N708DN
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.
42 reports on file, 2009-11-07 – 2020-08-13.
Part: SLIDE — MISSING (L4 DOOR) · airframe 54,769 hrs · 4,881 cycles
4L DOOR SLIDE MISSING. INSTALLED SLIDE ASSEMBLY. SYSTEM OPERATION IS NORMAL. MCO/PLAC REMOVED.
Part: SKIN — CRACKED (BS 1024-1035) · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 7108, L/P 1476890) DURING ACCOMPLISHMENT OF HFEC INSPECTION ON LH UNDERWING LONGERON FUSELAGE SKIN, FOUND CRACK INDICATION AROUND 02 EA FASTENER HOLES AT STA 1024 AND STA 1035, STR37L, APPROX 1.5" IN LENGTH EACH. CORRECTIVE ACTION: AREA REPAIR AND MODIFICATION PERFORMED I.A.W DELTA PRI 584527-14AD REV 1 ISSUE DATE: 21 JAN 2020. PENDING FINAL ER/A.COMPARED WITH FINAL ER/A 584527-14AD REV ORIGINAL FOUND COMPLIED WITH. ACCOMPLISHED DELTA ER/A 584527-14AD REV ORIGINAL TIME CONTROLLED ITEMS SECTION I; REFER TO LOG PAGE 1476272 FOR TIME CONTROLLED ITEMS SECTION II.
Part: LONGERON — CRACKED · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 7108, L/P 1476723) DURING ACCOMPLISHMENT OF HFEC OPEN HOLE INSPECTION ON LH UNDERWING LONGERON FRONT SPAR LOWER CHORD, FOUND CRACK INDICATION ON LOWER ROW O/B FASTENER HOLE AS MARKED. CORRECTIVE ACTION: REPAIR PERFORMED AS PER B777-200 SRM 57-10-10-2R-1 REPAIR 1 AND DELTA PRI 584527-14AD REV 1.
Part: LONGERON — CRACKED (BS 1035) · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 7108, L/P 1476686) DURING ULTRASONIC INSPECTION CARRIED OUT AT RH STA 1035 UNDERWING LONGERON, FOUND 02EA FASTENER HOLE AT VERTICAL FLANGE WITH CRACK INDICATION AS MARKED. CORRECTIVE ACTION: CRACKED UNDERWING LONGERON REPLACEMENT WORK AND MODIFICATION WORK CARRIED OUT I.A.W DELTA PRI 584566-14AD REV 0 ISSUE DATE: 14 JAN 2020 AND REV 3 ISSUE DATE: 03 FEB 2020.
Part: LONGERON — CRACKED (BS 1035) · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 7108, L/P 1476699) DURING ULTRASONIC INSPECTION CARRIED OUT AT LH STA 1035 UNDERWING LONGERON, FOUND 03 EA FASTERNER HOLES WITH CRACK INDICATION AS MARKED. CORRECTIVE ACTION: CRACKED UNDERWING LONGERON REPLACEMENT WORK AND MODIFICATION CARRIED OUT I.A.W DELTA PRI 584527-14AD REV 0 ISSUE DATE: 15 JAN 2020 AND REV 3 ISSUE DATE: 03 FEB 2020.
Part: SKIN — DAMAGED (BS 998) · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 71008, L/P 1476780) DURING ACCOMPLISHMENT OF BSB777-53-0087, LAYOUT FASTENER ON RH SIDE MOD DOUBLER FOUND COUNTERSUNK HOLE APPROXI STA998, STR35R FALL ON NEAR MILLING STEP. CORRECTIVE ACTION: FASTENER HOLE INSTALLED WITH BACB30NX8K* + BACN10YT4CD FASTENER AS PER PRI 584566-14AD REV 1 ISSUE DATE : 22 JAN 2020 PENDING FINAL ER/A. COMPARED WITH FINAL ER/A 584566-14AD REV ORIGINAL FOUND COMPLIED WITH. ACCOMPLISHED DELTA ER/A 584566-14AD REV ORIGINAL TIME CONTROLLED ITEMS SECTION I; REFER TO LOG 1476430.
