N415JN
Registered owner: ATARES FUNDING LLC, FL (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.
113 reports on file, 2015-11-10 – 2021-11-21.
Part: NONE — NONE · airframe 69,076 hrs · 14,648 cycles
AIR TURN BACK DUE TO ENGINE 2 ANTI-ICE OFF ALERT, ENGINE 2 A-ICE DUCT FAILED.
Part: NONE — NONE · airframe 68,925 hrs · 14,622 cycles
AIR RETURN DUE TO LEVEL 3 ENGINE 2 ANTI-ICE DUCT ALERT DISPLAYED IN FLIGHT.
Part: UNKNOWN — UNKNOWN · airframe 68,508 hrs · 14,548 cycles
LOST AUTOPILOT AND FCP SELECTION DURING DEPARTURE. AIR TURN BACKTO ICN DUE TO ABOVE DESCRIPTION.
Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 68,348 hrs · 14,509 cycles
LEVEL 2 "ENG 3 RPM LO" ON DESCENT. ATTEMPTED RESTART. SECURED ENGINE. EMERGENCY DECLARED.
Part: WARNING MESSAGE — ILLUMINATED (ANTI-ICE DUCT) · airframe 67,696 hrs · 14,369 cycles
LEVEL 3 ENGINE 2 A-ICE DUCT IN FLIGHT AT 7000 MSL AND 8500 MSL. SHUT DOWN NR 2 ENGINE, PER QRH.
Earlier reports · 2015–2020 · 108 reports
2020
Part: CABIN AIR SYS — FUMES (NR 3) · airframe 67,659 hrs · 14,358 cycles
UPPER DECK AND CARGO FILLED WITH FUMES FROM BLEED 3. TURNED OFF BLEED AND ECON ON.
Part: WARNING MESSAGE — ILLUMINATED (ANTI-ICE DUCT) · airframe 67,645 hrs · 14,341 cycles
AIR RETURN DUE TO LEVEL 3 ENGINE 2 ANTI-ICE DUCT ALERT.
Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 67,617 hrs · 14,312 cycles
SHORTLY AFTER TAKE-OFF AIRSPEED INDICATED 0 KAIS ON CAPTAINS SIDE. PERFORMED QRH AIRSPEED UNRELIABLE, RETURNED SDF.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RIGHT WING UPPER SKIN AT XORS 700 STRINGER 6 IS CORRODED.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
LEFT WING UPPER SKIN IS CORRODED AT XORS 537 STRINGER 5.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
LEFT WING UPPER SKIN HAS CORROSION AT XORS 562.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RIGHT WING UPPER SKIN IS CORRODED AT XORS 197 STRINGER 19.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
LEFT WING UPPER SKIN HAS CORROSION AT XORS STATION 320.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
LEFT WING UPPER FUEL TANK SKIN HAS CORROSION AT XORS STATION 510.
Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING AFT SPAR UPPER CHORD UPPER SURFACE AT XORS 1042.350.
Part: SPAR — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
LT HORIZONTAL STABILIZER REAR SPAR INSIDE THE STAB IS CORRODED AT STAB STATION 202.
Part: STRINGER CLIP — CRACKED (RT WING) · airframe 81,650 hrs · 14,726 cycles
RT WING STRINGER TIE AT WING STATION 434 AT STRINGER 9 IS CRACKED.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 146 STRINGER 8.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 339 STRINGER 9.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 345 STRINGER 10.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 316 STRINGER 22.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 402 STRINGER 13.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 396 STRINGER 9.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 376 STRINGER 3.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 345 STRINGER 6.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 420 STRINGER 22.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 354 STRINGER 9.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 375 STRINGER 5.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 348 STRINGER 9.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 378 STRINGER 1.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 351 STRINGER 9.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 395 STRINGER 3.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 157 STRINGER 13.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 198 STRINGER 3.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 447.5 STRINGER 8.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 455 STRINGER 2.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 378 AT STRINGER 1.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 402 AT STRINGER 13.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 146 AT STRINGER 8.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 81,650 hrs · 14,726 cycles
RT WING UPPER SKIN IS CORRODED AT WING STATION 395 AT STRINGER 3.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,650 hrs · 14,726 cycles
EMERGENCY LIGHTS FAILED TO ILLUMINATE
Part: WARNING MESSAGE — ILLUMINATED (CABIN PRESSURE) · airframe 67,441 hrs · 14,275 cycles
CABIN ALTITUDE LEVEL 3 ALERT IN FLIGHT. PERFORMED EMERGENCY DESCENT PER QRH. CABIN REACHED 12000 FEET.
