N9677W

Part: MEGAPHONE — DEFECTIVE (FWD CABIN) · airframe 52,904 hrs · 27,019 cycles

FORWARD MEGAPHONE VOLUME TOO LOW AND HANDLE COMING LOOSE. REPLACED THE MEGAPHONE IAW MM 23-34-00. OPS CHECKED NORMAL.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 52,407 hrs · 26,690 cycles

CORROSION ON LEFT WING OUTBOARD FLAP CENTER HINGE FITTING. REPLACED HINGE FITTING IAW AMM 57-40-01.

Part: SKIN — CRACKED (BS 100-110) · airframe 52,407 hrs · 26,690 cycles

FUSELAGE SKIN CRACKED AT THE NOSE LANDING GEAR AFT RT DOOR, AFT HINGE CUT OUT. REPAIRED THE SKIN IAW SRM 53-05-00, FIG 158.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 52,161 hrs · 26,535 cycles

AIRCRAFT WAS GROUNDED. BOTH A & B CHANNELS ON FUEL GAUGE WENT BLANK. AC RETURNED TO DFW, EMERGENCY DECLARED AND FLIGHT LANDED OVERWEIGHT AND WITHOUT INCIDENT. REPLACED FUEL QUANTITY INDICATOR PER MM 28-40-00. TEST GOOD.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 51,568 hrs · 26,150 cycles

SEAT ASSEMBLY 20DEF EMERGENCY LIGHT LENS BASE CRACKED. REPLACED THE LENS BASE IAW ESO 81553.

Part: CONNECTOR — LOOSE (CABIN) · airframe 51,462 hrs · 26,084 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT INOPERABLE AT SEAT 32D. FOUND CONNECTOR LOOSE AT SEAT 32D RECONNECTED PER AMM 33-53-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 51,462 hrs · 26,084 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 14D. MAINTENANCE FOUND A WIRE DISCONNECTED AND REPAIRED IAW AMM 33-53-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMEGENCY LIGHTS) · airframe 51,207 hrs · 25,926 cycles

SEAT MOUNTED ESCAPE LIGHTING FAILED DUAL FEED CHECK. REPLACED FORWARD BATTERY IN OVERHEAD LAVATORY AREA IAW AML 33-53-00.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 51,207 hrs · 25,926 cycles

SEAT MOUNTED EMERGENCY LIGHTS FAILED A DUAL FEED CHECK. REPLACED THE AFT BATTERY IN OVERHEAD GALLEY AREA IAW AML 33-53-00. OPS CHECKED NORMAL IAW AML 33-53-00/601.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 50,591 hrs · 25,522 cycles

EMERGENCY EXIT LIGHTS OVERHEAD IN THE COCKPIT AND FORWARD ENTRY DOOR DO NOT COME ON. REMOVED AND REPLACED BATTERY PACK B5-23 IAW AMM 33-50-00. OPS CHECKED GOOD. THE AIRCRAFT WAS GROUNDED.

Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 50,313 hrs · 25,321 cycles

LEFT AFT EMERGENCY EXIT LIGHT HAS TWO BARE WIRES FROM CHAFING. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM 33-53-01. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 50,243 hrs · 25,277 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT REPORTS THE AFT MEGAPHONE WILL NOT TEST. REMOVED AND REPLACED MEGAPHONE BATTERIES. OPERATIONAL CHECK GOOD.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 50,069 hrs · 25,151 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY PORTABLE LIGHT IS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 49,975 hrs · 25,090 cycles

THE AIRCRAFT WAS GROUNDED. CENTER FUEL PRESSURE LOW ANNUNCIATOR OCCURRED DURING CLIMB OUT. PERFORMED QRH PROCEDURE. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO KDFW BECAUSE OF RESULTING CONFIGURATION SITUATION. ACCOMPLISHED UFI'S IAW MM 28-20-28, NO FAULTS NOTED. REMOVED AND REPLACED R2-571 AND R2-593 RELAYS IAW CH 20-20-03 AS A PRECAUTION. REMOVED AND REPLACED BOTH CENTER TANK FUEL PRESSURE LOW SWITCHES PER AMM 28-41-01. LEAK CHECK AND OPS CHECK GOOD. FUNCTION CHECK AS REQUIRED 28-41-01, LEAK CHECK AND OPS CHECK GOOD. FUNCTION CHECK OF SYSTEM WAS NORMAL. FUEL WOULD TRANSFER IN AND OUT OF CENTER TANK WITH NO FAULTS AND LIGHT WOULD NOT ILLUMINATE WITH BOTH PUMPS SELECTED ON, OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,831 hrs · 25,001 cycles

