N442YX
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.
19 reports on file, 2015-08-10 – 2022-11-11.
Part: LIGHT — MISSING (ROW S 3-4D) · airframe 19,303 hrs · 13,099 cycles
PHOTOLUMINESCENT STRIP MISSING ROW 3-4D. INSTALLED MISSING PHOTOLUMINESCENT STRIPS.
Earlier reports · 2015–2021 · 18 reports
2021
Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 16,681 hrs · 11,257 cycles
WHILE IN HEAVY CHECK - SHEAR CLIP CORRODED AT FR 88, STGR 27R-28R. REMOVED AND REPLACED SHEAR CLIP AT FR 88, STGR 27R-28R. REF: SRM 51-40-08
Part: SIGN — CRACKED (CABIN) · airframe 15,344 hrs · 10,369 cycles
AFT LH EXIT IDENTIFIER SIGN CRACKED. R&R AFT RH EXIT IDENTIFIER SIGN IAW AMM 33-50-15.
2020
Part: HOOK — OBSTRUCTED (L1 DOOR) · airframe 13,635 hrs · 9,239 cycles
L1 DOOR DOES NOT OPEN ALL THE WAY UNLESS THE GUST LOCK IS MANUALLY MOVED OUT OF POSITION. CLEANED DEBRIS FROM L1 DOOR GUST LOCK HOOK, OPS CHECK NORMAL.
Part: GCU — FAULTY (NR 1) · airframe 13,375 hrs · 9,075 cycles
ELECTRICAL POWER LOSS, AVNX MAU 1B FAIL. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R GCU 1.
2019
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,596 hrs · 7,859 cycles
***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** CENTER FUSELAGE III FLOOR STRUCTURE RH SHEAR WEB BETWEEN FR 87-88 RBL 36 AND RBL 20 FOUND CORRODED. CENTER FUSELAGE III FLOOR STRUCTURE RT SHEAR WEB BTWN FR 87-88 RBL 20-LBL 20 BOTH REPLACED IAW SRM 51-42-01 & 51-42-03 & 51-43-03. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,596 hrs · 7,859 cycles
***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** CENTER FUSELAGE III FLOOR STRUCTURE GUSSET PLATE AT FR 90 RBL 20 FOUND CORRODED. CENTER FUSELAGE III FLOOR STRUCTURE GUSSET PLATE AT FR 90 RBL 20 REPLACED IAW SRM 51-41-02. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,596 hrs · 7,859 cycles
***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** CENTER FUSELAGE III FLOOR STRUCTURE GUSSET PLATE AT FR90 AND RBL12 FOUND CORRODED. CENTER FUSELAGE FLOOR STRUCTURE GUSSET AT FR90 AND RBL12 REPLACED IAW SRM 51-41-02. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 11,596 hrs · 7,859 cycles
***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** CENTER FUSELAGE I PASSENGER CABIN FLOOR STRUCTURE, CRACK FOUND AT ANGLE FR 12 BL 0 AREA. CENTER FUSELAGE I PASSENGER CABIN FLOOR STRUCTURE ANGLE AT FR 12 BL 0 REPLACED IAW SRM 51-41-01. CRACK LENGTH 0.5". A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: WINGLET — CRACKED (LT WING) · airframe 11,596 hrs · 7,859 cycles
WHILE AC WAS IN FOR HVY CK FOUND LT WINGLET FRONT SPAR CRACKED AT LOWER ATTACHMENT. MX REMOVED AND REPLACED LT WINGTIP PN 171-16240-407 IAW AMM 57-30-00. SEE NRC # 4000515-5000-0005 FOR WORK PERFORMED. AC REMAINS IN YRQ FOR COMPLETION.
Part: WINGLET — CRACKED (RT WING) · airframe 11,596 hrs · 7,859 cycles
WHILE AC WAS IN FOR HVY CK FOUND RH WINGLETT FRONT SPAR CRACKED AT LOWER ATTACHMENT. MX REMOVED AND REPLACED RT WINGLETT PN 171-16240-408 IAW AMM 57-30-00. AC REMAINS IN YRQ FOR COMPLETION.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,137 hrs · 7,542 cycles
EMERGENCY EXIT LIGHTED SIGN ABOVE L1 DOOR INOP. R&R EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. R&R L1 DOOR CEILING EXIT LIGHT IAW AMM 33-50-05. OPS CHECK GOOD.
Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 10,817 hrs · 7,320 cycles
AFT CABIN CEILING EMERGENCY LIGHT NOT ILLUMINATING. R&R NUMBER 3 EMERGENCY POWER UNIT.
2017
Part: LIGHT — MISSING (CABIN) · airframe 6,140 hrs · 4,334 cycles
EMERGENYC LIGHT STRIP AT ROW 10 AIRCRAFT LEFT MISSING. FOUND AND INSTALLED THE LIGHT IAW MM 33-50-21.
2016
Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 4,581 hrs · 3,297 cycles
CREW REPORTED THAT THE PHOTO LUMINESCENT STRIP WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED PHOTO LUMINESCENT STRIP PER AMM AND OPS CHECKED GOOD.
Part: SLAT — DAMAGED (RT WING) · airframe 3,413 hrs · 2,505 cycles
CREW REPORTED A BIRD STRIKE FOLLOWED BY A SLAT FAIL MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMAINS OUT OF SERVICE. MAINTENANCE R&R RIGHT HAND NR 4 SLAT PER EMB AMM AND OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,269 hrs · 1,679 cycles
CREW REPORTED THAT THE OVERHEAD EMERGENCY FLIGHT WAS INOPERATIVE. MAINTENANCE R & R ELPU IAW AMM AND OPS CHECKED GOOD.
2015
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,879 hrs · 1,388 cycles
CREW REPORTED THAT THE AFT CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE R & R EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,360 hrs · 998 cycles
MAINTENANCE REPORTED THAT THE FORWARD EXIT LOCATOR SIGN WAS INOPERATIVE. MAINTENANCE R & R EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD.