N9404V

Part: CASTING — CRACKED (LT WING) · airframe 64,264 hrs · 31,351 cycles

LEFT WING GND SPOILER ACTUATOR SUPPORT CASTING CRACKED. COMPLETED REPLACEMENT OF GND SPOILER CASTING IAW SRM 51-01-00-001.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,264 hrs · 31,351 cycles

FUSELAGE FRAME AT STATION 37, BULKHEAD IS CRACKED AT LT LOWER RADOME ALIGNMENT PIN LOCATION. INSTALLED DOUBLER REPAIR IAW AARD 53-10-00 REPAIR 19.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 64,264 hrs · 31,351 cycles

FORWARD CARGO DOOR STOP FITTING CRACKED, FWD SIDE OF DOOR, 2ND FROM BOTTOM. R & R FITTING IAW AARD 51-00-05-1, DWG 5910141 & DWG CDK2345.

Part: FUEL CONTROL — FAULTED (LT ENGINE) · airframe 63,658 hrs · 31,003 cycles

DURING TAKEOFF, LT ENGINE EPR INDICATION WAS ERRATIC. TAKEOFF ABORTED AT APPROXIMATELY 70 KNOTS. R & R FUEL FLOW CONTROL IAW CARD 73-91-99 & ENG FUEL PUMP IAW CARD 73-94-03. ACCOMPLISHED ENG PARAMETERS CHECK IAW CARD 71-91-20. SYS CHECKED NORMAL.

Part: PROBE — LEAKING (LT ENGINE) · airframe 63,649 hrs · 30,997 cycles

DURING MAX TAKEOFF ROLL WHEN AUTO THROTTLE ENGAGED THE LT ENG, EPR DROPPED BACK & EGT STARTED CLIMBING TO MAX LIMIT. TAKEOFF ABORTED AT 60 TO 70 KNOTS. FOUND PROBE AT 7 O`CLOCK POSITION ON LT ENG LEAKING. R & R PROBE IAW AMM 77-11-04.

Part: RELAY — FAULTY (BRAKE) · airframe 63,496 hrs · 30,905 cycles

DURING TAKEOFF ROLL CAPTAIN`S ATT & HDR FAIL LIGHTS ILLUMINATED. RETURNED TO NORMAL WHEN EFIS SWITCHED TO ON 2. DURING FLIGHT THE TRIM SWITCHES ON BOTH YOKES WOULDN`T TRIM WHEN PUSHED FWD. BOTH CONSOLE & ALT TRIM WORKED OK. R & R LONGITUDINAL TRIM BRAKE RELAY IAW AMM 27-20-03 WITH GOOD OPERATIONAL CHECKS.

Part: GENERATOR — FAULTY (LT ENGINE) · airframe 61,798 hrs · 30,006 cycles

LEFT CONSTANT SPEED DRIVE OIL TEMP RISING WITH APU ON PLACARD. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG CONSTANT SPEED DRIVE & GEN. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,613 hrs · 27,262 cycles

EMPENNAGE EXIT LIGHTS ILLUMINATED ON EXTERIOR OF FUSELAGE WITH EMERGENCY LIGHT SWITCH IN OFF POSITION. RECHARGED EXTERIOR EMERGENCY LIGHTS BATTERY. OPS CHECK NORMAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,445 hrs · 27,176 cycles

RIGHT CUSP FROM STATIONS 1174 TO 1185 CORRODED. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 56,445 hrs · 27,176 cycles

GUSSET AT FORWARD ENTRY DOOR FRAME AFT SIDE AT LONGERON 2 LEFT CRACKED. INSTALLED DOUBLER REPAIR PER AARD 53-10-00-11.

Part: DRAIN PAN — CORRODED (GALLEY) · corrosion level 2 · airframe 56,445 hrs · 27,176 cycles

G1 GALLEY DRAIN PAN CORRODED. REPLACED G1 GALLEY DRAIN PAN.

Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 56,445 hrs · 27,176 cycles

DOUBLER AT STATION 229 ABOVE LONGERON 18 LEFT INOPERATIVE. INSTALLED DOUBLER REPAIR PER SRM 53-04-05 FIGURE 2 SHEET 1.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,445 hrs · 27,176 cycles

LEFT CUSP AT STATION 759 CRACKED. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,445 hrs · 27,176 cycles

CORROSION ON BOTTOM SIDE OF RIGHT CUSP AT STATION 1180. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 56,445 hrs · 27,176 cycles

WEAR ON THE LOWER SIDE OF THE CABIN FLOORBEAM AT STATION 674. INSTALLED ANGLE DOUBLER ON LOWER SIDE OF FLOORBEAM AT STATION 674 PER AARD 53-20-00-21.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 56,445 hrs · 27,176 cycles

CORROSION ON THE ALTIMETER ANTENNA LANDING AT STATION 719 LONGERON 30 LEFT. INSTALLED NEW RADIO ALTIMETER MOUNTING DOUBLER AT STATION 719 LONGERON 30 TO 29 LEFT PER BOEING PRINT 5911412.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 56,445 hrs · 27,176 cycles

LEFT CUSP CRACKED AT STATION 1244. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,445 hrs · 27,176 cycles

DENT WITH BLEND ON FUSELAGE 221 BETWEEN LONGERONS 4 AND 5 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,445 hrs · 27,176 cycles

TWO DENTS IN FUSELAGE SKIN AT STATION 304 ABOVE AND BELOW LONGERON 24 LEFT. REMOVED DAMAGED AND INSTALLED REPAIR DOUBLER, FILLER AND FINGERS PER SRM 53-04-03.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,445 hrs · 27,176 cycles

LEFT FUSELAGE SKIN CRACKED AT LEFT NOSE LANDING GEAR STRUT DOOR AFT HINGE CUTOUT. STOP DRILLED CRACK AND INSTALLED EXTERNAL DOUBLER PER SRM 53-05-00, FIGURE 62.

Part: CONTROL VALVE — INOPERATIVE (AC BAY) · airframe 55,259 hrs · 26,545 cycles

DFW - CREW REPORTED PRESSURIZATION ISSUES ON CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT AND PACK FLOW CONTROL VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,460 hrs · 26,151 cycles

CEILING EMERGENCY LIGHTS BY FORWARD LAVATORY INOPERATIVE. REPLACED EMERGENCY BATTERY PACK. OPS CHECKS NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 54,460 hrs · 26,151 cycles

LEFT AND RIGHT FORWARD OVERWING DOOR UPPER EXIT SIGNS INOPERATIVE. RESEATED BATTERY PACK. OPS CHECKS NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 54,460 hrs · 26,151 cycles

LEFT AND RIGHT AFT OVERWING DOOR UPPER EXIT SIGN INOPERATIVE. RESEATED BATTERY PACK. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,460 hrs · 26,151 cycles

FORWARD PORTABLE EMERGENCY LIGHT BY LEFT NUMBER 1 DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 54,460 hrs · 26,151 cycles

CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 26 INOPERATIVE. RESEATED BATTERY PACK. OPS CHECK NORMAL.

Part: ENGINE — FAILED (RIGHT) · airframe 53,801 hrs · 25,820 cycles

RIC - INFLIGHT PHL-DFW. CREW REPORTED RIGHT ENGINE POWER LOSS FOLLOWED BY UNCOMMANDED ENGINE SHUTDOWN (SINGLE ENGINE TIME 1 MINUTE). EMERGENCY DECLARED FLIGHT DIVERTED RIC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT RIC ON 09/09/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DUCT — CRACKED (AC BAY) · airframe 53,161 hrs · 25,470 cycles

DFW - (REPEAT ITEM) CREW REPORTED AFTER TAKEOFF TAIL COMPARTMENT TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED QRH CHECKLIST AND LIGHT EXTINGUISHED AFTER ONE MINUTE. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED 8TH AND 13TH STAGE MIXING DUCT THAT WAS CRACKED AT WELD. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PERISEAL — LEAKING (AC BAY) · airframe 53,160 hrs · 25,467 cycles

DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. FOLLOWED QRH PROCEDURE AND LIGHT EXTINGUISHED AFTER FOUR SECONDS. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND DUCT PERI SEALS TO PRIMARY HEAT EXCHANGER LEAKING AND PNEAMATIC AIR CONTROL THERMOSTAT LEAKING. REPLACED PERI SEALS, THERMOSTAT AND SECURED CLAMPS FROM AIR CYCLE MACHINE TO HEAT EXCHANGER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 52,718 hrs · 25,254 cycles

AFT OF LONGERON 2 LEFT SHEAR TIE CRACK STATION CANT FRAME 1451. INSTALLED SHEAR TIE PER SRM 51-30-05.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 52,718 hrs · 25,254 cycles

ENTRY DOOR SKIN DAMAGED ON BOTTOM FORWARD CORNER OF DOOR. INSTALLED DOUBLER REPAIR PER ESO 80172.

Part: REGULATOR VALVE — INOPERATIVE (ANTI-ICE SYSTEM) · airframe 52,094 hrs · 24,962 cycles

STL - INFLIGHT PSP-ORD CREW REPORTED AIRFOIL ANTI-ICE ABNORMAL INDICATIONS. FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ICE PROTECTION PRESSURE REGULATING VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SWITCH — FAULTY (OIL SYSTEM) · airframe 49,389 hrs · 23,694 cycles

ELP - INFLIGHT DFW-SJD. CREW REPORTED RIGHT ENGINE OIL STRAINER BYPASS LIGHT ILLUMINATED. EMERGENCY DECLARED DIVERTED ELP LANDED WITHOUT INCIDENT. INSPECTED OIL FILTER WITH NO FINDINGS. REPLACED RIGHT ENGINE OIL STRAINER CLOG SWITCH. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,817 hrs · 23,452 cycles

CANTED FRAME 1474 CRACKED AT ELEVATOR ACCUMULATOR SUPPORT BRACKET FASTENERS. DOUBLER INSTALLED PER AARD 53-10-00-15.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,430 hrs · 23,273 cycles

CEILING EMERGENCY LIGHTS AT ROW 10 INOP DURING TEST AFTER A/C POWER OFF FOR MORE THAN 24 HOURS. REPLACED BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,430 hrs · 23,273 cycles

PORTABLE EMERGENCY LIGHT ASSY AT L1 DOOR DOES NOT LIGHT DURING TEST. REPLACED LIGHT ASSY.

Part: HORN — INOPERATIVE (FIRE DETECTION) · airframe 47,657 hrs

LGA FOUND AUXILIARY POWER UNIT FIRE DETECTION HORN INOPERATIVE. REPLACED FOUND AUXILIARY POWER UNIT FIRE DETECTION HORN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,657 hrs

LGA - FORWARD CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMP FOR FORWARD CEILING EMERGENCY LIGHTS.

Part: CONNECTOR — SHORTED (FIRE DETECTOR) · airframe 47,223 hrs · 22,733 cycles

ORD ON LANDING AFT CARGO FIRE LIGHT ILLUMINATED. LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED SHORTED CONNECTOR PLUG. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 46,561 hrs

SFX - LENS AT SEAT 8D BROKEN. REPLACED LENS AT SEAT 8D.

Part: LAMP — BROKEN (EMERGENCY LIGHTS) · airframe 46,561 hrs

SFX - EMERGENCY LIGHTS AT SEAT 8D INOPERATIVE. REPLACED LAMP AT SEAT 8D.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW- EMERGENCY LIGHTS AT ROW 25 REMAIN ON WITH BATTERY OFF AND POWER TO AIRCRAFT OFF. REPLACED BATTERY PACK AT ROW 25.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 45,881 hrs

LGA - OVERHEAD EMERGENCY EXIT LIGHT AT FIRST CLASS LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ROTOR — SEIZED (NR 1 ENGINE) · airframe 45,567 hrs

ORD INFLIGHT T779/20SEP. AT APPROX 2000 FEET NR 1 ENGINE LOST ALL POWER. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE ON 20 SEP AT ORD DUE TO ROTOR SEIZED. SYSTEM GROUND CHECKED NORMAL OPS.

