N794FD

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 75,699 hrs · 29,661 cycles

ON PRE-DAPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED R/H EMERGENCY LIGHT BATTERY ASSY IAW AMM 33-51-07-2. OPERATIONAL CHECK OK. A/C OK FOR SERVICE.

Part: DRAG FITTING — CRACKED (RT NACELLE) · airframe 74,904 hrs · 29,041 cycles

C/W EA F-5730-T0378682 WING - PLATES AND SKIN - RHW PYLON DRAG FITTING TO SKIN HOLES REINSPECTION OF PREVIOUS REPAIRS AND APPROVAL. COMPLIED WITH AND COMPLETED ALL STEPS 1-15 OF EA TF-5730-T0378682 PT1 WINGS - PLATES AND SKIN - RHW PYLON DRAG FITTING TO SKIN HOLES - REINSPECTION AND REWORK OF PREVIOUS REPAIRS AND APPROVAL. MAJOR REPAIR

Part: DRAG FITTING — CRACKED (LT NACELLE) · airframe 74,904 hrs · 29,041 cycles

CW EA F-5730-T0378768 WINGS - PLATES AND SKIN - LHW PYLON DRAG FITTING TO SKIN HOLES - REINSPECTION OF PREVIOUS REPAIRS AND APPROVAL. COMPLIED WITH AND COMPLETED ALL STEPS 1-13 OF EA TF-5730-T0378768 PT1. WINGS - PLATES AND SKIN - LHW PYLON DRAG FITTING TO SKIN HOLES - REINSPECTION AND REWORK OF PREVIOUS REPAIRS AND APPROVAL. MAJOR REPAIR

Part: NONE — DAMAGED (ZONE 20) · airframe 73,659 hrs · 28,143 cycles

PDIS 794 52-20 6569 02MAY22 BFM OPEN U FLT TEST: R1 DOOR SLIDE LIGHT INOP. INFO 02MAY22 19:33 ** ATTACHED TO WORK ORDER 00082315 ** INFO 02MAY22 19:46 ** DETACHED FROM WORK ORDER 00082315 ** NOT IN PCSE INFO 02MAY22 19:47 ** ATTACHED TO WORK ORDER 00082315 ** REPLACED TERMINAL ON WIRE GOING TO #1 LUG ON SLIDE INDICATOR LIGHT IAW SWPM 20-30- 11. OPS CHECK GOOD IAW AMM 52-11-25-5

Part: ANGLE — CRACKED (ZONE 200) · airframe 73,657 hrs · 28,142 cycles

FWD CARGO COMPT STA. 580 LBL 45.5 MDC FLOOR BEAM HAS CRACK. PERFORMED A ANGLE REPAIR AT STA. 580 LBL 45 PER FEDEX DRAWING #SR57-53-004 AND E.A. F- 5310-T0367757A P1, FUSELAGE-MAINFRAME-FLOOR BEAM AT STA 580 AND LBL 45 CRACKED- REPAIR PER DRAWING SR57-53-004, MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 20) · airframe 73,657 hrs · 28,142 cycles

ZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T22/1610229 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 20) · airframe 73,657 hrs · 28,142 cycles

ZONE 220 FLOOR BOARD 221MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MAF ON VT MAE TRAVELER T22/1610230 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR

Part: FLOOR PANEL — DAMAGED (ZONE 20) · airframe 73,657 hrs · 28,142 cycles

ZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T22/1610312 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 20) · airframe 73,657 hrs · 28,142 cycles

ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T22/1610228 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIR

Part: FLOORBOARD — DAMAGED (ZONE 20) · airframe 73,657 hrs · 28,142 cycles

ZONE 220 FLOOR BOARD 222MCF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MCF ON VT MAE TRAVELER #T22/1610311 IAW DWG SRZ-25-005. MAJOR REPAIR

Part: GUST LOCK — FAILED (R1 DOOR) · airframe 72,487 hrs · 27,306 cycles

R1 ENTRY DOOR GUST LOCK COLLAR CRACKED/BROKEN. REPLACED BROKEN R1 DOOR HOLD-OPEN LOCK COLLAR WITH A NEW SPLIT COLLAR AND CATCH, REF B757 AMM 52-11-08-8. ALLIANCE AEROSPACE ENGINEERING KIT PN 10-N0244-8 CONTAINS 10-N6008-4 (LOT 22457 SN 12-0010) 10-N6009-1 (LOT 23013).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,989 hrs · 26,984 cycles