Part: PUMP — UNKNOWN (FUEL SYSTEM) · airframe 66,793 hrs · 14,164 cycles
ENGINE 2 (RPM LOW) AUTO SHUTDOWN NO VIB NOTED, AFTER ENG #2 SHUTDOWN IN FLIGHT NOTED ALL PUMPS OFF ON #2 TANK.
Part: BOTTLE — DISCHARGED (L1 DOOR) · airframe 66,597 hrs · 14,127 cycles
DURING PRE-FLIGHT, FOUND L1 EMERGENCY DOOR BOTTLE EMPTY.
2019
Part: CADC — MALFUNCTIONED (COCKPIT) · airframe 66,072 hrs · 13,933 cycles
ON CLIMB OUT, ALTIMETER AND INDICATED AIRSPEED COMPARATOR ALERT DISPLAYED. REPLACED CADC OPERATIONAL AND LEAK CHECK OK.
2018
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LEFT WING UPPER CENTER AND AFT SKIN HAD CORROSION BETWEEN XORS 423 AND XORS 433, STRINGER 6L. ACCOMPLISHED A REPAIR IAW EA 011-5720-52-A7275, I/R.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LT WING UPPER SKIN L/E HAS CORROSION BETWEEN XORS 420 AND XORS 584. ACCOMPLISHED REPAIR ON LT WING UPPER SKIN BETWEEN XORS 420 AND XORS 584 PER EA 011-5740-52-A7279 I/R REF NRC A041634.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LEFT WING UPPER SKIN AND MAIN LANDING GEAR SUPPORT HAD CORROSION AT XORS 264 BETWEEN STRINGERS 3L AND REAR SPAR. ACCOMPLISHED A REPAIR IAW EA 011-5720-52-A7229, I/R.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
RT WING CENTER AND AFT UPPER SKIN HAS CORROSION BETWEEN XORS 270 AND XORS 505 STRGR 4 TO STGR 9. ACCOMPLISHED REPAIR ON RT WING CENTER AND AFT UPPER SKIN BETWEEN XORS 270 AND XORS 505 STGR 4 TO STGR 9 PER EA 011-5720-52-A7290 I/R REF NRC A040769.
Part: SKIN — CORRODED (RT WING) · airframe 65,371 hrs · 13,391 cycles
RT WING AFT AND CENTER UPPER SKIN BTWN XORS-270 AND XROS-505, BTWN STRINGER 4 AND 5 HAS LEVEL 1 CORROSION. REPAIRED RT WING AFT AND CENTER UPPER SKIN BTWN XORS-270 AND XROS-505, BTWN STRINGER 4 AND 5 PER EA 011-5720-52-A7290-I/R. REF: NRC A040770 AND WO 14676.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LT WING UPPER CENTER AND AFT SKIN HAS CORROSION AT XORS 131/163 AT STR 6. ACCOMPLISHED BLENDOUT REPAIR AT LT WING UPPER CENTER AND AFT SKIN BETWEEN XORS 131 AND 163 AT STR 6 PER EA 011-5710-52-A7259 I/R REF NRC A040750.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
CENTER AND AFT RT WING UPPER SKIN BETWEEN XORS 130 TO XORS 264 BETWEEN STR 5 AND 8 HAS CORROSION. ACCOMPLISHED REPAIR ON RT WING CENTER AND AFT UPPER SKIN BETWEEN XORS 130 AND XORS 264 STRINGER 5 AND STR 8 PER EA 011-5720-52-A7282 I/R REF NRC A040768.
