N993DL

Part: CONTROL BOX — CONTAMINATED (ANTI-SKID SYSTEM) · airframe 70,200 hrs · 50,768 cycles

SHIP 993 - BRAKE - AFTER LANDING GEAR EXTENSION ALL ANTI-SKID MESSAGES ILLUMINATED ON EOAP. THE CREW RAN THE QRH PROCEDURE BUT THE MESSAGES REMAINED. AFTER TOUCHDOWN, THE CREW HAD NO BRAKES AND USED REVERSERS TO SLOW THE AIRCRAFT. THE CREW THEN EXITED TO THE TAXIWAY, TURNED THE ANTI-SKID SYSTEM OFF, AND THE BRAKES STARTING WORKING NORMAL. CORRECTIVE ACTION: MAINTENANCE TROUBLESHOT PER AMM. ALL TEST CHECK GOOD. NO SKID BURNS WERE FOUND ON ANY TIRES. EVIDENCE OF PREVIOUS FLUID CONTAMINATION WAS FOUND ON THE ANTI-SKID CONTROL BOX. MAINTENANCE REPLACED ANTI-SKID CONTROL BOX AND TESTED PER AMM. (LP5214530)

Part: LIGHT — MISSING (ANTI-COLLISION) · airframe 69,818 hrs · 50,421 cycles

LOWER ANTI-COLLISION LIGHT MISSING. C/W ERA 572237-14 SECTION 1 TIME LIMITED REPAIR. SDR REPORTED DUE TO FACT THAT PART MAY HAVE DEPARTED FROM THE AIRCRAFT DURING FLIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 69,582 hrs · 50,212 cycles

SEAT 15-23 EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK IAW AMM 33-53 OP CHECK GOOD. OK FOR SRV.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,454 hrs · 50,106 cycles

OVERWING EXIT SIGNS INOPERATIVE. R & R BATTERY PACKS, B5103, AND B5105 IAW AMM 33-50, OPS CHECKED NORMAL.

Part: PANEL — DISLODGED (F/A CALL) · airframe 69,007 hrs · 49,720 cycles

AFT FLT ATTENDANT CALL PANEL DISLODGED DURING LANDING. F/A REPORTED AN ELECTRICAL SHOCK.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 68,861 hrs · 49,609 cycles

WIRE HARNESS TO SEAT 26D/E HAS BAD PLUG AT SIDE WALL PANEL. REPLACED SEAT JUMPER HARNESS AS REQ'D. ALL CKS GOOD. MEL AND PLACARD REMOVED.

Part: DOOR FRAME — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 68,716 hrs · 49,502 cycles

DURING INSPECTION, CORROSION FOUND ON THE LOWER BEAM OF THE AFT CARGO DOOR FRAME. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05, FIG 123, 51-10-4, AND 51-10-2.

Part: ANGLE — CRACKED (LT LG DOOR FRAME) · airframe 68,716 hrs · 49,502 cycles

CRACKED ANGLE ON THE AFT DOOR FRAME, OTBD END, AT THE LT MLG WW. THE ANGLE WAS REPLACED IAW SRM 51-30-2, AND 51-30-5.

Part: FRAME — CRACKED (BS 1463) · airframe 68,716 hrs · 49,502 cycles

BS 1463 CANTED FRAME CAP CRACKED. REPAIRED IAW ER/A 543145-14, REV A.

Part: INTERCOSTAL — CRACKED (BS 1510) · airframe 68,716 hrs · 49,502 cycles

CRAKED INTERCOSTAL, BS 1510, LONGERON 23L. THE INTERCOSTAL WAS REPLACED IAW SRM 53-14-4.

Part: STRAP — BROKEN (TAILCONE) · airframe 67,995 hrs · 48,987 cycles

VELCRO STRIP ON INTERIOR TAILCONE BARRIER STRAP BROKEN. REATTACHED VELCRO STRIP FOR AFT STAIR DOOR BARRIER STRAP. OPN CKS GOOD. OK FOR SVC.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,772 hrs · 48,845 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 32 CEILING. REPLACED BATTERY PACK IAW AMM 33-53. CHECKED NORMAL.

Part: HYDRAULIC SYSTEM — FAILED (LEFT) · airframe 67,166 hrs · 48,341 cycles

EXPERIENCED A LEFT SYSTEM HYDRAULIC FAILURE WHILE IN CRUISE TO CUN. AN EMERGENCY LANDING WAS DECLARED. NO LEAKS WERE FOUND BY MAINTENANCE. THE LEFT SYSTEM RESERVOIR WAS BLED AND RE-SERVICED. THE PTU, EDP PRESSURE FILTER, CASE DRAIN FILTER, AND THE LEFT SYSTEM RETURN FILTER WERE ALL REPLACED. AN ENGINE RUN WAS PERFORMED AND THE FLIGHT CONTROLS WERE CYCLED WITH NO PROBLEMS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — DEFECTIVE (HYDRAULIC SYS) · airframe 66,417 hrs · 47,789 cycles

RIGHT HYDRAULIC AUX PUMP CIRCUIT BREAKER POPPED AFTER TAKEOFF. CHECKED RT HYD AUX PUMP WIRING REF W/C 2920-01098-0201. FOUND NO POWER TO AUX PUMP ON ALL THREE PHASES. INSPECTED AUX PUMP C/B AND FOUND B PHASE WIRE BURNED AND B PHASE BUS BAR BURNED. REMOVED AND REPLACED RT AUX PUMP C/B B1-764 IAW WDM 29-21. REMOVED AND REPLACED BUS SENSE C/B B1-199 IAW WDM 24-21. REPLACED B PHASE BUSS BAR AND JUMPER ALL CKS GOOD IAW AMM 29-00.

Part: ALTIMETER — FAILED (CAPTAIN'S) · airframe 65,644 hrs · 47,321 cycles

CAPTAIN`S ALTIMETER OFF FLAG DURING CRUISE. MINOR BURNING ODOR AFTER ALTIMETER FROZE. PULLED A-3 CIRCUIT BREAKER AND ODOR SUBSIDED. REMOVED AND REPLACED CAPTAIN`S ALTIMETER IAW AMM 34-12, CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 64,092 hrs · 46,224 cycles

ON SERVICE, FOUND FIRST CLASS EMERGENCY PATH LIGHTS INOPERATIVE. T/S AND FOUND BATTERY AND POWER SUPPLY BAD. R & R POWER SUPPLY AND BATTERY IAW AMM 33-53. OP CHECK GOOD, OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,598 hrs · 45,884 cycles

THE FLIGHT CREW FOUND THE EMERGENCY LIGHTS AT ROWS 1 THROUGH 12 INOPERATIVE. MAINTENANCE REPLACED THE CHARGER AND BATTERY PACK AND THE LIGHTS CHECKED OK.

Part: LINE — LOOSE (FUEL SYSTEM) · airframe 63,542 hrs · 45,844 cycles

STRONG JET FUEL ODOR IN AIRPLANE AFTER STARTING APU GROUND PERSONNEL POINTED OUT FUEL FROM LT SIDE OF ACFT. FOUND RT WHEEL WELL UPPER AFT FUEL LINE IN SHROUD UNSAFTIED AND LOOSE. RESECURED LINE IAW AMM 28-20. REINST SHROUD IAW AMM 28-20.

Part: LINE — LOOSE (FUEL SYSTEM) · airframe 63,542 hrs · 45,844 cycles

STRONG JET FUEL ODOR IN AIRPLANE AFTER STARTING APU GROUND PERSONEL POINTED OUT FUEL FROM LT SIDE OF ACFT. FOUND RT WHEEL WELL UPPER AFT FUEL LINE IN SHROUD UNSAFTIED AND LOOSE. RESECURED LINE IAW AMM 28-20. REINST SHROUD IAW AMM 28-20.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 63,480 hrs · 45,809 cycles

CRACKED VERTICAL STABILIZER SPAR CAP ON WEB BS 1463 CANT POS 11 HRS AT AFT ACCESORIES COMPARTMENT. VERTICAL STABILIZER SPAR CAP WAS REPAIRED IAW ER/A 543145-14, REV ORIGINAL AND ETI 88-16-059, REV 7, LENGHT CRACK 6".

Part: CAP — CRACKED (BS 1463) · airframe 63,480 hrs · 45,809 cycles

CRACKED LOWER CAP BS 1463, CANT 11 HRS POSITION AT AFT ACCESORIES COMPARTMENT. LOWER CAP WAS REPAIRED IAW ETI 88-16-059, REV 7 AND ER/A 543145-14, REV ORIG SECTION I, TEMPORARY REPAIR, LENGHT CRACK 4".

Part: SKIN — CORRODED (HEATER) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON RT HEATER BLANKET SKIN AROUND ACCESS PLATE 1410C. RT HEATER BLANKET SKIN WAS REPAIRED WITH ER/A 543147-14AD, REV ORIGINAL.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 63,480 hrs · 45,809 cycles

CRACKED VERTICAL STABILIZER SPAR CAP ON WEB BS 1463 CANT POS 11 HRS AT AFT ACCESSORIES COMPARTMENT. VERTICAL STABILIZER SPAR CAP WAS REPAIRED IAW ER/A 543145-14 REV ORIGINAL SECTION I AND ETI-88-16-059, REV 7, TEMPORARY REPAIR. THIS REPAIR WILL BE MONITORING UNDER LOG PAGE 2399002 IAW ER/A 543145-14, REV ORIGINAL, SEC. II.

Part: FRAME — CRACKED (BS 1437) · airframe 63,480 hrs · 45,809 cycles

CRACKED FRAME ANGLE BS 1437 BETWEEN LONGERONS 3L - 3R. THE FRAME ANGLE WAS REPAIRED IAW ETI-88-16-113, REV 1 AND ER/A 543208-14, REVISION ORIGINAL.

Part: FRAME — CRACKED (BS 1463) · airframe 63,480 hrs · 45,809 cycles

CRACKED LOWER CAP BS 1463, CANT 11 HRS POSITION AT AFT ACCESORIES COMPARTMENT. LOWER CAP WAS REPAIRED IAW ETI-88-16-059, REV 7 AND ER/A 543145-14, REV ORIGINAL. SECTION I.

Part: PANEL — DAMAGED (RT SLAT) · airframe 63,480 hrs · 45,809 cycles

NICK ON RIB BORE AT RT SLAT PANEL NR 3 XOS= 286. BORE WAS REPAIRED IAW ER/A 543189-14 REV ORIG.

Part: SKIN — DENTED (CARGO DOOR) · airframe 63,480 hrs · 45,809 cycles

SEVERAL DENTS ON OUTER SKIN OF C3 DOOR. DENTS ON OUTER SKIN WERE MEASURED ARE CONSIDERED ADJACENT THEREFORE ARE OUT LIMITS IAW SRM 53-04-1, PAR 7C DENTS ADJACENT WERE ATTENDED WITH ERA 543153-14, REV ORIGINAL.

