N616FE

Part: NONE — NONE (NONE) · airframe 81,299 hrs · 20,313 cycles

EXISTING REPAIR AT LOWER FUSELAGE SKIN RIGHT HAND SIDE STATION 1191 BETWEEN LONGERON 46 RIGHT TO LONGERON 47 RIGHT REQUIRES REPLACEMENT (REFER M MOD NUMBER : SRM000078194N90 & WRI 53102005) LOWER FUSELAGE SKIN RIGHT HAND SIDE STATION 1191 BETWEEN LONGERON 46 RIGHT TO LONGERON 47 RIGHT EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01-0G AND REPAIR CARRIED OUT AS PER SRM 53-00-01-2R REPAIR 8 FIGURE 201 SHEET 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO PERFORM INITIAL INSPECTION AT 7,500 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 4,750 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT METHOD AS PER SRM 53-00-01-2R TABLE 201 REPAIR 8. ORIG SUB DATE: 9/13/2022

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,299 hrs · 20,313 cycles

CENTER CARGO - FORWARD SUPPORT CHORD STATION 1841 X = 11 FOUND CORROSION CENTER CARGO - FORWARD SUPPORT CHORD STATION 1841 X = 11 CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 REPAIR GENERAL. SUPPORT CHORD REMOVED AND REPLACED AS PER SRM 51-31-01-0G. SUPPORT CHORD FABRICATED AS PER DOUGLAS DRAWING : AGA7170 REVISION : T. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 81,299 hrs · 20,313 cycles

CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 50 RIGHT SPLICE FOUND CRACKED CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 50 RIGHT CRACKED SPLICE REMOVED AND REPLACED WITH FABRICATED MACHINED SPLICE AS PER SRM 51-33-01- 0G. SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7114 REVISION : J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 81,299 hrs · 20,313 cycles

CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 50 LEFT SPLICE FOUND CRACKED CENTER CARGO - BILGE STATION 5-113 TO STATION 1541 LONGERON 50 LEFT CRACKED SPLICE REMOVED AND REPLACED WITH FABRICATED MACHINED SPLICE AS PER SRM 51-33-01- 0G. SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : A5A7114 REVISION : J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: PANEL LATCH — DELAMINATED (ZONE 200) · airframe 81,299 hrs · 20,313 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231GF BELOW BALLMAT AREA FOUND DELAMINATED AT ( STATION 595 TO STATION 675 ) DELAMINATED FLOOR PANEL #231GF AT MAIN DECK STATION 595 - STATION 675 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #231GF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #231GF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 81,299 hrs · 20,313 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231HF BELOW BALLMAT AREA FOUND DELAMINATED AT ( STATION 595 - STATION 675 ) DELAMINATED FLOOR PANEL #231HF AT MAIN DECK STATION 595 - STATION 675 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #231HF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #231HF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 81,299 hrs · 20,313 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #233FF BELOW BALLMAT AREA FOUND FORWARD EDGE BROKEN AT ( STATION 575 TO STATION 735 ) FLOOR PANEL #233FF WITH FORWARD BROKEN EDGE AT MAIN DECK STATION 575 - STATION 735 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #233FF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #233FF INSTALLED AS PER AMM 53-21-04. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 500) · airframe 81,299 hrs · 20,313 cycles

03 EACH FASTENER HOLES #12 , #35 , #36 FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6, 03 EACH FASTENER HOLES #12, #35, #36 REPAIR CARRIED OUT AS PER SRM 57-20-02-2R REPAIR 5 FIGURE 201. TO PERFORM INITIAL INSPECTION AT 2,000 CYCLES AFTER COMPLETION OF THIS REPAIR AND REPETITIVE INSPECTION AT EVERY 2,000 CYCLES BY HIGH FREQUENCY EDDY CURRENT INSPECTION METHOD AS PER SRM 57-20-02-2R TABLE 201 REPAIR 5 FIGURE 202. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 81,299 hrs · 20,313 cycles

LEFT HAND WING TRAILING EDGE INBOARD FLAP UPPER SKIN FOUND WITH DENT AT STATION XIFH 231 LEFT HAND WING TRAILING EDGE INBOARD FLAP UPPER SKIN AT STATION XIFH 231 REPAIR CARRIED OUT AS PER SRM 57-00-01-2R RPAIR 2 FIGURE 201 AND EA : 1-5750-T0370697 P1 TITLE : WINGS - FLIGHT SURFACES - L/H INBD FLAP, UPPER SKIN DAMAGE - RSC TRACKING. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022

Part: SKIN — DELAMINATED (ZONE 600) · airframe 81,299 hrs · 20,313 cycles

RIGHT HAND WING TRAILING EDGE INBOARD ISLAND UPPER SKIN INTERNAL FINGER DOUBLER FOUND DETACH AT STATION XW 390. RIGHT HAND WING TRAILING EDGE INBOARD ISLAND UPPER SKIN AT STATION XW 390 REPAIR CARRIED OUT AS PER SRM 57-50-01-2R REPAIR 6 FIGURE 203. REPAIR CLASSIFEID AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022

Part: SKIN — CRACKED (ZONE 600) · airframe 81,299 hrs · 20,313 cycles

05 EACH FASTENER HOLES #12 , #14 , #16 , #17 , #36 FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6 RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND STATION XORS = 713.6, 05 EACH FASTENER HOLES #12, #14, #16, #17, #36 REPAIR CARRIED OUT AS PER SRM 57-20-02-2R REPAIR 5 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. TO PERFORM INITIAL INSPECTION AT 2,000 CYCLES AFTER COMPLETION OF THIS REPAIR AND REPETITIVE INSPECTION AT EVERY 2,000 CYCLES BY HIGH FREQUENCY EDDY CURRENT INSPECTION METHOD AS PER SRM 57-20-02-2R TABLE 201 REPAIR 5 FIGURE 202. ORIG SUB DATE: 9/6/2022

Part: TRUNNION — CRACKED (NLG) · airframe 81,299 hrs · 20,313 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND NOSE LANDING GEAR TRUNION FITTING STATION Y = 585 EXISTING TRIMMED OUT AREA FOUND CRACK APPROXIMATE 0.2" CRACK APPROXIMATE 0.2" FOUND AT LEFT HAND NOSE LANDING GEAR TRUNION FITTING STATION Y = 585 REPAIRED AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202 AND EA # 1-5310- T0311351 A P3 TITLE : FUSELAGE - MAIN FRAME - LH NLG TRUNION FITTING CRACK REPAIR, STA 595 - SRM 53-10-14, REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022

Part: SKIN — CRACKED (ZONE 100) · airframe 81,299 hrs · 20,313 cycles

FUSELAGE : RIGHT HAND AIRCON COMPARTMENT SERVICE DOOR CUTOUT UPPER AFT CORNER FOUND CRACKED AT STATION 535 LONGERON 33 RIGHT FUSELAGE : RIGHT HAND AIRCON COMPARTMENT SERVICE DOOR CUTOUT UPPER AFT CORNER AT STATION 535 LONGERON 33 RIGHT REPAIR CARRIED OUT AS PER SRM 53-20-15-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT 4,000 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 4,000 FLIGHT CYCLES AS PER SRM 53-20-15-2R TABLE 201 REPAIR 3 BY EXTERNAL VISUAL METHOD. ORIG SUB DATE: 9/6/2022

Part: SEAT TRACK — WORN (ZONE 200) · airframe 81,299 hrs · 20,313 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 5-5, X = - 8.5 FOUND CROWN WORN CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 5-5, X = - 8.5 CROWN WORN MARK REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 5-0 TO STATION 5-63 X = - 8.5 AS PER SRM 53- 00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: SEAT TRACK — CRACKED (BS 755) · airframe 81,299 hrs · 20,313 cycles

CABIN - SEAT TRACK STATION 755 X = 8.5 FOUND CRACKED CABIN CRACKED SEAT TRACK AT STATION 755 X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 625 TO STATION 765 X = 8.5 AS PER SRM 53-00- 52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: SEAT TRACK — WORN (ZONE 200) · airframe 81,299 hrs · 20,313 cycles

CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK AT STATION 5-5, X = - 47 FOUND CROWN WORN CABIN - MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK CROWN AT STATION 5-5 X = - 47 WORN MARK REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE STATION 5-0 TO STATION 5-63 X = - 47 AS PER SRM 53-00- 52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 81,299 hrs · 20,313 cycles

AFT CARGO - RIGHT HAND TUNNEL STATION 1863.125 - STATION 1871 LONGERON 38 RIGHT SPLICE FOUND CRACKED AFT CARGO - RIGHT HAND TUNNEL STATION 1863.125 - STATION 1871 LONGERON 38 RIGHT CRACKED SPLICE REMOVED AND REPLACED WITH FABRICATED MACHINED SPLICE AS PER SRM 51-33-01-0G. SPLICE FABRICATED BY MACHINING AS PER DOUGLAS DRAWING : AFA7105 REVISION : H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: FRAME — CHAFED (ZONE 200) · airframe 81,299 hrs · 20,313 cycles

CABIN - MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 535 BETWEEN LONGERON 22 - LONGERON 25 LEFT HAND EXISTING REPAIR LOWER FOUND HAVE CHAFFING MARKS. CABIN - MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 535 LOWER EXISTING OUTER REPAIR ANGLE CHAFFING MARK REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1 AT STATION 535 BETWEEN LONGERON 22 - LONGERON 25 LEFT HAND. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: FRAME — CHAFED (ZONE 200) · airframe 81,299 hrs · 20,313 cycles