Part: ANGLE — GOUGED (TE FLAP) · airframe 65,371 hrs · 13,391 cycles
RT WING OTBD FLAP INBD HINGE FAIRING ANGLE IS GOUGED. REMOVED, FABRICATED AND INSTALLED RT WING OTBD FLAP INBD HINGE FAIRING ANGLE PER EA 011-5750-52-A7298 I/R REF NRC A041748.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
RIGHT WING CENTER AND AFT UPPER SKIN HAD CORROSION AT XORS 270 TO XORS 505 BETWEEN STRINGERS 4 AND 9. REPAIRED IAW EA 011-5720-52-A7290, I/R.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LEFT WING UPPER SKIN HAD CORROSION AT XORS 340 - 375 BETWEEN STRINGERS 4 AND 6L. REPAIRED THE LT WING UPPER SKIN IAW EA 011-5720-52-A7292, I/R.
Part: SKIN — GOUGED (RT WING) · airframe 65,371 hrs · 13,391 cycles
RIGHT WING LOWER SKIN WAS GOUGED AT XORS 264 AND THE FRONT SPAR. ACCOMPLISHED A REPAIR IAW EA 011-5740-52-A7266, I/R.
Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
CENTER FUSELAGE/LONGERON 28R STA 1361 TO STA 1401 HAS CORROSION. ACCOMPLISHED REPAIR ON CENTER FUSELAGE LONGERON 28R BETWEEN STA 1361 TO STA 1401 PER EA 011-5340-52-A7249 I/R REF NRC A040825.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
FWD CARGO COMPARTMENT FLOOR CHANNEL IS CORRODED AT STA 999 X=47.75. ACCOMPLISHED REPAIR ON FWD CARGO COMPARTMENT FLOOR CHANNEL AT STA 999 X=47.75 PER EA 011-5310-52-A7272 I/R.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
RIGHT WING UPPER SKIN HAD CORROSION BETWEEN XORS 91 AND XORS 230, STRINGER 14. ACCOMPLISHED A BLENDOUT REPAIR ON THE RT WING SKIN IAW EA 011-5720-52-A7293, I/R.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
CORROSION FOUND ON THE RT WING FWD UPPER SKIN TO MID SKIN FROM APPROX XORS 285 - 318. BLENDED THE CORROSION IAW SRM 51-21-04, PG3. REPAIRED IAW EA 011-5720-52-A7293.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
RIGHT WING FWD AND CENTER UPPER SKIN HAD CORROSION BETWEEN XORS 145 AND 231, STRINGER 14R. ACCOMPLISHED A BLENDOUT REPAIR IAW EA 011-5720-52-A7293, I/R.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
CORROSION FOUND ON THE RT WING FWD UPPER SKIN TO MID SKIN FROM XROS 192 - 216. BLENDED OUT THE CORROISION IAW SRM 52-21-04, PG 4. REPAIRED THE WING SKIN IAW EA 011-5720-52-A7293.
Part: STRAP — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
CENTER CARGO DOOR INNER STRAP WAS CORRODED AT BS 1717.5. REPAIRED THE STRAP IAW EA 011-5230-52-A7252 I/R.
Part: DOUBLER — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
RIGHT WING L/E BEADED DOUBLER WAS CRACKED AT WS 584. REMOVED, FABRICATED AND INSTALLED A NEW BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15.
Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LH WING OUTER REAR SPAR UPPER CAP IS CORRODED AT XORS 412 TO 422. ACCOMPLISHED BLEND OUT REPAIR AT LH WING OUTER REAR SPAR UPPER CAP AT XORS 412 TO XORS 424 PER VT-SAA EA# 011-5720-52-A7270 I/R REF VT SAA NRC# A040745.
Part: LONGERON — CORRODED (BS 1461-1481) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
MAIN CABIN BS 1461 - 1481, LONGERON 16L WAS EXFOLIATED. REMOVED, FABRICATED AND INSTALLED A NEW LONGERON IAW SRM 51-31-01.
Part: FITTING — CORRODED (DRAIN PAN) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
L1 DOOR FLOOR DRAIN PAN LANDING HEADER FITTING CORRODED. PERFORMED A BLENDOUT REPAIR IAW EA 011-5310-52-A7235, I/R.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LH WING UPPER SKIN HAS CORROSION AT WS 170 AND FRONT SPAR. PERFORMED A BLENDOUT REPAIR IAW EA-011-5710-52-A7258, I/R.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LEFT WING UPPER SKIN HAD CORROSION AT XORS 197. ACCOMPLISHED A BLEND OUT REPAIR IAW EA 011-5710-52-A7233 I/R.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
RH WING UPPER SKIN HAD CORROSION AT XORS 676 TO XORS 792, STRINGER 6 AND 7. ACCOMPLIHED BLEND OUT REPAIR IAW EA 011-5720-52-A7274 I/R.
