N569AA

Part: APU — LEAKING (APU BAY) · airframe 87,209 hrs · 39,837 cycles

ACRID ODOR DURING INITIAL CLIMB, DISSIPATES QUICKLY. ODOR RETURNS DURING IDLE DESCENT. FOUND OIL LEAKING ON HOT SECTION OF APU. R & R APU IAW MCM 49-96-82 & PACK BURN MCM 21-92-12.

Part: SHUTOFF VALVE — UNSERVICEABLE (BLEED AIR SYS) · airframe 87,209 hrs · 39,837 cycles

FLIGHT ATTENDANT REPORTED ACRID BURNT RUBBER SMELL DURING TAKEOFF INITIAL CLIMB. THE SMELL DISSIPATED DURING FLIGHT. INSTALLED SERVICEABLE LT & RT PRSOVS VLV 5426 IAW AMM 21-31-01. RAN ENGS AT IDLE & TAKEOFF, NO LEAKS OR ODORS NOTED. OPERATIONALLY CHECKED NORMAL. OK FOR SERVICE.

Part: DOOR — OPEN (E&E BAY) · airframe 84,282 hrs · 38,211 cycles

E & E DOOR OPEN INDICATION ON TAKEOFF. FLIGHT RETURNED & LANDED WITHOUT INCIDENT. FOUND FWD E & E DOOR SECURED OPEN. INSPECTED FWD E & E BAY WITH NO DEFECTS NOTED. CLOSED FWD E & E DOOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 84,089 hrs · 38,084 cycles

RIGHT SIDE LONGERON 2 CRACKED AFT SIDE OF STATION 1418 FRAME. INSTALLED SPLICE REPAIR IAW SRM 53-02-00-001.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 84,089 hrs · 38,084 cycles

FORWARD CARGO DOORSTOP CRACKED THIRD DOWN ON FWD END OF DOOR. INSTALLED NEW DOORSTOP IAW AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 84,089 hrs · 38,084 cycles

FORWARD CARGO DOORSTOP CRACKED THIRD DOWN ON AFT END OF DOOR. REPLACED DOORSTOP IAW AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 84,089 hrs · 38,084 cycles

MID CARGO DOORSTOP CRACKED 5TH DOORSTOP DOWN ON AFT END OF DOOR. REPLACED DOORSTOP IAW AARD 50-00-05-1.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 84,089 hrs · 38,084 cycles

MID CARGO DOORSTOP CRACKED FIFTH DOORSTOP DOWN ON AFT END OF DOOR. REPLACED DOORSTOP IAW AARD 50-00-05-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 84,089 hrs · 38,084 cycles

STATION 1418, LONGERON 2 LT WAS CRACKED AT AFT END. ACCOMPLISHED LONGERON SPLICE REPAIR IAW SRM 53-02-00-001.

Part: RIB — CRACKED (LT WING) · airframe 83,870 hrs · 37,879 cycles

LEFT WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED DOUBLER IAW CARD 57-98-05.

Part: RIB — CRACKED (RT WING) · airframe 83,870 hrs · 37,879 cycles

RIGHT WING NR 4 SLAT TRACK LE SUPPORT RIB CRACKED. DOUBLER INSTALLED IAW CARD 57-98-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,766 hrs · 37,316 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 3 TO 7 INOPERATIVE. R & R BATTERY PACK B5-100, OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 82,766 hrs · 37,316 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 16D INOPERATIVE. FOUND CONNECTOR AT SIDEWALL DISCONNECTED. RECONNECTED CONNECTOR AT SIDEWALL FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 16D, OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,766 hrs · 37,316 cycles

SECTION OF CEILING EMERGENCY LIGHTS AROUND ROW 28 AFT INOPERATIVE. R & R BATTERY PACK B5-107, OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 82,766 hrs · 37,316 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 27D INOPERATIVE. FOUND CONNECTOR AT SIDEWALL DISCONNECTED. RECONNECTED CONNECTOR AT SIDEWALL FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 27D, OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 82,766 hrs · 37,316 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 24D INOPERATIVE. FOUND CONNECTOR AT SIDEWALL DISCONNECTED. RECONNECTED CONNECTOR AT SIDEWALL FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24D, OPERATIONS CHECKED NORMAL.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 79,905 hrs · 35,777 cycles

CRACK IN SUPPORT ANGLE ON FORWARD SIDE OF FRAME 788, BETWEEN LONGERONS 27 AND 28 RIGHT. REPLACED SUPPORT PER AARD 51-00-05-1.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,905 hrs · 35,777 cycles