Part: TRANSDUCER — INOPERATIVE (NR 3 WHEEL)

STL INFLIGHT T1603/17SEP - AT 120 KNOTS DURING TAKEOFF WHEEL NOT TURNING INDICATION ILLUMINATED. ABORTED TAKEOFF. REPLACED NUMBER THREE WHEEL TRANSDUCER ADAPTER AND TRANSDUCER. REPLACED NUMBER THREE AND FOUR TIRES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

LGA EMERGENCY LIGHT IN AFT TAIL COMPARTMENT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT IN AFT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS FROM ROW 3 TO 19 FLICKER. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS AT ROWS 3 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FORWARD RIGHT HAND EMERGENCY EXIT LIGHT IDENTIFIER INOPERATIVE. REPLACED BATTERY PACK/CHARGER FOR FORWARD RIGHT HAND EMERGENCY EXIT LIGHT IDENTIFIER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 31,693 hrs · 15,987 cycles

THE AFT CABIN EGRESS LIGHTING WAS INOPERATIVE. REPAIRED DAMAGED FLOOR CONNECTION AND RESEATED BATTERIES IN THE POWER SUPPLY. CHECK-C 9-15-03 MCI.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,905 hrs · 14,325 cycles

THE EMERGENCY LIGHT IN UPPER RIGHT SIDE OF TAIL CONE, AND THE EMERGENCY LIGHT IN THE MID GALLEY, WERE BOTH INOPERATIVE. REPLACED THE BATTERY PACK FOR EACH OF THEM.

Part: BATTERY PACK · airframe 26,455 hrs · 12,875 cycles

THE AFT OVERWING EXIT LIGHT WAS INOPERATIVE ON TEST. REPLACED THE BATTERY PACK. CHECK-C 1-22-01 MCI. --CLOSED--

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT COROSION WAS AROUND SCREW HOLES ON LT TIE DOWN TRACK FROM STA 1212 TO 1320R. INSTALLED NEW TRACK PER SRM 51-30-0.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT FOUND CORROSION ON TIE DOWN TRACK LT STA 1081 TO 1219. REPLACED TRACK AT STA 1087 TO 1222 LT PER SRM 51-30-0.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT BETWEEN STA 160 AND 200, 53 INCHES RBL. FABRICATED NEW TRACK AND INSTALLED PER SRM 51-30-2. TREATED PART PER SRM 51-10-3.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT FLOOR SUPPORT WAS CORRODED AT STA 1155, LONGERON 29R TO 28L. INSTALLED NEW FLOOR SUPPORT PER SRM 51-30-5.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, FOUND DOUBLER CORRODED AT DOOR JAMB STA 1193, LONGERON 28R TO 29R. FABRICATED NEW DOUBLER AND INSTALLED AND PAINTED PER SPM 6-70-01 AND SRM 51-10-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT IN AFT CARGO COMPT FLOOR SUPPORT BRACE WAS CORRODED AT STA 1155 TO 1212, LONGERON 29R, AND AT STA 1212 LONGERON 29R TO 28L TOP AND BOTTOM. REPLACED BOTH SUPPORTS REF IPC 25-52-00 FIG 3L.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT FLOOR SUPPORT AT STA 153 RBL 44 INCHES, AND STA 160 RBL 45 INCHES, WAS CORRODED. FABRICATED NEW TRACK AND INSTALLED PER SRM 51-30-2. TREATED PER SRM 51-10-3.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT FOUND TIE DOWN TRACK CORRODED AT STA 1219 TO 1320, LT SIDE AFT CARGO BIN. REPLACED TRACK PER SRM 53-01 PAGE 4.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT IN THE AFT CARGO COMPT, CORROSION WAS ON LOWER DOOR JAMB AT STA 1155 TO 1212. INSTALLED NEW BEAM PER DOUGLAS PRINT 5930483.

