N608FE

Part: SEAT TRACK — BROKEN (BS 625-652) · airframe 88,532 hrs · 21,692 cycles

DURING OFFLOAD FOUND MAIN CARGO LOCK M532 AT 2L HAS BROKEN LOBE IN SEAT TRACK, NO FURTHER DAMAGE. DSCRP IS PUT IN WORK REMOVE & REPLACED WORN SEAT TRACK SECTION USING MD11 SRM 53-00-52-2R

Part: BATTERY PACK — WARNING MESSAGE (EMERGENCY LIGHTS) · airframe 88,451 hrs · 21,669 cycles

EMER LT. BAT 1 LO ALERT ON. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY. ALL TEST PASSED AND ALERT WENT AWAY

Part: RETAINER — DAMAGED (PTT SWITCH) · airframe 87,984 hrs · 21,540 cycles

DURING PREFLIGHT, L1 LIGHT TEST FAIL. LIGHT RECEPTACLE FAILED. L1 EVAC SLIDE REMOTE PRESSURE INDICATOR INOP. PER MEL 25-61-02, VERIFYAND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY. RELEASED FOR SERVICE PER MEL : 25-61-02. T/S FOUND L1 PTT SWITCH LENS AND LAMP RETAINER INOP, R & R L1 LENS AND LAMP RETAINER IAW AMM 25-61-04-4.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 87,503 hrs · 21,427 cycles

CENTER CARGO COMPARTMENT - FLOORBEAM AT STATION 1741, BETWEEN X=-6.5 AND X= 6.5 FOUND CRACK. REPAIR CARRIED OUT ON CRACK FLOOR BEAM AT CENTER CARGO COMPARTMENT STATION 1741, BETWEEN X=-6.5 AND X= 6.5 AS PER EA NUMBER 1-5321-T0359449 PART 1 TITLE: FUSELAGE - CARGO COMP FLOORS - LOWER CENTER CARGO FLOOR BEAM REPAIR, STA1741, BETWEEN X = -15 AND X = 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 87,503 hrs · 21,427 cycles

FORWARD CARGO COMPARTMENT - STATION 1119 TO STATION 6-10, LONGERON 45 LEFT FOUND WITH CORROSION. CORRODED LONGERON AT FORWARD CARGO COMPARTMENT BETWEEN STATION 1119 TO STATION 6-10, LONGERON 45 LEFT REPAIRED AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 202 BY LONGERON SPLICE REPAIR BETWEEN STATION 6-5 TO STATION 6-20 LONGERON 45 LEFT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DUPLICATED SDR RAISED, REFER TO SDR #21- 0169 FOR WORK DETAILS.

Part: HINGE — WORN (UPPER CARGO DOOR) · airframe 87,503 hrs · 21,427 cycles

UPPER CARGO DOOR, FOUND FUSELAGE SIDE HINGE NUMBER 2 PART NUMBER ACA 7223-511 WITH 15 LOBES WORN. WORN 15 LOBES AT UPPER CARGO DOOR, FUSELAGE SIDE HINGE NUMBER 2 PART NUMBER ACA 7223-511 REWORKED AND FOUND NUMBER 14 AND NUMBER 15 COUNTING FROM FORWARD EXCEED LIMIT AND NUMBER 1 TO NUMBER 13 FOUND WITHIN LIMIT AS PER MD-11 SRM 53-30-16-1A FIGURE 101 SHEET 3. OVERSIZED REPAIR BUSHINGS 15 EACH FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 52-34-04 REPAIR- GENERAL, PARAGRAPH 2.Y AND EA # 1-5310-T0359333 PART 1 STEPS 2 AND 5. TITLE: FUSELAGE- MAINFRAME- UPPER CARGO DOOR JAMB- 2ND MOST FWD HINGE ( FUSELAGE SIDE ) - HINGE LOBE BORES FOUND WORN. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON — CRACKED (NLG WW) · airframe 87,503 hrs · 21,427 cycles

WHILE ACCOMPLISHING NOSE LEADING GEAR RIGHT HAND TRUNNION FITTING REPAIR FOUND LONGERON 49 RIGHT HAND CRACKED. NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING AT STATION 595 LONGERON 49 RIGHT HAND CRACKED LONGERON REMOVED AND REPLACED WITH FABRICATED LONGERON AS PER SRM 51-35-01-0G. LONGERON FABRICATED AS PER DOUGLAS DRAWING ACA 3796 REV A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 87,503 hrs · 21,427 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE FITTING BORE FOUND WITH CORROSION CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE FITTING BORE (PIVOT HOLE #3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44- 07 AND EA # 1-5750-73360 G PART 5 STEPS 1.F (1) AND (3). TITLE: WINGS- FLIGHT SURFACES- RH RH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 87,503 hrs · 21,427 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE FITTING BORE INBOARD FACE FOUND WITH CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE FITTING BORE INBOARD FACE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 87,503 hrs · 21,427 cycles

LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE FITTING BORE FOUND WITH CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE FITTING BORE ( (PIVOT HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND EA # 1-5750-T0328840 F PART 3 STEP 1.F. TITLE: WINGS- FLIGHT SURFACES- LH WING- INBD FLAP- OUTBD FWD HINGE (WING SIDE) REPAIR- PSE 57.55.01.1 INSPECTION- ALTERNATE ALTERNATE METHOD. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 87,503 hrs · 21,427 cycles

RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE FITTING BORE INBOARD FACE FOUND WITH CORROSION CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD FORWARD HINGE FITTING PIVOT PIVOT BORE INBOARD FACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 07. REPAIR EVALUATED AND FOUND DATA FOR THE PIVOT BORE REMAINING THICKNESS SHOWN IN FIGURE 2 IS CORRECT AS PER EA # 1-5750-73360 G PART 5 STEPS 1.E. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (FWD CARGO) · corrosion level 2 · airframe 87,503 hrs · 21,427 cycles

FORWARD CARGO COMPARTMENT - STATION 1119 TO STATION 6-10, LONGERON 45 LEFT LONGERON FOUND WITH CORROSION. CORRODED LONGERON AT FORWARD CARGO COMPARTMENT BETWEEN STATION 1119 TO STATION 6-10 LONGERON 45 LEFT REPAIRED AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 202 BY BY LONGERON SPLICE REPAIR BETWEEN STATION 6-5 TO STATION 6-20 LONGERON 45 LEFT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (CENTER CARGO) · airframe 87,503 hrs · 21,427 cycles

CENTER CARGO COMPARTMENT - STATION 5-113 TO STATION 5-123, LONGERON 44 LEFT LONGERON SPLICE FOUND CRACK. CENTER CARGO COMPARTMENT STATION 5-113 TO STATION 5-123, LONGERON 44 LEFT CRACK LONGERON SPLICE REMOVED AND REPLACED PER SRM 51-31-01-0G. LONGERON SPLICE FABRICATED PER DOUGLAS DRAWING A5A7116 REVISION D. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (MAIN DECK CARGO) · airframe 87,503 hrs · 21,427 cycles

MAIN DECK CARGO COMPARTMENT - CABIN , FOUND SEAT TRACK AT STATION 1421 , X = 47.5 CROWN WORN . MAIN DECK CARGO COMPARTMENT - CABIN AT SEAT TRACK STATION1421 , X = 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1431 TO EXISTING SPLICE STATION 1391 , X = 47.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — WORN (MAIN DECK CARGO) · airframe 87,503 hrs · 21,427 cycles

MAIN DECK CARGO COMPARTMENT - CABIN , FOUND SEAT TRACK AT STATION 1421 , X = 8.5 CROWN WORN . MAIN DECK CARGO COMPARTMENT - CABIN , AT SEAT TRACK STATION 1421 , X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1391 TO STATION 1431 X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SEAT TRACK — CRACKED (MAIN DECK CARGO) · airframe 87,503 hrs · 21,427 cycles

MAIN DECK CARGO COMPARTMENT - CABIN , FOUND SEAT TRACK CRACKED AT STATION 635 , X = 8.5 . MAIN DECK CARGO COMPARTMENT - CABIN , CRACKED SEAT TRACK AT STATION 635 X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 625 TO STATION 685 , X = 8.5 AS PER SRM 53-00-52-2R REPAIR 1 FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 .

Part: SUPPORT — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 87,503 hrs · 21,427 cycles

CABIN - FLOOR SUPPORT FROM STATION 1921 TO STATION 1941 , X = 56 FOUND WITH CORROSION ON THE UNDER SIDE . CABIN - AT FLOOR SUPPORT STATION 1921 TO STATION 1941 , X = 56 CORROSION ON THE UNDER SIDE EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 ALLOWABLE DAMAGE . CORRODED FLOOR SUPPORT REMOVED AND REPLACED AT AT STATION 1887 TO STATION 2007 X = 56 AS PER SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED FABRICATED BY MACHINING AS PER DOUGLAS DRAWING AGA7551 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 87,503 hrs · 21,427 cycles

LEFT HAND WING LEADING EDGE AT STATION XOS 881 FOUND BEADED DOUBLER CRACK LEFT HAND WING LEADING EDGE AT STATION XOS 881 DOUBLER REPAIR CARRIED OUT AS PER PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 87,503 hrs · 21,427 cycles

AGING AIRCRAFT - EXISTING REPAIR FOUND AT NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING STATION 583 LONGERON 49 RIGHT HAND EXISTING REPAIR AT NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING STATION 583 LONGERON 49 RIGHT HAND EVALUATED AND FOUND CRACK PROPAGATED FROM EXISTING TRIMMED OUT APPROXIMATELY 0.350". REPAIR CARRIED OUT AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202. INITIAL INSPECTION TO BE CARRIED OUT AT 1500 FLIGHT CYCLES AFTER REPAIR EMBODIMENT AND REPETITIVE INSPECTION TO BE CARRIED OUT EVERY 1500 FLIGHT CYCLES BY HIGH FREQUENCY EDDY CURRENT OR LIQUID PENETRANT INSPECTION AS PER SRM 53-10-14-2R REPAIR 2 FIGURE 202 / REPAIR 2 TABLE 201. EO 1-5100-7-5001 B6 PART 1 TITLE: STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS REQUIREMENTS 14 CFR 121.707 ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 100.

Part: LIGHT — NO TEST (CABIN) · airframe 85,545 hrs · 20,925 cycles

EMERENCY LIGHTS TEST WAS INOPERATIVE DURING PREFLIGHT. PERFORMED ADJUSTMENT AND TEST IAW MM 33-50-00-5. OPS CHECKED GOOD. ACFT OK TO CONTINUE.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 83,445 hrs · 20,285 cycles

CTR CARGO PIT FLOORBEAM UPPER AFT FLANGE DAMAGED AT STA. 1701 APPROX. X=30.000. REPAIRED PER E.A. 1-5310-T0347878. INSTALLED SPLICE/REPAIR TO FLOORBEAM AT STA 1701 LOWER CARGO FLOOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 83,277 hrs · 20,222 cycles

MDIS 608 53-30 8313 05MAY19 MEM OPEN U FOUND RIVETS PULLING THRU THE SKIN ON THE AFT RT SIDE OF FUSELAGE, APPROX 18 INCHES BELOW THE AFT CARGO DOOR FRAME, FROM CENTER OF DOOR FRAME GOING AFT. MARKED WITH GREEN TAPE. BETWEEN STA. 1721 AND STA. 1781 PER SRM 53-00-00-0G. SHGN 05MAY19 23:00 MEM U LONGERON 47R BETWEEN FR STA 1701 AND 1781 HAS INTERGRANULAR CORROSION. AFTER AREA IS OPENED UP WILL BE ABLE TO EVALUATE ANY OTHER STRUCTURE INVOLVED. FACT 16MAY19 20:23 MEM REPLACED DAMAGED LONGERON (L46R), AND REPAIRED SKIN CUTOUT TO FACILITATE LONGERON REPLACEMENT, REF FUSELAGE 46R- FUSELAGE SKIN REPAIR AT STATION 1787-1818/ L46R AFTER INSTALLATION OF NEW L46R EA 1-5310-T0346861 PARTS 1, 2 AND 3.

Part: SKIN — CHAFED (RT WING) · airframe 82,861 hrs · 20,106 cycles

RIGHT HAND WING DROOP LEADING EDGE INBOARD EDGE FOUND WITH CHAFING AT XDLE 309. REPAIR CARRIED OUT ON RIGHT HAND WING DROOP LEADING EDGE INBOARD EDGE AT XDLE 309 AS PER SRM 57-40-01-2R FIGURE 202 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: FORMER — CRACKED (RT WING) · airframe 82,861 hrs · 20,106 cycles

RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT FORMER AT APPROXIMATELY STATION XIS 237 FOUND CRACK. FORMER ON RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XIS 237. REMOVED AND REPLACED AS PER AMM 20-50-02. FORMER FABRICATED AS PER DWG ARB 3006 REV G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN PANEL — CRACKED (VERTICAL STAB) · airframe 82,861 hrs · 20,106 cycles

EMPENNAGE : UPON REMOVAL VERTICAL STABILIZER RIGHT HAND LOWER SKIN PANEL AT PYLON THROUGH REAR CENTER TO REAR SPAR STATION 2164 FOUND CRACK. VERTICAL STABILIZER RIGHT HAND LOWER SKIN PANEL AT PYLON THROUGH REAR CENTER TO REAR SPAR STATION 2164 SKIN PANEL CRACKED REPAIR CARRIED OUT AS PER ENGINEERING AUTHORIZATION 1-5530-T0345324 PART 2 TITLE : STABILIZERS - VERTICAL STABILIZER - CRACK REPAIRS ON LT & RT LOWER SKIN PANELS, PYLON CARRY THROUGH REAR CENTER TO REAR SPAR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: INTERCOSTAL — CRACKED (VERTICAL STAB) · airframe 82,861 hrs · 20,106 cycles

EMPENNAGE : UPON REMOVAL VERTICAL STABILIZER RIGHT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL STATION 2164 FOUND CRACK ON AFT END. VERTICAL STABILIZER RIGHT HAND CENTER SPAR TO REAR SPAR INTERCOSTAL AT STATION 2164 CRACK ON AFT END REPAIR CARRIED OUT AS PER ENGINEERING AUTHORIZATION 1-5530- T0345381 PART 1 TITLE : STABILIZERS - VERTICAL STABILIZER - REAR CENTER SPAR TO REAR SPAR - LOWER PANEL - CRACK DAMAGE FOUND ON RT INTERCOSTAL. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN PANEL — CRACKED (VERTICAL STAB) · airframe 82,861 hrs · 20,106 cycles

EMPENNAGE : UPON REMOVAL VERTICAL STABILIZER LEFT HAND LOWER SKIN PANEL AT PYLON THROUGH REAR CENTER TO REAR SPAR STATION 2164 FOUND CRACK. VERTICAL STABILIZER LEFT HAND LOWER SKIN PANEL AT PYLON THROUGH REAR CENTER TO REAR SPAR STATION 2164 SKIN PANEL CRACKED REPAIR CARRIED OUT AS PER ENGINEERING AUTHORIZATION 1-5530-T0345324 PART 1 TITLE : STABILIZERS - VERTICAL STABILIZER - CRACK REPAIRS ON LT & RT LOWER SKIN PANELS, PYLON CARRY THROUGH REAR CENTER TO REAR SPAR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 82,861 hrs · 20,106 cycles

CABIN, MAIN DECK CARGO COMPARTMENT LEFT 3 DOOR AFT LOWER FUSELAGE JAMB WEB CRACKED AT LEFT HAND STATION 1310 BETWEEN LONGERON 26L-27L. REPAIRED AS PER SRM 53-40-15-2R FIGURE 201 REPAIR 3 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1310) · airframe 82,861 hrs · 20,106 cycles

CABIN, MAIN DECK CARGO COMPARTMENT RIGHT 3 DOOR AFT LOWER FUSELAGE JAMB WEB CRACKED AT RIGHT STATION 1310 BETWEEN LONGERON 26R-27R. CARRIED OUT REPAIR AS PER SRM 53-40-15-2R FIGURE 201 REPAIR 3 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

CABIN - MAIN DECK CARGO COMPARTMENT R4 DOOR PLUG LOWER CUT - OUT FOUND CORROSION AT RIGHT HAND STATION 1875 CABIN - MAIN DECK CARGO COMPARTMENT RIGHT 4 DOOR PLUG LOWER CUT OUT CORROSION AT RIGHT HAND STATION 1875 REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202 REPAIR GENERAL. CABIIN RGHT 4 DOOR PLUG CUT OUT CARRIED OUT REPAIR AS PER EA # 1-5310-T0345359 PART 1 TITLE : " FUSELAGE - MAINFRAME - R4 DOOR LOWER JAMB TREADWAY LONGERON , P/N AGA 3942-12 CORROSION REPAIR." REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1781-1801) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSIONS AT STATION 1781- 1801, X = -75.25. CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSION REMOVED AT SEAT TRACK STATION 1781 AND 1801 X = -75.25 AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52- 1A FIGURE 101 ALLOWABLE DAMAGE 1 .SEAT TRACK REPAIR CARRIED OUT FROM STATION 1711 TO 1887 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 1841-1853) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSIONS AT STATION 1841-1853 , X= -75.25. CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSION AT STATION 1841 -1853 X = -75.25 REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 .SEAT TRACK REPAIR CARRIED OUT FROM STATION 1711 TO 1887 X = - 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.REFER TO SNRM # N00840 FOR REPAIR DETAILS .