CABIN - MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 535 BETWEEN LONGERON 18 - LONGERON 21 LEFT HAND EXISTING REPAIR UPPER FOUND HAVE CHAFFING MARKS. CABIN - MAIN DECK CARGO COMPARTMENT LEFT HAND FRAME STATION 535 UPPER EXISTING OUTER REPAIR ANGLE CHAFFING MARK REPAIRED AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1 AT STATION 535 BETWEEN LONGERON 18 - LONGERON 21 LEFT HAND. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: DOUBLER — CRACKED (RT WING) · airframe 81,299 hrs · 20,313 cycles

RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 545. RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 545 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: DOUBLER — CRACKED (ZONE 600) · airframe 81,299 hrs · 20,313 cycles

RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 638. RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 638 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: DOUBLER — CRACKED (LT WING LE) · airframe 81,299 hrs · 20,313 cycles

LEFT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 738. LEFT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 738 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: DOUBLER — CRACKED (ZONE 600) · airframe 81,299 hrs · 20,313 cycles

RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 817. RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 817 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: DOUBLER — CRACKED (RT WING) · airframe 81,299 hrs · 20,313 cycles

RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 708. RIGHT HAND WING FIXED LEADING EDGE SKIN INTERNAL DOUBLER AT STATION XOS 708 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/2/2022

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 80,576 hrs · 20,125 cycles

MDIS 616 32-60 1759 14MAY22 ANC FACT U UNSAFE RT MAIN GEAR INDICATION ON BOTH LIGHT AND CONFIG DISP. CYCLED GEAR PER QRH SHOWED UP/LOCKED. PER CAPT FACT 14MAY22 16:17 ANC U INSPECTED RIGHT MAIN GEAR. THE UPLOCK HOOK AND SENSORS. DOOR REMAINS UP AND LOCKED WHEN HYD PRESSURE IS REMOVED. PSEU SELF TEST PASSES. REF FIM 32-30-03. NO DEFECTS NOTED. NO HISTORY 30 DAYS.

Part: HINGE — CORRODED (CARGO DOOR) · airframe 80,267 hrs · 20,046 cycles

B CHECK #135 REV NO. PS ACCOMPLISH MAINTENANCE "B" CHECK - REP INSPECTION #135 NOTE: DURING B-CHK INSPECTION FOR THE FWD LOWER CARGO DOOR. THE UPPER HINGE WAS FOUND WORN AND CORRODED. THIS ISSUE WAS GENERATED ON NON ROUTINE N00027. UPPER HINGE REPLACED.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 78,724 hrs · 19,645 cycles

WHEN TESTING EMERGENCY LIGHTS RECEIVED LEVEL 1 EMER LT BAT 1 LO RELEASED FOR SERVICE PER MEL : 33-50-04 CATEGORY : C EXPIRATION : 04SEP21 "MEL 33-50-04: EMER LIGHTS - INOP. R/R'D EMERGENCY LIGHTING POWRSUPPLY MPN: 60-4411-5 ; S/N ON IS 0106 - REF MD11 AMM 33-51-01-4. OPS CHECK GOOD REF. MD11 AMM 33-51-01-700-802.

Part: BEARING — MIGRATED (ENGINE MOUNT) · airframe 76,429 hrs · 19,015 cycles

ENGINE NR 3 PYLON AFT MOUNT BEARING FOUND MIGRATED. ENGINE NR 3 PYLON AFT BULKHEAD AT STATION YWN 418.162. REMOVED AND REPLACED, AS PER MD-11 SRM 54-01-42-OG AND DOUGLAS DRAWING NR AUB 7500 REV ' AS '. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100. REFER TO ENGINEERING REQUEST SYSTEM NR 20-03641 FOR WORK DETAILS.

Part: FORMER — CRACKED (RT WING LE) · airframe 76,429 hrs · 19,015 cycles

RIGHT HAND WING, FIXED LEADING EDGE FORMER BETWEEN XOS 1010-1030, BEHIND NR 8 SLAT INBOARD SIDE, FOUND CRACKED AS MARKED. RIGHT HAND WING FIXED LEADING EDGE CRACKED FORMER BETWEEN XOS 1010-1030, BEHIND NR 8 SLAT INBOARD SIDE. REMOVED AND REPLACED WITH FABRICATED FORMER, AS PER MD-11, SRM 51-33-01-OG, FORMER FABRICATED, AS PER DOUGLAS DRAWING: ARB2920, REV BB. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING LE) · airframe 76,429 hrs · 19,015 cycles

LEFT HAND WING - LEADING EDGE FORMER AT APPROXIMATELY XORS 980 , BEHIND #8 SLAT CENTER AREA , FOUND CRACKED AS MARKED. LEFT HAND WING LEADING EDGE FORMER AT APPROXIMATELY XORS 980 , BEHIND #8 SLAT CENTER AREA REMOVED AND REPLACED WITH FABRICATED FORMER AS PER MD - 11 SRM 51- 31-01-OG , FORMER FABRICATED AS PER DOUGLAS DRAWING : ARB2920 REV. BB . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: DOUBLER — CRACKED (RT WING) · airframe 76,429 hrs · 19,015 cycles

AGING AIRCRAFT, EXISTING REPAIR FOUND AT RT WING FIXED LEADING EDGE LOWER SURFACE BETWEEN XOS 890 TO XOS 910. EXISTING REPAIR AT RT WING FIXED LEADING EDGE LOWER SURFACE BETWEEN XOS 890 TO XOS 910 EVALUATED AND FOUND REPAIRED IAW SRM 57-40-03-2R REPAIR 1 FIGURE 201. EO 1-5100-7-5001 B6 PART 1, TITLE: STRUCTURES-REPAIR CATALOG-MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN DECK) · corrosion level 2 · airframe 76,429 hrs · 19,015 cycles

MAIN DECK-UPON OPEN UP FLOOR PANEL FOR MODIFICATION, SEAT TRACK AT STATION 1700 X= -107.25 FOUND CORROSION AS MARKED. MAIN DECK RIGHT STATION 1700 X= -107.25 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1691 TO STATION 1731 X= -107.25, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 76,429 hrs · 19,015 cycles

01 EACH FASTENER HOLES #16 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=690 AND STATION XORS=700. LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700 . 01 EACH FASTENER HOLE #16 BUSHING REPAIR CARRIED OUT AS PER MD - 11 , SRM 57-20-02-2R , REPAIR 5 . FIGURE 201 . INITAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLE AFTER BUSHING REPAIR COMPLETION , AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLE BY HIGH FREQUENCY EDDY CURRENT INSPECTION METHOD PER MD -11 , SRM 57-20-02-2R , TABLE 201 REPAIR 5 . FIGURE 202 . REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100 .

Part: SKIN — CRACKED (LT WING LOWER) · airframe 76,429 hrs · 19,015 cycles

01 EACH FASTENER HOLES #13 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=690 AND STATION XORS=700. LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700 . 01 EACH FASTENER HOLE #13 BUSHING REPAIR CARRIED OUT AS PER MD - 11 , SRM 57-20-02-2R , REPAIR 5 . FIGURE 201 . INITAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLE AFTER BUSHING REPAIR COMPLETION , AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLE BY HIGH FREQUENCY EDDY CURRENT INSPECTION METHOD PER MD -11 , SRM 57-20-02-2R , TABLE 201 REPAIR 5 . FIGURE 202 . REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100 .

Part: SKIN — CRACKED (LT WING) · airframe 76,429 hrs · 19,015 cycles

01 EACH FASTENER HOLES #14 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS=690 AND STATION XORS=700. LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700 . 01 EACH FASTENER HOLE #14 BUSHING REPAIR CARRIED OUT AS PER MD - 11 , SRM 57-20-02-2R , REPAIR 5 . FIGURE 201 . INITAL INSPECTION TO BE CARRIED OUT AT 2000 FLIGHT CYCLE AFTER BUSHING REPAIR COMPLETION , AND REPETITIVE INSPECTION TO BE CARRIED OUT AT EVERY 2000 FLIGHT CYCLE BY HIGH FREQUENCY EDDY CURRENT INSPECTION METHOD PER MD -11 , SRM 57-20-02-2R , TABLE 201 REPAIR 5 . FIGURE 202 . REPAIR CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100 .

Part: SEAT TRACK — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 76,429 hrs · 19,015 cycles

CABIN LEFT HAND STATION 1425 X=47.5 SEAT TRACK FOUND CORROSION AS MARKED. CABIN LEFT HAND STATION 1425 X=47.5 SEAT TRACK CORROSION FOUND EXFLOLIATED AND EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1411 TO STATION 1451 X=47.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 76,429 hrs · 19,015 cycles

CABIN - LEFT HAND STATION 6-12 X = 27.5 SEAT TRACK FOUND CORROSION AS MARKED . CABIN LEFT HAND STATION 6-12 X=27.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 6-0 TO STATION 6-40 X=27.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (MAIN CABIN) · airframe 76,429 hrs · 19,015 cycles

CABIN RIGHT STATION 1421 X= -8.5 SEAT TRACK CROWN FOUND WORN, AS MARKED. CABIN RIGHT HAND STATION 1421 X= - 8.5 SEAT TRACK CROWN WORN AREA SMOOTHED OUT AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 1411 TO STATION 1451 X = - 8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1530) · airframe 76,429 hrs · 19,015 cycles

CABIN, LEFT STATION 1530 X=8.5 SEAT TRACK FOUND CORROSION. CABIN LEFT HAND STATION 1530 X=8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICE STATION 1531 TO STATION 5-83 X=8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1551) · airframe 76,429 hrs · 19,015 cycles

CABIN, LEFT STATION 1551 X=8.5 SEAT TRACK FOUND CORROSION. CABIN LEFT HAND STATION 1551 X=8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICE STATION 1531 TO STATION 1571 X=8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: UNKNOWN — MALFUNCTIONED (HYDRAULKIC SYS) · airframe 76,090 hrs · 18,892 cycles

LEVEL 1 HYD 1 OFF. QTY 7.5 TEMP 77 C SYS 2&3 TEMPS 43 AND 36 DEGRESS RESPECTIVELY.