Part: WEB — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT MEMBRANE BETWEEN STA 1271 AND 1309 AT STRINGER 18R WAS CRACKED AND CORRODED. CLEANED LIGHT CORROSION PER SPM 6-80-01 AND SRM 51-10-03. TREATED AND INSTALLED MEMBRANE REPAIR PER SRM 53-05, FIG 96.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT CORROSION WAS FOUND ON THE AFT CARGO DOOR JAMB CORNER SUPPORT AT STA 1155 LONGERON 28R, AND STA 1212 LONGERON 28R. REPLACED DOOR JAM CORNER SUPPORTS PER SRM 51-01, PAGE 1 ITEM C.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT FOUND CRACK AT CANT STA 1463 AND SUPPORT ANGLE AT TOP OF PYLON AND LEFT AFT FUSELAGE. ACCOMP HIGH FREQ EDDY CURRENT PER 51-00-01 PART 6 AND FOUND CRACK CONTAINED AT STOP DRILLED HOLES. REPAIRED PER SRM 54-04 FIG 10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT FOUND CORROSION AND WEAR ON CHAIR TRACK NUMBER 4, RBL 22 INCHES AND STA 807 TO 1022. REPLACED CHAIR TRACK PER SPM 6-70-01.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT FOUND CORROSION AT ATTACH HOLES FOR FUSELAGE FILLET AREA, BENEATH RUB STRIP AT STA 1104 TO 1136, LOWER LT SIDE. REMOVED CORROSION FROM ATTACH HOLES PER SPM 6-10-01. REPAIR MATERIAL LOSS PER PART 1-51-04-00 MARKED ON SKIN.

Part: WEB — CRACKED (AFT PAX DOOR) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT IN AFT ENTRY DOOR FOUND CRACK IN WEB ON RT OUTBOARD BOTTOM PORTION OF DOOR, APPROX 12 INCHES FROM BOTTOM OF DOOR. REPAIRED WEB PER SRM 51-70-4 FIG 2. INSTALLED STACK DOUBLER PER 52-61 FIG 2. TREATED AREA PER 51-10-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT AT STA 1231, LONGERON 29R TO 28L, FORMER HAD CORROSION ON AFT SIDE. CUT OUT DAMAGED FORMER AND SPLICED IN NEW PART PER SRM 53-03, PAGE 4C.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT, SEAT TRACK WAS CORRODED FROM STA 1032 TO 1122, LBL 44 INCHES. CUT OUT CORRODED TRACK SECTION AND SPLICED IN NEW SECTION OF TRACK PER SRM 53-05, FIG 4F.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT, FOUND FLOOR SUPPORT CORRODED AT STA 187 TO 194, RBL 6 TO 9. INSTALLED NEW FLOOR SUPPORT PER SRM 51-01.

Part: FAIRING — CRACKED (RUDDER) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT, FOUND 2 INCH BREAK IN RUDDER LEADING EDGE WRAP AROUND FAIRING ON RT SIDE, 60 INCHES DOWN FROM TOP. REPAIRED PER SRM 51-70-1A.

Part: WEB — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON BOTTOM OF FLOOR MEMBRANE, STA 671 AND LBL 57. REPAIRED MEMBRANE PER SRM 51-70-4.

Part: WEB — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE AT LONGERON 18R, STATION 1060 AND 1079. REPAIRED FLOOR MEMBRANE PER SRM 51-70-4.

Part: STOP — CORRODED (PAX DOOR) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT, FOUND ON THE AFT PASSENGER DOOR TWO STOPS AT THE BOTTOM OF THE DOOR HAD EXFOLIATION CORROSION DELAMINATING MATERIAL. REMOVED DAMAGED STOPS AT BOTTOM AFT PASSENGER DOOR. REPLACED BOTH ANGLES PER SPM 6-70-01.

Part: WEB — CRACKED (CABIN) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT FLOOR MEMBRANE WAS CRACKED AT LT SIDEWALL, STA 1298 TO 1304. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01, FIG 2. TREATED SURFACE PER SRM 51-10-03. INSTALLED HI-LOKS IN DOUBLER DUE TO ACCESS PER SRM 53-30-05. INSTALLED RIVETS PER SRM 51-30-2.