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 82,861 hrs · 20,106 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT FORWARD RADIUS OF LOWER VERTICAL CAP UPPER FORWARD LEFT HAND RADIUS STATION 2164 AND FOUND CRACK INDICATION LEFT HAND SIDE LOWER VERTICAL STABILIZER REAR SPAR UPPER CAP FORWARD FLANGE STATION 2164 CRACKED AREA TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAIR 5. REPAIR CARRIED OUT AS PER SRM 55-30-02-2R FIGURE 202 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT 5400 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2700 FLIGHT CYCLES AS PER SRM 55-30-02-2R TABLE 203 FIGURE 202 REPAIR 5. METHOD OF INSPECTION BY HIGH FREQUENCY EDDY CURRENT AND ULTRASONIC PER SN10550000.

Part: BULKHEAD WEB — PUNCTURED (BS 1841) · airframe 82,861 hrs · 20,106 cycles

LOWER CENTER CARGO COMPARTMENT , FLOOR AFT BULKHEAD LEFT HAND SIDE FOUND WEB WITH PUNCTURED AT STATION 1841 X = 50 LOWER CENTER CARGO COMPARTMENT , FLOOR AFT BULKHEAD LEFT HAND SIDE WEB WITH PUNCTURED AT STATION 1841 X = 50 REPAIRED AS PER SRM 53-00-00-2R FIGURE 211 REPAIR GENERAL . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 82,861 hrs · 20,106 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT FORWARD SIDE RADIUS OF LOWER VERTICAL STABILIZER REAR SPAR UPPER CAP STATION 2164 , AND FOUND 01 EACH CRACK INDICATION AT RIGHT HAND SIDE RADIUS RIGHT HAND SIDE LOWER VERTICAL STABILIZER REAR SPAR UPPER CAP FORWARD FLANGE STATION 2164 CRACKED AREA TRIMMED AS PER SRM 55-30-02-2R FIGURE 201 REPAIR 5. REPAIR CARRIED OUT AS PER SRM 55-30-02-2R FIGURE 202 REPAIR 5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. TO CARRY OUT INITIAL INSPECTION AT 5400 FLIGHT CYCLES AND REPETITIVE INSPECTION AT EVERY 2700 FLIGHT CYCLES AS PER SRM 55-30-02-2R TABLE 203 FIGURE 202 REPAIR 5. METHOD OF INSPECTION BY HIGH FREQUENCY EDDY CURRENT AND ULTRASONIC PER SN10550000.

Part: SEAT TRACK — CORRODED (BS 1561-1651) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSIONS AT STATION 1561- 1651, X= 8.5 CABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORROSIONS AT STATION 1561 - STATION1651 X = 8.5 REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 FROM STATION 1561 AND STATION 1641 X= 8.5. SEAT TRACK REPAIR CARRIED OUT FROM STATION 1531 TO STATION 1651 X = 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 82,861 hrs · 20,106 cycles

LOWER CENTER CARGO COMPARTMENT LONGERON 43 RIGHT SPLICE FITTING FOUND CRACKED BETWEEN STATION 5-113 - 1541 LOWER CENTER CARGO COMPARTMENT LONGERON 43 RIGHT SPLICE FITTIING CRACKED BETWEEN STATION 5-133 - 1541 REMOVED AS PER SRM 51-33-01-0G. NEW LONGERON SPLICE FITTING FABRICATED BY MACHINING AS PER DOUGLAS DRAWING A5A 7114 REVISION E AND INSTALLED AS PER SRM 51-33-01-0G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (BS 1581) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

LOWER CENTER CARGO BILGE AREA LONGERON 49 LEFT FOUND WITH CORROSION STATION 1581 LOWER CENTER CARGO BILGE AREA LONGERON 49 LEFT AT STATION 1581 CARRIED OUT REPAIR AS PER ENGINEERING AUTHORIZATION # 1-5310-T0345415 PART 1 .TITLE : " FUSELAGE - MAINFRAME -EXFOLIATION CORROSION LONGERON 49 L AT STA 1581 - CORROSION REPAIR ." REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING LE) · airframe 82,861 hrs · 20,106 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING FIXED LEADING EDGE SKIN , CORNER # 11 - FUEL ACCESS DOOR FORWARD INBOARD CORNER , FOUND 01 EACH CRACK APPROXIMATE 0.250 INCH LENGTH REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING EDGE SKIN CORNER #11 - FUEL ACCESS DOOR FORWARD INBOARD CORNER AT APPROXIMATELY STA XOS 610.8 AS PER SRM 57- 40-01-2R FIG 201 REPAIR 18. TO CARRY OUT INITIAL INSPECTION AT NEXT "C" CHECK NOT EXCEEDING 24 MONTHS AND REPETITIVE INSPECTION AT EVERY "C" CHECK NOT EXCEEDING 24 MONTHS. INSPECTION METHOD: VISUAL AS PER SRM 57-40-01-2R TABLE 204 REPAIR 18. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 82,861 hrs · 20,106 cycles

LOWER CENTER CARGO COMPARTMENT LONGERON 30 LEFT SPLICE FITTING FOUND CRACKED BETWEEN STATION 5-113 - 1541 LOWER CENTER CARGO COMPARTMENT LONGERON 35 LEFT SPLICE FITTING CRACKED BETWEEN STATION 5-113 - 1541 REMOVED AS PER SRM 51-33-01-0G. NEW LONGERON SPLICE FITTING FABRICATED BY MACHINING AS PER DOUGLAS DRAWING A5A 7114 REVISION E AND INSTALLED A S PER SRM 51-33-01-0G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 82,861 hrs · 20,106 cycles

LOWER CENTER CARGO COMPARTMENT LONGERON 30 RIGHT SPLICE FITTING FOUND CRACKED BETWEEN STATION 5-113 - 1541 LOWER CENTER CARGO COMPARTMENT LONGERON 30 RIGHT SPLICE FITTING CRACKED BETWEEN STATION 5-113 - 1541 REMOVED AS PER SRM 51-33-01-0G. NEW LONGERON SPLICE FITTING FABRICATED BY MACHINING AS PER DOUGLAS DRAWING A5A 7112 REVISION E AND INSTALLED AS PER 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 82,861 hrs · 20,106 cycles

LOWER CENTER CARGO COMPARTMENT LONGERON 38 LEFT SPLICE FITTING FOUND CRACKED BETWEEN STATION 5-113 - 1541 LOWER CENTER CARGO COMPARTMENT LONGERON 38 LEFT SPLICE FITTING CRACKED BETWEEN STATION 5-113 - 1541 REMOVED AS PER SRM 51-33-01-0G . NEW LONGERON SPLICE FITTING FABRICATED BY MACHINING AS PER DOUGLAS DRAWING A5A 7114 REVISION E AND INSTALLED AS PER SRM 51-33-01-0G . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1961-2007) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

MAIN DECK COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORROSION AT BETWEEN 1961 - 2007 X = 107 MAIN DECK COMPARTMENT FLOOR SEAT TRACK CORROSION BETWEEN STATION 1961-2007 X= 107 REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGED 1 AT STATION 1988. MATERIAL REMAINED : 0.013". SEAT TRACK REPAIR AT MAIN DECK FROM STATION 1751 TO STATION 2007 X = 107 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIG 201 REPAIR1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM # N00636 FOR REPAIR DETAILS.

Part: SEAT TRACK — CORRODED (BS 1801-1821) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

MAIN DECK COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORROSION BETWEEN STATION 1801 - 1821 X = 107 MAIN DECK COMPARTMENT FLOOR SEAT TRACK CORROSION BETWEEN STATION 1801 - 1821 X= 107 REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGED 1 AT STATION 1815. MATERIAL REMAINED : 0.025". SEAT TRACK REPAIR AT MAIN DECK FROM STATION 1751 TO STATION 2007 X = 107 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIG 201 REPAIR1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM # N00636 FOR REPAIR DETAILS.

Part: SEAT TRACK — CORRODED (BS 1771) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

MAIN DECK COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORROSION AT STATION 1771 X = 107 MAIN DECK COMPARTMENT FLOOR SEAT TRACK CORROSION AT STATION 1771 X= 107 REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGED 1. MATERIAL REMAINED : 0.012". SEAT TRACK REPAIR AT MAIN DECK FROM STATION 1751 TO STATION 2007 X = 107 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIG 201 REPAIR1 .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1667) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

MAIN DECK COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORROSION AT STATION 1667 X = - 107 MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK CORROSION AT STATION 1667 X = -107 REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT FROM STATION 1651 TO STATION 1791 X = -107 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 616 - 621 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,861 hrs · 20,106 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 879 - 883 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 879-883 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15.REPAIR CLASSFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,861 hrs · 20,106 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 728 - 734 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 728-734 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15.REPAIR CLASSFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 652 - 657 FOUND WITH CRACK REPAIR CARRIED OUT ON LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 652 - XOS 657 AS 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 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 685 - 691 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER 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 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 673 - 679 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER 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 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 541 - 546 FOUND WITH CRACK REPAIR CARRIED OUT ON LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 541 - XOS 546 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1965) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

MAIN DECK COMPARTMENT AFT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1965 X = - 56 MAIN DECK COMPARTMENT AFT FLOOR SUPPORT CORROSION AT STATION 1965 X = -56 REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 REPAIR GENERAL . REMAINED THCKNESS : 0.091" . NEW FLOOR SUPPORT FABRICATED AS PER DOUGLAS DRAWING # AGA 7551 REVISION G . DAMAGED FLOOR SUPPORT REMOVED AND REPLACED BY FABRICATED NEW SUPPORT AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,861 hrs · 20,106 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 753 - 759 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 753-759 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15.REPAIR CLASSFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,861 hrs · 20,106 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 610 - 616 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STA 610 - 616 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE NR 12 SLAT TRACK CUTOUT FOUND CRACKED AT APPROXIMATE XOS 776.8. REPAIR CARRIED OUT ON LEFT HAND WING LEADING EDGE #12 SLAT TRACK CUTOUT AT APPROXIMATELY STATION XOS 776.8 AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7 .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 767 - 772 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,861 hrs · 20,106 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 734 - 740 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 734-740 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15.REPAIR CLASSFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1290) · airframe 82,861 hrs · 20,106 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 1290, X = 8.5. MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 1290 X= 8.5 MEASURED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK FROM STATION 1250 TO STATION 1311 X= 8.5 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 705) · airframe 82,861 hrs · 20,106 cycles

CABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 705, X = 75.25. SEAT TRACK CROWN AREA DAMAMGED MEASURED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FOG 101 ALLOWABLE DAMAGE. SEAT TRACK CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIG 201 REPAIR 1 FROM STATION 685- 725 X= 75.25. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 554 - 558 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CHAFED (RT WING) · airframe 82,861 hrs · 20,106 cycles

RIGHT HAND WING LEADING EDGE INBOARD EDGE FOUND WITH CHAFFING AT APPROXIMATE XDLE 309.9. REPAIR CARRIED OUT ON RIGHT HAND WING DROOP LEADING EDGE INBOARD EDGE AT XDLE 309 AS PER SRM 57-40-01-2R FIGURE 202 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 747 - 752 FOUND WITH CRACK REPAIR CARRIED OUT ON LEFT AHND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STA XOS 747 - XOS 752 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJPR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 82,861 hrs · 20,106 cycles

LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 727 - 733 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1975) · corrosion level 2 · airframe 82,861 hrs · 20,106 cycles

MAIN DECK COMPARTMENT AFT FLOOR SUPPORT FOUND WITH CORROSION AT STATION 1975 X = 20 MAIN DECK COMPARTMENT AFT FLOOR SUPPORT CORROSION AT STATION 1975 X = 20 REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 206 REPAIR GENERAL . REMAINED THICKNESS : 0.063". NEW FLOOR SUPPORT FABRICATED AS PER DOUGLAS DRAWING # AGA 7087 REVISION M . DAMAGED FLOOR SUPPORT REMOVED AND REPLACED BY FABRICATED NEW FLOOR SUPPORT AS PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 82,861 hrs · 20,106 cycles

RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 647 - 652 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 647- 652 AS PER SRM 57-40-02-2R FIG 203 REPAIR 15.REPAIR CLASSFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 635) · airframe 82,861 hrs · 20,106 cycles

MAIN DECK COMPARTMENT SEAT TRACK FOUND CRACK AT STATION 635 X = - 8.5 MAIN DECK COMPARTMENT FLOOR SEAT TRACK CRACKED AT STATION 635 X = -8.5 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 FROM STATION 625 TO STATION 645 X = -8.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (BS 695) · airframe 82,861 hrs · 20,106 cycles

MAIN DECK COMPARTMENT FLOOR SEAT TRACK FOUND CRACK AT STATION 695 X = 27 MAIN DECK COMPARTMENT SEAT TRACK CARRIED OUT REPAIR FROM STATION 685- STATION 705 X = 27 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LIGHT — UNKNOWN (CABIN) · airframe 80,718 hrs · 19,453 cycles

EMERGENCY LIGHT SYSTEM INOPERATIVE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM, OPS CHECKED NORMAL IAW MM 33-51-01-5.

Part: BUSHING — LOOSE (HINGE) · airframe 79,968 hrs · 19,238 cycles

DURING A CURRENT B-CHECK, BUSHINGS WERE FOUND LOOSE. MX REPORTED LUG HOLE SIZES ARE THE SAME AS PREVIOUSLY REPORTED. COMPLIED WITH EA 1-5230-143587 REV C.

Part: AUTOBRAKE SYS — MALFUNCTIONED (MLG) · airframe 78,810 hrs · 18,922 cycles

DURING TAKE OFF ROLL, BRAKES BEGAN TO GRAB AND RUDDER PEDALS DISPLACED (LEFT RUDDER) AUTOBRAKES HAD BEEN DEFERRED DUE TO AUTOBRAKE FAIL. CYCLED BRAKE PEDALS NUMEROUS TIMES WITH NO DEFECTS NOTED WITH BRAKE APPLICATION. INSPECTED BRAKES WHILE CYCLING PEDALS ALL BRAKES APPLY & RELEASE NORMALLY. CYCLED RUDDER PEDALS NUMEROUS TIMES WITH NO DEFECTS NOTED. INSPECTED RUDDER DURING OPERATION, RUDDER MOVES & RETURNS TO NEUTRAL NORMALLY IAW MM 27-20-00-2 & SMP WRI 32-45/5650 FOR R&R OF AUTO BRAKE CONTROL UNIT. AIRCRAFT SET UP FOR HIGH SPEED TAXI TO CONFIRM POSITIVE FIX . AIRCRAFT OK FOR HIGH SPEED TAXI. SUCCESSFUL HIGH SPEED TAXI CHECK. NO GRABBING BRAKES OR UNCOMMANDED RUDDER DEFLECTION NOTED DURING TAXI CHECK. OK FOR SERVICE.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · airframe 77,619 hrs · 18,609 cycles

LEFT WING INBD FLAP FWD (WING SIDE) OTBD HINGE PIVOT HOLE BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07 AND PER EA 1-5750-T0328840 D, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · airframe 77,619 hrs · 18,609 cycles

RIGHT WING, INBD FLAP, FWD (WING SIDE) OTBD HINGE PIVOT HOLE BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07 AND EA 1-5750-73360 D, PART 3, STEP 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — DETACHED (LT WING) · airframe 77,619 hrs · 18,609 cycles

LEFT WING INBD TRAILING EDGE LOWER PANEL 541KB FOUND SKIN DETACHED. REPAIRED IAW SRM 51-71-00-0G, PARA 19, AND EA 1-5720-T0331275, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP INBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT BORE FOUND WITH CORROSION. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750- T0331077, PART 1, STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR OUTBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1C.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

LEFT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. TWO SHOULDER BUSHINGS AND REPAIR SHIMS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP 1A, AND STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR INBD HOLE SURFACE CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP AFT HINGE, FLAP SIDE, PIVOT OUTBD HOLE BORE FOUND CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132706 D, PART 4, STEP 2 & 3.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE SURFACE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1C.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE FOUND CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132706 D, PART 4, STEP 2 & 3.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

LEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1B.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1, AND STEP 1A.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT HAND WING OUTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE CORRODED. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1, AND STEP 1B.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE CORRODED. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1, AND STEP 1B.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

LEFT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP 1B.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1, AND STEP 1A.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1B.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

LEFT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP 1B.

Part: FRAME — CHAFED (BS 535) · airframe 77,619 hrs · 18,609 cycles

MAIN DECK CARGO BAY FRAME CHAFED AT LT BS 535, LONGERON 19L. REPAIRED IAW SRM 53-20-07-2R, FIG 202, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

LEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1B.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

LEFT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OUTBD HOLE BORE FOUND WITH CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-132705 C, PART 4, STEP 2A & 2C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP VANE NR 2 FITTING BUSHING HOLE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R FIG 201. A SLOT BUSHING WAS FABRICATED IAW EA 1-5750-T0331241, PART 1, STEP 2 AND INSTALLED IAW AMM 27-50-32-4.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1B.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

LEFT WING OTBD FLAP FWD INBD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1A.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

LEFT WING OTBD FLAP FWD INBD HINGE (WING SIDE) UPPER MOUNT OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1A.

Part: HINGE BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

LEFT WING INBD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBD HOLE BORE FOUND WITH CORROSION. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-132705 C, PART 4, STEP 2A & 2C. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE SURFACE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133 PART 1, STEP 1A.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

RIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1A.

Part: SKIN — CRACKED (RT WING) · airframe 77,619 hrs · 18,609 cycles

HFEC INSPECTION ON RT WING FIXED LEADING EDGE CORNER NR 5 SLAT ACTUATOR ACCESS DOOR. FOUND CRACKED AT XOS 490. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 17. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE) · airframe 77,619 hrs · 18,609 cycles

LEFT WING FIXED LEADING EDGE SLAT AT CORNER FOUND CRACKED XOS 490. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 17. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1540 - 1561) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

MAIN DECK CARGO BAY SEAT TRACK CORRODED AT BS 1540 - 1561, LBL 107.25. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

MAIN DECK CARGO SEAT TRACK FLANGE CORRODED AT BS 5-73 - 5-113, LBL 107.25. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

MAIN DECK CARGO SEAT TRACK FLANGE CORRODED AT BS 5-73 - 5-113, LBL 75.25. REPAIRED IAW SRM 53-00-52-2R FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1540-1561) · corrosion level 2 · airframe 77,619 hrs · 18,609 cycles

MAIN DECK CARGO SEAT TRACK FLANGE CORRODED AT BS 1540 - 1561, LBL 75.25. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,619 hrs · 18,609 cycles

RT WING LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 696. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,619 hrs · 18,609 cycles

RT WING LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 655. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. MAJOR REPAIR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 77,619 hrs · 18,609 cycles

RT WING LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 669. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 77,619 hrs · 18,609 cycles

CENTER CARGO LONGERON SPLICE FITTING CRACKED AT BS 5-113 TO 1541, LONGERON 33R. REMOVED AND INSTALLED WITH NEW FABRICATED SPLICE FITTING IAW SRM 51-33-01-0G. SPLICE FITTING FABRICATED AS PER DRAWING A5A7112 REVISION D. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,619 hrs · 18,609 cycles

LEFT WING LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 626. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.

Part: BRAKE DISC — FAILED (NR 7) · airframe 77,439 hrs · 18,554 cycles

NR 7 BRAKE INBD DISC DISINTERGRATING. REMOVED AND REPLACED THE BRAKE ASSY AND LEAK AND BLEED CHECKED OK IAW AMM 32-43-20-4-0.

Part: CONTROLLER — FAILED (COCKPIT) · airframe 77,370 hrs · 18,536 cycles

CAPT'S WINDSHIELD COMPLETELY COLD SOAKED AND APPEARS W/S HEAT INOP AND FOGGED OVER DURING DESCENT AND APPROACH. SEVERE FOGGING TO POINT OF CAPTS VISIBILITY SERIOUSLY REDUCED AND UNSAFE. REPLACED LT WINDSHIELD HEAT CONTROLLER PER AMM 30-41-01-4. OP CHK OK.

Part: WIRE — LOOSE (EXTINGUISHER) · airframe 77,325 hrs · 18,524 cycles

THE TWO AGT LOW LIGHTS DOES NOT ILLUMINATE IN THE COCKPIT. PERFORMED ENGINE FIRE TEST IAW AMM 26-11-02-5.TEST OK.DISCONECTED THE CONNECTORS FOR THE CARTRIDGES IAW AMM 26-21-05-4. INSPECTED THE DISCHARGE CATRIDGES, STILL GOOD, INSPECTED THE DISCHAGE LINES IAW AMM 26-21-01-4. CLEAN, NO DISCHARGE SIGNS NOTED. PERFORMED NR 1 ENG CONTAINER AGENT 1 & 2 .ELECTRICITY CONTINUITY TEST IAW AMM 26-21-01-5, TEST FAILED. FOUND ELECTRICAL WIRES LOOSE WHICH CONNECT TO THE ENGINE FIRE AGENT 1 AND 2 DISCHARGE SWITCHS, SECURED THE LOOSE WIRES IAW AMM 26-21-02-4, PERFORM CONTINUITY TEST IAW AMM 26-21-01- 5, TEST PASSED, RESET THE GENERATOR AUTO RESET IAW AMM 24-08-01-5, OPS TEST OF FIRE HANDLE GENERATOR FIELD DISC FUNCTION IAW AMM 24-20-00-5, TEST PASSED.

Part: ENGINE — FAILED (NR 1) · airframe 77,325 hrs · 18,524 cycles

NR 1 ENGINE FAILURE AFTER TAKEOFF. MULTIPLE COMPRESSOR STALLS AND LOSS OF POWER. RETURNED TO DEPARTURE. NO INDICATIONS OF FIRE OR EXTERNAL DAMAGE. PERFORMED STALL INSPECTION IAW AMM 72-00-05-6-1, REMOVED MASTER CHIP DETECTOR MAGNETIC PROBE NO METAL PARTICLES FOUND, ENGINE INLET NO DAMAGE FOUND. TURBINE EXHAUST, NO METAL PARTICKES FOUND, VBV ACTUATION HARDWARE, NO DAMAGE FOUND. LOW PRESSURE BLEED AIR CHECK VALVE, NO DEFECT FOUND. PS3 TUBE, NO CRACKS, BREAKS, OR BLOCKAGE FOUND. INSPECTORS FINISHED BORESCOPE INSPECTION ON THE COMPRESSOR STAGE 1&12, HPT. THE WORST DAMAGE IS ON STAGE 12, TEAR DAMAGE FROM THE LEADING EDGE. DIMENSION ABOUT 14MM EXCEEDED THE LIMITS IAW AMM 72-00-07-6-1, & AMM 72-36-00-8-1. R & R THE NR 1 ENGINE IAW AMM 71-00-01-4-1 AND GMM 6-1-550. RAN NR 1 ENGINE IAW JRH. ALL PARAMETERS NORMAL. ACFT OK FOR SERVICE.

Part: PUMP — FAULTED (HYDRAULIC SYS) · airframe 75,937 hrs · 18,082 cycles

INFO NR 3 HYD RES TEMP WAS RUNNING 40 - 5 DEGREES HOTTER THAN HYD SYS 1 & 2. TEMP NORMAL AFTER LANDING HSC HAS FAULTED NR 3 LT HYD PUMP THE LAST FOUR LEGS CREW INFO NOTED IN EAML. SEE MTSI 29-10-3801 & 29-10-3802. MEL 29-11-01-A IS APPLIED TO THE NR 3 ENG RT PUMP. RAN ALL THREE ENG'S IAW JRH FOR 6 MIN AT IDLE ENG PUMPS ONLY WITH NO RMP'S SELECTED. TEMP'S WERE 41, 50, 40, WITH NO HYD PUMP TEST FAIL & NR 3 ENG LT PUMP WAS INDICATING 3000 PSI. REF AMM 29-11-20-5 FOR PUMP TEST. RT PUMP IS STILL ON MEL & REMOVED FROM ACFT.

Part: CONNECTOR — DIRTY · airframe 75,926 hrs · 18,077 cycles

HYD SYSTEM NR 3 OFF. QTY 10.1 CONFIGURED HYD SYS 3 PRESSURIZED OK WITH NO LEAKS DETECTED. HOWVEVER RECEIVED RMP 2-3 DISAGREE ALERT. HYD 3 QUANTITY WAS AT PROPER SERVICE OF 7.5 WHEN ACFT BLOCKED IN. ON THE HYDRALUIC SYNOPTIC PAGE THE CYAN PREDEPARTURE QUANTITY LINE MATCHED THE BLOCK IN QUANTITY. BLED AIR FROM NR 3 RESERVOIR. FOUND THE HSC WAS INTERMITTENTLY NOT ALLOWING YOU TO MANUALLY TURN OFF THE NR 3 PUMPS THROUGH CFDS. REMOVED AND REPLACED THE HSC. WHEN HSC WAS REMOVED, FOUND GREASE FILM ON HSC RACK CONNECTOR. CLEANED RACK CONNECTOR. PERORMED OPERATIONAL CHECKS OR HSC. ALL TESTS PASSED

Part: CONTROL PANEL — FAULTED (COCKPIT) · airframe 74,823 hrs · 17,787 cycles

FSS PANEL CONTINUOUSLY FAULTS, ARGON PRESSURE, THEN BLINKS BLANK & BACK TO NORMAL EVERY 5 SECONDS. THEN STOPS FOR A FEW MINUTES & FAULTS AGAIN. SERVICED TO 2900 PSI IAW MM 26-00-120. NO LEAKS NOTED IAW 26-00-111. COMPLIED WITH POST MX RTS IAW 26-00-450. NO FAULTS NOTED. ACFT OK FOR SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 737 hrs · 17,485 cycles

LEVEL 1, HYD 1 OFF, ALERT DISPLAYED 2.9 GALLONS HYD FLUID REMAINING. AFTER LANDING, HYD 1 FAIL, ALERT DISPLAYED 0.5 GALLONS REMAINING. FOUND NR 1 HYD SYS LEAKING FROM LT SLAT ACTUATOR. REPAIRED THE PIPE IAW AMM 20-10-01-2. SERVICED HYD SYS 1 IAW AMM 12-13-02-3. INSPECTED HYD SYS 1 & ENG 1 HYD FILTER DPI, NO DEFECTS NOTED IAW AMM 29-12-42-6. RECYCLED SLATS SEVERAL TIMES, NO LEAK NOTED.

Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 729 hrs · 17,258 cycles

CREW REPORTED L1 DOOR REMOTE PRESS INDICATOR LIGHT INOPERATIVE. R & R REMOTE PRESS INDICATOR ASSEMBLY. PERFORMED OPERATIONAL TEST OF THE REMOTE PRESS INDICATOR, NO ABNORMALITY FOUND IAW AMM 25-61-04-4 & 25-61-04-5. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 729 hrs · 17,252 cycles

WALK AROUND CHECK, FOUND L1 DOOR REMOTE PRESS INDICATOR LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-02 CATEGORY C EXPIRATION 29 MAR 15. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQUATE ONCE EACH FLIGHT DAY.

Part: BATTERY — DISCHARGED (L1 DOOR) · airframe 729 hrs · 17,255 cycles

WALK AROUND CHECK, FOUND L1 DOOR REMOTE PRESS INDICATOR LIGHT INOPERATIVE AMM 25-61-15-5. R & R BOTH BATTERIES & OPERATION CHECKED NORMAL IAW AMM 25-61-15-5.

