N994FD

Part: NONE — NONE (N/A) · airframe 47,593 hrs · 16,833 cycles

MAIN CARGO FLOOR SEAT TRACK LOBE DAMAGED AT STA 579 AT BL45L. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STA.440-STA. 690 LBL 45.5 IN REF TO 757 SRM 51-40-02- 0G. SEE JPF FOR OTHER ACTIONS

Part: GIRT BAR — DISENGAGED (R1 DOOR) · airframe 47,161 hrs · 16,481 cycles

WHEN OPENING R1 DOOR NOTED GIRT BAR HANGING DOWN FROM BOTTOM OF DOOR. COMPLIED WITH B757 AMM 25-66-10-2 PAGES 14-15 STEPS 14-21. RENEGAGED THE GIRT BAR CAMS IN THE GIRT BAR SLIDERS OF THE R1 DOOR. OPERATED THE GIRT BAR MECHANISM BY ARMING AND DISARMING THE DOOR SLIDE SEVERAL CYCLES, NO DEFECTS NOTED, REMOVED SAFTIES AS REQUIRED AND RESECURED THE R1 DOOR SLIDE COVER. AC OK FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 46,847 hrs · 16,257 cycles

GEAR DISAGREE WHEN LANDING GEAR LEVER SELECTED DOWN BEFORE LANDING. NOSE GEAR INDICATED UNSAFE. RAN QRH FOR GEAR DISAGREE AND EXTENDED GEAR VIA ALTERNATE EXTENSION. EMERGENCY DECLARED. REMOVED AND REPLACED NOSE LANDING GEAR LOCKING ACTUATOR, REF B757 AMM 32-34-02-4. LEAK CHECK GOOD. OPERATIONS CHECK GOOD, REF B757 AMM 32-34-00-5. PERFORMED MULTIPLE GEAR SWINGS WITH ALL SYSTEMS, REF B757 32-32-00-5 FOR MLG AND NLG 32-34-00-5. ALL OPERATIONS CHECK GOOD.

Part: GATE — CORRODED (L1 DOOR) · airframe 46,835 hrs · 16,251 cycles

L1 DOOR LOWER GATE LOWER EDGE PITTED ACCOMPLISHED EA NR F-5210-T0358769. DOORS-PASSENGER/CREW-NR 1 PASS, DOOR LOWER GATE, EDGE PITTING.

Part: SHELF — CRACKED (E/E BAY) · airframe 46,835 hrs · 16,251 cycles

E&E COMPARTMENT E3-2 SHELF LT OUTBOARD MOUNT BRACKET CRACKED, REPAIRED PER SRZ-53-007.

Part: MOUNT — CRACKED (E/E BAY) · airframe 46,835 hrs · 16,251 cycles

E&E COMPARTMENT E3-1 SHELF LT OUTBOARD MOUNT BRACKET CRACKED, REPAIRED PER SRZ-53-007.

Part: FLANGE — CRACKED (E/E BAY) · airframe 46,835 hrs · 16,251 cycles

E&E COMPARTMENT E3-2 SHELF LT OUTBOARD MOUNT FLANGE CRACKED. REMOVED AND REPLACED FLANGE, IAW B SRM 51-40-02 AND DWG NR 284N1028 REV C.

Part: SKIN — CRACKED (NLG WW) · airframe 46,835 hrs · 16,251 cycles

NOSE WHEEL WELL RT DOOR CUT OUT UPPER SKIN STRIP IS CRACKED AT BS 324 RBL 19. REMOVED AND REPLACED STRIP, PER DWG 141N0094.

Part: ACTUATOR — FAILED (NLG) · airframe 46,714 hrs · 16,182 cycles

PDIS 994 32-30 8627 10NOV20 IND OPEN U. GEAR DISAGREE AND GEAR DOORS EICAS FOR 90 SECONDS UNTIL GEAR FULLY RETRACTED AND EICAS MESSAGES. NOISE FROM NOSE GEAR AREA UNTIL DOORS MESSAGES WENT AWAY. REPEAT WRITE UP. SHGN 10NOV20 06:12 IND U. CREW REPORTED THAT NOSE LANGING GEAR APPEARED TO TAKE LONGER THAN NORMAL TO RETRACT AND STOW. PERFORMED BITE OF PSEU. INFLIGHT FAULT CODES 243, 238, 065, 081, 078, 077. REMOVED AND REPLACED THE NLG RETRACT CYLINDER, IAW 32-34-01-4 UP TO RETRACTION AND EXTENSION TEST AND LEAK CHECK, REF WRI 32-30/8630.

Part: CLAMP — WORN (BLEED AIR SYS) · airframe 46,444 hrs · 15,993 cycles

LEFT BLEED DUCT LEAK AT FL 370 WITH ENGINE ANTI-ICE ON. COMPLETED QRH AND SECURED ENGINE ANTI-ICE AND LIGHT WENT OUT WITH NO SECONDARIES. REMOVED STAND OFF CLAMPS FOR ACCESS AND POSITIONING OF LEADING EDGE DUCTING. REMOVED AND REPLACED 5 WORN LEADING EDGE CLAMPS PER MM CHP 36-11-01-4. RE-INSTALLED STAND OFF CLAMPS AS WELL. PERFORMED FIRST LEAK CK WITH APU AIR PER JRH NO LEAKS NOTED. PERFORMED ENGINE RUN PER JRH AND RECHECKED TORQUE ON ALL REPLACED CLAMPS. NO LEAKS NOTED. CLOSED GEAR DOORS PER 32-10-00 AND A/C DOORS PER 52-48-03. LEADING EDGE PANELS NEED RE-INSTALL AND P-50 DOOR OPEN FOR FINAL CK OF CARD FOR FAULTS.

