N998FD

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 71,621 hrs · 26,412 cycles

DECLARED EMERGENCY DUE TO CABIN ALTITUDE WARNING. PERFORMED PHASE 1 AND QRH. RETURNED TO FIELD. THE RIGHT PACK WAS OFF AT THE TIME, DUE TO RUNNING THE CABIN ALTITUDE HOT QRH MOMENTS BEFORE. TROUBLESHOT, PER FIM 21-30 FAULT TREE 802. UPON DISCOVERY FOUND THAT THE CABIN ALTITUDE PRESSURE COMPUTER (M119), THE NO FAULT LIGHT DID NOT ILLUMINATE, AND THE LRU DID NOT COMPLETE THE BITE TEST. REMOVED AND REPLACED NR 2 CABIN PRESSURE CONTROLLER, IAW B757 AMM 21-31-02-4. OPERATIONS CHECK GOOD. A/C OK TO CONTINUE.

Part: CONTROL VALVE — FAILED (AC BAY) · airframe 71,077 hrs · 26,026 cycles

AT CRUISE FL410COCKPIT OVERTEMP OCCURED WITH TEMP CONTROL INPUTS HAVING NO EFFECT. RAN QRH PROCEDURE, "CABIN TEMP INOP" TO STEP 4 WHICH DIRECTED US TO "CABIN TEMP HOT" PROCEDURE. WE MADE IT TO STEP 12 WITH LEFT PACK SELECTED AUTO, RIGHT PACK OFF. THE LEFT PACK FAILED WITH INOP LIGHT ILLUMINATED. TURNED ON RIGHT PACK TO AUTO & REMAINED PACK OFF. CABIN ALTITUDE ALARM ANNUNCIATED AND CABIN ALTITUDE BEGAN RAPIDLY CLIMBING. DECENT INITATED TO FL250 WITH QUICK DON O2. RIGHT PACK DID NOT BEGIN OPERATING SO WE CONTINUED DESCENT TO 10,000 FEET. HEARD LOUD KNOCKING ON LEFT SIDE OF AIRCRAFT AFT OF THE COCKPIT. DECLARED EMERGENCY & DIVERTED TO KDEN. BIT CHECK OF LEFT PACK TEMP CONTROLLER SHOWED LEFT PACK TEMP CONTROL VLV FAULT, REF FIM 25-51-00. R&R LEFT PACK TEMP CONTROL VALVE, LEAK AND OPS CK'S NORMAL.

Part: COMPUTER — FAILED (E&E BAY) · airframe 70,632 hrs · 25,729 cycles

PDIS 998 34-11 5664 16JUL19 OKC OPEN U LOGPAGES:3000296 ON TAKEOFF AIRSPEED DISAGREE, COMPLIED WITH QRH, IDENTIFIED IT AS F/O AIRSPEED. OPS CHECKED AND LEAK CHECKED F/O PITOT TUBE IAW AMM 30-31-00-5. REPLACED RT AIR DATA COMPUTER IAW AMM 34-12-01-4. OPS CHECKS GOOD. OK FOR SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,075 hrs · 25,371 cycles

MAIN CABIN SEAT TRACK AT BS 365 TO BS 375 RBL 45.5 IS CORRODED. COMPLIED WITH EA F-5310-T0343923 P1, FUSELAGE- MAINFRAME- SEAT TRACK SUPPORT REPAIR AT STA 365 AT RBL 45.5.

Part: DECK PLATE — DAMAGED (BS 1683-1701) · airframe 70,075 hrs · 25,371 cycles

MAIN CABIN AFT WET AREA DECK PLATE HAS BLEND OUTS AT APPROX STA 1683 TO STA 1701 FROM LBL2 TO RBL2. MAX MATERIAL LOSS IS .022" OUT OF ALLOWABLE LIMITS PER SRM. CUT OUT DAMAGE, FABRICATED REPAIR FILLERS 2024-T3 .071 AND REPAIR DOUBLER FROM 2024-T3 .080" AND INSTALLED REPAIR TO MAIN CABIN AFT WET AREA DECK PLATE IAW B757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE II. AT STA 1683 TO 1701 LBL2 TO RBL 2.