Part: WEB — CRACKED (BS 1841) · airframe 729 hrs · 17,250 cycles

AFT CARGO WEB PANEL CRACKED AT BS 1841, X= 52. REMOVED IAW SRM 51-31-01-0G AND A NEW WEB FABRICATED IAW DRAWING AGA7170 REVISION R. INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 729 hrs · 17,250 cycles

RIGHT WING FIXED LE SKIN NR 15 SLAT TRACK INBD CUT OUT SUSPECT CRACK AT XOS 944.556. REPAIRED IAW SRM 57-40-02-2R FIGURE 201 REPAIR 7 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SLAT — WORN (RT WING) · airframe 729 hrs · 17,250 cycles

DUE TO SLAT REMOVED FOR WORK ACCESS, RT HAND WING NR 7 SLAT OTBD RIB FWD HOLE BORE FOUND WORN. RT HAND WING NR 7 SLAT OUTBOARD RIB FORWARD HOLE SPOTFACE REWORKED AND FOUND WITHIN LIMIT AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 10 AND EA 1-5750-T0316077 PART 1 STEP 2. EXISTING THICKNESS: 0.392 INCH, MATERIAL REMOVED: 0.022 INCH, REMAINING THICKNESS: 0.370 INCH, MINIMUM ALLOWABLE: 0.340 INCH REPAIR ACCOMPLISHED AS PER EA 1-5750-T0316077 PART 1 TITLE: WINGS - FLIGHT SURFACES - RT WING - NR 7 SLAT ASSY - SRM REPAIR - RSC TRACKING " REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SLAT — WORN (RT WING) · airframe 729 hrs · 17,250 cycles

DUE TO SLAT REMOVED FOR WORK ACCESS. RT WING NR 7 SLAT OTBD RIB FWD HOLE SPOT FACE FOUND WORN. BUSHING AT RIGHT HAND WING NR 7 SLAT OUTBOARD RIB FORWARD HOLE BORE REMOVED AS PER MD11 CMM 20-10-7 HOLE MEASURED DIA.: 0.875 INCH, AND FOUND WITHIN LIMIT AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 10 NEW BUSHING INSTALLED WITH WET PRIMER AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 10 AND EA 1-5750-T0316077 PART 1 STEP 2 TITLE: "WINGS -FLIGHT SURFACES - RT WING - NR 7 SLAT ASSY - SRM REPAIR - RSC TRACKING " REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REFER TO WRI 57502062 FOR WORK DETAILS

Part: RIB — DAMAGED (RT WING) · airframe 729 hrs · 17,250 cycles

RIGHT WING NR 8 SLAT INBD RIB FOUND AFT HOLE WORN ON SIDE OF RIB AT HOLE STATION XOS 1005.124. REMOVED AND REPLACED WITH NEW RIB AS PER SRM 51-31-01-0G AND DRAWING NRB6737 REVISION N REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FORMER — CRACKED (RT WING) · airframe 729 hrs · 17,250 cycles

RT WING LEADING EDGE CAVITY FORMER FOUND CRACKED AT STA XOS 584. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2931 REVISION H INSTALLED NEW FORMER AT RT WING LEADING EDGE AT STA XOS 584 AS PER SRM 51-33-01-0G REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100

Part: SKIN — DAMAGED (FUSELAGE) · airframe 729 hrs · 17,250 cycles

EXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT CENTER CARGO CUTOUT AFT SIDE STA 1781 BETWEEN LONGERON 40R - LONGERON 41R EXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT CENTER CARGO CUTOUT AFT SIDE STA 1781 BETWEEN LONGERON 40R - LONGERON 41R EVALUATED AND FOUND DAMAGED FUSELAGE SKIN AT CENTER CARGO CUTOUT AFT SIDE STA 1781 BETWEEN LONGERON 40R - LONGERON 41R REPAIRED AS PER EA#1-5330-T0316007 PART 1 TITLE: "FUSELAGE - PLATES & SKINS - EXISTING REPAIR AT CENTER CARGO DOOR AFT JAMB - ALI TRACKING". EO#1-5100-7- 5001 B5 PART 1 TITLE: "STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REFER TO WRI#53302054 FOR WORK DETAILS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 729 hrs · 17,250 cycles

EXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT FORWARD CARGO CUTOUT AFT SIDE STA 1002.3 BETWEEN LONGERON 40R - LONGERON 41R EXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT FORWARD CARGO CUTOUT AFT SIDE STA 1002.3 BETWEEN LONGERON 40R - LONGERON 41R EVALUATED AND FOUND DAMAGED. FUSELAGE SKIN AT FORWARD CARGO CUTOUT AFT SIDE STA 1002.3 BETWEEN LONGERON 40R - LONGERON 41R CARRIED OUT REPAIR AS PER EA#1-5330-T0316037 PART 1 TITLE: "FUSELAGE - PLATES & SKINS - EXISTING REPAIR AT FWD LOWER CARGO DOOR AFT JAMB - ALI TRACKING" ACCOMPLISHED.EO#1-5100-7-5001 B5 PART 1 TITLE: "STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REFER TO WRI#53302056 FOR WORK DETAILS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 729 hrs · 17,250 cycles

EXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT FORWARD CARGO CUTOUT FORWARD SIDE STA 895.7 BETWEEN LONGERON 40R - LONGERON 41R EXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT FORWARD CARGO CUTOUT FORWARD SIDE STA 895.7 BETWEEN LONGERON 40R - LONGERON 41R EVALUATED AND FOUND DAMAGED. FUSELAGE SKIN AT FORWARD CARGO CUTOUT FORWARD SIDE STA 895.7 BETWEEN LONGERON 40R - LONGERON 41R CARRIED OUT REPAIR AS PER EA#1-5330- T0315930 PART 1 TITLE: FUSELAGE - PLATES & SKINS - EXISTING REPAIR FOUND AT FWD EDGE OF FORWARD LOWER CARGO DOOR JAMB - DEVIATION TO SRM" EO#1-5100-7-5001 B5 PART 1 TITLE: "STRUCTURES - REPAIR CATALOG - MD-11 REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707" ACCOMPLISHED. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REFER TO WRI#53302055 FOR REPAIR DETAILS.

Part: DOUBLER — CRACKED (RT WING) · airframe 729 hrs · 17,250 cycles

RIGHT WING LE BEADED DOUBLER AT STATION XOS 636 - 643 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: BEAM — CRACKED (L3 DOOR) · airframe 729 hrs · 17,250 cycles

CABIN MAIN DECK CARGO COMPARTMENT L3 DOOR PLUG NR 5 DOOR BEAM FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01-0G REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 729 hrs · 17,250 cycles

LEFT WING, LE LOWER ACCESS PANEL 519CB INBD EDGE CUT OUT CORNER. FOUND CRACK AT STATION XOS 611. REPAIR CARRIED OUT PER SRM 57-40-01-2R FIGURE 201 REPAIR 18. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 INITIAL INSPECTION TO BE CARRIED OUT AT NEXT 'C' CHECK NOT EXCEEDING 24 MONTHS AND REPETITIVE INSPECTION AT EVERY 'C' CHECK NOT EXCEEDING 24 MONTHS PER SRM 57-40-01-2R TABLE 203 REPAIR 18 REQUIREMENTS.

Part: FAN — FAILED (LAVATORY) · airframe 72,511 hrs · 17,119 cycles

DURING COCKPIT SETUP SMELLED STRONG SMOKE & ELEC HOT SMELL. CALLED FIRE DEPT & MX. LAVATORY VENT FAN ON CONVENIENCE PANEL ASSEMBLY FAILED. REMOVED CONVENIENCE PANEL ASSEMBLY TO FACILITATE FAN MOTOR REPLACEMENT. ROUTED CONVENIENCE PANEL TO AVIONICS FOR REPAIR. WORK ACCOMPLISHED IAW CMM 25-45-09. R & R VENT FAN IN CONVENIENCE PANEL PN MD012710-041 IAW CMM 25-45-09. RETURNED ASSEMBLY TO LINE FOR INSTALL & TEST.

Part: CONTROL PANEL — FAILED (SLIDE PRESSURE) · airframe 68,195 hrs · 15,759 cycles

DURING TRANSIT CHECK, FOUND RT EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM NOT TESTING. R & R PRESSURE ASSY OPS CHECKED NORMAL IAW MM 25-61-04-4.

Part: INDICATOR — INOPERATIVE (DOOR SLIDE) · airframe 67,849 hrs · 15,677 cycles

LEFT SLIDE SYS PRESS-TO-TEST INDICATING SYS INOPERATIVE. R & R L1 SLIDE REMOTE PRESSURE INDICATOR IAW MM 25-61-04-4. OPS CHECK NORMAL IAW MM 25-61-04-5.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 67,846 hrs · 15,676 cycles

FLOOR SUPPORT CRACKED AT BS 2000-2007 X=20. R & R WITH NEW FLOOR SUPPORT IAW AMM 20-50-02 REV 75.2 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 116.

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,846 hrs · 15,676 cycles

CARGO DOOR CUTOUT LOWER FRAME UPPER SURFACE BS 660 FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 52 AND DRAWING ACA7224 REVISION G. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,846 hrs · 15,676 cycles

BS 5-49 X= -8.5 SEAT TRACK LOBE FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 5 SHEET 2 OF 3 REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,846 hrs · 15,676 cycles

BS 1219 -1259 X= -75.25. SEAT TRACK FOUND CORRODED. REPAIRED IAW 53-00-52 FIGURE 201 REPAIR 1REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116

Part: BULKHEAD WEB — CRACKED (ZONE 100) · airframe 67,846 hrs · 15,676 cycles

CENTER CARGO AFT BULKHEAD PANEL CRACKED AT BS 1841 X= -20. BULKHEAD WEB REMOVED AND REPLACED WITH NEW FABRICATED WEB AS PER SRM 51-31-01 REVISION 52 NEW WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REVISION T. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: FRAME — DENTED (ZONE 200) · airframe 67,846 hrs · 15,676 cycles

BS 1721 L12L FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52, REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.

Part: BULKHEAD WEB — CRACKED (ZONE 100) · airframe 67,846 hrs · 15,676 cycles

CENTER CARGO AFT BULKHEAD PANEL FOUND CRACKED AT BS 1841 X= - 52. BULKHEAD WEB REMOVED AND REPLACED WITH NEW FABRICATED WEB AS PER SRM 51-31-01 REVISION 52 NEW WEB FABRICATED AS PER DRAWING AGA7170 REVISION T. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,846 hrs · 15,676 cycles

BS 5-65 X= 8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 52 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116

Part: STRUCTURE — CORRODED (ZONE 500) · corrosion level 2 · airframe 67,846 hrs · 15,676 cycles

LT WING T/E LOWER CAP AT 541JB CUT OUT ACCESS FOUND SURFACE CORROSION AT XW326. REMOVED AND REPLACED WITH NEW CAP AS PER SRM 51-33-01 REVISION 52. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: TRUNNION — CRACKED (NLG) · airframe 67,846 hrs · 15,676 cycles

HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON STOP DRILL IN THE LT NLG TRUNNION FITTING AND FOUND CRACK PROPAGATION FROM THE SLOT OUT APPROX .2500 INCHES IN LENGTH. TRUNNION REPAIRED IAW SRM 53-10-14, FIG 202, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR AS IAW GMM 6-2-100, REV 116.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 67,846 hrs · 15,676 cycles

RIGHT OTBD AILERON INBD T/E UPPER SURFACE FROM XOA 841 TO XOA 860 FOUND DELAMINATED. EA 1-5750-166115 AND SRM 57- 60-80 REPAIR 1 PARA. 4A HAS BEEN COMPLIED WITH. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.

Part: CHARGER — MALFUNCTIONED (EMERGENCY POWER) · airframe 65,877 hrs · 15,123 cycles

EMERGENCY POWER TEST FAIL NOTED ON POST FLIGHT INSP. EPCU SHOWS BATTERY/INTFC UNDER CURRENT FAULTS AND LAST TWO FLIGHT LEGS. COMPLIED WITH FIM 24-30-03-00 BATTERY VOLTAGE FOUND TO BE WITHIN LIMITS. EMERGENCY POWER TEST ATTEMPTED THREE TIMES, TWO FAILED, PASSED ONCE BY RESETTING BATTERY CHARGER CIRCUIT BREAKER. REMOVED AND REPLACED BATTERY CHARGER.IAW AMM 24-34-03-4. OPS CHECKED GOOD IAW AMM 24-34-03-5. EMERGENCY POWER TESTED SEVERAL TIMES, NO DEFECTS NOTED IAW AMM 24-00-01-5.

Part: PSEU — FAILED (MLG) · airframe 64,409 hrs · 14,710 cycles

AFTER T/O, RETRACTED GEAR AND FLAPS. WHEN FLAPS CAME UP GOT GEAR HORN. GEAR SHOWED UP AND SAFE. SLATS EXTENDED, FLAPS UP. RECYCLED GEAR AND FLAPS AND GOT SAME RESULT. R & R PSEU IAW MM 31-71-01-2-0 AND OPS CHECKED NORMAL.

Part: WARNING HORN — FALSE ACTIVATION (MLG) · airframe 64,409 hrs · 14,709 cycles

ON DEPARTURE, AFTER FLAP RETRACTED, RECEIVED A MLG AURAL WARNING. RETRACTED SLATS & WARNING CONTINUED. CHECKED CONFIGURATION PAGE & ALL INDICATIONS OF SLATS/FLAPS & GEAR NORMAL. NO GEAR LIGHTS DISPLAYED. CYCLED GEAR & WARNING CONTINUED. CYCLED FLAPS TO 28 & AS SOON AS SLATS EXTENDED, AURAL WARNING STOPPED. CONTINUED TO FLAPS 28, FLAPS & SLATS UP & NO PROBLEMS AFTER. CONTINUED TO DESTINATION, NO FURTHER PROBLEMS. PERFORMED AFS LANDING GEAR /GROUND PROXIMITY UNIT RTS FROM FCC-1 & FCC-2 IAW AMM 32-45-03-5-0. RTS PASSED. PERFORMED FLAP LIMIT ACTUATOR & FLAP SYS RTS FROM FCC-1 & FCC-2 REF AMM 22-00-00-5-0. RTS PASSED. NO CURRENT FAULTS NOTED, AND NO FAULTS IN FLIGHT LEG HISTORY NOTED IN CFDS FCC-1 OR FCC-2. NO FAULTS NOTED DURING OPERATION OF FLAPS REF AMM. NO HISTORY OF THIS DISCREPANCY LAST 99 DAYS. OK TO CONTINUE.

Part: SWITCH — INOPERATIVE (SLIDE PRESSURE) · airframe 62,718 hrs · 14,280 cycles

DURING MX PREFLIGHT, FOUND L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATION INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 25-61-02. REPLACED ITS BATTERIES AND BULBS, NO HELP. R & R TEST LAMP SWITCH IAW SMP. OPS CHECKED GOOD.

Part: HINGE FITTING — WORN (CARGO DOOR) · airframe 62,681 hrs · 14,270 cycles

UPPER CARGO DOOR HINGE FITTING ASSEMBLY ON FUSELAGE AT MOST FWD 03 EA HOLES WORN READ 0.425". REPAIR CARRIED OUT AS PER SRM 52-30-16 REV46. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 112.

Part: HINGE FITTING — WORN (ZONE 200) · airframe 62,681 hrs · 14,270 cycles

UPPER CARGO MOST FWD HINGE FITTING ASSEMBLY LOPE HOLES WORN, READ 0.430" UPPER CARGO DOOR MOST FWD HINGE FITTING ASSEMBLY WORN LOPE HOLES AREA REPAIRED AS PER EA1-5230-143587 TITLE: DOORS - MAIN DECK CARGO DOOR FORWARD HINGE SUPPORT - REPAIR. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112. A TEMPORARY REPAIR A PERIOD OF TIME NO GREATER THAN 24 MONTHS FROM EA RELEASE DATE UNTIL SUCH TIME THAT THE FINAL DTA IS RECEIVED AND THIS EA IS REVISED.

Part: BRACKET — DAMAGED (BS 1741-1761) · airframe 62,681 hrs · 14,270 cycles

CENTER CARGO FOUND STRUCK DAMAGE ON THE STA 1721 CEILING SUPPORT INSTALLATION AT STA 1741 AND 1761 RESPECTIVELY. DAMAGED BRACKET AT STA 1741 AND 1761 REMOVED AND REPLACED WITH NEW FABRICATED BRACKET IAW DWG APA0161-259 FOR STA 1741 AND APA 0161-227 FOR STA 1761. CRACK AT FLOOR SUPPORT STA 1721 CARRIED OUT REPAIR IAW EA 1-5310-143579 TITLE (FUSELAGE-MAIN DECK FLOORBEAM DAMAGE AT STA 1721, X=-95 -REPAIR) FOR BRACKET INSTALLATION REF TO WRI 33306988. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (LT WING) · airframe 62,681 hrs · 14,270 cycles

HFEC OPEN HOLE INSP CARRIED OUT AND FOUND 7 EA HOLES WITH CRACKED INDICATION AT LT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUT-OUT AT BTW XORS=683.400 AND XORS=713.600. REPAIR CARRIED OUT AT LT WING LWR SKIN PANEL OUTER WING ACCESS DOOR CUTOUT BETWEEN XORS 683.400 AND XORS 713.600 IAW DWG S611570004, REV A. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 112.

