N618DL

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 92,455 hrs · 44,988 cycles

PASSING 90 KTS ON T/O ROLL, RECEIVED A CABIN AUTO INOP EICAS MSG AND CABIN ALT AUTO 1 AND 2 STATUS MSG. ALSO, AFT LT LAV SMOKE DETECTOR WENT OFF. ALSO THE CABIN ALT GAGE IS INOPERATIVE SO WE COULDN'T TELL OUR CABIN ALT AT ALL, FLEW AT 10,000 THE WHOLE WAY. BITE OF NR 1 AND 2 CABIN PRESSURE CONTROLLERS CURRENT LEG FAULTS THE CONTROLLER ON BOTH. REPLACED NR 1 AND NR 2 CABIN PRESSURE CONTROLLERS IAW AMM 21-31. OPS CKS NORMAL. REPLACED COCPIT SELECTOR PANEL IAW AMM 21-31. OPS CK NORMAL. FOUND UPPER OVER PRESSURE RELIEF VALVE OPEN. PERFORMED SYS TEST OF POSITIVE PRESSURE RELIEF VALVE IAW AMM 21-32. OPS CKS NORMAL. INSPECTED OUTFLOW VALVE LINKAGE AND RAN OUTFLOW VALVE IN MANUAL, OUTFLOW VALVE RUNS SMOOTHLY, ALL LINKAGE CHECKS OK. PRESSURIZED CABIN TO 3 PSID. REPLACED LT AFT LAV SMOKE DETECTOR IAW AMM26-19. OPS CK NORMAL. C/W NO GO ODI PREVENTION REQUIREMENT, MC NOTIFIED. OK FOR SERVICE.

Part: HANDLE — UNSECURE (PAX DOOR) · airframe 87,453 hrs · 42,710 cycles

AFTER TAKEOFF, A LEFT AFT ENTRY DOOR EICAS MESSAGE OCCURED. FLIGHT ATTENTED SAID HANDLE HAD POPPED UP. ACFT REMAINED PRESSURIZED AT ALL TIMES. F/A PUSHED HANDLE BACK DOWN AND THE EICAS MESSAGE WENT AWAY. DURING THE REST OF THE FLIGHT THE HANDLE HAS POPPED UP A FEW MORE TIMES. ALSO THE SLIDE LIGHT ILLUMINATES PERIODICALLY

Part: SKIN — DAMAGED (BS 620) · airframe 87,146 hrs · 42,595 cycles

SKIN BS 620, S16L GOUGED AND DENTED. REPAIRED IAW ER/A 522591-14.

Part: FRAME — GOUGED (BS 1640) · airframe 87,146 hrs · 42,595 cycles

FRAME FS 1640, BETWEEN S5-6L GOUGED. REPAIR COMPLETED IAW ERA 522365-14, REV ORIG.

Part: FRAME — GOUGED (BS 1640) · airframe 87,146 hrs · 42,595 cycles

DURING HMV, BS 1640, FRAME WEB WAS FOUND GOUGED BETWEEN S5-6L.

Part: SKIN — DAMAGED (BS 395) · corrosion level 2 · airframe 86,581 hrs · 42,352 cycles

WHILE PERFORMING CROWN CHEM MILL INSPECTION FOUND DEEP BLEND AT BS 395, STR 5L REPAIRED IAW SRM 53-00-01, REPAIR 3, FIG 201.

Part: SKIN — DAMAGED (L2 DOOR) · airframe 85,615 hrs · 41,972 cycles

GA DENT ON FUSELAGE JUST FWD OF LOWER PART OF DOOR 2L. COMPLIED WITH TIME LIMITED REPAIR WITH ERA ERA 517580-14, REV ORIG.

Part: SLIDE — DAMAGED (L2 DOOR) · airframe 85,583 hrs · 41,956 cycles

L2 DOOR EMERGENCY SLIDE BUSTLE DAMAGED. R & R BUSTLE IAW AMM 52-11.

