N942FD

Part: GUST LOCK — BROKEN (L1 DOOR) · airframe 74,872 hrs · 29,082 cycles

L1 DOOR GUST LOCK BROKEN. REMOVED ACCESS PANEL FOR L1 DOOR COLLAR ACCESS , REMOVED BROKEN COLLAR , WHILE TRYING TO INSTALL NEW COLLAR SPLINES WOULD NOT LINE UP SO REORDERED DIFFERENT PART. PANEL AND HARDWARE IN CREW REST AREA , ALL PER AMM 52-11-08-4-0.

Part: FRAME — CRACKED (ZONE 200) · airframe 74,844 hrs · 29,066 cycles

DURING OPEN HOLE INSP OF RH STA1640 S-14R. CRACK INDICATION NOTED IN O/B & I/B LOWER HOLES ON THE AFT TWO LAYERS AT 9 O'CLOCK (VIEW LOOKING AFT) COMPLETED & COMPLIED WITH STEPS 1-9 OF EA F-5310-T0368137 PART 1 ON R/H STA. 1640 CRACK INDICATION FINDINGS IN FRAME AT S-14R. MAJOR REPAIR

Part: GUST LOCK — BROKEN (L1 DOOR) · airframe 74,070 hrs · 28,506 cycles

L1 DOOR GUST LOCK INOPERATIVE. REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK REF AMM: 52-11-08-8. DOOR HOLD OPEN LOCK OPERATES NORMAL. DOOR HOLD OPEN LOCK MPN 10N0244-7 CPN 5214377 NSN. A/C OK FOR SERVICE.

Part: RELAY — FAILED (ADC) · airframe 73,922 hrs · 28,396 cycles

AT FL370 BEGAN DESCENT TO FL350.GOT IAS DISAGREE, ALT DISAGREE, MACH SPEED TRIM, RUDDER RATIO, L ENG EEC, R ENG EEC EICAS MESSAGES. FOLLOWED CHECKLISTS AND DETERMINED CAPT ADC WAS AT FAULT. SWITCHED TO ALTN SYSTEM. DECLARED AN EMERGENCY AND CONTINUED INTO MEMPHIS. LANDED AT FLAPS 20 PER CHECKLIST INSTRUCTIONS. REMOVED AND REPLACED LEFT CADC AND RELAY K10802

Part: ADC — FAILED · airframe 73,916 hrs · 28,394 cycles

ON CLIMBOUT PASSING 38.5 LOST AIRSPEED AND ALTITUDE ON CAPTAINS DISPLAYS-AIR DATA COMPUTER FAILED-ALSO GOT R AND L ENG EEC EICAS, RUDDER RATIO EICAS AND MACH/SPD TRIM EICAS-ELEV ASYM STATUS MGS-COMPLIED WITH QRH. REMOVED AND REPLACED LEFT ADC REF AMM 34-12-01-4, OPS CHECKED GOOD. R AND L ENG EEC EICAS TRANSFERRED TO LOGPAGE 3120647. REF FIM 27-21 FT 809 FIG 109 AND AMM 27-21-00-5-1 RUDDER RATIO OPS CHECKED GOOD. REF FIM 27-09 FT 813 FIG 106C MACH/SPD TRIM STAB SYS OPS CHECKED GOOD REF AMM 22-24-00-5. REF FIM 27-09 FT 809 FIG 106 ELEV ASYM LIMIT MODULE SYSTEM OPS CHECKED NORMAL.

Part: GUST LOCK — INOPERATIVE (L1 DOOR) · airframe 73,738 hrs · 28,269 cycles

L1 DOOR GUST LOCK INOP REMOVED AND REPLACED HOLD OPEN LOCK. IN REF TO AMM 52-11-08-4. OPERATIONS CHECKED GOOD. A/C OK TO CONTINUE.

Part: RETAINER — DIRTY (R1 DOOR GIRT BAR) · airframe 73,738 hrs · 28,269 cycles

R1 DOOR SLIDE ANNUNCIATOR LIGHT INOPERABLE. GIRT BAR OPERATION NORMAL CLEANED OUT THE GIRT BAR FLOOR RETAINER. LIGHT CHECKS GOOD, PER MM 25-66-00.

Part: SEAT TRACK — CORRODED (BS 1120-1180) · corrosion level 2 · airframe 73,276 hrs · 27,978 cycles

MAIN DECK BETWEEN STA 1120-1180 RBL44.5 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION AT SEAT TRACK AT STA 1080 - 1180 RBL 44.5, ORIG MAT 0.090", MAT REMOVED 0.038", MAT REMAINING 0.052" OUT OF LIMITS IAW SRM 53-00-52-1A. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-40-02-OG & 53-40-52-01 AND DWG 144N5002 REV-.

Part: BUTT JOINT — CORRODED (BS 1825) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

APU INLET AFT BUTTJOINT BS 1825 BETWEEN STRINGERS 3R-6R HAD CORROSION. REMOVED CORROSION ON APU INLET AFT BUTTJOINT IAW SRM 51-10-02. ORIG MAT .100 REM .020 LOSS .080, FOUND OUT OF LIMITS IAW SRM 53-00-01-1A. REPAIRED AREA IAW SRM 53-80-15-2R, REP 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CABIN STA 900 TO 1180 LBL 58 SEAT TRACK EXFOILATION CORROSION. REMOVED CORR ON SEAT TRACK STA 900 TO 1180 LBL58 IAW SRM 51-10-02. UPON EVAL FOUND OUT OF LIMITS DUE TO EXFOILATION IAW SRM 53-00-52-1A. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-52, 51-40-05, 51-40-08 AND 51-40-02.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO FLOOR SUPPORT STRAP HAS CORROSION AT STA 1020 BETWEEN BL-0 AND RBL-24.

Part: STRINGER — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

AFT CARGO BAY SRINGER 29R BETWEEN STA 1400 TO 1420 CORRODED. REPAIRED THE STRINGER IAW SRM 53-00-03-2R, REP 2, FIG 201, DETAIL III, 53-60-03-01, FIG 1, 51-40-05, 51-40-02, 51-20-01, AMM 51-21-10-7, DWG 146N3110 REV C, PL 146N3110, REV CB, AND DWG B57-51-001 REV F.

Part: STRINGER — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

AFT BAY STRINGER 29L BETWEEN BS 1400 TO 1420 CORRODED, REPAIRED THE STRINGER IAW SRM 53-00-03-2R, REPAIR 2, FIG 201, DETAIL III, 51-40-05, 51-40-02, 51-20-01, AMM 51-21-10-7, DWG 146N3110 REV C, BPL 146N3110, REV CB, AND DWG B57-51-001, REV F.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

AFT BAY STRINGER 29L BETWEEN STA 1400 TO 1420 CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO BAY LT OF BL0 AT FS 1019 FLOOR STRAP CORRODED. REMOVED CORR ON FLOOR SUPPORT STA 1019 BL0 IAW SRM 51-10-02. ORING MAT .050 REM.020 LOSS .030 OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02, 51-40-05 AND EA F-5310-T0354340 P1 FUSELAGE - MAINFRAME - MAIN CARGO FLOOR SUPPORT STA 1020 CORRODED, NEW PART FABRICATION ALTERATION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO FLOOR SUPPORT STRAP HAS CORROSION AT STA 1020 BETWEEN BL-0 AND RBL-24. REMOVED CORR ON FLOOR SUPPORT STA 1020 BETWEEN BLO AND RBL 24 IAW SRM 51-10-02. ORIG MAT .050 REM .010 LOSS .040 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT IAW SRM 51-40-05 AND EA F-5310-T0354338 P1 FUSELAGE MAINFRAME MAIN CARGO FLOOR SUPPORT STA 1020 CORRODED, NEW PART FABRICATION-TEMPER ALTERATION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

AFT CARGO BAY STRINGER 29R BETWEEN STA 1400 TO 1420 CORRODED.

