N995FD

Part: BOTTLE — EMPTY (ZONE 100) · airframe 50,647 hrs · 22,215 cycles

DURING B-CHECK FOUND AFT O2 BOTTLE AT ZERO PRESSURE. REPLACED BOTTLE PER AMM ON NON ROUTINE 8, PERFORMED MVP ON WRI 0000813271. REMOVED AND REPLACED AFT OXYGEN BOTTLE PER 757 AMM 35-11-30-4-99. AC OK FOR SERVICE

Part: GROUND STUD — UNSECURE (EMERGENCY LIGHTS) · airframe 50,563 hrs · 22,155 cycles

EMERGENCY LIGHTS WON'T TEST FROM NOSE GEAR SWITCH S10035. CK OK FROM TEST SWITCH ABOVE L1 DOOR. CHECKED FOR POWER AND GROUND AT SWITCH S10035. POWER GOOD AT TERMINAL 2 BUT FOUND NO GROUND ON TERMINAL 1. FOUND LOOSE CONNECTION AT GROUND STUD GD29-DC. SECURED LOOSE NUT. SLIDE LIGHT OPS TESTED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 50,550 hrs · 22,145 cycles

EMERGENCY LIGHTS WON'T TEST USING ANY/ALL SWITCHES. REMOVED AND REPLACED BATTERY PACK FOR POWER SUPPLY M 730 AND M731 OPS CHECK GOOD REF AMM 33-51-07- 2. PART REMOVED IS RADIANT POWER CORP BATTERY ASSEMBLY PART NUMBER 2103-1A.

Part: SKIN — UNKNOWN (N/A) · airframe 48,823 hrs · 20,910 cycles

DURING THE ACCOMPLISHMENT OF THE PREVENTATIVE DOUBLER INSTALLATION PER EO F- 5330-E0341230-P12, IT WAS NOTED THAT HAECO MX COULD NOT COMPLY WITH WORK INSTRUCTIONS AS DIRECTIED WITH IN THE EO AND ASSOCIATED INSTALLATION DRAWING DUE TO ACFT CONFIGURATION. COMPLIED WITH FEDEX EA F-5330-T0364361-P1 IN CONJUNCTION WITH EO F-5330-E0341230- P12.

Part: FLAP — DELAMINATED (ZONE 600) · airframe 48,823 hrs · 20,910 cycles

INBOARD FLAP LOWER INBOARD PANEL IS DELAMINATED. REPAIRED I/B FLAP LOWER I/B PANEL WITH PERMANENT REPAIR IAW B757 SRM 57-53-01-2R FIG 201 SHEET 2 AND 51-70-10-2R.

Part: WEB — DAMAGED (L1 DOOR CUTOUT) · airframe 48,823 hrs · 20,910 cycles

L1 DOOR CUTOUT, INNER WEB AT SNUBBER LOCATION IS DAMAGED DAMAGE BLENDED ON L1 DOOR CUTOUT WEB IAW B757-200 SRM 51-10-02 . ORIGINAL THICKNESS OF WEB IS .050 , REMAINING THICKNESS IS .025 , LOSS OF MATERIAL IS .025 FOUND TO BE OUT OF LIMITS IAW BAC DWG 141N8315 REV:M . REMOVED AND REPLACED WEB IAW BAC DWG 141N8315 REV:M , SRM 51-40-02 . ALODINED AND PRIMED IAW B757-200 SRM 51-20-01 , TOPCATED IAW B757-200 AMM 51-21-10

Part: NONE — NONE (NONE) · airframe 48,823 hrs · 20,910 cycles

LEFT ELEVATOR LOWER INBOARD SURFACE HAS TWO DENTS REPAIRED LEFT ELEVATOR LOWER INBOARD SURFACE IAW B757 SRM 55-20-01-2R AND 51-70- 05-0G PARA. 5.B.

Part: NONE — DELAMINATED (ZONE 500) · airframe 48,823 hrs · 20,910 cycles

LEFT WING, OUTBOARD FLAP, AFT FLAP, 6 - INCHES FROM INBOARD EDGE POSSIBLLY DELAMINATED. REMOVED DELAMINATED PREVIOUS REPAIR AND REPAIRED LEFT WING OUTBOARD FLAP AFT FLAP 6" FROM INBOARD EDGE IAW B757 SRM 57-53-01-2R1 FIG 201 SHEET 5.

Part: SKIN — DENTED (BS 1730) · airframe 48,823 hrs · 20,910 cycles

FUSELAGE LOWER EXTERIOR SURFACE AT STA 1730 HAS 3 EA PROTRUDING DENTS MEASURED DENTS ON FUSELAGE LOWER EXTERIOR SURFACE SKIN AT STA 1730 , DENT1 : A=.300 AND Y=.004 = .300/.004= 75 , DENT2 : A=.301 Y=.002 A/Y= 150 AND DENT 3 : A=.350 Y=.022=15 , DENT #3 IS OUT OF LIMITS AND DENT #1 AND DENT #2 ARE IN LIMITS IAW B757-200 SRM 53-80-01-1A , ALSO CRACK FOUND IN DENT #3 AFTER HFEC INSPECTION . DAMAGE CUTOUT AND INSTALLED SKIN REPAIR DOUBLER IAW B757-200 SRM 53-00-01- 2R . ALODINED AND PRIMED IAW B757-200 SRM 51-20-01 AND TOPCATED IAW B757-200 AMM 51-21-00

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 48,823 hrs · 20,910 cycles

RIGHT WING, OUTBD MAIN FLAP, CENTER LEADING EDGE SKIN HAS 2EA WEAR SPOTS. REPAIRED RH WING OB MAIN FLAP IAW EA F-5750-T0364593-P1,

Part: SEAT TRACK — DAMAGED (BS 580) · airframe 48,823 hrs · 20,910 cycles

MAIN DECK SEAT TRACK SECTION IS DAMAGED @ STA 580, LBL 45 REPAIRED SEAT TRACK SECTION FROM STA 530 - STA 610, LBL 45 IAW FEDEX EA # F-5310-T0364284-P1, RELEASED OCT 05, 2021, TITLED " FUSELAGE - MAINFRAME - SEAT TRACK, STA 580, LBL 45, DAMAGED SCALLOP"

Part: CONTROL PANEL — MALFUNCTIONED (COCPIT) · airframe 47,708 hrs · 20,132 cycles

WHILE FINISHING PRE-FLIGHT WITH 'BEFORE START CHECKLIST' COMPLETED 'TO-THE-LINE' THE AFT PEDESTAL FIRE/OVERHEAT FAIL LIGHT WAAS ILLUMINATING INTERMITTENTLY. THEN WE SMELLED AN ACID BURNING SMELL FOLLOWED BY A VISUALLY VERIFIED FIRE (FLAMES) INSIDE THE AFT PEDESTAL. WE IMMEDIATELY SHUT DOWN POWER TO THE AIRCRAFT, STOPPED LOADING, AND CALLED AIRCRAFT MX AND ARFF. INSTALLED NEW PANEL AS PER AMM 26-11-02-4. OPERATION CHECKS NORMAL. A/C OK FOR SERVICE.

