POLAR AIR CARGO WORLDWIDE INC
Also recorded as: POLAR AIR CARGO WORLDWIDE INC
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
No NTSB accidents or incidents linked to this operator.
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
9,327 reports on file — showing most recent 50.
DURING RON CHECK, FOUND MULTIPLE EMERGENCY LIGHTS INOP IN GALLEY AREA(<P>RELAMPED MULTIPLE LIGHTS IN GALLEY AREA PER AMM 33-51-01 & 33-51-03. OPS CHECK GOOD</P>)
CAPTAIN O2 MASK PRESS TO TEST AND RESET TAB IS BROKEN. SWAPPED CAPT & 1ST OBSERVER O2 BOX PER 777 AMM 35-11-18 FOR DISPATCH. PLACED 1ST OBSERVER SEAT & ASSOCIATED EQUIPMENT ON MEL. LP 1940127 M2: REMOVED AND REPLACED 1ST OBSERVER'S O2 BOX IAW AMM 35-11-18. OPS CHECK & LEAK CHECKED GOOD IAW IPC 35-11-18-01.
REJECT AT 62 KTS FOR CONFIG WARNING 421.6 KG. SPEED BRAKE ARMED EICAS AND COULD NOT BE RESET AFTER REJECT. VERIFIED INTERNAL SHORT IN SPEED BRAKE ARM SWITCH IAW WDM 32-41-31 & AMM 20-11-00. R & R SPEED BRK ARM SWITCH IAW AMM 27-62-10. OPS CHECK NORMAL. THIS CLEARS DMI 251286, PLACARD REMOVED.
#8 TIRE PRESSURE ADVISORY MESSAGE - TIRE PRESSURE DECREASING.(<P>FOUND #8 MAIN TIRE PRESSURE LOW. REMOVED AND REPLACED #8 MAIN WHEEL ASSY PER AMM 32-45-01. ALSO, REPLACED #7 MAIN WHEEL ASSY PER AMM 32-45-01. OPS & LK CHK OK</P>)
TIRE PRESSURE EICAS & STS MSG OCCURRED AFTER T/O. PERFORMED CONDITIONAL INSPECTION ON MLG 11 & 12 AXLE IAW AMM 05-51-25 (1-8) & AMM 32-45-04-206-011, NO DAMAGE NOTED TO RH BODY GEAR. BRAKE SYS TEST PASS. NO LEAKS NOTED. OPS CHK GOOD AT THIS TIME. R & R MLG 11 & 12 TIRE WHEEL ASSY IAW AMM 32-45-01 & IPC 32-45-03-07. OPS & LK CHK OK.
F/O FLASHLIGHT HOLDER CLIP BROKEN(<P>REPLACED F/O'S FLASHLIGHT AND HOLDER PER B777 AMM 20-11-00, OPS SERVICEABLE PER B777 AMM 25-64-01.</P>)
CAPT FLASHLIGHT BLINKS RED. REMOVED AND REPLACED CAPT FLASHLIGHT BATTERY IAW AMM 25-64-01. OPS CHK OK.
CPT OXYGEN MASK PANEL OXYGEN ON TAB INOPERATIVE - WORN OUT(<P>PERFORMED OXYGEN MASK STOWAGE BOX CHECK #5. NO DAMAGE FOUND SO STOWAGE BOX RESTOWED OK PER AMM 35-11-18/201</P>)
CRACK DAMAGE ON THE STRINGER S-8R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50870 (SRM 53-80-03-2R-2 REV: 47) JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50869 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-6R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50868 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-5L, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50867 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-2L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50876 (SRM 53-60-03-2R-8 REV: 47) AND EI T2026A53M-087 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-20R, AT AFT SIDE OF STA 2360. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S NO: 50872 (SRM 53-80-03-2R-3 REV 47). INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG NO: 148U2377 SHEET 24 REV A, SHEET 25 REV A. JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S 50877 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-7L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50878 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER S-9L, AT STA 930. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S NO: 60010 (SRM 53-20-03-2R-1 REV 47) AND EI NO: T2026A53M-050 REV 1. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG 142U0920 SHEET 37 REV, DWG 142U3725 SHEET 14 REV C. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK DAMAGE ON THE STRINGER AND STRINGER SPLICES S-10R, AT FWD AND FWD SIDE OF STA 2180. REPAIR DAMAGE AREA IAW W/S NO: 50871 (SRM 53-60-03-2R-3 REV: 47) AND EI NO: T2026A53M-076 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.
CRACK DAMAGE ON THE STRINGER S-3L, AT AFT SIDE OF STA 2360.(<P>1. REPAIR DAMAGE AREA IAW EI NO: T2026A53M-034 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
FOUND EXTERIOR EMER LT (L6690) INOP. PERFORM WIRING CONTINUITY CHECK AND SYSTEM TROUBLESHOOTING IAW WDM 33-51-72 REV 35, FOUND M5168 BATTERY FUNCTION FAILED. PERFORM BATTERY REPLACEMENT AT M5168 IAW AMM 33-51-04-900-803 REV 49. CONDITION CHECK NORMAL AND PERFORM POWER SUPPLY TEST, RESULT WAS SATISFACTORY.
