N614FE

Part: TRANSMITTER — LOOSE (TE FLAP) · airframe 91,679 hrs · 22,998 cycles

AFTER TAKEOFF RECEIVED AN MLG AURAL WARNING WITH MLG RAISED. HELD SPEED TO 240KTS & CONTINUED CLIMB. LEVELED AT 8K FT &CYCLED MLG. WITH MLG DOWN & LOCKED WARNING STOPPED. RAISED MLG & CONTINUED CLIMB TO FL230 & WARNING RETURNED AS MLG WAS RAISED. RETURNED TO BASE & NORMAL LANDING. NO OTHER INDS ON ANY SYNOPTIC DISPLAY, ALL INDS NORMAL. ONLY AURAL WARNING PRESENT. ON RETURN WITH MLG DOWN & LOCKED WARNING STOPPED. REF WDM 32-62-01 PG 1, SH 1, RECONNECTED P1-239 & P1-1111 IAW SWPM. INSTALLED CAWS UNIT IAW AMM 31-51-01-2. OPS CHECK GOOD. PERFORMED FCC-1 & FCC-2, FLAP SYS R-T-S IAW AMM 27-54-02-4. OPS CHECK GOOD. OPS TEST OF MLG WARNING SYS, ACFT NOT ON JACKS IAW AMM 32-62-00-5. OPS CHECK GOOD.

Part: FLANGE — CRACKED (ZONE 300) · airframe 90,420 hrs · 22,632 cycles

DURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM 2ND FASTERNER FROM BELOW TO LOWEST FASTERNER AND UNABLE TO PROCEED FURTHER INSPECTION DUE TO WEB BLOCKAGE. LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP STATION 2164 REPAIR CARRIED OUT PER EA #1-5530-T0313159 B P4. TITLE: TITLE: STABILIZERS Ï¿½ VERTICAL STABILIZER Ï¿½ REPAIR FOR CRACK AT VERTICAL STABILIZER REAR SPAR LHS AND RHS FWD AND AFT FLANGES. FOR FURTHER WORK DETAIL REFER TO SNRM: N01061. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 11/11/2022

Part: HINGE — WORN (CARGO DOOR) · airframe 90,420 hrs · 22,632 cycles

CABIN-UPPER CARGO DOOR, DOOR HINGE FITTING (FUSELAGE SIDE) PART NUMBER ACA7223-1 FOUND 1ST TO 11TH LOBES FROM FORDWARD FOUND OUT OF LIMIT. LOBE HOLES NUMBER 1 TO NUMBER 11 FROM FORWARD AT CABIN - UPPER CARGO DOOR , DOOR HINGE FITTING REWORKED AND FOUND NUMBER 1 TO NUMBER 11 HOLES EXCEED LIMIT AS PER MD-11 SRM52-30-16-1A FIGURE 101 SHEET 3. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD- 11 CMM52-34-04 REPAIR GENERAL PARAGRAPH 2.Y AND EA 1-5310-T0371243 PART 1 STEP 2 AND STEP 5. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE — WORN (CARGO DOOR) · airframe 90,420 hrs · 22,632 cycles

CABIN-UPPER CARGO DOOR, DOOR HINGE FITTING PART NUMBER ACA7332-1 FOUND 1ST TO 9TH LOBES FROM FORWARD FOUND OUT OF LIMIT. LOBE HOLES NUMBER 1 TO NUMBER 9 FROM FORWARD AT CABIN-UPPER CARGO DOOR. DOOR HINGE FITTING PART NUMBER ACA7332-1 REWORKED AS PER MD-11 CMM52-34-04 GENERAL REPAIR, PARAGRAPH 2.Y AND EA #1-5230-T0342123A PART 2 . OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM52-34-04 REPAIR GENERAL PARAGRAPH 2.Y AND EA#1-5230-T0342123A PART 2 STEP 2 AND STEP 5. TITLE: DOORS-CARGO DOOR/HYD SYS-MAIN DECK CARGO DOOR-ELONGATED HOLES ON FORWARD SUPPORT HINGE LOBE. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE — WORN (CARGO DOOR) · airframe 90,420 hrs · 22,632 cycles

CABIN- UPPER CARGO DOOR, DOOR HINGE FITTING FOUND 1ST TO 11TH LOBES FROM FORWARD FOUND OUT OF LIMITS. LOBE REWORKED AND FOUND NUMBER 1 TO NUMBER 5 HOLES EXCEED LIMIT. NUMBER 6 TO NUMBER 11 HOLES WITHIN LIMIT AS PER MD- 11 SRM52-30-16-1A FIGURE 101 SHEET 3. OVERSIZE REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM52-34-04 REPAIR GENERAL PARAGRAPH 2.Y AND EA 1-5310- T0371260 P1 STEP 2 AND STEP 5. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 90,420 hrs · 22,632 cycles

CABIN - UPPER CARGO FLOOR PANEL #231HF FOUND DELAMINATED BETWEEN STATION 595 TO STATION 675 CABIN - UPPER CARGO , DELAMINATED FLOOR PANEL #231HF BETWEEN STATION 595 TO STATION 675 REMOVED AND REPLACED AS PER AMM 53-21-04-4. FLOOR PANEL #231HF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 10/26/2022

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 90,420 hrs · 22,632 cycles

CABIN FLOOR PANEL #262LF FOUND DELAMINATED FROM STATION 1321 TO STATION 1361. CABIN - DELAMINATED FLOOR PANEL #262LF FROM STATION 1321 TO STATION 1361 REMOVED AND REPLACED AS PER AMM 53-21-04-4. FLOOR PANEL #262LF FABRICATED AS PER FEDEDX DRAWING SRZ-25-005 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 10/26/2022

Part: BEAM — CRACKED (R3 DOOR) · airframe 90,420 hrs · 22,632 cycles

CABIN - R3 DOOR #7 STOP BEAM FOUND CRACK. CABIN AT R3 DOOR CRACKED #7 BEAM REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. ORIG SUB DATE: 10/11/2022

Part: FRAME — CRACKED (VERTICAL STAB) · airframe 90,420 hrs · 22,632 cycles

EMPENNAGE: WHILE ACCOMPLISHING INSPECTION, ZONE 360 LEFT HAND SIDE FRAME FOUND CRACKED. FRAME REMOVED AND REPLACED IAW SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FRAME FABRICATED IAW DRAWING AJC7593 REVISION Z.

Part: FRAME — CRACKED (VERTICAL STAB) · airframe 90,420 hrs · 22,632 cycles

EMPENNAGE: WHILE ACCOMPLISHING INSPECTION, ZONE 360 RIGHT SIDE FRAME FOUND CRACKED. FRAME REMOVED AND REPLACED PER MD-11 SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. FRAME FABRICATED IAW DRAWING AJC7593 REVISION Z.

Part: ANCHOR FITTING — CORRODED (AFT ACCESSORY) · airframe 90,420 hrs · 22,632 cycles

: AFT ACCESSORY COMPARTMENT, LONGERON - 33 RIGHT TO LONGERON - 35 RIGHT, ATTACHMENT ANCHOR NUT SURROUNDING AREA FOUND WITH CORROSION. ANCHOR NUT AREA AT AFT ACCESSORY COMPARTMENT, LONGERON - 33 RIGHT TO LONGERON - 35 RIGHT, STATION 2144 TO STATION 2164 REMOVED AND FOUND OUT OF LIMIT PER MD-11 SRM 53-70-01-2R FIGURE 201. CORRODED AREA REPAIRED PER EA 1-5330-T0371185 P1. TITLE: FUSELAGE Ï¿½ PLATES & SKINS Ï¿½ AFT BODY Ï¿½ CORROSION FOUND ON FUSELAGE SKIN BETWEEN STA 2140 ANDSTA 2163, BETWEEN LONGERON L Ï¿½ 33R AND L Ï¿½ 35R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (BS 2164) · airframe 90,420 hrs · 22,632 cycles

WHILE ACCOMPLISHING LEFT HAND BANJO FORWARD FITTING INSPECTION, FOUND LEFT HAND BANJO AFT FITTING SUSPECTED CRACK AT STATION 2164. LEFT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA REPAIR CARRIED OUT PER E.A #: 1-5530-T0313159 B P4. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — DAMAGED (VERTICAL STAB) · airframe 90,420 hrs · 22,632 cycles

TO CARRY OUT BANJO FORWARD AND AFT FITTING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION AT STATION 2164. REPAIR CARRIED OUT ALONG STATION 2164 RIGHT HAND BANJO FITTING FORWARD AND AFT FLANGE AREA IAW EA 1-5530-T0313159 B P4. REPAIR CLASSIFIED AS MAJOR IAWGMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 100) · airframe 90,420 hrs · 22,632 cycles

CENTER UPPER AUX TANK - STRINGER 47 AT STATION XCW - 17 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (BS 1841) · airframe 90,420 hrs · 22,632 cycles

LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB LOWER FLOOR SUPPORT FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB , CORROSION AT LOWER FLOOR SUPPORT EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202 REPAIR GENERAL. CORRODED LOWER FLOOR SUPPORT AT STATION 1841 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. LOWER FLOOR SUPPORT FABRICATED AS PER DOUGLAS DRAWING AGA 7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. ORIG SUB DATE: 10/5/2022

Part: STRINGER — CRACKED (ZONE 100) · airframe 90,420 hrs · 22,632 cycles

CENTER UPPER AUX TANK - STRINGER 47 AT XCW 19 FOUND CRACK. CENTER UPPER AUX TANK STRINGER 47 AT XCW 19 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 100) · airframe 90,420 hrs · 22,632 cycles

CENTER UPPER AUX TANK - STRINGER 47 AT XCW 48 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CORRODED (LT WING) · airframe 90,420 hrs · 22,632 cycles

LEFT WING Ï¿½ UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER AT XORS 283 FOUND CORROSION. LEFT WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUX SPAR AND YW 467 AREA CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-20-01-1A FIGURE 101 ALLOWABLE DAMAGE 1. CARRIED OUT REPAIR AS PER EA 1- 5730-T0370103 PART 1 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,420 hrs · 22,632 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACK.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,420 hrs · 22,632 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 655 FOUND CRACK.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 90,420 hrs · 22,632 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 90,420 hrs · 22,632 cycles

LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB UPPER FLOOR SUPPORT FOUND WITH CORROSION. LOWER CENTER CARGO COMPARTMENT STATION 1841 WEB , CORROSION AT UPPER FLOOR SUPPORT EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 202 REPAIR GENERAL. CORRODED UPPER FLOOR SUPPORT AT STATION1841 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. UPPER FLOOR SUPPORT FABRICATED AS PER DOUGLAS DRAWING AGA 7170 REVISION R. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.

Part: DOUBLER — CRACKED (RT WING LE) · airframe 90,420 hrs · 22,632 cycles

RIGHT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,420 hrs · 22,632 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 544 FOUND CRACK.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 90,420 hrs · 22,632 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 906 FOUND CRACK.

Part: SKIN — CRACKED (LT WING LE) · airframe 90,420 hrs · 22,632 cycles

LEFT WING Ï¿½ FIXED LEADING EDGE NUMBER 12 SLAT TRACK CUTOUT CORNER AT XOS 776.5 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SPAR CAP — CORRODED (RT WING TE) · airframe 90,420 hrs · 22,632 cycles

RIGHT WING TRAILING EDGE REAR SPAR LOWER CAP AT XORS 1078 FOUND CORROSION. RIGHT WING TRAILING EDGE REAR SPAR LOWER CAP AT XORS 1078 CORROSION REMOVED AND FOUND EXCEED LIMITS IAW SRM 57-00-10-1A ALLOWABLE DAMAGE 1 FIG 101. CORRODED LOWER REAR SPAR CAP AT XORS 1078 REPAIR CARRIED OUT AS PER EA 1-5710- T0371060 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBOARD — DELAMINATED (MAIN DECK) · airframe 89,747 hrs · 22,461 cycles

FLOOR PANEL L/H 253DF IS DELAM WITH LARGE HOLE. FABRICATED NEW MAIN DECK FLOOR BOARD PANEL # 253DF PER FEDEX DRWG SRZ-25-005 ADA8396.. (MAJOR REPAIR)

Part: WINDSHIELD — CRACKED (N/A) · airframe 89,397 hrs · 22,379 cycles

PDIS 614 56-10 2933 06MAY22 YYZ OPEN U RIGHT WINDSHIELD CRACKED DUE TO ARCING. TURNED OFF WINDSHIELD HEAT. STOPPED CRACKING. FACT 08MAY22 22:56 YYZ REPLACED R/H WINDSHIELD PANEL ASSY I.A.W WITH MD11 AMM 56-11-01-4-1.

Part: TIRE — UNDERSERVICED (NR 3) · airframe 87,389 hrs · 21,798 cycles

RECEIVED LVL 2 TIRE FAIL FOR #3 TIRE TIRE PRESSURE LEAKED OUT AFTER TAKE OFF. T/S PER FIM 32-40-00-2 FIG 119, TIRE #3 BELOW 50PSI. REMOVED AND REPLACED #3 AND #4 TIRES REF AMM 32-41-01-4. PRESSURE CHECK GOOD.

Part: FINGER DOUBLER — DELAMINATED (RT WING) · airframe 85,747 hrs · 21,317 cycles

RIGHT WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 385 FOUND DELAMINATION. RIGHT WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 385 REPAIR CARRIED OUT, AS PER SRM 57-50-01-2R FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING LE) · airframe 85,747 hrs · 21,317 cycles

WING LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS 667 DOUBLER FOUND CRACK.

Part: SKIN — CRACKED (ZONE 500) · airframe 85,747 hrs · 21,317 cycles

WING, LEFT HAND WING FIXED LEADING EDGE LOWER SKIN AT SLAT TRACK NUMBER 14 CUT OUT OUTBOARD STATION XOS 892 FOUND CRACK WING LEFT HAND WING FIXED LEADING EDGE LOWER SKIN AT SLAT TRACK NUMBER 14 CUT OUT OUTBOARD STATION XOS 892. REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R, FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: FORMER — CRACKED (LT WING LE) · airframe 85,747 hrs · 21,317 cycles

WING LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS 584 FORMER ASSEMBLY FOUND CRACK.

