N971FD

Part: ACTUATOR — FAILED (SLAT SYS) · airframe 52,492 hrs · 18,496 cycles

SELECTED FLAPS 1 AT 5500 FEET AND ABOUT 200 KNOTS. RECEIVED LE SLAT DISAGREE EICAS MESSAGE. COMPLIED WITH QRH. MESSAGE REMAINED. QRH DIRECTED US TO RUN LE SLAT ASYMMETRY QRH. COMPLIED WITH QRH. DECLARED EMERGENCY AND LANDED WITH TE FLAPS AT 20 WITH NO FURTHER ISSUES. REPLACED #7 LE SLAT ROTARY ACTUATOR. ORIG SUB DATE: 11/20/2022

Part: IDG — FAILED (NR 1 GENERATOR) · airframe 52,299 hrs · 18,363 cycles

DURING CLIMB OUT AT 600 FEET L GEN OFF ILLUMINATED. RAN QRH AND ABLE TO RESET L GEN. STARTED APU FOR BACKUP AND APU RAN FOR ABOUT 5 MINUTES AND GOT AN APU FAULT EICAS AND APU SHUTDOWN. DURING DESCENT L GEN OFF EICAS ILLUMINATED AGAIN. QRH ONLY ALLOWS ONE RESET PER FLIGHT. DECLARED EMERGENCY AND LANDED AT DESTINATION. DECIDED TO TRY APU AGAIN SINCE FAULT LIGHT EXTINGUISHED BUT APU ONLY RAN FOR 3 MINUTES AND FAILED AGAIN. REMOVED AND REPLACED L/H ENGNE IDG USING B757 MM 24-11-01-4, LEAK CHECK GOOD, OPS CHECKED GOOD.

Part: FSEU — FAILED (SLAT/FLAPS) · airframe 50,988 hrs · 17,577 cycles

ON ILS 11 KPWM GOT LE SLAT DISAG AUDIBLE WARNING, BUT NO EICAS MESSAGE DISPLAYED. WHEN FLAPS POSITIONED TO FLAPS 15 THEN RECEIVED EICAS MESSAGE LE SLAT DISAG. NO SPLIT FLAP NEEDLES ON FLAP INDICATOR. FLAPS STOPPED MOVEMENT HYDRAULICALLY AT FLAPS 1. COMPLIED WITH QRH AND LANDED NEVENTFULLY RWY 11. EMER DECLARED (WRI WAS UPDATED BY MOC AFTER TALKING TO CAPT) FACT 27APR21 17:37 PWM U T/S PER 27-51 FAULT TREES 805 AND 803. FSEC #1 FAULTED CODE 310 AND FSEC #2 AULTED CODE 331. ( SLAT DISAGREE MESSAGE). REMOVED AND REPLACED #1 FSEC PER M.M. 27-51- 01-2. OPS CKS GOOD. A/C OK FOR SERVICE.

Part: SENSOR — BINDING (R1 DOOR) · airframe 50,772 hrs · 17,447 cycles

R1 DOOR LEVER PHYSICALLY MOVED ABOVE THE PANEL THAT COMES OUT WHEN THE DOOR IS CLOSED, UPON LANDING BLOCK IN MESSAGE/SUMMARY CAME UP BEFORE LEAVING THE RUNWAY. FAULT SEEMS TO OCCUR DURING CLIMBOUT AND PRESSURIZATION. RMVD SLIDE COVER AND INSPECTED FOR POSSIBLE SLIDE/LANYARD INTERFERENCE AND BINDING, NO FINDINGS. INSPECTED DOOR LATCH CAMS, FITTINGS AND MECHANISMS FOR WEAR AND SECURITY, NO FINDINGS, EVERYTHING WAS SECURE AND OPS NML. DOOR WAS FLUSH AND FAIRED WHEN CLOSED. PERF PUSH PULL TEST FOR DOOR CLOSING/OPENING AND WAS WITHIN LIMITS. REF AMM 52-11-00-6. WHEN COMPARING TO L1, FOUND THE DOOR SENSOR PLUNGER PROTRUDING MORE THAN L1 WITH THE PLUNGER BOTTOMED OUT. PUT A CRUSH INDICATOR IN R1 SENSOR, CLOSED DOOR AND IT FLATTENED. SUSPECT POSSIBLE BINDING BETWEEN LATCH CAM AND DOOR SENSOR CAUSING DOOR HANDLE TO MIGRATE DURING PRESSURIZATION. ADJ R1 DOOR SNSR, OPS NML - REF AMM 52-71-00-5.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 50,724 hrs · 17,417 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL 222BF DELAMINATED. FABRICATED MAIN CABIN FWD WET AREA FLOOR PANEL 222BF, IAW B757 AMM 53-01-01-7 AND FEDEX DWG SRZ-25-005.

Part: PANEL — CRACKED (RT WING) · airframe 50,724 hrs · 17,417 cycles

RT WING NR 10 SLAT LOWER COVE PANEL HAS EVIDENCE OF CRACK ON INBOARD SIDE OF OUTBOARD MAIN TRACK. REPAIRED RT WING NR 10 SLAT LOWER COVE PANEL ON INBOARD SIDE OF OUTBOARD MAIN TRACK, IAW B757 SRM 57-43-01-2R REP 4.

