N426SW

Part: VALVE — FAILED (NLG STEERING) · airframe 40,403 hrs · 34,966 cycles

NOSE WHEELS STEERING INOP IN FLIGHT. DECLARED AN EMERGENCY. RETURNED TO FIELD. (FLT 7395) FO: 10/08/2018 CLOSED REMOVED AND REPLACED EHSV IAW AMM. LEAK CHECK AND OPS CHECK GOOD AT THIS TIME. CHECKED THE RIGGING OF STEERING AND FOUND IT GOOD. CYCLED STEERING MULTIPLE TIMES DURING BLEEDING PROCEDURE WITHOUT INOP MESSAGES APPEARING. RETRACTED AND EXTENDED NOSE LANDING GEAR MULTIPLE TIMES AND INOP MESSAGES DID NOT APPEAR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,236 hrs · 34,773 cycles

FRAME FS364 CORRODED BETWEEN STR26R TO OTBD OF STR26L. (C-CHECK) RO: 09/01/2018. REMOVED AND REPLACED FS364 FRAME FROM STR26R TO STR26L IAW SRM. PRESSURE CHECK GOOD.

Part: PANEL — CORRODED (FUSELAGE) · airframe 40,236 hrs · 34,773 cycles

LT PRESSURE FLOOR SILL PANEL FROM FS 409+128 TO FS 559+0 HAS NUMEROUS SPOTS OF CORROSION. (C-CHECK) RO: 09/01/2018. REPAIRED LT PRESSURE FLOOR SILL PANEL FROM FS 409+128 TO FS 559.0 IAW REO.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 40,236 hrs · 34,773 cycles

SERVICE DOOR SURROUND STRUCTURE, AFT LOWER FRAME SUPPORT FITTING CORRODED. (C-CHECK) RO: 09/01/2018. REMOVED AND REPLACED SERVICE DOOR SURROUND STRUCTURE AFT LOWER FRAME SUPPORT FITTING IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,236 hrs · 34,773 cycles

SERVICE DOOR SURROUND STRUCTURE, LOWER FORWARD AND AFT SILL ANGLE HAS CORROSION. (C-CHECK) RO: 09/01/2018. REMOVED AND INSTALLED NEW SERVICE DOOR SILL ANGLE BETWEEN FS319.7 AND FS349.00 IAW SRM.

Part: STRIKER — CORRODED (FUSELAGE) · airframe 40,236 hrs · 34,773 cycles

SERVICE DOOR SURROUND STRUCTURE, FORWARD LOWER SEAL STRIKER HAS CORROSION. (C-CHECK) RO: 09/01/2018. INSTALLED NEW FORWARD LOWER SEAL STRIKER IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,236 hrs · 34,773 cycles

PAX DOOR SILL ANGLE CORRODED INBD AND OTBD SIDE. (C-CHECK) RO: 09/01/2018. REMOVED AND INSTALLED NEW ANGLE IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,236 hrs · 34,773 cycles

FRAME CORRODED IN SEVERAL PLACES (ON AFT SIDES OF FRAME) AT FS333.00 & BTWN STR26L - STR26R. (C-CHECK) RO: 09/01/2018. REMOVED AND INSTALLED NEW FRAME AT FS 333.00 IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 40,236 hrs · 34,773 cycles

FRAME CORRODED IN SEVERAL PLACES (ON FWD & AFT SIDES OF FRAME) AT FS349.00 & BTWN STR24L - STR24R. (C-CHECK) RO: 09/01/2018. REMOVED AND INSTALLED NEW FRAME SECTION AT FS349.00 IAW SRM.

Part: STRUT — DISCHARGED (NLG) · airframe 39,657 hrs · 34,132 cycles

GEAR DISAGREE AND NOSE DOOR OPEN CAUTION MESSAGE. SERVICE THE NLG STRUT IAW AMM. SWUNG GEAR MULTIPLE TIMES IAW AMM. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG) · airframe 39,657 hrs · 34,132 cycles

NOSE GEAR DISAGREE WARNING ON RETRACTION. PERFORMED A NR 3 HYD DECAY RATE IAW AMM. PERFORMED FUNCTIONAL TEST OF LDG GEAR RETRACT AND EXTEND IAW AMM. OPS CHECKED GOOD.

Part: BRACKET — DAMAGED (NLG OLEO SENSOR) · airframe 39,398 hrs · 33,863 cycles

GEAR DISAGREE, DECLARED AN EMERGENCY AND RETURNED TO FIELD. REMOVED AND REPLACED THE NLG CENTER OLEO SENSOR BRACKET. ADJUSTED THE SENSOR IAW AMM. OPS CHECKED GOOD. PERFORMED A LANDING GEAR EXTENSION AND RETRACTION IAW AMM. OPS CHECKED GOOD.

Part: SENSOR — BENT (NLG) · airframe 39,347 hrs · 33,811 cycles

GEAR DISAGREE, RETURNED TO FIELD. ADJUSTED A BENT NLG OLEO SENSOR IAW AMM. OPS CHECKED GOOD.

Part: BRACKET — NOT REPORTED (NLG) · airframe 39,034 hrs · 33,453 cycles

GEAR DISAGREE WARNING MSG AFTER TAKEOFF. NOSE GEAR. RETURNED TO THE FIELD. CREW DECLARED AN EMERGENCY. (FLT 4617) REMOVED AND REPLACED NLG BRACKET OPS CHECK GOOD.

