N776FD
Registered owner: FEDERAL EXPRESS CORP, TN (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
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.
17 reports on file, 2015-05-13 – 2017-08-02.
Part: RAIL — DAMAGED (NR 1 PYLON) · airframe 75,983 hrs · 28,393 cycles
NR 1 PYLON STRUT LT FAN COWL SUPPORT RAIL REQUIRES A SPLICE REPAIR NEAR NAC STA 93. COMPLIED WITH EA F-5400-T0334590 PART 1 , REMOVE DAMAGED SECTION. FABRICATED A REPLACEMENT SECTION, REPAIR ANGLE & TAPERED REPAIR STRAP & INSTALLED SPLICE REPAIR.
Part: SKIN — DENTED (BS 395-418) · airframe 75,983 hrs · 28,393 cycles
LEFT FUSELAGE SKIN, BETWEEN BS 395 AND 418, STRINGER 17L AND 18L. HAS A DENT THAT IS OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-01-2R, REPAIR 16.
Part: SCREW — SHEARED (SWITCH) · airframe 75,748 hrs · 28,205 cycles
DURING PRE-FLIGHT CHECK, FOUND THE L1 DOOR SLIDE LIGHT WILL NOT ILLUMINATE. FOUND THE NR 1 SWITCH MOUNTING SCREW SHEARED FROM SWITCH S10214. SWITCH DOES NOT INTERFERE WITH GIRT BAR ENGAGEMENT. INSPECTED THE L1 DOOR & FOUND THE GIRT BAR AFT POSITION MAGNETIC ACTUATOR MISSING. SECURED (S10214) IAW AMM 25-66-11-2, GIRT BAR ENGAGES & DISENGAGES NORMALLY. INSTALLED A NEW ACTUATOR IAW MM 25-66-11-2. L1 DOOR ARMED LIGHT OPS CHECKED GOOD.
Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 75,569 hrs · 28,103 cycles
AFT CARGO FIRE INDICATION MOMENTARILY ON TOUCHDOWN. DECLARED EMERGENCY, INSPECTED BY FIRE DEPARTMENT. PERFORMED MAIN DECK SMOKE DETECTION BITE TEST. NO FAULTS NOTED. SYSTEM OPS CHECKED NORMAL. ACFT OK FOR SERVICE.
Earlier reports · 2015–2016 · 13 reports
2016
Part: ECU — FAILED (APU) · airframe 75,252 hrs · 27,882 cycles
APU SHUTDOWN IN FLIGHT WITH FAULT LIGHT. ATTEMPTED ONE RESTART, THEN RETURNED TO DEPARTURE DUE TO SINGLE GENERATOR OPS. R & R ECU. ACCOMPLISHED 3 NORMAL SUCESSFUL STARTS WITH APU PNEUMATIC AND ELECTRICAL SYSTEMS, OPS CHECKING NORMAL.
Part: PUMP — CRACKED (HYDRAULIC SYS) · airframe 74,858 hrs · 27,608 cycles
LEFT HYD SYS FAILURE AS CONFIGURATION FOR LANDING, HAD TO SERVICE LT HYD SYS ON PREFLIGHT DUE TO LOW FLUID, FOUND LE SLAT BYPASS VLV LEAKING. REMOVED, REPLACED & TESTED IAW MM 27-81-09-4. R & R LT SYS EDP PRESS & CASE DRAIN FILTERS IAW MM 29-11-17-4 FILTERS CLEAN. LEAK CHECKED GOOD, DPI NOT POPPED. SERVICED LT HYD SYS IAW MM 12-12-01-3. RAN ENG IAW JRH & OPERATED FLIGHT CONTROLS & LT SYS COMPONENTS. LEAK CHECKED GOOD. OPERATIONS CHECKED GOOD. FOUND HOUSING CRACKED AT PORT B LE SLAT BYPASS VLV.
2015
Part: HYDRAULIC LINE — FAILED (HYDRAULIC SYS) · airframe 746 hrs · 27,455 cycles
LEFT SYS HYD FAILURE ON FINAL. LT HYD SYS PRESS. LANDED, COMPLIED WITH QRH PART 17 NOV 15. TROUBLE SHOT LT HYD SYS, FOUND FWD FLEX LINE TO LT GEAR DOWN LOCK ACTUATOR LEAKING. ORDERING BOTH FLEX LINES. IAW CREW DEBRIEF, LT HYD PUMPS WERE NOT OPERATED MORE THAN 2 MINUTES. REMOVED FWD FLEX LINE FROM LT MAIN GEAR DOWNLOCK ACTUATOR. CAPPED FITTINGS ALL IAW MM 20-10-10-4. R & R LT GEAR RETURN LINE, OPERATIONS GOOD.
Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 744 hrs · 27,329 cycles
RIGHT WING INBOARD FLAP, UPPER PANEL EXTERNAL SKIN HAS GOUGE. REMOVED DOUBLER & REWORKED IAW SRM 51-70-10 REPAIR 2 EA F-5730-T0318678 PT 1. MAJOR REPAIR.
Part: FILL PORT — CORRODED (LT WING) · corrosion level 2 · airframe 744 hrs · 27,329 cycles
LEFT WING TANK OVERWING FILL PORT FLANGE HAS CORROSION. COMPLIED WITH ALL STEPS 1 & 2 OF EA F-5720-T0318310 PT 1. CATEGORY A REPAIR, MAJOR REPAIR.
Part: FRAME — CRACKED (FUSELAGE) · airframe 744 hrs · 27,329 cycles
MAIN DECK CABIN ABOVE CEILING STATION 1580, FRAME CRACKED AT STRINGER 3L, APPROX L=1". REPAIRED FRAME STATION 1580, AT STRINGER 2L - 4L IAW SRM 53-00-07 2R REPAIR 3. MAJOR REPAIR CAT B.
Part: SKIN — CORRODED (BS 763-765) · corrosion level 2 · airframe 744 hrs · 27,329 cycles
SCRIBE LINE DAMAGE FOUND AT LAP SEAM, STRINGER 19L, BS 763 - 765 AND CORRODED. REPAIR & BLEND ACCOMPLISHED IAW EA 757-5331-16-F4972 REV. MAJOR REPAIR.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 744 hrs · 27,329 cycles
AFT PIT BULKHEAD LOWER CHORD SKIN CORRODED AT STATION 1720, STRINGER 28L. AREA AT FUSELAGE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08-1A FIG 101 DETAIL IX. COMPLIED WITH EA F5300-T0317468 PART 1. CAT A REPAIR, MAJOR REPAIR.
Part: KEELBEAM — CORRODED (BS 780-879) · corrosion level 2 · airframe 744 hrs · 27,329 cycles
FWD CARGO BAY, BS 780 - 879, RT KEEL BEAM EXTENSION CORRODED . REPAIRED IAW EA F-5310-T0317630 . MAJOR REPAIR
Part: SKIN — DAMAGED (BS 1682 - 1708) · airframe 744 hrs · 27,329 cycles
DAMAGE TO THE EXTERIOR SKIN SURFACE AT LAP SEAM S10L, BS 1682 - 1708. REPAIRED IAW EA F-5330-T0317373, PT.1. MAJOR REPAIR.
Part: SKIN — CORRODED (BS 1670) · corrosion level 2 · airframe 744 hrs · 27,329 cycles
AFT CARGO BAY BILGE AREA, LOWER SKIN AROUND CUTOUT CORRODED AT BS 1670 , BETWEEN S25 - 26R. CORROSION WAS FOUND OUT OF LIMITS IAW SRM 53-00-53, 1A. COMPLIED WITH EA F-5330 T0317434, PT.1. REPAIRED AND DOUBLER INSTALLED IAW SRM 51-40-02 AND DWG 146N3780. MAJOR REPAIR.
Part: SKIN — DENTED (BS 288) · airframe 744 hrs · 27,329 cycles
SKIN DENTED LBL 40, BS 288, & STRINGER 23 & 24L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01A DET III. REPAIRED IAW SRM 53-00-01-2R. MAJOR REPAIR.
Part: SKIN — DAMAGED (BS 480) · airframe 744 hrs · 27,329 cycles
FUSELAGE SKIN LIGHTNING STRIKE FASTENER, BS 480, BETWEEN STRINGER 22R - 23R, DEFORMED SKIN AT FRAME. ACCOMPLISHED WITH EA F-5330-T0317032, CATEGORY B REPAIR, MAJOR REPAIR.