N936SW
Registered owner: SKYWEST AIRLINES INC, UT (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.
159 reports on file, 2003-09-19 – 2020-08-13.
Part: WINDSHIELD — CRACKED (LEFT) · airframe 41,116 hrs · 36,829 cycles
FOUND LH WNDSHLD CRACKED AT CENTER TOP PORTION OF OUTER GLASS PLY. REMOVED AND REPLACED THE PILOTS WINDSHIELD.
Part: SKIN — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON BOTTOM RIVET LINE OF BELLY UNDER PANEL 195BB WHICH WAS REMOBE TO FACILITATE STRUCTURES REPAIR OF FRAME AT FS 574 STRG L25 TO STRG 26 (C-CHECK) RO 3/25/2020 REWORKED AREA I.A.W. REO.MAX. BLEND-OUT FOUND AT FS 559+96 STR 27 WITH A REMAINING THICKNESS OF .053. NO DEFECTS NOTED. REAPPLIED FINISHES. CAL. EQUIP.:OLYMPUS 650 EPOC CAL. DATE: JULY2020, AV8961, OLYMPUS 600 NORTEC CAL. DATE: JULY2020, AV4594B. REAPPLIED FINISHES I.A.W. SRM.
Part: NUT PLATE — BROKEN (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
BROKEN NUT PLATE ON FLOOR SUPPORT BEAM AT FS 559 LBL 10 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED DOME NUT ON FLOOR SUPPORT BEAM AT F.S. 559 LBL 10 IAW SRM.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
INTERCOSTAL AT LBL 42 WL 78.0 AND FS 295.0 TO FS 310.0 IS HEAVILY CORRODED (C-CHECK) RO 3/25/2020 REMOVED CORROSION FROM INTERCOSTAL, FOUND TO BE OUT OF LIMITS. REMOVED OLD INTERCOSTAL, DRILLED, LOCATED , AND INSTALLED NEW INTERCOSTAL PER CRJ 200 SRM. DAIL DEPTH GAUGE AV2417 DUE: 01-21
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CRACKED REAR PRESSURE BULKHEAD LINER SUPPORT BRACKET AT LBL 36 APPROX WL 112 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED LINER SUPPORT BRACKET ON REAR PRESSURE BULKHEAD AT LBL 36 APRROX WL 112 PER CRJ200 SRM.
Part: BULKHEAD — DENTED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
DENT IN FORWARD FACE OF FS 621 BULKHEAD WEB APPROX LBL 14 WL 91 (C-CHECK) RO 3/25/2020 REPAIRED DENT IN FORWARD FACE OF F.S. 621 BULKHEAD WEB APPROX LBL14 WL 91 IAW BOMBARDIER REO. ACCOMPLISHED HFEC OF AFT PRESSURE BULKHEAD (DENTED AREA) LBL14 WL 91 NO DEFECTS NOTED IAW CRJ200 NTM.
Part: NUT PLATE — BROKEN (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
15 BROKEN SHUR-LOK RUBBER ISOLATOR NUT PLATES ON THE FS 621 BULKHEAD (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED 15 BROKEN SHUR-LOK RUBBER ISOLATOR NUTPLATES ON THE F.S. 621 BULKHEAD PER CRJ200 SRM.
Part: FRAME — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON FRAME AT FS 605 STRG 20L TO STRG 19R FWD AND AFT (C-CHECK) RO 3/25/2020 BLENDED CORROSION ON FRAME AT FS 605 STR 20L TO 19R. FRAME 605 STR 21L TO 21R ORIGINAL THICKNESS IS .050, REMAINING IS .040 WITH TOTAL LOSS OF .010. FRAME IS OUT OF LIMITS PER SRM. REMOVED AND REPLACED FRAME. FRAME SECTION AT STR 20R TO 19R IS WITHIN LIMITS AT .047 WITH TOTAL LOSS AT .003. SEE W/C 1068 FOR CORROSION REPAIR OF FRAME SECTION AT STR 18L TO 20L. RESTORED ALL PROTECTIVE FINISHES. (OLYMPUS 650 EPOC: AV8959 DD: JULY 2020, OLYMPUS 600 NORTEC: AV8958 DD: JULY 2020) (REF: CRJ-200 NTM, NTM CRJ-200 SRM PERFORMED PRESSURIZATION CHECK PER AMM. CHECKS GOOD. CALIBRATED TOOLS: OLYMPUS 650 EPOC AV8959 CAL DUE 7/2020, OLYMPUS 600 NORTEC AV 8958 CAL DUE 7/2020
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON SEAT RAILS ON FLOOR AT FS 569 LBL 9 (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON FLOOR SEAT RAIL IN BETWEEN FS. 559.00 TO FS.559.00+16 LBL9. ORIGINAL FS.569 LBL9 FOUMD TO BE INCORRECT. ORIGINAL THICKNESS .110, REMOVED 0.030 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK LBL9 STATIONS FS. 559.00+4 TO FS.559.00+126. IAW CRJ 200 AMM BOMBARDIER DRAWING CALIBRATED TOOLING: DEPTH GUAGE AV2417 JAN. 2021/ TORQUE WRENCH AV3967 JULY 2020
Part: FRAME — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON SRAME 589 AT FS 589 STGR R21-STRG L19 FWD AND AFT (C-CHECK) RO 3/25/2020 BLENDED CORROSION ON FRAME 589 STR 21R TO 19L. ORIGINAL THICKNESS IS .050, REMAINING IS .032 WITH TOTAL LOSS OF .018. REWORK WAS OUT OF LIMITS PER SRM. REMOVED AND REPLACED FRAME 589 SECTION AT STR 18L TO STR 21L AND STR 21L TO STR 21R. RESTORED ALL PROTECTIVE FINISHES.
Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON FLOOR SUPPORT BRACKET AT FS 280 LBL3 AND RBL3 (C-CHECK) RO 3/25/2020 REPLACED FLOOR SUPPORT BRACKET AT FS 280 IAW CRJ200 REO. CRJ200 REO
Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CRACK FOUND ON 280 SUPPORT CLIP AT FS 280 RBL 10 WL 72 (C-CHECK) RO 3/25/2020 REPLACED 280 SUPPORT CLIP IAW CRJ200 REO. CRJ200 REO.
Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CRACKS FOUND ON 280 SUPPORT CLIP FS 280 LBL 11 WL 72 (C-CHECK) RO 3/25/2020 REPLACED 280 SUPPORT CLIP IAW CRJ200 REO. CRJ200 REO.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON FLOOR SEAT RAIL AT FS 386 RBL 9 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED CABIN SEAT TRACK RBL9 STATIONS FS. 364.00 TO FS. 399.00. / IAW CRJ 200 AMM/ SRM/ BOMBARDIER DRAWING. CALIBRATED TOOLING: TORQUE WRENCH AV7624 NOV. 2020/ DEPTH GUAGE AV2417 JAN 2021
Part: CLEAT — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON PASSENGER DOOR EXTREME FLOOR CLEATS ( 2 ) (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED CORRODED PASSENGER DOOR ENTRANCE FLOOR CLEATS IAW CRJ 200 SRM.
Part: FASTENER — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
DURING INSPECTION CORROSION WAS FOUND ON FLOOR SILL PANEL FASTENERS AT FS 280 - 283 LBL 43 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED 3 FASTENERS AT FS 280 - 283 LBL 43. RESTORED SURFACE FINISH.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON FLOOR SEAT TRACK FS 409 + 10 - 409 + 42 RBL 9 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED SEAT TRACK AT RBL9 STATIONS FS. 399.00 TP FS. 409.00+128. IAW CRJ 200 AMM. BOMBARDIER DRAWING. CALIBRATED TOOLING: TORQUE WRENCH AV3967 JULY 2020/ DEPTH GUAGE AV2417 JAN. 2020
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON FASTENER SERVICE DOOR AFT FLOOR SUPPORT AT FS 349 RBL 42 (C-CHECK) RO 3/25/2020 REMOVED FASTENER FROM FLOOR SUPPORT, AFT OF SERVICE DOOR AT FS 349 RBL 42. BLENDED CORROSION ON FLOOR SUPPORT. NOMINAL 0.063, REMOVED 0.012, REMAINING 0.051. FOUND TO OUT OF LIMITS. REPAIRED IAW REO. SEE SHEET 2 OF REO FOR ADDITIONAL REQUIREMENTS. IAW BOMBARDIER CRJ 200 REO.
Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON PASSENGER AFT DOOR FRAME AT FS 349 LBL 40 (C-CHECK) RO 3/25/2020 REMOVED (1) FASTENER TO ACCESS CORROSION AT FS 349 LBL 40. BLENDED OUT CORROSION I.A.W. REO.NDT PERFORMED FOUND NO DEFECTS. ORIGINAL THICKNESS: .160", MATERIAL REMOVED: .039", REMAINING THICKNESS:.121". MEASURING EQUIP: EPOC650, CAL DUE: JULY2020, AV8959, PER NDTM NO DEFECTS NOTED
Part: FASTENER — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
CORROSION FOUND ON FLOOR SUPPORT FASTENER AT FS 349 LBL 39 (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED FASTENERS AT F.S. 349 LBL 39 PER CRJ200 SRM.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
SERVICE DOOR CUTOUT-AREAS OF LIGHT CORROSION ON FLOOR SUPPORT ANGLE BETWEEN FS 319.70 AND FS 349.00 RBL 43 (C-CHECK) RO 3/25/2020 REMOVED DOOR STOP FITTINGS FROM FLOOR SUPPORT ANGLE, BETWEEN FS 319.70 AND FS349. RBL 43. CORROSION BLEND IS OUTSIDE OF ALLOWABLE LIMITS. NOMINAL 0.063, REMOVED 0.019, REMAINING 0.044. REMOVED FASTENERS AND DAMAGED PART. TREATED PRIMED AND PAINTED AS NEEDED. INSTALLED NEW PART AND NEW FASTENERS, FAY, SEALED, REINSTALLED SERVICE DOOR STOP FITTINGS. DEPTH MIC TOOL ID # AV 2417 CALIBRATION DUE.JAN. 2021, SCALE, TOOL ID # AV 4102 CALIBRATION DUE JUNE 2020. TORQUE WRENCH, TOOL ID # AV 6528, CALIBRATION DUE. NOV. 2020 BOMBARDIER CRJ 200 SRM
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
REMOVABLE FLOOR BEAM THAT GOES OVER MAIN FEED MANIFOLD HAS EVIDENCE OF CORROSION (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON FLOOR BEAM CAP STRIP FS 589 LBL9 TO RBL9, FOUND TO BE OUT OF LIMITS PER SRM. REMOVED CAP STRIP PER SRM. FABRICATED REPLACEMENT CAP STRIP PN 601R35031-159 IAW DRAWING. INSTALLED REPLACEMENT CAP STRIP IAW SRM.
