N777SA
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (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
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.
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>)
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>)
PORTABLE FLASHLIGHT CAPTAINS SIDE DOES NOT TEST.(<P>PERFORMED OPERATION TEST IAW AMM 25-64-01. GREEN LIGHT SHOWED UP, ITS STATUS IS THE SAME AS THE OTHER TWO, MDDR 233689 WAS CLEARED. A/C BACK TO NORMAL.</P>)
F/O FLASHLIGHT WILL NOT TEST.(<P>R/R F/O FLASHLITE ASSY IAW AMM 20-11-00 AND AMM 25-64-06. OPS CHECK GOOD. DMI 229885 CLOSED.</P>)
SUPPERNUMERARY FLASH LIGHT WILL NOT TEST.(<P>R/R RH SUPERNUMERARY FLASHLIGHT ASSY IAW AMM 20-11-00 AND 25-64-06. OPS CHECK GOOD. DMI 229884 CLOSED.</P>)
OPEN HOLE INSPECTION CARRIED OUT AS PER EO CARD: 7757A025 PART 1, ON LHW UPPER SKIN COMMON TO MLG TAB OUT FASTENER HOLES 0-6 AND FOUND HOLE #5 WITH CRACK INDICATION APPROX 0.030" INCHES LENGTH, VIEW LOOKING DOWN AFT AT 6 O'CLOCK &11 O'CLOCK POSITION.(<P>&NBSP;CRACKED FASTENER HOLE #5 ON LHW UPPER SKIN AREA REPAIRED AS PER EN #074-25 REV 0. REPAIR CATEGORIZED AS CAT B PERMANENT REPAIR REQUIRES REPETITIVE INSPECTION. REPAIR CLASSIFIED AS MAJOR REPAIR. INSPECTION REQUIREMENTS AND LIMITATIONS: FIRST AND SECOND STAGE APPROVAL (APPROVAL FOR STATIC STRENGTH AND INSPECTION THRESHOLD) THE INSPECTION THRESHOLD FOR THIS REPAIR IS PROVIDED BUT FULL COMPLIANCE TO 14CFR 25.571 AND 26.43 (D) HAS NOT BEEN EVALUATED. A NEW FAA APPROVAL WHICH CONTAINS THE INSPECTION REQUIREMENTS MUST BE ISSUED FINDING COMPLIANCE WITH 14 CFR 26.43 (D) AND 25.571 PRIOR TO THE INSPECTIONTHRESHOLD OF 10,200 TOTAL ACCUMULATED AIRPLANE FLIGHT CYCLES OR 80,900 TOTAL FLIGHT HOURS, WHICHEVER OCCURS FRIST. IF NEW FORM FINDING FULL COMPLIANCE TO 14 CFR 26.43 (D) AND 25.271 IS NOT ISSUED BY THE THRESHOLD, THE AIRWORTHINESS CERTIFICATE OF THE AIRPLANE WITH THIS REPAIR IS NO LONGER CURRENT AFTER THE TIME. THIS APPROVAL DOES NOT SUPERSEDE OR TERMINATE ANY AD, MPD OR OPERATOR MAINTENANCE INSPECTIONS OR REQUIREMENTS.
OPEN HOLE INSPECTION CARRIED OUT AS PER EO CARD: 7757A025 PART 2, ON RHW UPPER SKIN COMMON TO MLG TAB OUT FASTENER HOLES 0-6 AND FOUND HOLE NO.5 WITH CRACK INDICATION APPROX 0.030" INCHES LENGTH, VIEW LOOKING DOWN AFT AT 6 O'CLOCK & 1 O'CLOCK POSITION. CRACKED FASTENER HOLE #5 ON RT WING UPPER SKIN AREA REPAIRED IAW EN #075-25 REV 0. REPAIR CATEGORIZED AS CAT B PERMANENT REPAIR REQUIRES REPETITIVE INSPECTION. REPAIR CLASSIFIED AS MAJOR REPAIR. INSPECTION REQUIREMENTS AND LIMITATIONS: FIRST AND SECOND STAGE APPROVAL (APPROVAL FOR STATIC STRENGTH AND INSPECTION THRESHOLD) THE INSPECTION THRESHOLD FOR THIS REPAIR IS PROVIDED BUT FULL COMPLIANCE TO 14CFR 25.571 AND 26.43 (D) HAS NOT BEEN EVALUATED. A NEW FAA APPROVAL WHICH CONTAINS THE INSPECTION REQUIREMENTS MUST BE ISSUED FINDING COMPLIANCE WITH 14 CFR 26.43 (D) AND 25.571 PRIOR TO THE INSPECTIONTHRESHOLD OF 10,200 TOTAL ACCUMULATED AIRPLANE FLIGHT CYCLES OR 80,900 TOTAL FLIGHT HOURS, WHICHEVER OCCURS FRIST. IF NEW FORM FINDING FULL COMPLIANCE TO 14 CFR 26.43 (D) AND 25.271 IS NOT ISSUED BY THE THRESHOLD, THE AIRWORTHINESS CERTIFICATE OF THE AIRPLANE WITH THIS REPAIR IS NO LONGER CURRENT AFTER THE TIME. THIS APPROVAL DOES NOT SUPERSEDE OR TERMINATE ANY AD, MPD OR OPERATOR MAINTENANCE INSPECTIONS OR REQUIREMENTS.