Part: WEB — DAMAGED (FUSELAGE) · airframe 73,273 hrs · 27,975 cycles

MAIN DECK STA 1635 STR 14R WEB HAS ELONGATED HOLES. UPON EVALUATION FOUND WEB STA 1638 STR 14R TO BE OUT OF LIMITS IAW SRM 51-10- 02. REMOVED, FABRICATED AND INSTALLED NEW WEB IAW DWG 146N8735 REV N AND REV C AND SRM 51-40-02.

Part: SKIN — DELAMINATED (TAILCONE) · airframe 73,273 hrs · 27,975 cycles

TAIL CONE EXTERIOR LT SIDE HAS A DAMAGED REPAIR. REPAIR AT BS 1960, 8 O’CLOCK POSITION.

Part: REPAIR — DELAMINATED (TAILCONE) · airframe 73,273 hrs · 27,975 cycles

TAILCONE EXTERIOR LT SIDE HAS A DAMAGED REPAIR. REPAIR AT BS 1960, 8 OCLOCK POSITION. ACCOMPLISHED REPAIR ON TAIL CONE EXTERIOR LT SIDE BS 1960 IAW SRM 53-80-01-2R AND IAW SRM 51-70-10-2R REP 2.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

CORROSION ON AFT SHEAR DECK STA 1696 LBL50. REMOVED CORR ON AFT SHEAR DECK STA 1696 LBL50 IAW SRM 51-10-02. ORIG MAT .071 REM.056 LOSS.015 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A AND 53-60-51-2R REP 2. REPAIRED DAMAGE IAW SRM 53-60-51-2R REP2 ALT 1.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO BAY AT FS 1060 AT LBL 24.75 FLOOR STRAP CORRODED. EVALUATED FLOOR SUPPORT STRAP CRACKED AND OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW STRAP IAW DWG 144N5081 REV A AND C AND SRM 51-40-02, 51-40-05 AND 51-40-08.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO BAY SEAT TRACK AT FS 1200 LBL 24.75 CORRODED. REMOVED CORR ON SEAT TRACK IAW SRM 51-10-02 ORIG MAT .080 REM .042 LOSS .038. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02, 51-40-05 AND 51-40-08.

Part: STRAP — CORRUPTED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO FLOOR SUPPORT STRAP HAS CORROSION AT STA 1017 BETWEEN RBL-24 AND RBL-45. REMOVED CORR ON FLOOR SUPPORT STRAP IAW SRM 51-10-02. UPON REMOVAL OF CORR FOUND TO BE CRACKED AND OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW STRAP IAW DWG 144N5081 REV A, REV C AND SRM 51-40-02, 51-40-05 AND 51-40-08.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

CORROSION IN THE MAIN CABIN FLOOR STRUCTURE RT CREASE BEAM SUPPORT INTERCOSTAL LOWER SURFACE BS 1615 (VIEW FROM AFT CARGO CEILING AREA). REMOVED CORR ON RT CREASE BEAM SUPPORT INTERCOSTAL STA 1615 IAW SRM 51-10-02. ORIG MAT .050 REM .044 LOSS .006 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13-1A. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL (WEB) IAW DWG 146N8722 REV F & BK.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

CORROSION ON AFT SHEAR DECK STA 1681 RBL25 AND RBL33. REMOVED CORR ON SHEAR DECK IAW SRM 51-10-02. ORIG MAT .071 LOWEST .052 RBL25 AND .056 RBL33 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A AND 53-60-51-2R REP 2. REPAIRED AREA IAW SRM 53-60-51-2R REP 2 ALT 1.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO T-CHORD AT LBL-45 HAS CORROSION AROUND MULTIPLE FASTENER HOLES BETWEEN STA 920 AND STA 1040. REMOVED CORR ON T-CHORD STA 900 TO 1040 LBL45 IAW SRM 51-10-02. ORIG MAT .090 REM .070 LOSS .020 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW T-CHORD IAW SRM 51-40-02, 53-40-51 FIG 1 AND DWG 111N5201 REV E.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN DECK STATION 1605, RBL 64.20 CREASE BEAM CORRODED.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

CORROSION ON AFT SHEAR DECK STA 1688 RBL50. REMOVED CORR ON AFT SHEAR DECK STA 1688 RBL50 IAW SRM 51-10-02 ORIG MAT .071 REM .058 LOSS .013 OUT OF LIMITS IAW SRM 53-00-51-1A. REPAIRD DAMAGE IAW SRM 53-60-51-2R REP2 ALT 1.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN DECK STA 1605 RBL64.20 CREASE BEAM CORRODED. REMOVED CORROSION FROM MAIN DECK CREASE BEAM STA 1605 RBL 64.20, EVALUATED AREA FOUND OUT OF LIMITS WITH ORIGINAL MATERIAL .070 REMAINING .020, REPIARED AREA OF CREASE BEAM PER SRM 53-00-13-2R REPAIR 1 FIG 201.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO T-CHORD AT LBL 45 HAS CORROSION AROUND MULTIPLE FASTENER HOLES BETWEEN STATION 920 AND STATION 1040.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

CORROSION ON AFT SHEAR DECK STA 1688 RBL50. REMOVED CORR ON AFT SHEAR DECK IAW SRM 51-10-02 ORIG MAT .071 REM .058 LOSS .013 OUT OF LIMITS IAW SRM 53-00-51-1A. REPAIRD DAMAGE IAW SRM 53-60-51-2R REP2 ALT 1.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO T CHORD HAS CORROSION AT RBL 24 BETWEEN STATION 1020 AND STATION 1040.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

CORROSION ON AFT SHEAR DECK STA 1681 RBL25 AND RBL33. REMOVED CORR ON SHEAR DECK STA 1681 RBL25 AND RBL33 IAW SRM 51-10-02. ORIG MAT .071 LOWEST .052 RBL25 AND .056 RBL33 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A AND 531A AND 53-60-51-2R REP 2. REPAIRED AREA IAW SRM 53-60-51-2R REP2 ALT 1.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

CORROSION ON AFT SHEAR DECK STA 1681 LBL39. REMOVED CORR ON AFT SHEAR DECK STA 1681 LBL 39 IAW SRM 51-10-02. ORIG MAT .071 REM .060 LOSS .011 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A AND 53-60-51-2R REP 2. REPAIRED AREA IAW SRM 53-60-51-2R REP 2 ALT 1.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

MAIN CARGO T-CHORD HAS CORROSION AT RBL-24 BETWEEN STA 1020 AND STA 1040. EVALUATED T-CHORD STA 1020 AND 1040 RBL24 FOUND OUT OF LIMITS 100% MAT LOSS IAW SRM 53-00-51-1A. REMOVED, FABRICATED AND INSTALLED NEW T-CHORD IAW SRM 51-40-02 AND DWG 111N5202 REV M AND 111N5207 REV F.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,273 hrs · 27,975 cycles

CORROSION ON AFT SHEAR DECK STA 1681 LBL39. REMOVED CORR ON AFT SHEAR DECK IAW SRM 51-10-02. ORIG MAT .071 REM .060 LOSS .011 FOUND OUT OF LIMITS IAW SRM 53-00-51-1A AND 53-60-51-2R REP 2. REPAIRED AREA IAW SRM 53-60-51-2R REP 2 ALT 1.

