N918SW

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 47,291 hrs · 40,032 cycles

D: FLAP FAIL EVENTC: AD 2009-06-12/10, CREW RESETFULL FLAP AD EVALUATION DUE WITHIN 10 CYCLES DUE 40040 TACFLAP FAIL AT ZERO DEGREES.AT 3000 FT SPEED 195KTS. (FLIGHT 3915) RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL AD COMPLIANCE BY MCC.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 47,112 hrs · 39,904 cycles

ON APPROACH FLAPS 8, FLAPS FAIL CAUTION MESSAGE DISPLAYED (FLIGHT 3360 FILED CLOSED)RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL COMPLIANCE BY MCC

Part: FLAP SYSTEM — FAILED · airframe 47,112 hrs · 39,904 cycles

ON APPROACH FLAPS 8, FLAPS FAIL CAUTION MESSAGE DISPLAYED (FLIGHT 3360 FILED CLOSED)RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL COMPLIANCE BY MCC

Part: CONTROL LEVER — FAILED (TE FLAPS) · airframe 46,515 hrs · 39,393 cycles

FLAPS FAIL CAUTION ON APPROACH, WHEN ATTEMPTING TO SET 30 DEGREES FLAPS, FLAPS FAILED AT 20 DEGREES. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26117469 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED THE FLAP CONTROL LEVER IAW CRJ 200 AMM 27-51-01. OPS CHECK GOOD AT THIS TIME. REF CP26117663-1 FOR AD COMPLIANCE."

Part: FLOOR SUPPORT — OUT OF LIMITS (BS 484-499) · airframe 46,442 hrs · 39,326 cycles

FOUND LT FLOOR SSUPPORT NR 10 BLEND-OUT, OUT OF LIMITS. PERFORMED A REPAIR TO PRESSURE FLOOR SUPPORT BETWEEN BS 484 - 499, LHS AND PERFORMED REO 601R-53-41-3101, REV -. PRESSURE CHECK GOOD.

Part: CAP — CORRODED (DOOR HANDRAIL) · airframe 46,442 hrs · 39,326 cycles

FLOOR SILL AT PAX DOOR FWD HANDRAIL CAP HAS INTERGRANULAR CORROSION AND REQUIRES REPLACEMENT. REMOVED AND INSTALLED NEW PAX DOOR FWD HANDRAIL CAP IAW SRM 51-42-06, AND DWG 601R31527, REV AM.

Part: BRACKET — CRACKED (DOOR HANDRAIL) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR SILL AFT HANDRAIL CAP BRACKET BETWEEN FS 333.00 TO FS349.00 HAS CORROSION REMOVED AND REPLACED HANDRAIL CUP BRACKET AND CLEAT IAW SRM 51-42-06, 51-45-00, AND DWG 601R31527, REV AM.

Part: BRACKET — CORRODED (DOOR HANDRAIL) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR SILL FWD HANDRAIL CAP BRACKET BETWEEN FS 310.00 TO FS319.70 HAS CORROSION. REPLACED PAX DOOR SILL FWD HANDRAIL CAP BRACKET IAW SRM 51-42-06, DWG 601R-31527, REV AM.

Part: STIFFENER — CRACKED (KEELBEAM) · airframe 46,442 hrs · 39,326 cycles

FORWARD KEEL BEAM PRESSURE BOX, UPPER STIFFENER WAS DENTED WITH POSSIBLE CRACK. EVALUATED DENT ON FORWARD KEEL BEAM PRESSURE BOX, UPPER STIFFENER OUT OF LIMITS. REMOVED AND INSTALLED A NEW FORWARD KEEL BEAM PRESSURE BOX, STIFFENER IAW SRM 51-42-06, SRM 51-23-00, SRM 51-42-21, DWG 601R31060, REV F, AND REO 601R-53-31-1252 REV-. NO LEAKS NOTED.

Part: FRAME — CORRODED (BS 310 S24L-R) · airframe 46,442 hrs · 39,326 cycles

FRAME BS 310 HAD MULTIPLE SPOTS OF CORROSION FROM S24L TO S24R. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R32002 REV AD.