Part: STRINGER — CRACKED (BS 1024-1035) · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 7108, L/P 1476900) DURING ACCOMPLISHMENT OF HFEC INSPECTION ON R/H UNDERWING LONGERON FUSELAGE SKIN, FOUND CRACK INDICATION AROUND 02 EA FASTENER HOLES AT STA 1024 AND STA 1035, STR 37R, APPROX 1.5" IN LENGTH EACH. CORRECTIVE ACTION: REPAIR AND MODIFICATION PERFORMED IAW DELTA PRI 584566-14AD REV 1 ISSUE. DATE: 22 JAN 2020. PENDING FINAL ER/A. COMPARED WITH FINAL ER/A 584566-14AD REV ORIGINAL FOUND COMPLIED WITH.
Part: SKIN — DAMAGED (BS 998) · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 7108, L/P 1476773) LAYOUT FASTENER ON LH SIDE MOD DOUBLER FOUND COUNTERSUNK HOLE APPROX STA998, STR35L FALL ON NEAR MILLING STEP. CORRECTIVE ACTION: COMPLIED WITH 584527-14AD REV 1 AND FINAL ISSUED DELTA ER/A 584527-14AD REV ORIGINAL DATED: 05 FEB 2020.
Part: LONGERON — CRACKED (BS 1035) · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 7108, L/P 1476752) DURING ACCOMPLISHMENT OF HFEC OPEN HOLE INSPECTION ON 04EA OVERSIZE FASTENERS AT RH UNDERWING LONGERON FRONT SPAR LOWER CHORD STA 1035, FOUND 01EA AT LOWER ROW O/B FASTENER WITH CRACK INDICATION AS MARKED. CORRECTIVE ACTION: REPAIR PERFORMED AS PER B777-200 SRM 57-10-10-2R-1 REPAIR 1 AND DELTA PRI 584566-14AD REV 1.
Part: SKIN — DAMAGED (BS 995) · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 7108, L/P 1476764) DOUBLER PILOT HOLE PICKED UP ON LH FX SKIN AT APPROXI STA 995 BTW 34L-35L FOUND 03EA HOLES FAIL ON MILLING STEP. CORRECTIVE ACTION: HOLES SURROUNDING SKIN REWORK JOB PERFORMED AS PER DELTA PRI 584527-14AD REV 1 ISSUE DATED : 21 JAN 2020 PENDING FINAL ER/A. COMPARED WITH FINAL ER/A 584527-14AD REV ORIGINAL FOUND COMPLIED WITH.
Part: SKIN — DAMAGED (BS 995) · airframe 53,230 hrs · 4,748 cycles
(AIRCRAFT 7108, L/P 1476795) DURING ACCOMPLISHMENT OF BS B777-53-0087 MOD, DOUBLER PILOT HOLE PICKED UP ON RH FX SKIN AT APPROXI STA 995 BTW 34R - 35R FOUND 03EA. CORRECTIVE ACTION: HOLES SURRENDING SKIN REWORK JOB PERFORMED IAW DELTA PRI 584566-14AD REV 1 ISSUE DATE:22 JAN 2020 PENDING FINAL ER/A. COMPARED WITH FINAL ER/A 584566-14AD REV ORIGINAL FOUND COMPLIED WITH. REFER TO LOG PAGE 1476430 FOR TIME CONTROLLED ITEMS SECTION II "THE SECTION I REPAIR ON THE UNDERWING LONGERON 2020.
Part: STRUCTURE — DAMAGED (BS 1010-1014) · airframe 53,188 hrs · 4,744 cycles
(AIRCRAFT 7108, L/P 1471791) FWD CARGO LH SIDE FRAME INTERIOR SURFACE FOUND TOOL MARKS AT APPROX STA 1010-1014BTW =35L-36L AS MARKED. CORRECTIVE ACTION: REMOVED AND SMOOTHED OUT AS PER B777-200 SRM 51-10-02.
