N772FD

Part: TRANSMITTER — FAILED (TE FLAPS) · airframe 82,114 hrs · 32,337 cycles

PDIS 772 29-02 5906 28JUL22 RME OPEN U DURING THE CLIMB HAD A LOSS OF THE ENTIRE LEFT HYDRAULIC SYSTEM. FIRST INDICATION WAS A L HYD QTY CAS MESSAGE. THE LEFT HYDRAULIC RESERVOIR WAS RAPIDLY DEPLETING. WE THEN GOT A MOMENTARY L HYD ENGINE PUMP FOLLOWED BY A LHYD SYS PRESS MESSAGES. ALSO GOT A POWER XFER UNIT STATUS MESSAGE. RAN ALL CHECKLIST AND HAD TO DO AN ALTERNATE FLAP AND GEAR EXTENSION. THE ALTERNATE FLAP EXTENSION WOULD NOT LOWER THE FLAPS AND WE DID A NO FLAP/ SLAT LANDING. PART 28JUL22 10:08 MC1 U HYD ELEMENT MPN: 60B00211-3 CPN: 2911124 QTY: 1 PART 28JUL22 10:09 MC1 U IDENTIFIED PARTS FILTER MPN: 7515128 CPN: 2911001 QTY: 1 PART 28JUL22 10:10 MC1 U IDENTIFIED PARTS ELEMENT MPN: 7585381 CPN: 2912539 QTY: 1 PART 28JUL22 10:11 MC1 U IDENTIFIED PARTS SEE KIT CPN 2913461 MPN: K2912539K2 CPN: 2913409 QTY: 1 PART 28JUL22 10:13 MC1 U IDENTIFIED PARTS FILTER KIT MPN: 654T0035-5 CPN: 0133659 QTY: 1 PART 28JUL22 11:19 MC1 U IDENTIFIED PARTS (W/KIT) PUMP ASSY-HYD AC MPN: 731966 CPN: 2912446 QTY: 1 PART 28JUL22 11:35 MC1 U SHGN 29JUL22 01:42 RME U FOUND 0.05 IN THE LH HYD SYS AS WELL AS BROKEN LINE. INSTALLED FLEX LINE PER AMM20-10-10-8. THEN SERVICED RH AND LH HYD SYS INTO LIMITS PER AMM 12-12-01. RAN LH ENG TO VERIFY NO HYD LEAKS PER JRH CHAPTER 05 AND 06. LEAK CHECKS GOOD.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 81,278 hrs · 31,772 cycles

MAIN DECK FLOOR PANEL 251MVF (RH) HAS BROKEN CORNER. FABRICATED NEW PANEL IAW FED EX SRZ 25-005 REV R

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 81,278 hrs · 31,772 cycles

MAIN DECK FLOOR PANEL 251MFW(LH) HAS BROKEN CORNER. FABRICATED NEW PANEL IAW FED EX SRZ 25-005-REV R

Part: PLATE — CRACKED (FUEL ACCESS) · airframe 81,278 hrs · 31,772 cycles

RIGHT WING LEADING EDGE FUELING ACCESS PANEL, DOOR SWITH PLATE IS CRACKED FABRICATED & REPLACED NEW CLIP IAW BAC DWG 284N1138 REV -

Part: DOUBLER — CHAFED (BS 1862-1875) · airframe 81,278 hrs · 31,772 cycles

EXISTING REPAIR DOUBLER AT STA 1862 - 1875, S-17L IS CHAFED. REMOVED & REPLACED REPAIR DOUBLER IAW B757 SRM 53-80-01-2R, FIGURE 201, REPAIR 2

Part: SKIN — CHAFED (BS 1862-1875 S17) · airframe 81,278 hrs · 31,772 cycles

RH FUSELAGE @ STA 1862.7 - 1875, S-17R, EXISTING DOUBLER HAS CHAFING DAMAGE ON EXTERIOR SURFACE REMOVED & REPLACED REPAIR DOUBLER IAW B757 SRM 53-80-01-2R, FIGURE 201, REPAIR 2

Part: SKIN — CRACKED (LT WING) · airframe 81,278 hrs · 31,772 cycles

LEFT WING, FIXED LEADING EDGE SKIN @ FSS 550 IS CRACKED REPAIRED LEADING EDGE SKIN IAW B757 SRM 57-41-01, FIGURE 201. LEADING EDGE SKIN REMOVED & REINSTALLED FOR ACCESS IAW B757 SRM 51-40-02-0G & BAC DWG 114N2035 REV -.

Part: SKIN — CRACKED (LT WING) · airframe 81,278 hrs · 31,772 cycles

LEFT WING FIXED LEADING EDGE SKIN IS CRACKED @ FSS 360 REPAIRED LEADING EDGE SKIN IAW B757 SRM 57-41-01. LEADING EDGE SKIN REMOVED & REINSTALLED FOR ACCESS IAW B757 SRM 51-40-02-0G & BAC DWG 114N2035 REV -

Part: BRACKET — CRACKED (FWD CARGO DOOR) · airframe 81,278 hrs · 31,772 cycles

FWD LOWER CARGO DOOR AFT UPPER INTERIOR CORNER IS CRACKED REMOVED AND REPLACED FWD CARGO DOOR AFT INTERIOR CORNER IAW BAC DWG 143N6603 REV:F AND B757 SRM 51-40-02