Part: SKIN — CRACKED (RT WING) · airframe 62,681 hrs · 14,270 cycles

HFEC OPEN HOLE INSP CARRIED OUT AND FOUND 3 EA HOLES WITH CRACK INDICATION AT RT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUT-OUT AT BTW XORS=683.400 AND XORS=713.600. REPAIR CARRIED OUT AT RT WING LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT AT BTW XORS 683.400 AND XORS 713.600 IAW DWG S611570004, REV A. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 112.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 62,681 hrs · 14,270 cycles

MAIN DECK SEAT TRACK CROWN DAMAGED AT STATION 635 X= 27.5. REPAIRED BY SECTION SEAT TRACK REPLACEMENT FROM STA 625 TO STA 665 X= 27.5 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 46. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,681 hrs · 14,270 cycles

UPON REMOVAL OF FLOOR PANEL NR 282HF SEAT TRACK FOUND CORROSION AT STATION 1701 X=-75. REPAIRED SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1671 TO STA 1711 X=-75 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 62,681 hrs · 14,270 cycles

MAIN DECK SEAT TRACK CROWN DAMAGED AT STATION 635 X= 47.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 605 TO STA 645 X= 47.5 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REV 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 59,928 hrs · 13,632 cycles

DURING CRUISE FLIGHT AUTOPILOT CONNECTED RECEIVED STALL INDICATION (STICKSHAKER) AND RED IAS. IAS ON BOTH AIRSPEED TAPE READ APPROX 280KTS. STANBY AIRSPEED WAS 220 KTS. ACCOMPLISHED ERRACTIC AIRSPEED CHECKLIST AND FADEC ALT. CDG U PERFORMED STICK SHAKER ACTIVATION INSPECTION IAW MM05-51-12-6,FOUND NO DAMAGE ON ELEVATORS. CDG U CHECKED PITOTS AND PITOTS DRAIN HOLES FOR OBSTRUCTIONS. FOUND SATIS. PERFORMED PITOT STATIC SYS FUNCTIONAL CHECK IAW AMM 34-11-00-2. FOUND ALL INDICATIONS SATISFACTORY. PRECAUTIONARY R & R ADC NR1 IAW AMM 34-16-01-4. CHECKED FCC NR 1 & NR 2 FOR CURRENT FAULTS. NO FAULTS. ACFT OK TO CONTINUE. CDG U R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. FINAL CLOSED.

Part: LINE — RUPTURED (HYD SYSTEM) · airframe 58,836 hrs · 13,392 cycles

DURING SLAT RETRACT GOT LEVE 1 "SLAT DISAG" WITH ROLLING MOTION TO THE RT. COMPLIED WITH RED TABS AND RETURNED TO DTW DECLARING EMERGENCY LANDING. ACFT TOWED OFF RUNWAY. FOUND RT SLAT ACT INBD LINE BROKEN. INSTALLED PERMANANT REPAIR TO SLAT HYD LINE IAW MM 20-10-01-2. REPAIRED LINE INSTALLED, AND LEAK CHECK NORMAL, OPS CHECK NORMAL IAW 27-82-00-0. REMOVED AND REPLACED HYD SYS NR1 MANIFOLD FILTERS. REPLACED NR 1 ENG HYD PUMP MANIFOLD FILTERS. REPLACED NR 1 ENG RT AND LT EDPS, DUE TO HYD SYS FULLY DEPLEATED. ALL OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: FRAME — DAMAGED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

AGING INSPECTION - MAIN DECK CARGO FRAME AT STA 1681 ABOVE LONGERON 12 LEFT FOUND WITH EXISTING DOUBLER REPAIR. EXISTING REPAIR AT MAIN DECK CARGO FRAME STA 1681 ABOVE LONGERON 12 LEFT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH SRM 53-30-00 FIGURE I VOLUME I, REVISION 40 AND E.A. NO. 1-5310-75183, REPAIR TRACKING (TYPE B) OF SRM REPAIRS FOR DAMAGE TOLERANCE ASSESMENT PER E.O. (NO. 1-2520-7-3308). E.O. NO. 1-5100-7-5001 A4 PART 1, REPAIR CLASSIFIED MAJOR PER GMM 6-2- 100, REVISION 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

RIGHT WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER INBOARD ATTACH HOLE SPOT FACE FOUND CORROSION. REWORKED AS PER E.A. 1-5750-132702, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

RT WING OTBD FLAP FWD INBD HINGE FITTING LWR OTBD ATTACH HOLE SPOT FACE FOUND CORROSION. REWORKED AS PER E.A. 1-5750-132702, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - LT FLOOR SUPPORT ASSY FROM STA 1887 TO STA 2007 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 41. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7081 REVISION P. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: FLOOR SUPPORT — CORRODED (BS 1887-2007) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - RT FLOOR SUPPORT ASSY FROM STA 1887 TO STA 2007 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 41. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA7080 REVISION F. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK FLANGE AT STA 1890, X = -27.5 FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SKIN — CRACKED (ZONE 500) · airframe 57,193 hrs · 13,050 cycles

HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT. FOUND 07 EA HOLES WITH CRACKED INDICATION AT LT WING LWR SKIN OUTER WING FUEL TANK PANEL CUT OUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIR CARRIED OUT AS PER E.A. 1-5710-132718, REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK FLANGE FROM STA 1851 TO STA 1891, X = 8.5 FOUND WITH MULTIPLE SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK FLANGE FROM STA 900 TO STA 935, X = -8.5 FOUND WITH MULTIPLE SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK FLANGE AT STA 1845, X = 27.5 FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK FLANGE FROM STA 1851 TO STA 1891, X = 27.5 FOUND WITH MULTIPLE SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SKIN — CRACKED (ZONE 600) · airframe 57,193 hrs · 13,050 cycles

HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT. FOUND 02 EA HOLES WITH CRACKED INDICATION AT RT WING LWR SKIN OUTER WING FUEL TANK PANEL CUT OUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIR CARRIED OUT AS PER E.A. 1-5710-132717, REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK STA 785, X = 8.5 FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SKIN — CORRODED (ZONE 600) · airframe 57,193 hrs · 13,050 cycles

RT WING UPPER SURFACE SKIN AT XORS 250 FOUND SURFACE CORROSION AT 3 LOCATIONS. CORROSION ON RIGHT HAND WING UPPER SURFACE SKIN AT XORS 250, REPAIRED CARRIED OUT AS PER SRM 57-00-01 VOLUME I FIGURE 6, REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK STA 1229, X = -75.5 FOUND WITH SURFACE CORROSION. REPAIRED AS PER SRM 53-70-00 FIGURE 6 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK STA 735, X = 8.5 FOUND WITH CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 685 TO STA 745, X = 8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: VANE — CORRODED (LT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

LT WING OTBD FLAP VANE NR 4 FROM INBD TRACK TEE FITTING ATTACH HOUSING FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-32-4 REVISION 64. ADJUSTMENT AND TEST OF THE LT OUTBOARD FLAP VANE REFER TO WORK CARD E1-5750-7-5002 E2 PART 1.

Part: VANE — CORRODED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

RT WING OTBD FLAP VANE NR 4 FROM INBD TRACK TEE FITTING ATTACH HOUSING, FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-32-4 REVISION 64. ADJUSTMENT AND TEST OF THE RT OUTBOARD FLAP VANE REFER TO WORK CARD E1-5750-7-5002 E2 PART 2.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK STA 795, X = 8.5 FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 745 TO STA 800, X = 8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: PANEL — CRACKED (ZONE 300) · airframe 57,193 hrs · 13,050 cycles

VERTICAL STABILIZER - NR 2 ENGINE INTAKE DUCT INTERNAL INBD SUPPORT PANEL STA ZID 2160 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-20-00 VOLUME I FIGURE 2, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

MAIN DECK CARGO - SEAT TRACK STA 1621, X = -27.5 FOUND WITH SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1591 TO STA 1631, X = -27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

RT WING OTBD FLAP FWD OTBD HINGE FITTING ACTUATOR OTBD ATTACH HOLE BORE FOUND CORROSION. RIGHT WING OUTBOARD FLAP FORWARD OUTBOARD HINGE FITTING ACTUATOR OUTBOARD ATTACH HOLE BORE REWORKED AS PER EA 1-5750-132704. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — DAMAGED (LT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

LEFT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING ACTUATOR OUTBOARD ATTACH BORE FOUND CORROSION. LEFT WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING ACTUATOR OUTBOARD ATTACH BORE REWORKED AS PER E.A. 1-5750-132701, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

LT WING OTBD FLAP FWD OTBD HINGE FITTING ACTUATOR INBD ATTACH BORE FOUND CORROSION. REWORKED AS PER E.A. 1-5750-132703, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

RIGHT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER INBOARD ATTACH HOLE BORE FOUND CORROSION. RIGHT WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER INBOARD ATTACH HOLE BORE REWORKED AS PER EA 1-5750-132702, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

RIGHT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER OUTBOARD ATTACH HOLE BORE FOUND CORROSION. RIGHT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING LOWER OUTBOARD ATTACH HOLE BORE REWORKED AS PER E.A. 1-5750-132702, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — CORRODED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

RT WING OTBD FLAP FWD INBD HINGE FITTING ACTUATOR OTBD ATTACH HOLE BORE FOUND CORROSION. RIGHT HAND WING OUTBOARD FLAP FORWARD INBOARD HINGE FITTING ACTUATOR OUTBOARD ATTACH HOLE BORE REWORKED AS PER E.A. 1-5750-132702, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE FITTING — DAMAGED (LT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

SCRATCH MARK, LT WING INBD FLAP AFT OUTBD HINGE INBD PIVOT BORE. REWORKED AS PER E.A. 1-5750-132705, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 57,193 hrs · 13,050 cycles

DEEPLY CHAFED SEAT TRACK STA 1411 X=-47.5 IN MAIN DECK CARGO. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I, REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

CORROSION RT WING INBD FLAP AFT OUTBD HINGE OUTBD PIVOT SPOT FACE. REWORKED AS PER E.A. NO. 1-5750-132706, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — DAMAGED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

RIGHT HAND WING INBOARD FLAP AFT OUTBOARD HINGE OUTBOARD PIVOT BORE FOUND CORROSION. RIGHT WING INBOARD FLAP AFT OUTBOARD HINGE OUTBOARD PIVOT BORE REWORKED AS PER EA 1-5750-132706, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: HINGE BRACKET — DAMAGED (RT WING TE FLAP) · airframe 57,193 hrs · 13,050 cycles

UNABLE TO CARRY OUT HFEC INSPECTION ON INBD PIVOT HOLE AT RT WING INBD FLAP OUTBD HINGE (FLAP SIDE) DUE TO HOLE CORROSION. REWORKED AS PER E.A. NO. 1-5750-132706, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.

Part: SKIN — DAMAGED (BS 1902-1941) · airframe 57,193 hrs · 13,050 cycles

LOWER AFT FUSELAGE BELLY STA 1902 TO 1941, BETWEEN LONGERON 48 RIGHT AND LONGERON 48 LEFT FOUND WITH EXISTING SPLICE REPAIR. EXISTING REPAIR AT LOWER AFT FUSELAGE BELLY STA 1902 TO 1941, BETWEEN LONGERON 48 RIGHT AND LONGERON 48 LEFT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH SRM 53-20-00 FIGURE 11 VOLUME I, REVISION 40. E.O. 1-5100-7-5001 A4 PART 1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100, REVISION 107.

Part: SKIN — DAMAGED (BS 1781) · airframe 57,193 hrs · 13,050 cycles

CENTER CARGO DOOR CUT OUT AFT EDGE STA 1781, BETWEEN LONGERON 40 AND 41 RT FOUND WITH EXISTING DOUBLER REPAIR. EXISTING REPAIR AT CENTER CARGO DOOR CUT OUT AFT EDGE STA 1781, BETWEEN LONGERON 40 AND 41 RT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 53-50-00 FIGURE 17 VOLUME I, REVISION 40. EO 1-5100-7-5001 A4 PART 1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100, REVISION 107.

Part: FAIRING — BROKEN (AIR INTAKE) · airframe 56,219 hrs · 12,843 cycles

AFTER TAKEOFF VIOLENT VIBRATION IN NOSE AREA WHEN ACCELERATING THROUGH 230KTS. VIBRATION STOPPED WHEN DECELERATING TO 210 KTS. FLIGHT CREW ADVISED VIBRATION STARTED AFTER TAKEOFF AND ALL GEAR RETRACTED COMPLETELY. CHECKED A/C AROUND, LANDING GEAR FOUND NO DEFECT NOTED. AILERON, FLAP, ELEVATOR, RUDDER, SPOILER OPS NORMAL. NOSE TIRE DE-SPIN PAD NORMAL. FOUND NR 1 AIR INTAKE FAIRING PLATE BROKEN AND REMOVED IT THEN ALL PACK OPS NORMAL. ACN RELEASED FOR SERVICE PER MEL/CDL: 21-51-01-A CATEGORY: C EXPIRATION: 13APR09 "MEL 21-51-01-A: NR 1 PACK INOP. "RAM AIR SCOOP FAIRING PLATE MISSING. INSTALLED NR 1 PACK RAM AIR SCOOP FAIRING PLATE MPN, ABM7332-503, CPN: 0050633 PER MM 21-55-01-4. ADJUSTED NR 1 PACK RAM DOOR PER MM 21-55-01-4. REACTIVATED NR 1 PACK FLOW CONTROL VALVE. PERFORMED ACC-1, ACC-2, AC C-3 RTS TESTS PASSED PER MM 21-62-01-5.

Part: FAIRING — DAMAGED · airframe 56,243 hrs · 12,849 cycles

AFTER TO VIOLENT VIBRATION IN NOSE AREA WHEN ACCERATING THROUGH 230KTS.VIBRATION STOPPED WHEN DECCELATING TO 210KTS.276550 FLIGHT CREW ADVISED VIBRATION STARTED AFTER TAKEOFF AND ALL GEAR RETRACTED COMPLETELY. CHECKED A/C AROUND,LDG GEAR FOUND NO DEFECT NOTED. AILERON, FLAP, ELEVATOR, RUDDER, SPOILER OPS NORMAL.NOSE TIRE DE-SPIN PAD NORMAL.FOUND NR 1 AIR INTAKE FAIRING PLATE BROKEN AND REMOVED IT THEN ALL PACK OPS NORMAL. ACN RELEASED FOR SERVICE PER MEL 21-51-01-A NR 1 PACK - INOP. "RAM AIR SCOOP FAIRING PLATE MISSING. INSTALLED NR 1 PACK RAM AIR SCOOP FAIRING PLATE PER MM 21-55-01-4. ADJUSTED NR 1 PACK RAM DOOR PER MM 21-55-01-4. REACTIVED NR 1 PACK FLOW CONTROL VALVE. PERFORMED ACC-1, ACC-2,AC C-3 RTS TESTS PASSED PER MM 21-62-01-5.