Part: PANEL — CRACKED (RT WING) · airframe 50,724 hrs · 17,417 cycles

RT WING NR 10 SLAT LOWER COVE PANEL HAS EVIDENCE OF CRACK ON OUTBOARD SIDE OF OUTBOARD MAIN TRACK. REPAIRED RT WING NR 10 SLAT LOWER COVE PANEL ON OUTBOARD SIDE OF OUTBOARD MAIN TRACK, IAW B757 SRM 57-43-01-2R REP 4.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,724 hrs · 17,417 cycles

MAIN CABIN FLOOR CREASE BEAM STA 876 RT SIDE CORRODED. REMOVED CORROSION ON CREASE BEAM STA 876 RT SIDE, IAW B757 SRM 51-10-02. ORIG MAT .071 REM .046 LOSS .025 FOUND OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG 101. REPAIRED CREASE BEAM, IAW B757 SRM 53-00-13-2R REP 1 ALT 1.

Part: FLOOR SUPPORT — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 50,724 hrs · 17,417 cycles

MAIN CARGO FLOOR SUPPORT CHANNEL HAS CORROSION AT RBL-58 BETWEEN STA 324 AND STA 345. REMOVED CORROSION ON SUPPORT CHANNEL STA 324 AND STA 345 RBL 58, IAW B757 SRM 51-10-02. ORIG MAT .050 LOSS .040 REM .010 OUT OF LIMITS, IAW B757 SRM 5300-51-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT CHANNEL, IAW B757 SRM 51-40-02, 51-40-05, 51-30-01 AND BOEING DWG 141N5160 REV CD.

Part: WEB — CORRODED (CABIN) · corrosion level 2 · airframe 50,724 hrs · 17,417 cycles

MAIN CABIN FLOOR SUPPORT WEB HAS MULTIPLE AREAS OF CORROSION AT LBL 58 BETWEEN STA 1635 AND STA 1681. REMOVED CORR ON WEB LBL 58 STA 1635-1681, IAW B757 SRM 51-10-02. ORIG MAT .056 REM .028 LOSS .028 FOUND OUT OF LIMITS, IAW B757 SRM 53-60-15-1A FIG 101. REMOVED, FABRICATED AND INSTALLED NEW WEB IAW B757 SRM 51-40-02, 51-40-05 53-60-15-01 AND BOEING DWG 146N8722 REV BK.

Part: PANEL — DENTED (CARGO DOOR) · airframe 50,724 hrs · 17,417 cycles

MAIN CARGO DOOR AFT PRESSURE DOOR INTERNAL PROTRUDING DENTS AT THE WEB. REMOVED, FABRICATED, AND INSTALLED NEW AFT PANEL (WEB) ON MAIN CARGO, IAW B757 SRM 51-40-02 51-30-01, 51-40-05 AND BOEING DWG 65-49309 REV D. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS, IAW B757 SRM 52-30-02-1A FIG 101. APPLIED CIC, IAW FEDEX DGW B57-51-001 REV F. OPERATIONS CHECK GOOD, IAW B757 AMM 52-32-00-0 ON N00476.

Part: PANEL — CRACKED (CARGO DOOR) · airframe 50,724 hrs · 17,417 cycles

MAIN CARGO DOOR FWD PRESSURE DOOR INTERNAL DAMAGED (CRACK) AT THE WEB. REMOVED, FABRICATED AND INSTALLED NEW FWD PANEL (WEB) ON MAIN CARGO DOOR, IAW B757 SRM 51-40-02, 51-30-01, 51-40-05 AND BOEING DWG 65-49309 REV D. APPLIED CIC IAW FEDEX DWG B57-50-001 REV F, OPERATIONS CHECK GOOD, IAW B757 AMM 52-32-00-0 ON N00475.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 50,724 hrs · 17,417 cycles

MAIN CABIN SEAT TRACK FLANGE HAS COORSION @ RBL-57 BETWEEN STA. 1180 AND STA. 1300 REMOVED CORR ON SEAT TRACK STA 1180-1300 RBL58 IAW B757 SRM 51-10-02 ORIG MAT .090 REM .057 LOSS .037 OUT OF LIMITS IAW BAC 1520-792 BOEING DWG. REPAIR SEAT TRACK IAW B757 SRM 53-00-52-2R REP 3 OPT. 2 AND FEDEX EAF-5310-T0358955 P1 FUSELAGE - MAINFRAME - RBL58 SEAT TRACK REPAIR BETWEEN STA 1200-1220 - SRM REPAIR DEVIATION FOR ALTERNATE FINISH

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 49,954 hrs · 16,968 cycles

PDIS 971 27-30 6467 ON CLIMB IN CLEAR CONFIGURATION RECIVED EICAS MSG RUDDER RATIO AND MACH / SDD TRIM (AND OVERHEAD LT) ALONG WITH ELEV ASYM ON STATUS PAGE, NO AUTO PILOT, RAN QRH, NO HELP, CONTACTED GOC & COORDINATED RETURN TO SERVICE PERFORMED RESET OF BOTH LEFT AND RIGHT SAMS SYST IAW AMM 27-09-00-38-09, VERIFIED NO ADDICIONAL FAULTS FOUND, A/C OK FOR SERVICE

Part: COVER — UNSECURE (DOOR SLIDE) · airframe 49,627 hrs · 16,752 cycles

NOTICED LEFT FORWARD ENTRYDOOR WAS BINDING. HAD MAINTENANCE OPEN DOOR FROM THE OUTSIDE. KMEM WHILE PERFORMING INSPECTION CHECK IN REF. TO AMM 52-11-01-6. FOUND COVER TO SLIDE NOT SECURE BINDING. RESECURED COVER IN REF. TO AMM 25-66-01-4. FOUND L1 DOOR ASSIST BOTTLE OUT OF LIMITS. REMOVED AND REPLACED L1 DOOR ASSIST BOTTLE IN REF. TO AMM 52-11-30-4. OK FOR SERVICE (MFG HR-TEXTRON)

