N8884E
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.
89 reports on file, 2005-12-02 – 2020-03-24.
Part: PLATE — CORRODED (FUSELAGE) · airframe 33,016 hrs · 30,993 cycles
SERVICE DOOR SILL THRESHOLD PLATE HAS CORROSION DAMAGE. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED SERVICE DOOR THRESHOLD PLATE IAW CRJ200 SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,016 hrs · 30,993 cycles
CABIN FLOOR SEAT TRACK RBL 6 HAS CORROSION AT FASTENER HOLES FS 409+128 TO FS 574 (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED NEW SEAT TRACK PART# 66556-144 AT RBL6 409+128 FS574 IAW CRJ200 SRM.
Part: SPRING — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
RIGHT WING #3 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED RIGHT WING #3 O/B FLAP HINGE BOX BUTE COMPRESSION SPRING IAW CRJ200 CMM. TW:STS 3817 DUE: 05 APR 20
Part: SPRING — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
RIGHT WING #4 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING IS CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED RIGHT WING #4 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING IAW CRJ200 AMM.
Part: BOLT — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
L/H O/B FLAP #3 HINGE BOX UNDER SPRING HAS 4 CORRODED MOUNT BOLTS (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED L/H O/B FLAP #3 HINGE BOX MOUNTING BOLTS IAW CRJ 200 AMM.
Part: BOLT — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
L/H O/B FLAP #4 HINGE BOX UNDER SPRING HAS CORRODED MOUNT BOLTS. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED L/H O/B FLAP #4 HINGE BOX UNDER SPRING (04) FOUR MOUNT BOLTS. IAW CRJ200 AMM. CALIBRATED TOOL: TOOL WRENCH STS-3818 S/N 0518901775 CAL DUE DATE: 05 APR 2020
Part: BOLT — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
R/H O/B FLAP #5 HINGE BOX UNDER SPRING HAS 4 CORRODED MOUNTS BOLTS. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACE 4 MOUNT BOLTS AND 4 WASHERS ON R/H OUTBOARD FLAP NUMBER 5 HINGE BOX IAW CRJ200 AMM. TORQUE WRENCH STS 3818 SERIAL NUMBER 0518901775. CAL DUE DATE 05 APRIL 2020.
Part: BOLT — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
R/H O/B FLAP #4 HINGE BOX UNDER SPRING HAS 4 CORRODED MOUNT BOLTS. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED 4 MOUNT BOLTS AND 4 WASHERS ON R/H O/B FLAP # 4 HINGE BOX IAW CRJ200 AMM TORQUE WRENCH: P/N:STS 3818, S/N:0518901775, CAL DUE DATE:05/APR/2020.
Part: SPRING — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
LEFT WING #5 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #5 O/B FLAP HINGE BOX BUTE COMPRESSION SPRING IAW CRJ200 AMM.
Part: BOLT — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
R/H O/B FLAP #3 HINGE BOX UNDER SPRING HAS 4 CORRODED MOUNT BOLTS. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED R/H O/B FLAP #3 HINGE BOX UNDER SPRING (4) FOUR MOUNT BOLTS IAW CRJ-200 AMM. CALIBRATED TOOL: TORQUE WRENCH STS-3818 CAL DUE DATE: 05 APR 2020. SERIAL NO.:0518901775
Part: BOLT — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
L/H O/B FLAP #5 HINGE BOX UNDER SPRING HAS CORRODED MOUNT BOLTS. (C-CHECK) RO 4/22/2020 REPLACED 4 CORRODED MOUNTING BOLTS ON L/H O/B FLAP #5 HINGE BOX UNDER SPRING IAW CRJ200 AMM.
Part: LINK ASSY — CORRODED (RT AILERON) · airframe 33,016 hrs · 30,993 cycles
FOUND R/H WING AILERON FLUTTER DAMPER SHEAR LINK ASSY TO BE CORRODED. NEEDS TO BE REPLACED. (C-CHECK) RO 4/22/2020 REPLACED R/H WING AILERON FLUTTER DAMPER SHEAR LINK ASSY. IAW CRJ 200 AMM.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 33,016 hrs · 30,993 cycles
FS280 RIGHT SIDE OF COCKPIT ENTRY, AFT ATTACH ANGLE IS CRACKED (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED AFT ATTACH ANGLE,RIGHT SIDE COCKPIT ENTRY, FS 280, RBL45. IAW CRJ200 SRM AND CRJ200 (TR51-42) SRM.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 33,016 hrs · 30,993 cycles
FS280 LEFT SIDE OF COCKPIT ENTRY, FLOOR SUPPORT ANGLE IS CRACKED.(CAM-LOC ANGLE) (C-CHECK) RO 4/22/2020 REMOVED DAMAGED FLOOR SUPPORT ANGLE. LOCATED, DRILLED, DEBURRED AND COUNTERSUNK NEW FLOOR SUPPORT ANGLE. INSTALLED NEW FLLOR SUPPORT ANGLE IAW CRJ 200 SRM.
