N9630A

Part: RIB — CRACKED (RT WING) · airframe 59,569 hrs · 29,898 cycles

RIGHT WING NR 4 SLAT TRACK INBOARD RIB UPPER BOSS IS CRACKED. REPAIRED THE RIB IAW MCM 57-98-06.

Part: PRESSURE SWITCH — FAULTY (LT ENGINE) · airframe 59,499 hrs · 29,850 cycles

DURING APPROACH, THE LEFT OIL STRAINER CLOGGING LIGHT ILLUMINATED IN LEVEL FLIGHT FL220. PERFORMED QRH PROCEDURE. REDUCING THRUST CAUSED LIGHT TO EXTINGUISH. CAME ON DURING APPROACH, LANDED WITH LEFT ENGINE AT IDLE. EMERGENCY DELCARED, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED LEFT ENGINE PRESSURE TRANSMITTER SWITCH IAW AMM 79-35-01.

Part: TURBINE — FAULTY (AC BAY) · airframe 59,271 hrs · 29,698 cycles

AIRCRAFT WAS GROUNDED. ON CLIMB OUT FLIGHT CREW WAS UNABLE TO COOL DOWN THE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW FOR AN UNSCHEDULED LANDING. THE AC WAS NOT OVERWEIGHT AND LANDED WITHOUT INCIDENT. REPLACED THE RT AIRCRAFT TURBINE PER MCM CARD 21-94-02. SEE ALSO SDR'S AALA201807309049 & AALA20180729002.

Part: HEAT EXCHANGER — FAULTY (AC BAY) · airframe 59,271 hrs · 29,698 cycles

AIRCRAFT WAS GROUNDED. ON CLIMB OUT FLIGHT CREW WAS UNABLE TO COOL DOWN THE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW FOR AN UNSCHEDULED LANDING. THE AC WAS NOT OVERWEIGHT AND LANDED WITHOUT INCIDENT. REPLACED THE RT PRIMARY HEAT EXCHANGER PER AMM 21-51-04 AND 21-51-05. SEE ALSO SDR'S AALA201807309049 & AALA201807309050.

Part: HEAT EXCHANGER — FAULTY (AC BAY) · airframe 59,271 hrs · 29,698 cycles

AIRCRAFT WAS GROUNDED. ON CLIMB OUT FLIGHT CREW WAS UNABLE TO COOL DOWN THE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW FOR AN UNSCHEDULED LANDING. THE AC WAS NOT OVERWEIGHT AND LANDED WITHOUT INCIDENT. REPLACE THE RT SECONDARY HEAT EXCHANGER PER AMM 21-51-04 AND 21-51-05. SEE ALSO SDR'S AALA20180729002 & AALA201807309050.

Part: LANYARD — MISLOCATED (R1 DOOR GIRT BAR) · airframe 58,228 hrs · 29,001 cycles

FORWARD GALLEY R1 DOOR GIRT BAR LANYARD NOT ATTACHED PROPERLY. INSTALLED GIRT BAR LANYARD CORRECTLY IAW AMM 25-62-00. OKAY FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 58,141 hrs · 28,936 cycles

AIRCRAFT WAS NOT GROUNDED. DURING CRUISE FLIGHT ATTENDANT REPORTED EMERGENCY FLASHLIGHT AND LED DID NOT FLASH. CABIN EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED AFT EMERGENCY FLASHLIGHT IAW AMM 25-60-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (FUEL PRESSURE) · airframe 57,989 hrs · 28,811 cycles

CENTER FUEL PRESSURE LOW, ILLUMINATED INTERMITTENTLY SHORTLY AFTER LEVEL OFF TO CRUISE. CENTER TANK FUEL FEED NORMAL. INTERMITTENT INDICATION LASTED APPROXIMATELY FIVE MINUTES. REMAINDER OF FLIGHT SYSTEM OPERATED NORMALLY WITH NO FURTHER INDICATION. MAINTENANCE DETERMINED AIRCRAFT CENTER FUEL TANK FUEL FEED SYSTEM TEST IS NORMAL IAW AMM 28-20-00 PART 2C.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 56,973 hrs · 28,138 cycles

THE AIRCRAFT WAS GROUNDED. ELECTRICAL FUMES/ODOR IN THE CABIN AROUND ROWS 7,8, AND 9 DURING ARRIVAL TO DFW. NUMEROUS CIRCUIT BREAKERS ARE PULLED PER QRH. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND ROW 6-9 OVERHEAD LIGHT OUT. REPLACED BALLAST PER AMM 33-20-10, CHECKS GOOD. RESET PULLED C/B'S.