Part: STATIC LINE — OUT OF POSITION (R1 DOOR) · airframe 72,417 hrs · 27,428 cycles

UPON CLOSING THE R DOOR (ENTRY), THE HANDLE WENT IN THE ARMED POSITION, BUT THE ARMED LIGHT WASNT ILLUMINATED. DOOR HANDLE JAMMED IN THE ARMED POSITION. DOOR DIDNT APPEAR TO BE CLOSED AT THE AFT SEAL. ROUTED AND STOWED EXCESS STATIC LINE FROM GIRT BAR TO ESCAPE SLIDE ON R1 DOOR REF AMM 25-66-10-2. PLACARD REMOVED.

Part: TIRE — FAILED (NR 6) · airframe 72,354 hrs · 27,386 cycles

#6 TIRE FAILURE ON LANDING COMPLIED WITH TIRE BURST INSP PER AMM 05-51-16. NO DEFECTS NOTED EXCEPT #6 TIRE FAILURE. R&R #6 MLG WHEEL & TIRE ASSY PER AMM 32-45-01. R&R #5 MLG WHEEL & TIRE ASSY PER AMM 32-45-01.

Part: LATCH — UNLATCHED (ENTRY DOOR) · airframe 72,116 hrs · 27,231 cycles

RIGHT ENTRY DOOR LATCH CAME OUT OF LATCHED IN-FLIGHT ON ITS OWN PERFORMED OPS TEST OF R1 DOOR REF MM 52-11-00-2 DOOR CLOSES AND LOCKS WITH NO DEFECTS NOTED INSPECTED DOOR AND FOUND NO VISUAL DEFECTS NO HISTORY FOR 90 DAYS A/C OK FOR SERVICE.

Part: ACM — SEIZED (AC BAY) · airframe 71,915 hrs · 27,106 cycles

ON TAXI OUT, THERE GRINDING NOISE AND SMOKE BELLOWING OUT OF THE GASPERS. THE CREW TURNED OFF THE LEFT PACK AND RAN THE SMOKE AND FIRE, FUMES CHECKLIST. THE SMOKE CLEARED. CFR CHECK OUT THE AIRCRAFT. NO FIRE DETECTED. TAXI BACK TO GATE. COMPLIED WITH SMOKE/FUMES IN THE CABIN INSP PER AMM 05-51-56-2 AND FIM 21-00-01-3-0. FOUND LT ACM LOCKED UP AND CAUSING THE SMOKE AND SMELL IN THE A/C. NO OTHER DEFECTS NOTED SEE WRI 21-50 5841 FOR LT ACM R&R CORRECTIVE ACTION. COMPLIED WITH SMOKE/FUMES IN THE CABIN INSP PER AMM 05-51-56-2 AND FIM 21-00-01-3-0. FOUND LT ACM LOCKED UP AND CAUSING THE SMOKE AND SMELL IN THE A/C.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 71,641 hrs · 26,912 cycles

GND PROX SYS FAULT AND BOTH FO PFD AND ND DISPLAYED RED X TERR SYS STATUS MSG ON BLOCK IN. RECYCLED DCU CIRCUIT BREAKER REF AMM 34-22-01-4-99. SYSTEM CHECKS NORMAL.

Part: SKIN — DEBONDED (TE FLAP) · airframe 71,605 hrs · 26,886 cycles

RT INBD FWD FLAP UPPER SURFACE HAS A DISBONDED COMPOSITE REPAIR. REPAIRED RT INBD FWD FLAP UPPER SURFACE IAW SRM 51-71-10-2R REPAIR 4 & 57-53-01-2R FIG 201 DET I.

Part: SKIN — DAMAGED (BS 1500-1560) · airframe 71,605 hrs · 26,886 cycles

SKIN DAMAGED, BS 1500 AND 1560, STRINGERS 1L AND 2L. REPAIRED IAW EA F-2560-T0339100, B P2.

Part: BULB — INOPERATIVE (EXTERIOR) · airframe 71,114 hrs · 26,527 cycles

L1 DOOR EMERGENCY SLIDE LIGHT (EXTERIOR) INOPERATIVE. REMOVED BULB AND CLEANED SOCKET. INSTALLED A NEW BULB IAW MM 33-51-06-2-1. OPS CHECKED NORMAL.

Part: PIVOT — CRACKED (MLG) · airframe 70,891 hrs · 26,353 cycles

LEFT MAIN LANDING GEAR BEAM RETRACT ACTUATOR LINK PIVOT SHAFT AFT END HAS CIRCUMFERENTIAL CRACKED. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR BEAM RETRACT ACTUATOR LINK PIVOT SHAFT, REFERENCE 32-32-01-4

Part: ACTUATOR — INOPERATIVE (LT MLG) · airframe 70,884 hrs · 26,348 cycles

AFTER TAKEOFF, THE GEAR WOUILD NOT RETRACT PASSED THE OFF POSITION. RAN CHECKLIST , THE GEAR REMAINED DOWN WITH DOOR AND DISAGREE LIGHT LUMINATED SO WE PUT THE GEAR DOWN, GOT NORMAL INDICATION AND LANDED SAFELY. R & R THE LT MLG TRUCK POSITION ACTUATOR IAW AMM 32-32-15-4, PERFORMED GEAR SWINGS IAW AMM 32-30-00-5-0. OPS CHECKED NORMAL, NO LEAKS NOTED.

Part: GIRT BAR — OBSTRUCTED (PAX DOOR SLIDE) · airframe 70,697 hrs · 26,232 cycles

LT PASSENGER DOOR SLIDE WILL NOT ARM. CLEANED DEBREE FROM GIRT BAR AREA AND TESTED DOOR IAW MM 52-11-25-5-0. CHECKED AND ARMS GOOD.

Part: HARNESS — DEFECTIVE (COCKPIT SEAT) · airframe 70,533 hrs · 26,130 cycles

F/O RIGHT SHOULDER HARNESS DOES NOT RETRACT. REPLACED F/O SEAT IAW MM 25-11-01-2. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: SCREW — SHEARED (L1 DOOR) · airframe 70,314 hrs · 25,991 cycles

AT 02:30 ZULU AFTER LENGTHY WEATHER DELAY, CAM ON OUTSIDE OPENING MECHANISM OF LT FORWARD ENTRY DOOR BROKEN. RELEASED FOR SERVICE IAW MEL: 52-11-01-A, CATEGORY-B, EXPIRATION : 29AUG16. MEL 52-11-01-A: L1 DOOR INOPERATIVE. INSPECTED DOOR, BEARING DOESN`T AFFECT SECURITY OF THE DOOR, DEFERED L1 DOOR IAW MEL 52-11-01-A. INSPECTED EXTERIOR DOOR HANDLE. FOUND SCREW SHEARED OFF THAT SECURES LATCH PIN TO EXTERIOR HANDLE. R & R SCREW REF SMP. DOOR OPERATES NORMALLY FROM INTERIOR AND EXTERIOR HANDLE, MEL CLEARED, OK FOR SERVICE.

Part: WINDOW — OUT OF ADJUST (R2) · airframe 70,242 hrs · 25,937 cycles

FO'S R2 WINDOW DIFFICULT TO LOCK REMOVED R2 WINDOW LINING AND DISCONNECTED WIRING IAW MM 56-11-02-4. PULLED & COLLARED R2 WINDOW HEAT CIRCUIT BREAKER P70 PANEL. ADJUSTED R2 WINDOW AND INSTALLED LINING IAW AMM 56-11-02-5-0. RESET R2 WINDOW HEAT CIRCUIT BREAKER. WINDOW OPERATES SMOOTHLY.