Part: FSEU — MALFUNCTIONED (TE FLAPS) · airframe 81,033 hrs · 31,580 cycles

ON APPROACH TO MEMPHIS AT 2000 FEET , 170 KNOTS , FLAPS 25 WERE SELECTED AND WE RECEIVED A TE FLAP DISAGREE EICAS LIGHT. QRH WAS USED , UNEVENTFUL LANDING. EMERGENCY DECLARED. SHGN 09MAR21 17:18 MEM U DURING FLIGHT CREW DEBRIEF "THERE WAS NO NEEDLE SPLIT ON FLAP POSITION INDICATOR". FLAP SYSTEM REMAINS CONFIGURED THE SAME AS FLIGHT CREW HAD IT FOR LANDING. FACT 09MAR21 22:57 MEM U T/S PER FIM 27-51 FAULT TREE 808 AND TREE 805. FSEU 1 HAD FLA FAIL 217. PERFORMED FIM 27-51 TREE 810. FLAP LOAD RELIEF AND ADC TEST GOOD. INSPECTED FLAP OVERLOAD INDICATORS AND TRANSMISSIONS FOR SERVICE. ALL CHECK GOOD. FLAP POS IND, PDU, AND HANDLE TRANSMITTER WERE ALL WITHIN PARAMETERS AT ALL POSITIONS. REF M/M 27-58-01-5. REMOVED AND REPLACED FSEU-1 AFTER CONSULTING WITH MOCC. TESTS GOOD. NO FAULTS. REF M/M 27-51-01-2. OK FOR SERVICE

Part: COLLAR — BROKEN (L1 DOOR) · airframe 80,250 hrs · 31,035 cycles

L1 DOOR GUST LOCK BROKEN. REMOVED AND REPLACED L-1 DOOR HOLD-OPEN LOCK COLLAR. IAW 757 M/M 52-11-08-8.

Part: SENSOR — FAILED (LT MLG) · airframe 80,000 hrs · 30,858 cycles

AFTER TAKEOFF THE LANDING GEAR HANDLE WOULD NOT RAISE TO RETRACT. RAN QRH. LANDING GEAR RETRACTED WITH LOCK OVERRIDE QRH. REMOVED AND REPLACED LEFT FORWARD MAIN GEAR TRUCK TILT SENSOR IAW AMM 32-09-07-2. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. SDR INFO: PART NAME SENSOR, PROX SWITCH SYSTEM, PART NUMBER 8-935-01FS, AND SERIAL NUMBER- 0785.

Part: FITTING — CRACKED (FUSELAGE) · airframe 79,724 hrs · 30,645 cycles

MAIN CABIN - STA. 580 FLOORBEAM STUB FITTING AT LBL 45.5 HAS A CRACK IN AFT FLANGE UPPER RADIUS. COMPLIED WITH # F-5310-T0348175 P1. FUSELAGE- MAINFRAME- STA.580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.

Part: DOOR — NOT CLOSED (RT MLG) · airframe 79,628 hrs · 30,569 cycles

GEAR "DOORS" LIGHT AND EICAS GEAR DOORS MESSAGE AFTER EXTENDING GEAR FOUND RIGHT MAIN GEAR DOOR NOT FULLY CLOSED UPON BLOCK IN. OPENED GEAR DOORS, INSPECTED FOR LEAKS, DAMAGE AND MISALIGNMENT: NONE FOUND. INSTALLED GEAR PINS AND PERFORMED DUMMY EXTEND AND RETRACT MULTIPLE TIMES. SYSTEM IS OPERATING NORMAL AT THIS TIME. ACFT OK FOR SERVICE. REF AMM 32-32-05-4 SUB TASK 3 D.

Part: ACTUATOR — FAILED (NLG) · airframe 78,007 hrs · 29,479 cycles

AFTER TAKE OFF, RECEIVED AN AMBER GEAR LIGHT AND A GEAR DISAGREE MESSAGE ON EICAS. RAN CHECKLIST, PROBLEM DID NOT RESOLVE ITSELF. PUT GEAR DOWN AND RECEIVED A NORMAL THREE GREEN INDICATION. RETURNED TO DEPARTURE. THE NOSE LANDING GEAR LOCK ACTUATOR REMOVED AND REPLACED. PROXIMITY SWITCH ELECTRONICS UNIT (PSEU) REMOVED AND REPLACED. SYSTEMS OPS CHECKED GOOD IAW AMM 32-32-00-5. RETURNED VMO/MMO SWITCH TO NORMAL IAW AMM 34-12-00-5. REMOVED LANDING GEAR LOCKPINS IAW AMM 32-00-20-2. REMOVED COLLAR AND RESET LANDING GEAR LOCK LEVER CIRCUIT BREAKER IAW AMM 20-60-01-2.

Part: MODULE — MALFUNCTIONED (MLG) · airframe 78,003 hrs · 29,477 cycles

AT LEVEL FL360, RECEIVED A CONFIGURATION RED DISCRETE LIGHT AND GEAR NOT DOWN. RED EICAS MESSAGE RECEIVED AURAL ALERT AND INTERMITTENT EICAS MESSAGE DURING APPROACH. PERFORMED OPS CHECK OF LANDING CONFIGURATION WARNING MODULE. OPS CHECK FAILED. REMOVED AND REPLACED THE LANDING CONFIGURATION WARNING MODULE. OPS CHECKED GOOD IAW AMM 31-51-04-4-0. CHECKED PSEU FOR FAULTS. NONE NOTED. PERFORMED ERASE OF PSEU IAW FIM 32-09, TREE 802.