Part: FASTENER — CORRODED (FUSELAGE) · airframe 40,899 hrs · 36,569 cycles
PAX DOOR CUTOUT-AREAS OF LIGHT CORROSION ALONG FLOOR SUPPORT ANGLE BETWEEN FS 310.00 AND FS 349.00 LBL 43 (C-CHECK) RO 3/25/2020 CLEANED AND REMOVED SURFACE CONTAMINATIONS. DAMAGE WAS FOUND TO BE CONTAINED WITHIN FASTENERS WITH NO MATERIAL LOSS TO SURROUNDING SUBSTRATE IN PAX DOOR CUTOUT BETWEEN FS 310.00 AND FS 349.00 LBL43. REMOVED AND REPLACED DAMAGED FASTENERS IAW SKYWEST CRJ200 SRM. RESTORED AIRCRAFT FINISHES IAWSKYWEST CRJ200 SRM.
Part: VANE — CHAFED (TE FLAP) · airframe 40,899 hrs · 36,569 cycles
LH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 95.0 (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ON L/H, I/B FLAP VANE L/E AT W/S 95.0 PER CRJ-200 SRM. ORIGINAL MATERIAL THICKNESS IS 050". REMAINING THICKNESS IS .025". MATERIAL LOSS IS .025". AREA FOUND TO BE OUT OF LIMITS PER BA REO. REMOVED AND REPLACED L/E SKIN PER CRJ-200 SRM. TOOLING USED: DEPTH DIAL GAGE: AV 5185, CAL DUE DATE: 11/21/20. TOOLING USED: DEPTH DIAL GAGE: AV 5185, CAL. DUE DATE:11-21-20.
Part: VANE — CHAFED (TE FLAP) · airframe 40,899 hrs · 36,569 cycles
LH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 55.0 (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ONE L/H, I/B FLAP VANE L/E AT APPROX W/S 55.0. PER CRJ-200 SRM 51-12-00. ORIGINAL MATERIAL THICKNESS IS .050". REMAINING THICKNESS IS .023". MATERIAL LOSS IS .037". AREA FOUND TO BE OUT OF LIMITS PER BA REO. REMOVED AND REPLACED L/E SKIN PER CRJ-200 SRM. TOOLING USED: DEPTH DIAL GAGE AV 5185, CAL DUE DATE:11/21-20.
Part: VANE — CHAFED (TE FLAP) · airframe 40,899 hrs · 36,569 cycles
RH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 141.0 (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ON R/H, I/B FLAP VAN L/E AT APPROX W/S 141.0 PER CRJ-200 SRM-200 51-12-00. ORIGINAL MATERIAL THICKNESS IS .050". REMAINING MATERIAL THICKNESS IS .024". MATERIAL LOSS IS .026". AREA FOUND TO BE OUT OF LIMITS PER BA REO. REMOVED AND REPLACED L/E SKIN PER CRJ-200 SRM.TOOLING USED: DEPTH DIAL GAGE AV 2417, CAL DUE DATE: 01/10/21.
Part: VANE — CHAFED (TE FLAP) · airframe 40,899 hrs · 36,569 cycles
RH INBD FLAP VANE IS CHAFFED ON L/E AT APPROX WS 95. (C-CHECK) RO 3/25/2020 REMOVED CHAFFE DAMAGE ON R/H, I/B FLAP VANE L/E AT APPROX W/S 95.0 PER CRJ-200 SRM. ORIGINAL MATERIAL THICKNESS IS .050". REMAINING THICKNESS IS .025". MATERIAL LOSS IS .025". AREA FOUND TO BE OUT OF LIMITS PER BA REO. REMOVED AND REPLACE L/E SKIN PER CRJ-200 SRM. TOOLING USED: DEPTH DIAL GAGE AV 5185, CAL DUE DATE: 11/21/20.
