N826AY
Registered owner: SLATE CRJ ACQUISITIONS 1 LLC, PA (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.
26 reports on file, 2005-05-05 – 2013-03-07.
Part: SKIN — CHAFED (RT WING) · corrosion level 2 · airframe 17,712 hrs · 15,155 cycles
REMOVED CHAFE ON RIGHT WING FUEL CUTOUT PANEL LANDING 640BB, HOLE NR 1, IN THE NON-CRITICAL AREA WITHIN LIMITS IAW BOMBARDIER REO 601R-57-21-030 REV J.
Part: ANGLE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 17,712 hrs · 15,155 cycles
LEFT FLOOR SILL PLATE ANGLE OVERWING BOX CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.
Part: ANGLE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 17,712 hrs · 15,155 cycles
RIGHT FS 280 BEAM LOWER ANGLE IS CRACKED AT VERTICAL POSTS JUST OUTBOARD OF RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,712 hrs · 15,155 cycles
LEFT FS 280 BEAM UPPER ANGLE IS CRACKED JUST OUTBOARD OF LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-138.
Part: ANGLE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 17,712 hrs · 15,155 cycles
LEFT FS 280 BEAM LOWER ANGLE CRACKED JUST BELOW THE PULLEY BRACKET AND OUTBOARD OF LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,711 hrs · 15,155 cycles
AFT CARGO COMPARTMENT FLOORBOARD LANDING CORRODED ON FWD FACE OF THE FS 621 BULKHEAD AT LBL 39. REPAIRED IAW BOMBARDIER REO 601R-53-61-117.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,712 hrs · 15,155 cycles
RIGHT FLOOR SILL PLATE ANGLE OVERWING BOX CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.
Part: FUEL CONTROL — OUT OF RIG (ENGINE) · airframe 17,546 hrs · 14,999 cycles
DURING START TO TAKE AIRCRAFT TO THE GATE RECEIVED HOT ICON, NO FUEL APPLIED, FLAMES COMING OUT OF ENGINE AND ENGINE FIRE BOTTLES WERE DISCHARGED. REMOVED AND REPLACED NR 2 FIRE BOTTLE IAW AMM 26-21-10. RIGGED RIGHT FUEL CONTROL IAW AMM 76-10-00. OK FOR SERVICE.
Part: ACTUATOR — FAILED (TE FLAP) · airframe 17,543 hrs · 14,996 cycles
ON FLIGHT 3867 (BUF TO DTW) RECEIVED FLAPS FAIL AT 20 DEGREES ON APPROACH INTO DTW. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED DECEMBER 07, 2012 AND PA AD27-052J (DOCUMENT WORK PERFORMED) INSPECTED FLAP ACTUATORS FOR LEAKS & DAMAGE, OPERATED FLAPS 5 CYCLES CHECKED BALL NUTS FOR OVERHEAT ON LEFT WING. REMOVED AND REPAIRED FLAP ACTUATORS 1-1 & 1-2. REMOVED & REPAIRED FLEX SHAFT 2, 3, 4. ALL CHECKS GOOD AT THIS TIME.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,513 hrs · 14,969 cycles
CEILING EMERGENCY FLOOD LIGHT, LIGHT NR 1. RE-LAMP CEILING LEVEL EMERGENCY FLOOD LIGHT IAW 33-51-16.
Earlier reports · 2005–2012 · 16 reports
2012
Part: PRIORITY VALVE — MALFUNCTIONED (MLG) · airframe 17,430 hrs · 14,888 cycles
ON FLIGHT 4145 (PVD TO DTW) CREW RECEIVED NOSE GEAR DISAGREE MESSAGE AND THE CREW DECLARED AN EMERGENCY. HYDRAULIC PRESSURE SHOWED NORMAL (2900), NOSE GEAR STAYED DOWN (DID NOT RETRACT). MAIN GEAR RETRACTED NORMALLY. QRH COMPLETE. THE FLIGHT PERFORMED AN AIR RETURN BACK TO PVD AND RETURNED SAFELY. COMPLIED WITH PA 05-018J AND REPLACED THE MLG PRIORITY VALVE IAW AMM. ALL OP CHECKS GOOD.
Part: BRACKET — DAMAGED (NLG) · airframe 16,550 hrs · 14,007 cycles
AFTER T/O NOSE GEAR DID NOT RETRACT RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE MASTER WARNING. COMPLIED SCENARIO 1 OF PA -05-018F AND FOUND CENTERING /OLEO EXTENSION PROX SENSOR BRACKET DAMAGED. SEE AML 2167904 DISC NR 2 FOR CORRECTIVE ACTION.
Part: ARM — UNSECURE (RADOME) · airframe 15,930 hrs · 13,390 cycles
AIR RETURN FOR THE FOLLOWING: AFTER LIFT OFF, HEARD CLUNCKING IN RT NOSE AREA. FOUND RADOME SECURE ARMS UNSECURED AND FREE MOVING RESECURED ARMS IAW AMM 53-81-01.
2011
Part: WIRE — DAMAGED (RT IDG) · airframe 15,353 hrs · 12,877 cycles
IDG 2 CAUTION MSG. EMERGENCY DECLARED. IDG 2 INTERMITTENT BUT MOSTLY ON AFTER FL170. REPAIRED WIRE TO RT IDG OVERTEMP SWITCH IAW ESPM 20-17-10. RECONNECTED RT IDG IAW AMM 24-11-01. OPC GOOD.
Part: UPLOCK — MALFUNCTIONED (RT MLG) · airframe 14,477 hrs · 12,003 cycles
GEAR UP DISAGREE WARNING MSG IN FLIGHT, AFTER QRH MSG CLEARED REMOVED AND REPLACED RT MLG UPLOCK IAW AMM 32-32-05. VERIFIED PART EFFECTIVITY & COMPLIED WITH PA 05-018B GEAR DISAGREE EVENT PROCEDURES.
Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 14,293 hrs · 11,840 cycles
FLAPS FAILED AT ZERO AFTER TAKEOFF CONTINUED ON, LANDED WITHOUT INCIDENT. /R RT BPSU IAW AMM 27-51-10 OP CHECK GOOD.
Part: SKIN — DENTED (FUSELAGE) · airframe 14,087 hrs · 11,653 cycles
EXISTING FUSELAGE REPAIR DOUBLER JUST FORWARD OF FS 640 BETWEEN STRINGERS S-21R AND 23R FOUND DENTED. REPAIRED IAW BOMBARDIER SERVICE CORPORATION 601R-53-21208A AND ASSOCIATED 8110-3 DATED 4/21/11.
Part: FASTENER — MISSING (RT WING) · airframe 13,693 hrs · 11,299 cycles
ONE OF THE STUD NUT FASTENERS (P/N CA2023-5) FOR THE RT WING LANDING RECOGNITION LIGHT WAS FOUND MISSING. TEMPORARY REPAIR IAW STS ENGINEERING EA 09-2011-040. REPEAT INSPECT EVERY 150 FH. WITHIN 500 FLIGHT HOURS, ACCOMPLISH A PERMANENT REPAIR TO THE DAMAGED AREA.
Part: DOOR SEAL — LEAKING (DOOR) · airframe 13,657 hrs · 11,267 cycles
FLT 3837 YOW-DTW DIVERTED TO YYZ HAD LOUD DOOR SQUEAL FOLLOWED BY LOSS OF PRESSURIZATION APPROX 45 MIN INTO THE FIGHT. EMERGENCY DESCENT TO 1000 FT. EMERGENCY DECLARED AND DIVERTED TO YYZ. A/C LANDED SAFELY IN YYZ. INSPECTED AND CLEANED DOOR SEAL AND DOOR SURROUND PER AMM 52-11-00. OPS CHECK GOOD PER AMM 52-11-00 AND 21-32-00, RETURNED TO SERVICE TO DTW. DOOR SEAL WAS LATER REPLACED IN DTW IAW AMM 52-11-10.
2010
Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 13,428 hrs · 11,061 cycles
EN ROUTE AT FL290 FROM KBHM TO KDTW THE FLIGHT CREW DETECTED THE SOUND OF A HIGH PITCHED RUSHING AIR SOUND. CABIN ALTITUDE INDICATED A 1000-1300 FPM CLIMB. THE FLIGHT CREW DONNED O2 MASKS, DECLARED AN EMERGENCY AND BEGAN AN EMERGENCY DESCENT. ON DESCENT AROUND THE MID 20'S FLIGHT LEVEL THE FLIGHT CREW MANUALLY DEPLOYED THE PASSENGER O2 SYSTEM. THE FLIGHT WAS VECTORED TO KSDF, THE CLOSEST SUITABLE AIRPORT. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KSDF. DUE TO A BURNING SMELL, THE FLIGHT CREW REQUESTED CFR MEET THE AIRCRAFT. CFR DETERMINED THAT THERE WAS NO FIRE. THE PASSENGERS WERE BUSSED TO THE TERMINAL AND THE AIRCRAFT TOWED TO THE GATE. MAINTENANCE IS IN PROGRESS AND THE AIRCRAFT WILL BE FERRIED TO KFWA FOR DETAILED TROUBLESHOOTING AND REPAIR.
Part: DOUBLER — DENTED (FUSELAGE) · airframe 12,889 hrs · 10,553 cycles
DENT 2"L X 1.9"W X .075" DEEP, ON DOUBLER INSTALLED BETWEEN FS 640-625 AND STR 21R-23R PER PREVIOUS REO 601R-53-61-3563. FLY-ON FOR 1650 FH PER REO 601R-53-61-3823 TO NEXT C CHECK WHEN A PERMANENT REPAIR WILL BE PERFORMED.
2009
Part: ACM — FAILED (RIGHT) · airframe 10,386 hrs · 8,216 cycles
ON TAXI, ODOR OF SMOKE NOTICED IN CABIN, RETURNED TO BLOCK. AIRCRAFT INSPECTED AND DETERMINED TO BE A FAILED RIGHT AIR CYCLE MACHINE (ACM). DEFERRED PER MEL RETURNED TO SERVICE.
Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY)
AFTER TAKE OFF RECEIVED LAVATORY SMOKE MSG WITH NO ACTUAL VISUAL SMOKE OR FUMES. TROUBLESHOT LAVATORY SMOKE DETECTION SYSTEM AND DETERMINED TO BE A FALSE SMOKE INDICATION. SYSTEM DEFERRED UNDER MEL 26-16-01.
2005
Part: ACTUATOR — FAILED (TE FLAP) · airframe 1,221 hrs · 897 cycles
FLAPS FAIL ON APPROACH WHEN SELECTED TO 30. FOLLOWED QRH, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATORS POSITION 1 AND 2 P/N 852D100-19.
Part: FCU — FAILED (TE FLAPS)
(REF NR: 05-061) FLAPS FAIL AT ZERO ON CLIMB-OUT. QRH FOLLOWED, EMERGENCY DECLARED RETURNED TO DEPARTURE WITH UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT. (FECU) (K)
Part: BPSU — FAILED (TE FLAPS)
(REF NR: 05-060) FLAP FAIL MESSAGE UPON POWER UP. REMOVED AND REPLACED RT BRAKE POSITION SENSING UNIT (BPSU). (K)