N492SW

Part: WINDSHIELD — FAILED (RT COCKPIT) · airframe 47,706 hrs · 45,084 cycles

SHATTERED RT WINDSHIELD WHILE AT CRUISE ALTITUDE. FLIGHT 4642-FILED CLOSED. REMOVED AND REPLACED RT WINDSHIELD IN REFERENCE WITH AMM. COMPLIED WITH TASK CARD, OPERATIONS CHECKS GOOD WITH NO LEAKS NOTED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 46,895 hrs · 44,308 cycles

CABIN ALT CAUTION MESSAGE IN FLIGHT. DISAPPEARED ONCE CABIN PRESSURE REGAINED IN FLIGHT FLIGHT 5308 - FILED CLOSED PERFORMED GVI OF OUTFLOW VALVES. NO DEFECTS NOTED. ACFT WOULD NOT PRESSURIZE ABOVE .6 P UNTIL CABIN PRESSURE CONTROLLER 1 CB WAS PULLED. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER #1 IN REFERENCE TO CRJ 200 AMM. OPS CHECKS GOOD. ACFT PRESSURIZES NORMALLY.

Part: ACTUATOR — FAILED (LT MLG) · airframe 46,375 hrs · 43,836 cycles

LEFT MAIN GEAR DISAGREE WARNING MESSAGE IN FLIGHT. LEFT MAIN NEVER SHOWED DOWN AND LOCKED FLIGHT 5644 CLOSED INTERROGATED PSEU AND FOUND LT MLG DOWNLOCK PROX SENSORS S19 , S34 INDICATING FAR WITH GEAR DOWN/LOCKED. REPLACED LT MLG SIDE STAY ACTUATOR IAW AMM. PERFORMED MULTIPLE GEAR CYCLES WITH NO DEFECTS NOTED . OPS CHECK GOOD. NO LEAKS NOTED.

Part: ACTUATOR — FAILED (NLG) · airframe 45,632 hrs · 43,184 cycles

GEAR DISAGREE WARNING MESSAGE. FLT 5226. REMOVED AND REPLACED THE NLG EXTENSION/RETRACTION ACTUATOR IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: ACTUATOR — FAILED (AILERON TRIM) · airframe 45,632 hrs · 43,184 cycles

AILERON TRIM STUCK LEFT WING DOWN POSITION. FLIGHT 5117. REPLACED AILERON TRIM ACTUATOR IAW AMM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

RT FLOOR SILL FS409+73.2 - FS409+128 HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 02/20/2019 REPAIRED RIGHT FLOOR SILL FS 409+73 TO 409+128 IAW REO.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

EXTERNAL FUSELAGE SKIN IS DENTED AT FS605 - FS621 STR 21L-22L. (C-CHECK) RO: 02/20/2019 REPAIRED DENT IAW REO. ALL STEPS COMPLIED WITH.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

LT FS 621.00 BETWEEN LBL9 AND LBL27 CORROSION AT FLOOR SUPPORT ANGLE UNDER FLOOR PANEL 281JLF. (C-CHECK) RO: 02/20/2019 REPAIRED FLOOR SUPPORT ANGLE AT FS621 BETWEEN LBL9 AND LBL27 IAW SRM. ALL STEPS IAW REO COMPLIED WITH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

CENTER FS 617.00 BETWEEN RBL9 AND LBL9 CORROSION AT AFT FLOORBEAM SUPPORT TOP CAP UNDER FLOOR PANEL 281DLF. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED VENT ASSY AND PACKER PN: 601R35235-61 WITH NEW VENT ASSY AND PACKER AT CENTER FS 617 BETWEEN RBL9 AND LBL9 AT AFT FLOORBEAM SUPPORT TOP CAP UNDER FLOOR PANEL 281DLF IAW SRM.

Part: SKIN — DENTED (BS 640) · airframe 44,668 hrs · 42,329 cycles

DENT #5 LOCATED 3.5€? AFT OF FS640 AND 1.5€? ABOVE STR25R HAS OIL CANNING CONDITION. (C-CHECK) RO: 02/20/2019 REPAIRED DENT #5 LOCATED 3.5€? AFT OF FS640 AND 1.5€? ABOVE STR25R IAW REO.

Part: STIFFENER — CORRODED (PAX DOOR) · airframe 44,668 hrs · 42,329 cycles

PAX DOOR HAS CORROSION UNDER UPPER EDGE MEMBER ON STIFFENER. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED PAX DOOR UPPER EDGE MEMBER STIFFENER, PN 601R31907-43 IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

LT PRESSURE FLOOR SILL ANGLE HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 02/20/2019 BLENDED CORROSION FROM LT PRESSURE FLOOR SILL ANGLE IAW SRM.

Part: PANEL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

RT PRESSURE FLOOR SILL PANEL HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 02/20/2019 COMPLIED WITH REPAIR TO THE RT PRESSURE FLOOR SILL PANEL MULTIPLE AREAS OF CORROSION IAW REO.

