N958FD

Part: SUPPORT ANGLE — CORRODED (ZONE 500) · airframe 59,319 hrs · 26,942 cycles

UPON REMOVAL OF LH WING, TRIALING EDGE, UPPER SKIN PANEL, DISCOVERED THE FORWARD LAND AT REAR SPAR HAD CORROSION. STARTED REMOVAL OF CORROSION AT T/E OF LEFT WING UPPER SKIN PANEL, BETWEEN WS 150-180 & WS 194.5 IAW SRM 57-20-01-1A. FOUND CORROSION EXTENDS FWD INTO AFT SPAR FASTENERS IN FUEL TANK. COMPLIED WITH E.A. F-5700-T0364606 PART 1 AND PART 2 WING-GENERAL-CORROSION FOUND ON 112N3101-11 WING SKIN TRAILING EDGE.

Part: STOP FITTING — OUT OF RIG (ZONE 800) · airframe 58,585 hrs · 26,456 cycles

"CABIN ALT" MESSAGE AND LIGHTS AT FL 390 30 MIN AFTER "L EMER DOORS" MESSAGE. RT COMPLIED DESCENT TO 10,000 FT AT AROUND 11,000 FT BOTH MESSAGES EXTINGUISHED. DECLARDED EMERGENCY/DIVERT TO ICT FOUND "LOW INFLOW" ON THE NR 1 CONTROLLER. ICT U FOUND LOWER FORWARD ADJUSTING STOP PIN OUT OF RIG. ADJUSTED PIN, DID CABIN ALTITUDE PRESSURE CHECK W/REF TO B757 MM 52-21-01-5. OPERATIONS CHECK GOOD. AC OK TO CONTINUE FOUND LOWER FORWARD ADJUSTING STOP PIN OUT OF RIG ADJUSTED PIN, DID CABIN ALTITUDE PRESSURE CHECK W/REF TO B757 MM 52-21-01-5. OPERATIONS CHECK GOOD. AC OK TO CONTINUE.

Part: SENSOR — OUT OF ALIGNMENT (EMERGENCY EXIT) · airframe 58,585 hrs · 26,456 cycles

"EMER DOORS" OVERHEAD LIGHT. "L EMER DOOR" MESSAGE AT FL 390 30 MIN INTO CRUISE. FOUND FWD SENSOR OUT OF ALIGNMENT. ADJUSTED AND SHIMMED WITH REF TO B757 MM 52-71-00-5. OPERATIONS CHECKED GOOD, AC OK TO CONTINUE.

Part: STOP FITTING — OUT OF RIG (DOOR) · airframe 58,585 hrs · 26,456 cycles

"CABIN ALT" MESSAGE AND LIGHTS AT FL 390 30 MIN AFTER "L EMER DOORS" MESSAGE. QRH COMPLIED DESCENT TO 10,000 FT, AT AROUND 11,000 FT BOTH MESSAGES EXTINGUISHED. DECLARDED EMERGENCY/DIVERT TO ICT. FOUND LOWER FORWARD ADJUSTING STOP PIN OUT OF RIG. ADJUSTED PIN, DID CABIN ALTITUDE PRESSURE CHECK W/REF TO B757 MM 52-21-01-5. OPERATIONS CHECK GOOD. AC OK TO CONTINUE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,438 hrs · 26,351 cycles

ON AMT PREFLIGHT COURIER AREA, CENTER EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. L1 ADN R1 INTERIOR DOOR, SLIDE LIGHTS AND COCKPIT LIGHTS OPS NORMAL. REF. 757 WDM 33-51-12, DURING T/S FOUND BLOWN FUSE ON POWER SUPPLY BATTERY CHARGER TRAY ASSY SUPPLYING POWER TO CONNECTOR D66 PIN 11. REMOVED AND REPLACED POWER SUPPLY BATTERY CHARGER TRAY ASSY. IAW AMM 33-51-07-2. CENTER EMERGENCY EXIT LIGHT OPS CHECK NORMAL.

Part: FRAME — CRACKED (L3 DOOR) · airframe 58,410 hrs · 26,329 cycles

L-3 DOOR UPPER MAIN FRAME CRACKED FROM EDGE TO FASTENER IN RADIUS AT SPLICE END . REMOVED AND REPLACED L-3 DOOR PER EA F-5220-T0356544 P1.

Part: FLOOR SUPPORT — CORRODED (BS 738) · corrosion level 2 · airframe 58,410 hrs · 26,329 cycles

CORROSION IN THE FWD CARGO FLOOR SUPPORT INTERCOSTAL LOWER FLANGE , APPROX BS.738 RBL.7.5 DOT 129-047 REMOVED CORR ON INTERCOASTAL APPROX STA 738 RBL7.5 IAW B757 SRM 51-10-02-0G. UPON EVAL FOUND INTERCOASTAL TO BE WRONG MATERIAL IAW BOEING DWG 143N5367 REV F. REMOVED, FABRICATED AND INSTALLED NEW INTERCOASTAL IAW B757 SRM 51-40-02-0G, 51-40- 05-0G.AND BOEING DWG 143N5367 REV A, REV F AND 143N5362 REV A

Part: FLOOR SUPPORT — CORRODED (BS 645) · corrosion level 2 · airframe 58,410 hrs · 26,329 cycles

CORROSION IN THE FWD CARGO FLOOR SUPPORT INTERCOSTAL LOWER ATTACH ANGLE , APPROX BS645 LBL. 16.5 DOT 129-053 REMOVED FABRICATED AND INSTALLED INTERCOSTAL IN FWD CARGO AT BS645 LBL16.5 IAW B757 SRM 51-40-02-0G AND BOEING DWG 143N5367 REV A / REV F. UPON FURTHER EVALUATION FOUND INTERCOSTAL TO BE WRONG MATERIAL IAW BOEING DWG 143N5367- REV A / F.

