N702BR

Part: NONE — SMOKE · airframe 39,667 hrs · 35,691 cycles

SMOKE OFF OFF LEFT WINDSHIELD WAS FOLLOWED BY WINDSHIELD CRACKING. LEFT SIDE. (FLIGHT 4255 - FILED CLOSED) PLEASE REFERENCE AML 776009 PLEASE REFERENCE AML 776106. REMOVED AND REPLACED LEFT WINDSHIELD PER AMM 56-11-01 AND COMPLIED WITH TASK CARD 56-220-1000-SKY. WINDSHIELD OPERATIONAL CHECK GOOD.

Part: NONE — CRACKED · airframe 39,560 hrs · 35,556 cycles

DURING THE INSPECTION OF THE PASSENGER DOOR FITTINGS ON THE FUSELAGE, FOUND THE PASSENGER DOOR STOP BRACKET ON THE FORWARD SIDE OF THE PASSENGER DOOR CUTOUT IN THE FUSELAGE TO BE CRACKED ON THE LOWER SIDE OF THE BRACKET. (FILED CLOSED) REMOVED AND REPLACED THE PASSENGER DOOR FWD STOP BRACKET ON THE FUSELAGE IN REFERENCE TO SRM 51-42-21.

Part: FLAP SYSTEM — FAILED · airframe 39,085 hrs · 34,906 cycles

FLAP FAIL CAUTION APPEARED DURING CLIMB OUT 17000', FLAP FAIL AT 0 DEGREES RAN QRH FSI LESS THEN 400 FPM TOUCH DOWN ARE SPEED LESS THEN MAX TIRE SPEED (FLIGHT 4291) COMPLIED WITH AD 2009-06-12/09 FOR TROUBLESHOOTING. FLIGHT LEG 1589 LRU PROBABLES ARE 1. FECU/BPSU MISRIGG CODES 5 1B 5 2B . ALSO COMPLIED WITH CRJ200 FIM 27-50-00 FIG 111 BOX 1 . FOUND FECU POT 5 AND 6 AND 8 OUT OF RIG. RIGGED PER CRJ200 AMM 27-51-10 AND PREFORMED OPS CHECK.. OPS CHECK GOOD

Part: ENGINE — FLUCTUATES (ENGINE) · airframe 38,733 hrs · 34,412 cycles

LARGE N1 FLUCTUATIONS AT HIGH POWER SETTINGS AFTER TAKEOFF. ERRATIC FUEL FLOW, POWER FLUCTUATIONS COULD BE FELT. RETURNED TO FIELD. MEL 76-11-1 CAT: C DUE: 14JAN2021. LARGE N1 FLUCTUATIONS AT HIGH POWER SETTINGS AFTER TAKEOFF. ERRATIC FUEL FLOW, POWER FLUCTUATIONS COULD BE FELT. RETURNED TO FIELD. BOTH ENGINE SPEED CONTROL SYSTEMS PLACED ON DMI, PER MEL BY AUTHORITY OF MX CONTROL. BOTH SWITCHES SET TO OFF POSITION AND PLACARD INSTALLED. PERFORMED OPERATIONAL RUN OF BOTH ENGINES, IN REF TO CRJ 200 AMM. COULD ONLY DUPLICATE WITH SPEED SWITCHES ACTIVATED.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,278 hrs · 33,784 cycles

SMALL SEAT TRACK SEGMENT LOCATED BETWEEN FS559+80 TO FS559+96 AT RBL9 IS CORRODED. REMOVED & REPLACED SMALL SEAT TRACK LOCATED FS559+80 TO FS559+96 WITH NEW STOCK IAW REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,278 hrs · 33,784 cycles

2 EACH CABIN SEAT TRACK SEGMENTS LOCATED AT RBL9 AND LBL9 FROM FS559 TO FS559+80 AR CORRODED. (C-CHECK) RO 7/31/2020 REMOVED/FABRICATED AND INSTALLED NEW SEAT TRACK FABRICATED FROM 20276-288-0-0A IAW REO

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 38,278 hrs · 33,784 cycles

RIGHT FLOOR SILL IN CARGO BAY HAS 4 AREAS OF CORROSION AROUND NUT PLATES, LOCATED FROM FS559+112 TO FS621.00. REMOVED AND REPLACED 4 NUTPLATES AT RT FLOOR SILL LOCATED BETWEEN FS559+112 TO FS621.00 IAW SRM. REMOVED PEALED PAINT NO CORROSION FOUND AT THIS TIME IAW SRM. RESTORED FINISH IAW SRM

Part: SEAT TRACK — CORRODED (BS 574-559) · airframe 38,278 hrs · 33,784 cycles

3 EACH SEAT TRACK SEGMENTS ARE CORRODED IN CARGO BAY AREA, LOCATED BETWEEN FS574.00 TO FS559+80 AT RBL9 AND LBL9 AS MARKED. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED 3 SEAT TRACK IN CARGO BAY AREA BETWEEN F.S.574.00 TO F.S. 599+80RBL9 AND LBL9 IAW CRJ200 AMM

Part: SEAT TRACK — CORRODED (BS 559) · airframe 38,278 hrs · 33,784 cycles

SEAT TRACK SEGMENT LOCATED FROM FS 559+64 TO 559+80 AT RLB27 IS CORRODED. UPON FURTHER INVESTIGATION FOUND SEAT TRACK SEGMENT TO BE LOCATED AT F.S. 559+48 TO F.S. 559+64 RBL 27. REMOVED CORRODED SEAT TRACK SEGMENT IAW AMM. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE SEAT TRACK SEGMENT IAW SRM AND AMM.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 38,278 hrs · 33,784 cycles

FLOORBEAM AT RBL9 HAS A SMALL AREA OF CORROSION AROUND FLOORBOARD NUT PLATE AT FS 589.00. REMOVED AND REPLACED RBL 9 FLOORBEAM IAW SRM, AND GREO.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 38,278 hrs · 33,784 cycles

PASSENGER FLOOR SEAT TRACK BETWEEN FS 409+128 AND FS 559 AT LBL9 WAS CORRODED AT SEVERAL LOCATIONS. REMOVED CORRODED FLOOR SEAT TRACK BETWEEN F.S. 409+128 AND F.S. 559 AT LBL 9 IAW AMM. INSTALLED NEWLY FABRICATED SEAT TRACK IAW AMM.

Part: PANEL — CORRODED (BS 409-559) · airframe 38,278 hrs · 33,784 cycles

LH PRESSURE FLOOR SILL PANEL CORRODED AT 7EA. LOCATIONS BETWEEN FS 409+128 AND FS 559. REPAIRED LH FLOOR SILL PANEL AT 7EACH LOCATIONS IAW REO.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 38,278 hrs · 33,784 cycles

PASSENGER FLOOR SEAT TRACK BETWEEN FS 364 AND FS 409 AT RBL 9 IS CORRODED SEVERAL LOCATIONS. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SERVICEBLE PASSENGER SEAT TRACK BETWEEN F.S. 364 AND F.S. 409 AT RBL 9 IAW AMM

Part: SEAT TRACK — CORRODED (BS 409) · airframe 38,278 hrs · 33,784 cycles

PASSENGER FLOOR SEAT TRACK BETWEEN FS 409 AND FS 409+128 AT LBL 9 IS CORRODED AT SEVERAL LOCATIONS. REMOVED AND REPLACED PASSENGER FLOOR SEAT TRACK BETWEEN F.S. 409 AND F.S. 409+128 AT LBL9 IAW AMM.

Part: FASTENER — CORRODED (BS 349 FLOORBEAM) · airframe 38,278 hrs · 33,784 cycles

FS 349 FLOORBEAM DOUBLER BETWEEN LBL 27 AND LBL 42 HAD CORRODED FASTENERS. REPLACED THE FASTENERS IAW SRM.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 38,278 hrs · 33,784 cycles

PASSENGER FLOOR SEAT TRACK BETWEEN FS 409 AND FS 409+128 AT RBL 9 IS CORRODED SEVERAL LOCATIONS. REMOVED CORRODED FLOOR SEAT TRACK BETWEEN F.S.409 AND F.S. 409+128 AT RBL 9 IAW CRJ 200 AMM. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK P/N 601R31032-21 IAW SRM AND CRJ 200 AMM

Part: ATTACH BRACKET — CRACKED (BS 621 BULKHEAD) · airframe 38,278 hrs · 33,784 cycles

BS 621.00 REAR PRESSURE BULKHEAD, L/H UPPER INTERCOSTAL ANGLE BETWEEN F.S. 621.00 AND F.S. 625.00 IS CRACKED. (C-CHECK) RO 7/31/2020 REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ-200 SRM.

Part: PANEL — CORRODED (BS 409-559) · airframe 38,278 hrs · 33,784 cycles

RH PRESSURE FLOOR SILL PANEL IS CORRODED AT 6EA. LOCATIONS BETWEEN FS 409+128 AND FS 559. REPAIRED RH PRESSURE FLOOR SILL PANEL AT 6EACH LOCATIONS IAW REO.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 38,278 hrs · 33,784 cycles

PASSENGER FLOOR SEAT TRACK BETWEEN FS 364 AND FS 409 AT LBL9 IS CORRODED SEVERAL LOCATIONS. (C-CHECK) RO 7/31/2020 REMOVED FLOOR SEAT TRACK BETWEEN F.S. 364 AND F.S. 409 AT LBL9 IAW CRJ200 AMM. FABRAICATED WITH ALT MATERIAL AND INSTALLED IAW BOMBARDIER REO.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 38,278 hrs · 33,784 cycles

PASSENGER FLOOR SEAT TRACK BETWEEN FS 409+128 AND FS 559 AT RBL9 IS CORRODED SEVERAL LOCATIONS. REMOVED CORRODED FLOOR SEAT TRACK BETWEEN F.S. 409+128 AND F.S. 559 AT RBL 9 IAW AMM. INSTALLED NEWLY FABRICATED SEAT TRACK IAW AMM.

Part: DOUBLER — CORRODED (BS 319-333) · airframe 38,278 hrs · 33,784 cycles

PAX DOOR FLOOR SILL CANNON PLUG DOUBLERS 2EA. ARE BOTH CORRODED BETWEEN FS319 AND FS333. REMOVED AND REPLACED THE DOUBLERS IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 38,278 hrs · 33,784 cycles

RH FLOOR SILL IS CORRODED JUST FWD OF SERVICE DOOR CUTOUT AT FS 319.70. REMOVED AND REPLACED R/H FLOOR SILL P/N 601R-31148-79 IAW SRM.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 38,278 hrs · 33,784 cycles

PAX DOOR FWD ANCHOR FITTING SERRATED PLATE AT FS 310 IS CORRODED. REMOVED AND REPLACED PAX DOOR FWD ANCHOR FITTING AND GUSSET IAW AMM. ADJUSTMENT CHECK GOOD

Part: ANGLE — CORRODED · airframe 38,278 hrs · 33,784 cycles

PAX DOOR FLOOR SILL LWR ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR SILL LOWER ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED · airframe 38,278 hrs · 33,784 cycles

PAX DOOR FLOOR SILL UPPER ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR SILL UPPER ANGLE IAW CRJ 200 SRM.

Part: GUSSET — CORRODED (BS 349) · airframe 38,278 hrs · 33,784 cycles

SERVICE DOOR SURROUND LWR FRAME GUSSET AT FS 349 IS CORRODED. REMOVED AND REPLACED CORRODED GUSSET AT BS 349 SERVICE DOOR WITH NEW SERVICEABLE GUSSET IAW SRM

Part: NOT REPORTED — DAMAGED (NOT REPORTED) · airframe 38,278 hrs · 33,784 cycles

WHILE PERFORMING SB601R-57-046, FOUND 9TH HOLE FROM FRONT ON R/H SIDE TO BE OVERSIZED. REPAIRED 9TH HOLE FROM FRONT ON RH SIDE IAW REO.

Part: GUSSET — CORRODED (BS 310) · airframe 38,278 hrs · 33,784 cycles

PAX DOOR LWR SURROUND, FWD UPPER GUSSET AT FS 310 IS CORRODED. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED PAX DOOR LWR SURROUND FWD UPPER GUSSET AT F.S.310 IAW CRJ 200 SRM.

Part: INTERCOSTAL — CORRODED (BS 295-310) · airframe 38,278 hrs · 33,784 cycles

PAX DOOR SURROUND INTERCOSTAL BETWEEN FS 295 AND FS 310 STGR 14L IS CORRODED. (C-CHECK) RO 7/31/2020 REPLACED PAX DOOR SURROUND INTERCOASTAL BEWEEN FS 295 ABD FS 310 STR 14L IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE.

