POLAR AIR CARGO WORLDWIDE INC

Sanction: $24,500 · case closed 2022-06-23

Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 70,044 hrs · 8,331 cycles

F/O FLASHLIGHT TEST BUTTON INOPERATIVE. FOUND FO FLASHLIGHT POSITIONED INCORRECTLY. REPOSITIONED FLASHLIGHT & PERFORMED OPS CHECK IAW AMM 25-64-01. OPS CHECK GOOD. THIS CLEARS DMI 256038. PLACARD REMOVED.

Part: CRADLE — DAMAGED (ZONE 200) · airframe 70,015 hrs · 8,327 cycles

CAPT SEAT FLASHLIGHT BROKEN SEAL. CAPTAIN'S FLASHLIGHT HOLDER WAS FOUND DAMAGED. REMOVED AND REPLACED CAPT SIDE FLASHLIGHT ASSY IAW AMM 25-64-01. OPS CHECKED GOOD.

Part: CONTAINER — TORN (ZONE 200) · airframe 69,911 hrs · 8,313 cycles

SUPERNUMERARY POSITION 3 LIFE VEST BAG RIPPED(<P>REPLACED LIFE VEST AND CHECKS OK FOR SERVICE PER B777 AMM 25-62-01&AMP; IPC 25-62-01-54.</P>)

Part: BATTERY — NO TEST (ZONE 200) · airframe 69,575 hrs · 8,308 cycles

CAPT FLASHLIGHT BATTERY TEST RED. REPLACED CAPT FLASHLIGHT BATTERY IAW AMM 25-64-01, OPS CHK GOOD.

Part: SENSOR — FAULTED (FLAP SKEW) · airframe 63,192 hrs · 9,731 cycles

FLAPS DRIVE MSG IMMEDIATELY AFTER ROTATION BELOW 300 FT. REMOVED AND REPLACED FLAP SKEW SENSOR AND RE-SECURED CONNECTOR D25635J. OPS CHECK GOOD IAW AMM 27-51-01, AIRCRAFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 68,795 hrs · 8,196 cycles

DURING RON CHECK, FOUND MULTIPLE EMERGENCY LIGHTS INOP IN GALLEY AREA(<P>RELAMPED MULTIPLE LIGHTS IN GALLEY AREA PER AMM 33-51-01 &AMP; 33-51-03. OPS CHECK GOOD</P>)

Part: OXYGEN BOX — BROKEN (ZONE 200) · airframe 68,675 hrs · 8,180 cycles

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.

Part: SWITCH — FAULTED (SPEED BRAKES) · airframe 61,781 hrs · 9,589 cycles

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.

Part: TIRE — LEAKING (NR 8) · airframe 61,657 hrs · 9,566 cycles

#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 &AMP; LK CHK OK</P>)

Part: TIRE — WARNING MESSAGE (ZONE 700) · airframe 54,429 hrs · 8,676 cycles

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.

Part: CRADLE — BROKEN (ZONE 200) · airframe 68,224 hrs · 8,117 cycles

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>)

Part: BATTERY — FAULTED (FLASHLIGHT) · airframe 68,561 hrs · 8,123 cycles

CAPT FLASHLIGHT BLINKS RED. REMOVED AND REPLACED CAPT FLASHLIGHT BATTERY IAW AMM 25-64-01. OPS CHK OK.

Part: OXYGEN BOX — INOPERATIVE (ZONE 200) · airframe 68,027 hrs · 8,087 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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.

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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.

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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.

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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.

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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.

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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.

Part: STRING — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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>)

Part: STRINGER SPLICE — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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.

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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>)

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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.

Part: STRINGER — CRACKED (ZONE 200) · airframe 53,396 hrs · 8,529 cycles

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>)

Part: CONTROL PANEL — FAULTED (TCAS) · airframe 67,738 hrs · 7,993 cycles

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>)

Part: POWER SUPPLY — INOPERATIVE (ZONE 700) · airframe 59,389 hrs · 9,241 cycles

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.

Part: OUTFLOW VALVE — FAULTED (ZONE 100) · airframe 59,356 hrs · 9,237 cycles

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.

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

CRACK - FND CROWN STRINGER HAVE CRACK AT STA 780 S-10L.(<P>1. PERFORMED EI NO. T2025A53M-1973 REV 1 SEQUENCE A &AMP; B. 2. ACCOMPLISHED EI NO. T2025A53M-1973 REV 2 &AMP; T2025A53M-1909 REV 1. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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 - &AMP; 142U3440 SH 14 REV B &AMP; 142U3725 SH 10 REV B. 4. ACCOMPLISH EI NO. T2025A53M-1990 REV 2. 5. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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 &AMP; W/S NO. 50661 AND SRM 53-80-03-2R-2 REV 46/ TR:53-152. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 59,144 hrs · 9,208 cycles

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>)