Part: FLOOR SUPPORT — CORRODED (BS 738) · corrosion level 2 · airframe 58,410 hrs · 26,329 cycles

CORROSION IN THE FWD CARGO FLOOR SUPPORT INTERCOSTAL LOWER FLANGE, APPROX BS.738 RBL 7.5 DOT 129-047. REMOVED CORROSION ON INTERCOASTAL, APPROX STA 738 RBL 7.5 IAW B757 SRM 51-10-02-0G. UPON EVAL FOUND INTERCOASTAL TO BE WRONG MATERIAL, IAW BOEING DWG 143N5367 REV F. REMOVED, FABRICATED, AND INSTALLED NEW INTERCOASTAL IAW B757 SRM 51-40-02-0G, 51-40-05-0G AND BOEING DWG 143N5367 REV A, REV F AND 143N5362 REV A.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,410 hrs · 26,329 cycles

AFT CARGO BILGE AREA, CORROSION ON FWD END OF INTERCOSTAL STA 1420 BETWEEN S27L AND S28L. UPON EVAL FOUND TO BE OUT OF ALLOWABLE LIMITS, IAW B757 SRM 53-00-04-1A FIG 101 DETAIL V. REMOVED, FABRICATED, & INSTALLED NEW AFT CARGO BILGE INTERCOSTAL STA 1420 BETWEEN S27L & S28L IAW B757 SRM 51-40-02-0G & IAW BOEING DWG NR 143N5398 REV P P/N 143N5398-7.

Part: INTERCOSTAL — CORRODED (BS 1420) · corrosion level 2 · airframe 58,410 hrs · 26,329 cycles

AFT CARGO BILGE AREA , CORROSION ON FWD END OF INTERCOSTAL STA 1420 BETWEEN S27L AND S28L. UPON EVAL FOUND TO BE OUT OF ALLOWABLE LIMITS IAW B757 SRM 53-00-04-1A FIG 101 DETAIL V. REMOVED FABRICATED & INSTALLED NEW AFT CARGO BILGE INTERCOSTAL STA 1420 BTWN S27L & S28L IAW B757 SRM 51-40-02-0G & IAW BOEING DWG # 143N5398 REV P P/N 143N5398-7.

Part: FLOOR SUPPORT — CORRODED (BS 645) · corrosion level 2 · airframe 58,410 hrs · 26,329 cycles

CORROSION IN THE FWD CARGO FLOOR SUPPORT INTERCOSTAL LOWER ATTACH ANGLE, APPROX BS645 LBL 16.5 DOT 129-053. REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL IN FWD CARGO AT BS645 LBL16.5, IAW B757 SRM 51-40-02-0G AND BOEING DWG 143N5367 REV A/REV F. UPON FURTHER EVALUATION FOUND INTERCOSTAL TO BE WRONG MATERIAL, IAW BOEING DWG 143N5367-REV A/F.

Part: ANGLE — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 58,410 hrs · 26,329 cycles

MAIN CABIN L/H CUSP WEB ANGLE (MOP SILL) UPPER SURFACE HAS CORROSION AT BS 1623. REMOVED CORROSION AT MAIN CABIN L/H CUSP WEB ANGLE MOP SILL (CREASE BEAM)IAW B 757 SRM 51-10-02-OG.EVALUATED AREA ORIGINAL MAT .070" MAT REM .061",MAT LOSS .009" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-60-13-1A FIG 101 DETAIL VIII. CUT OUT DAMAGE AREA STA 1589,TRIMMED,LOCATED,DRILLED AND INSTALLED NEW MOP SILL (CREASE BEAM) SECTION DIM 40" LONG,REPAIR SPLICE CHANNEL DIM 12" LONG,REPAIR STRAP DIM 11"X1",IAW B 757SRM 53-00-13-2R REPAIR 1,FIG 201 DETAIL II., ALT 1

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 58,072 hrs · 26,146 cycles

CRZ FL340, CABIN ALTITUDE WARNING. CABIN APPROX 10,000FT WITH APPROX 200FPM CLIMB, DIFFERENTIAL 6.4 DESCENDED TO FL320 NO HELP DUCT PRESSURE OVER 40PSI. DECDENT TO FL280 REGAINED CONTROL CABIN DESCEND LIGHT WENT OUT AT 8400 CABIN ALTITUDE. 6.0 DIFFERENTIAL. EVENTUALLY DESCENDED TO ABOUT 7,000FT. DB RT PACK MEL CLEARED. PERF VISUAL INSP OF DOOR SEALS, ALL ARE INTACT AND SHOW EVIDENCE OF GOOD SEALING. CHKD OUTFLOW VALVE FOR DEBRIS, NONE FOUND. VERIFIED SMOOTH OPERATION AND FULL CLOSING OF OUTFLOW VALVE. PERF BITE ON CABIN PRSR CONT'S, NO FAULTS - REF AMM 21-31-00-5. NO HIST 90 DAYS.

