N987DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,958 hrs · 51,416 cycles

ON SERVICE CHECK, SOME CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY PATH LIGHTS AT 20DE, 23DE, AND 29DE. ALSO REPLACED BATTERIES IN EMERGENCY LIGHT BATTERY PACKS B5-100, B5-102, B5-103, B5-107, B5-27. EMERGENCY LIGHTS NOW TEST GOOD. (LP #4753454)

Part: THRESHOLD — CRACKED (L2 DOORWAY) · airframe 70,309 hrs · 50,837 cycles

L2 DOOR THRESHOLD FWD HALF WAS CRACKED AT THE FWD HOLE. REMOVED AND REPLACED THE THRESHOLD IAW DWG 5936441.

Part: WIRE — SHORTED (CABIN) · airframe 70,141 hrs · 50,690 cycles

EMERGENCY EXITLIGHTS ROWS 32 AND AFT INOP. FOUND WIRE L982T14 SHORTED TO GND. REPAIRED PER SWPM CHAPTER 20. ALSO REPLACED B5-212 PWR SUPPLY BASE PER AMM 33-53. OPERATION CHECKS OK.

Part: COVER — MISSING (CABIN) · airframe 70,024 hrs · 50,592 cycles

THE RIGHT AFT OVERWING EXIT LIGHT COVER IS MISSING. CONTRACT MAINTENANCE INSTALLED A NEW LIGHT COVER. OPERATIONAL CHECK WAS GOOD REF AMM 33-53. AIRCRAFT OK FOR SERVICE.

Part: FUSE — BLOWN (CABIN) · airframe 69,600 hrs · 50,252 cycles

SEAT 31 BACK EMERGENCY LIGHTS INOP. REPLACED FUSE PER CMM 25-60-03 OPS CHECK PER AMM 33-53.

Part: FUSE — BLOWN (CHARGER) · airframe 69,278 hrs · 50,016 cycles

SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE ROWS 31-36. FOUND THE BATTERY PACK CHARGER WITH A BLOWN FUSE. REPLACED THE FUSE. TESTED NORMAL.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 69,278 hrs · 50,016 cycles

AT 5000 - 6000 FT DURING CLIMB, THE RT ENGINE PRODUCED A LOUD BANG , SUDDEN ROLLBACK, GOOD OIL PRESSURE, N2 APPROXIMATELY 5 PERCENT . PERFORMED QRH, AND SHUTDOWN WAS NORMAL. EMEREGENCY DECLARED, EXCESSIVE OIL LEAK. CHANGED THE NR 2 ENGINE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,959 hrs · 49,794 cycles

UPPER SIDEWALL EMERGENCY SIGN HAS ONE LAMP INOPERATIVE. REPLACED THE LAMP IAW AMM 33-53. OPS NORMAL.

Part: SLIDE — FAILED (DOOR) · airframe 68,782 hrs · 49,664 cycles

FWD LEFT DOOR SLIDE FAILED W/C 2561-2001 SLIDE PIN ENGAGE. R&R LEFT FWD DOOR SLIDE PER W/C 2561-4964.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 68,377 hrs · 49,362 cycles

EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS. CHECKED NORMAL.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 68,336 hrs · 49,329 cycles

PANEL 6301A, INTERNAL DOUBLER IS CRACKED. REPAIRED PER ERA 563169-14 REV ORIGINAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,336 hrs · 49,329 cycles

CORROSION AT AFT LAV SERVICE PANEL, LOWER AFT CORNER. REPAIR COMPLETED AS PER ERA 563040-14 REV ORIG. TIME CONTROL ITEMS TO BE ACCOMPLISHED ON LOG 0293411.

Part: DOOR — BENT (AFT CARGO) · airframe 68,336 hrs · 49,329 cycles

AFT CARGO DOOR BENT ON THEAFT FRAME AT TORQUE TUBE. THE CARGO DOOR WAS REPLACED.

Part: LIFE RAFT — DAMAGED · airframe 68,336 hrs · 49,329 cycles

FWD CABIN CEILING LIFE RAFT TEMPERATURE INDICATORS SHOW TEMP GREATER THAN 160 DEGREES F. REFERENCED AMDS 2520-2573 STEP 8 FOR DISPOSITION. BOTH LIFE RAFTS REPLACED

Part: CABLE — FRAYED (TAILCONE) · airframe 68,336 hrs · 49,329 cycles

THE TAILCONE CABLE ASSY. (MID LOOP) FRAYED. REPLACED CABLE ASSY, REF AMM 53-53-02.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 66,653 hrs · 48,083 cycles

DURING DESCENT, BOTH AFT LAVATORY SMOKE DETECTORS SOUNDED AND THEN STOPPED BY THE TIME THE ACFT WAS ON THE RUNWAY. NO SMOKE OR HAZE WAS SEEN, ENGINE ANTI-ICE WAS IN USE DURING THE DESCENT AND TURNED OFF ON SHORT APPROACH. IAW AMDS CARD 2120-2367 RAN THE LT & RT ENGINES, NO SMOKE IN CABIN, BUT OIL ODOR WAS PRESENT. INSPECTED THE LT & RT COALESCER BAGS, NO OIL PRESENT, BUT HAD AN OIL ODOR. REPLACED THE COALESCER BAGS IAW AMM 21-20. FOUND SLIGHT RESIDUE ON RT ACM OUTLET DUCT. VERIFIED NO ELECTRICAL ODOR PRESENT IN ACFT.. ACFT OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 66,651 hrs · 48,081 cycles

SEAT 14 ED EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW CONNECTORS IAW SWPM 20. OPS CHECKED OK. OK FOR SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 66,651 hrs · 48,081 cycles

FIRST EMERGENCY LIGHT AFT OF REAR CABIN DOOR INOPERATIVE. REPLACED BROKEN WIRE SPLICE IAW AMM 33-53. CHECKED GOOD. OK FOR SERVICE.

Part: ACM — FAULTY (AC BAY) · airframe 66,408 hrs · 47,897 cycles

ON SHORT FINAL TO LAND, SMELLED A BURNING SMELL IN COCKPIT & ALARMS IN AFT LAVS WENT OFF. PASSENGERS & FWD FLT ATTENDANT REPORT A HAZE SEEN IN CABIN FROM UNKNOWN SOURCE. FOUND 2 DUCTS BLOWN OUT AND OIL IN ACM. REPAIRED DUCTS AND REPLACED ACM REF AMM 21-20. NEEDS CK OUT. REMOVED APU DOORS & WASHED APU INLET. FOUND 575 DEG THERMOSTAT BLOWN OUT RT SIDE, REPLACED SAME AMM 21-61-07. C/W WORK CARD 7100-2619 PNEU SYS DUCT BURNOUT AND WORK CARD 2170-4139 WATER BAGS REPLACEMENT. NO LEAKS. RAN BOTH ENGS TO CLIMB POWER WITH PACKS OPERATING. NO SMELL.

Part: CAM — DAMAGED (TAILCONE) · airframe 66,354 hrs · 47,855 cycles

DURING TAILCONE FINCTIONAL CHECK, FOUND TAILCONE CAM ASSEMBLE WORN. REPLACED CAM ASSY BASE IAW MD88 AMM 53-53-02 REQUIED INSPECTION COMPLETE. (LP2846437)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,336 hrs · 47,843 cycles

FWD ENTRY AND FLIGHT DECK EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACKS IAW AMM 33-58. OPS CHECKED GOOD.

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 66,318 hrs · 47,828 cycles

17DE EMERGENCY LIGHT INOPERATIVE. R & R THE SOCKET AND OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 66,255 hrs · 47,790 cycles

DURING APPROACH WITH ENGINE AND WING ANTI-ICE ON, F/A REPORTED BOTH AFT SMOKE DETECTORS ACTIVATED. F/A REPORTED SHE SMELLED A BURNING ODOR JUST BEFORE SMOKE DETECTOR ACTIVATED. FIRST OFFICER ALSO NOTED BURNING ODOR FROM HIS VENT . SELECTED WING ANTI -ICE OFF AND SMOKE DETECTOR WENT SILENT AFTER ABOUT 2 MINS. APU INLET CONTAMINATION SUSPECTED. NO OTHER TROUBLE FOUND. CLEANED APU INLET AND PERFORMED DUCT BURN.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 64,582 hrs · 46,572 cycles

MAINTENANCE FOUND AN EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 22ED. THE CONNECTOR WAS REPINNED AND THE LIGHT CHECKED OK.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 64,441 hrs · 46,470 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHTING INOPERATIVE FROM ROW 24 DEF TO THE BACK OF THE CABIN. FUSES F1 AND F2 WERE REPLACED IN BATTERY PACK B5-212. THE LIGHTS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,174 hrs · 46,290 cycles

MAINTENANCE FOUND 2 EMERGENCY LIGHTS INOPERATIVE AT THE G2 COAT CLOSET. BOTH LIGHT ASSEMBLYS WERE REPLACED.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 63,694 hrs · 45,974 cycles

MAINTENANCE FOUND EMERGENCY LIGHTING INOPERATIVE AT SEAT ROWS 31-36. AN OPEN SPLICE WAS FOUND AT SEAT ROW 31 AND REPAIRED. THE EMERGENCY LIGHTS CHECKED OK.

Part: FRAME — CRACKED · airframe 63,330 hrs · 45,708 cycles

CRACKED FRAME BEHIND DOOR STOP FITTING NR 2 AT AFT EDGE OF C1 DOOR. REPAIR WAS ACCOMPLISHED IAW ETI-88-15-352, REV 3 AND ERA 539874-14, REV ORIGINAL.

Part: BEAM — CORRODED (BS 1154-1174) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON LOWER BEAM UNDER PREVIOUS REPAIR DOUBLER BETWEEN BS 1154 - 1174. THE BEAM WAS REPAIRED IAW ER/A NR 539872-14, REV ORIGINAL.

Part: DUCT — CRACKED (COOLING EXHAUST) · airframe 63,330 hrs · 45,708 cycles

CRACKED RADIO RACK COOLING EXHAUST DUCT AT FUSELAGE SKIN. RADIO RACK EXHAUST DUCT WAS REPAIRED IAW ER/A 464964-14MA, REV C.