Part: HYDRAULIC LINE — LEAKING (RT MLG WW) · airframe 74,161 hrs · 18,404 cycles

PDIS 616 29-02 8465 03NOV19 EWR FACT U LOGPAGES:3153051 RECEIVED AT CRUISE "HYD 3 ELEV OFF" ALERT LEV1. QTY HYD 3 WAS 5.9 WELL BELOW CYAN LINE.FOLLOWED QRH.QTY CONTINUED TO DECREASE TO 2.4 THEN AUTO SHUT DOWN. #3 HYD SYSTEM WENT DOWN TO 2.0 STABILIZED WITH ZERO PRESSURE...PRESSURIZED #3 SYSTEM TO LOWER GEAR AND QTY WENT TO ZERO.AFTER LANDING WHEN DEPRESSURIZED WENT TO 1.2.... SHGN 03NOV19 20:39 EWR U INSPECTION FOUND HYDRAULIC LEAK COMING FROM A 1/4" HYDRAULIC LINE FROM A FACTORY SWAGED FITTING IN RIGHT WHEEL WELL FWD WALL GOING TO SPOILER SERVO ACTUATOR. LEAK AREA MARKED WITH RED STREAMER. SHGN 04NOV19 07:19 EWR U FACT 04NOV19 10:43 EWR U INSPECTED AND REPLACED PRESSURE/CASE DRAIN FILTERS AND FOUND NO CONTAMINANTS. REMOVED AND REPLACED UPPER AND LOWER #3 ENGINE DRIVEN PUMPS DUE TO HYDRAULIC QUANITY REACHED 0 AFTER GEAR EXTENSION IAW AMM 29-11-20-4-1. OPS CHECK OK AND LEAK CHECK GOOD. FOUND HYDRAULIC LEAK COMING FROM A 1/4" HYDRAULIC LINE FROM A FACTORY SWAGED FITTING IN RIGHT WHEEL WELL FWD WALL GOING TO SPOILER SERVO ACTUATOR. LEAK AREA MARKED WITH RED STREAMER. SHGN 04NOV19 07:19 EWR U ACP REPAIR OF HYD LINE USING RYNGLOK FITTING PER AMM 20-10-01-2. LEAK CKS GOOD.

Part: SWITCH — FAILED (R1 DOOR) · airframe 72,103 hrs · 17,761 cycles

THE "CABIN DOOR FWD R" LEVEL 1 ALERT WILL NOT GO AWAY AFTER ARMING R1. THE "DOOR DISARM" LIGHT BY R1 EXTINGUISHES. REPLACED R1 DOOR DOWN LIMIT SWITCH. DOOR WARNING SYS OPS NORMAL.

Part: TRANSMITTER — FAILED (NLG) · airframe 71,830 hrs · 17,678 cycles

"TIRE FAIL" ANNUNCIATED WHEN LEVELING AT FL350 LEFT NOSE WHEEL INDICATED LOW PRESS THEN TIRE FAIL. REMOVED AND REPLACED LT NOSE WHEEL TIRE PRESS TRANS, REF AMM 32-46-04-4, OPS CHKD GOOD.

Part: FITTING — CORRODED (TE FLAP) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

RT O/B FLAP VANE HORN FITTING "F" FOUND HOLE BORE CORROSION. RT O/B FLAP VANE HORN FITTING 'F' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0342271 PART 1 STEP 1B. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · airframe 71,588 hrs · 17,600 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09, REPAIR SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342161 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER BARREL NUT HOLE BORE CORROSION. HINGE LOWER BARREL NUT HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS EPR CMM 57-44-09, OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342161 P1 STEP 2A AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FITTING — CORRODED (TE FLAP) · airframe 71,588 hrs · 17,600 cycles

RT O/B FLAP VANE HORN FITTING "E" FOUND HOLE BORE CORROSION. RT O/B FLAP VANE HORN FITTING 'E' HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0342271 PART 1 STEP 1A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

RT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132149 C PART 5 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

LT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132148 C PART 5 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342161 P1 STEP 2A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342161 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

RT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342163 P1 STEP 2A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342163 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER BARREL NUT HOLE BORE CORROSION. HINGE UPPER BARREL NUT HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342161 P1 STEP 2B AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

RT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-132149 C PART 5 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS EPR CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342161 P1 STEP 2A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342161 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,588 hrs · 17,600 cycles

LT WING, ALONG NR 6 SLAT LOCATION, ALONG XOS 789, LT LEADING EDGE FORMER ATTACHED DOUBLER CRACKED. LEADING EDGE FORMER ATTACHED DOUBLER, REMOVED AND REPLACED AS PER SRM 51-31-01-0G AND SRM 51-33-01-0G, DOUBLER PART NUMBER: ARB3954-7 FABRICATED AS PER DRAWING ARB3954 REVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 71,588 hrs · 17,600 cycles

05EA FASTENER HOLES (NR 6, 7, 15, 34 & 35) FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. SKIN REPAIR CARRIED OUT AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

RT WING O/B FLAP O/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342163 P1 STEP 2B AND STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

RT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342163 P1 STEP 2A AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342163 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 71,588 hrs · 17,600 cycles

LT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1- 5750-132148 C PART 5 STEP 2A AND STEP 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 71,588 hrs · 17,600 cycles

CABIN MAIN DECK CARGO EXISTING REPAIR ANGLE FRAME LONGERON 24 LEFT AT STA 535 LEFT HAND FRAME FOUND CHAFFING MARK. REPAIR ANGLE LEFT HAND FRAME REPAIRED AS PER SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 71,588 hrs · 17,600 cycles

LT WING LEADING EDGE BOTTOM SURFACE AROUND STA XOS =787.5 FOUND CRACK. REPAIR CARRIED OUT AS PER EA 1-5730-T0342355 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LE SLAT) · airframe 71,588 hrs · 17,600 cycles

LEFT HAND WING NR 8 SLAT OUTBOARD EDGE INTERIOR LOWER SURFACE AREA FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57-40-01-2R REPAIR 3 FIGURE 201 AT STA XOS 1180.5 AND PER EA 1-5750-T0342354 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,588 hrs · 17,600 cycles

NR 1 AIR CONDITIONING COMPARTMENT DOOR CUT OUT STA 587, L-32L AFT UPPER CORNER AREA FOUND CRACK. CRACK REPAIRED AS PER SRM 53-20-15-2R FIG 201 REPAIR 3, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 71,588 hrs · 17,600 cycles

MAIN DECK CARGO SEAT TRACK AT STA 635, X = 8.5 FOUND CRACK. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICE STA 625 TO STA 665, X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 71,588 hrs · 17,600 cycles

MAIN DECK CARGO LEFT HAND NR 3 DOOR AFT DOOR JAMB WEB AT STA 1315.420 FOUND CRACK. DOOR JAMB WEB REPAIRED AS PER SRM 53-40-15-2R FIGURE 201 REPAIR 3 FROM STA 1305.25 TO STA 1315.420. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 71,588 hrs · 17,600 cycles

MAIN DECK CARGO EXISTING REPAIR ANGLE FRAME, LONGERON 20L AT STA 535 LEFT HAND FRAME FOUND CHAFFING MARK. EXISTING REPAIR ANGLE FRAME REPAIRED AS PER SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 71,588 hrs · 17,600 cycles

DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT HAND WING FIXED LEADING EDGE ACCESS DOOR CUTOUT CORNERS, FOUND 01 EACH CRACK AT CORNER 11 APPROXIMATELY 0.3 INCH IN LENGTH. ACCESS DOOR CUTOUT STA XOS 610 CARRIED OUT REPAIR AS PER SRM 57-40-01-2R REPAIR 18 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SENSING ELEMENT — FAILED (NR 2 ENGINE) · airframe 71,419 hrs · 17,541 cycles

AT CRUISE W NR 2 ANTI-ICE ON PER MEL. RECVD NR 2 ANTI-ICE OFF ALERT WITH ENGINE NR 2 A-ICE DUCT HAS FAILED. DIVERTED. INTERROGATED ESC VIA CFDS, NO FAULT FOUND ON CURRENT FAULT BUT GOT ANTI-ICE VLV FAULT ON FAULT. REPLACED D1-90 AND D1-91 SENSING ELEMENT FOR PREVENTION IAW AMM 30-22-11-5. PERFORMED NR 2 ENG COWL MANIFOLD FAILURE SENSING ELEMENT FUNCTIONAL TEST AND TEST PASSED IAW AMM 30-22-04. REPLACED NR 2 ANTI-ICE SHUTOFF AND REGULATING VALVE AND MUSCLE SUPPLY LINE IAW AMM 30-22-06-4-1. REPLACED NR 2 ENG ANTI-ICE VALVE MUSCLE SUPPLE IN-LINE FILTER. PER AMM 30-22-00-5-2 PERFORMED NR 2 ENG ANTI-ICE VALVE OPEARTION TEST NORMAL. ENGING COWLING AND WORK PLATFORM CLOSED AND LOCKED AS PER AMM 52-46-01-2, 71-10-00-2-1.

Part: LIGHT — NO TEST (EMERGENCY LIGHTS) · airframe 70,671 hrs · 17,324 cycles

EMERGENCY LIGHT SYSTEM TEST FUNCTION INOPERATIVE.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY LIGHTS) · airframe 70,603 hrs · 17,309 cycles

DURING AN EMERGENCY LIGHT TEST, RECEIVED AN EMERGENCY LIGHT BATTERY 1 LOW LEVEL 1 MESSAGE. PERFORMED AN EMERGENCY LIGHT BATTERY ADJUSTMENT AND TEST IAW AMM 33-51-01-5. OPS CHECKED GOOD.