Part: YAW DAMPER — MALFUNCTIONED · airframe 37,512 hrs · 31,788 cycles

WITH YAW DAMPERS ENGAGE, THE ACFT YAWED LEFT HARD. YAW DAMPER DISENGAGED, ACFT CONTINUED TO WANDER. REMOVED AND REPLACED LT YAW DAMPER LINEAR ACTUATOR. OPS CHECKED GOOD.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 36,722 hrs · 30,952 cycles

LEFT INBOARD FLAP VANE L/E SKIN CHAFED AT CENTER SECTION. REPAIRED IAW SRM.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 36,722 hrs · 30,952 cycles

RIGHT INBOARD FLAP VANE L/E SKIN CHAFED AT CENTER OTBD SECTION. REPAIRED IAW SRM.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 36,722 hrs · 30,952 cycles

RIGHT INBOARD FLAP VANE L/E SKIN CHAFED AT OUTBD SECTION. REPAIRED IAW SRM.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 36,722 hrs · 30,952 cycles

LEFT INBOARD FLAP VANE L/E SKIN CHAFED AT INBD SECTION. REPAIRED IAW SRM.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 36,722 hrs · 30,952 cycles

LEFT INBOARD FLAP VANE L/E SKIN CHAFED AT OUTBD SECTION. REPAIRED IAW SRM.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 36,722 hrs · 30,952 cycles

RIGHT INBOARD FLAP VANE L/E SKIN IS CHAFED AT INBD SECTION. REPAIRED IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,722 hrs · 30,952 cycles

PASSENGER DOOR INTERCOSTAL HAS CORROSION JUST BELOW THE LATCH LOCK BOX ASSEMBLY. REMOVED AND INSTALLED THE INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,722 hrs · 30,952 cycles

PASSENGER DOOR INTERCOSTAL HAS CORROSION VISIBLE AT ACCESS PANEL 832ER. REPLACED THE INTERCOSTAL IAW SRM.

Part: COMPUTER — FAILED (AUTOPILOT SYS) · airframe 30,384 hrs · 24,613 cycles

AIRCRAFT BEGAN A SERIES OF UNCOMMANDED YAWS IN BOTH DIRECTIONS AND BECAME MORE NOTICEABLE UPON DESCENT TO LANDING EVEN WITH AUTOPILOT ENGAGED AND DISENGAGED. (FLT 7374) REPLACED FCC NR 2 IAW AMM. OPS CHECKED GOOD AT THIS TIME. P/N: 622-9815-904 S/N ON: 393 S/N OFF: 1113

Part: LENS — DAMAGED (CABIN) · airframe 30,292 hrs · 24,515 cycles

LEFT OVERWING EMERGENCY LIGHT LENS CAVED IN. (FLT 4820) REPLACED LENS ASSEMBLY IAW AMM. P/N: BM5-0018-905

Part: SELECTOR VALVE — FAILED (NLG) · airframe 30,046 hrs · 24,261 cycles

GEAR DISAGREE WARNING MESSAGE, NOSE GEAR DID NOT COME DOWN. AFTER ABOUT 10-15 SECONDS, NOSE GEAR CAME DOWN, MESSAGE WENT AWAY, AND GEAR INDICATED DOWN AND LOCKED. (FLT 4635) REPLACED MLG PRIORITY VALVE, NLG SELECTOR VALVE IAW AMM. PERFORMED MULTIPLE NLG EXTENSION/RETRACTIONS. OPS CHECKS GOOD. NO DEFECTS NOTED.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 29,574 hrs · 23,778 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) REPAIRED BAD CONNECTOR AT SERVICE DOOR EXIT SIGN AND REPLACED 3 BAD FUSES ON BATTERY PACKS 1, 3, AND 4 IN REFERENCE TO CRJ 200 AMM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 29,541 hrs · 23,751 cycles

FS 280 FLOORBEAM IS CRACKED AT LBL 11.0 NEAR LOWER FLANGE. (C-CHECK) REPAIRED FS 280 FLOORBEAM LOWER FLANGE AT LBL 11.0 PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,541 hrs · 23,751 cycles

FS 621 BULKHEAD WEB CRACKED AT LINTEL FITTING. (C-CHECK) REPAIRED FS 621 BULKEAD WEB CRACK AT LINTEL FITTING IN REFERENCE TO CRJ-200 REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,541 hrs · 23,751 cycles

FS 621 AFT PRESSURE BULKHEAD CRACKS AT (1 EACH) LBL 36.20, LBL 9.5, BL 0.01, AND RBL 18.0. RBL 27.50 WITH 13 CRACKS, AND LBL 18.0 WITH 2 CRACKS. (C-CHECK) REPAIRED PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,541 hrs · 23,751 cycles

VERTICAL POST AT FS 409.0 +128 RBL 18.0 IS CRACKED OUTBOARD SIDE. (C-CHECK) REPLACED VERTICAL POST AT FS 409.0 + 128 RBL INBOARD AND OUTBOARD IN REFERENCE TO CRJ-200 REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,541 hrs · 23,751 cycles