Part: TEST PANEL — CONTAMINATED (COCKPIT) · airframe 47,708 hrs · 20,132 cycles

AFT PEDESTAL FIRE/OVERHEAT FAIL LIGHT ILLUMINATED INTRMITNLY. SMELLED SMOKE VISUALLY VERIFIED FIRE INSIDE THE AFT PEDESTAL. SHUT DOWN PWR TO AC. AIRCRAFT MX AND ARFF. FOUND BURNS ON FAIL/RESET SWITCH PANEL, LOOKS TO HAVE LIQUID SPILL RESIDUALS ON IT. PERFORMED GVI OF WIRING AND CONNECTORS TO THE FIRE/OVERHEAT PANEL AND PEDISTAL AREA. NO DISCREPANCIES NOTED IAW MM 20-60-04-2. INSTALLED NEW PANEL IAW AMM 26-11-02-4. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: BOTTLE — FAILED (L1 DOOR) · airframe 47,673 hrs · 20,110 cycles

L1 DOOR ASSIST BOTTLE HAS BEEN DEPLETED REMOVED REPLACED L-1 DOOR EMERGENCY POWER RESERVOIR PER BOEING AMM 52-11-30-4. A/C OK FOR SERVICE AT THIS TIME.

Part: PROBE — FAILED (PITOT/STATIC SYS) · airframe 47,498 hrs · 19,997 cycles

RT AUX PITOT EICAS AND LIGHT 15 MINS INTO FLIGHT. ON DECENT WENT INTO ICING CONDITIONS AFTER CONSULTATION WITH MOCC THAT THIS WOULD BE ACCEPTABLE. GOT EICAS IAS DISAGREE, RUDDER RATIO, MACH TRIM EICAS WHEN IN IMC. RECORD EVENT PRESSED SEEMED TO COME BACK WHEN ICING CONDITIONS IMPROVED RT SYSTEM WENT UNRELIABLE. FAILED PROBE PART MANF, SERIAL 3 IDENTIFIED IN WRI, PROBES INSTALLED REF AMM 34-11-01-5, PROBES LEAK CHECK PASSED REF AMM 34-11-01-5, PANELS INSTALLED ON WRI 53-00-6778, WIRE BUNDLES DISTURBED SECURED REF SWPM AND EA F-3030-T0352122 ACCOMPLISHED.

Part: SKIN — CHAFED (TE FLAP) · airframe 47,426 hrs · 19,949 cycles

REWORK REQUIRED OF EA F-5750-T0351491 PT1 STEP 3. REPAIR ACCOMPLISHED IAW SRM 57-53-01-2R REPAIR 2 AND EA F-5750-T0351491 A P1 WING - FLIGHT SURFACES. RT INBOARD MAIN FLAP LEADING EDGE SKIN REPAIR.

Part: DOUBLER — WORN (TE FLAP) · airframe 47,426 hrs · 19,949 cycles

RIGHT WING INBOARD FLAP HAS WORN MARKED IN MULTIPLES AREAS OF LEADING EDGE SURFACE. REMOVED DAMAGE ON RT WING I/B FLAP L/E O/B SIDE AND FOUND DAMAGE AT SKIN PLATE DOUBLER OF EXISTING REPAIR AND OUT OF LIMITS IAW SRM 57-53-01-1A FIG 101 DET VI. FORMED, LOCATED, DRILLED AND INSTALLED NEW SKIN PLATE DOUBLER IAW SRM 57-53 -01-2R REPAIR 3. GENERATED EA F-5450-T0351491 P1.

Part: SKIN — CHAFED (TE FLAP) · airframe 47,426 hrs · 19,949 cycles

CHAFED MARK SHOWING AT RIGHT WING OUTBOARD FLAP LEADING EDGE. COMPLIED WITH EA F-5750-T0351338 P1 TITLE: WING - FLIGHT SURFACE - RT OUTBOARD MAIN FLAP LEADING EDGE SKIN REPAIR. BLENDED AREA FOUND OUT OF LIMITS L/E AREA IAW SRM 57-53-01-1A FIG 101 DET VI. FABRICATE, LOCATED, DRILLED AND INSTALLED SKIN IAW SRM 57-53-01-2R REPAIR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,426 hrs · 19,949 cycles

MAIN DECK BETWEEN STA 1180 - 1200 BL0 SEAT TRACK FLANGE CORRODED. COMPLIED WITH EA F-5310-T0351165 P1. TITLE FUSELAGE - MAINFRAME - BL 0 SEAT TRACK SPLICE REPAIR BETWEEN STA 1220 AND STA 1240.

