N406KZ

Part: LONGERON — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

1EA CRACK WAS FOUND RH STA 1480 LONGERON EXTENSION FTG RADIUS AREA APPROX 3/8"(<P>FUS STA 1480 RH STR 32R TO STR 33R LONGERON EXTENSION FTG REPLACED AND INSTALLED IAW EO 4453A818 PART 4 . NO FURTHER DEFECTS NOTED</P>)

Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

STA 1000 FRONT SPAR SHEAR TIE LBL 57.5 FOUND CRACK(<P>STA 1000 LBL 57.5 FRONT SPAR SHEAR TIE P/N 69B14267U7 REPLACED AND INSTALLED IAW EO 4453C024 PART 5 AND SB 53A2904 FIG 11. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

RHW I/B AFT FLAP I/B L/E FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

RHW I/B MID FLAP UPPER SURFACE FOUND DENT(<P>PERFORMED REPAIR AT DENT AREA IAW SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

RHW INBOARD FORE FLAP LEADING EDGE MID FAIRING SKIN FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AT DELAMINATED AREA IAW SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

RHW INBOARD AILERON OUTBOARD AFT CORNER SKIN FOUND DELAMINATION(<P>PERFORMED COMPOSITE LAYUP REPAIR AT DELAMINATED AREA IAW SRM 51-70-06 PAR 5G. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

BULK CARGO - STA 2160 PARTITION LINER FOUND TORN(<P>REPAIRED CARRIED OUT AS PER RI-25-54-16324 REV A. NO FURTHER DEFECTS NOTED. PN 453U1553-14</P>)

Part: LAMP — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

MAIN DECK L1 DOOR CEILING AREA EMERGENCY LT FOUND INOP(<P>MAIN DECK L1 DOOR CEILING AREA EMERGENCY LIGHT RE-LAMPED AND EMERGENCY POWER SUPPLY ( M5170 ) REPLACED. EMERGENCY LIGHT OPERATION TEST RESULT NORMAL PER AMM 33-51-00</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

APU FWD FIRE BOTTLE COMP BEHIND FIRE BOTTLE FIRE WALL FOUND CRACK(<P>STA 2658 APU FIRE WALL LHS WEB (P/N: 65B02712-161) CRACK AREA REPAIRED IAW RI-53-83-16310 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

RHW I/B AFT FLAP LOWER SURFACE FOUND DENTS(<P>PERFORMED REPAIR AT DENTS IAW SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,694 hrs · 10,132 cycles

FX - SKIN STA 2618-2638 STR 50R-51R SKIN DENT DAMAGED(<P>FX - SKIN STA 2618-2638, STR 50R-51R SKIN DENT DAMAGE AREA REPAIRED IAW SRM 53-00-01-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,181 hrs · 10,048 cycles

ENGINE #1 INDICATED HIGH VIBE OF 4.9 CLIMBING THROUGH 15,000' UP TO FL 240.(<P>ACCOMPLISHED FIM TASK ON 71-00 FIGURE 118 STEPS 1 &AMP;2, NO DEFECTS FOUND. INSTALLED ACCELEROMETER IAW 77-31-01. PENDING OPS CHECK. ACCOMPLISHED VIBRATION SURVEY PER AMM 71-00-00.</P> / <P>FAN BLADE LUBE ACCOMPLISHED ON ENGINE #1 PER AMM 72-31-02 REV. 107. PER PPE, REMAPPED FAN BLADES. ALL MOMENT WEIGHTS ON SPINNER CONFIRMED TO P07 OR P014 BY REPLACING 2 EA WEIGHTS.</P> / <P>PERFORMED ENGINE #1 FAN TRIM BALANCE PER AMM 72-31-00. VIBRATION SURVEY CHECKED NORMAL 0.02 MPA.</P> / <P>RETORQUED ENGINE #1 SPINNER PER AMM 72-31-01.</P> / <P>REACTIVATED ENGINE #1 NORMAL ACCELEROMETER PER AMM 77-31-01.</P>)

Part: PANEL — MISSING · airframe 50,677 hrs · 9,816 cycles

#3 PYLON FOUND MISSING PANEL 471AL MISSING ON ARRIVAL(INSTALLED TEMP PANEL PER EO 4454A089 AND PERFORMED PART DEPARTURE INSPECTION PER AMM 05-51-58-200-801.)

