N443SW

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 40,808 hrs · 35,598 cycles

TRANSFER FROM EAML 410648 : SCRATCH DOWN TO BARE METAL. APROX 5 FEET BEHIND SERVICE DOOR, EYE LEVEL. DAMAGE FOUND TO BE AT FUSELAGE SKIN BETWEEN FS409.00 AND FS409.00+16 AND BETWEEN STR15R AND STR18R.REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN FS409.00 AND FS409.00+16 AND BETWEEN STR15R AND STR18R IN REF TO REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR AND FORM M-337.

Part: STRUT — FAILED (NLG) · airframe 39,717 hrs · 34,335 cycles

GEAR DISAGREE AFTER TAKEOFF. FOLLOWED QRH - RTF. FLT 4992. REMOVED AND REPLACED NLG DRESSED SHOCK STRUT IAW AMM. OPS CHECK GOOD.

Part: FITTING — DAMAGED (HORIZ STAB) · airframe 40,809 hrs · 35,599 cycles

THREE LOOSE BOLTS NOTED DURING INSPECTION OF HORIZONTAL STABILIZER STEADY FITTING (P/N 600-21402), REQUIRES FURTHER INSPECTION/REPAIR. REPAIRED HORIZONTAL STAB STEADY FITTING FASTENERS IAW REO. THIS SDR FOR T/STEADY FITTING IS BEING SUBMITTED AS A PART OF VDR_2020NM064006.

Part: FLOOR SUPPORT — CORRODED (BS 439-449) · airframe 39,717 hrs · 34,335 cycles

LH FLOOR SILL HAS TWO SPOTS OF CORROSION AROUND NUTPLATE HOLES BETWEEN F.S. 439.00 AND F.S. 449.85 LBL 42. (C-CHECK) REPAIRED LH FLOOR SILL IAW REO.

Part: ATTACH BRACKET — CORRODED (PAX DOOR) · airframe 39,717 hrs · 34,335 cycles

PAX DOOR INTERCOSTAL DD5, ATTACH BRACKET CORRODED. (C-CHECK) REMOVED AND REPLACED BRACKET IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,717 hrs · 34,335 cycles

PAX DOOR INTERCOSTAL DD6, CORRODED. (C-CHECK) REMOVED AND INSTALLED NEW SERVICEABLE CLEAT IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,717 hrs · 34,335 cycles

UPON REMOVAL OF PAX DOOR INNER SKIN, FOUND UPPER INTERCOSTAL UNDER LATCH-LOCK BOX TO BE CORRODED. (C-CHECK) RO: 08/06/2019 LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL (DD6) P/N#601R18057-1 IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,717 hrs · 34,335 cycles

PAX DOOR INTERCOSTAL CORRODED LOCATED APPROX: FS 347.25. (C-CHECK) REINSTALLED NEW PAX DOOR INTERCOSTAL IAW REO.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 39,717 hrs · 34,335 cycles

PAX DOOR CLEAT IS CORRODED. BS 311.75 ATTACHED TO INTERCOSTAL DD4. (C-CHECK) REMOVED AND INSTALLED NEW SERVICEABLE CLEAT IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,717 hrs · 34,335 cycles

PAX DOOR INTERCOSTAL DD6 IS CORRODED. (C-CHECK) LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,717 hrs · 34,335 cycles

PAX DOOR INTERCOSTAL DD7A IS CORRODED. (C-CHECK) LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR LWR FWD INTERCOSTAL (DD7A) IAW SRM.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 39,717 hrs · 34,335 cycles

RH TRUNNION HAS 1EA OVERSIZE FASTENER HOLE AT AFT MOST HOLE THROUGH STEEL PLATE. (C-CHECK) REPAIRED RT TRUNNION 1EA OVERSIZED FASTENER HOLE AT AFT MOST HOLE THROUGH STEEL PLATE IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 39,717 hrs · 34,335 cycles

FLOOR BEAM CAP IS CORRODED BETWEEN F.S. 589.00 AND F.S. 621.00 AROUND FASTENER HOLES ON LBL 9. (C-CHECK) RO: 08/06/2019 REMOVED DAMAGED FLOOR BEAM CAP AT FS589 TO FS621 ON LBL9 AND INSTALLED NEW SERVICEABLE FLOOR BEAM CAP IAW REO.

Part: FRAME — CORRODED (BS 349) · airframe 39,717 hrs · 34,335 cycles

FS 349 FRAME IS CORRODED ON THE AFT FACE OF THE FRAME BETWEEN STR 26L AND 26R. (C-CHECK) RO: 08/06/2019 REMOVED AND REPLACED FRAME SECTION WITH NEW P/N 601R32005-69 AT FS 349 FROM STR 24L - 24R IAW SRM.