SUBFLOOR CORRODED AT STATION 180, 9 TO 12 INCHES FROM SERVICE DOOR JAMB. INSTALLED SUBFLOOR DOUBLER FROM STATIONS 160 TO 200 RIGHT AND SUBFLOOR OVERLAY FROM STATIONS 160 TO 180 RIGHT PER 53-20-00-16.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,905 hrs · 35,777 cycles

CORROSION ON CENTER G-1 GALLEY MOUNT FITTING AT STATION 160, RIGHT BUTTLINE 45. INSTALLED SERVICEABLE CENTER GALLEY MOUNT FITTING AT STATION 160 PER SRM 51-30-02 SRM 51-30-05 AND AARD 51-00-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 79,905 hrs · 35,777 cycles

CRACK ON INTERCOSTAL AROUND FASTENER HOLE AT STATION 780, ON CENTER LINE. INSTALLED NEW INTERCOSTAL AT STATION 780 PER AARD 51-10-00-5.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,905 hrs · 35,777 cycles

GALLEY MOUNT AT STATION 160, SIX INCHES FROM RIGHT SIDEWALL CORRODED. INSTALLED SERVICEABLE OUTBOARD GALLEY MOUNT FITTING AT STATION 160 PER SRM 51-30-02 SRM 51-30-05 AND 51-00-05.

Part: WEB — CRACKED (FUSELAGE) · airframe 79,905 hrs · 35,777 cycles

WEB IS CRACKED AT STATION 364, BETWEEN LONGERONS 26 AND 27 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-24.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 79,905 hrs · 35,777 cycles

CRACK IN LONGERON AT STATION 200, LONGERON 7 RIGHT. REMOVED LONGERON SECTION AND INSTALLED NEW LONGERON SECTION AND SPLICE FROM STATIONS 180 TO 230 PER SRM 53-02-00, FIGURE 18.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 79,905 hrs · 35,777 cycles

CRACK IN LEFT CUSP AT STATION 845. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 79,905 hrs · 35,777 cycles

WINDOW PAN IS CRACKED IN THE LOWER AFT CORNER BETWEEN STATIONS 886 TO 905. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-25.

Part: SKIN — DENTED (CARGO DOOR) · airframe 79,905 hrs · 35,777 cycles

FORWARD CARGO DOOR HAS DENT AT AFT LOWER CORNER OF OUTER SKIN. INSTALLED DOUBLER REPAIR PER SRM 52-05-00 FIGURE 65 AND EA COMP-52-028192.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 79,905 hrs · 35,777 cycles

GUSSET CRACKED AT FRAME STATION 209, LONGERON 15 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: PAN — CRACKED (FUSELAGE) · airframe 79,905 hrs · 35,777 cycles

CRACK ON WINDOW PAN AROUND UPPER FASTENER RIGHT SIDE OF FUSELAGE AT STATION 1193 FRAME. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: SKIN — CRACKED (FUSELAGE) · airframe 79,905 hrs · 35,777 cycles

HFEC SURFACE SCAN INDICATED CRACK AT FRAME STATION 389, LONGERON 28 LEFT. INSTALLED DOUBLER PER SRM 53-04-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,541 hrs · 35,103 cycles

STAIRWAY ESCAPE PATH LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR STAIRWAY ESCAPE PATH LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,541 hrs · 35,103 cycles

ESCAPE PATH LIGHT AT 32DEF INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT 32DEF ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 77,384 hrs · 34,493 cycles

DENT WITH GOUGE AT FRAME STATION 348 BETWEEN LONGERON 27 TO 28 RIGHT. INSTALLED TEMPORARY DOUBLER PER SRM 53-04-03 FIGURE 2 SHEET 5.

Part: HYDRAULIC LINE — DAMAGED (HYDRAULIC SYS) · airframe 76,355 hrs · 33,961 cycles

ORD - CREW REPORTED RIGHT HYDRAULIC SYSTEM LOSS. CREW WAS ABLE TO EXTEND THE LANDING GEAR BUT WAS UNABLE TO RETRACT MAIN GEAR DOORS. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. FOUND DAMAGED HYDRAULIC LINE TO THE RIGHT RESERVOIR CAUSING FLUID LOSS. REPLACED DAMAGED LINE AND SERVICED SYSTEM. PRECAUTIONARY MAINTENANCE REPLACING RIGHT ENGINE DRIVEN PUMP AND FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 73,210 hrs · 32,440 cycles

