N982TW

Part: A/C PACK — ODOR (RIGHT) · airframe 51,982 hrs · 26,469 cycles

FUEL ODOR REPORTED BY FLIGHT ATTENDANT IN AFT, THREE ROWS NEAR AFT ENTRY DOOR. DURING DESCENT, ODOR DISAPATED WHEN COLDER SELECTED ON RIGHT PACK, AT A 10 MINUTE DURATION. THE AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED MCM CARD 05-96-70 TO TROUBLESHOOT. RAN APU, BOTH ENGINES PACKS, NO FINDINGS OR ODOR FOUND. MAINTENANCE ALSO PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: REGULATOR VALVE — FAILED (FUEL) · airframe 51,520 hrs · 26,161 cycles

A STRONG ODOR WAS DETECTED AFTER TAKEOFF AND WHEN LANDING, FUEL ODOR IN CABIN AND COCKPIT AREAS. THE AIRCRAFT WAS GROUNDED. FOUND THE LEFT PRESSURE REGULATOR VALVE FAILED. REPLACED THE PRESSURE REGULATOR VALVE IAW MM 21-31-01. SYSTEM OPS AND LEAK CHECKED GOOD, NO FURTHER ODORS NOTED.

Part: MOTOR — FAILED (PRIMARY TRIM) · airframe 50,896 hrs · 25,765 cycles

ON DEPARTURE, PRIMARY FORWARD TRIM WOULD NOT FUNCTION. EMERGENCY WAS DECLARED, FLIGHT LANDED WITHOUT INCIDENT. THE ACFT WAS GROUNDED. SUITCASE AND WHEEL SWITCHES WOULD NOT WORK. REPLACED THE HORIZONTAL STABILIZER PRIMARY TRIM MOTOR IAW WORK CARD NO. 27-94-15, OPS CHECKED NORMAL.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 50,188 hrs · 25,311 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM AFT CABIN DOOR THROUGH EMPENNAGE. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER IAW WDM 33-51-13 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 50,188 hrs · 25,311 cycles

COCKPIT & FWD GALLEY OVERHEAD EMERGENCY LIGHTS ARE DIM. THE AIRCRAFT WAS GROUNDED. REMOVED & REPLACED THE B5-23 BATTERY PACK ASSY IAW WDM 33-51-11, & 33-51-12. OPS CHECKED GOOD.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 50,188 hrs · 25,311 cycles

FOWARD RIGHT GALLEY EMERGENCY LIGHTS BATTERY PACK AND CHARGER SUSPECTED OF BEING BAD. MAINTENANCE REPLACED THE CHARGER IAW WDM 33-51-15, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 50,188 hrs · 25,311 cycles

FOWARD RIGHT GALLEY EMERGENCY LIGHT BATTERY PACK AND CHARGER SUSPECTED OF BEING BAD. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER IAW WDM 33-51-15 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,188 hrs · 25,311 cycles

RIGHT OVERWING EXIT SIGN INOPERATIVE. REPLACED THE BATTERY & CHARGER ASSEMBLY IAW AMM 33-53-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,188 hrs · 25,311 cycles

OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CHARGER IAW 33-51-13. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 50,188 hrs · 25,311 cycles

RIGHT GALLEY DOOR EMERGENCY LIGHT INOPERATIVE. FOUND THE QUICK DISCONNECT WIRE BROKEN. PINNED THE CONNECTOR IAW AWD 33-51-15.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,188 hrs · 25,311 cycles

OVERHEAD EMERGENCY LIGHTS ROWS 28 TO 31 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW WDM 33-51-12. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 50,188 hrs · 25,311 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM AFT CABIN DOOR THROUGH EMPENNAGE. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER IAW WDM 33-51-13, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,188 hrs · 25,311 cycles

