N14075

Part: CABLE — MISRIGGED (L4 DOOR) · airframe 104,334 hrs

DURING MAINTENANCE L4 DOOR FAILED TO OPEN WITH DOOR ARMED, EMERGENCY MODE. REMOVED LININGS, RIGGED AIR RELEASE CABLE AND ARMING ROD IAW DC10 MM 52-12-00. OPS CHECK GOOD. SERVICED DOOR OPENING RESERVOIR IAW DC10 MM 52-12-00. REPLACED L4 DOOR AND SURROUND LININGS IAW DC10 MM 25-61-01.

Part: FAIRING — PUNCTURED (FUSELAGE)

FLIGHT 8010 09/06/08 KBWI/ETAR - DURING FLIGHT A THUMP WAS HEARD AND FELT 5 HOURS INTO FLIGHT AT FL310, NO ABNORMAL INDICATIONS OR HANDLING FOLLOWED. DURING POST FLIGHT INSPECTION, MAINTENANCE FOUND LT WING LDG EDGE WING/BODY FAIRING PUNCTURED AND CRACKED. REMOVED FAIRING PER MM 57-31, REPAIRED IAW DAC DWG PL ANS7100, SPEC DPS 1.44. & REINSTALLED FAIRING.

Part: FITTING — CRACKED (CENTER FUEL TANK)

DURING INSPECTION, MAINTENANCE FOUND FITTING CRACKED IN CENTER FUEL TANK I/B CORNER ABOVE ACCESS DOOR 141AZ. REMOVED AND REPLACED FITTING. (S)

Part: FRAME — CORRODED (BS 1967)

DURING INSPECTION, MAINTENANCE FOUND AFT FUSELAGE WASTE TANK COMPARTMENT CORROSION ON FRAME LOWER LEG 1967 LBL 6-10. REPAIRED IAW SRM 63-30-00 FIG 9 & 10 VOL 1. (S)

Part: SLIDE — DISLODGED (L1 DOOR)

L1 DOOR SLIDE DROPPED OUT WHEN DOOR OPENED PNEUMATICALLY, SLIDE DID NOT DEPLOY CORRECTLY. REMOVED AND REPLACED SLIDE ASSY IAW MM 25-61-01. SERVICED PNEUMATIC DOOR ASSIST.

Part: OVEN — MALFUNCTIONED (GALLEY)

EDDP/KBGR OVEN 609 AFT GALLEY ON FOR 5 MIN. THEN GRAY AND WHITE SMOKE BILLOWED OUT, SHUT OFF OVEN. ITEM PLACED ON DMI PER MEL 25-29-01 CAT C DUE 04/17/08. REMOVED AND REPLACED OVEN 609, DMI CLEARED 04/10/08.

Part: CABLE ASSY — MISRIGGED (L4 DOOR)

DURING MAINTENANCE INSPECTION L4 PASSENGER DOOR FAILED PNEUMATIC TEST. RIGGED AIR RESERVOIR AIR RELEASE CABLE PER DC10 AMM 52-12-00 PAGE 534. ADJUSTED L4 DOOR EMERGENCY BACKLOCK PER DC10 AMM 52-12-00 PAGE 530A. PERFORMED PNEUMATIC TEST OF THE L4 DOOR PER DC10 AMM 52-10-01. REF SAA NRC 78379990001.

Part: SWITCH — LOCKED (COCKPIT)

RME/BWI CENTER GEAR TOOK 30 SEC TO RETRACT DID NOT EXTEND NORMALLY, EMERGENCY EXTENSION RELEASED. GEAR EXTENDED IN APPROXIMATLEY 15 SEC. FOUND CENTER GEAR SWITCH ON F/O PANEL LOCKED IN UP POSITION, RETURNED TO NORMAL. DEFLATED CENTER GEAR STRUT, CYCLED CENTER GEAR UP AND DOWN SEVERAL TIMES, ALL INDICATIONS NORMAL. SERVICED STRUT AND REMOVED PINS.

Part: SUPPORT FITTING — CORRODED (CORRODED)

DURING B-CHECK INSPECTION, CORROSION FOUND ON DIAMETER SUPPORT FITTING TIE BRACE ON LOWER INNER SURFACE IN CENTER LANDING GEAR WHEEL WELL RIGHT SIDE FS 1461. REPLACED SPLICE ANGLES AT FS 1461 PER SRM 51-33-01, SRM 53-14-01, SRM 53-00-01, SRM 51-21-01, SRM 51-31-01 AND DPS4 710-3 REV AJ PAGE 5.

Part: LONGERON — CORRODED (BS 1461)

DURING B-CHECK INSPECTION, CORROSION FOUND ON LOWER END OF LONGERON IN CENTER GEAR W/W RIGHT SIDE AT FS 1461. REMOVED CORRODED LONGERON FROM CENTER GEAR WHEEL WELL. FABRICATED A REPLACEMENT LONGERON FROM 7075-T6 511 AND INSTALLED IAW DC-10 SRM 51-38-01 PG 17.

Part: DOUBLER — CORRODED (FUSELAGE)

DURING B-CHECK INSPECTION, CORROSION FOUND ON FWD LOWER CORNER OF UPPER CUTOUT SUPPORT DOUBLER FOR AFT HINGE ON CENTER GEAR RIGHT FWD DOOR IN CENTER W/W AT FS 1441. REMOVED DOUBLER, FABRICATED DOUBLER AND INSTALLED DOUBLER, TEE STIFFENER AND SUPPORT FITTING IAW DC10 SRM VOL II 51-33-01 & 53-14-01.