Part: LIGHT — INOPERATIVE (ROW 42) · airframe 85,237 hrs · 41,832 cycles

CABIN EMERGENCY LIGHT INOPERATIVE AT ROW 42. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSY. AND TESTED IAW AMM 33-51-04.

Part: LAMP — LOOSE (EMERGENCY LIGHT) · airframe 84,874 hrs · 41,683 cycles

SEAT ROWS 33DEF AND 42DEF SEAT MOUNTED EMERGENCY LIGHTS WOULD NOT TEST. FOUND LAMPS PARTIALLY LOOSE. SECURED SAME AND TESTED IAW AMM 33-51-04 PB201, STEP I. OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (BS 358-418) · airframe 84,020 hrs · 41,338 cycles

DAMAGE FROM LIGHTNING AT BS 358-418 S26L. REPAIRED IAW SRM 53-00-01 ALLOWABLE.

Part: SKIN — DAMAGED (BS 451 S26L) · airframe 84,020 hrs · 41,338 cycles

DAMAGE AT FASTENER FROM LIGHTNING AT BS 451 S26L. REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 500-600) · airframe 84,020 hrs · 41,338 cycles

DAMAGE AT FASTENERS FROM LIGHTNING AT BS 500 - 560 BETWEEN S25L AND S26L. ALSO AT BS 600 BETWEEN S24L AND S25L. REMOVED FASTENERS IAW SRM 53-00-01 917734. C/W NDT EDDY CURRENT INSP IAW SRM 53-00-01. NO ITEMS. INSTALLED 4 BLIND FASTENERS IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 1580 S3L) · airframe 83,404 hrs · 41,087 cycles

LIGHTNING STRIKE DAMAGE AT BS 1580 BETWEEN S3L AND L/C. REPAIRED LIGHTNING STRIKE BY DRILL OUT 5/32 HOLE AND INSTALLED BLIND FASTENER IAW SRM 53-00-01, FIG 201. THIS CATAGORY C REPAIR.

Part: DOUBLER — MISLOCATED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

AIRFONE DOUBLER FOUND MISLOCATED. REPAIR PER ERA 483505-14 (DL757101857).

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

STRINGER CORROSION AT STA 750 STR 21R SPLICED STRINGER IN REF TO 5300-03- FIG 201 REPAIR 1 STEP 4 AND ERA 483500-14 (DL757101863).

Part: SKIN — DAMAGED (RT WING) · airframe 76,089 hrs · 37,849 cycles

NR 2 PYLON O/B SKATE ANGLES DRILL STARTS IN WING SKIN FROM PREVIOUS STOP DRILLS (DL757101861).

Part: STRAP — UNKNOWN (FUSELAGE) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

REMOVED AND REPLACED REPAIR STRAP REF SRM 51-40-02 PARA 4 PG 3 FIG 8 (DL757101875).

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

WEAR ON SEAT TRACK STA 876 AND STA 872 RBL 24.75. REMOVED AND REPLACED DAMAGE SECTION OF SEAT TRACK REF 53-00-52 FIG 201 REPAIR 3 (DL757101869).

Part: SILL — CORRODED (BS 695) · airframe 76,089 hrs · 37,849 cycles

L-2 DOOR LOWER SILL HAS CORROSION. REMOVED AND REPLACED NEW ANGLE STA 695.

Part: SEAT TRACK — WORN (FUSELAGE) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

WEAR MARK ON SEAT TRACK TOP SURFACE AT STA 876 RBL 45.5. DAMAGE OUT OF LIMITS PER SRM 53-00-52-PG 102. CUT OUT DAMAGED SEAT TRACK PER SRM 53-00-52 PG 201, FABRICATED SAME PER IAW SRM 53-00-52 FIG 201 REPAIR 3 (DL757101889).