THE AIRCRAFT WAS NOT GROUNDED. FIRST CLASS EMERGENCY CABIN LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK B5-100 PER AMM 33-53-00. OPS CHECK OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 49,745 hrs · 24,948 cycles

SEAT 32DEF MOUNTED EMERGENCY LIGHT IS INOPERATIVE. FOUND PIN PUSHED BACK ON CONNECTOR. RESET PIN. OPS CHECKED GOOD IAW AMM 33-53-00.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 49,735 hrs · 24,941 cycles

SEAT 14DEF MOUNTED EMERGENCY LIGHT IS INOPERATIVE. FOUND PIN PUSHED BACK ON CONNECTOR. RESET PIN. OPERATIONAL CHECKED GOOD IAW AMM 33-53-00.

Part: COVER — OUT OF ADJUST (TAIL CONE) · airframe 49,027 hrs · 24,506 cycles

TAIL CONE EXIT ARMING HANDLE BECAMES DISARMED DURING TAXI. ADJUSTED AFT CABIN ENTERACE DOOR ARMING HANDLE COVER PER MM 52-12-00 OPS CKED OK. THE AIRCRAFT WAS NOT GROUNDED.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 48,895 hrs · 24,426 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT CARGO DOOR STOP PAD SUPPORT FITTING IS CRACKED, AFT SIDE THIRD FROM TOP. REMOVED AND REPLACED FITTING IAW AARD 51-00-05-1 AND DRAWINGS CDK2345 AND 591014.

Part: LENS — DETACHED (CABIN) · airframe 48,726 hrs · 24,328 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE LOWER FORWARD GALLEY HAS A DETACHED LENS COVER. REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW AMM 33-53-01. OPERATIONAL CHECK GOOD.

Part: BATTERY — FAULTY (CABIN) · airframe 48,619 hrs · 24,254 cycles

AIRCRAFT WAS NOT GROUNDED. OVERHEAD EMERGENCY EXIT LIGHT ABOVE SEAT 28D ILLUMINATES WHEN AIRCRAFT POWER IS OFF. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: CLAMP — LEAKING (ZONE 100) · airframe 48,603 hrs · 24,238 cycles

TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. LANDING UNEVENTFUL. REMOVED AND REPLACED LEAKING CLAMP BETWEEN AIR CYCLE MACHINE AND HEAT EXCHANGER IAW MCM CARD 36-95-14. LEAK AND OPERATIONAL CHECK GOOD.

Part: LATCH — DIRTY (GIRT BAR) · airframe 48,263 hrs · 24,018 cycles

L2 DOOR EVACUATION SLIDE GIRT BAR BRACKET BROKEN ON RIGHT SIDE. CLEARED OBSTRUCTING DEBRIS AND LUBED GIRT BAR LATCH IAW AMM 25-62-00. OPERATIONAL CHECKED GOOD.

Part: LATCH — DIRTY (GIRT BAR) · airframe 48,258 hrs · 24,014 cycles

L2 DOOR EVACUATION SLIDE GIRT BAR LATCH IS STIFF AND DIFFICULT TO OPERATE. LUBRICATED AND CLEANED DEBRIS FROM GIRT BAR LATCH IAW AMM 25-62-00. OPERATIONAL CHECKED GOOD.