Part: STIFFENER — CORRODED (BS 1442)

DURING B-CHECK INSPECTION, CORROSION FOUND ON LOWER AFT CORNER OF SUPPORT STRAP IN CENTER W/W RIGHT SIDE ABOVE AFT HINGE ON FWD GEAR DOOR AT FS 1442. REMOVED, FABRICATED, AND INSTALLED TEE STIFFENER IAW DC10 SRM VOL II 51-31-01 & 51-33-01.

Part: ANGLE — CORRODED (BS 1370)

CORROSION FOUND DURING B-CHECK IN LEFT W/W AT FS 1370 BETWEEN TANK AFT PANEL CAP STRUCTURE AND SIDE FORGING AT SPLICE AREA LBL 115, 38 INCHES BWL. [08-07-07] REMOVED AND REPLACED CORRODED ANGLE, P/N ANB7392-1 IN ACCORDANCE WITH DC-10 SRM VOL.2 51-31-01.

Part: DOOR FRAME — CORRODED (OVERWING DOOR)

DURING B-CHECK INSPECTION, RIGHT HAND OVERWING DOOR R-3, AFT LOWER CORNER (AT FLOOR LEVEL) STA 1305 EVIDENCE OF CORROSION UNDER DOOR SILL PLATE. [08-07-07] SILL PLATE SUPPORT CHANNEL FOUND CORRODED BEYOND LIMITS. REMOVED CHANNEL, FABRICATED NEW SUPPORT CHANNEL FROM 7075-T651, AND INSTALLED IN ACCORDANCE WITH DC-10 SRM VOL.2 51-31-01.

Part: DOOR — MISSING (NR 1 COWLING)

DURING WALKAROUND FOUND MISSING PRESSURE RELIEF DOOR FROM NR 1 ENG LT HAND SIDE CORE COWL, DOOR HINGE DAMAGED AND COWLING SKIN CRACKED ABOUT .875 INCH FORWARD OF DOOR HINGE AREA; CHECKED WING FUSELAGE AND TAIL, NO DAMAGE NOTED. REPAIRED AS PE 14-121-379 BOEING SVC LETTER 1-23231981 DOC 06-71-134.

Part: STIFFENER — CORRODED (BS 1521)

DURING C-CHECK IN GSO FOUND LT WHEEL WELL BS1521 OB STIFFNER ANGLE HAS SECTION MISSING DUE TO CORROSION. REMOVED AND REPLACED STIFFNER WITH A NEW FABRICATED STIFFNER IAW DAC DWG AEA0025, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-01 VOL II.

Part: PRESSURE PANEL — CORRODED (BS 1521)

DURING C-CHECK IN GSO FOUND LT WHEEL WELL BS1521 LOWER WEB HAS SEVERE INTERGRANUALAR CORROSION. REMOVED AND REPLACED WITH A NEW FABRICATED INTERCOASTAL IAW DAC DWG AEA7163, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-01 VOL II.

Part: ANGLE — CORRODED (BS 1521)

DURING "C" CHECK IN GSO, FOUND LEFT WHEEL WELL BS1521 INBOARD BULKHEAD ANGLE CORRODED. REMOVED AND REPLACED WITH A NEW FABRICATED ANGLE IAW DAC DWG AEA0025, ALODINED, PRIMED AND PAINTED IAW DC10 SRM 51-21-01 VOL II.

Part: SEAT TRACK — CORRODED (BS 824-899)

DURING C-CHECK IN GSO FOUND MAIN CABIN BETWEEN STA 824 TO 899 SEAT TRACK AT APPROX RBL 106 CORRODED. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 765 TO 910 WITH A NEW SEAT TRACK IAW DC10-30 SRM 53-70-00 VOL I.

Part: SEAT TRACK — CORRODED (BS 1400-1412)

DURING C-CHECK IN GSO FOUND CABIN SEAT TRACK AT LBL 28, BS 1400 TO 1412 HAS CORROSION INSIDE LUGS AND IN UPPER SURFACE OF TRACK. FABRICATED REPAIR PART AND INSTALLED IAW DC10-30 SRM 51-31-01 VOL II, REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1391 TO 1511 WITH A NEW SEAT TRACK IAW DC10-30 SRM 53-70-00 VOL I.

Part: SEAT TRACK — CORRODED (BS 1481-1491)

DURING C-CHECK IN GSO FOUND CABIN SEAT TRACK AT LBL 28 BS 1481-1491 CORRODED INSIDE LUGS. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1391 TO 1531 WITH A NEW SEAT TRACK IAW DC10-30 SRM 53-70-00 VOL I.

Part: MOUNT — CRACKED (FUSELAGE)

DURING C-CHECK IN GSO FOUND LAV-B OUTBOARD AFT MOUNT CRACKED AND CORRODED. REMOVED AND REPLACED LAV-B OUTBOARD AFT MOUNT IAW DC10 MM 25-00-00.

Part: CHANNEL — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND HAT CHANNEL HAS SURFACE CORROSION AROUND FASTENER HOLE AT STA 1921 BL0. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-31-01 VOL II.

Part: SEAT TRACK — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND SEAT TRACK CORRODED AT LBL28 STA 420-457. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AT STA 1877 - 2007 RBL26. REMOVED AND REPLACED FLOOR SUPPORT CHANNEL IAW SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL CORRODED ON UPPER SURFACE APPROX STA 1915. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.