Part: DOUBLER — DELAMINATED (ZONE 500) · airframe 85,747 hrs · 21,317 cycles

LEFT WING, TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 383 FOUND DELAMINATION. LEFT WING TRAILING EDGE INBOARD ISLAND UPPER FORWARD SKIN LOWER SURFACE FINGER DOUBLER AT XW 383. REPAIR CARRIED OUT, AS PER SRM 57-50-01-2R, FIGURE 203 REPAIR 6. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: TRUNNION — CRACKED (NLG) · airframe 85,747 hrs · 21,317 cycles

CRACK INDICATION FOUND APPROXIMATELY 0.125 INCHES IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND SIDE NOSE LANDING GEAR TRUNNION FITTING EXISTING TRIM OUT AT STATION 583. LEFT HAND SIDE NOSE LANDING GEAR TRUNNION FITTING EXISTING TRIM OUT AT STATION 583 CRACK APPROXIMATELY 0.125 INCHES. CARRIED OUT REPAIR, AS PER EA NR: 1-5310-T0312012A PART 3. TITLE: FUSELAGE-MAIN FRAME-LT NLG TRUNNION FITTING CRACK INSPECTION. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 85,747 hrs · 21,317 cycles

MAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK AT STATION 760, X= -47.5 CROWN WORN. MAIN DECK CARGO COMPARTMENT CABIN AT SEAT TRACK STATION 760, X= -47.5, WORN CROWN EVALUATED AND FOUND TO EXCEED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REMOVED AND REPLACED AT EXISTING SPLICES STATION 725 TO STATION 765, X= -47.5, AS PER SRM 51-31-01-0G. SEAT TRACK SEGMENT REWORKED, AS PER DOUGLAS DRAWING VZZ 7330 REVISION B. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — WORN (MAIN DECK CARGO) · airframe 85,747 hrs · 21,317 cycles

MAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK AT STATION 1060, X=47.5 CROWN WORN. MAIN DECK CARGO COMPARTMENT CABIN AT SEAT TRACK STATION 1060, 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 1029 TO EXISTING SPLICE STATION 1069 X=47.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: SEAT TRACK — WORN (MAIN DECK CARGO) · airframe 85,747 hrs · 21,317 cycles

MAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK AT STATION 1018, X= -8.5 CROWN WORN. MAIN DECK CARGO COMPARTMENT CABIN AT SEAT TRACK STATION 1018, 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 989 TO STATION 1029, X= -8.5, AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100.

Part: TERMINAL — DAMAGED (LIGHT) · airframe 83,443 hrs · 20,693 cycles

APPROX 20 MIN AT CRUISE, FL 360, APU FIRE LIGHT ILLUMINATED WITH TRI-TONE ALERT FIRE BELL. APU WAS NOT OPERATING. PULLED APU FIRE HANDLE & ROTATED. PER QRH, WAITED 30 SECS, TRI-TONE ALERT CAME BACK ON & FIRE HANDLE REMAINED ILLUMINATED. MANIPULATING WIRES ON BACK OF LIGHT CAUSES LIGHT TO GO ON AND OFF, SUSPECT BAD TERMINAL RINGS AND LIGHT ASSY. FOUND LOOSE RING TERMINAL AND JUMPER WIRE CRACKED, ALSO LIGHT ASSY. LOOKS DAMAGED. REPLACED BAD RING TERMINALS, REPAIRED JUMPER WIRE, AND REMOVED AND REPLACED LIGHT ASSY. PERFORMED OPS CHECK OF ENGINE / APU FIRE LOOPS ALL CHECKS GOOD AT THIS TIME. ALL ACCESS PANELS REINSTALLED.

Part: FLEX LINE — FAILED (OXYGEN SYSTEM) · airframe 82,982 hrs · 20,537 cycles

AFTER APPROXIMATELY 30MIN OF FLIGHT WE HEARD A LOUD EXCAPING OF AIR COMING FROM THE COURRIER SECTION. WE NOTICED THAT THE O2 SYSTEM READINGS ON SYSTEM 1 & 3 WERE DECREASING, #2 REMAINED @ 2000 PSI. NO AIR WAS AVAILABLE THROUGH THE OXYGEN MASKS IN THE COURRIER SECTION. SYSTEM READINGS: 1=0 PSI 2= 1700 PSI 3=0PSI. FACT 24SEP19 INSTALLED NEW FLEX LINE IN COURIER AREA ABOVE JUMP SEATS, R&R'D #1 AND #2 O2 BOTTLES AND LEAK CHECKED BOTTLES AND LINE IAW MM 35-11-01-4-0. LEAK CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY LIGHTS) · airframe 82,052 hrs · 20,216 cycles

EMER LT BAT 1 LO DURING PREFLIGHT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

MDCC AFT FLOOR SUPPORT FOUND CORROSION AT STA 2007 X =-25. CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING THK 0.020". CORRODED FLOOR SUPPORT REMOVED PER AMM 20-50-02. NEW FLOOR SUPPORT FABRICATED PER DWG AGA7087 REV M. NEW FABRICATED FLOOR SUPPORT INSTALLED PER AMM 20-50-02. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: FITTING — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT O/B FLAP VANE HORN FITTING 'E' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHT 1. EXISTING SLOT HOLE: LENGTH 0.857", WIDTH 0.581", FINAL SLOT HOLE: LENGTH 0.952", WIDTH 0.652". REPAIR LIMIT - LENGTH 0.940", WIDTH 0.670". REPAIR SLOT BUSHING FABRICATED PER EA 1-5750-T0342094 P1 STEP 1A. REPAIR SLOT BUSHING INSTALLED PER AMM27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188"-1.256, FINAL HOLE DIA: 1.282", MAXIMUM ALLOWABLE DIA: 1.220. REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-71744 C PART 5 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT HOLE SURFACE CORROSION. HINGE UPPER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING THK 0.715", MATERIAL REMOVED 0.004", REMAINING THK 0.711", MINIMUM ALLOWABLE THK 0.72". REPAIR SHIM FABRICATED & INSTALLED PER CMM 57-44-09 & EA 1-5750-T0342093 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT O/B HOLE SURFACE CORROSION. HINGE UPPER MOUNT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING THK 0.715", MATERIAL REMOVED 0.004", REMAINING THK 0.711", MINIMUM ALLOWABLE THK 0.72". REPAIR SHIM FABRICATED & INSTALLED PER CMM 57-44-09 & EA 1-5750-T0342093 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT O/B HOLE BORE CORROSION. HINGE UPPER MOUNT O/B HOLE BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING HOLE DIA 0.880", FINAL HOLE DIA 0.948", MAXIMUM ALLOWABLE DIA 0.944". REPAIR BUSHING FABRICATED & INSTALLED PER CMM57-44-09 & EA 1-5750-T0342059 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 0.584", FINAL HOLE DIA 0.596", MAXIMUM ALLOWABLE HOLE DIA 0.584". SHOULDER BUSHING FABRICATED PER EA 1-5750-T0342059 P1 STEP 1B & INSTALLED PER CMM 57-44-09 & EA 1-5750-T0342059 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHING FABRICATED & INSTALLED PER CMM 57-44-09 & EA 1-5750-T0342059 P1 STEP 1C & STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP I/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 2.312", FINAL HOLE DIA 2.317", MAXIMUM ALLOWABLE DIA 2.3135". OVERSIZED BUSHING FABRICATED & INSTALLED PER CMM 57-44-08 & EA 1-5750-T0342122 P1 STEP 2A & STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA: 1.148' FINAL HOLE DIA: 1.163" MAXIMUM ALLOWABLE HOLE: 1.150" OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-04 AND EA 1-5750-T0342097 P1 STEP 1A AND STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100.

Part: BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING I/B FLAP I/B DRIVE LINK IDLER BRACKET BORE CORROSION. DRIVE LINK IDLER BRACKET BORE REWORKED PER CMM 57-52-03. EXISTING HOLE DIA 1.00", FINAL HOLE DIA 1.316". REPLACEMENT BUSHING FOR ARC3087-1 & ARC3086-1 FABRICATED PER EA 1-5750-T0342037 P1 STEP 4, 4A, 4B, 4C, STEP 5, 5A, 5B, 5C. REPLACEMENT BUSHING INSTALLED PER EA 1-5750-T0342037 P1 STEP 7. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100

Part: FITTING — CORRODED (TR FLAP VANE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT O/B FLAP VANE HORN FITTING 'F' HOLE BORE CORROSION. BORE REWORKED AND FOUND EXCEED LIMIT PER SRM 57-50-02-2R FIG 201 SHEET 1. EXISTING SLOT HOLE: LENGTH 0.852", WIDTH 0.600", FINAL SLOT HOLE: LENGTH 0.960", WIDTH 0.708". REPAIR LIMIT - LENGTH 0.940", WIDTH 0.670". REPAIR SLOT BUSHING FABRICATED PER EA 1-5750-T0342094 P1 STEP 1B. REPAIR SLOT BUSHING INSTALLED PER AMM 27-50-32-4. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 0.584", FINAL HOLE DIA 0.596", MAXIMUM ALLOWABLE HOLE DIA 0.584", SHOULDER BUSHING FABRICATED & INSTALLED PER EA 1-5750-T0342059 P1 STEP 1B & INSTALLED PER CMM 57-44-09 & EA 1-5750-T0342059 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-08. EXISTING HOLE DIA 0.708", FINAL HOLE DIA 0.728", MAXIMUM ALLOWABLE HOLE DIA 0.709". OVERSIZED BUSHING FABRICATED & INSTALLED PER CMM 57-44-08 & EA 1-5750-T0342122 P1 STEP 2C & STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.223", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHING FABRICATED & INSTALLED PER EA 1-5750-T0342012 P1 STEP 1B. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08, EXISTING THK - UPPER 0.378", LOWER 0.348", MATERIAL REMOVED, UPPER & LOWER 0.005", REMAINING THK - UPPER 0.373", LOWER 0.343". REPAIR SHIM FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-T0342122 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE SURFACE CORROSION. HINGE LOWER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING THK 0.400", MATERIAL REMOVED 0.004", REMAINING THK 0.396", MINIMUM ALLOWABLE THK 0.423". REPAIR SHIM FABRICATED & INSTALLED PER CMM 57-44-08 & EA 1-5750-T0342122 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188"-1.290, FINAL HOLE DIA: 1.328", MAXIMUM ALLOWABLE DIA: 1.220. REPAIR BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-71761 REV D PART 6 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 7 HOLE) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.709", FINAL HOLE DIA 0.729", MAXIMUM ALLOWABLE HOLE DIA 0.709". OVERSIZED BUSHING FABRICATED & INSTALLED PER CMM 57-44-08 & EA 1-5750-T0342122 P1 STEP 2B, 2C & STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP O/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE (HOLE 4) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 2.300", FINAL HOLE DIA 2.3185", MAXIMUM ALLOWABLE HOLE DIA 2.3135". REPAIR BUSHING FABRICATED & INSTALLED PER EA 1-5750-T0342093 P1 STEP 1B & STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 7) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.718". FINAL HOLE DIA 0.727", MAXIMUM HOLE DIA 0.709". REPAIR BUSHING FABRICATED & INSTALLED PER EA 1-5750-T0342012 P1 STEP 1A. CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED PER CMM 57-44-08. EXISTING THK - UPPER 0.389", LOWER 0.373", MATERIAL REMOVED - UPPER & LOWER 0.005", REMAINING THK - UPPER 0.384", LOWER 0.368" ACCEPTED PER EA 1-5750-T0342012 P1 FG 3. SHIM FABRICATED & INSTALLED PER CMM 57-44-08. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA 1.188"-1.220, FINAL HOLE DIA: 1.250", MAXIMUM ALLOWABLE DIA 1.220. REPAIR BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-71744 C PART 5 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP I/B AFT (FLAP SIDE) HINGE PIVOT I/B HOLE BORE CORROSION. HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.158", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING FABRICATED & INSTALLED PER CMM 57-52-04 & EA 1-5750-T0342095 P1 STEP 1A & STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHING FABRICATED & INSTALLED PER CMM57-44-09 & EA 1-5750-T0342059 P1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.280", FINAL HOLE DIA 1.1287", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHING FABRICATED & INST PER EA 1-5750-T0342093 P1 STEP 1D & STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP O/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED PER CMM 57-44-09. EXISTING THK - UPPER 0.381", LOWER 0.386", MATERIAL REMOVED - UPPER & LOWER 0.010", REMAINING THK - UPPER 0.371", LOWER 0.376". REPAIR SHIM FABRICATED & INSTALLED PER CMM57-44-09 & EA 1-5750-T0342093 P1 STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (HOLE 7) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.705", FINAL HOLE DIA 0.722", MAXIMUM ALLOWABLE HOLE DIA 0.709". REPAIR BUSHING FABRICATED & INSTALLED PER EA 1-5750-T0342012 P1 STEP 1A. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.2806", FINAL HOLE DIA 1.284", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHING FABRICATED & INSTALLED PER EA 1-5750-T0342012 P1 STEP 1B. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.222", FINAL HOLE DIA 1.252", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED & INSTALLED PER CMM 57-44-08 & EA 1-5750-T0342122 P1 STEP 2D & STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (RT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09, EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.248", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHING FABRICATED & INSTALLED PER EA 1-5750-T0342093 P1 STEP 1D & STEP 1. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.222", FINAL HOLE DIA 1.252", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING FABRICATED & INST PER CMM 57-44-08 & EA 1-5750-T0342122 P1 STEP 2D & STEP 2. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: HINGE — CORRODED (TE FLAP) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

RT WING I/B FLAP O/B AFT (FLAP SIDE) HINGE PIVOT O/B HOLE BORE CORROSION. HINGE PIVOT O/B HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.188" - 1.283, FINAL HOLE DIA: 1.3785", MAXIMUM ALLOWABLE DIA: 1.220. REPAIR BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-71761 REV D PART 6 STEP 2A AND 2B. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE SURFACE CORROSION. HINGE LOWER MOUNT I/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING THK 0.436", MATERIAL REMOVED - FWD FACE 0.004", AFT FACE 0.013", REMAINING THK 0.419", MINIMUM ALLOWABLE THK 0.423", REPAIR SHIM FABRICATED & INSTALLED PER CMM 57-44-08 & EA 1-5750-T0342122 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER GMM6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO COMPT FLOOR PANEL OPEN UP FOR SUPRORT REPAIR FOUND SEAT TRACK FLANGE CORROSION AT STA 1681, X= 8.5. CORROSION REMOVED 0.066", REMAIN 0.014", MATERIAL THK 0.080" AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT SEAT TRACK REPAIRED PER SRM 53-00-52-2R FIG 201 REPAIR 1 AT CABIN STA 1671 TO STA 1711 X= 8.5. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

MDCC CORROSIONS ON SEAT TRACK FLANGE AT RT STA 1830, X=-107. SEAT TRACK CORROSION REMOVED 0.048" REMAIN 0.032", REMAIN 0.032", MATERIAL THK 0.080" AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R FIG 201 REPAR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,766 hrs · 19,806 cycles

RIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 AT XOS 665 CUTOUT FOUND L/E PLATING BEADED DOUBLER CRACK . CRACKED BEADED DOUBLER AT XOS 665 TRIMMED AND REPAIR CARRIED OUT AS 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 80,766 hrs · 19,806 cycles

RIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 4TH AND 5TH RIBS (COUNT OUTBOARD FROM SLAT TRACK NR 10) AT XOS 687 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 687 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,766 hrs · 19,806 cycles