Part: FITTING — CRACKED (ZONE 200) · airframe 52,591 hrs · 12,050 cycles

MAIN DECK CARGO DOOR LOWER JAMB BACKUP FITTING FOUND CRACKED. REMOVED AND REPLACED WITH A FABRICATED FITTING AS PER SRM 51-33-01 VOLUME II. FITTING FABRICATED AS PER EA 1-5300-112586, REPAIR CLASSIFIED AS MINOR PER GM 6-2-100.

Part: FITTING — CRACKED (ZONE 200) · airframe 52,591 hrs · 12,050 cycles

MAIN DECK CARGO DOOR, LOWER JAMB SUPPORT FITTING AT NR 7 A POS HFEC CHECK FOUND FASTENER HOLE CRACKED. REPAIR CARRIED OUT AS PER FEDEX EA1-5310-112585, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 52,591 hrs · 12,050 cycles

MAIN DECK CARGO SEAT TRACK AT STA 5-33, RT = 75.25 UNDER FLOOR PANEL FOUND FLANGE DAMAGED. REPAIR CARRIED OUT AT MAIN DECK CARGO SEAT TRACK STA 5-33, RT=75.25 UNDER FLOOR PANEL FLANGE AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,591 hrs · 12,050 cycles

MAIN DECK CARGO, SEAT TRACK AT STA 555, RT X=27.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 200) · airframe 52,591 hrs · 12,050 cycles

HFEC INSPECTION CARRIED OUT AND FOUND CRACK AT L-1 RT SPLICE WITH CRACK LENGTH OF APPROX 1 INCH AT STA 6-100. REPAIR CARRIED OUT AS PER EA 1-5330-118767, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 200) · airframe 52,591 hrs · 12,050 cycles

HFEC INSPECTION CARRIED OUT AND FOUND CRACK AT L-1 LT SPLICE WITH CRACK LENGTH OF APPROX .25 INCH AT STA 6-100. REPAIR CARRIED OUT AS PER EA 1-5330-118768, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 52,591 hrs · 12,050 cycles

FOUND SIX FASTENER HOLES CRACK INDICATION DURING HFEC, OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-118760 PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SPLICE — CRACKED (ZONE 200) · airframe 52,591 hrs · 12,050 cycles

HFEC INSPECTION CARRIED OUT AND FOUND CRACK AT L-2 RT SPLICE WITH CRACK LENGTH OF APPROX 1 INCH AT STA 6-100. REPAIR CARRIED OUT AS PER EA 1-5330- 118769, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SKIN — CRACKED (ZONE 600) · airframe 52,591 hrs · 12,050 cycles

16 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING, LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS 690 AND XORS 700. REPAIR CARRIED OUT AS PER EA 1-5710-118761 PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: RIB — CRACKED (ZONE 600) · airframe 52,591 hrs · 12,050 cycles

RIGHT WING, UPON REMOVAL OF NR 1 SLAT INBOARD CRUISE PERFORMANCE FILLET FOR NR 1 SLAT INBOARD LEADING EDGE METAL SEAL REPLACEMENT, FOUND OUTBOARD RIB NEAR ALIGNMENT AREA CRACKED. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 5 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STIFFENER — CRACKED (ZONE 300) · airframe 52,591 hrs · 12,050 cycles

AFT FUSELAGE COMPT: AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT STA 2007, X=-10 UPPER END FOUND CRACKED. REPAIR CARRIED OUT AS PER EA 1-5310-117418, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: STRAP — CRACKED (ZONE 600) · airframe 47,667 hrs · 10,945 cycles

RIGHT WING, OUTBOARD FLAP INBOARD FORWARD FLAP HINGE TENSION STRAP FOUND CRACKED. RIGHT WING, OUTBOARD FLAP INBOARD FORWARD FLAP HINGE TENSION STRAP REMOVED AND REPLACED AS PER FEDEX EA NR 1-5750-104780, TITLE: WINGS, RIGHT WING, OUTBOARD TRAILING EDGE FLAP, INBOARD HINGE, TENSION STRAP, COMPLIANCE WITH BOEING S/B 57-10 CONDITION 2. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · airframe 47,667 hrs · 10,945 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD AFT BORE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD AFT BORE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-103514, TITLE: WINGS OUTBOARD TRAILING EDGE FLAP, RIGHT OUTBOARD SUPPORT BRACKET CORROSION REPAIR. ORIGINAL HOLE DIAMETER = 0.456", FINAL HOLE DIAMETER = 0.516". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · airframe 47,667 hrs · 10,945 cycles

RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT INBOARD MID BORE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT INBOARD MID BORE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-103514, TITLE: WINGS OUTBOARD TRAILING EDGE FLAP, RIGHT OUTBOARD SUPPORT BRACKET CORROSION REPAIR. ORIGINAL HOLE DIAMETER = 0.458", FINAL HOLE DIAMETER = 0.518". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: BRACKET — CORRODED (ZONE 600) · airframe 47,667 hrs · 10,945 cycles

RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD MID BORE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP OUTBOARD AFT HINGE (FLAP SIDE) FORWARD MOUNT OUTBOARD MID BORE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-103514, TITLE: WINGS - OUTBOARD TRAILING EDGE FLAP, RIGHT OUTBOARD SUPPORT BRACKET CORROSION REPAIR. ORIGINAL HOLE DIAMETER = 0.457", FINAL HOLE DIAMETER = 0.517". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: RIB — CRACKED (LT WING) · airframe 47,667 hrs · 10,945 cycles

LEFT WING, AFTER REMOVAL OF NR 1 SLAT PERFORMANCE FAIRING FOUND FAIRING RIB CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,667 hrs · 10,945 cycles

MAIN DECK CARGO, FOUND L3 DOOR CUTOUT LOWER FORWARD AND AFT CORNER SEAL LAND LOCATION WITH CORROSION. MAIN DECK CARGO LT HAND DOOR FORWARD AREA CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II. MATERIAL THICKNESS = 0.270", REMAINING THICKNESS = 0.235", MATERIAL REMOVED = 0.035" AND FOUND WITHIN LIMIT AS PER SRM 53-50-00 FIGURE 17 VOLUME I. AFT AREA MEASURED, MATERIAL THICKNESS = 0.270", REMAINING THICKNESS = 0.196", MATERIAL REMOVED = 0.074" AND FOUND EXCEEDED LIMIT AS PER SRM 53-50-00 FIGURE 17 VOLUME I. AFT AREA CARRIED OUT REPAIR AS PER SRM 53-50-00 VOLUME I FIGURE 17. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: PANEL — CRACKED (L/E SLAT) · airframe 47,667 hrs · 10,945 cycles

LEFT WING NR 2 SLAT TRAILING EDGE PANEL OUTBOARD CORNER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,667 hrs · 10,945 cycles

RIGHT CENTER WING FUSELAGE LONGERON 28 LOWER SIDE OF R3 DOOR STA 1256 FOUND WITH CORROSION. REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS = 0.250", REMOVED THICKNESS = 0.038", AND REMAINING THICKNESS = 0.212". REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 47,667 hrs · 10,945 cycles

MAIN DECK CARGO, FOUND R3 DOOR CUTOUT LOWER FORWARD AND AFT CORNER SEAL LAND LOCATION WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-50-00 FIGURE 17 VOLUME I. ORIGINAL THICKNESS = 0.270", MATERIAL REMOVED = 0.040", REMAINING THICKNESS = 0.228". R3 DOOR CUTOUT LOWER FORWARD AREA CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND EXCEEDED LIMIT AS PER SRM 53-50-00 FIGURE 17 VOLUME I. ORIGINAL THICKNESS = 0.345", MATERIAL REMOVED = 0.165", REMAINING THICKNESS = 0.228". FORWARD AREA REPAIRED AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 47,667 hrs · 10,945 cycles

RIGHT CENTER WING FUSELAGE LONGERON 28 LOWER SIDE OF R3 DOOR STA 1305 FOUND WITH CORROSION. REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-01 FIGURE 3 VOLUME I. ORIGINAL THICKNESS = 0.230", REMOVED THICKNESS = 0.063", AND REMAINING THICKNESS = 0.167". LONGERON 28 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,667 hrs · 10,945 cycles

MAIN DECK CARGO, FOUND WORN SEAT TRACK AT STA 715 RBL 27. REPAIR CARRIED OUT AT STA 715 RBL 27 AS PER SRM 53-70- 00 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N00661 FOR REPAIR DETAILS.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,667 hrs · 10,945 cycles

LEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 682 FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103502, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,667 hrs · 10,945 cycles

MAIN DECK CARGO, FOUND SEAT TRACK WORN AT STA 755 RBL 33.

Part: HINGE FITTING — CRACKED (TAILCONE) · airframe 47,667 hrs · 10,945 cycles

EMPENNAGE, FORWARD TAILCONE LEFT FORWARD HINGE FITTING FOUND CRACKED (LOCATED AT AFT ACCESSORY COMPARTMENT AFT BULKHEAD AREA). REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,667 hrs · 10,945 cycles

MAIN DECK CARGO, FOUND SEAT TRACK WORN AT RBL 67 JUST AFT OF LAVATORY LOCATION. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 7 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 47,667 hrs · 10,945 cycles

LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 737 FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103501, REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 47,667 hrs · 10,945 cycles

LEFT WING, FIXED LEADING EDGE SKIN AT TELESCOPIC DUCT CUTOUT FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103504, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,667 hrs · 10,945 cycles

MAIN DECK CARGO, FOUND SEAT TRACK WORN AT STA 675 RBL 55. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,667 hrs · 10,945 cycles

MAIN DECK CARGO, FOUND SEAT TRACK WORN AT STA 755 LBL 33. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (RT WING) · airframe 47,667 hrs · 10,945 cycles

CORROSION OBSERVED ON RIGHT WING REAR SPAR UPPER CAP AT XORS 683. RIGHT HAND WING REAR SPAR UPPER CAP AT XORS 683 CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I AND FEDEX EA NR 1-5710-104779. REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-104779, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (BS 700) · airframe 47,667 hrs · 10,945 cycles

MAIN DECK CARGO, FOUND SEAT TRACK WORN AT STA 700 RBL 55. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REFER TO SNRM N00591 FOR REPAIR DETAILS.

Part: DOUBLER — CRACKED (RT WING) · airframe 47,667 hrs · 10,945 cycles

RIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 643 FOUND CRACKED. REPAIRED AS PER FEDEX E.A 1-5730-103500, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 47,667 hrs · 10,945 cycles

RIGHT WING, FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. REPAIRED AS PER FEDEX EA 1-5730-103503, REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 47,667 hrs · 10,945 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT WING STRINGER 12 END AT XORS 642. CRACKED STRINGER END ON RIGHT HAND WING, STRINGER 12 END AT XORS 642 TRIMMED OUT AND SPLICE REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 47,667 hrs · 10,945 cycles

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

Part: STRINGER — CRACKED (LT WING) · airframe 47,667 hrs · 10,945 cycles

CRACK FOUND DURING HFEC INSPECTION ON LT WING STRINGER 13 END AT XORS 577. LT HAND WING STRINGER 13 END AT XORS 577 REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (RT WING) · airframe 47,667 hrs · 10,945 cycles

CRACK FOUND DURING HFEC INSPECTION ON RIGHT WING STRINGER 14 END AT XORS 521. RIGHT HAND WING STRINGER 14 END AT XORS 521 TRIMMED OUT AND SPLICE REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 47,667 hrs · 10,945 cycles

CRACK FOUND DURING HFEC INSPECTION ON LEFT WING STRINGER 12 END AT XORS 642. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 47,667 hrs · 10,945 cycles

LEFT NOSE LANDING GEAR TRUNNION FITTING FOUND WITH CRACK ON LOWER FORWARD SIDE. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-104776,

Part: TRUNNION — CRACKED (NLG) · airframe 47,667 hrs · 10,945 cycles

RIGHT NOSE LANDING GEAR TRUNNION FITTING FOUND WITH CRACK ON LOWER FORWARD SIDE. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-100699.

Part: STRINGER — CRACKED (LT WING) · airframe 47,667 hrs · 10,945 cycles

CRACK FOUND DURING HFEC INSPECTION ON LEFT WING STRINGER 7 END AT XORS 952. REPAIRED AS PER FEDEX EA 1-5720-100697, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: THRUST REVERSER — CRACKED (ZONE 400) · airframe 43,456 hrs · 9,970 cycles

NR 1 ENGINE, LEFT THRUST REVERSER COWL, UPPER TORQUE BOX FORWARD FRAME CHAMPFER FOUND CRACKED P/N 683L213G04 S/N R591-085. REPAIRED PER DRAWING SRZ-78-002.

Part: STRINGER — CRACKED (ZONE 600) · airframe 43,456 hrs · 9,970 cycles

RT WING NR 3 FUEL TANK, INTERIOR, UPPER STRINGER 9, MOST AFT FOUND WITH CRACK APPROXIMATELY 8 INCHES LONG. CARRIED OUT REPAIR PER SRM 57-20-00 VOLUME I, FIGURE 10.

Part: STRINGER — CRACKED (ZONE 600) · airframe 43,456 hrs · 9,970 cycles

RIGHT WING NR 3 FUEL TANK, INTERIOR, UPPER STRINGER 8, MOST AFT FOUND WITH CRACK APPROXIMATELY 8 INCHES LONG. CARRIED OUT REPAIR PER SRM 57-20-00 VOLUME I, FIGURE 10.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK, FLOOR SEAT TRACK AT STA Y= 804 TO Y= 810, X= -8.5 CROWN ELONGATED ADA8390-1. REWORKED IAW SRM 53-70-00 VOLUME I AND INSTALLED IAW SRM 51-35-01 VOLUME II.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 1199 TO Y= 1285, X= -47 CROWN ELONGATED AEA7579-1. REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 5-83, X= -47 CROWN ELONGATED A5A7082-1. REPAIRED IAW SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK, FLOOR SEAT TRACK AT STA Y= 970, Y=1027 AND Y= 1099, X= -47 CROWN ELONGATED ADA8389-1. REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME 1, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK, FLOOR SEAT TRACK AT STA Y= 1904 TO Y= 1059, X= 47 CROWN ELONGATED ADA8389-1. REMOVED AND REPLACED PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

SNRM NO.: N0592 - MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 1139 TO Y= 6- 60, X= 47 CROWN ELONGATED A5A7082-1. REWORKED AND INSTALLED IAW SRM 53-70-01 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK, FLOOR SEAT TRACK AT STA Y= 904 TO Y= 1059, X= 47 CROWN ELONGATED ADA8389-1. REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK, FLOOR SEAT TRACK AT STA Y= 794 TO Y= 810, X= -27 CROWN ELONGATED ADA8390-1. REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 5-83 TO Y= 5- 113, X= 47 CROWN ELONGATED A5A7082-1. REMOVED, AND REPLACED IAW SRM 53-70-00 VOLUME I, FIGURE 1

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK, FLOOR SEAT TRACK AT STA Y= 794, Y=800 AND Y= 908, X= -27 CROWN ELONGATED ADA8389-1. REMOVED IAW SRM 51-33-01 VOLUME II. NEW SEAT TRACK REWORKED AND INSTALLED IAW SRM 53-70-00 VOLUME I, FIGURE 1.