Part: WEB — CRACKED (RT WING) · airframe 63,480 hrs · 45,809 cycles

CRACKED INNER WEB XRS 173 AT RT WING FIXED L/E INNER STRUCTURE. WEB CREAKED WAS REPAIRED IAW ETI-88-16-06 REV 2 AND ER/A 543205-14 REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1338) · airframe 63,480 hrs · 45,809 cycles

CRACK ON LONGERON END FITTING 1 BS 1338. LONGERON END WAS REPLACED IAW SRM 53-14-3, 51-30-5 AND 51-10-3, PAR 21 AND 14.

Part: FRAME — CRACKED (BS 1463) · airframe 63,480 hrs · 45,809 cycles

CRACKED CAP ON FRAME, BS 1463, CANT 4 HRS POS AT AFT ACCESSORY COMPARTMENT. CAP WAS REPAIRED IAW SRM 53-01, FIG 1, FIG 2, SRM 51-30-5, SRM 51-01, PAR 21.

Part: FINGER DOUBLER — CORRODED (BS 1193-1231) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON INNER FINGER DOUBLER AT SPLICE 26 LT BETWEEN BS 1193 AND BS 1231. FASTENERS WERE REMOVED IAW SRM 51-30-2. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. FINGER DOUBLER WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. FINGER DOUBLER WAS FABRICATED IAW SRM 53-04, FIG 12E. FINGER DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,480 hrs · 45,809 cycles

CRACKED LONGERON 4 RT BS 1437 AT AFT ACC COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 1, 51-30-5, 51-10-3 PAR 21 AND 14 51-10-4.

Part: PRESSURE PANEL — CORRODED (BS 939) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON SLANT PRESSURE PANEL BS 939 BETWEEN BS 939 BETWEEN X=22 TO X=44 AT WING BOX. SLANT PRESSURE PANEL WAS REPLACED IAW SRM 51-30-2, 51-10-3 PAR 14, 21, 38 51-10-4 DWG 9923419, REV AG, AMM 20-30-01.

Part: INTERCOSTAL — CORRODED (BS 769-788) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON INTERCOSTAL FROM BS 769 TO BS 788 BETWEEN LONGERON 27RT TO 28RT AT MID CARGO COMPARTMENT. INTERCOSTAL WAS REMOVED AND NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2, 51-30-5 NEW INTERCOSTAL WAS FABRICATED IAW DWG 9915554, REV J AND SRM 51-10-2.

Part: INTERCOSTAL — CORRODED (BS 769-788) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON INTERCOSTAL FROM BS 769 TO BS 788 BETWEEN LONGERON 28LT TO 27LT AT MID CARGO COMPARTMENT. INTERCOSTAL WAS REPLACED BY NEW 1 IAW SRM 51-30-2, 51-30-5, 51-10-4.

Part: FRAME — CRACKED (BS 1463) · airframe 63,480 hrs · 45,809 cycles

CRACKED WEB ON FRAME BS 1463 CANT 2 HRS POS AT AFT ACCY COMPARTMENT. WEB AND DOUBLER WERE REPLACED IAW DWG 9953015, REV CB ITEMS -58 AND -38 AND SRM 51-10-3, 51-10-3, 51-30-5 AND 51-30-2.

Part: HINGE — CORRODED (ELEVATOR) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON BORE TO ATTACH BUSINGS AT LT ELEVATOR HINGE NR 1. BORES WERE REPAIRED IAW ETI-88-16-101, REV 1 AND ER/A 543191-14 REV ORIGINAL.

Part: STIFFENER — CRACKED (BS 1463) · airframe 63,480 hrs · 45,809 cycles

CRACKED STIFFENER ON FRAME BS 1463 CANT POS 11 HRS AT AFT ACCESSORIES COMPARTMENT. STIFFENER WAS REPLACED IAW SRM 51-10-3, 51-30-5 AND 51-10-4 AND DWG 9953015 REV. CB.

Part: BUSHING — CORRODED (LT SPOILER) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON BUSHING HOUSING AT REACTION LEVER FITTING LT INBD SPOILER AREA. BUSHINGS HOUSINGS WERE REPAIRED IAW ER/A 543179-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 463) · airframe 63,480 hrs · 45,809 cycles

CRACKED WEB ON FRAME STA 463 CANT POS 11 HRS AT AFT ACCESORIES COMPARTMENT. WEB, STIFFENERS AND DOUBLERS WERE REMOVED IAW SRM 51-30-2 AND 51-30-5. WEB WAS FABRICATED IAW DWG 9953015, REV. CB ITEM-53. NEW WEB AND STIFFENERS DOUBLER WERE INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3 AND DWG 9953015, REV CB.

Part: BUSHING — CORRODED (RT SPOILER) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON BUSHING HOUSING AT REACTION LEVER FITTING RT INBD SPOILER AREA. BUSHINGS HOUSINGS WERE REPAIRED IAW ER/A 543179-14, REV ORIGINAL.

Part: DOUBLER — DELAMINATED (LT WING TE FLAP) · airframe 63,480 hrs · 45,809 cycles

DELAMINATED UNDER DOUBLER UPPER SKIN STA- XOVIF 66 ON LT INBOARD FLAP OUTBOARD GUIDE VANE. DAMAGE AREA WAS REAPAIRED IAW ERA NR 543167-14, REV ORIG.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,480 hrs · 45,809 cycles

CRACKED LONGERON 16R BS 1437 AT AFT ACC COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 51-30-2 , 51-30-5, 51-10-3 PAR 14 AND 21.

Part: FRAME — CRACKED (BS 1510) · airframe 63,480 hrs · 45,809 cycles

CRACKED FRAME, BS 1510 CANT 5 HRS POS AT AFT ACC COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, PAR 21, 14.

Part: SKIN — CRACKED (BS 374) · airframe 63,480 hrs · 45,809 cycles

CRACKS OF 1.156" AND 0.093" ON FUSELAGE SKIN ON BS 374 AT THE UPPER FWD DOOR JAMB CORNER OF THE FWD CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED IAW ER/A 543154-14AD, REV ORIG.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,480 hrs · 45,809 cycles

CRACKED DOOR PAN ON AFT, FWD SIDE AND BEAM NR 5 AT AFT CARGO DOOR INNER STRUCTURE. C3 DOOR WAS REPLACED IAW IPC-52-30-02.

Part: FRAME — CRACKED (BS 1418) · airframe 63,480 hrs · 45,809 cycles

CRACKED UPPER CAP FRAME BS 1418, LONG 2 LT AT AFT ACCESSORY COMPARTMENT. UPPER CAP FRAME WAS REPAIRED IAW SRM 53-01, FIG 2 , SRM 51-30-5 AND DWG SR09530003.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION WAS FOUND ON FASTENER HOLES COMMON TO THE LT LOWER ACCESS DOOR CUTOUT, AT THE XRS 199- 200 AND BETWEEN STR 12 AND 15. CORROSION WAS REPAIRED IAW ER/A 543177-14AD, REV ORIG.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION WAS FOUND ON FASTENER HOLES COMMON TO THE RT LOWER ACCESS DOOR CUTOUT, AT THE XRS=191-211 BETWEEN STR 12 AND 15. CORROSION WAS REPAIRED IAW ER/A 543177-14AD, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1380) · airframe 63,480 hrs · 45,809 cycles

CRACKED FRAME CLIP BS 1380 PROYECTION LONG 15 LT AT AFT ACC COMPARTMENT. FABRICATED AND REPLACED FRAME CLIP IAW SRM 53-14-4 AND 51-10-3, PAR 14 AND 21 AND 51-30-5 AND 51-30-2, 51-10-4.

Part: LONGERON — CRACKED (BS 1418) · airframe 63,480 hrs · 45,809 cycles

CRACKED END LONGERON 2L BS 1418 AT AFT ACCESSORY COMPARTMENT. REPAIR LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, SRM 51-30-5.

Part: FLOOR SUPPORT — CRACKED (NOT REPORTED) · airframe 63,480 hrs · 45,809 cycles

CRACKED FLOOR SUPPORT. NEW FLOOR SUPPORT INSTALLED. REMOVED SRM 51-30-1. DRILLED SRM 51-10-4. INSTALLED DWG 9936639, REV P.

Part: SKIN — CRACKED (LT WING) · airframe 63,480 hrs · 45,809 cycles

CRACK ON FIXED L/E LOWER SURFACE LT WING BS XRS=218. FIXED L/E LOWER LT WING WAS REPAIRED IAW ER/A 380953-14MA, REV A.

Part: FRAME — CRACKED (BS 1380) · airframe 63,480 hrs · 45,809 cycles

CRACKED FRAME CLIP BS 1380 LONG 15 RT AT AFT ACCESSORY COMPARTMENT. FRAME CLIP WAS REPLACED IAW SRM 53-14-4, SRM 51-30-2, SRM 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,480 hrs · 45,809 cycles

CRACKED LONGERON 3 LT BS 1437 AT AFT ACCESSORY COMPARTMENT. SPLICE, SUPPORT AND LONGERON WERE REMOVED IAW SRM 51-30-2 AND 51-30-5. SPLICE, SUPPORT AND LONGERON WERE INSTALLED IAW SRM 51-30-5, SRM 53-02, FIG 18. LONGERON WAS FOUND PREVIOUSLY REPAIRED IAW SRM 53-02, FIG 18.

Part: BULKHEAD — NICKED (BS 1338) · airframe 63,480 hrs · 45,809 cycles

NICKS FOUND ON REAR FACE OF LOWER T-CAP AT BS 1338, P DOME, BETWEEN PROYECTION OF LONGERONS 27 LT AND 29 LT, REF CARD 4, ZONE 59 20000102603. T-CAP AT BS 1338, P-DOME BETWEEN PROYECTION OF LONGERON 23 LT AND 23 RT WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND SRM 53-03D, FIG 37A.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 63,480 hrs · 45,809 cycles

PUCTURED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 63,480 hrs · 45,809 cycles

CRACKED SKIN ON UPPER SURFACE OF RT OTBD FIXED GUIDE VANE INBD FLAP. UPPER SURFACE OF RT OTBD FIXED GUIDE VANE INBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR. II.

Part: BEAM — CRACKED (BS 173) · airframe 63,480 hrs · 45,809 cycles

CRACKED BEAM Z=30.187 AND BS 173.5 AT FWD AREA OF FWD SERVICE DOOR. DAMAGE BEAM WAS REPLACED IAW SRM 51-30-2, 51-30-5.

Part: ANGLE — CORRODED (BS 190) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON CUSP ANGLE UNDER R1 DOOR JAMB PAN APPROXIMATELY BS 190. EXCESSIVE CORROSION WAS FOUND, THEREFORE AREA WAS REPAIRED IAW SRM 53-05, FIG 55, 51-30-1, 51-30-2, 51-30-5, 51-10-3, 51-10-4 AMM 21-20-00, 21-00-00 AND ER/A 543175-14 REV ORIGINAL.