RIGHT WING LEADING EDGE COMPARTMENT INBOARD OF ACCESS PANEL 626FB CUTOUT FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO AFT FLOOR PANEL SUPPORT FOUND WITH CORROSION AT STA 1887 - STA 2007 X=-25. FLOOR PANEL SUPPORT CORROSION REMOVED PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING THK 0.020". CORRODED FLOOR SUPPORT REMOVED PER SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED PER DWG AGA7088 REV B. NEW FABRICATED FLOOR SUPPORT INSTALLED PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,766 hrs · 19,806 cycles

RIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 5TH AND 6TH RIBS, XOS 696 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 696 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

UPON REMOVAL OF FLOOR PANEL FOR ACCESS, SEAT TRACK REPAIR FOUND CORROSION ON FLOOR SUPPORT AT RT STA 1761, X=- 8.5 TO X=-27.5. FLOOR SUPPORT CORROSION REMOVED AS PER SRM 51-21-01-0G AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIG 202. MATERIAL THK 0.70", MATERIAL REMOVED 0.050" REMAINING THK 0.020". FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FABRICATED FLOOR SUPPORT AS PER DWG ACA3140 REV AB. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

MDC AFT FLOOR SUPPORT ASSY FOUND WITH CORROSION AT STA 1887 TO STA 2007 X=0. FLOOR SUPPORT CORROSION REMOVED PER SRM 51- 21-01-0G ORIGINAL THK 0.080", MATERIAL REMOVED 0.060", REMAINING THK 0.020" AND FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. SUPPORT REMOVED AND REPLACED AS PER AMM 20-50-02. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO COMPT CORROSION ON SEAT TRACK FLANGE AT RT STA 975, X=-75.25. SEAT TRACK CORROSION REMOVED 0.056" REMAIN 0.015" MATERIAL THICKNESS 0.071" AND FOUND EXCEEDED LIMT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT. SEAT TRACK AT CABIN STA 969 TO STA 1009 X=-75.25 REPAIRED AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 80,766 hrs · 19,806 cycles

UPON REMOVAL OF FLOOR PANEL FOR ACCESS OF SEAT TRACK REPAIR FOUND CORROSION ON FLOOR SUPPORT AT RT STA 1821, X=- 8.5 TO X=- 27.5. FLOOR SUPPORT CORROSION REMOVED AS PER SRM 51- 21-01-0G AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIG 202. MATERIAL THK 0.071", MATERIAL REMOVED 0.052" REMAINING THK 0.019". FLOOR SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FABRICATED FLOOR PANEL SUPPORT AS PER DWG AGA3814 REV AA. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO COMPT SEAT TRACK CORROSIONS AT RT STA 485, X= - 27.5. CORROSION REMOVED 0.070", REMAINING THK: 0.020", ORIGINAL MATERIAL THK: 0.090" AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIGURE 101 AND EXCEEDED LIMIT SEAT TRACK REPAIRED PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT CABIN STA 455 TO STA 525 X=-27.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 80,766 hrs · 19,806 cycles

RIGHT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 CUTOUT BETWEEN 2ND AND 3RD RIBS (COUNT OUTBOARD FROM SLAT TRACK NR 10) AT XOS 677 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO COMPT CORROSION ON SEAT TRACK FLANGE AT RT STA 1037, X =-75.25. SEAT TRACK CORROSION REMOVED 0.046", REMAIN 0.025", MATERIAL THK 0.071" AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT SEAT TRACK REPAIRED PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT CABIN STA 1009 TO 1129 X=-75.25. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 80,766 hrs · 19,806 cycles

CRACK LINE IMAGE FOUND ON X-RAY FILM AT FWD TRANSVERSE SKIN SPLICE ASSY AT STA 6-100, LT LONGERON 4, NR 5 HOLE TO NR 6 HOLE (FROM CENTER OF SPLICE ASSY) OF CENTER FASTENER ROW. CRACK LONGERON SPLICE AT STA 6-100, LT LONGERON 4 REMOVED AND REPLACED WITH NEW FABRICATED LONGERON SPLICE AS PER SRM 51-33-01-0G. LONGERON SPLICE FABRICATED AS PER DRAWING AGA7112 REVISION A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

LOWER CTR CARGO COMPT CEILING FOUND CABIN FLOOR SEAT TRACK WITH CORROSION AT STA 5-73 TO 5-113 X =-75. CORROSION REMOVED 0.044", REMAINING THK 0.027", ORIGINAL THK 0.071" AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R REPAIR 1 FIG 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 755 X = 47.5. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R FIG 201 REPAIR 1 AT CABIN STA 725 TO 765 X= 47.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 695 X =27.5. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT STA 685 TO STA 705 X=27.5 SEAT TRACK. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,766 hrs · 19,806 cycles

LEFT WING LEADING EDGE COMPARTMENT INBOARD OF SLAT TRACK NR 14 AT XOS 885. FOUND L/E PLATING BEADED DOUBLER CRACK, XOS 885 LEFT WING LEADING EDGE COMPARTMENT INBOARD OF SLAT TRACK 14, CRACKED BEADED DOUBLER AT XOS 885 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,766 hrs · 19,806 cycles

MDC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 1821, X=- 8.5. SEAT TRACK CORROSION MATERIAL REMOVED 0.055", MATERIAL REMAIN 0.016", MATERIAL THK 0.071" FOUND EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1 AND EXCEEDED LIMIT. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT CABIN STA 1800 TO 1887, X=-8.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,766 hrs · 19,806 cycles

LEFT WING LEADING EDGE COMPARTMENT OUTBOARD OF SLAT TRACK NR 10 XOS 670 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 670 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,766 hrs · 19,806 cycles

LEFT WING LEADING EDGE COMPARTMENT AT XOS 528 ABOVE OUTBOARD SLAT DRIVE CYLINDER FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 528 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 635 X= 8.5. CRACKED SEAT TRACKED REPAIRED PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT CABIN STA 625 TO STA 705 X= 8.5. SEAT TRACK REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,766 hrs · 19,806 cycles

LEFT WING LEADING EDGE COMPARTMENT OUTBOARD OF OUTBOARD REFUEL ADAPTER PORT XOS 646 FOUND L/E PLATING BEADED DOUBLER CRACK. CRACKED BEADED DOUBLER AT XOS 646 TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO COMPT FLOOR SEAT TRACK FOUND CRACK AT STA 635 X = 47.5. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R REPAIR 1 FIG 201 AT CABIN STA 605 TO STA 655 X=47.5. SEAT TRACK REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 80,766 hrs · 19,806 cycles

LEFT WING LEADING EDGE COMPARTMENT AT XOS 618 ABOVE INBOARD REFUEL ADAPTER PORT FOUND L/E PLATING BEADED DOUBLER CRACK, XOS 618. CRACKED BEADED DOUBLER AT XOS 618 TRIMMED AND REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG203 REPAIR 15. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 80,766 hrs · 19,806 cycles

CABIN MAIN DECK CARGO COMPT. FRAME EXISTING REPAIR CHAFED AT LT STA 535 LONGERON 19L. REPAIR ANGLE FABRICATED PER SRM 53-20-07-2R FIG 202 REPAIR 1. CHAFFED REPAIR ANGLE REMOVED AND REPLACED WITH NEW FABRICATED REPAIR ANGLE AS PER SRM 53-20-07-2R FIG 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 80,766 hrs · 19,806 cycles

CABIN MAIN DECK CARGO COMPT FRAME EXISTING REPAIR CHAFED AT LT STA 535, LONGERON 24L. REPAIR ANGLE FABRICATED AS PER SRM 53-20-07-2R FIG 201 REPAIR 1. CHAFED REPAIR ANGLE REMOVED AND REPLACED WITH NEW FABRICATED REPAIR ANGLE AS PER SRM 53-20-07-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 80,766 hrs · 19,806 cycles

MAIN DECK CARGO COMPT FLOOR SEATRACK FOUND CRACK AT STA 635 X = 27.5. MAIN DECK CARGO COMPARTMENT STA 635 X= 27.5 CRACKED SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R FIG 201 REPAIR1 AT CABIN STA 625 TO STA 645 X= 27.5. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FITTING — CRACKED (ZONE 100) · airframe 80,766 hrs · 19,806 cycles

LOWER FWD CARGO DOOR COUNTER BALANCE DRIVE BEAM ATTACHMENT FITTING CRACK. CRACK ATTACHMENT FITTING AT LOWER FWD CARGO DOOR COUNTER BALANCE DRIVE BEAM AT STA 984.551. REMOVED AND REPLACED WITH NEW FABRICATED FITTING AS PER SRM 51-33-01-0G. NEW FITTING FABRICATED AS PER DRAWING ADA8032 REVISION NC. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CHAFED (LT WING) · airframe 80,766 hrs · 19,806 cycles

LT WING ANTI ICING TELESCOPIC DUCT DOOR CUTOUT REPAIR DOUBLER SURFACE CHAFED XOS 464. LT WING ANTI ICING TELESCOPIC DOOR CUTOUT WORN EXISTING REPAIR DOUBLER REMOVED PER SRM 51-31-01-0G AND REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 10 FIG 202. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: TRANSMITTER — FAILED (MLG) · airframe 79,451 hrs · 19,412 cycles

LEVEL 2 TIRE FAIL ALERT 2, 10 MINUTES INTO FLIGHT AT FL 310. INTERROGATED BTMTP FAULT REVIEW SHOWED THE NR 10 TPI TRANSMITTER FAILED.

Part: LAMP — INOPERATIVE (EVAC SLIDE) · airframe 78,134 hrs · 19,047 cycles

L1 MAIN CREW ENTRANCE SLIDE LIGHT WILL NOT TEST. RELACED THE LAMPS. CHECKED OK IAW MM 25-61-04-5. ACFT OK TO CONTINUE.

Part: LAMP — INOPERATIVE (DOOR SLIDE) · airframe 77,759 hrs · 18,932 cycles

L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST LIGHT INOPERATIVE. REPLACED THE LAMP. OPS CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (DOOR SLIDE) · airframe 77,444 hrs · 18,848 cycles

LEFT MAIN CREW ENTRANCE SLIDE LIGHT WILL NOT TEST. REMOVED AND REPLACED DOOR SLIDE BATTERIES. OPS CHECKED NORMAL IAW AMM 25-61-06-5.

Part: TRUNNION — CORRODED (CNTER MLG) · corrosion level 2 · airframe 76,886 hrs · 18,669 cycles

CENTER LANDING GEAR RIGHT TRUNNION SUPPORT FITTING LOWER FACE HAS AREAS OF CORROSION. REPAIRED THE CENTER LANDING GEAR RT TRUNNION FITTING IAW SRM 53-40-14, REP 1.

Part: TRUNNION — WORN (NLG) · airframe 76,886 hrs · 18,669 cycles

NOSE LANDING GEAR LT FUSELAGE TRIUNION FITTING OUTBOARD BUSHING HAS WEAR AT THE UPPER SIDE AND INBOARD BUSHING LOOSE IN FITTING AND CAN BE REMOVED BY HAND. ACCOMPLISHED A REPAIR ON THE NOSE LANDING GEAR, LEFT TRUNNION FITTING OTBD BUSHING IAW SRM 53-10-14-2R.

Part: ACTUATOR — LACK OF LUBE (RUDDER TRIM) · airframe 76,698 hrs · 18,613 cycles

RUDDER TRIM KNOB IS FROZEN AT CRUISE & AFTER LANDING. UNFROZE ONCE BLOCKED IN. PERFORMED LUBRIFICATION OF RUDDER TRIM ACTUATOR IAW MM 12-24-06-3. PERFORMED OPERATIONAL TEST OF THE RUDDER IAW MM 27-20-00-2. NO DEFECT FOUND.

Part: LAMP — INOPERATIVE (TEST LIGHT) · airframe 76,652 hrs · 18,601 cycles

DURING PRE-FLIGHT INSPECTION, FOUND THE L1 DOOR SLIDE PRESSURE PRESS TO TEST LIGHT ASSY INOPERATIVE. REPLACED LAMPS AND OPS CHECKED GOOD.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 76,095 hrs · 18,437 cycles

LEFT WING OUTBOARD AILERON INBOARD TRAILING EDGE UPPER SURFACE DELAMINATION. REPAIRED IAW SRM 57-60-80-2R PARA 4A(1)A REPAIR 1 AND EA 1-5750-T0328952 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING) · airframe 76,095 hrs · 18,437 cycles

LT WING SKIN FASTENER HOLES FOUND TO HAVE CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION. REPAIRED IAW SRM 57-20-02- 2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6- 2-100.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 76,095 hrs · 18,437 cycles

WHILE ACCOMPLISHING DETAILED INSPECTION IAW WIC 57C1501 STEP 2, FOUND CORROSION ALONG REAR SPAR UPPER CAP AT LT WING XORS 685.65 TO 706.65 CORROSION REWORKED IAW EA 1-5710-T0328871 PT 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (RT WING) · airframe 76,095 hrs · 18,437 cycles

RT WING SKIN FOUND CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION. REPAIRED IAW SRM 57-20- 02-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1219) · corrosion level 2 · airframe 76,095 hrs · 18,437 cycles

MAIN DECK SEAT TRACK CORRDED AT BS 1219, LBL 75.25. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1541) · corrosion level 2 · airframe 76,095 hrs · 18,437 cycles

MAIN DECK SEAT TRACK CORRODED BS 1541, RBL 8.5. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STANCHION — CORRODED (BS 1967) · airframe 76,095 hrs · 18,437 cycles

AFT CARGO BAY STANCHION AT BS 1967 LONGERON 43L FOUND SKIN BULGED. STANCHION REMOVED AND REPLACED IAW SRM 51-31-01-0G. DWG AGA7978 REV. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1311) · corrosion level 2 · airframe 76,095 hrs · 18,437 cycles

MAIN DECK SEAT TRACK CORRODED BS 1311, LBL 75.25. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (RT WING) · airframe 76,095 hrs · 18,437 cycles

RIGHT HAND WING FIXED LEADING EDGE CAVITY AT STA XOS 667 RIB DOUBLER FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G, DWG #ARB3954 REV K. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: RIB — CRACKED (RT WING) · airframe 76,095 hrs · 18,437 cycles

RIGHT HAND WING FIXED LEADING EDGE CAVITY AT STA XOS 584 RIB FORMER FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G, DWG #ARB2931 REV 'H'. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (LT WING LE) · airframe 76,095 hrs · 18,437 cycles

DURING HFEC INSPECTION, FOUND CRACK INDICATION ON THE LT WING FIXED LEADING EDGE SKIN.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,095 hrs · 18,437 cycles

LT WING FIXED LEADING EDGE CAVITY AT STA XOS 755 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,095 hrs · 18,437 cycles

LT WING FIXED LEADING EDGE CAVITY AT STA XOS 733 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,095 hrs · 18,437 cycles

RT WING FIXED LEADING EDGE AT STA XOS 606 PANEL SUPPORT DOUBLER FOUND CRACKED. DOUBLER REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER PER SRM 51-31-01-0G AND DRAWING ARB2933 REV 'AJ' AND REV 'T'. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,095 hrs · 18,437 cycles