INBOARD AND OUTBOARD CLIP CRACKED AT LBL 9 FS 280.0. (C-CHECK) REPLACED INBOARD AND OUTBOARD CLIPS AT FS 280 LBL 9.0 PER CRJ 200 SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 29,541 hrs · 23,751 cycles

VERTICAL POST AT FS 409.0 +128 BL 0.0 RIGHT SIDE IS CRACKED. (C-CHECK) REPLACED VERTICAL POST AT FS 409+128 BL 0 LEFT AND RIGHT SIDE IN REFERENCE TO CRJ200 SRM.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 29,332 hrs · 23,559 cycles

THE LEFT ENGINE FORWARD YOKE MOUNT UPPER LINK HAS PITTING ON THE BUSHINGS. (C-CHECK) REPLACED LINK ASSEMBLY FOR THE LEFT ENGINE FORWARD YOKE MOUNT.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 29,332 hrs · 23,559 cycles

LEFT ENGINE FORWARD ENGINE MOUNT YOKE LOWER BUSHING PITTED. (C-CHECK) REPLACED LEFT ENGINE FORWARD ENGINE MOUNT YOKE ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,258 hrs · 23,494 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4838) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,882 hrs · 23,117 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7805) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,311 hrs · 22,544 cycles

RIGHT MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: FAIRING — DELAMINATED (FUSELAGE) · airframe 28,109 hrs · 22,344 cycles

LEFT MID SECTION WING TO FUSELAGE FAIRING HAS DELAMINATION ON LOWER AFT SECTION. (SERVICE) REPAIR DELAMINATION.

Part: FAIRING — DELAMINATED (FUSELAGE) · airframe 28,109 hrs · 22,344 cycles

CENTER AFT WING TO FUSELAGE FAIRING HAS DELAMINATION ON LEFT UPPER FORWARD SIDE. (SERVICE) REPAIRED DAMAGE DELAMINATION.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 27,901 hrs · 22,142 cycles

STANDBY ALTIMETER IS OFF BY 500 FEET. (FLT 4645) REPLACED STANDBY ALTITUDE INDICATOR.

Part: WIRE — BROKEN (CABIN) · airframe 27,756 hrs · 22,007 cycles

FLOOR LEVEL EMERGENCY LIGHTS WILL NOT ILLUMINATE IN THE FORWARD HALF OF THE CABIN. (FLT 3762) REPAIRED WIRE AT FORWARD FLOOR LEVEL EMERGENCY LIGHT STRIP.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 27,732 hrs · 21,985 cycles

FLOOR LEVEL EMERGENCY LIGHTS ARE OUT BETWEEN ROW 2-5. (FLT 4656) SECURED LOOSE CONNECTION AT FLOOR LEVEL EMERGENCY LIGHT STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,585 hrs · 21,841 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4451) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,378 hrs · 21,633 cycles

LEFT SIDE EXTERIOR CENTER OVERWING EMERGENCY EXIT LIGHT IS OUT. (FLT 4477) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,298 hrs · 21,557 cycles

LEFT OVERWING EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,128 hrs · 21,409 cycles

LEFT FORWARD EMERGENCY EXIT LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,113 hrs · 21,397 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,526 hrs · 20,872 cycles

FORWARD CEILING EMERGENCY LIGHT IS OUT. (FLT 4733) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,214 hrs · 20,591 cycles

CEILING EMERGENCY LIGHT AT ROW 2 IS OUT. (FLT 4768) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,044 hrs · 20,450 cycles

FS 559.0 BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (BS 621) · airframe 26,044 hrs · 20,450 cycles

FS 621.0 BULKHEAD WEB NEAR TOP OF CARGO DOOR TRACK IS CRACKED. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,384 hrs · 20,744 cycles

FS 559.0 PRESSURE BULKHEAD CRACKED AT RT SIDE. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,384 hrs · 20,744 cycles

FS 202 FORWARD BULKHEAD CRACKED AROUND PARKING BRAKE CABLE. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,987 hrs · 20,407 cycles

RIGHT FORWARD EXTERNAL EMERGENCY LIGHT IS OUT. (FLT 4774) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,950 hrs · 20,378 cycles

OVERHEAD EMERGENCY LIGHT ABOVE SERVICE DOOR INOPERATIVE. (FLT 4844) REPLACED EMERGENCY LIGHT ASSEMBLY ABOVE SERVICE DOOR EXIT.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 24,695 hrs · 19,268 cycles

EMERGENCY LIGHT AFT OF ROW 8 INOP. (FLT 4692) REPLACED LIGHT CABLE HARNESS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,405 hrs · 19,025 cycles

NR 4 OVERHEAD EMERGENCY LIGHT INOP. (FLT 4510) RELAMPED EMERGENCY LIGHT.

Part: PAINT — DEFECTIVE (TE FLAP) · airframe 24,065 hrs · 18,715 cycles

AT FLAPS 45° ON APPROACH AIRCRAFT ROLLS TO THE RIGHT. (FLT 4615) REMOVED ROUGH EDGES OF PAINT ON LEFT INBOARD FLAP TRAILING EDGE.

Part: WEB — CRACKED (RT WING) · airframe 23,515 hrs · 18,251 cycles

RIGHT WING OUTBOARD LEADING EDGE WEB CRACKED. (C CHECK) REPLACED WEB SRM.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 22,850 hrs · 17,701 cycles

APU WENT INOP WITH NR 1 IDG DEFERRED. (FLT 4554) REPLACED NR 1 IDG.