Part: SKIN — WORN (TE FLAP) · airframe 47,426 hrs · 19,949 cycles

RIGHT WING LEADING EDGE WORN MARKED AT INBOARD SIDE, OUTBD FLAP INBD L/E. BLENDED AREA AT RIGHT WING LEADING EDGE OF O/B FLAP IB SIDE, INBD L/E FOUND AREA OUT OF LIMITS IAW SRM 57-53-01-1A FIG 101 NOTE S. FABRICATED, LOCATED AND DRILLED DOUBLER RT WING L/E OUTBD FLAP IAW SRM 57-53-01-2R REPAIR 5. GENERATED EA F-5750-T0351338 P1.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,426 hrs · 19,949 cycles

MAIN DECK BETWEEN STA 1640 - 1681 RBL 50 WEB CORRODED ON TOP AND UNDER NUT PLATE. REMOVED CORROSION IN AREA AT MAIN DECK BETWEEN STA 1640 - 1681 RBL 50 WEB, ORIGINAL THICKNESS MAT OF WEB .071", MAT REM .054", MAT LOSS .017" FOUND OUT OF LIMTS IAW SRM 53-60-15-1A FIG 101 DET VI, FABRICATED NEW WEB IAW DWG 146N8722 REV N, INSTALLED NEW WEB IAW DWG 146N8722 REV N AND SRM 51-40-02-0G.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 47,426 hrs · 19,949 cycles

CRACK FLOORBEAM T CAP STA 580 LBL 45.5. COMPLIED WITH EA F-5310-T0351069 P1. TITLE : FUSELAGE - MAINFRAME - STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,141 hrs · 19,726 cycles

EMERGENCY EXIT LIGHTS ABOVE R1 DOOR AND COCKPIT DOOR INOP. REMOVED AND REPLACED NR 1 RADIANT POWER CORP BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,468 hrs · 19,291 cycles

L1 DOOR EXTERIOR EMER EXIT LIGHT IS INOP. RELAMPED L1 EMER EXIT SLIDE LIGHT REF AMM 33-51-06-2-1, OP'S NORMAL. HISTORY SHOWS POWER SUPPLY R&R AND LOOSE GROUND WIRE RESECURED, RELAMPED AT THIS TIME OP'S AS ADVERTISED WHEN OPERATED BY EMER LIGHT TEST SWITCH ABOVE L1 DOOR OR COCKPIT EMER LIGHT SWITCH ON THE P-5 PANEL. OK FOR SERVICE.

Part: GROUND WIRE — LOOSE (EXTERIOR LIGHT) · airframe 46,356 hrs · 19,200 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT IS INOP. REMOVED LIGHT ASSY FROM A/C FOUND GROUND WIRE LOOSE TIGHTEN WIRE PER GMP AND OPS CHECKED SYSTEM. ALL LITES OK.

Part: COMPUTER — MALFUNCTIONED (TCAS) · airframe 46,092 hrs · 19,003 cycles

TCAS WAS NOT SHOWING MULTIPLE KNOWN OTHER TRAFFIC AND ON FINAL COURSE TRAFFIC DIRECTLY IN FRONT OF AIRCRAFT WAS DISPLAYED 20 TO 30 DEGREES RIGHT OF NOSE. REMOVED AND REPLACED THE TCAS COMPUTER IAW AMM 34-45-01-4-99, AND TESTED IAW AMM 34-45-00-5-99. ACFT OK FOR SERVICE.

Part: SKIN — MECHANIC ERROR (FUSELAGE) · airframe 45,750 hrs · 18,792 cycles

REPAIR DOUBLER AT STA. 1380-1400 S23L-26L DOES NOT COMPLY WITH THE SRM. ALL WORK WAS ACCOMPLISHED IAW FEDEX EA F-5330-T0336912 P1 FUSELAGE - PLATES & SKINS - FUSELAGE SKIN REPAIR BETWEEN STA 1380 AND 1400 BETWEEN STRINGERS S-23L AND S-26L

Part: SKIN — MECHANIC ERROR (FUSELAGE) · airframe 45,750 hrs · 18,792 cycles

REPAIR DOUBLER AT STA. 1380-1400 S20L-22L DOES NOT COMPLY WITH THE SRM. ALL WORK WAS ACCOMPLISHED IAW FEDEX EA F-5330-T0336913 P1 FUSELAGE- PLATES & SKINS - FUSELAGE SKIN REPAIR BETWEEN STA 1380 AND STA 1400 BETWEEN STRINGERS S-20L AND S-22L

Part: SKIN — MECHANIC ERROR (FUSELAGE) · airframe 45,750 hrs · 18,792 cycles

REPAIR DOUBLER AT STA. 1560-1580 S17R TO 20R DOES NOT COMPLY WITH THE SRM. ALL WORK ACCOMPLISHED IAW FEDEX EA F-5330-T0336798 P1 FUSELAGE PLATES & SKINS - FUSELAGE SKIN REPAIR BETWEEN STA. 1560 AND 1580 BETWEEN STRINGERS S-17R AND S20R

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,750 hrs · 18,792 cycles

FORWARD WET AREA CORROSION UPPER CHORD, UPPER SURFACE OF STA 365 FLOORBEAM, APPROX RBL 50. REMOVED PREVIOUS REPAIR ON FLOOR BEAM @ STA 365 DUE TO NO ALLOWABLE DAMAGE. REPAIRED UPPER T-CHORD STA 365 IAW B757 SRM 53-00-51-2R REPAIR 3

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 45,750 hrs · 18,792 cycles

FORWARD WET AREA CORROSION LBL8 SEAT TACK FORWARD FLANGE, UPPER SURFACE AT NUT PLATE RIVETS APPROX STA 370. REMOVED CORR LBL8 APPROX STA. 370 SEAT TRACK IAW B757 SRM 51-10-02. 100% MATERIAL LOSS OUT OF LIMITS IAW B757 SRM 53-00-52. REMOVED SEAT TRACK IAW B757 SRM 51-40-02. FABRICATED NEW SEAT TRACK IAW B757 SRM 51-40-05 AND INSTALLED NEW SEAT TRACK IAW B757 SRM 51-40-02

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,750 hrs · 18,792 cycles

FORWARD WET AREA CORROSION STA 345 FLOORBEAM UPPER CHORD UPPER SURFACE, APPROX BBL 0- LBL 25. REMOVED CORR. ON FLOOR BEAM UPPER CHORD IAW B757 SRM 51-10-02 @ STA 345 100% MAT LOSS. REPAIRED UPPER T-CHORD IAW B757 SRM 53-00-51-2R REP 3

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,687 hrs · 18,743 cycles

L1 DOOR EMERGENCY SIGN AND L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-07-2, ALL INTERIOR AND EXTERIOR EMERGENCY LIGHTS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,169 hrs · 18,371 cycles

RT EXTERIOR SLIDE LIGHT IS INOP. RELEASED FOR SERVICE PER MEL 33-51-02-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 442 hrs · 17,761 cycles

MAIN CABIN AFT 9G SHEAR WEB AT STATION 422.5, RBL 15.5, AREA CORROSION. COMPLIED WITH EA F-5310-T0321795 PT1 FUSELAGE-MAINFRAME-MAIN CABIN SHEAR PANEL CORROSION REPAIR AT STA 422 BETWEEN BL0 AND RBL 24.