Part: TRUNNION — CRACKED (LT MLG) · airframe 38,278 hrs · 33,784 cycles

LH MLG TRUNNION HAS AN INDICATION IN EACH FASTENER HOLE (2ND HOLE(1" LONG BY 55%FSH), (3RD HOLE (.1" LONG BY 15% FSH), (MOST AFT INBD HOLE (.15" BY 90% FSH). FAILED NDT INSPECTION. (C-CHECK) RO 7/31/2020 REPAIRED LH MLG TRUNNION 2ND AND 3RD HOLE IAW REO. TASK CARD COMPLETED AND ATTACHED. M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE REQUIRED

Part: TRUNNION — CRACKED (RT MLG) · airframe 38,278 hrs · 33,784 cycles

RH MLG TRUNNION FASTENER HOLE HAS AN INDICATION .1" LONG BY 55% FSH IN 7TH FASTENER HOLE AFT(MARKED WITH SHARPIE). FAILED NDT INSPECTION. REPAIRED MLG TRUNNION FASTENER HOLE 7TH FASTENER HOLE AFT IAW REO.

Part: BULKHEAD — CHAFED (BS 621) · airframe 38,278 hrs · 33,784 cycles

FS621 BULKHEAD FORWARD SIDE REPAIR DOUBLERS CHAFED FROM CONTACT WITH SCREWS AT WL103 AT RBL36, RBL27, RBL18, LBL7, LBL9, LBL18, LBL27 WITH DEEPEST CHAFE AT .005" (C-CHECK) RO 7/31/2020 REPAIRED F.S 621 BULKHEAD FORWARD SIDE REPAIR DOUBLER CHAFES IAW REO. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 38,278 hrs · 33,784 cycles

RIGHT SIDE SEAT RAIL BETWEEN F.S. 364.00 AND F.S. 409.00+16 IS CORRODED IN SEVERAL PLACES. (C-CHECK) RO 7/31/2020 REMOVED CORRODED R/H SIDE SEAT RAIL BETWEEN F.S. 364.00 AND F.S. 409.00+16 IAW CRJ 200 AMM. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE SIDE SEAT RAIL IAW CRJ 200 SRM AND CRJ 200 AMM

Part: SEAT TRACK — CORRODED (BS 499-559) · airframe 38,278 hrs · 33,784 cycles

RIGHT SIDE SEAT RAILS BETWEEN F.S. 499.00 AND F.S. 559.00+80 IS CORRODED IN SEVERAL AREAS. REMOVED AND INSTALLED SERVICABLE SEAT TRACK BETWEEN 499.00 AND 559.00+80 IAW AMM, REFERENCE CAMP 21201733 FOR PART FABRICATION

Part: SEAT TRACK — CORRODED (BS 409) · airframe 38,278 hrs · 33,784 cycles

LEFT SIDE SEAT RAIL BETWEEN BS 409+16 AND 409+112 WAS CORRODED AT SEVERAL PLACES. REPLACED THE SEAT TRACK IAW REO.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 38,278 hrs · 33,784 cycles

RIGHT SIDE SEAT RAIL BETWEEN BS 409+112 AND 449.85 WAS CORRODED AT SEVERAL PLACES. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 38,278 hrs · 33,784 cycles

LEFT SIDE SEAT RAIL BETWEEN F.S. 544.00 AND F.S. 559.00+80 IS CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED LEFT SIDE SEAT RAIL IAW AMM.

Part: SEAT TRACK — CORRODED (BS 409-499) · airframe 38,278 hrs · 33,784 cycles

LEFT SIDE SEAT RAILS BETWEEN BS 409.00+112 AND BS 499.00 ARE CORRODED IN SEVERAL PLACES. REPLACED THE SIDEWALL SEAT TRACK IAW AMM.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 38,278 hrs · 33,784 cycles

FS 280 STGR 3L ATTACH ANGLE IS CRACKED APPROX. .500" IN LENGTH. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED ATTACH ANGLE AT FS 280 STRG 3L IAW CRJ-200 SRM

Part: ANGLE — CRACKED (BS 409) · airframe 38,278 hrs · 33,784 cycles

FS409+128 RH & LH SIDE OF BL0 VERTICAL POST HAS ONE EACH INDICATION .15" LONG BY 80% FSH IN THE UPPER AFTER RADIUS @ WL69. FAILED NDT INSPECTION. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED FS 409+128 VERTICAL POST AT RH AND LH OF BL0 IAWE CRJ 200 SRM AND REO AND SKYWEST TASK CARD. M-337 ATTACHED. NO WEIGHT CHANGE REQUIRED

Part: POST — CRACKED (BS 409) · airframe 38,278 hrs · 33,784 cycles

FS409+128 RBL18 VERTICAL POST HAS AN INDICATION .13" LONG BY 75% FSH IN THE UPPER AFT RADIUS @ WL69. FAILED NDT INSPECTION. REPAIRED AREA IAW SRM AND REO.

Part: TRACK — GOUGED (CARGO DOOR) · airframe 38,278 hrs · 33,784 cycles

CARGO DOOR FWD TRACK AT FS 574 IS GOUGED 1.5" IN LENGTH, .156" IN WIDTH, AND APPROX. .075" IN DEPTH. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED CARGO DOOR FWD TRACK IAW CRJ 200 SRM NO DEFECTS NOTED OPS TEST GOOD

Part: CHANNEL — CRACKED (DOOR FRAME) · airframe 38,278 hrs · 33,784 cycles

CARGO DOOR SURROUND STRUCTURE, FWD/LWR C-CHANNEL IS CRACKED 1" IN LENGTH. REMOVED DAMAGED CARGO DOOR SURROUND STRUCTURE FWD/LWR C-CHANNEL, LOCATED AND DRILLED NEW C-CHANNEL, AND INSTALLED IAW CRJ200 SRM

Part: CHANNEL — CHAFED (BS 574) · airframe 38,278 hrs · 33,784 cycles

CARGO DOOR SURROUND STRUCTURE FWD UPPER WEB CHANNEL AT FS 574 IS CHAFED APPROX. .750" IN LENGTH, .062" IN WIDTH, AND .030" IN DEPTH. (C-CHECK) RO 7/31/2020 REMOVED AND REPLACED CARGO DOOR SURROUND STRUCTURE UPPER WEB CHANNEL IAW SRM.

Part: BOLT — CORRODED (LT WING) · airframe 38,278 hrs · 33,784 cycles

LEFT INBD GROUND SPOILER ACTUATOR HARDWARE IS CORRODED. REPLACED HARDWARE ON L/H INBD GRND SPOILER IAW AMM. BLEED LEAK AND OPS CHECKED GOOD.