Part: DOUBLER — CRACKED (BS 180) · airframe 56,926 hrs · 28,107 cycles

CRACK ON THE R1 DOOR FRAME PAN DRAIN HOLE DOUBLER AT BS 180. REMOVED AND REPLACED THE DOUBLER IAW DWG 51-00-05 AND DRAWING FDK 5825.

Part: STRAP — CRACKED (VERTICAL STAB) · airframe 56,926 hrs · 28,107 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CRACK IN VERTICAL STABILIZER LEADING EDGE SPAR CAP RIGHT SIDE AT VSS ZFS 52.267. REPAIRED IAW DRAWING SG09550005 AND EA#270718.

Part: SKIN — CORRODED (BS 1151) · corrosion level 2 · airframe 56,926 hrs · 28,107 cycles

CORROSION ON FUSELAGE SKIN UNDER DRAIN FLAPPER VALVE ASSEMBLY AT BS 1151, LONGERON 30R. REPAIRED IAW SRM 53-05-00-001 AND SRM 53-04-01.

Part: SKIN — CRACKED (BS 1418) · airframe 56,926 hrs · 28,107 cycles

SKIN CRACKED AT BS 1418 OTBD OF LONGERON 2R. REPAIRED IAW SRM 53-04-00-001.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 56,926 hrs · 28,107 cycles

CORROSION ON SEAT TRACK . REPAIRED IAW EA270742 AND 53-20-00-13.

Part: CUSP WEB — CORRODED (BS 1041) · corrosion level 2 · airframe 56,926 hrs · 28,107 cycles

CORROSION ON RIGHT CUSP WEB AT BS 1041. REPAIRED IAW 53-20-00-016.

Part: CUSP WEB — CORRODED (BS 370-389) · corrosion level 2 · airframe 56,926 hrs · 28,107 cycles

CORROSION ON FORWARD CABIN CUSP WEB BETWEEN BS 370 AND 389. REPAIRED IAW 53-20-00-16.

Part: SKIN — CRACKED (BS 1474) · airframe 56,926 hrs · 28,107 cycles

FUSELAGE SKIN CRACKED AT BS 1474, STRINGER 24R, 10TH FASTENER BELOW RAIN GUTTER END OF CRACK. REPAIRED IAW SRM 53-01-00 AND SRM 51-60-00.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 56,926 hrs · 28,107 cycles

SHEAR TIE CRACKED IN THE AFT ACCESSORY COMPARTMENT AT BS 1380, LONGERON 13R FORWARD SIDE. REPAIRED IAW 53-10-00-20.

Part: BEAM — CRACKED (BS 1309) · airframe 56,926 hrs · 28,107 cycles

AFT CARGO CEILING BEAM INTERCOSTAL IS CRACKED AT FUSELAGE STATION 1309, LBL30. REMOVED AND REPLACED THE BEAM IAW SRM 51-30-05, AND DRAWING 9936580.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 3 · airframe 56,926 hrs · 28,107 cycles

CORROSION ON THE RIGHT WING OTBD FLAP CENTER HINGE FITTING AT STUD ATTACH POINTS. REMOVED AND REPLACED THE HINGE FITTING IAW AMM 57-40-01-201.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 3 · airframe 56,926 hrs · 28,107 cycles

CORROSION ON THE LFT WING OTBD FLAP CENTER HINGE FITTING AT STUD ATTACH POINTS. REMOVED AND REPLACED HINGE FITTING IAW AMM 57-40-01-201.