Part: FRAME — CORRODED (BS 319 S25-26L) · airframe 46,442 hrs · 39,326 cycles

FRAME BS 319 HAD MULTIPLE SPOTS OF CORROSION FROM STR 25L TO STR 26. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R32003, REV P. PRESSURE CHECKS GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 46,442 hrs · 39,326 cycles

R/H FLOOR SILL ANGLE FROM FS310.00 TO FS319.70 HAS AREAS OF CORROSION. REMOVED AND REPLACED THE FLOOR SILL ANGLES WITH NEW IAW SRM 51-42-06, 51-42-13, DWG 601R31148, REV Y.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 46,442 hrs · 39,326 cycles

RIGHT PRESSURE FLOOR SILL FROM BS 409 - 559 HADS AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-21-06. FOUND PARTS TO BE OUT OF LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-53-41-666 REV-C, DISPOSITION 1.2, AND REO 601R-53-41-3102 REV--, NO LEAKS NOTED.

Part: FRAME — CORRODED (BS 605 S23L-25R) · airframe 46,442 hrs · 39,326 cycles

CORROSION NOTED ON FRAME BS 605 BETWEEN S25R-23L. FOUND OUT OF LIMITS. REMOVED AND INSTALLED A NEW LOWER FRAME IAW DWG 601R36026, REV AF, DWG 601R35005 REV Y, SRM 51-42-06, AND SRM 51-42-21. NO LEAKS NOTED.

Part: ANGLE — CRACKED (BS 484 RBL 27-36) · airframe 46,442 hrs · 39,326 cycles

TWO ANGLES FOR INTERCOSTAL AT BS 484 BETWEEN RBL 27 AND RBL 36 ARE CRACKED. REMOVED AND INSTALLED NEW ANGLES IAW SRM 51-42-06, SRM 51-42-21 AND DWG 601R31171, REV B. NO LEAKS NOTED.

Part: ANGLE — CRACKED (BS 484 LBL 27-36) · airframe 46,442 hrs · 39,326 cycles

TWO ANGLES FOR INTERCOSTAL AT BS 484 BETWEEN FLOORBEAM LBL 27 AND LBL 36 WERE CRACKED. REMOVED AND INSALLED THE TWO ANGLES IAW DWG 601R31171, REV B, AND SRM 51-42-21. NO LEAKS NOTED

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 46,442 hrs · 39,326 cycles

LEFT PRESSURE FLOOR SILL FROM BS409+128 - 559 HAD AREAS OF CORROSION. BLENDED OUT CORROSION AND FOUND AREAS TO BE OUT OF LIMITS. COMPLIED WITH ALL STEPS OF REO'S 601R-53-41-666 REV-C AND REO 601R-53-41-3102 REV-. NO LEAKS NOTED. PERFORMED REPAIR ON BLEND-OUT LOCATION 10.

Part: SUPPORT FITTING — CRACKED (BS 460 LBL 27) · airframe 46,442 hrs · 39,326 cycles

SUPPORT FITTING FOR LBL27 FLOOR BEAM AT FS460 HAS A POSSIBLE CRACK. NDT VERIFIED CRACK ON SUPPORT FITTING . REMOVED AND INSTALLED A NEW SUPPORT FITTING WITH REPLACEMENT FASTENERS IAW SRM 51-42-21, AND DWG 600-31143, REV E. NO LEAKS NOTED.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR CLEAT COMMON TO FS320.163 FORMER AND MID LWR CHANNEL CORRODED. REMOVED AND REPLACED THE PAX DOOR CLEAT IAW DWG 601R31702, REV N, AND SRM 51-42-06.

Part: FRAME — CRACKED (BS 235 S11-12R) · airframe 46,442 hrs · 39,326 cycles

CRACKED FRAME FS 235.00 BETWEEN STRINGERS 11-12R. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-06, DWG 601R34032, REV V, AND REO 601R-53-11-3810, REV-. PRESSURE CHECKED GOOD.

Part: FRAME ANGLE — CRACKED (BS 235 S11-12L) · airframe 46,442 hrs · 39,326 cycles

CRACK ON FRAME BS 235 BETWEEN STRINGERS 11-12L. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-06, AND DWG 601R34032, REV -V. PRESSURE CHECKS GOOD.

Part: DRAIN VALVE — DAMAGED (LEFT) · airframe 46,442 hrs · 39,326 cycles

UPON REMOVAL OF LEFT HAND COLLECTOR TANK WATER DRAIN VALVE NOTICED TWO WASHERS UNDER WATER DRAIN VALVE FASTENERS ON WING PLANK SIDE. UPON REMOVAL OF THE WASHERS IDENTIFIED THAT THE LEFT HAND COLLECTOR TANK WATER DRAIN VALVE FASTENER HOLES TWO EACH ARE ELONGATED. PERFORMED REPAIR ON LH COLLECTOR TANK WATER DRAIN SCREW HOLES REF REO 601R-57-21-3660 REV-. NO LEAKS NOTED.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 46,442 hrs · 39,326 cycles