Part: NUT — CORRODED (RT WING) · airframe 38,278 hrs · 33,784 cycles

RIGHT FLIGHT SPOILER INBD AND OTBD HINGE HARDWARE WAS CORRODED. REPLACED HARDWARE IAW AMM. OPS CHECKED GOOD.

Part: NUT — CORRODED (RT WING TE FLAP) · airframe 38,278 hrs · 33,784 cycles

RIGHT OTBD FLAP CENTER HINGE BOX FWD NUT WAS CORRODED. REMOVED AND INSTALLED A NEW NUT IAW AMM.

Part: LINK — CORRODED (RT WING) · airframe 38,278 hrs · 33,784 cycles

RIGHT OTBD GROUND SPOILER ACTUATOR HARDWARE WAS CORRODED. REMOVED AND REPLACED THE CORRODED HARDWARE ON THE RT OTBD GROUND SPOILER ACTUATOR WITH SERVICABLE HARDWARE IAW AMM. PERFORMED THE BLEEDING OF HYDRAULIC SYSTEM NR 1 IAW AMM. NO DEFECTS NOTED. OPS TESTED GOOD OF THE GROUND SPOILERS IAW AMM.

Part: NUT — CORRODED (LT WING) · airframe 38,278 hrs · 33,784 cycles

LEFT SPOILERON INBD AND OTBD HINGE HARDWARE IS CORRODED. FOUND LT SPOILERON INBD AND OTBD NUTS CORRODED. REMOVED AND REPLACED THE NUTS IAW AMM.

Part: BOLT — CORRODED (RT WING) · airframe 38,278 hrs · 33,784 cycles

RIGHT SPOILERON INBD HINGE HARDWARE WAS CORRODED. REPLACED THE HARDWARE IAW AMM. OPS CHECKED GOOD.

Part: BOLT — CORRODED (LT WING) · airframe 38,278 hrs · 33,784 cycles

LEFT SPOILERON INBD AND OTBD ACTUATOR HARDWARE WAS CORRODED. REPLACED CORRODED NUTS AND MINOR HARDWARE WITH NEW IAW AMM. NO DEFECTS NOTED.

Part: BOLT — CORRODED (RT WING) · airframe 38,278 hrs · 33,784 cycles

RIGHT SPOILERON INBD AND OTBD ACTUATOR HARDWARE WAS CORRODED. REPLACED THE RT SPOILERON INBD AND OTBD ACTUATOR HARDWARE IAW AMM. OPS CHECKED GOOD.

Part: NUT — CORRODED (RT WING) · airframe 38,278 hrs · 33,784 cycles

RIGHT FLIGHT SPOILER INBD AND OTBD ACTUATOR HARDWARE WAS CORRODED. REPLACED THE RT FLIGHT SPOILER INBD AND OTBD ACTUATOR HARDWARE IAW AMM. OPS CHECKED GOOD.

Part: BOLT — CORRODED (LT WING) · airframe 38,278 hrs · 33,784 cycles

LEFT FLIGHT SPOILER INBD AND OTBD HINGE HARDWARE WAS CORRODED. REPLACED AND REPLACED THE HARDWARE IAW AMM. OPS CHECKED GOOD.

Part: BOLT — CORRODED (LT WING) · airframe 38,278 hrs · 33,784 cycles

LEFT INBD FLAP INBD FWD FLAP FITTING TWO FWD HARDWARE WAS CORRODED. REMOVED HARDWARE IAW AMM AND INSTALLED NEW HARDWARE IAW AMM.

Part: ATTACH FITTING — GOUGED (RT MLG) · airframe 38,278 hrs · 33,784 cycles

RH MLG SIDE BRACE ATTACH FITTING IS GOUGED. (C-CHECK) RO 7/31/2020 REPAIRED RH MLG SIDE BRACE ATTACH FITTING IAW REO AND SKY CARD. M-337 ATTACHED. NO WEIGHT CHANGE.

Part: BOLT — CORRODED (SPOILER ACTUATOR) · airframe 38,278 hrs · 33,784 cycles

L/H FLIGHT SPOILER I/B AND O/B ACTUATOR HARDWARE IS CORRODED. REPLACED L/H FLGHT SPOILER INBD AND OTBD ACTUATOR HARDWARE IAW AMM. OPS CHECKED GOOD.

Part: ENGINE — POWER LOSS (LEFT) · airframe 37,963 hrs · 33,404 cycles

PASSING THROUGH 17,500 WE RECEIVED A L ENG OIL PRESS WARNING. AROUND 18,000 FEET WE RECEIVED N2 AND N1 VIB AND A LOUD EXTERIOR NOISE HEARD FROM COCKPIT. THE ENGINE QUICKLY DETERIORATED AND WE RAN THE L ENG FIRE OR SEVERE DAMAGE IN FLIGHT QRC AND SHUT DOWN THE LEFT ENGINE. WE COULD SMELL A BURNING FUMES SMELL AS WELL ONCE THE ENGINE VIB INDICATIONS WERE PRESENT. WE THEN RAN THE APPLICABLE QRH PROCEDURES AND PROCEEDED TO ATL AND COMPLETED A SINGLE ENGINE APPROACH TO LAND. FLIGHT 3518 FILED CLOSED PLEASE REFERENCE AML 376649 PLEASE REFERENCE AML 376684. RECONNECTED AND SECURED C-SUMP OIL-SCAVENGE HOSE IN REF TO CRJ 200 AMM. DOWNLOADED FDR IN REF TO CRJ 200 AMM. UPLOADED TO SKYWEST SERVER.

Part: STRUT — LOW (NLG) · airframe 37,392 hrs · 32,788 cycles

AFTER TAKEOFF WHEN SELECTING GEAR UP, GEAR DISAGREE WARNING APPEARED. NOSE GEAR INDICATED YELLOW X WHILE MAIN GEAR WERE UP. RAN QRH FOR GEAR DISAGREE. MAN EXTENSION WAS PERFORMED, ALL 3 GEAR DOWN ALL LOCKED. (FLT#3528) CLOSED SERVICED THE NOSE GEAR STRUT IAW AMM. ALL OPS AND LEAK CHECKS ARE GOOD. NOSE GEAR CENTERS ITSELF ONCE IN THE AIR AND CYCLES UP AND DOWN SMOOTHLY.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 34,796 hrs · 29,814 cycles

RIGHT INBOARD FLAP UPPER SKIN SPLICE BETWEEN FLAP STATIONS 61 - 68 DAMAGED. REPAIRED THE SKIN SPLICE IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 34,796 hrs · 29,814 cycles