LT WING FIXED LEADING EDGE LOWER SURFACE AT STA XOS 548 PANEL SUPPORT DOUBLER FOUND CRACKED. DOUBLER REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER PER SRM 51-31-01-0G AND DRAWING ARB2933 REV 'AJ' AND REV 'T'. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,095 hrs · 18,437 cycles

LT WING FIXED LEADING EDGE CAVITY AT STA XOS 627 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,095 hrs · 18,437 cycles

LT WING FIXED LEADING EDGE CAVITY AT STA XOS 693 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,095 hrs · 18,437 cycles

RT WING FIXED LEADING EDGE CAVITY AT STA XOS 639 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,095 hrs · 18,437 cycles

LT WING FIXED LEADING EDGE CAVITY AT STA XOS 766 BEADED DOUBLER FOUND CRACKED. CARRIED OUT INNER DOUBLER REPAIR PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,095 hrs · 18,437 cycles

MAIN DECK RT STA 1099, X=-27 SEAT TRACK ASSEMBLY FOUND WITH FOUND SURFACE CORROSION AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1009 TO STA 1129 X = -27 PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,095 hrs · 18,437 cycles

MAIN DECK RT STA 1039, X=-47 SEAT TRACK ASSEMBLY FOUND WITH FOUND SURFACE CORROSION AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1009 TO STA 1049 X = -47 PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,095 hrs · 18,437 cycles

MAIN DECK STA 1099, X= 27 SEAT TRACK ASSEMBLY FOUND WITH FOUND SURFACE CORROSION AS MARKED. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1069 TO STA 1129 X = 27 PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: CRANK ASSY — CRACKED (LT PEDAL) · airframe 728 hrs · 17,432 cycles

SETTING PARKING BRAKE, CAPTAIN LT RUDDER PEDAL FLOPPED FWD WITH NO EFFECT. FOUND CRANK UNDER THE BRAKE PEDAL BROKEN, CAPTAINS LT SIDE. REF IPC 32-44-05-01 ITEM 350. PN ABH7236-501. ALSO FOUND PN ON BROKEN PART SHOWS, PN ABH7236-7D. TRY TO REMOVE THE BROKEN CRANK IAW CMM 27-21-02, BUT FOUND THE SLIDE SHIFT JAMMED. APPLIED PENETRATE OIL & WILL CONTINUE TO REMOVE THIS SLIDE SHIFT BY NEXT SHIFT. ORDER SLIDE SHIFT & SPACERS FOR PRECAUTION IAW CMM 27-21-02 ITEM 173. PN ABH7240-1 SLIDE SHIFT NR 1 ITEM 190 PN ABH7237-1 SPACER 2. TROUBLESHOOT PER CMM 27-21-02. REPLACED CAPT LT PEDAL CRANK (P/N ABH7236-501) AND SLIDE SHAFT(P/N ABH7240-1) AND BUSHING( P/N ABH7237-1). PERFORMED RUDDER AND BRAKE OPERATION CHECK ALL NORMAL. AS PER AMM 27-20-00-5 AND 32-46-00-2. A/C OK FOR SERVICE

Part: UNKNOWN — ODOR · airframe 724 hrs · 17,298 cycles

EN-ROUTE GOT BURNT OIL ODOR, SEE MX HISTORY. TRIED ISOLATING EACH PACK & THEN EACH BLEED WITH NO CLEAR IMPROVEMENT. ODOR WAIVED IN & OUT. TURNED TRIM AIR OFF & IT APPEARED TO MOSTLY DIMINISH BUT HARD TO TELL IF IT WAS DUE TO TRIM AIR OR JUST SOMEWHAT CYCLIC NATURE OF EVENT. AFTER 20 MIN ODOR RETURNED WITH TRIM AIR OFF. NO RELEVANT ACC OR ESC FAULTS IN CFDS. PERFORMED AIR CONDITIONING ODOR CLEARANCE PROCEDURE IAW MM 21-53-00-7. PACK 1, 2 & 3 COALESCERS RENEWED IAW MM 21-54-05-2. DURING PACK OPERATION USING INDIVIDUAL ENGS & APU CHECKED ALL COCKPIT OUTLETS FOR ODOR, NONE NOTED. ALSO CHECKED FWD AVIONICS COMPARTMENT FOR ODOR, NONE NOTED. ENGS OPERATED IAW JRH. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 724 hrs · 17,295 cycles

VERY OBVIOUS RUBBER SMELL IN THE COCKPIT. NOT EVIDENT IN THE CABIN. INFO ONLY WRITE UP. MAYBE ASSOCIATED WITH THE HEAT REPAIR. RAN ALL PACK'S IAW AMM 21-22-00-5. CHECKED AIR FLOW & FOR SMELLS, NO ABNORMAL SMELLS COULD BE FOUND. PACKS OPERATE NORMAL & ALL PRESSURES ARE GOOD. NO EVIDENCE OF RUBBER SMELL FROM ANY PACKS. ACFT OK FOR SERVICE.

Part: BATTERY — OUT OF POSITION (L1 DOOR SLIDE) · airframe 723 hrs · 17,284 cycles

ON PRE-FLIGHT, CREW FOUND L1 DOOR EVAC SLIDE PRESSURE PRESS TO TEST INOPERATIVE. ADJUSTED BATTERIES IN BATTERY CRADLE. OPERATIONAL CHECKED GOOD.

Part: SWITCH — LOOSE (L1 DOOR SLIDE) · airframe 719 hrs · 17,142 cycles

WALK AROUND FOUND L1 DOOR SLIDE TEST LIGHT INOPERATIVE. FOUND LOOSE WIRE TERMINAL ON BACK OF SWITCH ASSEMBLY. RECONNECTED LOOSE TERMINAL IAW MM 25-61-04-4. INSTALLED NEW BATTERIES IAW MM 25-61-04-4. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: CARGO TRACK — CRACKED (ZONE 200) · corrosion level 2 · airframe 71,170 hrs · 16,938 cycles

CABIN MAIN DECK CARGO TRACK BS 6-40 X -8.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1310) · airframe 71,170 hrs · 16,938 cycles

MAIN DECK CARGO BAY BS 1310 LONGERON 26R AFT R3 DOOR LOWER DOOR FRAME FOUND WEB CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1310) · airframe 71,170 hrs · 16,938 cycles

CABIN MAIN DECK CARGO COMPARTMENT LT BS 1310 LONGERON 26L AFT L3 DOOR LOWER JAMB FOUND WEB CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1256) · airframe 71,170 hrs · 16,938 cycles

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

Part: FUEL CELL — CORRODED (CENTER) · airframe 71,170 hrs · 16,938 cycles

UPPER CARGO BAY UNDER FLOOR AREA BS 1229, CTR TANK TOP SURFACE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 AND FOUND WITHIN LIMITS IAW SRM 57-10-01 FIGURE 101. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: DOOR FRAME — CRACKED (BS 1256) · airframe 71,170 hrs · 16,938 cycles

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

Part: CARGO TRACK — CORRODED (BS 1139) · corrosion level 2 · airframe 71,170 hrs · 16,938 cycles

MAIN DECK CARGO TRACK BS 1139 X 8.5L FLANGE FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 71,170 hrs · 16,938 cycles

CABIN MAIN DECK CARGO COMPARTMENT LT STATION 6 - 70 X=8.5 SEAT TRACK FLANGE FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FUEL CELL — CORRODED (CENTER) · airframe 71,170 hrs · 16,938 cycles

UPPER CARGO BAY UNDER FLOOR AREA RT BS 1215. CTR TANK TOP SURFACE FOUND WITH CORRODED. CORROSION REMOVED IAW SRM 51-21-01 AND FOUND WITHIN LIMITS IAW SRM 57-10-01 FIGURE 101. REPAIR CLASSIFED AS MINOR IAW GMM 6-2-100.

Part: STOP FITTING — CRACKED (R3 DOOR) · airframe 71,170 hrs · 16,938 cycles

MAIN DECK CARGO COMPARTMENT R3 DOOR PLUG NR 5 DOOR BEAMS TO FITTING FOUND CRACKED. THE STOP FITTING WAS REMOVED AND REPLACED IAW SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: STOP FITTING — CRACKED (L3 DOOR) · airframe 71,170 hrs · 16,938 cycles

CABIN MAIN DECK CARGO COMPARTMENT L3 DOOR PLUG NR 1 DOOR BEAM STOP FITTING FOUND CRACKED. STOP FITTING REMOVED AND REPLACED IAW SRM 51-31-01. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.

Part: STOP FITTING — CRACKED (R3 DOOR) · airframe 71,170 hrs · 16,938 cycles

MAIN DECK COMPARTMENT R3 DOOR PLUG NR 2 DOOR BEAM STOP FITTING FOUND CRACKED. THE STOP FITTING REMOVED & REPLACED IAW SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STOP FITTING — CRACKED (L3 DOOR) · airframe 71,170 hrs · 16,938 cycles

CABIN MAIN DECK COMPARTMENT L3 DOOR PLUG NR 4 DOOR BEAM STOP FITTING FOUND CRACKED. THE STOP FITTING WAS REMOVED & REPLACED IAW SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100.

Part: CARGO TRACK — DAMAGED (FUSELAGE) · airframe 71,170 hrs · 16,938 cycles

CABIN MAIN DECK CARGO BAY RT STATION 6 - 40, X= -47.5 CARGO TRACK CROWN AREA FOUND DAMAGED. REPAIRED IAW SRM 53-00-52 FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: CARGO TRACK — CORRODED (ZONE 200) · airframe 71,170 hrs · 16,938 cycles

MAIN DECK CARGO RT BS 6 - 10, X= -8.5 CARGO TRACK CROWN FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-52 FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.

Part: RECEPTACLE — UNSECURE (L1 DOOR) · airframe 70,104 hrs · 16,598 cycles

ENTRY DOOR L1 DISARMED LIGHT HANGING LOOSE FROM RECEPTACLE. REPLACED L1 DOOR DISARM LIGHT RECEPTACLE IAW SWP & PERFORMED OPERATIONAL CHECK STEPS 1 & 2 IAW AMM 52-10-01-2. OPERATIONS CHECKED GOOD.

Part: PUMP — FAILED (FUEL TRANSFER) · airframe 69,769 hrs · 16,491 cycles

LEVEL OFF AT FL350, RECEIVED LEVEL ONE TANK 3 TIP TRAPPED & TANK 3 FUEL QTY LOW. SHORTLY FOLLOWED BY FUEL CROSSFEED 3 DISAGREE. TRANSFER PUMP INOPERATIVE. TAIL FUEL MANAGEMENT INOPERATIVE. OPS NOT AUTHORIZED ABOVE 78 N LAT OPERATE FSC IN MANUAL. RESET CB`S FOR NR 3 TRANSFER PUMP & PERFORMED RTS OF THE FSC IAW MM 28-08-01-5, TEST PASSED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 69,638 hrs · 16,449 cycles

EMERGENCY LIGHT 1 LOW ILLUMINATED AFTER TEST. R & R BATTERY IAW MM 33-51-01-4, TEST PASSED.

Part: PILOT VALVE — FAILED (NR 2) · airframe 69,456 hrs · 16,391 cycles

NR 2 BLEED AIR SYS IN AUTO. NR 1 AND 2 PACKS CYCLE ON & OFF WITH CONTROLLER IN AUTO. IAW FIM 36-11-01, FIG 103, NO CURRENT FAULTS OR FAULTS LAST FLIGHT LEG IN PSC 1, PSC 2 OR ESC, NO SENSORS IN SENSOR READOUT X'ED OUT IN EITHER PSC. RAN NR 2 ENGINE PER JRH. OPERATED NR 2 BLEED & RAN PACKS, NR 2 BLEED CHECKED NORMAL AT IDLE. READINGS IN PSC 1 AS FOLLOWS PI2, 22 PSI, PE2, 20 PSI, PM, 18 PSI. PERFORMED A FAULT REVIEW OF PSC 2. THE PRESS REGULATOR PILOT VALVE WAS FAULTED ON THREE DIFFERENT LEGS. R & R NR 2 PRV PILOT VALVE PER MM36-12-20-4.

Part: LONGERON — CRACKED (ZONE 700) · airframe 66,608 hrs · 15,516 cycles

ON TRIMMING OF NLG TRUNNION FITTING FOUND LONGERON 49R CRACKED.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 66,608 hrs · 15,516 cycles

MAIN DECK CABIN LT BS 1521, X= 47.5 SEAT TRACK FOUND DAMAGED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 66,608 hrs · 15,516 cycles

MAIN DECK CABIN LT BS 5-20 TO 5-53, X= 75.25 SEAT TRACK FLANGE FOUND WITH CORROSION.

Part: TRUNNION — CRACKED (NLG) · airframe 66,608 hrs · 15,516 cycles

NLG RT TRUNNION FITTING FORWARD SECTION FOUND CRACKED.

Part: PANEL — CRACKED (ZONE 300) · airframe 66,608 hrs · 15,516 cycles

LOWER VERTICAL STABILIZER, NR 2 ENGINE INTAKE DUCT REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED.

Part: SEAT TRACK — DAMAGED (BS 615) · airframe 66,608 hrs · 15,516 cycles

MAIN DECK CARGO BS 615, X= -47 SEAT TRACK CROWN FOUND CHIPPED OFF.

Part: HINGE FITTING — CRACKED (ZONE 500) · airframe 66,608 hrs · 15,516 cycles

LT WING OTBD FLAP INBD FORWARD HINGE OTBD SIDE LOAD FITTING CRACKED.

Part: SLAT TRACK — CRACKED (ZONE 600) · airframe 66,608 hrs · 15,516 cycles

RT WING SLAT TRACK NR 12 LOWER CUT-OUT CRACKED.

Part: SEAT TRACK — CORRODED (BS 1259) · airframe 66,608 hrs · 15,516 cycles

MAIN DECK CABIN LEFT STATION 1259, X= 75.25 SEAT TRACK FLANGE FOUND WITH CORROSION.

Part: FRAME — CRACKED (BS 2007 BULKHEAD) · airframe 66,608 hrs · 15,516 cycles

AFT FUSELAGE COMPARTMENT FORWARD BULKHEAD RT CHORD FOUND CRACKED AT STA 2007.

Part: SKIN — DENTED (NR 8 SLAT) · airframe 66,608 hrs · 15,516 cycles

RT NR 8 SLAT FOUND DENTED AT L/E AREA.

Part: SKIN — CORRODED (ZONE 500) · airframe 66,608 hrs · 15,516 cycles

LEFT WING LOWER T/E ACCESS 541JB CUT-OUT FORWARD FOUND CORROSION.

Part: MOUNT — CRACKED (ZONE 100) · airframe 66,608 hrs · 15,516 cycles

FORWARD AVIONICS COMPARTMENT CEILING. RT OBSERVER SEAT MOUNTING BASE PLATE FORWARD SECTION FOUND CRACKED.