Part: CLAMP — WORN (BLEED AIR SYS) · airframe 46,444 hrs · 15,993 cycles

LEFT BLEED DUCT LEAK AT FL 370 WITH ENGINE ANTI-ICE ON. COMPLETED QRH AND SECURED ENGINE ANTI-ICE AND LIGHT WENT OUT WITH NO SECONDARIES. ACCOMPLISHED WING AND BODY DUCT LEAK DETECTION BITE PROCEDURE AND FOUND HARD FAULT CODE 14 (LEFT WING LEADING EDGE ALARM, LOOPS A&B). REMOVED LEFT WING LEADING EDGE ACCESS PANELS AND FOUND LEADING EDGE DUCT LEAKING SEVEARLY AT EACH CLAMP AND BLOWING DIRECTLY ONTO DETECTOR ELEMENTS. REMOVED CLAMPS AND INSPECTED FLANGES FOR DAMAGE. NO DAMAGE FOUND AROUND DUCT FLANGES. ORDERED ALL NEW CLAMPS FOR LEADING EDGE DUCTING. A/C BAY DOORS ARE OPENED FOR MX ALSO MAIN AND NOSE LANDING GEAR DOORS ARE OPENED FOR MX. REMOVED STAND OFF CLAMPS FOR ACSESS AND POSITIONING OF LEADING EDGE DUCTING. REMOVED AND REPLACED 5 WORN LEADING EDGE CLAMPS PER MM. RE-INSTALLED STAND OFF CLAMPS AS WELL. PERFORMED FIRST LEAK CK WITH APU AIR PER JRH NO LEAKS NOTED. PERFORMED ENGINE RUN PER JRH AND RECHECKED TOURQE ON ALL REPLACED CLAMPS. NO LEAKS NOTED. CLOSED GEAR DOORS AND A/C DOORS. CLOSED THE P50 PANEL CLOSED PANELS 511KT, 511JB, AND 511BB.

Part: PROXIMITY SENSOR — INOPERATIVE (EVAC SLIDE) · airframe 46,069 hrs · 15,741 cycles

RIGHT DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN ARMED. VERIFIED 28VAC AT SLIDE LIGHT L404. VERIFIED GOOD CONTINUITY THROUGH AFT GIRT BAR PROX SENSOR S10217 WITH THE SWITCH ACTUATED. VERIFIED GOOD GROUND AT GD2922-AC. NO CONTINUITY FOUND THROUGH FWD PROX SENSOR S10216. REFERENCE WDM 25-66-11. REMOVED AND REPLACED SENSOR S10216 IAW AMM 25-66-11-2. SLIDE LIGHT NOW ILLUMINATES WITH THE DOOR MODE SELECTOR LEVER IN THE ARMED POSITION. MEL IS CLEARED, PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 46,021 hrs · 15,715 cycles

PDIS 994 25-60 7876 26NOV19 BUF OPEN U LOGPAGES:3167525 R1 DOOR SLIDE LIGHT NOT ILLUMINATED WHILE ARMED. MEL 26NOV19 00:00 BUF U RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : C EXPIRATION : 06DEC19 "MEL 25-66-05-A: ______R1__ (IDENTIFY L1 AND/OR R1) ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - INOP. VERIFY AND RECORD IN AML/EAML THAT ASSOCIATED SLIDE IS VISUALLY VERIFIED ENGAGED PRIOR TO EACH DEPARTURE." C/7208745 UPDT 26NOV19 06:29 MEM U RELAMPED R1 DOOR SLIDE ARM LIGHT REF AMM 33-13-00-2. NO HELP, FURTHER T/S REQUIRED. RELAMPED R1 DOOR SLIDE ARM LIGHT REF AMM 33-13-00-2. NO HELP, FURTHER T/S REQUIRED.

Part: SEAT TRACK — CORRODED (BS 1540) · corrosion level 2 · airframe 45,361 hrs · 15,220 cycles

MAIN CABIN SEAT TRACK STA 1540 RBL 45.7 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIG MAT .075 REM .050 LOSS .025 FOUND OUT OF LIMITS IAW SRM 53-00-52-1A. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R REPAIR 3 DIM 51.

Part: CREASE BEAM — CORRODED (BS 800) · corrosion level 2 · airframe 45,361 hrs · 15,220 cycles

MAIN CABIN LBL 62 CREASE BEAM AT STA 800 HAS CORROSION. REMOVED CORROSION ON CREASE BEAM STA 800 LBL 62 IAW B757 SRM 51-10-02. ORIG MAT .071 REM .051 LOSS .020 OUT OF LIMITS IAW B757 SRM 53-30-13-1A FIG 101 DET. VIII. REPAIRED CREASE BEAM IAW B757 SRM 53-00-13-2R REPAIR 1. DIM OF CUT OUT OF CREASE BEAM 53.300".