Part: SKIN — DENTED (LT ELEVATOR TAB) · airframe 63,330 hrs · 45,708 cycles

DENTS ON LT ELEVATOR GEARED TAB UPPER SKIN. CARD 02, ZONE 65. DENTS ON LT ELEVATOR GEARED TAB UPPER SKIN WERE REPAIRED IAW SRM 55-04, PAR 2, OPN 1031.

Part: SKIN — WORN (LT WING) · airframe 63,330 hrs · 45,708 cycles

WEAR ON LT L/E PREVIOUS REPAIR DOUBLER AT LT WING BETWEEN BS XRS=509 TO XRS=531. CARD 2, ZONE 11 L/E WAS REAPAIRED IAW ER/A 47800-14, REV B AND ETI -88-15-363, REV 2.

Part: FLOOR SUPPORT — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON FLOOR SUPPORT BS 1155 AND 1212, LONGERONS 28 - 29R. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON SETTLEMENT AREA AT LT WING ACCESS PANEL 1303C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 1409C ON RT WING. THE ACCESS PANEL WAS REPLACED.

Part: SPAR — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON LT HORIZONTAL STABILIZER REAR SPAR XE=225. REPAIRED IAW ER/A 539890-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON COUNTERSINK AT LT FUEL TANK NR 1371C. ACCESS WAS REPAIRED IAW SRM 51-22-2A AND COUNTERSINK HOLES WERE MEASURED AND MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS .561" IN 3 HOLES THEREFORE IS WITHIN LIMITS AND WAS REPAIRED UNDER CONDITION II IAW SRM 51-22-2A.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON RT CARGO TRACK BETWEEN BS 1212 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1, 51-10-4, 51-30-2, AND 51-10-3, PAR 21, 14, AND 38.

Part: CARGO TRACK — CORRODED (BS 1212-1236) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON SPLICE BETWEEN BS 1212-1236 AND LT TIE TRACK AT AFT CARGO COMPARTMENT. SPLICES WERE REPLACED IAW SRM 51-30-5 , 51-10-4 AND 51-10-3 PAR. 21,14 AND 38.

Part: CARGO TRACK — CORRODED (BS 1003-1322) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 1003 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1, 51-10-4, 51-10-3, AND 51-30-2.

Part: FRAME — CRACKED (BS 1322) · airframe 63,330 hrs · 45,708 cycles

CRACK ON FRAME AT BS 1322 AND LONGERON 17L. THE FRAME WAS REPAIRED IAW ER/A 493697-14MA, REV B.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON COUNTERSINK ON LT WING ACCESS PANEL NR 1367C. ACCESS PANEL WAS REPLACED.

Part: HINGE — WORN (LT PYLON) · airframe 63,330 hrs · 45,708 cycles

FREEPLAY ON UPPER HINGES OF HARDWARE ON YN=80, NR 1, YN=100 NR 2, YN=184 NR 3 AND YN=214 NR 4, LT APRON PYLON. UPPER HINGES ON BS YN=80, YN=184, AND YN=214 AT LT APRON PYLON WERE REPAIRED AND HARDWARE REPLACED AND FREE PLAY WAS CORRECTED IAW CMM 71-10-10 AND HINGE BS YN=100 WAS REPLACED IAW CM 71-10-10 AND EA 09-372728-14, REV. B FC9-71-10. FREE PLAY WAS CORRECTED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON COUNTERSINK AT RT WING ACCESS PANEL 1472C. THE ACCESS PANEL WAS REPLACED AND COUNTERSINK WERE MEASURED AND MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS .620" IN, 5, HOLES THEREFORE IS OUT OF LIMITS IAW SRM 51-22-2A.

Part: SUPPORT — CORRODED (BULKHEAD) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON AFT BULKHEAD PANEL SUPPORTS AT AFT CARGO COMPARTMENT UPPER, LT, RT AND CENTER SIDE. CORROSION ON LT AND RT SUPPORTS PANELS BULKHEAD WAS ATTENDED WITH MEASSURED AS FOLLOW: UT, WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1-2. ORIGINAL THICKNESS IS 0.040" AND REMAINING THICKNESS IS 0.038" THEREFORE ITS WITHIN LIMITS IAW ER/A 511165-14, MA REV C AND DUE TO EXCESSIVE DAMAGE SUPPORT CENTER WAS REPLACED IAW SRM 53-24-0.

Part: LONGERON — CORRODED (BS 1446-1463) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON END LONGERON 12L BETWEEN BS 1446 TO 1463. LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5,53-01 FIG 1,51-10-01, FIG 14.

Part: SKIN — CORRODED (BS 1180-1200) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON SKIN BELOW OF LONG 26 LT BETWEEN BS 1180 - 1200 AT AFT CARGO COMPARTMENT. FINGER DOUBLER WAS REPAIRED IAW SRM 53-04, FIG 12D AND 12E.

Part: DOUBLER — CRACKED (LT MLG WW) · airframe 63,330 hrs · 45,708 cycles

CRACK LT MLG UPPER DOUBLER AT LT WING XCW 110. UPPER DOUBLER WAS REPAIRED IAW SRM 57-03, FIG 34 AND SRM 51-30-5, SRM 51-10-3, PAR 14, 21.

Part: FRAME — CORRODED (BS 1287) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON FRAME BS 1287 BETWEEN LONGERONS 29L TO 29R AT AFT CARGO COMPARTMENT. FRAME WAS REPAIRED IAW SRM 53-03, FIG 2A.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,330 hrs · 45,708 cycles

CRACK ON AFT OUTPAN BELOW STOP FITTING NR 5. AFT OUTPAN WAS REPAIRED IAW ER/A 539914-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1458) · airframe 63,330 hrs · 45,708 cycles

CRACKED FRAME ANGLE AT BS 1458 AT LONGERONS 2L AND 2R. FABRICATED AND INSTALLED IAW DWG 9911860, REV 2 AND SRM 51-10-3, PARTS 21, 14 AND 51-30-5.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 63,330 hrs · 45,708 cycles

LIGHTNING STRIKE AND GOUGE ON LT INBD FLAP LOWER SKIN BETWEEN BS XW 89 TO XW 99. CARD 17, ZONE 10. LIGHTNING STRIKE IN BS XW-99 WAS ATTENDED IAW SRM 57-01, FIG 1, UT, WAS ACOMPLISHED IAW NDT 04-00-07, FIG 3, SHEET 1 ORIGINAL THICKNESS IS 0.040" AND MINIMUM REMAINING IS 0.038" THEREFORE IS WITHIN LIMITS IAW SRM 57-01, FIG 1 AND GOUGE IN BS XW-89 WAS REPAIRED IAW SRM 57-03D, FIG 8, SRM 51-10-3 PAR 21, SRM 51-30-8.

Part: FORMER — CRACKED (BS 1458) · airframe 63,330 hrs · 45,708 cycles

CRACKED FORMER BS 1458, BESIDE LONGERON 3L AT AFT ACCESSORIES COMPARTMENT. THE FORMER WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: RIB — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON RIB HOLE XIS 83, XIS 136 AND XIS 186 AT LT SLAT PANEL NR 1. RIB HOLES WERE REPAIRED IAW SRM 57-02, PAR 9.

Part: DOOR FRAME — CORRODED · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME AFT WEB BTW LONGERONS 27R-28R, AND FWD WEB BETWEEN LONGERONS 25R-26R. IN REF OR NRC CARD 145, ZONE 201. 20000080586. CORROSION ON WEB DOOR JAMB Y=1155 AND Y=1212 WERE REPAIRED IAW SRN 53-01, FIG 2, SHEET 3.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON COUNTERSINK ELONGED HOLE AND TOOL MARK ON RT WING FUEL ACCESS NR 1470C. ADJACENT HOLES THEREFORE WAS FOUND OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A AND ACCESS PLATE NR 1470C WILL BE INSTALLED UNDER CARD JIC 2800-0390.

Part: DOOR FRAME — CRACKED (BS 937) · airframe 63,330 hrs · 45,708 cycles

CRACK ON DOUBLER REPAIR UPPER BS 937 MLG DOOR JAMB FWD FRAME, RT SIDE. NEW CHANEL WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3, PAR 21 AND 14, DWG 5930584, REV.

Part: BEAM — CRACKED (NR 4) · airframe 63,330 hrs · 45,708 cycles

CRACK ON BEAM NR 4 BETWEEN FWD PAN AND FWD FRAME AT FWD SERVICE DOOR. BEAM NR 4 WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9911582, REV T.

Part: SKIN — PUNCTURED (CARGO DOOR) · airframe 63,330 hrs · 45,708 cycles

PUCTURES ON INNER SKIN AT FWD CARGO COMPARTMENT DOOR. PUCTURES ON INNER SKIN AT FWD CARGO COMPARTMENT DOOR BARRIER, C1, WERE REPAIRED IAW SRA 094625-14MA, REV.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 63,330 hrs · 45,708 cycles

DELAMINATED AND DAMAGE FERRULES ON FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201. REPLACED IAW AMM 53-20-01-201.

Part: FRAME — CRACKED (BS 1322) · airframe 63,330 hrs · 45,708 cycles

CRACK ON FRAME AT BS 1322 BETWEEN LONGERON 12L TO 13L. CRACK ON FRAME AT BS Y=1322 BETWEEN LONGERON 12L TO 13 LT WAS REPAIRED IAW SRM 53-03D, FIG 4,

Part: SEAL DEPRESSOR — CORRODED (BS 1350) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION UNDER SEAL DEPRESSOR AT VENTRAL LOWER DOOR JAMB BS 1350, LBL 34. VENTRAL LOWER DOOR JAMB WAS REPAIRED IAW ERA 539881-14, REV ORIGINAL AND ETI -88-15-357, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON COUNTERSINK AT RT WING FUEL ACCESS NR 1466C. PANEL WAS REPLACED FOR A NEW AND PN VERIFICATED IAW IPC 57-30-00 AND WILL BE INSTALLED UNDER JIC 2800-0390, JOB 001-0402 AND STICK WAS INSTALLED IAW AMM 28-40-02.

Part: INTERCOSTAL — CORRODED (BS 1147-1155) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1147-1155 AND BETWEEN LONGERON 30-29R. A NEW INTERCOSTAL WAS FABRICATED, AND INSTALLED IAW D5936071, REV F 51-10-2 AND 51-10-4.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON SEATING AREA AND COUNTERSINK AT LT WING ACCESS PLATE NR 1377C, AYP, CARD 118, ZONE 00. CORROSION ON COUNTER SINK WAS REMOVED AND COUNTERSINK HOLES WERE MEASURED, MAXIMUM DIAMETER AVALIBLE IS "0.532" AND MAXIMUM DIAMETER MEASURED IS "0.544" IN, 7 HOLES, THEREFORE, FOUND OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A AND ACCESS PLATE NR 1377C WILL BE INSTALLED UNDER CARD JIC 2800-0120, JOB 001-0396.