Part: LENS — MISSING (CABIN) · airframe 22,427 hrs · 17,378 cycles

EMERGENCY FLOOR LIGHT LENS MISSING. (FLT 4552) REPLACED LIGHT ASSEMBLY.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,609 hrs · 16,750 cycles

DURING C-CHECK, RIGHT FLOORBEAM FS 280 RBL11 CRACKED. REPAIRED PER REO.

Part: ATTACH FITTING — CORRODED (DOOR HANDRAIL) · airframe 21,609 hrs · 16,750 cycles

DURING C-CHECK, PASSENGER DOOR HANDRAIL CLIPS IN FLOOR CORRODED. REPLACED CLIPS PER SRM.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 21,609 hrs · 16,750 cycles

C-CHECK, ANCHOR FITTING FORWARD PASSENGER DOOR CRACKED. REPLACED PER AMM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 21,609 hrs · 16,750 cycles

C-CHECK, PICCOLO TUBE BRACKET CRACKED. REPLACED PER AMM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 20,433 hrs · 15,835 cycles

FLT 3835 - CAPTAINS SIDE WINDOW IS CRACKED. REPLACED CAPTAINS SIDE WINDOW IAW CRJ 200 MM 56-12-01, P/N OFF 601R33033-11, S/N OFF 00258H7823.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 19,146 hrs · 14,846 cycles

FLT 3811 - LEFT WINDSHIELD IS CRACKED. REPLACED LEFT WINDSHIELD IAW CRJ 200 MM 56-11-01, PN/OFF NP-139321-9, SN/OFF 02192H9830.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 18,592 hrs · 14,431 cycles

FLT 3987 - FOUND EXIT LIGHT ON LEFT SIDE OF SERVICE DOOR IS INOP. REPAIRED WIRE ON THE EXIT LIGHT IAW WM 20-00-00. OPS CHECK IS OK.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,868 hrs · 13,103 cycles

FS280 LT/RT CLIPS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)INSTALLED NEW BRACKET ANGLES AT FS280 LT/RT PER CRJ200 SRM 51-42-06 PG 11 (9) 51-42-21 PG 17.

Part: STEP — CRACKED (PAX DOOR) · airframe 16,868 hrs · 13,103 cycles

PAX DOOR STEPS HAVE CRACKS AT STEP 832DT AND 832CT AFT RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PER BOMBARDIER REO 601R-52-11-702 AND CRJ200 SRM 51-42-06.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 16,868 hrs · 13,103 cycles

BRACKET SUPPORT CLIP CRACKED RT RBL27 OTBD AND FS484 UNDER FLOORBD. (DISCOVERED DURING C-CHECK INSPECTION) INSTALLED NEW CLIP SUPPORT BRACKET AT RT RBL27 FS484 UNDER FLOORBOARD PER CRJ200 SRM51-42-06 PG 11 AND SRM 51-42-21 PG 17.

Part: WEB — CRACKED (PAX DOOR) · airframe 16,868 hrs · 13,103 cycles

PAX DOOR AFT WEB AT 2ND STAIR CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)INSTALLED REPAIR DOUBLER & SHIMS PER CRJ200 REO 601R-52-11-1188 REV A ON PAX DOOR AFT WEB STEP 2.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 16,868 hrs · 13,103 cycles

PAX DOOR PULL-IN MOTOR BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SIDE PNL STIFFENER PER CRJ200 51-42-06 PG 11.

Part: STEP — CRACKED (PAX DOOR) · airframe 16,868 hrs · 13,103 cycles

PAX DOOR STEP 832DT HAS CRACK ON FWD RADIUS, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLES AND DOUBLER PER REO 601R-52-11-702 REV A REPAIR ZONE 2 AND CRJ200 SRM 51-42-06,51-42-21 AND 51-23-00.

Part: ADC — MALFUNCTIONED (NR 1 & NR 2) · airframe 15,138 hrs · 11,842 cycles

WHILE IN CRUISE FLIGHT, RECEIVED IAS FLAGS ON BOTH THE CAPTAINS AND FO'S SIDE FOLLOWED BY MACH TRIM, EFIS COMP MON CAUTION MESSAGES FOLLOWED BY ADI TEMP DISAGREE MESSAGE. PURGED NR 1 AND NR 2 PITOT STATIC SYSTEM AND REPLACED NR 1 AND NR 2 ADC IAW MM 34-13-07 AND ST34-406. OPS CHECK, PN: 822-0372-445, SN ON: 18PRW SN OFF: 1725.