Part: FLOOR SUPPORT — DAMAGED (BS 559) · airframe 44,668 hrs · 42,329 cycles

REPLACE R/H FLOOR BEAM UPPER CAP AT RBL 9 FROM FS 559+12 TO FS 559+120 DUE TO DAMAGE. (C-CHECK) RO: 02/20/2019 REPLACED FLOOR BEAM CAP WITH NEW BEAM CAP LOCATED AT RBL9 BETWEEN FS559+12 TO FS559+120 IAW REO AND SRM.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 44,668 hrs · 42,329 cycles

REPLACE THE RH FLOOR SILL FROM FS 559.0+16 TO 559.0+80 WITH SERVICEABLE DUE TO OUT OF LIMITS CORROSION. REMOVED AND INSTALLED NEW RH FLOOR SILL FROM FS 559+16 TO FS 559+84.9 IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 44,668 hrs · 42,329 cycles

REPLACE RH FLOOR BEAM AT FS.589.00 TO FS.621.00 RBL27 WITH SERVICEABLE DUE TO OUT OF LIMITS CORROSION. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED RH FLOOR BEAM AT FS.569.00 TO FS.621.00 RBL27 IAW REO.

Part: PANEL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

LT PRESSURE FLOOR SILL PANEL HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 02/20/2019 BLENDED CORROSION ON LT PRESSURE FLOOR SILL PANEL IAW SRM AND REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

LT FLOOR SILL CORRODED FROM FS 559.0 TO FS 559.0+80. (C-CHECK) RO: 02/20/2019 REPLACED THE LT FLOOR SILL FROM FS559.00 TO FS559+84.9 WITH NEW SILL IAW SRM AND REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

CENTER FS 589.00 + 00 BETWEEN RBL9 AND LBL9 CORROSION AT AFT FLOORBEAM TOP CAP UNDER FLOOR PANEL 281CLF. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED FS589 BETWEEN RBL9 AND LBL9 CAP STRIP IAW SRM.

Part: SKIN — DENTED (BS 672-690) · airframe 44,668 hrs · 42,329 cycles

EXTERNAL FUSELAGE SKIN DENTS. A/C R/H SIDE , BETWEEN FS672 AND FS690 BETWEEN STGRS 23R AND 26R. (C-CHECK) RO: 02/20/2019 PERFORMED DRESS-BACK DENTS ON EXTERNAL FUSELAGE SKIN R/H SIDE BETWEEN FS672 AND FS690 BETWEEN STGR23R AND STGR26R IAW REO.

Part: SKIN — DENTED (BS 672-690) · airframe 44,668 hrs · 42,329 cycles

EXTERNAL FUSELAGE SKIN DENTS ON A/.C R/H SIDE BETWEEN FS672 AND FS690 BETWEEN STGRS 23R AND 26R. (C-CHECK) RO: 02/20/2019 DRESSED BACK 4EA DENTS LOCATED ON AFT RH SIDE OF FUSELAGE FROM FS672-690 BETWEEN STGRS 23R AND 26R IAW REO.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,668 hrs · 42,329 cycles

EXTERNAL FUSELAGE SKIN DENTS. A/C LT SIDE BETWEEN FS621 AND FS672 BETWEEN STGRS 21L AND 26L. (C-CHECK) RO: 02/20/2019 PERFORMED HAND DRESS DENT NR 1, NR 2, NR 3 AND NR 4 IAW REO.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 44,668 hrs · 42,329 cycles

SERVICE DOOR SILL AREA €“ ANGLE ATTACHED TO LOWER SILL HAS CORROSION. (C-CHECK) RO: 02/20/2019 REMOVED AND REPLACED WITH NEW SERVICE DOOR SILL ANGLE IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 44,668 hrs · 42,329 cycles

AVIONICS BAY RH INTERCOSTAL OUTBOARD OF STR 27 BETWEEN FS 349 AND FS 364 HAS CORROSION. (C-CHECK) RO: 02/20/2019 REPLACED AVIONICS BAY RH INTERCOSTAL OUTBOARD OF STR 27 BETWEEN FS 349 AND FS 364. ALL CHECKS GOOD.

Part: DOOR FRAME — CORRODED (BS 349) · airframe 44,668 hrs · 42,329 cycles

AVIONICS BAY DOOR SURROUND FS349 FRAME ATTACHMENT FLANGE AND VERTICAL FLANGE HAS CORROSION BETWEEN S 25L AND S 26R. (C-CHECK) RO: 02/20/2019 REMOVED CORROSION FROM FRAME FS349.00 AT STR 25 LH TO 26 RH IAW SRM.

Part: DOOR FRAME — CORRODED (BS 364) · airframe 44,668 hrs · 42,329 cycles

AVIONICS BAY DOOR SURROUND FS364 FRAME HAS CORROSION ON ATTACHMENT AND VERTICAL FLANGES BETWEEN STR 25R TO APPROXIMATELY 1€? OUTBOARD OF STR 26L. (C-CHECK) RO: 02/20/2019 COMPLIED WITH ALL STEPS OF REO. PERFORMED PRESSURIZATION CHECK IAW AMM. NO DEFECTS NOTED.