Part: PROBE — OBSTRUCTED (EGT) · airframe 49,522 hrs · 16,681 cycles

PDIS 971 77-00 6015 12SEP19 RIC OPEN U LOGPAGES:3180701 CONTINUED FROM LOG PAGE 2966550, CONTINUED OPERATION OF RT ENG AT IDLE TO LANDING. FIRST INDICATION OF PROBLEM WAS 1 SEC AMBER EGT INDICATION ON RT ENG PRIOR TO THRUST REDUCTION. NO OTHER ACCOMPANYING EICAS ALERTS OR ENG EXCEEDANCE. SEE WRI 77-00 6014. FACT 12SEP19 05:37 RIC UPON INSPECTION OF THE #2 ENGINE P1 PROBE, FOUND EVIDENCE OF INSECT OBSTRUCTING P1 PROBE, REMOVED OBSTRUCTION WITH NITOGEN INSECT REMAINS CAUGHT IN PAPER TOWEL. RAN ENGINE AT POWER SETTING ALL ENGINE PARAMETERS NORMAL, ALSO PERFORMED BITE ON #2 EEC FAULT CODES 43 AND 47 DISPLAYED ALL WORK ACCOMPLISHED IAW FIM 73-21-00-3 AND 757 JRH. ACFT OK FOR SERVICE. SEE WRI 77-00/6014 FOR MORE INFO.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 49,457 hrs · 16,633 cycles

ON TAKEOFF ROLL,WHEN ENGINES WERE SET TO TAKEOFF THRUST AND ABOUT 30 KNOT AIRSPEED RECEIVED A SPOILER EICAS WITH CORRESPONDING MASTER WARNING LIGHTS AND TONE. REJECTED TAKEOFF IAW QRH. UNABLE TO DUPLICATE THE ABOVE DISCREPENCY IAW FIM 27-61-00-815-802. NOTE FOUND NO CURRENT OR HISTORY FAULTS FROM SPOILER CONTROL MODULE (SCM) OR POWER CONTROL ACTUATOR (PCA) PER MANUAL NO FAULTS NOTED. SYSTEM IS OK. OPERATED SPOILER SYSTEM SEVERAL TIMES NO FAULTS RECORDED.

Part: SWITCH — FAILED (SLAT SYSTEM) · airframe 47,970 hrs · 15,747 cycles

DURING FINAL APPROACH, RECEIVED A LEADING EDGE SLAT ASSYMETRY EICAS AND ASSOCIATED CUE LIGHT. RAN QRH PROCEDURES, FLAPS 20 LANDING. LANDING NORMAL. R & R THE RT LOSS SENSING SWITCH FOR THE L/E SLATS IAW MM 27-81-41-4. PREFORMED A TEST OF THE RT LOSS SENSING SWITCH. OPS CHECKED NORMAL IAW MM 27-81-41-5.

Part: SEAT TRACK — DAMAGED (BS 614-620) · airframe 47,726 hrs · 15,584 cycles

FOUND A BROKEN LOCK AT POS 3 MAIN DECK CENTER LINE. LOCK D611. FOUND DAMGED SEAT TRACK AT SAME LOCATION. COMPLIED WITH EA F-5320-T0336761 PART 1. REPAIRED THE SEAT TRACK BS 614 - 620, BL 0.

Part: TRANSMITTER — OUT OF ADJUST (TE FLAP) · airframe 47,551 hrs · 15,452 cycles

RECEIVED EICAS MSG "TE FLAP ASYM" RAN QRH LANDED WITH MAX AUTO BRAKES LANDING WEIGHT 167.0LB. R&R LT TE FLAP POSITION XMITTER PER MM 27-58-03-4 AND PERFORM ADJ/TEST PER MM 27-58-01-5. TE FLAP INDICATION SYS OP'S CK. GOOD OK FOR SERVICE.

Part: GIRT BAR — INOPERATIVE (R1 DOOR) · airframe 47,034 hrs · 15,166 cycles

R1 DOOR SLIDE ARM LIGHT WOULD NOT ARM. REMOVED AND REPLACED R1 GIRT BAR IAW MM 25-66-10-2. SLIDE ARM LIGHT OPS CHECKED GOOD. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: INDICATOR — READS LOW (R1 DOOR) · airframe 46,626 hrs · 14,897 cycles

PRESSURE REGULATOR GAUGE ON R1 DOOR SHOWS RED. R & R THE R1 DOOR SLIDE IAW MM 25-66-01-4.

Part: VALVE — LEAKING (HYDRAULIC SYS) · airframe 457 hrs · 14,327 cycles

LEFT HYD SYS LEAK & LOW FLUID FAILURE. SEVERAL ASSOCIATED EICAS & STATUS MSGS. LT HYD QTY WENT TO .12, FOLLOWED BY A LT QTY LOW EICAS MSG, LT RESERVOIR PSI LIGHT, SHUT PUMPS OFF UNTIL LANDING. ADDED 4 GALLONS TO LT HYD RESERVOIR, PRESSURIZED LT SYS, ISOLATED LEAK TO FWD STAB AREA AROUND THE ELEVATOR PRESSURE REDUCER & BYPASS VLVS IAW AMM 27-31-13-4. FOUND VALVE HYD PRESSURE REDUCER LEAKING. R & R ELEVATOR BYPASS VALVE, LEAK CHECKED GOOD.