Part: DECK PLATE — DAMAGED (BS 1685) · airframe 70,075 hrs · 25,371 cycles

MAIN CABIN AFT WET AREA AFT DECK HAS A BLEND OUT AT APPROX STA 1685 AT RBL 45.5 ORIGINAL THICKNESS IS .071" REMAINING MATERIAL IS .057" OUT OF ALLOWABLE LIMITS PER SRM. FABRICATED REPAIR SHIM FROM 2024 -T3 .012 1"X1" , REPAIR DOUBLER FROM 2024-T3 .063, 5"X6" AND INSTALLED REPAIR TO AFT DECK AT STA .1685 RBL 45.5 IAW B757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I.

Part: TORQUE TUBE — LACK OF LUBE (L1 DOOR) · airframe 69,392 hrs · 24,908 cycles

DURING A POST FLIGHT INSPECTION, THE L1 DOOR WILL NOT OPEN FULLY. DOOR BINDING HALFWAY DURING OPENING SEQUENCE. LUBRICATED THE DOOR HINGE TORQUE TUBES, BODY TORQUE TUBES, UPPER AND LOWER CAM PLATES IAW AMM 12-21-18-3. OPERATED THE DOOR NORMALLY WITH NO BINDING SEVERAL TIMES.

Part: GIRT BAR — DAMAGED (L1 DOOR) · airframe 69,345 hrs · 24,885 cycles

L FWD ENTRY DOOR RAFT SLIGHTLY AJAR. NOT FULLY STOWED. R&R L1 EMERGENCY DOOR ASSSIST BOTTLE REF M/M 52-11-33-4. FOUND GIRT BAR DAMAGED. INSTALLED ORIGINAL SLIDE ASSY REF MM 25-66-01-4. INSTALLED NEW GIRT BAR REF MM 25-66-10-2. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: VALVE — FAILED (NLG STEERING) · airframe 68,959 hrs · 24,616 cycles

FIRST OFFICER HAD NO RUDDER STEERING DURING TAKE OFF. REJECTED THE TAKE OFF AT 40 KNOTS. REMOVED AND REPLACED THE NOSE WHEEL STEERING METERING VALVE IAW MM 32-51-12-4, OPS AND LEAK CHECKED OK. COMPLIED WITH NOSE WHEEL STEERING SYSTEM ADJUSTMENT AND TEST IAW 32-51-00-5-3, TESTED OK. CAPTAIN'S AND FIRST OFFICER'S RUDDER INPUTS TO NOSE WHEEL STEERING ARE IDENTICAL.

Part: LIGHT — FALSE ACTIVATION (DOOR ARMING) · airframe 68,830 hrs · 24,510 cycles

F/O SIDE ENTRY DOOR SLIDE LIGHT ILLUMINATED WITH ARMING HANDLE IN DISARMED POSITION. INSPECTED R1 DOOR PROXIMITY SENSORS AND GIRT BAR ENGAGEMENT REF M.M. 25-66-11-2. GIRTBAR CLEARANCE CHECK PERFORMED PER MM 25-66-11-2, CHECKED OK. OPS CHECK OF DOOR ARMING PER MM 52-11-00-0-0 NUMEROUS TIMES LIGHT OPERATES NORMALLY. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (BS 1715) · airframe 68,508 hrs · 24,288 cycles

CRACK IN SKIN BS 1715 MEASURING 2.7 INCHES LONG BETWEEN STRINGERS 18 - 19L. COMPLIED WITH EA F-5330-T0329499 P1.

Part: WINDOW — CRACKED (COCKPIT) · airframe 68,055 hrs · 23,965 cycles

IN CRUISE AT FL320, RT FWD WINDOW, OUTER PANE SHATTERED, ACCOMPANIED BY RT FWD WINDOW EICAS. COMPLIED WITH QRH. R & R R1 WINDOW IAW MM 56-11-01-4. FIRST TORQUE COMPLETED AT 00:30Z ON 14 APR 16. RII PERFORMED. OK FOR SERVICE.

