N742CK
Registered owner: KALITTA AIR LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
EMERGENCY LIGHT OVER L1 FAILED LIGHT TEST
L/H WING T/E STIFFENER ON AFT SIDE OF AFT SPAR AT WBL 1150 DAMAGED.
EVIDENCE OF CORROSION FOUND ON CENTER TANK UPPER SKIN FWD OF TENSION FITTING AT STA 1180 RBL 98
MAIN DECK FLOOR STATION 140-160 LBL 40 SHEAR WEB CRACKED MULTIPLE LOCATIONS
DURING TROUBLESHOOTING OF ARM/ DISARM HANDLE OF L/H UPPER DECK DOOR , THE EMERGENCY ESCAPE SLIDE WAS UNINTENTIONALLY DEPLOYED AND REQUIRES REPLACEMENT
MAIN DECK CENTER FUEL TANK UPPER SKIN CORROSION STA 1050 LBL 80-100
EVIDENCE OF CORROSION FOUND ON CENTER TANK UPPER SKIN AT STA 1150 RBL 110
EVIDENCE OF CORROSION FOUND ON CENTER TANK UPPER FWD SKIN SECTION AT BS 1139, RBL 100.
NOSE RADOME O/B RING ANGLE CRACKED AT APPROX 11 O'CLOCK POSITION
CRACK FOUND ON MAIN DECK FLOORBEAM CLIP AT STA 280 LBL 6.
CRACK FOUND IN BS 1000 FRONT SPAR SHEAR TIE AT RBL 33.99
LEFT UPPER DECK DOOR AFT UPPER CORNER SEAL DEPRESSOR CRACKED
EVIDENCE OF CORROSION FOUND ON CENTER TANK UPPER SKIN AT STA 1140 RBL 100
FLIGHT DECK R/H UPPER SILL OUTER CHORD CRACKED AT STA 315 JUST ABOVE R2 WINDOW
MAIN DECK FLOOR BS 160-180 LBL 48, SHEAR WEB CRACKED.
MAIN DECK FLOOR STA 140-160 RBL 40, SHEAR WEB CRACKED MULTIPLE LOCATIONS
MAIN DECK AT BS 2360, RBL 33 JUST BELOW FLOOR LEVEL ANGLE SUPPORT CRACKED.
RT UPPER DECK DOOR FWD UPPER CORNER SEAL DEPOESSOR CRACKED
MAIN DECK AT STA 2360 LBL 33 JUST BELOW FLOOR LEVEL ANGLE SUPPORT CRACKED.
MAIN DECK FLOOR SUPPORT LOWER CHORD AT STA 1220 RBL 98 IS CRACKED
CENTER EMERGENCY LIGHTS ON UPPER DECK DO NOT STAY ILLUMINATED.
DOOR UPPER DECK FLIGHT LOCK CAUTION MESSAGE. PERFORMED FLIGHT LOCK ACTUATOR OPS TEST IAW AMM 52-23-00. OPS TESTED GOOD. NO DEFECTS NOTED.
DOOR UPPER DECK FLIGHT LOCK CAUTION MESSAGE. TRANSFERRED TO DMI LIST NUMBER 100272910 IAW KA B747-400 MEL 52-23-3-2. CAT C. DUE 10-5-25. PLACARDS INSTALLED. : REFERENCE DMI 100272910. REMOVED AND REPLACED RIGHT HAND UPPER DECK DOOR LOCK ACTUATOR IAW KA B747-400 AMM 52-23-08. OPERATIONAL CHECK GOOD. THIS CLEARS DMI 100272910. PLACARDS REMOVED.
DOOR UPPER DECK FLIGHT LOCK CAUTION MESSAGE. PERFORMED FLIGHT LOCK ACTUATOR OPERATIONAL TEST IAW AMM 52-23-00. OPERATIONAL TEST GOOD. NO DEFECTS NOTED.
AILERON CAVITY I/B STRUCTURE 20 IN. FWD OF HINGE POINT VERTICAL STIFFENER CRACKED AT LOWER EDGE
DOOR UPPER DECK FLIGHT LOCK MESSAGE. PERFORMED ADJUSTMENT TEST OF UPPER DECK DOOR LOCK IAW AMM 52-23-00. NO DEFECTS NOTED. MESSAGE CLEARED.