LEFT MAIN LANDING GEAR WHEEL WELL, BRAKE HYDRAULIC FUSE AFT BRACKET IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06 AND DWG 601R75278 REV-G. NO LEAKS NOTED

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 46,442 hrs · 39,326 cycles

REPAIR DAMAGED UPPER SKIN ON R/H ELEVATOR INBOARD AFT TRAILING EDGE. PERMEANNTLY REPAIRED RT ELAVATOR INBD AFT EDGE IAW SRM 55-20-00.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 46,442 hrs · 39,326 cycles

LEFT MAIN LANDING GEAR WHEEL WELL, BRAKE HYDRAULIC FUSE FORWARD BRACKET IS CRACKED. REMOVED THE LT MAIN LANDING GEAR WHEEL WELL, HYDRAULIC FUSE FWD BRACKET IAW SRM 51-42-06, INSTALLED A NEW BRACKET IAW SRM 51-42-06 AND DWG 601R75278 REV-G. LEAK CHECK GOOD

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 46,442 hrs · 39,326 cycles

UPON REMOVAL, FOUND RT ELEVATOR L/E HINGE FITTING ASSY TO BE EXCESSIVELY WORN AT BEARING LOCATION. REPLACE HINGE FITTING ASSY IAW DWG 601R24025, REV G, SRM 51-42-06, AND 51-42-21

Part: HINGE FITTING — CORRODED (LT ELEVATOR) · airframe 46,442 hrs · 39,326 cycles

UPON REMOVAL FOR BEARING REPLACEMENT, FOUND LT ELEVATOR L/E HINGE FITTING ASSY HAVE PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REMOVED AND REPLACED THE LT ELEVATOR NR 1 HINGE FITTING ASSY WITH NEW HINGE FITTING ASSY IAW DWG 601R24025, REV G, SRM 51-42-06, AND 51-42-21.

Part: SKIN — DENTED (BS 559-574) · airframe 46,442 hrs · 39,326 cycles

SMALL DENT ON TOP OF AFT FUSELAGE BETWEEN BS 559+112 AND 574, BETWEEN STR 0 AND STR 1R. COMPLIED WITH PERMANENT REPAIR IAW REO 601R-53-61-7912, REV -., PRESSURE CHECK GOOD.

Part: BRACKET — CRACKED (TRANSDUCER) · airframe 46,442 hrs · 39,326 cycles

RIGHT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET CRACKED & BROKEN IN TWO PLACES. REMOVED AND INSTALLED A NEW BRACKET IAW SRM 51-42-06 AND DWG 601R31146 REV J, PRESSURE CHECKS GOOD.

Part: BRACKET — CRACKED (TRANSDUCER) · airframe 46,442 hrs · 39,326 cycles

LEFT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET CRACKED IN TWO PLACES. REMOVED AND INSTALLED A NEW BRACKET IAW SRM 51-42-06, AND DWG 601R31146, REV J. PRESSURE CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR DD3 MID INTERCOSTAL CORRODED. REMOVED AND INSTALLED PAX DOOR DD3 MID INTERCOSTAL IAW SRM 51-42-06 , SRM 51-42-21 AND DWG 601R31702, REV N. PRESSURE CHECKS GOOD

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR CLEAT COMMON TO FS320.163 FRAME AND MID LWR CHANNEL CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT COMMON TO FS320.163 FRAME AND MID LWR CHANNEL IAW DWG 601R31702REV. N AND SRM 51-42-06.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR DD6 MID INTERCOSTAL CORRODED. PAX DOOR DD6 INTERCOSTAL OUT OF LIMITS. REMOVED AND INSTALLED NEW DD6 INTERCOSTAL IAW DWG 601R31702 REV: N, SRM 51-42-06, SRM 51-42-21. NO LEAKS NOTED.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR DD3 AFT INTERCOSTAL CORRODED. REMOVED AND INSTALLED NEW DD3 INTERCOSTAL IAW DWG 601R31702, REV: N, AND SRM 51-42-06. PRESSURE CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR DD4 MID INTERCOSTAL CORRODED. REMOVED AND INSTALLED PAX DOOR DD4 MID INTERCOSTAL IAW SRM 51-42-06 , SRM 51-42-21 AND DWG 601R31702, REV N. CHECKED GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR DD4 AFT INTERCOSTAL CORRODED. PAX DOOR DD4 AFT INTERCOSTAL OUT OF LIMITS. REMOVED AND INSTALLED NEW DD4 AFT INTERCOSTAL IAW DWG 601R31702, REV N AND SRM 51-42-06. NO LEAKS NOTED.