Part: SKIN — CRACKED (NR 7 SLAT) · airframe 53,188 hrs · 4,744 cycles
(AIRCRAFT 7108, L/P 1468936) HFEC OPEN HOLE INSPECTION ON LH WING INBOARD SLAT ASSEMBLY NO.7 OUTER SKIN COMMON TO THE RIB STRUCTURE LOCATION FOUND 04EA FASTENER HOLES CRACK AS MARKED. CORRECTIVE ACTION: CRACK REPAIRED AS PER PRI ER/A 584453-14 REV. 0.
Part: CLAMP — CORRODED (ACCESS PANEL) · airframe 53,182 hrs · 4,743 cycles
RIGHT WING FUEL TANK PANEL 633EB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED AS PER SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (ACCESS PANEL) · airframe 53,182 hrs · 4,743 cycles
RIGHT WING FUEL TANK PANEL 633DB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED AS PER SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (RT WING) · airframe 53,182 hrs · 4,743 cycles
RT WING FUEL TANK PANEL 633AB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (LT WING) · airframe 53,182 hrs · 4,743 cycles
LEFT WING FUEL TANK PANEL 533BB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (LT WING) · airframe 53,182 hrs · 4,743 cycles
LEFT WING FUEL TANK PANEL 531BB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6, REPAIR 6, PARA 4B, AND 4C.
Part: CLAMP — CORRODED (RT WING) · airframe 53,182 hrs · 4,743 cycles
RT WING FUEL TANK ACCESS PANEL 631BB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (RT WING) · airframe 53,182 hrs · 4,743 cycles
RIGHT WING FUEL TANK ACCESS PANEL 631CB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (RT WING) · airframe 53,182 hrs · 4,743 cycles
RIGHT WING FUEL TANK ACCESS PANEL 631AB CLAMP RING WAS FOUND WITH SURFACE CORROSION. THE CORROSION WAS REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (LT WING) · airframe 53,182 hrs · 4,743 cycles
LEFT WING FUEL TANK PANEL 533DB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (ACCESS PANEL) · airframe 53,182 hrs · 4,743 cycles
RIGHT WING FUEL TANK ACCESS PANEL #633CB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (LT WING) · airframe 53,182 hrs · 4,743 cycles
LEFT WING FUEL TANK PANEL 533CB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (LT WING) · airframe 53,182 hrs · 4,743 cycles
LH WING FUEL TANK PANEL 531AB CLAMP RING WAS FOUND WITH SURFACE CORROSION. THE CORROSION WAS REMOVED IAW SRM 57-20-01-2R-6, REPAIR 6, PARA 4B, AND 4C.
Part: CLAMP — CORRODED (ACCESS PANEL) · airframe 53,182 hrs · 4,743 cycles
RH WING FUEL TANK ACCESS PANEL #633BB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED AS PER B777-200 SRM 57-20-01-2R-6 REPAIR 6.
Part: CLAMP — CORRODED (LT WING) · airframe 53,182 hrs · 4,743 cycles
LEFT WING FUEL TANK 531CB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (LT WING) · airframe 53,182 hrs · 4,743 cycles
LT WING FUEL TANK PANEL 533EB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Part: CLAMP — CORRODED (LT WING) · airframe 53,182 hrs · 4,743 cycles
LEFT WING FUEL TANK PANEL 533AB CLAMP RING FOUND WITH SURFACE CORROSION. CORROSION REMOVED IAW SRM 57-20-01-2R-6 REPAIR 6 PARA 4B AND 4C.
Earlier reports · 2009–2019 · 13 reports
2019
Part: TUBE — DAMAGED (BEARING SUPPLY) · airframe 53,182 hrs · 4,743 cycles
DUE TO OIL QUANTITY FELL TO L01 ON LEFT ENGINE. PRESSURE AND TEMP NORMAL. PRECAUTIONARY DIVERSION. FOUND THE NR 4 AND 5 BEARING SUPPLY OIL TUBE DAMAGE. REMOVED AND REPLACED THE OIL TUBE IAW AMM 70-00-01-400-804-H01. LEAK CHECKED GOOD.
Part: CONNECTOR — LOOSE (CABIN) · airframe 50,545 hrs · 4,534 cycles
(AIRCRAFT 7108, L/P 5673472) EMERGENCY LIGHT ABOVE 2B INOP. LOWERED CEILING PNL FOUND PLUG LOOSE FROM LIGHT ASSY, CONNECTED AND OPS CHECK PER AMM 33-51. OK FOR SERVICE.