Earlier reports · 2003–2019 · 132 reports
2019
Part: RESERVOIR — DEFECTIVE (LANDING GEAR) · airframe 39,630 hrs · 35,117 cycles
GEAR DISAGREE WARNING. LEFT MAIN LANDING GEAR SLOW. COMPLIED WITH QRH GEAR DISAGREE. (FLT#3587) CLOSED REMOVED AND REPLACED RESERVOIR. PERFORMED FULL GEAR SWINGS, IAW AMM. NO DEFECTS NOTED.
Part: ACTUATOR — SLOW (LT MLG) · airframe 39,059 hrs · 34,468 cycles
GEAR DISAGREE MESSAGE ON GEAR RETRACTION. LEFT MAIN SLOW TO RETRACT. MESSAGE WAS ILLUMINATED ONLY FOR A FEW SECONDS. (FLT 7359) CLOSED REMOVED AND REPLACED LEFT MLG SIDESTAY ACTUATOR IAW AMM. SYSTEM OPS CHECKS GOOD NO FURTHER FAULTS NOTED.
2018
Part: NONE — NONE (NONE) · airframe 38,692 hrs · 34,070 cycles
OUTBOUND PILOT REPORTS A DENT IN THE RT. WING LEADING EDGE DUE TO A BIRD STRIKE. FLIGHT # 7389 FO: 10/29/2018. CLOSED REMOVED AND REPLACED RT O/B LEADING EDGE SKIN IAW SRM.
2014
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,196 hrs · 25,414 cycles
LEFT CENTER OVER WING EXTERIOR EMERGENCY LIGHT IS BURNED OUT, REPLACED THE LAMP.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,755 hrs · 25,098 cycles
NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT, REPLACED LAMP.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,703 hrs · 25,058 cycles
LEFT INBD FLAP VANE CHAFED. BLENDED FLAP VANE IAW REO.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,703 hrs · 25,058 cycles
RIGHT INBD FLAP VANE L/E CHAFED. BLENDED FLAP VANE IAW REO.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,703 hrs · 25,058 cycles
LEFT INBD FLAP VANE CHAFED. BLENDED FLAP VANE IAW REO.
Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 29,703 hrs · 25,058 cycles
ANGLE ON OTBD END OF INTERCOSTAL CRACKED BS 621. REPLACED INTERCOSTAL ANGLE IAW SRM.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,703 hrs · 25,058 cycles
LEFT INBD FLAP VANE CHAFED AT FLAP. BLENDED FLAP VANE IAW REO.
Part: INTERCOSTAL — CRACKED (BS 621) · airframe 29,703 hrs · 25,058 cycles
CRACK IN INTERCOSTAL AFT OTBD CORNER AT LT AFT SIDE OF BS 621, REPLACED INTERCOSTAL IAW SRM.
Part: HINGE — GOUGED (PAX DOOR) · airframe 29,703 hrs · 25,058 cycles
PAX DOOR HINGE GOUGED. BLENDED HINGE IAW REO.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 29,703 hrs · 25,058 cycles
CORROSION ON RT FLOOR SUPPORT. BLENDED CORROSION IAW SRM AND REO.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,692 hrs · 25,049 cycles
3RD OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT 5540 RELAMPED.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,246 hrs · 23,937 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#5228 RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,064 hrs · 23,788 cycles
OVERHEAD EMERGENCY LIGHT ROW 5 IS BURNED OUT. FLT#6204 RELAMPED.
Part: TIRE — FAILED (NLG) · airframe 27,751 hrs · 23,549 cycles
RT NOSE TIRE BLOWN AT 140 KTS. REPLACED LEFT AND RIGHT NOSE TIRE ASSEMBLY IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,576 hrs · 23,380 cycles
FORWARD SECTION OF EMERGENCY LIGHTS DO NOT ILLUMINATE. RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,889 hrs · 22,832 cycles
NR 1 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5337) RELAMPED EMERGENCY LIGHT.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,487 hrs · 22,525 cycles
NR 1 EMERGENCY OVERHEAD LIGHT BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: UPLOCK — FAILED (LT MLG) · airframe 26,211 hrs · 22,311 cycles
GEAR DISAGREE UPON GEAR RETRACTION. (FLT 5633) REPLACED LEFT MLG UPLOCK ASSEMBLY IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,130 hrs · 22,240 cycles
AFT EMERGENCY FLOOD LIGHT BURNED OUT. (FLT 6473) RELAMPED EMERGENCY LIGHT.
Part: BYPASS VALVE — FAILED (MLG) · airframe 26,020 hrs · 22,160 cycles
SELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE MESSAGE. MAIN GEAR SHOWING UP AND NOSE GEAR DOWN. (FLT 6362) REPLACED THE MLG RUNAROUND BYPASS VALVE, MLG SELECTOR VALVE, RIGHT MLG UPLOCK ASSEMBLY IAW AMM. P/N: 750004000-003 S/N OFF: 1110A, P/N OFF: 750005000 S/N OFF: 0180, P/N: 17051-101 S/N OFF: CWDD2150-02.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,703 hrs · 21,901 cycles
LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5354) RELAMPED EMERGENCY LIGHT.