ATL - INFLIGHT CLT-DFW. CREW REPORTED A CHEMICAL SMELL IN THE AFT OF THE CABIN. ODOR WAS STRONGEST FROM THE WHEEL WELL AFT AREA. EMERGENCY DECLARED FLIGHT DIVERTED ATL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT MAIN LANDING GEAR ACTUATOR AND SWIVEL GLAND. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 72,509 hrs · 32,126 cycles

SFO - INFLIGHT SJC-ORD. AIRCRAFT EXPERIENCED PRESSURIZATION PROBLEMS. FLIGHT DIVERTED TO SFO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CABIN PRESS CONTROLLER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUT — FAILED (NLG) · airframe 72,411 hrs · 32,083 cycles

ON GEAR RETRACTION THE NOSE GEAR HAD A RED UNSAFE LIGHT AND PILOT STATED THAT HE WAS NOT SURE IF THE GEAR DID NOT STOW COMPLETELY OR THE GEAR DOORS WERE NOT COMPLETELY CLOSED DUE TO A LOUDER THAN NORMAL AIR NOISE. RETURNED TO DFW. GEAR EXTENDED AND LANDING NORMAL. FOUND STRUT DEFLATED WITH NO VISIBLE FLUID LEAK. ACCOMPLISHED A REPACK AND SERVICE OF NOSE GEAR STRUT.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 68,673 hrs · 30,471 cycles

RIGHT TIE DOWN CORRODED FROM STATION 1211-1287 ABOVE LONGERON 27 RIGHT. INSTALLED NEW RIGHT HAND TIE DOWN TRACK PER AARD 51-00-00-012.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

CORROSION AROUND UPPER NUT CLIP HOLE ON LEFT TIE DOWN TRACK FROM SPLICE STATION 1220 TO AFT END OF TRACK. INSTALLED NEW TIE DOWN TRACK PER SRM 53-05-00 FIG 4G.

Part: CARGO TRACK — DAMAGED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

DAMAGE ON LEFT TIE DOWN TRACK IN AFT CARGO FROM STATION 1110 TO 1220. INSTALLED NEW TIE DOWN TRACK.

Part: STRAP — CORRODED (FUSELAGE) · airframe 68,673 hrs · 30,471 cycles

STATION 1193 IN AFT CARGO, WEB STRAP HAS CORROSION AT LONGERON 28R TO 29R. INSTALLED NEW STRAP PER SRM 51-30

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 68,673 hrs · 30,471 cycles

CORROSION ON INTERCOSTAL UNDER RIGHT HAND TIE- DOWN TRACK AFT CARGO BAY STATION 1309-1322. REPLACED INTERCOSTAL WITH SERVICEABLE PART, PER SRM 51-30-5.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

CORROSION ON INTERCOSTAL UNDER RIGHT TIE DOWN TRACK AFT CARGO BAY STATION 1309-1322. REPLACED DEFECTIVE INTERCOSTAL WITH SERVICEABLE PART PER SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

CRACK IN INTERCOSTAL AT CENTERLINE BETWEEN FLOORBEAMS 1271-1287. INSTALLED NEW INTERCOSTAL.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

SEAT TRACK NUMBER 4 HAS CORROSION AT STATION 1215. INSTALLED PLUG REPAIR PER AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

LEFT CUSP CORRODED AT STATION 872. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

STIFFENER CASING IS CRACKED ON INBOARD WALL OF LEFT LAV APPROXIMATELY 24 INCHES FROM FLOOR FORWARD OF PRESSURE BULKHEAD. INSTALLED SERVICEABLE STIFFNER CASTING PER SRM 51-01.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

RIGHT CUSP CRACKED AT STATION 1245. REMOVED DAMAGE AND INSTALLED DOUBLER.

Part: STRAP — CORRODED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

STATION 1193 IN AFT CARGO, WEB STRAP HAS CORROSION AT LONGERON 28R TO 29R. INSTALLED NEW STRAP PER SRM 51-30.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 68,673 hrs · 30,471 cycles

BRACKET STIFFENER IS CRACKED ON FORWARD SIDE AT AFT PRESSURE BULKHEAD TOP END AT LONGERON 1 STATION 1338. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-15.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

LEFT CUSP CRACKED AT STATION 227. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16

Part: FITTING — CORRODED (GIRT BAR) · airframe 68,673 hrs · 30,471 cycles

CORROSION BELOW AFT GIRT BAR FITTING AT AFT SERVICE DOOR STATION 1098. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: PAN — CORRODED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

FORWARD LAV SERVICE PAN HAS CORROSION LOWER EDGE. INSTALLED DOUBLER PER ESO 80559 DATED 10-5-08.