Part: TRIM SWITCH — STICKS (COCKPIT) · airframe 14,273 hrs · 11,196 cycles

FOS TRIM SWITCH IS STICKY. REPLACED FOS PITCH TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 14,165 hrs · 11,113 cycles

LT FLIGHT SPOILER CAUTION MESSAGE. REPLACED LEFT OB FLIGHT SPOILER PCU IAW CRJ 200 MM 27-62-01, OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 13,896 hrs · 10,909 cycles

EMERGENCY LIGHTS WILL NOT ILLUMINATE IN ROW 9 AND BEYOND. REPLACED NR 4 EMERGENCY BATTERY IAW MM 33-51-04. OPERATIONAL CHECK GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (SPOILERS) · airframe 13,198 hrs · 10,381 cycles

LEFT FLIGHT SPOILER CAUTION ON TOUCHDOWN AT SLC. REPLACED HYDRAULIC PRESSURE SWITCHES IAW MM 29-34-1. REPLACED LT IB PCU IAW MM 27-62-01. REPLACED NR 1 AND NR 2 SECU'S. OPERATIONAL CHECK GOOD IAW 27-61-05, PN 27000-7 SN/OFF 4704, PN 49-164-05, SN/OFF 00156, PN 49-164-05, SN/OFF 1137.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 13,163 hrs · 10,352 cycles

FLIGHT SPOILER FAULT STATUS MESSAGE DURING FLIGHT. REPLACED NR 2 SECU IAW MM 27-61-05, OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILERS) · airframe 12,510 hrs · 9,835 cycles

SPOILERON FAULT STATUS MESSAGE ON GROUND. REPLACED RT SPOILERON IB PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED · airframe 12,567 hrs · 9,882 cycles

FS 484 CABIN FLOOR RT INTERCOSTAL OB ANGLE RBL36 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A".

Part: INTERCOSTAL — CRACKED · airframe 12,567 hrs · 9,882 cycles

FS 484 CABIN FLOOR LT INTERCOSTAL INBOARD AND OUTBOARD ANGLES LBL 27 AND LBL 36 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV "A".

Part: ANGLE — CRACKED · airframe 12,567 hrs · 9,882 cycles

FS 625 AFT EQUIPMENT COMPARTMENT RT ANGLE ST 14R CRACKED, ITEM FOUND AT C-CHECK. REPAIRED ANGLE IAW CRJ REO 601R-53-100 "REV NC", REO 601R-53-61-422 REV "NC".

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,567 hrs · 9,882 cycles

FS 280 CABIN FLOOR TRANVERSE BEAM LOWER FLANGE CRACKED, ITEM FOUND AT C-CHECK. REPAIRED BEAM IAW CRJ REO 601R-53-11-171 REV "B".

Part: ANGLE — CRACKED · airframe 12,567 hrs · 9,882 cycles

FS 625 AFT EQUIPMENT COMPARTMENT LT ANGLE STR 14L CRACKED, ITEM FOUND AT C-CHECK. REPAIRED ANGLE IAW CRJ REO 601R-53-61-100 "REV NC", REO 601R-53-61-422 REV "NC".

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,567 hrs · 9,882 cycles

FS 280 FLOOR SUPPORT ANGLE LBL 13 CRACKED, ITEM FOUND AT C-CHECK. REPAIRED ANGLE IAW CRJ REO 601R-53-11-138 REV "NC".

Part: TRACK — CRACKED · airframe 12,567 hrs · 9,882 cycles

RT ENG INBOARD LOWER MAIN TRACK ASSEMBLY IS CRACKED, ITEM FOUND AT C-CHECK. MAIN TRACK ASSEMBLY REPLACED IAW CRJ AMM 78-34-11-400-801 & 78-34-11-000-801.

Part: BRACKET — CORRODED · airframe 12,567 hrs · 9,882 cycles

PAX DOOR CUT-OUT LOWER LONGERON BRACKETS AND CLEATS AT FS 316 AND 343 - CORRODED, ITEM FOUND AT C-CHECK. CORROSION REMOVED IAW CRJ SRM 51-21-06, 53-00-00. .002 MAT LOSS, .063 NOM .061 REMAINING WITHIN LIMITS IAW CRJ SRM 53-00-00.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,452 hrs · 9,789 cycles

EXIT LIGHT AT GALLEY SERVICE DOOR INOP. RELAMPED EXIT LIGHT AT GALLEY SERVICE DOOR. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 12,437 hrs · 9,775 cycles

EMERGENCY LIGHTS ON GALLEY SERVICE DOOR OUT. REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 12,437 hrs · 9,775 cycles

CEILING LEVEL EMERGENCY FLOOD LIGHTS INOP. REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 12,274 hrs · 9,639 cycles

EMERGENCY LIGHTS NOT WORKING. RECONNECTED AFT SECTION OF LIGHTING. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 10,756 hrs · 8,443 cycles

FO'S STAB TRIM SWITCH INOPERATIVE. REMOVED AND REPLACED FO'S STAB TRIM SWITCH IAW MM 27-41-05, OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 10,524 hrs · 8,268 cycles

LEFT SPOILERON INBOARD PCU POSITION FAIL. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW 27-62-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 10,121 hrs · 7,955 cycles

STAB CH 1 INOPERATIVE INFLIGHT. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR IAW AMM 27-42-01 AND MOTOR CONTROL UNIT IAW AMM 27-42-05. OPERATIONAL CHECK GOOD. HSTCU P/N 8396-3, S/N OFF 1159.

Part: VANE — OBSTRUCTED (AOA) · airframe 8,630 hrs · 6,792 cycles

LOUD BUZZING/WHISTLING SOUND FROM NOSE AND STALL FAIL MESSAGE. RETURNED TO BASE AND EMERGENCY EQUIPMENT RESPONDED. SUSPECT O2 SERVICE DOOR PARTIALLY OPEN CAUSING AIRFLOW INTERFERENCE OVER RIGHT AOA VANE. PROPERLY SECURED DOOR. PERFORMED STALL PROTECTION SYSTEM TEST PER MM 27-35-01. NO DEFECTS NOTED.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 8,637 hrs · 6,798 cycles

DISCOVERED DURING C-CHECK INSPECTION, PAX DOOR SUPPORT ANGLE CRACKED ADJACENT TO DOOR ASSIST CABLE BRACKET. REPAIRED DAMAGE IAW CRJ REO 601R-52-11-448 REV ''NC''.