Part: RETAINER — CORRODED (RT OVRWNG DOOR) · airframe 44,668 hrs · 42,329 cycles

RH OVERWING EMERGENCY EXIT DOOR HAS CORROSION ON SEAL RETAINER AT LOWER AFT FITTING. (C-CHECK) RO: 02/20/2019 COMPLETED REPAIR OF RH OVERWING EMERGENCY EXIT DOOR IAW REO.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 44,668 hrs · 42,329 cycles

PASSENGER DOOR PIANO HINGE ON FUSELAGE SIDE HAS MIGRATED ROLL PIN. (C-CHECK) RO: 02/20/2019 REMOVED DAMAGE FROM PAX DOOR (FUSELAGE SIDE) AFT LUG LAND IAW REO.

Part: SKIN — DENTED (BS 349) · airframe 44,668 hrs · 42,329 cycles

PASSENGER DOOR CUTOUT €“ DENT IN FUSELAGE SKIN AT FS 349 (LOCATED AT AFT UPPER LATCH PIN FITTING). (C-CHECK) RO: 02/20/2019 REPAIRED PASSENGER DOOR CUTOUT €“ DENT IN FUSELAGE SKIN AT FS 349 IAW REO.

Part: STRUCTURE — CRACKED (BS 193) · airframe 44,668 hrs · 42,329 cycles

RH TRU BAY FLOOR CRACKED FS193 LOCATED BY ADG PUMP. PERFORMED PERMANENT REPAIR TO RH TRU BAY FLOOR AT FS 193.00 IAW REO.

Part: WIRE HARNESS — FAILED (TE FLAPS) · airframe 43,198 hrs · 40,736 cycles

FLAPS FAILED ENROUTE. DECLARED AN EMERGENCY. REMOVED AND REPLACED THE RT BPSU WIRE HARNESS IAW AMM. CYCLED FLAPS NUMEROUS TIMES WITHOUT FAILURE. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 43,194 hrs · 40,731 cycles

FLAPS FAILED MID FLIGHT, ONCE RETRACTED FULLY THE FLAPS FAILED AT ZERO. EMERGENCY DECLARED. RETURNED TO FIELD. RESET IAW FIM AND OPERATED FLAPS FOR MULTIPLE CYCLES. OK FOR SERVICE.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 43,183 hrs · 40,719 cycles

FLAPS FAIL DURING CRUISE. DECLARED EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. RESET THE SYSTEM IAW FIM AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 42,480 hrs · 39,893 cycles

CARGO COMPARTMENT FLOORBEAM CORRODED AT SCREW HOLES. REMOVED AND REPLACED FLOORBEAM IAW REO.

Part: FLOORBEAM — CORRODED (NOT REPORTED) · airframe 42,480 hrs · 39,893 cycles

FLOORBEAM CORRODED AT SCREW HOLES. REMOVED AND REPLACED FLOORBEAM IAW REO.

Part: PANEL — CORRODED (PAX DOOR) · airframe 42,480 hrs · 39,893 cycles

PAX DOOR PANEL CORRODED. REPLACED THE DOOR PANEL.

Part: TIRE — FAILED (NLG) · airframe 37,992 hrs · 35,065 cycles

CREW REPORT NOSE WHEEL SHIMMY DURING TAKEOFF-RETURNED TO THE FIELD. MAINTENANCE CHANGED BOTH NOSE TIRES AND THE AFT SPADE DOOR. R & R IAW AMM.

Part: TRIM SWITCH — FAILED (PITCH) · airframe 37,576 hrs · 34,670 cycles

CREW REPORTS STAB TRIM CAUTION MESSAGE DURING DESCENT. R & R F/O'S PITCH TRIM SWITCH. OPS CHECK GOOD IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,157 hrs · 34,238 cycles

ALL EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED NR 1 AND 2 EMERGENCY BATTERY PACKS IAW AMM.

Part: LOCK — OBSTRUCTED (PAX DOOR) · airframe 37,055 hrs · 34,133 cycles

UNABLE TO OPEN MAIN CABIN DOOR. REMOVED INSULATION FOULING TOP DOOR LOCK PINS AND LUBRICATED DOOR IAW AMM.

Part: PANEL — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

FLOOR SILL PANEL CORRODED AT FS 527.00 TO 529.00 LBL 40. C-CHECK REPAIRED BLEND AREA AT FS 527.00 TO 529.00, LBL 40 IAW REO.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

ATTACH CLIP CRACKED AT FLOOR BEAM AT FS 484, LBL 36. C-CHECK REPLACED CRACKED CLIP ON FS 484, LBL 36 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 540 LBL 36. C-CHECK REPAIRED BLEND AREA AT FS 540.00 LBL 36 IAW REO.