Part: ANGLE — CRACKED (BS 1309) · airframe 63,480 hrs · 45,809 cycles

CRACK ON FRAME ANGLE BS 1309, LONG 16LT. ANGLE WAS REPLACED IAW SRM 51-30-5 AND DWG 9912243, SRM 53-14-3.

Part: STRUCTURE — CRACKED (RT WING) · airframe 63,480 hrs · 45,809 cycles

CRACK ON RT WING L/E BS XOS=286. REPAIRED IAW ER/A 397957-14MA, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA AT WING ACCESS PLATE NR 1478C. CORROSION WAS REMOVED, MEASURED SETTLEMENT WAS ACCOMPLISHED ORIGINAL THICKNESS IS .150", REMAINING THICKNESS IS .138", THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MAXIMUN DIAMETER ALLOWABLE IS .532" AND WAS FOUND 1 COUNTERSINK OUT OF LIMITS, MEASURE .545" THEREFORE HOLE AND COUNTERSINK WERE REWORKED AND MEASURED WITH ID .608" COUNTERSINK AND HOLE .346", BUSHING WAS FABRICATED OD .347" AND COUNTERSINK .509", AREAS AND BUSHING WERE TREATED AND BUSHING WAS INSTALLED IAW SRM 51-22-2A, COND II AND 51-10-3.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 63,480 hrs · 45,809 cycles

DELAMINATED UPPER SURFACE ON INBD GUIDE VANE AT LT WING OTBD FLAP, POSITION 3, BS XV1=170. UPPER SURFACE ON INBD GUIDE VANE AT LT WING OTBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR II.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE 1377C. CORROSION WAS REMOVED, MEASURED SETTLEMENT AREA WAS ACCOMPLISHED, ORIGINAL THICKNESS IS .150" REMAINING THICKNESS IS .140", THEREFORE IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS .532" AND WAS FOUND COUNTERSINK OUT OF LIMITS MEASURED .550" THEREFORE HOLE AND COUNTERSINK WERE REWORKED AND MEASURED WITH 1D .320" COUNTERSINK .609" AND BUSHING WAS FABRICATED OD .331" COUNTERSINK .512", AREAS AND BUSHING WERE TREATED AND BUSHING WAS INSTALLED IAW SRM 51-22-2A COND II AND 51-10-3.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1414C. CORROSION WAS REMOVED, MEASURED ON SETTLEMENT WAS ACCOMPLISHED, ORIGINAL THICKNESS IS .180" REMAINING THICKNESS IS .172" THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MINIMUM DIAMETER ALLOWABLE WERE REWORKED AND MEASURED WITH NR 1 ID .3865" AND COUNTERSINK .729", 2 ID .387"AND COUNTERSINK .731", NR 3 ID 0.387" AND COUNTERSINK .734", THEREFORE WITHIN LIMITS OF MAXIMUM HOLE DIAMETER REWORK, BUSHINGS WERE FABRICATED NR 1 OD .388" AND COUNTERSINK .635", NR 2, OD 388" AND COUNTERSINK .632" NR 3 OD .388" AND COUNTERSINK .639", AREAS AND BUSHINGS WERE TREATED AND BUSHINGS WERE INSTALLED IAW SRM 51-22-2A, COND II AND 51-10-3.

Part: FRAME — CORRODED (BS 1250) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON PREVIOUS DOUBLER REPAIR ON FRAME BS 1250, BETWEEN LONGERON 27LT - 27RT AT AFT CARGO COMPARTMENT. AREA RT WAS CLEANED AND CORROSION NO WAS FOUND, PREVIOUS DOUBLER REPAIR, LT WAS REPLACED IAW SRM 53-03, FIG 2A, PS. 900-1-2-1 N 01. (LP2384607)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE 1363C. CORROSION WAS REMOVED, MEASURED SETTLEMENT WAS ACCOMPLISHED, ORIGINAL THICKNESS IS .150", REMAINING THICKNESS IS .137" THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED, MAXIMUN DIAMETER ALLOWABLE IS .532" AND WAS FOUND 1 COUNTERSINK OUT OF LIMITS MEASSURED .544", THEREFORE HOLE AND COUNTERSINK WERE REWORKED AND MEASURED WITH ID .346" COUNTERSINK .608" THEREFORE WITHIN LIMITS OF MAXIMUM HOLE REWORKED DIAMETER, BUSHING WAS FABRICATED OD .347", COUNTERSINK OF .509" AREAS AND BUSHING WERE TREATED AND BUSHING WAS INSTALLED IAW SRM 51-22-2A, COND II AND 51-10-3.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AT WING ACCESS PLATE NR 1367C. CORROSION WAS REMOVED, COUNTERSINKS WERE MEASURED, MAXIMUN DIAMETER ALLOWABLE IS .532" AND WERE FOUND 2 COUNTERSINK OUT OF LIMITS MEASURED .551" AND .554" THEREFORE HOLES AND COUNTERSINKS WERE REWORKED, AND WERE MEASURED NR 1 ID .329" AND COUNTERSINK .622"N NR 2 ID .3295" AND COUNTERSINK .620" THEREFORE IT IS WITHIN LIMITS OF MAXIMUN HOLE DIAMETER REWORK AND BUSHINGS WERE FABRICATED NR 1, OD .330" COUNTERSINK .511", NR 2 OD .330" COUNTERSINK .512", AREAS AND BUSHINGS WERE TREATED, BUSHINGS WERE INSTALLED IAW SRM 51-22-2A, COND II AND SRM 51-10-3.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,480 hrs · 45,809 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL REPAIRED IAW AMM 53-20-01.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AT WING ACCESS PLATE NR 1464C. CORROSION WAS REMOVED, COUNTERSINKS WERE MEASURED AND MAXIMUN DIAMETER ALLOWABLE IS .532" AND WAS FOUND 1 COUNTERSINK OUT OF LIMITS MEASURE .568", THEREFORE HOLE AND COUNTERSINK WAS REWORKED AND MEASURED WITH I.D. .3455" AND COUNTERSINK .607" THEREFORE IS WITHIN LIMITS OF MAXIMUN HOLE DIAMETER REWORK AND BUSHING WAS FABRICATED OD .3465" AND COUNTERSINK .508" AREAS AND BUSHING WERE TREATED AND BUSHING WAS INSTALLED IAW SRM 51-22-2A, COND II AND 51-10-3, MEASURED SETTLEMENT WAS ACCOMPLSHED ORIGINAL THICKNESS IS .150" REMAINING THICKNESS IS .134" THEREFORE IT IS WITHIN LIMITS IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE NR 1472C. CORROSION WAS REMOVED, MEASURED SETTLEMENT AREA WAS ACCOMPLISHED ORIGINAL THICKNESS IS .150", REMAINING THICKNESS .138" THEREFORE IT IS WITHIN LIMITS, COUNTERSINK WERE MEASURED MAXIMUM DIAMETER ALLOWABLE IS .532" AND WAS FOUND 1 COUNTERSINK OUT OF LIMITS MEASURED .550" THEREFORE HOLE AND COUNTERSINK WERE REWORKED AND MEASURE WITH ID .3465" AND COUNTERSINK .606", BUSHING WAS FABRICATED WITH OD .347" AND COUNTERSINK OD .507 ", AREAS AND BUSHING WERE TREATED AND BUSHING WAS INSTALLED IAW SRM 51-22-2A, COND II AND 51-10-3.

Part: DOOR FRAME — PUNCTURED (BS 629) · airframe 63,480 hrs · 45,809 cycles

PUNCTURED MID CARGO DOOR JAMB WEB BS 629, PROJECTION LONGERON 26RT AT C2. DAMAGE WAS REPAIRED IAW SRM 51-70-4.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK OF WING ACCESS PLATE 1365C. CORROSION WAS REMOVED, COUNTERSINKS WERE MEASURED MAXIMUM DIAMETER ALLOWABLE IS .532 AND FOUND COUNTERSINK OUT OF LIMITS IN .547, THEREFORE HOLE AND COUNTERSINK WERE REWORKED AND MEASURED WITH ID HOLE .3305 AND COUNTERSINK .605, BUSHING WAS FABRICATED OD 3320 AND COUNTERSINK .510 AREAS AND BUSHING WERE TREATED AND BUSHING WAS INSTALLED SRM 51-22-2A, COND II.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AT WING ACCESS PLATE 1373 C. CORROSION WAS REMOVED , COUNTERSINKS WERE MEASURED. MAXIMUM DIAMETER ALLOWABLE IS .532" AND WERE FOUND 2 COUNTERSINKS OUT OF LIMITS IN .540" AND .559" THEREFORE HOLES AND COUNTERSINKS WERE REWORKED AND WERE MEASURED ID .345" AND .3445" AND COUNTERSINK IN .608" AND .605". BUSHING WERE FABRICATED WITH OD .3465" AND COUNTERSINK .510" OD .3465" AND COUNTERSINK .513" AREAS AND BUSHINGS WERE TREATED AND BUSHINGS WERE INSTALLED IAW SRM 51-22-2A COND II AND SRM 51-10-3.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,480 hrs · 45,809 cycles

DELAMINATION PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: FLOORBEAM — CRACKED (BS 927) · airframe 63,480 hrs · 45,809 cycles

CRACKED FLOORBEAM X 54, BS 927 AT FLOOR STRUCTURE CABIN. CRACKED FLOORBEAM WAS REMOVED AND NEW FLOORBEAM WAS DRILLED AND WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5 AND 51-10-3 AND DWG 5930561, REV AC.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AT WING ACCESS PLATE NR 1357C. SM, CARD 407, ZONE 100. CORROSION WAS REMOVED, COUNTERSINK WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS .532" AND WERE FOUND 2 COUNTERSINKS OUT OF LIMITS, MEASURED .539" AND .539" THEREFORE HOLES AND COUNTERSINKS WERE REWORKED AND MEASURED 1, 1.0 .329" COUNTERSINK .617" NR 2, 1.0 .330" COUNTERSINK .605" , BUSHINGS WERE FABRICATED WITH OD NR 1 .330 AND COUNTERSINK .511" NR 2, OD. .3305" AND COUNTERSINK .512" AREAS AND BUSHINGS WERE TREATED AND BUSHINGS WERE INSTALLED IAW SRM 51-22-2A, COND II AND 51-10-3. TOOL USED GAGE, PN 1127, S/N 55759 D/D 23-MAR-16.

Part: SUPPORT — CORRODED (BS 1343) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON SUPPORTS BS, 2EA AT LWR AREA OF AFTER ACCESSORIES BS 1343. SUPPORTS INTERCOSTAL WERE REPLACED IAW SRM 51-302, 51-30-5 DWG: 9915520, REV M.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA AT WING ACCESS PLATE 2301C. CORROSION WAS REMOVED, MEASURE SETTLEMENT WAS ACCOMPLISHED ORIGINAL THICKNESS IS .180" REMAINING THICKNESS IS .172", THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS . 660" AND WAS FOUND 2, COUNTERSINKS OUT OF LIMITS MEASURED .673" AND .679" THEREFORE HOLE AND COUNTERSINKS WERE REWORKED AND MEASURED WITH NR 1 ID 4045" AND COUNTERSINK .727" NR 2 ID .4045" AND COUNTERSINK .733" THEREFORE WITHIN LIMITS OF MAXIMUM HOLE REWORK DIAMETER BUSHING WERE FABRICATED NR 1 OD.4055 AND COUNTERSINK .630" NR 2 .4055" AND COUNTERSINK .636", AREAS AND BUSHINGS WERE TREATED AND BUSHING WAS INSTALLED IAW SRM 51-22-2A, COND II.