DURING PRE-FLIGHT NOTED EMERGENCY EXIT LIGHT OVER L1 DOOR NOT TESTING. ALONG WITH THE EMERGENCY LIGHT JUST OUTSIDE OF L1 DOOR

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 71,989 hrs · 26,984 cycles

EXTERIOR EXIT DOOR LIGHT OUTSIDE OF L1 DOOR NOT TESTING.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,907 hrs · 26,937 cycles

POPPED RIVET HEAD EXTERIOR FUSELAGE STA 1460 STR 29L. REMOVED RIVETS AT STA 1460,STR 29L IAW B 757 SRM 51-40-02-OG,REMOVED AND REINSTALLED STRINGER SPLICE AT STA 1452 TO 1468 IAW B 757 SRM 51-40-02-OG.FOUND CORROSION ON STRINGER SECTION,29L 100% MAT. LOSS,FOUND TO BE OUT OF LIMITS REMOVED,FABRICATED AND INSTALLED STR. SECTION AND SPLICE REPAIR @ STA 1460 TO 1498,S-29L IAW B 757 SRM 51-10-02-OG AND 53-00-03-2R,REP 2,FIG 201.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 71,907 hrs · 26,937 cycles

AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #5 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 607.47 EVALUATED FWD CARGO LOWER #5 ANGLE 100% MATERIAL LOSS DUE TO CORR. OUT OF LIMITS IAW B 757 SRM 52-30-02-1A DET VI REMOVED,FABRICATED AND INSTALLED NEW ANGLE IAW B 757 SRM 51-40-02 AND BOEING DWG 143N6603 REV AT AND B.AT STA 607.47

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,907 hrs · 26,937 cycles

AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #1 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 572.53 EVALUATED FWD CARGO DOOR LOWER # 1 ANGLE 100% MATERIAL LOSS DUE TO COORR. OUT OF LIMITS IAW B 757 SRM 52-30-02-1A DET VI. REMOVED,FABRICATED AND INSTALLED NEW ANGLE IAW B 757 SRM 51-40-02 BAND BOEING DWG 143N6603 REV AT AND REV B.AT STA 572.53

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,907 hrs · 26,937 cycles

AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #4 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 600. EVALUATED FWD CARGO DOOR LOWER #4 ANGLE,ORIF. MAT=.050",REM. MAT= .024",MAT LOSS=.026" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 52-30-02-1A,DETAIL VI. REMOVED,FABRICATED AND INSTALLED NEW ANGLE IAW B 757 SRM 51-40-02-OG AND BOEING DWG: 143N6603,REV: AT AND REV: B. AT STA 600.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,907 hrs · 26,937 cycles

AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #2 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 580. EVALUATED FWD CARGO DOOR LOWER #2 ANGLE 100% MATERIAL LOSS DUE TO CORR. OUT OF LIMITS IAW B 757 SRM 52-30-02-1A DET.VI. REMOVED,FABRICATED AND INSTALLED NEW ANGLE IAW B 757 51-40-02 AND BOEING DWG 143N6603 REV AT AND REV B.AT STA 580.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 71,907 hrs · 26,937 cycles

AFTER REMOVING C1 DOOR LOWER CENTER DEPRESSOR,FOUND #3 ANGLE CORRODED,LOKING FWD TO AFT AT APPROX. STA 588.93 EVALUATED FWD CARGO DOOR LOWER #3 ANGLE 100% MATERIAL LOSS DUE TO CORR. OUT OF LIMITS IAW B 757,SRM 52-30-02-1A,DETAIL VI. REMOVED,FABRICATED AND INSTALLED NEW ANGLE IAW B 757 SRM 51-40-02-OG AND BOEING DWG: 143N6603,REV: AT AND REV: B.

Part: SKIN — GOUGED (TE FLAP) · airframe 71,907 hrs · 26,937 cycles

R / WING OB FLAP L/E UPPER SKIN GOUGE. REMOVED GOUGE ON RT WING O/B FLAP L/E FOUND O/B BLENDOUT TO BE OUT LIMITS IAW B757 SRM 57-53-01-1A FIG 101 DET. VI AND SRM 51-10-02-OG,CUT OUT DAMAGE AREA AND INSTALLED REPAIR DOUBLERS,STRAPS AND REPAIR PLATE IAW B757 SRM 57-53-01-2R REPAIR 2.

