N959LR
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.
39 reports on file, 2016-09-08 – 2024-03-23.
Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 16,801 hrs · 12,708 cycles
FUSELAGE SKIN UNDER FOOTPRINT OF R/H VENTRAL FIN HAS NUMEROUS GOUGES AND DENTS. REPAIRED FUSELAGE SKIN UNDER FOOTPRINT OF R/H VENTRAL FIN IAW MHI RJ REO 690-53-00-555 REV-- DATED 2024-03-01. REFERENCE TASK CARD FOR DETAILS OF WORK PERFORMED
Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,801 hrs · 12,708 cycles
R/H COCKPIT FLOOR BEAM AT RBL 12.00 IS CRACKED ALONG THE OUTBOARD VERTICAL FLANGE AT F.S. 280.00. REPAIRED DAMAGE I.A.W. MHIRJ AVIATION REO 690-53-11-1688 REV.--, DATED 2024-02-13.
Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 16,801 hrs · 12,708 cycles
FUSELAGE SKIN UNDER FOOTPRINT OF L/H VENTRAL FIN HAS NUMEROUS GOUGES AND DENTS. REPAIRED FUSELAGE SKIN UNDER FOOTPRINT OF L/H VENTRAL FIN IAW MHI RJ REO 690-53-00-554 REV-- DATED 2024-03-01. REFERENCE TASK CARD FOR DETAILS OF WORK PERFORMED
Earlier reports · 2016–2023 · 36 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 16,340 hrs · 12,345 cycles
AFT CABIN FLASHLIGHT INOP- INSP, OP CHECK GOOD
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 16,132 hrs · 12,188 cycles
PAX DOOR LWR EME LIGHT COVER DETACHED APPLIED ADHESIVE TO LWR EME LIGHT COVER 62743
2022
Part: NONE — NONE · airframe 15,831 hrs · 11,964 cycles
ROW 12 EMER EXIT SIGNS INOP. R2 #3 BATTERY PACK.
Part: NONE — NONE · airframe 15,372 hrs · 115,687 cycles
DCP FAILURE (EMER DECLARED). REPLACED DCP1.
2021
Part: NONE — BENT (STRUCTURE PLATE) · airframe 13,684 hrs · 10,399 cycles
AVIONICS BAY DOOR SURROUND STRUCTURE PLATE WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-21-23-001-003-A01, ITEM 31, EA 79-2021-236.
Part: NONE — NONE (FS 1015, LBL 9.0) · airframe 13,684 hrs · 10,399 cycles
CORROSION AFFECTING THE FLOOR BEAM AT FS1015, LBL 9.00. PERFORMED PERMANENT REPAIR IAW SRM 53-61-43-991-801, ITEM 1B, EA 80-2021-136.
Part: NONE — NONE (LOCATION OUTER) · airframe 13,684 hrs · 10,399 cycles
FWD BAGGAGE BAY DOOR OUTER SKIN WAS DISCOVERED WITH NICKS. PERFORMED PERMANENT REPAIR IAW SRM 52-35-01-001-001-A01, FIGURE 52-35-01-991-801, ITEM 1, EA 79-2021-234
Part: NONE — NONE (OUTER SKIN & DOU) · airframe 13,684 hrs · 10,399 cycles
FWD BAGGAGE-BAY DOOR OUTER SKIN AND DOUBLER WERE DISCOVERED WITH NICKS. PERFORMED PERMANENT REPAIR IAW SRM 52-35-01-001-001-A01, FIGURE 52-35-01-991-801, ITEMS 1, A, AND 2, EA 79-2021-235.
Part: NONE — NONE (FS469.00-FS477.0) · airframe 13,684 hrs · 10,399 cycles
LOWER FUSELAGE SKIN BETWEEN FS469.00 - FS477.00 AND STGR 22R - STGR 23R WAS FOUND TO HAVE PREVIOUS BLEND OUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-807, ITEM 1E, EA 69-2021-158.
Part: NONE — NONE (FS311.75&INTERC) · airframe 13,684 hrs · 10,399 cycles
PASSENGER DOOR FORMER AT FS 311.75 AND INTERCOSTAL DD6 WERE FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 523-11-06-001-001-A01, ITEMS 3A, 19A, 33, AND 44, EA 20-2021-177.