Part: FRAME — GOUGED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

STA 1640 GOUGES ON FRAME L4. REPAIRED IN IAW WITH ERA 482433-14 (DL757101871).

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

FUSELAGE STRINGER CRACKED AT STA 460 AND STA 480 (DL757101858).

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

FUSELAGE STRINGER 16L CRACKED AT STA 460. REPAIRED IN REF TO ERA 483496-14 AND SRM 53-00-03 REPAIR 1 (DL757101859).

Part: STRINGER — CRACKED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

STRINGER 15L CRACKED AT STA 460. INSTALLED STRINGER SECTION REF ERA 482437-14 (DL757101868).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

MAIN CABIN STA 365 RBL 46 SEAT TRACK CORROSION. REMOVED AND REPLACED SECTION OF SEAT TRACK (DL757101866).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1600-1620 BETWEEN STR 30 AND 29 RIGHT. REMOVED AND REPLACED DAMAGED INTERCOSTAL (DL757101876).

Part: PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

FUEL PANEL 542BB CORRODED THRU OUT THE LANDING SURFACE. FOUND OUT OF LIMITS, PER SRM 57-20-01 FIG 201 NOTE B. REPLACED PANEL 542BB WITH SERVICEABLE PART PER MM 28-11-01 STEP E (1-7). REPLACED DIPSTICK HOUSING ON PANEL 542BB PER MM 28-44-01 404-053 E (1-6) BONDING METER ID 03-72 CAL DATE 05/04/11 (DL757101882).

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

MAIN CABIN STA 1670 LBL 56 AFT DRAIN SUPPORT CHANNEL HAS UPPER SURFACE CORROSION - 53-251-01-02-05I.665. REPLACED CHANNEL SUPPORT AT MAIN CABIN FS 1670 LBL 56 757 SRM 51-40-02 PG 07 (DL757101885).

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

RT WING FUEL PANEL 643AB HAS CORROSION AROUND THE MATING SURFACES. FOUND OUT OF LIMITS AND REPAIRED PER SRM 757-200 57-20-01 PG 201 REPAIR 5 NOTE B (DL757101873).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1400- 1420 BETWEEN STR 30 AND 29L. REMOVED AND REPLACED INTERCOSTAL REF 51-20-01 (DL757101881).

Part: PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

FUEL PANEL 641JB HAS CORROSION THRU OUT LANDING SURFACE. REMOVED AND REPLACED PANEL (DL757101872).

Part: PANEL — CORRODED (WING) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

FUEL PANEL 541FB CORRODED. REMOVED AND REPLACED WITH NEW PANEL (DL757101874).

Part: GATE — WORN (R4 DOOR) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

R4 DOOR LOWER GATE AFT CORNER WORN AND OUTER LOWER EDGE WORN. REMOVED AND REPLACED LOWER GATE PER B757 MM 52-11-38-404-009 (DL757101888).

Part: SKIN PANEL — DELAMINATED (FUSELAGE) · corrosion level 2 · airframe 76,089 hrs · 37,849 cycles

THREE AREAS OF DELAM FOUND ON FUSELAGE SKIN PANEL, BETWEEN STA 1963 - 1992 OUT OF LIMITS PER B757 SRM 51-70-10 FIG 201 PG 207 & 208. PANEL NR 148N3770-15 WAS SENT TO DELTA'S SHOP FOR REPAIR, SHOP ORDER CN 1117 (DL757101883).

Part: PAN — GOUGED (E&E DOOR) · airframe 76,089 hrs · 37,849 cycles

MAIN E&E DOOR PAN GOUGED OUT OF LIMITS. REMOVED AND REPLACED DOOR (DL757101855).

Part: SKIN — DENTED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

DENT IN FUSELAGE SKIN STA 543 BETWEEN STR 27 AND 28 LEFT. REPAIRED IN REF TO SRM 53-00-01 REPAIR 3 FIG 201 (DL757101867).