Part: SKIN — CHAFED (LT WING) · airframe 39,717 hrs · 34,335 cycles

L/H LOWER WING PLANK CHAFED AT TRAILING EDGE OF ACCESS PANEL 193AB LBL 45.0. (C-CHECK) PERFORMED CHAFING REPAIR TO L/H LOWER WING PLANK AT TRAILING EDGE OF ACCESS PANEL 193B AT LBL 45.00 IAW REO.

Part: DOOR FRAME — CORRODED (MAIN PAX) · airframe 39,717 hrs · 34,335 cycles

PAX DOOR FWD FRAME IS CORRODED INSIDE PANEL 832HL.(C-CHECK). INSTALLED NEW SERVICEABLE PAX DOOR FWD FORMER IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 39,717 hrs · 34,335 cycles

PAX DOOR FWD INTERCOSTAL IS CORRODED INSIDE PANEL 832GL. C-CHECK. REMOVED AND REPLACED PAX DOOR FWD INTERCOSTAL IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 39,717 hrs · 34,335 cycles

4EA AREAS OF CRACK INDICATIONS NOTED ON FS621 RPB WEB IN THE HEEL LINE AREA OF VERT POSTS, (C-CHECK) RO: 08/06/2019 REPAIRED IAW REO.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 39,675 hrs · 34,287 cycles

MOMENTARY GEAR DISAGREE ON FINAL WHEN PUTTING GEAR DOWN (NOSE WHEEL), NOSE DOOR WARNING MESSAGE. EXTINGUISHED AND ALL INDICATIONS WERE GREEN AND NORMAL WITHOUT ANY QRH PROCEDURES. (FLT#4855) FO:05/22/2019 CLOSED REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM. PERFORMED EXTENSION/RETRACTION OF THE MLG IAW AMM. OPS CHECK GOOD. NO LEAKS NOTED. ACFT OK FOR SERVICE.

Part: STRUT — DISCHARGED (NLG) · airframe 38,607 hrs · 33,044 cycles

GEAR DISAGREE MASTER WARNING. NOSE GEAR WOULD NOT RETRACT. (FLT#4574) CLOSED PERFORMED FULL OIL AND NITROGEN SERVICE ON THE NLG ASSY IAW AMM. JACKED AIRCRAFT AND PERFORMED GEAR SWINGS IAW AMM. ALL OPS CHECKS ARE GOOD.

Part: PUMP — WEAK (HYD SYSTEM) · airframe 38,031 hrs · 32,400 cycles

GEAR DISAGREE ON APPROACH. REMOVED AND REPLACED HYDRAULIC PUMP 3A IAW AMM. OPS CHECKED GOOD, NO LEAKS NOTED. PERFORMED GEAR SWINGS IAW AMM. OPS CHECKED GOOD

Part: WINDOW FRAME — CRACKED (NOT REPORTED) · airframe 37,926 hrs · 32,278 cycles

WINDOW FRAME CRACKED.

Part: FLOOR SUPPORT — CORRODED (BS 319.7) · airframe 36,107 hrs · 30,291 cycles

FLOOR SUPPORT HAS CORROSION ON THE RIGHT SIDE BS 319.7. INSTALLED A NEW FLOOR SUPPORT IAW SRM AND REO.

Part: ANGLE — CORRODED (PAX DOOR LOCK) · airframe 36,107 hrs · 30,291 cycles

LOWER STOP FITTING ON PAX DOOR LOCK MECHANISM IS CORRODED AROUND THE STOP BOLT. INSTALLED A NEW LOWER STOP FITTING ANGLE IAW SRM.

Part: PANEL — CHAFED (AILERON LE) · airframe 36,107 hrs · 30,291 cycles

AILERON LEADING PANEL 599AB IS CHAFED. INSTALLED A NEW LEADING EDGE PANEL IAW SRM.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 32,492 hrs · 26,424 cycles

FLOOR PANEL 343AR HAS DELAMINATION. R & R THE FLOOR PANEL IAW EA.

Part: FLOOR PANEL — CRACKED (BS 461) · airframe 32,492 hrs · 26,424 cycles

CRACKS NOTED ON FUSELAGE PRESSURE FLOOR PANEL BS 461, RBL 9 TO LBL 9. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 499-513) · airframe 32,492 hrs · 26,424 cycles

PRESSURE FLOOR SUPPORT BS 499 - 513 AT LBL 45 HAS CORROSION. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 473) · airframe 32,492 hrs · 26,424 cycles

PRESSURE FLOOR SUPPORT BS 473.15 RBL 45.0 HAS CORROSION. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 424) · airframe 32,492 hrs · 26,424 cycles

PRESSURE FLOOR SUPPORT BS 424 LBL 45 HAS CORROSION. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 32,492 hrs · 26,424 cycles

PRESSURE FLOOR SUPPORT BS 559 LBL 45 HAS CORROSION. REPAIRED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 460-473) · airframe 32,492 hrs · 26,424 cycles