Part: CHARGER — FAILED (CABIN) · airframe 25,405 hrs · 21,657 cycles
CABIN FLOOR EMERGENCY LIGHTS ARE OUT. (FLT 5412) REPLACED NR 2 BATTERY CHARGER ASSEMBLY AND REPLACED NR 2 EMERGENCY LIGHT INVERTER.
Part: CONNECTOR — LOOSE (CABIN) · airframe 25,098 hrs · 21,425 cycles
FIRST 4 ROWS OF FLOOR LEVEL EMERGENCY LIGHTING IS OUT. (FLT 5352) RECONNECTED LOOSE CONNECTION AT ROW 7.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,078 hrs · 21,409 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6443) RELAMPED EMERGENCY LIGHT.
Part: WIRE — LOOSE (CABIN) · airframe 24,969 hrs · 21,323 cycles
LOWER GREEN LEFT EMERGENCY EXIT LIGHT IS OUT. (FLT 5395) CONNECTED A LOOSE WIRE ON FLOOR LIGHT TRACK.
Part: CABLE — DISCONNECTED (CABIN) · airframe 24,862 hrs · 21,232 cycles
EMERGENCY EXIT SIGN LIGHT IS OUT AT OVERWING EXIT A/B SIDE. (FLT 5592) RECONNECTED FLOOR LIGHT CABLE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,808 hrs · 21,189 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6304) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,758 hrs · 21,144 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5521) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,710 hrs · 21,110 cycles
NR 3 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,503 hrs · 20,928 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5410) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,503 hrs · 20,928 cycles
AFT LEFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5321) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,405 hrs · 20,826 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5247) RELAMPED EMERGENCY LIGHT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,354 hrs · 20,774 cycles
TWO OVERHEAD EMERGENCY POD LIGHTS ARE OUT. (FLT 5513) REPLACED NR 4 BATTERY CHARGER AND EMERGENCY LIGHT BATTERY PACK. P/N: AD 2013-1A, S/N OFF: 77256.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,279 hrs · 20,713 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5332) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,256 hrs · 20,698 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5561) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 24,203 hrs · 20,650 cycles
FLT 5472, RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,190 hrs · 20,635 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6205) RELAMPED EMERGENCY LIGHT.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,865 hrs · 20,374 cycles
AFT CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,791 hrs · 20,322 cycles
FORWARD RIGHT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5650) RELAMPED EMERGENCY LIGHT.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 23,640 hrs · 20,192 cycles
ALL NR 1 EMERGENCY BATTERY PACK POWERED EMERGENCY LIGHTS ARE INOPERATIVE. (SERVICE) REPLACED NR 1 EMERGENCY BATTERY CHARGER.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,570 hrs · 20,134 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5636) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,533 hrs · 20,102 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5518) RELAMPED EMERGENCY LIGHT.
Part: INDICATOR — FAILED (STANDBY ALTITUDE) · airframe 23,400 hrs · 19,969 cycles
STANDBY ALTITUDE INDICATOR READS 6000FT HIGH. (FLT 6303) REPLACED STAND BY ALTITUDE INDICATOR. P/N: WL102AMS5 S/N OFF: AK091
Part: ALTIMETER — FAILED (COCKPIT) · airframe 23,391 hrs · 19,964 cycles
STANDBY ALTIMETER READS 500FT OFF. (FLT 6303) REPLACED STANDBY ALTIMETER.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,400 hrs · 19,969 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6216) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,321 hrs · 19,905 cycles
NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6374) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,281 hrs · 19,865 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5334) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,238 hrs · 19,829 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6514) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,167 hrs · 19,753 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5348) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,108 hrs · 19,709 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6433) RELAMPED EMERGENCY LIGHT.
Part: BALLAST — FAILED (CABIN) · airframe 23,108 hrs · 19,709 cycles
EMERGENCY LIGHT BY RIGHT EMERGENCY EXIT IS OUT. (FLT 6244) REPLACED NR 3 EMERGENCY LIGHT BALLAST.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,108 hrs · 19,709 cycles
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5293) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,054 hrs · 19,670 cycles
NR4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5841) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,023 hrs · 19,644 cycles
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5482) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,980 hrs · 19,619 cycles
NR 1 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5466) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,963 hrs · 19,605 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5622) RELAMPED EMERGENCY LIGHT.