FLOOR LEVEL EMERGENCY EXIT LIGHT ACROSS FROM FOWARD LAVATORY WAS MISSING THE LENS. MAINTENANCE REPLACED THE LIGHT ASSY IAW WDM 33-51-15, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: LINE — UNSECURE (OXYGEN SYSTEM) · airframe 49,588 hrs · 24,931 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. SDF-DFW FLIGHT DIVERTED TO BNA ACCOUNT OF FLIGHT DECK OXYGEN PRESSURE LOSS. OVERWEIGHT LANDING UNEVENTFUL. SECURED SUPPLY LINE AND REPLACED CREW OXYGEN BOTTLE PER AMM 35-10-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 49,528 hrs · 24,895 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY LED FLASHLIGHT BY THE L1 DOOR DOES NOT FLASH. REMOVED AND REPLACED FLASHLIGHT BATTERY PACK PER AMM 25-60-02. OPERATIONAL CHECK GOOD.

Part: LIGHT — DEFECTIVE (COCKPIT) · airframe 49,281 hrs · 24,729 cycles

AIRCRAFT WAS NOT GROUNDED. ELECTRICAL ODOR FROM CAPTAINS CHART HOLDER LIGHT. THE LIGHT WAS EXTREMELY HOT TO TOUCH AND COULD NOT TURN OFF. PULLED CIRCUIT BREAKER AND SMELL/HEAT WENT AWAY. REMOVED AND REPLACED CHART HOLDER LIGHT PER AMM 33-10-00. OPERATIONAL CHECK GOOD.

Part: LANYARD — FRAYED (ZONE 800) · airframe 49,229 hrs · 24,691 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD GALLEY DOOR GIRT BAR LANYARD CABLE IS FRAYED. REPLACED GIRT BAR LANYARD CABLE. OPERATIONAL CHECK GOOD.

Part: FITTING — BROKEN (ZONE 800) · airframe 49,229 hrs · 24,691 cycles

AIRCRAFT WAS GROUNDED. FORWARD GALLEY DOOR GIRT BAR CLIP IS BROKEN. REPLACED GIRT BAR AFT STOW CLIP. OPERATIONAL CHECK GOOD.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 49,168 hrs · 24,657 cycles

THE AIRCRAFT WAS GROUNDED. WEATHER RADAR FAILED. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO ORD WITHOUT FURTHER INCIDENT. REPLACED WEATHER RADAR RT IAW AMM 34-41-04; OPS CHECK GOOD.

Part: FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 48,485 hrs · 24,237 cycles

CORROSION ON LT WING OUTBOARD FLAP CENTER HINGE UPPER MOUNTING STUDS AT WING STATION XW 251.683. REMOVED AND REPLACED THE FITTING IAW AMM 57-40-01.

Part: STUD — CORRODED (RT WING) · airframe 48,485 hrs · 24,237 cycles

CORROSION ON RT WING OUTBOARD FLAP INBOARD HINGE UPPER AND LOWER MOUNTING STUDS AT WING STATION XW 154.584. REMOVED AND REPLACED THE STUDS IAW AMM 57-40-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,485 hrs · 24,237 cycles

NOSE LANDING GEAR AFT FOLLOW UP DOOR IS CRACKED AT THE RIGHT AFT CUT OUT. REPAIRED IAW SRM 53-05-00-001 AND SGO9530030.

Part: GIRT BAR — OBSTRUCTED (CABIN DOOR) · airframe 48,484 hrs · 24,237 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD CABIN DOOR GIRT BAR DIFFICULT TO DISARM. MAINTENANCE CLEANED TRASH FROM FORWARD CABIN DOOR GIRT BAR FLOOR FITTING PER AMM 25-62-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — ODOR (CABIN) · airframe 48,267 hrs · 24,101 cycles

CLIMB OUT OF KRDU, FLIGHT ATTENDANTS REPORTED STRONG BURNING ODOR IN CABIN. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO KRDU WITHOUT FURTHER INCIDENT. DEBRIEF INDICATED NON ELECTRICAL OR OIL, SUSPECT PINE POLLEN. ACCOMPLISHED MCM CARD 21-96-01. NO ODOR NOTED. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,847 hrs · 23,828 cycles

AIRCRAFT NOT GROUNDED. CEILING EMERGENCY EXIT LIGHTS IN ROWS 7 THROUGH 12 FAILED TEST. REMOVED AND REPLACED BATTERY ASSEMBLY B5-101 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,847 hrs · 23,828 cycles

AIRCRAFT NOT GROUNDED. OVERHEAD EMERGENCY EXIT LIGHTS AT AFT BULK DOOR L2-615 AND L2-671 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY B5-27 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.

Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 47,732 hrs · 23,753 cycles

STRONG FUMES AND ODORS IN CABIN. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED WATER SEPARATOR COALESCER BAGS IAW AMM 21-20-02. LEAK AND OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 47,668 hrs · 23,713 cycles

EMERGENCY LIGHT POWER SUPPLY AB5-2 FAILED. REMOVED AND REPLACED POWER SUPPLY BATTERY PACK IAW AMM 33-60-98. OPERATIONAL CHECKED GOOD.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 47,324 hrs · 23,482 cycles

AIRCRAFT WAS GROUNDED. DFW, AIR INTERRUPT, DFW-STL. EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING CLIMB THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. REMOVED AND REPLACED WATER SEPARATOR TEMPERATURE CONTROL VALVE IAW AMM 21-20-03. ACCOMPLISHED CARD 36-95-14 WITH NO LEAKS FOUND.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 45,904 hrs · 22,616 cycles

L1 DOOR SLIDE FELL FROM HOUSING. SLIDE DID NOT DEPLOY, BUT SLIDE DEPLOYMENT PIN WAS COMING APART. R & R L1 DOOR SLIDE IAW MM 25-62-00. THE ACFT WAS GNDED.

Part: SLIDE — DEFECTIVE (ZONE 800) · airframe 45,551 hrs · 22,375 cycles

AIRCRAFT WAS GNDED. FWD GALLEY GIRT BAR APPEARS SKEWED ON ONE SIDE. WHITE LINE IS FURTHER ON LT SIDE. R & R SLIDE IAW AMM 25-62-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

L2R IS CRACKED AT FS 1418. ACCOMPLISHED SPLICE REPAIR IAW SRM 53-03-00-001 FIGURE 31A & AARD 53-10-00-15.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

L2L IS CRACKED AT FS 1418. ACCOMPLISHED SPLICE REPAIR IAW SRM 53-02-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

DENT FOUND IN FUSELAGE SKIN AT STATION 427, BETWEEN L20R - L21R, OUT OF SRM LIMITS. CUT OUT DAMAGED AREA, INSTALLED DOUBLER, TRIPLER & SKIN FILLER IAW SRM 53-05-00 FIGURE 105 SHEETS 1 - 3. ACFT IN BASE MX.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

AFT VAULT DOOR JAMB, LOWER LT DOOR STOP PAD, SUPPORT FITTING IS CRACKED. REMOVED & INSTALLED NEW STOP FITTING IAW AARD 51-05-00-1, SRM 53-14-03-001, DWG 5917579, & DWG 53632. ACFT IN BASE MX.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

AIRCRAFT IN BASE MX. CORROSION ON RT CUSP AT STATION 1139. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-16.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

HC VISIT 4, FUSELAGE FRAME AT STATION 1401 CRACKED ON FWD SIDE AT L1, INSTALLED DOUBLER REPAIR IAW SRM 53-01-00-001 & AARD 53-10-00-15.

Part: SKIN — CHAFED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

APU SHROUD CHAFING ON AFT SKIN NEAR NR 3 RIB AT RADIUS. REPAIRED IAW AARD 53-20-00-11 REPAIR 11.