Part: DOOR SILL — DIRTY (FUSELAGE) · airframe 441 hrs · 17,627 cycles

L1 CABIN DOOR HANDLE EXTREMELY HARD TO ROTATE & LOCKED CLOSED. CLEANED DEBRIS FROM L1 DOOR SILL & GIRT BAR FLOOR FITTINGS. L1 DOOR OPERATIONS CHECKED NORMAL. OK FOR SERVICE. REFERENCE MM 52-11-00-0.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 440 hrs · 17,573 cycles

ONE EXT EMER LIGHT INOPERATIVE. RELAMPED IAW SMP, OPERATIONS NORMAL IAW AMM 33-51-00-5.

Part: CAM — WORN (L1 DOOR) · airframe 43,092 hrs · 16,883 cycles

L1 DOOR IS JAMMED. R & R L1 DOOR CONTROL CAM & FWD CRANK BEARING, OPERATIONS CHECKED GOOD IAW AMM 52-11-13-2 & IPC 52-11-13-01C.

Part: SKIN — PUNCTURED (BS 1622) · airframe 42,811 hrs · 16,666 cycles

ACFT SKIN PUNCTURED BS 1622 BETWEEN S25-26R. REMOVED DAMAGE IAW SRM 51-10-02. FABRICATED REPAIR DOUBLER, STRINGER FILLER AND FILLER IAW SRM 51-40-05, 51-40-08, EA F-5330-T0304035 PT 1. INSTALLED REPAIR DOUBLER, STRINGER FILLER, FILLER IAW EA F-5330- T0304035 PT 1 AND SRM 51-40-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,338 hrs · 16,248 cycles

L1 SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW MM 33-51-06-2-1.

Part: COVER — DISLODGED (PAX DOOR HINGE) · airframe 42,253 hrs · 16,199 cycles

WHILE OPENING L1 CREW ENTRY DOOR UPPER DOOR HINGE COVER FELL OFF. REPLACED L1 DOOR UPPER HINGE PLATE IN REF TO SRM 51-40-02.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 42,187 hrs · 16,160 cycles

F/O'S WINDSCREEN SHATTERED ON CLIMBOUT AFTER DE-ICING. RETURNED TO DEPARTURE IAW QRH. R & R IAW AMM 56-11-01-4. F/O'S WINDOW CHECKED SERVICEABLE.

Part: CAM — OUT OF RIG (L1 DOOR) · airframe 41,888 hrs · 15,978 cycles

DURING B CHECK, L1 DOOR UPPER FWD CAM PLATE NEEDS TO BE RIGGED. ACCOMPLISHED RIGGING OF L1 DOOR UPPER FWD CAM PLATE IAW AMM. NO FAULTS NOTED.

Part: ROLLER — OUT OF ADJUST (L1 DOOR) · airframe 41,888 hrs · 15,978 cycles

DURING B-CHECK, FOUND L1 DOOR UPPER FWD CRANK ARM ROLLER CONTACTS THE CAM PLATE WHEN CLOSING THE DOOR. ACCOMPLISHED RIGGING OF L1 DOOR UPPER FWD CRANK ROLLER CAM PLATE AND ROLLER IAW AMM NO FAULTS NOTED.

Part: CIRCUIT BREAKER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 41,873 hrs · 15,966 cycles

RT SIDE EMERGENCY EXIT LIGHT STAYS ILLUMINATED WITH DOOR ARMED AND DISARMED. RESET CIRCUIT BREAKERS AND PERFORMED OPS CHECK IAW MM 33-51-00-5. OPS CHECKED GOOD.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 41,866 hrs · 15,962 cycles

F/O SLIDING WINDOW DOES NOT STAY CLOSED WITH LOCK IN LOCKED CLOSED. WINDOW WILL CRANK OPEN WITH WINDOW IN LOCKED CLOSED. PERFORMED ADJUSTMENT TEST OF F/O'S SLIDING WINDOW IAW MM 56-11-02-5. FINAL CLOSED.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 41,866 hrs · 15,962 cycles

CAPTAIN`S SLIDING WINDOW DOES NOT STAY CLOSED WITH LATCH LOCKED CLOSED. WINDOW WILL CRANK OPEN WITH WINDOW LOCKED CLOSED. PERFORMED ADJUSTMENT TEST IAW MM 56-11-02-5. CAPTAINS SLIDING WINDOW, OPS CHECK NORMAL. RII ACCOMPLISHED.

Part: GUARD — OUT OF ADJUST (EMERGENCY LIGHTS) · airframe 41,596 hrs · 15,765 cycles

THE EMERGENCY LIGHTS GUARD CANNOT BE CLOSED WITH THE SWITCH IN ARM, WITHOUT THROWING THE SWITCH TO OFF. RESET SAFETY GUARD ON EMERGENCY LIGHT SWITCH. SYS OPS CHECKED GOOD IAW AMM 33-51-00-5-0.

Part: SKIN — MISREPAIRED (BS 530 S26-27R) · airframe 41,441 hrs · 15,658 cycles

SKIN AT BS 530, S26-27R MISREPAIRED. REPAIRED IAW EAF-5330-152662.

Part: FRAME — CORRODED (BS 1645) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

FRAME AT STA 1645 LOWER END HAS CORROSION AT W.L.210, INBD FLANGE RBL 55. REMOVED CORROSION IAW-SRM-51-10-02, ORIGINAL MATERIAL .063 AFTER REWORK .055, REMOVED .008 FOUND TO BE OUT OF LIMITS IAW SRM-53-00-07, PG 103, FIG 101, DETAIL II. REPAIR WAS ACCOMPLISHED ON AREA ON MAE NR 46865590001 AND MAE EA 757-5362-16-F3487, REV. THIS N/R IS FOR TRACKING PURPOSES ONLY. "MAJOR REPAIR"

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

MAIN CARGO DOOR FRAME AT BS 1645 HAS CORROSION ON LOWER END WL 210 INBD FLANGE, LT SIDE, LBL 55. REMOVED CORROSION IAW SRM-51-10-02, CHECKED LIMITS: ORIGINAL MATERIAL .063, AFTER RE-WORK .046, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-07, PG 108 FIG 101, DETAIL II. REPAIR IAW EA 757-5362-16-F3487 REV. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1220) · airframe 41,441 hrs · 15,658 cycles

AFT CARGO, BS 1220 FRAME S24R-S26R, MISREPAIRED. REMOVED FRAME IAW SRM 51-40-02. REPLACED FRAME IAW SRM 51-40-02, AND DWG 146N1027. MAJOR REPAIR.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 41,441 hrs · 15,658 cycles

SKIN MISREPAIRED AT BS 1630, S24-26L. REPAIRED IAW EA F-5330-152661.