PRESSURE FLOOR SUPPORT BS 460 - 473.15 LBL 45 HAS CORROSION. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 499) · airframe 32,492 hrs · 26,424 cycles

PRESSURE FLOOR SUPPORT BS 499 RBL 45 HAS CORROSION. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 460-461) · airframe 32,492 hrs · 26,424 cycles

PRESSURE FLOOR SUPPORT BS 460 - 461 RBL 45 HAS CORROSION. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 484) · airframe 32,492 hrs · 26,424 cycles

PRESSURE FLOOR SUPPORT BS 484 RBL 45 HAS CORROSION. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 599) · airframe 32,492 hrs · 26,424 cycles

PRESSURE FLOOR SUPPORT BS 599 RBL 45.0 HAS CORROSION. REPAIRED IAW REO.

Part: BULKHEAD — CRACKED (BS 202) · airframe 32,492 hrs · 26,424 cycles

CRACK NEXT TO PARKING BREAK BULKHEAD FITTING BS 202. REPAIRED IAW REO.

Part: DOOR — DENTED (WATER SERVICE) · airframe 32,492 hrs · 26,424 cycles

RT FUSELAGE BELOW POTABLE WATER SERVICE DOOR DENTED. REPAIRED THE DOOR IAW EA AND AMM.

Part: LUG — GOUGED (LT AILERON) · airframe 32,492 hrs · 26,424 cycles

LEFT AILERON CENTER OTBD PCU LINK LUG ON AILERON IS GOUGED. REPAIRED LT AILERON CENTER OTBD PCU LINK LUG GOUGE IAW REO.

Part: SKIN — CHAFED (GROUND SPOILER) · airframe 32,492 hrs · 26,424 cycles

LT INBD GROUND SPOILER IS CHAFED ON LOWER L/E SKIN OTBD OF INBD HINGE APPROXIMATELY SP STA 56.177. BLENDED CHAFE AT LOWER FLANGE OF LT INBD GROUND SPOILER AT LOWER L/E OF SKIN APPROXIMATELY SP STA 56.177 IAW SRM.

Part: CAP — CHIPPED (HORIZONTAL STAB) · airframe 32,492 hrs · 26,424 cycles

RIGHT HORIZONTAL STABILIZER END CAP CHIPPED OTBD L/E. REPAIRED THE HORIZONTAL STAB END CAP L/E IAW SRM.

Part: CAP — CHIPPED (HORIZONTAL STAB) · airframe 32,492 hrs · 26,424 cycles

LT HORIZONTAL STABILIZER END CAP L/E INBD CHIPPED. REPAIRED THE LT HORIZONTAL STAB END CAP L/E IAW SRM.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 32,492 hrs · 26,424 cycles

DENT ON RT ELEVATOR LOWER SURFACE BETWEEN ES 69.103 - 77.682, AND BETWEEN RIBS 9 AND 10. COMPLIED WITH PERMANENT REPAIR IAW EA.

Part: O-RING — FAILED (APU FCU) · airframe 32,384 hrs · 26,322 cycles

FUEL ODOR IN FLIGHT AND ON THE GROUND COMING FROM THE GASPER VENTS. REPLACED O-RING ON APU FUEL CONTROL OUTLET, NO FUEL ODOR.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 31,599 hrs · 25,557 cycles

EMERGENCY LIGHTS FLOOR STRIP BETWEEN ROW 2 THRU 8 AND LT LOWER SIDEWALL EXIT LIGHT AT OVERWING E EXIT INOPERATIVE. R & R BATTERY PACK NR 1 AND NR 4 ALSO RESEATED E-LIGHT FLOOR STRIPS BETWEEN ROW 2 THRU 8, OPS CHECKED E-LIGHTS ON FLOOR STRIPS BETWEEN ROWS 2 THRU 8 AND EXIT LIGHT ON LEFT LOWER SIDEWALL OVERWING EMERGENCY EXIT, OPS CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 31,599 hrs · 25,557 cycles

AFTER TAKEOFF AT 1100 FT, RECEIVED RT PITOT HEAT CAUTION MESSAGE. RAN QRH - DID NOT FIX. RETURNED TO FIELD. RESET IAW FIM INTRODUCTION - MSG CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 31,599 hrs · 25,557 cycles

DURING TAKEOFF AT 800 FT, RECEIVED RT AOA HEAT CAUTION MESSAGE. RAN QRH. DID NOT FIX. RETURN TO FIELD. RESET IAW FIM INTRODUCTION-MSG CLEARED.

Part: SKIN — DENTED (RT ELEVATOR) · airframe 31,568 hrs · 25,524 cycles

RIGHT ELEVATOR BOTTOM SIDE DENTED. REPAIRED IAW REO.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,568 hrs · 25,524 cycles

SECOND OVERHEAD EMERGENCY FLOODLIGHT FROM THE BACK IS INOPERATIVE. R & R NR 3 EMERGENCY LIGHT BATTERY IAW AMM. PN ON: 2013-1A, PN OFF: AD-2013-1A, SN ON: 112416, SN OFF: 69085.

