N775SA
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
41 reports on file, 2012-10-23 – 2024-05-29.
Part: BATTERY — INOPERATIVE (C/P FLASHLIGHT) · airframe 66,826 hrs · 7,793 cycles
CAPT EMERGENCY FLSHLIGHT BATTERY DEAD(<P>R/R BATTERY FOR CAPT EMERGENCY FLASHLIGHT PER B777 AMM 25-64-01. OPS CK GOOD</P>)
Part: UNKNOWN — NOISE (L1 DOOR) · airframe 65,633 hrs · 7,605 cycles
L1 DOOR MAKES WHISTLE SOUND IN FLIGHT.(<P>CLEANED AND INSPECTED L1 DOOR SEAL WITH NO DEFECTS NOTED. PERFORMED L1 DOOR LEAK CHECK BY PRESSURIZING AC WITH NO LEAKS NOTED IAW B777 AMM 05-51-24 AND 52-09-01.</P>)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,955 hrs · 7,548 cycles
L1 DOOR EMERGENCY LIGHT OUTSIDE INOP(<P>RELAMPED LIGHT. OPS CK GOOD IAW B777 AMM 33-51-04. P/N 767</P>)
Earlier reports · 2012–2023 · 38 reports
2023
Part: BATTERY — UNKNOWN (UNKNOWN) · airframe 64,928 hrs · 7,491 cycles
CAPT EMERGENCY FLASHLIGHT INOP(<P><SPAN>REPLACED CAPT EMERGENCY FLASH LIGHT BATTERY PACK IAW B777 AMM 25-64-01. OPS CHECK GOOD</SPAN></P>)
Part: FLASHLIGHT — UNKNOWN (UNKNOWN) · airframe 63,842 hrs · 7,336 cycles
EMERGENCY FLASHLIGHT RT SIDE SUPERNUMERARY INOP.(<P>REMOVED AND REPLACED FLASHLIGHT ASSY AND OPS TEST NORMAL PER AMM 25-64-01/501. CLEARED DMI #194286. PLACARDS REMOVED.</P>)
Part: FLASHLIGHT — UNKNOWN (UNKNOWN) · airframe 63,806 hrs · 7,332 cycles
EMERGENCY FLASHLIGHT SHOWS RED LED WHEN PUSH TO TEST. REMOVED AND REPLACED FLASHLIGHT ASSY AND OPS TEST NORMAL PER AMM 25-64-01/501. THIS CLEARED DMI #194286. PLACARDS REMOVED.
2022
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 59,692 hrs · 6,744 cycles
L1 DOOR EMERGENCY FLASHLIGHT INOP ( FLASHLIGHT HOLDER ASSEMBLIES (INCLUDING FLASHLIGHT) - ( MAY BE INOPERATIVE OR MISSING PROVIDED CREWMEMBER HAS A FLASHLIGHT OF EQUIVALENT CHARACTERISTICS READILY AVAILABLE). )(<P>R/R FLASHLIGHT AT L1 DOOR IAW B777 AMM 25-64-01. OPS CHECKS GOOD. DMI 175500 CLOSED.</P>)
Part: ELT — INTERMITTENT · airframe 58,536 hrs · 6,534 cycles
ELT ON ADVISORY MSG INTERMITTENT IN FLT(<P>NO ACTIVE MSG, ELT CHKS OK PER AMM 25-63-01.</P>)
Part: STEERING SYS — WARNING MESSAGE · airframe 57,778 hrs · 6,439 cycles
CONFIG MASTER WARNING MAIN GEAR STEERING ECIAS MSG(TRANSFER TO MDDR #167143 CAT "C" DUE DATE 26 JUN 22 IAW MEL 32-53-01)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D STA 1035 LBL 6.5 FLOOR FITTING FOUND CORRODED(<P>M/D STA 1035 LBL 6.5 FLOOR FITTING CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - LBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1335(<P>M/D - LBL 6.5 FLOOR FITTING STA 1335 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - RBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1413(<P>M/D - RBL 6.5 FLOOR FITTING STA 1413 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - LBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1392(<P>M/D - LBL 6.5 FLOOR FITTING STA 1392 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - RBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1292(<P>M/D - RBL 6.5 FLOOR FITTING STA 1292 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - RBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1270(<P><SPAN>M/D - RBL 6.5 FLOOR FITTING STA 1270 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</SPAN></P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - RBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1335(<P><SPAN>M/D - RBL 6.5 FLOOR FITTING STA 1335 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</SPAN></P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - RBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1392(<P>M/D - RBL 6.5 FLOOR FITTING STA 1392 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · airframe 55,701 hrs · 6,176 cycles