Part: SLAT — DAMAGED (NR 5) · airframe 70,216 hrs · 25,916 cycles

NR 5 LE SLAT HAS 6 FT TRAILING EDGE MISSING. REMOVED AND REPLACED THE NR 5 LE SLAT ASSY IAW 27-81-01-4 AND EA F-5710-T0326621. OPS CHECKED GOOD.

Part: SLAT — DAMAGED (WING) · airframe 70,218 hrs · 25,917 cycles

FIXED WING UNDER NR 5 LE SLAT HAS A HOLE CRACK. FURTHER INSPECTION FOUND DELAMINATION OF FIXED WING LE TO EXTEND TO ALL AREA UNDER THE MISSING TRAILING EDGE OF NR 5 SLAT. REPLACED SLAT AND MADE TEMP REPAIR TO LEADING EDGE. FERRY FLIGHT TO VQQ FOR PERMANENT REPAIR.

Part: FITTING — DAMAGED (NR 1 PYLON) · airframe 70,173 hrs · 25,876 cycles

NR 1 PYLON OTBD AFT TR FITTING LOWER AFT HOLE DAMAGED. COMPLIED WITH EA F-5450-T0325811 P1 OF NR 1 PYLON OB AFT TR FITTING LOWER AFT HOLE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 70,173 hrs · 25,876 cycles

FORWARD ACCESSORY BS 231 FRAME HAS A GOUGE. REPAIRED FWD ACCESSORY BS 231, FRAME IAW F-5310-T0325521 P1.

Part: SKIN — WORN (FUSELAGE) · airframe 70,173 hrs · 25,876 cycles

C1 DOOR CONTROL PANEL DOOR CUT OUT LOWER EDGE HAS DEEP WEAR MARK CTR AREA. REPAIRED C1 DOOR CONTROL PANEL DOOR CUT OUT LOWER EDGE IAW EA F-5330-T0325633, P1.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 69,864 hrs · 25,665 cycles

RIGHT BLEED DUCT LEAK EICAS MSG AT FL 380. COMPLIED WITH QRH. ASSOCIATED STATUS MSG, DUCT LEAK LP, AFTER LANDING. TROUBLE SHOT IAW TSM 26-18 FAULT TREE 802, FAULT CODE 64. RT WING LE ALARM A & B. RESET CARD FILE IAW FIM, FOUND RT WING PNEUMATIC DUCT IN INBD LE WITH SEVERE LEAKS AT 2 CLAMPED JOINTS FOUND LOOSE. REMOVED CLAMPS, INSPECTED DUCT & REINSTALLED CLAMPS. RAN LEAK CHECK USING APU AIR. NO LEAKS NOTED, OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (PARKING BRAKE) · airframe 691 hrs · 25,192 cycles

ON TAXI INTO GATE, PARKING BRAKE WOULD NOT SET. ACCOMPLISHED TEST OF THE PARKING BRAKE SYS IAW AMM 32-44-00-5. ALL CHECKED NORMAL, NO PREVIOUS HISTORY. OK FOR SERVICE.

Part: COLLAR — DAMAGED (L1 DOOR) · airframe 68,864 hrs · 24,995 cycles

WHILE PERFORMING ACFT ORIENTATION, L1 DOOR GUST LOCK FAILED. REMOVED AND REPLACED THE L-1 DOOR HOLD OPEN LOCK COLLAR

Part: STRAP — OUT OF POSITION (L1 DOOR) · airframe 68,834 hrs · 24,977 cycles

ENTRY DOOR L1 WOULD NOT ARM. FOUND SMALL STRAND OF NYLON STRAP IN WAY OF GIRT BAR WHILE CLOSING. REMOVED & STOWED STRAP BACK IN POUCH & OPERATIONS CHECKED NORMAL. LIGHT ILLUMINATED NORMAL IAW AMM 52-11-25-5-0.

Part: SKIN — CORRODED (BS 1304) · corrosion level 2 · airframe 68,464 hrs · 24,765 cycles

DURING INSPECTION, CORROSION WAS FOUND AT LAP SEAM APPROXIMATELY BS 1304, STRINGER 14R. REPAIRED IAW EA F-5330-T0308220 P1.

Part: SKIN — CORRODED (BS 755-760) · corrosion level 2 · airframe 68,464 hrs · 24,765 cycles

CORROSION CLOSE TO LAP SEAM AT BS 755 - 760, STRINGER 26R. REPAIRED IAW EA F-5330-T0308242 P1.

Part: GUST LOCK — BROKEN (L1 DOOR) · airframe 67,560 hrs · 24,189 cycles

L1 DOOR GUST LOCK COLLAR BROKEN. R & R L1 DOOR GUST LOCK REF AMM 52-11-08-8. OK FOR SERVICE.

Part: GUIDE ARM — BROKEN (R1 DOOR) · airframe 67,319 hrs · 24,009 cycles

ON ARRIVAL, FOUND R1 DOOR PARTIALLY CLOSED. UPON FUTHER INSPECTION FOUND ROD END ASSY BROKEN OFF OF ARM GUIDE, SAME MANUAL, FIG AND SHEET ITM 348. R & R GUIDE ARM ASSY IAW MM 52-11-04-2. INSTALLED SLIDE IAW MM 25-66-01-4. PERFORMED PRESSURE STOP ADJUSTMENT OF R1 DOOR IN REF TO AMM 52-11-00-5

Part: VALVE — INOPERATIVE (PARK BRAKE SYS) · airframe 67,177 hrs · 23,924 cycles

PARKING BRAKE TAKES EXCESSIVE AMOUNT OF PRESSURE TO REACH "DETENT". ACFT WILL STILL MOVE WITH "PARKING BRAKE" LIGHT ON EICAS. R & R THE PARK BRAKE VALVE.

Part: GUST LOCK — BROKEN (L1 DOOR) · airframe 67,052 hrs · 23,835 cycles

L1 DOOR GUST LOCK BROKEN. REMOVED GUST LOCK IAW AMM 52-11-08-4. REASSEMBLED L1 DOOR HANDLE WITH REPLACED BEARINGS AND WITH NEW CENTER SHAFT, COLLAR REF MM 52-11-13 THROUGH NR 3. COMPLETED DOOR HANDLE MECHANISM ASSY, AND PERFORMED OPS CHECK IAW AMM 52-11-13-4, DOOR OPS CHECKED NORMAL. ALSO REINSTALLED ESCAPE ASSY IAW AMM 25-66-01-4. OPS CHECKED NORMAL.

Part: HANDLE — UNKNOWN (L1 DOOR) · airframe 67,052 hrs · 23,835 cycles

L1 DOOR WILL NOT CLOSE. L1 DOOR EXTERIOR HANDLE IS BROKEN, THE FLIPPER HANDLES WILL SPIN 360 DEGREES WITHOUT RESISTANCE. COMPLETED DOOR HANDLE MECHANISM ASSY AND PERFORMED OPS CHECKED IAW AMM 52-11-13-4, DOOR OPS CHECKED NORMAL.

Part: COLLAR — BROKEN (L1 DOOR LOCK) · airframe 66,917 hrs · 23,753 cycles

DURING PRE-DISPATCH CHECK, NOTED L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED BROKEN PIECES. REPLACED LOCKING COLLAR AND LATCHING MECHANISM ON L1 DOOR IAW MM 52-11-08-4, OPS CHECKED GOOD.