Part: CONNECTOR — DIRTY (CABIN) · airframe 22,963 hrs · 19,605 cycles
LEFT FLOOR EMERGENCY LIGHT BY THE OVERWING EMERGENCY EXIT IS OUT. (FLT 5342) CLEANED CONNECTOR ON FLOOR MOUNTED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,885 hrs · 19,539 cycles
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5297) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,868 hrs · 19,524 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5496) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,814 hrs · 19,484 cycles
FORWARD 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6361) RELAMPED EMERGENCY LIGHTS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,764 hrs · 19,450 cycles
AFT CEILING EMERGENCY LIGHT OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: CONNECTOR — DIRTY (CABIN) · airframe 22,684 hrs · 19,388 cycles
RIGHT SIDE FLOOR AND LOWER EXIT EMERGENCY LIGHTS ARE OUT. (FLT 5623) CLEANED CONNECTIONS ON FLOOR LEVEL LIGHTING.
Part: ROLLER — DIRTY (CABIN DOOR) · airframe 22,569 hrs · 19,305 cycles
MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6399) REMOVED DEBRIS FROM UPPER AFT SPIGOT ROLLER.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,178 hrs · 19,000 cycles
OVERHEAD EMERGENCY LIGHT BY ROW 13 IS OUT. (FLT 6555) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,059 hrs · 18,909 cycles
NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 6243) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,970 hrs · 18,825 cycles
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6812) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,855 hrs · 18,732 cycles
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7024) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,581 hrs · 18,528 cycles
NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 6274) RELAMPED EMERGENCY LIGHT.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,174 hrs · 18,187 cycles
FS 202 BULKHEAD HAS MULTIPLE CRACKS AT PARKING BRAKE CABLE HOLE. (C-CHECK) REPAIR PER REO.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,045 hrs · 18,073 cycles
AFT CABIN CEILING EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,985 hrs · 18,027 cycles
NR 1 EMERGENCY CEILING LIGHT INOPERATIVE. (FLT 6734) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,889 hrs · 17,939 cycles
SECOND TO LAST OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6933) RELAMPED EMERGENCY LIGHT.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,438 hrs · 17,579 cycles
THE 3RD EMERGENCY LIGHT CEILING LEVEL FLOODLIGHT INOPERATIVE. (FLT 4687) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,356 hrs · 17,509 cycles
MIDDLE EXTERNAL EMERGENCY LIGHT ON THE RIGHT SIDE OF THE AIRCRAFT BY THE OVERWING EMERGENCY EXIT IS INOPERATIVE. (FLT 6429) RELAMPED EMERGENCY LIGHT.
Part: DOOR — DIRTY (CABIN) · airframe 19,951 hrs · 17,185 cycles
MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6937) CLEANED & LUBRICATED MAIN CABIN DOOR.
Part: UNKNOWN — MALFUNCTIONED (CABIN DOOR) · airframe 19,630 hrs · 16,913 cycles
MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6452)UNABLE TO DUPLICATE, OPERATIONAL CHECK NORMAL.
Part: FASTENER — SHEARED (NR 2 PCU) · airframe 19,630 hrs · 16,913 cycles
ELEVATOR JAMS DURING FLIGHT CONTROL CHECKS ON HYDRAULIC SYSTEM NR 2. (FLT 6293) REPLACED SHEARED FASTENER ON NR 2 PCU.
Part: GENERATOR — MALFUNCTIONED (APU) · airframe 18,881 hrs · 16,253 cycles
APU GENERATOR INOPERATIVE, LEADS T2 AND T3 BURNED. (FLT 5859) REPLACED APU GENERATOR.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,516 hrs · 15,921 cycles
FLT 6037 - AFT CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,462 hrs · 15,873 cycles
NR 1 CABIN OVERHEAD EMERGENCY LIGHT INOP. (FLT 6604) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,238 hrs · 15,704 cycles
NR 4 OVERHEAD EMERGENCY LIGHT INOP. (FLT 5931)RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,066 hrs · 15,570 cycles
NR 2 EMERGENCY CEILING LIGHT INOP. (FLT 6518) RELAMPED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,851 hrs · 15,393 cycles
FORWARD AND AFT CABIN CEILING EMERGENCY LIGHTS INOP. (FLT 6024) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,745 hrs · 15,309 cycles
CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 5934) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,136 hrs · 14,845 cycles
AFT EMERGENCY LIGHT IN AISLE INOP. (FLT 6744) RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,994 hrs · 14,726 cycles
NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6614) RELAMPED EMERGENCY LIGHT.
Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 16,849 hrs · 14,620 cycles
NOSE GEAR DISAGREE MESSAGE DISPLAYED. (FLT 5790) RE-ADJUSTED PROXIMITY SENSOR AND BRACKET.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 17,149 hrs · 14,856 cycles
FS 280 STRINGER BRACKET CRACKED. (C CHECK) REPAIRED PER SRM.
Part: FITTING — CRACKED (FUSELAGE) · airframe 17,149 hrs · 14,856 cycles
FS 280 CLIP CRACKED. (C CHECK) REPAIRED PER REO.