Part: FLOORBEAM — CRACKED (BS 1482)

DURING C-CK IN GSO FOUND MAIN CABIN FLOORBEAM CRACKED AT STA 1482 B/N LBL 107 AND LBL 80. FABRICATED FLOOR SUPPORT IAW DC 10 DWG. INSTALLED FLOOR SUPPORT.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND CABIN ZONE 220 UNDER FLOOR AREA STA 475 BL95R CORRODED INTERCOSTAL. FABRICATED INTERCOSTAL IAW DC10 DRWG 7186-502. ALODINED & PRIMED IAW DC10 SRM 51-21-01 VOL II. INSTALLED FLOOR SUPPORT IAW SRM 51-31-01.

Part: WEB — CRACKED (BS 1960-1986)

DURING C-CK IN GSO FOUND WEB AT STA 1960-1986 AT RBL 50 CRACKED AROUND FASTENER HOLES. REMOVED WEB IAW DC10 SRM 51-31-01 COL II. FABRICATED DOUBLER IAW DC10 SRM 53-16-01 VOL III. ALIGNED, PRIMED, AND PAINTED, IAW DC10 SRM 51-21-01 VOL I. INSTALLED DOUBLER ON WEB IAW DC10 SRM 51-35-01 VOL II. INSTALLED WEB IAW DC10 SRM 51-33-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" CHECK IN GSO FOUND MAIN CABIN AT STA 828 AT BL-0 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT BEAM IAW DC10 SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND MAIN CABIN AT STA 832 AT APPROX RBL46 TO LBL46 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" CHECK IN GSO FOUND CABIN ZONE 220 UNDER FLOOR AREA STA 450 BL35L SCALLOPED BEAM CAP CORRODED. REMOVED AND FABRICATED NEW FLOOR SUPPORT IAW DOUGLAS DWG ABA8306 REV K. INSTALLED FLOOR SUPPORT IAW SRM 51-35-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR SUPPORT IN MAIN CABIN HAS CORROSION AT STA 879 RBL60. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" CHECK IN GSO FOUND MAIN CABIN FLOOR PANEL NR 224AF SUPPORT CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT IAW WITH SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND MAIN CABIN BETWEEN STA 808 TO 899 FLOOR SUPPORT AT APPROX RBL 46 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31-01 VOL I.

Part: LONGERON — CORRODED (FUSELAGE)

ITEM: DURING "C" CHECK FOUND AT STA 1521 LONGERON 46L HAS EXFOLIATION AND HEAVY PITTING CORROSION. FABRICATED NEW REPAIR ANGLE AND CHANNEL, INSTALLED PER SRM CHAP 51 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR SUPPORT IN MAIN CABIN HAS SURFACE CORROSION AT STA899 RBL60. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR SUPPORT IN MAIN CABIN HAS CORROSION AT STA 824 RBL60. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AROUND NUT PLATE CLIP HOLES AT STA 1900 LBL22-RBL22. REMOVED AND REPLACED FLOOR SUPPORT CHANNELS IAW SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AT STA 1900 LBL28-LBL53. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-33-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS SURFACE CORROSION AT STA 1887 RBL50. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-33-01 VOL II.

Part: FRAME — CORRODED (LT MLG WW)

ITEM: DURING "C" CHECK IN GSO FOUND LEFT WHEEL WELL STA 1510 FRAME CORRODED ON LOWER LEG. FORMED NEW FRAME IAW DAC DWG AEA7165 REV K. INSTALLED NEW FRAME SECTION IAW SRM 53-00-01 VOL I.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT ANGLE HAS SURFACE CORROSION AT STA 1986 LBL14. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT IAW SRM 51-31-01 VOL II.

Part: DOUBLER — CORRODED (RT MLG WW)

DURING C3 CK, FOUND CORROSION ON DOUBLER IN RT WHEEL WELL STA 1520-1500. FAB NEW DOUBLER.

Part: FITTING — CORRODED (RT MLG WW)

DURING C3 CK, FOUND CORROSION ON RT W/W FITTING, STA 1505 B/N LONG 44 AND 45. REPLACE SUPPORT FITTING.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ITEM: DURING "C" IN GSO FOUND FLOOR BOARD SUPPORT CHANNEL HAS CORROSION AT STA 1913 - 2007 LBL24. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT CHANNEL IAW SRM 51-31-01 VOL II.

Part: BULKHEAD — CORRODED (FUSELAGE)

DURING C3 CK, FOUND CORROSION IN MAIN CABIN AFT PRESSURE BULKHEAD UNDER SPLICE ANGLE LOWER CORD. REMOVED AND REPLACED T CHORD DC10 SRM 51-31-01 VOL II.

Part: SUPPORT — CORRODED (FUSELAGE)

DURING C3 CK IN GSO, FOUND CORROSION R MLG MOST AFT ACCESS SUPPORT IS CORRODED. SPLICE NEW EXT ANGLE REPAIR.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE)

ITEM: DURING "C" CHECK IN GSO FOUND LAV SUPPORT CHANNEL CORRODED ON UPPER SURFACE STA 859 LBL70. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED & REPLACED SUPPORT CHANNEL IAW DC10 SRM.

Part: FITTING — CORRODED (LT MLG WW)

DURING C3 CK, FOUND CORROSION ON LT WHEEL WELL AT STA 1509 INBOARD FITTING. REMOVE AND REPLACE FITTING.

Part: TEE FITTING — CORRODED (FUSELAGE)

DURING C3 CK, FOUND CORROSION ON TEE CHORD AT L43 LT WHEEL WELL, STA 1521. REMOVE CORROSION AND REEVALUATE, AND GENERATE RFTS FOR REPAIR. FASTENERS REQ'D REMOVAL.