Part: MECHANISM — BROKEN (L1 HOLD OPEN) · airframe 66,908 hrs · 23,748 cycles

DURING PRE-DISPATCH CHECK, NOTED L1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REPLACED LOCKING COLLAR AND LATCHING MECHANISM ON L-1 DOOR IAW MM 52-11-08-4, OPS CHECKED GOOD IAW SAME.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 66,868 hrs · 23,717 cycles

LEFT ENTRY DOOR WAS DISARMED. DOOR WAS CRACKED OPEN FROM INSIDE. PERSONNEL FROM THE OUTSIDE OPENED THE DOOR FURTHER, AT WHICH TIME IT APPEARED THE DOOR CAUGHT AND THE SLIDE FELL OUT. SLIDE DID NOT FULLY DEPLOY. STILL SHOWS GREEN PRESSURE ON THE SLIDE. WITH SLIDE PARTICALLY DEPLOYED, NOTICED THE SLIDE WAS STILL ARMED. DISARMED THE SLIDE AND R & R SLIDE USING AMM 25-66-01-4. PRESSURE CHECKED GOOD AND DOOR ARMED AND DISARMED. DOOR EMERGENCY POWER RESERVIOR DISCHARGED. R & R RESERVIOR USING AMM 52-11-30-4.

Part: SKIN — DAMAGED (ZONE 100) · airframe 66,851 hrs · 23,694 cycles

EXTERNAL LOWER FUSELAGE LAVATORY SERVICE PANEL CUT OUT EDGE DOUBLER AFT/INBD CORNER BUCKLED COMPLIED WITH EA F-5330-157269 FUSELAGE PLATES AND SKIN-SECTION 41-SKIN CORROSION. REPAIR STA 418-430 S-28L REF 8100-9 DATED MAY 17, 2012. MAJOR REPAIR.

Part: STRUCTURE — CRACKED (ZONE 400) · airframe 66,851 hrs · 23,694 cycles

NR 2 PYLON, HORIZ FLANGE FASTENER HOLE CRACKED IN TITANIUM RT THIRD HOLE FROM AFT BULKHEAD. REAMED HOLE TO .405 IAW EA F-5450-157204 STEP1, AND 2ND HOLE TO .437 IAW EA F-5450-157204, STEP 3, NDT CHECK FOR CRACK, NO CRACK NOTED. INSTALLED FASTNER IAW-SRM-51-40-02 AND EA F-5450-157204. FAA FORM 8100-9, DATED 02 APRIL,2012, CLASSIFIED RE-PAIR AS A CAT."B" MAJOR REPAIR.

Part: BUSHING — MIGRATED (PYLON ATTACH) · airframe 66,851 hrs · 23,694 cycles

NR 2 PYLON MID SPAR ATTACH FITTING LUG RT SIDE BUSHING MIGRATED. (RT SIDE) ACFT SIDE. REMOVED MIGRATED BUSHING IAW SOPM-20-50-03. NO CORROSION NOTED, MEASURED LUG BORE AND IT IS 1.8140 FOUND TO BE OVERSIZE DIAMETER IAW DWG 112N7003, HFEC INSPECTED IAW NDTM PT.6 51-00-16. NO CRACK INDICATIONS NOTED, INSTALLED NEW BUSHING IAW SOPM-2050-03. COMPLIED WITH EA F-5720-157232, GAP CHECKED GOOD, IAW SB 757-54-0035. INBD=.067, OTBD=.071. "MAJOR REPAIR"

Part: SKIN — DAMAGED (ZONE 200) · airframe 66,851 hrs · 23,694 cycles

FOUND SCRIBE LINE AT S14R LAP JOINT FROM BS 439.094 - 445.813. REPAIR ACCOMPLISHEDIAW EA F-5330-157266. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 100) · airframe 66,851 hrs · 23,694 cycles

FOUND VERTICAL CUT ON SKIN PANEL AT BS 661 S26R, LEADING INTO BUTT JOINT, REMAINING ON LOWER SKIN SURFACE. ACCOMPLISHED EA F-5330-157270. "MAJOR REPAIR".

Part: SKIN — DENTED (BS 1720) · airframe 66,851 hrs · 23,694 cycles

FUSELAGE SKIN DENTED FWD OF AFT PRESSURE BULKHEAD BS 1720, S24-25R.

Part: STRINGER — GOUGED (ZONE 200) · airframe 66,851 hrs · 23,694 cycles

RIGHT UPPER LOBE OF R4 DOOR, STA 1681.8. GOUGED ALONG STRINGER 13R. COMPLIED WITH EA F-5310-157257. MAJOR REPAIR.

Part: SKIN — DENTED (BS 760) · airframe 66,851 hrs · 23,694 cycles

LEFT LOWER EXTERNAL FUSELAGE AT BS 760 S18L DENTED. REPAIRED STAM 47461000001 AND STAM EA 757-5331-16-F3678. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 760-780) · airframe 66,851 hrs · 23,694 cycles

FUSELAGE SKIN MISREPAIRED AT BS 760-780 BETWEEN S16-17L. REPAIRED ON STAM 47461010001 AND STAM EA 757- 5331-16 -F3678, REV. MAJOR REPAIR.

Part: PANEL — DAMAGED (NR 1 PYLON) · airframe 66,851 hrs · 23,694 cycles

NR 1 PYLON DOOR CUTOUT FOR DOOR PANEL 433LR HAS MISSING MATERIAL IN UPPER AFT CORNER. REPAIRED IAW EA F-5450-157272.

Part: PANEL — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

NR 2 PYLON CUTOUT FOR PANEL 443LL HAS CORROSION IN UPPER AFT CORNER. COMPLIED WITH EA F-5450-159901, CAT."A" MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 66,851 hrs · 23,694 cycles

SKIN AT BS 1871 AT S-21-L DENTED A=2.65 Y=.010 A/Y=265, DENT OUT OF LIMITS DUE TO AXIS ON STRINGER,IAW-SRM-53-00-01 FIG 101, DET III. ACCOMPLISHED EA F-5330-157262. CAT A, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (NR 2 PYLON) · airframe 66,851 hrs · 23,694 cycles

NR 2 PYLON OTBD SKIN HAS AN EXISTING REPAIR THAT EXCEEDS LIMITS OF SB 757-54-0022. R & R NR 2 PYLON OTBD SKIN IAW EA F-5450-159905. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

BS 310, FLOORBEAM CAP CORRODED LBL 62-RBL 62. REMOVED CORROSION IAW-SRM-51-10-02, CHECKED LIMITS IAW-SRM-53-00-01 PG 101-103. DETAIL II AND III, ORIGINAL MAT THICKNESS .100, D=.027 L=1.1 W=1.3, FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM UPPER TEE CAP, INSTALLED NEW UPPER TEE CAP IAW SRM-51-40-02. CAT A, MAJOR REPAIR.

Part: SKIN — DENTED (BS 1862) · airframe 66,851 hrs · 23,694 cycles

SKIN AT BS 1862 S21L, DENTED. ACCOMPLISHED EA F-5330-157239. MAJOR REPAIR.

Part: SKIN — CORRODED (BS 660) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

CORROSION ON LOWER OUTSIDE SKIN BS 660 S26 - 30L. REMOVED CORROSION IAW SRM 51-10-02 ORIGINAL MATERIAL .063, REMAINING .052. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETIAL II. REPAIRED IAW SRM 51-40-02. MAJOR REPAIR

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

LEFT WING REAR SPAR HAS CORROSION. BLEND LIMIT TOLERENCES HAVE BEEN EXCEEDED IAW EA F-2822-7-5009, PT3, STEP B1 ACCOMPLISHED EA F-5710-156998 STEPS 1 THRU 5.