Part: GOVERNOR — FAULTY (NR 2 ENGINE) · airframe 57,535 hrs · 25,804 cycles

PDIS 958 72-00 6611 14SEP19 TLH OPEN U LOGPAGES: 3112691 DURING TAKEOFF RIGHT ENGINE DID NOT REACH FULL POWER. LEFT ENGINE 1.6 EPR RIGHT ENGINE 1.3 EPR. AFTER TAKEOFF RIGHT ENGINE REMAINED AT REDUCED POWER UNTIL LANDING. RIGHT POWER MATCHED LEFT AT SETTINGS LOWER THAN APPROX 1.3 EPR. FACT 15SEP19 00:20 TLH REPLACED #2 ENG FUEL GOVERNOR REF MM 73-21-01-4-4 LEAK/OPS CHECK GOOD.

Part: BATTERY — OUT OF POSITION (CABIN) · airframe 57,526 hrs · 25,797 cycles

DURING SERVICE CHECK FOUND EMERGENCY LIGHT ABOVE R1 DOOR AND EXTERIOR R1 DOOR LIGHT INOP. PROPERLY INSTALLED BATTERIES IN BOTH FWD CHARGER UNITS M730, M731 PER MM 33-51-07-2. FWD LEFT AND RIGHT EMERG LIGHTS CHECK NORMAL PER MM 33-51-00-5.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 56,825 hrs · 25,318 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED THE L1 SLIDE LIGHT, OPS CHECK GOOD IAW AMM 33-51-06-2-1.

Part: FLOOR SUPPORT — CRACKED (BS 325-345) · airframe 56,650 hrs · 25,206 cycles

FLOOR SUPPORT BS 325 TO 345, LBL 2 WAS CRACKED IN AFT LWR CORNER. FABRICATED A REPLACEMENT FLOOR SUPPORT IAW DWG 141N5150, REV BN.

Part: FLOORBEAM — CORRODED (BS 345) · airframe 56,650 hrs · 25,206 cycles

CORROSION PREVIOUS REPAIR IN THE MAIN CABIN WET AREA FLOOR BEAM UPPER SURFACE,BS.345 BETWEEN RBL. 5.0 TO LBL. 7.5. REMOVED THE EXISTING REPAIR IAW SRM 51-40-02-0G, FABRICATED, HEAT TREATED AND INSTALLED A NEW REPAIR IAW SRM 53-00-51-2R.

Part: SEAT TRACK — CORRODED (BS 345-365) · airframe 56,650 hrs · 25,206 cycles

CORROSION FOUND ON THE MAIN CABIN FWD WET AREA SEAT TRACK, UPPER SURFACE, BETWEEN BS 345 TO 365, RBL 14.50. FOUND TO BE OUT OF LIMITIS IAW SRM 53-00-52. REMOVED THE SEAT TRACK, FABRICATED A REPLACEMENT SEAT TRACK IAW DWG 3504-NC-2. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-02-02-0G.

Part: TRANSCEIVER — MALFUNCTIONED (RADAR ALTIMETER) · airframe 56,521 hrs · 25,116 cycles

CAPTAINS RADAR ALT BREAKS LOCK REPEATLY DURING CLIMB AND DECSENT THROUGH APPROX FL 200. REMOVED AND REPLACED THE LEFT RADIO ALTIMETER TRANSCEVER IAW MM 34-33-01-4. COMPLETED MCDP TEST 30/40 WITH NO FAULTS. IAW 22-00-02-2. OK FOR SERVICE.

Part: INDICATOR — MALFUNCTIONED (TE FLAP) · airframe 56,510 hrs · 25,111 cycles

DURING APPROACH AFTER F/O CALLED FLAPS 15, NOTICED A SPLIT IN THE FLAP INDICATOR WITH RIGHT NEEDLE AT FLAP 1 AND LEFT NEEDLE AT FLAP 15. DISCONTINUED APPROACH. NO EICAS OR OTHER INDICATIONS OF A FLAP PROBLEM. F/O SAID THERE WAS NO LATERAL CONTROL ISSUES HE COULD FEEL. RAN THE FLAP INDICATION DISAGREE CHECKLIST. LANDED NORMALLY WITH FLAPS 30. REMOVED AND REPLACED FLAP POSITION INDICATOR.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS) · airframe 56,395 hrs · 25,034 cycles

NOTED FLAP ASSYMETRY WHEN FLAPS 30 SELECTED. ONE FLAP REMAINED AT 20. FLAPS CAME UP TOGETHER DURING GO-AROUND. FLAPS CAME DOWN NORMALLY FOR SUBSEQUENT LANDING. NO EICAS OR STATUS MESSAGE NOTED. EMERGENCY DECLARED. REMOVED AND REPLACED FLAP POSITION INDICATOR.