Part: FLOORBEAM — CORRODED (BS 395)

DURING C-CK IN GSO FOUND FLOORBOARD ATTACH ANGLE CORRODED IN MAIN CABIN AT STA 395 BELOW THE COCKPIT DOOR. FLOORBOARD ATTACH ANGLE REMOVED AND REPLACED WITH NEW P/N BAC1503-4162 EXTRUSION 7075-T6105111 (PO 541368.1) IAW DC 10 SRM 51-31-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (BS 430)

DURING C-CHECK IN GSO FOUND MAIN CABIN AT APPROX STA 430, AT RBL 10, FLOOR SUPPORT CORRODED. RECEIVED FLOOR SUPPORT P/N ABA8225-503 PO 541338, REMOVED OLD SUPPORT. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-31-01 VOL II. INSTALLED FLOOR SUPPORT AND DOOR JAMB PER 51-31-01 VOL II. BLENDED CORROSION, FOUND OUT OF LIMITS IAW SRM 51-21-01 VOL II AND 53-00-01 VOL I.

Part: FLOORBEAM — CORRODED (BS 495)

DURING C-CK IN GSO FOUND FLOORBEAM CORRODED IN MAIN CABIN AT STA 495 AT APPROX RBL 56. REPLACED FLOOR SUPPORT IAW CAB DWG ACA 7364 AND DC10 SRM 51-31-01 VOL II AND DC10 SRM 51-33-01 VOL II.

Part: FLOOR SUPPORT — CORRODED (BS 879-755)

DURING C-CK IN GSO FOUND FLOOR SUPPORT CORRODED IN MAIN CABIN B/N STA 879-755 AT APPROX LBL 46. RECEIVED NEW PART P/N ADA 7327-1 PO 540808-12; INSTALLED NEW FLOOR SUPPORT AIW DC10 SRM 51-31-01 VOL II.

Part: SEAT TRACK — CORRODED (BS 1960)

DURING C-CK IN GSO AT STA 1960, FOUND RT O/B TRACK AND LAV MOUNT CORRODED. BLEND OUT CORROSION IN SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 1909-1913)

DURING C-CK IN GSO FOUND RIGHT O/B SEAT TRACK AND LAV MOUNT CORRODED AT STA 1909-1913. BLENDED AREA IN ELECTRIC SEAT TRACK. FABRICATED STRAP.

Part: BULKHEAD — CORRODED (LT MLG WW)

DURING C3 CHECK, FOUND CORROSION IN LT MAIN GEAR WHEEL WELL AFT PRESSURE BULKHEAD, STA 1521, VERTICAL STIFFENER LOWER SUPPORT WEB AND ASSOCIATED ANGLES. REMOVED CORROSION AND REPLACED STIFFENER, WEB, AND ANGLES PER SRM PROCEDURES.

Part: STIFFENER — CORRODED (LT MLG WW)

DURING C3 CK, FOUND CORROSION IN LT MAIN GEAR WELL AFT PRESSURE BULKHEAD, STA 1521, ON THE VERTICAL STIFFENER (LWR AFT AREA). REMOVED CORROSION AND REPLACED STIFFENER.

Part: FIRE WARNING — FALSE ACTIVATION (APU)

APU AUTOSHUTDOWN WITH A FIRE WARNING ALERT. FIRE AGENT CYLINDER 1 DISCHARGED. REPLACED NR 1 REAR FIRE BOTTLE PER MM CHAP 26. INSPECTED APU AREA FOR LEAK AND POSSIBLE FIRE DAMAGE, NONE FOUND. OK FOR CONTINUED SERVICE.

Part: FUEL SYS — LEAKING (NR 3)

DIVERSION DUE TO 1+20HR INTO FLIGHT NR 3 FUEL FLOW STARTED TO INDICATE 15,000 LBS PER HOUR ON THE NEEDLE, 29,320 ON DIGITAL. FUEL USED ON NR 3 ROSE TO OVER 5,000 LBS MORE THAN 1 AND 2. ENGINE SHUTDOWN PER PROCEDURES. FUEL PRESSURE ON NR 3 STILL INDICATES 80 PSI AND FUEL FLOW INDICATED 2,500 LBS PER HOUR. FIRE HANDLE WAS PUT DOWN AND FUEL FLOW DROPPED. FLEW 45 MINUTES WITH FIRE HANDLE DOWN AND ENGINE SHUT DOWN. INSPECTED ENGINE, FOUND NO FUEL LEAKS STATIC OR WITH PUMPS. ENGINE IDLE RUN FOUND NO LEAKS. REINSPECTED AFTER ENGINE RUN. NO LEAKS NOTED. HIGH POWER ENGINE RUN ALL PARAMETERS NORMAL (EGT, N1, N2, FUEL FLOW, FUEL PRESSURE) NO LEAKS NOTED. AIRCRAFT DETERMINED TO BE OK FOR SERVICE.

Part: LEVER — STUCK (COCKPIT)

ON APPROACH, LANDING GEAR HANDLE WOULD NOT RELEASE. COMPLIED WITH ALTERNATE GEAR EXTENSION PROCEDURE AND COMPLETED NORMAL LANDING. CLEANED AND LUBED CABLES, CLEANED CANNON PLUG ON HOLDING COIL AND CHECKED FOR BINDING ON GROUND. NO BINDING OR BROKEN CABLES, GEAR HANDLE OPERATION NORMAL IAW MM PROCEDURES.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING "B4" CHECK IN BYH, FOUND RBL30 F/S 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATELY .002 OF MATERIAL RBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW DC-10 SRM 51-21-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING "B4" CHECK IN BYH, FOUND LBL30 FS 1907 TO 2007 FLOOR SUPPORT CORRODED. REMOVED SURFACE CORROSION OF APPROXIMATELY .002 OF MATERIAL LBL30 FS 1907 TO 2007 FLOOR SUPPORT. TREATED BARE AREAS WITH ALODINE, CLEANED THEN PRIMED AREA IAW DC-10 SRM 51-21-01.