Part: SILL — DAMAGED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS PULLED FREEZE PLUG AT FS 535 LBL42. C-CHECK REPAIRED LT PRESS FLOOR SILL WEB IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 544, LBL 36. C-CHECK REPAIRED BLEND AREA AT FS 544.00 LBL 36 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 532 LBL 42. C-CHECK REPAIRED BLEND AREA AT FS 532.00 LBL 42 IAW REO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR, LOCAL TO FLOOR BEAM AT LBL 3 HAS CORROSION ON STRAP AT FS 559, LBL 36-42. C-CHECK R & R STRAP AT FS 559 LBL 36-42 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 558, LBL 36. C-CHECK REPAIRED BLEND AREA AT FS 558.00 LBL 36 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 538 LBL 42 OVER NUT PLATE. C-CHECK REPAIRED BLEND AREA AT FS 538.00 LBL 42 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 HAS CORROSION AT FS 547 RBL 45 AROUND NUT PLATE. C-CHECK REPAIRED PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 AT FS 547 RBL 45 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM LBL 36 HAS CORROSION ON SKIN DOUBLER AT FS 530 LBL42. C-CHECK REPAIRED BLENDED AREA AT FS 530.00 LBL 42 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM LBL 36 HAS CORROSION ON SKIN DOUBLER AT FS 516 LBL42. C-CHECK REPAIRED BLEND AREAS AT FS 516.00 LBL 42 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM LBL 36 HAS CORROSION ON SKIN DOUBLER AT FS 500 LBL 42. C-CHECK REPAIRED BLEND AREA AT FS 500.00 LBL 42 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM LBL 36 HAS CORROSION ON SKIN DOUBLER AT FS 449 LBL42. C-CHECK REPAIRED LT PRESS FLOOR ANGLE AT FS 449 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 HAS CORROSION AT FS 510 RBL 45 AROUND NUT PLATE. C-CHECK REPAIRED PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 AT FS 510 RBL 45 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 HAS CORROSION ON SKIN DOUBLER AT FS 510 - 512 RBL 42 - 46. C-CHECK REPAIRED PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 ON SKIN DOUBLER AT FS 510 - 512 RBL42 - 46 IAW REO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 HAS CORROSION ON STRAP AT FS 559 RBL 36 - 45. C-CHECK REPLACED STRAP 601R31025-29 IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 HAS CORROSION AT FS 499 RBL 44 AROUND NUT PLATE & FASTENERS. C-CHECK REPAIRED PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 AT FS 499 RBL44 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM LBL 36 HAS CORROSION ON SKIN DOUBLER AT FS 510 LBL42. C-CHECK REPAIRED LT PRESS FLOOR ANGLE AT FS 510 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 520 LBL42 AROUND NUT PLATE. C-CHECK REPAIRED BLENDED AREA AT FS 520.00 LBL 42 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM LBL 36 HAS CORROSION ON SKIN DOUBLER AT FS 471 LBL 42. C-CHECK REPAIRED BLEND AREA AT FS 471.00 LBL 42 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 HAS CORROSION AT FS 557 RBL 45 AROUND NUT PLATE. C-CHECK REPAIRED PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 AT FS 557 RBL 45 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 HAS CORROSION ON SKIN DOUBLER AT FS 472 - 484 RBL 42-44. C-CHECK REPAIRED PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 ON SKIN DOUBLER AT FS 472 - 484 RBL 42 - 44 IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT RBL 36 HAS CORROSION AT FS 476 RBL 43 AROUND NUT PLATE. C-CHECK REPAIRED PRESS FLOOR SILL PANEL IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL 36 HAS CORROSION AT FS 516 LBL 36. C-CHECK REPAIRED BLEND AREA AT FS 516.00 LBL 36 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM AT LBL36 HAS CORROSION AT FS 439 LBL42. C-CHECK REPAIRED BLEND AREA AT FS 439.00 LBL 42 IAW REO.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

PRESS FLOOR LOCAL TO FLOOR BEAM LBL 36 HAS CORROSION ON SKIN DOUBLER AT FS 480 LBL 42. C-CHECK REPAIRED LT PRESS FLOOR SILL ANGLE AT FS 480 IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

MAIN CABIN DOOR SILL UPPER FLANGE IS CORRODED. C-CHECK REPAIRED MAIN CABIN DOOR SILL UPPER FLANGE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

LT SIDE WEB AT FS 409 & FWD OF FS 409 HAS CORROSION ON WEB & AROUND NUT PLATE HOLES. C-CHECK BLENDED CORROSION IAW REO.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

LT FLOOR SUPPORT STRUCTURE IN MAIN CABIN AT FS 310 & FS 349 AT THE CUTOUTS FOR THE AIR STAIR HAND RAILS. AFT STRUCTURE IS CORROSION LEVEL 2 & FWD STRUCTURE IS CORROSION LEVEL 1. C-CHECK BOTH FWD & AFT MAIN CABIN DOOR FLOOR SUPPORT HAND RAIL BRACKETS EXFOLIATED BEYOND REPAIRABLE LIMITS. ORIGINAL THICKNESS .063, REMAINING .000 REPLACED CORRODE BRACKETS WITH NEW BRACKETS PN 601R31527-217 PO T-20412 IAW REO.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

LT SIDE WEB FROM FS 349 TO FS 394 HAS CORROSION ON WEB AROUND SEVEN NUT PLATE HOLES & ON ATTACH BRACKET FOR LIGHTING PANE IN MAIN CABIN. C-CHECK REPAIRED CORROSION BY BLENDING ON LT SIDE WEB FROM APPROXIMATELY FS 355 TO FS 394 AROUND SEVEN EACH NUT PLATE HOLES, WITHIN ALLOWABLE LIMITS, IAW REO.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