Part: HINGE FITTING — CRACKED (BS 1640) · airframe 78,002 hrs · 29,476 cycles

LOWER HINGE FITTING AT BS 1640 LT SIDE IS CRACKED. REMOVED AND REPLACED THE HINGE FITTING IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 1640) · airframe 78,002 hrs · 29,476 cycles

LT FRAME BS 1640, STRINGER 14L FOUND CRACKED AT THE INBD AFT RADIUS. REPAIRED IAW EA F-5310-T0334370 P1.

Part: SKIN — CRACKED (BS 395-418) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN, CROWN SKIN, THERE IS A CRACK BETWEEN BS 395 - 418 AT STRINGER 4R THAT MEASURES 2.4 INCHES. REPAIRED IAW EA F-5330-T0318521 PART 1. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — CRACKED (BS 395-418) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN, HAS A CRACK BETWEEN BS 395 - 418 AT STRINGER 4 RT THAT MEASURES APPROX 0.4. REPAIRED IAW EA F-5330-T0318521 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

CABIN STATION 1681, RBL 53 AFT DECK PLATE UPPER SURFACE FOUND CORROSION. COMPLIED WITH PART 1 OF EA F-5310-T0316711. REPLACED DECK PLATE WITHOUT CHEM-MILLED POCKETS. REPAIR CLASSIFIED AS MAJOR.

Part: REPAIR — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXISTING REPAIR FINDING. THE REPAIR AT BS 540 - 640 FROM STRINGER 24 RT TO 28 LT. THE STRUCTURE FILLER HAS NUMEROUS SCRATCHES TOOL MARKS & GOUGES. EXISTING QUADRUPLER REPAIR AT NR 1 FWD CARGO DOOR CUT-OUT-REPAIR. REPAIR CLASSIFIED AS MAJOR

Part: REPAIR — GOUGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXISTING REPAIR FINDING. THE REPAIR AT BS 540 - 640 FROM STRINGER 24 RT TO 28 LT. THE DOUBLER HAS NUMEROUS SCRATCHES TOOL MARKS & GOUGES. EXISTING QUADRUPLER REPAIR AT NR 1 FWD CARGO DOOR CUT-OUT-REPAIR. REPAIR CLASSIFIED AS MAJOR

Part: REPAIR — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXISTING REPAIR FINDING, THE REPAIR AT BS 540 - 640 FROM STRINGER 24 RT TO 28 LT. THE QUADRUPLER HAS NUMEROUS SCRATCHES, TOOL MARKS & GOUGES. QUADRUPLER REPAIR AT NR 1 FWD CARGO DOOR CUT-OUT-REPAIR. REPAIR CLASSIFIED AS MAJOR

Part: REPAIR — GOUGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXISTING REPAIR FINDING. THE REPAIR AT BS 540 - 640 FROM STRINGER 24 RT TO 28 LT. THE TRIPLER HAS NUMEROUS SCRATCHES TOOL MARKS & GOUGES. QUADRUPLER REPAIR AT NR 1 FWD CARGO FOOR CUT-OUT - REPAIR. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — DAMAGED (BS 1600-1620) · airframe 763 hrs · 28,324 cycles

EXTERIOR SKIN, HAS AN OVERSIZE HOLE BETWEEN BS 1600 - 1620, STRINGERS 26 - 27R. REPAIRED IAW EA F-5310-T0316044. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 760-770) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 760 - 770 BETWEEN STRINGER 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE, EXTERIOR SKIN, THERE IS A NEW LIGHTNING STRIKE AT BS 700 - 720 BETWEEN STRINGER 28 LT & 28 RT.

Part: SKIN — DAMAGED (BS 740-760) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN, HAS A LIGHTNING STRIKE AT BS 740 - 760 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 760-770) · airframe 763 hrs · 28,324 cycles

FUSELAGE, EXTERIOR SKIN, HAS A LIGHTNING STRIKE AT BS 760 - 770 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 700-720) · airframe 763 hrs · 28,324 cycles

EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 700 - 720 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 760-770) · airframe 763 hrs · 28,324 cycles

FUSELAGE, EXTERIOR SKIN, HAS A LIGHTNING STRIKE AT BS 760 - 770 BETWEEN STRINGER 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 740-760) · airframe 763 hrs · 28,324 cycles

FUSELAGE, EXTERIOR SKIN, HAS A LIGHTNING STRIKE AT BS 740 - 760 BETWEEN STRINGER 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE, EXTERIOR SKIN, THERE IS A NEW LIGHTNING STRIKE AT BS 660 - 680 BETWEEN STRINGER 28 LT & 28 RT.