Part: CUSP WEB — CORRODED (BS 1060-1079) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON CUSP WEB FROM BS 1060 TO 1079, X -60 TO X -54. CUSP WEB REPLACED IAW SRM 51-30-2 , 51-30-5 , 51-30-1 AND DWG 9930612, 51-10-3, PAR 14 AND 21.

Part: FRAME — WORN (BS 1497) · airframe 63,480 hrs · 45,809 cycles

WEAR ON FRAME BS 1497 CANT 10 HRS POSITION AT AFT ACC COMPARTMENT. WEAR WAS BLENDED OUT, MEASURE ORIGINAL THICKNESS 0.040, REMAINING 0.039 WITH IN LIMITS REWK AREAS WERE TREATED AND PAINTED IAW ER/A 511165-14 AM REV C AND SRM 51-10-3, PAR 14/21.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE NR 2302C. CORROSION WAS REMOVED, MEASURED SETTLEMENT AREA WAS ACOMPLISHED ORIGINAL THICKNESS IS .172" THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS .660" AND WAS FOUND COUNTERSINK OUT OF LIMITS MEASURE .672" THEREFORE HOLE AND COUNTERSINK WERE REWORKED AND MEASURED WITH ID .4435" COUNTERSINK .730", BUSHING WAS FABRICATED WITH OD .4445" AND COUNTERSINK .728" AREAS AND BUSHING WERE TREATED AND BUSHING WAS INSTALLED IAW SRM 51-22-2A COND II.

Part: LONGERON — CRACKED (BS 180) · airframe 63,480 hrs · 45,809 cycles

CRACKED LONGERON 2L BS 180. DAMAGED WAS REMOVED, A NEW LONGERON AND SPLICE WERE DRILLED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2, 51-30-5, 53-02, FIG 18 51-10-3, PAR 14 AND 21.

Part: CUSP WEB — CRACKED (BS 885-906) · airframe 63,480 hrs · 45,809 cycles

CRACKED CUSP WEB BELOW SEAT TRACK X=-54, BS 885 AND 906 IN PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 51-30-2 , 51-30-5 , 51-10-3, PAR 11, 21 AND 38, 53-05, FIG 131A.

Part: FLOOR PANEL — DELAMINATED · airframe 63,480 hrs · 45,809 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,480 hrs · 45,809 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: DOOR FRAME — CORRODED · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON AFT VENTRAL DOOR LOWER FRAME X=9. DUE TO EXCESSIVE DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 34.

Part: FITTING — CORRODED (BS 1271) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON RT FRAME FITTING BS 1271 AT FLOOR LEVEL. FITTING WAS REPLACE IAW SRM 51-30-01.

Part: FITTING — CORRODED (BS 1271) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON RT FRAME FITTING BS 1271 AT FLOOR LEVEL. FITTING WAS REPLACE IAW SRM 51-30-01.

Part: FLOOR PANEL — BROKEN (PAX CABIN) · airframe 63,480 hrs · 45,809 cycles

BROKEN PAX CABIN FLOOR PANEL. FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-01, FIG 4, SL 4 51-10-3, PAR 14, 21.

Part: FRAME — CORRODED (BS 1150) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON FRAME ANGLE BS 1150 BETWEEN LONGERON 29 - 30R. THE FRAME ANGLE WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-30-3, 51-10-2, 51-10-2A, 51-10-3 PAR 21 AND 14 AND DWG 9936074.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 63,480 hrs · 45,809 cycles

DAMAGE FERRULES ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: CUSP WEB — CORRODED (BS 845-839) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON RT REPAIR DOUBLER ON CUSP WEB UPPER SURFACE BETWEEN BS 845 TO 839 AND BETWEEN X -54 TO X -60. REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14, 21 AND 38, 53-05 FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 1060-1079) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 1060 TO 1079 BETWEEN X 54 TO X 60 UPPER SURFACE. REPAIRED IAW SRM 53-05, FIG 131A-14 51-10-3, PAR 26, 21, 14 AND 38 51-30-2, 51-30-5.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 63,480 hrs · 45,809 cycles

DELAMINATED UPPER SURFACE ON OTBD GUIDE VANE AT RT WING INBD FLAP. OTBD GUIDE VANE AT RT WING INBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR II.

Part: ANGLE — CORRODED (BS 1380) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

SEVERAL CORROSION POINTS ON ANGLE OF FRAME BS 1380 FROM LONGERON 24L - 24R. THE ANGLE WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 760) · airframe 63,480 hrs · 45,809 cycles

CRACK ON MEMBRANE CUSP WEB LOWER SURFACE BS 760 BETWEEN X= 54 AND X=60RT. CRACK WAS REPAIRED IAW SRM 53-05, FIG 131, 51-10-3, PAR 14, 21, 38, 51-30-5, 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 1322) · airframe 63,480 hrs · 45,809 cycles

CRACK ON INTERCOSTAL, BS 1322 BETWEEN X=1 TO X=2. INTERCOSTAL WAS REPAIRED IAW SRM 53-01.

Part: SEAT TRACK — CORRODED (BS 580-581) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION OUT OF LIMIT ON LT SEAT TRACK, X=22, BS 580-581 IN PASSENGER CABIN FLOOR STRUCTURE. SEAT TRACK WAS REPAIRED IAW SRM 51-30-1, 51-10-3 PAR 14 AND 21 AND 53-05, FIG 4A.

Part: SKIN — DELAMINATED (LT WING SPOILER) · airframe 63,480 hrs · 45,809 cycles

INBD FLIGHT SPOILER LOWER SURFACE OF LT WING DELAMINATED AT BS XRS=214. FLIGHT SPOILER WAS REPAIRED IAW SRM 51-70-1B, PAR 5.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,480 hrs · 45,809 cycles

DAMAGE FERRULES ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AT WING ACCESS PLATE NR 1361C. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 758-769) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION OUT LIMITS ON LT CUSP WEB BETWEEN BS 758 TO 769, X=44 TO 60 AT PAX CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-2, 51-10-3, PAR 21, 14 AND 38 , 51-30-5 AND 51-30-2.

Part: DOUBLER — CRACKED (BS 1409) · airframe 63,480 hrs · 45,809 cycles

CRACKED INNER PRODUCTION DOUBLER, BS 1409, LONGERON 2 LT AT AFT ACCY COMPARTMENT. DOUBLER WAS REPLACED IAW SRM 51-30-2 AND 53-34-0, 51-10-4.

Part: INTERCOSTAL — CRACKED (BS 1287-1307) · airframe 63,480 hrs · 45,809 cycles

CRACKED INTERCOSTAL BEYOND STOP DRILL, X=0 BETWEEN BS 1307-1287 AT FLOOR STRUCTURE CABIN. INTERCOSTAL WAS REPLACED BY NEW 1 IAW SRM 51-30-2, 51-30-5 AND 51-10-3 PAR 14 AND 21.

Part: SKIN — DAMAGED (RT MLG DOOR) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON SKIN UNDER RUB STRIP AT RT MLG STRUT DOOR. MLG DOOR WAS REPLACED IAW AMM 32-12-01.

Part: LONGERON — CRACKED (BS 522-541) · airframe 63,480 hrs · 45,809 cycles

CRACK ON LONG 4 RT BETWEEN BS 522 - 541 AT PASSENGER CABIN INTERNAL STRUCTURE. REMOVE AND INSTALL INTERCOSTAL, LONGERON 4 WAS REPAIRED IAW SRM 53-02, FIG 18 AND 51-30-5 AND 51-30-2.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 63,480 hrs · 45,809 cycles

DELAMINATED FLOOR PANEL. FABRICATED IAW AMM 53-20-01-201.

Part: PAN — CRACKED (BS 1250-1231) · airframe 63,480 hrs · 45,809 cycles

CRACKED LT RING PAN ON UPPER/AFT CORNER BETWEEN BS 1250/1231 AT PAX CABIN. DAMAGE WAS REMOVED AND REPAIR PARTS WERE FABRICATED, TREATED AND PAINTED AND WERE INSTALLED IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (DOO) · airframe 63,480 hrs · 45,809 cycles

CRACK ON FWD PAN BETWEEN BEAM 3 AND BEAM 4 AT FWD SERVICE DOOR (R1). DOUBLER AND SHIMS WERE FABRICATED AND PAN WAS REPAIRED IAW SRM 52-03D, FIG 3.

Part: PAN — CRACKED (BS 712-1022) · airframe 63,480 hrs · 45,809 cycles

CRACKED LT RING PAN ON LOWER, AFT CORNER BETWEEN BS 712 - 1022 AT PAX CABIN. DAMAGE WERE REMOVED AND REPAIR PARTS WERE FABRICATED TREATED AND PAINTED AND WERE INSTALLED IAW SRM 53-05, FIG 122.

Part: WEB — CORRODED (BS 168) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON WEB BS 187, BS 168.750 BETWEEN X=-53 TO X=-48. WEB WAS REPLACE IAW SRM 51-30-2 AND 51-30-5, 53-14-1 AND 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CRACKED (BS 224) · airframe 63,480 hrs · 45,809 cycles

CRACKED RT CUSP WEB BS 224 BETWEEN X=-54 TO -60 AT PAX CABIN FLOOR STRUCTURE. CRACKED WAS ATTENDED IAW SRM 51-30-2, 53-05 131A-13, 51-10-3 PAR 14, 21, 38.

Part: FLOOR PANEL — CORRODED (PAX CABIN) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON FLOOR PANEL 160G AT PAX CABIN. FLOOR PANEL WAS REPLACED IAW SRM 51-10-3 PAR 14 AND 21 51-30-2 AND DWG 9957828, REV AB.

Part: WEB — CORRODED (BS 148-160) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON MEMBRANES BETWEEN 148 AND 160 BETWEEN X=-22 AND X=-54 AT COCKPIT. DUE TO EXCESSIVE DAMAGE, MEMBRANE FROM BS 150 TO 160 BETWEEN X= -40 AND X -60 WAS REPAIRED IAW SRM 51-70-4, FIG 1.

Part: SEAT TRACK — CORRODED (BS 416-528) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION OUT LIMITS ON RT SEAT TRACK BS X=-54, BS 416 AND 528 AT PAX CABIN. DAMAGE AREA WAS REMOVED IAW SRM 53-05, FIG 4A AND ER/A 485415-14MA. NEW HOLES OF REPAIRS WERE DRILLED IAW SRM 53-05, FIG 4A AREA AND NEW HOLES WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21. PLUGS WERE INSTALLED IAW SRM 53-05, FIG 4A.