Part: GIRT BAR — DIRTY (R1 DOOR SLIDE) · airframe 67,910 hrs · 23,872 cycles

R1 DOOR EVACUATION SLIDE, ARMED & DISARMED, HANDLE JAMMED. WILL NOT DISARM SLIDE. CLEANED DEBRIS OUT OF GIRT BAR FLOOR FITTINGS & LUBED IAW MM 25-66-01-4. OPS CHECKED NORMAL IAW MM. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 677 hrs · 23,727 cycles

ON LANDING NOTICED SLIDE LIGHT LEFT ENTRY DOOR INOPERATIVE. RELAMPED THE L1 DOOR SLIDE LIGHT IAW SMP. OPERATIONS CHECKED DOOR SYS IAW AMM 25-66-01-6. OPERATIONS CHECKED NORMAL. OK FOR SERVICE.

Part: LIGHT — UNKNOWN (COCKPIT) · airframe 674 hrs · 23,509 cycles

DURING TESTING OF EMERGENCY EXIT LIGHTS FOUND THE FLIGHT DECK DOME & EMERGENCY LIGHT INOPERATIVE. OPERATIONS CHECKED COCKPIT EMER LIGHTING IAW MM CHAPT 33-51-00-5. TESTED SYS 6 TIMES WITH NO DISCREPANCIES NOTED.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 66,842 hrs · 23,128 cycles

NUMBER 2 PYLON THE MOST AFT SECTION OTBD SIDE SKATE ANGLE TO WING ATTACHED IS CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,842 hrs · 23,128 cycles

MAIN CABIN COURIER AREA RT SEAT TRACK IS CORRODED. SEAT TRACK IN COURIER AREA RT SIDE FOUND TO HAVE 100% MAT LOSS AND IS OUT OF LIMITS IAW B757 SRM 53-00-52 FIG 101. REMOVED SEAT TRACK IAW VA DWG 3470 REV D & B757 SRM 51-40-02. FAB NEW SEAT TRACK IAW VA DWG 3470 REV D & B757 SRM51-40-05 & 51-40-08 AND DWG VA 3540-NC-2 SHEET 2. ALODINED & PRIMED NEW SEAT TRACK IAW B757 SRM 51-20-01. TOP COATED NEW SEAT TRACK IAW B757 AMM 51-21-10-7. INSTALLED NEW SEAT TRACK IAW DWG VA 3504-NC-2 AND DWG # 3470 REV D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,842 hrs · 23,128 cycles

MAIN CABIN COURIER AREA SEAT TRACK CORRODED LT SIDE. FABRICATED NEW SEAT TRACK AT MAIN CABIN COURIER AREA LT SIDE IAW BOEING DWG VA3470 REV D AND B757 SRM 51-40-02, INSTALLED NEW SEAT TRACK

Part: SKIN — DENTED (FUSELAGE) · airframe 66,842 hrs · 23,128 cycles

RIGHT SIDE OF FUSELAGE HAS A DENT WITH A CREASE IN IT AT BS 1673 JUST BELOW STRINGER 20R. COMPLIED WITH EA F-5330-T0313400 REV NR PS P1 FUSELAGE - PLATES & SKINS - STA 1675 SKIN DENT JUST BELOW S20R.

Part: DOOR — CRACKED (CABIN) · airframe 66,842 hrs · 23,128 cycles

L2 DOOR UPPER HINGE CUT OUT IS CRACKED. MARKED CUT OUT DAMAGE ON L2 DOOR IAW B757 SRM 51-10-02. LOCATED, DRILLED AND INSTALLED REPAIR ANGLE P/N 143N6158-11 ON L2 DOOR IAW B757 SRM 52-10-02 REPAIR 1 AND EA F-5210-T0313620 REV A. DOORS PASSENGER/CREW L2 DOOR EXSISTING SRM REPAIR - RSC TRACKING - SUPPLEMENTAL INSPECTIONS.