Part: LINE — PERFORATED · airframe 50,420 hrs · 9,776 cycles

HYDRAULIC PRESS #4 SYSTEM IN FLIGHT.(<P>FOUND RIGID LINE ON RIGHT WING MLG RETRACT ACTUATOR PERFORATED. REMOVED RIGID LINE AND INSTALLED TEMPORARY FLEX LINE PER ATLAS AIR GMM 3.24.1. TRANSFERRED TO DMI 173812 PER NON-MEL, DUE DATE APR 15, 2024.</P>)

Part: ENGINE — VIBRATION · airframe 49,702 hrs · 9,664 cycles

ENGINE 3 FAN VIBRATION 4.3 - 5.0 IN CLIMB(<P>PERFORMED BOROSCOPE INSPECTION AND TRIM BALANCE REF LOG PAGE 1194652 M5 &AMP; M6.</P> / <P>M5: PERFORMED #3 ENG BSI THEN OPS CHECK NORMAL AND RE-INSTALLED INSPECTION PORT (B1-0, B1-3, B4-3, B4-4, B4-2) AND N2 CRANK PAD THEN RUN UP LEAK CHECK NORMAL AS PER AMM 72-00-00 &AMP; 71-00-00.</P> / <P>M6: PERFORMED ECM 2022P-235. WEIGHT SCREW NOT MATCH WITH AVM. UPDATE AVM THEN PERFORMED #3 ENG TRIM BALANCE THEN VIB CHECK NORMAL (FAN VIB 1.3) AS PER AMM 72-31-00 &AMP; 71-00-00.</P>)

Part: PDU — NONE · airframe 47,604 hrs

INDICATION AND OTHER EVIDENCE OF LE RH MIDSPAN FLAP, AT CRUISE AFTER DEPARTURE, FLAP DEPLOYMENT AT CRUISE.(<P ><SPAN>REMOVED AND REPLACED R2 LE PDU ASSEMBLY IAW AMM 05-51-04. INSPECTION COMPLETED, NO DEFECTS NOTED.</SPAN></P> / <P>&NBSP;</P>)

Part: ACTUATOR — FAULTED (GEAR TRUCK)

GEAR TILT EICAS FOR RH BODY GEAR GEAR MONITOR, GEAR TILT STATUS(<P>R BODY GEAR TRUCK POSITIONING ACTUATOR REPLACED AND HYD BLEEDING AND HYD FUSE RESET TO USUAL COND. PERFORMED IAW AMM 32-13-15/401.</P> / <P>REMOVED AND REPLACED THE HYD HOSE FOR THE R BODY GEAR TRUCK TILT ACTUATOR (PN&NBSP;<SPAN>65B83248-43, NSN)</SPAN><SPAN>. LEAK CHECK SATISFACTORY IAW AMM 32-13-15/401.</SPAN></P>)

Part: SKIN — DEBONDED (RT AILERON) · airframe 44,452 hrs · 8,817 cycles

DISBOND - SKIN, LOWER FACE OF R/H WING T/E INBD AILERON LOWER SKIN, WBL 508.(<P>REPAIR DISBOND - SKIN, LOWER FACE OF R/H WING T/E INBD AILERON LOWER SKIN WBL 508. PLEASE SEE THE JOB CARD ATTACHING SHEET CNTRL NO. 0238229 FOR REPAIR DETAIL. CONDITION CHECK IS SATISFACTORY.</P>)

Part: KEELBEAM — CORRODED (BS 1270 RBL 9) · corrosion level 2 · airframe 44,452 hrs · 8,817 cycles

CORROSION - KEEL BEAM, LOWER CHORD UPR FLANGE UPR SURFACE AT STA 1270, RBL 9.(<P>ACCOMPLISHED EI NO T2021A53M-1573 REV 1 AND THIS EI ATTACHING WITH T/C: 5915682 (451). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: KEELBEAM — CORRODED (BS 1387 LBL 9) · corrosion level 2 · airframe 44,452 hrs · 8,817 cycles

CORROSION - KEEL BEAM, LOWER CHORD UPR FLANGE UPR SURFACE AT STA 1387 LBL9.(<P>ACCOMPLISHED EI NO T2021A53M-1573 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 44,452 hrs · 8,817 cycles

AFT CARGO SKIN LOWER EDGE EXISTING TRIM BETWEEN STA 1816 - STA 1822.8.(<P>ACCOMPLISHED AFT CGO DOOR EDGE REPAIR IAW EI NO T2021A52M-1540 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: CONNECTOR — DISCONNECTED (IDG) · airframe 44,452 hrs · 8,817 cycles

IDG-3 FAILED DISCONNECT(<P>IAW WDM 24-11-13 REV 28 PERFORM WIRING CHK, FOUND W5302-007-16 INSULATION LOW. IAW WDM 24-11-13 REV 28 SWPM 20-00-12, 20-63-13, 20-61-11, 20-10-11 REV 76 REPLACE WIRE W5302-007-16. CONDITION CHK NORMAL. IAW WDM 24-11-13 REV 28 PERFORM WIRING CHECK, RESULT WAS SATISFACTORY. IAW AMM 24-11-01-752-001, 24-11-752-022 REV 101 PERFORM IDG-3 DISCONNECT TEST AND THE RESULT WAS SATISFACTORY</P>)