Part: SEAT TRACK — CORRODED (BS 618) · corrosion level 2 · airframe 45,361 hrs · 15,220 cycles

MAIN CABIN SEAT TRACK LBL 24.75 AT STA 618 HAS CORROSION. REMOVED CORROSON ON SEAT TRACK STA 618 LBL 24.75 IAW B757 SRM 51-10-02. ORIG MAT .070 REM .035 LOSS .035 FOUND OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101 DET VII. REPAIRED SEAT TRACK IAW B757 SRM 53-00-52-2R REP 3 OPT 2

Part: SEAT TRACK — CORRODED (BS 1020-1040) · corrosion level 2 · airframe 45,361 hrs · 15,220 cycles

CORROSION IN THE MAIN CABIN SEAT TRACK, RT FLANGE UPPER SURFACE, BETWEEN BS 1020 TO BS 1040 LBL 58. REMOVED CORR ON SEAT TRACK STA 1020 TO 1040 LBL58 IAW SRM 51-10-02 ORIG MAT .90 REM .050 LOSS .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-40-52-1A. REMOVED, TRIMMED, LOCATED ,DRILLED AND INSTALLED IAW SRM 51-40-02 AND 51-40- 05 AND BOEING DWG 657N3321 REV - DIM 23"3" SEAT TRACK

Part: FLOORBEAM — CORRODED (BS 1020) · corrosion level 2 · airframe 45,361 hrs · 15,220 cycles

MAIN CABIN FLOOR SUPPORT BTWN LBL 24.75 / BL 0 AT BS 1020 CORROSION. REMOVED CORR ON FLOOR SUPPORT BETWEEN LBL 24.75 / BL0 STA. 1020 IAW B757 SRM 51-10 10-02. FOUND OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DET VII. DIM 23". ACCOMPLISHED FEDEX EA F-5310-T-0344072 P1, FUSELAGE - MAINFRAME - MAIN CARGO FLOOR SUPPORT STA 1020 CORRODED, NEW PART FABRICATION - TEMPER ALTERATION. REMOVED, FABRICATED & INSTALLED FLOOR SUPPORT IAW B757 SRM 51-40-02 AND EA F-5310- T0344072 T0344072 P1 T0344072 T0344072 P1

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 45,361 hrs · 15,220 cycles

STUB BEAM IN FORWARD CARGO AT STA 580 AND LBL 45. COMPLIED WITH MAINFRAME STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR AT LBL 45.

Part: CONTROLLER — MALFUNCTIONED (RT A/C PACK TEMP) · airframe 45,094 hrs · 15,044 cycles

AT FL 340, NOTICED EARS POPPING. LOOKED AT THE CABIN ALTITUDE INDICATOR & IT INDICATED NORMAL, THE RATE GAUGE FLUCTUATED. AFTER A FEW MINUTES, THE RIGHT PACK INDICATED INOPERATIVE. DESCENDED TO 9000 FT. REMOVED AND REPLACED THE RIGHT PACK TEMP CONTROLLER, AND THE RIGHT FLOW CONTROL CARD AS A PRECAUTION IAW AMM 21-51-14-4, AND 21-51-09-4, OPS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 45,008 hrs · 14,953 cycles

RT EMERGENCY EXIT SIGN DID NOT TEST, LAMPS OUT/MISSING. REMOVED AND REPLACED BATTERY PACK/ CHARGER TRAY FOR RT EMERGENCY EXIT SIGN, REF AMM 33-51-07-2. OPS CHECKS GOOD, A/C OK FOR SERVICE.

Part: LOCK — OUT OF ADJUST (L1 GIRT BAR) · airframe 44,715 hrs · 14,733 cycles

LEFT FORWARD ENTRY DOOR WAS DISARMED THEN OPENED. PARTS FELL OFF DOOR AND SLIDE PARTIALLY HANGING OUT. INSTALLED THE AFT BAR LOCK ONTO GIRT BAR IAW MM 25-66-01-4, PARA 3H (19). INSTALLED SLIDE COVER. WHEN ARMING DOOR, AFT BAR LOCK FOUND TO BE TOO FAR INBOARD TO FULLY ENGAGE EASILY. REMOVED AND REPLACED FWD GIRT BAR CRANK AND ADJUSTED IAW AMM 52-11-25-5. ACFT OK FOR SERVICE.

Part: GIRT BAR — DISLODGED (DOOR) · airframe 44,384 hrs · 14,517 cycles

RT DOOR SLIDE LIGHT IS INOP. DURING T/S FOUND THAT THE GIRT BAR WAS DISLODGED FROM DOOR. REINSTALLED GIRT BAR ON DOOR REF AMM 25-66-10-2-0. OPS CHECKS GOOD. SLIDE LIGHT OPS CHECKS GOOD. ACFT OK FOR SERVICE.

Part: SENSOR — DIRTY (DOOR) · airframe 44,354 hrs · 14,489 cycles

SLIDE ARMED INDICATOR LIGHT ON R FWD ENT DOOR DOES NOT ILLUMINATE. INSPECTED GIRT BAR DETECTION PER AMM 25_66_11_2_0. SOME DEBRIS NOTED, CLEANED SENSOR AREA. OPS CHECKED NORMAL SEVERAL TIMES. OK FOR SERVICE

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 44,290 hrs · 14,432 cycles

FOUND THE L1 DOOR ASSIST BOTTLE PRESSURE LOW R & R THE L1 DOOR ASSIST BOTTLE IAW AMM 52-11-30-4.