Part: MOTOR — CRACKED (HORISONTAL STAB) · airframe 65,552 hrs · 15,247 cycles

HYD SYS 3 FAILED DURING CLIMBOUT , FAIRLY RAPID LOSS OF QTY, HISTORY HAD RT OTBD FLAP DROOP SITTING ON RAMP. RAMP MAINT CHECKED ALL NORMAL BUT HYD/RMP AUX PUMPS USED TO REMOVE FLAP DISAG. MANUALLY DROPPED LANDING GEAR IAW RED TAB PROCEDURE. AFTER BLOCK-IN OTBD FLAPS INDICATE DROOP TO SHOW 0-9. COMPLETED REPLACEMENT OF NR 3 HYD SYS HORIZONTAL STAB MOTOR IAW AMM 27-43-30-4. LEAK AND OPS CHECK OF HORIZONTAL STAB MOTORS GOOD IAW AMM 27-40-00-5. REMOVED ALL WORK MATERIALS FROM HORIZONTAL STAB AREA. RESET LANDING GEAR ALTERNATE EXTENSION HANDLES IAW AMM 32-32-00-5. OK FOR SERVICE.

Part: ACCESS PANEL — MISSING (WING) · airframe 62,916 hrs · 14,563 cycles

DURING PRE-FLIGHT, FOUND ACCESS PANEL 633AB, NR 3 FWD FUEL BOOST PUMP ACCESS PANEL MISSING. COMPLIED WITH EA 1-2820-155476, REV, POS P3. INSTALLED NEW BLOCK AND NEW DOOR IAW AMM 28-22-01-4. ACFT OK FOR SERVICE.

Part: FLOORBEAM — CRACKED (BS 1761) · airframe 61,038 hrs · 14,109 cycles

MAIN DECK CARGO FLOORBEAM LOWER CHORD AT STA 1761, "X" = -107 FOUND DEFORMED, CRACKED. REPAIRED AS PER E.A. 1-5310-143855, PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 111.

Part: SKIN — CORRODED (NR 2 NACELLE) · airframe 61,038 hrs · 14,109 cycles

ENGINE NR 2 NOSE INLET COWL, NOSE LIP SKIN INNER SURFACE PITTING CORROSION BETWEEN 6 O'CLOCK AND 7 O'CLOCK POSITION. REMOVED AND REPAIRED AS PER E.A. 1-7110-143854, PART 1, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.

Part: SKIN — CRACKED (ZONE 600) · airframe 61,038 hrs · 14,109 cycles

05 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT STA XORS= 683.4 TO XORS= 713.6. CARRIED OUT RECTIFICATION AS PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SUPPORT BEAM — CRACKED (PAX DOOR) · airframe 61,038 hrs · 14,109 cycles

MAIN DECK L3 DOOR NR2 STOP SUPPORT BEAM FOUND CRACKED AT AFT STOP. STOP. MAIN DECK L3 DOOR NR 2 STOP CRACKED SUPPORT BEAM REMOVED AND REPLACED AS PER SRM 51-31-01, REVISION 45 AND E.A.1-5210-143856, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — CRACKED (ZONE 500) · airframe 61,038 hrs · 14,109 cycles

08 EA, FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT STA XORS= 683.4 TO XORS= 713.6. CARRIED OUT RECTIFICATION AS PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,038 hrs · 14,109 cycles

LOWER FWD CARGO COMPARTMENT BILGE AREA STA 6-30 TO STA 6-50, LONGERON 42 RT TO LONGERON 43 RT INTERCOASTAL FOUND CRACKED. INTERCOSTAL REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. NEW INTERCOSTAL FABRICATED AS PER DRAWING ACA7049 REVISION G. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CRACKED (ZONE 200) · corrosion level 2 · airframe 61,038 hrs · 14,109 cycles

CABIN - UPON REMOVAL OF FLOOR PANELS FOR REPAIR ACCESS ON RT STA 1781 TO STA 1801, X= -107.25 SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 61,038 hrs · 14,109 cycles

LOWER CTR CARGO COMPARTMENT TUNNEL, STATION 5-123, LONGERON 35 LT, SPLICE FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, REVISION 45. NEW SPLICE FABRICATED AS PER DRAWING A5A7114, REVISION J. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 61,038 hrs · 14,109 cycles

LOWER CTR CARGO COMPARTMENT - TUNNEL STA 5-123, LONGERON 38 LT SPLICE FITTING FOUND WITH CRACK. REMOVED AND REPLACED AS PER SRM 51-33-01, REVISION 45. NEW SPLICE FABRICATED AS PER DRAWING A5A7114, REVISION J. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON SPLICE — CRACKED (ZONE 200) · airframe 61,038 hrs · 14,109 cycles

MAIN DECK - CRACK FOUND DURING X-RAY INSP AT STA 5-0, LONG 10R, LONGERON SPLICE. CRACK LENGTH APPROX 0.8". REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1069 TO STATION 1129, "X" = -27.5 AS PER SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 111.

Part: LONGERON SPLICE — CRACKED (BS 1129 L42L) · airframe 61,038 hrs · 14,109 cycles

LWR FWD CARGO COMPARTMENT, STATION 1129, LONGERON 42 LT, LONGERON SPLICE WITH CRACK. LONGERON SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01, REVISION 45. NEW SPLICE FABRICATED AS PER DRAWING ADA8424 REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SPAR CAP — CORRODED (RT WING) · airframe 61,038 hrs · 14,109 cycles

RT WING T/E UPPER AFT SPAR CAR TOP SURFACE FOUND CORRODED AT WING STA XORS 980. SPAR CAP CORROSION REPAIRED AS PER E.A. 1-5710-143520, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 61,038 hrs · 14,109 cycles

CABIN - RT STA 1079 TO STA 1099, X= -27.5 SEAT TRACK FOUND CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1069 TO STATION 1129, "X" = -27.5 AS PER SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 111.

Part: FRAME — DENTED (ZONE 200) · airframe 61,038 hrs · 14,109 cycles

CABIN - RT STA 1741, LONGERON 11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 111. REPETITIVE INSPECTION REQUIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 45.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 61,038 hrs · 14,109 cycles

LOWER CENTER CARGO COMPARTMENT - BILGE AREA, STATION 5-123, LONGERON 43, RT SPLICE FITTING FOUND CRACKED. CRACKED SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01, REVISION 45. NEW SPLICE FABRICATED AS PER DRAWING A5A7114, REVISION J. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,038 hrs · 14,109 cycles

MAIN DECK CARGO STA 1741, X= -75.25 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1671 TO STATION 1751, "X" = -75.25 AS PER SRM 53-00-52 FIGURE 201, REPAIR 1, REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 111.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 61,038 hrs · 14,109 cycles

LOWER FWD CARGO COMPARTMENT - STA 6-30 TO SATION 6-50 BETWEEN LONGERON 42 LT TO LONGERON 43 LT, INTERCOSTAL FOUND CRACKED. INTERCOSTAL REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. NEW INTERCOSTAL FABRICATED AS PER DRAWING ACA7049 REVISION G. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 61,038 hrs · 14,109 cycles

LWR FWD CARGO COMPARTMENT - BILGE AREA STA 6-10 TO STA 6-30 BETWEEN LONGERON 42 LT AND LONGERON 43 LT INTERCOSTAL CRACKED. INTERCOSTAL REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. NEW INTERCOSTAL FABRICATED AS PER DRAWING ACA7049 REVISION G. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 61,038 hrs · 14,109 cycles

LWR CTR CARGO COMPARTMENT - STA 5-123, LONGERON 33 RT SPLICE FITTING, CRACKED. SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 45. NEW SPLICE FITTING FABRICATED AS PER DRAWING A5A7112 REVISION D. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.

Part: SEAT TRACK — CORRODED (BS 1663) · corrosion level 2 · airframe 61,038 hrs · 14,109 cycles

MAIN DECK STA 1663 "X" = -75.25 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-00-52 FIGURE 201 REPAIR 1, REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 111.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,565 hrs · 14,001 cycles

R-1 EMERGENCY LIGHT INOP. INSTALLED LWR PORTION ON RT DOOR ARTICULATING SLIDING CEILING PANEL AND EMERGENCY EXIT LIGHT REF EA 1-5210-146019 AND MM 25-23-23-4. LIGHT OPS CHECKED NORMAL. REF WRI 52-10-6451 FOR REPLACEMENT OF UPPER PORTION OF PANEL AND WRI 52-10 6454 FOR REPAIR OF LOWER PORTION OF PANEL. COMPLIED WITH PARTS 1 AND 2 OF EA 1-5210-146019. A/C OK FOR SERVICE.

Part: MSC — MALFUNCTIONED (SMOKE DETECTION) · airframe 56,903 hrs · 13,123 cycles

ON DEPARTURE PASSING 11000 FT GOT A LEVEL 3 INCH CABIN "SMOKE" ALERT. IT STAYED ON FOR ABOUT 10SEC, WENT OUT FOR ABOUT 10SEC CAME ON AGAIN FOR ABOUT 20SEC THEN WENT OUT AND STAYED OUT FOR REMAINING OF THE FLT. WE DID THE PHASE 1 AND RAN THE QRH PROCEDURE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. IAW FIM26-15-01-00 AND SSM26-15-00,T/S FOUND ALL MAIN DECK CARGO SMOKE DETECTORS OK AT THIS TIME. FOR PERCAUTION, REMOVED AND REPLACED MSC IAW MM31-42-01, PERFORMED MSC R-T-S TEST AND CARGO FIRE MANUAL TEST COUPLE TIMES, ALL TEST PASSED. ACFT OK FOR SVC.

Part: MOUNT — CORRODED (RT TE FLAP HINGE) · airframe 55,704 hrs · 12,837 cycles

CORROSION, RT WING OUTBOARD FLAP OUTBOARD HINGE UPPER MOUNT FWD AND AFT SURFACE AT WING SIDE. REWORKED AS PER EA 1-5750-129202, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: DOUBLER — CORRODED (ZONE 600) · airframe 55,704 hrs · 12,837 cycles

RT WING TRAILING EDGE LOWER WING DOUBLER BELOW NR 1 SPOILER ACTUATOR AREA FOUND WITH SEVERAL AREA CORROSION. COMPLIED WITH EA 1-5710-127841. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = 56 FOUND WITH CORROSION. COMPLIED WITH FEDEX EA 1-5710-129209, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = -25 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-129209, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR AREA, TOP SURFACE OF AUX TANK AT STA 1227 X = -104 FOUND WITH CORROSION. CORROSION ON MAIN DECK CARGO FLOOR AREA, TOP SURFACE OF AUX TANK REPAIRED AS PER E.A.1-5710-129209, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = 60 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-129209, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = -14 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-129209, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = 49 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-129209, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = -35 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-129209, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1219 X = -100 FOUND WITH CORROSION. COMPLIED WITH EA 1-5710-129209. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = -54 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-129209, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = 64 FOUND WITH CORROSION. COMPLIED WITH EA 1-5710-129209, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = 88 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-129209, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: FUEL TANK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO FLOOR, TOP SURFACE OF AUX TANK AT STA 1227 X = 81 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-129209, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 55,704 hrs · 12,837 cycles

FUSELAGE EXTERIOR SKIN, EXISTING REPAIR OBSERVED AT STA 495 TO STA 515, LONGERON 40R TO LONGERON 42R. EXISTING REPAIR AT FUSELAGE EXTERIOR SKIN STA 495 TO 515 LONGERON 40R TO LONGERON 42R EVALUATED AND FOUND NOT CARRIED OUT IAW SRM REPAIR. EXISTING REPAIR DOUBLER AT FUSELAGE EXTERIOR SKIN STA 495 TO 515 LONGERON 40R TO LONGERON 42R. REMOVED AND REPLACED AS PER SRM 53-20-00 FIGURE 6 VOLUME I REVISION 40. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION AT 7,500 CYCLES AND REPETITIVE INSPECTIONS AT EVERY 4,750 CYCLES FEDEX EO NR 1-5100-7-5001 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 55,704 hrs · 12,837 cycles

EXISTING REPAIR, RT WING NR 1 SLAT LEADING EDGE AT XIS213.344 FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-10-00 VOL 1 FIG 37 REV 40. REPAIR CARRIED OUT AS PER EA 1-5740-127840, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 55,704 hrs · 12,837 cycles

EXISTING REPAIR, FUSELAGE SKIN STA 1955-1963 S48R-S50R FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 53-20-00 VOL 1 FIG 2 REV40. CARRIED OUT REPAIR AS PER SRM 53-20-00 FIGURE 2 VOLUME I REVISION 40. EO 1-5100-7-5001, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO COMPARTMENT FLOOR, SEAT TRACK X = -8.5 FOUND WITH FLANGE CORRODED AT STA 1139. MAIN DECK CARGO COMPARTMENT CORRODED SEAT TRACK AT STA 1139 X = -8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1129 TO STA 1179 X = -8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 500) · airframe 55,704 hrs · 12,837 cycles

LEFT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT FORWARD AND AFT SURFACES FOUND CORROSIONS. LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT FORWARD AND AFT SURFACES REWORKED AS PER FEDEX EA NR 1-5750-129203, TITLE: WINGS - FLIGHT SURFACES, LT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) REPAIR. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO COMPARTMENT FLOOR, SEAT TRACK X = 8.5 FLANGE FOUND CORRODED AT STA 1139. CORROSION ON MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 1139 X = 8.5 REMOVED AS PER SRM 51-21-01 VOLUME II REVISION 40. ORIGINAL THICKNESS = 0.080", REMAINING THICKNESS = 0.075 INCH, MATERIAL REMOVED 0.005 INCH AND FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MINOR AS PER AS PER GMM 6-2-100 REVISION 107.