Part: UPLOCK SWITCH — OUT OF ADJUST (LT MLG) · airframe 31,040 hrs · 25,009 cycles

LT MAIN GEAR EICAS BOX DID NOT GO GREEN. PSEU FLAGS S20. ADJUSTED UPLOCK PROXIMITYSWITCH S20.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,638 hrs · 24,610 cycles

RIGHT AND LEFT WING MIDDLE EMERGENCY LIGHTS INOPERATIVE, REPLACED THE LAMPS.

Part: SKIN — DAMAGED (BS 430) · airframe 30,632 hrs · 24,604 cycles

SKIN DAMAGED ON RT SIDE OF ACFT BELOW WINDOW APPROXIMATELY FS430 AND STRINGER 15A. DAMAGE IS ACTUALLY LOCATED BETWEEN FS409+96-FS409+112, STR 15R-STR 16R DENT MEASURES 3.0" L, 3.75"W, 0.066" D. CUTOUT DAMAGED AREA ON FS409+96 -FS409+112, STR 15R-STR 16R AND APPLIED DOUBLER IAW SRM.

Part: SKIN — DAMAGED (BS 220-235) · airframe 30,632 hrs · 24,604 cycles

SKIN DAMAGED UNDERNEATH F/O WINDSHIELD FWD OF SIDE WINDOW DUE TO BIRDSTRIKE. DAMAGE IS LOCATED BETWEEN FS 220.00-FS235.00 AND BETWEEN THE CO-PILOT WINDSHIELD AND STR 12R. DENT WAS CAUSED BY A BIRDSTRIKE AND MEASURES APPROXIMATELY 18"L, 11"W, 0.5" D. DENT CAUSED A DEFLECTION TO FS 220.00 FRAME ASSY, DWG 600-34013 AND A 9.5" CRACK TO THE WINDSHIELD SILL-LOWER SIDE MEMBER, DWG 600-33114. ALL REPAIRS COMPLETED IAW AMM AND SRM, PN 601R51158-7, PN 600-34013-166, PN 601R33036-5.

Part: SIGN — BROKEN (CABIN) · airframe 30,207 hrs · 24,199 cycles

MAIN CABIN DOOR EMERGENCY EXIT SIGN BROKEN. FLT 4647 RELAMPED, PN BR9279-22.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,763 hrs · 23,749 cycles

EMERGENCY LIGHT POD BURNED OUT. FLT 4475 RELAMPED.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 29,565 hrs · 23,558 cycles

RT EXTERNAL FS SKIN PANEL DAMAGED BETWEEN FS 625.30 & FS640, STRINGERS 18R TO 20R. C-CHECK REPAIRED IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,565 hrs · 23,558 cycles

FS 280 BULKHEAD WEB CRACKED OUT OF FASTENER HOLE AT INBD SIDE OF RBL9.0. C-CHECK REPAIRED IAW REO.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 29,678 hrs · 23,657 cycles

REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT BL0.0 WL 110 APPROXIMATELY 1.3 INCHES IN LENGTH. C-CHECK REPAIRED REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT BL0.0 WL 110 APPROXIMATELY 1.3 INCHES IN LENGTH, IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,462 hrs · 23,468 cycles

EMERGENCY OVERHEAD LIGHT ROW 12 & 13 IS BURNED OUT. FLT#7428 RELAMPED.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 29,426 hrs · 23,440 cycles

FIRST EMERGENCY LIGHT STRIP ON FLOOR DOES NOT ILLUMINATE. FLT#5337 RE-CONNECTED FIRST EMERGENCY LIGHT STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,026 hrs · 23,110 cycles

LEFT AFT OVERWING EMERGENCY LIGHT IS BURNED OUT. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,653 hrs · 22,170 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5373) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,254 hrs · 21,794 cycles

OVERHEAD EMERGENCY EXIT SIGN AT ROW 8 IS OUT. (FLT 4458) REPLACED BATTERY PACK ELBP NR 2 AND ELBP BATTERY CHARGER NR 2 IN REFERENCE TO AMM. P/N: AD-2013-1A S/N: 42052 AND P/N: 11-0049.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,878 hrs · 21,480 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 5261) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,643 hrs · 21,289 cycles

NR 1 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4754) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,469 hrs · 21,135 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4499) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,150 hrs · 20,850 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4557) RELAMPED EMERGENCY LIGHT.

Part: DRAIN LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 25,794 hrs · 20,638 cycles

FIRST OFFICER'S IVSI FLUCTUATING +/- 1000 FT. ALTIMETER FLUCTUATING +/- 100. BOTH WHILE CAPTAIN SIDE STABLE. (FLT 3975) REMOVED MOISTURE FROM NR 2 ADC PITOT DRAIN TUBE.