Part: STRAP — CRACKED (ZONE 500) · airframe 43,456 hrs · 9,970 cycles

LEFT HAND WING, OUTBOARD FLAP INBOARD HINGE, TENSION STRAP FOUND CRACKED ARB0029-509N. REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 43,456 hrs · 9,970 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 1398 TO Y= 1521, X= 47 CROWN ELONGATED AEA7579-1. REMOVED AND REPLACED IAW SRM 53-70-00 VOLUME I, FIGURE 1.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 41,939 hrs · 9,657 cycles

1 HOUR INTO FLIGHT, THE LEVEL 2 ALERT FUEL QTY/USED CHK CAME ON. CHECKED FUEL ON BOARD, SHOWED 4,300 NR DIFFERENCE. SHORTLY AFTER, THE ALERT WENT AWAY. PRIOR THE LAT FUEL UNBAL LEVEL TWO ALERT HAD COME ON TWICE DURING FIRST HOUR OF FLIGHT. CALCULATED FOB AND COMPARED TO INDICATED FUEL ON BOARD AND DURING FLIGHT. UNRELIABLE QTY AND POSSIBLE FUEL LEAK. DIVERTED TO EWR. ON POST FLIGHT INSPECTION, FOUND NO VISIBLE EVIDENCE OF FUEL LEAK. INTERROGATED FQBU FOR FAULTS NR 3 TANK SHOWING NR 15 T/U SHOWING "CAP OUT" AND "OPEN PROBE" FAULTS. R-T-S OF FSC, ALL PASSED. RELEASED FOR SERVICE PER MEL: TANK NR 3 FUEL TANK SYNOPTIC QTY DISPLAY, INOP.

Part: RECEPTACLE — BURNED (HYD PUMP) · airframe 41,648 hrs · 9,597 cycles

NR 1 AUX HYD PUMP ELECTRIC POWER PLUG WAS FOUND BURNED. ENT BY: 500170 RPT BY: 500170 FACT 09NOV04 00:50 TPE R NR 1 AUX HYD PUMP PLUG REPLACED PER SMP AND PER MD-11, W/D 29-21-01 WIRING CHECKED NML. PRECAUTIONARY RCCB (B1-625) AND NR 1 AUX HYD PUMP REPLACED ALSO. PREMATURE REMOVAL/INSTALLATION OFF MFG 86155.

Part: RECEPTACLE — BURNED (AUX HYD PUMP) · airframe 41,648 hrs · 9,597 cycles

NR 1 AUX HYD PUMP ELECTRIC POWER PLUG WAS FOUND BURNED. ENT BY: 500170 RPT BY: 500170 FACT 09NOV04 00:50, TPE R NR 1 AUX HYD PUMP PLUG REPLACED PER SMP AND PER MD-11, W/D 29-21-01 WIRING CHECKED NML. PRECAUTIONARY RCCB(B 1-625) AND NR 1 AUX HYD PUMP REPLACED ALSO. PREMATURE REMOVAL/INSTALLATION OFF MFG 861555.

Part: PANEL — CRACKED (LT WING) · airframe 38,083 hrs · 8,812 cycles

LT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT FOUND CRACKED APPROXIMATELY 1.5 INCHES IN LENGTH. C/A: SNRM N0235 LT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT CRACKED PANEL REMOVED IAW AMM 20-50-02, REPLACED WITH NEW PANEL BY FABRICATION IAW EA 1-5750-75180, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, WING PANEL FABRICATION.

Part: HINGE — CORRODED (LT WING) · airframe 38,083 hrs · 8,812 cycles

LEFT WING - O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT O/B HOLE BORE CORRODED. LEFT WING - O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT O/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73355 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LEFT OUTBD FLAP OUTBD HINGE BRACKET REPAIRS.

Part: STRAP — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING - INBD FLAP OUTBD HINGE (FLAP SIDE), INBD STRAP, PIVOT POINT BORE CORRODED. LEFT WING - INBD FLAP OUTBD HINGE (FLAP SIDE), INBD STRAP REMOVED AND REPLACED AS PER SRM 51-33-01, VOL II AND AMM 20-50-02.

Part: STRAP — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING, INBD FLAP OUTBD HINGE (FLAP SIDE), OUTBD STRAP, PIVOT POINT SPOT FACE CORRODED. LEFT WING - INBD FLAP OUTBD HINGE (FLAP SIDE), OUTBD STRAP REMOVED AND REPLACED WITH NEW AS PER SRM 51-33-01, VOL II.

Part: CHANNEL — DAMAGED (ZONE 200) · airframe 38,083 hrs · 8,812 cycles

MAIN CARGO DECK RIGHT STA 735 TO STA 755 HAT SECTION BEHIND BUMPER STRIP DAMAGED. MAIN CARGO DECK RT STA 735 TO STA 755 HAT SECTION REMOVED AS PER SRM 51-35-01, VOL.II AND NEW HAT SECTION INSTALLED AS PER SRM 51-35-01, VOL.II & MM 20-50-02.

Part: CASE — CHAFED (COMPRESSOR) · airframe 38,083 hrs · 8,812 cycles

NEW ENGINE AT 4 O'CLOCK AFT FAN CASE AREA FOUND CHAFING MARK. CHAFING MARK AT NR 3 ENGINE ON 4 O'CLOCK POSITION, AFT FAN CASE 'T' RIB SMOOTHED OUT WITH FINAL DIMENSION : LENGTH = 0.470, WIDTH = 0.300 AND DEPTH APPROX. = 0.120, FOUND WITHIN LIMITS AS PER GE MANUAL 72-23-01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 38,083 hrs · 8,812 cycles

MAIN CARGO DECK LT STA 839 SEAT TRACK REF X=27.5 BENEATH FLOOR PANEL 241JF SEAT TRACK FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL 2 & SRM 53-70-00 FIG 1 VOL 1.

Part: FITTING — DAMAGED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RIGHT WING INBOARD FLAP VANE INBOARD ATTACHMENT T- FITTING, 3 EA HOLE BORE SIZE EXCEED LIMIT. INBD FLAP VANE OUTBD ATTACHMENT 'T' FITTING REMOVED AND INSTALLED NEW FITTING AS PER AMM 27-50-22.

Part: FITTING — WORN (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RIGHT WING - INBOARD FLAP VANE, INBOARD TRACK ATTACHMENT FITTING, BOLT HOLES (3) FOUND EXCEED LIMIT. RT WING - INBD FLAP VANE, INBD TRACK ATTACHMENT FITTING, BOLT HOLES REPAIRED AS PER EA 1-5750-73366, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT INBD. FLAP VANE ATTACH FITTINGS REWORK.

Part: FITTING — OUT OF LIMITS (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RIGHT WING INBD FLAP VANE INBD ATTACHMENT T-FITTING , 2 EA HOLE BORE SIZE EXCEED LIMIT. RIGHT WING - INBD FLAP VANE INBD ATTACHMENT T-FITTING REMOVED AND INSTALLED NEW FITTING AS PER AMM 27-50-22.

Part: FITTING — WORN (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RIGHT WING - INBOARD FLAP VANE, OUTBOARD TRACK ATTACHMENT FITTING, BOLT HOLES (3) FOUND EXCEED LIMIT. RT WING - INBD FLAP VANE, OUTBD TRACK ATTACHMENT FITTING, BOLT HOLES REPAIRED AS PER EA 1-5750-75176, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT INBD. FLAP VANE ATTACH FITTINGS REWORK.

Part: FITTING — WORN (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING - INBOARD FLAP VANE, OUTBOARD TRACK ATTACHMENT FITTING, BOLT HOLES, FOUND 3 THAT EXCEED LIMITS. LT WING - INBD FLAP VANE, OUTBOARD TRACK ATTACHMENT FITTING, BOLT HOLES REPAIRED AS PER EA 1-5750-75176, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT INBD. FLAP VANE ATTACH FITTINGS REWORK.

Part: FITTING — DAMAGED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFY WING - INBOARD FLAP VANE, INBOARD TRACK ATTACHMENT FITTING, BOLT HOLES (3 EA) FOUND EXCEED LIMIT.

Part: TRACK — DENTED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING, INBOARD FLAP CENTER VANE TRACK CUTOUT DENTED. INBOARD FLAP CENTER VANE TRACK CUTOUT DENTED, REPAIR CARRIED OUT AS PER EA 1-5750-75184, TITLE : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBOARD FLAP / CTR. RIB ASSY AND SKIN.

Part: TRACK — DENTED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING, INBOARD FLAP CENTER VANE TRACK CUTOUT DENTED. INBOARD FLAP CENTER VANE TRACK CUTOUT REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-75185, TRAILING EDGE AND TRAILING EDGE DEVICES - RT INBOARD, FLAP/CTR RIB ASSY AND SKIN.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 38,083 hrs · 8,812 cycles

FORWARD CARGO RIGHT TUNNEL BETWEEN STA 6-30 TO STA 6-50 AROUND NR 41 LONGERON, INTERCOSTAL FOUND CRACKED. REMOVED CRACKED INTERCOASTAL AS PER SRM 51-31-01, VOL.II AND FABRICATED NEW INTERCOASTAL AS PER DRAWING ACA7049. INSTALLED NEW INTERCOASTAL AT FORWARD CARGO R/H TUNNEL BETWEEN STA 6-30 TO STA 6-50 AROUND NO. 41 LONGERON AS PER SRM 51-31-01, VOL.II.

Part: FAIRING — WORN (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING FIX LEADING EDGE FAIRING ADJACENT TO OUTBOARD END OF LEADING EDGE SLAT FOUND WORN AT 02 LOCATIONS. COMPLIED WITH FEDEX EA 1-5720-73368, OUTER WING FIXED LEADING EDGE SKIN.

Part: FAIRING — WORN (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING FIX LEADING EDGE FAIRING ADJACENT TO NR 8 SLAT OUTBOARD END FOUND WORN. COMPLIED WITH FEDEX EA 1-5720-73367, OUTER WING, FIXED LEADING EDGE SKIN.

Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 38,083 hrs · 8,812 cycles

SUPPORT BRACKETS FOR TOILET SHROUD CRACKED.

Part: FRAME — DEBONDED (ZONE 300) · airframe 38,083 hrs · 8,812 cycles

AFT TAIL CONE INTERIOR LEFT SIDE FRAME ASSEMBLY FOUND DISBONDED. AFT TAIL CONE INTERIOR LT SIDE FRAME ASSEMBLY CARRIED OUT. REPAIR AS PER FEDEX EA 1-5240-75188, SERVICE DOORS, AFT EXTENDED TAILCONE PANEL ASSY REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 38,083 hrs · 8,812 cycles

MAIN CARGO DECK RT STA 455 TO STA 515 SEAT TRACK AT X=27.5 RT SEAT TRACK HAS HEAVY CORROSION. REMOVED AS PER SRM 53-70-00 FIG. 1 VOL. I AND INSTALLED NEW SEAT TRACK AT MAIN DECK CARGO RT STA 455 TO 525 AS PER SRM 53-70-00 FIG. 1 VOL I.

Part: WIRE HARNESS — DAMAGED (ZONE 400 IDG) · airframe 38,083 hrs · 8,812 cycles

NR 1 ENGINE PYLON IDG HARNESS NEAR YN = 315.5 FOUND DAMAGED. NR 1 ENGINE PYLON IDG HARNESS WIRE NR U01003-3/OC REMOVED AND REPLACED AS PER AMM 54-51-01-4 AND SWPM 20-10-01 AND NR 1 ENGINE POWER ASSURANCE CHECK CARRIED OUT AS PER AMM 71-00-00 FOUND 'SATIS'.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 38,083 hrs · 8,812 cycles

FORWARD CARGO LT TUNNEL BETWEEN STA 840 TO STA 859, NR 33 LONGERON SPLICE FOUND CRACKED. REMOVED CRACKED LONGERON SPLICE AS PER SRM 51-31-01, VOL.II AND FABRICATED NEW SPLICE AS PER DRAWING ADA8423. INSTALLED NEW SPLICE AT FWD CARGO LT TUNNEL BETWEEN STA 840 TO 859, NR 34 LONGERON AS PER NDA6712.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE BORE CORRODED. OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT, INBOARD HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73358, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - R/H OUTBD FLAP INBD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING, INBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT BEARING HOUSING, SPOT FACE CORRODED. I/B FLAP O/B HINGE (WING SIDE) PIVOT BEARING HOUSING SPOT FACE CORROSION REMOVED AS PER FEDEX EA 1-5750-73360 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT INBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE BORE CORRODED. RT WING, O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT I/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73356 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE BORE CORRODED. O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT I/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73355 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.

Part: SPLICE — CRACKED (ZONE 200) · airframe 38,083 hrs · 8,812 cycles

CENTER CARGO BETWEEN STA 5-113 TO STA 1541, NR 49L LONGERON SPLICE FOUND CRACKED.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORRODED. RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORROSION REMOVED AND FOUND WITHIN LIMITS AS PER CMM 57-44-08 AND DWG ARC0502 AND FEDEX EA 1-5750-73358, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), SIDE LINK SPOT FACE CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LINK SPOT FACE CORROSION REMOVED & FOUND WITHIN LIMITS AS PER CMM 57-44-08 & DRAWING ARC0502, AND EA 1-5750-73357, TRAILING EDGE & TRAILING EDGE DEVICES. LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIR.

Part: FRAME — CRACKED (ZONE 300) · airframe 38,083 hrs · 8,812 cycles

FORWARD TAIL CONE MOST AFT STA 2244 (UPPER HINGE AREA) FRAME FOUND CRACKED. FRAME AND ANGLE REPAIRED AS PER SRM 53-00-01 FIG. 9 VOL. I AND SRM 51-31-01 VOL. II.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER CMM 57-44-09.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD HOLE BORE CORRODED. O/B FLAP I/B HINGE (WING SIDE) ACTUATOR ATTACHMENT I/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73357 WINGS. TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), LOWER MOUNT BOLT HOLE SPOT FACE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE BORE CORRODED. LT WING, O/B FLAP I/B HINGE (WING SIDE) ACTUATOR ATTACHMENT O/B HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73357 WINGS - TRAILING EDGE & TRAILING EDGE DEVICES - LT OUTBOARD FLAP INBOARD HINGE BRACKET REPAIRS.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE BORE CORRODED. WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT, OUTBOARD HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73358, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBD FLAP INBOARD HINGE BRACKET REPAIR.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 38,083 hrs · 8,812 cycles

CENTER CARGO BETWEEN STA 5-113 TO STA 1541, NR 52 L LONGERON SPLICE FOUND CRACKED. REMOVED DAMAGED LONGERON SPLICE AS PER SRM 51-31-01, VOL.II AND INSTALLED NEW SPLICE AT CENTER CARGO BETWEEN STA 5-113 TO STA 1541, NO.52 LONGERON AREA AS PER DRAWING N5A6774.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE BORE CORRODED. OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT, OUTBOARD HOLE BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73356, WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES - RT OUTBOARD FLAP OUTBOARD HINGE BRACKET REPAIRS.

Part: FRAME — CRACKED (ZONE 300) · airframe 38,083 hrs · 8,812 cycles

FORWARD TAIL CONE MOST AFT STA 2244 LOWER RT SIDE FRAME FOUND CRACKED. TRIMMED OUT DAMAGED FRAME AS PER SRM 53-00-01, FIG.9, VOL.I. FABRICATED FRAME AS PER DRAWING AKC5739. FABRICATED REPAIR ANGLE AS PER SRM 53-00-01, FIG.9, VOL.I. INSTALLED FRAME AND REPAIR ANGLE AT FORWARD TAIL CONE MOST AFT STA 2244 LOWER RH SIDE AS PER SRM 51-31-01, VOL.II AND 53-00-01, FIG.9, VOL.I.