CRACK DAMAGE ON THE STRINGER S-5L, AT AFT SIDE OF STA 2360.(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. 2. REPAIR DAMAGE AREA IAW EI NO: T2026A53M-033 REV 1. 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG NO: 148U2377 SHEET 22 REV A. 4. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
EICAS TRANSPONDER R STATUS MSG, EICAS TRANSPONDER L STATUS MSG, EICAS TCAS STATUS MSG. R & R TCAS CONTROL PANEL IAW B777 AMM 34-53-02. OPS CHECK GOOD.</P>)
MULTIPLE GEAR MESSAGES INCLUDING GEAR MONITOR, GEAR DISAGREE, AND GEAR DOOR AND GEAR WOULD NOT RETRACT. R & R PSEU & PERFORMED CMC GND TEST & ZONAL INSPECTION OF NOSE LANDING GEAR & NOSE LANDING GEAR DOOR IAW AMM 32-09-03/401 & AIPC 32-61-01-01, OPS CHK GOOD. NO FURTHER DEFECTS NOTED.
AT FLT 310, CABIN PRESSURE BECAME UNCONTROLLABLE. OUTFLOW VALVES WERE INDICATING FULLY CLOSED. CABIN ALTITUDE WAS CLIMBING 200 FPM.(<P>COMPLETED THE FOLLOWING CHECKS PER BOEING SR: CABIN SYSTEM CONTROL PRESSURE TEST AMM TASK 21-31-00-735-011 AND EXCESSIVE CABIN PRESSURE LEAKAGE TEST PER AMM 05-51-08-702-001. PARTS REPLACED. REF AMM 21-26-15/401. R & R FWD CARGO OVERBOARD VALVE.
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880, S-8R.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50668 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 980+15, S-8L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50670 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 882, S-8L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50659 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 892, S-8L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50659 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50659 ATTACH WITH T/C: 11454336. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880, S-10R.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50669 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 866, S-10R.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50669 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50669 ATTACH WITH T/C: 11454311 (098) 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 840, S-11L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
FOUND STRINGER CRACK ON S-11L STA 885. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S 50664 ATTACHING WITH THE T/C 11454296. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 860, S-11L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50664 ATTACHING WITH THE T/C 11454296. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT AFT OF STA 1660, S-10R.(<P>1. ACCOMPLISHED EI NO. T2025A53M-1965 REV 1. 2. ACCOMPLISHED EI NO. T2025A53M-1965 REV 2. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880 S-10L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50671 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 780 S-10L.(<P>1. PERFORMED EI NO. T2025A53M-1973 REV 1 SEQUENCE A & B. 2. ACCOMPLISHED EI NO. T2025A53M-1973 REV 2 & T2025A53M-1909 REV 1. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 760 S-8L.(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 46. 2. PERFORM EI NO. T2025A53M-1990 REV 1 SEQUENCE B. 3. INSTALL AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 46 AND DWG NO. 142U3625 SH 13 REV - & 142U3440 SH 14 REV B & 142U3725 SH 10 REV B. 4. ACCOMPLISH EI NO. T2025A53M-1990 REV 2. 5. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK BETWEEN STA 2177 AND STA 2185 S-8R.(<P>1. PERFORM STRINGER REPAIR IAW W/S NO. 50672 AND SRM 53-60-03-2R-3 REV 46/ TR: 53-154. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER CRACK FRAME FWD SIDE BETWEEN STA 1957 AND STA 1966 S-9R.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50674 AND SRM 53-60-03-2R-4 REV 46/ TR: 53-155. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT AFT OF STA 2180, S-11R.(<P>1. PERFORMED STRINGER REPAIR IAW W/S NO. 50658 AND SRM 53-60-03-2R-3 REV 46/ TR: 53-154. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FOUND STRINGER HAVE CRACK AT FWD OF STA 2598 S-6R.(<P>1. REMOVED FASTERNERS IAW SRM 51-40-02-0G-0 REV 46. 2. REPAIR STRINGER IAW W/S NO. 50660 AND SRM 53-80-03-2R-2 REV 46/ TR:53-152. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FOUND STRINGER HAVE CRACK AT FWD OF STA 2598 S-8L.(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 46. 2. REPAIR STRINGER IAW SRM 51-40-02-0G-0 REV 46 & W/S NO. 50661 AND SRM 53-80-03-2R-2 REV 46/ TR:53-152. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
CRACK - FND CROWN STRINGER CRACK BETWEEN STA 2177 AND STA 2185 S-10R.(<P>1. PERFORM STRINGER REPAIR IAW W/S NO. 50673 AND SRM 53-60-03-2R-3 REV 46/ TR:53-154. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
FOUND CROWN STRINGER HAVE CRACK AT STA 920, S-9L.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50666 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
FOUND CROWN STRINGER HAVE CRACK AT STA 905, S-9L.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50666 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50666 ATTACH WITH T/C:11454301 (095). 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND FUSELAGE CROWN STRINGER HAVE CRACK AT STA 780, S-12R.(<P>1. REPAIR STRINGER AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 793, S-12R.(<P>1. REPAIR STRINGER CRACK AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50663 ATTACH WITH T/C:11454292. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 746, S-12R.(<P>1. REPAIR STRINGER CRACK AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50663 ATTACH WITH T/C:11454292. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
CRACK - FND CROWN STRINGER HAVE CRACK AT STA 860, S-9L.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50667 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
FOUND RH WLG ALTERNATE EXTENSION ACTUATOR FUNCTION ABNORMAL.(<P>1. REPLACED RH WLG ALTERNATE EXTENSION ACTUATOR IAW AMM 32-36-01-004-001 REV 48A AND AMM 32-36-01-404-009 REV 48A. 2. PERFORMED R/H WLG ALTERNATE EXTENSION TEST IAW AMM 32-36-00-705-009 REV 48A, TEST RESULT WAS PASS. 3. CONDITION CHECK SATISFACTORY.</P>)
Linked aircraft
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