Part: INVERTER — FAILED (CABIN) · airframe 25,703 hrs · 20,584 cycles

LEFT EMERGENCY EXIT LIGHT IS OUT. (FLT 6281) REPLACED NR 2 EMERGENCY LIGHT INVERTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,544 hrs · 20,466 cycles

LEFT FORWARD, RIGHT FORWARD AND RIGHT AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. (FLT 5263) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,544 hrs · 20,466 cycles

THE 3RD OVERHEAD EMERGENCY CEILING LIGHT INOPERATIVE. (FLT 5363) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,348 hrs · 20,317 cycles

LEFT SIDE MIDDLE EXTERIOR OVERWING EMERGENCY LIGHT IS OUT. (FLT 5484) RELAMPED EMERGENCY LIGHT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,242 hrs · 20,233 cycles

FUSELAGE SKIN ABOUT 20 INCHES ABOVE GROUND AIR PORT, AFT OF 1ST SPLICE OF CARGO IS DENTED. (C-CHECK) REPAIRED PER REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,581 hrs · 21,231 cycles

FORWARD FUSELAGE SKIN CRACKED AT LEFT TRU DOOR AFT LATCH. (C-CHECK) REPLACED FUSELAGE SKIN PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,581 hrs · 21,231 cycles

CRACK INDICATED ON THE LEFT SIDE FS 559.0 PRESSURE BULKHEAD. (C-CHECK) REPAIRED PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,581 hrs · 21,231 cycles

CRACK AT FS 409.0+128 BL 0.00 LEFT AND RIGHT AFT RADIUS OF VERTICAL POST. (C-CHECK) REPAIRED IN REFERENCE TO CRJ200 SRM.

Part: SKIN — CRACKED (PAX DOOR) · airframe 26,581 hrs · 21,231 cycles

PASSENGER DOOR INNER SKIN HAS A CRACK AT FS 340 WHERE SKIN MATES TO INTERCOSTAL AT LOWER PORTION OF PAX DOOR. (C-CHECK) REPAIRED IAW CRJ200 SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 26,581 hrs · 21,231 cycles

CRACK AT FS 409.0+128 BL 18.00 OUTBOARD AFT RADIUS OF VERTICAL POST. (C-CHECK) REPLACED VERTICAL POST IN REFERENCE TO CRJ200 SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,741 hrs · 18,946 cycles

LEFT AND RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 6872) RELAMPED EMERGENCY LIGHT.

Part: SIGN — LOW (CABIN) · airframe 23,545 hrs · 18,804 cycles

AFT OVERWING EMERGENCY EXIT SIGN ILLUMINATES VERY DIMLY. (FLT 6407) REPLACED AFT OVERWING EMERGENCY EXIT SIGN ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,502 hrs · 18,772 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6452) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,863 hrs · 18,230 cycles

AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6700) RELAMPED EMERGENCY LIGHT.

Part: SHAFT — DAMAGED (ENGINE MOUNT) · airframe 22,458 hrs · 17,878 cycles

RIGHT ENGINE AFT THRUST SHAFT SCORED. (ENGINE CHANGE) REPLACED RIGHT ENGINE AFT MOUNT THRUST SHAFT PER AMM.

Part: LINK — CORRODED (ENGINE MOUNT) · airframe 22,458 hrs · 17,878 cycles

RIGHT ENGINE FORWARD MOUNT LINK ASSEMBLY PITTED. (ENGINE CHANGE) REPLACED RIGHT ENGINE FORWARD MOUNT YOKE LINK ASSEMBLY PER AMM.

Part: BOLT — DAMAGED (ENGINE MOUNT) · airframe 22,458 hrs · 17,878 cycles

RIGHT ENGINE FORWARD MOUNT BOLT IS SCORED. (ENGINE CHANGE) REPLACED ONE RIGHT ENGINE FORWARD MOUNT BOLT PER AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,524 hrs · 16,216 cycles

FS 621 AFT BULKHEAD CRACKED AT CARGO DOOR ROLLER GUIDE TRACK. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,109 hrs · 16,724 cycles

FS 559 BULKHEAD AT RBL 18 WL 59 CRACKED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,438 hrs · 16,146 cycles

NR 2 AND NR 4 EMERGENCY CEILING LIGHTS INOP. (FLT 6450) RELAMPED EMERGENCY CEILING LIGHT.