Part: SKIN — DAMAGED (BS 760-770) · airframe 763 hrs · 28,324 cycles

FUSELAGE, EXTERIOR SKIN, HAS A LIGHTNING STRIKE AT BS 760 - 770 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 760-770) · airframe 763 hrs · 28,324 cycles

FUSELAGE, EXTERIOR SKIN, HAS A LIGHTNING STRIKE AT BS 760 - 770 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 760-770) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 760 - 770 BETWEEN STRINGERS 28L & 29R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 680-700) · airframe 763 hrs · 28,324 cycles

EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 680 - 700 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 700-720) · airframe 763 hrs · 28,324 cycles

EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 700 - 720 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 760-770) · airframe 763 hrs · 28,324 cycles

FUSELAGE, EXTERIOR SKIN, HAS A LIGHTNING STRIKE AT BS 760 - 770 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN. THERE IS A NEW LIGHTNING STRIKE AT BS 740 - 760 BETWEEN STRINGER 28LT & 28RT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN. THERE IS A NEW LIGHTNING STRIKE AT BS 700 - 720 BETWEEN STRINGER 28 LT & 28RT. REPAIR CARRIED OUT AS PER EA F-5310-T0316230 PART 1 TITLE: FUSELAGE - MAINFRAME - LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN STA 700 TO STA 720 AND STRINGER 28L AND STRINGER 28R. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN. THERE IS A NEW LIGHTNING STRIKE AT BS 740 - 760 BETWEEN STRINGER 28 LT & 28 RT. FUSELAGE EXTERIOR SKIN, A NEW LIGHTNING STRIKE COMPLIED WITH EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — WORN (TE FLAP) · airframe 763 hrs · 28,324 cycles

LEFT INBD MAIN FLAP, OTBD NOSE SKIN WORN 36" FROM OTBD EDGE TO MOST OTBD EDGE. REPAIRED IAW EA F-5750-T0316370 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 740-760) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN, A LIGHTNING STRIKE WAS FOUND AT BS 740 -760 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 700-720) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN, HAS A LIGHTNING STRIKE AT BS 700 - 720 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 700-720) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN, FOUND A LIGHTNING STRIKE AT BS 700 - 720 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN, THERE IS A NEW LIGHTNING STRIKE AT BS 680 - 700 BETWEEN STRINGER 28 LT & 28 RT. A NEW LIGHTNING STRIKE REPAIR CARRIED OUT IAW EA F-5310-T0316230 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 740-760) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN, HAS A LIGHTNING STRIKE AT BS 740 - 760 BETWEEN STRINGERS 28L & 28R. REPAIRED IAW EA F-5310-T0316230 PART 1. CLASSIFIED AS A MAJOR REPAIR.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE RT SIDE, EXISTING REPAIR DEFECT. THE SHEAR TIE AT BS 580 BETWEEN STRINGER 26 - 27 HAS 3 HOLES. ACCOMPLISHED EA F-5310- TO317519 . REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER SPLICE — DAMAGED (BS 1617-1643) · airframe 763 hrs · 28,324 cycles

AFT CARGO BAY BS 1617 - 1643, STRINGER 19L. STRINGER SPLICE FASTENER HOLES ELONGATED. R & R THE STRINGER SPLICE IAW DWG 146N3700 SHT 3 REV G, AND DWG 146N3821 SHT 2 REV B. MAJOR REPAIR.

Part: SPAR — CORRODED (LT WING) · airframe 763 hrs · 28,324 cycles

LEFT WING, AFTER CORROSION REMOVAL, FOUND LT REAR SPAR BLENDED AREA, BOTH DEPTH & WIDTH OUT OF LIMITS AT LT AFT BOOST PUMP LOWER BONDING LEAD CONNECTION POINT. REPAIRED IAW EA F-5710-T0317079 P1. REPAIR CLASSIFIED AS MINOR.

Part: DECK PLATE — CHAFED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

CABIN STATION 1681 - 1690, RBL 45 - 55, AFT DECK PLATE UPPER SURFACE FOUND CHAFED MARKS. COMPLIED WITH PART 1 OF EA F-5310-T0316711 A. REPLACEMENT OF DECK PLATE WITHOUT CHEM-MILLED POCKETS. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — GOUGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FWD E & E COMPARTMENT BS 231.25, LBL 9 FRAME WEB HAS A GOUGE. REPAIRED IAW EA F-5310-T0317393. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 1681, RBL 50 - 52 FLOORBEAM UPPER FLANGE FOUND CORROSION AFTER DECK PLATE REMOVED. R & R THE FLOORBEAM FLANGE IAW EA F-5310-T0317368. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CHAFED (R2 DOOR) · airframe 763 hrs · 28,324 cycles

R2 DOOR OUTER SKIN, 6 INCHES TO AFT EDGE & 8 INCHES TO LOWER EDGE, FOUND CHAFED. COMPLIED WITH EA F-5210-T0317397 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 1681, RBL 21 - 42 FLOORBEAM UPPER FLANGE FOUND CORROSION AFTER DECK PLATE REMOVED. FLOORBEAM R & R IAW EA F-5310-T0317368. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

LEFT WING, AFTER FILL PORT REMOVAL, UPPER SKIN UPPER SURFACE FOUND CORRODED AT OVERWING FILL PORT ADAPTER MATING AREA. REPAIRED IAW EA F-5730-T0317149. REPAIR CLASSIFIED AS MAJOR.