Part: CLOSEOUT PANEL — CRACKED (CARGO DOOR) · airframe 66,842 hrs · 23,128 cycles

MCD LOWER FWD CLOSE OUT PANEL CRACKED. REMOVED MCD LOWER CLOSE OUT PANEL IAW SRM 51-40-02. FABRICATED NEW PANEL IAW DWG 65-49309 REV D. INSTALLED NEW PANEL IAW SRM 51-40-02 & DWG 65-49309 REV D.

Part: MODULE — MISWIRED (COCKPIT) · airframe 66,784 hrs · 23,092 cycles

DURING SVC CHECK FOUND COCKPIT EMER LIGHT INOPERATIVE. RELAMPED NO HELP. TROUBLE SHOT IAW WDM 33-51-12. FOUND NO GND PRESENT AT LIGHT ASSEMBLY. LOCATED GND LOCK GD602-DC IN OVERHEAD PANEL BETWEEN CB PANELS P 11 - 1 & P 11 - 2. HUD OHU WILL HAVE TO BE REMOVED SO P 11 - 1 CAN BE LOWERED. TROUBLE SHOT USING WDM 33-51-12 & 33-11-31. FOUND GND ON L2 OF MODULE M10549 INCORRECTLY INSTALLED. REWIRED IAW WDM CH 33-11-31. SYS OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,530 hrs · 22,918 cycles

RIGHT EMER EXIT SIGN M730 WILL NOT ILLUMINATE DURING TEST. R & R BATTERY PACK IAW MM 33-51-07-2-2. OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: SKIN — PUNCTURED (NR 3 SLAT) · airframe 65,431 hrs · 22,121 cycles

NR 3 SLAT L/E LOWER SIDE PUNCTURED 2 FT FROM INBD EDGE. FOUND DAMAGE TO BE OUT OF LIMITS PER SRM 57-43-01 FIG 101. REPAIRED IAW SRM 57-43-01 FIG 201 REPAOR 1. CATEGORY A MAJOR REPAIR.

Part: SKIN — CORRODED (NR 10 SLAT) · airframe 65,431 hrs · 22,121 cycles

NR 10 SLAT HAS SPOT AREAS OF CORROSIONS ON THE T/E WEDGE UPPER SURFACE. REPAIRED NR 10 SLAT T/E WEDGE UPPER SURFACE IAW-SRM-51-70-10, REP NR 2.

Part: FRAME — CHAFED (ZONE 100) · airframe 65,431 hrs · 22,121 cycles

BS 418.00 FRAME HAS DEEP CHAFE, BETWEEN S20-21R. ACCOMPLISHED EA F-5310-162460. REMOVED CHAFE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101. MAJOR REPAIR.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 65,431 hrs · 22,121 cycles

RT WING, INBD FLAP UPPER SURFACE, OTBD OF WS 313, HAS A DENT. REPAIRED FLAP UPPER SURFACE IAW-SRM-51-70-10, CAT."A" MAJOR REPAIR,

Part: SKIN — DENTED (BS 520-540) · airframe 65,431 hrs · 22,121 cycles

BETWEEN BS 520 & 540 AT STR 26 & 27L, A DENT IN FUSELAGE SKIN. REPAIRED IAW EA 757-5331-16-F3986, REV -.

Part: BEAM — CRACKED (R4 DOOR) · airframe 65,431 hrs · 22,121 cycles

R-4 DOOR INNER SKIN, EDGE OF LIGHTING HOLE, NR 4 BEAM, CRACKED. REPAIRED IAW EA F-5210-162564. MAJOR REPAIR.