Part: FITTING — CRACKED (FUSELAGE) · airframe 17,177 hrs · 14,880 cycles
LINTEL FITTING CRACKED. (C CHECK) REPAIRED PER REO.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,321 hrs · 14,199 cycles
FLT 6657 - 2 OF 5 LIGHT BULBS BURNED OUT IN EMERGENCY "EXIT" LIGHT ON GALLEY DOOR. RELAMPED.
Part: BEARING — CORRODED (ENGINE MOUNT) · airframe 16,703 hrs · 14,506 cycles
LEFT ENGINE THRUST FITTING BEARING CORRODED ON INNER SURFACE. SB COMPLIANCE, REPLACED FITTING.
Part: BEARING — CORRODED (ENGINE MOUNT) · airframe 16,703 hrs · 14,506 cycles
RIGHT ENGINE THRUST FITTING BEARING CORRODED ON INNER SURFACE. SB COMPLIANCE, REPLACED FITTING.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,248 hrs · 14,142 cycles
FLT 6695 - AFT CEILING EMERGENCY LIGHT INOP. RELAMPED.
Part: SERVO — OUT OF ADJUST (ELEVATOR TRIM) · airframe 16,162 hrs · 14,080 cycles
FLT 5912 - HEAVY CONTROL FORCES ON ELEVATOR ON LANDING FLARE AND ON TAXI IN. ADJUSTED ELEVATOR SLIP CLUTCH AND REPLACED ELEVATOR SERVO.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,908 hrs · 13,882 cycles
FLT 5901 - SECOND TO LAST EMERGENCY LIGHT INOP. RELAMPED.
2008
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,772 hrs · 13,773 cycles
FLT 6018 - EMERGENCY LIGHT OVER ROW 10 INOP. RELAMPED.
Part: SELECTOR VALVE — FAILED (NLG) · airframe 15,310 hrs · 13,414 cycles
FLT 5969 - GEAR DISAGREE WARNING ON SHORT FINAL AFTER GO AROUND, NOSE GEAR FELL DOWN AND LOCKED AFTER ABOUT FOUR MINUTES. REPLACED NOSE GEAR SELECTOR VALVE, PN 750006000 SN ON 0242T SN OFF 2093.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,172 hrs · 13,300 cycles
FLT 6663 - FORWARD AND AFT CEILING EMERGENCY FLOOD LIGHTS INOP. RELAMPED.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,948 hrs · 13,126 cycles
LT WING FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED, CHECKS GOOD.
Part: LIGHT — UNSECURE (CAIBN) · airframe 13,838 hrs · 12,138 cycles
FLT 6672 - AFT CEILING LEVEL EMERGENCY FLOOD LIGHT IS NOT SECURE. RESECURED AFT CEILING EMERGENCY FLOOD LIGHT COVER.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,675 hrs · 11,982 cycles
AFT CEILING EMERGENCY POD LIGHT IS INOP. RELAMPED THE EMERGENCY POD LIGHT. OPS CHECK GOOD.
Part: RIB — DAMAGED (LT WING) · airframe 13,062 hrs · 11,468 cycles
LEFT WINGLET DAMAGED WHILE ON THE RAMP. INSTALLED NEW RIB AND PANEL PER SRM 57-31-31 AND CRJ DRAWING 600-15108.
2007
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,062 hrs · 11,468 cycles
FS 280 RBL9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT FS 280 RBL 9 LOWER FLOOR SUPPORT IAW CRJ200 REO 601R-53-11-171.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 13,062 hrs · 11,468 cycles
FS 484 AT RBL 27 IS CRACKED AT TOP OF ANGLE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R 53-41-059 REV A.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 13,062 hrs · 11,468 cycles
UPPER FLOOR SUPPORT FRAME IS CRACKED AT RBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT RBL9 PER CRJ200 SRM 51-42-06 P 11.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,062 hrs · 11,468 cycles
LOWER FLOOR SUPPORT IS CRACKED AT STA 280 LBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AT LBL9 LOWER FRAME PER CRJ200 SRM 51-42-06.
Part: RADAR — FAILED (WEATHER RADAR) · airframe 11,067 hrs · 9,830 cycles
RADAR FAILED AFTER TAKEOFF. RETURNED TO DEN. REMOVED AND REPLACED WEATHER RADAR. REF CRJ 200 MM CHPT 34-41-01 & 34-41-00.
2006
Part: WINDOW — CRACKED (COCKPIT) · airframe 9,487 hrs · 8,475 cycles
IN CRUISE AT FL350, LEFT SIDE WINDOW CRACKED BUT DID NOT SHATTER. REPLACED LEFT SIDE WINDOW IAW CRJ 200 AMM 56-12-01 AND SKYWEST RII 56-220-1000, SN/OFF 02156H7506. FUNCTIONAL CHECKS GOOD.
Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 9,151 hrs · 8,172 cycles
2ND EMERGENCY FLOOD LIGHT FROM FRONT IS OUT. RELAMPED SECOND EMERGENCY FLOOD LIGHT IAW AMM 33-51-01. OPERATIONAL CHECKS GOOD.