Part: NONE — NONE (FS1015.00, LBL27) · airframe 13,684 hrs · 10,399 cycles
UPPER CAP OF THE LBL27.00 FLOOR BEAM AT FS1015.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-61-43-001-001-A01, FIGURE 53-61-43-991-801, ITEM 3C, EA 79-2021-230.
Part: NONE — NONE (AFT INNER ARM) · airframe 13,684 hrs · 10,399 cycles
CENTER BAGGAGE BAY DOOR WAS FOUND WITH GOUGE DAMAGE ON THE INNER ARM. PERFORMED PERMANENT REPAIR IAW SRM 51-21-16 & 52-35-09, EA 20-2021-178.
Part: NONE — DAMAGED (LEADING EDGE SKI) · airframe 13,684 hrs · 10,399 cycles
RH WING FIXED LEADING EDGE SKIN SS57.16 -SS144.94 (PANEL NUMBER 622AR AND PIN CC670-12201-8) & LEADING EDGE SKIN SS294.04-SS37.66 (PANEL NUMBER 631AR AND P/N CC670-12401-8) WERE FOUND TO HAVE WEAR DAMAGE ON THE OUTER SKIN SURFACE. PERFORMED PERMANENT REPAIR IAW SRM 57-41-01-001-001-A01, EA 12-2021-240.
Part: NONE — NONE (FS193.00 ABVE ST) · airframe 13,684 hrs · 10,399 cycles
HYDRAULIC BAY FUSELAGE SKIN AT FS193.00 ABOVE STGR19L WAS FOUND TO HAVE SCRATCH DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-11-01-001-007-A01, FIGURE 53-11-01-991-807, ITEMS 1A, B, AND C, EA 79-2021-232.
Part: NONE — BENT (FS310.00 & FS349) · airframe 13,684 hrs · 10,399 cycles
LOWER STRIKER WAS FOUND TO BE BENT / DEFORMED FROM CONTOUR. PERFORMED PERMANENT REPAIR IAW SRM 53-21-23-001-001-A01, EA 83-2021-043.
Part: NONE — NONE (FS 1051.30 & STR) · airframe 13,684 hrs · 10,399 cycles
FUSELAGE SKIN AT FS 1051.30 AND STR 21L WAS FOUND TO HAVE DENT DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 51-24-21, EA 69-2021-095.
Part: NONE — NONE (COPPER MESH) · airframe 13,684 hrs · 10,399 cycles
LH/RH WINGLET TIP FAIRING ASSEMBLIES WERE FOUND TO HAVE EROSION DAMAGE AFFECTING THE COPPER MESH.PERFORMED PERMANENT REPAIR IAW SRM 54-30-84-001-001-A01 & 51-73-00-201-001-A01, EA 12-2021-231.
Part: NONE — NONE (RH LIGHTNING PRO) · airframe 13,684 hrs · 10,399 cycles
RH WINGLET TIP FAIRING ASSEMBLY WAS FOUND TO HAVE A CORROSION DAMAGE AFFECTING THE RH LIGHTNING PROTECTION. PERFORMED PERMANENT REPAIR IAW SRM 57-30-84-001-001-A01, EA 12-2021-238.
Part: NONE — NONE (FS311.75&INTERC) · airframe 13,684 hrs · 10,399 cycles
PASSENGER DOOR FORMER AT FS 311.75 AND INTERCOSTAL DD6 WERE FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 523-11-06-001-001-A01, ITEMS 3A, 19A, 33, AND 44, EA 20-2021-177.
Part: NONE — NICKED (FWD BAGGAGE BAY) · airframe 13,684 hrs · 10,399 cycles
FOWARD BAGGAGE-BAY DOOR OUTER SKIN AND DOUBLER WERE DISCOVERED WITH NICKS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 52-35-01-001-001-A01, FIGURE 52-35-01-991-801, ITEMS 1A, EA 79-2021-235.