Part: RIB — CORRODED (ZONE 600) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

RT WING AFT SPAR AT WSTA 815 BONDING JUMPER ATTACHMENT TO RIB CORRODED. REMOVED CORROSION AT GROUNDING POINT. FOUND TO BE OUT OF LIMITS IAW SRM 57-51-09, FIG 101 DET VI. RIB FABRICATED & INSTALLED IAW DWG 113N1511. MAJOR REPAIR.

Part: FRAME — CRACKED (BS 760 S9L) · airframe 65,431 hrs · 22,121 cycles

FRAME BS 760 S9L RIVET HAS SET MARK AND AT STRINGER 10L-11L THERE IS A TRAPPED HOLE. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3. MAJOR REPAIR.

Part: WEDGE — DAMAGED (NR 4 SLAT) · airframe 65,431 hrs · 22,121 cycles

NR 4 SLAT WEDGE EDGE, CHIPPED OFF, .5" X .0625", WS 344.0. REPAIRED NR 4 SLAT WEDGE EDGE IAW SRM 51-70-10, REPAIR NR 4. MAJOR REPAIR.

Part: BULKHEAD — CHAFED (ZONE 400) · airframe 65,431 hrs · 22,121 cycles

LEFT STRUT BULKHEAD, LT LWR SIDE, CHAFED ACCOMPLISHED IAW EA F-5450-162447, FOUND OUT OF LIMITS IAW SRM 54-51-02 FIG 101 DET VII.THIS IS A CATEGORY A, MAJOR REPAIR.

Part: FRAME — CORRODED (BS 760) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

FWD CARGO LT SIDE AT BS 760 BETWEEN STR 23-25L CORROSION ON FRAME. REMOVED CORROSION ON FRAME BETWEEN STR 23 & STR 25 AT STA 760 LT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II. REMOVED FRAME AT STA 760 LT STR 13 TO STR 26. REPLACED FRAME IAW DWG 143N1018. THIS IS A CATEGORY A, MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1260) · airframe 65,431 hrs · 22,121 cycles

FRAME BS 1260 S4L- 4R HAS DOUBLE DRILLED AND ELONGATED HOLES. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3.

Part: FRAME — DAMAGED (BS 1520) · airframe 65,431 hrs · 22,121 cycles

FRAME BS 1520 BETWEEN S4L-S4R HAS DOUBLE DRILLED AND ELONGATED FASTENER HOLES AT BS 1520, FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3.

Part: FRAME — DAMAGED (BS 1560) · airframe 65,431 hrs · 22,121 cycles

FRAME STA 1560, BETWEEN S5L AND S5R HAS DOUBLE DRILLED AND ELONGATED FASTENER HOLES. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3. MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1540) · airframe 65,431 hrs · 22,121 cycles

FRAME BS 1540, S3R -S6L, HAS DOUBLE DRILLED AND ELONGATED FASTENER HOLES. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 3. MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 418) · airframe 65,431 hrs · 22,121 cycles

BS 418, FRAME BETWEEN STR 5L AND STR 4R DAMAGED. FRAME REPAIRED IAW EA 757-5312-16-F3926, REV, MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1620) · airframe 65,431 hrs · 22,121 cycles

FRAME BS 1620, S5L TO S5R HAS DOUBLE DRILLED AND ELONGATED FASTENER HOLES. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, SHEET 2, DETAIL 1, REPAIR 3. MAJOR REPAIR.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

LEFT WING UPPER SKIN UPPER SURFACE CORRODED. FOUND TO BE OUT OF LIMITS, WITHIN 1.5 IN. OF ANY CHORD WISE ROW OF FASTNERS IAW SRM 57-20-01, FIG 101, NOTE "A". THIS REPAIR IS A CATEGORY A , MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 760) · airframe 65,431 hrs · 22,121 cycles

FUSELAGE FRAME AT BS 760, STR 24-26R, MISREPAIRED. REPLACED FRAME PER DRAWING 143N1018. THIS REPAIR IS A CATEGORY A, MAJOR.