Part: SKIN — DENTED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

DENT IN FUSELAGE SKIN STA 1712 BELOW STR 23L. CUT OUT AND INSTALLED DOUBLER IN REF TO 53-00-01 REPAIR 3 FIG 201 (DL757101862).

Part: SKIN — DENTED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

DENT IN FUSELAGE SKIN ABOVE LAP STR 20 L STA 1700. COMPLIED WITH ERA 482432-14 (DL757101860).

Part: SKIN — DENTED (FUSELAGE) · airframe 76,089 hrs · 37,849 cycles

DENT IN FUSELAGE SKIN STA 1392 RT SIDE OF STR 30. REPAIR IN REF TO ERA 482435-14 (DL757101870).

Part: SKIN — DENTED (BS 610, S17L) · airframe 73,501 hrs · 36,539 cycles

DURING AN AGING AIRCRAFT INSPECTION, A DENT AND CREASE WERE FOUND IN THE FUSELAGE SKIN AT STA 610 BETWEEN S-17L AND S-18L. THE DAMAGED SKIN WAS CUT OUT AND REPAIRED PER BOEING INSTRUCTIONS.

Part: SKIN — DENTED (FS 1652 S20L) · airframe 73,501 hrs · 36,539 cycles

DURING AGING AIRCRAFT INSPECTION, A DENT WAS FOUND AT FS 1652 JUST ABOVE THE S-20L LAP JOINT. DUE TO THE CLOSE PROXIMITY TO THE SUBJECT LAP, IT WAS OUT OF LIMITS PER SRM REQUIREMENTS. AS SUCH, MANUFACTURER WAS CONTACTED FOR REPAIR INSTRUCTIONS. MANUFACTURER APPROVED REPAIR INSTALLED PER ERA 471508-14.

Part: FLOOR SUPPORT — CORRODED (BS 1465) · airframe 73,501 hrs · 36,539 cycles

FLOOR SUPPORT STRINGER BS 1465 LBL 16 IS CORRODED AT THE NUTPLATE. REPAIRED FLOOR SUPPOR IAW MM 53-87-01-801.

Part: ANGLE — CRACKED (BS 660) · airframe 73,501 hrs · 36,539 cycles

FOUND UPPER WEB ANGLE CRACKED WL 208, BS 660 RBL 24.

Part: MOUNT — CORRODED (G1A GALLEY) · airframe 73,501 hrs · 36,539 cycles

CORROSION ON OTBD AFT GALLEY MOUNT BS 322 RBL 38 WL 209. REMOVED AND REPLACED GALLEY FITTING IAW SRM 51-40-02, SRM 51-40-03, SRM 51-40-04.

Part: CARGO TRACK — CORRODED (BS 1520) · airframe 73,501 hrs · 36,539 cycles

CORROSION ON TIE DOWN SUPPORT LOWER SURFACE BS 1520 RBL 22 BILGE AREA. FOUND CORROSION ON DOUBLER FOR TIE DOWN FITTING OUT OF LIMITS, REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02, SRM 51-20-01.

Part: FITTING — CORRODED (BS 1400) · airframe 73,501 hrs · 36,539 cycles

AFT CARGO BAY DOOR WAY THRESHOLD SUPPORT FITTING IS CORRODED BS 1400 RBL 28. REMOVED AND REPLACED FITTING DUE TO CORROSION OUT OF LIMITS.

Part: SUPPORT — CORRODED (BS 1400) · airframe 73,501 hrs · 36,539 cycles

SUPPORT COMMON TO FITTING CORRODED BS 1400 RBL 28. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02, DRW 146N8560.

Part: WEB — CORRODED (AFT CARGO) · airframe 73,501 hrs · 36,539 cycles

CORROSION AFT CARGO BAY, FLOOR WEB CORRODED FS 1460-1480 S28R. REPLACED WEB IAW SRM 51-40-02, SRM 51-40-03, SRM 51-20-01.