FS 409+32 LT SIDE WEB & FS 409+80 HAVE CORROSION AROUND THREE NUT PLATE HOLES. C-CHECK REPAIRED CORROSION BY BLENDING ON LT SIDE WEB BETWEEN FS 409+32 & FS 409+80 AROUND THREE EACH NUTPLATE HOLES IAW REO.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

MAIN CABIN LT SIDE WEB FWD OF FS 310 HAS CORROSION ACROSS THE TOP OF THE WEB. C-CHECK REMOVED CORROSION AT LT WEB FWD OF FS 310.00. ORIGINAL MATERIAL THICKNESS .063 IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

FS 409.0+128 VERTICAL POST AT BL 00 LT FWD RADIUS FASTENER CRACK INDICATION NOTED. C-CHECK REPLACED FS 409.0+ 128 VERTICAL POST AT BL 00 LT IAW REO.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

FS 349 TO FS 364 RT SIDE WEB HAS CORROSION AROUND TWO NUT PLATE HOLES & ON SUB FLOOR ATTACH ANGLE MAIN CABIN. C-CHECK REPAIRED SUB FLOOR BLENDED AREA, ORIGINAL MATERIAL THICKNESS .063 IAW DRAWING 601R31148 DATE 25-10-89, REMOVED .001, & REMAINING .062 WITHIN LIMITS IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

MAIN CABIN DOOR UPPER FLOOR SILL ANGLE FS 332 HAS NUMEROUS AREAS ACROSS THE FACE OF THE ANGLE WITH CORROSION. THIS IS WHERE THE TOP STEP FOR THE AIR STAIR HINGE ATTACHES. C-CHECK REMOVED CORROSION FROM MAIN CABIN DOOR UPPER SILL ANGLE. ORIGINAL MATERIAL THICKNESS .063, REMOVED .001, REMAINING .062 WITHIN LIMITS IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

SERVICE DOOR AFT FRAME FS 349. TOP OF FLOOR BEAM AT SILL HAS HEAVY CORROSION ON TOP OF THE FLOOR BEAM ALSO GOING UNDER FIBERGLASS CAP & ACROSS THE AFT FACE OF THE FLOOR BEAM BETWEEN FRAME ATTACH FITTING & BEAM. C-CHECK REPAIRED SERVICE DOOR AFT FRAME AT FS 349 IAW STS.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

FS 409 RT SIDE WEB HAS CORROSION APPROXIMATELY 6" X 3" AREA, MAIN CABIN. C-CHECK REPAIRED CORROSION BY BLENDING AT FS 409 RT SIDE WEB APPROXIMATELY 6" X 3" AREA IN MAIN CABIN IAW REO.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

CRACK UNDER FLOOR ON ANGLE BRACKET AT FS 280, WL 72.5, LBL 9. C-CHECK REPLACED CRACKED ANGLE BRACKET AT FS 280 WL72.5, LBL9 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

RT SEAT TRACK FROM FS 394 SPLICE TO FS 409 HAS CORROSION ON TOP & INSIDE OF TRACK NUMEROUS AREAS. C-CHECK EVALUATED RT SEAT TRACK FROM FS 394.00 TO 409.00. ORIGINAL MATERIAL THICKNESS .370, REMOVED .035 & REMAINING .335 TOOL TUC4164 CAL DATE 01/2014 IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

LT SEAT TRACK FROM FS 364 TO FS 394 SPLICE HAS CORROSION ON TOP & INSIDE TRACK NUMEROUS AREAS. C-CHECK EVALUATED SEAT TRACK FROM FS 364.00 TO 394.00. ORIGINAL MATERIAL THICKNESS .110, REMOVED .025 & REMAINING .085 TOOL TUC4164 CAL DATE 01/2014 IAW REO.

Part: DOOR — CHAFED (LT MLG) · airframe 35,346 hrs · 32,500 cycles

LT MLG DOOR CHAFED ON THE FWD OTBD EDGE. C-CHECK REPAIRED CHAFING DAMAGE ON LT MLG DOOR, OTBD EDGE, INNER SKIN IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,346 hrs · 32,500 cycles

LT SEAT TRACK FROM FS 409 TO SPLICE AT FS 394 HAS CORROSION ON TOP & INSIDE TRACK. C-CHECK EVALUATED SEAT TRACK FROM FS 394.00 TO 409.00. ORIGINAL MATERIAL THICKNESS .370, REMOVED .030 & REMAINING .340 TOOL TUC4164 CAL DUE DATE 01/2014 IAW SRM.

Part: LATCH — LACK OF LUBE (CABIN DOOR) · airframe 34,530 hrs · 31,706 cycles

MAIN CABIN DOOR CANNOT BE OPENED FROM OUTSIDE. FLT#4446 LUBRICATED MCD LATCH PINS & ROLLERS IAW AMM. OPENED DOOR SEVERAL TIMES FROM OUTSIDE. NO DEFECTS NOTED. OPERATIONS CHECKED GOOD.