Part: BRAKE — LACK OF LUBE (TE FLAP) · airframe 71,055 hrs · 26,378 cycles

TE FLAPS DISAGEE WHEN SELECTING FLAPS 25. FLAPS DID NOT MOVE PAST 20. TROUBLESHOT PER FIM 27-51-01 FT 808 FIG 105. FOUND RIGHT INBOARD FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. PERFORMED LUBRICATION OF THE FLAP TRANSMISSION TORQUE BRAKE AND BALLSCREW/GIMBAL PER 12-21-09-3. VERIFIED RIGHT INBOARD FLAP TRANSMISSION FLUID IS FULL. RESET OVERLOAD IDICATOR AND CHECKED FOR BINDING OF THE FLAP, AFT FLAP, CARRIAGE AND BALLSCREW/GIMBAL. NO EVIDENCE OF BINDING FOUND. OPERATED FLAPS FROM 0-30 SEVERAL TIMES AND ALL INDICATIONS ARE NORMAL. RIGHT INBOARD FLAP TRANS OVERLOAD INDICATOR STAYED SET. A/C OK FOR SERVICE.

Part: TAIL CONE — DAMAGED (FUSELAGE) · airframe 70,465 hrs · 25,996 cycles

TAIL SECTION DAMAGE AROUND APU EXHAUST AREA ALONG WITH APU DR(S). APU DOOR DAMAGE WILL BE WORKED ON WRI 52-40/3817. REMOVED DAMAGED APU EXHAUST TAIL CONE REF AMM 49-81-01-2. NO DAMAGE FOUND TO APU EXHAUST DUCT REF AMM 49-81-01-2. FIVE MISS-ALIGNED HOLES NEED WELDED ON LOWER LEADING EDGE OF EXHAUST DUCT. FILLED 5 MISALIGNED HOLES BY WELDING FOR REDRILLING. TRIMMED TO FIT LEADING EDGE MATCHED DRILLED 6 HOLES IN REF TO SRM 51-40-01. REMOVAL/INSTALLATION OFF MPN: 148N8301-22 CPN: 5317327 POS: ONL ON MPN: 148N8301-22 SRL: FX0001. FINISHED DRILLING TAILCONE, REF SRM 51-40-01. INSTALLED TAILCONE IN REF TO AMM 49-81-03-4. WELD REPAIR COMPLIED WITH, PER EA F-5318-T0341262.

Part: DOOR — DAMAGED (TAILCONE) · airframe 70,465 hrs · 25,996 cycles

APU ACCESS DOORS DAMAGED. REMOVED DAMAGED LEFT AND RIGHT APU ACCESS DOORS REFERENCING AMM 52-48-05-4. INSTALLED A SERVICEABLE LEFT DOOR ASSY (315AL) REFERENCING AMM 52-48-05-4 AND ERS 18-03216. REMOVED PART HAS NO P/N OR S/N. WORKBENCH REMOVAL AND INSTALLATION TRANSACTION WARNINGS ( ALERT 18-0064) ADDRESSED BY ERS 18-03216 WHICH AUTHORIZES THE R&R. INSTALLATION REVIEWED BY ENGINEERING PER GMM 06-1-50.

Part: DOOR — DAMAGED (TAILCONE) · airframe 70,465 hrs · 25,996 cycles

APU ACCESS DOORS DAMAGED. REMOVED DAMAGED LEFT AND RIGHT APU ACCESS DOORS REFERENCING THE AMM 52-48-05-4. INSTALLED SERVICEABLE RIGHT APU ACCESS DOOR REFERENCING AMM 52-48-05-4. OPERATIONAL CHECKS GOOD FOR FUNCTION AND SECURITY.

Part: UNKNOWN — UNKNOWN · airframe 70,063 hrs · 25,722 cycles

A/C WAS HIT BY GROUND VEHICLE DURING LOADING REPAIR CURRENTLY IN PROGRESS REQUIRING SHEET METAL FABRICATION AND ENGINEERING SUPPORT. SDR SUBMITTED TO DOCUMENT MAJOR REPAIR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,929 hrs · 25,643 cycles

R1 DOOR EMERGENCY SLIDE LIGHT INOP DURING TEST. RELAMPED AND OPS CHECK NORMAL REF MM 33-51-06-2-1. A/C OK FOR SERVICE.