Part: BYPASS VALVE — LEAKING (HYD SYSTEM) · airframe 457 hrs · 14,327 cycles

LEFT HYD SYS LEAK & LOW FLUID FAILURE. SEVERAL ASSOCIATED EICAS & STATUS MESSAGES. LT HYD QTY WENT TO .12, FOLLOWED BY A LT QTY LOW EICAS MESSAGE, LT RESERVOIR PSI LIGHT, SHUT PUMPS OFF UNTIL LANDING. EMERGENCY DECLARED, FOUND VALVE HYD PRESSURE REDUCER, RUDDER ELEVATOR LEAKING. R & R ELEVATOR PRESS BYPASS VALVE IAW AMM 27-31-13-4. LEAK & OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 456 hrs · 14,266 cycles

R1 DOOR EXTERNAL EMER LIGHT INOPERATIVE. RELAMPED R1 SLIDE LIGHT & CHECKED OK IAW AMM 33-51-06-2-1.

Part: LATCH — LOOSE (ESCAPE ROPE) · airframe 455 hrs · 14,193 cycles

ESCAPE ROPE COVER ON CAPTAINS SIDE DOES NOT STAY LATCHED. BOTTOM LATCH LOOSE. SECURED BOTTOM LATCH ON CAPTAINS SIDE ESCAPE ROPE COVER & CLOSED PANEL.

Part: PANEL — CRACKED (CARGO DOOR) · airframe 45,012 hrs · 13,886 cycles

MAIN DECK CARGO DOOR AFT PRESS RELIEF DOOR COVE PANEL IS CRACKED.

Part: SHEAR WEB — CORRODED (BS 420) · corrosion level 2 · airframe 45,012 hrs · 13,886 cycles

MAIN DECK SHEAR WEB HAS CORROSION AT RBL 25 BS 420. REMOVED CORROSION, FABRICATED, LOCATED, DRILLED & INSTALLED THE DOUBLER IAW SRM 51-40-02 & SRM 5 4 3.

Part: SHEAR WEB — CORRODED (BS 420) · corrosion level 2 · airframe 45,012 hrs · 13,886 cycles

MAIN DECK SHEAR WEB HAS CORROSION AT LBL 25 BS 420. REMOVED CORROSION, FABRICATED DOUBLER, LOCATED, DRILLED & INSTALLED THE DOUBLERIAW SRM 51-40-02 & SRM 5 4 3.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 45,012 hrs · 13,886 cycles

MAIN CARGO DOOR INNER SKIN CRACKED. FABRICATED & INSTALLED NEW ACCESS PANEL ON MAIN CARGO DOOR INNER SKIN BS 500 - 520 IAW SRM 51-40-02 & DWG 65-49309 REV D.

Part: FIRE WARNING — FALSE INDICATION (COCKPIT) · airframe 44,419 hrs · 13,505 cycles

MOMENTARY WW FIRE EICAS ALERT & BELL ON TOUCHDOWN, LASTED 1 - 2 SECONDS, COULD NOT DUPLICATE. INSPECTED DETECTOR LOOPS & ELEC CONNECTIONS IN BOTH MLG WW, NO DEFECTS NOTED. ADJUSTMENT TEST OF WW FIRE DETECTION SYS NORMAL IAW MM 26-17-00-5.

Part: TARGET — OUT OF ADJUST (THRUST REVERSER) · airframe 44,274 hrs · 13,396 cycles

ON TAKEOFF ROLL THE RT REVERSER ECAS MESSAGE CAME INTERMITTENT REJECT AT 80 KTS. REVERSER SECURED IN FWD THRUST POSITION. FOUND THE RIGHT LOCK PROX TARGET, TOO FAR AWAY FROM SENSOR. INSTALLED SHIMS ON RIGHT LOCK PROX SENSOR, PER AMM 78-30-00-5-4. GAP IS WITHIN LIMITS ON TARGET SENSOR. OPS CHECKS GOOD. REFERENCE WRI 78-30-1168.

Part: GUARD — FAILED (EMERGENCY LIGHTS) · airframe 43,936 hrs · 13,167 cycles

THE OVERHEAD EMERGENCY LIGHT SWITCH GUARD SPRING IS WEAK AND NOT WORKING PROPERLY, MANUAL OPERATION OF THE SWITCH IS NOT EFFECTED. REMOVED BROKEN EMERGENCY LIGHT SWITCH GUARD. REPLACED WITH NEW GUARD. CHECK FUNCTION OF GUARD AND SWITCH ALONG WITH OPS CHECK OF LIGHTS. ALL OPS CHECKED GOOD. OK FOR SERVICE.

Part: CABLE — SHEARED (ESCAPE SLIDE) · airframe 43,883 hrs · 13,110 cycles

DURING OPENING OF RT SIDE ENTRY DOOR, GIRT BAR HUNG UP ON DOOR SILL, SLIDE PARTIALLY DISENGAGED AS WELL AS SAFETY CABLE SHEARED. R & R R1 DOOR SLIDE ASSY REF AMM 25-66-01. ACFT OK TO CONTINUE SERVICE.

Part: LATCH — BROKEN (ESCAPE SLIDE) · airframe 43,721 hrs · 12,995 cycles

DOOR ESCAPE SLIDE COVER LOWER STRAP LATCH BROKEN. REPLACED LATCH IAW AMM 25-66-01-4. ACFT OK FOR SERVICE.

