIDE AT STATION 160. CRACK LENGTH IS 1/4 INCH. INSTALLED SPLICE REPAIR IN ACCORDANCE WITH SRM 53-02-00 FIGURE 18.

Part: STRUCTURE — CRACKED (BS 214) · airframe 68,753 hrs · 30,886 cycles

RT SUBFLOOR CRACKED AT STATION 214. CRACK LENGTH IS 1 INCH. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH AARD 53-20-00-16.

Part: ANGLE — CORRODED (BS 168) · airframe 68,753 hrs · 30,886 cycles

RT CUSP ANGLE CORRODED AT STATION 168. AREA OF DISCREPANCY IS 1 INCH BY 1 INCH WITH A DEPT OF .033 INCH. BLENDED OUT CORROSION AND INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ESO 80559 DATED 19 SEP 2008.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 68,753 hrs · 30,886 cycles

TUL RT OTBD SIDE OF GROUND SPOILER SUPPORT FITTING CRACKED. REPLACED SUPPORT FITTING IN ACCORDANCE WITH SRM 51-30-05.

Part: FITTING — CRACKED (BS 1140) · airframe 68,753 hrs · 30,886 cycles

AFT SERVICE DOOR FORWARD GIRT BAR FITTING DOUBLER CRACKED AT STATION 1140. AREA OF DISCREPANCY IS 3 INCHES BY 3 INCHES. CRACK LENGTH IS .25 INCH. INSTALLED DOUBLER FOR AFT SERVICE DOOR FORWARD GIRT BAR FITTING IN ACCORDANCE WITH AARD 53-20-00-16.

Part: BRACKET — CORRODED (GIRT BAR) · airframe 68,753 hrs · 30,886 cycles

GIRT BAR BRACKET AT AFT SERVICE DOOR HAS CORROSION. AREA OF DISCREPANCY IS 4 INCH BY 4 INCH WITH A DEPTH OF .030 INCH. REPLACED BRACKET IN ACCORDANCE WITH SRM 51-01.

Part: CUSP WEB — CORRODED (BS 219) · airframe 68,753 hrs · 30,886 cycles

CORROSION FOUND ON RT CABIN FLOOR CUSP MEMBRANE AT STATION 219. AREA OF DISCREPANCY IS 4 INCHES BY 6 INCHES WITH A DEPTH OF .015 INCH. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH AARD 53-20-00-16.

Part: SEAT TRACK — CRACKED (BS 578-579) · airframe 68,753 hrs · 30,886 cycles

TANGS ARE CRACKED ON NR 6 SEAT TRACK BETWEEN STATIONS 578 AND 579. AREA OF DISCREPANCY IS 41 INCH BY 1 INCH. REPAIRED WITH PLUG AND BACKING PLATE IN ACCORDANCE WITH AARD 53-20-00-10.

Part: PAN — CRACKED (BS 905) · airframe 68,753 hrs · 30,886 cycles

RT WINDOW PAN CRACKED AT STATION 905. CRACK LENGTH IS .5 INCH. INSTALLED DOUBLER IN ACCORDANCE AARD 53-10-00-25.

Part: FLOORBEAM — CRACKED (BS 927) · airframe 68,753 hrs · 30,886 cycles

FLOORBEAM CRACKED AT STATION 927. CRACK LENGTH IS 1 INCH. REPLACED FLOORBEAM IN ACCORDANCE WITH SRM 51-01.

Part: CSD — FAILED (NR 1 ENGINE)

BNA EN ROUTE ORD - ATL DURING CLIMBOUT LEFT CSD OIL PRESSURE LOW LIGHT ILLUMINATED FOLLOWED BY LEFT GENERATOR TRIPPED OFF. CONFIRMED CSD OVERTEMP AND DISCONNECTED. ALSO APU GENERATOR WOULD NOT GO ONLINE AFTER INFLIGHT START. RESET, NO HELP. LANDED BNA WITHOUT INCIDENT. REPLACED LEFT HAND ENGINE CSD AND OIL COOLER AND APU GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

SEA - OVERHEAD EMERGENCY EXIT LIGHT IN AFT ENTRY AISLE INOPERATIVE. REPLACED BATTERY POWER SUPPLY AT B5-27 FOR OVERHEAD EMERGENCY EXIT LIGHTS IN AFT ENTRY AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — DISPLACED (L2 DOOR)

AUS L2 AFT SERVICE DOOR SLIDE FOUND BELOW GREEN BAND ON A CHECK. REPLACED L2 AFT SERVICE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DFW - MAINTENANCE OBSERVED EMERGENCY LIGHT IN TAIL INOPERATIVE. SPLICED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (TAIL)