Part: ATTACH ANGLE — CRACKED (DOOR FRAME) · airframe 8,637 hrs · 6,798 cycles

DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT TRANSVERSE BEAM ATTACH ANGLE FOR CARGO DOOR STOPS IS CRACKED AT FS 605.00 LBL 43.00. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21 AND MM 20-21-00 & RII 53-401.

Part: DOOR — CRACKED (WATER SERVICE) · airframe 8,637 hrs · 6,798 cycles

RIGHT EXTERIOR AFT FUSELAGE, AFT POTABLE WATER SERVICE DOOR, DOOR PANEL REBATE IS CRACKED IN AFT LOWER CORNER. DISCOVERED DURIING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ SRM 53-00-31 FIG 103 SHEETS 1 & 3.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,637 hrs · 6,798 cycles

DISCOVERED DURING C-CHECK INSPECTION, MAIN FUSELAGE RBL 9.0 HAS INBOARD AND OUTBOARD FLOORBEAM ANGLES CRACKED AT FS 280.00. ANGLES REPLACED AT FS 280.0, RBL 9.0 IAW CRJ SRM.

Part: FAIRING — CRACKED (RT PYLON) · airframe 8,637 hrs · 6,798 cycles

DISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON LOWER STANG FAIRING 444BB CRACKED ON INBOARD SIDE. REPAIRED DAMAGE IAW SHORTS CMM 78-30-00, SRS 049.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,637 hrs · 6,798 cycles

DISCOVERED DURING C-CHECK INSPECTION, MAIN FUSELAGE LBL 9.0 HAS INBOARD AND OUTBOARD FLOORBEAM ANGLES CRACKED AT FS 280.00. REPLACED IAW CRJ SRM.

Part: FRAME — CRACKED (ACCESS PANEL) · airframe 8,637 hrs · 6,798 cycles

DISCOVERED DURING C-CHECK INSPECTION, RIGHT PYLON UPPER ACCESS PANEL 422AB STIFFENER FRAME CRACKED. REPLACED STIFFENER IAW SHORTS CMM 20-40-11, 20-42-06, 20-27-11 & 20-27-11.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,637 hrs · 6,798 cycles

DISCOVERED DURING C-CHECK INSPECTION, CARGO PIT FLOORBEAM ANGLE CRACKED AT FS 621.00 RBL 42.0. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV ''A'' & RII 53-401.

Part: SENSOR — FAILED (STALL WARNING) · airframe 7,190 hrs · 5,694 cycles

AFTER T/O, GOT A STALL FAIL MSG. CAPT SLOW SPD CUE CLIMBED TO 200 KTS AND CONTINUED TO 280 KTS AS A/C ACCEL TO 290 KTS. THIS CONDITION CONTINUED UNTIL DESCENT. FOUND AOA FAILED IN MDC. REMOVED AND REPLACED LEFT AOA SENSOR IAW CL600 MM 27-35-05. OPS CHECKS GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILER) · airframe 6,922 hrs · 5,492 cycles

LT FLIGHT SPOILER INDICATES FAULT AFTER PERFORMING THE FIRST FLIGHT OF THE DAY TEST. REMOVED AND REPLACED LEFT INBOARD FLIGHT SPOILER PCU. OPS AND LEAK CHECKS GOOD IAW MM 27-62-01. S/N OFF: 3957

Part: CONTROL UNIT — MALFUNCTIONED (ANTI-SKID SYS) · airframe 6,850 hrs · 5,443 cycles

INFLIGHT (ANTISKID INBD ANTISKID OUTBOARD) YELLOW MESSAGES ILLUMINATED - QRH COMPLIED WITH - MESSAGES WOULD NOT EXTINGUISH. BOTH LEFT SIDE MAIN LANDING GEAR TIRES FAILED ON LANDING. FOUND LEFT AND RIGHT ANTISKID CB'S POPPED. RESET CB'S AS REQUIRED IAW MM 32-44-00. OUTBOARD CHECKS GOOD, IB CHECKS BAD. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IAW 32-44-06. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (LT SPOILERS) · airframe 6,552 hrs · 5,211 cycles

RECEIVED A SPOILERON FAULT MESSAGE IN FLIGHT. TESTED THE SYSTEM AND FOUND THE LEFT INBOARD SPOILER PCU TO BE NON-FUNCTIONAL. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU IAW 27-62-01. OPS CHECK GOOD, LEAK CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NR 1 YAW DAMPER) · airframe 6,440 hrs · 5,125 cycles

NR 1 YAW DAMPER WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW LINEAR ACTUATOR WITH A SERVICEABLE UNIT IAW MM 22-22-01. PERFORMED OPS CHECK IAW MM 22-22-01.

Part: VALVE — MALFUNCTIONED (SELECTOR) · airframe 6,100 hrs · 4,865 cycles

NOSE GEAR WILL NOT RETRACT INTO UP AND STOWED POSITION WHEN GEAR LEVER SELECTED UP. RETURNED TO COS. REMOVED AND REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW MM 32-33-10. SWUNG NOSE GEAR 15-20 TIMES. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME.