Part: SKIN — DAMAGED (ZONE 100) · airframe 66,851 hrs · 23,694 cycles

FOUND MULTIPLE TOOLING MARKS, FAIRING CONTACT AREA OF LAP SEAM AT S-20L BS 1326-1332. ACCOMPLISHED EA F-5330-157215. MAJOR REPAIR.

Part: SKIN — DELAMINATED (ZONE 500) · airframe 66,851 hrs · 23,694 cycles

LT INBD AFT T/E FLAP LOWER SKIN HAS PREVIOUS REPAIR THAT IS CRACKING. REPAIRED LT INBD AFT T/E FLAP LOWER SKIN IAW SRM 51-70-06. REF EA F-5750-157259 ISSUED FOR TRACKING-WINGS -FLIGHT SURFACES -EO F-5100-7-5001 LT INBD AFT FLAP-RSC REPAIR TRACKING. MAJOR REPAIR.

Part: SUPPORT BEAM — CORRODED (ZONE 100) · airframe 66,851 hrs · 23,694 cycles

NLG STRUCTURE UPPER SUPPORT BEAM STA 345 HAS CORROSION FWD AND AFT SIDES. REMOVED NLG UPPER SUPPORT BEAM IAW SRM 51-40-02 AT STA 345. COMPLIED WITH EA F-5310-157258. INSTALLED NLG UPPER SUPPORT BEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 700) · airframe 66,851 hrs · 23,694 cycles

FUSELAGE SKIN BS 700 BETWEEN S24-26R MISREPAIRED. REPAIRED IAW EA F-5330-157216

Part: SKIN — DENTED (BS 470) · airframe 66,851 hrs · 23,694 cycles

EXTERNAL FUSELAGE SKIN BS 470 BETWEEN S21-22R DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101 DETAIL III. REPAIRED DENT IAW SRM 53-00-01, FIG 201 REPAIR 3 REF SRM 53-00-01, FIG 201. REPAIR 17 NOTE "D" CATEGORY "B" MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1720-1726) · airframe 66,851 hrs · 23,694 cycles

FUSELAGE SKIN BS 1720 TO 1726, S16 TO 17L MISREPAIRED. REPAIRED IAW EA F-5330-157000.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

STA 377 BL-0 NOSE WHEEL WELL UPPER TORQUE BOX BEAM CORRODED. REMOVED CORROSION AT STA 377 BL-0. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-04, FIG 101 DETAIL IV, COMPLIED WITH EA F5310-157249. FUSELAGE MAIN FRAME - SECT 41 STA 377.5 NOSE WHEEL WELL TOP PANEL BEAM CORROSION. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 66,851 hrs · 23,694 cycles

CARGO DOOR INNER SKIN MISREPAIRED. REPAIRED IAW SRM 51-70-13 FIG 1, & EA F5230-157271. MAJOR REPAIR.

Part: DOOR FRAME — CORRODED (L2 DOORWAY) · airframe 66,851 hrs · 23,694 cycles

L2 DOOR CUT OUT LOWER FWD FRAME INNER CHORD CORRODED. REMOVED CORROSION IAW SRM 51-10-02 BLENDED AREA MEASURES L= 3.0 W= 1.5 D= .018 ORIGINAL MATERIAL .080, .062 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II PG 103. REMOVED AND REPLACED LOWER FWD FRAME INNER CHORD IAW SRM 51-40-02. MAJOR REPAIR

Part: SKIN — CORRODED (LAP SEAM) · airframe 66,851 hrs · 23,694 cycles

FOUND CORROSION ON LAP SEAM AT S20L, BS 1334.5. REPAIRED IAW EA F-5330-157215. MAJOR REPAIR.

Part: SKIN — BUCKLED (BS 1720-1740) · airframe 66,851 hrs · 23,694 cycles

EXTERNAL SKIN STA 1720 - 1740 BETWEEN S-27L TO S-29L BUCKLING. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III. ACCOMPLISHED EA F-5330-159906. MAJOR REPAIR.

Part: BEAM — CORRODED (BS 360) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

NOSE LANDING GEAR STRUCTURE UPPER SUPPORT BEAM STA 360 HAS CORROSION FWD AND AFT SIDES. COMPLIED WITH EA F-5310-157209. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (MAIN CARGO DOOR) · airframe 66,851 hrs · 23,694 cycles

CARGO DOOR MISREPAIRED. REPAIR ACCOMPLISHED EA F-5230-157264. MAJOR REPAIR.

Part: DOOR — MISREPAIRED (MAIN CARGO) · airframe 66,851 hrs · 23,694 cycles

CARGO DOOR MISREPAIRED. REPAIRED IAW SRM 52-30-01, REPAIR 4, PG 201, FIG 201. CATEGORY "B" MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1681-1661) · airframe 66,851 hrs · 23,694 cycles

FUSELAGE SKIN BS 1681 TO 1661, S-5 TO S-6R MISREPAIRED. REPAIRED IAW EA F-5330-157251. MAJOR REPAIR.

Part: STRINGER — GOUGED (BS 620-640) · airframe 66,851 hrs · 23,694 cycles

FWD PIT STA 620-640 S-25R, UPPER AND LOWER SIDES OF STRINGER GOUGED. BLENDED STRINGER IAW-SRM-51-10-02, ORIG MAT .080 REMAINING .062, OUT OF LIMITS IAW-SRM-53-00-03, FIG 101, DET II. R & R STRINGER CAT "A", MAJOR. REPAIR.

Part: WEB — DAMAGED (BS 1681-1701) · airframe 66,851 hrs · 23,694 cycles

AFT FLOOR WEB HAS A ROW OF DOUBLE DRILLED HOLES AT BL 0, STA 1681-1701. REPAIRED FLOOR WEB IAW SRM 53-60-51 PAGE 201 FIG. 201. MAJOR REPAIR.

Part: SKIN — DAMAGED (ZONE 200) · airframe 66,851 hrs · 23,694 cycles

FOUND SCRIBE LINE IN BUTT JOINT AT STA 781 BETWEEN S-6R TO S-10R ACCOMPLISHED EA F-5330-157233, FUSELAGE-PLATES AND SKINS (AD 2007-19-07) EO F-5330-7-5000 PT 3 BUTT JOINT SCRIBE LINE AT STA 781 BETWEEN S-6R TO S-10R. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

FLOORBEAM AT STA 345, RBL 12 TO LBL 30, REPAIR STRAP IS CORRODED. REMOVED CORRODED STRAP IAW SRM 51-40-02. FABRIRICATED NEW STRAP OUT OF 7075-T6 MAT, IAW SRM 53-00-51.TREATED PRIMED AND PAINTED PER AMM 20-50-14, 20-44-04. INSTALLED FABRICATED STRAP PER SRM 51-40-02, SRM 53-00-51 REPAIR #3 DETAIL 1. MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 1681) · airframe 66,851 hrs · 23,694 cycles

STA 1681, FLOORBEAM HAS 2 EA DOUBLE DRILLED HOLES NEAR BL-0. FOUND WHILE ACCOMMPLISHING DECK PLATE REPAIR. R & R FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (NR 4 SLAT) · airframe 66,851 hrs · 23,694 cycles

NR 4 SLAT LT WING L/E NOSE SKIN AT OSS375 MISREPAIRED. REPAIRED IAW EA F-5750-157213 STEPS 1 THRU 4 EA. MAJOR REPAIR.

Part: STRINGER — DAMAGED (BS 418 S6R) · airframe 66,851 hrs · 23,694 cycles

STRINGER 6R HAS DOUBLE DRILLED HOLE AT STA 418. REMOVED STRINGER IAW SRM 51-40-02 INSTALLED NEW STRINGER IAW SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 620-660) · airframe 66,851 hrs · 23,694 cycles

FUSELAGE SKIN AT BS 620- 660 BETWEEN S-23R TP S-26R MISREPAIRED. REPAIRED IAW EA F-5330-157267.