Part: STRINGER — NONE (BS 1573) · airframe 41,441 hrs · 15,658 cycles

EXISTING STRINGER REPAIR AT STA 1573, STR 27R, REQUIRES SUPPLEMENTAL INSP. PERFORM THE SUPPLEMENTAL INSP ON THE STRINGER REPAIR AREA IAW THE SRM 53-00-03, FIG 201, REPAIR 1, TABLE IV, ZONE 1 REQUIREMENTS IAW FORM 8100-9, DATED OCT 17, 2011. REF: N00121 FOR SKIN REPAIR COMMON TO EXISTING STRINGER REPAIR,CATEGORY A REPAIR, MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 1604-1620) · airframe 41,441 hrs · 15,658 cycles

SKIN DAMAGED AT BS 1604-1620, STR 18-21R. REPAIRED IAW EA 757-5361-F3555.

Part: GATE — CORRODED (ZONE 200) · airframe 41,441 hrs · 15,658 cycles

PASSENGER R1 DOOR LOWER GATE BOTTOM EDGES HAS GOUGED AND CORROSION. R & R LOWER GATE IAW AMM 52-11-38-4. REMOVED CORROSION ON GATE IAW SRM 51-10-02 CHECKED LIMITS IAW SRM 52-10-02 ORIG MAT 170 MAT REMAINING AFTER BLEND .040. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 DETAIL XII, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1540-1580) · airframe 41,441 hrs · 15,658 cycles

SKIN AT BS 1540-1580, S2-3L MISREPAIRED. REPAIRED IAW EA F-5330-147745.

Part: GATE — CORRODED (R4 DOOR) · airframe 41,441 hrs · 15,658 cycles

R-4 DOOR LOWER GATE HAS CORROSION AROUND THE SEAL RETAINER BRACKET. REMOVED CORROSION FROM R-4 DOOR LOWER GATE FOUND TO BE OUT OF LIMITS I.A.W. SRM 52-10-02 FIG 101. REMOVED AND REPLACED LOWER GATE ASSY IAW MM 52-11-38. PERFORMED R-4 DOOR ADJUSTMENT IAW MM 52-11-00-5, CHECKED GOOD. MAJOR REPAIR.

Part: STRAP — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

LT HORIZONTAL STAB PIVOT FITTING UPPER STRAP HAS CORROSION. ACCOMPLISHED EA F-5510-152652. CORROSION WAS DETERMINED TO BE OUT OF LIMITS PER SRM 55-10-01, PAGE 104, FIG.101, DETAIL 3.

Part: SEAT TRACK — CORRODED (BS 1280) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

SEAT TRACK CORRODED AT BS 1280, RBL 24. REMOVED CORROSION WITH .013" MATERIAL LOSS, WITH .072" REMAINING, ORIGINAL WAS .085". FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. FABRICATED NEW SEAT TRACK FROM BAC 1520-792, BATCH 1964663. LOCATED AND DRILLED AND INSTALLED NEW SEAT TRACK IAW SRM 51-10-02 /51-40-02 AND DWG 144N5021. MAJOR REPAIR.

Part: GATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

L-1 DOOR LOWER GATE HAS PITTED CORROSION AROUND THE SEAL RETAINER BRACKET. REMOVED AND REPLACED LOWER GATE ASSY, PER AMM 52-11-38. PERFORMED DOOR ADJUSTMENT CHECKED PER AMM 52-11-00-5 CHECKED GOOD, MAJOR REPAIR.

Part: SKIN — CRACKED (ZONE 500) · airframe 41,441 hrs · 15,658 cycles

LT WING L/E GAP PANEL,114N1801-951, ABOVE PYLON HAS APROX 1' CRACK IN SKIN. REMOVED SKIN FROM LT WING GAP PANEL IAW SRM 51-40-02, FABRICATED NEW SKIN ON TR T11/896272, LOCATED & DRILLED IAW SRM 51-40-05, INSTALLED NEW SKIN, 5 EA FITTINGS AND PANEL IAW SRM 51-40-02 AND DWG 114N1803, MAJOR REPAIR.

Part: FIREWALL — CHAFED (NR 2 NACELLE) · airframe 41,441 hrs · 15,658 cycles

NR 2 PYLON INBD SIDE FWD FIREWALL AFT SIDE CHAFED. REPAIRED IAW EA F-5450-147735. MAJOR REPAIR.

Part: GUSSET — CHAFED (NR 2 NACELLE) · airframe 41,441 hrs · 15,658 cycles

NR2 PYLON OTBD AFT LOWER CORNER CHAFED. COMPLIED WITH EA F-5450-147737. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1480 S26-28L) · airframe 41,441 hrs · 15,658 cycles

SKIN AT STA 1480 S26L- S28L MISREPAIRED. REPAIRED IAW SRM 51-40-02 & 53-00-01, TABLE I & II, FIG 201 P203 REPAIR 16. CATEGORY B MAJOR REPAIR.

Part: GATE — CORRODED (R2 DOOR) · airframe 41,441 hrs · 15,658 cycles

R2 DOOR LOWER GATE CORRODED. R & R R2 DOOR LWR GATE ASSY, IAW AMM 52-11-38 AND ADJUSTED R2 DOOR IAW AMM 52-11-00-5 CHECKED GOOD. REMOVAL OF CORROSION WAS FOUND TO BE OUT LIMITS IAW SRM 52-10-02, FIG 101, DETAIL 5. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1701-1720) · airframe 41,441 hrs · 15,658 cycles

SKIN MISREPAIRED AT STA 1701-1720 S16L-17L. REPAIRED IAW EA 757-5361-16-F3556.