Part: WIRE — CHAFED (FLUTTER DAMPER) · airframe 5,593 hrs · 4,471 cycles

FLUTTER DAMPER STATUS MESSAGE IN FLIGHT, AMBER ARC ON L AILERON ON FLIGHT CONTROL SYNOPTIC PAGE. NO CHANGES TO CONTROLLABILITY ON CONTROL FEEL NOTED. FOUND CHAFED WIRE IN MIDDLE WING SECTION LEADING EDGE. REPAIRED WIRE IAW WMM 20-16-00. OPS CHECK GOOD.

Part: DAMPER — MALFUNCTIONED (LEFT) · airframe 5,578 hrs · 4,458 cycles

LT AILERON FLUTTER DAMPER STATUS MESSAGE AND ICON ON FLIGHT CONTROL PAGE BETWEEN 160-200 KIAS, INTERMITTANTLY. REMOVED AND REPLACED LT AILERON FLUTTER DAMPER IAW MM 27-15-05. OPS CHECKS GOOD ON GROUND. FAILED FLIGHT TEST.

Part: DAMPER — MALFUNCTIONED (LT AILERON) · airframe 5,435 hrs · 4,345 cycles

DURING FLIGHT, RECEIVED A -FLUTTER DAMPER- STATUS MESSAGE FOR THE LEFT AILERON. REMOVED AND REPLACED LEFT AILERON FLUTTER DAMPER IAW CRJ 27-15-05. OPS CHECKS GOOD.

Part: VALVE — MALFUNCTIONED (ANTI ICE SYSTEM) · airframe 5,234 hrs · 4,176 cycles

ON END OF RUNWAY, APPLIED 80 PERCENT N1 WITH A LT WING A/I CAUTION MSG THAT WOULD NOT EXTINGUISH. 10 SECONDS LATER RECEIVED A WING OVERHEAT MESSAGE FOR THE RT WING, ALSO POPPED B-4 CB ON CBP-4. REDUCED THRUST, EXITED RUNWAY, RAN QRH AND RETURNED TO GATE. REPLACED LT 14TH STAGE ANTI-ICE MODULATING VALVE PER MM 30-12-04. OPS CHECK GOOD.

Part: DAMPER — MALFUNCTIONED (LT AILERON) · airframe 5,234 hrs · 4,176 cycles

LT AILERON FLUTTER DAMPER MESSAGE INTERMITTENT. REPLACED LT AILERON FLUTTER DAMPER IAW 27-15-05. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (NR 2 GEN) · airframe 5,096 hrs · 4,068 cycles

AT START OF TAKEOFF WE RECIEVED IDG NR 2 AND GEN NR 2 CAUTION MESSAGES. CLEARED RUNWAY, RESET PER QRH AND CLEARED FAULTS. NR 2 GENERATOR CHECKS NORMAL ON GROUND RUN UP.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 4,675 hrs · 3,756 cycles

DURING TAKEOFF ROLL, CONFIG TRIM THEN CONFIG SPOILERS WARNING ILLUMINATED. ABORTED TAKEOFF. RESET SPOILER SYSTEM, VERIFIED AILERON TRIM AT NEUTRAL.

Part: BATTERY PACK — DISCHARGED (EMERG LIGHTS) · airframe 4,200 hrs · 3,383 cycles

AFT SECTION OF FLOOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 23-51-04.

Part: CASE — CRACKED (APU) · airframe 4,059 hrs · 3,274 cycles

APU AUTO SHUTDOWN ON GROUND. OIL OBSERVED UNDER THE TAIL. REPLACED APU WITH SERVICEABLE UNIT DUE TO CRACKED CASE. NEW APU ASSEMBLY OPS AND LEAK CHECKS NORMAL. INSTALLED IAW CRJ MM 49-10-00.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 3,423 hrs · 2,744 cycles

RECEIVED SPOILERON FAULT STATUS MESSAGE. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT INBOARD SPOILERON PCU WITH SERVICEABLE UNIT IAW MM 27-62-01. OPS CHECK GOOD.

Part: OIL SYSTEM — LOW (NR 2 IDG) · airframe 3,297 hrs · 2,650 cycles

NR 2 GENERATOR DROPPED OFF LINE DURING THE TAKEOFF ROLL. ABORTED TAKEOFF. SERVICED NR 2 IDG IAW MM 12-13-24. RAN RIGHT ENGINE GENERATOR. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 3,282 hrs · 2,641 cycles

WHILE AT THE GATE, STAB TRIM PERFORMED UNCOMMANDED FULL NOSE UP TO FULL NOSE DOWN MOVEMENT. STAB CH2 INOP STATUS MESSAGE APPEARED. DISCONNECTED STAB TRIM. STAB TRIM REENGAGED SEVERAL TIMES ON ITS OWN. INSTALLED SERVICEABLE HSTCU. OPS CHECKS OF STAB/YAW SYSTEM IAW 27-41-00. OPS CHECK GOOD.