Part: MOTOR — FAULTY (OUTFLOW VALVE) · airframe 47,118 hrs · 23,277 cycles

AIRCRAFT WAS GROUNDED. DURING CLIMB THE PRESSURIZATION AUTO INOPERATIVE AND BLUE INOPERATIVE LIGHTS ILLUMINATED. CABIN ALTITUDE CLIMBED. OUTFLOW VALVE CLOSED AND LOCKED MANUALLY. CABIN ALTITUDE REMAINED UNCONTROLLABLE. MAINTAINED 10,000 FOOT ALTITUDE TO DESTINATION. MAINTENANCE R & R BOTH OUTFLOW VALVE AC MOTORS IAW AMM 21-32-05. ACCOMPLISHED FUSELAGE LEAK TEST IAW AMM 21-00-00-501 AND PRESSURE CONTROLLER BITE IAW AMM 21-32-00. SYSTEM CHECKS NORMAL.

Part: MOTOR — FAULTY (OUTFLOW VALVE) · airframe 47,118 hrs · 23,277 cycles

AIRCRAFT WAS GROUNDED. DURING CLIMB, THE PRESSURIZATION AUTO INOPERATIVE AND BLUE INOPERATIVE LIGHTS ILLUMINATED. CABIN ALTITUDE CLIMBED. OUTFLOW VALVE CLOSED AND LOCKED MANUALLY. CABIN ALTITUDE REMAINED UNCONTROLLABLE. MAINTANED 10,000 FOOT ALTITUDE TO DESTINATION. MAINTENANCE R & R BOTH OUTFLOW VALVE AC MOTORS IAW AMM 21-32-05. ACCOMPLISHED FUSELAGE LEAK TEST IAW AMM 21-00-00-501 AND PRESSURE CONTROLLER BITE IAW AMM 21-32-00. SYSTEM CHECKS NORMAL.

Part: B-NUT — LOOSE (APU) · airframe 46,827 hrs · 23,108 cycles

AIRCRAFT WAS GNDED, FLIGHT ATTENDANTS REPORT VERY STRONG ODOR, MUSTY SOUR SMELL, FROM MID CABIN AFT THAT BEGAN DURING TAKEOFF ROLL DIMINISHED DURING CLIMB THEN INCREASED DURING DESCENT. ACCOMPLISHED CARD 21-96-01 & FOUND AN OIL LEAK AT THE APU LOW OIL PRESS SWITCH B NUT. TORQUED B NUT IAW AMM STANDARD PRACTICES & ACCOMPLISHED LEAK CHECK. SYS CHECKS NORMAL.

Part: A/C PACK — FAILED (AC BAY) · airframe 46,234 hrs · 22,763 cycles

TOPPING CIRCUIT ON LT PACK FAILED. SINGLE PACK OPERATION & LT PACK SHUTDOWN DUE TO OVER TEMP & HEAT. RUNNING IN AUTO AT FL 250, PRESSURIZATION FLOW LIGHT CAME ON, SUPPLY TEMP SHOWED 158 DEGREES & PACK RETURNED AFTER COOL DOWN & DESCENT TO 14,000 FEE. PRESSURIZED LT PACK FOR 20 MINUTES WITH SELECTOR IN AUTO. MANUAL COOL & MANUAL HOT POSITION, OPERATIONS CHECK NORMAL IAW MM 21-00-00. THE ACFT WAS GNDED.

Part: MODULE — FAULTY (FUEL SYSTEM) · airframe 45,876 hrs · 22,528 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW LIGHT ILLUMINATED. CTR TANK PUMPS NOT FEEDING. R & R FWD & AFT CTR PUMP UFI & RAM MODULES IAW AMM 28-20-28. SEE ALSO AALA20151220002, AALA20151223004 & AALA20151223006.

Part: UFI — FAULTY (FUEL SYSTEM) · airframe 45,876 hrs · 22,528 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW LIGHT ILLUMINATED. CTR TANK PUMPS NOT FEEDING. R & R FWD & AFT CTR PUMP UFI & RAM MODULES IAW AMM 28-20-28. SEE ALSO AALA20151224004, AALA20151224005 & AALA20151224006.

Part: MODULE — FAULTY (FUEL SYSTEM) · airframe 45,876 hrs · 22,528 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW LIGHT ILLUMINATED. CTR TANK PUMPS NOT FEEDING. R & R FWD & AFT CTR PUMP UFI & RAM MODULES IAW AMM 28-20-28. SEE ALSO AALA20151220002, AALA20151223004 & AALA20151223005.