Part: GEAR — BROKEN (L1 DOOR) · airframe 56,322 hrs · 24,992 cycles

DURING PREFLIGHT FOUND L1 LOCKING OPEN MECHANISM GEAR BROKE, DOOR OPENS AND CLOSES NORMALLY, LOCKING CLOSED MECHANISM GOOD. REMOVED AND REPLACED THE L1 DOOR HOLD OPEN LOCK IAW AMM 52-11-08-4-0. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: FSEU — MALFUNCTIONED (TE FLAP SYS) · airframe 55,503 hrs · 24,470 cycles

DURING ARRIVAL, AT SELECTION OF FLAPS TO 20, ONE FLAP POINTER REMAINED AT 15 WHILE OTHER CONTINUED TO 20. NO EICAS MESSAGE OR TRAILING EDGE LIGHT ILLUMINATED. LANDING EXECUTED AT FLAPS 20. DURING APPROACH BOTH POINTERS RESET TO 20. UNEVENTFUL LANDING AND ROLLOUT. OPERATED FLAPS NUMEROUS TIMES AT GATE, COULD NOT DUPLICATE THE PROBLEM. REMOVED AND REPLACED THE NR 1 FSEU. ACCOMPLISHED ALL REQUIRED CHECKS AND ALL CHECKED NORMAL.

Part: SKIN — CORRODED (BS 535) · corrosion level 2 · airframe 53,294 hrs · 23,007 cycles

LOWER FUSELAGE SKIN HAS AN AREA OF CORROSION AT BS 535 BL 0 UNDER ATC ANTENNA AREA. REPAIRED IAW EA F-5330-T0311516 REV PSP1.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,294 hrs · 23,007 cycles

RIGHT WING TE AFT FLAP TAPS DELAMINATION ON LOWER SURFACE, APPROX WING STATION 537, AFT OF NR 11 SPOILER BOARD. REMOVED DAMAGE, DIMENSION 6 X 6, SANDED, CLEANED, PREPPED RT WING AFT FLAP, APPLIED REPAIR, PRIMED & TOP COATED AREA ALL IAW SRM 51-70-17, 51-20-01, 57-53-01, AMM 51-21-10-7 & EA F-5750-TO311697 PT1.

Part: SEAT TRACK — CORRODED (BS 345-378) · corrosion level 2 · airframe 53,294 hrs · 23,007 cycles

LEFT COURIER AREA SEAT TRACK IS CORRODED BS 345 - 378. REMOVED, FABRICATED & INSTALLED NEW SEAT TRACK IAW SRM 51-40-02, 51-20-01 DWG 3504-NC-2.

Part: CHARGER — FAILED (CABIN) · airframe 53,280 hrs · 22,994 cycles

R1 DOOR INTERIOR & EXTERIOR EMER LIGHTS INOPERATIVE. R & R FWD EMER BATTERY & CHARGER IAW MM 33-51-07-2. ACFT OK TO CONTINUE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,199 hrs · 22,944 cycles

R1 DOOR EMER EXIT SIGN WILL ONLY ILLUMINATE FOR A FEW SECONDS ON PREFLIGHT TEST. R & R R1 DOOR EMER SIGN BATTERY PACK IAW MM 33-51-07-2. OPERATIONS CHECKED NORMAL OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 52,692 hrs · 22,586 cycles

PARKED AT GATE, SET PARKING BRAKE, PARKING BRAKE SHOWED ON EICAS. ACFT ROLLED FWD ANYWAY. SET PARKING BRAKE SEVERAL TIMES, FUNCTIONS NORMAL. PERFORMED ADJUSTMENT TEST IAW 757-200 MM 32-44-00-5. OPERATIONS CHECKED OK, NO HISTORY, OK FOR SERVICE.

Part: CONTROL ROD — LOOSE (PAX DOOR) · airframe 52,328 hrs · 22,322 cycles

L1 DOOR ARMED KNOCKER LOOSE. REMOVED & REPLACED AND ADJUSTED L1 DOOR RETRACTABLE DOOR MECHANISM ROD ASSY IAW MM 52-11-20-5. OP'S CHECKED NORMAL.

Part: SWITCH — ARCED (EXTERIOR LIGHTS) · airframe 51,834 hrs · 22,015 cycles

BURNING RUBBER ODOR AT INITIAL POWER UP ON TAXI OUT. THEN ON TAKE OFF ROLL. ODOR GOES AWAY IN ABOUT 10 SECONDS. TURNED ON ALL EXTERIOR LIGHTS. DETECTED A BURNING ODOR. TURNED OFF LIGHTS WOULD DIMINISH THE ODOR. PULLED DOWN LIGHT OVERRIDE PANEL, AND NOTICE LIGHT SWITCH ARCING. R & R LIGHT OVERIDE CONTROL PANEL ASSY IAW AMM 20-60-00, GROUND OPS CHECKED ALL LIGHTS ON CONTROL PANEL. ALL CHECKED GOOD, NO FUTHER ODOR NOTICED, ACFT OK FOR CONTINUED SERVICE AT THIS TIME.

Part: SWITCH — ARCED (EXTERIOR LIGHTS) · airframe 51,834 hrs · 22,015 cycles

BURNING RUBBER ODOR AT INITIAL POWER UP ON TAXI OUT. ON TAKEOFF ROLL, ODOR GOES AWAY IN ABOUT 10 SECONDS. ODOR BOTH TIMES WAS WITH THE APU OFF. RAN BOTH ENGINES AT THE GATE AND ISOLATED THE APU AND RAN WITH ONE PACK AT A TIME, AND THEN WITH BOTH PACKS ON, NO ODOR WAS DETECTED AT ANY TIME. TURNED ON ALL EXTERIOR LIGHTS, DETECTED A BURNING ODOR . TURNING OFF LIGHTS WOULD DIMINISH THE ODOR. PULLED DOWN LIGHT OVERRIDE PANEL, AND NOTICE RT RUNWAY TURNOFF LIGHT SWITCH ARCING. R & R LIGHT OVERIDE CONTROL PANEL ASSY, WHICH INCLUDES THE RT TURNOFF LIGHT SWITCH, IAW AMM 20-60-00, GROUND OPS CHECKED ALL LIGHTS ON CONTROL PANEL. ALL CHECKED GOOD, NO FUTHER ODOR NOTICED, ACFT OK FOR CONTINUED SERVICE.