Part: BATTERY — WARNING MESSAGE (EMERGENCY LIGHTS) · airframe 70,416 hrs · 17,249 cycles

DURING A PREFLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW. PERFORMED EMERGENCY LIGHT TEST 3 CONSECUTIVE TIMES IAW MM 33-51-01-5. ALL GOOD IAW WRI 30-30/6329. SUSPECT MISC FAILING AND GENERATING SPURIOUS LOW BATTERY VOLTAGE ALERTS FOR EMERGENCY LIGHTS ALSO. EMERGENCY LIGHT BATTERY WAS ALSO CHANGED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,365 hrs · 17,239 cycles

WITH EMER LT SWITCH IN ARM POS AND TEST BUTTON PUSHED, GET EMER LT BAT1 LO ALERT. EMER LT TEST DOES NOT DISPLAY. EMER LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY REF AMM 33-51-01-4. OPS CHECKS GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 70,356 hrs · 17,236 cycles

HAD LEVEL 1 ENG ANTI-ICE OFF ALERT ON CLIMB OUT WITH A/I ENGINE 2 SELECTED. ALSO HAD A/I DISAGREE ON SELECTOR.

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 70,356 hrs · 17,236 cycles

LEVEL 1 ENGINE ANTI-ICE OFF ALERT DURING CLIMB OUT, WITH ANTI-ICE NR 2 ENGINE SELECTED. ALSO HAD AN ANTI-ICE DISAGREE ON SELECTOR. REMOVED AND REPLACED THE NR 2 ENGINE ANTI -ICE VALVE IAW AMM 30-22-01-4. ADJUSTMENT AND TESTED GOOD IAW AMM 30-22-00-5-1.

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 70,356 hrs · 17,236 cycles

HAD A LEVEL 1 ENGINE ANTI-ICE OFF ALERT DURING CLIMB OUT. WITH ANTI-ICE NR 2 ENGINE SELECTED. REMOVED AND REPLACED THE NR 2 ENGINE ANTI -ICE VALVE IAW AMM 30-22-01-4. ADJUSTMENT AND TESTED GOOD IAW AMM 30-22-00-5-1. ENGINE RUN PERFORMED.

Part: SKIN — DAMAGED (LT WING) · airframe 68,596 hrs · 16,730 cycles

ON POST FLIGHT, FOUND THE LT WING UPPER SKIN PEELED BACK BETWEEN INBD AILERON AND OTBD FLAP. REMOVED DAMAGED AREA. FABRICATED A REPAIR IAW SRM 57-50-01-2R, FIGURE 203, REPAIR 6.

Part: SLIDE — DETACHED (L1 DOOR) · airframe 66,969 hrs · 16,276 cycles

L1 DOOR SLIDE FELL OUT. REMOVED AND REPLACED L1 SLIDE IAW AMM 25-61-01-4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,738 hrs · 16,193 cycles

MAIN DECK BS 725 - 765, X 8.5 SEAT TRACK ASSEMBLY FOUND CORRODED. CORRODED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 665 TO STA 765 X=8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 66,738 hrs · 16,193 cycles

RIGHT WING EXTERIOR, FOUND FIXED LEADING EDGE LOWER FORWARD DOUBLER AT XOS 547 CRACKED. CRACKED DOUBLER REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER PER SRM 51-31-01-0G. NEW DOUBLER FABRICATED PER DWG #ARB2933 REV 'T'. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 66,738 hrs · 16,193 cycles

LEFT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 770 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR NR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 66,738 hrs · 16,193 cycles

RIGHT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 665 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR NR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,738 hrs · 16,193 cycles

MAIN DECK BS 1831, X 27 SEAT TRACK FOUND WITH SURFACE CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1811 TO STA 1884 X=27 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 66,738 hrs · 16,193 cycles

LEFT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 665 FOUND CRACKED. BEADED DOUBLER REPAIRED PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 66,738 hrs · 16,193 cycles

LEFT WING FIXED LEADING EDGE LOWER FORWARD DOUBLER AT XOS 547 FOUND CRACKED. R & R WITH NEW FABRICATED DOUBLER IAW SRM 51-31-01-0G. NEW DOUBLER FABRICATED IAW DWG ARB2933, REV-T. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,738 hrs · 16,193 cycles

MAIN DECK BS 1541 - 1561 X -8.5 SEAT TRACK FOUND WITH CORROSION. CORRODED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1531 TO STA 1591 X=-8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 66,738 hrs · 16,193 cycles

MAIN DECK BS 685, X -8.5 SEAT TRACK FOUND WTH DAMAGED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 665 TO STA 765 X=-8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 66,738 hrs · 16,193 cycles

LT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 731 FOUND CRACKED. CRACKED BEADED DOUBLER REPAIRED PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 66,738 hrs · 16,193 cycles

LEFT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 766 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR NR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 66,738 hrs · 16,193 cycles

LEFT WING FIXED LEADING EDGE LOWER FORWARD DOUBLER AT XOS 489 FOUND CRACKED. R & R WITH NEW FABRICATED DOUBLER IAW SRM 51-31-01-0G. NEW DOUBLER FABRICATED IAW DWG ARB2933 REV-T. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 66,738 hrs · 16,193 cycles

RIGHT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 792 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR NR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 66,738 hrs · 16,193 cycles

FORWARD CARGO STA 895.700 BETWEEN LONGERON L-40R TO L-41R DOOR JAMB EXISTING REPAIR DOUBLERS FOUND CHAFED. FORWARD CARGO STA 895.700 BETWEEN LONGERON L40R TO LONGERON L41R DOOR JAMB EXISTING REPAIR DOUBLERS CHAFED MARKS REPAIRED IAW EA NR 1-5330-T0311886B, PT 3, TITLE : FUSELAGE-PLATES AND SKINS, EXISTING REPAIR FOUND ON FORWARD LOWER CARGO DOOR, FORWARD JAMB. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53304311 FOR WORK DETAILS.

Part: TRUNNION — CRACKED (NLG) · airframe 66,738 hrs · 16,193 cycles

NOSE LANDING GEAR WHEEL WELL RT TRUNNION SUPPORT FITTING SUSPECT CRACKED BS 595. REPAIRED IAW SRM 53-10-14-2R, FIG 202, REPAIR 2.

Part: DOOR — STUCK (R1) · airframe 66,213 hrs · 16,020 cycles

DURING PREFLIGHT, R-1 DOOR WOULD NOT OPEN.

Part: LIMIT SWITCH — MALFUNCTIONED (PAX DOOR) · airframe 66,119 hrs · 15,985 cycles

RIGHT FORWARD PASSENGER DOOR WILL CLOSE, BUT WILL NOT OPEN ELECTRICALLY. R & R GIRT BAR LIMIT SWITCH AND POWER INTERLOCK SWITCH IAW AMM 52-11-02-5. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: SWITCH — MALFUNCTIONED (COCKPIT) · airframe 64,990 hrs · 15,597 cycles

ENROUTE, AT :50 MINUTES INTO FLIGHT, RECEIVED LVL 2 AVIONICS AIR FLOW OFF. AS SOON AS QRH WAS REFERENCED LVL 2 WENT OUT. CONTROLLER PUT AVIONICS FAN IN OVERRIDE. WHEN THAT HAPPENED LVL 2 WENT OUT, LVL 1 AVIONICS FAN OVRD ON. SAT COMM WITH GOC & MX. AIR TURN BACK. INSTALLED REPAIRED DUCT IAW SMP & REPLACED AVIONICS COMPARTMENT OVERHEAT SWITCH IAW AMM 21-62-22-5.

Part: DOOR — MISSING (THRUST REVERSER) · airframe 645 hrs · 15,465 cycles

DURING POST FLIGHT WALK AROUND, FOUND THE NR 1 OTBD THRUST REVERSER BLOCKER DOOR MISSING & ATTACH STRUCTURE BROKEN. ALSO TRANS COWL DAMAGED FROM DOOR. INSTALLED NR 1 ENG LT OTBD TRANSLATING COWL IAW M 78 3116 41. THE 3 LOWER BLOCKER DOORS ARE INSTALLED UP TO STEP F. THE 3 UPPER BLOCKER DOORS STILL NEED INSTALLATION. THE 3 BALL SCREW ROD END BOLTS NEED TO BE SAFE TIED AFTER FINAL ADJUSTMENTS. INSTALLED UPPER 3 BLOCKER DOORS IAW AMM 78-31-14-4-1. TRANSLATING COWL OPERATIONS CHECKED GOOD. SAFE TIED ALL SCREW END ROD BOLTS & COVERS INSTALLED IAW AMM 78-31-16-4-1.