Part: SKIN — CHAFED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

APU ENCLOSURE HAS DEEP CHAFING DAMAGE ON THE UPPER SKIN LEFT AFT SIDE, 8 1/4" FROM OTBD EDGE. REPAIRED IAW AARD 53-20-00-11 REPAIR 11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

CABIN FLOORBOARD SUPPORT CRACKED AT STATION 237 & BL0. R & R SUPPORT IAW SRM 51-01-00-001 & SRM 51-30-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,360 hrs · 22,263 cycles

CORROSION ON FLOORBOARD SUPPORT AT STATION 237 & LBL 15L. R & R SUPPORT IAW SRM 51-01-00-001 & SRM 51-30-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,360 hrs · 22,263 cycles

HC VISIT 4, NR 6 SEAT TRACK, CORRODED FROM STATION 212 TO 589. R & R NR 6 SEAT TRACK SECTION FROM STATION 218 TO 588 IAW AARD 51-00-05-1 & SRM 53-40-01-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,360 hrs · 22,263 cycles

PAINT FLAKING ON RT CUSP, BETWEEN STATIONS 897 & 900, DUE TO CORROSION. R & R CUSP SHEET, BETWEEN STATIONS 845 & 905 IAW AARD 51-00-05-1 & DWG 9910151.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 45,005 hrs · 22,059 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, RT HYD SYS PRESS DROPPED TO ZERO. ACFT STOPPED ON RUNWAY & WAS TOWED TO GATE. R & R RT HYD EDP IAW AMM 29-10-0 5. PERFORMED HYD RESERVOIR LEAK CHECK IAW MCM 29-96-10. ALL OPERATIONAL CHECKED GOOD, NO LEAKS NOTED & HYD PRESS NORMAL.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 44,135 hrs · 21,549 cycles

FLASHLIGHT AT NR 4 JUMP SEAT IS INOPERATIVE & DOES NOT SEEM TO RECHARGE. R & R FLASHLIGHT & BASE IAW AMM 25-60-00.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 43,256 hrs · 21,050 cycles

AFT STAIRS LEFT WALL EMER LIGHTS NOT WORKING IN 2 PLACES. SECURED LOOSE CONNECTOR.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 45,360 hrs · 22,263 cycles

AIRCRAFT IN BASE MX. A 1/4 INCH HOLE IS THE RT CUSP AT STATION 249. INSTALLED DOUBLER REPAIR IAW AARD 53-20-00-01.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 43,107 hrs · 20,975 cycles

FORWARD PORTABLE EMER LIGHT IS INOPERATIVE. R & R FWD PORTABLE EMER LIGHT. SYS CHECKED NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,504 hrs · 20,656 cycles

CRACK IN FUSELAGE AT STATION 1474, RT SIDE AFT OF ELEVATOR ACCESS DOOR. INSTALLED REPAIR DOUBLER IAW SRM 53-01-00-001.

Part: CASTING — CRACKED (LE SLAT) · airframe 42,504 hrs · 20,656 cycles

RIGHT WING NR 4 SLAT TRACK CASTING CRACKED. INSTALLED REPAIR DOUBLER.

Part: RIB — CRACKED (LT WING) · airframe 42,504 hrs · 20,656 cycles

CRACK IN LT WING NR 4 SLAT TRACK SUPPORT FITTING. INSTALLED REPAIR DOUBLER.

Part: CASTING — CRACKED (RT SPOILER) · airframe 38,023 hrs · 18,272 cycles

RIGHT WING, GROUND SPOILER ACTUATOR CASTING IS CRACKED AT INBOARD FORWARD AREA. INSTALLED FITTING/CASTING PER AARD 51-00-05-1.