Part: TRIM PANEL — FAILED (RUDDER SYS) · airframe 20,109 hrs · 15,881 cycles

RUDDER TRIM RUNAWAY DURING APPROACH WITH FULL RIGHT DEFLECTION. (FLT 5928) REPLACED RUDDER TRIM PANEL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,033 hrs · 15,826 cycles

EMERGENCY EXIT LIGHT ON AIRCRAFT EXTERIOR ABOVE RIGHT WING INOP. (FLT 5848) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,856 hrs · 15,676 cycles

NR 1 EMERGENCY LIGHT POD IN CABIN INOP. (FLT 6575) RELAMPED IAW CRJ200 MM 33-51-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,518 hrs · 15,413 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. (FLT 4844) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,296 hrs · 15,251 cycles

EMERGENCY LIGHT NR 4 INOP. (FLT 5991)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,219 hrs · 15,187 cycles

OVERHEAD EMERGENCY CABIN LIGHT INOP. (FLT 5814) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,574 hrs · 14,697 cycles

FLT 4674 - OVERHEAD EMERGENCY EXIT LIGHT ABOVE ROW 10 INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,203 hrs · 14,412 cycles

FLT 6391 - NR 2 OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 17,889 hrs · 14,177 cycles

FLT 4390 - FLOOR EMERGENCY LIGHTING INOP. REPLACED INVERTER AT EMERGENCY BATTERY NR 3.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,882 hrs · 14,172 cycles

FLT 4507 - THIRD AFT CEILING EMERGENCY FLOOD LIGHTS INOP. RELAMPED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 17,809 hrs · 14,114 cycles

FLT 5800 - EMERGENCY EXIT SIGN AT ROW 8D INOP. RESECURED CONNECTOR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,729 hrs · 14,046 cycles

C-CHECK, FS 280 FORWARD FLOOR SUPPORT CRACKED AT RADIUS, REPLACED.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 17,729 hrs · 14,046 cycles

C-CHECK, RIGHT ENGINE FORWARD MOUNT YOKE FLANGED BUSHINGS CORRODED, REPLACED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,729 hrs · 14,046 cycles

C-CHECK, FS 280 RBL9 LOWER FLOOR SUPPORT CRACKED. REPAIRED PER REO.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 17,729 hrs · 14,046 cycles

C-CHECK, LEFT ENGINE FORWARD MOUNT YOKE FLANGED BUSHING CORRODED, REPLACED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,729 hrs · 14,046 cycles

C-CHECK, FS 280 LOWER FLOOR SUPPORT CRACKED AT LBL9.. REPAIRED PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,729 hrs · 14,046 cycles

C-CHECK, FS 280 RBL9 SUPPORT CRACKED. REPAIRED PER REO.

Part: FITTING — CORRODED (RT ENGINE) · airframe 17,729 hrs · 14,046 cycles

C-CHECK, RIGHT ENGINE THRUST FITTING CORRODED, REPLACED.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 17,067 hrs · 13,489 cycles

BROKEN WINDSCREEN EMERGENCY EXIT SIGN. (FLIGHT NR 4122) REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 15,276 hrs · 12,090 cycles

FLT 3751 - EMERGENCY LIGHT PODS AT ROWS 5 AND 10 ARE INOP. RELAMPED AS REQUIRED. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,804 hrs · 10,182 cycles

THE 280 FLOOR SUPPORT CRACKED RIGHT HAND UPPER RBL 9.0 RIGHT HAND INBOARD AND OUTBOARD CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS P/N 601R31113-58 -4 & ANGLES AT FS 280, RBL 9.0 IAW CRJ200 REO 601R-53-11-136 AND 601R-53-0057A SRM 51-42-13.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,804 hrs · 10,182 cycles

PAX DOOR FWD WEB CRACKED BETWEEN FIXED STEPS 1 & 2. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER, ANGLE AND SHIMS PER REO 52-11-1141.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,804 hrs · 10,182 cycles

PAX DOOR FWD WEB CRACKED UNDER THE HAND RAIL HOLD DOWN BRACKET. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND ANGLES PER REO 601R-52-11-702.

Part: ATTACH BRACKET — CRACKED (BS 484) · airframe 12,804 hrs · 10,182 cycles

STA 484 FAIRLEAD BRACKET INBOARD AND OUTBOARD CLIPS CRACKED LBL 27 AND 36. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AND NEW REPAIR ANGLE IAW CRJ200 REO 601R-53-41-059 STEP 8, 11, 12, 14.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,804 hrs · 10,182 cycles

THE 280 FLOOR SUPPORT CRACKED LT UPPER LBL 10 LT INBOARD CLIP CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS P/N 601R31113-57 & ANGLES AT FS 280, LBL 9.0 IAW CRJ200 REO 601R-53-11-136 AND 601R-53-0057A SRM 51-42-13.

Part: ARM — CRACKED (ESCAPE HATCH) · airframe 12,804 hrs · 10,182 cycles

CREW ESCAPE HATCH - LT HINGE ARM IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AND ADJUSTED LT HINGE ARM ON CREW ESCAPE HATCH REF CRJ200 AMM 52-22-00-820-804 STEP 3D (2).