Part: FLOOR SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

COCKPIT FLOOR SKIN AT BS 239 - 247, RBL 34 HAS SCRATCHES AND CORROSION. REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

FLT DECK FLOOR SKIN FROM BS 225 TO 231, RBL 36 - 40, HAS CORROSION. REPAIRED AREA IAW EA 5310-162556. REPAIR IS CLASSIFIED AS A MAJOR.

Part: FLOOR SKIN — CORRODED (COCKPIT) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

COCKPIT FLOOR SKIN AT BS 239-247, LBL30-40 CORRODED. REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.

Part: STRUCTURE — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

DURING REMOVAL OF CAPTAINS LT FOOT HEATER PANEL FOUND AREAS OF CORROSION BS 205 TO 231, LBL-24. REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.

Part: FLOOR SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

DURING REMOVAL OF CAPTAIN'S RT FOOT HEATER PANEL FOUND AREAS OF CORROSION BS 205 TO 231 LBL-15. REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.

Part: FITTING — DAMAGED (RT WING) · airframe 65,431 hrs · 22,121 cycles

RIGHT WING, SIDE LINK FITTING HOLE "H" FOUND TO BE OVERSIZED. REPAIRED IAW EA F5740-162444. MAJOR REPAIR.

Part: FLOOR SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

DURING REMOVAL OF CAPTIAN'S RT SEAT TRACK FOUND AREA OF CORROSION BS 245 TO 255 LBL 17 REPAIRED AREA IAW EA 5310-162556. CLASSIFIED AS A MAJOR REPAIR.

Part: CARGO TRACK — CORRODED (BS 680-780) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

MAIN DECK CARGO TRACK AT STA 680 -780, LBL 24 HAS GOUGES AND CORROSIONS. REMOVED CORROSION IAW SRM 51-10-02. CHECKED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 DETAIL I FIG 101, PG 102. R & R CARGO TRACK AT LBL24.75 STA 680-780 IAW SRM 51-40-02 AND DWG 143N5090. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 660-680) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

RT INBD CREASE BEAM CORRODED UPPER & LOWER SURFACE, BS 660-680. REMOVED CREASEBEAM BS 660-755, IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 51-10-02. CHECKED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DET. III. REPLACED CREASE BEAM IAW SRM 51-40-02 AND DRAWING 143N8324. THIS REPAIR IS A CATEGORY A MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1520) · airframe 65,431 hrs · 22,121 cycles

FRAME, BS 1520, BETWEEN STRINGERS 4L -4R, HAS SEVERAL ELONGATED AND DOUBLE DRILLED HOLES. REPAIR ACCOMPLISHED IAW SRM 53-00-07, FIG 201, REPAIR 3. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1600-1640) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

MAIN CABIN AREA BETWEEN BS 1600 -1640 CREASE BEAM CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 101 SH 3 DETAIL III. REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 146N5590. FABRICATED IAW BOEING DRAWING 146N5590 AND SRM 51-40-05. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — MISMANUFACTURED (BS 660) · airframe 65,431 hrs · 22,121 cycles

MAIN DECK FLOORBEAM BS 660 CAME SHORT AT LT END TO PICK UP CREASE BEAM OTBD CHORD FASTENER HOLE. REMOVED SHORT FLOORBEAM IAW SRM 51-40-02 & DWG 143N5012 SH 19. FABRICATED NEW FLOORBEAM IAW DWG 146N5012, SH 19, INSTALLED NEW FLOORBEAM IAW SRM 51-40-02 & DWG 143N5430, PAGE 23 AT STA. 660. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CHAFED (BS 400-900) · airframe 65,431 hrs · 22,121 cycles

SEAT TRACK HAS CHAFE MARKS AND PAINT CHIPPED FROM BS 400 - 900, LBL 45. REMOVED CHAFE MARKS, MAX CLEAN UP DEPTH .040" ALLOWED. CHAFFED AT .060", OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL IV. FABRICATED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND DRAWING 143N5060-6. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