Part: UFI — FAULTY (FUEL SYSTEM) · airframe 45,876 hrs · 22,528 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CTR FUEL PRESS LOW LIGHT ILLUMINATED. CTR TANK PUMPS NOT FEEDING. R & R FWD & AFT CTR PUMP UFI & RAM MODULES IAW AMM 28-20-28. SEE ALSO AALA20151220002, AALA20151223005 & AALA20151223006.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,376 hrs · 22,243 cycles

FORWARD CARGO HAS SEVERAL SPOTS OF CORROSION ALONG LOWER DOOR PAN, STATION 370 - 427. INSTALLED NEW LOWER DOOR PAN & DOUBLERS IAW SRM 53-05-00-001 FIGURE 44A.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 45,376 hrs · 22,243 cycles

VAULT DOOR JAMB 2ND FROM BOTTOM, STOP PAD FITTING CRACKED, LOCATED RT AFT LAVATORY. REMOVED CRACKED FITTING, INSTALLED NEW FITTING IAW DWG 5917579 & SRM 53-14-03-001.

Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 45,376 hrs · 22,243 cycles

FIRST OFFICER`S AFT RT SEAT RAIL HAS CORROSION AT STATION 120 & 148.5. REPLACED FIRST OFFICER`S AFT RT SEAT RAIL ASSEMBLY AT STATION 120 -148.5 IAW MM 53-40-01, SRM 51-10-03 & SRM 53-01-00.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 45,376 hrs · 22,243 cycles

VAULT DOOR JAMB 2ND FROM BOTTOM, STOP PAD FITTING CRACKED, LOCATED LT AFT LAVATORY. REMOVED CRACKED FITTING, INSTALLED NEW FITTING AT STATION 1338 IAW DWG 5917579 & SRM 53-14-03-001.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,376 hrs · 22,243 cycles

FORWARD GALLEY DRAIN PAN OTBD SUPPORT CORRODED. INSTALLED SERVICEABLE SUPPORT IAW DWG 9923667 & AARD 51-10-03.

Part: MOUNT — WORN (FUSELAGE) · airframe 45,376 hrs · 22,243 cycles

G2 GALLEY MOUNT WORN ON SEAT TRACK NR 6. REPLACED G2 GALLEY MOUNT ON NR 6 TRACK IAW SRM 53-05-00-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,376 hrs · 22,243 cycles

CORROSION ON SEAT TRACK 6, STATION 287 - 290 IS OUT OF LIMITS IAW SRM 53-05-00. REMOVED & INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 200 - 310 IAW SRM 53-05-00 FIGURE 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,376 hrs · 22,243 cycles

SEAT TRACK NR 6 IS CORRODED AT BS 1212 - 1214. INSTALLED A SEAT TRACK PLUG REPAIR IAW SRM 53-05-00.

Part: CUSP WEB — CORRODED (BS 408-481) · airframe 45,376 hrs · 22,243 cycles

RIGHT CUSP WEB BETWEEN BS 480 & 481 HAS CORROSION ON TOP & BOTTOM. REMOVED DAMAGE & INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 45,376 hrs · 22,243 cycles

AFT ACCESSORY COMPARTMENT, SHEAR TIE CRACKED AT RADIUS, FWD SIDE OF FRAME 1380, ABOVE LONGERON 14R. INSTALLED REPAIR ANGLE IAW AARD 53-10-00-20.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,376 hrs · 22,243 cycles

FLOORBOARD SUPPORT AT STATION 120 HAS CORROSION ON INBD SIDE. INSTALLED NEW FLOORBOARD SUPPORT AT STATION 120 IAW DWG 9936533, AASRM 51-10-03-101, AARD 53-20-00-16 & AAMM 53-20-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,376 hrs · 22,243 cycles

FLOORBOARD SUPPORT AT STATION 148.5 HAS CORROSION, LOCATED ON FWD SIDE OF G1 GALLEY DRAIN PAN. INSTALLED NEW SUPPORT IAW DWG 9936533, AASRM 51-10-03 & AAMM 53-20-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 45,376 hrs · 22,243 cycles