Part: TRIM SYSTEM — OUT OF ADJUST (HORIZ STAB) · airframe 56,257 hrs · 27,703 cycles

AIRCRAFT WAS NOT GROUNDED. WHEN THROTTLES WERE ADVANCED FOR TAKE OFF A STABILIZER TAKE OFF WARNING WAS RECEIVED. TAKE OFF WAS ABORTED. CREW ADJUSTED STABILIZER TRIM. SUBSEQUENT TAKE OFF WAS UNEVENTFUL.

Part: INDICATOR — FALSE INDICATION (SLATS) · airframe 55,898 hrs · 27,474 cycles

THE AUTO SLAT FAIL LIGHT ILLUMINATED DURING TAKEOFF. FLIGHT LOW SPEED ABORT. CREW RECYCLED FLAPS AND SLATS AND FLIGHT CONTINUED. OPERATIONAL CHECKED GOOD.

Part: TARGET — OUT OF ADJUST (CARGO DOOR) · airframe 55,877 hrs · 27,461 cycles

MID CARGO DOOR LIGHT ILLUMINATED AT 65 KNOTS, ABORTED TAKEOFF. ADUSTED DOOR WARNING LIGHT TARGET TO MINIMUM GAP IAW AMM 52-70-02. OPERATINAL CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,674 hrs · 27,322 cycles

AIRCRAFT WAS NOT GROUNDED. WHILE ACCOMPLISHING WORK CARD 5403 EGRESS POWER SUPPLY AB5-3 FAILED TO TEST. REMOVED AND REPLACED POWER SUPPLY BATTERY PACK IAW AMM 33-60-98. SYSTEM CHECKS NORMAL.

Part: WARNING LIGHT — INTERMITTENT (ANTI ICE VALVE) · airframe 55,498 hrs · 27,200 cycles

DURING TAKE OFF ROLL, THE NR 1 ENGINE MASTER CAUTION AND ENGINE ANTI-ICE VALVE WARNING LIGHTS FLICKERED. THE AIRCRAFT WAS GROUNDED.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 54,764 hrs · 26,775 cycles

AIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL. DURING CLIMB THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. NR 2 ENGINE POWER REDUCED TO IDLE AND ACFT RETURNED TO FIELD. ENGINEERING REPORTS FAN BLADES WITH LEADING EDGE FOREIGN OBJECT DAMAGE CAUSED COMPRESSOR STALL.

Part: SUPPORT FITTING — CRACKED (CARGO DOOR) · airframe 54,474 hrs · 26,594 cycles

AIRCRAFT WAS IN BASE MX. FWD CARGO COMPARTMENT, MID DOOR, STOP SUPPORT FITTING, FWD SIDE OF DOOR & 2ND FROM TOP IS CRACKED. R & R STOP FITTING IAW DWG 5910141 & AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 50,736 hrs · 24,415 cycles

AFT CARGO DOOR STOP CRACKED. R & R DOOR STOP.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 50,736 hrs · 24,415 cycles

AFT CARGO DOOR STOP CRACKED. R & R DOOR STOP.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 50,726 hrs · 24,410 cycles

SKIN DAMAGE ON BOTTOM OF FUSELAGE JUST FWD OF AFT AIR STAIR FWD EDGE AT FUSELAGE STATION 1361. REPAIRED SKIN IAW SRM 53-01-00-001 & AAED 53-30-00-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,502 hrs · 24,287 cycles

WHEN ELEC POWER IS TURNED OFF, OVERHEAD AISLE LIGHTS FROM ROW 23 TO 30 COME ON ALONG WITH 2 OVERHEAD LIGHTS IN AFT GALLEY. R & R BATTERY PACK IAW AMM 33-53-00. SYSTEMS CHECKED NORMAL.

Part: APU — FAILED (APU BAY) · airframe 47,090 hrs · 22,519 cycles

DFW CREW REPORTED AUXILIARY POWER UNIT FAILED WITH AC CROSS TIE ON PLACARD. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUXILIARY POWER UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,679 hrs · 22,285 cycles

FUSELAGE SKIN DAMAGED BS 1463 BELOW SKATE ANGLE LT HAND SIDE. CUT OUT DAMAGED AREA & INSTALLED DOUBLER IAW SRM 53-01-00 FIGURE 2 SHEET 3 & SUPPORTING EA.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 46,679 hrs · 22,285 cycles