LT WING AILERON OTBD BONDING WIRE ATTACHMENT, HINGE BRACKET RIB CORRODED. REMOVED AND REPLACED RIB ASSY, WS 817.27, IAW SRM 51-40-02 AND DWG 113N1501 DUE TO OUT OF LIMITS PER SRM 57-51-09, FIG 101, DETAIL IV. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 630-640) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

RBL 25.0 SEAT TRACK CORRODED BS 630 - 640. REMOVED CORROSION, MAX CLEANUP DEPTH IN BOTTOM OF TRACK .040", REMOVED .090" OF MATERIAL, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1, PAGE 102. REMOVED AND REPLACED SEAT TRACK, RBL 25, BS 440-640, PER DWG 143N5090-6, AND SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 646-665) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

RT INB CREASE BEAM CORRODED AT BS 646-665. REMOVED DAMAGED CREASEBEAM AND FABRICATED AND INSTALLED NEW CREASEBEAM, IAW DRAWING 143N5520 AND SRM 51-40-02, RT I/B CREASEBEAM, BS 450-665. REMOVED CORROSION IAW SRM 53-30-13, FIG. 101, DETAIL III; ORIGINAL MATERIAL: .070, AFTER REWORK: .038", FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG. 101, DETAIL III. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

FLOORBEAM UPPER TEE CORRODED, BS 324, LBL 20. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-10-08 FIG 101 DETAIL IX. REMOVED AND REPLACED FLOORBEAM UPPER TEE IAW SRM 51-40-02 AND DRAWING 141N2930. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — GOUGED (BS 1180-1320) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

MAIN CARGO DECK SEAT TRACK AT BS 1180-1320, LBL 24.75 HAS AREAS WITH GOUGES, CORROSION AND DAMAGED DOME NUTS. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I SHEET 2 OF 6. FABRICATED NEW SEAT TRACK IAW SRM 53-60-52 FIG 1 SH 2 OF 5 AND DWG 146N5120. INSTALLED NEW SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5120. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 665-690) · airframe 65,431 hrs · 22,121 cycles

MAIN CARGO DECK LEFT INBD CREASE BEAM AND ANGLE BS 665-690 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, DETAIL III. R & R LT INBD CREASEBEAM IAW SRM 51-40-02 AND DWG 143N8324. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 744) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

RT INBD CREASE BEAM CORRODED, BS 774. FOUND TO BE OUT OF LIMITS AT BS 774 RBL 70 IAW SRM 53-30-13 DETAIL VIII FIG.101 PG.105. REMOVED AND REPLACED CREASE BEAM AT BS 760-900 RBL 70 IAW SRM 51-40-02 AND DRAWING 143N5520.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 65,431 hrs · 22,121 cycles

FLOORBEAM UPPER TEE CORRODED, BS 344, BL 0 - LBL 25.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 65,431 hrs · 22,121 cycles

FLOORBEAM UPPER TEE CORRODED, BS 344, BL 0 - LBL 25. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS AFTER REWORK FOUND FLOORBEAM UPPER TEE OUT OF LIMITS IAW SRM 53-00-510 DETAIL III. R & R FLOORBEAM TEE IAW SRM 51-40-02, AND REPAIR 3 OF SRM 53-00-51. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

FLOORBEAM UPPER CHORD BS 365, RBL52, CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 SH 4 DETAIL III. REPAIRED FLOORBEAM LBL 15.5 TO RBL 70 IAW SRM 53-00-51 FIG 201 SH 1-6 REPAIR 3. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 600-640) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

RBL 45.0, SEAT TRACK CORRODED BS 600 - 640. FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. REPLACED SEAT TRACK IAW SRM 51-40-02, DWG 143N5149 AND DWG 143N5080. REPAIR CLASSIFIED AS MAJOR.