Part: LONGERON — CORRODED (BS 460-595) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
CORROSSION FOUND ON LONGERON 38L AT BS 460 TO 595. REMOVED, FABRICATED, AND INSTALLED A NEW LONGERON IAW SRM 51-31-01, AND EA 011-5300-52-A7260 I/R.
Part: CASE — CORRODED (NR 1 ENGINE) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
NR 1 ENG FWD FAN CASE BOLT HOLES HAVE CORROSION. ACCOMPLISHED NR 1 ENG FWD FAN CASE BOLT HOLE BUSHING REPAIR PER ENGINEERING CONSULTANTS REPAIR 18-WGA-002 REV ORINGINAL.
Part: RETAINER — DENTED (ZONE 100) · airframe 65,371 hrs · 13,391 cycles
CENTER CARGO PRESSURE BULKHEAD CARGO LINER RETAINER HAS A DENT AT STA 1521 X=+12.5 AND Z=-45. ACCOMPLISHED REPAIR ON CENTER FUSELAGE COMPARTMENT PRESSURE BULKHEAD CARGO LINER RETAINER AT STA 1521 X=+12.5 AND Z=-45 PER EA 011-5300-52-A7243 I/R REF NRC A040906.
Part: REINFORCEMENT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
HINGE FITTING REINFORCEMENT ANGLE IS CORRODED IN NR 2 AC BAY STA 520 TO STA 535 LONGERON 38L. REMOVED, FABRICATED AND INSTALLED NR 2 AC BAY HINGE FITTING REINFORCEMENT ANGLE AT STA 520 TO STA 535 LONGERON 38L PER SRM 51-31-01 REF NRC A041714.
Part: DRAG ANGLE — CRACKED (FUSELAGE) · airframe 65,371 hrs · 13,391 cycles
LT UNDER WING BARREL CANTED PANEL DRAG ANGLE IS CRACKED AT STA 1236 STR 43. ACCOMPLISHED REPAIR ON LT FUSELAGE WING BARREL CANTED PANEL CAP AT STA 1236 STR 43 PER EA 011-5310-52-A7214 I/R REF NRC A040820.
Part: RETAINER — DENTED (FUSELAGE) · airframe 65,371 hrs · 13,391 cycles
CENTER CARGO PRESSURE BULKHEAD CARGO LINER RETAINER STA 1521 HAS A DENT. ACCOMPLISHED REPAIR ON CENTER CARGO PRESSURE BULKHEAD RETAINER AT STA 1521 X=+12.5 AND Z= 59.010 PER EA 011-5300-52-A7242 I/R REF NRC A040908.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
AFT CARGO FLOORBEAM IS CORRODED AT STA 1841 RBL 12 TO 20. ACCOMPLISHED AFT CARGO FLOORBEAM REPAIR AT STA 1841 RBL 12 TO RBL 20 IAW EA 011-5316-52-A7221 I/R REF NRC3 A040900.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LT WING UPPER SKIN HAS CORROSION XORS 518 TO XORS 536. ACCOMPLISHED REPAIR ON LT WING UPPER SKIN BETWEEN XORS 518 TO XORS 536 PER EA 011-5720-52-A7273 I/R REF NRC A040733.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
AFT CARGO FLOOR SUPPORT STA 1841 LBL54 TO RBL 54 HAS CORROSION. REMOVED, FABRICATED AND INSTALLED AFT CARGO FLOOR SUPPORT AT STA 1841 LBL54 TO RBL 54 IAW DWG AGA7170 AND SRM 51-31-01 REF NRC A040903
Part: DRAG ANGLE — CORRODED (ZONE 100) · airframe 65,371 hrs · 13,391 cycles
RH FUSELAGE WING BARREL CANTED PANEL DRAG ANGLE IS CRACKED AT STA 1236 STGR 43. REPAIRED IAW EA 011-5310-52-A7215, I/R3
Part: CARGO TRACK — CORRODED (BS 1849) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
AFT CARGO BAY, CARGO TRACK AT BS 1849, RBL 15 IS CORRODED. REMOVED, FABRICATED, LOCATED, DRILLED, AND REPLACED THE CARGO TRACK IAW DWG AG3855, REV P, SRM 51-21-01, AND EA 011-5300-52-A7254.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
NUMEROUS AREAS OF CORROSION ON RT WING LOWER SKIN AT XORS 346 AND XORS 402 STRINGER 31 TO 40. ACCOMPLISHED REPAIR AT RT WING LOWER SKIN AT XORS 346 TO XORS 402 BETWEEN STRINGER 31 TO STRINGER 40 PER EA 011-5720-52-A7220 IR REF NRC A040473.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LEFT WING UPPER SURFACE FWD SKIN HAS CORROSION AT XORS 130. ACCOMPLISHED A REPAIR IAW EA 011-5720-52-A7223, IR.