Part: TRANSMISSION — FAILED (TE FLAPS) · airframe 69,793 hrs · 25,532 cycles

ON APPROACH, RECEIVED A TE FLAPS DISAGREE EICAS AND LIGHT THROUGH FLAPS 15 TO 20 SETTING. COMPLIED WITH QRH AND FOUND THE RIGHT INBD FLAP INBD FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. RESET OVERLOAD INDICATOR,. LUBRICATED THE FLAP BALLSCREW, GIMBLE AND CARRIAGE ROLLERS. FLUID LEVEL IN RIGHT INBOARD TRANSMISSION NORMAL. INSPECTED ALL OTHER JACKSCREWS AND FLAP TRANSMISSIONS FOR FLUID LEVEL AND TRIPPED OVERLOAD INDICATORS. ALL CHECKED NORMAL. RAN FLAPS UP AND DOWN SEVERAL TIMES. FLAPS RAN WITHIN MM LIMITS. IAW FIM 27-51, TREE 808, MM 12-21-09-3, AND 27-51-00-5. AIRCRAFT OK FOR SERVICE

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 69,235 hrs · 25,183 cycles

DURING FLAP EXTENSION FROM 20 TO 30, L FLAP INDICATOR MOVED TO 30 WHILE R FLAP INDICATOR REMAINED AT 20. NO FLAP ASYM EICAS, NO ROLLING MOTION FELT (AUTOPILOT WAS OFF). REPOSITIONED FLAPS TO 20, COMPLIED WITH QRH, LANDED FLAPS 20. INSTALLED NEW INDICATOR AND CHECKED GOOD PER MM 27-58-2-4.

Part: RESERVOIR — LOW PRESSURE (R1 DOOR) · airframe 67,331 hrs · 23,872 cycles

R1 DOOR EMER POWER RESERVOIR PRESS LOW. REPLACED EMER POWER RESERVOIR FOR R1 DOOR. CHECK GOOD IAW MM.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 67,158 hrs · 23,736 cycles

L1 DOOR SLIDE EMER LIGHT INOPERATIVE. RELAMPED L1 DOOR SLIDE LIGHT IAW MM 33-51-06-2-1. OPERATIONS CHECKED GOOD.

Part: SKIN — GOUGED (BS 1498) · airframe 67,032 hrs · 23,649 cycles

FUSELAGE SKIN REPAIRGOUGED AT BS 1498 BETWEEN STRINGERS 22 - 23L. REPAIRED IAW EA F-5330- T0305873 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

CABIN FLOORBEAM BS 365 EXISTING REPAIR HAS CORROSION AT RBL 8 & 24. ACCOMPLISHED EA F-5310-T0307490 PART 1 TITLE FUSELAGE, MAINFRAME & FLOORBEAM REPAIR, STATION 365.25 LBL 10 - RBL 70. REFER TO SNRM N01804 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (BS 1480-1500) · airframe 67,032 hrs · 23,649 cycles

FUSELAGE SKIN REPAIR SCRATCHED BS 1480 - 1500 STRINGER 21L. REPAIRED IAW EA F-5330-T0305873 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — GOUGED (BS 1500-1520) · airframe 67,032 hrs · 23,649 cycles

FUSELAGE SKIN REPAIR GOUGED AT BS 1500 - 1520 BETWEEN STRINGERS 21 - 22 LT. REPAIRED IAW EA F-5330-T0305873 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

AFT CARGO COMPARTMENT CARGO DOOR CUT OUT NUTPLATE RETAINING STRAP HAS CORROSION. COMPLIED WITH EA F-5310-T0306966 PT 1, TITLE FUSELAGE, MAINFRAME, ACCOMPLISH EXISTING REPAIR AT LOWER NR 2 CARGO DOOR WAY LOWER MAIN SILL STATION 1391, 1400, 1406 & 1429. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — GOUGED (BS 1485) · airframe 67,032 hrs · 23,649 cycles

FUSELAGE REPAIR GOUGED AT BS 1485 BETWEEN STRINGER 22 - 23L. REPAIRED IAW EA F-5330-T0305873 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — SCRATCHED (BS 1440-1460) · airframe 67,032 hrs · 23,649 cycles