Part: SLIDER — DISCONNECTED (GIRT BAR) · airframe 43,653 hrs · 12,943 cycles

RT FWD ENTRY DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN DOOR ARMED. INSPECTED AND FOUND R1 DOOR GIRT BAR SLIDERS NOT ATTACHED TO DOOR MECHANISM. REINSTALLED GIRT BAR SLIDERS IAW AMM 25-66-01-4. LUBRICATED SLIDER AREA IAW AMM 12-21-18-3. CHECKED OPERATION OF THE R1 GIRT BAR IAW AMM 52-11-25-5. DOOR GIRT BAR OPS CHECKED NORMAL, SLIDE ARMED LIGHT CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,553 hrs · 12,867 cycles

EMERGENCY EXTERIOR LIGHT AFT OF R1 DOOR INOPERATIVE. REPLACED LAMP IAW SMP'S. OPS CHECKED GOOD.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

FUSELAGE SKIN BS 1200 -1220 BETWEEN STRINGER 29 LT AND 29 RT. THERE IS CORROSION AROUND THE TOILET SERVICING HOLES IN THE SKIN. REPAIR CARRIED OUT AS PER EA F-3830-163852. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

AFT CARGO LOWER COMPARTMENT INTERIOR SKIN BETWEEN BS 1200 AND 1205 NEAR LBL 2. CUT OUT AREA WITH CORROSION. REPAIR CARRIED OUT IAW EA F-3830-163852. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: CHANNEL — DAMAGED (BS 1620) · airframe 43,482 hrs · 12,822 cycles

MAIN DECK -DURING OK TO INSTALL, FOUND SPLICE CHANNEL WITH ELONGATED HOLE AT STR 1, BS 1620. REMOVED CHANNEL IAW SRM 51-40-02 REV 107. NEW CHANNEL FABRICATED IAW DWG 146N3820 SHT 1 REV C. CHANNEL INSTALLED IAW DWG 146N3106 SHT 1 REV E. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.

Part: STIFFENER — SHEARED (FLOORBEAM) · airframe 43,482 hrs · 12,822 cycles

AFT CARGO COMPARTMENT RT SIDE LOWER FLOORBEAM STIFFENER STRAP IS BROKEN, BS 1640, RBL 45. COMPLIED PART 1 OF EA F-5330-163846. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (BS 1320) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

BS 1320, FLOORBEAM UPPER TEE HAS CORROSION, LBL 56 TO LBL 64. COMPLIED WITH EA F-5310-163824, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — DENTED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

FUSELAGE SKIN DENTED AT BS 1620, BELOW STR 24R. REPAIR CARRIED OUT IAW EA F-5330-163828. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CORRODED (BS 1259) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

BS 1259, RBL 64 CREASE BEAM HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-30-13, ALLOWABLE DAMAGE 1, FIG 101, REV 107. REPAIR CARRIED OUT IAW EA F-5310-162909.

Part: SEAT TRACK — CORRODED (BS 1050-1075) · airframe 43,482 hrs · 12,822 cycles

SEAT TRACK AT BS 1050 TO 1075, RBL 24 HAS DEEP DRILL MARK WITH CORROSION ON CHANNEL. SEAT TRACK REPAIRED IAW SRM 53-00-52 FIG.201 REPAIR 4 REV.107. REPAIR MAJOR.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

BS 1340 R3 DOOR SILL WEB HAS CORROSION. SILL WEB REPLACED WITH NEW SILL WEB FABRICATED AS PER DWG 146N8326 SHT.1 REV.C AND INSTALLED IAW DWG 146N8322 SHT.1 REV.F. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (BS 600-620) · airframe 43,482 hrs · 12,822 cycles

BS 600 TO 620 RBL 64 CREASE BEAM INNER CHORD HAS CORROSION.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN CREASE BEAM AT BS 760 RBL 64 HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-30-13 ALLOWABLE DAMAGE 1, FIG 101, REV 107. REPAIR CARRIED OUT IAW EA: F-5310-162907. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

SEAT TRACK AT BS 418 TO 440, RBL 24 FOUND WITH DEEP GOUGES IN CROWN. BLENDED AREA AND FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I ALLOWABLE DAMAGE 1 REV 107. DAMAGED SEAT TRACK REMOVED IAW SRM 51-40-02 REV 107. NEW SEAT TRACK FABRICATED IAW DRAWING 141N5131 SHT 3 REV C. AND INSTALLED IAW DRAWING 141N5130 SHT 2 REV E. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (BS 1360-1380) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 1360 TO 1380, LBL 24 HAS SEAT FITTING DAMAGE TO THE CROWN AND DRILLED HOLE ON THE CHANNEL. FOUND EXCEED LIMITS IAW SRM 53-00-52, FIG 101 ALLOWABLE DAMAGE 1 REV 107, SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52, FIG 201, REPAIR 3, REV 107 AND COMPLIED WITH PART 1 OF EA F-5310-162913. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

BS 754 TO 760 LBL 64 CREASE BEAM INNER ANGLE HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND EXCEEDED 10 PERCENT LIMIT IAW SRM 53-30-13 ALLOWABLE DAMAGE 1, FIG 101. REV 107. REPAIR CARRIED OUT IAW EA F-5310-162906. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

FLOORBEAM AT BS 345, LBL 24 TO RBL 10 HAS CORROSION ON UPPER TEE. REPAIRED IAW EA F-5310-162905 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — DAMAGED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

FRAME AT BS 1620, S2L TO S3L FOUND WITH DEEP DRILL MARK. REPAIRED IAW PART 1 OF EA: F-5310-163848. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRAP — CORRODED (ZONE 300) · airframe 43,482 hrs · 12,822 cycles

FOUND CORROSION ON THE OUTER STRAP AT BS 1825 BETWEEN STR 2 -7 R. REPLACED WITH STRAP FABRICATED IAW DWG 148N3138, SHT 1, REV C AND INSTALLED IAW DWG 148N3105 SHT 1, REV C. REPAIR IS MAJOR.