Part: FLOOR PANEL — CORRODED (FUSELAGE)

DURING "B4" CHECK IN BYH, FOUND FLOOR PANEL FWD OF LEFT FWD STORE CLOSET HAD EXFOLIATION CORROSION. REMOVED AND REPLACED FLOOR PANEL FWD OF LEFT STORE CLOSET IAW DC-10 MM 53-22-01.

Part: CADC — INOPERATIVE (AIRSPEED IND)

ITEM: RCH725/13 NGU/NAP REJECTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON CAPT'S INDICATOR, F/O'S INDICATED OK. RTO AT 105KTS. REMOVED AND REPLACED CADC, PERFORMED PITOT STATIC CHECK, FOUND ALL NORMAL. REMOVED AND REPLACED PITOT STATIC TUBE PRECAUTIONARY. PRESSURE CHECK ALL NORMAL.

Part: SLIDE — FAILED (R-1 DOOR)

DURING MAINTENANCE CHECK, GYR R-1 DOOR SLIDE SCHEDULE FOR TEST DEPLOYMENT, THE TEST ACCOMPLSHED PER DC-10 MM, DURING THE TEST CHECK THE SLIDE INFLATED WHEN THE DOOR WAS APPROXIMATELY 3/4 OPEN AND DEPLOYED INSIDE THE AIRCRAFT (THE SLIDE NEVER LEFT THE DOOR WAY). REMOVED AND REPLACED THE SLIDE.

Part: CONTROL UNIT — FAILED (ANTI SKID SYS)

AIRCRAFT N14075 FLIGHT 8012 FROM LIRN TO KNGU, DURING THE LANDING AT THE KNGU THE RIGHT OUTBOARD ANTI-SKID FAIL LIGHT ILLUMINATED IN FLIGHT. DUE TO THE SHORT RUNWAY AT KNGU THE CREW DECIDED TO LAND AT KNTU. AT THE KNTU MAINTENANCE REMOVED & REPLACED THE ANTI-SKID CONTROL UNIT, OP'S CHECKED NORMAL.

Part: INDICATOR — FAILED (ATTITUDE)

THE AIRCRAFT NR 1 VERTICAL GYRO WAS INOPERATIVE, ON CLIMBOUT OF BAHRAIN N2 (FIRST OFFICER) FAILED, THE CREW UNABLE TO RESET OR RESTORE IT AND DECIDED TO RETURN BACK TO BAHRAIN. AT BAHRAIN MAINTENANCE REPLACED THE F/O ATTITUDE DIRECTOR INDICATOR PER MM 34-23-02 OP'S CHECK GOOD, AIRCRAFT RETURN TO SERVICE.

Part: COWL DOOR — MISSING (NACELLE)

AIRCRAFT N14075 DEPT. FROM LIRN TO KNGU AT 2100Z WHILE AIRCRAFT CRUISING AFTER 5 HOURS AND 40 MIN.APPROX. 0240Z (ACCORDING TO THE CAPTAIN REPORT) THE ACFT. SHUDDERED AND BOUNCED FOR APPROX. 1/2 SECOND, THEN RETURNED TO STABLE FLIGHT, ACFT. CONTINUE TO KNGU AND HAD NORMAL LANDING AND NO CONTROL PROBLEMS. THE GROUND CREW NOTED THE NR 2 ENGINE COWL DOOR LT & RT SIDE WAS MISSING, SIGNIFICANT DAMAGE TO R/H INBOARD ELEVATOR WITH THE TAILCONE DISPLACED BUT ATTACHED.

Part: LIGHT — INOPERATIVE (ROW 21J)

EMERGENCY ISLE LIGHT INOPERATIVE AT 21J. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED GOOD

Part: HEAT EXCHANGER — LEAKING (PNEUMATIC SYS)

NR 2 PNEUMATIC MANIFOLD FAILURE LIGHT ILLUMINATED WITH TWO PACKS OFF AND TWO PNEUMATIC SYSTEMS OFF. AGAIN EXECUTE VOL II 01-10-09 EMERGENCY PROCEDURE. FOUND EXCESSIVE HOT AIR LEAKAGE FROM NR 1 AND NR 2 HEAT EXCHANGERS TO BOTH ACM'S CONNECT SLEEVES AND FROM BOTH HEAT EXCHANGERS TO PLENUMS INTERFACE. SECURED NR 2 PACK SLEEVES AND HEAT EXCHANGER TO PLENUMS. LEAK CHECK FOUND GOOD DURING TEST WITH MODERATE PWR ON ALL 3 ENGINE. NO AMC NR 2/3 OR PNEUMATIC SYSTEMS FAULTS NOTED. VISUALLY CHECKED ACCESSIBLE NR 2 MANIFOLD AND NO OBSERVED LEAKS NOTED. DEFERRED NR 1 PACK INOPERATIVE IAW MEL 21-1 ESTABLISHED ON NR 1 ENTERED DMI M21JUU23-44, HEAT EXCHANGER LEAK. AIRCRAT RETURNED TO LGSA FOR REPAIRS. REMOVED AND REPLAC