FUSELAGE REPAIR SCRATCHED AT BS 1440 - 1460 STRINGER 23 - 24L. REPAIRED IAW EA F-5330-T0305827 PART 1. REPAIR CLASSIFIED MAJOR IAW 6-2-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,032 hrs · 23,649 cycles

FUSELAGE EXISTING REPAIR, THERE IS A DAMAGED RIVET WITH A BULGE AT BS 1455 AT STRINGER 18 - 20 LT. COMPLIED WITH EA F-5330-T0305872 PART 1, TITLE FUSELAGE, PLATES & SKINS & FUSELAGE SKIN LAP JOINT REPAIR STATION 1400 - STATION 1459 STRINGER 18L - STRINGER 23L. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SILL — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

AFT CARGO BAY DOOR LOWER SILL BS 1380 - 1440 CORRODED AROUND SCREW HOLES. CORROSION REMOVED IAW SRM 51-40-05 REV 111. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 310) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

CABIN FLOORBEAM BS 310 RT SIDE, CORRODED ON THE EXISTING REPAIR. REPAIRED IAW SRM 51-40-02 REV 111 & DWG 141N5810 SHT 13 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (ZONE 200) · airframe 67,032 hrs · 23,649 cycles

BS 1320 - 1350, LBL 24.75, SEAT TRACK CROWN & BOTTOM FOUND CHAFED. REPAIRED IAW SRM 53-00-52 FIG. 201 REPAIR 1 REV 111. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CHAFED (BS 1280-1320) · airframe 67,032 hrs · 23,649 cycles

BS 1280 - 1320, SEAT TRACK CROWN & BOTTOM FOUND CHAFED. REPAIRED IAW SNRM N02161. REPAIR CLASSIFIED AS MAJOR.

Part: SEAL DEPRESSOR — CHAFED (ZONE 200) · airframe 67,032 hrs · 23,649 cycles

R4 DOOR CUTOUT UPPER INNER SURFACE SEAL DEPRESSOR CHAFED. SEAL DEPRESSOR REMOVED AND REPLACED WITH NEW DEPRESSOR FABRICATED AS PER DWG 146N6123 SHT.1 REV.- AND INSTALLED IAW DWG 146N3700 SHT.11 REV.B. REPAIR IS MAJOR.

Part: FLOORBEAM — GOUGED (ZONE 100) · airframe 67,032 hrs · 23,649 cycles

FLOORBEAM GOUGED ON THE EXISTING REPAIR AT BS 1680 AT LBL 13 UPPER SIDE. REPAIRED IAW EA F-5310-T0306261 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR PANEL — SCRATCHED (ZONE 100) · airframe 67,032 hrs · 23,649 cycles

FLOOR PANEL SCRATCHED ON EXISTING REPAIR AT BS 1683 AT LBL 5 - 17 UPPER SIDE. REPAIRED IAW EA F-5310-T0306261 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR PANEL — GOUGED (ZONE 100) · airframe 67,032 hrs · 23,649 cycles

FLOOR PANEL GOUGED ON THE EXISTING REPAIR AT BS 1683 AT RBL 55 UPPER SIDE. REPAIRED IAW EA F-5310-T0306261 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — GOUGED (ZONE 100) · airframe 67,032 hrs · 23,649 cycles

FLOORBEAM GOUGED ON THE EXISTING REPAIR AT BS 680 AT LBL 9 UPPER SIDE. REPAIRED IAW EA F-5310-T0306261 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

CABIN RT SIDE FLOOR PANEL CORRODED ON EXISTING REPAIR AT BS 1681 AT RBL 12 UPPER SIDE. REPAIRED IAW EA F-5310-T0306261 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

CABIN FLOORBEAM CORRODED ON EXISTING REPAIR AT BS 1683 AT RBL 15 - 18 LOWER SIDE.

