N170CR

No registry detail on file · not in current registry

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.

30 reports on file, 2016-08-10 – 2016-10-14.

OTHER · 2016-10-14 Matched by certificate designator
ATA 5415

Part: ATTACH FITTING — CRACKED (NR 2 PYLON) · airframe 86,317 hrs · 21,676 cycles

NR 2 PYLON I/B MIDSPAR FITTING CLIP HAS AN APPROX 1.5" CRACK IN THE RADIUS OF THE PART.

Source: SDR KCSA201610141088
OTHER · 2016-10-14 Matched by certificate designator
ATA 5320

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

FWD LWR CARGO DOOR SILL BEAM AT STA 478 RBL 42 HAS POSSIBLE CORROSION.

Source: SDR KCSA201610141080
OTHER · 2016-10-14 Matched by certificate designator
ATA 5313

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER SPLICE FITTING AT STRINGER 35L STA 434.

Source: SDR KCSA201610141087
OTHER · 2016-10-14 Matched by certificate designator
ATA 5730

Part: SKIN — DAMAGED (LT WING) · airframe 86,317 hrs · 21,676 cycles

LEADING EDGE WING SKIN, FORWARD OF FRONT SPAR AT NR 1 SLAT I/B SLAT TRACK DAMAGED.

Source: SDR KCSA201610141082
OTHER · 2016-10-14 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

EVIDENCE OF CORROSION BULK PIT FLOOR AT STA 1395 BUTTLINE 0.

Source: SDR KCSA201610141079
OTHER · 2016-10-14 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER 35L FWD OF EXISTING SPLICE STA 424.

Source: SDR KCSA201610141086
OTHER · 2016-10-14 Matched by certificate designator
ATA 5320

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

LT TORQUE BOX PANEL AT STA 544-566 HAS POSSIBLE EVIDENCE OF CORROSION.

Source: SDR KCSA201610141083
OTHER · 2016-10-14 Matched by certificate designator
ATA 5512

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON HORIZ STAB UPPER SURFACE STR 11-10 RBL 48.

Source: SDR KCSA201610141081
OTHER · 2016-10-14 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER 36L JUST AFT OF FACTORY SPLICE AT STA 434.

Source: SDR KCSA201610141085
OTHER · 2016-10-14 Matched by certificate designator
ATA 5320

Part: TORQUE BOX — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

LT TORQUE BOX PANEL HAS CORROSION AT STA 544-566 LBL 26.

Source: SDR KCSA201610141084
OTHER · 2016-10-01 Matched by certificate designator
ATA 5512

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 86,316 hrs · 21,676 cycles

CORROSION ON HORIZ STAB UPPER SURFACE RBL 48 STR 3.

Source: SDR KCSA201610011076
OTHER · 2016-10-01 Matched by certificate designator
ATA 5512

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 86,316 hrs · 21,676 cycles

CORROSION ON HORIZ STAB UPPER SURFACE RBL 48 STR 5-9.

Source: SDR KCSA201610011077
OTHER · 2016-09-22 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (BS 434-456) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON SKIN UNDER STRINGER 37L, BS 434 - 456.

Source: SDR KCSA201609221072
OTHER · 2016-09-20 Matched by certificate designator
ATA 4910

Part: FIREWALL — CRACKED (APU BAY) · airframe 86,316 hrs · 21,676 cycles

APU FIREWALL BS 1843 AT 5 O'CLOCK CRACKED.

Source: SDR KCSA201609201070
OTHER · 2016-09-16 Matched by certificate designator
ATA 5730

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

POSSIBLE CORROSION UNDER RT WING NR 7 FWD FLAP TRACK FAIRING.

Source: SDR KCSA201609161069
OTHER · 2016-09-13 Matched by certificate designator
ATA 5313

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER SPLICE 37L, BS 434,

Source: SDR KCSA201609131068
OTHER · 2016-09-13 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (BS 445) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER 37L AT BS 445.

Source: SDR KCSA201609131067
OTHER · 2016-09-13 Matched by certificate designator
ATA 5330

Part: SKIN — CHAFED (BS 1809-1832) · airframe 86,317 hrs · 21,676 cycles

LEFT EXTERIOR SKIN FROM APPROX BS 1809 - 1832, WL 240 CHAFED.

Source: SDR KCSA201609131065
OTHER · 2016-09-13 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

SUPPORT PLATE ASSEMBLY INTERCOSTAL AT BS 1329 - 1351, STR 34L IN AFT CARGO BAY HAS CORROSION

Source: SDR KCSA201609131066
OTHER · 2016-09-09 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (BS 438) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER 34L BS 438.

Source: SDR KCSA201609091064
OTHER · 2016-09-06 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (BS 1307-1329) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

EVIDENCE OF CORROSION IN THE AFT CARGO BAY AT BS 1307 - 1329 BL 0 ON THE SHEAR TIE

Source: SDR KCSA201609061063
OTHER · 2016-09-06 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

SKIN CORROSION TIME LIMITED REPAIR FROM FUSELAGE BS 1329 TO 1351 ON STRINGER 34L, AROUND FASTENER HOLES.

Source: SDR KCSA201609061062
OTHER · 2016-08-22 Matched by certificate designator
ATA 5313

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER SPLICE 36L AT BS 434.

Source: SDR KCSA201608221055
OTHER · 2016-08-22 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (BS 430) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER 37R AT BS 430.

Source: SDR KCSA201608221057
OTHER · 2016-08-22 Matched by certificate designator
ATA 5313

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER SPLICE 37R AT BS 434.

Source: SDR KCSA201608221054
OTHER · 2016-08-22 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 86,317 hrs · 21,676 cycles

CORROSION ON STRINGER 34L AT BS 1329 - 1351.

Source: SDR KCSA201608221056
OTHER · 2016-08-12 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (FUSELAGE) · airframe 86,316 hrs · 21,676 cycles

STA 903.5, LBL-89, WL-194: FRAME INNER CHORD HAS 1.125" CRACK, APPROXIMATELY, MARKED.

Source: SDR KCSA201608121050
OTHER · 2016-08-12 Matched by certificate designator
ATA 5414

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 86,316 hrs · 21,676 cycles

NR 2 NACELLE INBD SIDE NS 231.0 JUST AFT OF THE FOOTBALL PANEL OPENING HAS A POSSIBLE CRACK

Source: SDR KCSA201608121049
OTHER · 2016-08-12 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 903) · airframe 86,316 hrs · 21,676 cycles

BS 903.5, RBL 89, WL-194. FRAME HAS 1.250" CRACK.

Source: SDR KCSA201608121051
OTHER · 2016-08-10 Matched by certificate designator
ATA 5312

Part: STRUCTURE — CRACKED (NLG WW) · airframe 86,317 hrs · 21,676 cycles

A FOUR INCH CRACK IN THE NOSE WHEEL WELL LT AFT VERTICAL STRUCTURE AT BS 287 AT ABOUT WL 173.

Source: SDR KCSA201608101046