STRAP DOUBLER BLENDED OUT OF LIMITS. FABRICATED STRAP DOUBLER IAW AARD 51-00-00-1 & EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 46,679 hrs · 22,285 cycles

INNER FILLER SKIN DOUBLER CRACKED AT BS 1463 & LONGERON 3 LT. STOP DRILLED CRACK & DOUBLER INSTALLED IAW SRM 53-01-00 FIGURE 2 SHEET 3 & EA.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 46,679 hrs · 22,285 cycles

CORROSION ON FORWARD GALLEY MOUNT AT STATION 160 & RIGHT BUTTLINES 43 & 51. REPLACED GALLEY TIEDOWN FITTINGS IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,679 hrs · 22,285 cycles

LT CUSP AT STATION 698 CORRODED. INSTALLED DOUBLER AT STA 698 IAW AARD 53-20-00-16.

Part: DOOR FRAME — GOUGED (SERVICE DOOR) · airframe 46,679 hrs · 22,285 cycles

FORWARD SERVICE DOOR, GOUGES ON BOTTOM MAIN DOOR FRAME. REMOVED DAMAGE AND INSTALLED DOUBLER IAW EA COMP 52-030157.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,679 hrs · 22,285 cycles

RIGHT HAND CUSP HAS HOLE AT BS 876. REMOVED CORROSION & INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,679 hrs · 22,285 cycles

CORROSION ON CUSP UNDER NR 1 SEAT TRACK AT STA 1174. INSTALLED CUSP DOUBLER ON SEAT TRACK NR 1 FROM STATIONS 1174 TO 1177 IAW AARD 53-20-00-16.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 46,679 hrs · 22,285 cycles

FORWARD SERVICE DOOR, DOOR BEAM CRACKED AT LOWER DOOR HINGE MOUNT FITTING. INSTALLED DOUBLER IAW SRM 52-05-00, FIGURE 25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,679 hrs · 22,285 cycles

SEAT TRACK NR 6 FROM STA 855 TO 856 CORRODED. SEAT TRACK NR 6 FROM STA 855 TO 856 REPAIRED BY ROUTING OUT DAMAGED AREA AND INSTALLING SEAT TRACK PLUG IAW AARD 53-20-00-10 AND SRM 53-05-00, FIG 4A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,679 hrs · 22,285 cycles

RT CUSP SHEET CORRODED FROM STA 503 TO 579. REPLACED RT CUSP FROM STATIONS 503 TO 579 IAW AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 46,679 hrs · 22,285 cycles

NR 2 RT LONGERON CRACKED AT STA 1429. INSTALLED NEW LONGERON AND SPLICE IAW SRM 53-02-00.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 46,679 hrs · 22,285 cycles

RT CUSP AT STA 1163, OTBD SEAT TRACK NR 6 CORRODED. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,679 hrs · 22,285 cycles

CORROSION ON BOTTOM OF RIGHT HAND CUSP AT BS 487. REMOVED CORROSION AND INSTALLED DOUBLER IAW AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,679 hrs · 22,285 cycles

RT CUSP CORRODED AT STATION 1115, OTBD OF NR 6 SEAT TRACK. INSTALLED CUSP DOUBLER IAW AARD 53-20-00-16.

Part: MEMBRANE — DAMAGED (FUSELAGE) · airframe 46,679 hrs · 22,285 cycles

DAMAGE ON SUB-FLOOR AT BS 200 & 12 INCHES LT OF CENTERLINE. INSTALLED REPAIR DOUBLER IAW AARD 53-20-00-16.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,679 hrs · 22,285 cycles

WEB CRACKED AT BS 207 & LONGERON 15 LT. REMOVED DAMAGE & INSTALLED DOUBLER IAW 53-10-00-11.

Part: LIGHT — NOT SEATED (CABIN) · airframe 44,317 hrs · 21,081 cycles

RIGHT AND CENTER CEILING EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,317 hrs · 21,081 cycles

ESCAPE PATH LIGHTS AT SEAT 7D INOPERATIVE. REPLACED LAMP FOR ESCAPE PATH LIGHT AT SEAT 7D. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,317 hrs · 21,081 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM ROWS 7 TO 11. OPS CHECK NORMAL.