Part: FAILSAFE — GOUGED (BS 1420) · airframe 763 hrs · 28,324 cycles

AFT CARGO COMPARTMENT BS 1420, STRINGER 25L - 26L, FRAME FAIL SAFE CHORD HAS EXISTING GOUGE. R & R IAW EA F-5310-T0316972 P1 & DWG 146N1012 SHT 2 REV D. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE EXTERIOR SKIN THERE IS CORROSION AT STATION 1787 - 1806, STRINGER 25L - 25R. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN P/NO 148N3216Y1 SEE SNRM NO N01669 FOR DETAIL. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE EXTERIOR SKIN THERE IS CORROSION AT STATION 1844 - 1862, STRINGER 25L - 25R. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN PN 148N3216Y1 SEE SNRM NO N01669 FOR DETAIL. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE, EXTERIOR SKIN THERE IS CORROSION AT STATION 1825 - 1844, STRINGER 25L - 25R. CORROSION REMOVED, FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN PN 148N3216Y1 SEE SNRM NO N01669 FOR DETAIL. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE EXTERIOR SKIN THERE IS CORROSION AT STATION 1806 - 1825, STRINGER 25L - 25R. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN P/NO: 148N3216Y1 SEE SNRM NO N01669 FOR DETAIL. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE AREA INTERIOR COMPARTMENT, THERE IS CORROSION ON THE INTERIOR SKIN BETWEEN STATION 1806 - 1825 FROM STRINGER 25L - 27L. CORROSION REMOVED, FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN PN 148N3216Y1 SEE SNRM NO N01669 FOR DETAIL. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE FUSELAGE SKIN INTERIOR SURFACE FOUND CORROSION AT STATION 1787 - 1806, STRINGER 25L - 27L. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED FROM STA 1787-1862 STR 25L-25R AND REPLACED NEW SKIN PN 148N3216Y1 SEE SNRM NO N01669 FOR DETAIL. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — DAMAGED (BS 1720-1743) · airframe 763 hrs · 28,324 cycles

EMPENNAGE EXTERIOR SKIN HAD NICKS & SCRATCHES AT BS 1720 - 1743, STRINGERS 7 - 8L. FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 114. REPAIR CARRIED OUT IAW EA F-5330-T0317255 PART 1. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 1681 FLOORBEAM FOUND CORRODED. BLENDED OUT, AND FOUND OUT OF LIMITS AT RBL 25. R & R THE FLOORBEAM IAW EA F-5310-T0317368. MAJOR REPAIR.

Part: FAILSAFE — CORRODED (BS 1500) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 1500, STRINGER 17R, FRAME FAILSAFE FOUND CORRODED. REPAIRED IAW EA F-5310-T0317107 B PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: DOOR SILL — CRACKED (BS 1641) · airframe 763 hrs · 28,324 cycles

BS 1641 R4 DOOR LOWER SILL FOUND CRACK. REPAIRED IAW EA F-5310-T0316973. MAJOR REPAIR.

Part: STRINGER — DENTED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

CABIN STATION 1600 - 1620, STRINGER 16L, STRINGER FOUND DENT & EXISTING TRIM OFF. R & R CARRIED OUT IAW EA F-5310-T0316871. UNDOCUMENTED REWORK ON STRINGER 16L UPPER FREE FLANGE, STATION 1600 - 1620. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — WORN (FUSELAGE) · airframe 763 hrs · 28,324 cycles

EMPENNAGE EXTERIOR SKIN RT SIDE, THERE IS A WEAR AT BS 1862.70 - 1875, WHERE THE LOWER BLADE SEAL CONTACTS THE SKIN ABOVE STRINGER 17R. FOUND OUT OF LIMITS IAW SRM 53-80-01 FIG 101 DETAIL VII REV 114. REPAIRED IAW SRM 53-80-01-2R FIG 201 DETAIL II REV 114. MAJOR REPAIR.

Part: SKIN PANEL — DENTED (TE FLAP) · airframe 763 hrs · 28,324 cycles

LEFT WING- AFTER SANDING. I/B MAIN FLAP I/B UPPER SKIN PANEL (113N2401) FOUND WITH MULTIPLE DENT MARKS FROM MF STA 165 TO STA 184. LEFT WING, I/B MAIN FLAP I/B UPPER SKIN PANEL (113N2401) MARKED DENT AREA FROM MF STA 165 TO MF STA 184 FOUND OUT OF LIMIT PER B757 SRM 57-53-01-1A ALLOWABLE DAMAGE DETAIL VII REV 114. LENGTH - 0.85" DEPTH - 0.055" 0.085" / 0.055" = 15.5 A/Y MIN MUST NOT BE LESS THAN 30. MARKED DAMAGED AREA REMOVED. DRIED OUT, REPAIR PAIR FABRICATED, SURFACE TREATED AND REPAIR PARTS INSTALLED USING 250Ï¿½F HOT BONDING PROCESS PER B757 SRM 57-53-01 REPAIR DETAIL 1 REV 114 AND SRM 57-70-10 REPAIR GENERAL REV 114. TAP TEST PERFORMED PER 51-10-06 REPAIR 1 REV 114. NO DISBOND NOTED. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — WORN (BS 1862-1875) · airframe 763 hrs · 28,324 cycles

EMPENNAGE EXTERIOR SKIN LT SIDE, THERE IS A WEAR AT BS 1862.7 - 1875, WHERE LOWER BLADE SEAL CONTACTS THE SKIN ABOVE STRINGER 17L. FOUND OUT OF LIMITS IAW SRM 53-80-01 FIG 101 DETAIL VII REV 114. REPAIRED IAW SRM 53-80-01-2R FIG 201 DETAIL II REV 114. MAJOR REPAIR.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN, NUMEROUS SMALL SCRATCHES ALONG THE WING TO BODY PERIMETER AT BS 1300 - 1280, STRINGER 27 - 30L. SCRATCHES REMOVED, FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 114. REPAIRED IAW EA F-5330-T0316875 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (BS 1280-1300) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN HAS NUMEROUS SMALL SCRATCHES ALONG THE WING TO BODY PERIMETER AT BS 1300 - 1280, STRINGER 27 - 30R. SCRATCHES REMOVED, AND FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 114. REPAIRED IAW EA F-5330-T0316875 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SPAR — DAMAGED (TE FLAP) · airframe 763 hrs · 28,324 cycles

RIGHT WING, INBD TE MAIN FLAP FRONT SPAR LOWER CHORD & LOWER SKIN FOUND TO HAVE HOLES ELONGATED AT MF STATION 224. REPAIRED IAW EA F-5710-T0318167 PART 1. MAJOR REPAIR.