Part: SKIN — DENTED (ZONE 100) · airframe 68,673 hrs · 30,471 cycles

DENT WITH SCRATCH IN FUSELAGE SKIN AT STATION 275 AT LONGERON 24L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B. CLASS II REPAIR.

Part: BATTERY — LOOSE (EMERGENCY LIGHT) · airframe 67,852 hrs · 67,852 cycles

SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3B TO 6B INOPERATIVE. RESEATED BATTERIES FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3B TO 6B. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: ACTUATOR — LEAKING (T/E FLAP)

BOS INFLIGHT T1466/15APR - CREW REPORTED LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY. LANDED BOS WITHOUT INCIDENT. FOUND RIGHT INBOARD FLAP ACTUATOR AND RUDDER SHUTOFF VALVE LEAKING. REPLACED RIGHT INBOARD FLAP ACTUATOR AND RUDDER SHUTOFF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,200 hrs

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

Part: APU — UNKNOWN (APU BAY)

LAX INFLIGHT - AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED LIGHT SMOKE AND ODOR IN CABIN. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED APU AT LGA ON 15 MAR 2007. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRUT — INOPERATIVE (NLG)

SFO INFLIGHT T860 - NOSE LANDING HEAR BOTTOMED OUT ON TAKEOFF ROLL AND COLLAPSED AFTER HITTING A BUMP RISE ON RUNWAY. AFTER GEAR RETRACTION NOSE LANDING GEAR DOORS REMAINED OPEN. GEAR UP RED LIGHT ILLUMINATED. CYCLED GEAR WITH SAME INDICATION. NOSE LANDING GEAR DOORS CONFIRMED OPEN. INSPECTED NOSE STRUT PISTON AND REPLACED NOSE STRUT SCHRADER VALVE O-RING. REPACKED NOSE STRUT. INSPECTED NOSE GEAR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY OVERWING EXIT SIGN LIGHT INOPERATIVE. CLEANED AND ADJUSTED CONTACTS OF BATTERY POWER SUPPLY FOR EMERGENCY OVER WING EXIT SIGN LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - OVERHEAD EMERGENCY LIGHTS FOR ROWS 8, 9, AND 11 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 8, 9, AND 11. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DTW - CEILING EMERGENCY EXIT LIGHT AT ROWS 7 TO 9 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY EXIT LIGHT AT SEAT ROWS 7 TO 9. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (ELECTRICAL)

TUL - WIRE CABLE NR 3X3D2C AND 3X3C2C TO LEFT HAND AUXILLARY RELAY AT FORWARD LOWER EXTERNAL POWER CONTACTOR SHOWS SIGNS OF OVERHEATING. REMOVED AND REPLACED WIRE CABLE 3X3D2C AND 3X3C2C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MSP - OVERHEAD EMERGENCY LIGHTS AT ROWS 18-21 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 18-21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MSP - FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT AIRSTAIR FORWARD CEILING PANEL INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ELECTRICAL QUICK DISCONNECT FOR AFT AIRSTAIR FORWARD CEILING PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, CATWALK EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED AFT LAVATORY EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — NOT SEATED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED TAIL CONE EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LONGERON — CORRODED (FUSELAGE)

TUL - FOUND LONGERON 22L CORRODED (BLOW OUT). REPAIRED AREA WITH LONGERON SPLICE PER SRM 53-02 PAGE 50. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 6 SEAT TRACK HAS CORROSION STATION 215. REMOVED AND REPLACED SEAT TRACK FROM STATION 210-323 PER SRM 53-05 PART 1 FIG 4E SHT 1,5. (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND CUSP UNDER NR 6 SEAT TRACK DAMAGED STATION 297 TO 310 RT. SPLICED IN NEW SECTION OF CUSP FROM STATION 289 TO 313 RIGHT IAW SRM 53-01 FIG 4. (M)

Part: ACCESS PANEL — DAMAGED (CENTER TANK)