Part: FLOORBEAM — GOUGED (ZONE 100) · airframe 67,032 hrs · 23,649 cycles

FLOORBEAM GOUGED ON THE EXISTING REPAIR AT BS 1680 AT LBL 11 UPPER SIDE. REPAIRED IAW EA F-5310-T0306261 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — GOUGED (ZONE 100) · airframe 67,032 hrs · 23,649 cycles

FLOORBEAM GOUGED ON THE EXISTING REPAIR AT BS 1680 AT LBL 12 UPPER SIDE. REPAIRED IAW EA F-5310-T0306261 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (R4 DOOR) · airframe 67,032 hrs · 23,649 cycles

R4 DOOR INNER SKIN CRACKED. REPAIRED IAW EA F-5210-T0306364 PART 1. REPAIR CLASSIFIED AS MAJOR

Part: SKIN — CHAFED (R4 DOOR) · airframe 67,032 hrs · 23,649 cycles

R4 DOOR INNER SKIN CUT OUT EDGE CHAFED. REPAIRED IAW EA F-5210-T0306364 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (R4 DOOR) · airframe 67,032 hrs · 23,649 cycles

R4 DOOR INNER SKIN CRACKED. REPAIRED IAW EA F-5210-T0306364 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FAILSAFE — CHAFED (BS 1620) · airframe 67,032 hrs · 23,649 cycles

AFT CARGO BAY LT SIDE FRAME BS 1620, FAILSAFE CHAFED BETWEEN STRINGERS 29R & 29L. REPAIRED IAW EAF-5310-T0306258 PART 1. REPAIR IS MAJOR.

Part: SUPPORT ANGLE — CORRODED (BS 1789) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED AT BS 1789, STRINGER 6R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 111. SUPPORT ANGLE REMOVED AND REPLACED. NEW FABRICATED IAW DWG 148N3141 SHT 1 REV. B & DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SUPPORT ANGLE — CORRODED (BS 1790-1825) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED BETWEEN BS 1790 - 1825, STRINGER 3R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 111. SUPPORT ANGLE REMOVED AND REPLACED WITH NEW IAW DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SUPPORT ANGLE — CORRODED (BS 1790-1825) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT, SUPPORT ANGLE FOUND CORRODED BETWEEN BS 1790 - 1825 STRINGER 6R. CORROSION REMOVED, AND FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 111. SUPPORT ANGLE REMOVED AND NEW FABRICATED IAW DWG 148N3152 SHT 1 REV - . INSTALLED IAW DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRAP — CORRODED (BS 1787) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

APU AIR INLET DOOR CUT OUT, FWD STRAP HAS CORROSION AT BS 1787, STRINGERS 3 - 6R. CORROSION REMOVED FOUND OUT OF LIMITS IAW SRM 51-10-02 REV 111. STRAP REMOVED AND REPLACED WITH NEW STRAP IAW DWG. 148N3105 SHT 1 REV C. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FITTING — CHAFED (ENGINE MOUNT) · airframe 67,032 hrs · 23,649 cycles

DURING COMPLYING EO F7120-7-5000 PT1 FIG 1 SHEET 1 STEP 7. AFTER REMOVAL OF NR 1 PYLON AFT ENG MOUNT INBD SHEAR BOLT FLANGED BUSHING, BUSHING HOLE FOUND WITH FRETTING. REPAIRED IAW EA F-5450-T0307098 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 997) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

CREASE BEAM INBD ANGLE UPPER EDGE FOUND CORRODED BS 997. REPAIRED IAW EA F-5310-T0306904 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — DENTED (BS 1500) · airframe 67,032 hrs · 23,649 cycles

AFT CARGO BAY LT SIDE FRAME BS 1500, HAS TWO DENTS AT UPPER FLANGE, BETWEEN STRINGERS 25 & 27L. REPAIRED IAW EA F-5310-T0306362 P1. REPAIR CLASSIFED AS MAJOR.

Part: FRAME — CORRODED (BS 1500) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

AFT CARGO BAY LT SIDE FRAME BS 1500, FRAME HAS CORROSION ON UPPER FLANGE, BETWEEN STRINGERS 26 & 27L. REPAIRED IAW EA F-5310-T0306362 P1. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

BS 1020 - 1040 CREASE BEAM INBD ANGLE UPPER SURFACE FOUND CORRODED. REPAIRED IAW EA F-5310-T0306951 PART 1. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

CABIN FLOORBEAM AT BS 1681 IS CORRODED, RBL 45 - 60. REMOVED AND REPLACED WITH NEW FABRICATED IAW DWG 146N5111 SHT.1 REV.B AND INSTALLED IAW DWG 146N5091 SHT.11 REV-. REPAIR IS MAJOR.

Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

EMPENNAGE, APU AIR INLET DOOR CUT OUT INNER STRAP FOUND CORRODED AT BS 1825, STRINGER 3 - 6R. AFTER APU AIR INLET DOOR HOUSING REMOVED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-80-15 TABLE 101 AD 1 REV 111 & REPAIRED IAW SRM 53-80-15 REPAIR 1 DETAIL II FIG 202REV 111 REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — CRACKED (BS 1362) · airframe 67,032 hrs · 23,649 cycles

AFT CARGO BAY BS 1362, STRINGER 20R, STRINGER CRACKED. REPAIRED IAW EA F-5310-T0306906 P1.

Part: FRAME — CHAFED (FUSELAGE) · airframe 67,032 hrs · 23,649 cycles

CABIN BS 940 STRINGER 15R, FRAME INBD CHORD AFT SURFACE FOUND CHAFED. COMPLIED WITH EA F-5310-T0306707 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOOR FRAME — CHAFED (FUSELAGE) · airframe 67,032 hrs · 23,649 cycles

CABIN STATION 340, STRINGER 7L - 8L L1 DOOR CUTOUT FWD FRAME INBD FLANGE FOUND CHAFED. COMPLIED WITH EA F-5310-T0306332 TITLE, FUSELAGE, MAINFRAME CHAFE MARK ON STUB FRAME FLANGE, FWD OF NR 1 LT DOOR CUT OUT, STATION 338.

Part: CREASE BEAM — CHAFED (BS 936) · airframe 67,032 hrs · 23,649 cycles

BS 936 RT CREASE BEAM WEB UPPER SURFACE FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 110. FOUND OUT OF LIMIT SIAW SRM 53-40-13 AD 1 FIG 101 REV 110. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 111. NEW CREASE BEAM WEB FABRICATED & INSTALLED IAW DWG 114N5140 SHT 3 REV D.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

CABIN, STATION 760 - 780 LT CREASE BEAM INNER CHORD FOUND CORROSION & CHAFED. COMPLIED WITH EA F-5310-T0305978 PART 1, TITLE, FUSELAGE MAINFRAME CREASE BEAM INBD CHORD. SPLICE REPAIR AT BS 790 & LBL 64.40, REPAIR.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

CABIN STATION 377 - 395 L1 DOOR LOWER SILL WEB FOUND CORROSION AT LOWER SURFACE. REMOVED IAW SRM 51-10-02 REV 110. REWORK AREA, EVALUATED MATERIAL THICKNESS REMOVED 0.018 INCHES, FOUND EXCEED 10% LIMIT IAW SRM 53-10-15, ALLOWANCE DAMAGE 1 FIG 101 REV 110. L1 DOOR LOWER SILL WEB FABRICATED & INSTALLED IAW DRAWING 141N8322 SHT 1 REV K & 141N8322 SHT 2 REV F.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

CABIN STATION 377 - 395 L1 DOOR LOWER SILL WEB FOUND CORROSION AT LOWER SURFACE. REMOVED IAW SRM 51-10-02 REV 110. REWORKED AREA EVALUATED MATERIAL THICKNESS, REMOVED 0.018 INCHES FOUND EXCEED 10 % LIMIT IAW SRM 53-10-15, ALLOWANCE DAMAGE 1 FIG 101 REV 110. L1 DOOR LOWER SILL WEB REMOVED IAW SRM 51-40-02 REV 111. L1 DOOR LOWER SILL WEB FABRICATED & INSTALLED IAW DWG 141N8322 SHTTE 1 REV K & 141N8322 SHT 2 REV F.

Part: CREASE BEAM — CORRODED (BS 620-640) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

BS 620 - 640 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 110. FOUND OUT OF LIMITS IAW SRM 53-30-13 AD 1 FIG 101 REV 110. CREASE BEAM WEB R & R IAW SRM 51-40-02 REV 111 & DWG 143N5520 SHT 3 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 620-640) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

BS 620 - 640 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 110. FOUND OUT OF LIMITS IAW SRM 53-30-13, AD 1 FIG 101 REV 110. CREASE BEAM WEB R & R IAW SRM 51-40-02 REV 111 & DWG 143N5520 SHT 3 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (BS 1218) · airframe 67,032 hrs · 23,649 cycles

BS 1218 LBL 45.5 SEAT TRACK OTBD FLANGE UPPER FLANGE FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 110. FOUND WITHIN LIMITS IAW SRM 53-00-52 AD 1 FIG 101 REV 110. REPAIR CLASSIFIED AS MINOR.