Part: ATTACH ANGLE — BROKEN (FUSELAGE) · airframe 33,016 hrs · 30,993 cycles
CARGO DOOR STRUCTURE SUPPORT FRAME, ATTACH ANGLE IS BROKEN AT AFT SIDE, WHERE IT ATTACHES TO FS621 BULKHEAD. BELOW DOOR TRACK AT LBL36. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED CARGO DOOR STRUCTURES SUPPORT FRAME ATTACH ANGLE AT AFT SIDE FS 621 BULKHEAD IAW CRJ200 SRM
Part: FASTENER — CORRODED (RT SPOILER) · airframe 33,016 hrs · 30,993 cycles
4 CORRODED HARDWARE AT I/B HINGE AREA OF RT. WING FLIGHT SPOILER . (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED 4 CORRODED HARDWARE AT I/B HINGE ARE OF RT. WING FLIGHT SPOILER IAW CRJ200 AMM TORQUE WRENCH STS 3819 S/N0518901770 CAL DUE 05-APR-20
Part: FASTENER — CORRODED (SPOILER) · airframe 33,016 hrs · 30,993 cycles
5 EACH, CORRODED HARDWARES AT FLIGHT SPOILER CENTER HINGE ; INCLUDES GROUND JUMPER WIRE HARDWARE. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED 5 CORRODED HARDWARE TO INCLUDE GROUND JUMPER WIRE IAW CRJ AMM
Part: FASTENER — CORRODED (RT SPOILERON) · airframe 33,016 hrs · 30,993 cycles
6 EACH, HARDWARES CORRODED AT CENTER HINGE AREA OF RT. WING SPOILERON. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED 4 CORRODED HARDWARE, REMOVED AND REINSTALLED 2 AT CENTER HINGE AREA OF RIGHT SPOILERON I.A.W. CRJ200 AMM. TORQUE WRENCH: STS0384 DUE DATE: 05APR20.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,016 hrs · 30,993 cycles
LIGHT CORROSION ON SEAT TRACKAT FUS. STA. 409.00 TO FUS. STA.409.00 + 96; RBL 9 R (C-CHECK) RO 4/22/2020 REMOVED CORROSION FROM SEAT TRACK F.S. 409.00TO 409+128 RBL 9 IAW CRJ200 SRM. PERFORMED U.T. THICKNESS CK IAW BOMBARDIER CRJ200 NDTM. ORIGINAL WAS .100. REMAINING IS .075. CORROSION IS OUT OF LIMITS IAW CRJ200 SRM. LOCATED AND DRILLED NEW SEAT TRACK P/N 6656-144 IAW CRJ2OO SRM TEMP. REV. 51-42. TREATED NEW SEAT TRACK IAW CRJ200 SRM. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW P/N 6656-144 IAW CRJ200 SRM
Part: FASTENER — CORRODED (RT SPOILERON) · airframe 33,016 hrs · 30,993 cycles
5 EACH, HARDWARES AT O/B SPOILERON HINGE FITTING AREA CORRODED. ( RT. WING ) (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED 5 EACH HARDWARE AT O/B SPOILERON HINGE FITTING AREA ( R.T WING ) IAW CRJ200 AMM. TORQUE WRENCH-STS-3819 CAL DATE-5 APR 19 DUE DATE 5 APR 20
Part: BOLT — CORRODED (RT SPOILERON) · airframe 33,016 hrs · 30,993 cycles
5 CORRODED HARDWARES AT I/B HINGE AREA OF RT. WING SPOILERON. (C-CHECK) RO 4/22/2020 REMOVED & REPLACED 1 NUT ON I/B HINGE BOLT & 4 BOLTS ON I/B HINGE RETENTION ANGLE SAFETY TABS IAW CRJ 200 AMM. TW:STS-3819 CAL DUE: 04/2020
Part: NUT — CORRODED (LT SPOILER) · airframe 33,016 hrs · 30,993 cycles
LT. I/B FLT. SPOILER CENTER I/B HINGE BOLT NUT IS CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED L/T I/B FLIGHT SPOILER CENTER I/B HINGE NUT IAW CRJ200 AMM. TW: STS-0381 CAL DUE: 10 DEC 20.