Part: STRINGER SPLICE — CRACKED (BS 1620) · airframe 41,441 hrs · 15,658 cycles

AFT CARGO STA 1620 AT S-25R SPLICE IS DENTED. R & R 5 EA FASTENERS F.O.M IAW SRM 51-40-02. FOUND SPLICE TO BE CRACKED AND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, SH 1, P.101. RECEIVED SPLICE ON MAE TRAVELER T11/894584, PN FX-146N3820-56. REMOVED CRACKED SPLICE, AND INSTALLED FABBED SPLICE IAW SRM 51-40-02, AND DWG 146N3820, AT BS 1620, S25R. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 41,441 hrs · 15,658 cycles

SEAT TRACK AT STA 418, STA 440, LBL 45 IS GOUGED. BLENDED GOUGE ORIGINAL: .200", AFTER: .140", LOSS: .060"; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1. FABRICATED SEAT TRACK, BAC1520-792, BATCH NR 1904663, IAW SRM 53-10-52, FIG 1, DETAIL 3. INSTALLED SEAT TRACK LBL 45, BS 418-440, IAW SRM 51-40-02. MATERIAL ID FROM SRM 53-10-52, FIG 1, DETAIL 3 AND DWG 141N5131. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 41,441 hrs · 15,658 cycles

SEAT TRACK AT STA 418-STA 440 RBL 24 GOUGED. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52, FIG.101, DETAIL 1. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02. TREATED AND PRIMED PER SRM 51-20-01. PAINTED PER SRM 51-20-01. INSTALLED NEW SEAT TRACK, PER SRM 51-40-02, AND DRAWING 141N5131. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 41,441 hrs · 15,658 cycles

SEAT TRACKAT STA 418, STA 440, RBL 48 IS GOUGE. BLENDED GOUGE ORIGINAL MAT .200, AFTER REPAIR .130 MATERIAL, REMOVED .070, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I, FIG 101. R & R SEAT TRACK MATERIAL BAC1520-792, BATCH 1904663 IAW SRM 51-40-02, MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 41,441 hrs · 15,658 cycles

SEAT TRACK AT BS 418 - 440, LBL 24, IS GOUGED. BLENDED GOUGE AREA; ORIGINAL: .200", AFTER: .150", FOUND TO BE OUT OF LIMTS IAW SRM 53-00-52, FIG 101, DETAIL 1, REWORK AREA 2"X.9". R & R SEAT TRACK IAW SRM 51-40-02, REPLACEMENT SEAT TRACK, BATCH NR 0001904663, AND DWG 141N5131. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 41,441 hrs · 15,658 cycles

SKIN AT BS 1681 S-17L -S-18L MISREPAIRED. R & R REPAIR IAW SRM 51-40-02, FABRICATED NEW REPAIR IAW SRM 53-00-01, TABLE I & III FIG 101, PG 203. MAJOR REPAIR.

Part: DOOR FRAME — GOUGED (BS 337.5 S8L) · airframe 41,441 hrs · 15,658 cycles

PASENGER DOOR 1 L FWD DOOR FRAME AT BS 337.5, ADJACENT TO S8L GOUGED. BLENDED GOUGE IAW 51-10-02 CHECKED LIMITS, ORIGINAL MAT .063" AFTER REWORKED .038" FOUND TO OUT LIMITS IAW SRM 53-10-15, FIG 101 DETAIL IV. REMOVED FRAME IAW SRM 51-40-02, FABRICATED, LOCATED AND DRILLED. TREATED TOP COAT AND INSTALLED, IAW SRM 51-40-02 AND DWG141N8315, MAJOR REPAIR.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 41,441 hrs · 15,658 cycles

AFT PRESSURE DECK UPON REMOVAL OF DECK FOUND CUSP WEB CORRODED LBL-55, STA 1701-STA 1720.

Part: TEE FITTING — CORRODED (BS 1720) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

MCD AFT PRESSURE DECK UPON REMOVAL FOUND TEE ANGLE CORRODED BS 1720 LBL-50 REMOVED TEE ANGLE FOR ACCESS TO CORROSION, PER SRM 51-40-02. REMOVED CORROSION PER SRM 51-10-02. FOUND OUT OF LIMITS PER SRM 53-80-05, DETAIL 9, P.109. LOCATED AND DRILLED NEW TEE PER SRM 51-40-05. INSTALLED TEE ANGLE PER SRM 51-40-02 AND DRAWING 146N8722. MAJOR REPAIR.

Part: FITTING — CORRODED · airframe 41,441 hrs · 15,658 cycles

AFT PRESSURE DECK UPON REMOVAL, FOUND FITTING CORRODED.

Part: WEDGE — DAMAGED (RT WING TE FLAP) · airframe 41,441 hrs · 15,658 cycles

RT WING INBD FLAP, TRAILING FLAP WEDGE HAS DAMAGE AT T/E 21 INCHES FROM OTBD EDGE. REPAIRED IAW SRM 51-70-10 REPAIR 4. MAJOR REPAIR.

Part: FRAME — DAMAGED (CARGO DOOR) · airframe 41,441 hrs · 15,658 cycles

FWD CARGO DOOR FWD LOWER CORNER ANGLE FRAME DAMAGE. REPLACED LOWER CORNER ANGLE FRAME IAW SRM 51-40-02, CHECKED LIMITS MAT FOUND TO BE PUNCTURED THROUGH THE LOWER CORNER FRAME & EXCEED THE ALLOWABLE DAMAGE IAW SRM 52-30- 02, FIG 101 NOTE L=1.0" W=0.5" RECEIVED LOWER CORNER FRAME PN 654N0244-602, BATCH NR 0002094353, MAJOR REPAIR.

Part: SKIN — CORRODED (BS 1661) · airframe 41,441 hrs · 15,658 cycles

LWR FUSELAGE HAS CORROSION ON SKIN RUNNING UNDER RAIN DIVERTER FOR POTABLE WATER SERVICE AT BS 1661.

Part: CREASE BEAM — GOUGED (ZONE 200) · airframe 41,441 hrs · 15,658 cycles

CREASEBEAM AT BS 1290-1370 HAS NUMEROUSE GOUGES AND SCRATCHES. FUTHER INVESTIGATION FOUND A PUNCTURE HOLE WAS FOUND, IAW SRM 53-60-15, FIG 101, DETAIL IV. NOTE C, PUNTURE HOLES ARE NOT PERMITED ADJACENT TO FASTENER HOLES LESS THAN 1" AWAY, R & R DAMAGED CREASE BEAM WITH A NEW 1 PN 146N8326U1, BATCH PN 0002101970 IAW SRM 51-40-02 AND 51-10-02, MAJOR REPAIR.