Part: ECU — MALFUNCTIONED (SPOILERON) · airframe 3,235 hrs · 2,607 cycles

LEFT SPOILERON FAULT STATUS MESSAGE. INSTALLED SERVICEABLE SECU IN NR 2 POSITION IAW CRJ MM 27-61-05. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 3,235 hrs · 2,607 cycles

ON TAXI OUT SPOILERON FAULT STATUS MESSAGE CAME ON WITH THE LEFT SPOILERON INDICATING WHITE BOX/NOX. INSTALLED NEW PCU ON LEFT SPOILERON INBOARD POSITION IAW CRJ MM 27-62-01. OPS AND LEAK CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 2,975 hrs · 2,410 cycles

SPOILERON FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 1 SECU IAW 27-61-05. OPS CHECKS GOOD.

Part: PCU — FAILED (SPOILER) · airframe 2,867 hrs · 2,323 cycles

SPOILERON FAULT STATUS MESSAGE ON WITH ALL HYDRAULICS ON. REMOVED AND REPLACED LT O/B SPOILERON PCU ASSEMBLY. OPS CHECK GOOD. NO DEFECTS NOTED. NO LEAKS NOTED.

Part: WIRE — GROUNDED (LT WING) · airframe 2,783 hrs · 2,254 cycles

AFTER TAKEOFF OUT OF SLC, RECEIVED WING OVERHEAT MESSAGE. DID QRH PROCEDURE, MESSAGE WENT OUT. THEN A FEW MINUTES LATER RECEIVED ANTI-ICE DUCT MESSAGE. DID QRH PROCEDURE. ANTI-ICE DUCT MESSAGE CONTINUED THEN WENT OUT AFTER SEVERAL MINUTES. FOUND A GROUNDED WIRE ON THE WING DUCT OVERHEAT SENSOR OVER LEFT LANDING LIGHT. REPOSITIONED WIRES AWAY FROM ATTACHING SCREW. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (RT OB SPOILERON) · airframe 2,783 hrs · 2,254 cycles

RIGHT OUTBOARD SPOILERON MESSAGE. CIRCUIT BREAKER IS POPPED FOR PCU. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU, REF. MM 27-62-01. OPERATIONAL CHECKS GOOD.

Part: ECU — MALFUNCTIONED (E/E BAY) · airframe 2,758 hrs · 2,234 cycles

ON TAXI OUT, RECEIVED SPOILERON FAULT MESSAGE. REMOVED AND REPLACED SECU NR 1 DUE TO FAILURE IN SECU NR 1 MODULE-A. OPS CHECK GOOD IAW MM 27-61-00 AND 27-61-05.

Part: CONTROLLER — FAILED (ANTI-ICE SYS) · airframe 2,615 hrs · 2,115 cycles

WING OVERHEAT MESSAGE ON CLIMBOUT. ALSO HAD A RT WING ANTI ICE CAUTION MESSAGE. WING OVERHEAT MESSAGE WAS ON LEFT WING. RETURNED TO FIELD. REMOVED AND REPLACED WING ANTI TEMP CONTROLLER. RAN SYSTEM, OPS CHECKS OK.

Part: IDG — FAILED (NR 1 ENGINE) · airframe 2,557 hrs · 2,070 cycles

IDG1 MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF. RESET GEN BUT CAME OFF LINE AGAIN. REMOVED AND REPLACED NR 1 IDG WITH SERVICEABLE UNIT IAW MM 24-11-01. LEAK AND OPS CHECK GOOD.

Part: FASTENER — UNLATCHED (ACCESS DOOR) · airframe 2,547 hrs · 2,064 cycles

SHORTLY AFTER TAKEOFF HIGH PITCH SQUEAL EMITTED FROM LEFT FRONT OF AIRCRAFT. RETURNED TO SLC. FOUND THUMB LATCH ON EXTERNAL ACCESS PANEL UNLATCHED. INSPECTED DOOR AND RE-SECURED THUMB LATCH AS REQUIRED. NO DAMAGE NOTED.

Part: PCU — MALFUNCTIONED (SPOILERONS) · airframe 1,098 hrs · 925 cycles

LEFT SPOILERONS FAULT STATUS MESSAGE ON PDI2 IN FLIGHT. REMOVE AND REPLACE LEFT SPOILERON OUTBOARD PCU IAW 27-62-00 AND RESET CB4CN THEN CLEARED SECU FAIL LOGS. OPS CHECKS GOOD ON FLIGHT CONTROL. NO DEFECTS NOTED AT THIS TIME. P/N ON 27000-7, S/N ON MAL-347, S/N OFF 3979.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 975 hrs · 818 cycles

RIGHT FIRST OFFICERS WINDSHIELD CRACKED ON FINAL APPROACH. REMOVED AND REPLACED THE RIGHT WINDSHEILD ASSEMBLY IAW RII 56-401 AND MM 56-11-01. LEAK AND OPS CHECKS GOOD. P/N ON PPGNP-13921-10, S/N ON 01095H5012, S/N OFF 00083H3537.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 635 hrs · 520 cycles

FIRST OFFICER''''S WINDSHIELD SHATTERED. CABIN DIFFERENTIAL PRESSURE ON 7.3, NO PRESSURE LOSS. REMOVED AND REPLACED WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-11-01. C/W PRESSURIZATION CHECK. LEAK CHECK GOOD. P/N: NP139321-6, S/N ON: 00083H3538, S/N OFF: 00165H9933, P/N: 601R33033-10.