Part: PDU — TRIPPED (TE FLAPS) · airframe 44,184 hrs · 14,359 cycles

TE FLAP DISAGREE MESSAGE AFTER SELECTING FLAPS 20 ON VISUAL APPROACH. QRH COMPLETED AND LANDED FLAPS 20. TROUBLESHOT TE FLAP DISAGREE IAW FIM 27-51 FT 808. FOUND LEFT INBOARD PDU OVERLOAD INDICATOR TRIPPED. BITE CHECKED ALL 3 FSEU'S AND NO FAULTS WERE FOUND. FOLLOWED PROCEDURE IAW FIM 27-51 FT 808 BLOCK 21, 23, AND 59. TE FLAP OPERATION IS NORMAL AT THIS TIME. ACFT OK FOR SERVICE.

Part: FRAME — DENTED (BS 1340) · airframe 43,863 hrs · 14,108 cycles

AFT CARGO FRAME AT BS 1340 HAS A DENT BETWEEN STRINGERS 25L AND 26L. REPAIRED IAW EA F-5310-T0329984 P1. MAJOR REPAIR.

Part: FRAME — DENTED (BS 1420) · airframe 43,863 hrs · 14,108 cycles

AFT CARGO BAY FRAME AT BS 1420 HAS A DENT ABOVE STRINGER 26L. COMPLIED WITH EA F-5310-T0329906 P1.

Part: WEB — CORRODED (BS 4121) · corrosion level 2 · airframe 43,863 hrs · 14,108 cycles

MAIN CARGO WEB AT BS 4121 RBL 67, FOUND CORRODED, UPPER RT CORNER. REMOVED AND REPLACED THE WEB IAW DRAWING 146N5590 REV E.

Part: GIRT BAR — DAMAGED (L1 DOOR) · airframe 43,767 hrs · 14,041 cycles

L1 DOOR SLIDE ARMED LIGHT WILL NOT ILLUMINATE. THE GIRT BAR WILL NOT FULLY ENGAGE. R & R THE GIRT BAR IAW MM 25-66-10-2. PERFORMED ADJUSTMENT AND TEST IAW MM 25-66-11-2 . OPS CHECKED GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 41,052 hrs · 12,035 cycles

EMERGENCY EXIT LIGHT CONTROL PANEL "UNARMED" ANNUNCIATOR INOPERATIVE. R & R OVERHEAD EMERGENCY EXIT LIGHTS CONTROL PANEL IAW AMM 33-51-08, OPS CHECKED NORMAL.

Part: ANGLE — CRACKED (ZONE 400) · airframe 40,883 hrs · 11,907 cycles

ANGLE CRACKED NR 2 PYLON INBD SIDE NAC STA 102.1. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02 AND DWG 311N3510, REV C.

Part: SUPPORT ANGLE — CRACKED (ZONE 400) · airframe 40,883 hrs · 11,907 cycles

ANGLE CRACKED NR 1 PYLON INBD SIDE NAC STA 102.1. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02 AND DWG 311N3510, REV C.

Part: LINER — OUT OF POSITION (L1 DOOR) · airframe 40,662 hrs · 11,761 cycles

WHEN ARMING L1 DOOR, EXCESSIVE FORCE HAD TO BE APPLIED TO GET SLIDE ARM INDICATOR TO DISPLAY. FOUND ESCAPE SLIDE ARMING TAB RUBBING ON LOWER LINING OF L1 DOOR. REF MM 52-11-02-4, ADJUSTED LOWER LINING. ALL DOOR COMPONENTS RE-INSTALLED. SLIDE ARMING TAB OPS CK NORMAL. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 40,413 hrs · 11,571 cycles

R1 DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. R & R R1 EXTERIOR SLIDE LIGHT IAW AMM 33-51-06-2-1. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 39,934 hrs · 11,286 cycles

R1 DOOR SLIDE ARMING LEVER IS BINDING BEFORE IT GOES FULL TRAVEL TO ARM. ORIGINAL GSP-LINE. ADJUSTED GIRT BAR FLOOR FITTINGS PER MM 52-11-25-5-0. OPS CHECKED GOOD

Part: PANEL — LOOSE (L1 DOOR) · airframe 39,925 hrs · 11,279 cycles

PANEL BEHIND ARMED/DISARMED SLIDE ON LT DOOR IS LOOSE. REMOVED THE L-1 DOOR INTERIOR COVER. INSTALLED THE NEW PLATE RETAINER RAIL IAW AMM 52-11-02 & SRM 51-70-06.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 39,785 hrs · 11,203 cycles

EMERGENCY EXIT LIGHTS WILL NOT TEST. EMERGENCY EXIT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION.