Part: WEB — CRACKED (CABIN FLOOR) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT, FOUND AFT CABIN FLOOR MEMBRANE CRACKED AT LT SIDEWELL, STA 1298 TO 1304. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01, FIG 2. TREATED SURFACE PER SRM 51-10-3. INSTALLED HI-LOK''S IN DOUBLER DUE TO ACCESS PER SRM 53-30-05. INSTALLED RIVETS PER SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 1155, BETWEEN LONGERON 28R AND 29R. INSTALLED NEW FLOOR SUPPORT PER SRM 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,647 hrs · 11,910 cycles

DURING CHECK-C MAINT A CLASS III LIMITED TIME REPAIR WAS FOUND INSTALLED, STA 256, ABOVE CUSP ON LT SIDE. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, AND NO CRACKS FOUND. INSTALLED DOUBLER PER SRM 53-04, FIG 38, SHEET 32. ---CLOSED---

Part: LIGHT — MALFUNCTIONED (LT OVERWING) · airframe 23,433 hrs · 11,229 cycles

DURING ROUTINE INSPECTION, FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHT VERY DIM. REPLACED LIGHT ASSEMBLY. AC03 5-12-00 JFK.

Part: BATTERY — DISCHARGED (ROW 29DEF)

DURING PREFLIGHT THE CABIN EGRESS LIGHTS WERE INOP AT ROW 29 D/E/F AND TAIL CONE EMERGENCY LIGHTS. INSTALLED A NEW MODULE AND INSTALLED NEW BATTERY.

Part: LAMP — FAILED (CABIN)

FOUND EMERGENCY EGRESS LIGHTS INOPERATIVE AT SEAT ROWS 23, 24, 26 AND 29. REPLACED LAMP AT EACH LOCATION. CHECK-C 11-20-98 STL.

Part: COVER — MISSING (CABIN)

FOUND EGRESS LIGHT COVER MISSING. REPLACED COVER AND LAMP, (P/N 7732). CHECK-C 11-12-98 STL.

Part: CIRCUIT BREAKER — TRIPPED (CABIN)

MCI - DURING OVERNIGHT MAINTENANCE, THE FIRST CLASS EGRESS LIGHTS WERE FOUND INOPERATIVE. RESET CIRCUIT BREAKER. CHECK-C 1-31-98 LAX. (M)

Part: SKIN — DENTED (BS 232)

MCI - DURING C-CHECK, FOUND LEFT FORWARD SKIN AT BS 232, LONGERON 18L, HAD DENT .75 INCH BY 1.375 INCH BY .143 IN DEEP. INSTALLED EXTERNAL DOUBLER REPAIR PER ARA 11483. (M)

Part: ENGINE — FAILED (LEFT)

JFK - FLT 1315 - DURING CRUISE, FL 31,000. LEFT ENGINE, SN 3210, SHUT DOWN WITH NO WARNING, WITH HIGH EGT OBSERVED. CHANGED ENGINE. ENGINE TOTAL TIME: 38,114 HOURS; 19,531 CYCLES. CHECK C-1D - 12-22-96 - JFK. (X)

Part: COMPRESSOR — STALL (NR 1 ENG)

SFO - DURING CLIMB NR 1 ENGINE, S/N 3210, EXPERIENCE A COMPRESSOR STALL AND VIBRATION. SHUT DOWN ENGINE. CHECKED ENGINE INLET AND EXHAUST, BORESCOPE OF 6TH AND 7TH STAGE COMPRESSOR, CHECKED 8TH AND 16TH STAGE BLEED AIR DUCT END CAPS, CHECKED ALL MAGNET CHIP DETECTORS AND OIL FILTER. ALL CHECKS WERE NORMAL. ENGINE PERFORMANCE RUNUP CHECKED NORMAL. (M)

Part: STRUT — REQUIRED SERVICE (NLG)

STL - FLT 39 - AFTER TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT ON LANDING GEAR RETRACTION. CYCLED LANDING GEAR. FOUND NLG AIR CHARGE DEPLETED. SERVICED NLG WITH OIL AND NITROGEN. NLG LEAK CHECKED AND OPERATION CHECKED NORMAL. CHECK C-2D - 12-4-95 - JFK.