Part: HINGE — CORRODED (T/E FLAP) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73351, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. REMOVED AS PER EA 1-5750-73351, WINGS - TRAILING EDGE & TRAILING EDGE DEVICES, RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT BORE CORRODED. LT WING, OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73348, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES, LT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (T/E FLAP) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73351, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. REMOVED CORROSION AS PER EA 1-5750-73351, WINGS, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: RIB — CRACKED (RT WING) · airframe 38,083 hrs · 8,812 cycles

RT WING LEADING EDGE SLAT TRACK NR 16 INBOARD SUPPORT RIB WITH A CRACK. DAMAGED SUPPORT RIB REMOVED AS PER SRM 51-31-01, VOL 2 & NEW RIB INSTALLED AS PER SRM 51-31-01 VOL 2 & DWG ARB 2873.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 38,083 hrs · 8,812 cycles

AFT PRESSURE BULKHEAD LOWER EXTRUDED LONGERON RIGHT SIDE FOUND CRACKED. REMOVED CRACKED LONGERON AS PER SRM 51-31-01 VOL 2 & FABRICATED NEW LONGERON AS PER DRAWING AJC7001. INSTALLED NEW LONGERON AT FX - AFT PRESSURE BULKHEAD LOWER EXTRUDED RT SIDE AS PER SRM 51-35-01 VOL2 & SRM 51-33-01 VOL2.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 38,083 hrs · 8,812 cycles

CENTER CARGO LT TUNNEL BETWEEN STA 1821 TO STA 1841 APPROX LONGERON 37 INTERCOSTAL FOUND CRACKED. AIR CONDITIONING - HEATING - WELD REPAIR BAFFLE / AFT CARGO COMPARTMENT HAS BEEN COMPLIED WITH.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. OUTBOARD FLAP OUTBD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73352, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD HOLE SPOT FACE CORRODED. LT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73352, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73352, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73351, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORRODED. OUTBOARD FLAP INBD HINGE (FLAP SIDE), INBOARD PIVOT BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73348, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD BORE CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73352, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT POINT BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73359. TRAILING EDGE & TRAILING EDGE DEVICES. LT INBOARD FLAP HINGE BRACKET REPAIR

Part: SPLICE — CRACKED (ZONE 100) · airframe 38,083 hrs · 8,812 cycles

CTR CARGO RT TUNNEL BETWEEN STA 5-113 TO STA 1541 NR 38 LONGERON SPLICE FOUND CRACK. REMOVED DAMAGED LONGERON SPLICE AS PER SRM 51-31-01, VOL.II AND FABRICATED NEW SPLICE AS PER DRAWING A5A7114. INSTALLED NEW SPLICE AT CENTER CARGO RT TUNNEL BETWEEN STA 5-113 TO 1541, NR 38 LONGERON AS PER DRAWING N5A6774.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73348, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORRODED. OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73348 : WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: RIB — CRACKED (LT WING) · airframe 38,083 hrs · 8,812 cycles

LEFT WING LEADING EDGE SLAT TRACK NR 16 INBOARD SUPPORT RIB SUSPECT CRACK. LT WING LEADING EDGE SLAT TRACK NR 16 INBOARD SUPPORT RIB REMOVED AS PER SRM 51-31-01 VOL II AND NEW RIB INSTALLED AS PER SRM 51-31-01 VOL II.

Part: RIB — CRACKED (LT WING) · airframe 38,083 hrs · 8,812 cycles

LEFT WING LOWER WINGLET INTERIOR RIB FOUND CRACK AT THE FWD EDGES.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 38,083 hrs · 8,812 cycles

MAIN CARGO DECK RIGHT STA 495 AT X=75.25 SEAT TRACK DAMAGED. DAMAGED SEAT TRACK AT MAIN CARGO DECK RH STA 495, REFERENCE 75.25. REMOVED AND REPLACED WITH NEW SEAT TRACK AS PER SRM 51-31-01, VOL.II.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD BORE CORRODED. OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73352, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. OUTBOARD FLAP OUTBD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73352, TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FLAP / OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD HOLE SPOT FACE CORRODED. LT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73352, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), INBOARD PIVOT POINT, SPOT FACE CORRODED. LT WING OUTBD FLAP INBOARD HINGE (FLAP SIDE) INBD PIVOT POINT, SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73348, WINGS. TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT POINT, SPOT FACE CORRODED. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD PIVOT POINT, SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73348, WINGS, TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LEFT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. LT WING OUTBD FLAP INBD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73348, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES. LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. LT WING OUTBD FLAP INBD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORROSION REMOVED AS PER EA 1-5750-73348, WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP / INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE CORRODED. CORRODED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT POINT INBOARD BORE CORRODED. AREA REPAIR CARRIED OUT AS PER EA 1-5750-73351, TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING, OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD BORE CORRODED. AREA REPAIR CARRIED OUT AS PER EA 1-5750-73351, WINGS, TRAILING EDGE & TRAILING EDGE DEVICES - RT OUTBOARD FLAP, OUTBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: HINGE — CORRODED (ZONE 500) · airframe 38,083 hrs · 8,812 cycles

LT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT POINT BORE CORRODED. LT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT POINT BORE CORRODED AREA REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-73359 WINGS -TRAILING EDGE & TRAILING EDGE DEVICES - LT INBOARD FLAP HINGE BRACKET REPAIR.

Part: LONGERON — CRACKED (ZONE 100) · airframe 38,083 hrs · 8,812 cycles

CTR CARGO LEFT TUNNEL BETWEEN STA 5-113 TO STA 1541 NR 37 LONGERON SPLICE FOUND CRACK. REMOVED CRACKED LONGERON SPLICE AS PER SRM 51-31-01, VOL. II AND FABRICATED NEW SPLICE AS PER DRAWING A5A7114. INSTALLED NEW SPLICE AT CENTER CARGO LT TUNNEL BETWEEN STA 5-113 TO STA 1541, NR 37 LONGERON AS PER DRAWING N5A6774.

Part: HINGE — CORRODED (ZONE 600) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT POINT OUTBOARD HOLE SPOT FACE CORRODED. CORROSION REMOVED AS PER EA 1-5750-73350, TRAILING EDGE & TRAILING EDGE DEVICES, RT OUTBOARD FLAP. INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.

Part: STOP FITTING — CRACKED (RT WING) · airframe 38,083 hrs · 8,812 cycles

RT WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. CRACKED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73349, TRAILING EDGE AND TRAILING EDGE DEVICES. LT & RT OUTBOARD FLAP SECONDARY UP STOP REPAIR.

Part: STOP FITTING — CRACKED (LT WING) · airframe 38,083 hrs · 8,812 cycles

LT WING OUTBOARD FLAP STOP FITTING FOUND CRACK. LT WING OUTBOARD FLAP STOP FITTING CRACKED AREA REPAIR CARRIED OUT AS PER EA 1-5750-73349, - TRAILING EDGE AND TRAILING EDGE DEVICES - LT & RT OUTBOARD FLAP SECONDARY UP STOP REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,083 hrs · 8,812 cycles

FUSELAGE, STA Y=275 NOSE RADOME CUTOUT FUSELAGE EXTERIOR SKIN RIGHT UPPER FOUND WITH CRACK. FUSELAGE STA Y=275 NOSE RADOME FUSELAGE EXTERIOR SKIN CARRIED OUT REPAIR IAW SRM 53-00-01, FIG 5, VOL I.

Part: HEATER — SPARKS (ICE PROTECTION) · airframe 33,363 hrs · 7,736 cycles

SPARK FOUND EMITTING FROM THE FORWARD WASTE DRAIN HEATER AT FORWARD AVIONICS COMPARTMENT SIDE, WHEN POWER SWITCHED ON.

Part: SHROUD — CRACKED (CARGO BAY) · airframe 33,363 hrs · 7,736 cycles

CENTER CARGO COMPARTMENT, FUEL DRAIN SHROUD ASSEMBLY CRACKED AT BS 1801. PERFORMED STOP DRILL ON CRACK PER SRM.

Part: BOLT — CORRODED (T/E FLAP) · airframe 33,363 hrs · 7,736 cycles

RIGHT WING INBOARD T/E FLAP OUTBOARD HINGE LWR INBOARD BOLT FOUND CORRODED AND RUBBING SCARS ON SHANK.

Part: SHIM — OUT OF POSITION (RT WING) · airframe 33,363 hrs · 7,736 cycles

RIGHT WING FWD OF INBOARD FLAP OUTBOARD HINGE LWR OUTBOARD MOUNTING FOUND SUPPORT FITTING MOUNTING SHIM MIGRATED. LOCATED AT REAR SPAR BETWEEN POS XORS 298.5 TO 316.9.

Part: BOLT — CORRODED (T/E FLAP) · airframe 33,363 hrs · 7,736 cycles

LEFT WING INBOARD T/E FLAP OUTBOARD HINGE LWR INBOARD BOLT FOUND CORRODED AND RUBBING SCARS ON SHANK.

Part: BOLT — CORRODED (T/E FLAP) · airframe 33,363 hrs · 7,736 cycles

RIGHT WING INBOARD T/E FLAPS OUTBOARD HINGE LWR OUTBOARD BOLT FOUND CORRODED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 33,135 hrs · 7,679 cycles

PRIOR TO PUSHBACK F/O WINDSHIELD CRACKED AND CAUGHT ON FIRE. FOUND F/O WINDSHIELD DAMAGED FROM OVERHEAT CONDITION IMMEDIATELY AFTER CREW REPORTED FIRE IN THE COCKPIT. REMOVED AND REPLACED WINDSHIELD ANTI-ICE CONTROLLER AND WINDSHIELD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 30,020 hrs · 7,003 cycles

SNRM N 552 MAIN DECK COMPT FLOORBEAM AT BS 1661 FND CRACKED. R&R PER EA 1-5310-57085.

Part: ANTENNA — FAILED (WX RADAR)

WX RADAR FAILURE BOTH SYS WX FAIL ON VAV DISPLAY AND ALL INFO DISAPPEARED. REMOVED AND REPLACED RADAR ANTENNA, OPS CK OK PER MD11 MM 34-41-07-4.

Part: ANGLE — CRACKED (TORQUE BOX) · airframe 28,546 hrs · 6,655 cycles

SNRM N 6 - UPPER TORQUE BOX, AFT BULKHEAD YA 2122.8, UPPER ATTACH ANGLE CRACKED AT EACH END. LT 1.75 INCH, RH END 1.0 INCH. *S/D* REMOVED AND REPLACED PER MD-11 SRM 53-30-00. INCLUDES EA 1-5530-53281.

Part: ANGLE — CRACKED (TORQUE BOX)

SNRM N 13, N 3, N 4, N 8 UPPER TORQUE BOX 3 EA FRAME TO CROWN ATTACH ANGLES CRACKED. YA 2046 RT END 1 INCH, LT END .25 INCH YA 2069 RT END 2 INCH, YA 2092 RT END 1 INCH. *S/D* REMOVED AND REPLACED PER MD11 SRM 53-30-00.

Part: CLAMP — BROKEN (FUEL LINE)

LEFT HAND WHEEL WELL UPPER AUX TANK FUEL SUPPLY LINE, RETAINING CLAMPS ARE ALL BROKEN.

Part: CLAMP — BROKEN (FUEL LINE)

LT WHEEL WELL - UPR AUX TANK FUEL SUPPLY LINE, RETAINING CLAMPS ARE ALL BROKEN. ADJUSTED FWD MT BRACKET ASSY WHICH REMOVED PRELOAD ON CLAMP & REPLACED BROKEN CLAMPS (4 EA) PER SMP.

Part: WIRE — DAMAGED (PAX DOOR)

MAIN CABIN, ABOVE R3 DOOR CUT OUT, (20) WIRE SHORTED CAUSING ELECT- FIRE, DAMAGE IN AREA. ** S/D ** R&R PER W/O 24-56-02 DEACTIVATED CAB IN UTILITY OUTLETS PER EO 1-2400-7-5000.

Part: KEELBEAM — DAMAGED (FUSELAGE)

UNDERWING KEEL STRUCTURE OF SUBJECT A/C WAS DAMAGED IN LANDING INCIDENT AND HAS BEEN OPERATING UNDER REPETITIVE INSP PER EA 1-5330-46611 REV D. *S/D* REPAIRED BULKHEAD AT BS 595 INCLUDES EA 1-5310-46694. REF SNRM NR N00019.

Part: SKIN — DAMAGED (FUSELAGE)

SPLICING FUSELAGE SKIN AT BS 623 FROM L36 TO L48 LT AND RT OF SUBJECT A/C WAS DAMAGED IN LANDING INCIDENT AND HAD BEEN OPERATING UNDER REPETITIVE INSP PER EA 1-5330-46611 REV D. *S/D* REPAIRED BULKHEAD BS 595 LT & RT SIDE. REF N00019 INCLUDES EA 1-5330-46692.

Part: BULKHEAD — DAMAGED (FUSELAGE)

FWD FUSELAGE BULKHEAD AT BS 595 OF SUBJECT A/C WAS DAMAGED IN LANDING INCIDENT AND HAS BEEN OPERATING UNDER REPETITIVE INSP PER EA 1-5330-46611 REV D. *S/D* REPAIRED BULKHEAD AT BS 595 LT & RT SIDES. REF SNRM N00019 INCLUDES EA 1-5310-46693.

Part: ENGINE — FAILED (NR 2)

97-0079 STA-MNL, ON ROTATION THE NR 2 ENGINE EGT WAS BOXED AND AMBER. BROUGHT ENGINE BACK TO IDLE AND EGT ROSE TO 982, THEN HEARD AND FELT LOUD BANG. SHUT NR 2 ENGINE DOWN, DID NOT DUMP FUEL AND MADE EMERGENCY LANDING IN MANILA. REMOVED AND REPLACED THE NUMBER 2 ENGINE.

Part: SHUT OFF VALVE — FAILED (NR 2 ENGINE)

AIRCRAFT WAS ON THE GROUND IN SFO. THE NR 2 ENGINE WOULD NOT SHUT DOWN USING START LEVEL. THE FIRE HANDLE WAS PULLED AND ENGINE WAS SHUT DOWN. REMOVED AND REPLACED SOLENOID SHUT-OFF VALVE AS PER M/M 73-35-01-4-1. ALSO, REMOVED AND REPLACED FUEL SHUT CLOSE RELAY. ALL CHECKS GOOD. RAN NR 2 ENGINE PER JRH MD-1, ALL CHECKS GOOD.

Part: ENGINE — FAILED (NR 2 ENGINE)

ENGINE FAILED INSPECTION PER EA 7-7220-31529 INSP OF FIRST STAGE BOOSTER VANES.

Part: DOOR — CRACKED (LT MLG)

SNRM 7045 AND 7046, LT MAIN LANDING GEAR DOOR CRACKED FWD AND AFT OF CENTER HINGE INTER SKIN. *S/D* STOP DRILLED CRACK PER SRM 51-00-01 AND FABRICATED DOUBLERS AND SKIN FOR REPAIR PER SRM 52-10-00.

Part: WEB — CRACKED (BS 2007)

HORIZONTAL WEB CRACKED 0.500 JUST AFT OF PRESSURE BULKHEAD STA 2007, APPROX RBL 20 TO 30 AND ABOVE TAG HORIZONTAL BOX SECTION. *S/D* REMOVED NECESSARY FASTENERS. NDT VERIFIED END OF CRACK. FABRICATED AND INSTALLED REPAIR PER EA 1-5310-28046.

Part: CASTING — CRACKED (WS 562)

NR 5002, LT WING O/B FLAP I/B HINGE TENSION TIE SUPPORT STRAP CRACKED AT LOWER ATTACH BOLT HOLE AS SEEN FROM LWR EXTERNAL SURFACE STA XORS562, VERIFIED BY HFEC.