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,804 hrs · 10,182 cycles

PASSENGER DOOR AFT DRAG CRACKED AT THE DOOR ASSIST CABLE PULLEY BRACKET. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW DRAG ANGLE SECTION P/N 601R-31772-5, AS PER REO 601R-52-513.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 12,804 hrs · 10,182 cycles

ENGINE SUPPORT BEAM LOWER WEB CRACKED AT RT ACCESS COVER OPENING. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, WEB FILLER & STRAP IAW REO601R-61-358 REV A.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,804 hrs · 10,182 cycles

PASSENGER DOOR AFT WEB CRACKED BETWEEN THE FIXED STEPS 1 AND 2 UNDER HANDRAIL HOLD DOWN BRACKET. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER & ANGLES PER CRJ 200 REO 601R-52-11-702.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,804 hrs · 10,182 cycles

PASSENGER DOOR AFT WEB CRACKED BETWEEN THE 3RD AND 4TH FIXED STEPS. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER, ANGLE & FILLERS PER REO 601R-52-11-1140.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 12,804 hrs · 10,182 cycles

PASSENGER DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED PASSENGER DOOR OUTER HANDLE P/N 601R31704-7 PER CRJ200 AMM REF 52-11-03 PG 401-411.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 12,804 hrs · 10,182 cycles

ENGINE SUPPORT BEAM LOWER WEB CRACKED AT LT ACCESS COVER OPENING. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR DOUBLER, SHIM, STRAP AND WEB FILLER IAW CRJ200 REO 601R 53-61-358 SHEET 3 NOTE 7.

Part: PUMP — LEAKING (NR 2) · airframe 12,188 hrs · 9,695 cycles

HYDRAULIC PAGE SHOWED PRESSURE BUT "O" (QUANTITY) FLUID. REPLACED NR 2 EDP IAW 29-11-01. OPERATIONAL CHECKS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 11,030 hrs · 8,748 cycles

ONE OVERHEAD EMERGENCY FLOODLIGHT IS INOP. REPLACED OVERHEAD EMERGENCY FLOODLIGHT BULB. OPERATIONAL CHECK GOOD.

Part: DOOR — OUT OF RIG (SERVICE) · airframe 10,494 hrs · 8,291 cycles

SERVICE DOOR IS HARD TO OPEN AND CLOSE. RIGGED DOOR AS NEEDED, OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,296 hrs · 8,128 cycles

CEILING "LEVEL" EMERGENCY LIGHT (FLOOD) 1 AT FARTHEST AFT "INOP". RELAMPED LAMP. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 9,479 hrs · 7,485 cycles

ON DEPARTURE THROUGH 2000' RT FLIGHT SPOILER DEPLOYED MSG WAS DISPLAYED, FOLLOWED BY A SPOILER FAULT MESSAGE. REPLACED RT OB FLIGHT SPOILER PCU IAW MM 27-62-01, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 8,905 hrs · 7,022 cycles

FLAPS HALFSPEED STATUS MESSAGE. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW MM 27-51-05. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 8,565 hrs · 6,765 cycles

DURING DESCENT INTO SLC, F/O'S SIDE WINDOW CRACKED. REPLACED RIGHT SIDE WINDOW PER MM 56-12-01. OPERATIONAL CHECK GOOD. P/N OFF 601R33033-12, S/N OFF 01353H5453.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 8,502 hrs · 6,716 cycles

SMOKE CARGO WARNING ON THE GROUND, NO SMOKE OBSERVED. REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR IAW M/M 26-15-01. OPERATIONAL CHECK GOOD. P/N 478597-19; S/N OFF 1929.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,358 hrs · 6,617 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CEILING EMERGENCY LIGHT IAW CRJ MM33-51-00. OPERATIONAL CHECK GOOD.

Part: SILL — CORRODED (FUSELAGE) · airframe 8,267 hrs · 6,546 cycles

FS 589.0 CARGO BAY FLOOR SILL RBL 44 ANGLE CORRODED, 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, 51-41-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,267 hrs · 6,546 cycles

FS 484 RIGHT INTERCOSTAL OUTBOARD FLANGE RBL 36 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV A.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,267 hrs · 6,546 cycles

FS 621 RIGHT SIDE FLOOR SUPPORT ANGLE RBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. CRACKED ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV "B" .

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,267 hrs · 6,546 cycles

FS 460 RIGHT OUTBOARD FLOOR FITTING RBL 9.0 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 51-42-06, 51-42-21, 51-23-00, 51-25-16 & 51-21-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,267 hrs · 6,546 cycles

FS 625 LEFT INTERCOSTAL ANGLE STR 14L CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,267 hrs · 6,546 cycles

FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.