Part: CONTROL CABLE — BROKEN (RUDDER)

LEFT RUDDER CABLE BROKE AT APPROXIMATE STATION 1920. REPLACED RUDDER LEFT CONTROL CABLE SEGMENT 1D AND PERFORMED RIGHT CHECK IAW DC-10 MM 27-20-00. RIG CHECKED ACCOMPLISHED. FOUND CHAFED WIRE HARNESS FOR L4 FLIGHT ATTENDANT CONTROL PANEL BELOW FLOOR AT APPROXIMATE STATION 1820. ACCOMPLISHED WIRING REPAIR IAW SWP 20-10-01. REPLACED RUDDER CABLE AND REPAIRED CHAFED WIRES. (M)

Part: TERMINAL — BURNED (ACCY BAY)

DURING PREFLIGHT SERVICING, AC BUS NR 1 CIRCUIT BREAKERS POPPED. FURTHER NOTED TERMINAL STRIP BURNED IN CENTER ACCESSORY COMPARTMENT. ACCOMPLISHED ALL NECESSARY REPAIRS. REPLACED THE FOLLOWING COMPONENTS REPAIRED TERMINAL STRIP S3521, LUGS ON FEEDER TO THE TERMINAL STRIP AND DATA PLATE FOR TERMINAL STRIP. WITH INSPECTION OF THE FEEDERS AND INSULATION. THE FOLLOWING OTHER COMPONENTS WERE REPLACED DC BUS TIE C/B NR 1 (B15), AC BUS NR1 B PHASE C/B (B17) AND AC BUS NR 1 C PHASE C/B (B18). REPLACED COMPONENTS, TERMINAL STRIP.

Part: CONTROL VALVE — FAILED (OUTBOARD FLAPS)

AFTER TAKEOFF OB FLAP FAILED TO RETRACT-CONFIRMED BY FLAP INDICATIONS TAPES AND PHYSICAL INSP. COMMENCING FUEL DUMP TO RETURN, FLAPS RETRACTED ON THERE OWN AND OPERATED NORMALLY FOR LANDING. DETERMINED LT OB FLAP AND RT OB FLAP ONE DID REMAIN EXTENDED AFTER HANDLE WAS POSITIONED TO RETRACT POSITION. REMOVED ALL REAR SPAR LWR PANELS AND FLAP HINGE TO FLAP CONTROL VALUE ASSYS. RESCUED PILOT OVERRIDE CLAPPER CABLE. SUSPECT POSSIBLE OB FLAP CONTROL VALUE LT OR RT MALFUNCTION. REMOVED AND REPLACED LT AND RT OUTBOARD CONTROL VALUE ASSEMBLIES. ACCOMPLISHED FLAP OPS AND LEAK CHECKED. WITH NO DEFECTS NOTED. ALL PANELS REMOVED TO ACCOMPLISH CABLE ASSEMBLY. RUNS RESCUED. REPLACED BOTH OB FLAP CONTROL VALUES.

Part: GPS — FAILED (COCKPIT)

AIRCRAFT RETURNED TO FRANKFORT DUE TO GPS NAVIGATIONAL ERROR. RESET GPS (ALL THREE UNITS) BY SWAPPING NAVIGATIONAL DATA, TO EXPIRED DATA BASE AND BACK TO ACTUAL NAVIGATIONAL DATA BASE. ALL FUNCTIONS BACK TO NORMAL. DATA BASE RELOADED. (M)

Part: SLIDE — DEPLOYED (PAX DOOR)

DEPLOYED L1 SLIDE PER WORLD AIRWAYS WORK CARD NON ROUTINE TASK CARD AND DC-10 AIRCRAFT MAINTENANCE MANUAL. SLIDE FAILED TO FULLY DEPLOY DUE TO 2 EACH RETENTION CABLES BEING HUNG UP IN THEIR RETAINERS, ALSO DUE TO THE FAILURE TO FULLY DEPLOY, THE PRESSURE RELIEF VALVE OPENED RELEASING PRESSURE FROM THE SLIDE. WHEN THE SLIDE CABLES WERE RELEASED, THE SLIDE FELL OPEN, HANGING LOOSELY FROM THE SIDE OF THE AIRCRAFT. SLIDE LAST OVERHAULED 06-2000. REMOVED AND REPLACED L1 DOOR SLIDE. (M)

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 87,495 hrs · 19,150 cycles

INSPECTION FOUND LT WING FUEL TANK ACCESS PANELS 534BT, 534AT, AND 539CB DAMAGED. THE PANELS WERE REPLACED IAW MM 57-31-00.

Part: BRACKET — CRACKED (TE FLAPS) · airframe 87,495 hrs · 19,150 cycles

INSPECTION FOUND A .5 INCH CRACK IN LT WING O/B FLAP AFT HINGE UPPER BRACKET. A NEW BRACKET WAS INSTALLED IAW SRM 51-31-01.

Part: RIB — CRACKED (NR 2 PYLON) · airframe 87,495 hrs · 19,150 cycles

INSPECTION FOUND A 6 INCH CRACK IN NR 2 PYLON SAILBOAT FAIRING LOWER RIB. REPAIR WAS COMPLETED IAW ECRA 5412-01011, SRM 51-31-01, AND DOUGLAS DRAWING AVB7306.

Part: BULKHEAD TEE — CORRODED (BS 2007)

INSPECTION FOUND ANGLE TEE ATTACHED TO PRESSURE BULKHEAD AT STA 2007, LBL 5 CORRODED. THE ANGLE TEE WAS REPAIRED IAW SRM 53-40-00, FIGURE 16.