Part: SKIN — CRACKED (ZONE 500) · airframe 55,704 hrs · 12,837 cycles

FIVE FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-127835, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: SKIN — CRACKED (ZONE 600) · airframe 55,704 hrs · 12,837 cycles

FIVE FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-127836, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 55,704 hrs · 12,837 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR HOLE FOUND CORROSIONS. REWORKED AS PER EA 1-5750-128686, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: HINGE BRACKET — CORRODED (ZONE 600) · airframe 55,704 hrs · 12,837 cycles

RIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE FOUND CORROSIONS. REWORKED AS PER EA 1-5750-129202, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND ON FIRST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 3 LOWER JAMB FITTING AT HOLE A. REPAIRED AS PER EA 1-5310-129206, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40 AND BUSHING REPAIR CARRIED OUT FOR FIRST AND SECOND LAYER WEBS AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40 AND BUSHING REPAIR CARRIED OUT FOR FIRST AND SECOND LAYER WEBS AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 6 LOWER JAMB FITTING AT HOLE A. COMPLIED WITH E.A. 1-5310-129206, REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 REV. 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 3 LOWER JAMB FITTING AT HOLE B. COMPLIED WITH EA 1-5310-129206. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40 AND BUSHING REPAIR CARRIED OUT FOR FIRST AND SECOND LAYER WEBS AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 107.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO COMPARTMENT FLOOR, SEAT TRACK X = 8.5 AT STA 6-40, CROWN BASE FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: WEB — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND ON FIRST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 1 LOWER JAMB AT HOLE B AND C. REPAIRED AS PER EA 1-5310-129206, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: STRUCTURE — CORRODED (ZONE 500) · airframe 55,704 hrs · 12,837 cycles

LEFT WING, TRAILING EDGE UPPER CAP UPPER SURFACE FOUND CORROSIONS AT XORS 984. COMPLIED WITH EA 1-5710-129201. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLES A AND D. COMPLIED WITH E.A. 1-5310-129206, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40 AND BUSHING REPAIR CARRIED OUT FOR FIRST AND SECOND LAYER WEBS AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND ON FIRST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 5 LOWER JAMB FITTING AT HOLE B. REPAIRED AS PER EA 1-5310-129206, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACKED INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40 AND BUSHING REPAIR CARRIED OUT FOR FIRST AND SECOND LAYER WEBS AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND ON FIRST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLES A AND D. COMPLIED WITH E.A. 1-5310-129206. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40 AND BUSHING REPAIR CARRIED OUT FOR FIRST AND SECOND LAYER WEBS AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SEAT TRACK — CORRODED (BS 1205) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK CARGO COMPARTMENT FLOOR, SEAT TRACK X = -75.25 FLANGE FOUND CORRODED AT STA 1205. MAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK FLANGE AREA REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 6 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 40 AND BUSHING REPAIR CARRIED OUT FOR FIRST AND SECOND LAYER WEBS AS PER SRM 53-50-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: WEB — CORRODED (DOOR FRAME) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 1 LOWER JAMB AT HOLE C. REPAIRED AS PER EA 1-5310-129206, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 55,704 hrs · 12,837 cycles

CRACK INDICATION FOUND APPROXIMATELY 0.250 INCH IN LENGTH DURING HFEC INSPECTION ON LEFT SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP. REPAIR CARRIED OUT AS PER SRM 55-20-00 FIGURE 3 VOLUME I REVISION 40. REPAIR PARTS INSTALLED AS PER SRM 51-33-01 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SKIN — CRACKED (ZONE 200) · airframe 55,704 hrs · 12,837 cycles

MAIN DECK FORWARD PAX/CREW ENTRY DOOR R1, EXTERIOR SURFACE FOUND WITH CRACKS AT AFT UPPER EDGE. REPAIR CARRIED OUT AS PER SRM 52-10-00 FIGURE 10 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.

Part: SKIN — CRACKED (ZONE 600) · airframe 55,704 hrs · 12,837 cycles

RIGHT WING LEADING EDGE NR 3 SLAT MOST OUTBOARD TRACK CUT-OUT INBOARD CORNER SKIN FOUND CRACKED. AREA TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,082 hrs · 11,812 cycles

MAIN DECK, SEAT TRACK BELOW FLOOR PANEL NR 281HF LOWER SURFACE FOUND CORROSION AROUND FASTENER HOLE AT STA 1731 LBL 75. MAIN DECK, SEAT TRACK BELOW FLOOR PANEL NR 281HF LOWER SURFACE CORROSION AROUND FASTENER HOLE AT STA 1731 LBL 75 REPAIRED AS PER FEDEX EA NR 1-5310-117060, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK, SEAT TRACK BELOW FLOOR PANEL NR 281CS LOWER SURFACE FOUND CORROSION AT STA 5-83 AND STA 1531. REPAIRED AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT, AFTER FLOOR PANEL REMOVAL AT ABOUT STA 1558 LBL 8 SEAT TRACK FLOOR PANEL SUPPORT FLANGE FOUND CORRODED. REPAIRED AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (AUX TANK) · airframe 51,082 hrs · 11,812 cycles

CABIN, AT ABOUT STA 1228 LBL 30 TO LBL 75 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REPAIRED AS PER FEDEX EA. 1-5710-117064, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (AUX TANK) · airframe 51,082 hrs · 11,812 cycles

CABIN, AT ABOUT STA 1228 RBL 40 TO RBL 54 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5710-117062, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (AUX TANK) · airframe 51,082 hrs · 11,812 cycles

CABIN, AT ABOUT STA 1234 LBL 18 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REMOVED CORROSION AS PER SRM 51-21-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT, AFTER FLOOR PANEL REMOVAL AT ABOUT STA 1661 TO STA 1701 SEAT TRACK FLOOR PANEL SUPPORT FLANGE FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5310-117060. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (AUX TANK) · airframe 51,082 hrs · 11,812 cycles

CABIN, AT ABOUT STA 1228 RBL 65 TO RBL 80 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5710-117063. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SKIN — CORRODED (AUX TANK) · airframe 51,082 hrs · 11,812 cycles

CABIN, AT ABOUT STA 1228 LBL 8 TO RBL 8 UPPER AUX TANK UPPER SKIN FOUND CORRODED. REPAIRED AS PER FEDEX EA 1-5710-117061, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1280 TO 1321 LBL 8 SEAT TRACK FLOOR PANEL SUPPORT FLANGE FOUND CORRODED. REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. NEW SEAT TRACK AND SPLICES REWORKED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE BRACKET — CORRODED (T/E FLAP) · airframe 51,082 hrs · 11,812 cycles

RIGHT WING OUTBOARD FLAP OUTBOARD HINGE BRACKET OUTBOARD NR 3 BOLT HOLE FOUND CORROSION. CORROSION REMOVED AS PER BOEING SOPM 20-11-02, REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5750-117054. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1280 TO 1321 RBL 8 SEAT TRACK FLOOR PANEL SUPPORT FLANGE FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT, AFTER FLOOR PANEL REMOVAL SEAT TRACK FLOOR SUPPORT FLANGE AT STA 1741 TO 1821 RBL 47 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE — CORRODED (RT WING TE FLAP) · airframe 51,082 hrs · 11,812 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FORWARD INBOARD NR 2 BOLT HOLE, FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-50-00-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · airframe 51,082 hrs · 11,812 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING AFT STRUT FORWARD BOLT HOLE, FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-30-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1485-1520) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1485 TO STA 1520 RBL 75 SEAT TRACK SUPPORT FLOOR PANEL FLANGE FOUND CORRODED. AREA REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM BS 1451-1531 RBL 75 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ACCESS DOOR — CRACKED (BS 683-713) · airframe 51,082 hrs · 11,812 cycles

1 EACH FASTENER HOLE FOUND DAMAGED DURING HFEC OPEN HOLE INSPECTION ON LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683 AND STA 713. REPAIRED AS PER FEDEX EA 1-5710-117058, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ACCESS DOOR — CRACKED (LT WING) · airframe 51,082 hrs · 11,812 cycles

3 EACH CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683 AND STA XORS 713 FASTENER HOLES. REPAIRED AS PER FEDEX EA 1-5710-117058, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · airframe 51,082 hrs · 11,812 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FORWARD OUTBOARD NR 3 BOLT HOLE, FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-30-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ACCESS DOOR — CRACKED (RT WING) · airframe 51,082 hrs · 11,812 cycles

2 EACH CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683 AND STA XORS 713 FASTENER HOLES. REPAIRED AS PER FEDEX EA 1-5710-117059. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAPS) · airframe 51,082 hrs · 11,812 cycles

RIGHT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FORWARD OUTBOARD NR 2 BOLT HOLE, FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-30-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1059) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1059 RBL 47 SEAT TRACK FOUND DAMAGED. REMOVED AND REPLACED AS PER SRM 53-70-00. NEW SEAT TRACK REWORKED AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT AT ABOUT STA 889 LBL 8 SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 869 TO STA 909 LBL 8 AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 900) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK COMPARTMENT AT ABOUT STA 900 RBL 47 SEAT TRACK FOUND DAMAGED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (BS 1821) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1821 RBL 75 SEAT TRACK FOUND CORROSION. REPAIRED BY REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: LOCK FASTENER — CRACKED (ZONE 300) · airframe 51,082 hrs · 11,812 cycles

EMPENNAGE AFT FUSELAGE COMPARTMENT UPPER DOG HOUSE AT STA 2102 FRAME CLIP AROUND 1 LOCK FASTENER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1280) · airframe 51,082 hrs · 11,812 cycles

MAIN DECK CARGO COMPARTMENT AT ABOUT STA 1280 LBL 47 SEAT TRACK FOUND DAMAGED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1249 TO STA 1331 LBL 47 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STOP FITTING — CRACKED (RT WING TE FLAP) · airframe 51,082 hrs · 11,812 cycles

RIGHT WING OUTBOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED. RIGHT HAND WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 30-4. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. REFER TO SNRM N00654 FOR WORK DETAILS.

Part: TRUNNION — CRACKED (NLG) · airframe 51,082 hrs · 11,812 cycles

LEFT NOSE LANDING GEAR TRUNNION FITTING FWD LOWER CORNER FOUND CRACKED. REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRUCTURE — DENTED (NR 4 SLAT) · airframe 51,082 hrs · 11,812 cycles

RIGHT WING NR 4 SLAT LEADING EDGE FOUND DENT. REPAIR CARRIED OUT AT RIGHT HAND WING NR 4 SLAT LEADING EDGE DENTED AREA AS PER SRM 57-10-00 FIGURE 5 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 51,082 hrs · 11,812 cycles

RIGHT WING LEADING EDGE ACCESS PANEL 619CB INBOARD FORWARD CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 47,432 hrs · 10,962 cycles

ON ROTATION SUSPECT BIRD STRIKE, MODERATE ENGINE VIBRATION EVM COMP 5.0 CARRIED-OUT BIRDSTRIKE INSPECTION CHECK PER MM 5-52-01-6 1 - SATISFACTORY; THIS ENGINE WAS APPROVED FOR REPLACEMENT. REPLACED THE NR 1 ENGINE AND NOSE COWL.

Part: SENSE LINE — BROKEN (NR 2 ENGINE) · airframe 47,367 hrs · 10,947 cycles

AFTER T/O RECEIVED LVL 1 ALERT ANTI ICE SENSOR FAIL WHEN ANTI ICE SELECTED ON RECEIVED BLEED 2 OFF LVL 1 ALERT PACK 2 OFF LVL 1 ALERT. FOUND SENSE LINE AT HIGH STAGE VALVE BROKE IN HALF. REPAIRED NR 2 ENG HIGH STAGE SENSE LINE UTILIZING PNEUMATIC FLEX LINE AND NECESSARY FITTINGS PER EA 1-3610-98999 PART 1. RAN ENG PER JRH NO FAULTS NOTED. A/C OK FOR SERVICE.

Part: INTERCOSTAL — MISSING (FUSELAGE) · airframe 46,815 hrs · 10,820 cycles

WHILE ACCOMPLISHING EA 1-2328-102981, INTERCOSTAL P/N: AFA8905-525 FOUND MISSING. FABRICATED NEW INTERCOSTAL AND CLIP AS PER DRAWING AFA8905 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: HINGE FITTING — CRACKED (T/E FLAP) · airframe 46,815 hrs · 10,820 cycles

LEFT HAND WING OUTBOARD FLAP INBOARD MID HINGE SUPPORT FITTING FOUND CRACKED. LEFT HAND WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30. OUTBOARD FLAP VANE ADJUSTMENT AND TEST CARRIED AS PER AMM 27-50-32-5. OUTBOARD FLAP ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-30-5.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 46,815 hrs · 10,820 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA 1853 X = 27.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FINGER DOUBLER — CRACKED (ZONE 600) · airframe 46,815 hrs · 10,820 cycles

RIGHT WING LEADING EDGE CAVITY THROUGH ACCESS PANEL 619CB CEILING AREA FINGER DOUBLER AS MARKED. REPAIRED AS PER FEDEX EA 1-5730-100703.

Part: STRUCTURE — CRACKED (ZONE 500) · airframe 46,815 hrs · 10,820 cycles

LT WING LEADING EDGE TELESCOPIC DUCT CUTOUT INBOARD AND OUTBOARD CORNER FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-100713. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1341) · airframe 46,815 hrs · 10,820 cycles

SEAT TRACK STA 1341 X=-47.5 FOUND DAMAGED. REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FINGER DOUBLER — CRACKED (ZONE 500) · airframe 46,815 hrs · 10,820 cycles

LT WING LEADING EDGE CAVITY THROUGH ACCESS PANEL 519CB CEILING AREA FINGER DOUBLER CRACKED AS MARKED AT XOS 623. REPAIRED AS PER FEDEX E.A. 1-5730-100687. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1371) · airframe 46,815 hrs · 10,820 cycles

SEAT TRACK STA 1371 X=-47.5 FOUND DAMAGED. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRUCTURE — CRACKED (ZONE 600) · airframe 46,815 hrs · 10,820 cycles

RIGHT WING LEADING EDGE TELESCOPIC DUCT CUTOUT INBOARD AND OUTBOARD CORNER FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-100714. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FINGER DOUBLER — CRACKED (ZONE 600) · airframe 46,815 hrs · 10,820 cycles

RIGHT WING LEADING EDGE CAVITY THROUGH ACCESS PANEL 619CB CEILING AREA FINGER DOUBLER AS MARKED AT XOS 625. REPAIRED AS PER FEDEX E.A. 1-5730-100703.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 46,815 hrs · 10,820 cycles

MAIN DECK SEAT TRACK AT STA 1085 X = -47.5 FOUND WITH THE LOCK CROWN DAMAGED. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW REPAIR SEAT TRACK FABRICATED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FINGER DOUBLER — CRACKED (ZONE 500) · airframe 46,815 hrs · 10,820 cycles

FOUND LT WING LEADING EDGE CAVITY THRU ACCESS PANEL 525AB CEILING AREA FINGER DOUBLER CRACKED AT XOS 699. REPAIRED AS PER FEDEX E.A. 1-5730-100701. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FINGER DOUBLER — CRACKED (ZONE 500) · airframe 46,815 hrs · 10,820 cycles

LT WING LEADING EDGE CAVITY THRU ACCESS PANEL 519CB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS 613. REPAIRED AS PER FEDEX E.A. 1-5730-100687. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FINGER DOUBLER — CRACKED (ZONE 600) · airframe 46,815 hrs · 10,820 cycles

RT WING LEADING EDGE CAVITY THRU ACCESS PANEL 619DB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS 680. REPAIRED AS PER FEDEX E.A. 1-5730-100704.