Part: ENGINE — ERRATIC · airframe 39,675 hrs · 11,140 cycles

AT CRUISE FL 400, THE RT ENGINE BECAME ERRATIC WITH EPR FLUCTUATIONS BETWEEN 1.10 TO 1.29 WITH ASSOCIATED VARIATIONS IN N1 AND FUEL FLOW. TURNED AUTO THROTTLES OFF AND THE PROBLEM CONTINUED. REDUCING POWER DID NOT HELP. R & R RT(NR 2) ENGINE EEC IAW AMM 73-21-04-4-0. PERFORMED EEC STATIC TEST IAW AMM 71-00-00-5. TEST PASSED, NO CODES DISPLAYED ON EPCS PAGE. RAN BOTH ENGINES IAW JRH. ALL INDICATIONS STABLE AND NORMAL. RECHECKED FOR CODES ON EPCS AFTER ENGINE RUNS. NO CODES PRESENT. ACFT OK FOR SERVICE. INSTALL BORROWED PART AND REMOVE OPERATOR PART.

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 39,592 hrs · 11,084 cycles

ON DESCENT INTO MEM GOT RT ENG OIL PRESS ALERT WITH OIL PRESS ABOVE 70 PSI (RED) SHUTDOWN RT ENGINE IAW QRH. RECIEVED STATUS MESSAGES, RT ENG SEC SEL RT ENG LOW N1 R ENG OIL PRESS R ENG SPEED CARD RT ENG SEC CONT RT ENG FUEL ON SOL. INSTALLED RT ENGINE EEC IAW AMM 73-21-04-4. CHECKED GOOD. OPERATED ENGINE IAW JRH FPR 5 MINUTES. NO FAULTS FOUND.

Part: SUPPORT — CHAFED (LT WING LE) · airframe 39,368 hrs · 10,921 cycles

LT WING- L/E WING APPROX W/S 240 - L/E DUCT SUPPORT CHAFING INTO VERTICAL SUPPORT. REMOVED & INSTALLED NEW STIFFNER IAW SRM 51-40-02. RECIEVED NEW STIFFNER ON TR T10/861406. P/N 112N2038-79. NO NOTED DAMAGE TO BRACKET. MAJOR REPAIR.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 39,368 hrs · 10,921 cycles

LT WING OTBD MAIN FLAP L/E INBD SIDE HAS A WORN SECTION APPROX 10" LONG . EVALUATED LT WING OTBD MAIN FLAP AND FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01, PG 106, DETAIL VI. R & R L/E SKIN IAW SRM 51-40-02. CLASSIFIED CATEGORY "A". MAJOR REPAIR.

Part: SKIN — DENTED (ZONE 100) · airframe 39,368 hrs · 10,921 cycles

EXTERNAL FUSELAGE SKIN STA 1720-1740 BETWEEN S-25R TO S-16R HAS DENT AT LAP SEAM. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO LAP SEAM. REPAIRED DENT IAW EA F-5330-143218. CLASSIFIED CATEGORY "A" MAJOR REPAIR.

Part: SKIN — DAMAGED (LT WING AILERON) · airframe 39,368 hrs · 10,921 cycles

LT WING AILERON OTBD AREA LWR SURFACE PUNCTURED THRU SKIN DIAMETER OF HOLE 0.250 BY 1"X1" REPAIRED LT WING AILERON OTBD AREA IAW SRM 51-70-17 SB 757-51-0006 IAW SRM 57-60- 01. FINAL DIAMENTION OF REPAIR 5"X4" AND LOCATED AT THE IM EDGE OF STATIC FRAME REF EA F-5750-142298. CLASSIFIED CAT "A" MAJOR REPAIR.

Part: SKIN — DAMAGED (NR 2 SLAT) · airframe 39,368 hrs · 10,921 cycles

LT WING NR 2 SLAT HAS NUMEROUS CHAFED MARKS ALONG BOTTOM SKIN AFT EDGE REPAIRED LT WING NR 2 SLAT IAW SRM 51-70-10 IAW SRM 57-43-02 DAMAGE LOCATED AT STA 652.50 APPROX 1" FWD OF T/E SLAT REPAIR DIAM. 1"X1.5". REF EA F-5750-142276. CLASSIFIED CAT "A" MAJOR REPAIR.

Part: WEDGE — CHAFED (NR 6 SLAT) · airframe 39,368 hrs · 10,921 cycles

NR 6 SLAT T/E WEDGE UNDER SKIN HAS CHAFE MARKS, REPAIRED NR6 SLAT T/E IAW SRM 51-70-10 IAW SRM 57-43-02. DAMAGE WAS LOCATED AT STA 177.5, APPROX 3" FWD OF T/E. REF EA F-5750-143211. CLASSIFIED CAT "A" MAJOR REPAIR.

Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

L1 LOWER GATE PANEL HAS SEVERE CORROSION ALONG LOWER EDGE AND ON GATE SKIN PANEL AT LOWER EDGE. REMOVED AND REPLACED L1 DOOR LOWER GATE ASSY, PER AMM 52-11-38. ADJUSTMENT AND TEST GOOD PER AMM 51-11-00-5. (CORROSION WAS OUT OF LIMITS PER SRM 51-10-01, FIG.101, DETAIL 9; EEDGES HAS OVER .040" LOSS). MAJOR REPAIR

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

AT RBL 24, BL 1600- 1640 HAS HEAVY PITTING IN INBD RADIUS OF SEAT TRACK CROWN TO FLANGE. CHECKED LIMITS FOUND TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DET VII. PAGE 104. REMOVED SEAT TRACK IAW SRM 51-40-09. TRIMED NEW SEAT TRACK PER SAMPLE IAW SRM 53-00-52. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-40-05, TREATED AND PRIMED SEAT TRACK IAW SRM 51-20-06, PAINTED SEAT TRACK IAW AMM 51-20-00. INSTALLED SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: SKIN — DENTED (BS 309 S18L) · airframe 39,368 hrs · 10,921 cycles