Part: TIP — BENT (LT&RT ELEVATOR)

INSPECTION FOUND THE LEFT AND RIGHT I/B ELEVATOR T/E TIPS BENT. THE BENT AREAS WERE TRIMMED OUT AND NEW EDGE PORTIONS WERE INSTALLED IAW SRM 55-30-00, FIGURE 2 51-35-02, AND 51-31-01.

Part: SKIN — CRACKED (NR 2 PYLON)

INSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON PRE-COOLER CUTOUT AT RT SIDE. THE CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH A REPAIR ANGLE IAW ECRA 5450-01283.

Part: CONTROLLER — INOP (NR 1 PACK)

THE AIRFLOW FROM PACKS WERE NOT EFFICIENT DURING FLIGHT. THE NR 1 PACK WAS PLACED IN MANUAL AND FLOW WAS ZERO. UPON INCREASING FLOW ON NR 1 PACK, THE CABIN RATE INCREASED TO 1,000 FEET IN STANDBY AND SMOKE ENTERED THE COCKPIT. THE NR 1 PACK WAS PUT TO FULL COLD IN MANUAL AND THE SMOKE CEASED. THE AIRCRAFT WAS RETURNED TO SCL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ZONE TEMP CONTROLLER. THE NR 1 ENGINE WAS RUN WITH THE NR 1 PACK AT FULL HOT FOR 45 MINUTES IAW MM 21-60-00 AND NO SMOKE WAS DETECTED.

Part: BATTERY PACK — DISCHARGED (CABIN)

THE EMERGENCY LIGHTS WOULD NOT TEST DURING PREDEPARTURE CHECK. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK AND CHARGER AND OPERATION CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN)

THE EMERGENCY LIGHTS WOULD NOT TEST ON PREDEPARTURE CHECK. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK AND CHARGER AND OPERATIONAL CHECKS WERE GOOD.

Part: RIB — CRACKED (WS 1042-1192)

INSPECTION FOUND A 1 INCH CRACK IN LT WING FIXED LEADING EDGE RIB BETWEEN XFS 1042 AND XFS 1192. THE RIB WAS REMOVED. A NEW PART WAS INSTALLED IAW SRM 57-21-00 FIGURE 8, 51-21-01 AND 51-31-01.

Part: ANGLE — CRACKED (LT & RT WING)

INSPECTION FOUND A 1.6 INCH CRACK ON RT AND LT WING INBOARD ISLAND LOWER AFT INBOARD SPLICE ANGLE OF RIB. THE SPLICE ANGLE WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 57-22-01, FIGURE 2, 51-21-01, AND 51-33-01.

Part: FRAME — CORRODED (BS 1721 & 1780)

INSPECTION FOUND CORROSION ON LOWER FLANGE OF FRAMES IN CENTER CARGO COMPARTMENT AT STA 1721 BETWEEN STRINGER 50L AND 50R AND AT STA 1780 BETWEEN STRINGER 50L AND 50R. THE CORRODED OUTER CAPS OF FRAMES WERE TRIMMED OUT. THE AREAS WERE REINFORCED WITH OUTER CAPS AND DOUBLERS IAW SRM 57-21-00, FIGURE 8, 53-30-00, FIGURE 5, 51-21-01 AND 51-31-01.

Part: CAP — CRACKED (LT HORIZ STAB)

INSPECTION FOUND A 6 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE INBOARD SIDE CAP AT L3. THE CAP WAS REMOVED AND A NEW CAP WAS INSTALLED IAW SRM 51-33-01 AND 55-12-01.

Part: SKIN — CORRODED (BS 1520-1560)

INSPECTION FOUND CENTER CARGO COMPARTMENT INTERIOR SKIN SWELLING AT STA 1520 TO 1560 BETWEEN STRINGER 45R AND 46R. THE SKIN WAS REPAIRED IAW ENGINEERING ORDER MF-MAN-D10-53-86829.

Part: CAP — CRACKED (LT HORIZ STAB)

INSPECTION FOUND AN 11 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE LOWER OUTBOARD CAP AT L4. THE CAP WAS REMOVED AND A NEW CAP WAS INSTALLED IAW SRM 51-21-01, 51-31-01, AND 55-12-01, FIGURE 3.

Part: SUPPORT — CORRODED (BS 1920-2007)

INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 1920 AND 2007, RBL 55. THE FLOOR SUPPORT WAS REMOVED. A NEW PART WAS INSTALLED IAW SRM 51-31-01.

Part: SUPPORT — CORRODED (BS 1910)

INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED AT STA 1910, LBL 25. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-31-01.

Part: SUPPORT — CORRODED (BS 1887)

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1887 BETWEEN RBL 0 - RBL 25, RBL 25 - 35, RBL 35 - 60, AND RBL 60 - 90. THE FLOOR SUPPORTS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-31-01.

Part: SUPPORT — CORRODED (BS 1900)

INSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1900, LBL 6 AND RBL 6. THE FLOOR SUPPORTS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-31-01.

Part: SUPPORT — CORRODED (BS 1887)

INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1887 BETWEEN LBL 35 & 45 AND BETWEEN LBL 45 & 90. THE FLOOR SUPPORTS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-31-01.

Part: SUPPORT — CORRODED (BS 460)

INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 460, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-31-01.

Part: FASTENER — FAILED (WS 402)

RIVET HEAD POPPED ON LEFT WING LOWER SKIN FWD OF REAR SPAR WING STA XORS402, JUST OUTBOARD OF SAILBOAT PANEL. REMOVED AND REPLACED FASTENER PER SRM 51-33-01.