Part: FASTENER — CORRODED (RT SPOILERON) · airframe 33,016 hrs · 30,993 cycles
RT. I/B FLT. SPOILER 2 EA. HINGE BOLT KEEPER HARDWARE IS CORRODED. (C-CHECK) RO 4/22/2020 REMOVED, REPLACED AND TORQUED RT. I/B FLT. SPOILER 2 EA. HINGE BOLT KEEPER HARDWARE IAW CRJ200 AMM. TORQUE WRENCH P/N: STS-3819, S/N: 0518901770, CAL DUE DATE: 05 APR 2020
Part: FASTENER — CORRODED (LT SPOILER) · airframe 33,016 hrs · 30,993 cycles
LT. I/B FLT. SPOILER I/B HINGE BOLT RETENSION CLIP HARDWARE IS CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LT I/B FLIGHT SPOILER I/B HINGE RETENSION CLIP BOLTS IAW CRJ200 AMM
Part: NUT — CORRODED (LT SPOILER) · airframe 33,016 hrs · 30,993 cycles
LT. I/B GRD. SPOILER O/B HINGE NUT IS CORRODED (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED L/H I/B GROUND SPOILER OUTBOARD HINGE NUT AND COTTER PIN IAW CRJ 200 AMM. TORQUE WRENCH: STS-0381 CAL DUE 10 DEC 20.
Part: NUT — CORRODED (RT SPOILERON) · airframe 33,016 hrs · 30,993 cycles
R.T. WING I/B SPOILERON HINGE NUT IS CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED NUT ON R/H WING INBOARD SPOILERON HINGE IAW CRJ200 AMM. TORQUE WRENCH STS-3819 CAL DUE DATE 05 APR 2020.
Part: NUT — CORRODED (RT SPOILERON) · airframe 33,016 hrs · 30,993 cycles
RT. O/B GRD. SPOILER O/B HINGE NUT IS CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED CORRODED HARDWARE ON RH OB GROUND SPOILER OB HIMGE IAW CRJ/200 AMM TQ WR STS-3744 SN:0610033638 CAL DUE: 14 JAN 21
Part: NUT — CORRODED (RT SPOILERON) · airframe 33,016 hrs · 30,993 cycles
RIGHT WING INBD CENTER SPOILERON HINGE NUTS WERE CORRODED. REPLACED SPOILERON HINGE NUTS IAW AMM.
Part: NUT — CORRODED (RT SPOILER) · airframe 33,016 hrs · 30,993 cycles
RT. O/B GRD. SPOILER I/B HINGE NUT IS CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED O/B GRD SPOILER I/B HINGE NUT IAW CRJ 200 AMM.
Part: FITTING — CORRODED (CARGO DOOR) · airframe 33,016 hrs · 30,993 cycles
LOWER FITTING ON CARGO DOOR WORN OVER LIMITS WITH CORROSION AT LOWER SEAL SURFACE. (C-CHECK) RO 4/22/2020 CORROSION REMOVED USING HAND METHODS, NO MATERIAL REMOVED FROM LOWER SEAL SURFACCE CARGO DOOR. REMOVED AND REPLACED LOWER FITTING FWD IAW CRJ200 SRM
Part: FASTENER — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
LEFT WING #5 O/B FLAP HINGE BOX AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #5 O/B FLAP HINGE BOX AFT ATTACHING HARDWARE IAW CRJ200 AMM TOOL = STS-2250 S/N = AB77460 CAL DUE = 25NOV20
Part: SPRING — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
LEFT WING #3 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #3 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING IAW CRJ 200 AMM.
Part: FASTENER — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
LEFT WING #4 O/B FLAP HINGE BOX AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #4 OUTBOARD FLAP HINGE BOX AFT ATTACHING HARDWARE IAW CRJ200 AMM TOOL = STS-2250 S/N = AB77460 CAL DUE = 25NOV20
Part: BOLT — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
LEFT WING #3 FLAP HINGE BOX AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #3 FLAP HINGE BOX AFT ATTACHING HARDWARE IAW CRJ200 AMM TASK TOOL = STS-2250 S/N = AB77460 CAL DUE = 25NOV20
Part: SPRING — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
LEFT WING #4 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRING CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED LEFT WING #4 O/B FLAP HINGE BOX BUTE DOOR COMPRESSION SPRIING IAW CRJ200 CMM.