Part: SKIN — DEBONDED (RT WING AILERON) · airframe 44,452 hrs · 8,817 cycles

DISBOND - SKIN, OUTBD SIDE AFT EDGE OF R/H WING INBD AILERON, WBL 515(<P>REPAIR DISBOND - SKIN, OUTBD SIDE AFT EDGE OF R/H WING INBD AILERON UPPER SURFACE. PLEASE SEE THE JOB CARD ATTACHING SHEET CNTRL NO. 0238254 FOR REPAIR DETAIL. CONDITION CHECK IS SATISFACTORY.</P>)

Part: KEELBEAM — CORRODED (BS 1375 RBL9) · corrosion level 2 · airframe 44,452 hrs · 8,817 cycles

CORROSION - KEEL BEAM, LOWER CHORD UPPER FLANGE UPPER SURFACE AT STA 1375 RBL 9(<P>ACCOMPLISHED EI NO T2021A53M-1573 REV 1 AND THIS EI ATTACHING WITH T/C NO: 5915682 (451). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: FLOOR SUPPORT — DAMAGED (BS 480-500 RBL96) · airframe 44,452 hrs · 8,817 cycles

MAIN DECK FLOOR STRUCTURE BETWEEN BS 480 AND 500 RBL 96. ACCOMPLISHED EI NO T2021A53-1575 REV 1. JOB COMPLETED AND CONDITION CHK NORMAL

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 39,768 hrs · 8,048 cycles

#4 ENG BLEED OVERHEAT MESSAGE(<P>REMOVED AND REPLACED #4 PRV AND #4 PRV CONTROLLER AND THEN PERFORMED OPERATIONAL CHECK PER AMM 36-11-19/401 AND AMM 36-11-20/401 (PRV OFF PART: PN 802170-12, SN 98080594).</P>)

Part: FLAP TRACK — CORRODED · airframe 38,239 hrs · 7,758 cycles

EVIDENCE OF LIGHT SURFACE CORROSION ON ALL EIGHT FLAP TRACKS.(<P>FOR #4 AND #5 FLAP TRACK REPAIR, REF EI NO. T2019A57M-3693 REV. 1 AND T2019A57M-3700 REV.1. REFERENCE J/C ATTACHING SHEET FOR REPLACEMENT OF FLAP TRACKS #1, #2, #3, #6, # 7, AND #8. CONDITION CHECKS NORMAL.&

Part: SKIN — DAMAGED (RT WING AILERON) · airframe 38,239 hrs · 7,758 cycles

OUTBOARD EDGE OF R/H WING INBD AILERON, T/E SKIN, WBL 515 DAMAGED. CUT OUT THE DAMAGED MATERIAL AND CLEANED. MEASURED THE DAMAGED AREA, L = 1.5", W = 0.25", DEPTH = 2 PLIES. BOND REPAIR PLIES, USED WET LAYUP IAW SRM 57-60-01-2R-1, REPAIR 1, AND SRM 51-70-06-0G-0, REV 86. CONDITION CHECKED NORMAL.

Part: RUB STRIP — CORRODED (THRUST REVERSER) · corrosion level 2 · airframe 38,239 hrs · 7,758 cycles

NR 2 ENG R/H THRUST REVERSER CORE COWL ON INNER AFT EDGE HAS WEAR STRIP CORRODED. REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV. 86. INSTALLED NEW PARTS IAW SRM 51-40-02 REV. 86 AND IPC 78-32-22 REV. 82. JOB COMPLETED AND CONDITION CHECKS NORMAL.

Part: RUB STRIP — CORRODED (THRUST REVERSER) · corrosion level 2 · airframe 38,239 hrs · 7,758 cycles

WEAR STRIP ON NR 3 ENG LT THRUST REVERSER, NEAR UPPER REAR CORRODED. REMOVED DAMAGED WEAR STRIP IAW SRM 51-40-02 REV. 86. INSTALLED NEW WEAR STRIP IAW SRM 51-40-02 REV. 86 AND IPC 78-32-21 REV. 82. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SKIN — DEBONDED (RT AILERON) · airframe 38,239 hrs · 7,758 cycles

OUTBOARD EDGE OF RT WING, INBD AILERON LOWER SKIN, WBL 515 SKIN DEBONDED. CUT OUT THE DAMAGED MATERIAL AND CLEANED. MEASURED THE DAMAGED AREA (L = 1", W = 0.3", D = 1 PLY). BOND REPAIR PLIES (L = 5", W = 5"), USED PREPREG LAYUP WITH FILM ADHESIVE. IAW SRM 57-60-01-2R-1, REPAIR 1 AND SRM 51-70-07-0G-0 REV. 86. CHECK CONDITION IS SATISFACTORY.

Part: RUB STRIP — CORRODED (NR 3 NACELLE) · corrosion level 2 · airframe 38,239 hrs · 7,758 cycles

NR 3 ENG LT CORE COWL ON L/E HAS WEAR STRIP CORRODED AT THE 9 O'CLOCK POSITION. REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV. 86. INSTALLED NEW PARTS IAW GOODRICH CMM 71-13-23 REV. 41 AND SRM 51-40-02 REV. 86. JOB COMPLETED AND CONDITION CHECKS NORMAL.