Part: GUARD — DEFECTIVE (EMERGENCY LIGHT) · airframe 49,678 hrs · 4,460 cycles
(AIRCRAFT 7108, L/P 5740242) EMERG LIGHT SWITCH WILL NOT STAY IN THE ARMED POSITION WITH GUARD CLOSED. REPLACED SWITCH GUARD CKS OK REF WDM 33-51-12.
2018
Part: FRAME — CRACKED (NR 2 PYLON) · airframe 48,279 hrs · 4,337 cycles
FRAME-CRACKED INT OF PYLON, AFT AND ABOVE PNL 443 DL. COMPLETED REPAIR OF NR 2 PYLON I/B SIDE NR 4 FRAME IAW ER/A572845-14 REV O PRI AND ER/A MATCH.
Part: LIGHT — DAMAGED (SEAT 50F) · airframe 45,480 hrs · 4,103 cycles
SEAT MOUNTED EMERGENCY LIGHT DAMAGED, SEAT 50F. REMOVED AND REPLACED SEAT LIGHT.
2017
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 43,694 hrs · 3,951 cycles
EMERGENCY LIGHT MISSING THE LENS. REPLACED THE LENS, CHECKED GOOD.
Part: LIGHT — UNSECURE (CABIN) · airframe 41,720 hrs · 3,777 cycles
LIGHT NEAR FLOOR AND ADJACENT TO 1L CREW REST IS LOOSE. SECURED THE EMERGENCY LIGHT.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,327 hrs · 3,562 cycles
STA 2119 TO STA 2129, BET STR 39L & STR 42L, FX SKIN AREA FOUND EXISTING BLEND OUT CONDITION. STA 2119 TO STA 2129, BET STR 39L & STR 42L, EXISTING BLEND-OUT MEASURED ORG THK 0.090", MATERIAL REMOVED 0.018" ( L-1.5" X W-1") AND FOUND OUT LIMIT PER SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 102. REPAIR CARRIED OUT PER SRM 53-00-01 FIG 202 REPAIR 4. THIS IS CATEGORY 'B' REPAIR AND REQUIRE REPEAT INSPECTION PER SRM 53-00-01 REPAIR 4, TABLE 204, INSPECTION THRESHOLD: 30,000 FLIGHT CYCLES, METHOD: HFEC AND DETAILED VISUAL. INTERVAL: 16,000 FLIGHT CYCLES.
2016
Part: STRINGER — CORRODED (BS 2273-2364) · airframe 36,031 hrs · 3,261 cycles
STRINGER 40R CORRODED BELOW APU PNEUMATIC DUCT BS 2273.5-2364-5. C/W ERA 546462-14, REV A.
Part: SKIN — CORRODED (BS 2273-2364) · airframe 36,031 hrs · 3,261 cycles
SKIN, STR AND SKIN CLIP CORRODED BELOW APU PNEUMATIC DUCT, BS 2273.5-2364.5. C/W ON NR'S 91 AND 190.
2013
Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 19,441 hrs · 1,742 cycles
F/C AND AFT CABIN EMERGENCY LIGHTS TIME OUT. R & R TWO BATTERIES IAW AMM 33-50, CHECKED OK.
2012
Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,832 hrs · 1,296 cycles
DURING A MAINTENANCE VISIT, THE EMERGENCY EXIT LIGHTS IN FIRST CLASS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FUSES AT DOOR 1R AT POWER SUPPLY. SYSTEM OPERATION WAS NORMAL AFTER THE FUSES WERE REPLACED.
2009
Part: CHARGER — INOPERATIVE (CABIN) · airframe 1,988 hrs · 170 cycles
DURING -A- CHECK FOUND SEATS 10-14CD WITH EMERGENCY LIGHTS INOP. R&R EMERGENCY LIGHTS CHARGER AND BATTERY PACK AT 2R AFT. LIGHTS AT 10-14 CD NOW WORK CORRECTLY. CHARGER P/N D717-02- 030. BATTERY P/N D717-01-100.