CAPTAIN OXYGEN MASK MIC INTERMITTENT WHEN USING INTERCOM SWITCH ON AUDIO PANEL AND GLARESHIELD MIC SWITCH.(<P>REPLACED CAPTAIN'S MASK WITH FIRST OBS MASK PER AMM 35-11-18. OPS CHECK AND LEAK CHECK GOOD. OBS SEAT & ASSOCIATED EQUIPMENT PLACED ON DMI 224831 PER MEL 25-11-02-01B CAT A. R/R O2 MASK STOWAGE BOX IAW AMM 35-11-18. OPS TEST GOOD. DMI 224831 CLOSED.</P>)
FO'S FLASHLIGHT TEST GREEN LIGHT FAILED TO ILLUMINATE.(<P>F/O'S FLASHLIGHT BATTERY PACK REINSTALLED & TEST OK PER AMM 25-64-01.</P>)
DUE TO #1 ENG HIGH OIL CONSUMPTION, REMOVED #1 ENG BACKUP GENERATOR IAW AMM 24-25-01(<P>REMOVED AND REPLACED #1 ENG ACCESSORY GEARBOX SEAL OIL FACE SEAL AND MATING RING AT BACKUP GEN PER B777 AMM 72-64-01-420-801-H01. RE-INSTALLED #1 ENG BACKUP GENERATOR PER B777 AMM 24-25-01-000-804-001. LEAK AND OPS CHECK REQUIRED. SEE ITEM M7.</P> / <P>LOG PAGE 1702288 - ITEM M7 CONT - PERFORMED HIGH POWER ENG RUNS PER AMM 71-00-00. OPS CHECK & LEAK CHECK GOOD PER AMM 24-25-01. P/N OFF - 2205M8301. NO S/N.</P>)
REJECTED TAKEOFF DUE TO CONFIG GEAR STEERING 20 KNOTS .(<P>MAT TEST PER FIM 31-78130 & 31-51-00-810-892, MSG CLEARED.</P>)
FO OXY MASK MIC HOWL BOTH SPEAKERS.(<P>REPLACED FO OXY MASK STOWAGE BOX AND TO OXY MASK MIKE CHECKED NORMAL PER AMM 35-11-18/401.&NBSP;</P>)
CAPT EMERGENCY FLASHLIGHT WEAK.(<P>R/R FLASHLIGHT BATTERY PER AMM 25-64-01. OPS CHECK NORMAL.</P>)
F/O FLASH LIGHT NOT TESTING GREEN(<TABLE STYLE="WIDTH: 748PX; HEIGHT: 30PX;" BORDER="0" WIDTH="163" CELLSPACING="0" CELLPADDING="0"> / <TBODY> / <TR> / <TD CLASS="XL63" DIR="LTR" STYLE="HEIGHT: 33.75PT; WIDTH: 747PX;" HEIGHT="45">RESET & OPERATION CHECK OK AT F/O FLASH LIGHT PER AMM 25-64-01</TD> / </TR> / </TBODY> / </TABLE>)
CAPT SIDE FLASHLIGHT INOP.(<P>REMOVED AND REPLACED CAPT FLASHLIGHT ASSY. OPS CHECKED IAW AMM 25-64-01. THIS CLEARS MDDR 185482, PLACARDS REMOVED.</P>)
CAPT OXYGEN MASK EMERGENCY TEST SELECTOR IS LOOSE(<P>PERFORMED MASK AND DEMAND REGULATOR INSPECTION IAW AMM 35-11-18-210-801. OPS CHK NORMAL</P>)
FO SLIDE WINDOWS HAD LOUD NOISE FROM LOWER LEFT PORTION OF WINDOW, HAPPENED IN CLIMB THROUGH 24,000FT CONTINUED TO 30,000FT. STOPPED DESCENDING THROUGH 23,000FT STEP CLIMB BACK TO 30,000FT WITH NOISE RETURNING BUT QUIETER THAN PREVIOUS EVENT. NO EICAS INDICATORS. NO PRESSURIZATION INDICATORS.(FOUND A TEAR IN FO R2 WINDOW SEAL UPON INSPECTION. R/R R2 WINDOW SEAL IAW B777 AMM 56-11-13 PN: SF15-141T487-10)