Part: FLOOR PANEL — PUNCTURED (COCKPIT) · airframe 63,330 hrs · 45,708 cycles

SEVERAL PUNCTURES ON FLOOR PANEL NR 120A AT COCKPIT. . FLOOR PANEL NR 120A AT COCKPIT WAS REPLACED IAW AMM 20-30-01.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON COUNTERSINK OF RT WING FUEL ACCESS NR 1454C. CORROSION ON COUNTERSINK WAS REMOVED. COUNTERSINK HOLES WERE MEASURED. MAX DIAMETER ALLOWABLE IS ".532" AND MAX DIAMETER MEASURED IS .541 IN 3 HOLES ADJACENT. THEREFORE IT IS OUT OF LIMITS AND WAS REPLACED ACCESS PLATE NR 1454C IAW SRM 51-22-2A AND WILL BE INSTALLED UNDER CARD JIC 2800-0390, JOB 001-0402.

Part: RIB — CORRODED (LT SLAT) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON RIB HOLES XOS 288 AT LT SLAT PANEL NR 2. HOLES BS XOS 288 AT LT SLAT PANEL NR 2 WERE REPAIRED IAW SRM 57-02 PAR 9.

Part: FITTING — CRACKED (R1 DOOR) · airframe 63,330 hrs · 45,708 cycles

CRACK ON FITTING BELOW BEAM NR 4 BETWEEN AFT PAN AND AFT FRAME AT FWD R1 DOOR. FITTING WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3 PAR 14 AND 21, DWG 9911582, REV T.

Part: FRAME — CORRODED (BS 1322) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON PREVIOUS REPAIR OF FRAME BS 1322 BTW LONG 28R TO 28L AT AFT CARGO COMPARTMENT. THE REPAIR WAS REPLACED IAW SRM 53-03D, FIG 2A, 51-30-2, 51-30-5, AND 51-10-3 PAR 21, 14 AND 38.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON COUNTERSINK AT RT WING FUEL ACCESS, NR 1456C, RW, AYP, CARD 109, ZONE 00. CORROSION ON COUNTERSINK WAS REMOVED. COUNTERSINK HOLES WERE MEASURED. MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS ".538" IN 3 ADJACENT HOLES. THEREFORE, WAS FOUND OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A AND ACCESS PLATE NR 1456C WILL BE INSTALLED UNDER CARD JIC 2800-0390, JOB 001-0402.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON SEATING AREA AND COUNTERSINK AT LT WING ACCESS PLATE NR 1363C. CORROSION ON SEATING AREA AND COUNTERSINK WAS REMOVED AND COUNTERSINK HOLES WERE MEASURED. MAX DIAMETER ALLOWABLE IS 0.532 AND MAX DIAMETER MEASURED IS 0.564, 3 ADJACENT HOLES. THEREFORE WAS FOUND OUT LIMITS AND WAS REPLACED IAW SRM 51-22-2A AND ACCESS PLATE NR 1363C WILL BE INSTALLED UNDER CARD JIC 2800-0120, JOB 001-0396.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,330 hrs · 45,708 cycles

CRACK ON FWD PAN AT BEAM NR 1 AT AFT CARGO COMPARTMENT DOOR. CRACK ON PAN WAS REPAIRED IAW STEP BY STEP OF ER/A 539875-14, REV ORIGINAL CRACK 1.187.

Part: PAN — CRACKED (DOOR FRAME) · airframe 63,330 hrs · 45,708 cycles

CRACKED PAN JUST IN THE UPPER FWD CORNER NEXT TO BEAM 1 AT FWD ENTRY DOOR. CRACKED PAN WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-4. SEAL WILL BE INSTALLED IAW CARD 41, NR 20000083320 ACFT ZONE 15. LENGTH CRACK 2.375".

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 63,330 hrs · 45,708 cycles

CORROSION ON FWD AND AFT DOOR FRAME WEB BETWEEN LONGERON 25-30R, UPPER AND LOWER SURFACES AT AFT CARGO COMPARTMENT. THE CORROSION WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR, 14, 21, 26, 38, AND 53-01, FIG 1, ER/A 511165-14MA REV C.

Part: RIB — DAMAGED (LT SLAT) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

WEAR ON HOLE OF RIB XOS 530 AT LT SLAT PANEL NR 5 ON REF CARD 2700-4224-LH-05. CARD 18, ZONE 11. HOLES RIB BS XOS 530 AT LT SLAT PANEL NR 5 WERE REPAIRED IAW SRM 57-02 PAR 9.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON BARREL NUT HOLE NR 14 AND 26 AT RT HORIZONTAL STABILIZER UPPER SKIN BS XH=27.234. DAMAGE ON BARREL NUT HOLES WAS REPAIRED IAW ETI-88-15-349, REV 2 AND ER/A 539870-14, REV.

Part: RIB — CORRODED (RT SLAT) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON RIB HOLES XOS 198 AND XOS 288 AT RT SLAT PANEL NR 2. RIB XOS=198 AND XOS=288 AT RT SLAT PANEL NR 2 WERE REPAIRED IAW SRM 57-02, PAR. 9.

Part: SKIN — WORN (FLAP DOUBLER) · airframe 63,330 hrs · 45,708 cycles

WEAR ON PREVIOUS REPAIR DOUBLER IN BS XV2=258 ON MID VANE OF OTBD FLAP AT RT WING. REPAIR DOUBLER IN BS 258 ON MID VANE OF OTBD FLAP AT RT WING WAS REPLACED IAW SRM 57-03D, PAR 11 AND A/C 0987, CARD 2000-8149-04, CREW O2, 1116268, JOB 000-0015.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON BARREL NUT HOLE AT LT HORIZONTAL STABILIZER UPPER SKIN XH=7.2. DAMAGE ON BARREL NUT HOLE WAS REPAIRED IAW ER/A 539871-14 REV.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,330 hrs · 45,708 cycles

CRACKED INTERCOSTAL BETWEEN BS 1322 AND AFT PRESSURE DOME BETWEEN X -18 AND X -22 AT PAX CABIN FLOOR STRUCTURE. THE INTERCOSTAL WAS REMOVED, NEW DOUBLER WAS FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3, PAR 14, 21, AND 53-01, FIG 2 SHEET 3. INTERCOSTAL WAS INSTALLED IAW SRM 51-30-5.

Part: FRAME — CORRODED (BS 1155) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON FRAME IN BS 1155 BTW LONGERONS 28-29L. CORROSION WAS ATTENDENT IAW SRM 51-10-3, PAR 26.

Part: SKIN — CORRODED (BS 750-788) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON FUSELAGE SKIN UNDER RUB STRIPS BS 750 TO 788 BETWEEN LONG 26 TO 29R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIG 57.

Part: INTERCOSTAL — CORRODED (BS 1212-1219) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1212 - 1219 AND LONGERONS 29 TO 30R IN AFT CARGO BAY. THE INTERCOSTAL WAS REPLACED IAW DWG 5936071, REV: W, SRM 51-10-2, 51-10-3, 51-30-5, AND 51-30-2.

Part: FRAME — CORRODED (BS 180) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON FRAME BS 180 LONGERON 30. CORROSION WAS REMOVED IAW SRM 51-10-3 PAR 2. FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. DAMAGE WAS REMOVED IAW SRM 53-03, FIG 2A, REPAIR FABRICATED, TREATED AND PAINTED IAW SRM 53-03, FIG 2A, 51-10-3, PAR 21-14.

Part: CUSP WEB — CRACKED (BS 875) · airframe 63,330 hrs · 45,708 cycles

CRACK ON LT CUSP WEB, BS 875 BETWEEN X=54 TO X=60, IN REF CARD 198, ZONE 201, CARD 280 ZONE 201. LT CUSP WEB BS Y=875 BETWEEN X=54 TO X=60 WAS REPAIRED IAW SRM 53-05, FIG 131A-8.

Part: SKIN — DEBONDED (RUDDER) · airframe 63,330 hrs · 45,708 cycles

DISBONDED METALLIZED COAT REPAIR OF BOTH SIDE RUDDER, CARD 9, ZONE 65. METALLIZED ON BOTH SIDES WERE REPAIRED IAW 51-70-1A-D, PAR 23 AND ACFT 0987, CARD 2000-8149-01 CREW 02, 1096305, JOB 000-0011. RII WAS COMPLETED BY INSPECTOR STAMP RSGI, LIC. 200802802, ID 627181.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,330 hrs · 45,708 cycles

DELAMINATED AND DAMAGE FERRULE ON FLOOR PANEL. FLOOR PANEL REPLACED FERRULE IAW AMM 53-20-01-201.

Part: INTERCOSTAL — CORRODED (BS 1320) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION FOUND ON FLOORBEAM INTERCOSTAL BS 1320, X=0, Z=-5, UPPER SURFACE. CORROSION WAS REMOVED AND TREATED AREA IAW SRM 51-10-3, PAR 14, 21, 26, 38. HFEC WAS ACCOMPLISHED AND A CRACK WAS FOUND OF .320", INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: INTERCOSTAL — CRACKED (BS 780) · airframe 63,330 hrs · 45,708 cycles

CRACK ON INTERCOSTAL BS 780 X=0, CFS, AT PAX CABIN. INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2 51-01, PAGE 9, PAR 21, 51-10-3 PAR 14, 21.

Part: SEAT TRACK — CORRODED (BS 1146-1148) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON RT PREVIOUS REPAIR PLUG BS 1146-1148 X-22. PREVIOUS REPAIR PLUG WAS REPLACED IAW SRM 53-05, FIG 4A AND 51-10-3, PAR 14, 21.

Part: INTERCOSTAL — CRACKED · airframe 63,330 hrs · 45,708 cycles

CRACKED INTERCOSTAL JUST BEHIND OPERATIVE MECHANISM BETWEEN BEAM 4 AND 5 AT FWD ENTRY DOOR. NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — CORRODED (BS 1463) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORRODED REPAIR DOUBLER AT BS 1463 BETWEEN LONGERONS 1 - 2L. REPAIRED IAW ER/A 478004-14, REV A AND SRM 51-30-5, 51-10-3 PAR 14 AND 21.