E & E COMPARTMENT, CORROSION ON LOWER SURFACE OF SUBFLOOR, AROUND G1 GALLEY DRAIN FLANGE, STATION 148 TO 160. REMOVED CORROSION & INSTALLED DOUBLER IAW DWG 9923667 & AARD 53-20-00-16 REPAIR 16 PARAGRAPH 6.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,376 hrs · 22,243 cycles

CORROSION AT STATION 1155 - 1165, RT CUSP. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: RIB — CRACKED (LT WING) · airframe 42,474 hrs · 20,674 cycles

RIB IS CRACKED ON INBD SIDE OF NR 4 SEAT TRACK ON TOP SIDE OF PULLEY BRACKET MOUNT. ACCOMPLISHED REPAIR IAW EA MD80-57-036079.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,474 hrs · 20,674 cycles

CRACK IN FUSELAGE SKIN ON RT SIDE AT STATION 1380 ABOVE LONGERON 14 RT. INSTALLED EXTERNAL DOUBLER IAW AARD 53-30-00-02.

Part: FORMER — CRACKED (LE SLAT) · airframe 42,324 hrs · 20,586 cycles

RIGHT WING NR 4 SLAT TRACK INBD CRACKED. INSTALLED RT WING NR 4 FORMER DOUBLER IAW WORK CARD 57-98-06 & EA MD80-57-035721.

Part: COVER — OUT OF ALIGNMENT (EVAC SLIDE) · airframe 40,730 hrs · 19,750 cycles

AFT GALLEY SLIDE PACK COVER OUT OF ALIGNMENT & RUBS AIRFRAME OPENING UPON DOOR USE. REPLACED AFT GALLEY SLIDE AFT COVER.

Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 40,526 hrs · 19,647 cycles

SJC CREW REPORTED BIRD STRIKE TO RT HAND ENG DURING CLIMB OUT. RT HAND ENG SHUT DOWN SINGLE ENGINE TIME 8 MINUTES. BOTH FIRE BOTTLES WERE BLOWN. EMERGENCY DECLARED FLIGHT RETURNED SJC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT HAND ENG AT SJC ON 11/17/2013. SYSTEM GROUND CHECKED NORMAL OPERATION OPEN.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 40,128 hrs · 19,411 cycles

EMERGENCY LIGHT AT SEAT ROW 8D IS INOPERATIVE. FOUND CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 8D. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 40,128 hrs · 19,411 cycles

EMERGENCY LIGHT AT SEAT ROW 19D INOPERATIVE. FOUND CONNNECTOR OFF. RECONNECTED CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,128 hrs · 19,411 cycles

OVERHEAD EMERGENCY LIGHT AT SEAT ROW 18 IS INOPERATIVE. REPLACED BATTERY PACK OVERHEAD EMERGENCY LIGHT AT SEAT ROW 18. OPERATIONS CHECKED NORMAL.

Part: COVER — MISSING (CABIN) · airframe 40,128 hrs · 19,411 cycles

EMERGENCY LIGHT AT SEAT ROW 25D MISSING COVER. REPLACED COVER FOR EMERGENCY LIGHT AT SEAT ROW 25D. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 40,128 hrs · 19,411 cycles

CEILING EMERGENCY LIGHT LENS COVER MISSING AT SEAT ROW 8DEF. REPLACED LENS COVER FOR CEILING EMERGENCY LIGHT AT SEAT ROW 8DEF. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,128 hrs · 19,411 cycles

EMERGENCY LIGHT AT SEAT ROW 16D IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 16D. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,128 hrs · 19,411 cycles

OVERHEAD EMERGENCY LIGHT AT SEAT ROW 21 IS INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT SEAT ROW 21. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,128 hrs · 19,411 cycles

EMERGENCY LIGHT AT SEAT ROW 32D IS INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW D. OPERATIONS CHECKED NORMAL.