Part: INTERCOSTAL — DENTED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR DD7 FWD INTERCOSTAL DENTED. REMOVED AND INSTALLED A NEW DD7 FWD INTERCOSTAL IN PASSENGER DOOR IAW DWG 601R31702, REV: N, SRM 51-42-06. PRESSURE CHECK GOOD

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR CLEAT ON DD4 FWD COMMON TO FS313.56 FRAME CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT ON DD4 FWD COMMON TO FS313.56 FRAME REF. DRWG 601R31702 REV. N AND SRM 51-42-06.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR DD6 MID CLEAT COMMON TO FS329.76 FORMER CORRODED. REMOVED AND REPLACED PAX DOOR DD6 MID CLEAT COMMON TO BS 329.76 FORMER IAW DWG 601R31702, REV. N AND SRM 51-42-06.

Part: FORMER — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR FWD FORMER CORRODED. PAX DOOR FWD FORMER FOUND TO BE CORRODED OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER REF. DRWG 601R31702 REV. N, SRM 51-42-06 AND SRM 51-42-21. NO LEAKS NOTED.

Part: FORMER — CORRODED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR AFT FORMER CORRODED. REMOVED AND INSTALLED NEW AFT FORMER IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R31702, REV N. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — DENTED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR DD1 AFT INTERCOSTAL DENTED. PAX DOOR DD1 AFT INTERCOSTAL OUT OF LIMITS. REMOVED AND INSTALLED NEW DD1 INTERCOSTAL IAW DWG 601R31702, REV: N, AND SRM 51-42-06. NO LEAKS NOTED.

Part: HINGE ARM — CHAFED (LT WING TE FLAP) · airframe 46,442 hrs · 39,326 cycles

LEFT INBOARD FLAP, INBOARD HINGE ARM, INBOARD GUIDE PLATE IS CHAFED. INSTALLED A NEW INBOARD HINGE ARM ,INBD GUIDE PLATE IAW SRM 51-42-06 AND DWG 601R14116, REV H.

Part: HINGE ARM — CHAFED (LT WING TE FLAP) · airframe 46,442 hrs · 39,326 cycles

LEFT INBOARD FLAP, OUTBOARD HINGE ARM, INBOARD GUIDE PLATE IS CHAFED. REPLACED INBOARD GUIDE PLATE AT LT INBOARD FLAP, OUTBOARD HINGE ARM IAW SRM 51-42-06 AND DWG 601R14116 REV H.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 46,442 hrs · 39,326 cycles

LEFT INBD FLAP VANE HAS CHAFING ON LEADING EDGE AT INBD LOCATION AT APPROXIMATELY WS 56.30. (C-CHECK) UPON BLENDING LT INBD FLAP VANE IB LOCATION, MATERIAL LOSS AT 100%, THROUGH PART AND REQUIRES REPLACEMENT IAW SRM 51-12-00. REMOVED BAD VANE CAP IAW SRM 51-42-10. LOCATE HOLES IN REPLACEMENT CAP IAW SRM 51-42-10. INSTALLED REPLACEMENT VANE CAP IAW SRM 51-42-13, REV 39, AND DWG 601R14302, REV E. COMPLETED CARD 51-900-1003.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 46,442 hrs · 39,326 cycles

LEFT INBD FLAP VANE HAS CHAFING ON LEADING EDGE AT MID LOCATION AT APPROXIMATELY WS 104.099. (C-CHECK) REMOVED AND INSTALLED NEW LT INBD FLAP VANE CAP, LEADING EDGE MID LOCATION PER DWG 601R14303, REV J AND SRM 51-42-13.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

PAX DOOR PIANO HINGE (FUSELAGE SIDE) HAS NUMEROUS ELONGATED HINGE PIN HOLES (C-CHECK) REMOVED AND INSTALLED NEW PAX DOOR HINGE HALF IAW SRM 53-21-23 STEPS 4. R-V AND REO 601R-53-21-656 REV A. NO LEAKS NOTED.

Part: SKIN — CRACKED (PAX DOOR) · airframe 46,442 hrs · 39,326 cycles

REMOVE AND REPLACE PAX DOOR INNER SKIN DUE TO CRACKED. REMOVED AND REPLACED PAX DOOR INNER SKIN IAW SRM 51-42-06, SRM 51-42-10, SRM 51-42-21, AND SRM 51-42-22.