TUL - FOUND 16 HOLES ON CENTER TANK LEFT, RIGHT ACCESS PLATE LANDINGS ELONGATED. REPAIRED 16 HOLES IN LEFT RIGHT ACCESS PANEL LANDINGS PER ESO 80559 DATED 3-23-01. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET HOLE STATION 1380 LONGERON 14R. INSTALLED DOUBLER IAW SRM 53-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND SKIN DENTED AT STATION 237 LEFT LONGERON 18. REPAIRED PER SRM 53-04 AND AARD 320. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK CORRODED AND PITTED STATION 1237. REMOVED CORROSION, OUT OF LIMITS. TRIMMED RETAINING IAW ESO 80569 DATED 3-21-2001 TREATED AND PRIMED AREA. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND AREAS OF CORROSION LEFT CUSP STATION 641-655. CUTOUT DAMAGED AREAS AND INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND CLASS III TEMP REPAIR INSTALLED ON FUSELAGE FROM STATION 446-490 STRINGER 21R AND 22R. DENT IN SKIN STATION 503 STRINGER 21R HAS ADL STICKER. CUTOUT DAMAGED FROM STATION 447-490, 4 INCHES ABOVE STRINGER 21R TO STRINGER 22R AT STATION 503 3 INCH DIAMETER. INSTALLED PERM CLASS 1 DOUBLER INTERNAL AND EXT PER ESO 80559 DATED 3-19-01. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED AT RIVET HOLE STATION 1380 LONGERON 14L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01. (M)

Part: FRAME — TOOL DAMAGE (FUSELAGE)

TUL - FOUND TOOLING MARK IN FRAME STATION 313 LONGERON 9R. INSTALLED J-ANGLE REPAIR AS PER AARD 53-10-00-14. (M)

Part: LONGERON — GOUGED (FUSELAGE)

TUL - FOUND DEEP DRILL BIT GOUGE IN LONGERON 9R, STATION 313. INSTALLED LONGERON REPAIR AS PER SRM 53-02 PAGE 48-53. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 1. PERFORMED SEAT TRACK REPAIR PLUG PER 53-05 FIG 4A. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TUL - FOUND RIGHT CUSP SPLICE CORRODED STATION 1162-1165. REMOVED CORROSION FABRICATED AND INSTALLED NEW SPLICE/DOUBLER PER SRM 53-01 AND AARD 53-00-00-02. (M)

Part: BALLAST — BURNED (CABIN)

DFW - FLT 1283 - EN ROUTE DFW-SNA, FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE AND ODOR IN CABIN. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED OVERHEAD BALLAST ASSEMBLY AT SEAT ROW 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BALLAST — DEFECTIVE (CABIN)

DFW - FLT 1283 - EN ROUTE DFW-SNA - SHORTLY AFTER TAKEOFF FLIGHT ATTENDANT REPORTED ELECTICAL SMELL IN CABIN. RETURNED DFW AND LANDEDN WITHOUT FUTHER INCIDENT. REPLACED OVERHEAD BALLAST AT SEAT 22ND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (STAIRWAY)

ORD - DURING OVERNIGHT MAINTENANCE, AFT VENTRAL STAIRWAY FORWARD EMERGENCY EXIT LIGHT ASSY BROKEN. REPLACED AFT VENTRAL STAIRWAY FORWARD EMERGENCY EXIT LIGHT ASSY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTROLLER — DEFECTIVE (NR 1/2)

DSM - FLT 1009 - AFTER T/O ORD, DURING CLIMB-OUT, LOST SECONDARY PRESS CONTROLLER. SELECTED PRIMARY CONTROLLER AND REGAINED PRESS CONTROL. SUBSEQUENTLY LOST PRIMARY PRESS CONTROLLER IN CRUISE AT FL 350. PAX 02 CANISTERS ACT, INITIATED EMERG DESCENT AND A/C DIVERTED TO DSM AND LANDED W/O INCIDENT. O2 CANISTERS AT FWD DOOR F/A POSITION AND AFT GALLEY F/A POSITION FAILED TO EJECT. ALL OTHER CANISTERS EJECTED NORM. A/C MX FERRY DSM/ORD. REPLACED NR 1 AND NR 2 PRESS CONTROLLERS. ALSO, REPLACED CABIN AIR OUTFLOW VLV MOTOR. ACCOMP GROUND ENG AND PRESS CHECK W/NO DEFECTS FOUND. SYS GROUND CHECKED NORMAL OP. REPLACED ALL 02 CANISTERS AND RESTOWED MASKS. REPLACED 02 HOUSING ASSY AT AFT GALLEY F/A POSITION AN

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AFT OF PASSENGER SEAT ROW 21D FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY LAST ROW OF PASSENGER SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)