Part: BOTTLE — LEAKING (EVAC SLIDE) · airframe 636 hrs · 15,204 cycles

ON ACFT ARRIVAL FOUND L1 DOOR SLIDE BOTTLE EMPTY. R&R BOTTLE PER AMM 25-61-01-4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

CENTER CARGO DOOR AFT JAMB STA 1781 LONGERON 41R, REPAIR CARRIED OUT AT CENTER CARGO DOOR AFT JAMB STATION 1781 LONGERON 41R AREA AS PER EA 1-5330-T0305743A PART 3. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REFER TO WRI 53301210 FOR DETAILS.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

MAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635, X= -47.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X=-47.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

CABIN MAIN DECK CARGO COMPARTMENT LT STATION 1256 LONGERON 26L FWD L3 DOOR LOWER JAMB FOUND WEB CRACKED. CRACKED WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 61,596 hrs · 14,597 cycles

RIGHT WING LE BEADED DOUBLER AT STATION XOS 861 - XOS 867 FOUND CRACKED. CRACKED REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

MAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X=27.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X= 27.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

MAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 755 X=27.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 745 TO STATION 785, X= 27.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

MAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X= 47.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X= 47.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

MAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X= -8.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT STATION 625 TO STATION 665, X=-8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

MAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X= 27.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X=-27.5 AS PER SRM 53- 00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

AGEING ACFT EXISTING REPAIR FOUND AT FWD CARGO DOOR JAMB CUT OUT AFT LOWER AT STATION 1002 BETWEEN LONGERON 40R TO 41R. EXISTING REPAIR FOUND DAMAGED. REPAIRED PER SRM 53-00-15 FIGURE 202 REPAIR 8 EO 1-5100-7-5001B5 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO WRI 53301199 FOR WORK DETAILS.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

CABIN MAIN DECK CARGO COMPARTMENT RT STATION 1310 LONGERON 26R AFT R3 DOOR LOWER JAMB FOUND WEB CRACKED. CRACKED WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 61,596 hrs · 14,597 cycles

RIGHT WING LE FORMER AT STATION XOS 559 FOUND CRACKED. FORMER REMOVED AND FABRICATED NEW FORMER AS PER DRAWING ARC1162 REVISION S INSTALLED NEW FORMER AT RIGHT HAND WING LEADING EDGE STATION XOS 559 AS PER SRM 51-33-01 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

CABIN MAIN DECK CARGO COMPARTMENT RT STATION 1256 LONGERON 26R. FWD R3 DOOR LOWER JAMB FOUND WEB CRACKED. CRACKED WEB REPAIRED AS PER SRM 53-40-15 FIGURE 201. REPAIR 3 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

MAIN DECK CARGO COMPARTMENT FOUND CARGO TRACK AT STATION 635 X= 8.5 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 625 TO STATION 665, X= 8.5 AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: FRAME — DENTED (FUSELAGE) · airframe 61,596 hrs · 14,597 cycles

CABIN MAIN DECK CARGO COMPARTMENT LT STATION 1721 LONGERON 12L FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — WORN (CARGO DOOR) · airframe 58,107 hrs · 13,469 cycles

UPPER CARGO DOOR ATTACHED FORWARD HINGE LOWER LOBES WORN. REAMED AS PER CMM 52-34-04 REVISION 75. REPAIR ACCOMPLISHED AS PER EA 1-5230-167401 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: SKIN — CHAFED (ZONE 500) · airframe 58,107 hrs · 13,469 cycles

LT WING FIXED L/E UPPER SURFACE STATION XIS 247 FOUND WITH CHAFING. REPAIRED AS PER SRM 57-40-02 REPAIR 8 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100 REVISION 116.

Part: BULKHEAD — CRACKED (MLG WW) · airframe 58,107 hrs · 13,469 cycles

CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD, RT SPOILER MIXER CONTROL ROD FEED THROUGH CUTOUT DOUBLER FOUND CRACKED. FABRICATED DOUBLER INSTALLED AS PER SRM 51-33-01 REVISION 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 58,107 hrs · 13,469 cycles

LEFT WING INBD FLAP ASSY, INBD LOWER SEGMENT LOWER SURFACE FOUND DENTED. REPAIRED AS PER SRM 57-50-01 FIGURE 201 REPAIR 1 REVISION 52 AND E.A. 1-5750-166104.

Part: DOUBLER — CRACKED (LT WING) · airframe 58,107 hrs · 13,469 cycles

LEFT WING FIXED L/E XOS 690 BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 58,107 hrs · 13,469 cycles

LT WING T/E PANEL NR 541JB CUTOUT FORWARD CAP FOUND CORROSION AT XW 338. REPAIRED IAW SRM 51-31-01 REVISION 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.

Part: DOUBLER — SCRATCHED (ZONE 100) · airframe 58,107 hrs · 13,469 cycles

FORWARD CARGO DOOR CUTOUT AFT JAMB LOWER DOUBLER FOUND SCRATCHED. REPAIRED IAW SRM 53-00-15 REPAIR 8 FIGURE 202 REVISION 51.

Part: CONTROL UNIT — FAILED (GENERATORS) · airframe 57,835 hrs · 13,387 cycles

AFTER TAKEOFF CLIMBING OUT OF 3000 FT LOST ALL GENERATORS, APPEARED TO BE PRODUCING POWER BUT COULD NOT CONNECT TO THE SYSTEM. DEPLOYED ADG AND RETURNED TO AIRPORT. REMOVED AND REPLACED EPCU REF AMM. RAN ALL ENGINES PER JRH. ALL INDICATIONS NORMAL NO FAULTS.

Part: TIRE — FAILED (MLG) · airframe 57,798 hrs · 13,370 cycles

NR 10 TIRE BLOWN ON LANDING. R & R RED CENTER WHEEL NR 9 AND NR 10 IAW MM 32-41-01-4. DURING WHEEL REPLACEMENT ON NR 10 FOUND WHEEL AIR TRANSDUCER AND HUBCAP BROKEN, R & R RED TRANSDUCER AS MM 32-46-03-4, REPLACED HUBCAP IAW MM 32-46-11-4, ADJUSTED TIRE PRESSURE ON BOTH WHEELS. PERFORMED VISUAL INSP ON AFT FUSELAGE AND CENTER WHEEL COMPARTMENT FOR DAMAGE, NO DEFECT FOUND. DURING T/ FOUND BOTH FWD HYD LINES CROSSED BETWEEN BRAKE NR 9 AND NR 10. REINSTALLED ALL LINES ON ORIGINAL PLACE IAW MM 20-40-01-2. PERFORMED OPS TEST ON ASCU AS MM 32-45-01-5, ALL TEST PASSED. ACFT OK FOR SERVICE.

Part: FIRE DETECTOR — FAILED · airframe 57,927 hrs · 13,424 cycles

AFTER DEPARTURE, CLIMBING THROUGH FL300 FOR FL330. RECEIVED FIRE DET 3 FAIL ALERT. DUMPED APPROX 17,000 LBS FUEL AND RETURNED TO DEPARTURE. AFTER BLOCK IN WITH EXTERNAL POWER ON EXTERNAL POWER DROPPED OFF. AFTER STARTING APU POWER, RECEIVED ENG 3 FIRE WARNING. VERIFIED FROM GROUND THAT THERE WAS NO ACTUAL FIRE. R & R NR 3 ENG LOOP A AND B FROM DH5C TO TB2C. OPS CHECK GOOD. REF AMM 26-11-03-4. ALSO RAN ENG IAW JRH ALL INDICATIONS NORMAL.

Part: TEE FITTING — CRACKED (FUEL SYSTEM) · airframe 54,625 hrs · 12,510 cycles

RUNNING TANK TO ENGINE ON ALL 3 ENGINES. ALL FILL VALVES WERE CLOSED BUT FUEL LEVEL IN TANK 1 WAS NOT DECREASING. VERIFIED ON GROUND WITH TANK 2 AND 3 TRANSFER PUMPS ON THE NR1 TANK QUANTITY INCREASED WITH THE FILL VALVE SELECTED (AND INDICATED) CLOSED. UNCOMMANDED FUEL TRANSFER WAS APPROX 1000 LBS EVERY 7 MINUTES. R & R THE NR 1 MAIN TANK FILL SHUTOFF VALVE CONTROLLER IAW AMM 28-21-02-4. NO HELP. UNCOMMANDED FUEL TRANSFER STILL TAKES PLACE AT THE SAME RATE. TANK ACCESSED AND FOUND CRACKED LINE AT TEE FITTING FROM NR 1 TANK FILL VALVE ON TOP SIDE OF WELDED FLANGE. REPLACED IAW MM 28-00-00-2-0 & 28-00-00-4-0. PRESSURISED REFUEL/CROSSFEED MANIFOLD USING NR 2 TRANSFER PUMP, NO FUEL TRANSFER EVIDENT AFTER 10 MINUTES.

Part: LONGERON SPLICE — CORRODED (ZONE 100) · airframe 52,864 hrs · 12,085 cycles

LONGERON SPLICE L-52 AT APPROX STA 6-10 FOUND CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 46. LONGERON SPLICE FABRICATED AS PER DRAWING AAA7088 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 52,864 hrs · 12,085 cycles

VERTICAL STABILIZER LT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 2 REVISION 46 AND SRM 51-33-01 REVISION 46. OPS TEST OF THE ENG IGNITION/FADEC MODE SWITCH AND ADVISORY LIGHTS CARRIED OUT AS PER AMM 73-21-10-5 REVISION 69.2 FOUND SATISFACTORY. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: SKIN — CRACKED (ZONE 500) · airframe 52,864 hrs · 12,085 cycles

LT WING - 15 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 TO STA XORS 713.6. CARRIED OUT REPAIR AS PER BOEING DRAWING : SG11570004 REVISION B. QUANTITY 01 EACH CRACKED FASTENER HOLE AT LEFT HAND WING FUEL TANK ACCESS PANEL 536AB CUTOUT AT XORS 683 TO XORS 713 CARRIED OUT REPAIR AS PER EA1-5710-143551. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 112.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 52,864 hrs · 12,085 cycles

LOWER CTR CARGO COMPARTMENT BILGE, STA 5-123 LONGERON 46RT SPLICE FITTING FOUND CRACKED. LONGERON SPLICE FITTING FABRICATED AS PER DOUGLAS DRAWING A5A7116 REVISION D. SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SKIN — CRACKED (ZONE 600) · airframe 52,864 hrs · 12,085 cycles

RT WING - 13 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 TO STA XORS 713.6. CARRIED OUT REPAIR AS PER DRAWING : SG11570004 REVISION B. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 112.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 52,864 hrs · 12,085 cycles

VERTICAL STABILIZER RT CTR SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIG 201 REPAIR 2 REVISION 46 AND SRM 51-33-01 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: STIFFENER — CRACKED (BS 2164) · airframe 52,864 hrs · 12,085 cycles

EMPENNAGE FORWARD TAIL CONE RIGHT HAND LOWER ALIGNING PIN SUPPORT CHANNEL FOUND CRACKED AT BULKHEAD STATION 2164 AFT FACE. EMPENNAGE LOWER BULKHEAD STATION 2164 RIGHT HAND LOWER ALIGNING PIN SUPPORT STIFFENER REPAIR CARRIED OUT AS PER SRM 53-80-02 FIG 201 REPAIR 1 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: FRAME — DENTED (ZONE 200) · airframe 52,864 hrs · 12,085 cycles

CABIN RIGHT HAND STATION 1701 L-11 FRAME FOUND DENT. CABIN RIGHT HAND STATION 1701 L-11 DENTED FRAME REPAIRED AS PER SRM 53-00-07 FIG 201 REPAIR 2 REVISION 46. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-00-07 FIG 201 REPAIR 2 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.