Part: STIFFENER — CORRODED (BS 1600 S16-17L) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

MAIN DECK CARGO FRAME STIFFENER AT BS 1600, STR 16L-17L, HAS CORROSION. REMOVED CORROSION, ORIGINIAL THICKNESS .100, REMAINING THICKNESS .080, MATERIAL LOST .020. FOUND OUT OF LIMITS IAW SRM 53-00-07 FIG 101, SH3 DETAIL I AND II AND SRM 51-10-02. REMOVED DAMAGE FRAME STIFFENER IAW SRM 51-40-02. LOCATED AND INSTALLED NEW PART IAW SRM 51-40-02 AND DWG 146N1021. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 377.7) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

FLOORBEAM UPPER TEE CORRODED BS 377.7, LBL 45 - 60. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. REPAIRED UPPER TEE FROM LBL 70 TO RBL 35.75, BS 377.7, IAW SRM 53-00-51, REPAIR 3. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

CABIN FLOORBEAM BS 1640 HAS CORROSION ON UPPER ANGLE. UPPER AND LOWER SURFACES FROM LBL 58 TO RBL 58. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG. 101, DETAIL III. REMOVED, FABRICATED AND INSTALLED NEW FLOORBEAM IAW SRM 51-40-02 AND DRAWING 146N5089. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

MAIN DECK FLOORBEAM BS 1681, LBL 58 TO RBL 58, UPPER TEE HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL III. REMOVED, FABRICATED AND INSTALLED NEW FLOORBEAM IAW SRM 51-40-02 AND DWG 146N5091. MAJOR REPAIR

Part: CREASE BEAM — CORRODED (BS 1040-1180) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

LEFT INBD CREASE BEAM CORRODED BS 1045 - 1080. REMOVED CORROSION ORIG .080 REMAINING .005 FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13, DETAIL VIII. R & R CREASE BEAM IAW SRM 51-40-02, SRM 51-10-02 AND DWG REF 14N5200. MAJOR REPAIR.

Part: DECK PLATE — CORRODED (BS 1710-1720) · airframe 65,431 hrs · 22,121 cycles

AFT DECK PLATE FROM BS 1710 TO 1720, RBL 56 TO LBL 56 HAS CORROSION AND EXFOLIATED SURFACES. AFT DECK PLATE FROM STA 1710 TO STA 1720, RBL 56 TO LBL 56 HAS CORROSION AND EXFOLIATION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III SH 4. REMOVED PRESSURE DECK IAW SRM 51-40-02. FABRICATED NEW AFT DECK PLATE IAW DWG 146N5318. INSTALLED NEW AFT DECK PLATE IAW SRM 51-40-02 AND DWG 146N5318. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1370-1625) · airframe 65,431 hrs · 22,121 cycles

MAIN DECK CARGO LEFT INBD CREASE BEAM AT BS 1625-1370 HAS AREAS OF SCRATCHES AND CORROSION. CORROSION REMOVED IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 DETAIL VIII, FIG.101 SH5. REMOVED AND REPLACED CREASE BEAM IAW SRM 51-40-02 AND DWG 146N5590.

Part: FLOORBEAM — CORRODED (BS 1661) · airframe 65,431 hrs · 22,121 cycles

FLOORBEAM UPPER TEE BS 1661 HAS CORROSION LBL 58 TO RBL 58. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL II. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02 AND DWG 146N5090. FABRACATED FLOORBEAM IAW DWG 146N5090. REPAIR CLASSIFIED AS A MAJOR.

Part: FLOORBEAM — CORRODED (BS 700) · airframe 65,431 hrs · 22,121 cycles

MAIN CARGO DECK FLOORBEAM UPPER TEE AT BS 700 HAS SCATCHED AND CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III, PG 104. FABRICATED & REPLACED FLOORBEAM IAW SRM 51-40-02 & DWG 143N5064-2.

Part: FLOORBEAM — CORRODED (BS 720) · corrosion level 2 · airframe 65,431 hrs · 22,121 cycles

MAIN CARGO DECK FLOORBEAM UPPER TEE AT BS 720 HAS AREAS WITH SCATCHES AND CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM53-00-51, FIG.101 DETAIL III PG.104. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02.MAJOR REPAIR