Part: FLOOR PANEL — PUNCTURED · airframe 63,480 hrs · 45,809 cycles

PUNCTURED 120B FLOOR PANEL UPPER SURFACE. DAMAGE WAS REPAIRED IAW SRM 53-01, 51-10-3, AND 51-30-2.

Part: BEAM — CRACKED (BS 173) · airframe 63,480 hrs · 45,809 cycles

CRACKED BEAM Z=11.083 AND BS 173.5 AT FWD AREA OF FWD SERVICE DOOR. BEAM WAS REPLACED IAW SRM 51-30-2, 51-30-4 AND 51-30-5.

Part: PAN — CRACKED (BS 807-1117) · airframe 63,480 hrs · 45,809 cycles

CRACKED LT RING PAN ON LWR/FWD CORNER BTW BS 807-1117. DAMAGE REMOVED AND REPAIR FABRICATED TREATED AND PAINTED AND INSTALLED IAW SRM 53-05, FIG 122.

Part: DUCT — CRACKED · airframe 63,480 hrs · 45,809 cycles

CRACKS ON DUCT, 4 EA, UPPER SETTLEMENT AREA, 1EA, LUGS 2EA AND NEAR OF FLANGE. UPPER SETTLEMENT AREA WAS REPAIRED IAW SOPM 20-10-19, PAR 3D. LUGS WERE REPAIRED IAW ER/A 494638-14MA, REV B. FLANGE WAS REPAIRED IAW ER/A 503276-14MA, REV C AND AREA WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21, CRACK ON FLANGE .300", UPPER SETTLEMENT AREA 2", CRACK LUGS .250".

Part: PAN — CRACKED (BS 731965) · airframe 63,480 hrs · 45,809 cycles

CRACKED LT RING PAN ON UPPER/FWD CORNER BETWEEN BS 731 - 965 IN PAX CABIN. DAMAGE WERE REMOVED AND REPAIR PARTS WERE FABICATED TREATED AND PAINTED AND WERE INSTALLED IAW SRM 53-05, FIG 122.

Part: DOOR FRAME — CRACKED (BS 207) · airframe 63,480 hrs · 45,809 cycles

CRACKED PREVIOUS REPAIR ON L1 AFT DOOR JAMB BS 207, LONG, 15LT. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 142, 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,480 hrs · 45,809 cycles

CRACK ON DOOR PAN INNER STRUCTURE AT FWD UPPER SIDE AND BEAM NR 5 OF FWD CARGO COMPARTMENT DOOR. INNER PAN WAS REPAIRED IAW SRM 52-03, FIG 8.

Part: RETAINER — CRACKED · airframe 63,480 hrs · 45,809 cycles

CRACK ON RETAINER Z=11.06 AT FWD EDGE OF FWD SERVICE DOOR. RETAINER WAS FABRICATED AND REPLACED IAW SRM 51-30-4 AND DWG 5910084, REV CRACK LT 0.250".

Part: WEB — PUNCTURED (BS 133) · airframe 63,480 hrs · 45,809 cycles

PUNCTURED ON WEB BS 133 X 52 APPROXIMATELY AT COCKPIT. WEB WAS REPAIRED IAW SRM 53-01, FIG 4, SRM 51-10-3, PAR 14, 21, 38.

Part: CUSP WEB — CORRODED (BS 731-750) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 731 - 750, X 54 TO X 60 AT CABIN STRUCTURE UPPER/LOWER SURFACE. CORROSION WAS ATTENDED IAW SRM 53-05, FIG 131A-7, SRM 51-30-2, 51-10-3, PAR 14, 21, 38.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AT WING ACCESS PLATE NR 1307C. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: DOOR FRAME — CRACKED (BS 1338) · airframe 63,480 hrs · 45,809 cycles

CRACKS ON RT/LT UPPER CORNERS OF VENTRAL STAIRWAY DOOR JAMB FRAME BS 1338 AT PAX CABIN INNER STRUCTURE. CRACK WAS REMOVED IAW 53-01, FIG 1 X=S/5, X=.650/5=.130. REWORKED AREA WAS TREATED, PAINTED IAW SRM 51-10-3, PAR 21/14.

Part: SEAT TRACK — NOT REPORTED (BS 880-881) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

OUT OF LIMITS SEAT TRACK BS 880 - 881, X -22. . REPAIRED IAW SRM 53-05, FIG 4A AND 51-10-3, PAR 14, 21.

Part: CUSP WEB — CRACKED (BS 1250) · airframe 63,480 hrs · 45,809 cycles

ELONGATED HOLE ON RT CUSP WEB BS 1250 AND X=-49 UPPER SURFACE. FASTENERS WERE REMOVED, DAMAGE WAS REMOVED, REPAIR PART WAS FABRICATED, NEW REPAIR PART WAS TREATED, PAINTED AND INSTALLED. CIC WILL BE APPLIED WITH NRC 20000100381 CARD NR 20 ZONE 201 IAW SRM 53-05, FIG 131A-17, 51-10-3, PAR 14 , 21, 51-30-2.

Part: FLOOR SUPPORT — DAMAGED (BS 1271-1287) · airframe 63,480 hrs · 45,809 cycles

CRACKED AND WEAR ON FLOOR SUPPORT X=3 BETWEEN BS 1287 AND 1271. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01, FIG 2 , 51-10-3, P 14, 26, 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA AT WING ACCESS PLATE NR 1410C. FOUND TO BE OUT OF LIMITS AND WAS REPLACED IAW SRM 51-02-2A, COND II.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 63,480 hrs · 45,809 cycles

CRACK ON SLAT PANEL NR 5 INNER SKIN BS XOS= 503 LT WING. DOUBLER WAS FABRICATED, TREATED AND PAINTED , INSTALLED IAW SRM 57-01, FIG 3, 51-10-3, 51-30-8.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTER SKIN AND SETTLEMENT OF FUEL ACCESS PLATE 1311C. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A, CONDITION II.

Part: SPAR — NOT REPORTED (RT WING) · airframe 63,480 hrs · 45,809 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND SEVEN DIFFERENT FASTENERS OF THE PSE ON RT LOWER WING SKIN REAR SPAR BETWEEN BS XRS= 162 TO XRS= 168.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AT WING ACCESS PLATE NR 1470C. ACCESS PLATE NR 1470C WAS REPLACED IAW SRM 51-22-2A, COND II.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON LONG 23 LT BETWEEN BS 1287 AND 1309. DUE TO EXCESSIVE CORROSION LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE NR 1454C. ACCESS PLATE NR 1454C WAS REPLACED IAW SRM 51-22-2A, COND II.

Part: CUSP WEB — CORRODED (BS 655-712) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON LT CUPS WEB BETWEEN 655 TO 674, 674 TO 693 AND 693 TO 712, X=44 TO X=60 AT CABIN FLOOR STRUCTURE, UPPER, LOWER SURFACE. SEAT TRACK AND CUSP WEB WERE REMOVED SEAT TRACK ON BS 579- 712 CUSP WEB 598- 712 AND PARTS ON CUSP WEB , NEW CUSP WEB WAS DRILLED TREATED AND PAINT INSTALLED SEAT TRACK AND CUSP WEB IAW SRM 53-14-02, FIG 4, 51.30.2, 51.30.1, 51.30.5, 51.10.4, 51.10.3.

Part: SKIN — DAMAGED (RUDDER) · airframe 63,480 hrs · 45,809 cycles

DAMAGED ALLUMINIZED ON RUDDER. METALLIZED ON RUDDER WAS REPAIRED IAW ER/A 092613-14MA, REV A.

Part: SPAR — NOT REPORTED (LT WING) · airframe 63,480 hrs · 45,809 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND SEVEN DIFFERENT FASTENERS OF THE PSE ON LT LOWER WING SKIN REAR SPAR BETWEEN BS XRS =162 TO XRS= 168. REPAIRED IAW ER/A NR 543146-14AD, REV ORIGINAL .

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE 1465C. ACCESS PLATE NR 1465C WAS REPLACED IAW SRM 51-22-2A, COND II.

Part: SKIN — WORN · airframe 63,480 hrs · 45,809 cycles

WEAR ON PREVIOUS REPAIR DOUBLERS AT OUTER SKIN FWD AND AFT BOTTOM CORNERS OF FWD CARGO COMPARTMENT. DAMAGE REPAIR DOUBLERS WERE REPLACED IAW ERA 486624-14MA, REV ORIGINAL.

Part: LONGERON — WORN (BS 522-541) · airframe 63,480 hrs · 45,809 cycles

WEAR ON LONG 2 RT BETWEEN BS 522-541 AT PAX CABIN INTERNAL STRUCTURE. LONGERON WAS REPLACED IAW SRM 51-30-2 , 51-30-5, 53-05, FIG 18, SHEET 1 AND 51-10-3, PAR 21, 14.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 63,480 hrs · 45,809 cycles

CRACK ON PAN AT LT EMERGENCY EXIT DOOR, FWD, AT STOP NR 12. CRACK ON PAN AT LT EMERGENCY EXIT DOOR WAS REPAIRED IAW SRM 52-05D, FIG 51.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 63,480 hrs · 45,809 cycles

CRACKED CLIPS ON RT FWD EMERGENCY EXIT DOOR AT STOP NR 1 AND 2. CLIP NR 1 WAS REPLACED IAW SRM 51-30-2 AND 51-30-5. HFEC INSPECTION WAS PERFORMED ON CLIPS ON RT FWD EMERGENCY DOOR AT STOP NR 1 AND 2, AND WAS FOUND A CRACK OF 0.187" LENGTH ON CLIP AT NR 1 STOP ONLY IAW NDT SPM 06-10-01.001.

Part: WEB — PUNCTURED (BS 150-160) · airframe 63,480 hrs · 45,809 cycles

PUNCTURE ON MEMBRANE BETWEEN 150-160, X=-5AT COCKPIT STRUCTURE. DAMAGE WAS REMOVED AND NO CRACKS WERE FOUND. NEW DOUBLER WAS FABRICATED AND NEW DOUBLER WAS INSTALLED IAW SRM 53-01 AND 51-10-3.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 63,480 hrs · 45,809 cycles

CRACKED CLIP ON LT FWD EMERGENCY EXIT DOOR AT STOP NR 1. CLIP WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG: 9957735, REV G.