Part: WEB — CORRODED (BS 106.20) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

LEFT WING CENTER TANK FUEL QTY HARNESS FEED THRU JUST OTBD OF WBL 79.50 ON L/E SPAR CORRODED. COMPLIED WITH EA F-5710-162408 (WING-SPAR WEB CORROSION AT FUEL GAUGE CONNECTOR). CAT "A" REPAIR REF: FAA FORM 8100-9. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 57-20-10, FIG 101, DETAIL 5. MAJOR REPAIR.

Part: SPAR — CORRODED (ZONE 500) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

LT OTBD MAIN FLAP FRONT SPAR AFT FACE CORRODED AT APPROX WS 600. COMPLIED WITH EA F-5750-162538, MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 51,823 hrs · 22,005 cycles

SURFACE CORROSION AROUND FASTENERS ON LT OTBD CREASE BEAM REPAIR ANGLE BS 1500-1520 AT BS 1460-1540, STR 17L. REPAIRED IAW EA 757-5361-16-F3872. MAJOR REPAIR.

Part: SPAR — CORRODED (ZONE 600) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

RT AFT WING SPAR WEB SURFACE BOTTOM SURFACE HAS CORROSION AT IRSS 183. COMPLIED WITH EA F-5710-162544-WINGS-MAIN FRAME-OUTER TANK-REAR SPAR CORROSION IRSS 183.0. RTS (AFT BOOST PUMP) REF FAA FORM 8100-9. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 418-439) · airframe 51,823 hrs · 22,005 cycles

TCAS ANTENNA STRUCTURE, EXTRANEOUS FASTENER HOLES IN SKIN BETWEEN BS 418 AND 439, STR 1 TO 2R. REPAIRED IAW EA 757-5311-16-F3842, REV. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 440-640) · airframe 51,823 hrs · 22,005 cycles

MAIN DECK CARGO TRACK BS 440- 640, RBL 24 HAS SEVERAL NICKS, GOUGES, SCRATCHES AND CORROSION. EVALUATED GOUGED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5080. MAJOR REPAIR.

Part: SKIN — DAMAGED (L4 DOOR) · airframe 51,823 hrs · 22,005 cycles

L4 DOOR FWD EDGE EXTERIOR SKIN IS DEFORMED APPROX ABOUT TWO INCHES OPPOSITE OF DOOR FWD STOP FITTING NR 3. REPAIRED ON 48208890001 AND EA 757-5210-16-F3857, REV - .

Part: STRINGER — DAMAGED (BS 1640-1661) · airframe 51,823 hrs · 22,005 cycles

STRINGER HAS SEVERAL FASTENERS HOLES BLOWN OUT (DAMAGED) BETWEEN STA 1640-1661, STR 4L. REMOVED STRINGER FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, NOTE A , FIG 101 PAGE 101. INSTALLED NEW STRINGER IAW SRM 53-00-03 FIG 201 (SHEET 1 OF 8 ) REPAIR 2 PAGE 201. MAJOR REPAIR

Part: STRINGER — DAMAGED (BS 1630-1650 S4R) · airframe 51,823 hrs · 22,005 cycles

SEVERAL FASTRNER HOLES DAMAGED & CRACKED BETWEEN BS 1640-1661, STR 4R. REPAIRED STRINGER IAW SRM 53-00-03, FIG 201, REPAIR 2. CATEGORY A REPAIR.

Part: RIB — CORRODED (RWS 806.5) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

RT WING AT STATION 806.50, AILERON B. WIRE ATTACHMENT POINT CORRODED. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS ORIGINAL MATERIAL .070, MATERIAL REMAINING .040, MATERIAL LOSS .030. FOUND OUT OF LIMITS IAW SRM 57-51-09, PG 106, DETAIL IV, FIG.101. REMOVED AND REPLACED RIB IAW SRM 51-40-02, 51-40-05, AND DRAWING 113N1511. MAJOR REPAIR

Part: BEAM — DENTED (ZONE 100) · airframe 51,823 hrs · 22,005 cycles

AFT CARGO DOOR LOWER SUPPORT EDGE BEAM HAS MULTIPLE DENTS. CHECKED LIMITS LOWER EDGE BEAM BS 1380 -1440 FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02, R & R LOWER EDGE BEAM, IAW SRM 51-40-02 AND DWG 146N6603.

Part: SPAR CAP — CORRODED (LT WING) · airframe 51,823 hrs · 22,005 cycles

CORROSION ON LT WING REAR SPAR UPPER ANGLE AT WS 160, ALSO BETWEEN ANGLE AND SKIN. REPAIRED IAW EA F-5710-162424. MAJOR REPAIR.