BS 280 FLOORBEAM OUTBOARD SIDE OF LBL 9 ANGLE CRACKED. REPAIRED IAW REO.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 34,796 hrs · 29,814 cycles

DAMAGE ON RT PRESSURE FLOOR SILL AT FS 467 RBL 45. (C-CHECK) 05/20/2018 CUT DAMAGE, FABRICATED AND INSTALLED APPLICABLE REPAIR DOUBLERS IAW REO. PRESSURE CHECKS GOOD.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 34,796 hrs · 29,814 cycles

BS 349 FLOORBEAM HAS AREAS OF CORROSION BETWEEN RBL 30 AND THE OUTBD END. REPAIRED IAW REO.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 34,796 hrs · 29,814 cycles

CORROSION ON THE LEFT HAND PRESSURE FLOOR SILL FROM FS 439.00 TO FS 535.00. (C-CHECK) 05/20/2018 REMOVED CORROSION ON LT PRESSURE FLOOR SILL FROM FS 439.00 TO FS 535.00 IAW REO.

Part: FRAME — CORRODED (BS 333) · airframe 34,796 hrs · 29,814 cycles

AVIONICS BAY. FUSELAGE FRAME BS 333 CORRODED IN SPOTS ON THE FLANGE BETWEEN STRINGERS 25R AND 26R. REMOVED AND REPLACED THE FRAME SECTION IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,796 hrs · 29,814 cycles

FRAME AT FS 319.70 IN A-BAY HAS CORROSION ON VERTICAL FLANGE AND ATTACH FLANGE BETWEEN STR 25R AND STR27. (C-CHECK) 05/20/2018 REMOVED AND REPLACED LWR FRAME LOCATED AT FS 319.70 IAW SRM. PRESSURE CHECK GOOD.

Part: SKIN — DENTED (BS 755) · airframe 34,796 hrs · 29,814 cycles

DENT FOUND ON THE LOWER FUSELAGE SKIN AT BS 755, STRINGER 27. CUT OUT THE DAMAGE, FABRICATED A DOUBLER REPAIR AND INSTALLED IAW REO.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 34,796 hrs · 29,814 cycles

SERVICE DOOR LOWER SILL HAD AREAS OF CORROSION. REMOVED AND REPLACED THE SERVICE DOOR LOWER SILL ANGLE IAW SRM.

Part: FUEL CONTROL — FAILED (RIGHT ENGINE) · airframe 33,565 hrs · 28,447 cycles

ACFT YAWED TO THE RIGHT. RT ENGINE N1, N2, ITT AND OIL PRESSURE WERE FLUCTUATING. N1 FLUCTUATION WAS APPROX 3 TO 4%. UNKNOWN FUEL FLOW. AFTER PULLING POWER BACK EVERYTHING STABILIZED. AFTER ADDING POWER EVERYTHING STILL STAY STABILIZED. ATC DECLARED AN EMERGENCY. REMOVED AND REPLACED THE RIGHT ENGINE MAIN FUEL CONTROL IAW AMM.

Part: UPLOCK — ICED (MLG) · airframe 32,776 hrs · 27,550 cycles

LANDING GEAR WOULD NOT FULLY RETRACT. GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR UP NOSE GEAR REMAINED DOWN LOCKED. PERFORMED VISUAL INSPECTION OF MLG AND NLG ASSY FOUND EXTREME AMOUNTS OF ICE HAD ACCUMULATED ON ALL THREE GEAR OBSTRUCTING UPLOCKS REMOVED ICE AND PERFORMED OPS CHECK OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 31,399 hrs · 26,095 cycles

CORROSION ON RT FLOOR TRANSVERSE FLOORBEAM AT FS 559 FROM RBL 32 TO RBL 43. BLENDED CORROSION RT TRANSVERSE FLOORBEAM, STRAP AT FS 559 FROM RBL 36-RBL 43 IAW SRM AND REO.

Part: FLOOR SUPPORT — CORRODED · airframe 31,399 hrs · 26,095 cycles

CORROSION ON PAX DOOR FLOOR SUPPORT AFT CAP ANGLE. R & R NEW PAX DOOR FLOOR SUPPORT AFT CAP ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,399 hrs · 26,095 cycles

CORROSION ON PAX DOOR FLOOR SUPPORT FWD CAP ANGLE. R & R NEW PASSENGER DOOR FLOOR SUPPORT FWD CAP ANGLE IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 31,399 hrs · 26,095 cycles

RT INBD FLAP VANE CENTER VANE CAP CHAFED. REMOVED AND INSTALLED NEW SERVICEABLE CENTER VANE CAP AT RT INBD FLAP, PN 601R14303-52 IAW SRM.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 31,399 hrs · 26,095 cycles

CRACKED INTERCOSTAL ON PAX DOOR AT FS 349. R & R PASSENGER DOOR INTERCOSTAL DD7 AT FS 349.00, PN 601R318825-1 IAW SRM. FUSELAGE PRESSURE LEAK CHECK GOOD.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 31,399 hrs · 26,095 cycles

RT INBD FLAP VANE SKIN IS CHAFED. REMOVED AND INSTALLED NEW RT INBD FLAP VANE CAP OTBD LOCATION IAW SRM.

Part: PANEL — CHAFED (RT WING) · airframe 31,399 hrs · 26,095 cycles

RT WING PANEL 699BB IS CHAFED. REPLACED PANEL IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 31,399 hrs · 26,095 cycles

RT INBD FLAP VANE CHAFED INBD LOCATION. REMOVED AND INSTALLED NEW RT INBD FLAP VANE INBD LOCATION IAW SRM.

Part: SKIN — DENTED (BS 310) · airframe 31,399 hrs · 26,095 cycles

DENT ON BOTTOM OF FUSELAGE BETWEEN STR 27 AND STR 26R, FWD OF FS 310. REPAIRED IAW EA. FUSELAGE PRESSURE LEAK CHECKED GOOD.

Part: SKIN — DENTED (BS 589-605) · airframe 31,399 hrs · 26,095 cycles

DENT IN FUSELAGE SKIN BETWEEN FS 589 - 605 AT 4" BELOW STR 21L AND 4" FWD OF FS 605 IN FUSELAGE BELOW CARGO DOOR JUST UNDER EXISTING REPAIR PATCH. REPAIRED IAW SRM AND COMPLIED WITH STS EA.