Part: MOTOR — INOPERATIVE (CABIN PRESSURE) · airframe 36,441 hrs · 17,444 cycles

DFW - CREW REPORTED NUMBER 2 CABIN PRESSURE CONTROLLER INOPERATIVE DURING CLIMBOUT WITH NUMBER 1 ON PLACARD. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BOTH PRESSURE CONTROLLER MOTORS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 35,598 hrs · 16,978 cycles

FORWARD EMERGENCY LIGHT IN AFT STAIRWELL IS MISSING LENS. REPLACED LIGHT ASSEMBLY FOR FORWARD EMERGENCY LIGHT IN AFT STAIRWELL. OPS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 35,598 hrs · 16,978 cycles

EMERGENCY PROXIMITY LIGHT AT ROW 10 DEF INOPERATIVE. RECONNECTED EMERGENCY PROXIMITY LIGHT ASSEMBLY AT ROW 10DEF. OPS CHECKED NORMAL.

Part: CONTACT — DEFECTIVE (COCKPIT) · airframe 35,241 hrs · 16,804 cycles

DFW - CREW REPORTED MUTIPLE NAVIGATION ISSUES. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CONTACT AT 530-19. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

SKIN DENTED AND GOUGED STATION 300 BETWEEN LONGERONS 23 AND 24 LEFT. ACCOMPLISHED DOUBLER REPAIR PER DRAWING SG09530002.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

FORWARD CARGO CORROSION ALONG DOOR CUTOUT BEAM STATIONS 389 TO 408. REMOVED AND REPLACED LOWER DOOR PAN PER SRM 53-05-00 FIGURE 44.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

CRACK IN LEFT CUSP SHEET STATION 226 BELOW NUMBER 2 SEAT TRACK. REPAIRED CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

LEFT CUSP CRACKED STATION 219. REPAIRED CUSP PER AARD 53-20-00-16.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

AFT CARGO HAS CORROSION ON FRAME STATION 1271 ABOVE LONGERONS 29 LEFT AND 29 RIGHT. REPAIRED CORRODED FRAME PER AARD 53-10-00-14 FIGURE 1, SHEET 2.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

REPAIR DOUBLER AT STATIONS 229 TO 245, BELOW LONGERON 18 LEFT, DENTED. INSTALLED PERMANENT REPAIR PER SRM 53-34-00 FIGURES 1 AND 2, SRM 53-04-05 FIGURE 2 AND SRM 51-60-00.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

CRACK IN SUB-FLOOR UNDER FORWARD LAVATORY MOUNT, STATION 200 LEFT BUTTLINE 44. REPAIRED PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

CORROSION AT STATION 196 LEFT BUTTLINE 54. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

LEFT CUSP CORRODED, STATION 1174 TO 1250. REPLACED CUSP, STATIONS 1174 TO 1250 PER AARD 51-10-00-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

INTERCOSTAL STATIONS 1271 TO 1287, BETWEEN FLOORBEAMS, BUTTLINE 0 CRACKED. REPLACED INTERCOSTAL PER AARD 51-10-00-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

CORROSION AT NUMBER 4 SEAT TRACK STATION 1267. SPLICE REPAIR FROM STATIONS 1240 TO 1309 PER SRM 53-05-00 FIGURE 4F.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

H FITTING AT FLOORLINE LEFT STATIONS 1170 TO 1174 CORRODED. INSTALLED NEW H FITTING PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

LEFT CUSP SHEET STATIONS 1174 TO 1250 CORRODED. REPLACED LEFT CUSP SHEET AT STATIONS 1174 TO 1250 PER AARD 51-10-00-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

AFT CARGO HAS CRACKED INTERCOSTAL IN CEILING FROM STATIONS 1287 TO 1309 BUTTLINE 0. REPLACED INTERCOSTAL PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

LEFT CUSP CORRODED AT STATIONS 1172 TO 1174. REPLACED LEFT CUSP AT STATIONS 1098 TO 1174 PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

BLENDED CORRISON BEYOND MANUAL LIMITS AT STATIONS 725 TO 729 LEFT. INSTALLED CUSP REPAIR AT STATIONS 725 TO 729 LEFT PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

DENT IN FUSELAGE SKIN AT STATION 225 LONGERONS 15 AND 16 LEFT. INSTALLED DOUBLER PER SG09530001 ZONE 52.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

G2 GALLEY FORWARD OUTBOARD MOUNT AT FORWARD END OF NUMBER 6 SEAT TRACK CORRODED. REPLACED MOUNT PER AARD 51-10-00-5.