Part: SEAT TRACK — CORRODED (BS 470-495) · corrosion level 2 · airframe 52,864 hrs · 12,085 cycles

CABIN RIGHT HAND STATION 470 TO 495 X=-27.5 SEAT TRACK FOUND CORROSION. CABIN RIGHT HAND STATION 470 TO 495 X=-27.5, CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 455 TO STATION 525 X=-27.5 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REVISION 46. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112.

Part: SKIN — CRACKED (ZONE 100) · airframe 51,657 hrs · 11,814 cycles

WHILE CARRYING OUT WALKAROUND CHECK, FOUND LOWER CTR CARGO DOOR WITH 01 EACH EDGE CRACK AT FWD LOWER CORNER. REPAIRED AS PER SRM 52-30-16 FIGURE 201 REVISION 44.0. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 111.

Part: STRUCTURE — CRACKED (MLG WW) · airframe 47,492 hrs · 10,821 cycles

CENTER LANDING GEAR - RT CUT-OUT FOR SPOILER MIXER INPUT ROD DOUBLER CRACKED. CTR LANDING GEAR - RT CUT-OUT FOR SPOILER MIXER INPUT ROD DOUBLER REMOVED AND REPLACED WITH NEW DOUBLER IAW SRM 51-31-01 VOL. II REV. 40. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV. 107.

Part: STRUCTURE — CRACKED (MLG WW) · airframe 47,492 hrs · 10,821 cycles

CENTER LANDING GEAR- LT CUT-OUT FOR SPOILER MIXER INPUT ROD DOUBLER CRACKED. CTR LANDING GEAR- LT CUT-OUT FOR SPOILER MIXER INPUT ROD DOUBLER REMOVED AND REPLACED WITH NEW DOUBLER IAW SRM 51-31-01 VOL. II REV. 40. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV. 107.

Part: HINGE — CORRODED (ZONE 600) · airframe 47,492 hrs · 10,821 cycles

RT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT INBD HOLE FOUND WITH CORROSION. REPAIRED IAW EA 1-5750-132146.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 47,492 hrs · 10,821 cycles

LT WING INBD FLAP AFT HINGE FITTING OTBD HINGE OTBD PIVOT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-132148.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 47,492 hrs · 10,821 cycles

LT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) BARREL NUT LWR BORE FOUND WITH CORROSION. REPAIRED IAW EA 1-5750-132147.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 47,492 hrs · 10,821 cycles

LT WING INBD FLAP AFT HINGE FITTING OTBD HINGE INBD PIVOT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-132148.

Part: SKIN — CRACKED (ZONE 300) · airframe 47,492 hrs · 10,821 cycles

SKIN CRACK FOUND AT APPROX STA 2140 LONGERON 36 RT JUST ABOVE APU EXHAUST AREA. REPAIR IAW SRM 53-20-00 VOL1, FIG4, REV40 (MAJOR REPAIR).

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 47,492 hrs · 10,821 cycles

RT WING INBD FLAP AFT HINGE FITTING OTBD HINGE INBD PIVOT HOLE FOUND CORROSION. REPAIR IAW EA 1-5750-132149.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 47,492 hrs · 10,821 cycles

AFT BODY FAIRING ENCLOSED AREA AT APPROX 2164 LONGERON, 33RH TO LONGERON 35RT FOUND WITH CORROSION ADJACENT TO SCREW HOLES. REPAIR IAW SRM 53-20-00 VOL1, FIG18, REV40 (MAJOR REPAIR).

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 47,492 hrs · 10,821 cycles

RT WING INBD FLAP AFT HINGE FITTING OTBD HINGE OTBD PIVOT HOLE FOUND CORROSION. REPAIRED IAW EA 1-5750-132149.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 47,492 hrs · 10,821 cycles

LT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) BARREL NUT UPPER BORE FOUND WITH CORROSION. REPAIRED IAW EA 1-5750-132147.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,492 hrs · 10,821 cycles

CABIN - RT STA 1259 TO STA 1301 X= -107 SEAT TRACK FOUND CORROSION. CABIN CORRODED SEAT TRACK AT RT STA 1259 TO STA 1301 X= -107, REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1229 TO STA 1331 X= -107 IAW SRM 53-70-00 FIG. 1, VOL I, REV. 40. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,492 hrs · 10,821 cycles

CABIN - SEAT TRACK FLANGE AT STA 1655 X= -107 FOUND EXFOLIATION CORROSION. CABIN - SEAT TRACK FLANGE AT STA 1655 X= -107 REPAIRED IAW SRM 53-70-00 FIG 6, VOL I, REV. 40. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 107.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 47,492 hrs · 10,821 cycles

CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 6 LWR JAMB FITTING AT HOLES B AND D. REPAIRED IAW EA 1-5310-132150.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 47,492 hrs · 10,821 cycles

CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 6 LWR JAMB FITTING AT HOLE D. REPAIR IAW EA 1-5310-132150.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 47,492 hrs · 10,821 cycles

CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 1 LWR JAMB FITTING AT HOLES A AND C. REPAIR IAW EA 1-5310-132150.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 47,492 hrs · 10,821 cycles

CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLE AT MAIN CARGO DOOR NO. 7 LOWER JAMB FITTING AT HOLE B. REPAIRED IAW EA 1-5310-132150.

Part: TERMINAL — BROKEN (FIRE DETECTOR) · airframe 46,245 hrs · 10,516 cycles

DURING POWER REDUCTION LEVEL 3 ENGINE 2 FIRE ALERT. BEGAN CHECKLIST ALERT/LIGHTS WENT AWAY. ENG 2 FIRE DET FAIL ILLUMINATED. FOLLOWED BY ENGINE FIRE, DETECT FAIL, DETECT FAULT. ALL ALERTS CLEARED EXCEPT ENG 2 FAULT (PREVIOUS WRITE-UP/MEL). ON RETURN, SAME INDICATIONS ON FINAL, AS ABOVE. FOUND TERMINAL TB2-C BROKEN FROM RESPONDER ON "A" LOOP, REPAIRED PER WIRING DIAG 26-11-02, LOOP "A". OPS CHECK NORMAL, RAN ENG TO TEST PER JRH, ALL CHECK NORMAL. STILL HAVE "UP RIGHT FIRE DET ASSY B" FAULT, WILL PLACE ON MEL AND DISPATCH ACFT. THIS WRI TO BE CLOSED AND NEW WRI FOR NR 2 B LOOP OPENED.

Part: DOOR — CHAFED (MLG) · airframe 42,787 hrs · 9,786 cycles

RT MLG FLIPPER DOOR FORWARD SIDE FOUND CHAFED. RT MLG FLIPPER DOOR FORWARD SIDE CHAFFED EDGE SMOOTHENED OFF AND FOUND WITHIN LIMIT AS PER SRM 52-00-01 FIGURE 1 VOLUME I. RT MLG AND GEAR WHEEL DOOR OPERATION CHECK CARRIED OUT AS PER AMM 32-31-00-700-803. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 42,787 hrs · 9,786 cycles

CENTER CARGO COMPARTMENT, BILGE AREA, LONGERON SPLICE AT STA 5-123, L-52, FOUND CRACKED ABOUT 6 INCHES. CRACKED LONGERON SPLICE AT CENTER CARGO COMPARTMENT BILGE AREA STA 5-123, LONGERON 52, REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,787 hrs · 9,786 cycles

MAIN DECK SEAT TRACK AT STA 1831 - 2007, -X107, SEVERAL CORROSION FOUND NEAR CLIPNUTS, VIEW FROM WASTE TANK COMPARTMENT. REPAIR CARRIED OUT AS PER E.A. 1-5340-117264, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,787 hrs · 9,786 cycles

MAIN DECK SEAT TRACK AT STA 1831 - 2007, X107, SEVERAL CORROSION FOUND NEAR CLIPNUTS, VIEW FROM WASTE TANK COMPARTMENT. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (ZONE 700) · airframe 42,787 hrs · 9,786 cycles

NOSE LANDING GEAR LEFT TRUNNION SUPPORT FITTING FOUND CRACK. CARRIED OUT REPAIR AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 37,827 hrs · 8,662 cycles

M/D CARGO LT SEAT TRACK (STA 695, LT, X=27.5) FOUND EDGE UNDER FLOOR CRACKED. REPAIR CARRIED OUT AT M/D CARGO, LH SEAT TRACK (STA 695, LT, X=27.5) PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — DAMAGED (ZONE 100) · airframe 37,827 hrs · 8,662 cycles

CTR CARGO DOOR CUTOUT AFT LOWER SKIN REPAIR DOUBLER EDGE FOUND DAMAGED. REPAIR DOUBLER REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. NEW REPAIR DOUBLER FABRICATED PER SRM 53-50-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: RIB — CRACKED (ZONE 500) · airframe 37,827 hrs · 8,662 cycles

LEFT WING LOWER WINGLET FOUND RIB CRACK. RIB REMOVED AS PER SRM 51-33-01 VOLUME II. NEW RIB FABRICATED AS PER DRAWING ARB7774 AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 37,827 hrs · 8,662 cycles