Part: RIB — CRACKED (RT WING) · airframe 8,200 hrs · 7,321 cycles
RIGHT BATTERY ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT WS 53.60 RIGHT IAW REO 601R-57-51-046.
Part: FLOOR SUPPORT — CRACKED (BS 640 S9-12L) · airframe 8,200 hrs · 7,321 cycles
FS 640 LT SIDE REINFORCEMENT ANGLE CRACKED BETWEEN STR 9L AND 12L. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REINFORCEMENT ANGLE AT FS 640 LT PER CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21.
Part: RIB — CRACKED (LT WING) · airframe 8,200 hrs · 7,321 cycles
LEFT BATTERY ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT LT WS 53.60 IAW REO 601R-57-51-046.
Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 8,200 hrs · 7,321 cycles
ENGINE SUPPORT BEAM CRACKED AT FS 627 WL 111.09 LBL 37.5 COMING FROM FWD INBOARD CORNER OF ACCESS PANEL. ITEM FOUND AT C-CHECK INSPECTION. ENGINE SUPPORT BEAM AT FS 627 WL 111.09 LBL 37.5 REPAIR COMPLETE IAW REO 601R-53-61-258.
Part: TRIM PANEL — MALFUNCTIONED (AILERONS) · airframe 7,689 hrs · 6,839 cycles
AILERON TRIM WOULD NOT MOVE AFTER LANDING IN DEN. REPLACED AILERON AND RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD.
2005
Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 6,589 hrs · 5,884 cycles
LEFT INBOARD FLAP DAMAGE ON UNDERSIDE OF FLAP AFTER NR 1 MAIN BLEW OUT ON LANDING. REPLACED LEFT INBOARD FLAP IAW MM 27-54-01. OPERATIONAL CHECK GOOD.
Part: TRIM SWITCH — MALFUNCTIONED (ELEVATOR) · airframe 6,209 hrs · 5,575 cycles
CAPT ELEVATOR TRIM INOP. REPLACED ELEVATOR TRIM SWITCH IAW 27-41-05. OPERATIONAL CHECK GOOD.
Part: SWITCH — STUCK (TRIM) · airframe 5,381 hrs · 4,890 cycles
F/O TRIM SWITCH STICKS. REPLACED F/O PITCH TRIM SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD.
Part: WINDOW — CRACKED (COCKPIT) · airframe 5,323 hrs · 4,846 cycles
F/O'S SIDE WINDOW CRACKED TOP TO BOTTOM. REMOVED AND REPLACED F/O'S SIDE WINDOW IAW CRJ 200 MM ATA CHPT 56-12-01. P/N OFF 601R33033-12, S/N OFF 05T4TH9290.
Part: ENGINE — LEAKING (NR 1) · airframe 5,266 hrs · 4,798 cycles
NR 1 ENGINE HAS OIL LEAKING, FOUND A SUMP DRAIN LEAKING BEYOND LIMITS. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY IAW 71-00-00, OPERATIONAL CHECK GOOD.
Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 4,938 hrs · 4,504 cycles
STALL FAIL CAUTION ILLUMINATED ON TAKEOFF. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ 200 MM ATA CHPT 27-35-01. OPERATIONAL CHECK GOOD.
Part: TRIM PANEL — MALFUNCTIONED (COCKPIT) · airframe 4,823 hrs · 4,417 cycles
RUDDER TRIM WILL NOT MOVE NOSE LEFT. REPLACED RUDDER TRIM PANEL. OPERATIONAL CHECK GOOD.
2004
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,143 hrs · 3,802 cycles
FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21, 51-23-00, 51-21-11.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,143 hrs · 3,802 cycles
FS 621 FLOOR SUPPORT ANGLE RIGHT HAND SIDE CRACKED. ITEM FOUND AT C-CHECK. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV-B.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,143 hrs · 3,802 cycles
FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD ATTACH ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,143 hrs · 3,802 cycles
FS 621 FLOOR SUPPORT ANGLE LEFT HAND SIDE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV-B.
Part: CONTROL PANEL — MALFUNCTIONED (AILERONS) · airframe 3,539 hrs · 3,285 cycles
AILERON TRIM SWITCH STICKS, WILL NOT ALLOW RIGHT TRIM INPUT. REMOVED AND REPLACED TRIM PANEL IAW CRJ AMM 27-12-00. OP CHECKS GOOD. P/N: 601R51226-23SW.
2003
Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 1,953 hrs · 1,885 cycles
STALL FAIL CAUTION MESSAGE ILLUMINATED INFLIGHT. REPLACED STALL PROTECTION COMPUTER. OPS CHECK GOOD.
Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 1,687 hrs · 1,624 cycles
STALL TEST FAILED. INSTALLED SERVICEABLE STALL PROTECTION COMPUTER IAW MM 27-34-00. PN: 3995100208 SN OFF: 955