Part: STRINGER — CRACKED (LT WING) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
LEFT WING NR 1 FUEL TANK UPPER STRINGER 10 FOUND CRACKED AT XORS 753. REPAIRED THE STRINGER IAW SRM 57-00-03, REPAIR 5, FIG 202.
Part: LONGERON — CORRODED (ZONE 100) · airframe 65,371 hrs · 13,391 cycles
CENTER CARGO LONGERON 38 IS CORRODED BETWEEN STA 5-123 & 5-113. REPAIRED IAW SRM 53-00-05, REPAIR 1, SHEET 1.
Part: STRINGER — CRACKED (48 LEFT) · airframe 65,371 hrs · 13,391 cycles
CENTER WING UPPER AUX TANK LOWER STRINGER 48 IS CRACKED AT XCW 17.00 AND 46.50. ACCOMPLISHED REPAIR ON CENTER WING UPPER AUX TANK LOWER STRINGER 48 PER MD-11 SRM 57-10-03 REPAIR 1 FIG 201 REF VT SAA NRC# A040935.
Part: STRINGER — CRACKED (ZONE 100) · airframe 65,371 hrs · 13,391 cycles
CENTER WING UPPER AUX FUEL TANK LOWER STRINGER 52 IS CRACKED AT XCW 17.00 AND XCW 46.50. ACCOMPLISHED REPAIR ON CENTER WING UPPER AUX TANK LOWER STRINGER 52 AT XCW 0 TO XCW 64 PER MD-11 SRM 57-10-03 REPAIR 1 FIG 201 REF VT SAA NRC#A040936.
Part: STRINGER — CRACKED (ZONE 100) · airframe 65,371 hrs · 13,391 cycles
CENTER WING UPPER AUX FUEL TANK LOWER STRINGER 47 IS CRACKED AT XCW -46.50, XCW -17, XCW 17.00,XCW -46.50 XCW 46.50. ACCOMPLISHED REPAIRS ON CENTER WING UPPER AUX FUEL TANK LOWER STRINGER 47 BETWEEN XCW -17.00 XCW 17.00, XCW -46.50, XCW 46.50, XCW 64, XCW -64 PER MD-11 SRM 57-10-03 REPAIR 1 FIG 201 REF VT SAA NRC# A040933.
Part: STRINGER — CRACKED (FUEL TANK) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
CENTER AUX FUEL TANK LOWER STRINGER 45 CRACKED AT XCW -17.00 AND XCW 17.00. REPAIRED IAW SRM 57-10-03, REPAIR 1.
Part: ANGLE — CORRODED (NR 2 NACELLE) · airframe 65,371 hrs · 13,391 cycles
NR 2 PYLON, LT SIDE ACCESS PANEL 457AL COMPARTMENT HAS A CORRODED ANGLE. REMOVED, FABRICATED AND INSTALLED A NEW ANGLE AND DOUBLER IAW SRM 51-31-01.
Part: DOUBLER — CRACKED (LT WING) · airframe 65,371 hrs · 13,391 cycles
LEFT WING CUT OUT AREA AFT OF THE NR 5 SLAT AT XORS 696, THE BEADED DOUBLER WAS FOUND CRACKED IN TWO PLACES. FABRICATED AND INSTALLED A REPAIR IAW SRM 57-40-02, REPAIR 15, FIG 205.