Part: INTERCOSTAL — CORRODED (BS 1500 LBL 2.9) · airframe 73,501 hrs · 36,539 cycles

CORROSION ON INTERCOSTAL BS 1500 LBL 2.9 INBD SIDE OF INTERCOSTAL, BILGE. REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 73,501 hrs · 36,539 cycles

CORROSION ON INTERCOSTAL BS 1500 RBL 2.9 O/B SIDE OF INTERCOSTAL BILGE. REPLACED INTERCOSTAL.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 73,501 hrs · 36,539 cycles

FWD CARGO BAY, BS 550 - 650 LBL 19 - RBL 19, FLOOR PANEL MATING SURFACES HAVE AREAS OF SURFACE CORROSION. FABRICATED AND REPLACED FLOOR PANEL IAW SRM 51-40-02, SRM 53-30-53.

Part: FLOORBEAM — CORRODED (BS 1530) · airframe 73,501 hrs · 36,539 cycles

CORROSION AROUND NUTPLATES BS 1530 RBL 22 COMMON TO FLOOR TO SIDE WALL SPLICE LOWER SURFACE OF SPLICE, BULDGED. REPLACED SPLICE IAW 51-40-02.

Part: FLOOR PANEL — CORRODED (BS 1380-1460) · airframe 73,501 hrs · 36,539 cycles

AFT CARGO BAY BS 1380-1460 RBL 20 FIXED FLOOR PANEL CORRODED AT NUTPLATE LOCATIONS. AREAS OF CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FIXED FLOOR PANEL IAW SRM 51-40-05.

Part: SUPPORT — CORRODED (BS 1527-1530) · airframe 73,501 hrs · 36,539 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT RT LOWER FLANGE INBD COMMON TO FASTENERS. REPAIRED PER DELTA ER/A 471503-14 REV ORIG.

Part: INTERCOSTAL — CORRODED (BS 1538 LBL 11.4) · airframe 73,501 hrs · 36,539 cycles

CORROSION ON LOWER FLANGE OF INTERCOSTAL COMMON TO SKIN BILGE AREA LBL 11.40 BS 1538. REPAIRED DAMAGE PER DELTA ER/A 471504-14 REV ORIG.

Part: VIDEO UNIT — ODOR (CABIN) · airframe 72,993 hrs · 36,262 cycles

IFE REPORTED BY FA THAT IT SMELLED AS IF IT WERE OVERHEATING. SECURED IFE. AFTER SECURING IFE ODOR IS SLOWLY GOING AWAY. F/A REPORTED ODOR COMING FROM NR 1 VIDEO UNIT. REPLACED NR 1 VIDEO UNIT OPS CHECKS GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 71,517 hrs · 35,614 cycles

TWO RED EMERGENCY LIGHT AT 26FED INOP. REPLACED CONNECTOR UNDER SEAT 26F, OP OK.

Part: BULB — INOPERATIVE (EMERGNECY LIGHT) · airframe 71,517 hrs · 35,614 cycles

EMERGENCY LIGHT OUTSIDE R4 DOOR INOP. RELAMPED.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 67,183 hrs · 33,697 cycles

ON INITIAL CLIMB-OUT, CAPTS WINDSHIELD CRACKED AND BEGAN TO ARC. LEFT WINDOW HEAT WAS SHUT OFF. RETURNED TO JFK. REPLACED CAPTAIN'S WINDOW AND WINDOW HEAT CONTROLLER.

Part: COFFEEMAKER — BURNED (AFT GALLEY) · airframe 66,743 hrs · 33,502 cycles

BURNING SMELL IN AFT GALLEY, DISCOVERED MELTED PLASTIC ON HOT PLATE OF COFFEE MAKER. NEEDS TO BE CLEANED OUT. REPLACED COFFEE MAKER. OP CKS OK.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 66,561 hrs · 33,439 cycles

.025 LONG CRACK IN THE BEAR STRAP EXTENDING FROM THE UPPER CORNER OF THE L1 DOOR CUTOUT. REPAIR INSTALLED IN ACCORDANCE WITH ERA 457208-14AD.