Part: FRAME — CHAFED (BS 1640) · airframe 67,032 hrs · 23,649 cycles

BS 1640 STRINGER 6R - 7R FRAME CHAFED. REPAIRED IAW EA F-5310-T0306207 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (BS 1320-1380) · airframe 67,032 hrs · 23,649 cycles

BS 1320 - 1380, LBL 24.75, SEAT TRACK INBD FLANGE UPPER SURFACE FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 110. FOUND OUT OF LIMITS IAW SRM 53-00-52 AD 1 FIG 101 REV 110. REPAIRED IAW SRM 53-00-52 FIG 201 REPAIR 1 REV 111. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (BS 1182) · airframe 67,032 hrs · 23,649 cycles

BS 1182, RBL 45.5, SEAT TRACK OTBD FLANGE UPPER FLANGE FOUND CHAFED. CHAFE REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-52 AD 1 FIG 101 REV 110. SEAT TRACK REMOVED IAW SRM 51-40-02 REV 111. NEW SEAT TRACK FABRICATED IAW DRAWING 146N5133 SHT 2 REV - & INSTALLED IAW DRAWING 146N5120 SHT 24 REV -. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — GOUGED (BS 1640) · airframe 67,032 hrs · 23,649 cycles

BS 1640 STRINGER 5 - 8L, FRAME IS GOUGED. REPAIRED IAW EA F-5310-T0306287 PART 1. MAJOR REPAIR.

Part: SEAT TRACK — CHAFED (BS 1260-1320) · airframe 67,032 hrs · 23,649 cycles

BS 1260 - 1320, LBL 24.75 SEAT TRACK INBD FLANGE UPPER SURFACE FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 110, FOUND OUT OF LIMITS IAW SRM 53-00-52 AD 1 FIG 101 REV 110. REPAIRED IAW SRM 53-00-52 FIG 201 REPAIR 1 REV 111. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 377.7) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

BS 377.7, LBL 46 - 60 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 110. FOUND OUT OF LIMITS IAW SRM 53-00-51 1 FIG 101 REV 110. FLOORBEAM TEE REMOVED RBL 70 TO LBL 70 IAW SRM 51-40-02 REV 111. NEW TEE FABRICATED IAW DWG 141N5123 SHT 1 REV A & INSTALLED IAW DWG 141N5113 SHT 1 REV F. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 67,032 hrs · 23,649 cycles

BS 560 LBL 14 - RBL 10 FLOORBEAM UPPER FLANGE FOUND CHAFED. REPAIRED IAW EA 757-5335-08-E2522 REV. REPAIR CLASSIFIED AS MINOR.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 67,032 hrs · 23,649 cycles

BS 377.7, LBL 62 - 64 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 110. FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101 REV 110. FLOORBEAM TEE REMOVED RBL 70 - LBL 70 IAW SRM 51-40-02 REV 111. NEW TEE FABRICATED IAW DWG 141N5123 SHT 1 REV A & INSTALLED IAW DWG 141N5113 SHT 1 REV F. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (BS 440-460) · airframe 67,032 hrs · 23,649 cycles

FUSELAGE SKIN NICKED & SCRATCHED BETWEEN STRINGER 26L & 26R BS 440 - 460. REPAIRED IAW EA F-5330-T0306587 PART 1. REPAIR IS MINOR.

Part: SKIN — DAMAGED (BS 1600-1620) · airframe 67,032 hrs · 23,649 cycles

FUSELAGE SKIN NICKED & SCRATCHED BETWEEN STRINGERS 26L & 26R BS 1600 - 1620. REPAIRED IAW EA F-5330-T0305865 PART 1. REPAIR IS MINOR.

Part: SKIN — DAMAGED (BS 680-700) · airframe 67,032 hrs · 23,649 cycles

FUSELAGE SKIN NICKED & SCRATCHED BETWEEN STRINGERS 26L & 26R BS 680 - 700. NICKS AND SCRATCHES REMOVED IAW SRM 51-10-02 REV 110. FOUND WITHIN LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 111. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.