Part: FINGER DOUBLER — CRACKED (ZONE 500) · airframe 46,815 hrs · 10,820 cycles

LT WING LEADING EDGE CAVITY THRU ACCESS PANEL 526DB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS 883. REPAIRED AS PER FEDEX E.A. 1-5730-100702. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 46,815 hrs · 10,820 cycles

RT WING LEADING EDGE CAVITY THRU ACCESS PANEL 619DB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS667. REPAIRED AS PER FEDEX E.A. 1-5730-100704. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 46,815 hrs · 10,820 cycles

RT WING LEADING EDGE CAVITY THRU ACCESS PANEL 625AB CEILING AREA FINGER DOUBLER CRACKED AT XOS 692. REPAIRED AS PER FEDEX EA 1-5730-100704. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: FINGER DOUBLER — CRACKED (ZONE 500) · airframe 46,815 hrs · 10,820 cycles

LT WING LEADING EDGE CAVITY THRU ACCESS PANEL 525DB CEILING AREA, FINGER DOUBLER CRACKED AT XOS 705. REPAIRED AS PER FEDEX E.A.1-5730-100701. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 46,815 hrs · 10,820 cycles

MAIN DECK SEAT TRACK AT STA 810 X = 27.50 FOUND WITH THE LOCK CROWN DAMAGED. REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: FINGER DOUBLER — CRACKED (ZONE 600) · airframe 46,815 hrs · 10,820 cycles

RT WING LEADING EDGE CAVITY THRU ACCESS PANEL 619DB CEILING AREA, FINGER DOUBLER FOUND CRACKED AT XOS 643. REPAIRED AS PER FEDEX EA 1-5730-100703. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.

Part: LONGERON SPLICE — CRACKED (ZONE 100) · airframe 46,815 hrs · 10,820 cycles

CTR CARGO COMPARTMENT TUNNEL, LONGERON 37R SPLICE AT STA 1531 FOUND CRACKED. REMOVED AS PER SRM 51-33-01 VOL.II. NEW LONGERON SPLICE FABRICATED AS PER DWG NR A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER SPLICE — CRACKED (ZONE 100) · airframe 46,815 hrs · 10,820 cycles

CENTER CARGO COMPARTMENT, LONGERON 38R STA 1531 SPLICE FOUND CRACKED. REMOVED AS PER SRM 51-33-01 VOL.II. NEW LONGERON SPLICE FABRICATED AS PER DWG. NO. A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: DOUBLER — CHIPPED (ZONE 100) · airframe 46,815 hrs · 10,820 cycles

CENTER CARGO DOOR AFT CUTOUT LOWER CORNER EXISTING DOUBLER FOUND CHIPPED. REMOVED AS PER SRM 51-33-01 VOLUME II AND NEW REPAIR DOUBLER FABRICATED AND INSTALLED AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 500) · airframe 46,815 hrs · 10,820 cycles

HFEC INSPECTION CARRIED OUT ON LT WING STRINGER END OF STRINGER 14L (XORS 521) FOUND CRACK (APPROX 12" LONG) AS MARKED. REPAIRED WITH SPLICE ANGLE AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (LT WING) · airframe 46,815 hrs · 10,820 cycles

FOUND CRACK FOUND APPROX 12" IN LENGTH DURING HFEC INSPECTION ON LT WING TANK AT THE END OF STRINGER 10 (UPPER STRINGER) AT APPROX XORS 760. REPAIRED WITH ANGLE AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.

Part: STRINGER — CRACKED (ZONE 600) · airframe 46,815 hrs · 10,820 cycles

CRACK FOUND APPROX 10" IN LENGTH DURING HFEC INSPECTION ON RT WING TANK AT THE END OF STRINGER 11 (UPPER STRINGER) AT APPROX WING STA XORS 704. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,237 hrs · 9,790 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK CROWN FOUND CHAFED AT STA Y= 965, X= -47. MAIN DECK CARGO COMPARTMENT, CHAFED SEAT TRACK AT STA Y= 949 TO Y= 1009, X= -47 TRIMMED, REMOVED AND REWORKED SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,237 hrs · 9,790 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK CROWN FOUND CHAFED AT STA Y= 965, X= -47. MAIN DECK CARGO COMPARTMENT, CHAFED SEAT TRACK AT STA Y= 949 TO Y= 1009, X= -47. TRIMMED, REMOVED AND REWORKED SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I FIGURE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 42,237 hrs · 9,790 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK CROWN AT RIGHTHAND STA Y= 1090, X= -47 FOUND ELONGATED. MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT RIGHTHAND STA Y= 1049 TO Y= 1129 , X= -47 TRIMMED, REMOVED AND REWORKED SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: VANE — WORN (ZONE 600) · airframe 42,237 hrs · 9,790 cycles

RIGHT HAND WING, INBOARD FLAP VANE, LEADING EDGE, ABOUT 25 INCHES (FROM OUTBOARD TO INBOARD). FOUND WITH CHAFFING DAMAGE OF 3 INCHES DIAMETER. REMOVED AND REPLACED PER AMM 27-50-22-02. ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-50-22-05.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 42,237 hrs · 9,790 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 1100, X= 47 FOUND WITH CHAFED MARK. REMOVED PER SRM 53-70-00 VOLUME I, FIGURE 1. FABRICATED SEAT TRACK AND SPLICES INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,237 hrs · 9,790 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 5-90, X= 8.5 FOUND WITH CORROSION. REMOVED AT EXISTING SPLICE PER SRM 51-33-01 VOLUME II. REWORKED SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,237 hrs · 9,790 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 635, X= -27 FOUND WITH APPROX 4 INCHES LONG CRACKED. TRIMMED PER SRM 53-70-00 VOLUME I, FIGURE 1. REWORKED SEAT TRACK AND SPLICES INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE 1.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 42,237 hrs · 9,790 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 5-83, X= -8.5 FOUND WITH CORROSION. REWORKED TRACK INSTALLED PER SRM 53-70-00 VOLUME I FIGURE 1.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 42,237 hrs · 9,790 cycles

MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STA Y= 635, X= -8.5 FOUND WITH APPROXIMATELY 4 INCHES LONG CRACKED. REWORK SEAT TRACK INSTALLED PER SRM 53-70-00 VOLUME I, FIGURE1

Part: STRINGER — CRACKED (ZONE 600) · airframe 42,237 hrs · 9,790 cycles

RIGHT HAND WING, NR 3 FUEL TANK THRU ACCESS PANEL 635AT, STRINGER 13 FOUND CRACKED OF ABOUT 2.5 INCHES LONG. REPAIRED PER SRM 57-20-00 VOLUME I, FIGURE 10. EXISTING SPLICES AND FABRICATED REPAIR ANGLES INSTALLED PER SRM 51-33-01 VOLUME II.

Part: BRACKET — BROKEN (SCISSOR LINK) · airframe 41,967 hrs · 9,723 cycles

RIGHT MAIN LANDING GEAR DID NOT RETRACT ON T/O. CYCLED GEAR AND LANDED UNEVENTFULLY. FOUND RIGHT MLG SCISSOR LINK BRACKET BROKEN DURING INSPECTION. APPEARS WIRING CONDUIT MAY HAVE HUNG UP ON DOOR LATCH MECHANISM DURING RETRACTION. RIGHT MLG DOOR LATCH NOT DAMAGED. REPLACED CONDUIT GUIDE. ACCOMPLISHED A/C JACKING AND RIGHT MLG SWING AND ADJUSTMENT TEST. ALL TESTS PASSED. NO DEFECTS NOTED. A/C OK FOR CONTINUED SERVICE.

Part: LINE — CRACKED (ZONE 100) · airframe 37,444 hrs · 8,678 cycles

DURING THE PRESSURE TEST OF TAIL TANK FUEL SHROUD DRAIN SYSTEM FOUND TAIL TANK TRANSFER FUEL SHROUD TUBING LOCATED AT STA. Y 1791 LT SIDEWALL OF CENTER CARGO WITH A CRACK LINE MEASURED APPROX. 1 INCH IN LENGTH. COMPLIED WITH EA 1-2822-71762 FUEL SYSTEM - FUEL SHROUD AND DRAIN - CRACK REPAIR ON TUBE FOR TAIL TANK.

Part: SHROUD — CRACKED (ZONE 100) · airframe 37,444 hrs · 8,678 cycles

DURING THE PRESSURE TEST OF TAIL TANK FUEL SHROUD DRAIN SYSTEM FOUND TAIL TANK TRANSFER FUEL SHROUD TUBING LOCATED AT STA. Y 1801 LT SIDEWALL OF CENTER CARGO WITH A CRACK LINE MEASURED APPROX. 2.0 INCHES IN LENGTH. COMPLIED WITH EA 1-2822-71762 FUEL SYSTEM, FUEL SHROUD & DRAIN - CRACK REPAIR ON TUBE FOR TAIL TANK.

Part: BARREL NUT — CORRODED (ZONE 300) · airframe 37,444 hrs · 8,678 cycles

HORZ STAB LT NR 36 BORE FOUND BEARING, SIDEWALL AND BOTTOM WITH CORROSION. BLEND OUT CORROSION FOUND EXCEED SB LIMIT. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000.

Part: BARREL NUT — CORRODED (ZONE 300) · airframe 37,444 hrs · 8,678 cycles

HORIZONTAL STAB RT NR 1 BORE FOUND BEARING, SIDEWALL AND BOTTOM WITH CORROSION. BLEND OUT CORROSION FOUND EXCEED SB LIMIT. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE WING SIDE - LOWER MOUNT I/B CAVITY FOUND CORRODED. COMPLIED FEDEX EA 1-5740-71748, WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: BARREL NUT — CORRODED (ZONE 300) · airframe 37,444 hrs · 8,678 cycles

HORZ STAB RT NR 17 BORE FOUND BEARING, SIDEWALL AND BOTTOM WITH CORROSION. REAMED BORE UP TO MAX SB LIMIT CORROSION STILL EXIST ON SIDEWALL. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE WING SIDE LOWER MOUNT O/B CAVITY FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71748 - WINGS - RIGHT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 37,444 hrs · 8,678 cycles

HORIZONTAL STAB LT NR 26L BORE FOUND BEARING, SIDE WALL & BOTTOM WITH CORROSION. REAMED BORE FOUND CORROSION EXCEED SB LIMIT. COMPLIED WITH FEDEX EA 1-5510-71741, STABILIZERS- HORIZONTAL STABILIZER- BARREL NUT BORE REWORK / REPAIR- 1-5510-7-5000.

Part: STOP FITTING — CRACKED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT O/B FLAP FWD UP STOP FITTING FOUND CRACKED. RT O/B FLAP FWD UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51- 33-01 VOL. II.

Part: STOP FITTING — CRACKED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LEFT O/B FLAP FWD UP STOP FITTING FOUND CRACKED. LEFT O/B FLAP FWD UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.

Part: SKIN — CHAFED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RIGHT WING I/B FLAP LEADING EDGE O/B FLAP VANE TRACK CAVITY FOUND CHAFE MARKS ON RIB.

Part: FLAP TRACK — CHAFED (T/E FLAP) · airframe 37,444 hrs · 8,678 cycles

SNRM N0776 - LT WING IB FLAP LEADING EDGE OB FLAP VANE TRACK CAVITY FOUND CHAFING MARKS ON FITTING AND SKIN. ** S/D ** COMING

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LEFT WING O/B FLAP I/B HINGE (WING SIDE), I/B ACTUATOR ATTACHMENT HOLE AND LUG FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71749, WINGS - LEFT OUTBOARD FLAP, INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: FITTING — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE FITTING (WING SIDE)- SIDE ATTACHMENT BARREL NUT HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71748, WINGS - RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LT WING O/B FLAP I/B HINGE (WING SIDE) - I/B LOWER ATTACHMENT TO REAR SPAR, HOLE AND LUG FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71749, WINGS - LEFT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LT WING O/B FLAP I/B HINGE (WING SIDE) - O/B LOWER ATTACHMENT TO REAR SPAR, HOLE AND LUG FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71749, WINGS - LT OUTBOARD FLAP INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: FITTING — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE FITTING (WING SIDE)- O/B ACTUATOR ATTACH HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71748, WINGS - RIGHT OUTBOARD FLAP- INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LT WING O/B FLAP I/B HINGE (WING SIDE) O/B ACTUATOR ATTACHMENT HOLE AND LUG FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71749, WINGS LT OUTBOARD FLAP- INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE FITTING — CORRODED (RT WING) · airframe 37,444 hrs · 8,678 cycles

SNRM N0825 - RT WING OB FLAP IB HINGE FITTING (WING SIDE)- LOWER OB ATTACHMENT TO REAR SPAR, HOLE AND LUG SURFACE FOUND CORRODED. ** S/D ** COMING

Part: FITTING — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE FITTING (WING SIDE)- I/B ACTUATOR ATTACH HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH CMM 57-44-08 AND FEDEX EA 1-5740-71748, WINGS - RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: BRACKET — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RIGHT WING O/B FLAP O/B HINGE BRACKET (WING SIDE) CORRODED ON SURFACE IN LOWER O/B ATTACHMENT HOLE CAVITY. COMPLIED WITH FEDEX EA 1-5740-71745, WINGS - LEFT AND RIGHT OUTBOARD FLAP, OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: BRACKET — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP O/B HINGE BRACKET (WING SIDE) - O/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71745 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION AND CMM 57-44-09

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LEFT WING O/B FLAP O/B HINGE (WING SIDE) - I/B ACTUATOR ATTACHMENT HOLE AND LUG FOUND CORRODED.

Part: SKIN — CHAFED (TE FLAP) · airframe 37,444 hrs · 8,678 cycles

RT WING I/B FLAP LEADING EDGE I/B FLAP VANE TRACK CAVITY FOUND WITH CHAFING MARKS ON FITTING AND SKIN. RT WING I/B FLAP LEADING EDGE I/B FLAP VANE TRACK CAVITY ON FITTING AND SKIN AS PER FEDEX EA 1-5750-74240, WINGS - RIGHT INBOARD FLAP VANE SUPPORT - RIB CHAFED.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LEFT WING O/B FLAP O/B HINGE (WING SIDE) - O/B ACTUATOR ATTACHMENT HOLE AND LUG FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71745, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: BRACKET — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP O/B HINGE BRACKET (WING SIDE) - I/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71745 - WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET ASSEMBLY CORROSION AND CMM 57-44-09

Part: FITTING — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE FITTING (WING SIDE) - LOWER I/B ATTACHMENT TO REAR SPAR, HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71748, WINGS - RT OUTBOARD FLAP - INBOARD HINGE BRACKET ASSEMBLY CORROSION.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LT WING I/B FLAP O/B HINGE- O/B HINGE LUG HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-71744 - WINGS - LT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE) - SIDE ATTACHMENT BARREL NUT HOLE AND LUG SURFACE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5740-71745 - WINGS LT AND RT OUTBOARD FLAP OUTBOARD HINGE BRACKET ASSEMBLY CORROSION AND CMM 57-44-09

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG SURFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE HOLE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: FITTING — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LT WING OB FLAP OB HINGE FITTING (FLAP SIDE)- IB HINGE LUG HOLE AND SURFACE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE)- I/B HINGE LUG HOLE AND SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B HINGE HOLE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B HINGE HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 LT AND RT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED.