Part: LONGERON — CRACKED (BS 541) · airframe 63,330 hrs · 45,708 cycles

CRACK FOUND ON LONGERON 4L, BS 541. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG. 18.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 63,330 hrs · 45,708 cycles

FOUND A CRACKED FLOOR PANEL, 1003F. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-01.

Part: CUSP WEB — CRACKED (BS 789-807) · airframe 63,330 hrs · 45,708 cycles

CRACK ON RT CABIN FLOOR CUSP WEB BETWEEN BS 789-807 AND X -54 TO -60. A NEW CUSP WEB AND RINGS DOUBLER WERE TREATED, PAINTED, FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131A-6, 51-10-3 PAR. 14, 21, 51-30-2, 51-30-5.

Part: CUSP WEB — CRACKED (BS 886) · airframe 63,330 hrs · 45,708 cycles

CRACKED RT CUSP WEB BS 886, X -54. REPAIR FABRICATED IAW ERA 398191-14MA, REV B, SRM 53-05, FIG 131-A AND 51-10-3, PAR 14, 21.

Part: FLOOR PANEL — DAMAGED · airframe 63,330 hrs · 45,708 cycles

FERRULES ON FLOOR PANEL DELAMINATED AND DAMAGED. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: CHANNEL — CRACKED · airframe 63,330 hrs · 45,708 cycles

CRACK WAS FOUND ON CHANNEL FOR THE GENERATOR FLOOR PANEL. REPAIRED IAW SRM 53-05, FIG 131B.

Part: CUSP WEB — CRACKED (BS 906) · airframe 63,330 hrs · 45,708 cycles

A CUSP WEB CRACKED AT BS 906 BETWEEN X-54 TO X-60. THE CUSP WEB WAS REPAIRED IAW SRM 51-01, PAR 21, 53-05, FIG 131A-1, SHEET 1, 51-10-3, PAR 21, 14 AND 51-30-2.

Part: PAN — CRACKED (PAX DOOR) · airframe 63,330 hrs · 45,708 cycles

ACFT HAS A CRACKED PAN JUST IN THE AFT UPPER CORNER NEXT TO BEAM 1 AT FWD ENTRY DOOR. CRACK WAS STOP DRILLED, DOUBLER AND SHIMS WERE FABRICATED, TREATED/PAINTED AND INSTALLED. RETAINER WILL BE INSTALLED WITH NRC 41 ZONE 58 PAN AFT UPPER CORNER NEXT TO BEAM 1 AT FWD ENTRY DOOR WAS REPAIRED IAW SRM 52-05, FIG 1817.

Part: ANGLE — CRACKED (BS 1463) · airframe 63,330 hrs · 45,708 cycles

TWO CRACKED ANGLES AT BS 1463 BETWEEN LONGERONS 7 TO 9L. THE ANGLES WERE REPLACED IAW SRM 51-30-5, AND DWG 5920838.

Part: BEAM — CRACKED (PAX DOORWAY) · airframe 63,330 hrs · 45,708 cycles

CRACKED BEAM NR 1 ON FWD POSITION AT FWD ENTRY DOOR. BEAM NR 1 WAS REPAIRED IAW SRM 52-05D, FIG 98.

Part: SEAT TRACK — CORRODED (BS 935-936) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION FOUND OUT OF LIMITS ON RT SEAT TRACK X 54 BS 935-936. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A AND 51-10-3, PAR 14, 21.

Part: INTERCOSTAL — CRACKED (BS 1353) · airframe 63,330 hrs · 45,708 cycles

CRACKED INTERCOSTAL, BS 1353 X -25 Z -6. THE INTERCOSTAL WAS REPAIRED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-3, PAR 21 AND 14 AND 53-01, FIG 2.

Part: ANGLE — CRACKED (BS 1463) · airframe 63,330 hrs · 45,708 cycles

CRACKED ANGLE AT BS 1463. THE ANGLE WAS REPLACED IAW SRM 51-30-5, DWG 5920838, REV N.

Part: SEAT TRACK — CORRODED (BS 475) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

ACFT HAS CORROSION ON PLUG AT SEAT TRACK X=22, BS 457. PLUG WAS REPLACED IAW SRM 53-05, FIG 4A, SHEET 2 AND 51-30-1.

Part: HINGE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION FOUND ON HINGE NR 6, XE= 225, AT HORIZONTAL STABILIZER REAR SPAR. CORROSION ON HOLE OF HINGE NR 6 WAS REMOVED IAW CMM 27-30-2 PAR 2, B, FIG 601, HOLES WERE MEASURED WITH A ID 0.3755", 2 HOLES WITHIN LIMITS OF REPAIR IAW CMM 27-30-2, PAR 2, B, FIG 601, AREA WAS TREATED, BUSHINGS WERE FABRICATED AND INSTALLED IAW CMM 27-30-2, PAR 2, B, FIG 601.

Part: SEAT TRACK — CORRODED (BS 595-697) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

ACFT HAS CORROSION ON PREVIOUS REPAIR PLUG BS X=-54 BETWEEN Y=595-597 AND Y=695-697. CARD 39, ZONE 201. PLUGS WERE REPLACED IAW SRM 53-05, FIG 4A AND 51-10-3 PAR 14, 21.

Part: CUSP WEB — CORRODED (BS 862-844) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

ACFT HAS CORROSION ON LT CUSP WEB PREVIOUS REPAIR DOUBLER BETWEEN BS 832 TO 844 AND X=54 TO X=60 AT CABIN FLOOR STRUCTURE IN REF CARD 197, ZONE 201, CARD 278, ZONE 201. PREVIOUS REPAIR DOUBLER WAS REPLACED IAW SRM 51-30-2, 53-05, FIG 131A-14, 51-30-5, 51-10-3, PAR 14 AND 21.

Part: CUSP WEB — CRACKED (BS 807-819) · airframe 63,330 hrs · 45,708 cycles

UPPER SURFACE OF LT CABIN FLOOR CUSP WEB CRACKED BS 807 - 819, X 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 51-30-5, 51-30-2, 51-30-1, 51-01 PAR 21, 53-05, FIG 131A-2, 51-10-3, PAR 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 532) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

HAS CORROSION ON LT SEAT TRACK X=22, BS 532 AT CABIN PAX. CORROSION ON SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4A AND 51-10-3 PAR 14, 21.

Part: SHEAR TIE — CRACKED (BS 1174) · airframe 63,330 hrs · 45,708 cycles

CRACK ON SHEAR TIE AT BS 1174 BETWEEN LONGERONS 6 & 7L. SHEAR TIE REMOVED REPLACED IAW SRM 51-30-2, 51-10-2, 51-10-3 PAR 14/21, 51-30-5 AND DWG, 5936081-3, REV V.

Part: CUSP WEB — CORRODED (BS 722-739) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

LT CUSP WEB FOUND CORRODED FROM BS 722 - 739 BETWEEN X -54 TO X -60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: SEAT TRACK — CORRODED (BS 826) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON LT SEAT TRACK X=22 REPAIR PLUG BS 826 CABIN FLOOR STRUCTURE. PLUG ON BS Y 826 WAS REPLACED IAW SRM 53-05, FIG 4A AMD 51-10-3, PAR 14, 2.

Part: FRAME — CRACKED (BS 1322) · airframe 63,330 hrs · 45,708 cycles

A CRACK WAS FOUND ON FRAME BS 1322, LONGERON 17R. THE FRAME WAS REPAIRED IAW ER/A 493697-14MA, REV B.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

ACFT HAS TOOL MARK AND CORROSION ON COUNTERSINK AT LT FUEL ACCESS NR 1355C. FUEL ACCESS NR 1355C WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0396.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION FOUND ON THE COUNTERSINK OF LT WING FUEL ACCESS PANEL 1361C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: ANGLE — CRACKED · airframe 63,330 hrs · 45,708 cycles

CRACKED ANGLE, FWD POSITION ON UPPER PAN AT FWD ENTRY DOOR. THE ANGLE WAS FABRICATED IAW DWG 5961804, REV CF SRM 51-10-2, AND INSTALLED.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION FOUND ON FRAME BS 1380 BETWEEN LONGERONS 25L - 25R. THE FRAME WAS REPLACED IAW SRM 51-10-3, PAR 14, 21, SRM 51-30-2, SRM 51-30-5, SRM 51-10-4 AND DWG 9912246, REV. CE.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 63,330 hrs · 45,708 cycles

DELAMINATED FLOOR PANEL 160F. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: CUSP WEB — CORRODED (BS 639-710) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON LT CUSP WEB FROM BS 639 - 710 X -54 TO Y -60 IN PAX CABIN. CUSP WEB REPAIRED IAW SRM 51-30-2, 53-05, FIG 131A-14, 51-10-3 PAR 14 AND 21.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,330 hrs · 45,708 cycles

DELAMINATED AND DAMAGED FERRULE ON FLOOR PANEL IN PASSENGER CABIN. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201. FLOOR PANEL FERRULE REPLACED IAW AMM 53-20-01-201.

Part: ANGLE — CRACKED (BS 1437) · airframe 63,330 hrs · 45,708 cycles

A CRACKED FRAME ANGLE WAS FOUND AT BS 1437, BETWEEN LONGERON 2 - 3L. THE ANGLE WAS REPLACED IAW SRM 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,330 hrs · 45,708 cycles

CRACK ON AFT PAN AND BEAM NR 1 AT AFT CARGO COMPARTMENT DOOR. CRACK ON AFT PAN WAS REPAIRED IAW SRM 52-03D, FIG 8.

Part: CUSP WEB — CORRODED (BS 566-587) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON LT CUSP WEB, BS 566 TO 569 AND BS 587 BETWEEN X -54 TO X -60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

AICORROSION ON REPAIR BUSHINGS, COUNTERSINK AND SETTLEMENT AREA AT RT WING FUEL ACCESS NR 1410C. ACCESS DOOR 1410C WAS REPLACED.

Part: BOLT — DAMAGED (LT AILERON) · airframe 63,330 hrs · 45,708 cycles

DAMAGED DIRT COVER ON LT AILERON HINGE EYEBOLT NR 1. LT AILERON HINGE BEARING EYE BOLT WAS REPLACED IAW CMM 27-10-10.