Part: SHUTOFF VALVE — FAILED (AC BAY) · airframe 34,380 hrs · 31,560 cycles

OVERBOARD COOL CAUTION AND PASSENGER DOOR OUTER HANDLE. FOLLOWED QRH, RESTOWED DOOR HANDLE BUT ACFT WOULD NOT PRESSURIZE AND CABIN ALTITUDE CONTINUED TO RISE. VERIFIED OPERATION OF PASSENGER DOOR HANDLE AND PULL-IN HANDLE. INSPECTED PASSENGER DOOR OUTER HANDLE PROXIMITY SENSORS AND SWITCHES. NO DAMAGE NOTED AND PROPER GAP VERIFIED. REPLACED OVERBOARD COOL SOV IAW AMM. PN: VP1257C00, SN: 0919, PN OFF: VP1257AA1, SN OFF: 47.

Part: FLAP — DIRTY (WING) · airframe 34,000 hrs · 31,198 cycles

AIRCRAFT ROLLS LEFT WHEN FLAPS 45° IS SELECTED. (FLT 4543) CLEANED FLAP AREA, REMOVED DEBRIS, SANDED DOWN HIGH SPOTS IN PAINT AND REMOVED CHIPPED PAINT IAW AMM. PASSED FUNCTIONAL FLIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,687 hrs · 30,888 cycles

NR 2 OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 4785) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,971 hrs · 30,138 cycles

NR 1 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4597) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,957 hrs · 30,124 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7806) RELAMPED EMERGENCY LIGHT.

Part: SECU — FAILED (SPOILER) · airframe 32,826 hrs · 29,987 cycles

INBOARD AND OUTBOARD GROUND SPOILER FAULT STATUS MESSAGES. FIRST OFFICER EXPERIENCED UNCOMMANDED LEFT WING/ RIGHT WING UP CONTROL INPUT AT THE SAME TIME. (FLT 4832) REPLACED NR 2 SECU IN REFERENCE TO AMM. P/N: 49-164-05 S/N OFF: 01362

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,804 hrs · 29,964 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4543) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,702 hrs · 29,869 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4705) RELAMPED EMERGENCY LIGHT.

Part: HOUSING — DEBONDED (CABIN) · airframe 32,521 hrs · 29,711 cycles

EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR HANGING DOWN. (SERVICE) REPLACED HOUSING ASSEMBLY EXIT SIGN IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,413 hrs · 29,607 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4714) RELAMPED EMERGENCY LIGHT.

Part: WIRE — DISCONNECTED (CABIN) · airframe 32,333 hrs · 29,525 cycles

FORWARD BULKHEAD EMERGENCY LIGHT ON LEFT SIDE IS INOPERATIVE. (FLT 4544) CONNECTED WIRING FOR FORWARD BULKHEAD EMERGENCY LIGHT.

Part: ANCHOR FITTING — DEFECTIVE (CABIN DOOR) · airframe 32,333 hrs · 29,525 cycles

MAIN CABIN DOOR STUCK IN CLOSED POSITION. (FLT 4749) REPLACED PASSENGER DOOR AFT ANCHOR FITTING AND AFT ANCHOR FITTING ADJUSTMENT BOLT IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,307 hrs · 29,498 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4571) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,177 hrs · 29,371 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. (FLT 4821) RELAMPED EMERGENCY LIGHT.

Part: SERVO — FAILED (AUTOPILOT SYS) · airframe 32,141 hrs · 29,327 cycles

IMMEDIATELY AFTER AUTO PILOT DISCONNECT, THE ELEVATOR CONTROL STUCK, AS IF THE AUTO PILOT WAS STILL ENGAGED. IT THEN RELEASED AFTER ABOUT 1 OR 2 SECONDS. (FLT 4711) REPLACED ELEVATOR SERVO ACTUATOR IN REFERENCE WITH CRJ200 AMM. P/N 622-5027-101, S/N OFF 1CJ6C

Part: SELECTOR VALVE — FAILED (NLG) · airframe 31,956 hrs · 29,135 cycles

ON TAKEOFF RECEIVED A GEAR DISAGREE AND A NOSE DOOR OPEN MESSAGE. (FLT 4614) REPLACED NLG SELECTOR VALVE AND SENSOR BRACKET IN REFERENCE TO AMM. P/N 750006000 S/N OFF 2083.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,295 hrs · 29,486 cycles

RIGHT FLOOR TRACKS CORRODED BETWEEN FS 559+14.00 THRU FS 559+80.00. (C-CHECK) REPLACED FLOOR SEAT TRACKS FROM FS 559+14 THRU FS 559+80.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 32,295 hrs · 29,486 cycles

RIGHT FLOOR SEAT TRACK BETWEEN FS 559+80.00 AND 559+96.00 CORRODED. (C-CHECK) REPLACED RIGHT FLOOR SEAT TRACK BETWEEN FS 559 + 80.00 AND FS 559 + 96.00 IAW CRJ 200 AMM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 32,295 hrs · 29,486 cycles

DAMAGED FS 621.00 FRAME. (C-CHECK) REPAIRED IAW REO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,295 hrs · 29,486 cycles

LOWER 640 FRAME SECTION HAS A CRACK BETWEEN STRINGERS 24L AND 25L. (C-CHECK) REPLACED LOWER FRAME SECTION AT FS 640 IAW CRJ 200 SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,911 hrs · 29,096 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4769) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,737 hrs · 28,926 cycles