PREVIOUS SKIN DENTED AT BS 309, S18L. ACCOMPLISHED SKIN REPAIR IAW EA F-5330-141203, BS 309, BELOW S17L. DENT WAS OUT OF LIMITS DUE TO PROXIMITY TO BS 310.5 FRAME. 2EA. SHEAR TIES WERE FABRICATED ON TRAVELERS T10/855076 AND T10/855075. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (BS 1460 S26-27L) · airframe 39,368 hrs · 10,921 cycles

STA 1460 FRAME SHEAR-TIE BETWEEN STRINGER 26L AND 27L CORRODED. REPLACED SHEAR TIE, FABRICATED ON TRAVELER T10/850999, IAW SRM 51-40-02/ DWG 140N2002. SHEAR TIE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, DETAIL 2, FIG 101. CORROSION REWORK; L=1.74",W=.510",D=.020". SHEAR TIE REPLACED AT BS 1460, S26L/S27L. MAJOR REPAIR

Part: GATE — CORRODED (L2 DOOR) · airframe 39,368 hrs · 10,921 cycles

L2 DOOR LOWER GATE EDGE HAS CORROSION L2 DOOR LOWER GATE OUT OF LIMITS MAX DEPTH MEASURED 0.15 IAW SRM 52-10-02, FIG 101, DETAIL IV SHEET 4 OF 8 PAGE 104. REPLACED GATE IAW SRM 51-10-02. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

FLOORBEAM STA 377, BL 0, RBL 10, UPPER TEE CORRODED. REMOVED CORROSION PER SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3. REMOVED DAMAGED AREA OF THE FLOORBEAM PER SRM 53-00- 51. FABRICATED NEW TEE AND REPAIR ANGLES PER SRM 53-00-51, FIG.201, REPAIR 3. LOCATED/DRILLED PER SRM 51-40-05. INSTALLED ALL REPAIR PARTS PER SRM 51-40-02, AND SRM 53-00-51, FIG.201, REPAIR 3, MAJOR REPAIR.

Part: SKIN — DENTED (BS 668 S19R) · airframe 39,368 hrs · 10,921 cycles

PREVIOUS SKIN DENT AT BS 668, S19R. EVALUATED DENT L=1.3 W = 1.0 D= .033 FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO SKIN SPLICE. CUT OUT DAMAGE & FABRICATED DOUBLER AND STRUCTURAL FILLER FROM .063 2024-T3 BATCH 1862687 AND SHIM .032 2024 - T3, BATCH 1827514 IAW EA F--5330-142246. INSTALLED REPAIR AT BS 668, JUST BELOW S19R, PER SRM 51-40-02, EA F-5330-142246, AND FAA FORM 8110-3 DATED 10/13/10. DTA IS REQUIRED NO LATER THAN 12 MONTHS FROM DATE OF 8110-3. THIS IS A MAJOR REPAIR

Part: GATE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

R 1 DOOR LOWER GATE HAS CORROSION ALONG EDGE R1 DOOR GATE FOUND OUT OF LIMITS PER SRM 52-10-02, FIG.201, DETAIL 4, SH. 4 OF 8; MEASURED .200" LOSS. REMOVED AND REPLACED R1 DOOR LOWER GATE ASSY PER SRM 51-10-02 / 51-40-02. MAJOR REPAIR CAT. "A".

Part: SKIN — MISREPAIRED (RT APU DOOR) · airframe 39,368 hrs · 10,921 cycles

RT APU DOOR EXISTING FLUSH REPAIR AT BS 1957, STR 29R DOES NOT COMPLY WITH KNOWN APPROVED DATA. REMOVED EXISTING REPAIR IAW SRM 51-40-02. REPAIRED APU DOOR SKIN, RT, IAW SRM 52-40-01, FIG 201, P205, REPAIR NR 5. CAT "A" MAJOR REPAIR, NO REPETITIVE INSP REQUIRED.

Part: FITTING — MISALIGNED (ZONE 200) · airframe 39,368 hrs · 10,921 cycles

AT STA 1640 LT THE 657N3161-11 FITTING HAS 2EA EXISTING SED FASTENERS AT LWR, INBD, END OF FITTING ALSO 5EA, EXISTING FASTENERS WHERE DWG SHOWS 4EA, AT LWR END OF FITTING APPROX WL 202 TO WL 208 AND JUST INBD OF THAT LOCATION 5EA EXISTING FASTENERS AT INBD, EDGE OF 11 FITTING THAT CAN NOT BE INSTALLED IAW DWG AT STA 1640 LT, WL 202 TO WL 208. FRAME REPAIR WAS ACCOMPLISHED EFFECTING THE PTF CONVERSION, ON MAE MOD W/C NR118350399EZ2R02, AND MAE EA 757-5362-16-F2843 AUG19, 2010. THIS NON- ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION.