FIRE CARGO FWD MSG. FAK & ALL SRCS MVD TO U/D XFER TO DMI 100259185 IAW MEL 26-23-1-2 CAT C DUE 08-06-2025 MX PROC C/W PLCDS INSTL. REF DMI 100259185 FOR DEACT FWD LWR LOBE SMOKE DET SYS. SYS DEACT, XFER TO DMI 100259186 IAW MEL 26-16-1-2-2B CAT C, MX PROC C/W. PLCDS INSTL. REF DMI #100259185 FIRE CARGO FWDâMOVED FAK ITEMS ONTO M/D. IAW WO 742049403 & DMI 100259185. RET FAK INTO ORIG POS, CLRS DMI 100259185 PLCDS REM. REF DMI 100259186â FWD LWR LOBE SMOKE DETECT DEACT FOR FIRE BOTTLES. REACT FWD LWR LOBE SMOKE DET SYS IAW AMM 26-16-01. CLRS DMI 100259186, PLCDS REM REF WO 742049404. ACCOMP DROP IN WP 742CK/L-280725. ACCOMP W/P 742CK/L-280725 DURING DROP IN 742049410,411,412,413,414,416. LWR CARGO FIRE BOTTLES REQ RPLCMNT. REM AND REP LWR CARGO FIRE BOTTLE F,E,D,C,B,A IAW AMM 26-23-01.OPS CHKS GOOD IAW AMM 26-23-01.
RIGHT UPPER DECK DOOR BATTERY "OK LIGHT" INOPERATIONAL. COMPLIED WITH PLACARD INSTALLED. RIGHT UPPER DECK DOOR BATTERY LIGHT. OPERATIONS CHECK GOOD IAW B747-400 AMM 51-23-14.
DOOR UPPER DECK FLIGHT LOCK. TRANSFERRED TO DMI 100259089 IAW MEL 52-23-6-2 CATEGORY C DUE. PLACARDS INSTALLED MAINTENANCE PROCEDURES COMPLIED WITH. 100259106 - PERFORMED ADJUSTMENT TEST OF UPPER DECK FLIGHT LOCK IAW B747-400 AMM 52-23-00. NO DEFECTS NOTED.
UPPER DECK FLIGHT LOCK. PERFORMED ADJUSTMENT TEST IAW AMM 52-23-00. NO DEFECTS NOTED.
RIGHT UPPER DECK GROUND MODE LIGHT INOPERATIVE. COMPLIED WITH (M) PROCEDURES IAW MEL 52-23-4-2. CYCLED DOOR C/B ON P180 DOOR MODE LIGHT TEST OK IAW AMM 52-23-16. THIS CLEARS DMI 100259027.
RIGHT HAND UPPER DECK GROUND MODE LIGHT INOPERATIVE. TRANSFERRED TO DMI 100259027 IAW MEL 52-23-4-2 CATEGORY C DUE DATE 07/15/25 PLACARDS INSTALLED (M) PROCEDURES COMPLIED WITH.
AFT EMERGENCY LIGHT INOP
L1 DOOR SILL EMERGENCY LIGHTS INOP
FAILS CONTROL CHECK RIGHT OUTBOARD AILERON REMAINS UP. REFERENCE LOGBOOK ENTRY 100231222/100231226 FOR AILERON CONTROL CABLE REPLACEMENT, AILERON ADJUSTMENT AND TEST. PERFORMED AILERON ADJUSTMENT TEST IAW B747-400 AMM 27-11-00 ALL CHECKS GOOD. 100231223- REFERENCE WORK ORDER 100231222: WHILE TROUBLESHOOTING THE RIGHT-HAND OUTBOARD AILERON STUCK IN THE UP POSITION, FOUND RIGHT HAND INBOARD AILERON EXTREMELY SLOW TO TRAVEL TO DOWN POSITION. PERFORMED AILERON TRIM CONTROL ADJUSTMENT AND TEST IAW AMM 27-11-00 ALL CHECKS GOOD. 100231225- PERFORM GENERAL VISUAL INSPECTION OF OUTBOARD RIGHT-HAND AILERON PER COMPANY REQUEST IN REFERENCE TO LOG PAGE 100231222. PERFORMED GENERAL VISUAL INSPECTION OF RIGHT-HAND OUTBOARD AILERON. NO DEFECTS NOTED AT THIS TIME IAW B747-400SF 51-00-00. 100231226- REFERENCE WORK ORDER 100231222: UPON FURTHER INVESTIGATION FOUND CONTROL CABLE AA10 FOR RIGHT HAND OUTBOARD AILERON TO BE BROKEN. REMOVED AND REPLACED RIGHT HAND OUTBOARD AILERON CONTROL CABLE AA10 IAW AMM 27-11-00 RIG AND OPS CHECK GOOD. 100231230- DUE TO THE REMOVAL AND REPLACEMENT OF AILERON CONTROL CABLES AA10/AB10 AIRCRAFT REQUIRES EVALUATION FLIGHT PER GMM 3.4.1. AIRCRAFT RELEASED FOR FUNCTIONAL EVALUATION FLIGHT ONLY.