Part: FRAME — GOUGED (ZONE 100) · airframe 43,482 hrs · 12,822 cycles

FWD EQUIPMENT BAY FRAME BS 231 HAS SEVERAL GOUGES AT BL 0 TOP AFT SIDE OF FRAME. REPAIR CARRIED OUT IAW EA: F-5310-162910. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRAP — CORRODED (ZONE 300) · airframe 43,482 hrs · 12,822 cycles

FUSELAGE INTERIOR STRUCTURE, RT SIDE THERE IS CORROSION ON THE APU INLET STRAP FROM BS 1825 ALONG STR 3 TO 6. REPLACED WITH STRAP FABRICATED IAW DWG 148N3138, SHT 1, REV C AND INSTALLED IAW DWG 148N3105 SHT 1, REV C. REPAIR IS MAJOR.

Part: SKIN — MISREPAIRED (ZONE 300) · airframe 43,482 hrs · 12,822 cycles

EXISTING REPAIR -EMPENNAGE- 10" FWD LOWER ELEVATOR SECTION 48, BETWEEN 1844 -1862. EXISTING REPAIR ON LOWER FUSELAGE SKIN FROM STA 1844 TO STA 1862 BETWEEN STR 29L AND STR 29R EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A PT 1, TITLE : STRUCTURES - REPAIR CATALOG - REPAIR IDENTIFICATION AND TRACKING REQUIREMENTS 14 CFR 121.707 AND FOUND REPAIR DOES NOT MATCH DOCUMENTATION, EXISTING REPAIR R & R EA : F-5330-163826 PART 1 TITLE: FUSELAGE - PLATES AND SKIN EXISTING FLUSH PATCH REPAIR FOUND AT LWR FUSELAGE SKIN FROM BS 1844 TO BS 1862.70 BETWEEN STR 29L AND STR 29R. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (ZONE 100) · airframe 43,482 hrs · 12,822 cycles

FWD CARGO BAY LT SIDE FRAME AT BS 680 HAS DENT ON TOP OF FRAME AT STR 23L. COMPLIED IAW EA: RF-5310-162903. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — DENTED (ZONE 100) · airframe 43,482 hrs · 12,822 cycles

AFT CARGO BAY LT SIDE FRAME BS 1480 HAS DENT ON TOP OF FRAME, BETWEEN STR 25 AND 26L. REPAIRED IAW EA : F-5310-162902. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 377 TO 395 RBL 24 HAS CORROSION ON TRACK FLANGES. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND EXCEEDED LIMITS IAW SRM 53-00-52, FIG 101 ALLOWABLE DAMAGE 1, REV 107. SEAT TRACK IAW SRM 51-40-02, REV 107. NEW SEAT TRACK INSTALLED IAW DWG 141N5130 SHT 2, REV E. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN CREASE BEAM AT BS 362 TO STA 395, LBL 64 HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02, REV 107 AND FOUND OUT OF LIMIT IAW SRM 53-00-15, FIG 101 ALLOWABLE DAMAGE 1, REV 107. NEW CREASE BEAM INNER CHORD FABRICATED IAW DWG 141N8322 SHT 3, REV G. NEW CREASE BEAM INNER CHORD ANGLE INSTALLED IAW DWG 141N8322, SHT 1, REV K. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN CREASE BEAM ANGLE HAS CORROSION AT BS 710 TO 730 LBL 64. NEW ANGLE INSTALLED IAW DWG 143N8322, SHT 1, REV K, REPAIR CLASSIFED MAJOR IAW GMM 6-2-100.

Part: DECK PLATE — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1703 TO 1710, RBL 48 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 418 TO STA 440 LBL 45 HAS SEAT FITTING DAMAGE TO CROWN. SEAT TRACK INSTALLED IAW DWG 141N5130, SHT 1, REV F. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 1610 TO 1640, RBL 45 HAS CROWN CORROSION. REPLACED SEAT TRACK SECTION FABRICATED AND INSTALLED IAW SRM 53-00-52, FIG 201. REPAIR 3 REV 107. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN FLOORBEAM AT BS 365, RBL 12 TO RBL 47 HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND OUT OF LIMIT IAW SRM 53-00-51, FIG 101 ALLOWABLE DAMAGE 1, REV 107. FLOORBEAM REMOVED IAW SRM 51-40-02, REV 107. NEW FLOORBEAM FABRICATED IAW DWG 141N5122, SHT 1, REV A. NEW FLOORBEAM INSTALLED IAW DWG 141N5112, SHT 1, REV D. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CORRODED (BS 740) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

BS 740 LBL 64 CREASE BEAM HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 106. MATERIAL THICKNESS REMOVED 0.014 INCHES FOUND EXCEEDS LIMITS IAW SRM 53-30-13 FIG 101 ALLOWABLE DAMAGE 1 REV 106. CREASE BEAM REMOVED IAW SRM 51-40- 02 REV 106. NEW CREASE BEAM INSTALLED AS PER DRAWING 143N8322 SHT 1 REV K. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 1610 TO 1640, RBL 24 HAS CHANNEL AND CROWN CORROSION. REPLACED SEAT TRACK WITH FABRICATED SECTION AND INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 3, REV 107. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN, BS 734 LBL 64 CREASE BEAM ANGLE HAS CORROSION. NEW ANGLE INSTALLED IAW DWG 143N8322, SHT 1, REV K. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 418 TO 440 LBL 24 HAS SEAT FITTING DAMAGE TO CROWN. SEAT TRACK INSTALLED IAW DWG 141N5130, SHT 1, REV F. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN, AT BS 1615 RBL 45 SEAT TRACK HAS CORROSION IN CHANNEL. REPLACED SEAT TRACK SECTION. FABRICATED AND INSTALLED IAW SRM 53-00-52, FIG 201. REPAIR 3 REV 107. REPAIR IS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN, AT BS 1640 RBL 54 TO 45 FLOORBEAM HAS CORROSION. NEW FLOORBEAM INSTALLED IAW DWG 146N5089, SHT 1, REV B. REFER TO SNRM: N01086 FOR WORK DETAILS. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 365 TO 377 RBL 24 HAS CORROSION ON TRACK FLANGES. NEW SEAT TRACK SUPPORT INSTALLED IAW DWG 141N5130, SHT 2, REV E. REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CORRODED (BS 1295-1360) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