CRACK FOUND DURING HFEC INSP ON RT WING TANK AT THE END OF STRINGER-11 AT WING STA XORS 704. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON RH WING TANK, END OF STRINGER 11, WING STA XORS 704 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (LT WING) · airframe 37,827 hrs · 8,662 cycles

CRACK FOUND DURING HFEC INSP ON LT WING TANK AT THE END OF STRINGER-10 AT WING STA XORS 760. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 37,827 hrs · 8,662 cycles

RIGHT HAND WING FIXED L/E RIB DOUBLER FOUND CRACK AT XOS 667. REMOVED PER SRM 51-33-01 VOLUME II. NEW RIB DOUBLER FABRICATED PER DRAWING ARB3954 AND INSTALLED AS PER SRM 51 -33-01 VOLUME II. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 37,827 hrs · 8,662 cycles

LEFT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACK. REPAIR CARRIED OUT AT LH WING FIXED L/E TELESCOPING DUCT CUTOUT CRACK AS PER FEDEX EA 1-5730-103531. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 37,827 hrs · 8,662 cycles

LEFT WING, LEFT RIB DOUBLER AT XOS 667 FOUND CRACK. REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 37,827 hrs · 8,662 cycles

RT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACK. REPAIRED AS PER FEDEX EA1-5730-103532, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (LT WING) · airframe 37,827 hrs · 8,662 cycles

CRACK FOUND DURING HFEC INSP ON LT WING TANK AT THE END OF STRINGER-11 AT WING STA XORS 704. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (LT WING) · airframe 37,827 hrs · 8,662 cycles

CRACK FOUND DURING HFEC INSP ON LT WING TANK AT THE END OF STRINGER 9 AT WING STA XORS 819. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON LT WING TANK, END OF STRINGER 9, WING STA XORS 819 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 37,827 hrs · 8,662 cycles

RIGHT HAND WING FIXED L/E RIB DOUBLER FOUND CRACK AT XOS 667. REMOVED PER SRM 51-31- 01 VOLUME II. NEW RIB DOUBLER FABRICATED PER DRAWING ARB3954 AND INSTALLED PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED MINOR PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (LT WING) · airframe 37,827 hrs · 8,662 cycles

CRACK FOUND DURING HFEC INSP ON LT WING TANK AT THE END OF STRINGER-12 AT WING STA XORS 642. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON LT WING TANK, END OF STRINGER 12, WING STA XORS 642 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 37,827 hrs · 8,662 cycles

CRACK FOUND DURING HFEC INSP ON RIGHT WING TANK AT THE END OF STRINGER 42 AT WING STA XORS 629. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON RT WING TANK, END OF STRINGER 42, WING STA XORS 629 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRUCTURE — CRACKED (RT WING) · airframe 37,827 hrs · 8,662 cycles

CRACK FOUND DURING HFEC INSP ON RT WING TANK AT THE END OF STRINGER 41 AT WING STA XORS 685. REPAIR CARRIED OUT AT CRACK FOUND DURING HFEC INSP ON RH WING TANK, END OF STRINGER 41, WING STA XORS 685 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: ENGINE — FLUCTUATES (NR 2) · airframe 34,640 hrs · 7,926 cycles

NR 2 ENGINE DISPLAYED GRADUAL OIL LOSS TO AN INDICATION OF 1 QT JUST BEFORE DESCENT TO KIX. OIL PRESSURE BEGAN TO FLUCTUATE A LITTLE AND DURING DESCENT AN ALERT "OIL PRESS LO" DISPLAYED. PRECAUTIONARY SHUTDOWN PER QRH. NR 2 OIL PRESSURE WAS AROUND 35 PSI WITH 1 AND 3 ABOUT 50 PSI. IN IDLE DESCENT PRESSURE WAS SOMEWHERE BELOW 30 PSI WHEN "LO PRESS" ALERT CAME ON.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER FORWARD SKIN PLANK NR 3L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939

Part: SUPPORT BRACKET — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

FLOOR PANEL SUPPORT BRACKET AT STA 457 LBL 82 FOUND CORRODED. REMOVED IAW SRM 51-35-01 VOL II. FABRICATED NEW SUPPORT IAW DRAWING NR ABA8356 AND INSTALLED IAW SRM 51-33-01 VOL II.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER AFT SKIN PLANK NR 34L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82941.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT HAND UPPER AFT SKIN PLANK NR 34R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82942.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 1R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR 1-5510-7-5000 HAS BEEN COMPLIED WITH.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PLANK NR 36L BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR 33R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 2L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82939.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER FORWARD SKIN PLANK NR 4L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82939.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR29R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82942.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON NR 14R BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 23R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82953.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON NR 26R BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 3R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER CENTER SKIN PLANK NR 17R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82953.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER CENTER SKIN PLANK NR 16L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER CENTER SKIN PLANK NR 22L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER CENTER SKIN PLANK NR 20L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 15R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82953.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER AFT SKIN PLANK NR 27R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 13R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH.

Part: SUPPORT — CRACKED (ZONE 600) · airframe 33,528 hrs · 7,688 cycles

RIGHT WING FIXED LEADING EDGE ACCESS PANEL FORWARD SUPPORT AT STA XOR 450 FOUND CRACKED. REMOVED CRACKED SUPPORT AS PER SRM 51-31-01 VOLUME II AND FABRICATED NEW SUPPORT DOUBLER AS PER DRAWING ARB2933. INSTALLED NEW SUPPORT DOUBLER AT RIGHT WING FIXED LEADING EDGE ACCESS PANEL FORWARD AT STA XOR 450 AS PER SRM 51-35-01 VOLUME II AND SRM 51-33-01 VOLUME II.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER CENTER SKIN PLANK NR 24L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 33,528 hrs · 7,688 cycles

LEFT WING, FIXED LEADING EDGE ACCESS PANEL FORWARD SUPPORT AT STA XOR 450 FOUND CRACKED. REMOVED CRACKED SUPPORT AS PER SRM 51-31-01 VOLUME II AND FABRICATED NEW SUPPORT DOUBLER AS PER DRAWING ARB2933. INSTALLED NEW SUPPORT DOUBLER AT LEFT WING FIXED LEADING EDGE ACCESS PANEL FORWARD AT STA XOR 450 AS PER SRM 51-35-01 VOLUME II AND SRM 51-33-01 VOLUME II.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER RIGHT UPPER FORWARD SKIN PLANK NR 5R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82943.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER FORWARD SKIN PLANK NR 14L BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED IAW SRM 51-33-01, VOL II.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT UPPER AFT SKIN PLANK NR 28L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STABILIZER LEFT HAND UPPER CENTER SKIN PLANK NR 26L BARREL NUT BORE FOUND EXCEEDED LIMITS. REMOVED AND REPLACED IAW SRM 51-33-01, VOL II.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 20R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953.

Part: SPAR CAP — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB RT UPPER AFT SPAR CAP NR 36R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82959.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER CENTER SKIN PLANK NR 23L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZONTAL STAB RT UPPER CENTER SKIN PLANK NR 16R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 29L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 22R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER CENTER SKIN PLANK NR 25L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB RT UPPER AFT SKIN PLANK NR 30R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 24R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 31L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 33L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER CENTER SKIN PLANK NR 21L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 27L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB RT UPPER AFT SKIN PLANK NR 32R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 18R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82953.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER AFT SKIN PLANK NR 35L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82941.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB RT UPPER CENTER SKIN PLANK NR 28R BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82942.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 11L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939.

Part: SPAR CAP — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT FWD SPAR CAP NR 1L BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR - 1-5510-7-5000 HAS BEEN COMPLIED WITH.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER CENTER SKIN PLANK NR 17L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB RT UPPER FWD SKIN PLANK NR 10R BARREL NUT BORE FOUND EXCEEDED LIMITS. REWORK/REPAIR 1-5510-7-5000 HAS BEEN COMPLIED WITH.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 7L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK RBL 107 CORRODED AT STA 435. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 13L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 5L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA 1-5510-82939.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HORIZ STAB LT UPPER FWD SKIN PLANK NR 9L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82939.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,528 hrs · 7,688 cycles

CTR CARGO, DOOR ENTRANCE AFT AREA STA 1781 RT MOST OUTBD END LATERAL FLOORBEAM UPPER CAP FOUND CRACK. CARRIED OUT REPAIR IAW FEDEX EA 1-5310-83087.

Part: SKIN — CORRODED (ZONE 300) · airframe 33,528 hrs · 7,688 cycles

CORROSION REMOVED ON HOR STAB LT UPPER CENTER SKIN PLANK NR 15L BARREL NUT BORE FOUND EXCEEDED LIMITS. REPAIRED IAW FEDEX EA 1-5510-82940.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK RBL 47.5 CORRODED AT STA 1401. CARRIED OUT REPAIR IAW SRM 53-70-00 VOLUME I FIGURE 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK RBL 47.5 CORRODED AT STA 1885. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK RBL 27.5 FOUND WITH SCRATCHES AT STA 758. CARRIED OUT REPAIR IAW SRM 53-70-00 FIGURE 1 VOLUME I.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK 47.5 CORRODED AT STA 1661 TO STA 1751. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK 47.5 FOUND CORRODED AT STA 1605. CARRIED OUT REPAIR IAW SRM 53-70-00 VOLUME I FIGURE 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK LBL 107 CORRODED AT STA. REMOVED AND REPLACED AS IAW SRM 51-33-01 VOLUME II.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK LBL 47.5 FOUND WITH SCRATCHES AT STA 936. CARRIED OUT REPAIR IAW SRM 53-70-00 FIGURE 1 VOLUME I.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK AT 47.5 CORRODED AT STA 1581. CARRIED OUT REPAIR IAW SRM 53-70-00 VOLUME I FIGURE 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK RBL 27.5 CORRODED AT STA 1691. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK LBL 75 CORRODED AT STA 1608. FOUND WITHIN LIMIT AS PER SRM 53-70-00 VOLUME I FIGURE 3. REWORKED AREA PROTECTED AND PAINTED AS PER SRM 51-21-01 VOLUME II.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 33,528 hrs · 7,688 cycles

CAC - LONGERON SPLICE 51L, FOUND CRACKED AT STA 6-80. REMOVED AS PER SRM 51-33-01 VOL II. FABRICATED IAW DRAWING NR AAA7088. FABRICATED PART INSTALLED IAW SRM 51-33-01 VOL II AND FEDEX EA 1-5310-83095.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 33,528 hrs · 7,688 cycles

MAIN DECK, SEAT TRACK 47.5 CORRODED AT STA 1531. CARRIED OUT REPAIR IAW SRM 53-70-00 VOLUME I FIGURE 1.

