N942
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
10 reports on file, 2021-07-09 – 2021-08-03.
Part: SKIN — CRACKED (THRUST REVERSER) · airframe 37,006 hrs · 30,279 cycles
RH UPPER TRANSCOWL WAS FOUND TO HAVE (2) CRACKS IN THE INNER SKIN, THE CRACKS EMANATE FROM A FASTENER HOLE FOR A NAS1720H FASTENER. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 54-21-01, FIGURE 54-21-05-991-801, ITEM 2, 3A, 12, EA 12-2021-189
Part: SKIN — DENTED (LT NACELLE DOOR) · airframe 37,006 hrs · 30,279 cycles
LH ENGINE FAN COWL DOOR LOWER OUTER SKIN PANEL WAS FOUND WITH (3) MINOR DENTS. PERFORMED PERMANENT REPAIR AIW CRJ?00/900 SRM 54-14-00-101-001-A01, EA 12-2021-176.
Part: WEDGE — GOUGED (NR 1 RT SLAT) · airframe 37,006 hrs · 30,279 cycles
TRAILING EDGE OF THE RH SLAT #1 WAS FOUND TO HAVE A GOUGE ALONG THE AFT MOST SURFACE OF TH TRAILING EDGE AT SS 128.00. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 57-41-01-001-002-A01, ITEM 2A, EA 10-2021-035. (PART DEFECT LOCATION: TRAILING EDGE AT SS 128.00)
Part: CHANNEL — CORRODED (BS 1031-1051) · airframe 37,006 hrs · 30,279 cycles
CHANNEL BETWEEN FS1031.00-FS1051.30 AT STGR27 WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 53-61-04, FIGURE 53-61-04-991-804, ITEM 17, EA 48-2021-017. (PART DEFECT LOCATION CHANNEL FS1031,00-FS 1051,30 AT STGR27)
Part: SKIN — DAMAGED (RT ELEVATOR TE) · airframe 37,006 hrs · 30,279 cycles
RH ELEVATOR UPPER SKIN WAS FOUND TO HAVE LIGHTNING STRIKE DAMAGE. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 55-21-01, FIGURE 55-21-01-991-804, ITEM 3C, EA 69-2021-116. (PART DEFECT LOCATION TRAILING EDGE/RIBS 11 & 13)
Part: SKIN — DAMAGED (BS 333-349) · airframe 37,006 hrs · 30,279 cycles
FUSELAGE SKIN BETWEEN FS333.00 & FS349.00 AND AT STGR 23 WAS FOUND TO HAVE A PREVIOUS BLEND OUT, THE BLEND TOOK PLACE OVER A FASTENER ROW. PERFORMED PERMANENT REPAIR AIW CRJ700/900 SRM 53-21-01, FIGURE 53-21-01-991-807, ITEM 1C, EA 83-2021-021. (PART DEFECT LOCATION: FUSELAGE/FS333.00 & FS349,00I STGR 23)
Part: SEAT TRACK — CORRODED (BS 677-830 RBL9) · airframe 37,006 hrs · 30,279 cycles
CORROSION ON FLOOR SEAT RAILS IN SECTION [ FS= 677 TO FS= 830, 9RBL ] AND SECTION OF SEAT RAIL WAS REPLACED PER CRJ-900 AMM 53-00-49-400-801-A11
Part: FRAME — CORRODED (BS 319 S26R/L) · airframe 37,006 hrs · 30,279 cycles
FRAME FS= 319 BETWEEN STRG 26LH TO 26RH WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 847-977 RBL9) · airframe 37,006 hrs · 30,279 cycles
CORROSION ON FLOOR SEAT RAILS IN SECTION [ FS= 847+48 TO FS= 977, 9RBL] CORRECTIVE ACTION: SEAT RAIL WAS REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A11)
Part: SEAT TRACK — CORRODED (BS 847-977 LBL9) · airframe 37,006 hrs · 30,279 cycles
CORROSION ON FLOOR SEAT RAILS IN SECTION [ FS= 847+48 TO FS= 977, 9LBL] CORRECTIVE ACTION: SEAT RAIL WAS REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A11)