Part: SKIN — DENTED (TE FLAP) · airframe 43,615 hrs · 20,679 cycles

RIGHT INBOARD FLAP LOWER SURFACE HAS A SMOOTH DENT APPROXIMATELY 6 INCHES BY 9 INCHES BY 0.25 INCH DEEP. SPLICED IN NEW SECTION OF SKIN ON OUTBOARD END OF FLAP WEDGE PER EA MD8057-023631.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 43,297 hrs · 20,513 cycles

LIGHTNING STRIKE DAMAGE TO LEFT ELEVATOR TIP AND STATIC DISCHARGER BASE. REPAIRED LEFT HAND ELEVATOR TIP AND DISCHARGER BASE PER AARD 55-20-00-6 REPAIR 6 AND AARD 51-10-05 REPAIR 1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,979 hrs · 20,343 cycles

EMERGENCY EXIT SIGN LIGHT AT RIGHT FORWARD GALLEY AREA INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY B5-23 AND BATTERY PACK AB5-2. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,394 hrs · 20,050 cycles

OVERWING EMERGENCY EXIT DOOR LIGHT WILL NOT TEST. REPLACED BATTERY PACK FOR OVERWING EMERGENCY EXIT DOOR LIGHT. OPS CHECK NORMAL.

Part: GENERATOR — OVERTEMP (ZONE 400) · airframe 41,745 hrs · 19,734 cycles

DFW - CREW REPORTED RIGHT CONSTANT SPEED DRIVE OVERTEMP INDICATION WITH AUXILIARY POWER UNIT ON PLACARD. ACCOMPLISHED QRH PROCEDURE AND TURNED OFF THE RIGHT GENERATOR. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CONSTANT SPEED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TIRE — SEPARATED (RT MLG) · airframe 41,538 hrs · 19,620 cycles

DFW - CREW REPORTED RIGHT ENGINE COMPRESSOR STALLED AFTER TIRE TREAD INGESTION. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT DFW ON 07/19/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: NOSE CONE — DEFECTIVE (RT ENGINE) · airframe 38,281 hrs · 18,074 cycles

DFW - CREW REPORTED AUTOPILOT AND AUTO THROTTLE KICKED OFF AND BOTH ENGINES EXPERIENCED LOW EPR INDICATIONS. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE NOSE CONE ASSEMBLY AND TWO PT7 LINES ON LEFT ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FIRE LOOP — FAULTY (LT ENGINE) · airframe 37,701 hrs · 17,794 cycles

DFW - CREW REPORTED FIRE LOOP "B" LIGHT ILLUMINATED ON CLIMBOUT. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE LOWER BARRIER LOOP ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PROXIMITY SENSOR — FAILED (LANDING GEAR) · airframe 36,956 hrs · 17,456 cycles

CREW REPORTED GEAR DOOR OPEN LIGHT AFTER GEAR RETRACTION. NO RED LIGHTS. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR.

Part: VALVE — INOPERATIVE (FUEL SYSTEM) · airframe 35,304 hrs · 16,724 cycles

INFLIGHT DEN-DFW. LEFT GAUGE INDICATION SHOWED NO FUEL. EMERGENCY DECLARED LANDED AMA WITHOUT INCIDENT. FOUND CIRCUIT BREAKER POPPED, MAY HAVE BEEN TRANSFERRING FUEL FROM LEFT TO RIGHT TANK. REPLACED RIGHT FUELING VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,988 hrs · 16,592 cycles

DENT AT STATION 1304 ABOVE LONGERON 19R. BLENDED GOUGE, DYE CHECKED, NO CRACKS. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIGURE 38.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

CORROSION ON LEFT TIE DOWN TRACK SPLICE FROM STATION 1212-1231. REMOVED AND REPLACED TIE DOWN TRACK SPLICE PER IPC 25-52-00-03L.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,989 hrs · 16,592 cycles

DEAD BATTERY ON EMERGENCY LIGHTS. REMOVED AND REPLACED BATTERY PACK PER 33-50-00-12D.

Part: CARGO TRACK — CORRODED (CARGO TRACK) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

CORROSION ON AFT CARGO LEFT TIE DOWN TRACK FROM STATION 1212-1231. REMOVED AND REPLACED TIE DOWN TRACK PER 25-52-00-03L.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

CORROSION ON LEFT TIE DOWN TRACK FROM STATION 1085-1155. REMOVED AND REPLACED LEFT TIE DOWN TRACK PER 53-24-00.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

CORROSION ON FRAME AT STATION 1309 BETWEEN LONGERONS 28R AND 28L. REMOVED CORRODED FRAME AND INSTALLED FRAME SPLICE REPAIR PER SRM 53-03-00 FIGURE 2A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,989 hrs · 16,592 cycles

ANGLE CRACKED OUTBOARD OF RUDDER ACTUATOR ROD END AT THE STATION 1510 CANTED FRAME. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-01 AND IPC 53-14-04.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

RIGHT CUSP HAS CORROSION AT STATION 1160. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

CORROSION ON LEFT CUSP BETWEEN STATION 560-579. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

CORROSION ON RIGHT CUSP AT STATION 530. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,988 hrs · 16,592 cycles

LONGERON 20R AT STATION 1003 CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER EA MD80-53-005631.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

MID CARGO DOOR BEAM HAS CORROSION BETWEEN STATIONS 653 AND 681. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: WEB — GOUGED (NLG WW) · airframe 34,989 hrs · 16,592 cycles

WEB AT NOSE LANDING GEAR JAMB BEAM IS GOUGED AND BENT. INSTALLED DOUBLER PER AARD 53-10-00-4.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

MID CARGO DOOR BEAM VERTICAL LEG CORRODED FROM STATIONS 642-653. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

MID CARGO DOOR BEAM CORRODED ON THE VERTICAL LEG AT STATION 681. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

CORROSION ON NR 2 SEAT TRACK FROM STATION 1108-1309. INSTALLED NEW NR 2 SEAT TRACK PER SRM 53-05.

Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

INBOARD FACE OF OUTBOARD BORE ON LEFT MAIN LANDING GEAR RETRACT ACTUATOR FITTING IS CORRODED. REMOVED CORROSION AND REWORKED FITTING PER EA MD80 57-00-5663 DATED 03/01/09.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

SEAT TRACK NR 6 CORRODED FROM STATION 1212-1216. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 34,988 hrs · 16,592 cycles

UPPER ANGLE INSIDE AFT CARGO DOOR AT HINGE IS CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 52-03-00.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,989 hrs · 16,592 cycles

RIGHT CUSP CRACKED AT STATION 840. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 34,988 hrs · 16,592 cycles

LONGERON 2L CRACKED AT STATION 1418. INSTALLED LONGERON REPAIR SPLICE PER AARD 53-30-00-2 FIGURE 1.

Part: RIB — CRACKED (LE SLAT) · airframe 34,989 hrs · 16,592 cycles

LEFT NR 5 SLAT OUTBOARD RIB CRACKED IN RADIUS. REPLACED OUTBOARD RIB PER ESO 80117.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,988 hrs · 16,592 cycles

CORROSION ON SEAT TRACK NR 6 FROM STATION 1183-1188. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

SEAT TRACK NR 6 CORRODED BETWEEN STATIONS 1207-1208. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

LEFT CUSP CORRODED BETWEEN STATIONS 930-935. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

CORROSION ON RIGHT CUSP BETWEEN STATIONS 541 AND 560. INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

LEFT CUSP CORRODED AT STATION 1155, 5 INCHES OUTBOARD OF NR 2 SEAT TRACK. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 34,988 hrs · 16,592 cycles

RIGHT CUSP CRACKED AT STATION 997. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,988 hrs · 16,592 cycles

CORROSION ON NR 6 SEAT TRACK FROM STATION 1193-1198. INSTALLED SEAT TRACK PLUG PER SRM 53-05-00 FIGURE 4A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

RIGHT CUSP CORRODED BETWEEN STATION 886 AND 905. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,989 hrs · 16,592 cycles

DENT AT STATION 1304 ABOVE LONGERON 19R. INSTALLED INTERNAL DOUBLER PER SRM 53-04-00 FIGURE 38.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

RIGHT CUSP CORRODED AT STATION 602. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

LEFT CUSP CORRODED BETWEEN STATIONS 845-864. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

RIGHT CUSP CORRODED AT STATION 920. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,989 hrs · 16,592 cycles

LEFT CUSP CORRODED STATION 630-632. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 34,989 hrs · 16,592 cycles

FORWARD CARGO DOOR NR 3 BEAM STOP PAD FITTING CRACKED ON THE FORWARD END. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 34,989 hrs · 16,592 cycles

MID CARGO DOOR NR 5 BEAM DOOR STOP FITTING FORWARD END CRACKED. REMOVED AND REPLACED DOOR STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 34,989 hrs · 16,592 cycles

MID CARGO DOOR NR 4 BEAM STOP FITTING CRACKED AT THE FORWARD END. REMOVED AND REPLACED DOOR STOP FITTING PER ESO 80174.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 34,989 hrs · 16,592 cycles

MID CARGO DOOR NR 2 BEAM STOP FITTING CRACKED AT FORWARD END. REMOVED AND REPLACED STOP FITTING PER ESO 80174.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHT AT AFT OVERWING EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,737 hrs

LGA - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: O-RING — LEAKING (RT ENGINE)

STL - DURING CLIMB, RIGHT HAND ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. RIGHT ENGINE OIL QUANTITY DROPPED TO ZERO. CREW SHUT DOWN RIGHT ENGINE. WINDMILL TIME WITH ZERO OIL PRESSURE 10 MINUTES. LANDED STL WITHOUT INCIDENT. FOUND BLOWN FILTER O-RING IN GEARBOX. REPLACED NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - CEILING EMERGENCY LIGHTS AT SEATS 30DEF INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 30DEF FOR INOPERATIVE CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: VALVE — INOPERATIVE (APU)

DEN INFLT T887/09 SEPT SEVERAL MINUTES AFTER ENGINE WAS ON WING ICE, SMOKE WAS PRESENT IN COCKPIT AND CABIN. DIVERTED TO DEN AND LANDED WITHOUT INCIDENT. TURNED ANTI ICE ON AGAIN AND SMOKE REAPPEARED. PRESSURE ABNORMAL LIGHT ILLUMINATED. REPLACED ANTI ICE PRESSURE REGULATING AND SHUT OFF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BNA - EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY ESCAPE LIGHT IN CEILING ABOVE SEAT ROWS 28 AND 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY ESCAPE LIGHT IN CEILING ABOVE SEAT ROWS 28 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, OBSERVED EMERGENCY LIGHT INOPERATIVE AT AFT SERVICE DOOR. SECURED DISLODGED BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING OVERNIGHT MAINTENANCE, FORWARD LEFT TAIL COMPARTMENT EMERGENCY EXIT LIGHTING SIGN INOPERATIVE. REPLACED FORWARD LEFT TAIL COMPARTMENT EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 17,050 hrs · 8,848 cycles

THE FLOOR EGRESS LIGHTS WERE INOPERATIVE FROM ROW 27 TO 30. RESEATED THE ELECTRICAL CONNECTOR AT ROW 30. CHECK-C 3-1-02 STL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 16,084 hrs · 8,308 cycles

THE EGRESS LIGHTS WERE INOPERATIVE FROM SEAT ROW 26 TO 28. REPLACED LAMP MODULE ASSEMBLY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,378 hrs · 7,261 cycles

DURING PREFLIGHT THE FIRST CLASS EGRESS LIGHTS FLASHED DURING TEST. THEY DID NOT REMAIN ON. REPLACED THE BATTERIES IN THE POWER SUPPLY.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 12,283 hrs · 6,110 cycles

DURING CHECK-C MAINT IN THE LT MAIN GEAR WELL, THE FWD INBOARD CORNER OF THE LT GEAR WELL DOOR FRAME WAS CRACKED. STOP DRILLED CRACK AND INSTALLED 2 DOUBLERS PER SRM 53-01, FIG 2 SHEET 4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,174 hrs · 6,050 cycles

THE EGRESS FLOOR PATH LIGHT WAS INOPERATIVE BETWEEN ROWS 21 AND 22. REPLACED THE LIGHT MODULE. CHECK-C 4-21-00 STL.

Part: WIRE — DAMAGED (ROW 21) · airframe 10,752 hrs · 5,341 cycles

IN FLIGHT A PASSENGER BAG DAMAGED THE EGRESS LIGHT NEAR SEAT 21D. REPLACED THE EGRESS FLOOR TRACK WIRING AND LAMP BASES. CHECK-C 4-21-00 STL.

Part: PRESSURE SWITCH — LEAKING (RT ENGINE OIL) · airframe 9,397 hrs · 4,589 cycles

ON PUSHBACK STARTED RT ENGINE, WHEN STABILIZED TURNED ON RT AIR CONDITIONING PACK AND RT ENG EGT BEGIN TO CLIMB NOTICED HOT SMELL IN CABIN THEN SMOKE REPORTED. REPLACED APU OIL PRESSURE SWITCH DUE TO OIL LEAK. AC10 03-14-00 JFK.

Part: LIGHT — INOPERATIVE (CABIN DOOR) · airframe 9,122 hrs · 4,423 cycles

THE LT SIDE NUMBER 1 CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. CHECK-C 5-6-99 STL.

Part: LIGHT — LOOSE (ROW 7)

DURING LANDING, SECTION OF EGRESS LIGHTS AT ROW 7 APPEARED TO BE LOOSE. REPLACED LIGHT SECTION. AC07 7-27-99 JFK.

Part: LIGHT — WORN (CABIN)

THE EGRESS LIGHTS WERE INOPERATIVE AT CABIN ROWS 3 TO 6, ROWS 21 TO 24, AND ROW 30. REPLACED THE LIGHT STRIP AT EACH LOCATION, (P/N 0105606-005) FOR ROW 3 TO 6, AND (P/N 0105606-004) AT EACH OF THE OTHER TWO LOCATIONS. CHECK-C 5-6-99 STL.

Part: BULB — LOOSE (ROW 22-24)

THE EGRESS LIGHTS WERE INOPERATIVE AT FWD END OF FIRST CLASS, AND AT CABIN ROWS 22, 23, AND 24. AT FWD END OF FIRST CLASS SECURED LAMP IN THE SOCKET. FOR AFT CABIN SECURED CONNECTOR AT ROW 24. CHECK-C 6-7-98 MCI.

Part: BULB — FAILED (ROW 22)

THE EGRESS LIGHT AT CABIN ROW 22 WOULD NOT LIGHT AND LENS WAS BROKEN. REPLACED THE LAMP AND LENS.

Part: WIRE — BROKEN (ROW 22-29)

FOUND EGRESS LIGHTS OUT ON FLOOR ROWS 22 TO 29. REPAIRED BROKEN WIRE.

Part: LIGHT — INOPERATIVE (CABIN)

STL - FLT 201 - TWO SECTIONS OF EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE TWO LAMP MODULE ASSEMBLES. CHECK-C 6-7-98 STL. (X)

Part: COMP BLADES — FRACTURED (LT ENGINE)

SEA - FLT 30 - CLIMBING OUT, LEFT ENGINE HAD COMPRESSOR STALL AT 5000 FT AND ANOTHER AT 7000 FT. EGT JUMPED 40 TO 50 DEGREES HIGHER THAN RT ENGINE. RETURNED TO SEA. FOUND METAL IN TAIL PIPE. CHANGED THE ENGINE. DURING ENGINE TEAR DOWN FOUND SEVEN EACH NINTH STAGE COMPRESSOR BLADES FRACTURED. MISSING BLADES AND DAMAGE TO THE OTHER STAGES CAUSED HIGH PRESSURE COMPRESSOR STALLS. BLADES MFG PART NR 798209 AND 809809. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

LGA - FLT 427 - DURING TAKEOFF ROLL, WHEEL-NOT-TURNING LIGHT ILLUMINATED. ABORTED TAKEOFF AT 60 KNOTS. PERFORMED CHECK OF BRAKE AND ANTI-SKID SYSTEMS. OPS NORMAL. PLACARDED LIGHT INDICATION PER MEDP 32-12. NEW AIRCRAFT. (X)