Part: GATE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

L-2 DOOR LOWER GATE HAS PITTED CORROSION AT SEAL RETAINER BRACKET. REMOVED CORROSION, CHECKED LIMITS ORIG .200 REMOVED .035 REMAINING .165 FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101. REMOVED LOWER GATE ASSY IAW AMM 52-11-38. RECEIVED NEW GATE ASSY PN 143N6106-45, BATCH 0002079607. INSTALLED NEW LOWER GATE ASSY IAW SRM 51-40-02 & DWG 143N6106, MAJOR REPAIR.

Part: SEAT TRACK — MISALIGNED (BS 440) · airframe 41,441 hrs · 15,658 cycles

SEAT TRACK, RBL 45, STA 440. DOES NOT JIG (MISALIGNED). SPLICED A NEW SEAT TRACK SECTION BETWEEN BS 440-490, RBL 45, IAW SRM 53-00-52, FIG 201. MAJOR REPAIR.

Part: GATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

L-4 DOOR LOWER GATE CORRODED AT SEAL RETAINER BRACKET. REMOVED CORROSION AT LOWER SEAL AREA . CHECKED LIMITS ON WORKED AREA FOUND OUT OF LIMITS IAW SRM 52-10-02, FIG 101. ORIG MAT .200 MAT LOSS .040 REM. 160. REMOVED L-4 LOWER GATE IAW 51-40-02. RECEIVED NEW LOWER GATE B/N 0002079610. INSTALLED L-4 LOWER GATE IAW AMM 52-11-38-4. MAJOR REPAIR.

Part: SKIN — DENTED (PAX DOOR) · airframe 41,441 hrs · 15,658 cycles

DOOR OUTER SKIN HAS AN OUTER DENT AT S13R,4" FROM L/E. EVALUATED DENT ON R-1 DOOR OUTER SKIN AT S13R, 4" FROM THE L/E;W=.008", D=.007, A/Y=114. DENT IS W/I LIMITS IAW SRM 52-10-01, FIG.101, DETAIL7. HFEC IAW NTM 51-00-19,PT.6, NO CRACKS NOTED. APPLIED DENT DOT IAW GMM 6-3-101.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

FLOORBEAM AT LBL 45 CORRODED AT STA 377. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 201, REPAIR NR 3 AT STA 377 FROM RBL 24 TO LBL 70. MAJOR REPAIR.

Part: PRESSURE DECK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

PRESSURE DECK WEB HAS CORROSION AT STA 1681.8-1720, RBL 50. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS MAT THICKNESS .071", BLENDED MAT, .053" FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DET III, REMOVED PRESSURE WEB IAW SRM 51-40-02. FABRICATED PRESSURE WEB IAW SRM 53-60-51 LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED PRESSURE WEB IAW DWG 1146N5300, MAJOR REPAIR.

Part: SEAT TRACK — MISALIGNED (BS 440-470) · airframe 41,441 hrs · 15,658 cycles

SEAT TRACK, STA 440-470, LBL 24, DOES NOT JIG. CUT OUT SECTION OF SEAT TRACK & REPLACED PER SRM 53-00-52, FIG 201, SHEET 1 OF 5, REPAIR 1. MAJOR REPAIR.

Part: SKIN — GOUGED (APU DOOR) · airframe 41,441 hrs · 15,658 cycles

APU DOOR 316AR EXTERNAL SKIN LATCH HOLES, -2- PLACES GOUGED WITH KNIFE EDGE.

Part: FLOORBEAM — MISREPAIRED (BS 1300) · airframe 41,441 hrs · 15,658 cycles

FLOORBEAM STA 1300 HAS IN COMING REPAIR THAT DOES NOT COMPLY WITH SRM, EA OR ANY DOCUMENT. REMOVED REPAIR, FABRICATED REPAIR ANGLES, STRAP, AND FILLER. LOCATED AND DRILLED NEW PARTS, TREATED ALODINED, PRIMED AND INSTALLED REPAIR PARTS AT FLOORBEAM UPPER CHORD PER SRM 53-00-51, FIG. 201, REPAIR 5. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 41,441 hrs · 15,658 cycles

SKIN, BS 1560-1585, S26-29R MISREPAIRED. FABRICATED DOUBLER IAW EA F-5330-147736 AND INSTALLED NEW DOUBLER IAW SRM 51-40-02 AND EA 5330-147736.

Part: BEAM — GOUGED (ZONE 100) · airframe 41,441 hrs · 15,658 cycles

NR 1 CARGO DOOR LOWER EDGE BEAM HAS SEVERAL DENTS AND GOUGES. REPLACED EDGE BEAM IAW SRM 51-40-02, CHECKED LIMITS ON EDGE BEAM ORIGINAL MATERIAL .050 MAT LOSS .025 REMAINING .025 FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02 FIG 101 DETAIL III PAGE 105.

Part: FRAME — CORRODED (BS 1645) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

FRAME AT STA 1645 (FWD OF L-4 DOOR) HAS CORROSION ON LOWER END WL 210 INBD FLANGE LT SIDE LBL 55.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 41,441 hrs · 15,658 cycles

SEAT TRACK GOUGE AT STA 1210 TO 1220, LBL 45 AROUND THE CROWN AREA. REMOVED ANGLE AND SEAT TRACK IAW SRM 51-40-02, FABED NEW PART IAW SRM 53-00-52, FIG 201 SHEET 1, BATCH 1904663, PN BAC 1520-792, LOCATED AND DRILLED IAW SRM 51-40-05, TREATED AND PRIMED AND PAINTED IAW 51-20-01, INSTALLED SEAT TRACK AND ANGLE IAW SRM 51-40-02 AND DWG 144N5024, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 343-346) · airframe 41,441 hrs · 15,658 cycles

FUSELAGE SKIN REPAIR AT BS 343-346, S-21R-S-23R IS NOT IN COMPLINCE WITH SRM. REMOVED EXISTING REPAIR AT BS 343-346 S-21R - S-23R IAW SRM 51-40-02 , HFEC INSP IAW NTM 51-00019 PT6 & 51-00-16 PT6, FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 53-00-01 REPAIR 15, THIS IS A CATEGORY (B) REPAIR, MAJOR REPAIR.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