LH EMERGENCY SLIDE BOTTLE BATTERY INOP
L EMERGENCY DOOR SLIDE HARD TO ARM.
AIRCRAFT ROLLED FORWARD AFTER ENGINE START STRIKING VAN CAUSING DAMAGE AIRCRAFT RIGHT. AIRCRAFT DAMAGE INSPECTED, REPAIRED, AND LEAK CHECKED IAW E-52 #11533, DWG 52302402-1, 53302408-1 REV OR AND AMM 21-31-00 B747-400 REFERENCE M44 JOB CONTINUATION FORM FOR ADDITIONAL WORK ACCOMPLISHED. AIRCRAFT OK TO RETURN TO SERVICE.
UPPER DECK LEFT HAND EMERGENCY DOOR LIGHT INOP.
FLIGHT COMPARTMENT CREW OVERHEAD HATCH INNER SKIN HAS 1/2 INCH CRACK AT INNER HANDLE OPENING NEAR NUTPLATE LOCATION
CANTED PRESSURE DECK STA 1240 LBL 89 COMPOSITE CLOSE OUT PANEL CRACKED
CANTED PRESSURE DECK STA 1240 RBL 89 COMPOSITE CLOSE OUT PANEL CRACKED
CRACK ON CANTED PRESSURE WEB AT STA 1240 APPROXAMETLY RBL 80
L/H AFT CARGO COMPARTMENT SLOPE SIDEWALL FRAME WEB AT STA 1620 AND APROX LBL47 CRACKED APPROX 7 INCHES FROM TOP CHORD.
FWD E/E COMPARTMENT STA 400 BULKHEAD APPROXIMATELY S-43L HAS MARKED CRACK.
OUTBOARD SEAL RIB ON L/H WING @ APPROXIMATELY WBL 470 FSSI 702 ABOVE #2 PYLON HAS CRACK @ ROD ATTACHMENT POINT.
CRACK ON CANTED PRESSURE WEB AT STA. 1240 APPROXAMETLY LBL 80
POSSIBLE CRACK AT STA 400 BULKHEAD CHORD APPROX WL 124 LBL 23
L/H HORIZONTAL STAB CLOSEOUT RIB WEB CRACKED AT APPROX STAB STA 593.876
AFT CARGO PIT, SIDE WALL FRAME WEB CRACKED, 7" FROM TOP CHORD. STA 1600, LBL 47.
CRACK ON L/H HORIZONTAL STAB CLOSURE RIB UPPER CHORD AT APPROX STAB STA 593.876
POSSIBLE CRACK AT STA. 400 BULK HEAD WEB LBL 40 AT WL 124
AFT CARGO DOOR, FWD DOOR SIDE LIFT LINK MOUNT STIFFNER HAS A CRACK.
CORRODED UPPER DECK SEAT TRACK BETWEEN STA 660-700 LBL 20
O/B GUIDE ROLLER FITTING CRACKED ON L/H I/B FLAP.
FWD CARGO DOOR, FWD DOORSIDE LIFT LINK MOUNT STIFFNER HAS CRACK.