Part: STRINGER — GOUGED (BS 620-640) · airframe 66,851 hrs · 23,694 cycles

FWD CARGO BAY BS 620- 640, S25R LWR SIDE GOUGED. REMOVED GOUGE IAW SRM 51-10-02 BLENDED AREA ORIG MAT .065 MATERIAL REMAINING .035, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03. R & R STRINGER IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (BS 1300-1360) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

MAIN CABIN AREA BET BS 1300-1360, S17R, RT SIDE CREASE BEAM INBD CHORD CORRODED. REMOVED CORROSION, ORIG MAT .100 AFTER MAT. REMAINING .060 MAT. LOSS IS .040 MAT. OUT OF LIMITS IAW SRM-53-60-13 DETAIL VIII FIG 101.R & R ANGLE BS 1290-1410 "CAT A, MAJOR REPAIR".

Part: SKIN — MISREPAIRED (BS 415) · airframe 66,851 hrs · 23,694 cycles

FUSELAGE SKIN AT STA 415 BETWEEN S-21R TO S-22R MISREPAIRED. REPAIRED IAW SRM 53-00-01, REPAIR 15. CATEGORY "B" MAJOR REPAIR.

Part: PANEL — CRACKED (NR 2 SLAT) · airframe 66,851 hrs · 23,694 cycles

SLAT NR 2 OTBD MAIN TRACK, COVE PANEL CRACKED. REMOVED CRACKED COVE PANEL AND INSTALLED NEW IAW-SRM-51-40-02. MAJOR,CAT A REPAIR.

Part: PANEL — CRACKED (ZONE 500) · airframe 66,851 hrs · 23,694 cycles

NR 1 SLAT INBD AUX TRACK, COVE PANEL CRACKED. REMOVED DAMAGED COVE PANEL IAW SRM 51-40-02, FABRICATED NEW COVE PANEL. INSTALLED NEW COVE PANEL ON SLAT NR 1 IAW SRM 51-40-02. MAJOR REPAIR.

Part: PANEL — CRACKED (LT NR 1 SLAT) · airframe 66,851 hrs · 23,694 cycles

SLAT NR 1 COVE PANEL AT INBD AUX TRACK HAS A CRACK AT INBD FASTENER HOLE. REMOVED CRACKED PANEL AND INSTALLED NEW COVE PANEL IAW 51-40-02. MAJOR REPAIR.

Part: FAIRING — CORRODED (RT WNG - BDY) · airframe 66,851 hrs · 23,694 cycles

RT WING TB FAIRING 192AR CORRODED CIRCUMFERENCE OF PANEL AT FASTENER HOLES. CHECKED LIMITS OF ALL REWORKED AREAS. FOUND IN LIMITS EXCEPT 1 EA SPOT AT RBL 2.75 ORIGINAL THICKNESS .075 REMAINING THICKNESS .042 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II, L= 2.5" W= 2" D= 0.33". REMOVED DAMAGED AREA IAW SRM 53-00-01. INSTALLED REPAIR DOUBLER IAW SRM 51-40-02. INSTALLED TAPERED SHIMS IAW SOPM 20-50-24. MAJOR REPAIR.

Part: BULKHEAD — CHAFED (BS 1885) · airframe 66,851 hrs · 23,694 cycles

APU COMPT FWD BULKHEAD CHAFED FS -1885-RT SIDE 7". REPAIRED IAW SRM-53-80-08, FIG 101, REPAIR NR2 AND SRM-51-40-02, CATEGORY A MAJOR REPAIR.

Part: BULKHEAD — CHAFED (BS 1885) · airframe 66,851 hrs · 23,694 cycles

APU COMPT FWD BULKHEAD HAS CHAFE MARKS, FS 1885 RT SIDE 7". REPAIRED IAW-SRM-53-80-08, FIG 201, REPAIR 2.

Part: SKIN — DENTED (ZONE 100) · airframe 66,851 hrs · 23,694 cycles

RT LOWER FUSELAGE SKIN HAS DENT AT BS 745, S25R. DENT DIMENSIONS= A=2.5" Y=.002 A/Y=1250, FOUND TO BE OUT OF LIMITS, ACCOMPLISHED SKIN IAW SRM-53-00-01, FIG 201, CAT B MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

BS 418-440, RBL 45 SEAT TRACK CORRODED REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ORIGINAL MATERIAL .090 AFTER REWORK L=2.5 W=1.5 D=.090 MATERIAL REMAINING .000 FOUND OUT OF LIMITS IAW SRM 53-00- 52. REMOVED SEAT TRACK AT STA 418-440 RBL 45 IAW SRM 51-40-02. PURCHASED NEW SEAT TRACK PN BAC1520-792, BATCH NR 0001904663. INSTALLED NEW SEAT TRACK AT STA 418-440, RBL 45 IAW SRM 51-40-02. MAJOR REPAIR.

Part: FITTING — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

STA 440 RBL 45 SEAT TRACK FITTING CORRODED REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS ORIGINAL MATERIAL .200 AFTER REWORK L=2.5 W= 1.0 D= .023 REMAINING MATERIAL .177 FOUND OUT OF LIMITS IAW SRM 53-00- 01. REMOVED SEAT TRACK FITTING IAW SRM 51-40-02. RECEIVED NEW SEAT TRACK FITTING PART NUMBER 140N2504-1. INSTALLED NEW SEAT TRACK FITTING IAW SRM 51-40-02. MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 418-440) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

STRINGER BS 418.00 TO 440.0, S22R CORRODED. REMOVED CORROSION IAW SRM 51-10-02 . ORIGINAL MATERIAL .040 REMAINING .030, FOUND OUT OF LIMITS IAW SRM 53-00-03 DETAIL II. R & R STRINGER IAW SRM 51-40-02. MAJOR REPAIR.

Part: FRAME — CORRODED (BS 1500) · airframe 66,851 hrs · 23,694 cycles

AFTER REMOVAL OF FLOOR SUPPORT AT STA 1500, RBL 2.50 FOUND CORROSION ON FRAME IN AFT CARGO PIT. REMOVED CORROSION AT FRAME IAW SRM 51-10-02. BLENDED AREA. ORIGINAL MATERIAL .063, MATERIAL LOSS .033, MATERIAL REMAINING .030. FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II. R & R FRAME. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 800) · airframe 66,851 hrs · 23,694 cycles

FRAME BS 800 BETWEEN S28L TO S28R MISREPAIRED. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 418-440) · airframe 66,851 hrs · 23,694 cycles

SEAT TRACK GOUGED/CORRODED, RBL24 BS418-440. REMOVED DAMAGE AND CHECKED LIMITS. FOUND TO BE OUT OF LIMITS L=3" W=1" D=.025. ORIGINAL MATERIAL .090 AFTER REWORK .065 IAW SRM 53-00-52 FIG 101. INSTALLED NEW SEAT TRACK IAW SRM 51-40-02, STA 418-440, RBL 24. MAJOR REPAIR.

Part: FRAME — GOUGED (BS 365 S8-9R) · airframe 66,851 hrs · 23,694 cycles

FUSELAGE UPPER LOBE INTERIOR BS 365 STR 8-9R FRAME GOUGED. COMPLIED WITH EA F-5310-157243, "CAT A MAJOR REPAIR".