CUSTOMER REQUEST - PLEASE CARRY OUT MDDR 126201 DNET MARK ACCESSMENT AT FX SKIN FWD OF STA 220 BTN S-34R TO S-36R(<P>FX - RH SKIN DENT 1 LOCATED AFT OF BS 220.5 AND DENT 2 LOCATED AFT OF BS 228.5, BOTH DENTS BTN S-34R TO S-36R INTERIM REPAIRED AS PER RI NO.RI-53-11-15337 REV A</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - LBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1350(<P>M/D - LBL 6.5 FLOOR FITTING STA 1350 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - RBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1434(<P>M/D - RBL 6.5 FLOOR FITTING STA 1434 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - LBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1292(<P>M/D - LBL 6.5 FLOOR FITTING STA 1292 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · airframe 55,701 hrs · 6,176 cycles
LHW O/B T/E FLAP TE LWR SKIN MID AREA FOUND DELAMINATION(<P>PERFORMED COMPOSITE REPAIR AT LHW O/B T/E FLAP TE LWR SKIN DELAMINATION AREA AS PER SRM 51-70-04 REPAIR 1</P>)
Part: NONE — NONE · airframe 55,701 hrs · 6,176 cycles
RHW O/B T/E FLAP TE LWR SKIN MID AREA FOUND DELAMINATION(<P>PERFORMED COMPOSITE REPAIR AT <SPAN>RHW O/B T/E FLAP TE LWR SKIN DELAMINATION AREA AS PER SRM 51-70-04 REPAIR 1</SPAN></P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - RBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1310(<P>M/D - RBL 6.5 FLOOR FITTING STA 1310 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - RBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1350(<P>M/D - RBL 6.5 FLOOR FITTING STA 1350 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - LBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1434(<P><SPAN>M/D - LBL 6.5 FLOOR FITTING STA 1434 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</SPAN></P>)
Part: RING — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
FX - LAVATORY SERVICE PAN BTN STA 755.5 AND STA 772 STR 42R AND STA 44R FOUND CORROSION(<P>FX - LAVATORY SERVICE PEN BTN SKIN DOUBLER RING REPLACED AS PER SRM 51-10-02 AND NEW DOUBLER RING INSTALLED AS PER SRM 51-40-02</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - RBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1371(<P><SPAN>M/D - RBL 6.5 FLOOR FITTING STA 1371 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</SPAN></P>)
Part: NONE — NONE · airframe 55,701 hrs · 6,176 cycles
CUSTOMER REQUEST - PLEASE CARRY OUT MDDR 126200 DENT MARK ACCESSMENT AT FX SKIN FWD OF BS 228 BTN S-34R TO S-36R(<P>FX - RH SKIN DENT 1 LOCATED AFT OF BS 220.5 AND DENT 2 LOCATED AFT OF BS 228.5, BOTH DENTS BTN S-34R TO S-36R INTERIM REPAIRED AS PER RI NO. RI-53-11-15337 REV A</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - LBL 6.5 FLOOR FITTING FOUND CORROSION AT STA 1270(<P>M/D - LBL 6.5 FLOOR FITTING STA 1270 CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
Part: NONE — NONE · corrosion level 2 · airframe 55,701 hrs · 6,176 cycles
M/D - STA 1035 RBL 6.5 FLOOR FITTING FOUND CORROSION(<P>M/D - STA 1035 RBL 6.5 FLOOR FITTING CORROSION AREA BLENDED OUT AND REPROTECTED AS PER SRM 53-00-52-1A-3</P>)
2019
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,794 hrs · 4,381 cycles
AIRCRAFT GROUNDED. LT DR1 BATTERY PACK CAPACITY CHECK FOUND EMERGENCY LIGHTS AND SIGNS STAY ON LESS THAN 15 MINUTES. LT DR1 BATTERY PACK REPLACED AND TEST OK AS PER AMM 33-51-06.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,794 hrs · 4,381 cycles
AIRCRAFT GROUNDED. RT DR1 BATTERY PACK CAPACITY CHECK FOUND EMERGENCY LIGHTS AND SIGNS STAY ON LESS THAN 15 MINUTES. RT DR1 BATTERY PACK REPLACED AND TEST OK AS PER AMM 33-51-06.