Part: CASTING — CRACKED (RT SPOILER) · airframe 38,392 hrs · 18,417 cycles

RIGHT WING GROUND SPOILER CENTER WING ACTUATOR CASTING IS CRACKED INBOARD OF ACTUATOR FORWARD ATTACH BOLT. INSTALLED RIGHT WING GROUND SPOILER CASTING ASSEMBLY WITH NEW FASTENERS. INSTALLED NEW FASTENERS IN X BRACE, FORWARD AND AFT LOCATIONS AND INSTALLED NEW FASTENERS IN PANEL FORWARD OF CASTING PER AARD 51-00-05-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,392 hrs · 18,417 cycles

SHEAR TIE CRACKED AFT SIDE OF STATION 1451 AFT OF LONGERON 2 LEFT. REPLACED SHEAR TIE PER AARD 51-00-05-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 38,392 hrs · 18,417 cycles

SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2R. INSTALLED NEW SHEAR TIE PER AARD 51-00-05-01.

Part: CONNECTOR — LOOSE (CABIN) · airframe 36,386 hrs · 17,414 cycles

EMERGENCY PATH LIGHTING AT SEAT 32 WILL NOT ILLUMINATE. SECURED LOOSE CONNECTOR FOR EMERGENCY PATH LIGHT AT SEAT 32. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 36,386 hrs · 17,414 cycles

EMERGENCY PATH LIGHTING WILL NOT ILLUMINATE AT ROW 8. SECURED LOOSE CONNECTOR FOR EMERGENCY PATH LIGHTING AT ROW 8. OPS CHECK NORMAL.

Part: GENERATOR — FAILED (ZONE 400) · airframe 35,439 hrs · 16,931 cycles

CREW REPORTED LEFT ENGINE GENERATOR FAILED WITH AUXILIARY POWER UNIT ON PLACARD. FLIGHT RETURNED LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT GENERATOR AND CONSTANT SPEED DRIVE. SYSTEM GROUND CHECKED NORMAL.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 34,813 hrs · 16,621 cycles

DFW - CREW REPORTED CENTER TANKS WENT EMPTY AT FL330 AND THE RIGHT FUEL PRESSURE LOW LIGHT FLICKERED SEVERAL TIMES. RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 25 MINS). RIGHT AFT BOOST PUMP WAS ON AND RIGHT FORWARD BOOST PUMP WAS ON PLACARD. ENGINE FLAMED OUT SHORTLY AFTER. EMERGENCY DECLARED FLIGHT RETURND DFW LANDED WITHOUT INCIDENT. REPLACED ENGINE DRIVERS FUEL PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

CRACK IN STATION 37 BULKHEAD AT RIGHT LOWER RADOME ALIGNMENT PIN. INSTALLED DOUBLER PER AARD 53-10-00-19.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

LEFT SIDE LONGERON 2 LEFT IS CRACKED AFT SIDE OF FRAME 1418. INSTALLED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

AFT ACCESSORY FRAME 1418 IS CRACKED AT LONGERON 2 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-03-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

LEFT CUSP CORRODED STATIONS 1003 TO 1022. REMOVED AND REPLACED CUSP SHEET PER AARD 51-10-00-5.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

STIFFNER CRACKED RIGHT SIDE BELOW TORQUE TUBE IN AFT ACCESSORY FOR AIR STAIRS. INSTALLED NEW STIFFENER ON RIGHT SIDE BELOW AIR STAIRS TORQUE TUBE PER BOEING DRAWING 9911992 AND AA DRAWING CDK2946 AND PER AARD 51-00-00-012.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,435 hrs · 16,415 cycles

RIGHT CUSP CORRODED STATION 387. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

LEFT CUSP STATION 218 CRACKED. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,435 hrs · 16,415 cycles

LEFT CUSP CORRODED STATIONS 1022 TO 1030. ACCOMPLISHED REPAIR PER AARD 53-20-00-16.

Part: SKIN PANEL — DENTED (TE FLAP) · airframe 34,435 hrs · 16,415 cycles

LEFT WING, DENT IN OUTBOARD FLAP INBOARD TRAILING EDGE WEDGE AT OUTBOARD AFT CORNER. REPLACED DENTED SKIN WITH NEW SKIN AS PER ESO 80096 PER SRM 57-50-14.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

CORROSION ON RIGHT CUSP SHEET AT STATION 387. INSTALLED CUSP DOUBLER AT STATION 387 RIGHT SIDE PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

FORWARD CARGO - DOORWAY, LOWER CUSP HAS CORROSION BETWEEN STATIONS 386 TO 392. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