Part: FITTING — CORRODED (TORQUE TUBE) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

R1 DOOR FWD LOWER TORQUE TUBE ROLLER FITTING HAS PITTING CORROSION. R & R FWD LOWER TORQUE TUBE CAM ROLLER FITTING IAW CMM 52-11-05. MAJOR REPAIR.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 39,368 hrs · 10,921 cycles

LT WING- INBD MAIN FLAP L/E, OTBD SIDE HAS 3 WORN SECTIONS WITH TOTAL LENGTH APPROX 20 INCHES. COMPLIED WITH EA F-5750-141199, CLEANED AREAS IAW SRM 51-10-02, OUT OF LIMITS, IAW SRM 57-53-01, FIG 101, SHEET 6. DAMAGE REPAIRED IAW SRM 57-53-01, LOCATED & DRILLED AND INSTALLED DOUBLER .090", 2024-T3. TRAV T/10849301, & FILLER .080" 2024-T4 TRAV T/10849302, IAW SRM 51-40-02 & 51-40-05. TREATED AND PRIMED ALL PARTS IAW SRM 51-20-01. REPAIR IS CLASS B, REPAIR, USING REPAIR 3 IAW - SRM -57-53-01.

Part: FLOORBEAM — MISLOCATED (BS 440) · airframe 39,368 hrs · 10,921 cycles

EXISTING FASTENER HOLE AT STA 440, BL-0, AFTSIDE OF FLOORBEAM WILL BE IN THE RADIUS ON LT SIDE OF L-0 SEAT TRACK CROWN IF DRILLED. AT STA 440, BL-0 EXISTING HOLE PLUGED AND RELOCATED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE MOD W/C NR 118350425BZ2R10 AND MAE EA 757- 5335-16-F2802, DATED 07-27-2010. THIS NON-ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION.

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

R2 DOOR LOWER GATE HAS CORROSION ALONG EDGE CHECKED LIMITS ON CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-02, FIG.101, DETAIL 4. MEASURED .150" MATL. LOSS. REMOVED AND REPLACED R2 DOOR GATE, LOWER, P/N 143N6106-26, BATCH 0001899033,PER SRM 51-10-02 / 51-40-02. DOOR GATE RIG WAS NOT DISTURBED.MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

AFT CARGO FLOOR SUPPORT RBL 7.55 BETWEEN STA 1500 TO STA 1640 NUMEROUS BROKEN SCREWS, NUT PLATES AND ATTACHING RIVETS. REMOVED CORROSION ON FLOOR SUPPORT RBL 7.55, STA. 1500 - 1640 OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL V. ORIG MATERIAL .063" MAT LOST .015". REMOVED CORROSION AND CHECKED LIMITS ON WEB, OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL V, ORIG MAT .032", MAT LOST .016". FABRICATED NEW FLOOR SUPPORT IAW SRM 51-40-02. MAJOR REPAIR.

Part: GATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

L-4 DOOR LOWER GATE CORRODED ALONG EDGE AND FWD POCKET INNER SURFACE. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG. 101 DETAIL IV. REMOVED LOWER GATE FROM L-4 DOOR IAW SRM 51-40-02. REMOVED SEAL FROM GATE ASSEMBLY IAW AMM 52-09-01. RECEIVED NEW GATE ASSEMBLY. LOCATED AND DRILLED IAW SRM 51-40-05, AND SRM 51-40-08. INSTALLED SEAL ON NEW GATE ASSEMBLY IAW AMM 52-09-01. INSTALLED NEW GATE ASSEMBLY ON L-4 DOOR IAW 51-40-02. CLASSIFIED AS A MAJOR REPAIR.

Part: GATE — CORRODED (L2 DOOR) · airframe 39,368 hrs · 10,921 cycles

L-2 DOOR UPPER GATE, AFT POCKETS INNER SURFACE CORRODED. REMOVED CORROSION ON L-2 DOOR UPPER GATE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02. REMOVED SEAL FOR ACCESS IAW AMM 52-09-01. REMOVED HINGE FOR ACCESS IAW SRM 51-40-02. RECEIVED NEW GATE ASSEMBLY. LOCATED AND DRILLED IAW SRM 51-40-05. REINSTALLED HINGE IAW SRM 51-40-02, INSTALLED SEAL IAW AMM 52-09-01, AND INSTALLED NEW UPPER GATE ASSEMBLY IAW SRM 51-40-02. CLASSIFIED AS A MAJOR REPAIR.

Part: GATE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

R4 DOOR, LOWER GATE EDGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02; ORIGINAL MATERIAL: .150", LOSS: .102", REMAINING: .048", FOUND OUT OF LIMITS IAW SRM 52-10-02, DETAIL 7, P 107, FIG 101. REMOVED DOOR GATE ON R4 DOOR IAW SRM 51-40-02. INSTALLED NEW DOOR GATE ON R4 DOOR IAW SRM 51-40-02/ 51-40-05. MAJOR REPAIR.