Part: BRACKET — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B LUG AND HOLE FOUND CORRODED. LEFT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RIGHT I/B FLAP O/B HINGE (FLAP SIDE) BRACKET- I/B HINGE PIN HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-71761 - WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG AND HOLE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B HINGE LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES FOUND CORRODED. RT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B ACTUATOR ATTACHMENT HOLE AND LUG SURFACES CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750- 71755, TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LT WING OB FLAP OB HINGE FITTING (FLAP SIDE) IB ACTUATOR ATTACHMENT LUG HOLE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE) - I/B ACTUATOR ATTACHMENT LUG HOLE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE) - I/B ACTUATOR ATTACHMENT LUG HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 LT AND RT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LH WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR LUG AND HOLE CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, LEFT AND RIGHT OUTBOARD FLAP- INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (T/E FLAP) · airframe 37,444 hrs · 8,678 cycles

RIGHT I/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B HINGE PIN HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-71761 - WINGS - RIGHT INBOARD TRAILING EDGE FLAP - HINGE BRACKETS CORRODED.

Part: HINGE — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR ATTACHMENT LUG SURFACE FOUND CORRODED. RT WING O/B FLAP O/B HINGE (FLAP SIDE) BRACKET- O/B ACTUATOR ATTACHMENT LUG SURFACE FOUND CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED.

Part: FITTING — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LT WING OB FLAP OB HINGE FITTING (FLAP SIDE)- OB HINGE LUG HOLE AND SURFACE CORRODED. LT WING O/B FLAP O/B HINGE FITTING (FLAP SIDE)- O/B HINGE LUG HOLE AND SURFACE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71742 TITLE: WINGS- LEFT AND RIGHT OUTBOARD FLAP- OUTBOARD HINGE BRACKET BORE CORRODED

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LT WING OB FLAP IB HINGE (FLAP SIDE) BRACKET- OB HINGE LUG AND HOLE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- O/B HINGE LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, WINGS- LEFT AND RIGHT OUTBOARD FLAP- INBOARD HINGE BRACKET BORE CORRODED.

Part: HINGE — CORRODED (ZONE 500) · airframe 37,444 hrs · 8,678 cycles

LT WING OB FLAP IB HINGE (FLAP SIDE) BRACKET- IB ACTUATOR LUG AND HOLE FOUND CORRODED. LT WING O/B FLAP I/B HINGE (FLAP SIDE) BRACKET- I/B ACTUATOR LUG AND HOLE CORROSION REMOVED AND REPAIRED AS PER FEDEX EA 1-5750-71755, WINGS- LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKET BORE CORRODED.

Part: FITTING — CRACKED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RIGHT WING - SLAT TRACK NR 16 I/B FITTING FOUND CRACKED. RIGHT WING - SLAT TRACK NR 16 I/B FITTING REMOVED AND REPLACED AS PER DRAWING ARB 7565 AND SRM 51-33-01 VOL II.

Part: SPAR — CORRODED (ZONE 600) · airframe 37,444 hrs · 8,678 cycles

RIGHT WING - REAR SPAR UPPER SURFACE O/B OF O/B AILERON FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5710-74238 - WINGS, BASIC STRUCTURE - RIGHT REAR SPAR UPPER SURFACE CORROSION - XORS 1044.800.

Part: FITTING — CRACKED (L/E SLAT) · airframe 37,444 hrs · 8,678 cycles

LEFT WING - FOUND NR 16 SLAT TRACK INBOARD FITTING WITH CRACK. LEFT WING NR 16 SLAT TRACK INBOARD FITTING CRACK RIB REMOVED AND REPLACED AS PER DWG ARB7565, SRM 51-33-01 VOL II AND SRM 51-35-01 VOL II.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHT)

CREW REPORT ON AML: BEFORE START GOT (BATT CHARGER INOP) AND (EMER PWR TST FAIL) ALERTS. TROUBLESHOOTING IAW F/M 24-30-03-00 CARRIED OUT. BOTH MAIN REPLACED IAW AMM 24-32-02 IAW MMDC AD. BATTERY CHARGER REPLACED IAW AMM 24-34-03. EPCU REMOVED AND REPLACED IAW AMM 24-32-6. EMERGENCY INVERTER RCCB B1-134 REMOVED AND REPLACED IAW AMM54-50-1. CLEANED AND INSPECTED TERMINALS AT S4-1 SHUNT. REMOVED AND REPLACED BATTERY CHARGER RELAY R2-24 IAW SMP. CARRIED OUT EMERGNCY PWR TEST AND BATTERY TES IAW AMM 24-34-03. ALL OPS NORMAL. AIRCRAFT RELEASED TO SERVICE.

Part: HINGE — CRACKED (CARGO DOOR) · airframe 32,863 hrs · 7,589 cycles

MAIN DECK CARGO DOOR HINGE (AFT HINGE) CRACKED APPROX 0.025 INCH.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 32,863 hrs · 7,589 cycles

MAIN DECK CARGO DOOR FWD SUPPORT ASSY, HINGE LOBES ELONGATED AND BORE ID EXCEEDED CLEARANCE LIMIT. REMOVED AND REPLACED CARGO DOOR FWD SUPPORT ASSY PER 51-35-01 VOL II.

Part: HINGE — DAMAGED (FUSELAGE) · airframe 32,863 hrs · 7,589 cycles

MAIN DECK CARGO DOOR FUSELAGE HALF HINGE, HINGE LOBES ELONGATED AND ID EXCEEDED FITS CLEARANCE LIMITS. REMOVED AND REPLACED HINGE PER JAMB INSTL DRAWING ACA7211.

Part: BOLT — SHEARED (NR 3 PYLON) · airframe 32,863 hrs · 7,589 cycles

NR 3 PYLON FWD WING TO PYLON ATTACHMENT BULKHEAD FOUND 2 EA BOLT SHEARED BELOW LOWER BEARING. R&R WING PER EA 1-5450-62179.

Part: FITTING — CRACKED (THRUST REVERSER) · airframe 32,863 hrs · 7,589 cycles

NR 2 ENG LT T/R COWL UPPER TRANSLATING SLEEVE CHANNEL END FOUND CRACK. HFEC CARRIED OUT CRACK LENGTH APPROX .625 INCH LONG. R&R COWL & INSTALLED FITTING AT UPPER TRACK BEAM.

Part: STOP FITTING — BROKEN (T/E FLAP)

LT INBOARD FLAP VANE SPRING CARTRIDGE STOP ASSY BROKEN FROM STOP FASTENER HOLES. DISCONNECTED CARTRIDGE.

Part: BATTERY — FAILED · airframe 30,834 hrs · 7,098 cycles

01-346 AFTER T/O 1 BAT CHARGING ANNUNCIATED. BATTERY DISCHARGED. VOLTAGE DROPPED. ** S/D ** COMING

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

01-246 AFT T/O DURING FLAP/SLAT RETRACT GOT AILERON DEFLECT DISAGREE ALERT. RAN CHECKLIST UNABLE TO CORRECT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,484 hrs · 6,565 cycles

SNRM N 76 LWR VERTICAL STABILIZER INTERNAL SUPPORT FRAME CRACKED AT RT END AS VIEW THRU ACCESS PNL 364FR BS 2069. *S/D* REMOVED AND REPLACED PER SRM 51-00-01.

Part: CLIP — CRACKED (HORIZONTAL STAB) · airframe 28,484 hrs · 6,565 cycles

SNRM N 75 ABOVE HORIZONTAL STAB IN UPPER TORQUE BOX STA 2047 ANGLE CLIP FROM BULKHEAD TO CROWN AREA TO BE NDT FOR SUSPECT CRACK. *S/D* PERF HFEC OF ANGLE, NO DEFECT IND.

Part: CLIP — CRACKED (HORIZONTAL STAB) · airframe 28,484 hrs · 6,565 cycles

SNRM N 69 ABOVE HORIZONTAL STAB UPPER TORQUE BOX AREA STA 2084 ANGLES CLIP CRACKED RT SIDE FROM FRAME TO CROWN AREA. *S/D* REMOVED AND REPLACED PER SRM 53-3-00 FIG 8.

Part: ANGLE — CRACKED (TORQUE BOX) · airframe 28,484 hrs · 6,565 cycles

SNRM N 67 ABOVE HORZ STAB IN UPPER TORQUE BOX AREA STA 2122 (DOG HOUSE) TOP ANGLE FROM BULKHEAD TO CROWN AREA HAS CRACKS, LT AND RT ENDS. LT CRACK APPROX .625 INCH LONG AND RT CRACK APPROX 1 INCH LONG. *S/D* REMOVED AND REPLACED PER SRM 53-30-00BB WORKED WITH EA 5530-5382.

Part: SEAT TRACK — CORRODED (BS 484)

SNRM 434 - MAIN DECK LAVATORY, RT BS 484, RBL 75.25, INBD AFT LAVATORY TIE DOWN FITTING SEAT TRACK CORRODED. REMOVED AND REPLACED PER SRM 51-31-01 VOL 11 AND SRM 53-70-00 VOL 1.

Part: SEAT TRACK — CRACKED (BS 695 & 635)

SNRM 452/572, FOUND CRACK MAIN DECK SEAT TRACK, BS 695 X EQUALS 8.5 LT-452. CRACK SEAT TRACK, BS LT 635, LBL 8.5 - 572. SEAT TRACK TRIMMED OUT AND REPAIRED PER SRM 53-70-00 VOL 1.

Part: WIRE — CHAFED (AUTO FLIGHT SYST)

DEFECTIVE AUTO PILOT, AUTOTHROTTLES, FLIGHT DIR SYS, TAT PROBE HEAT, FLAPS ALERT, PRESS, AVIONICS FAN, TRANSPONDER, AUTO BRAKE. FOUND DEFECT CAUSE BY CHAFING AND SHORTING OF THREE WIRES.

Part: BOLT — SHEARED (LT MLG STRUT)

DURING LT MLG SHOCK-STRUT LWR BEARING SEAL REPLACEMENT, ANTI-ROTATION BOLT (P/N NAS 4504 U11) FOUND SHEAR FROM CHAMBER (ARG 7477-1) OF UPPER CYLINDER ASSY. *S/D* LT MLG CHAMBER ASSY REPLACED PER CMM 32-11-12.

Part: BOLT — SHEARED (LT MLG STRUT)

DURING LT MLG SHOCK STRUT LWR BEARING SEAL REPLACEMENT, ANTI-ROTATION BOLT SHEARED FROM CHAMBER (ARG 7477-1) UPPER CYL ASSY. DAMAGED FOUND ON UPPER CHAMBER (NRG 6720-5) AND UPPER BEARING (ARG 7607-1). LEFT MLG CHAMBER ASSY REPLACED PER CMM 32-11-12.

Part: WIRE — FIRE (CARGO COMPT)

CENTER CARGO COMPARTMENT NR 4L ROLLER INOP., PAP5 C/B. REMOVED FLOOR BOARDS, FOUND THE WIRING, UNDER THE FLOOR HAD A FIRE. WIRING WAS BURNED UP, ALSO BELLFRAME HAD HOLE BURNED THRU FRAME AT STA 1641, BETWEEN LONG 47 AND 48. NOTED ON NO. 02 AND 24, DURING B-CHECK MAINT REMOVED DAMAGED AREA, VERIFIED ALL DAMAGE REMO VED EDDY CURRENT INSPECTED AREA. NO INDICATIONS OF CRACKS NOTED. INSTALLED DOUBLER PER SRM 53-30-00, ITEM 2. WIRING PROBLEM: SPLICED WIRES PER WIRING DIAGRAM 25-52-06, OPS. CHK OF LOADING SYSTEM FOUND NORMAL, PER M/M 25-50. SIGNED OFF MACH ITEM 25-50/2769. RELEASE A/C 1-7-98.

Part: FRAME — CRACKED (LT MLG DOOR)

N00098 CENTER GEAR LT DOOR CORNER CRACKED, FRAME OUTER FLANGE RADIUS I/B FWD CORNER. REMOVED CORNER SECTION AND DRILLED OUT NEW CORNER SECTION OF DOOR AND INSTALLED NEW CORNER SECTION PER SRM 51-00-00.

Part: EGT INDICATION — MALFUNCTIONED (NR 2 ENGINE)

SHUT DOWN NUMBER 2 ENGINE BECAUSE OF FLUCTUATING EGT, THEN COMPLETE FAILURE OF THE EGT GAUGE. ALL OTHER ENGINE PARAMETERS WERE NORMAL. NO FAULTS LISTED ON NR 2 ECU A AND B CHANNELS. INSPECTED THERMOCOUPLES TERMINAL AND FOUND SEVERAL TERMINALS ENDS LOOSE. SECURED THE TERMINAL ENDS. RAN ENGINE PER JET RUN UP HANDBOOK, OK FOR SERVICE.

Part: HYDRAULIC TUBE — LEAKING (NR 3 ENGINE)

HYD SYS NR 3 FAIL ALERT DISPLAYED. REMOVED AND REPLACED LEAKING PRESSURE LINE AT NR 3 HYD MANIFOLD. REMOVED AND REPLACED HYD FILTERS AND BOTH ENGINE DRIVEN PUMPS.

Part: STRUCTURE — DAMAGED (AFT FUSELAGE)

HARD LANDING WITH TAIL STRIKE. STRUCTURAL DAMAGE BEING EVALUATED IN ANC BY ENGINEERING AND DAC RAMS TEAM. *S/D* DURING MAINTENANCE C-CHECK, A HARD LANDING INSPECTION WAS ACCOMPLISHED. ALSO, DURING THE C-CHECK THE STRUCTURAL DAMAGE CAUSED AS A RESULT OF HARD LANDING WAS REPAIRED IAW EA 15310-28929.

Part: SPLICE PLATE — GOUGE (WS 118)

CENTER WING TO RT LOWER WING LONGITUDINAL SPLICE PLATE HAS A WEAR MARK APPROX 5 FEET IN LENGTH, WITH L/E TIP OF SPLICE PLATE WORN APPROX 90 PERCENT OF MATERIAL THICKNESS AT XCW118 INTERSECTING FUSE STA 1156. C/W EA 1-5710-24326 WING OUBT TO CENTER, SPLICE PLATE BLEND OUT (RT).

Part: O-RING — FAILED (NR 1 HYD SYST)

HYD NR 1 OFF ALERT AFTER 50 MINUTES OF FLIGHT AT FLT LEVEL 320. QUANTITY FELL TO 2.8, PRESS DROPPED TO 40 PSI, NR 2, NR 3 NORMAL. HYD TEMP NR 1 - 48C TEMP ROSE TO 92C, THEN CAME BACK DOWN. FOUND HYD LEAK FROM LINE FITTING ON FILTER HEAD TO NR 1L HYD PUMP PRESS LINE. REMOVED AND REPLACED PACKING AT PRESS FITTING. CHANGED ALL FOUR FILTER ELEMENTS PRECAUTIONARY. NO CONTAMINATION FOUND. SERVICED NR 2 HYD SYS. ENGINE RUN OK. HYD TEMP WITHIN LIMITS PER MM 29-10-00.