2 X O/H EMRG LTS INOP IN GALLEY AREA PER LRA RAMP INSP.(RELAMPED O/H GALLEY EMERG LTS IN CTR & L/H POS IAW AMM 33-51-03, NOW OPS SATIS.</P>)
2X O/H EMERG LTS INOP IN GALLEY AREA PER LBA RAMP INSP. RELAMPED O/H GALLEY EMERG LTS IN CTR & LH POS IAW AMM 33-51-03, OPS CHECK GOOD</P>)
EMERGENCY LIGHT NOT ON (L1 DOOR LWR FWD)(<P>REMOVED AND REPLACED WITH NEW LAMP AND THEN OPERATION CHECKED NORMAL IAW AMM 35-51-00.</P>)
2 EACH AREA EMERGENCY LIGHTS INOP.(<P>RELAMPED BULBS IAW AMM 33-51-03. OPS CHECK GOOD&NBSP;</P>)
AIRCRAFT GROUNDED, UNABLE TO CONTROL CABIN ALTITUDE PRESSURIZATION. CABIN PRESSURE OUTFLOW VALVE ASSEMBLY REPLACED, IAW AMM 21-31-03-000-812-002/21-31-03-400-811-002. TEST PASSED AND STATUS CLEARED.
AIRCAFT GROUNDED. W/O 63155 - EMERGENCY LIGHT BATTERY PACK M33093 REPLACED IAW MM 33-51-06-960-802. TEST SATIS.
AIRCAFT GROUNDED. W/O 63155 - EMERGENCY LIGHT BATTERY PACK M33094 REPLACED IAW MM 33-51-06-960-802. TEST SATISFACTORY.
RT ENGINE INLFIGHT SHUTDOWN, STARTED NORMALLY. IAW FIM 73-22 THE HMU WAS REPLACED. THE AIRCRAFT GROUNDED. FDE RECEIVED MAINT MSG 73-34802. FOLLOWED FIM 73-22 TASK 849 ITEM C (1) TO (7) ACCOMPLISHED AND FOUND GOOD. NO FAULT NOTED IAW FIM 73-22 TASK 849. REPLACED THE RT HMU. LEAK AND OPS CHECKED GOOD IAW AMM 73-21-14. RT ENG BOROSCOPE INSPECTION ON HPC STAGE 1-8 IAW AMM 72-00-00-290-803-1101. FOUND HPC STAGE 1 - 3 STAGE 5 - 8, NO DEFECTS NOTED. HPC STAGE 2 FOUND 2. FOUND ONE BLADE LE TIP CORNER NICKED. DEFECT ACCEPTED IAW AMM SUBTASK T-2-0000-220-H01 PAGE11 (9) ITEM 1. NO ACTION REQUIRED. HPC STAGE 4 #36 BLADE LE TIP CORNER NICK .016MM FROM THE TIP 11.6MM. DEFECT IS PERMITTED DEFERRAL TO REMOVAL OF DAMAGE FOR UP TO 15 CYCLES AS PER AMM SUBTASK 72-00-00-290-002-H01 ITEM B AND ITEM 2. LP 098435: DEFERRED RT ENG HPC STAGE 4 #36 BLADE PER AMM 72-0000 FOR 15 CYCLES. ITEM TRANSFERRED TO MDDR 094383. EXPIRES 3154 CYCLES. LP: MC REQUEST REPLACE RT ENG FUEL FILTER. RT ENG FUEL FILTER REPLACED AND LEAK CHECK C/OUT. NO LEAK NOTED PER AMM 73-11-02. LP 098436: MC REQUEST C/OUT RT ENG SCAVENGE OIL SCREEN AND CHIP DETECTOR INSPECTION. RT ENG SCAVENGE OIL INLET SCREEN AND CHIP DETECTORS INSPECTED IAW AMM 79-21-04.