Part: FRAME — GOUGED (BS 1280 S11-14R) · airframe 51,823 hrs · 22,005 cycles

FRAME BS1280 S11 - 14R, DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, DETAIL II FIG 101 SH. 3. INSTALLED NEW FRAME REPAIR IAW SRM 51-40-02 AND SRM 53-00-07 REPAIR 3, DETAIL II, FIG 201, SHEET 3 . MAJOR REPAIR

Part: CHANNEL — GOUGED (BS 1280 S11L) · airframe 51,823 hrs · 22,005 cycles

CHANNEL HAS GOUGES AT FRAME BS 1280, S11L. DAMAGE FOUND OUT-OF-LIMITS IAW SRM 53-00-07, FIG 101 DETAIL V. INSTALLED NEW FRAME REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 3.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,823 hrs · 22,005 cycles

SEAT TRACK BS 780-879 LBL 45, CORRODED, NICKED AND GOUGED. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. DETAIL VII, FRABRICATED NEW SEAT TRACK IAW DWG 143N5090, INSTALLED SEAT TRACK IAW DWG 143N5080 AND SRM 51-40-02. MAJOR REPAIR.

Part: CHANNEL — CORRODED (BS 680-740) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

STRINGER 17L, CHANNEL BS 680 -740, CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, PAGE 103, DETAIL II, FIG.101. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02 AND DRAWING 143N8322. MAJOR REPAIR

Part: FRAME — MISREPAIRED (BS 1520 S23-26R) · airframe 51,823 hrs · 22,005 cycles

FRAME BS 1520, STR 23R -26R MISREPAIRED.

Part: FLOOR SUPPORT — CORRODED (BS 700-720) · airframe 51,823 hrs · 22,005 cycles

MAIN DECK CARGO, RT FLOOR CHANNEL WEB & STIFFENER AT STA 700 - 720, RBL 55 HAS CORROSION BOTH UPPER & LOWER SURFACE AROUND NUTPLATES SDR WAS GENERATED IN ERROR. DETERMINED TO BE A MINOR REPAIR ON SECONDARY STRUCTURE.

Part: FLOOR SUPPORT — CORRODED (BS 720-740) · airframe 51,823 hrs · 22,005 cycles

FLOOR SUPPORT BS 720-740, RBL 55 CORRODED BOTH UPPER AND LWR SURFACES AROUND NUTPLATES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15 DETAIL VI, FIG 101. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 51,823 hrs · 22,005 cycles

SEAT TRACK FROM STA 780-880, RBL 45 HAS SEVERAL SCRATCHES, NICKS & CORROSIONS ON FLANGE & CROWN AREA. FOUND SEAT TRACK FASTENER HOLES OUT OF LIMITS IAW SRM 51-10-02 AND SRM 53-00-52, FIG 101, DETAIL V. R & R SEAT TRACK AT STA 780-880, RBL 45 IAW SRM 51-40-02 AND DWG NR 143N5080.

Part: CREASE BEAM — CORRODED (BS 600-640) · airframe 51,823 hrs · 22,005 cycles

MAIN DECK CARGO RT CREASE BEAM BS 600 -640 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, PAGE 102 AND 101 DETAIL V. R & R CREASE BEAM BS 460 THRU 660 RT IAW SRM 51-40-02 AND DWG 143N5520. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 780-880) · airframe 51,823 hrs · 22,005 cycles

SEAT TRACK BS 780-880 RBL 24, HAS SEVERAL AREAS WITH SCRATCHES, NICKS & CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-52, FIG 101, DETAIL I. R & R SEAT TRACK FROM STA 780 -880, RBL 24 IAW SRM 51-40-02 AND DWG 143N5080 AND 143N5090. MAJOR REPAIR.

Part: ATTACH FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

LT WING AFT SPAR AT W STA 820 , RIB ATTACHMENT TO BONDING JUMPER CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 57-51-09 FIG 101 DETAIL VI PG 106.. REMOVED AND REPLACED RIB WITH NEW RIB, IAW SRM 51-40-02, SRM 51-40-05, AND DWG 113N1511 SH.1. MAJOR REPAIR

Part: CREASE BEAM — CRACKED (ZONE 200) · airframe 51,823 hrs · 22,005 cycles

INBD CREASE BEAM AT STA 800 -820 NOTCHED REPAIR CUTOUT. AFTER EVALUATION CREASE BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, PAGE 103, DETAIL V. R & R CREASE BEAM STA 800 -900 RT IAW SRM 51-40-02 AND DWG 143N5520. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 51,823 hrs · 22,005 cycles

SKIN MISREPAIRED. REPAIRED IAW EA F-5330-162426. REPAIR MAJOR.

Part: SKIN — GOUGED (BS 1580) · airframe 51,823 hrs · 22,005 cycles

AFTER REMOVAL OF DISCREPANT FRAME AT BS 1580 FOUND GOUGED IN INNER FUSELAGE SKIN AT BS1588 BETWEEN S28L AND S29L. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101. HFEC TRIMMED AREA IAW NTM 51-00-19 PT 6, NO CRACK NOTED. RECEIVED REPAIR DOUBLER MADE OUT OF2024-T3.063C ON STAM BATCH 0002260813; INSTALLED REPAIR DOUBLER IAW SRM 53-00-01, FIG 201. REPAIR 16 AND 51-40-02 AT STA 1588 BETWEEN STR28 -29L. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1580) · airframe 51,823 hrs · 22,005 cycles