THE 2ND FROM BACK OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4471) RELAMPED EMERGENCY LIGHT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 31,737 hrs · 28,926 cycles

LEFT WINDSHIELD ARCING & CRACKING DURING CRUISE FLIGHT. (FLT 4457) REPLACED LEFT WINDSHIELD PER AMM. P/N NP-139321-13, S/N OFF 96131H7501

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,653 hrs · 28,841 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4685) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,516 hrs · 28,705 cycles

SECOND TO AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4552) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,481 hrs · 28,669 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4787) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,360 hrs · 28,551 cycles

NR 5 EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4451) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,300 hrs · 28,495 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4521) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 31,241 hrs · 28,435 cycles

LOWER EMERGENCY LIGHT AT ROW 8 IS OUT. (FLT 4812) REPAIRED BROKEN WIRE AT ROW 8 LOWER EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,241 hrs · 28,435 cycles

MIDDLE FLOOR EMERGENCY LIGHT STRIP IS OUT. (FLT 4812) REPLACED MIDDLE POWER LIGHT STRIP AT ROW 8.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,204 hrs · 28,401 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4642) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DIRTY (CABIN) · airframe 31,204 hrs · 28,401 cycles

LEFT SIDE EMERGENCY EXIT SIGN IS OUT. (FLT 4642) CLEANED LEFT SIDE EMERGENCY EXIT SIGN CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,156 hrs · 28,360 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4732) RELAMPED EMERGENCY LIGHT.

Part: LATCH — LACK OF LUBE (CABIN DOOR) · airframe 30,958 hrs · 28,187 cycles

MCD DIFFICULT TO OPEN. (FLT 4704) LUBED DOOR LATCH AND PINS.

Part: WIRE — BROKEN (CABIN) · airframe 30,523 hrs · 27,803 cycles

EMERGENCY EXIT SIGN AT MAIN CABIN DOOR IS OUT. (FLT 4582) REPAIRED BROKEN WIRE AT PAX DOOR EMERGENCY EXIT SIGN.

Part: WIRE — DISCONNECTED (CABIN) · airframe 30,523 hrs · 27,803 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN AT PAX DOOR IS OUT. (FLT 4582) RECONNECTED FLOOR EMERGENCY LIGHT WIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,991 hrs · 27,378 cycles

THE 2ND CEILING EMERGENCY LIGHT IS OUT. (FLT 7768) RELAMPED EMERGENCY LIGHT.

Part: CONTACTOR — FAILED (ELECTRICAL SYS) · airframe 29,187 hrs · 26,682 cycles

TURNING ON/OFF GENERATOR NR 1 CAUSES FLIGHT MANAGEMENT SYSTEM, LEFT PRIMARY FLIGHT DISPLAY AND MULTI-FUNCTIONAL DISPLAY SCREENS GO BLANK, YAW DAMPENER 2 AND MACH TRIM DISENGAGE. (FLT 4830) REPLACED CONTACTOR GENERATOR TRANSFER CONTACTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,063 hrs · 26,581 cycles

EMERGENCY EXIT WALL LIGHTS AT CABIN DOOR OR GALLEY DOOR ARE NOT ILLUMINATING. (FLT 4535) RELAMPED EMERGENCY LIGHTS.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 29,003 hrs · 26,535 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4571) CLEANED AND LUBED DOOR ROLLERS.

Part: PIVOT — DAMAGED (CABIN DOOR) · airframe 28,701 hrs · 26,274 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4595) INSTALLED FORWARD PIVOT FOR GAS STRUT CABLES AND ADJUSTED.

Part: UNKNOWN — OUT OF ADJUST (CABIN DOOR) · airframe 28,596 hrs · 26,190 cycles

MAIN CABIN DOOR WILL NOT FULLY OPEN. (FLT 4571) ADJUSTED DOOR.

Part: FASTENER — SHEARED (NR 3 PCU) · airframe 28,353 hrs · 25,983 cycles

CONTROL COLUMN STIFF WITH PUMP 3A ON. (FLT 4794) REPLACED SHEARED HI-LOK ON NR 3 PCU ROD END ATTACH POINT PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,299 hrs · 25,945 cycles

NR 2 EMERGENCY CEILING LIGHT INOP. (FLT 4556) RELAMPED EMERGENCY LIGHT.

Part: SILL — CORRODED (FUSELAGE) · airframe 28,540 hrs · 26,143 cycles

LEFT AND RIGHT PRESSURE FLOOR SILLS CORRODED. (C CHECK) DAMAGE WITHIN LIMITS FOR BLEND OUT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,477 hrs · 26,087 cycles

FS 280 LBL 13 VERTICAL ANGLE CRACKED FORWARD OF FRAME. (C CHECK) REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,477 hrs · 26,087 cycles

FS 202 BULKHEAD CRACKED AT PARKING BRAKE CABLE RUN. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,973 hrs · 25,683 cycles

MOST AFT EMERGENCY OVERHEAD LIGHT INOP. (FLT 4545) RELAMPED EMERGENCY LIGHT.