Part: FRAME SPLICE — GOUGED (BS 1520) · airframe 763 hrs · 28,324 cycles

AFT CARGO COMPARTMENT, BS 1520 24R FRAME SPLICE HAS GOUGED. REMOVED AND REPLACED IAW DWG 146N1017 SHT 3 REV. D, SPLICE FABRICATED IAW DWG 146N1042 SHT 1 REV A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: WINDOW FRAME — CORRODED (BS 1080-1100) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 1080 - 1100, STRINGER 13R WINDOW FRAME LOWER EDGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 114. OUT OF LIMITS IAW SRM 56-20-02 FIG 101 ALLOWABLE DAMAGE 1 REV 114. WINDOWS FRAME ASSY REMOVED IAW SRM 51-40-02 REV 114 AND REPLACED IAW DWG 144N3201 SHT 6 REV C REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (BS 560-580) · airframe 763 hrs · 28,324 cycles

BS 560 - 580, RBL 45.5 SEAT TRACK FOUND CHAFED. REPAIRED IAW EA F-5310-T0317294. MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

AFT CARGO COMPARTMENT STATION 1440, RBL 10 BOTTOM FRAME CORROSION. R & R WITH NEW FRAME IAW DWG NR & 146N1013 SHT 3 REV D. REPAIR CLASSIFIED MAJOR IAW GM 6-2-100.

Part: BULKHEAD — CHAFED (NR 2 PYLON) · 28,324 cycles

NR 2 PYLON, AFT BULKHEAD INBD LOWER FLANGE EXTERNAL SURFACE FOUND WITH A DEEP CHAFE. REPAIRED IAW EA F-5450-T0316504 PART 1. CLASSIFIED AS A MAJOR REPAIR.

Part: BULKHEAD — CHAFED (NR 2 PYLON) · 28,324 cycles

NR 2 PYLON AFT BULKHEAD, OTBD LOWER FLANGE EXTERNAL SURFACE FOUND A DEEP CHAFE. REPAIRED IAW EA F-5450-T0316504 PART 1. CLASSIFIED AS A MAJOR REPAIR.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

CABIN, STATION 324 - 365 R1 DOOR CUT OUT LOWER SILL WEB FOUND CRACK AT AFT EDGE & FOUND CORROSION AT MID-AREA AFTER WEB REMOVED FOR ACCESS, SNRM N03651. NEW LOWER SILL WEB FABRICATED AS PER DWG 141N8422 SHT 1 REV R AND INSTALLED AS PER BOEING DWG 141N8422 SHT 1 REV R REPAIR CLASSIFIED AS MAJOR

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE AREA INTERIOR COMPARTMENT THERE IS CORROSION ON THE INTERIOR SKIN BETWEEN STATION 1844 - 1862 FROM STRINGER 25L - 27L. CORROSION REMOVED, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 114. CORRODED SKIN REMOVED. REPLACED NEW SKIN. MAJOR.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE AREA INTERIOR COMPARTMENT, THERE IS CORROSION ON THE INTERIOR SKIN BETWEEN BS 1825 - 1844 FROM STRINGERS 25 - 27L. FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101, ALLOWABLE DAMAGE 1 REV 114. CORRODED SKIN PANEL REMOVED. REPLACED WITH NEW SKIN PANEL IAW DWG 148N3206 SHT 1 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE AREA INTERIOR COMPARTMENT THERE ARE CORROSION ON STRINGER 25L BETWEEN BS 1825 - 1862. FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 114. CORRODED STRINGER REMOVED. REPLACED WITH NEW STRINGER IAW DWG 148N3206 SHT 1 2 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE AREA INTERIOR COMPARTMENT BETWEEN BS 1844 - 1862 STRINGER 27L CORRODED. FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 114. CORRODED STRINGER REMOVED. REPLACED WITH NEW STRINGER IAW DWG 148N3206 SHT 1 2 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CHAFED (TE FLAP) · airframe 763 hrs · 28,324 cycles

RIGHT WING INBD TE MAIN FLAP NOSE SKIN FOUND CHAFED, 3.5 INCHES LONG FROM OTBD EDGE. REPAIRED IAW EA F-5750-T0316509 PART 1.

Part: BUSHING — WORN (LT PYLON) · airframe 763 hrs · 28,324 cycles

LEFT WING PYLON OTBD SIDE LOAD FITTING BUSHING WORN. REPAIRED IAW EA F-5740-T0316366 PART 1. CLASSIFIED AS A MAJOR REPAIR.