Part: FRAME — CRACKED (BS 1380) · airframe 63,330 hrs · 45,708 cycles

CRACKED FRAME ANGLE ON FRAME BS 1380 BETWEEN LONGERON 13-14R. FRAME ANGLE WAS REPLACED IAW SRM 53-14-4, FIG 1 AND 51-10-3, PAR 21 AND 14, 51-30-5 AND 51-30-2.

Part: DOOR — CRACKED (SLAT TRACK) · airframe 63,330 hrs · 45,708 cycles

A CRACKED WAS FOUND ON THE SLAT TRACK DOOR NR 7R. THE SLAT TRACK DOOR WAS REPLACED IAW ERA: 512356-14 MA, REV: ORIG, LP2172495.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,330 hrs · 45,708 cycles

A CRACKED LONGERON 4R BS 1437. THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-10-2, 51-10-2A, 51-10-4 AND 51-10-3, AND REPAIRED IAW SRM 50-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,330 hrs · 45,708 cycles

A CRACKED LONGERON 4L BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON INNER DOUBLER AT AFT LAVATORY SERVICE PANEL. DOUBLER WAS REPAIRED IAW ER/A 397822-14, MA REV B.

Part: SKIN — WORN (PAX DOOR) · airframe 63,330 hrs · 45,708 cycles

WEAR ON SKIN LOWER EDGE AT FWD ENTRY DOOR. REPAIR DOUBLER WAS REPLACED IAW SRM 52-05D, FIG 37, SHEET 1.

Part: BEAM — CRACKED (DOOR FRAME) · airframe 63,330 hrs · 45,708 cycles

CRACK FOUND ON NR 1 BEAM BETWEEN AFT PAN AND AFT FRAME AT FWD SERVICE DOOR. THE BEAM WAS REPLACED IAW SRM 51-30-2, 51-30-5.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON PREVIOUS REPAIR OF FRAME BS 1309 BETWEEN LONGERONS 28 - 29LT AT AFT CARGO COMPARTMENT. DOUBLER REPLACED IAW SRM 53-03D, FIG 2A 51-30-2, AND 51-10-3, PAR 21, 14 AND 38.

Part: CUSP WEB — CORRODED (BS 1201-1212) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON DOUBLER REPAIR ON CUSP WEB BS 1201 - 1212 BETWEEN X-54 AND X-60 RT CABIN. THE DOUBLER WAS REMOVED, FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2, 53-05, 51-10-3 PAR-21 AND 14.

Part: CUSP WEB — CORRODED (BS 439) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

ACFT HAS CORROSION ON RT CUSP WEB BS 439 X -54 TO X -60 AT PAX CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, 51-30-5, 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CRACKED (BS 1166) · airframe 63,330 hrs · 45,708 cycles

A CRACK WAS FOUND ON THE CUSP WEB, AROUND FASTENER HOLE AT BS 1166 BETWEEN X-54 AND X-60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131-A-1.

Part: WEB — CRACKED (BS 101) · airframe 63,330 hrs · 45,708 cycles

CRACKED WEB BS 101, BELOW CENTER PEDESTAL. REPAIRED IAW SRM 53-01, FIG 2 AND SRM 51-10-3, PAR 14, 21, SRM 51-30-2, AND SRM 51-30-5.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION FOUND ON FLOOR PANEL 160G A W1 AREA. THE FLOOR PANEL WAS REPLACED IAW SRM 51-10-3, PAR 21 AND 14, 51-30-02 AND DWG 9957828, REV AB.

Part: CUSP WEB — CORRODED (BS 1044-1045) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION OUT LIMITS ON RT CUSP WEB FROM BS 1044 - 1045 BETWEEN X-54 AND X-60. THE CUSP WEB WAS REPAIRED IAW SRM 51-30-2, SRM 53-05, FIG 131A-14, SRM 51-10-3 PAR 21, 14, AND 38 AND SRM 51-30-5.

Part: CUSP WEB — PUNCTURED (BS 1041-1060) · airframe 63,330 hrs · 45,708 cycles

PUNCTURE FOUND ON LT CABIN CUSP WEB BETWEEN BS 1041-1060 AND X=44 TO 54. CUSP WEB REPAIRED IAW SRM 53-05 FIG 131A-15, 51-30-0.

Part: PAN — CRACKED (CARGO DOORWAY) · airframe 63,330 hrs · 45,708 cycles

A CRACK WAS FOUN ON AFT INNER PAN BELOW STOP FITTING 4 AT THE CARGO DOOR. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIG 50 AND WAS REPAIRED IAW SRM 52-05D, FIG 50.

Part: FLOOR SUPPORT — DEBONDED (NOT REPORTED) · airframe 63,330 hrs · 45,708 cycles

DEBONDED RUB STRIP AND CHANNEL ON FLOOR PANEL 1155A. DAMAGE AREA WAS REPARED IAW 51-70-1D, PAR 10.

Part: BUSHING — WORN (RUDDER) · airframe 63,330 hrs · 45,708 cycles

ACFT HAS WORN BUSHINGS 2 E/A TO ATTACH RUDDER ON HINGES. WORN BUSHINGS 2 E/A TO ATTACH RUDDER ON HINGE WERE REPLACED FOR A NEW AND PN VERIFIED IAW IPC 55-50-00 AND WILL BE INSTALLED UNDER JIC 2720-4421, JOB 001-0348.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 63,330 hrs · 45,708 cycles

CRACKED FLOOR PANEL 1250A. THE FLOOR PANEL WAS REPARED IAW SRM 51-70-1, PAR 10.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,330 hrs · 45,708 cycles

ELONGATED HOLES ON CABIN FLOOR PANEL. THE FLOOR PANEL WAS REPARED IAW SRM 51-70-1, PAR 9.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 63,330 hrs · 45,708 cycles

CRACKS ON LT SLAT NR 2 INNER SKIN AT MID RIB. CRACKS ON SLAT PANEL NR 2 LT WERE REPAIRED IAW SRM 57-01, FIG 3.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,330 hrs · 45,708 cycles

A CRACK WAS FOUND ON AFT NR 1 STOP FITTING AT AFT CARGO DOOR. AFT COMPARTMENT DOOR C3, STOP FITTING NR 1 WAS REPLACED IAW SRM. 51-30-1 AND 51-30-5.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 63,330 hrs · 45,708 cycles

CRACKED LOWER SKIN OF RT SLAT NR 2 AT MID RIB. CRACK ON SLAT PANEL NR 2 RT WAS REPAIRED IAW SRM 57-01, FIG 3, SHEET 2.

Part: DOOR FRAME — CRACKED (BS 189-191) · airframe 63,330 hrs · 45,708 cycles

A CRACKED WEB WAS FOUND ON LOWER ENTRY DOOR JAMB BETWEEN BS 189 - 191 X=54 TO X=60 AT CABIN STRUCTURE. WEB ON LOWER ENTRY DOOR JAMB STA Y=189 TO Y=191, X=54 TO X=60 AT CABIN STRUCTURE WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: PAN — CRACKED (BS 845-864) · airframe 63,330 hrs · 45,708 cycles

ACFT HAS A CRACK RT AFT LOWER CORNER RING PAN BETWEEN BS Y=845 TO Y=864. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-10-2, 51-10-3, 51-10-4, 51-30-2 & 51-30-5 AND ER/A 493648-14MA REV A.

Part: PAN — CRACKED (BS 1060-1098) · airframe 63,330 hrs · 45,708 cycles

CRACK ON RT FWD LOWER CORNER RING PAN BETWEEN BS Y=1079 TO Y=1098 AND Y=1060 TO Y=1079. AREA WAS REPAIRED IAW SRM. 53-05, FIG 122, 51-10-2, 51-10-3, 51-10-4, 51-30-2 & 51-30-5 AND ER/A 493648-14MA REV A AND 487747-14MA, REV A.

Part: PAN — CRACKED (BS 886-905) · airframe 63,330 hrs · 45,708 cycles

A CRACK WAS FOUND ON THE RT AFT LOWER CORNER RING PAN BETWEEN BS 886 - 905. REPAIRED IAW SRM 53-05, FIG 122, 51-10-2, 51-10-3, 51-10-4, 51-30-2 & 51-30-5.

Part: PAN — CRACKED (BS 946-965) · airframe 63,330 hrs · 45,708 cycles

CRACK ON RT FWD UPPER CORNER OF RING PAN BETWEEN BS 946 - 965. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-10-2, 51-10-4, 51-30-2 & 51-30-5 AND ER/A 493648-14MA, REV A., 487747-14MA, REV A.

Part: CUSP WEB — CORRODED (BS 1227) · airframe 65,959 hrs · 47,583 cycles

CORROSION ON CUSP WEB BS 1227 BETWEEN RBL 54 AND 60. THE CUSP WEB WAS REPAIRED.

Part: CUSP WEB — CRACKED (BS 1124-1127) · airframe 63,330 hrs · 45,708 cycles

A CRACK WAS FOUND ON FLOOR CUSP WEB BS 1124 - 1127 BETWEEN X-54 AND X-60 RT CABIN. THE CUSP WEB WAS REPAIRED IAW 51,01, PAR 21, SRM 53-05, FIG 131A-13, SRM 51-10-3, PAR 21 AND 14 AND SRM 51-30-2 V.

Part: CUSP WEB — CORRODED (BS 1043-1054) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON FLOOR CUSP WEB FROM BS 1043 - 1054 BETWEEN X-54 AND X-60 RT CABIN. CORROSION WAS ATTENDED IAW SRM 51-30-2, SRM 51-10-3, PAR 26, 14, 21 AND 38 AND SRM 51-30-5. CUSP WEB ON AREAS OUT LIMITS WILL BE ATTENDED WITH NR 20000082601, CARD 267, ZONE 201.

Part: PAN — CRACKED · airframe 63,330 hrs · 45,708 cycles

A CRACK WAS FOUND ON VENTRAL DOOR PAN AT UPPER HINGE RT EDGE. VENTRAL DOOR PAN AT UPPER HINGE RT WAS REPARED IAW SRM 52-05D, FIG 34.