Part: PIN — CORRODED (EVAC SLIDE) · airframe 57,743 hrs · 30,133 cycles

ON HMV-3 OPN 5726, PIN CORRODED BS 1181 STR 21L ON OVERWING SLIDE ACTIVATION/DEACTIVATION LEVER. LEVER WAS STIFF IN INITIAL OPERATION. REMOVED PINS FOR INSPECTION. OK TO INSTALL. INSTALLED NEW PINS AND OPN NOW NORMAL. REPLACED PINS WERE BACP18T4-41 AND BACP18T4-38 ITEMS 230.

Part: PIN — CORRODED (EVAC SLIDE) · airframe 57,743 hrs · 30,133 cycles

ON HMV-3 INSPECTION OPN 5726. PIN CORRODED BS 1180 S21-R/L BL 48R/L ON OVERWING ESCAPE SLIDE ACTIVATION/DEACTIVATION HANDLE RIGHT/LEFT SIDE. DEACTIVATION HANDLE HARD TO MOVE DUE TO CORROSION ON ATTACH PIN FOR BELLCRANK. BOTH SIDES FOUND CORRODED. REPLACED SAME.

Part: NUT — CORRODED (ESCAPE SLIDE) · airframe 57,743 hrs · 30,133 cycles

EMERGENCY ESCAPE MANUAL RELEASE CABLE JAM NUT CORRODED BELOW AND BETWEEN EXIT CUTOUTS STA 984-996 AND STRINGER 17R. REMOVED SAFETY WIRE, CLEANED AREA OF CORROSION. OK TO INSTALL NEW HARDWARE. INSTALLED NEW HARDWARE.

Part: CLEVIS — CORRODED (ESCAPE SLIDE) · airframe 57,743 hrs · 30,133 cycles

NR 915 HMV-3 VISIT INSPECTION OPN 5876, HARDWARE CORRODED ON CABLE FOR MANUAL EMERGENCY RELEASE CABLE LT SIDE OF FUSELAGE BETWEEN OVERWING EXITS STA 984-996 STRINGER 17L. REMOVED SAFETY WIRE, CLEANED AREA OF CORROSION. OK TO INSTALL NEW HARDWARE. INSTALLED NEW HARDWARE AND RESAFTIED. IPC ITEMS NR 150/155/160/173/175 REPLACED. P/N'S MS24665-132/MS20392-2C17/BACW10P270L/AN960-10/MS35650-302/MS35812-1.

Part: SKIN — GOUGED (LT WING SLAT) · airframe 57,743 hrs · 30,133 cycles

NR 2 SLAT GOUGED. COMPLETED PERMANENT REPAIR PER SRM 51-70-10D REF SRM 57-43-02D. C/W PERMANENT REPAIR ON OPN 1000 CARDS 1135-1143.

Part: SKIN — DENTED (RT WING SLAT) · airframe 57,743 hrs · 30,133 cycles

NR 9 SLAT DENTED ON I/B END. COMPLETED PERMANENT REPAIR PER SRM 51-70-10D REF SRM 57-42-02D. C/W REPAIR ON OPN 1000 CARDS 1126-1134.

Part: BEARING — CORRODED (L2 DOOR) · airframe 57,743 hrs · 30,133 cycles

NR 264 HMV3 L2 ENTRY DOOR INSPECTION OPN 5836 CP53-231-01I. ROLLER CORRODED EPAS HAMMER ROLLER CORRODED 2L. REMOVED EPAS ROLLER AT L2 DOOR, NO FURTHER CORROSION FOUND. OK TO INSTALL L2 DOOR. INSTALLED EPAS ROLLER AT L2 DOOR POSITION. OPN OF EPAS SYSTEM TO BE CW ON DOOR INSTALLATION. THIS BEARING WORKS WITH THE TRIGGER MECHANISM ON THE UPPER GUIDE ARM OF THE DOOR TO SET OFF THE EPAS BOTTLE WHEN THE SLIDE ID DEPLOYED. IPC 52-11-01-24 ITEM 270.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 57,466 hrs · 30,023 cycles

ON LAYOVER FOUND FIRST THREE ROWS IN FIRST CLASS MISSING OVERHEAD EMERGENCY LIGHTS. REMOVED AND REPLACED PWR SUPPLY BATTERY, SYSTEM CHECKS NORMAL.