BS 1295 TO 1360, RBL 64 CREASE BEAM HAS CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 106. MATERIAL THICKNESS LOSS MORE THAN 50%. CREASE BEAM REMOVED IAW SRM 51-40-02 REV 106. NEW CREASE BEAM INSTALLED IAW DRAWING 146N8322 SHT 1 REV F. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 395 TO 418 RBL 45 HAS CORROSION ON TRACK FLANGES. SEAT TRACK REPLACED IAW DWG 141N5130, SHT 2, REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DECK PLATE — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1681 LBL 12 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300 SHT 16, REV C. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 377 TO 395 RBL 45 HAS CORROSION ON TRACK FLANGES. REPLACED IAW DWG 141N5130, SHT 2, REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT STA 365 TO 377 RBL 45 HAS CORROSION ON TRACK FLANGES. CORROSION REMOVED IAW SRM 51-10-02 REV 106. FOUND EXCEED LIMITS IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 106. SEAT TRACK SUPPORT REMOVED IAW SRM 51-40-02 REV 106. SEAT TRACK SUPPORT INSTALLED AS PER DWG 141N5130 SHT 2 REV E. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 395 TO STA 418, RBL 24 HAS CORROSION ON TRACK FLANGES. NEW SEAT TRACK INSTALLED IAW DWG 141N5130, SHT 2, REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — MISALIGNED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 1610, LBL 24 HAS SEAT FITTING MISMATCH. SEAT TRACK SECTION INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 3, REV 107.

Part: DECK PLATE — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE STA 1681 TO STA 1683, RBL 23 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300 SHT 16, REV C. REPAIR IS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT BS 1524, RBL 45 HAS A DRILL HOLE ON THE CHANNEL. FOUND EXCEEDED LIMITS IAW SRM 53-00-52, FIG 101, ALLOWABLE DAMAGE 1, REV 107. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52, FIG 201. REPAIR 3, REV 107 AND COMPLIED WITH PART 1 OF EA F-5310-162914, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1717, RBL 16 TO RBL 20 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300 SHT 16 REV C. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

SEAT TRACK AT BS 1610 TO 1640, LBL 24 HAS CHANNEL CORROSION AND SEAT FITTING DAMAGE TO THE CROWN. SEAT TRACK REMOVED IAW SRM 51-40-02 REV 107. NEW SECTION FABRICATED AND INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 3, REV 107. MAJOR REPAIR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1717 TO 1714, LBL 47 TO LBL 37 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318 SHT 3, REV AND INSTALLED IAW DWG 146N5300 SHT 16, REV C. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN, DECK PLATE AT BS 1701 TO 1703, LBL 47 TO LBL 50 CORRODED. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318. INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT STA 1610 TO 1620, RBL 24 HAS CROWN BROKEN. SEAT TRACK REMOVED IAW SRM 51-40-02, REV 107. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-00-52, FIG 201, REPAIR 3, REV 107. MAJOR REPAIR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1681, LBL 40 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300 SHT 16, REV C. REPAIR IS MAJOR.

Part: CREASE BEAM — CORRODED (BS 680) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

BS 680, RBL 64, CREASE BEAM HAS CORROSION. CREASE BEAM REMOVED IAW SRM 51-10-02 REV 106. BLENDED AREA FOUND EXCEEDED 10% LIMIT AS PER SRM 53-30-15 ALLOWABLE DAMAGE 1 FIG. 101 REV. 106. CREASE BEAM SECTION REMOVED IAW SRM 51-40-02 REV 106. NEW SECTION INSTALLED IAW DWG 143N8322 SHT 1 REV K. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

SEAT TRACK AT BS 1610 TO 1640, LBL 445 HAS CHANNEL AND CROWN CORROSION. SEAT TRACK REMOVED IAW SRM 51-40-02, REV 107. NEW SECTION FABRICATED AND INSTALLED IAW SRM 53-00-52, FIG 201, REPAIR 3, REV 107. MAJOR REPAIR.

Part: DECK PLATE — DAMAGED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1681 RBL 30, DOUBLE HOLE DRILLED. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3 REV AND INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1693 TO 1695, LBL 47 TO LBL 50 CORRODED. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV - AND INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1681 TO 1683 LBL 34 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1717 RBL 23 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318 SHT 3 REV - AND INSTALLED IAW DWG 146N5300 SHT 16, REV C. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1717, BL 0 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3 REV.- AND INSTALLED IAW DWG 146N5300 SHT 16 REVC. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1681, LBL 24 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1681 LBL 46 HAS CORROSION. REPLACED WITH FABRICATED PLATE IAW DWG 146N5318, SHT 3, REV.- AND INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1681 TO 1682, RBL 3 TO RBL 5, HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300 SHT 16, REV C. REPAIR IS MAJOR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN DECK PLATE AT BS 1681, LBL 9 TO BL0 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV AND INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.