Part: SKIN — CHAFED (TE FLAP) · airframe 763 hrs · 28,324 cycles

RIGHT WING OTBD TE MAIN FLAP NOSE SKIN FOUND WITH CHAFE MARK AT 2.5" FROM OTBD EDGE. REPAIRED IAW EA F-5750-T0316372 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

BS 1460 - 1480 RBL 24.75, SEAT TRACK CROWN CHAFED. REMOVED IAW SRM 51-10-02 REV 114. REWORKED AREA, EVALUATED CLEAN UP DEPTH OF 0.09" EXCEEDS SEAT TRACK CROWN LIMIT 0.06" IAW SRM 53-00-52 DETAIL II FIG 101 ALLOWABLE DAMAGE 1 REV 114. SEAT TRACK REPAIR CARRIED OUT BETWEEN BS 1450 - 1540, RBL 24.75 IAW SRM 53-00-52 FIG 201 REPAIR 1 OPTION 1 REV 114. REPAIR CLASSIFIED AS MAJOR.

Part: FAILSAFE — CORRODED (BS 1480) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

CABIN, BS 1480, STRINGER 17R, FRAME FAIL SAFE FOUND CORRODED. REPAIRED IAW EA F-5310-T0317422. REPAIR CLASSIFIED AS MINOR.

Part: PANEL — CORRODED (FUEL TANK) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 960, RBL 53 - 65 CTR FUEL TANK UPPER PANEL JOINT AREA FOUND CORROSION AFTER SEALANT REMOVED. REPAIRED IAW EA F-5730-T031634.

Part: SEAT TRACK — CHAFED (BS 1570-1590) · airframe 763 hrs · 28,324 cycles

BS 1570 - 1590, LBL 45.5 SEAT TRACK CROWN CHAFED. REPAIRED IAW EA F-5310-T0317370 PT 1. CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

BS 1010 - 1020, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. REMOVED IAW SRM 51-10-02 REV 114. REWORKED AREA EVALUATED & FOUND EXCEEDS LIMIT IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 114. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00- 52 FIG 201 REPAIR 4 REV 114. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: TIE — CRACKED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

COCKPIT STATION 200 - 205, LBL 40 - 43 FLOOR TIE FOUND CRACK. CRACKED FLOOR TIE AT COCKPIT REMOVED IAW SRM 51-40-02 REV 114. NEW FLOOR TIE FABRICATED IAW DWG 141N5811 SHT 1 REV B & INSTALLED IAW DWG 141N5810 SHT 1 REV G. REPAIR CLASSIFIED AS MAJOR.

Part: PAN — CHAFED (L1 DOOR) · airframe 763 hrs · 28,324 cycles

CABIN L1 DOOR EXTERNAL HANDLE PAN FOUND CHAFFED. REMOVED IAW SRM 51-10-02 REV 114. REWORKED AREA EVALUATED & FOUND CLEAN UP DEPTH OF 0.029" EXCEED 10% LIMIT IAW SRM 52-10-01 FIG 101 ALLOWABLE DAMAGE 1 REV 114. L1 DOOR EXTERNAL HANDLE PAN REMOVED IAW SRM 51-40-02 REV 114 & REPLACED IAW DWG 141N6100 SHT 8 REV K. REPAIR CLASSIFIED AS MAJOR.

Part: PAN — CHAFED (L4 DOOR) · airframe 763 hrs · 28,324 cycles

CABIN L4 DOOR EXTERNAL HANDLE PAN FOUND CHAFED. CHAFED AREA AT L4 DOOR EXTERNAL HANDLE PAN REMOVED IAW SRM 51-10-02 REV 114 & FOUND EXCEEDED LIMIT IAW SRM 52-10-01 FIG 101. ALLOWABLE DAMAGE 1 REV 114. L4 DOOR EXTERNAL HANDLE PAN R & R IAW SRM 51-40-02 REV 114. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: TIE — CRACKED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

COCKPIT STATION 200 - 208, RBL 40 - 44 FLOOR TIE FOUND CRACK. CRACKED FLOOR TIE REMOVED IAW SRM 51-40-02 REV 114. NEW FLOOR TIE FABRICATED IAW DWG 141N5811 SHT 1 REV B. INSTALLED IAW DWG 141N5810 SHT 1 REV G. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (BS 1135-1140) · airframe 763 hrs · 28,324 cycles

CABIN STATION 1135 - 1140 RBL 45.5 SEAT TRACK CROWN FOUND CHAFED. COMPLIED WITH EA F-5310-T0316567 PART 1. REPAIR CLASSIFIED AS MINOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

CABIN STATION 1150 - 1170, LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. CHAFFED MARK REMOVED IAW SRM 51-10-02 REV 114. REWORKED AREA EVALUATED CLEAN UP DEPTH OF 0.042" FOUND EXCEEDED CROWN LIMIT OF 0.020" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 114. SEAT TRACK REMOVED FROM STATION 1080 - 1180, LBL 45.5 IAW SRM 51-40-02 REV 114. NEW SEAT TRACK FABRICATED IAW DWG 144N5021 SHT 1 REV A. INSTALLED IAW DWG 144N5001 SHT 2 REV A. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

CABIN STATION 1160 - 1180 LBL 24.75 SEAT TRACK CROWN FOUND CHAFED. REMOVED IAW SRM 51-10-02 REV 114. REWORKED AREA EVALUATED CLEAN UP DEPTH OF 0.043", FOUND EXCEEDED CROWN LIMIT OF 0.020" IAW SRM 53-00-52 FIG 101, ALLOWABLE DAMAGE 1 REV 114. SEAT TRACK REMOVED FROM STATION 1080 - 1180, LBL 24.75 IAW SRM 51-40-02 REV 114. NEW SEAT TRACK FABRICATED IAW DWG 144N5021 SHT 1 REV A & INSTALLED IAW DWG 144N5001 SHT 3 REV A. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