Part: SUPPORT — GOUGED (LE SLAT) · airframe 34,609 hrs · 16,492 cycles

RIGHT WING NUMBER 15 SLAT TRACK OUTBOARD SUPPORT GOUGED AT FORWARD END. REMOVED AND REPLACED DAMAGED NUMBER 15 SLAT TRACK SUPPORTS PER AARD 51-00-00-1.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,609 hrs · 16,492 cycles

RIGHT CUSP SHEET STATIONS 218 TO 237, CORROSION OUT OF LIMITS. INSTALLED RIGHT CUSP STATIONS 218 TO 237 PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 34,609 hrs · 16,492 cycles

CRACK AT RIGHT WINDOW PAN UPPER AFT CORNER, STATION 1022. TRIMMED DAMAGE AND INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

VAULT DOOR JAMB, RIGHT SIDE, CENTER PAD SUPPORT FITTING IS CRACKED ON THE AFT SIDE OF THE JAMB. REMOVED OLD FITTING AND INSTALLED SERVICABLE FITTING PER AARD 51-10-00-5.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 34,609 hrs · 16,492 cycles

VAULT DOOR JAMB, RIGHT SIDE, CENTER PAD SUPPORT FITTING IS CRACKED ON THE AFT SIDE OF THE JAMB. REMOVED OLD FITTING AND INSTALLED SERVICABLE FITTING PER AARD 51-10-00-5.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 33,702 hrs · 16,012 cycles

SEAT 21D EMERGENCY LIGHT INOPERATIVE. RE-SEATED CONNECTOR AT SIDEWALL. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 33,702 hrs · 16,012 cycles

AFT VAULT DOOR LEFT SIDE LOWER LENS MISSING. REPLACED LENS. OPS CHECK NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 33,702 hrs · 16,012 cycles

SEAT 14D EMERGENCY LIGHT INOPERATIVE. RE-SEATED CONNECTOR AT SIDEWALL. OPS CHECK NORMAL.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 33,064 hrs · 15,713 cycles

DFW - CREW REPORTED WEATHER RADAR FAILED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED WEATHER RADAR RECEIVER/TRANSCEIVER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DUCT — DAMAGED (AC BAY) · airframe 33,056 hrs · 15,710 cycles

MCI - CREW REPORTED TAIL TEMPERATURE HIGH LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED MCI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED DUCT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GASKET — LEAKING (ANTI-ICE SYS) · airframe 33,056 hrs · 15,709 cycles

MCI - INFLIGHT ORD-AUS. CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. ACCOMPLISHED QRH AND LIGHT WENT OUT. EMERGENCY DECLARED FLIGHT DIVERTED MCI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND GASKET FOR LEFT ANTI-ICE LOW TEMP SWITCH LEAKING. REPLACED LOW TEMP SWITCH AND GASKET. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SENSOR — INOPERATIVE (LT MLG) · airframe 32,113 hrs · 15,233 cycles

DFW - CREW REPORTED GEAR DOOR OPEN LIGHT ILLUMINATED AFTER GEAR EXTENSION. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT LANDED WITH MAIN LANDING GEAR DOORS OPEN. GEAR DOOR SKID PLATES UTILIZED UPON LANDING. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT MAIN GEAR DOOR SENSOR AND LEFT AND RIGHT GEAR DOOR SKIDS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COMPUTER — FAULTY (NR 2) · airframe 30,920 hrs · 14,647 cycles

SEA - INFLIGHT PDX-DFW. CREW REPORTED THE DIRECT FLIGHT GUIDANCE COMPUTER (A) CHANNEL CIRCUIT BREAKER TRIPPED. EMERGENCY DECLARED FLIGHT DIVERTED SEA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 2 DIRECT FLIGHT GUIDANCE COMPUTER AND SWITCH (A). SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,703 hrs · 14,541 cycles

SHEAR CLIP CRACKED AT AFT SIDE OF 1437 LONGERON 2 LEFT. REMOVED AND REPLACED SHEAR CLIP PER EA MD 8051-011068.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 30,703 hrs · 14,541 cycles

SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 LEFT. INSTALLED NEW SHEAR TIE CLIP PER SRM 51-01-00.