Part: DUCT — SEPARATED (NR 1 ENGINE)

THE NR 1 ENGINE HAD A FIRE WARNING AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. INITIAL FINDINGS REVEALED NR 1 ENGINE 14TH STAGE DUCT SEPARATION. THE AIRCRAFT WAS TAKEN OUT OF SERVICE FOR REPAIR. THE 14TH STAGE DUCT WAS REMOVED AND REPLACED. IN ADDITION, THE ENGINE WAS BOROSCOPED DUE TO HIGH EGT EXPERIENCED AND NO DAMAGE WAS FOUND. AN ENGINE RUN WAS PERFORMED AND OPERATION CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 2007)

INSPECTION FOUND FLOORBEAM CORRODED AT JOINT TO BULKHEAD TO T-CAP ANGLE, STA 2007(J LAV). THE FLOORBEAM WAS REPAIRED IAW SRM 53-70-00.

Part: FILLET — MISSING (LT WING)

INSPECTION FOUND THAT A PORTION OF THE LT WING UPPER FILLET FAIRING WAS MISSING DURING A WALKAROUND AFTER AIRCRAFT ARRIVED IN FRA. INSPECTION OF THE AIRCRAFT REVEALED THE ATTACH SCREWS HAD PULLED THROUGH THE FIBERGLASS PANEL (FILLET) AND THE ATTACH SCREWS WERE STILL ON THE AIRCRAFT. THE FILLET WAS NEVER RECOVERED. AN AIRWORTHY REPAIR WAS PERFORMED IAW ECRA 5350-01325 AND A DIP WAS ISSUED TO REINSPECT THE REPAIR FOR SECURITY AT EACH SERVICE CHECK AND TO REPLACE THE FAIRING WITHIN 500 HOURS. IN ADDITION, THE NR 2 ENGINE AND LT SIDE OF AIRCRAFT WERE INSPECTED AND NO DAMAGE WAS FOUND.

Part: SHUTOFF VALVE — LEAKING (NR 3 HYD SYST)

THE NR 3 HYDRAULIC SYSTEM QUANTITY DROPPED APPROXIMATELY TWO GALLONS SHORTLY AFTER TAKEOFF. THE QUANTITY STABILIZED FOR A SHORT WHILE AND THEN BEGAN TO SLOWLY DECREASE. THE HYDRAULIC LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE SHUTOFF VALVE TO 2-3 NON-REVERSIBLE MOTOR PUMP LEAKING. THE SHUTOFF VALVE WAS REPLACED, LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: OVERFLOW VALVE — STICKING (WATER SERV PNL)

INSPECTION FOUND THE LT WING NR 1 LEADING EDGE SLAT DENTED IN SEVERAL PLACES AFTER AIRCRAFT ARRIVED. THE DENTS WERE CAUSED BY IMPACT FROM ICE. MAINTENANCE FOUND THE NR 2 WATER TANK SYSTEM LEAKING AT SERVICE PANEL. THE DRAIN T-HANDLE COULD NOT BE STOWED AND WAS BINDING. THE NR 2 TANK OVERFLOW VALVE ASSEMBLY WAS FOUND TO BE STICKING, AND NOT ALLOWING THE FILL/DRAIN VALVE ASSEMBLY TO CLOSE. THE OVERFLOW VALVE WAS REMOVED AND REPLACED, LEAK AND OPERATIONAL CHECKS WERE GOOD. THE NR 1 LEADING EDGE SLAT WAS REMOVED AND REPLACED IAW MM 27-80-01 CONFIGURATION 1 PAGE 401.

Part: FUEL SO VLV — OUT OF RIG (NR 2 ENGINE)

THE NR 2 ENG SPOOLED DOWN TO IDLE RPM SHORTLY AFTER TAKEOFF. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED. MAINTENANCE FOUND THE NR 2 ENG FUEL PUMP HAD FAILED. THE NR 2 ENG FUEL PUMP WAS REMOVED AND REPLACED. IN ADDITION, THE FUEL/OIL HEAT EXCHANGER AND ENG FUEL CONTROL WERE REPLACED AS A PRECAUTIONARY MEASURE. FUEL LEAK CHECKS WERE ALSO GOOD. *S/D* THE FUEL PUMP AND FUEL CONTROL UNIT WERE BOTH TESTED IAW THE CF6 COMPONENT MM AND NO TROUBLE WAS FOUND. THIS AIRCRAFT HAD AN ABORTED TAKEOFF THE FOLLOWING DAY (10/24) FOR THE SAME PROBLEM. ENGINEERING REPORTED THAT THE NR 2 ENGINE FIRE SHUTOFF VALVE WAS RERIGGED AT THAT TIME, AND IT CORRECTED THE PROBLEM.

Part: FAIRING — DAMAGED (LT WING/FUS)

THE LT WING INBOARD SLAT TO FUSELAGE FAIRING WAS FOUND DAMAGED ON ARRIVAL. ICE DAMAGE WAS SUSPECT DUE TO THE NR 2 WATER SYSTEM WAS FOUND LEAKING FROM OVERFLOW AT SERVICING PANEL. THE NR 2 WATER SYSTEM WAS EMPTY ON ARRIVAL. THE NR 2 WATER SYSTEM WAS PLACARDED INOPERATIVE. THE FAIRING WAS REPAIRED IAW ECRA 5350-01284. A DIP WAS ISSUED TO REINSPECT THE REPAIR EVERY FLIGHT UNTIL A PERMANENT REPAIR IS ACCOMPLISHED WITHIN 15 DAYS.