Part: AMPLIFIER — MALFUNCTIONED (LT ENGINE) · airframe 27,907 hrs · 25,632 cycles

WHILE SETTING TAKEOFF POWER THE LEFT ENGINE N1 ROLLED BACK 10-15 PERCENT. (FLT 4620) REPLACED LEFT ENGINE CONTROL AMPLIFIER P/N 5071T98P03, S/N ON LMDK2797, S/N OFF LMDK2532.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,747 hrs · 25,501 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 4697) RELAMPED EMERGENCY LIGHT.

Part: MANIFOLD — LEAKING (APU) · airframe 26,878 hrs · 24,798 cycles

FUEL SMELL AT ALTITUDE AFTER APU USE. (FLT 4430) REPLACED APU FUEL MANIFOLD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 26,560 hrs · 24,548 cycles

FLOOR LEVEL EMERGENCY LIGHTING INOP AFT OF ROW 8. (FLT 4473) RESECURED CONNECTION.

Part: LIGHT — BROKEN (CABIN) · airframe 26,445 hrs · 24,459 cycles

EMERGENCY FLOOR FLOODLIGHT ON WARDROBE UNIT BROKEN. (SVC CK) REPLACED LIGHT ASSEMBLY.

Part: ANCHOR FITTING — OUT OF ADJUST (CARGO DOOR) · airframe 26,297 hrs · 24,344 cycles

FLT 4480 - CABIN DOOR HARD TO OPEN FROM OUTSIDE. ADJUSTED FORWARD ANCHOR FITTING.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,533 hrs · 23,743 cycles

FLT 4873 - RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED.

Part: GROUND WIRE — OUT OF POSITION (CABIN) · airframe 25,447 hrs · 23,671 cycles

FLT 4844 - EMERGENCY OVERHEAD CABIN LIGHT INOP. REPOSITIONED GROUND WIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,019 hrs · 23,339 cycles

THIRD AFT EMERGENCY LIGHT IN MAIN CABIN INOP (FLT 3802). RELAMPED EMERGENCY LIGHT.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 24,362 hrs · 22,817 cycles

PAX DOOR IS HARD TO OPEN FROM OUTSIDE. (FLIGHT NR 4091) ADJUSTED INNER HANDLE RETENSION MECHANISM IAW AMM 52-11-00. PAX DOOR OPS CHECK GOOD AT THIS TIME.

Part: STRINGER CLIP — CRACKED (BS 625 S13) · airframe 24,975 hrs · 23,303 cycles

STRINGER CLIP AT STA 625 BETWEEN STRINGER 14 CRACKED. C-CHECK, REPLACED CLIP.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,975 hrs · 23,303 cycles

FS 280 FLOORBEAM CORRODED ON TOP FROM LBL 2.0 TO RBL 2.0. C-CHECK, REPAIRED PER SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,975 hrs · 23,303 cycles

FS 280 FLOORBEAM LOWER FLANGE IS CRACKED AT RBL12. C-CHECK, REPAIRED PER REO.

Part: PULLEY — CRACKED (BS 559) · airframe 24,855 hrs · 23,210 cycles

C-CHECK, STA 559 RT SIDE AT PULLEY QUADRANT CRACKED OFF LOWER MOUND BOLT. REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,975 hrs · 23,303 cycles

ONE AFT PRESSURE BULKHEAD ISOLATOR CRACKED. C-CHECK, REPLACED ISOLATOR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,975 hrs · 23,303 cycles

FS 280 RBL9 INBOARD AND OUTBOARD CLIPS CRACKED. C-CHECK, REPLACED CLIPS.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 24,975 hrs · 23,303 cycles

PASSENGER DOOR AFT ANCHOR FITTING CRACKED. C-CHECK, REPLACED FITTING.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,673 hrs · 22,295 cycles

FLT 3905 - RIGHT SIDE EXIT ROW EMERGENCY EXIT LIGHT IS INOP. REPLACED RIGHT EMERGENCY LIGHT SIDEWALL INVERTER. OPS CHECK GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 23,363 hrs · 22,059 cycles

FLT 3776 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. REPLACED LEAKING FLEX LINE TO ACTUATOR. NO LEAKS NOTED.

Part: TIRE — FAILED (NR 4 MLG) · airframe 22,985 hrs · 21,769 cycles

NR 4 MAIN TIRE BLEW OUT ON LANDING, DAMAGING THE RIGHT INBOARD FLAP. REPLACED FLAP ASSEMBLY IAW CRJ 200 AMM 27-54-01, P/N: 601R14002-2, S/N OFF: SB/RJ/784.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,789 hrs · 21,625 cycles

FLT 3882 - FOUND SEVERAL FLOOR EMERGENCY LIGHTS DON'T WORK. REPLACED TRACK LIGHT CONNECTOR.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 22,693 hrs · 21,559 cycles

FLT 3797 - O2 MASKS AT SEATS 8A AND B DROPPED. RESTOWED OXYGEN MASKS AT SEAT 8A AND B AS NEEDED.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,453 hrs · 21,377 cycles

FLOOR EMERGENCY LIGHTING IS PARTIALLY INOP. REPLACED NR 3 ELBP WITH A SERVICEABLE UNIT IAW 33-51-17. OPS CHECK GOOD.