Part: HANDLE — UNSECURE (PARK BRAKE) · airframe 57,047 hrs · 29,841 cycles

FOR INFO ONLY ON T/O ROLL AT 20KTS RECEIVED T/O CONFIG WARNING. TAKEOFF WAS REJECTED. FOUND PARK BRAKE HANDLE NOT FULLY SEATED. EXERCISED HANDLE AND PARK BRAKE OP NORMAL. TEMPS READ 7 ZEROS AND 1 ONE.

Part: PUMP — CRACKED (NR 2 ENGINE) · airframe 55,767 hrs · 29,288 cycles

LOST RT HYD SYSTEM QUANTITY WHILE HOLDING SHORT OF RUNWAY FOR TAKEOFF. FOUND RT ENGINE DRIVEN HYD PUMP HOUSING CRACKED. REPLACED RT ENGINE DRIVEN HYD PUMP, CASE DRAIN FILTER AND PRESURE FILTER. ALL LEAKED CHECKED GOOD. SERVICED HYD SYSTEM TO FULL.

Part: ODOR — DETECTED (CABIN) · airframe 55,392 hrs · 29,098 cycles

FLT ATTENDANTS REPORTED AN ODOR SIMILAR TO HOT PLASTIC IN THE REAR OF THE AFT CABIN THAT THE APPARENT CAUSE OF HEADACHES FOR SEVERAL PASSENGERS AND FLT ATTENDANTS. AIRCRAFT WAS IN CRUISE. ANTI ICE WAS NOT IN USE. ODOR DID NOT INCREASE WHEN USING ANTI ICE IN DESCENT. OPERATED AIR CONDITION SYSTEM FOR 30 MINS. COULD NOT DUPLICATE ANY SMELL OR ODOR.

Part: WIRE — DAMAGED (CABIN) · airframe 54,308 hrs · 28,546 cycles

ON INSPECTION FOUND RED EMERGENCY PATH LIGHT ON, AFT LAV INOP. FOUND WIRING BROKEN FOR LIGHT ASSY. REPLACED LIGHT ASSY AND REPAIRED WIRING. OPS NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,070 hrs · 28,434 cycles

ON LAYOVER FOUND EXTERIOR EMERGENCY LIGHT AT L2 DOOR DID NOT ILLUMINATE. RELAMPED EMERGENCY LIGHT.

Part: CONTROLLER — MALFUNCTIONED (NR 1) · airframe 51,489 hrs · 27,192 cycles

CRUISE ALT 370 -DISCRETE CABIN ALT LIGHT ILLUM AND ASSOCIATED EICAS MSG CBN ALT APPEARED. CABIN ALT REACHED 11500 AND SLOWLY INCREASING BY TIME WE WERE EMERG DESCENDING. CABIN REMAINED ABOVE 10000 DURING DESCENT UNTIL APPROX 140 MSL. AFTER LEVELING AT 100 MSL CABIN ALT CONTINUED TO DESCEND TO LOW THOUSANDS 1000-2000 FT. THIS OCCURRED WHILE IN AUTO 1 ON CABIN PRESS PANEL. BITE CHECKED NR 1 AND NR 2 AUTOPRESS CONTROLLERS, NOFAULTS. REPLACED NR 1 AUTO PRESS. CONTROLLER AND SEL PNL PER M/M. REPLACED NR 1 PRESS. CONTROLLER C/B. PRESS A/C CKS OK. CKED IXT

Part: ENGINE — STALLED (NR 2) · airframe 46,999 hrs · 25,055 cycles

RIGHT ENGINE COMPRESSOR STALL ON DEPARTURE AT APPROXIMATELY 6,000 FEET, BROUGHT IT BACK TO IDLE. FOUND METAL IN TAILPIPE. REPLACING NR TWO ENGINE.