Part: STRUCTURE — DAMAGED (BS 220) · airframe 27,851 hrs · 22,973 cycles

BIRDSTRIKE TO THE FUSELAGE BELOW THE F/O`S WINDOW IN AND ABOVE THE RVSM AREA. FORWARD OF BS 220 AND SPANS BETWEEN STR 13 AND STR 15 AND DIRECTLY OVER STR 14. REPAIRED RT FWD FUSELAGE BS 210 - 220 BETWEEN STRINGERS 13-15R ORIGINAL CONTOUR IAW REO.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 26,925 hrs · 22,234 cycles

STRINGER 3L AT BS 280 HAS CRACKED INBD STRINGER CLIP. C-CHECK, R & R STRINGER CLIP IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 26,925 hrs · 22,234 cycles

RIGHT INBD FLAP, INBD VANE ACTUATOR HAS CHAFE ON UPPER FLAP SKIN, INTERNAL SIDE. C-CHECK, REPAIRED IAW REO.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 26,925 hrs · 22,234 cycles

LEFT WING FUEL ACCESS PANEL 540BB CLAMP RING HAS PITTING. C-CHECK, REPAIRED IAW REO.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 26,925 hrs · 22,234 cycles

LT WING FUEL ACCESS PANEL 510AB, CLAMP RING HAS PITTING. C-CHECK, REPAIRED IAW REO.

Part: ATTACH ANGLE — CRACKED (BS 625) · airframe 26,925 hrs · 22,234 cycles

LEFT REAR PRESSURE BULKHEAD AFT SECTION AT BS 625.00, STRINGER 14, ATTACH ANGLE IS CRACKED. C-CHECK, R & R CRACKED ATTACH ANGLE IAW SRM.

Part: FITTING — CRACKED (BS 621 BULKHEAD) · airframe 26,925 hrs · 22,234 cycles

FS 621, BULKHEAD IS CRACKED AT THE LINTEL FITTING. C-CHECK, REPAIRED IAW REO.

Part: BULKHEAD — CRACKED (BS 621) · airframe 26,925 hrs · 22,234 cycles

FS 621, BULKHEAD HAS FIVE CRACKS AT BL 0. C-CHECK, REPAIRED IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,925 hrs · 22,234 cycles

BS 280 FLOORBEAM IS CRACKED ON LOWER SECTION AT RBL 9. C-CHECK, REPAIRED IAW REO.

Part: BULKHEAD — CRACKED (BS 621) · airframe 26,925 hrs · 22,234 cycles

FS 621, BULKHEAD HAS A CRACK AT RBL 27.5. C-CHECK, REPAIRED IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 26,925 hrs · 22,234 cycles

LEFT AILERON TOP L/E, OTBD OF INBD HINGE CHAFED. C-CHECK, REPAIRED LT AILERON UPPER SKIN L/E IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 26,925 hrs · 22,234 cycles

LEFT AILERON TOP L/E, OTBD OF CENTER HINGE CHAFED. C-CHECK, REPAIRED LT AILERON UPPER L/E SKIN IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 26,925 hrs · 22,234 cycles

LEFT AILERON TOP L/E, INBD OF OTBD HINGE CHAFED. C-CHECK, REPAIRED LT AILERON UPPER L/E SKIN IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 26,925 hrs · 22,234 cycles

RT AILERON LOWER L/E INBD FIXED PANEL CHAFED. C-CHECK, BLENDED DAMAGE ON RT AILERON LOWER L/E INBD SKIN IAW REO AND SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 26,925 hrs · 22,234 cycles

RT AILERON UPPER L/E OTBD OF OTBD HINGE CHAFED. C-CHECK REPAIRED RT AILERON UPPER L/E SKIN IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 26,925 hrs · 22,234 cycles

LT AILERON TOP L/E, INBD OF CENTER HINGE CHAFED. C-CHECK, REPAIRED LT AILERON UPPER SKIN SHROUD IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 26,925 hrs · 22,234 cycles

RT AILERON UPPER L/E INBD OF CENTER HINGE CHAFED. C-CHECK, REPAIRED RT UPPER L/E SKIN IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 26,925 hrs · 22,234 cycles

LT AILERON TOP L/E, OTBD OF OTBD HINGE CHAFED. C-CHECK, REPAIRED LT AILERON UPPER L/E SKIN IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 26,925 hrs · 22,234 cycles

RIGHT AILERON LOWER L/E OTBD FIXED PANEL CHAFED. C-CHECK, BLENDED DAMAGE ON RT AILERON LOWER L/E OTBD SKIN IAW REO AND SRM.

Part: DOOR — CHAFED (RT MLG) · airframe 26,925 hrs · 22,234 cycles

RIGHT MLG DOOR IS CHAFE ON FWD OTBD BOTTOM EDGE. C-CHECK, REPAIRED IAW REO.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 26,925 hrs · 22,234 cycles

LT MLG DOOR IS CHAFE ON FWD OTBD BOTTOM EDGE. C-CHECK, R & R IAW REO AND SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 26,925 hrs · 22,234 cycles

RT AILERON UPPER L/E OTBD OF CENTER HINGE CHAFED. C-CHECK, REPAIRED RT AILERON LEADING SKIN IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 26,925 hrs · 22,234 cycles

RT AILERON UPPER L/E INBD OF OTBD HINGE CHAFED. C-CHECK, REPAIRED RT AILERON UPPER LEADING SKIN IAW REO.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 26,813 hrs · 22,131 cycles

HYDRAULIC 2 LOW PRESSURE CAUTION. NR 2 ACMP AND EDP2 SHOW YELLOW, PSI FLUCTUATES. REPLACED HYD SYSTEM NR 2 ACMP, NR 2 ENGINE DRIVEN PUMP AND HYD SYSTEM NR 2 RESERVOIR IAW AMM.

Part: CONTROL UNIT — FAILED (STAB TRIM) · airframe 26,813 hrs · 22,131 cycles

STAB TRIM CAUTION AND MACH TRIM CAUTION MESSAGE DISPLAYED. FOLLOWED QRH TO TRY TO ENGAGE. WHEN F/O USED TRIM A STAB TRIM AND MACH TRIM CAUTION MESSAGE AGAIN DISPLAYED. REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT. OPS CHECKS GOOD ON BOTH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,388 hrs · 20,977 cycles

EMERGENCY LIGHT BURNED OUT. FLT#5485 RELAMPED.

Part: SHUTOFF VALVE — FAILED (AC BAY) · airframe 24,903 hrs · 20,594 cycles

RECEIVED RT PACK OVER PRESSURE CAUTION MESSAGE, PERFORMED QRH PROCEDURES MULTIPLE TIMES WITH NO CHANGE. FLT#6290 REPLACED RT PACK PRESSURE REGULATING SHUT OFF VALVE IAW ATA. PN 3215622-1, SN OFF 1557 & SN ON 5520.