Part: SEAT TRACK — CORRODED (BS 1620-1640) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

SEAT TRACK AT BS 1620 TO 1640, RBL 45 HAS CORROSION ON FLANGES. SEAT TRACK REMOVED IAW SRM 51-40-02, REV 107. FABRICATED AND INSTALL NEW SEAT TRACK SECTION IAW SRM 53-00-52, FIG 201, REPAIR 3, REV 107. MAJOR REPAIR.

Part: DECK PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

DECK PLATE AT BS 1717 RBL 10 TO RBL 12 HAS CORROSION. REPLACED WITH DECK PLATE FABRICATED IAW DWG 146N5318, SHT 3, REV.- AND INSTALLED IAW DWG 146N5300, SHT 16, REV C. REPAIR IS MAJOR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 43,482 hrs · 12,822 cycles

SKIN AT BS 1420 -1440 BETWEEN STRINGER 29 -30 MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, REV 107.

Part: ATTACH ANGLE — CORRODED (ZONE 300) · airframe 43,482 hrs · 12,822 cycles

INTERIOR STRUCTURE, RT SIDE CORRODED ON THE APU INLET ATTACH ANGLE FROM BS 1787-1825, STR 3. CORROSION REMOVED, FOUND OUT OF LIMIT IAW SRM 53-80-15, FIG 101 DETAIL I, REVISION 107. CORRODED ANGLE REMOVED AND NEW ANGLE FABRICATED IAW DWG 148N3152, SHT 1, REV- AND INSTALLED IAW DWG 148N3105, SHT 1, REV C. REPAIR CLASSIFIED MAJOR GMM 6-2-100.

Part: CREASE BEAM — CORRODED (BS 1320-1330) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CREASE BEAM BS 1320 TO 1330, LBL 64 CORRODED. REPAIRED IAW DWG 146N8322 SHT 1 REV. F. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT STA 377 LBL 24 HAS CORROSION ON TRACK FLANGES. CORROSION REMOVED AS PER SRM 51-10-02 REV 106. MATERIAL THICKNESSS REMOVED 0.032 INCHES. FOUND EXCEEDED LIMITS 10% AS PER SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 106. SEAT TRACK REMOVED AS PER SRM51-40-02 REV 106. SEAT TRACK FABRICATED AS PER DWG 141N5131 SHT 1 REV A. INSTALLED AS PER DWG 141N5130 SHT 1 REV F. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN FLOORBEAM AT BS 377 LBL 56 TO LBL 58 HAS CORROSION TO UPPER TEE. NEW FLOORBEAM INSTALLED AT STA 377 IAW DWG 141N5113, SHT 1, REV F. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN SEAT TRACK AT STA 377 LBL 45 HAS CORROSION ON TRACK FLANGES. CORROSION REMOVED AS PER SRM 51-10-02 REV 106. MATERIAL THICKNESS REMOVED 0.027 INCHES. FOUND EXCEEDED LIMITS AS PER SRM 53-00-52 FIG 101, ALLOWABLE DAMAGE 1 REV 106. SEAT TRACK REMOVED AS PER SRM 51-40-02 REV 106. SEAT TRACK FABRICATED AS PER DWG 141N5131 SHT 1 REV A. SEAT TRACK INSTALLLED AS PER DWG 141N5130 SHT 1 REV F. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.

Part: ATTACH FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

FUSELAGE INTERIOR RT SIDE THERE IS CORROSION ON THE APU INLET ATTACH STRUCTURE FROM BS 1787, STRINGER 3 TO 6R. CORROSION REMOVED & FOUND OUT OF LIMIT IAW SRM 53-80-15, FIG 101, DETAIL 1, REV 107. CORRODED STRAP R & R WITH NEW STRAP, IAW DWG 148N3105, SHT 1, REV C. REPAIR CLASSIFIED MAJOR, IAW GMM 6-2-100.

Part: ATTACH ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

FUSLELAGE INTERIOR RT SIDE THERE IS CORROSION ON THE APU INLET ATTACH ANGLE FROM BS 1787 TO 1825 ALONG STRINGER 6. ATTACH ANGLE REMOVED AND NEW ANGLE FABRICATED IAW DWG 148N3152, SHT 1 REV. INSTALLED IAW DWG 148N3105, SHT 1, REV C. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,482 hrs · 12,822 cycles

CABIN FLOORBEAM AT BS 377, LBL 12 TO LBL 24 HAS CORROSION TO UPPER TEE. CORROSION REMOVED IAW SRM 51-10-02, REV 107. FOUND OUT OF LIMIT IAW SRM 53-00-51, FIG 101, ALLOWABLE DAMAGE, 1 REV 107. FLOORBEAM REMOVED IAW 51-40-02, REV 107. NEW FLOORBEAM FABRICATED IAW DWG 141N5123, SHT 1, REV A & INSTALLED IAW DWG 141N5113, SHT 1, REV F. REPAIR CLASSIED MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 43,482 hrs · 12,822 cycles

CABIN FLOORBEAM AT BS 1640 FOUND WITH CORROSION AT UPPER TEE SURFACES. CORROSION FOUND 100 PERCENT THROUGH AND OUT OF LIMITS IAW SRM 53-00-51, FIG 101 ALLOWABLE DAMAGE 1, REV 107. FLOORBEAM REMOVED IAW SRM 51-40-02, REV 107. NEW FLOORBEAM FABRICATED IAW DWG 146N5109, SHT 1, REV A. NEW FLOORBEAM INSTALLED IAW DWG 146N5089, SHT 1, REV B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.