Part: CONTROLLER — MALFUNCTIONED (CABIN)

CABIN ALT MASTER WARNINGS ACTIVATED WHILE AT CRZ FL350. CREW REPORTS CABIN ALT CONTINUED TO CLIMB PAST 12K SO O2 MASKS DEPLOYED MANUALLY. SYSTEM SWITCHED TO MANUAL MODE AND OUTFLW VLV WENT TO FULL CLOSED AS COMMANDED DURING EMERGENCY DESCENT INTO TYS. CREW REPORTED ATTEMPTS TO RETURN SYS TO AUTO MODE WERE UNSUCCESSFUL, BUT SHIP DID PRESS IN MANUAL MODE AND CABIN ALT RETURNED TO NORMAL. FOUND CABIN PRESS CONTROLLER FAULTING A/C MOTOR ON AFT CABIN OUTFLOW VALVE. REPLACED SAME. AS PRECAUTION, REPLACED BOTH CABIN PRESS. CONTROL MODULES AND ALT CONTROL PANEL, PRESS OP CKS NORMAL.

Part: ELT — MALFUNCTIONED (COCKPIT)

MTC COORDINATION RECIEVED MESSAGE THAT THE MILITARY IS RECIEVING A ELT SIGNAL FROM SHIP 618. REPLACED ELT.

Part: FSEU — FAILED (LE SLATS)

DIVERSION, PILOT REPORT: L/E SLAT ASYM EICAS MSG ILLUMINATED ALONG WITH T/E ANNUNCIATOR AT FL 350. FOUND AND REPLACED NR 1 FSEU CAUSING FALSE SLAT LOSS MSG ALL WIRING FROM PIN C9, PER FIM OK EVEN WITH FAULT DISPLAYED. ALSO, RESET BOXES 2 AND 3. OPERATIONAL CHECK GOOD PER MM CHAPTER 27.

Part: SLIDE — MALFUNCTIONED (L 1 DOOR)

THE LEFT SLIDE INADVERTANTLY DEPLOYED BY FLIGHT CREW. SLIDE DID NOT FULLY INFLATE. REPLACED SLIDE.

Part: SKIN — DENTED (BS 1690)

A DENT WAS FOUND IN THE FUSELAGE SKIN AT APPROX BS 1690 JUST BELOW THE LAP JOINT AT STGR 20R. REPAIRED PER ERA 364767-14.

Part: FLOORBEAM — CORRODED (BS 1681.8)

FLOORBEAM BS 1681.8 WAS FOUND WITH CORROSION DAMAGE ALONG ENTIRE LENGTH OF UPPER CAP. REPAIRED PER ERA 364763-14.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE)

757 NR 2 ENGINE HIGH PRESSURE AIR LINE NOT CONNECTED AT FIREWALL, BLEW HOLE IN THRUST REVERSER INNER CORE (315N3101 ASSY) AT NAC STA 110, APPOX 3 INCH BY 8 INCH AT 1 O'CLOCK POSITION. REQUIRES REPAIR AT NORDAM PER LIASON ENGINEERING. ERA PENDING, SENT TO OUTSIDE REPAIR 01-26-96.

Part: K117 RELAY — FAILED (APU)

WORKING INOP APU, FOUND STARTER BURNED UP AND APU BATTERY DEAD. RELAY K-117 CONTACTS WELDED CLOSED CAUSING STARTER TO RUN CONTINUOUS UNTIL APU BATTERY WENT DEAD.