Part: FASTENER — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
RIGHT WING #5 FLAP HINGE ARM ASSEMBLY AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACEDR/H WING #5 FLAP HINGE ARM ASSEMBLY AFT ATTACHING HARDWARE IAW CRJ200 AMM TW:ID STS 2250 / CAL DUE:25 NOV 2020
Part: FASTENER — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
RIGHT WING #4 FLAP HINGE ARM ASSEMBLY FWD ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED R/H WING #4 FLAP HINGE ARM ASSEMBLY FWD ATTACHING HARDWARE IAW CRJ 200 AMM. TW; STS 2250 CAL DUE;25 NOV 20
Part: FASTENER — CORRODED (TE FLAP) · airframe 33,016 hrs · 30,993 cycles
RIGHT WING #4 FLAP HINGE ARM ASSEMBLY AFT ATTACHING HARDWARE CORRODED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED R/H #4 HINGE ARM ASSEMBLY AFT ATTACHING HARDWARE IAW CRJ200 AMM.
Part: FITTING — CRACKED (FUSELAGE) · airframe 33,016 hrs · 30,993 cycles
INTERCOASTAL CLIP BETWEEN FS 621 AND FS 625 LEFT SIDE, MID FUSELAGE ON AFT SIDE OF BULKHEAD IS CRACKED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED INTERCOSTAL CLIP BETWEEN FS61 AND FS625 LEFT SIDE, MID FUSELAGE ON AFT SIDE OF BULKHEAD IAW SRM.
Part: FITTING — CRACKED (FUSELAGE) · airframe 33,016 hrs · 30,993 cycles
INTERCOASTAL CLIP BETWEEN FS 621 AND FS 625 RIGHT SIDE, MID FUSELAGE ON AFT SIDE OF BULKHEAD IS CRACKED. (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED INTERCOSTAL CLIP BETWEEN FS621 AND FS625 RIGHT SIDE MID FUSELAGE ON AFT SIDE OF BULKHEAD IAW CRJ200 SRM
Part: BEARING — DEFECTIVE (LT AILERON) · airframe 33,016 hrs · 30,993 cycles
ROUTE LH AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBD, MID, OUTBD) ON LH AILERON PER AMM (C-CHECK) RO 4/22/2020 REMOVED AND REPLACED BEARINGS AND BUSHINGS AT HINGE POINTS (IB, MID, OB) ON L/H AILERON IAW BOMBARDIER CMM ASSY SECTION REV 5 DTD 10 JULY 2019. INSPECTED FOR FAA AIRWORTHINESS DIRECTIVES ON 23 JAN 2020 AND 29 JAN 2020. FOUND NO APPLICABLE AD'S FOR THIS ARTICLE.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 33,016 hrs · 30,993 cycles
COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) . AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7884, POSITION: (C-CHECK) RO 4/22/2020 COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND; MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. / COMPLIED WITH SERIAL NUMBER 7884.
Part: BUSHING — CORRODED (LT AILERON) · airframe 33,016 hrs · 30,993 cycles
REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM (C-CHECK) RO 4/22/2020 REPLACED LH AILERON BUSHINGS AND HARDWARE IAW CRJ200 AMM.
Earlier reports · 2005–2018 · 46 reports
2018
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,349 hrs · 26,842 cycles
LEFT WING, INBD FLAP VANE CHAFED ON THE LEADING EDGE. REMOVED AND REPLACED THE FLAP VANE IAW SRM. OPS CHECKED GOOD.
2016
Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 26,069 hrs · 23,328 cycles
GEAR DISAGREE MESSAGE AFTER RETRACTION, NLG. ADJUSTED LT NLG DOOR PROXIMITY SWITCH. OPS CHECK GOOD.
Part: PANEL — DENTED (BS 640) · airframe 25,554 hrs · 22,792 cycles
OUT OF LIMITS ADM DENT APPROXIMATELY 14" DIRECTLY BELOW THE HIGH PRESSURE AIR PANEL AT BS 640 BETWEEN STR 20L - STR 22L. REPAIRED DENT APPROXIMATELY 14" BELOW THE HIGH PRESSURE AIR PANEL AT FS640 BETWEEN STR 20L-STR 22L IAW STS EA.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 25,554 hrs · 22,792 cycles
RIGHT INBD FLAP VANE CAP CHAFED AT OTBD L/E. R & R IAW SRM.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 25,554 hrs · 22,792 cycles
RIGHT INBD FLAP VANE CAP CHAFED AT CENTER L/E. R & R RT INBD FLAP VANE CENTER L/E IAW SRM.