CABIN STATION 1380 - 1400 RT CREASE BEAM WEB UPPER SURFACE FOUND CORRODED. REMOVED IAW SRM 51-40-02 REV 114. NEW CREASE BEAM WEB FABRICATED IAW DWG 146N5590 SHT 08 REV B & INSTALLED IAW DWG 146N5590 SHT 8 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

BS 1540, LBL 10 - RBL 14.75 FLOORBEAM UPPER FLANGE UPPER SURFACE FOUND CHAFED. REPAIRED IAW EA F-5310-T0318496. CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 1420 - 1440 RT CREASE BEAM WEB UPPER SURFACE FOUND CORRODED. REMOVED IAW SRM 51-40-02 REV 114. NEW CREASE BEAM WEB FABRICATED IAW DWG 146N5590 SHT 08 REV B & INSTALLED IAW DWG 146N5590 SHT 8 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT ANGLE — CORRODED (BS 1790-1825) · airframe 763 hrs · 28,324 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT, SUPPORT ANGLE FOUND CORROSION BETWEEN BS 1790 - 1825, STRINGER 3R AFTER APU AIR INLET DOOR HOUSING REMOVED. FOUND CORROSION OUT OF LIMIT IAW SRM 53-80-02 FIG 101 DETAIL IV REV 114. SUPPORT ANGLE R & R WITH NEW FABRICATED SUPPORT ANGLE IAW EA F-5310-T0316739 A PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 740 RBL 46 - RBL 62 FLOORBEAM UPPER FLANGE FOUND CORROSION. REPAIRED IAW EA F-5310-T0318556. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

BS 345 BL 0 - LBL 20 FLOORBEAM UPPER FLANGE FOUND CHAFED. REPAIRED IAW EA F-5310-T0318494.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 1661 BL 0 - LBL 30, FLOORBEAM UPPER FLANGE UPPER SURFACE CORRODED. REPAIRED IAW EA F-5310-T0318529. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT, SUPPORT ANGLE FOUND CORROSION BETWEEN BS 1790 - 1825, STRINGER 3R, AFTER APU AIR INLET DOOR HOUSING REMOVED. FOUND CORROSION OUT OF LIMIT IAW SRM 53-80-02 FIG 101 DETAIL IV REV 114. CORRODED SUPPORT ANGLE R & R NEW FABRICATED SUPPORT ANGLE IAW EA F-5310-T0316739 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT, OUTER STRAP FOUND CORROSION AT STATION 1825, STRINGER 6R, AFTER APU AIR INLET DOOR HOUSING REMOVED. CORROSION REMOVED, FOUND OUT OF LIMIT IAW SRM 53-80-15 FIG 101 TABLE 101 ALLOWABLE DAMAGE 1 REV 114. REPAIR CARRIED OUT IAW SRM 53-80-15-2R FIG 202 DETAIL II REV 114 . REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT, SUPPORT ANGLE FOUND CORROSION AT STATION 1790 - 1825, STRINGER 6R, AFTER APU AIR INLET DOOR HOUSING REMOVED. FOUND OUT OF LIMIT IAW SRM 53-80-02 FIG 101 DETAIL IV REV 114. CORRODED SUPPORT ANGLE R & R WITH NEW SUPPORT ANGLE IAW DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 960 - 984 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 114. CREASE BEAM WEB, SHEAR WEB, REMOVED IAW SRM 51-40-02 REV 114. FABRICATED & INSTALLED IAW DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 920 - 940 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 114. REMOVED CREASE BEAM WEB, SHEAR WEB IAW SRM 51-40-02 REV 114. FABRICATED & INSTALLED IAW DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1560 - 1580 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1560 - 1580 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T60316044 PART 1.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 1080 - 1100 LT CREASE BEAM WEB FOUND CORRODED. REMOVED IAW SRM 51-40-02 REV 114. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 01 REV & INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

BS 1120 - 1140 LT CREASE BEAM WEB FOUND CORRODED. REMOVED IAW SRM 51-40-02 REV 114. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 01 REV & INSTALLED IAW DWG 144N5200 SHT 2 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1540 - 1560 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 1061) · corrosion level 2 · airframe 763 hrs · 28,324 cycles

CABIN STATION 1061 RT CREASE BEAM WEB FOUND CORROSION. REMOVED IAW SRM 51-40-02 REV 114. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 01 REV & INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1520 - 1540 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1580 - 1600 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1540 - 1560 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1600 - 1620 BETWEEN STRINGER 26 & 27. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1540 - 1560 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE, EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1600 - 1620 BETWEEN STRINGER 26 & 27. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1580 - 1600 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1540 - 1560 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1580 - 1600 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1600 - 1620 BETWEEN STRINGER 26 & 27. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1600 - 1620 BETWEEN STRINGER 26 & 27. REPAIR CARRIED OUT IAW F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 763 hrs · 28,324 cycles

FUSELAGE EXTERIOR SKIN RT SIDE, THERE IS A NEW LIGHTNING STRIKE AT BS 1560 - 1580 BETWEEN STRINGER 27 & 28. REPAIR CARRIED OUT IAW EA F-5310-T0316044 PART 1. REPAIR CLASSIFIED AS MAJOR.