Part: MOUNT BRACKET — CRACKED (BS 1278) · airframe 65,371 hrs · 13,391 cycles
MAIN CABIN L3 DOOR FRAME UPPER AFT LONGERON 15L HAS A CRACKED MOUNTING BRACKET. REMOVED THE CRACKED MOUNTING BRACKET IAW SRM 51-35-01. FABRICATED REPAIR MOUNTING BRACKET IAW DWG AEA7568, AND INSTALLED THE MOUNTING BRACKET, BS 1278 LONGERON 15L IAW SRM 51-35-01
Part: MOUNT BRACKET — CRACKED (BS 1278) · airframe 65,371 hrs · 13,391 cycles
MAIN CABIN R3 DOOR FRAME UPPER AFT LONGERON 15R HAS A CRACKED MOUNTING BRACKET. REMOVED THE MOUNTING BRACKET IAW SRM 51-00-12. FABRICATED A REPAIR MOUNTING BRACKET IAW DWG AEA7568. INSTALLED THE REPAIR MOUNTING BRACKET, BS 1278 IAW SRM 51-33-01, PG 30, PARA 8.
Part: DOUBLER — CRACKED (LT WING) · airframe 65,371 hrs · 13,391 cycles
LEFT WING L/E AT WING XOS 863 BEADED DOUBLER IS CRACKED. REMOVED AND REPLACED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205.
Part: DOUBLER — CRACKED (LT WING) · airframe 65,371 hrs · 13,391 cycles
LEFT WING LEADING EDGE BETWEEN REFUEL VALVES XOS 627, THE BEADED DOUBLER HAD CRACKS AROUND FASTNER HEADS. REMOVED AND REPLACED THE BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205.
Part: DOUBLER — CRACKED (LT WING) · airframe 65,371 hrs · 13,391 cycles
LEFT WING CUT OUT AREA AT WING XOS 770 BEADED DOUBLER IS CRACKED. REMOVED AND REPLACED THE DOUBLER IAW SRM 57-40-02, REPAIR 15.
Part: DOUBLER — CRACKED (RT WING) · airframe 65,371 hrs · 13,391 cycles
RIGHT OTBD WING L/E BEADED DOUBLER FOUND CRACKED AT RWS 588. REMOVED AND REPLACED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205.
Part: DOUBLER — CRACKED (RT WING) · airframe 65,371 hrs · 13,391 cycles
RIGHT WING L/E LOWER SURFACE BEADED DOUBLER AT RWS 690 FOUND CRACKED. CUT OUT THE BEADED DOUBLER SECTION IAW SRM 57-40-02, FIG 205, REPAIR 15. FABRICATED AND INSTALLED A NEW BEADED DOUBLER IAW SRM 57-40-02, FIG 205, REPAIR 205.
Part: SKIN — CHAFED (BS 1159) · airframe 65,371 hrs · 13,391 cycles
R/H UNDER WING TO BODY FAIRING BELLY SKIN REPAIR DOUBLER IS CHAFED BEYOND REPAIR. REMOVED SKIN REPAIR DOUBLER AT R/H STA 1159 STR 44 R/H PER MD-11 SRM 51-30-01. FABRICATED AND INSTALLED NEW REPAIR DOUBLER PER MD-11 SRM 51-40-01 AND SRM 53-40-01 8.4" X 13.5"
Part: DOUBLER — CRACKED (RT WING) · airframe 65,371 hrs · 13,391 cycles
RT LE WING AT XORS 884 HAS A CRACKED BEADED DOUBLER. FABRICATED A NEW BEADED DOUBLER IAW SRM 57-40-02. LOCATED, DRILLED AND INSTALLED THE BEADED DOUBLER IAW SRM 57-40-02, FIG 205, REPAIR 15.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 65,371 hrs · 13,391 cycles
FRAME SHEAR TIE EXFOLIATED AT BS 6-30 BETWEEN LONGERON 51 - 52R, IN THE FWD CARGO BAY. CUT OUT THE DAMAGED SHEAR TIE IAW SRM 53-00-06, FIG 201. FABRICATED AND INSTALLED A NEW SHEAR TIE IAW SRM 53-00-06, FIG 201, REPAIR 1.
Part: BRACKET — CRACKED (WINDOW FRAME) · airframe 65,371 hrs · 13,391 cycles
MAIN CABIN RIGHT WINDOW FRAME UPPER INTERCOSTAL BRACKET CRACKED AT BS 1159. REMOVED THE INTERCOSTAL IAW SRM 51-33-01, PG 1. FABRICATED AND INSTALLED A REPLACEMENT BRACKET IAW DWG AEA0349.