Part: PCU — MALFUNCTIONED (FLT SPOILER) · airframe 8,183 hrs · 6,481 cycles

SPOILERON FAULT STATUS MESSAGE. REPLACED LEFT SPOILERON INBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 6,629 hrs · 5,193 cycles

ONE CEILING EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EMERGENCY LAMP. OPERATIONAL CHECK GOOD.

Part: GEARBOX — MALFUNCTIONED (NR 1 THRUST) · airframe 5,218 hrs · 4,083 cycles

NR 1 THRUST LEVER STUCK AT CRUISE POWER SETTINGS. PERFORMED QRH AND SHUT DOWN NR 1 ENGINE. REMOVED AND REPLACED LT POWER LEVER CONTROL GEAR BOX IAW CRJ MM 76-11-17. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 5,016 hrs · 3,924 cycles

FLAPS HALFSPEED STATUS ON TAXI OUT. FOUND 3 OF THE 4 ACTUATORS FAILED TORQUE CHECK. REMOVED AND REPLACED ALL FLAP ACTUATORS LT AND RT SIDE IAW MM 27-53-01 AND 27-53-05. LEFT WING FLAP ACTUATORS - OPS CHECK GOOD. (RIGHT WING) RIGGING AND OPS CHECKS GOOD. LEFT NR 1 FLAP ACTUATOR S/N OFF: 3278, LEFT NR 2 FLAP ACTUATOR P/N: 852D100-19, S/N OFF: 3201, LEFT NR 3 FLAP ACTUATOR P/N: 853D100-19, S/N OFF: 1908, LEFT NR 4 FLAP ACTUATOR P/N: 854D100-19, S/N OFF: 1671 RIGHT NR 4 FLAP ACTUATOR P/N: 854D100-20, RIGHT NR 3 P/N: 853D100-20, S/N OFF: 1916, RIGHT NR 1 P/N: 852D100-19, S/N OFF: FRO361, RIGHT NR 2 P/N: 852D100-19, S/N OFF: FRO354.

Part: FCU — OUT OF RIG (TE FLAPS) · airframe 4,910 hrs · 3,842 cycles

AFTER TAKEOFF, SELECTED FLAP FROM 20 DEGREES TO 8 DEGREES AND GOT A FLAPS FAIL MESSAGE. RETURNED TO FAT. RE-RIGGED FECU IAW 27-51-10. OPS CHECK GOOD ON GROUND.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 4,474 hrs · 3,515 cycles

SPOILERONS FAULT ON TAXI OUT. REMOVED AND REPLACED LEFT INBOARD FLIGHT SPOILERON PCU IAW CRJ AMM 27-62-01. OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,158 hrs · 3,250 cycles

FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R31113-58

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,158 hrs · 3,250 cycles

FS 280 LT FLOORBEAM LBL 9.0 IB AND OB ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R31113-57

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,158 hrs · 3,250 cycles

FS 621.00, LBL 42, FLOOR SUPPORT ANGLE CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV ''A'', RII 53-401. P/N: 601R-53-61-117-3

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,158 hrs · 3,250 cycles

FS 484 LT INTERCOSTAL OB FLANGE LBL 36 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED INTERCOSTAL IAW CRJ RE 601R-53-41-059 REV ''A'' & RII 53-401.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 3,097 hrs · 2,414 cycles

RT WING FORWARD EMERGENCY LIGHT INOP. REPLACED BULB PER CRJ MM 33-51-21. OPS CHECK GOOD.

Part: WIRE — CORRODED (EMERGENCY LIGHT) · airframe 2,427 hrs · 1,886 cycles

EMERGENCY ROW EXIT LIGHTS OUT IN THE BACK SECTION. FOUND WIRE PIGTAIL FOR AFT LIGHT SECTION TO BE CORRODED. REPLACED PIGTAIL. OPS CHECK GOOD.

Part: HEATER — MALFUNCTIONED (LT AOA PROBE) · airframe 2,041 hrs · 1,587 cycles

LT AOA HEAT CAUTION MESSAGE CAME ON IN FLIGHT, WOULD NOT GO OUT. CYCLED POWER AND COULDN'T DUPLICATE PROBLEM. PROBE HEATED OK.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 1,077 hrs · 841 cycles

STAB TRIM CH 2 AND MACH TRIM DISENGAGED CLIMBING OUT OF SLC. RAN QRH PROCEDURE. DID NOT RE-ENGAGE. RETURNED TO SLC. REMOVED AND REPLACED HORIZONTAL STABILIZER TRIM UNIT WITH SERVICEABLE UNIT. OPS CHECK SATISFACTORY IAW CRJ MM 27-41-01.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 861 hrs · 661 cycles

SHORTLY AFTER ROTATION, STAB TRIM NR 2 AND MACH TRIM WENT INOP AND WOULD NOT RESET. PERFORMED QRH AND RETURNED TO DFW. REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01 AND 27-42-05. OPS CHECK GOOD.