Part: STRIKER — NONE (FS310.00 -FS349.) · airframe 13,684 hrs · 10,399 cycles
LOWER STRIKER WAS FOUND TO BE BENT/ DEFORMED FROM CONTOUR. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-23-001-001-A01, EA 83-2021-043.
Part: SKIN — NONE (FS469.00-FS477.0) · airframe 13,684 hrs · 10,399 cycles
LOWER FUSELAGE SKIN BETWEEN FS469.00 - FS477.00 AND STR 22R - STR 23R WAS FOUND TO HAVE PREVIOUS BLEND OUTS. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, FIGURE 53-21-01-991-807, ITEM 1E, EA 69-2021-158.
Part: DOUBLER — CORRODED (FS913.00 & FS881) · airframe 13,684 hrs · 10,399 cycles
POTABLE WATER SERVICING DOUBLER BETWEEN FS913.00 & FS881.00 WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23, FIGURE 53-51-23-991-803, ITEM 3, EA 83-2021-042.
Part: SKIN — DAMAGED (FS 349/STR 22R &) · airframe 13,684 hrs · 10,399 cycles
FUSELAGE SKIN AFT OF FS 349, BETWEEN STR. 22R AND STR. 23R (ADJACENT TO THE POTABLE WATER SERVICE CUT OUT}, WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01, EA 20-2021-175.
Part: PLATE — NONE (LAV WASTE SVC SS) · airframe 13,684 hrs · 10,399 cycles
SACRIFICIAL PLATE OF THE LAVATORY WASTE SERVICING SURROUND STRUCTURE WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-51-23, FIGURE 53-51-23-991-802, ITEM 6, EA 81-2021-075.
Part: SKIN — DAMAGED (FS 1051.30 & STR) · airframe 13,684 hrs · 10,399 cycles
FUSELAGE SKIN AT FS 1051.30 AND STR 21L WAS DELIVERED WITH DENT DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 51-21-11, 51-25-06, 51-25-16, 51-21-11, EA 69-2021-159
Part: NONE — NONE (FS485,00-FS501.0) · airframe 13,684 hrs · 10,399 cycles
LOWER FUSELAGE SKIN BETWEEN FS485.00 - FS501.00 & STGR26R - STGR26L WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-991-806, ITEM 1C, EA 72-2021-169.
Part: SKIN — CORRODED (FS485.00-FS501.0) · airframe 13,684 hrs · 10,399 cycles
LOWER FUSELAGE SKIN BETWEEN FS485.00 - FS501.00 & STGR26R - STGR26L WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-31-01, FIGURE 53-31-01-991-806, ITEM 1C, EA 72-2021-169
Part: SKIN — CORRODED (BS 469-477) · airframe 13,684 hrs · 10,399 cycles
LOWER FUSELAGE SKIN BETWEEN FS469.00 - FS477.00 & STR 22R - STR 23R WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ700/900 SRM 53-21-01, FIGURE 53-21-01-991-807, ITEM 1E, EA 69-2021-158.
Part: FLOORBEAM — CORRODED (BS 1015 LBL 9.0) · airframe 13,684 hrs · 10,399 cycles
CORROSION AFFECTING THE FLOOR BEAM AT FS1015, LBL 9.00. PERFORMED PERMANENT REPAIR IAW CRJ700/900 SRM 53-61-43-991-801, ITEM 1B, EA 80-2021-136.
2020
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 1,172 hrs · 8,585 cycles
MID CABIN EXIT SIGN FWD FACING LTS INOP. ALLOWED BATTERY TO CHARGE.
2019
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,776 hrs · 6,779 cycles
AFT FA FLASHLIGHT INOP. PERFORMED OPS CHECK, OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,979 hrs · 6,178 cycles
LT AFT EMERGENCY LIGHT INOP. REPLACED BULBS.
2017
Part: DOOR — UNKNOWN (CABIN) · airframe 5,285 hrs · 4,123 cycles
PAX DOOR DIFFICULT TO OPEN.
2016
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 2,500 hrs · 1,947 cycles
FORWARD F/A FLASHLIGHT INOPERATIVE. PLACED ON MEL.
Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 2,422 hrs · 1,885 cycles
ELECTRICAL BURNING ODOR IN CABIN AND COCKPIT.