Part: DOUBLER — CRACKED (RT WING) · airframe 65,371 hrs · 13,391 cycles
RT WING TE, XORS 887, CRACKED BEADED DOUBLER. FABRICATED AND INSTALLED A NEW BEADED DOUBLER IAW SRM 57-40-02, FIG 205, REPAIR 15.
Part: WEB — CRACKED (BS 1305) · airframe 65,371 hrs · 13,391 cycles
L3 DOOR FRAME LOWER AFT WEB CRACKED ON FWD SIDE. STOP DRILLED THE CRACK IAW SRM 53-40-15, REPAIR 3, FIG 201. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-40-15, REPAIR 3-9, FIG 201.
2017
Part: ENGINE — POWER LOSS (NR 1) · airframe 65,007 hrs · 13,311 cycles
LOW THUD HEARD FROM LEFT SIDE #1 ENGINE. SPOOLED TO 30% N1. EGT WAS 200 DEGREES HIGHER THAN 2 & #. FUEL FLOW 640. NO CONTROL OF THROTTLE MOVEMENT. NO CURRENT FAULTS-NO LAST LEG FAULTS-NO FADEC MAINT OR FAULT IN FLIGHT. RTS TEST PERFORMED SATISFACTORY ON BOTH CHANNELS IN ACCORDANCE WITH AMM 73-21-02. MINIMUM IDLE CHECK SATISFACTORY IN ACCORDANCE WITH AMM 71-00-00. ON "A CHECK REVIEW" FOUND FAULT 323-25 AS PER FIM 73-21-01 TABLE 101 NO MAINT ACTION NECESSARY.
Part: AILERON SYS — MALFUNCTIONED · airframe 64,859 hrs · 13,272 cycles
DURING CLIMB, THE AILERON DEFLECTION DISENGAGED. DUMPED FUEL, PERFORMED UNSCHEDULED LANDING.
2016
Part: UNKNOWN — MALFUNCTIONED (NR 2 ENGINE) · airframe 62,855 hrs · 12,769 cycles
DURING CLIMB, HEARD LOAD BANGS, ALL ENG SYS PARAMETERS WERE NORMAL, RETURNED. GND CREW REPORTED SEEING FLAMES SHOOT OUT OF ENG NR 2 POSITION. SYS BEING TROUBLE SHOT IAW FAULT ISOLATION MANUAL.
Part: UNKNOWN — VIBRATION (ZONE 700) · airframe 62,854 hrs · 12,769 cycles
DURING LG RETRACTION, HEARD SERIOUS BANG NOISE WITH ASSOCIATED AIRFRAME VIBRATIONS. INSPECTED ALL FOUR LG ASSEMBLIES WITH WHEELS & BRAKES, & ALL FOUR WW WITH NO DISCREPANCIES FOUND. CHECKED INLET & TAIL PIPES OF ALL THREE ENGS WITH NO DISCREPANCIES NOTED. REPLACED BOTH NLG WHEEL ASSEMBLIES AS A PRECAUTION.
2015
Part: SKIN — DELAMINATED (TE FLAP VANE) · airframe 61,750 hrs · 12,471 cycles
LEFT WING OTBD TE FLAP VANE, LOWER SURFACE AT APPROX WING STATION 713 VANE FAILED TAP TEST, SKIN HAS DELAMINATION.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,750 hrs · 12,471 cycles
POSSIBLE CORROSION BETWEEN STATION 5-32 & 5-52, BETWEEN LONGERON 50R & 49R.
Part: SPAR — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 61,750 hrs · 12,471 cycles
POSSIBLE CORROSION ON VERTICAL RT STATION 396 - 410 AFT CTR SPAR.
Part: ACCESS PANEL — CRACKED (NR 1 PYLON) · airframe 61,750 hrs · 12,471 cycles
NUMBER 1 PYLON ACCESS PANEL 437AR CORNER CRACKED.
Part: PANEL — DEBONDED (NR 2 PYLON) · airframe 61,750 hrs · 12,471 cycles
PANEL 364AR ON NR 2 PYLON IS BECOMING DISBANDED BETWEEN PANEL LAYERS.