DFW - FOUND LEFT AFT STAIRWELL EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED AFT STAIRWELL EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT DOOR LIGHTS INOPERATIVE. SECURED AFT EMERGENCY EXIT DOOR LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WARNING SYSTEM — DEFECTIVE (E&E BAY)

EN ROUTE ACA-ORD, DURING CLIMB, RECEIVED INTERMITTENT APU AURAL WARNING, NO LIGHTS. WARNING STOPPED BUT AFTER LEVEL OFF AT 29,000 FT WARNING STARTED AGAIN. RECEIVED RT ENGINE FIRE WARNING (AGAIN NO LIGHTS). LANDED MEX WITHOUT INCIDENT. INSPECTED AND CHECKED ENGINE AND APU FIRE DETECTION SYSTEM, NO FAULTS NOTED. REPLACED CENTRAL AURAL WARNING UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FOUND DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4E INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (TAIL)

DURING OVERNIGHT MAINTENANCE TAIL CONE EMERGENCY EXIT BATTERY WIRE LOOSE. TIGHTENED SCREW ON TAIL CONE EMERGENCY EXIT BATTERY FOR WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON WEB OF BOX FRAME AT STATION 1217 AFT CARGO DOOR (TOP AND BOTTOM OF WEB). CUT OUT OLD WEB AND INSTALLED NEW WEB PER MD80 AARD/RP/DR/DH 53-10-00-24. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND ADL5710040-1/4 SHARP EDGE GOUGE IN LEFT SIDE FUSELAGE 25 INCHES FORWARD AND 7 INCHES DOWN OF FORWARD CABIN PRESSURE SAFETY VALVE STATIC PORT. REMOVE DAMAGE. INSTALLED DOUBLER PER SRM 53-04 FIG 12B. (M)

Part: STIFFENER — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN RADIUS OF STIFFENER BETWEEN FRAMES. REMOVED AND REPLACED STIFFENER PER SRM 51-01. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON REPAIR DOUBLERS. BLENDED OUT CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-3. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP BELOW FORWARD AND AFT GIRT BAR SUPPORT STRUCTURE AT AFT GALLEY DOOR JAMB. INSTALLED DOUBLERS ON FORWARD AND AFT GIRT BAR SUPPORT STRUCTURES PER AARD 53-00-00-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 2 SEAT TRACK CORRODED STATION 1203. REMOVED AND REPLACED SEAT TRACK AT EXISTING TRACK SPLICES FROM STATION 1185 TO STATION 1220 WITH SAME TRACK PART NUMBER AND SAME FASTENER TYPE PER SRM 51-01. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 4L CRACKED 1 INCH AT STATION 160. REMOVED LONGERON STATION 145-175. REPLACED STATION PER SRM 53-02 PAGE 648. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON RIGHT CUSP STATION 680-690. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-01 PAGE 18 AND 53-00-00-02 PAGE 1-3. (M)

Part: WIRE — BROKEN (ROW 19)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT ROW 19 INOPERATIVE. SPLICED WIRE AT ROW 19 ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LATCH — BROKEN (GALLEY)

ORD - FLT 2326 - DURING MAINTENANCE, AFT GALLEY DOOR GIRT BAR LATCH IS BROKEN. MAINTENANCE REPLACED AFT GALLEY DOOR GIR BAR LATCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FAN — DEFECTIVE (ACM BAY)

SEA - FLT 2061 - DURING DESCENT INTO SEA, SMOKE AND ODOR NOTED IN MAIN CABIN. TURNED OFF RECIRCULATION FAN AND PACKS TO HP BLEED OFF AND AIRCRAFT LANDED SEAT WITHOTU INCIDENT. PLACARDED GASPER RECIRCULATION FAN INOPERATIVE. SUSBSEQUENTLY REPLACED GASPER FAN AT ORD AND REMOVED PLACARD. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE OR ODOR NOTED. (M)

Part: HYD LINE — LEAKING (RT TR UNIT)

SJC - FLT 1128 - AFTER TAKEOFF SJC DURING CLIMB-OUT, SMOKE NOTED IN CABIN. AIRCRAFT RETURNED TO SJC AND LANDED WITHOUT INCDIENT. REPLACED LEAKING HYDRAULIC LINE AT RT THRUST REVERSER CONTROL VALVE. ACCOMPLISHED PACK BURNOUT AND REPLACED BOTH COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN WITH NO SMOKE OR OTHER DEFECTS NOTED. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO SMOKE OR OTHER DEFECTS NOTED. SYSTEM OPERATIONAL CHECKED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD HALF OF MAIN CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHTS STRIPS AT PAX SEAT ROWS 6E, 10D, 14D, AND 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (TAIL CONE)

SFO - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY LIGHT ABOVE TAIL CONE SLIDE INOPERATIVE. REPAIRED SHORTED WIRES AT AFT RT UPPER AIR CONDITIONING BAY WIRE CLAMP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)