FRAME BS 1580, S25-26R MISREPAIRED. REMOVED AND REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1020. MAJOR REPAIR

Part: FLOORBEAM — DAMAGED (BS 660) · airframe 51,823 hrs · 22,005 cycles

MAIN CABIN BS 660 FLOORBEAM UPPER FWD FLANGE HAS ONE HOLE WITH SHORT ED LBL 69. OUT OF LIMITS IAW SRM 51-40-06, FIG 3. REMOVED FLOORBEAM IAW SRM 51-40-02. INSTALLED NEW FLOORBEAM IAW SRM 51-40-02 AND DWG 143N5012. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 1844-1862.7) · airframe 51,823 hrs · 22,005 cycles

FUSELAGE SKIN MISREPAIRED AT BS 1844-1862.7, STR 30 . REPAIRED IAW SRM 53-00-01, FIG 201, DETAIL II. REPAIR 16, PAGE 206. CATEGORY B, MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 465) · airframe 51,823 hrs · 22,005 cycles

SEAT TRACK RBL 45 HAS DOUBLE DRILLED HOLE AT BS 465 AND OTHER AREAS HAS SEVERAL NICKS, GOUGES AND CORROSIONS AT THE CROWN AND FLANGE AREA.

Part: SEAT TRACK — GOUGED (BS 1350-1540) · airframe 51,823 hrs · 22,005 cycles

SEAT TRACK HAS GOUGES AT RBL 45 BETWEEN BS 1350 TO 1540. DAMAGE FOUND OUT OF LIMITS IAW SRM 53-00-52 PAGE 102 FIG 101 DETAIL I. REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 AND DRAWING 146N5130. MAJOR REPAIR

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

STRINGER 17L BS 333- 377, CORRODED . REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS FOUND STRINGER TO BE OUT OF LIMITS. R & R STRINGER IAW SRM 51-40-02 AND DWG 141N8322. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1360 S26R) · airframe 51,823 hrs · 22,005 cycles

EXISTING FRAME REPAIR AT BS 1360, S26R MISREPAIRED R & R FRAME AND FAILSAFE IAW SRM 51-40-02, AND DWG 146N1009 AND 146N1028. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440-680) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

LEFT SEAT TRACK BS 440-680, LBL 24.75, CORRODED, NICKED AND GOUGED. EVALUATED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL III. R & R SEAT TRACK STA 440- 680, LBL 24.75, IAW DWG NR 143N5080 AND SRM 51-40-02, AT BS 440-680, LBL 24.75. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 896-1075) · airframe 51,823 hrs · 22,005 cycles

MAIN CABIN SEAT TRACK AT LBL 25, FROM BS 896 TO 1074 IS DIRTY, NICKED, GOUGED AND WITH LIGHT CORROSION. CLEANED SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. R & R WITH NEW SEAT TRACK, IAW DWG 144N5001, AND SRM 51-40- 02. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 1320-1540) · airframe 51,823 hrs · 22,005 cycles

LBL 25 SEAT TRACK DIRTY AND GOUGED BS 1320- 1540. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52. INSTALLED NEW SEAT TRACK AT LBL 24.75 BS 1320- 1540 IAW SRM 51-40-02 AND REF DWG 146N5120. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1520) · airframe 51,823 hrs · 22,005 cycles

FRAME MISREPAIRED AT BS 1520, STR 23R-26R. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1017. CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 1540-1640) · airframe 51,823 hrs · 22,005 cycles

LBL 45 SEAT TRACK DIRTY AND GOUGED STA 1540 -1640. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I, PAGE 102. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5135. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 896-1074) · airframe 51,823 hrs · 22,005 cycles

MAIN CABIN SEAT TRACK AT RBL25, FROM BS 896 TO 1074, IS DIRTY, NICKED, GOUGED AND HAS LIGHT CORROSION. CLEANED SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED AND REPLACED WITH NEW SEAT TRACK, PER DRAWING 144N5001 AND SRM 51-40-02, MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1320) · airframe 51,823 hrs · 22,005 cycles

FRAME MISREPAIRED AT BS 1320, STR 23L -26L. R & R FRAME IAW SRM 51-40-02 AND DWG 146N1007. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1500 S23-26R) · airframe 51,823 hrs · 22,005 cycles

FRAME AT BS 1500, STR 23 - 26R, MISREPAIRED. R & R FRAME IAW SRM 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 896-1074) · airframe 51,823 hrs · 22,005 cycles

MAIN CABIN SEAT TRACK AT LBL 45, FROM BS 896 TO 1074 IS DIRTY, NICKED, GOUGED, AND HAS LIGHT CORROSION. CLEANED SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED AND REPLACED WITH NEW SEAT TRACK, PER DRAWING 144N5001, AND SRM 51-40-02. MAJOR REPAIR

Part: CREASE BEAM — CORRODED (BS 1350) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

LT INBD CREASE BEAM CORRODED AT BS 1350. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, PAGE 103, FIG. 101, DETAIL VII. REMOVED AND REPLACED CREASE BEAM AT BS 1280-1380, LT, I/B, IAW SRM 51-40-02 AND DRAWING 146N8326. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 1540-1640) · airframe 51,823 hrs · 22,005 cycles

LBL 25 SEAT TRACK DIRTY AND GOUGED STA 1540-1640. FOUND DAMAGED SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 PAGE 102 DETAILS I AND III. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5135 .