FUSELAGE MAIN DECK CREASE BEAM WEB HAS A CRACK BETWEEN STA 1241 TO STA 1264.8 AND APPROX S-5R
FUSELAGE MAIN DECK CREASE BEAM WEB HAS A CRACK STA 1241 AND APPROX S-7L
FIRE MAIN DOOR FORWARD EICAS MESSAGE APPEARED MOMENTARILY IN CRUISE. NO FIRE WAS DETECTED BY FLIGHT CREW. PERFORMED FIRE TEST GROUND TEST IAW B747-400 AMM 26-00-00. TEST PASS, NO DEFECTS NOTED.
R/H UPPER DECK DOOR EMERGENCY LIGHTS INOP
FIXED TRAILING EDGE BEAM WBL 429 WEB DAMAGED
FIXED TRAILING EDGE BEAM WBL 429 STIFFENER DAMAGED
LH UD EMERGENCY POWER SYS BATTERY PACK BAD
RH UPPER DECK SLIDE EMERGENCY POWER SYSTEM BATTERY PACK DOESN'T LIGHT BATTERY OK LIGHT
THE UPPER DECK AFT AISLE EMERGENCY EXIT SIGN IS INOP
THE L/H UPPER DECK EMERGENCY EXIT DOOR EXIT SIGN IS INOP
DOOR UPPER DECK FLIGHT LOCK. CLEANED SWITCH CONTACT ON RIGHT UPPER DECK EMERGENCY HATCH AND RESEATED DOOR IN ACCORDANCE WITH BOEING 747 AMM 52-23-00 OPERATIONS CHECK GOOD MESSAGE CLEARED
NO FRM FOUND. EMERGENCY LIGHTS ON ADVISORY FLASHES IN ARM POSITION. REFERENCE LOG PAGE 100010081 EMERGENCY LIGHTS ON ADVISORY FLASHES IN ARM POSITION. PER E50 22-110 AND B747-400 AMM 33-51-04 REMOVED POWER SUPPLY AND APPLIED ELECTRICAL CONNECTORS. REINSTALLED ALL REMOVED SIDEWALL AND CEILING PANELS PER AMM 25-21-02 AND AMM 25-22-03. SEE LOG PAGE 100010082 FOR CARRY OVER ITEM. APPROVED FOR CARRY OVER ITEM 100010082 PER AMM 35-51-04 AND KA E50 22-110. SEE LOG PAGE 100010098 ITEM 100010100. REFERENCE LOG PAGE 100010089: EMERGENCY BATTERY PACK REMOVED AND CAPPED AND STOWED DUE EMERGENCY LIGHTS INTERMITTENTLY COMING ON IN THE ARM POSITION. INSTALLED POWER SUPPLY IAW B747-400 AMM 33-51-04, ALL CHECKS GOOD. REFERENCE WORK ORDER #742026224 FOR ORIGINAL SIGNATURES AND WORK PERFORMED. REFERENCE CARRY OVER ITEM 100010082: EMERGENCY LIGHTING/FERRY FLIGHT. REFERENCE WORK ORDER #742026224 FOR INSTALLATION OF SERVICEABLE POWER SUPPLY AND OPERATIONS CHECK. THIS CLEARS CARRY OVER ITEM 100010082.
LEFT AFT UPPER DECK EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED M7050 BATTERY ASSEMBLY IAW B747-400 AMM 33-51-04. OPERATIONS CHECK GOOD.
EMERGENCY LIGHTS DON'T AGREE WITH COMMANDED SWITCH POSITION. REMOVED AND REPLACED UPPER DECK RIGHT BACK EMERGENCY BATTERY SUPPLY ASSEMBLY IAW B747-400 AMM 33-51-04. ALL CHECKS GOOD.
MULTIPLE UPPER DECK EMERGENCY LIGHTS INOP.
FOUND CRACK INDICTION WITH HFEC OPEN HOLE INSPECTION ON R/H UPPER HOLE OF STRINGER 11 STATION 2598.
L/H WING L/E RIB AT STATION 1048 HAS CRACK AT FASTENER HOLE ON FWD LWR SIDE
L/H WING L/E RIB AT STATION 974 HAS CRACK AT FASTENER HOLE ON FWD LWR SIDE
L/H UPPER DECK DOOR SQUIB TEST LIGHT INOP.