STATION 240 LONGERON 19 LEFT DENTED. REMOVED CLASS 2 REPAIR AND INSTALLED PERMANENT CLASS 1 EXTERNAL DOUBLER REPAIR PER SRM 53-04-05 FIGURE 5 SHEETS 1-2 AND 7 THROUGH 10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,435 hrs · 16,415 cycles

LEFT LOWER CUSP HAS CORROSION BETWEEN STATIONS 484 TO 503. INSTALLED CUSP DOUBLER AT STATIONS 484 TO 503 LEFT SIDE PER AARD 53-20-00-16.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,435 hrs · 16,415 cycles

WEB CRACKED AT STATION 210, LONGERON 15 LEFT. REMOVED CRACKED WEB AT STATION 210, LONGERON 15 LEFT. FABRICATED REPAIR DOUBLER, ALODINED AND PRIME PAINTED AND INSTALLED DOUBLER PER AARD 53-10-00-11.

Part: DUCT — CRACKED (AC BAY) · airframe 32,870 hrs · 15,582 cycles

PHX - INFLIGHT PSP-DFW. CREW REPORTED TAIL COMPARTMENT OVERHEAT WARNING DURING FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND DUCT IN TAIL SECTION WITH LARGE CRACK. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 31,675 hrs · 15,000 cycles

EMERGENCY LIGHT AT SEAT 5E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. OPS CHECKED NORMAL.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 31,456 hrs · 14,893 cycles

YYC - CREW REPORTED LOST RIGHT HYDRAULIC SYSTEM PRESSURE. EMERGENCY DECLARED, LANDED YYC WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RELIEF VALVE — FAILED (HYDRAULIC SYS) · airframe 31,350 hrs · 14,841 cycles

SEA - CREW REPORTED RIGHT HYDRAULIC SYSTEM LOSS PRESSURE WENT TO 0 PSI IN FLIGHT. EMERGENCY DECLARED LANDED SEA WITHOUT INCIDENT. RIGHT PRESSURE RELIEF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DUCT — BLOWN (RT ENGINE) · airframe 30,070 hrs · 14,275 cycles

PVR - CREW REPORTED AFTER TAKEOFF RIGHT ENGINE MASTER CAUTION LIGHT AND FIRE LOOP LIGHT ILLUMINATED. DECLARED EMERGENCY RETURNED PVR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE INLET GUIDE VANE ANTI ICE DUCT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DUCT — BLOWN (RT ENGINE) · airframe 30,066 hrs · 14,274 cycles

PVR - CREW REPORTED RIGHT ENGINE MASTER CAUTION LIGHT AND FIRE LOOP LIGHT ILLUMINATED. EMERGENCY DECLARED RETURNED PVR WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE ANTI DUCT AND ACCOMPLISHED ENGINE RUNS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PIN — PULLED (CABIN) · airframe 29,173 hrs · 13,899 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM FIRST CLASS TO FIRST OVERWING EXIT INOPERATIVE. AISLE PATH ONLY. FOUND CONNECTOR PINS PULLED LOOSE. REPAIRED CONNECTOR AT SEAT ROW 13DEF.

Part: SENSOR — OUT OF ADJUST (CARGO DOOR) · airframe 28,752 hrs · 13,734 cycles

DFW - ON CLIMBOUT AFT CARGO DOOR WARNING ILLUMINATED. RETURNED DFW WITHOUT INCIDENT. CLEARED DEBRIS FROM DOOR SILL AND ADJUSTED SENSOR GAP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 28,607 hrs · 13,659 cycles

LGA - ONE FORWARD FLASHLIGHT HAS SAFETY STRAP MISSING. REPLACED SAFETY STRAP FOR FORWARD FLASHLIGHT.

Part: BATTERY — NOT SEATED (CABIN) · airframe 27,987 hrs

LGA - AFT STAIRWAY EMERGENCY LIGHT ABOVE EVACUATION SLIDE INOPERATIVE. RESEATED BATTERIES IN CHARGER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,987 hrs

LGA - EMERGENCY LIGHTS IN CEILING AT SEAT 20F INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20F.