2014
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,982 hrs · 19,754 cycles
AFT CABIN EMERGENCY LIGHTS INOPERATIVE. R & R NR 3 & 4 EMERGENCY LIGHT BATTERIES IAW AMM 33-51-04. OPS CHECKED GOOD. OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,924 hrs · 20,145 cycles
EMERGENCY LIGHTS, WHITE INTERIOR BY SERVICE DOOR SEVERAL INOPERATIVE. R & R THE SERVICE DOOR EMER SIGN LIGHT BULB IAW AMM 33-51-13. OPERATIONS CHECKED GOOD.
Part: LIFE VEST — OPEN (CABIN) · airframe 22,374 hrs · 19,607 cycles
FLIGHT ATTENDANT'S LIFE VEST FOUND OPEN. R & R LIFE VEST IAW AMM 25-61-03.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,367 hrs · 19,599 cycles
ACCESS PANEL 132AL ATTACH HOLE FREEZE PLUG DAMAGED ON SKIN. REPAIRED IAW REO 601R-53-11-162.
2013
Part: CONTAINER — TORN (LIFE VEST) · airframe 22,232 hrs · 19,472 cycles
CAPTAIN`S LIFE VEST HAS HOLE IN THE BAG. R & R LIFEVEST IAW AMM 25-61-03.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 21,974 hrs · 19,219 cycles
FLOOR EMERGENCY LIGHT INOPERATIVE AT ROW 7. FOUND LIGHT UNPLUGGED AT ROW 7. CONNECTED, OPS CHECKED GOOD IAW AMM 33-51-01.
Part: ELEMENT — MALFUNCTIONED · airframe 21,573 hrs · 18,849 cycles
AT 25000 FT, CLIMBING OUT, RECEIVED A ANTI-ICE DUCT WARNING MESSAGE. RAN QRH AND CLOSED BOTH 14TH STAGE SWITCHES, WING ANTI ICE WAS OFF/NEG ICING CONDITIONS. A FEW MINS RECEIVED A RT 14TH DUCT WARNING MESSAGE. R & R SENSING ELEMENT A38WK IAW AMM 36-21-04 PERFORMED OPC OF WING ANTI ICE IAW AMM 30-11-00-790-802. ALL OPS NORMAL, OK FOR SVC.
Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 21,573 hrs · 18,849 cycles
DURING CRUISE AT FL200, RECIEVED A LEFT ENGINE N2 OVERSPEED INDICATION. N1, ITT, FF, OIL TEMP, OIL PRESSURE ALL REMAINED NORMAL. THRUST REDUCED TO 80 PERCENT AND N2 INDICATION RETURNED TO NORMAL. CONTINUED FLIGHT WITH PERFORMED OPS CHECK AND INSPECTED BLUE HARNESS ON LT ENGINE IAW MM 72-00-00. PERFORMED HIGH POWER RUNS IAW GEMM 72-00-00. ALL OPERATIONS NORMAL.
Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 21,571 hrs · 18,846 cycles
AT 600 FT AGL ANTI-ICE DUCT MASTER WARNING. PERFORMED QRH MESSAGE WENT AWAY. AT ABOUT 2000 FT AGL MESSAGE RETURNED. PERFORMED QRH AND THE MASTER WARNING FOR RT 14TH DUCT DISPLAYED WITH 14TH STAGE BLEEDS CLOSED. QRH R 14TH DUCT PERFORMED. LANDED A REPLACED RT MODULATING/SHUTOFF VALVE IAW AMM 30-12-04. PERFORMED OPS CHECK OF VALVE IAW AMM 30-12-00. ALL CHECKS GOOD. PERFORMED OPS CHECK OF THE BLEED-AIR LEAK DETECTION/ WARNING SYSTEM IAW AMM 36-21-00. PERFORMED HIGH POWER RUN-UP IAW AMM 71-00-00. NO DEFECTS NOTED.
Part: FLAP — FAILED (WING) · airframe 19,384 hrs · 16,689 cycles
FLAPS FAIL WHEN THEY REACHED 30 DEG ON APPROACH LEVEL AT 4000 FT., 175KTS, 21C - 70MIN IN TO FLIGHT.