L5604 EMERGENCY LIGHT STA 470 WON`T TURN ON
"BATTERY OK" LIGHT SWITCH ON THE DOOR ANNUNCIATOR MODULE ABOVE RIGHT UPPER DECK EMERGENCY DOOR INOP.
SUPPLEMENTAL INFORMATION: IN SECTION 3.(A) TOTAL CYCLES SHOULD BE 23662 NOT 23622
SUPPLEMENTAL INFORMATION: IN SECTION 3.(A) TOTAL CYCLES SHOULD BE 23662 NOT 23622
RH UPPER DECK DOOR EMERGENCY LIGHT INOP
EQUIPMENT COOLING. REMOVED AND REPLACED FLIGHT DECK. LOW FLOW DETECTOR IAW B747-400 AMM CHAPTER 21-58-02. PERFORMED OPS CHECK IAW 21-58-00. OPS CHECK GOOD. PERFORMED EQUIPMENT COOLING TASK IAW CHAPTER 21-58-00-705-062. OPS CHECK GOOD. AIRCRAFT OK FOR CONTINUED SERVICE.
LEFT WING, WING LANDING GEAR SUPPORT BEAM FUSE PIN HAS CRACK INDICATIONS. CONFIRMED BY HFEC INSPECTION.
UPPER DECK LT DOOR EMERGENCY BATTERY PACK OK, LIGHT INOPERATIVE.
CORROSION ON POTABLE WATER OVER FLOW VALVE DOUBLER.
RIGHT UPPER DECK DOOR EMERGENCY BATTERY OK, LIGHT INOPERATIVE.
RIGHT WING LANDING GEAR SUPPORT BEAM END FITTING HAS CRACK/ CORROSION INDICATION ON AFT SIDE OF FITTING O/B END
L/H WING LANDING GEAR SUPPORT BEAM END FITTING HAS 2 INCH CRACK INDICATION AT APPROX 2 O'CLOCK POS. OF FWD HALF OF FITTING
CORROSION ON POTABLE WATER OVERFLOW VALVE DOUBLER
AFT PIT DOOR BOTTOM ANGLE IS CORRODED IN MULTIPLE SPOTS
EVIDENCE OF CRACK ON L1 DOOR UPPER SILL CENTER SECTION
EVIDENCE OF CRACK AT FASTENER LOCATION AT L/H NWW CUTOUT AFT CORNER
#5 FLAP THRUST BEARING BORE CORRODED
DURING HANDS ON EMERGENCY EQUIPMENT TRAINING, DISCOVERED THAT COCKPIT ESCAPE HATCH WILL NOT OPEN. REMOVED AND REPLACED CREW COMPARTMENT OVERHEAD HATCH IAW B747-400 M/M 52-21-01. CLEARANCES AND RIG HAVE NOT BEEN DISTURBED. OPS AND CHECKS PASS.
UPPER DECK AND STAIRWELL EMERGENCY LIGHTS AT STA 350, 490, 500, AND 540 INOP.
LEFT WHEEL BS 1241.01, LEFT HAND JETTISON FUEL PUMP HAS CORROSION ON WEB AT BONDING WIRE ATTACH POINT.
CRACK NOTED AT BS 2231 FRAME STRAP AT THE TOP AFT FASTENER HOLE BELOW STRINGER 25R. CRACK IS FROM THE HOLE TO THE AFT EDGE OF THE STRAP.
E&E BAY BILGE AREA, BS 406.0, STRINGER 42R HAS DENT IN STRINGER SPLICE ON FREE FLANGE AND WEB AREA.
UPPER DECK, RT SIDE ESCAPE SLIDE DEPLOYED. REMOVED DEPLOYED SLIDE IAW MM 25-68-00, PG 201; SECURED SLIDE IN AFT BULK. INSTALLED RT UPPER DECK SLIDE ASSEMBLY IAW 25-68-01 UP T-STEP 13. SAFETY PINS WILL REMAIN INSTALLED IN BOTH RESERVOIRS. INSTALLED FORWARD STORED GAS RESERVOIR IAW AMM 25-68-02. INSTALLED AFT STORED GAS RESERVOIR IAW AMM 25-68-02. REMOVED AND REPLACED RT UPPER DECK EMERGENCY POWER RESERVOIR. ALL CHECKS GOOD IAW AMM 52-23-13.