Part: WEB — DAMAGED (BS 362-370) · airframe 63,330 hrs · 45,708 cycles

ELONGATED HOLE ON PREVIOUS REPAIR ON WEB BETWEEN BS 362 - 370 LONGERON 25 AND 2LR AT FWD CARGO DOOR FRAME. REPAIR WAS REPLACED IAW SRM 51-70-4, FIG 2, SRM 51-30-2, 51-30-8, 51-30-3, PAR 14, 21.

Part: HINGE — DAMAGED (VERTICAL STAB) · airframe 63,330 hrs · 45,708 cycles

ACFT HAS SCRATCHED BORE ON OTBD LUG AT LT VERTICAL STABILIZER HINGE WHERE ATTACH HORIZONTAL STABILIZER. SCRATCHED BORE ON OTBD LUG AT LT VERTICAL STABILIZER HINGE WERE ATTACH HORIZONTAL STABILIZER WAS REPAIRED IAW SRM 51-02, PAR. 6.

Part: INTERCOSTAL — CORRODED (BS 1309-1320) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION WAS FOUND ON INTERCOSTAL BETWEEN BS 1309 - 1320 IN THE AFT CARGO COMPARTMENT. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9936718, REV M.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,330 hrs · 45,708 cycles

WEAR ON AFT/FWD LOWER EXTERNAL DOUBLER AT AFT CARGO COMPARTMENT DOOR. DOUBLERS FWD/AFT WERE REMOVED IAW SRM 51-30-2 AND NEW DOUBLERS WERE DRILLED IAW SRM 51-10-4 AND DOUBLERS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14, 21 AND DOUBLERS WERE INSTALLED IAW SRM 51-30-2.

Part: PAN — CRACKED (BS 674-693) · airframe 63,330 hrs · 45,708 cycles

ACFT HAS A CRACK LT FWD UPPER CORNER RING PAN BETWEEN BS Y=674 TO Y=693. LT FWD UPPER CORNER RING PAN BETWEEN BS Y=674 TO Y=693 WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 487747-14 MA, REV A AND 493648-14 MA REV A, D.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 63,330 hrs · 45,708 cycles

CRACKED FRAME BEHIND DOOR STOP FITTING NR 2 AT FWD EDGE OF C1 DOOR. CRACK WAS REWORKED AND AREA WAS INSPECTED AND NO CRACKS EVIDENCE WAS FOUND ALSO AREA WAS PROTECTED IAW SRM 52-03, D FIG 10 AND SRM 51-10-3.

Part: SEAT TRACK — CORRODED (BS 965) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

HAS CORROSION ON REPAIR PLUG OF SEAT TRACK LT BS 965, LBL 22. THE REPAIR PLUG WAS REPLACED IAW SRM 51-30-1, 53-05, FIG 4A SHEET 1 AND 2, AND 51-10-3, PAR 14, 21 AND 38.

Part: PAN — CRACKED (BS 1003-1022) · airframe 63,330 hrs · 45,708 cycles

CRACK ON LT AFT UPPER CORNER OF RING PAN BETWEEN BS 1003 TO 1022. REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 487747-14MA, REV A AND 493648-14MA REV. A, D.

Part: DOOR FRAME — CRACKED (BS 207) · airframe 63,330 hrs · 45,708 cycles

CRACKED WEB ON BS 207, LONGERON 11 AT L1 DOOR FRAME. WEB WAS REPAIRED IAW SRM 51-30-21, 53-05, FIG 142 AND 51-10-3, PAR 14 AND 21.

Part: PAN — CRACKED (BS 1117-1198) · airframe 63,330 hrs · 45,708 cycles

A CRACK WAS FOUND ON RT AFT UPPER CORNER RING PAN BETWEEN BS 1117 - 1198. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-10-2, 51-10-3, 51-10-4, 51-30-2 AND 51-30-5 AND ER/A 493648-14MA, REV A 487747-14MA REV.

Part: STRUCTURE — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

CORROSION ON INTERNAL STRUCTURE TO ATTACH CLEVIS IN XV2=325 ON OTBD VANE OF OTBD FLAP AT LT WING. OTBD VANE OF OTBD FLAP AT LT WING WAS REPLACED IAW SRM 57-50-14, FIG 2 SH 2.

Part: DOOR FRAME — CORRODED (MID CARGO BAY) · corrosion level 2 · airframe 63,330 hrs · 45,708 cycles

HAS CORROSION ON MID CARGO LOWER DOOR FRAME BEAM. REPAIRED IAW SRM 53-05, PAR 140, FIG 123 AND 51-10-3, PAR 21 AND 14.

Part: PAN — CRACKED (BS 1060-1098) · airframe 63,330 hrs · 45,708 cycles

CRACK ON RT AFT UPPER CORNER AT RING PAN BETWEEN BS 1060 - 1098. THE AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-10-2, 51-10-3, 51-10-4, 51-30-2 AND 51-30-5 AND ER/A 493648-14MA, REV AND 487747-14, REV A.

Part: PAN — CRACKED (BS 1231-1250) · airframe 63,330 hrs · 45,708 cycles

CRACK ON LT AFT LOWER CORNER OF RING PAN BETWEEN BS 1231 - 1250. REPAIRED IAW SRM 53-05, FIG 122 AND ERA 493648-14MA, REV "A" AND 487747-14MA, REV "A".

Part: PAN — CRACKED (BS 1041-1060) · airframe 63,330 hrs · 45,708 cycles

ACFT HAS A CRACK ON RT FWD LOWER CORNER OF RING PAN BETWEEN BS 1041 - 1060. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, 51-10-4, 51-10-2, 51-30-2 AND 51-30-5 AND ER/A 493648-14MA, REV A AND 487747-14MA, REV. A.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 63,330 hrs · 45,708 cycles

DENTS FOUND ON UPPER SKIN AT RT ELEVATOR GEARED TAB. RT ELEVATOR GEARED TAB WAS REMOVED. RT ELEVATOR GEARED TAB AND WILL BE INSTALLED WITH A/C 0987, CARD 2730-4590 RT.

Part: PAN — CRACKED (BS 1041-1079) · airframe 63,330 hrs · 45,708 cycles

CRACK ON RT AFT LOWER CORNER OF RING PAN BETWEEN BS 1041- 1079 . AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-10-2, 51-10-3, 51-10-4, 51-30-2 AND 51-30-5 AND ER/A 493648-14MA REV A, 487747-14MA, REV A.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 63,330 hrs · 45,708 cycles

DELAMINATION FOUND ON UPPER/LOWER SURFACE ON LT ELEVATOR CONTROL TAB. LT CONTROL TAB WAS REMOVED DUE TO DAMAGE. LT CONTROL TAB WILL BE INSTALLED WITH CARD A/C 0987, CARD 2730-4590-LT.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 63,330 hrs · 45,708 cycles

DELAMINATED LOWER SKIN ON MID VANE OF OTBD FLAP AT LT WING. THE VANE OF OTBD FLAP WAS REPLACED IAW SRM 57-50-14, FIG. 2, SH 2.

Part: PAN — CRACKED (BS 1136-1193) · airframe 63,330 hrs · 45,708 cycles

A CRACK WAS FOUND ON FWD LOWER CORNER AT RING PAN BETWEEN BS 1136 - 1193 RT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122, 51-10-2, 51-10-3, 51-10-4, 51-30-2 AND ER/A 493648-14MA, REV A AND 487747-14, REV A.

Part: TAB — DENTED (RT ELEVATOR) · airframe 63,330 hrs · 45,708 cycles

DENTS FOUND ON THE UPPER SKIN OF THE RT ELEVATOR ANTI-FLOAT TAB. THE TAB WAS REPLACED.

Part: PAN — CRACKED (BS 750-769) · airframe 63,330 hrs · 45,708 cycles

LT FWD UPPER CORNER RING PAN BETWEEN BS 750 - 769 FOUND CRACKED. THE LT FWD UPPER CORNER RING PAN REPAIRED IAW SRM 53-05, FIG 122.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 60,732 hrs · 44,003 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT AT 35E WAS INOPERATIVE. MAINTENANCE REPLACED THE PIGTAIL AT 35D AND THE OPS CHECK WAS GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 60,186 hrs · 43,616 cycles

DURING CHECK, MAINTENANCE FOUND THE EMERGENCY PATH IN SEAT LIGHTS WERE INOPERATIVE AT ROWS 11 AND 16. MAINTENANCE FOUND THE CONNECTORS DISCONNECTED AND THEY RECONNECTED THEM. LIGHTS RETURNED TO AN OPS STATE.

Part: UNKNOWN — ODOR (CABIN) · airframe 59,495 hrs · 43,166 cycles

AT TOP OF CLIMB, F/A REPORTED ODOR OF ELECTRICAL SMOKE IN CABIN. SMOKE WAS STRONGER IN FRONT OF CABIN. RETURN TO DEPARTURE. DURING QRH PROCEDURE F/A REPORTED SMOKE DISSIPATING. DURING TOP OF DESCENT AND ONCE DURING FINAL APPROACH FLIGHT CREW COULD DETECT AN ELECTRICAL ODOR IN COCKPIT. CAPTAIN'S LOCALIZER, GLIDESLOPE WOULD NOT COME UP. AUTOPILOT DISCONNECTED ON SHORT FINAL IN DFGC2. MAINTENANCE PERFORMED AMDS WC 2120-2367 WITH NO TROUBLE FOUND. PERFORMED DUCT BURN OUT WITH ENGINES, REF AMDS WC 7100-2619 WITH NO TROUBLE FOUND. ACFT OK FOR SERVICE. PERFORMED RETURN TO SERVICE ON BOTH DFGC'S.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,174 hrs · 42,954 cycles

CRACKED FUSELAGE SKIN REPAIR DOUBLER AT RT AFT NOSE WHEEL WELL DOOR AFT HINGE. REPLACED REPAIR DOUBLER SRM 53-05, FIG 62.

Part: BRACKET — LOOSE (TAILCONE) · airframe 59,174 hrs · 42,954 cycles

DURING CHECK, NOTED THE LOWER ATTACH BRACKET FOR THE TAILCONE UPPER LT LOCK RECEPTICLE PAD WAS LOOSE AND WORKING. REPLACED TAILCONE BRACKET IAW SRM 53-30-01.

Part: CABLE — FRAYED (TAILCONE) · airframe 59,174 hrs · 42,954 cycles

DURING CHECK, NOTED THE TAILCONE KEVLAR CABLE WAS FRAYED AND DETERIORATED. REPLACED KEVLAR CABLE IAW AMDS 5350-01077-0101.

Part: RECEPTACLE — WORN (TAILCON) · airframe 59,174 hrs · 42,954 cycles

DURING CHECK, NOTED THE PIN RECEPTICLES ON THE TAILCONE ARE WORN. REPLACED TAILCONE RECEPTICLES IAW SRM 51-30.

Part: DOOR — NOT REPORTED (CARGO) · airframe 58,626 hrs · 42,623 cycles

CARGO DOOR REPAIRED IAW AA 5230-01159.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 58,353 hrs · 42,421 cycles

DURING LINE CHECK, OVERHEAD EMERGENCY EXIT COVER DIFFUSER LENS WAS NOTED TO BE MISSING AT THE L2 DOOR. LENS/DIFFUCER COVER REPLACED.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 57,900 hrs · 42,096 cycles

LEFT HORIZONTAL STABILIZER, UPPER AFT SKIN, DAMAGED XHS 14.649, STR 3. REPAIRED IAW ERA 507705-14.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,009 hrs · 41,502 cycles

DURING OVERNIGHT MX, EMERGENCY SEAT MOUNTED ESCAPE LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 15. REPLACED EMERGENCY LIGHT ASSY AND OPS CHECKED NORMAL.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,708 hrs · 41,321 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 3D IN THE CABIN WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,393 hrs · 41,116 cycles

DURING LINE CHECK, MX FOUND THAT THE SEAT MOUNTED EMERGENCY PATHWAY LIGHTING AT SEAT 32DE WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYS.

Part: RELIEF VALVE — NOT REPORTED (AIR STARTER) · airframe 56,375 hrs · 41,106 cycles

STARTER AIR SHUTOFF VALVE, INSTALLED PRESSURE RELIEF VALVE IAW AA 8012-01009.

Part: TAB — CORRODED (RT ELEVATOR) · airframe 1 hrs · 1 cycles

DURING CPCP INSPECTION, FOUND RT ELEVATOR CONTROL TAB CORRODED OUT OF LIMITS. REF NR CARD 295. THE CONTROL TAB R & R IAW AMD WC 2730-4590RH.

Part: SKIN — CRACKED (BS 1419 L1-2L) · airframe 1 hrs · 1 cycles

BS 1419 BETWEEN L1 AND 2L SKIN CRACKED. CUT OUT DAMAGE WITH .7500" CUT OUT. FABRICATED INTERNAL REPAIR DOUBLER IAW AND INSTALLED IAW SRM 53-04, PAGE 225 AND ER/A 507597-14.

Part: LONGERON — CRACKED (BS 1419) · airframe 55,916 hrs · 40,790 cycles

LONGERON 2L, BS 1419, IS CRACKED AFT ACCESSORY. REMOVED CRACKED SECTION OF LONGERON AT PREVIOUS REPAIR SPLICE. FABRICATED, MATCH DRILLED, TRIMMED, DEBURRED, TREATED, AND PRIMED. INSTALLED LONGERON AND SPLICE IAW SRM 53-02, FIG 18.

Part: SILL — CORRODED (BS 1154-1211) · airframe 1 hrs · 1 cycles

AFT CARGO DOOR SILL HAS CORROSION BETWEEN BS 1154 AND 1211. REPAIRED IAW SRM 53-05 AND ERA/A 499523-14MA.

Part: SKIN — NOT REPORTED (HORIZONTAL STAB) · airframe 55,916 hrs · 40,790 cycles

HORIZONTAL STABILIZER UPPER CENTER SKIN PANEL REPAIRED IAW AA 5510-01086.

Part: LUG — NOT REPORTED (HORIZONTAL STAB) · airframe 55,913 hrs · 40,788 cycles

HORIZONTAL STABILIZER HINGE RIB PIVOT BEARING LUG REPAIRED IAW AA 5500-01011.

Part: LIGHT — INOPERATIVE (SEAT 24A) · airframe 55,360 hrs · 40,432 cycles

DURING CHECK, FOUND SEAT 24A EMERGENCY PATHWAY LIGHT DAMAGED, INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER AMM. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,584 hrs · 39,949 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHTS OVER THE LEFT AND RIGHT WINGS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 54,563 hrs · 39,938 cycles

THE AIRCRAFT RETURNED TO MSP DUE TO THE LOSS OF CABIN PRESSURIZATION ACCOMPANIED BY OXYGEN MASK DEPLOYMENT. MAINTENANCE PERFORMED CONFIDENCE CHECK PER AMM, PER MCC REQUEST, WITH APU AND ENGINE RUNNING. CHECK PASSED. NOTIFIED MCC.

Part: WIRE — DAMAGED (CABIN) · airframe 53,665 hrs · 39,376 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHTS AT ROWS 27 AND 28 INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AND RELAMPED. OPERATIONAL CHECK WAS GOOD.

Part: LONGERON — DAMAGED (BS 256) · airframe 52,257 hrs · 38,384 cycles

LONGERON 17L DAMAGED AT BS 256. REPAIRED IAW SRM 53-02, FIGURE 18.

Part: SKIN — DENTED (BS 256) · airframe 63,508 hrs · 45,844 cycles

DAMAGE FOUND ON ARRIVAL, FUESLAGE DENT APPROXIMATELY 3 FT AFT OF L1 DOOR, THRESHOLD LEVEL, SKIN REPAIRED IAW SRM 53-04D, FIGURE 12C AND REPAIRED DAMAGED LONGERON 17L AT BS 256 IAW SRM 53-02, FIG 18.

Part: FAN — DEFECTIVE (CABIN) · airframe 51,905 hrs · 38,174 cycles

AT CRUISE THE FLIGHT ATTENDANTS REPORTED SMOKE SMELL AND HAZE IN THE MID CABIN. CREW COMPLIED WITH THE QRH AND TURNED OFF CERTAIN COMPONENTS AND CIRCUIT BREAKERS. SMOKE GENERATION STOPPED AND DECREASED. FLIGHT LANDED WITHOUT FURTHER INCIDENTS. GSO MAINTENANCE FOUND RECIRCULATION FAN TRIPPING ITS CIRCUIT BREAKER AND PLACED THE SYSTEM ON MEL. ATL MAINTENANCE REPLACED CABIN RECIRCULATION FAN AND RELAY R2-59 PER THE AMM. RECIRCULATION FAN CHECKS GOOD AND MCO/PLAC REMOVED.

Part: SPAR — CRACKED (WING) · airframe 51,812 hrs · 38,123 cycles

WING REAR SPAR CRACKED AT XRS 164 REPAIRED IAW AA 5710-01110.

Part: HEATER — NOT REPORTED (STATIC PORT) · airframe 51,812 hrs · 38,123 cycles

STATIC PORT HEATER REPAIRED IAW AA 3030-01027.

Part: HEATER — NOT REPORTED (STATIC PORT) · airframe 51,812 hrs · 38,123 cycles

STATIC PORT HEATER REPAIRED IAW EA 09-465286-03.

Part: SKIN — DENTED (BS 234 S16) · airframe 51,393 hrs · 37,889 cycles

WHILE PICKING UP ACFT, THE SKIN WAS FOUND DENTED WITH CREASE AT FS 234, STR 16. REPLACED PREVIOUS UPPER AFT SECTION OF 4 CORNER REPAIR IAW BAC DWG SG09530008 WITH THE EXCEPTION OF CROSSING STR 16 IAW ERA 487622-14 REV ORIG.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,828 hrs · 36,841 cycles

MX FOUND THE FLOOR EMERGENCY LIGHTS AT 10DE TO BE INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT WIRE HARNESS. AN OPS CHECK WAS NORMAL AND THE ACFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (BS 224 L17-18L) · airframe 49,037 hrs · 36,365 cycles

DURING HMV A DENT WAS FOUND ON PREVIOUS REPAIR DOUBLER AT FUSELAGE SKIN AT STA Y=224 BTW LONGERON 17 AND 18LT. DOUBLER WAS REPLACED IAW SRM 53-04D FIG 12B.

Part: BEAM — CRACKED (R1 DOOR) · airframe 49,037 hrs · 36,365 cycles

DURING HMV A CRACK WAS FOUND ON FWD EDGE OF NR 4 BEAM OF R1 DOOR BEAM WAS REPAIRED IAW SRM 52-05D FIG 25.

Part: FITTING — DAMAGED (LT MLG) · airframe 49,037 hrs · 36,365 cycles

DURING HMV A ELONGATED HOLE WAS FOUND ON LT WING MLG FITTING. BUSHING BORE WAS REPAIRED IAW EA 09-093855-03AD 0104.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 49,037 hrs · 36,365 cycles

DURING HMV LIGHTNING STRIKE WAS FOUND ON WINDOW FRAME NR 46 AT AFT AND FWD MID EDGE WINDOW BELT WAS REPAIRED IAW ERA 478007-14 REV ORIG.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 49,037 hrs · 36,365 cycles

DURING HMV A CRACK WAS FOUND ON RT UPPER SKIN ON VERTICAL STABILIZER L/E CRACK WAS REPAIRED IAW ERA 478005-14 REV ORIG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 49,037 hrs · 36,365 cycles

DURING HMV A CRACK WAS FOUND ON NR 1 BEAM AND CLIP AT R1 DOOR. CLIP AND BEAM WAS REPAIRED IAW SRM 52-05D FIG 25.

Part: BEAM — CORRODED (C3 DOOR FRAME) · airframe 49,037 hrs · 36,365 cycles

DURING HMV EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR JAMB LOWER BEAM STA Y=1155 TO 1212. LWR DOOR BEAM WAS REPAIRED IAW SRM 53-05 FIG 123.

Part: FITTING — DAMAGED (RT MLG) · airframe 49,037 hrs · 36,365 cycles

DURING HMV AN OUT LIMIT BUSHING BORE WAS FOUND ON RT MLG FITTING BUSHING BORE WAS REPAIRED IAW EA 09-093855-03AD 0204.

Part: FRAME — CRACKED (BS 886) · airframe 49,037 hrs · 36,365 cycles

DURING HMV A CRACK WAS FOUND ON LT FUSELAGE FRAME OVERWING STA Y=886 IN PAX CABIN. FRAME WAS REPLACED IAW DWG SR059530282 REV ORIG.

Part: SKIN — ERODED (RUDDER) · airframe 49,037 hrs · 36,365 cycles

DURING HMV DAMAGED METALLIZED COAT WAS FOUND ON THE RUDDER. RUDDER WAS REPAIRED IAW SRM 51-70-1AD PARA 23.