Part: FRAME — GOUGED (BS 1280 S10-13R) · airframe 39,368 hrs · 10,921 cycles

MAIN CABIN, FRAME BS 1280 S10-13R HAVE GOUGES. REMOVED DAMAGE AT STRG 11R- 13R IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II, REMOVED DAMAGE FRAME FROM STRG 11-13R, STOP 4(B) HFEC REWORK AREA IAW NTM 51--00-19 PH 6. NO CRACK NOTED, RECEIVED PART. REPAIR FRAME SEGMENT, TO/848286, AND REPAIR CHANNELS TO/848287, LOCATED AND DRILLED IAW SRM 51-40-05, INSTALLED REPAIR FRAME SEGMENT AND REPAIR CHANNELS IAW SRM 51-40-02. CAT."B" REPAIR, REPAIR 1, PAR 5. ZONE 3. DVI 12,000 F/C OR 50, 000 AIRFRAME CYCLES WHICH EVER COMES FIRST. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365.25) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

STA 365.25 FLOORBEAM HAS CORROSION ON TOP OF BEAM AND UNDERNEATH TOP OF BEAM AT SEVERAL LOCATIONS RT OF BL 0. REMOVED CORROSION IAW SRM 51-10-02. OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. REMOVED DAMAGED FROM LBL 13-RBL 68.6. FABRICATED REPAIR PARTS; TEE CHORD, BAC 1505-100880, BATCH3 1787163. FABRICATED SPLICES (ANGLES) ON TRAVELER T10/848225 AND STRAPS ON TRAVELER T10/848228. MATERIAL LOSS ON BEAM; ORIG.=.125",AFTER=.093",LOSS=.032". INSTALLED ALL REPAIR PARTS IAW SRM 53-00-51, REPAIR NR3, DETAIL 1, FIG 101, AT BS 365.25, LBL 13 -RBL 68.6. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1605) · airframe 39,368 hrs · 10,921 cycles

AT STA 1605 STR 26L- PROTRUDING DENT, OTWD. FOUND DENT TO BE OUT OF LIMITS PER SRM 53-00-01, FIG.101,DETAIL 3,DUE TO BEING LESS THAN 3" FROM A SKIN SPLICE. ACCOMPLISHED A FUSELAGE SKIN DOUBLER REPAIR, BS 1605, BETWEEN S26L/27L, PER SRM 53-00-01, REPAIR 7. DOUBLER/FILLER FABBED FROM 2024-T3, .063" AND 2024-T3, .040" MATERIAL RESPECTIVELY. THIS IS A CAT. "B" MAJOR REPAIR WITH FOLLOW UP INSPECTIONS AS FOLLOWS; INITIAL AT 24,000 FC, THEREAFTER EVERY 12,000 FC.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 39,368 hrs · 10,921 cycles

SEAT TRACK STA 418-440 RBL-24 GOUGED R & R SEAT TRACK, BS 418-440,RBL 24, SRM 51-40-02. BLENDED AREAS IAW SRM 53-00-52, FIG.101; ORIGINAL MATERIAL: .080", AFTER REWORK; .040", ON THE FLANGE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVED SEAT TRACK DAMAGE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SEAT TRACK, PN BAC 1520- 792, IAW SRM 51-40-02. REATED/PRIMED NEW SEAT TRACK IAW SRM 51-20-01. INSTALLED NEW SEAT TRACK, BS 418-440, RBL 24, IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 39,368 hrs · 10,921 cycles

SEAT TRACK STA.418-440 RBL.45, GOUGED. R & R SEAT TRACK BS 418-440, RBL 45, IAW SRM 51-40-02. BLENDED AREAS IAW SRM 53-00-52, FIG 101; ORIGINAL MATERIAL: .080", AFTER REWORK: .035", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7. REMOVED SEAT TRACK DAMAGE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SEAT TRACK, PN BAC 1520-792, IAW SRM 51-40-02. TREATED/PRIMED IAW SRM 51-20-01. INSTALLED NEW SEAT TRACK, BS 418-440, RBL 45, IAW SRM 51-40-02. MAJOR REPAIR

Part: SKIN — DENTED (BS 1640-1660) · airframe 39,368 hrs · 10,921 cycles

AT STA.1640-1660 BETWEEN STR 27 & 28R, 2 EA. PROTRUDING DENTS. OUTWARD. CONVEX CHECKED LIMITS; DENT NR 1 L=.50", W=.50", D=.043", A/Y=11 / DENT NR 2 L=.50", W= .50", D= .035", A/Y=14. FOUND BOTH DENTS TO BE OUT OF LIMITS PER SRM 53-00-01, FIG.101. REPAIRED AREA PER SRM 53-00-01, FIG.201, P.201, INSTRUCTIONS 1-11, REPAIR NR 3. THIS IS A CAT. "B" MAJOR REPAIR WITH THE FOLLOWING TRACKING; INITIAL AT 37,500 FC, THEREAFTER EVERY 6,000 FC, USING HFEC.

Part: FRAME — DENTED (BS 1500) · corrosion level 2 · airframe 39,368 hrs · 10,921 cycles

STA 1500 FRAME BETWEEN STR 26L AND 27L DENTED, GOUGED AND CORRODED. REMOVED CORROSION PER SRM 51-10-02; L=3", W=1", D=.004", WITHIN LIMITS PER SRM 53-00- 53, FIG.101. GOUGE AREA; L=1.2",W=.01", D=.003", WITHIN LIMITS PER SRM 53-00-53, FIG.101; DENT OUT OF LIMITS. NO DENTS ALLOWED, IN THIS AREA, PER SRM 53-00-07, FIG.101. HFEC NOTED NO CRACKS IN CUTOUT AREA. RECEIVED NEW DOUBLER ON TRAVELER T10/846636. INSTALLED DOUBLER PER SRM 53-00-07 AT BS 1500, S26L / 27L. MAJOR REPAIR.