L3 DOOR CUTOUT, INSIDE FWD UPPER EDGE AT BS 1265 BETWEEN STR 16 AND STR 17, CRACKED.
RIGHT MED NR 5 UPPER AFT CORNER LOWER HOLE HAS A CRACK INDICATION.
LEFT MED NR 5 UPPER AFT CORNER LOWER HOLE HAS A CRACK INDICATION.
AFT CARGO BAY BS 1620, FRAME IS CRACKED BETWEEN BS 39 AND 40 RT.
PRECAUTIONARY SHUTDOWN NR 4 ENGINE AT 0308Z, FL300 DUE TO LOSS OF OIL QTY, ENGINE WAS STABLE WITH 3 QUARTS OIL AT SHUTDOWN WITH NO OTHER EXCEEDANCES. WINDMILLED 189 MINUTES AT 12 PSI, WINDMILLED 9 MINUTES BELOW 10 PSI. ENGINE 4 WAS SHUTDOWN IAW QRH. PERFORMED ENGINE POST WINDMILLING INSPECTION IAW MM 72-00-00. CLEANED OIL FROM ENGINE. PERFORMED EXAMINATION FOR OIL LEAKAGE IAW MM 79-00-00. FOUND EXCESS OIL ACCUMULATING AROUND AND ON IDG QAD RING. SUSPECT BAD IDG SHAFT SEAL. R & R IDG SHAFT SEAL IAW AMM 24-11-01. OPS AND LEAK CHECK IS GOOD.
ON FINAL, INTERMITTENT AFT CARGO FIRE WARNING, PERFORMED TROUBLESHOOTING IAW FIM 26-16, TASK 894. REMOVED, INSPECTED AND CLEANED AFOLTS CARDS YLPA033 AND YLPA034 AND PERFORMED OPS CHECK. ALL CHECKED GOOD, IAW AMM 26-10-01 AND 26-16-01.
CREW RECEIVED FIRE CARGO AFT DETECTION MESSAGE ABOUT 1500 TO 1000. R & R AFT CARGO AFT BOTTLE IAW AMM 26-23-01.
RIGHT UPPER DECK DOOR WILL NOT ARM. ACCOMPLISHED WITH TASK 52-11-B07, P203. REACTIVATION RT UPPER DECK FLOOR MOUNTED ESCAPE SLIDE IAW MM 25-68-01, P 410. OPS CHECKS PASS IAW MM 25-68-00. ACCOMPLISHED WITH INSPECTION AND CHECKS AT RT UPPER EMERGENCY DOOR IAW MM 52-23-00, P 601. NO DEFECTS NOTED. ACCOMPLISHED WITH CHECKS AT RT UPPER EMERGENCY DOOR TEST PASS IAW MM 52-23-00, P501.
RIGHT UPPER DECK SLIDE BLOWN. R & R RT UPPER DECK DOOR SLIDE IAW MM 25-68-01. OPS AND CHECKED PASSED IAW MM 25-68-02.
BS 570, RBL 45 END OF SEAT TRACK CRACKED AT ATTACH FLANGE.
UPPER DECK DOOR FLIGHT LOCK DAMAGED. REMOVED AND REPLACED FLIGHT LOCK ACTUATOR IAW MM 52-23-08. OPS CHECKED GOOD.
AFT CARGO BS 1660-1680 TORQUE BOX WEB CRACKED.
UPPER DECK FLOORBEAM UPPER TEE AT BS 440 HAS A CRACK INDICATION IN THE FLOOR PANEL ATT. FASTENER HOLE AT RBL 50 ON THE AFT SIDE.
BS 340, RBL 68 UPPER DECK FLOORBEAM HAS CRACK IN FASTENER HOLE COMMON TO FLOORBEAM UPPER TEE AND FRAME INNER CHORD.
BS 800 FRAME AFT INNER CHORD HAS CRACK INDICATION S17R UPPER AFT FASTENER HOLE.
DURING UNLOADING OF AIRCRAFT FUSELAGE RECEIVED DAMAGE TO FUSELAGE AT STATION 2020 TO 2060.
UPPER DECK EMERGENCY EXIT SIGN AT STA 600 MID CEILING HAS A BROKEN STUD.