Part: BATTERY — NOT SEATED (AC BAY)

LGA - AFT STAIRWAY EMERGENCY LIGHT ABOVE CATWALK INOPERATIVE. RESEATED BATTERIES IN CHARGER.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 27,987 hrs

LGA - AFT GALLEY FLASHLIGHT RETAINING SECURITY STRAP MISSING. INSTALLED NEW SECURITY STRAP FOR AFT GALLEY FLASHLIGHT.

Part: LONGERON — CRACKED (ZONE 100) · airframe 26,263 hrs · 12,652 cycles

LONGERON 2 RIGHT CRACKED AFT OF STATION 1418. REPLACED LONGERON AND SPLICE, INSTALLED PER AARD 53-30-00-2.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 26,263 hrs · 12,652 cycles

SHEAR TIE CRACKED AFT SIDE OF 1451 FRAME, AFT OF LONGERON 2 LEFT. INSTALLED NEW SHEAR TIE.

Part: PIN — LOOSE (ESCAPE SLIDE) · airframe 26,263 hrs · 12,652 cycles

SLIDE PACK CONTAINMENT PIN PULLED LOOSE AND FRANGIBLE LINK (STRING) BROKEN. REPLACED SLIDE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,671 hrs

SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: START VALVE — FAILED (RT ENGINE) · airframe 23,947 hrs

SLC INFLIGHT T2036/23JAN - AT ROTATION RIGHT START VALVE OPEN LIGHT ILLUMINATED AND FIRE BELL SOUNDED FOR ABOUT 2 TO 3 SECONDS THEN EXTINGUISHED. THE RIGHT START VALVE OPEN LIGHT ALSO EXTINGUISHED. RETURNED TO SLC AND LANDED WITHOUT INCIDENT. INSPECTED ENGINE AND FOUND START VALVE FAILED AND CAUSED DAMAGE TO BYPASS DUCT AND OTHER HARDWARE. REPLACED NUMBER TWO ENGINE ON 25 JAN 2008 AT SLC. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - OVERHEAD EMERGENCY LIGHTS AT AFT JUMPSEAT INOPERATIVE. REPLACED OVERHEAD EMERGENCY LIGHT AT AFT JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

SFO - EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROW 31 INOPERATIVE. RECONNECTED SEAT CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SCHRADER VALVE — INOPERATIVE (NLG STRUT)

SAN INFLIGHT T400/31JAN - NOSE GEAR WOULD NOT RETRACT. RETURNED TO SAN AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT FLAT. REPLACED SCHRADER VALVE AND SERVICED STRUT WITH FLUID AND AIR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS FROM FORWARD TO AFT INOPERATIVE. REPLACED BATTERY PACK IN AFT CARGO FOR EMERGENCY LIGHTS FROM FORWARD POSITION TO AFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

MSP - CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED ALL BATTERY PACKS FOR CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

STL - CEILING EMERGENCY LIGHTS AT ROWS 11 THROUGH 26 INOPERATIVE. REPLACED BATTERY PACKS AT B5-102 AND B5-104 FOR CEILING EMERGENCY LIGHTS AT ROWS 11 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS AT CABIN CEILING INOPERATIVE. REPLACED BATTERY PACK AT B5-27 FOR CABIN CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,484 hrs · 5,279 cycles

THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 10-05-02 STL.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 9,455 hrs · 5,262 cycles

THE EMERGENCY CEILING LIGHT WAS INOPERATIVE AT ROW 26. REPLACED THE LAMP P/N 7732. CHECK-C 10-05-2002.

Part: BATTERY — DISCHARGED (CABIN) · airframe 5,402 hrs · 2,887 cycles

THE COCKPIT OVERHEAD EMERGENCY LIGHTS DID NOT ILLUMINATE DURING TEST. REPLACED THE POWER SUPPLY BATTERIES. CHECK-C 11-9-00 JFK.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 3,349 hrs · 1,839 cycles

THE LT AFT LAVATORY SMOKE DETECTOR ANNUNCIATED. MADE UNSCHEDULED LANDING AT GTF. THE LT AFT LAVATORY SMOKE DETECTOR WAS DEFERRED PER MEL. THE DETECTOR WAS LATER REPLACED. CHECK-C 10-26-00 JFK.