N406KZ
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ATLAS AIR INC (UIEA) | Operator | 2024-06-16 – 2024-06-16 | Operator named in NTSB report |
| ATLAS AIR INC | Operator | 2024-06-16 – 2024-06-16 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EGT ROLLBACK #4 ENGINE SHORTLY AFTER TAKE-OFF. AIRCRAFT DIVERTED TO ICN.(<P>R/R #4 ENG C/W ENG RUN UP & LEAK CHECK NORMAL PER AMM 71-00-00, 71-00-02 & TASK CARD 71-099-02-01</P>)
STARTER CUTOUT ENG 4 MSG IN FLIGHT(<P>INSPECTED ENGINE STARTER FOR CONDITION AND SERVICING & STARTER VALVE FOR CONDITION. REPLACED N2 SPEED CARD IAW AMM 73-21-00. OPS CHECKS GOOD</P>)
TIRE FAILURE ON TAKE OFF. LOSS OF HYD 1 SYS. HYD QTY LOW 1 & HYD PRESS SYS 1 AFTER LEVEL OFF FL290. ON LANDING, HYD SYS 2 & 4 FAIL HYD QTY ON 2 & 4 WENT TO ZERO. REF ITEM M12 & M13, 9 & 10 WHEEL ASSY REPLACED. IAW AMM 29-11-00 REV 110 REF WO 3415330 / N406KZ 00081 RH BLG WW 3 HYD LINE REPLACED & WO 3415343 / N406KZ 00083 RH WLG WW 2 EA HYD LINE REPLACED. LEAK CHECK GOOD, NO MSG NOTED IAW AMM 20-51-01 REV 110. NR 9 MWA R/R IAW AMM 32-45-01 REV 110. OPS CHK GOOD. NR 10 MWA R/R IAW AMM 32-45-01 REV 110. OPS CHK GOOD. R/R RH BLD HYD SUPPORT SWIVEL BRACKET PER AMM 32-13-01 & IPC 32-53-11-06. HYD LEAK CHECK GOOD IAW AMM 29-00-99 REV 110. C/W AP 28224 (RH BODY GEAR WHEEL WELL DAMAGED INSPECTION & BRAKE TEST)
DURING CLIMB, EICAS MESSAGE GEAR DOOR DISPLAYED WHEN MOVING GEAR HANDLE FROM UP TO OFF.ÃÂ RETURNED HANDLE TO UP, EICAS MESSAGE CLEARED. DIVERTED TO LAX.(<P>PERFORMED DVI OF RH BODY GEAR PROX SWITCH AND TARGET BRACKET. FOUND TARGET BRACKET BENT. READJUSTED TARGET BRACKET IAW 32-61-31. PERFORMED GND TEST OF PSEU. PERFORMED DIMENSION CHECK OF TARGET AND SENSOR GAP. TOLERANCE PASS IAW 32-09-03. CYCLED LG DOORS MULTIPLE TIMES. ALL LG DOORS OPERATE NORMAL. STS MSG CLEAR, NO EXISTING FAULTS&NBSP;</P>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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>)
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 &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>)
#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.)
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>)
ENGINE 3 FAN VIBRATION 4.3 - 5.0 IN CLIMB(<P>PERFORMED BOROSCOPE INSPECTION AND TRIM BALANCE REF LOG PAGE 1194652 M5 & 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 & 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 & 71-00-00.</P>)
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>)
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>)
MAIN DECK FLOOR STRUCTURE BETWEEN BS 480 AND 500 RBL 96. ACCOMPLISHED EI NO T2021A53-1575 REV 1. JOB COMPLETED AND CONDITION CHK NORMAL
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>)
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>)
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>)
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>)
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>)
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>)
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>)
#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>)
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.&
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.
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.
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.
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.
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.