Part: OVEN — DIRTY (GALLEY) · airframe 29,641 hrs · 14,056 cycles

EWR - CREW REPORTED STRONG ODOR IN CENTER COACH SECTION. FOUND PLASTIC IN FIRST CLASS INBOARD OVEN CAUSING ODOR. CLEANED FORWARD INBOARD GALLEY OVEN. OPERATED OVEN AT HIGH TEMPERATURE FOR ONE HOUR AND NO ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 29,190 hrs · 13,876 cycles

SEAT ROW 29DEF EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK AT SEAT ROW 29DEF.

Part: CONNECTOR — LOOSE (CABIN) · airframe 29,190 hrs · 13,876 cycles

SEAT 22 DEF EGRESS EMERGENCY LIGHT INOPERATIVE. RECONNECTED EGRESS LIGHT ASSEMBLY CONNECTOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,190 hrs · 13,876 cycles

FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT FIRST CLASS SECTION.

Part: BATTERY — NOT SEATED (AC BAY) · airframe 27,384 hrs

LGA - EMERGENCY LIGHTS ABOVE TAIL COMPARTMENT CATWALK INOPERATIVE. RESEATED BATTERY FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT CATWALK.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 27,384 hrs

LGA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. RESEATED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 14D.

Part: SHROUD — DAMAGED (CABIN) · airframe 27,384 hrs

LGA - SEAT MOUNTED EMERGENCY LIGHT SHROUD DAMAGED. REPLACED SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,384 hrs

LGA - CEILING EMERGENCY LIGHTS FROM ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK AT ROW 28 FOR EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,083 hrs

SAN - CEILING EMERGENCY LIGHTS AT ROWS 23 TO 27 AND OVER THE EMERGENCY EXIT FORWARD OVERWING DOORS. REPLACED BATTERY PACKS,

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 26,220 hrs · 12,608 cycles

EMERGENCY BATTERY PACK ABS-1 WEAK. REPLACED BATTERY PACK WITH SERVICEABLE UNIT AND OPERATIONAL CHECKED. PART NUMBER BAT5016/SERIAL NUMBER 18858 AMM 33-60-98-4.

Part: FITTING — CORRODED (ZONE 100) · airframe 26,220 hrs · 12,608 cycles

LEFT MAIN LANDING GEAR WHEEL WELL, TRAPEZOID FITTING TOP ATTACH ANGLE CORRODED. REPLACED TRAPEZOID FITTING ATTACH ANGLE PER SRM 57-09-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,777 hrs

LGA - OVERHEAD EMERGENCY LIGHT AT AFT GALLEY SERVICE DOOR INOPERATIVE. INSTALLED LAMP FOR OVERHEAD EMERGENCY LIGHT AT AFT GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,777 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD AFT GALLEY SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD AFT GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · 25,271 cycles

LGA SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 24,613 hrs

SFO - EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. RECONNECTED SIDEWALL CONNECTOR FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 24,202 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROWS 7 TO 2O INOPERATIVE. REPAIRED HARNESS AT SEAT 14DEF FOR EMERGENCY LIGHTS AT SEAT ROWS 7 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,202 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROWS 7 TO 2O INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,202 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROWS 7 TO 2O INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — LOOSE (BATTERY PACK)

LGA - EMERGENCY LIGHTS AT BOTH AFT OVERWING EXITS INOPERATIVE. SECURED LOOSE WIRE ON BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS AT BOTH AFT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY EXIT LIGHT LENS AND BULBS AT SEAT 3E MISSING. REPLACED LENS AND BULBS FOR EMERGENCY EXIT LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — STUCK (LT ENGINE)