Part: SKIN — CRACKED (CARGO DOOR) · airframe 51,823 hrs · 22,005 cycles

AFT CARGO COMPARTMENT DOOR AFT LOWER CORNER SKIN DAMAGED. HFEC INSPECTED DAMAGE IAW NDTM PT6 51-00-19 FOUND CRACKED. FABRICATED DOUBLER AND INSTALLED DOUBLER IAW SRM 52-30-01, FIG 201. REPAIR 4. CAT B MAJOR.

Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 51,823 hrs · 22,005 cycles

NR 1 PYLON RT SIDE SKIN INNER SURFACE, STA 153 - 172, HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL III. LOCATED AND DRILLED. INSTALLED NEW RT AFT SKIN AND ALL ATTACHING PARTS IAW SRM 51-40-02 AND DWG 311N5002. MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 51,823 hrs · 22,005 cycles

SEAT TRACK HAS GOUGES BETWEEN STA1350 TO 1540, RBL 25 . REMOVED DAMAGE FROM SEAT TRACK AT STA 1320 - 1540, RBL 25 IAW SRM 51-10-02. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1, FIG 101, SH 2 . FABRICATED NEW SEAT TRACK IAW SRM 51- 10-02, SRM 53-60-52 FIG 1, SH 2 AND DWG 146N5134. INSTALLED NEW SEAT TRACK AT STA 1320 - 1540, RBL 25 IAW 51-40-02. MAJOR REPAIR .

Part: SEAT TRACK — GOUGED (BS 1540-1610) · airframe 51,823 hrs · 22,005 cycles

SEAT TRACK HAS GOUGES AT RBL 25 BETWEEN BS 1540 TO 1610. REMOVED DAMAGED SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. FABRICATED SEAT TRACK IAW SRM 53-60-52 AND REF DWG 146N5120. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5120. MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 400) · airframe 51,823 hrs · 22,005 cycles

NR 1 PYLON RT SIDE AT ACCESS DOOR 433GR CUT-OUT IS CORRODED. REMOVED SKIN & CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01 FIG 101 DETAIL III . ORIG MAT .188 REMAINING MAT .122. RECEIVED NEW SKIN. LOCATED AND DRILLED IAW SRM 51-40-02 . INSTALLED NEW SKIN IAW SRM 51-40-02 AND DRAWING 311N5400. MAJOR REPAIR

Part: SKIN — CORRODED (NR 2 NACELLE) · airframe 51,823 hrs · 22,005 cycles

NR 2 PYLON LT SIDE SKIN INTERNAL SURFACE BET, PP STA 144 AND 174 HAS CORROSION. REMOVED CORROSION IAW SRM 51-40-02, FOUND OUT LIMITS IAW SRM 54-50-01, PG 101 DETAIL III. ORIGINAL THICKNESS .090" REMAINING THICKNESS .060". REPAIRED NR 2 PYLON LT SIDE SKIN IAW EA F-5450-162405, NACELLES/PYLONS- NR 2 PYLON INBD SKIN CORROSION REPAIR. REF FORM 8100-9, DATED 08/01/12 FOR APPROVAL. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 1700-1706) · airframe 51,823 hrs · 22,005 cycles

FOUND SCRIBE LINE AT S10L LAPJOINT, FROM BS 1700.094 TO BS 1706.2019. ACCOMPLISHED EA F-5330-160576, PART 1. CAT "B" MAJOR REPAIR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

SHEAR WEB BS 1680 -1720 LBL 62 -RBL 62. UPPER SURFACE CORRODED. REMOVED DAMAGED PRESSURE DECK/ SHEAR WEB FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. INSTALLED NEW DECK IAW SRM 53-60-51, SRM 51-40-02 AND DWG 146N5300. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

FLOORBEAM, BS 345 BL 0 - LBL 26, UPPER TEE CORRODED. REMOVED CORROSION, ORIG MAT .125, AFTER REWORK .108. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DET III. REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 201 REPAIR 3 . CATEGORY A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 51,823 hrs · 22,005 cycles

MAIN DECK CARGO FLOORBEAM AT BS 1640, LBL 58 - RBL 58, HAS SEVERAL ELONGATED HOLES AT UPPER TEE ANGLE, CORROSION AROUND FASTENERS ATTACHED TO WEB AT BL 0 AND GOUGED ADJACENT TO NUT PLATES. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI . REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02 AND DWG 146N5180. MAJOR REPAIR .

Part: CREASE BEAM — CORRODED (BS 297-428) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

CREASE BEAM S17R, BS 297-428 CORRODED. REMOVED CORROSION BY BLENDING IAW SRM 51-40-02. CHECKED LIMITS AFTER REWORK FOUND INBD CREASE BEAM OUT OF LIMITS IAW SRM 53-30-13 DETAIL III. FABRICATED NEW INBD CREASE BEAM, LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED NEW INBD CREASE BEAM IAW SRM 51-40-02 AND DWG 141N8322. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1340) · corrosion level 2 · airframe 51,823 hrs · 22,005 cycles

BS 1340, FLOORBEAM UPPER SURFACE HAS CORROSION AT FASTENER HOLES BL 0 TO LBL 25. REMOVED DAMAGED FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. INSTALLED NEW FLOORBEAM IAW SRM 53-60-51, SRM 51-40-02 AND DWG 146N5008. MAJOR REPAIR.