Part: INTERCOSTAL — CRACKED (BS 1022-1041) · airframe 63,480 hrs · 45,809 cycles

CRACKED INTERCOSTAL BETWEEN BS 1022-1041 AND X=0 AT PAX CABIN FLOOR STRUCTURE. DAMAGE INTERCOSTAL WAS REPLACED IAW DWG 9936580, REV: BS SRM 51-10-4 , 51-10-3 PAR. 14 AND 21 AND 51-30-5 , 51-30-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSKIN AND SETTLEMENT OF FUEL ACCESS PLATE 1335C. ACCESS WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON OTBD GUIDE VANE AT RT WING OTBD FLAP, POSITION 5, BS XV2=297-327. FIXED VANE AT RT OTBD FLAP WAS REPLACED IAW SRM 57-03D PAR 11 AND AIPC 27-50-04-01A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE 1462C. ACCESS PLATE 1462C WAS FOUND OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A, CONDITION II.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AT WING ACCESS PLATE 1355C. ACCESS PLATE NR 1355C WAS FOUND OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A, COND II.

Part: MEMBRANE — CORRODED (BS 200-218) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON MEMBRANE BETWEEN 200 AND 218 BETWEEN X=-22 AND X=-60 AT CPAX. MEMBRANE WAS REPLACED IAW SRM 53-14-1 AND 51-10-3, PAR 14 AND 21 AND 51-10-4.

Part: PAN — CRACKED (BS 275-598) · airframe 63,480 hrs · 45,809 cycles

CRACKS ON AFT/LOWER CORNER OF LT WINDOW RING PAN AT BS 275-598 PASSENGER CABIN, SM REASON FOR RE-WRITE INADECUATE WASHERS ON REPAIR RE-WRITE FROM CARD 86, ZONE 201. NEW HARDWARE WERE INSTALLED IAW SRM 51-30-5, PAR 7 AND SRM 53-05, FIG 122.

Part: CUSP WEB — CORRODED (BS 242-246) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 242 TO 246 AND BETWEEN X=54 TO X=60. FASTENERS WERE REMOVED DUE TO EXCESIVE CORROSION WAS REPAIR. REPAIR PARTS WERE FABRICATED, DRILLED TREAT AND PAINT AND APPLIED CIC IAW SRM 53-05, FIG 131A-13, 51-10-3 PAR 14 AND 21 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 484-503) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION OUT OF LIMITS RT CUSP WEB BETWEEN BS 484 - 503 X=-54 TO -60 AT PAX CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, SRM 51-10-3, PAR 21 AND 14 AND SRM 51-30-5 CIC WILL BE APPLIED WITH CARD 17, ZONE 201.

Part: DOOR FRAME — CORRODED (BS 1338) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON LT LOWER SECTION OF VENTRAL STAIRWAY DOOR JAMB FRAME BS 1338 AT PASSENGER CABIN INTERNAL STRUCTURE. LOWER SECTION OF VENTRAL STAIRWAY DOOR JAMB FRAME WAS REMOVED, REPAIR PARTS WERE FABRICATED, TREATED, PAINTED INSTALLED IAW SRM 51-70-4, FIG 1, 51-10-3, PAR 14, 21, 51-30-2.

Part: CUSP WEB — DELAMINATED (BS 408-427) · airframe 63,480 hrs · 45,809 cycles

DELAMINATED CUSP WEB BETWEEN 408 TO 427, X=54 AND X=60 LT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 550) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION OUT LIMIT ON LT CUSP WEB BS Y= 550, X=57 AT PASSENGER FLOOR STRUCTURE. CUSP WEB BS 550 X=57 WAS REPAIRED IAW SRM 53-05, FIG 131A-13 AND SRM 51-30-2, 51-10-3 PAR 14, 21, 38.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 63,480 hrs · 45,809 cycles

CRACKED RT SLAT NR 2, XOS=200 APPROXIMATELY INTERNAL SKIN. CRACKS WERE STOPED IAW SRM 57-01, FIG 3, SHEET 2. DOUBLER REPAIR WAS FABRICATED IAW SRM 57-01, FIG SHEET 2. DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21. DOUBLER WAS INSTALLED IAW SRM 51-30-8 AND 51-30-2.

Part: LONGERON — CRACKED (BS 1309) · airframe 63,480 hrs · 45,809 cycles

CRACKED LONGERON 8 LT BS 1309 AT INTERNAL FUSELAGE STRUCTURE. CRACKED ON LONGERON 8LT BS 1309 WAS REPAIRED IAW SRM 53-02 PAR 12 AND 51-30-2, 51-30-5, 51-10-3, PAR 14, 21. (LP2363750)

Part: FLOOR SUPPORT — CORRODED (BS 175-200) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON FOOR SUPPORT BETWEEN BS 175 TO BS 200 SEVERAL POINTS X=-6. NEW FLOOR SUPPORT WAS ADJUSTED AND DRILLED IAW SRM 53-14-1 AND 51-10-4.

Part: CUSP WEB — CORRODED (BS 270) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION OUT OF LIMITS ON LT CUSP WEB BS 270 BETWEEN X=54 AND 60. AREA OUT OF LIMITS ON LT CUSP WEB BS 270 BETWEEN X=54 AND X=60 WAS REPAIR IAW SRM 51-30-2,51-10-3, PARR. 14 AND 21 AND 53-05 FIG. 131A-1.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AREA AT WING ACCESS PLATE 1371C. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: VANE — WORN (LT WING TE FLAP) · airframe 63,480 hrs · 45,809 cycles

WORN AFT CORNER ON INBD GUIDE VANE AT LT WING OTBD FLAP, POSITION 3, BS XV1=211. AFT CORNER ON INBD GUIDE VANE AT LT WING OTBD FLAP BS XV1=211 WAS REPAIRED IAW ER/A 492663-14MA, REV ORIGINAL.

Part: PAN — CRACKED (BS 731-1231) · airframe 63,480 hrs · 45,809 cycles

CRACKED AFT/LWR CORNER ON RT RING PAN BS 731, 905, 1136, AND 1231. DAMAGES WERE REMOVED, INSPECTION WAS PERFORMED ON TRIMMED AREA, NO CRACKS WERE FOUND. REPAIR PARTS WERE FABRICATED, TREATED, PAINTED, INSTALLED IAW SRM 53-05, FIG 122, 51-10-3 PAGE 14 AND 21, NDTSPM 06-10-01-001, ER/A 487747-14MA, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1309) · airframe 63,480 hrs · 45,809 cycles

CRACK ON LONGERON 5R, BS 1309. THE LONGERON WAS REPAIRED IAW SRM 53-05, FIG 18.

Part: PAN — CRACKED (BS 294-693) · airframe 63,480 hrs · 45,809 cycles

CRACKS ON FWD/UPPER CORNER OF LT WINDOW RING PAN AT BS 294, 617, 655, 693 PAX CABIN. REASON FOR RE-WRITE: INADECUATE WASHERS ON REPAIR. NEW HARDWARE WAS INSTALLED IAW SRM 51-30-5, PAR 7 AND SRM 53-05, FIG 122.

Part: WEB — CRACKED (BS 202) · airframe 63,480 hrs · 45,809 cycles

CRACK WEB ON BS 202, X=2. AREA DAMAGE WAS REPAIRED IAW 53-01, FIG 4.

Part: FITTING — CRACKED (BS 927) · airframe 63,480 hrs · 45,809 cycles

CRACKED FITTING ON BS 927 X=44 Z=-15 AT WING BOX AREA. CRACKED FITTING ON BS 927, X= 44Z=-15 AT WING BOX WAS R & R IAW 51-30-5 AND DWG 9923417 ID:1, REV:B.

Part: CUSP WEB — CRACKED (BS 1244) · airframe 63,480 hrs · 45,809 cycles

CRACK ON CUSP WEB BS 1244, BETWEEN X=54 TO X=60. CRACK ON CUSP WEB WAS REPAIR IAW SRM 53-05, FIG 131A AND 51-30-1, 51-10-3 PAR 14, 21 AND 38.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE 1409C AND 1303C. ACCESS PLATE'S NRS 1409C AND 1303C WERE REPLACED IAW SRM 51-22-2A.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,480 hrs · 45,809 cycles

CRACKED STOP FITTING NR 1 AND NR 5 AT AFT AREA OF C2 DOOR. CRACKED STOPS FITTING NR 1 AND NR 5 WERE REPLACED IAW SRM 51-30-1 AND 51-30-5 AND CRACK UNDER STOP FITTING NR 1 WAS ATTENDED WITH CARD NR 393 AC ZONE 100, NRC 20000102642.

Part: PAN — CRACKED (BS 1136-1231) · airframe 63,480 hrs · 45,809 cycles

CRACKED AFT/UPPER CORNER ON RT RING PAN BS 1231 AND 1136. CRACKED WAS REPAIRED IAW SRM 53-05, FIG 122.

Part: INTERCOSTAL — CRACKED (BS 1310) · airframe 63,480 hrs · 45,809 cycles

CRACK ON LONGERON 8R, BS 1310 INTERCOSTAL, LONGERON AND END LONGERON WERE REMOVED IAW SRM. 51-30-2 , 51-30-3 AND 51-30-5. NEW LONGERON AND SPLICE WERE DRILLED IAW SRM 51-30-2, FIG 18. REPAIRS WERE TREATED/PAINTED IAW SRM 51-10-3, PAR 14 AND 21. NEW LONGERON , SPLICE , INTERCOSTAL AND END LONGERON WERE INSTALLED IAW SRM 53-02, FIG 18, 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 63,480 hrs · 45,809 cycles

CRACKED PAN ON RT EMERGENCY DOOR EXIT, FWD AT STOP NR 12. PAN ON RT EMERGENCY DOOR EXIT, FWD AT STOP NR 12 WAS REPAIRED IAW SRM 52-05D, FIG 51.

Part: CUSP WEB — CORRODED (BS 282-285) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION OUT OF LIMIT ON LT CUSP WEB FROM BS 282-285 BETWEEN X=54/60 AT PASSENGER CABIN AREA. AREA OUT OF LIMITS WAS REPAIR IAW SRM 53-05, FIG 131A-13 , 51-10-3 PAR 14 AND 21, 51-30-2.

Part: PAN — CRACKED (BS 788-1193) · airframe 63,480 hrs · 45,809 cycles

CRACKED FWD/LWR CORNER ON RT RING PAN WINDOW BS 788, 1060, 1079, 1098 AND 1193. DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 750-788) · airframe 63,480 hrs · 45,809 cycles

CRACKED UPPER/FWD CORNER ON RT RING, PAN BS 750-788. DAMAGE AREA WAS REPAIRED IAW SRM 53-05, FIG 122.

Part: CUSP WEB — CORRODED (BS 826-845) · corrosion level 2 · airframe 63,480 hrs · 45,809 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER LT CUSP WEB BETWEEN BS 826-845, X=54 - X=60 AT CABIN STRUCTURE. NEW DOUBLER WAS INSTALLED IAW SRM 53-05, FIG 131A-6, 51-30-5 AND 51-10-3 P. 14,21.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 63,480 hrs · 45,809 cycles

CRACKED PAN ON RT FWD EMERGENCY EXIT DOOR AT STOP NR 1. PAN ON RT FWD EMERGENCY EXIT DOOR AT STOP NR 1 WAS REPAIRED IAW SRM 52-05D, FIG.51.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,480 hrs · 45,809 cycles

CRACKED STOP FITTING NR 1 AT FWD AREA OF C3 DOOR. CRACK STOP FITTING WAS REPLACED IAW SRM 51-30-1 AND 51-30-5.