PVR - INFLIGHT, LEFT ENGINE OIL TEMPERATURE 175 DEGREES WITH FUEL HEAT ON. RETURNED TO PVR AND LANDED WITHOUT INCIDENT. FOUND FUEL HEAT VALVE STUCK OPEN. ACCOMPLISHED ENGINEERING PRE FERRY BILL OF WORK. REPLACED LEFT ENGINE AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 3 TO 19 INOPERATIVE. REPAIRED WIRING AT SEAT ROW 14CDE AND REPLACED BATTERY PACKS AT B5103, B523 AND B5107 FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 3 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - CEILING EMERGENCY LIGHTS AT ROW 3D INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 3D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - CEILING EMERGENCY LIGHTS AT ROWS 27 AND 29 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FOR ROWS 27 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WARNING LIGHT — ILLUMINATED (NLG)

ORD - INFLIGHT T1335/22 NOSE GEAR RED LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. ACCOMPLISHED FULL SERVICE ON NOSE LANDING GEAR STRUT AND GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS INOPERATIVE ON SIDES OF SEATS FROM SEAT ROW 20D BACK. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 9,600 hrs · 5,351 cycles

THE EGRESS LIGHTING HAD WIRES EXPOSED AND PULLED OUT AT CABIN ROWS 15 AND 16. MADE AIRWORTHY REPAIR TO WIRING. CHECK-C 11-19-02 STL.

Part: SKIN — DENTED (FUSELAGE) · airframe 9,499 hrs · 5,290 cycles

FOUND A DENT ON THE LEFT SIDE OF THE FUSELAGE BETWEEN LONGERON L18 AND L19, AT STA 237. REPAIRED DENT PER ARA 18325. CHECK-C 11-19-02 STL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,374 hrs · 5,218 cycles

THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 8 TO 10. RESEATED BATTERIES IN THE BATTERY PACK AT ROW 8. CHECK-C 11-19-02 STL.

Part: BATTERY · airframe 9,117 hrs · 5,071 cycles

THE TAIL CONE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED BOTH BATTERY PACKS, AT B5-27 AND B5-28. CHECK-C 11-19-02 STL. --CLOSED--

Part: BULB · airframe 8,781 hrs · 4,890 cycles

IN ARM EGRESS FLOOR LIGHT OUT AT ROW 5 DUE TO WEAR OF DESIGN DEFICIENCY. RESEATED BULB IN ROW 5 EGRESS FLOOR LIGHT SOCKET. EMERGENCY EGRESS LIGHT SYSTEM OPS CHECK PER MM33-59-00. CKECK-C 11-19-02 STL. --CLOSED--

Part: BATTERY · airframe 8,781 hrs · 4,890 cycles

EMERGENCY LIGHTING SYSTEM BATTERIES IN ROW 9 WERE INOPERATIVE. REPLACED FWD BATTERY PACK PER MM33-53-11. OPS CHECKED NORMAL PER MM33-59-00. CHECK-C 11-19-02-STL. --CLOSED--

Part: BATTERY · airframe 8,741 hrs · 4,865 cycles

BOTH COCKPIT EMERGENCY LIGHTS FAILED TO ILLUMINATE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 11-19-02 STL. --CLOSED--

Part: RECEPTACLE — DENTED (CARGO DOOR) · airframe 5,952 hrs · 3,136 cycles

DURING CHECK-C MAINT THE FWD CARGO DOOR, THE FWD AND LOWER EDGE OF THE DOOR HANDLE RECEPTACLE WAS DENTED. REPAIRED PER SRM 52-05 FIG 30.

Part: LAMP — LOOSE (ROW 20)

THE EGRESS LIGHTING WAS INOPERATIVE AROUND CABIN ROW 20. SECURED A LOOSE LAMP IN THE CONNECTOR. NO CHECK-C.