Part: SEAT TRACK — GOUGED (BS 1180-1280) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

RBL 45 SEAT TRACK GOUGED BS 1180 -1280. REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK IAW SRM 53-60-52 AND IAW DWG 146N5120, INSTALLED NEW SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — MISREPAIRED (BS 1661) · airframe 66,851 hrs · 23,694 cycles

FLOORBEAM STA 1661, MISREPAIRED. REMOVED FLOORBEAM AT STA 1661 IAW SRM 51-40-02. FABRICATED FLOORBEAM IAW DWG 146N5110. INSTALLED FLOORBEAM AT STA 1661 IAW SRM 51-40-02. MAJOR REPAIR.

Part: SUPPORT — CORRODED (BS 365-418) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

BS 365-418, RBL 45 SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .070 AFTER REWORK L=2.5 W=2 D=.025 REMAINING MATERIAL .045. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. DETAIL VII. INSTALLED NEW SEAT TRACK SUPPORT IAW SRM 51-40-02. MAJOR REPAIR.

Part: SUPPORT — CORRODED (BS 365-418) · airframe 66,851 hrs · 23,694 cycles

BS 365-418 RBL 24, SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-10-02 CHECKED LIMITS ORIGINAL MATERIAL .070 AFTER REWORK L=2 W=1.5 D=.030 REMAINING MATERIAL .040. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-02, FIG 101, DETAIL VII. INSTALLED NEW SEAT TRACK SUPPORT IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — GOUGED (BS 1280) · airframe 66,851 hrs · 23,694 cycles

MAIN CABIN AREA RT SIDE AT BS 1280 CREASE BEAM GOUGED.

Part: CREASE BEAM — CORRODED (BS 776) · airframe 66,851 hrs · 23,694 cycles

RIGHT MAIN DECK CREASEBEAM CORRODED, BS 776. BLENDED AREA IAW SRM 51-10-02. ORIGINAL MATERIAL .090 AFTER BLENDING MATERIAL .040 MATERIAL LOSS .050. OUT OF LIMITS IAW SRM 53-30-13, DETAIL III, FIG 101. REMOVED CREASE BEAM IAW SRM 51-40-02. FABED INBD CHORD FROM MAT BAC 1515-533 7075-T6511 IAW DWG D634N201 BATCH NR 1896249. LOCATED AND DRILLED INBD CHORD IAW SRM 51-40-05. INSTALLED CREASE BEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440-640) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

SEAT TRACK CORRODED AND GOUGED RBL 45 , BS 640 - 440. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 660-664) · airframe 66,851 hrs · 23,694 cycles

MAIN DECK RT CREASEBEAM CORRODED BS 660 - 664. BLENDED IAW SRM 51-10-02. ORIGINAL MATERIAL .090 AFTER BLENDING MATERIAL .050 MATERIAL LOSS .040 MATERIAL OUT OF LIMITS IAW SRM 53-30-13, DETAIL III, FIG 101. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM IAW SRM 51-40-02, SRM 51-40-05, AND SRM 53-30-13. INSTALLED NEW CREASE BEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — MISREPAIRED (BS 377) · airframe 66,851 hrs · 23,694 cycles

FLOORBEAM STA 377 MISREPAIRED. REMOVED AND REPLACED IAW 51-40-02.

Part: FRAME — MISREPAIRED (BS 1600) · airframe 66,851 hrs · 23,694 cycles

FRAME STA 1600 BETWEEN S-21R TO S-23R MISREPAIRED. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1350 S17L) · airframe 66,851 hrs · 23,694 cycles

CREASE BEAM 17L BS 1350 CORRODED. ORIGINAL MATERIAL .100 AFTER BLENDING .065 MATERIAL LOSS .035 MATERIAL OUT OF LIMITS IAW SRM 53-60-13 ALLOWABLE DAMAGE 2 FIG 101 DETAIL VIII. R & R CREASE BEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 780) · airframe 66,851 hrs · 23,694 cycles

MAIN DECK FLOORBEAM UPPER CHORD CORRODED, BS 780, LBL 24 - RBL 24. BLENDED FLOOR BEAM UPPER CHORD IAW SRM 51-10-02 AT STA 780, LBL 24-RBL 24. AFTER REWORK AREA AT STA 780, LBL 24 -BL 0 ORIGINAL MATERIAL IS .125 AFTER REWORK D=.005, L=23 W=1.3 AREA IS WITHIN LIMITS IAW SRM 53-00-51, RBL AT STA 780, BL 0 TO RBL 24 AFTER REWORK D=.109 W=1.2 L=14.5 AREA FOUND OUT OF LIMITS AT STA 780, RBL 15.5 IAW SRM 53-00-51, FIG 201. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 53-00-51, FIG 201, REPAIR 5. CATEGORY "A" MAJOR REPAIR.

Part: GATE — CORRODED (L2 DOOR) · airframe 66,851 hrs · 23,694 cycles

L2 DOOR LWR GATE CORRODED. REMOVED L2 LOWER GATE IAW AMM 52-11-38. DETERMINTED CORROSION EXCEEDING LIMIT IAW SRM 52-10-02. REMOVED HINGE FROM LOWER GATE IAW SRM 51-40-02. INSTALLED HINGE ON NEW LOWER GATE IAW SRM 51-40-02. INSTALLED GATE ON L2 DOOR BOTTOM POSITION IAW AMM 52-11-38-4. DOOR SKIN CLEARANCES WITHIN TOLERANCE IAW AMM 52-11-00-5. NO DOOR RIG REQUIRED. DOOR RIG NOT DISTURBED. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1320) · airframe 66,851 hrs · 23,694 cycles

FLOORBEAM CORRODED BS 1320, BL 0-LBL 24, UPPER TEE. R & R FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 440) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

RT CREASE BEAM CORRODED BS 440. REMOVED CORROSION FOUND TOOL MARKS OVER 50 PERCENT OF THE THICKNESS OF THE MATERIAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 DETAIL III. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM IAW SRM 53-10-13 DWG 141N8422. INSTALLED CREASE BEAM IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — GOUGED (BS 405) · airframe 66,851 hrs · 23,694 cycles

RT CREASE BEAM GOUGED AT STA 405. BLENDED GOUGE CHECKED LIMITS IAW SRM 53-00-51. MATERIAL REMOVED EXCEEDS 10 PERCENT, .040 REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, DRAWING III. REMOVED CREASE BEAM IAW 51-40-02 FABRICATED NEW CREASE BEAM IAW SRM 53-10-13 DWG 141N8422. INSTALLED NEW CREASE BEAM STA 405, RBL 62 IAW SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — GOUGED (BS 374) · airframe 66,851 hrs · 23,694 cycles

RT CREASE BEAM GOUGED BS 374. BLENDED GOUGE IAW SRM 51-10-00. CHECKED LIMITS FOUND DOUBLE DRILLED HOLE OUT OF LIMITS IAW SRM 53-00-51. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM AND INSTALLED IAW SRM 51-40-02. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 1681) · airframe 66,851 hrs · 23,694 cycles

RT FRAME SHEAR TIE CORRODED BS 1681.0 S22-23R. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA MAX MATERIAL REMOVED .020 ORIG MAT, .050 REMAINING MAT .030 OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DET II. R & R SHEAR TIE IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 66,851 hrs · 23,694 cycles

R2 DOOR ENTRANCE FLOORBEAM CORRODED, BS 324.0, RBL 30.0-62.0. REMOVED CORROSION, ORIGINAL MATERIAL .125 THICK AFTER REWORK .070 THICK L=5', W=2'D=.055, IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW-SRM-53-00-51. R & R TOP FLOORBEAM TEE IAW SRM-51-40-02. CAT "A", MAJOR REPAIR.