Part: FLAP — FAILED (WING) · airframe 21,174 hrs · 18,448 cycles
FLAPS FAIL WHEN THEY REACHED 30 DEG ON APPROACH LEVEL AT 4000FT. 175KTS -21C-70 MIN IN TO FLIGHT ACFT LANDED SAFELY , UNKNOWN IF EMERGENCY WAS DECLARED. COMPLIED WITH MEL 27-50-00, NO RECENT HISTORY OF ISSUES WITH THE FLAPS.
Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 20,812 hrs · 18,092 cycles
FLIGHT ATTENDANT FLASHLIGHT WON'T WORK. REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY PACK IAW AMM 25-61-00-701.
2012
Part: ACTUATOR — FAILED (TE FLAP) · airframe 20,384 hrs · 17,672 cycles
FLAPS FAILED ON APPROACH WHEN FLAPS WERE SELECTED FROM 20 TO 30. FLAPS DID NOT MOVE FROM 20 ALL 4 LT FLAP ACTUATORS REMOVED AND REPLACED FOR LOW TEMP TORQUE CHECK OR REPLACEMENT.
Part: BPSU — FAILED (TE FLAP) · airframe 14,113 hrs · 17,535 cycles
DURING APPROACH SET-UP ON FLIGHT 3684 FROM DTW TO DAY FLAPS FAILED AT 15°. COMPLETED QRH. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED IN DAY SAFELY. FLAPS FAIL CAUTION MSG, INFLIGHT, FLAP EXTENSION FLAPS 15, 180 KTS, 33MIN, 0 DEGREES (REQUIRED ITEMS CFM 6-23). REMOVED AND REPLACED LEFT BPSU IAW CRJ200 AMM 27-51-10. FLAP SYSTEM OP CHECK GOOD IAW CRJ200 AMM 27-50-00. PERFORMED TROUBLESHOOTING PER BOMBARDIER FM REV 43 IAW AD2009-06-12 PARAGRAPH (H)(6)(1).
Part: FLEX DRIVE — MALFUNCTIONED (TE FLAP) · airframe 20,365 hrs · 17,653 cycles
ON FLIGHT 4205 RST TO MSP DEVELOPED A FLAPS FAIL AT 33 DEGREE ON APPROACH. AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. MAINTENANCE RAN RESET PROCEDURES TO CLEAR THE FLAP FAIL AND APPLIED MEL 27-50-00, PLACARD INSTALLED. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM AND REMOVED AND REPLACED FLEX SHAFTS. THIS CLEARS DM 75951. PLACARD REMOVED.
Part: FLEX DRIVE — FAULTY (TE FLAP) · airframe 20,365 hrs · 17,653 cycles
ON FLIGHT 4141 FROM MSP TO CID RECEIVED FLAP FAIL AT 14 DEGREES DURING EXTENSION ON APPROACH INTO CID. FLAP SYSTEM WAS ON MEL 27-50-00 DUE TO PREVIOUS FAILURE EARLY IN THE DAY. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 4 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I) AMOC DATED APRIL 19 2012 AND PA AD27-052H. COMPLIED WITH STEPS 1-22,8-20 NA PER CHECKLIST OF CRJ200 FLAP HEALTH CHECKLIST. COMPLIED WITH STEPS 8-12 & 55-83 IAW CHECKLIST PROVIDED & AMM 27-50-00. REMOVED AND REPLACED NR 2 FLEX SHAFT ON LT SIDE IAW AMM27-53-10. REMOVED AND REPLACED NR 1, 3 AND 5 FLEX SHAFTS ON RT SIDE IAW AMM 27-53-10.
Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 20,351 hrs · 17,637 cycles
CREW REPORTED ON APPROACH IN YOW (ON FLIGHT 4089) THEY SELECETED FLAPS FROM 0 - 20 GEDRESS AND RECEIVED HALF SPEED. CREW THEN SELECTED FLAPS FROM 20-30 DEGREES AND RECEIVED A FLAPS FAIL MESSAGE WITH FLAPS STOPPING AT 20 DEGRESS. THE CREW RAN THE QRH AND LANDED THE AIRCRAFT. PERFORMED RESET PROCEDURES AND MEL'D 27-50-00. PERFORMED RESET PROCEDURES AND MEL'D 27-50-00. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 43 IAW AD 2009-06-12 PARAGRAPH H6I, AMOC DATED APRIL 19 2012 AND PA AD 27-052H. REPLACED LT NR 1 ACT, NR 5 FLEX SHAFT, RT NR 1 & 3 ACT.
Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 20,171 hrs · 17,456 cycles
OBSERVER'S LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVER'S LIFE VEST IAW AMM 25-61-03.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 20,171 hrs · 17,456 cycles
FLIGHT ATTENDANT'S LIFE VEST BAG TORN. REMOVED AND REPLACED LIFE VEST IAW AMM 25-61-03.
Part: CONTROL PANEL — FAILED (AILERON TRIM) · airframe 19,492 hrs · 16,784 cycles
AILERON TRIM SYSTEM IS INTERMITTENT WHEN COMMANDING RIGHT WING DOWN. REMOVED AND REPLACED AILERON TRIM PANEL IAW AMM 27-12-10. OPS CHECKED GOOD.
Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 19,373 hrs · 16,663 cycles
CAPTAIN'S LIFE VEST BAG DAMAGED. REMOVED AND REPLACED CAPTAIN'S LIFE VEST IAW AMM 25-61-03.
Part: UNKNOWN — MALFUNCTIONED (THRUST REVERSER) · airframe 19,294 hrs · 16,581 cycles
LEFT THRUST REVERSER DOES NOT DEPLOY. PERFORMED OPS CHECK ON LEFT THRUST REVERSER IAW AMM 78-30-00. OPC GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,202 hrs · 16,490 cycles
CEILING EMERGENCY LIGHT BURNED OUT. RELAMPED CEILING EMERGENCY LIGHT IAW AMM 33-20-00. OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,163 hrs · 16,454 cycles
LEFT NR 1 EXT EMER LIGHT INOP. REMOVED AND REPLACED BULB IAW AMM 33-51-21. OPS CHECK GOOD.
Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE DUCT) · airframe 19,075 hrs · 16,365 cycles
ANTI-ICE DUCT MASTER WARNING ON CLIMBOUT. COULD NOT DUPLICATE MESSAGE. REMOVED AND REPLACED LAVATORY LOOP IAW AMM 32-21-04 AS PROBABLE CAUSE, OPS CHECKED GOOD. OK FOR SERVICE.
Part: ECU — FAULTY (TE FLAP) · airframe 18,930 hrs · 16,231 cycles
FLAPS FAIL AT 30 ON APPROACH. EMERGENCY DECLARED. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV.39 IAW AD 2009-06-12 PARAGRAPH(H)(6)(I), AMOC DATED MARCH 27,2009, TR#27-012 PER AMOC DATED DECEMBER 18,2009 AND PA AD 27-052G. R/R FECU AND SKEW DETECTION UNIT. REMOVED AND REPLACED FECU IAW AMM 27-51-05. OPS CHECKS GOOD.
Part: ACTUATOR — FAILED (TE FLAP) · airframe 18,917 hrs · 16,219 cycles
FLAPS FAIL AT 17 WITH HANDLE AT 20. FLAPS EXTENDED AT 8000FT AND 190KTS. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED MARCH 27, 2009, TR # 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. REF CONTINUATION CARD N38877 FOR RT O/B, O/B FLAP ACTUATOR REMOVED AND REPLACED.
Part: FLEX DRIVE — BENT (TE FLAP) · airframe 18,898 hrs · 16,200 cycles
FLAPS FAIL AT 16 DEG ON APPROACH FLAPS FAIL MESSAGE IN FLIGHT EXTENSION AIRSPEED 190 KTS TRIM 1:40. C/W FLAP FAIL FIM 27-50-00. FOUND LT NR 2 & 3 RT NR 1, 2, & 4 FLEX SHAFTS BENT. REMOVED AND REPLACED IAW AMM 27-53-10. REFER TO NRC 22170 FOR FURTHER INFO. OPERATIONAL CHECK GOOD. OK FOR SVC.
Part: IDG — LACK OF LUBE (NR 1) · airframe 18,803 hrs · 16,112 cycles
ABORTED TAKEOFF AT ABOUT 70 KNOTS. ALL THE SCREENS IN THE FRONT FLASHED, WE LOST BOTH UTILITY BUSSES. THEN HAD THE YELLOW GEN 1 MESSAGE POP UP. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND IDG NR 1 LOW OIL. SERVICED NR 1 TDG, REF 12-13-24, OPERATION IS NORMAL WITH NO DEFECTS. NO LANDING INSPECTIONS REQUIRED FOR ABORTED TAKEOFF.
2011
Part: STRUCTURE — PUNCTURED (FUSELAGE) · airframe 18,067 hrs · 15,418 cycles
DAMAGE FOUND BETWEEN FS 589 AND FS 605 BETWEEN S-23L AND S-24L. THE PUNCTURED 6" X 5". REPAIRED IAW SRM 53-00-31 REPAIR 2.
Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,932 hrs · 15,281 cycles
THE 621.00 PRESSURE BULKHEAD HAS CHAFE MARKS ON PREVIOUSLY BLENDED REPAIRS FROM LINER SCREWS AT LBL 8.5, 9, 18, 27, 35 AND RBL 18, 27, 36 APPROX 30 INCHES ABOVE FLOOR .002 INCH DEEP. ALSO 1 EACH CHAFE AT RBL 9 APPROX 13 INCHES ABOVE FLOOR .002 INCH DEEP (TOTAL OF 9 CHAFES). REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,932 hrs · 15,281 cycles
THE 621.00 PRESSURE BULKHEAD HAS CHAFE MARKS ON PREVIOUSLY BLENDED REPAIRS FROM LINER SCREWS AT LBL 8.5, 9, 18, 27, 35 AND RBL 18, 27, 36 APPROX 30 INCHES ABOVE FLOOR .002" DEEP. ALSO 1 EACH CHAFE AT RBL 9 APPROX 13 INCHES ABOVE FLOOR .002 INCH DEEP (TOTAL OF 9 CHAFES). REPAIRED IAW REO 601R-53-61-2155.
Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 17,453 hrs · 14,777 cycles
RIGHT ENG ITT SPIKE PERFORMED ENGINE RUNS AT ALL POWER SETTINGS. NO DEFECTS NOTED IAW AMM 76-10-0.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 17,343 hrs · 14,714 cycles
LEFT WING LOWER WING PLANK ACCESS HOLE AT 510AB HAS CORROSION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
2009
Part: APU — LACK OF LUBE (APU BAY) · airframe 13,704 hrs · 11,267 cycles
ON APU START UP AT KDTW, THE GROUND CREW INFORMED THE CAPTAIN OF SMOKE COMING FROM THE REAR OF THE AIRCRAFT. THE FLIGHT CREW SHUT DOWN THE APU AND DEPLANED THE PASSENGERS. CFR WAS CALLED AND VERIFIED THERE WAS NO FIRE. MAINTENANCE INSPECTED THE AFT EQUIPMENT BAY AND DETERMINED THE SMOKE WAS CAUSED BY THE APU. THE APU WAS INSPECTED AND FOUND TO BE LOW ON OIL. THE APU WAS SERVICED AND RUN UP TO CHECK FOR OIL LEAK OR CONSUMPTION. NO LEAKAGE OR UNUSUAL OIL CONSUMPTION WAS DETECTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
2008
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)
ON APPROACH INTO ERI FLAPS WERE SELECTED TO 30 DEGREES AND FAILED AT TWENTY DEGREES, QRH FOLLOWED. EMERGENCY DECLARED WITH UNEVENTFUL LANDING. RESET FLAP SYSTEM IAW AD 2006-12-21 AND PLACED ON 72 HOUR WATCH. (S)
2006
Part: UNKNOWN — SMOKE (CABIN) · airframe 7,463 hrs · 6,038 cycles
ON TAXI, SMOKE/FUMES IN CABIN, RETURNED TO BLOCKS. PERFORMED ENGINE IGNITION AND RUNS. INSPECTED AIRCRAFT FOR LEAKS, NONE FOUND ALL OPERATIONS CHECK NORMAL, POSSIBLE DE-ICE FLUID INGESTION.
Part: FLAP — MALFUNCTIONED (WING) · airframe 7,111 hrs · 5,751 cycles
FLAP FAIL CAUTION ON TAXI. SYSTEM REST AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.
2005
Part: DETECTION SYS — MALFUNCTIONED (TE FLAPS) · airframe 4,933 hrs · 4,010 cycles
FLAPS FAIL WHEN FLAPS 45 DEGREES WAS SELECTED. PEFORMED QRH. LANDING UNEVENTFUL. REMOVED AND REPLACED SKEW DETECTION UNIT IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL. OPERATIONALLY CHECKS GOOD. OKAY FOR SERVICE.
Part: DETECTOR — MALFUNCTIONED (T/E FLAP) · airframe 4,928 hrs · 4,007 cycles
FLAP FAIL AT 42 DEGREES. LANDING UNEVENTFUL.REMOVED AND REPLACED FLAP SKEW DETECTION UNIT IAW AIRCRAFT MM. OPERATIONALLY CHECK GOOD.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,934 hrs · 4,012 cycles
FLAPS FAIL ON APPROACH WHEN SELECTED DOWN. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01