Part: STRUT — OVERSERVICED (NLG) · airframe 24,564 hrs · 20,341 cycles

RECEIVED NOSE GEAR DISAGREE, NOSE DOOR OPEN WARNING MESSAGES AND WOW INPUT, STEERING INOP CAUTION MESSAGES AND A WOW OUTPUT FAIL STATUS MESSAGE. FOUND TOO MUCH HYD FLUID IN NLG STRUT. SERVICED AND PERFORMED GEAR SWINGS IAW AMM.

Part: ENGINE — FAILED (RIGHT) · airframe 23,924 hrs · 19,795 cycles

SMOKE TOILET EICAS MSG ON TAKEOFF AT 100 KNOTS. BLEEDS FROM ENGINES. ABORTED TAKEOFF. (FLT 4464) REMOVED AND REPLACED RIGHT ENGINE. P/N: CF34-3B1 S/N ON: 873691 S/N OFF: 872710.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 23,856 hrs · 19,726 cycles

SMOKE TOILET CAUTION MESSAGE RECEIVED AFTER TAKEOFF. MESSAGE CLEARED DURING CLIMBOUT. CREW DID NOT OBSERVE ANY SMOKE. (FLT 4547) PERFORMED GROUND RUN UP OF LEFT AND RIGHT ENGINES WITH BLEEDS ON AND PACKS ON. RECEIVED SMOKE TOILET. RAN RIGHT ENGINE AND RECEIVED MESSAGE AGAIN. RAN LEFT ENGINE AND GOT NO MESSAGE. PERFORMED COMPRESSOR WASH OF RIGHT ENGINE, REPLACED LEFT AND RIGHT WATER SEPARATOR COALESCER SOCKS IAW AMM.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 23,831 hrs · 19,697 cycles

SMOKE TOILET MESSAGE APPEARED. (FLT 4458 )INSPECTED LAVATORY FOR SIGNS OF SMOKE AND FOUND NO SMOKE AND DID NOT SMELL ANY SMOKE OR ODORS. PERFORMED TEST OF LAVATORY SMOKE DETECTOR AND FOUND NO FAULTS AT THIS TIME. LAVATORY SMOKE DETECTOR OPS CHECKS GOOD.

Part: CAM — OUT OF ADJUST (CABIN DOOR) · airframe 23,453 hrs · 19,409 cycles

MAIN CABIN DOOR WILL NOT OPEN OR CLOSE. (FLT 4499) ADJUSTED ICE BREAKER DOOR CAM AND RE-ALIGNED ROLLER IAW AMM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 23,225 hrs · 19,192 cycles

LEFT WINDOW HEAT MESSAGE IN FLIGHT ACCOMPANIED BY A HAIRLINE CRACK ACROSS WINDOW AND ARCING NOTICED ALONG BOTTOM OF WINDOW. (FLT 4571) REPLACED LEFT SIDE WINDOW IN REFERENCE TO CRJ200 M/M. P/N OFF: NP-139322-9 S/N OFF: 03219H1563.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,962 hrs · 18,954 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5322) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,902 hrs · 18,904 cycles

EMERGENCY LIGHT IS OUT OVER GALLEY SERVICE DOOR. (FLT 6362) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,609 hrs · 18,652 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5330) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — LOOSE (CABIN) · airframe 22,314 hrs · 18,409 cycles

FORWARD CEILING EMERGENCY LIGHTS WILL NOT TURN ON. (FLT 6477) FOUND NR 1 CEILING EMERGENCY FLOOD LIGHT LOOSE. SECURED BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,314 hrs · 18,409 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5358) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,267 hrs · 18,368 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5332) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,238 hrs · 18,332 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5314) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,172 hrs · 18,267 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6478) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,020 hrs · 18,138 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5407) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,889 hrs · 18,017 cycles

EXTERIOR SERVICE DOOR EMERGENCY EXIT LIGHT IS OUT. (FLT 5304) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,797 hrs · 17,937 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6274) RELAMPED EMERGENCY LIGHT.

Part: CONTROLLER — MALFUNCTIONED (ADG) · airframe 21,721 hrs · 17,867 cycles

ADG DEPLOYED. (FLT 6219) REPLACED ADG AUTO DEPLOYMENT CONTROLLER. PN: 82046-5 SN OFF: 049

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,660 hrs · 17,821 cycles

FLT 6494, NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,630 hrs · 17,794 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5393) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,392 hrs · 17,604 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5327) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,240 hrs · 17,476 cycles

NR 3 AND 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6314) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,214 hrs · 17,454 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 5572) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,174 hrs · 17,422 cycles

LAST EMERGENCY LIGHT BURNT OUT. (FLT 6250) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,836 hrs · 17,122 cycles

EXTERIOR EMERGENCY LIGHT BY SERVICE DOOR IS OUT. (FLT 5503) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,443 hrs · 16,806 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2946) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,264 hrs · 16,623 cycles

NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 2855) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,264 hrs · 16,623 cycles

LEFT WING FORWARD AND AFT EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 2972) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,807 hrs · 16,164 cycles

LEFT AFT EXTERNAL EMERGENCY LIGHT IS OUT. (FLT 2843) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,675 hrs · 16,033 cycles

NR 1 EMERGENCY LIGHT OVER THE LEFT WING IS BURNED OUT. (FLT 3071) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,472 hrs · 15,824 cycles

NR 3 CEILING EMERGENCY LIGHT IS INOPERATIVE. (FLT 3047) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,260 hrs · 15,612 cycles

FORWARD LEFT EMERGENCY LIGHT ON FUSELAGE IS BURNED OUT. (FLT 3048) RELAMPED EMERGENCY LIGHT.

Part: MOTOR — BINDING (CABIN DOOR) · airframe 18,855 hrs · 15,267 cycles

MAIN CABIN DOOR WOULD NOT FULLY OPEN. (FLT 6668) REPLACED THE PAX DOOR POWER ASSIST MOTOR ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,855 hrs · 15,267 cycles

NR 3 CABIN EMERGENCY OVERHEAD LIGHT IS OUT. (FLT 6831) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,013 hrs · 15,377 cycles

FS 202.75 BULKHEAD HAS CRACKS AT THE PARKING BRAKE FEED-THROUGH LOCATION. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,013 hrs · 15,377 cycles

FS 621 BULKHEAD CRACKED ON WEB AT UPPER AFT CARGO TRACK. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,566 hrs · 15,026 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 7006) RELAMPED EMERGENCY LIGHT.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 18,161 hrs · 14,701 cycles

DURING CRUISE THE FLIGHT CREW REPORTED THAT THE WINDSHIELD WAS BEGINNING TO DELAMINATE. IT WAS DECIDED TO DIVERT TO KSDF DUE TO PARTS AND MAINTENANCE ON SITE. THE AIRCRAFT DIVERTED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE IS CURRENTLY IN THE PROCESS OF REPLACING THE NR 1 WINDSHIELD. THE CAPTAIN’S WINDSHIELD WAS REPLACED WITH NO FURTHER DEFECTS NOTED.

Part: FAN BLADE — OUT OF BALANCE (NR 1 ENGINE) · airframe 17,933 hrs · 14,510 cycles

DURING OVERNIGHT MAINTENANCE ON 10/13/2009, THE FAN DISK ON E1 WAS REPLACED BY CONTRACT MAINTENANCE. DURING POST MAINTENANCE GROUND POWER ASSURANCE RUN THE E1 FAN VIBES WERE AT 2.2MILS. MAINTENANCE REPLACED THE EVM SENSOR AND DURING THE SECOND POWER RUN THE VIBES WERE AT 1.7MILS AND THE AIRCRAFT WAS RETURNED TO SERVICE. ON 10/14/2009 DURING CLIMB OUT OF SDF AT APPROXIMATELY 16,000FT THE FLIGHT CREW NOTICED THE E1 FAN VIBE GAUGE INDICATING IN THE AMBER CAUTION RANGE. AS THE CREW CONTINUED CLIMB THE INDICATION REMAINED IN THE AMBER RANGE AND POWER HAD TO BE REDUCED TO KEEP THE VIBES WITHIN THE GREEN RANGE. THE AIRCRAFT THEN RETURNED TO SDF AND LANDED WITHOUT INCIDENT. AT THAT POINT CONTRACT MAINTENANCE RETURNED WITH DIFFERENT TECHNICIANS, MAINTENANCE PERFORMED POWER RUNS WHILE REPOSITIONING THE AIRCRAFT TO THE HANGAR AND THE VIBRATIONS WERE AT 1.7MILS. THE VIBRATION SENSOR WAS INSPECTED FOR SECURITY ALONG WITH THE HARNESS FOR DAMAGE AND SECURITY WITH NO DEFECTS NOTED. THE MASTER CHIP DETECTOR WAS INSPECTED FOR DEBRIS WITH NONE NOTED. AT THIS POINT THE FAN DISK WAS REPLACED AND THE FAN BLADES WERE INSPECTED AND INSTALLED ACCORDING TO THEIR POSITIONS ON THE PREVIOUSLY INSTALLED DISK. DURING POWER RUNS THE E1 FAN VIBES WERE STILL AT 1.7MILS. THE FAN BLADES WERE THEN REMOVED AND A FAN TRIM BALANCE WAS PERFORMED, THE FAN BLADES WERE RE-INSTALLED, AND THE AFT SPINNER WEIGHTED BOLTS WERE NULLED OUT. DURING THE POWER RUNS THAT FOLLOWED THE E1 FAN VIBES WERE BELOW 1.0MILS AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DUCT — DIRTY (CABIN) · airframe 17,244 hrs · 13,950 cycles

FLIGHT 5512, SDF TO CLE. AT FL220 THE CREW RECEIVED A DISPLAY COOL MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND IT WAS DECIDED TO DIVERT TO IND, WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE SYSTEM ON MEL AND THE AIRCRAFT CONTINUED ON THE STANDBY SYSTEM. THE MEL WAS CLEARED IN CLE WHEN MAINTENANCE CLEANED DEBRIS FROM THE DISTRIBUTION DUCTS AND THE DISPLAY COOLING SYSTEM OPERATED NORMALLY.

Part: TRIM PANEL — FAULTY (COCKPIT) · airframe 15,889 hrs · 12,895 cycles

FLIGHT 5601, IAH TO JAX. DURING CLIMB, THE FLIGHT CREW EXPERIENCED AN AILERON TRIM RUN-AWAY. THE QRH WAS FOLLOWED AND THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AILERON/RUDDER TRIM PANEL AND THE AILERON TRIM SYSTEM OPERATED NORMALLY.

Part: WARNING SYSTEM — MALFUNCTIONED (THRUST REVERSER) · airframe 11,444 hrs · 9,737 cycles

FLIGHT 3276 - IAH-MCI - EN ROUTE AT FL310 -R REV UNLOCKED- MESSAGE APPEARED. REDUCED THRUST ON RIGHT ENGINE TO IDLE AND RAN QRH. DETERMINED REVERSER DID NOT DEPLOY. DECLARED AN EMERGENCY. APPROACH AND LANDING WERE UNEVENTFUL. MAINTENANCE DEFERRED THRUST REVERSER.

Part: LIGHT — INOPERATIVE (COCKPIT)

ALL COCKPIT OVERHEAD PANEL LIGHTS FLICKERING. REMOVED AND REPLACED LAMP DRIVER UNIT REF 31-41-07. OPS CHECK NORMAL.

Part: ENGINE — INOPERATIVE (LEFT)

LEFT ENGINE WOULD NOT SHUTDOWN WHEN THRUST LVR SET TO CUT OFF. C/W TWO ENGINE START/SHUTDOWN SEQUENCES IAW AMM 71-00-00-868-807. NO DEFECTS WERE NOTED DURING EITHER SHUTDOWN. OK FOR SERVICE.

Part: PROXIMITY SENSOR — DIRTY (EMERGENCY EXIT)

RIGHT EMERGENCY DOOR INDICATOR INOP. CLEANED AND LUBED RIGHT EMERGENCY DOOR PROX SENSOR AND PARAMETER SEAL. OPS CHECKED SEVERAL TIMES. NO FAULT NOTED AT THIS TIME.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,595 hrs · 5,363 cycles

DURING MAINTENANCE INSPECTION THE NR 3 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LAMP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: ENGINE — FAILED (RIGHT)

DURING CRUISE, CREW HEARD A LOUD NOISE AND THEN EXPERIENCED A SLIGHT YAW. ITT READINGS ON THE RT ENGINE ROSE TO OVER 900; CREW FOLLOWED QRH AND SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY IN. MANITENANCE PERSONNEL REMOVED AND REPLACED THE RT ENGINE. OPERATIONAL CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING INSPECTION LT EXIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED LT EMERGENCY OVERWING LIGHT. OPS CHECK GOOD AND AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.