Part: RIB — CRACKED (ZONE 500) · airframe 33,528 hrs · 7,688 cycles

LT WING NR 16 SLAT TRACK INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED WITH NEW RIB IAW SRM 51-33-01 VOLUME II.

Part: RIB — CRACKED (ZONE 600) · airframe 33,528 hrs · 7,688 cycles

RT WING NR 16 SLAT TRACK INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED WITH NEW RIB AS PER SRM 51-33-01 VOLUME II.

Part: INDICATOR — MALFUNCTIONED (FUEL QTY) · airframe 29,244 hrs · 6,659 cycles

NR 3 FUEL QTY INDICATOR FAILED INFLIGHT. RETURN TO HKG. DUMPED 50000 LBS OF FUEL, INDICATOR RETURN TO NORMAL. MEL 28-01-01-02: TANK NR 3 FUEL TANK SYNOPTIC QTY DISPLAY INOP. FUEL TO KNOWN QTY, AND AFTER REFUELING, VERIFY TANK NR 3 QTY WITH FUEL LEVEL STICKS AND RECORD IN THE AML/EAML. OPERATE FSC IN MANUAL. OPS NOT AUTHORIZED ABOVE 78 N LAT. TAIL FUEL MGMT, INOP.

Part: BLOCK — CORRODED (LANDING GEAR) · airframe 24,673 hrs · 5,569 cycles

CENTER LANDING GEAR RIGHT PILLOW BLOCK FOUND CORRODED. REMOVED AND REPLACED CTR LANDING GEAR PER CMM 32-1501.

Part: BLOCK — CORRODED (LANDING GEAR) · airframe 24,673 hrs · 5,569 cycles

CENTER LANDING GEAR LT PILLOW BLOCK FOUND CORRODED. REMOVED AND REPLACED PILLOW BLOCK PER CMM 32-15-01.

Part: BOLT — CORRODED (RT MLG) · airframe 24,673 hrs · 5,569 cycles

RIGHT TRUNNION MOUNTING BOLTS FOUND EMITTING RUST. REMOVED AND REPLACED BOLTS PER MM.

Part: BOLT — CORRODED (LANDING GEAR) · airframe 24,673 hrs · 5,569 cycles

TRUNNION MOUNTING LT BOLTS FOUND EMITTING WITH RUST. R&R BOLTS PER MM 32-15-01.

Part: RELAY — FAILED (COCKPIT) · airframe 23,913 hrs · 5,395 cycles

ON APPROACH PRIMARY & SECONDARY GEAR IND UNSAFE (RED). REMOVED AND REPLACED GEAR HANDLE INTERLOCK RELAY-3 FOR PRIMARY GEAR POS IND SYS PER MM 32-31-00. RESET ALTERNATE GEAR EXTENSION LEVER PER MM 32-32-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,179 hrs · 4,759 cycles

LT FRAME AT BS 1621 STR 12 FOUND 3 INCH CRACK. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-30-30 FIG 1 VOL 1.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,179 hrs · 4,759 cycles

LT FRAME AT BS 1761, STR 12 FOUND WITH 4.25 INCH CRACK. *S/D* REMOVED AND REPLACED FRAME PER SRM 53-30-00 FIG 3 VOL 1.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 20,991 hrs · 4,712 cycles

TAXI OUT RT OUTBOARD FLAP SHOW AMBER X NO GREEN BOX DURING FLT CONTROL CK FOR RT SPOILER. AFTER FLAP RETRACTION, RT FLAP IND SHOW 0 AND AN AMBER X.

Part: CONTROL CABLE — DISCONNECTED (LT FLAP FAIRING) · airframe 20,990 hrs · 4,712 cycles

DURING WALKAROUND, FOUND CABLE HANGING FROM LEFT INBD FLAP FAIRING.

Part: TURBINE — DAMAGED (NR 1 ENGINE) · airframe 19,370 hrs · 4,344 cycles

ON T/O, NR 1 ENG HAD SEVERE VIBRATION AND EVM TURBINE INDICATIONS. NO REDUCTION WITH REDUCED POWER, SECURED NR 1 ENGINE AND RETURNED TO PEK. MX FOUND METAL IN TAILPIPE AND LAST STAGE TURBINE SEVERELY DAMAGED. *S/D* REMOVED AND REPLACED NR 1 ENG PER WORK CARD MD11 71T07 C1. COWLING OPEN AND CLOSE PERF PER MM 7-13-00.

Part: IGNITER — FAILED (NR 1 ENGINE)

NR 1 ENG FLAMED OUT WHILE DESCENDING. RPM LO ALERT IGN OVERRIDE WAS ON AT TIME OF FLAME-OUT. REMOVED AND REPLACED A SYS IGN BOX AND FUEL FILTER PRECAUTIONARY PER MM 74-10-01 AND MM 73-11-02.

Part: GENERATOR — FAILED (ADG)

AFT T/O AT APPROX 500 FT ADG DEPLOYED. RETURNED TO HKG. NORMAL LANDING. ADJUSTED AIR DRIVEN GENERATOR, ADG DEPLOY AND STOW OK.

Part: GENERATOR — DEPLOYED (AIR DRIVEN)

UPON ARRIVAL FOUND ADG DEPLOYED. STOWED THE AIR DRIVEN GENERATOR AS PER MM 24-25-01-2. ACFT OK FOR SERVICE.

Part: GENERATOR — WILL NOT TEST (ADG) · airframe 17,479 hrs · 3,924 cycles

AIR DRIVEN GENERATOR WOULD NOT DEPLOY DURING TEST FLIGHT. *S/D* REMOVED AND REPLACED ROLLER PER CMM 24-27-06. ADG DEPLOY AND STOW FUNCTIONAL CK PER MM 24-25-01-02 FOUND SATISFACTORY.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 17,479 hrs · 3,924 cycles

CORROSION FOUND AROUND FLOOR SUPPORT ALONG BS 415 LHS JUST AFT OF COURIER SEAT AREA AS MARKED. REMOVED AND REPLACED, FAB AND INSTALLED PER EA 1-5320-52065, FUSELAGE - AUXILIARY STRUCTURE - SUPPORT REPAIR.

Part: ACTUATOR — DISLODGED (RUDDER) · airframe 17,497 hrs · 3,924 cycles

VERTICAL STAB LWR RUDDER ACTUATOR UPPER ATTACHMENT BLOCK ASSY FOUND BUSHING, WASHER RETAINER AND ATTACHMENT BOLT FOUND DISLODGED. *S/D* REMOVED AND REPLACED PARTS PER AMM 20-50-02.

Part: DUCT — CRACKED (BLEED AIR)

00-172- NR 2 ENGINE FIRE LIGHT & HORN CAME ON. DUMPED FUEL TO 60,000 LBS. & LANDED. FIRE LIGHT WENT OUT AFTER THROTTLE WAS PULLED TO IDLE. R&R BLOWN & CRACKED DUCTING PER JRH 4,5,6,7 DPM 112721. NR 2 EVM OPS NORMAL NO OTHER DEFECTS NOTED.

Part: TRANSMITTER — FAILED (NR 1 ENGINE)

99-279 - DURING CLIMB, NR 1 ENG OIL PRESS DROPPED TO 0. REMOVED AND REPLACED NR 1 ENG OIL PRESS TRANSMITTER PER MM 79-33-01-4. OPS CK SATISFACTORY.

Part: FLOORBEAM — CRACKED (BS 939)

FWD CARGO DOOR ENTRY MID UPPER FLOORBEAM LWR CHORD AT BS 939, X=78.0, RHS FOUND WITH ABOUT ONE-INCH CRACK AND DENT. *S/D* CARRIED OUT REPAIR ON FWD CARGO DOOR IN ACCORDANCE WITH FEDEX AUTH NR 1-5310-42383.

Part: TRANSMITTER — INOP (LT TE FLAP)

FLAP DISAGREE ALERT, LEFT FLAP SHOW 20 DEG, RT FLAP SHOW 25 DEG. ACCOMP FLAP 25 LAND AT PANC FLAP HANDLE REMAIN AT T/O. REMOVED AND REPLACED LT O/B FLAP POS TRANSMITTER AS PER MM 27-54-02-4 IND SAT AS PER ADJ TEST.

Part: PROX SWITCH — FAILED (CENTER MLG)

AFTER TAKEOFF, WE GOT AN UNSAFE CENTER GEAR ON CONFIG PAGE. RECYCLED GEAR UNSAFE UP AND DOWN CENTER GEAR ON CONFIG PAGE. SAFE UP AND DOWN ON GEAR LIGHTS. RETURNED TO NRT DUE ATC UNABLE 240 TO 250 FOR SPEED POSITION. PERFORMED BITE TEST ON PROXIMITY SWITCH ELECTRONIC UNIT. FOUND CENTER LOCKED SENSOR NO GOOD (D1-84). REMOVED AND REPLACED CENTER GEAR PROXIMITY SWITCH AND CHECKED PER M/M 32-31-16, OPS CHECKED GOOD.