Part: SKIN — CRACKED (LE SLAT) · airframe 40,794 hrs · 4,381 cycles
AIRCRAFT GROUNDED. RT NR 8 SLAT ISS 196 SKIN CRACKED. SKIN REPAIRED.
Part: SKIN — CRACKED (LE SLAT) · airframe 40,794 hrs · 4,381 cycles
AIRCRAFT GROUNDED. LT NR 7 SLAT INBD L/E SKIN CRACKED AT ISS 196. SKIN REPAIRED.
Part: SKIN — CRACKED (LE SLAT) · airframe 40,794 hrs · 4,381 cycles
AIRCRAFT GROUNDED. RT NR 8 SLAT SKIN CRACKED AT ISS 186. SLAT SKIN REPAIRED.
2014
Part: APU — SMOKE · airframe 18,519 hrs · 2,090 cycles
DURING START UP OF APU, SMOKE ENTERED COCKPIT. APU OIL QTY DROPPED FROM 7.0 TO 1.2 WITHIN 10 MINUTES.
2013
Part: TIRE — DELAMINATED (LT MLG) · airframe 13,104 hrs · 1,540 cycles
LEFT GEAR, INBD MIDDLE TIRE DELAMINATED ON LANDING. R & R LT GEAR INBD MIDDLE TIRE ASSY IAW AMM 32-45-01.
Part: POWER SUPPLY — FAILED (CABIN) · airframe 12,039 hrs · 1,437 cycles
EMERGENCY LIGHTS FOUND AT RIGHT DOOR EXTERIOR EMERGENCY LIGHT INOP. TROUBLESHOT TO RIGHT DOOR EMERGENCY POWER SUPPLY. REMOVED AND REPLACED POWER SUPPLY. OPS CHECK OK IAW A/M/M 33-51-06.
Part: BUSHING — GALLED (RT MLG) · airframe 10,904 hrs · 1,325 cycles
AFTER VISUAL INSPECTION, RT MLG FOUND HAS A GALLED BUSHING ON RETRACTION TRUNNION SLEEVE. FOUND THE AREA OF THE PITTING ON THE SLEEVE. AREA IS WIDTH APPROX 2 CM AROUND THE SLEEVE. PERFORMED IAW RECOMMEND TO REMOVE THE BRONZE TRANSFER WITH SCOTCHBRITE , THE CORROSION ON SLEEVE AND BUSHING WERE NOT FOUND. ASSEMBLED USING A LIGHT COAT OF GREASE AND THEN LUBRICATE THE JOINT WITH MIL-PRF-32014 GREASE; ENSURE THERE IS SQUEEZE OUT AT LEAST SIX LOCATIONS ON THE AFT SIDE AND 2 ON THE FWD SIDE OF THE RETRACT ARM. LUBRICATE THIS IS JOINT EVERY 30-45 DAYS WITH MIL-PRF-32014 GREASE. DISASSEMBLE AND INSPECT THE PITTED AREA AT THE NEXT "C" CHECK AND REPORT FINDING TO MFG FOR FURTHER DISPOSITION.
2012
Part: SIGN — INOPERATIVE (CABIN) · airframe 9,600 hrs · 1,193 cycles
LEFT DOOR AFT INTERIOR EMERGENCY EXIT SIGN INOP. TRANSFER TO DI 2789 PER MEL 33-51-01. PLACARD INSTALLED.