Part: CUSP WEB — DAMAGED (BS 313) · airframe 63,480 hrs · 45,809 cycles

ELONGATED HOLE ON CUSP WEB, BS 313 LT SIDE X=49. ELONGATED HOLE WAS REPAIRED IAW SRM 53-05, FIG 131A-16, 51-30-2 AND SRM 51-10-3 PAR 14 AND 21.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 63,480 hrs · 45,809 cycles

CRACKED ANGLE BS 195 BETWEEN 4/5 AT INNER STRUCTURE OFF WD ENTRANCE DOOR. ANGLE WAS REPLACED IAW SRM 51-30-2/51-30-5.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 63,480 hrs · 45,809 cycles

CRACKS ON CHANNEL OF FLOOR PANEL. FLOOR PANEL REPAIRED. DOUBLERS WERE INSTALLED IAW SRM 53-05, FIG 131B, SHEET 3, SHEET 1, 2, 3 FIG 131C.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 62,618 hrs · 45,227 cycles

DURING A WALK AROUND, CENTER VANE OF OTBD FLAP ON LT WING DAMAGED. REMOVED OTBD AND CENTER VANE FROM OTBD LT FLAP. REMOVED OTBD FLAP L/E. TEMP INSTALLED CENTER AND OTBD VANE FOR RIG CHECK. FITTING INSTALLED BOTH VANES INSTALLED. FLAP L/E CAP INSTALLED. OPS CHECK AND DIMENSION CK GOOD. REF MS88, AMM 27-51.

Part: SKIN — CORRODED (SERVICE PANEL) · airframe 62,237 hrs · 44,959 cycles

AFT LAV SERVICE PANEL SKIN BULGING WITH FASTENER PULLED THROUGH. COMPLIED WITH ER/A 538259-14, REV "A". ASSOCIATED ER/A 14-538259, ADDED FOR AC 0993.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,183 hrs · 44,930 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 27-34 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 61,813 hrs · 44,700 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 21DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BRACKET — BROKEN (TAILCONE) · airframe 61,042 hrs · 44,149 cycles

CREW REPORTED THAT TAIL CONE APPEARED LOOSE. MAINTENANCE FOUND THE UPPER RT BRACKET SUPPORT CABLE BROKEN. MAINTENANCE R & R THE TAILCONE ASSEMBLY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,347 hrs · 43,686 cycles

DURING CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT ROWS 1-4. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER AND BATTERIES AT ROW 4 AND THE OPERATIONAL CHECK WAS GOOD. (LP 6171988)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,942 hrs · 43,427 cycles

DURING CHECK, MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE IN THE FWD GALLEY AND ENTRYWAY. MAINTENANCE REPLACED THE BATTERIES IN THE FORWARD EMERGENCY LIGHT POWER SUPPLY AND THE LIGHTS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,956 hrs · 42,765 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT LT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND REPLACED THE BULBS. THE LIGHT HAS RETURNED TO AN OPS CONDITION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,956 hrs · 42,765 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN WOULD REMAIN ON AFTER POWER WAS REMOVED. MAINTENANCE REPLACED THE BATTERY CHARGER. OPS CHECK WAS GOOD.

Part: SKIN — DAMAGED (SERVICE DOOR) · airframe 58,464 hrs · 42,459 cycles

DURING CHECK, NOTED FWD SERVICE DOOR HAS DAMAGED SKIN ON LOWER EDGE OF DOOR. INSTALLED DOUBLER SKIN REPAIR IAW SRM 52-05, FIG 64.

Part: DOOR FRAME — CORRODED (BS 636-693) · corrosion level 2 · airframe 58,464 hrs · 42,459 cycles

CORROSION NOTED ALONG CENTER LOWER CARGO DOOR FRAME BETWEEN BS 636-693. REPAIRED IAW SRM 51-30-1 & 53-05, FIG 123.

Part: SKIN — DAMAGED (R1 DOOR) · airframe 58,464 hrs · 42,459 cycles

DURING C-CHECK, NOTED FWD R1 SERVICE DOOR HAS DAMAGED SKIN ON LOWER EDGE. BLENDED AND EVALUATED DAMAGED SKIN IAW SRM 5201, FIG 1, SHEET 1. EDGE DISTANCE FOUND TO BE OUT OF LIMITS IAW SRM 52-01, FIG 1, SHEET 1. REPAIRED IAW SRM 52-05, FIG 64.

Part: DOOR FRAME — CORRODED (BS 1154-1211) · airframe 58,464 hrs · 42,459 cycles

DURING C-CHECK, NOTED CORROSION ON LOWER AFT CARGO DOOR FRAME BETWEEN BS 1154-1211. REPAIRED IAW SRM 51-30-03, 53-05, FIG 123, OPTION 1, 51-30-05.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 58,464 hrs · 42,459 cycles

DURING C-CHECK, NOTED A CRACK ON THE INTERNAL STRUCTURE UPPER FWD CORNER OF L-1 DOOR. MRB 52-001-02. REPAIRED IAW SRM 52-05, FIG 18, 51-10-03, 51-30-2, NDT SPM PART 6, 06-10-01 & INSTALLED ID TAG IAW DELTA PSM 900-5-01 NR 04.

Part: DOOR FRAME — CORRODED (BS 1154-1211) · corrosion level 2 · airframe 58,464 hrs · 42,459 cycles

DURING C-CHECK, NOTED CORROSION ON LOWER AFT CARGO DOOR FRAME BETWEEN BS 1154-1211. REPAIRED IAW SRM 51-30-03, 53-05, FIG 123 OPTION 1, 51-30-05.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 57,796 hrs · 42,003 cycles

DURING LINE CHECK, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 23DE WAS INOPERATIVE. REPLACED WIRE PIGTAIL & LIGHT ASSEMBLY IAW AMM 33-52 AND OPS CHECKED NORMALLY.

Part: LANYARD — FRAYED (L1 DOOR SLIDE) · airframe 57,762 hrs · 41,980 cycles

DURING LINE CHECK, L1 DOOR SLIDE LANYARD WAS FOUND TO BE FRAYED. REPLACED LANYARD IAW AMM 25-62.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 57,129 hrs · 41,517 cycles

DURING ROUTINE LINE INSPECTION, EMERGENCY PATH LIGHT AT SEAT 19DE WAS FOUND TO BE INOPERATIVE. A BROKEN WIRE WAS FOUND AND WAS REPAIRED IAW SWPM 20. SYS OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,805 hrs · 41,287 cycles

DURING LINE CHECK, TWO LIGHTS WERE NOTED TO BE INOPERATIVE ON THE AFT STAIR WALKWAY LIGHTS. LAMPS WERE REPLACED AND OPERATION CHECKED GOOD.

Part: DOUBLER — CORRODED (BS 598) · airframe 54,950 hrs · 40,075 cycles

RADIO ALTIMETER INTERIOR DOUBLER CORRODED BS 598 BETWEEN LONGERON 30 AND 29R. REMOVED CORRODED DOUBLER AND DRILLED NEW ONE. TREATED AND PRIMED. INSTALLED NEW DOUBLER PER SRM 51-30.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 52,868 hrs · 38,743 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR TRAILING EDGE EMERGENCY FLOOD LIGHTS ON BOTH THE LEFT AND RIGHT WINGS WERE INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED CHARGER AND BATTERY ASSEMBLY. OPERATIONAL CHECK WAS GOOD.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 52,101 hrs · 38,195 cycles

HOLES WORN LEADING EDGE OF VERTICAL LT SIDE IN CHORD ABOVE SPLICE. REPAIRED PER ER/A 493530-14 REV ORIG ON NRC 96.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 52,101 hrs · 38,195 cycles

VERTICAL STAB REMOVABLE L/E HOLES COMMON TO LOWER SPLICE - HOLES / COUNTERSINKS WORN. REPAIRED PER ER/A 493465-14 REV ORIG ON NRC 95.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 52,101 hrs · 38,195 cycles

HOLES WORN - L/E VERTICAL STAB RT SIDE ABOVE SPLICE IN CHORD. REPAIRED PER ER/A 493539-14 REV ORIG ON NRC 98.

Part: ACTUATOR — LEAKING (AFT AIRSTAIR) · airframe 51,552 hrs · 37,817 cycles

FLIGHT RETURNED TO ATL DUE TO CREW REPORT OF BURNING RUBBER/ELECTRICAL SMELL IN THE CABIN AFT OF ROW 16. LAVATORY SMOKE DETECTORS DID NOT SOUND. MAINTENANCE FOUND VENTRAL AIRSTAIR ACTUATOR LEAKING AND APU INLET CONTAMINATED. PERFORMED OPERATION 5090 AND 5089 ALTERNATE AND FULL DUCT BURNOUT.

Part: PAN — CORRODED (CARGO FRAME) · airframe 49,406 hrs · 36,403 cycles

DURING HMV3, FOUND FWD CARGO COMPT DOOR JAMB LOWER JAMB CORROSION BETWEEN PAN AND SKIN CAUSED PAN TO CRACK. REMOVED THRESHOLD WEB AND CUT OUT SECTION OF DOOR JAMB WEB PAN AT STA 370-STA 427 IAW SRM 53-05D, 51-30-5, FAB -5, -7, -6 & -8 SPLICES FROM 2024T4 .040. RECEIVED NEW PAN. LOCATED, DRILLED, DEBURRED ALL PARTS IAW SRM 51-10-4. INSTALLED SPLICES, PAN, WEB IAW SRM 51-30-5, 51-30-2 & 53-05D, FIG 804D.

Part: CUSP WEB — CORRODED (BS 1155-1174) · airframe 49,406 hrs · 36,403 cycles

HMV3 MAIN CABIN STA 1155 TO 1174 RT SIDE L18R CUSP WEB HAS CORROSION, REWRITE OF CARD W00/131 FOR WRONG REPAIRS NEED TO USE SRM 53-20-02D REPAIR REMOVED CUSP WED INSTALLED NEW CUSP WEB IAW SRM 53-20-02D.

Part: ANGLE — CRACKED (BS 1497-1510) · airframe 49,406 hrs · 36,403 cycles

DURING HMV3 DHN FOUND AFT ACCESSORY CANTED FRAME STA 1497 TO STA 1510 L12R TO L13R ATTACH ANGLE CRACKED IN RADIUS. REMOVED ANGLE, FABBED AND INSTALLED NEW ANGLE IAW DWG 9953956 AND SRM 51-30-5.