Part: TEE FITTING — DAMAGED (BULKHEAD) · airframe 49,037 hrs · 36,365 cycles

DURING HMV TOOLING MARKS WERE FOUND ON AFT FACE AT P-DOME LOWER TEE STA Y=1338 BTW X=-8 TO 8, P-DOME LOWER TEE WAS REPAIRED IAW SRM 53-03D FIG 37.

Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 49,037 hrs · 36,365 cycles

DURING HMV LIGHTNING STRIKE WAS FOUND ON WINDOW FRAME NR 31 AT AFT LOWER CORNER DAMAGE WAS REPAIRED IAW SRM 53-05 FIG 111.

Part: ATTACH FITTING — CORRODED (TAILCONE) · airframe 49,037 hrs · 36,365 cycles

DURING HMV RUSTED ATTACH CLIPS WAS FOUND OF TAILCONE EXTERNAL EMERGENCY RELEASE HANDLE. CLIPS WERE REPLACED IAW AMM 20-30-01-201.

Part: WINDOW FRAME — DAMAGED (CABIN) · airframe 49,037 hrs · 36,365 cycles

DURING HMV LIGHTNING STRIKE WAS FOUND ON WINDOW FRAME NR 41 AT AFT UPPER CORNER. DAMAGE WAS REPAIRED IAW SRM 53-05 FIG 111.

Part: DOOR FRAME — CORRODED (CARGO BAY) · airframe 49,037 hrs · 36,365 cycles

DURING HMV CORROSION WAS FOUND ON REPAIR DOUBLER ON C1 FWD DOOR JAMB BTW LONGERON 28-26 RT REPAIR DOUBLER WAS REPLACED IAW SRM 53-05D FIG 804D.

Part: DOOR FRAME — DAMAGED (CARGO DOORWAY) · airframe 49,037 hrs · 36,365 cycles

DURING HMV ELONGATED HOLE WAS FOUND ON FWD DOOR JAMB STA Y=370 BTW LONGERON 27-28 RT AT FWD CARGO COMPARTMENT. HOLE WAS REPAIRED IAW ERA 478002-14 REV ORIGINAL.

Part: RELAY — BURNED (STAB TRIM) · airframe 39,310 hrs · 30,144 cycles

ON DEPARTURE FROM VPS PRIMARY STAB TRIM FAILED ACCOMPANIED BY C/B TRIPPING AND VISIBLE SMOKE/SPARKS SEEN AT SEAT 3D THROUGH SIDEWALL VENT. FOUND RELAY R20-16 BURNED. CHECKED WIRING TO COCKPIT AND STAB MOTOR NTF. A1 AND A2 TERMINALS BURNED. REPLACED RELAY R20-16, ALSO REPLACED C1213A8 AND C1202B8 WIRES. RE-TERMINATED C1202A8, SYS CHECKS GOOD.

Part: FIRE LOOP — FAILED (NR 1 ENGINE) · airframe 38,303 hrs · 29,394 cycles

IN FLIGHT NR 1 ENGINE LOOP A FAIL LIGHT ILLUMINATED, CREW SAID SELECTED THE A LOOP AND THE FIRE WARNING ILLUMINATED, SECURED THE ENGINE AND DIVERTED TO MCN. UNABLE TO DUPLICATE, REPLACED A LOOP.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 36,299 hrs · 27,955 cycles

PASSENGER SEAT 13D EMERGENCY TRACK LIGHTING INOP. REPLACED DAMAGED HARNESS.

Part: LINE — FAILED (NR 2 ENGINE) · airframe 35,287 hrs · 27,246 cycles

LOST COMPLETE RIGHT HYD SYS. PERFORMED EMERGENCY PROC AND RET TO ATL. FOUND NR 2 ENGINE HYDRAULIC PRESSURE LINE BLOWN. REPLACED SAME.

Part: CONTROL BOX — LEAKING (OXY SYSTEM) · airframe 35,041 hrs · 27,052 cycles

CREW LOSS O2 IN FLIGHT. FOUND F/O MASK STUCK IN TEST. REPLACED F/O MASK BOX.

Part: HEATER — FAILED (PITOT HEAD) · airframe 33,730 hrs · 26,155 cycles

RECEIVED THE PITOT/STALL HEAT OFF OAP MSG. CYCLED THROUGH METER SEL AND NOTED 0 AMPS AT RUDDER LIMITER POS. AIRBORNE RETURNED TO CVG. REPLACED RUDDER LIMITER PITOT PROBE PER M/M. NOW PROBE HEAT AND LEAK CHECK NORMAL PER TOPPS 20-50 NOT AN RII ITEM.

Part: PACKING — LEAKING (A/C BAY) · airframe 30,262 hrs · 23,734 cycles

THE TAIL COMPARTMENT TEMP HI LIGHT ON DURING CLIMB. EXTINGUISHED TEMPORARILY WITH HP BLEED OFF, THEN RE-ILLUMINATED. COMPLIED WITH CHECK LIST, PULLED LEFT THROTTLE TO IDLE AND LIGHT EXTINGUISHED, LEFT PACK OFF AND LEFT THROTTLE BACK TO NORMAL. POWER AND LIGHT REMAINED EXTINGUISHED. FOUND 2 PACKINGS LEAKING AT RT ANTICIPATOR AND THERMOSTAT. REPLACED PACKINGS. REPLACED RT AND LT TAIL COMPT TEMP HIGH TEMP SENSORS, PRECAUTIONARY. FOUND 2 LOOSE PACK CLAMPS ON LT PACK. TIGHTENED SAME. LEAK CHECKS GOOD. ENGINE RUN TO PWR CHECKS GOOD.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 28,371 hrs · 22,375 cycles

SEAT 3C EMERGENCY TRACK LIGHT INTERMITTENT. REPLACED SEAT CABLE PER M/M, OPS CHECK OK.

Part: SKIN — CORRODED (FS 650, S-29R) · airframe 27,979 hrs · 22,076 cycles

FUSELAGE / SKIN / FS 650 / STRG. 29R-30 : CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 650 BETWEEN STRINGERS 30 AND 29R. THE CORROSION WAS REMOVED WITH A 7.5" X 9.5" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN ESTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 381586-14, REV A.

Part: OXYGEN MASK — FAILED (COCKPIT) · airframe 24,959 hrs · 19,884 cycles

CAPTAINS O2 MASK WOULD NOT INFLATE. REPLACED CAPTAINS O2 MASK.

Part: PUMP — UNSERVICEABLE (NR 1 ENGINE) · airframe 24,658 hrs · 19,661 cycles

ON APPROACH LEFT HYD PRESS LOW LIGHT ON WITH 0 PRESS ON GAUGE. HYD QTY NORMAL. REPLACED ENG HYD PUMP CASE DRAIN FILTER AND PRESS FILTER.

Part: COALESCER — CONTAMINATED (CABIN)

AFTER TAKEOFF SMOKE APPEARED IN CABIN FROM TAIL SECTION CAUSING BOTH AFT LAV SMOKE DETECTORS TO SOUND. BORESCOPED BOTH ENGINES, REPLACED BAGS, PERFORMED DUCT BURNOUT.

Part: APU — MALFUNCTIONED (APU COMP)

AFTER T/O, AFT LAV SMOKE DETECTORS STARTED SIGNALING WITH SOME HAZE IN THE CABIN. RETURNED TO CVG. PERFORMED DUCT BURNOUT PER M/M CH 36 AND REPLACED WATER BAGS, RAN BOTH ENGS TO T/O AND NO SMOKE/HAZE NOTED. ENGS STARTED WITH EXT AIR APU NOT USED. REPLACED APU, CLEANED DOORS. RAN APU, NO LEAKS NOTED AND ALL INDS NORMAL. RAN SEVERAL HRS, NO SMOKE.

Part: COALESCER — DIRTY (CABIN)

ATB - RIGHT AFT LAV SMOKE ALARM SOUNDED SHORTLY AFTER TAKEOFF F/A REPORTED MUSTY SMELL AND FAINT HAZE IN AFT CABIN FAINT SMELL WAS ALSO PRESENT IN COCKPIT. RAN A/C DUCT BURNOUT PER M/M AND REPLACED BOTH WATER SEPARATOR BAGS. RAN ENG CHECKS GOOD.

Part: COALESCER — DIRTY (CABIN)

AFTER TAKEOFF, AFT LAV SMOKE DETECTORS STARTED SIGNALING WITH SOME HAZE IN THE CABIN. RETURNED TO CVG. PERFORMED DUCT BURNOUT PER M/M CH 36. CHANGED WATER BAGS, RAN BOTH ENGS TO TAKEOFF AND NO SMOKE OR HAZE NOTED. ENGS STARTED WITH EXT AIR. APU NOT USED. REPLACED APU AND CLEANED DOORS, RAN APU AND NO LEAKS. ALL INDICATIONS NORMAL. RAN SEVERAL HRS, NO SMOKE OR HAZE.

Part: FRAME — CRACKED (BS 1418)

FS 1418 CRACKED AT L2L AND L2R AT THE TYP LOCATIONS. REPAIRED PER ERA 331436-14.

Part: APU — FAILED (AFT FUSELAGE)

AFTER T/O PASSING 3000 FT, CABIN FILLED WITH SMOKE. FOUND APU OIL LEAKING, CAUSING CONTAMINATION. CONDUCTED BURN-OUT PROCEDURES. REPLACED WATER SEPARATOR BAGS. ACCOMPLISHED RUN-UP, NO SMOKE. REPLACED WATER SEPARATOR BAGS SECOND TIME AND PER FORMED HIGH POWER RUN UP, OPS OK NO SMOKE. FWD APU TO MCO PER MEL 49-00-01A APU INOP.

Part: ICE DUCT — BLOWN (NR 2 ENGINE)

ON TAKEOFF, GOT RT ENG FIRE LOOP 'B' MSG FOLLOWED BY RT ENG ANTI-ICE MSG AND RT ENG VLV MSG. THEN FIRE WARNING CAME ON, WARNING CX BY RETARDING THROTTLE. FOUND RT ENG COWL ANTI-ICE DUCT 759102250 BLOWN, BRACKET 719201023 AND WIRING NEAR DUCT DAMAGED. ALSO, INSIDE OF COWL NEAR DUCT DAMAGED.