MAIN GEAR STEERING FAULT. AIRCRAFT GROUNDED. OPEN
AC HAD POSSIBLE BRAKE FIRE AT LEFT OB WHEEL/BRAKE ASSY AREA. FOUND AREA ON IB SIDEWALL OF TIRE, SHOWED EVIDENCE OF FIRE, RUBBER WAS CHARRED IN AREA FROM WHEEL RIM AND OUT TO TREAD AREA ABOUT 3 INCHES IN LENGTH, 1.5 INCHES WIDE LIKE A WATER TEAR DROP. OPERATOR NOTIFIED AND PROVIDED WITH BUILT UP WHEEL AND TIRE ASSY. THE MFG SAID CAUSE WAS WHEN WHEEL ASSY WAS CLEANED FOR INSP WHOLE WHEEL ASSY WAS SUBMERGED IN CLEANING FLUID. THIS ALLOWED LAMINATED HEAT SHIELD TO COLLECT CLEANING FLUID. WHEN UNIT WAS NEXT INSTALLED ON AC THE HEAT FROM THE BRAKES DRIED OUT THE LAM SHIELD, AFTER NR OF LANDINGS, ALLOWING HOT BRAKE TO IGNITE LAM HT SHIELD. INSTALLED A REPLACEMENT ASSY. DEFECTIVE WHEEL ASSY WAS RETURNED TO OPER.
AFTER THREE LANDINGS WITH FULL STOPS (CHECK AIRMEN RIDE), ON TAXI IT WAS OBSERVED BY ANOTHER AIRCRAFT THAT FLAMES WERE COMING FROM THE NR 1 MAIN WHEEL. GROUND WAS NOTIFIED AND ALERTED THE CREW WHO IMMEDIATELY STOPPED. THE CREW OBSERVED A SMALL BLUISH FLAME EMANATING FROM A LIGHTNING HOLE OF THE WHEEL. AN AIRCRAFT FIRE EXTINGUISHER WAS USED TO EXTINGUISH THE FLAME. LOCAL MAINTENANCE DETERMINED THE AIRCRAFT SAFE TO MOVE FOR FURTHER INVESTIGATION. INVESTIGATION REVEALED NO CONCLUSIVE INFORMATION AS TO THE CAUSE OF IGNITION AND THE COMBUSTION SOURCE FOR SUSTAINING THE FIRE. THE LANDING GEAR, BRAKE, WHEEL WELL AND SURROUNDING STRUCTURE WERE INSPECTED WITH NO CONCLUSIVE EVIDENCE. THE WHEEL/TIRE ASSY WAS REMOVE
LINE ASSEMBLY FOUND KINKED AT LOWER END. THIS PART IS AN ENGINE MAIN FUEL LINE (FLEXIBLE). THIS LINE MUST BE DISCONNECTED IN ORDER TO ALLOW CERTAIN DEFUELING OPERATIONS. CARE MUST BE EXERCISED WHEN DISCONNECTING THE LOWER FITTING; OTHERWISE, KINKING WILL OCCUR RESULTING IN DIMINISHED FUEL SUPPLY TO THE ENGINE. SUBMITTER SUGGESTS MECHANICS SHOULD BE ADIVSED TO USE MORE CARE WHENEVER THIS LINE ASSEMBLY IS DISTURBED. ACFT TT 2,952 HRS.
THIS PART FOUND BROKEN AT STOPS AFTER PILOTS REPORTED MAIN DOOR ASSY 'LOOSE' WHEN OPEN AND PERSON STEPS ON DOOR STEPS (UNSTABLE). CAUSE HAS BEEN DETERMINED AS RAPID OR HARSH OPERATION OF THE DOOR LOCKING HANDLES WHEN CLOSING THE DOOR. SUBMITTER SUGGESTS CARE BE EXERCISED, WHEN OPERATING THE DOOR, BY FLIGHT CREWS AND GROUND PERSONNEL.