DURING A CHECK, INSTALLED DOUBLER REPAIR AT STA.1500, STR 22L,FOUND S-22L CORRODED AROUND FASTENER HOLES AT STA 1510. CUT OUT DAMAGED STRINGER 22L BTW BS 1510 TO BS 1530 IAW SRM 53-00-03 REPAIR 2 PG 201, RECEIVED FABRICATED STRINGER, FABRICATED SPLICE HAT IAW SRM 53-00-03-1, INSTALLED THE REPAIR PARTS AND ACCOMPLISHED REPAIR SRM 51-40--2. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1394-1420) · airframe 41,441 hrs · 15,658 cycles

SKIN REPAIR AT 1394-1420 S-20L-S-22L IST NOT IN COMPLIANCE WITH SRM. REMOVED & REPLACED DOUBLER AS PER SRM 51-40-02 / 53-00-01. FABRICATED DOUBLER AS PER SRM 53-00-01 TABLE I & III FIG 201 P. 203 . CATEGORY B MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 41,441 hrs · 15,658 cycles

REPAIR AT STA 17800-1720, S-23L-S-25L DOES NOT MEET SRM REQUIREMENTS. REMOVED &REPLACED DOUBLER STA. 1700-1720 S-23L-25L AS PER SRM 51-40-02/ 53-00-01, REPAIR 16, FABRICATED DOUBLER AS PER SRM 53-00-01 FIG 201 TABLE I & III PG 203. CATEGORY B REPAIR 16, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1560-1580) · airframe 41,441 hrs · 15,658 cycles

SKIN AT 1560-1580, S-18R-S19R DOES NOT MEET SRM REPAIR STANDARDS. CORRECTED REPAIR IAW SRM 53-00-01. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 365 S21-22L) · airframe 41,441 hrs · 15,658 cycles

FUSELAGE SKIN REPAIR AT BS 365, S21-22L, IS NOT IN COMPLIANCE WITH SRM. REMOVED EXISTING SKIN REPAIR DOUBLER AT STA 365 S-21L-22L IAW SRM 51-40-02. FABRICATE NEW REPAIR DOUBLER AND REINSTALLED WITH FILLER AND CONICAL WASHER IAW SRM 53-00-01 AND 51-40-02. HFEC PERFORMED IAW NTM 51-00-19 PT6, CAT B REPAIR 16, MAJOR REPAIR.

Part: FRAME — CORRODED (BS 1645) · corrosion level 2 · airframe 41,441 hrs · 15,658 cycles

FRAME AT BS 1645, LOWER END HAS CORROSION AT WL 210 INBD FLANGE RBL 55.

Part: SEAT TRACK — MISALIGNED (ZONE 200) · airframe 41,441 hrs · 15,658 cycles

SEAT TRACK, LBL 45, BS 440 MISALIGNED. REMOVED SEAT TRACK IAW SRM 51-40-02, FABRICATED NEW SEAT TRACK IAW DWG 143N5110, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-05 AND DWG 143N5110 INSTALLED SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5110 AND PART MARKED IAW GMM 7-0-1001-1. MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 41,441 hrs · 15,658 cycles

SKIN DENTED AT BS 1540, S-23-24R. REMOVED DAMAGE & FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, DETAIL 3, FIG. 101 & SRM 51-40-02. HFEC , NO CRACK INDICATION NOTED. FABRICATED DOUBLER PER SRM 53-00-01, TABLE 1 / 3, FIG. 201, REPAIR 16. INSTALLED DOUBLER PER SRM 51-40-02 AND SRM 53-00-01. MAJOR REPAIR.

Part: SEAT TRACK — MISINSTALLED (BS 440) · airframe 41,441 hrs · 15,658 cycles

SEAT TRACK STA 440, RBL 24, DOES NOT JIG. CUT OUT SECTION OF SEAT TRACK AT BS 440-470 IAW SRM 53-00-52, REPAIR 1. FABRICATED NEW SEAT TRACK AND REPLACED IAW SRM 53-00-52, FIG 201 REPAIR 1. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 41,441 hrs · 15,658 cycles

SKIN AT BS 1380-1400, S-23L-S-25L MISREPAIRED. REMOVED AND REPLACED DOUBLER PER SRM 51-40-02 AND SRM 53-00-01, REPAIR 16. FABRICATED DOUBLER PER SRM 53-00-01, TABLE 1 AND 2, FIG. 201, P. 203. MAJOR REPAIR

Part: SKIN — MISREPAIRED (BS 1500-1570) · airframe 41,441 hrs · 15,658 cycles

REPAIR AT STA 1500-1570, S-21L-S-22L DOES NOT MEET SKIN REPAIR 757SF SRM REQUIREMENTS. REMOVED AND REPLACED DOUBLER, BS 1511-1522, S22L - S23L, AS PER SRM 51-40-02, 53-00-01, REPAIR 16. FABRICATED DOUBLER, AS PER SRM 53-00-01, TABLE 1, FIG. 201, P.203, REPAIR 16. MAJOR REPAIR

Part: DOOR FRAME — GOUGED (BS 690) · airframe 41,441 hrs · 15,658 cycles

L2 DOOR CUTOUT FWD FRAME AT STA 690 HAS 2 GOUGES BETWEEN S15R AND S17R. OUT OF LIMITS STRAP & FRAME, REMOVED STRAP & FRAME REMOVED ANGLES & DOOR LOCK, DOOR STOP FITTING IAW SRM 51-40-02, LOCATED DRILLED NEW FRAME & STRAP & ANGLE, DOOR LOCK, DOOR STOP FITTING, INSTALLED FRAME, STRAP, ANGLE DOOR LOCK, DOOR STOP FITTING IAW SRM 51-40-05 & SRM 51-40-02. MAJOR REPAIR.

Part: DOOR FRAME — GOUGED (CARGO DOOR) · airframe 41,441 hrs · 15,658 cycles

AFT CARGO DOOR MID LOWER FRAME SECTION HAS SEVERAL GOUGES. EVALUATED GOUGE AFT CARGO DOOR MID LOWER FRAME, FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02, FIG 101, DETAIL IV. R & R IAW SRM 51-40-02 AND DWG NR 146N6621, MAJOR REPAIR.