Part: ATTACH ANGLE — CRACKED (STA 1428 L5R) · airframe 49,406 hrs · 36,403 cycles

DURING HMV3 DHN FOUND AFT ACCESSORY STA 1428 L5R ATTACHMENT ANGLE CRACKED. R & R ANGLE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,406 hrs · 36,403 cycles

DURING HMV3, FOUND AFT ACCESSORY AFT SIDE STA 1464 CANTED FRAME WEB HAS 2 EA CRACKS. CUTOUT DAMAGE 1.5 X 2 INCHES NDT VERIFIED DAMAGE REMOVED. FABRICATED AND INSTALLED FILLER FROM .025 & 075T6 AND REPAIR DOUBLER FROM .032 7075T6 IAW SRM FIG 4, SH 4.

Part: FRAME — CRACKED (BS 1485 L5L) · airframe 49,406 hrs · 36,403 cycles

DURING HMV3 FOUND AFT ACCESSORY STA 1485 CANTED FRAME WEB CRACKED APPOX 1". REMOVED DAMAGED AREA, NDT NO CRACK REMAINING. INSTALLED FILLER AND DOUBLER IAW SRM 53-01, FIG 4, SH4.

Part: PAN — CORRODED (BS 1155-1212) · airframe 49,406 hrs · 36,403 cycles

DURING HMV3 DHN FOUND AFT CARGO COMPT CORROSION ON DOOR LOWER JAMB PAN BS 1155-BS 1212. REMOVED CORROSION FROM PAN IAW SRM 51-10-3, FOUND AREA AT STA 1163 OUT OF LIMITS IAW SRM 53-01, REMOVED EXISTING REP DOUBLER & DOOR STOP AT STA 1174, FORMED & FABBED NEW REPAIR DOUBLER FROM TITANIUM .040 6AL-4V, FABRICATED SPACER FROM 7075 T6 .071 & 2EA STRIPS FROM 7075 T6 .050 IAW SRM 53-05 FIG 123, ADDED IN WEIGHT OF REPAIR PARTS 2.3 OZ USING SCALE NR H9574 22 SEP 10, INSTALLED REPAIR PARTS IAW SRM 53-05, FIG 123.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 49,406 hrs · 36,403 cycles

DURING HMV3 DHN FOUND AFT ACCESSORY STA 1437 L3R ATTACHMENT ANGLE CRACKED IN RADIUS. REMOVED AND REPLACED NEW ANGLE.

Part: FRAME — DENTED (FS 237 L17-18L) · airframe 49,406 hrs · 36,403 cycles

DURING HMV FOUND A 1 INCH DENT AT STA 237 L-18-L ON EXISTING REPAIR. FOUND DENT IN REPAIR DOUBLER TO BE OUT OF LIMITS DUE TO CREASE. FOUND FORMER STA 237 L18L -17L DENTED AND BENT. REMOVED, OBTAINED AND INSTALLED NEW FORMER 9911524U3 IAW SRM 51-30-2, 51-30-5, 51-30-4. REMOVED EXISTING REPAIR DOUBLER AND FILLE, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 53-04 FIG 12B, SHT 34.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 49,406 hrs · 36,403 cycles

HMV3 FUSELAGE EXTERIOR L22L STA 1330 OLD REPAIR CORRODED. REMOVED AND REPLACED DOUBLER AND TRIPLER PER ERA 090262-14 REV ORIGINAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 49,406 hrs · 36,403 cycles

HMV3 MAIN CABIN STA 1155 TO 1174 RT L18R CUSP WEB CORRODED. CORROSION OUT OF LIMITS, REPAIRED PER MD88 SRM 53-05D FIG 827D.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 49,406 hrs · 36,403 cycles

HMV3 MAIN CABIN STA 1044 L54R CUSP WEB CORRODED. CORROSION OUT OF LIMITS, REPAIRED PER MD88 SRM 53-05D FIG 827D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 49,406 hrs · 36,403 cycles

HMV3 AFT CARGO FLOOR FRAME STA 1268 L30 CORRODED. REPAIRED FRAME PER MD88 SRM 53-03 FIG 2A SHEET 1.

Part: TRACK — CORRODED (CARGO BAY) · airframe 49,406 hrs · 36,403 cycles

HMV3 AFT CARGO COMP CORROSION ON LEFT TIE DOWN TRACK. REPLACED TIE DOWN TRACK PER SRM 51-30-1 AND 51-30-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 49,406 hrs · 36,403 cycles

HMV3 MAIN CABIN STA 1044 L54R CUSP WEB HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR PER MD88 SRM 53-05D FIG 827D.

Part: PAN — CRACKED (CARGO DOOR) · airframe 49,406 hrs · 36,403 cycles

HMV3 FWD CARGO DOOR PAN HAS 1 INCH CRACK JUST AFT OF UPPER INSIDE OF WEB. STOP DRILL CRACK PER MD80 SRM 51-01 AND INSTALLED REPAIR DOUBLER PER MD80 SRM 52-02 FIG 8 SRM 51-10-2 SRM 51-30-2 SRM 51-30-4 SRM 51-30-5. INSTALLED ID TAG PER PS 900-5-1 NR 4.

Part: WEB — CRACKED (PYLON) · airframe 49,406 hrs · 36,403 cycles

HMV3 AFT ACCY COMP STA 1380 L5L ENGINE PYLON WEB HAS A CRACK AT HOLE. TRIM OUT DAMAGE AREA, FAB DOUBLER AND FILLER AND INSTALLED PER MD88 SRM 51-30-5 AND 53-11D.

Part: BRACKET — CORRODED (E&E DOOR) · airframe 49,406 hrs · 36,403 cycles

HMV3 E&E COMP RT SIDE DOOR LATCH HOLE OPEN FITTING CORRODED. REMOVED AND REPLACED DOOR PAN, 2 EA FITTINGS, 2 EA BRACKETS PER SRM 51-30-1, 51-30-1, 51-30-4.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,197 hrs · 36,282 cycles

FIRST CLASS OVERHEAD EMERGENCY LIGHT INOP. INSTALLED NEW BATTERIES. OPS CHECKS GOOD

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,324 hrs · 30,002 cycles

CORROSION WAS FOUND ON THE FUSELAGE SKIN NEAR THE SUMP DRAIN AT BL 0 FS 578. THE CORRODED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 36,514 hrs · 27,980 cycles

ABOUT 100 KIAS ON T/O ROLL THROTTLES KICKED OFF AND CAPT LOST AIRSPEED, ALT, AND VSI. ALSO HAD GPWS WARNING. ALTI WINDOW WAS BLANK ON DFGC PANEL. FOUND PITOT AND STATIC LINE NOT SECURED ON NR 1 CADC. REPLACED NR 1 CADC PER MM 34-16-01-201 AS A PRECAUTION. PERFORMED RTS, BOTH NR 1 AND NR 2 DFGC GOOD. CADC FUNCTIONS NORMAL.

Part: APU — LEAKING (APU BAY) · airframe 36,024 hrs · 27,649 cycles

AFTER TAKEOFF, F/A REPORTED FUMES/SMOKE IN CABIN. COMPLIED WITH QRH CABIN FUMES CLEARED. PERFORMED DUCT BURNOUT OPERATIONS.

Part: CONTROL CABLE — BROKEN (BRAKE SYSTEM) · airframe 34,239 hrs · 26,428 cycles

RT BRAKE PEDAL HAS EXCESSIVE PLAY, FEELS LIKE ONE OF THE RIGHT BRAKES IS LOCKED. IT TOOK 80 PERCENT N1 TO TAXI IN WITH ONLY 123K LBS WEIGHT. FOUND RIGHT BRAKE CONTROL CABLE BROKEN AT LEFT BRAKE CONTROL VALVE. REPLACED SAME.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,222 hrs · 26,416 cycles

DAMAGE WAS NOTED JUST AFT OF THE AFT LAV SERVICE DOOR CUTOUT. DAMAGE WAS FOUND IN THE SKIN AND UNDERLYING DOUBLER. DAMAGE WAS REMOVED AND AREA REPAIRED PER ERA 090262-14.

Part: BATTERY — SMOKE (E/E BAY) · airframe 33,723 hrs · 26,080 cycles

AMT NOTICED SMOKE COMING OUT OF VENT BEHIND NOSE GEAR. REPLACED BATTERY, CHARGER, AND CIRCUIT BREAKER.

Part: BATTERY PACK — DISCHARGED (AFT CABIN) · airframe 32,088 hrs · 24,906 cycles

ON L/O CHECK FOUND AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,363 hrs · 22,973 cycles

OVERWING EMERGENCY LIGHTS FLICKERING. REPLACED BATTERY RACK, CHECKS GOOD.

Part: SWITCH — FAULTY (RT MLG) · airframe 28,889 hrs · 22,612 cycles

GEAR DOOR OPEN LIGHT REMAINS ON WITH LANDING GEAR IN UP OR DOWN POSITION. IN DOWN POSITION 3 GREEN LIGHTS ILLUMINATE. IN UP POSITION ALL GEAR LIGHTS EXTINGUISHED. APPROX BOX FAULTS SENSOR RT GEAR DOOR-FAIL 20. REPLACED D1-29R MAIN GEAR DOOR SW PER M/M, RT GEAR DOOR INDICATION CHECK GOOD PER MM.

Part: STRUT — DISCHARGED (NLG) · airframe 23,612 hrs · 18,673 cycles

AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. DCA MTC FOUND STRUT FLAT. SERVICED SAME, SWUNG GEAR ALL NORMAL.

Part: BRACKET — BROKEN (LT MLG DOOR)

DURING DESCENT, GEAR DOOR LIGHT CAME ON AFTER LOWERING GEAR. A/C WAS MET ON THE RUNWAY AND THE DOORS TIED UP SO THAT THE A/C COULD TAXI TO THE GATE. FOUND LT GEAR DOOR PROX SWITCH BRACKET BROKEN. REPLACED SAME.

Part: FRAME — CRACKED (BS 1418)

STA 1418 FRAME WAS FOUND WITH A 1.25 LONG CRACK IN THE RADIUS AT L2R. THE CRACK IS TYP PER SB 53-184; BUT SB EFFECTIVITY DOES NOT COVER THIS AC. REPAIRED PER ERA 331877-14.

Part: PRESS RELIEF VLV — FAILED (NR 1 ENGINE)

ON CLIMBOUT, NR 1 OIL PRESS FLASHING AND ABOVE 55 PSI OIL QTY\NORM. PRESS REDUCED TO BELOW 55 PSI WITH PWR BACK BELOW 1.3 EPR. REPLACED OIL PRESS RELIEF VLV, LK CKD/ADJ, CLEANED RESTRICTOR BELOW PRESS SW. CHECKS NORM, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

FLT CREW MCO EMERG TRACK LIGHT DAMAGED AT SEAT 10D. INSTALLED CLEAR LENS MODULE AT SEAT 10D.

Part: SKIN — SCRATCHED (AFT OF ENTRY DR)

FOUND DURING D-1 LETTER CHECK - MINOR SCRATCHES BELOW AND AFT OF ENTRY DOOR. DYE CHECKED AREA - BURNISHED - TREATED - AND TOUCHED UP PER SRM 53-04, FIG 38, I.D. AREA PER PS 900-5-1, NR 4 NO MRR. GT 595 07/10/95.