Part: SKIN — CHAFED (LT AILERON) · airframe 46,442 hrs · 39,326 cycles

LEFT AILERON LOWER FWD EDGE HAS 3 SPOTS THAT ARE CHAFED. (C-CHECK) BLENDED CHAFING ON LT AILERON LOWER FWD LEADING EDGE SKINS IAW SRM 51-12-00, TWO AREAS FOUND IN LIMITS IAW SRM 57-60-00 AND LOCATION AILS 370 TO 375 FOUND OUT OF LIMITS, REPLACED WITH NEW SKIN IAW SRM 51-42-06 AND SRM 51-42-21 AND DWG CC670-13000 REV D. COMPLIED WITH CARD 51-900-1003. MAJOR REPAIR.

Part: AILERON — NOT REPORTED (RT WING) · airframe 46,442 hrs · 39,326 cycles

REINSTALL RT AILERON PER AMM IAW AMM 27-15-01-000-801. COMPLY WITH TASK CARD 27-900-1001-SKY (C-CHECK RO 12/17/2022) REMOVED AND REINSTALLED THE RH AILERON WITH NEW HARDWARE - REF CRJ 200 AMM 27-15-01-400-801. RIGGING, BONDING AND OPERATIONAL TESTS ARE GOOD. COMPLIED WITH SKYWEST TASK CARD 27-900-1001-SKY.

Part: BUSHING — OUT OF LIMITS (RT WING) · airframe 46,442 hrs · 39,326 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RT AILERON WING AFT SPAR IAW AMM 20-26-00-910-804. REMOVED, INSTALLED AND SEALED A NEW SERVICEABLE RT AILERON BUSHINGS ON WING AFT SPAR AMM 20-26-00-910-804.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 45,998 hrs · 38,922 cycles

CLIMBING UP, PRESSURE WAS GOOD THEN RECEIVED A OVERBOARD COOL CAUTION MESSAGE AND A INBOARD COOL FAIL STATUS MESSAGE. RAN QRH, PRESSURE WAS STILL GOOD. THEN, CONTINUED ENROUTE CLIMB TO DEN, CABIN RATE AND CABIN ALT WAS INCREASING. RECEIVED CABIN ALT CAUTION ALONG WITH CABIN ALT WARNING. RAN QRC, DECLARED EMERGENCY AND TURNED BACK TO GTF. PAX MASK WERE DEPLOYED, WAS NOT AN OVERWEIGHT LANDING, VSI LESS THAN 100 FT PER MIN, AND CURRENT CREW O2 IS AT 1140. FOUND TO BE THE OVERBOAD EXHAUST SOV TO BE FAULTY. PRESSURIZED AIRCRAFT AS REQUIRED, PER MEL. CABIN HELP PRESSURE. NO OVERWEIGHT LANDING OR HARD LANDING NOTED, REF AML 522207 FOR OVERBOARD COOL CAUTION AND INBOARD COOL STATUS MESSAGE MEL, REF AML 522227 FOR SERVICE CREW OXY SYS. REM AML 522229 FOR DEFERRING PAX OXY SYS MEL.

Part: STRAP — CORRODED (BS 559) · airframe 42,879 hrs · 36,102 cycles

FS 559 LBL FLOOR STRAP AT PRESSURE FLOOR SILL CORRODED. (C-CHECK) RO: 02/23/2019 REMOVED AND REPLACED THE FS559 LBL27 FLOOR STRAP AT PRESSURE FLOOR SILL IAW SRM. LEAK CHECKS GOOD.

Part: SKIN — DAMAGED (RT WING FLAP) · airframe 42,879 hrs · 36,102 cycles

REPLACE THE RH INBOARD FLAP LEADING EDGE, INBOARD CAP. (C-CHECK) RO: 02/23/2019 REMOVED AND REPLACED RH INBOARD FLAP LEADING EDGE, INBOARD CAP IAW SRM.

Part: DOOR SILL — CORRODED (BS 579-620) · airframe 42,879 hrs · 36,102 cycles

CARGO DOOR SILL CORRODED FROM FS 579 TO FS620. (C-CHECK) RO: 02/23/2019 REMOVED AND REPLACED CARGO DOOR SILL AT FS 579.000-FS620.00 IAW SRM.

Part: SKIN — DENTED (BS 627) · airframe 42,879 hrs · 36,102 cycles

FUSELAGE SKIN DENTED AT APPROX FS627 BETWEEN STR27 AND STR26R. (C-CHECK) RO: 02/23/2019 DRESSED BACK FUSELAGE SKIN DENT AT APPROX. FS627 BETWEEN STR27 AND STR26R TO ORIGINAL CONTOUR IAW REO. NO FURTHER DEFECTS NOTED.

Part: DOOR FRAME — CORRODED (E/E BAY DOOR) · airframe 42,879 hrs · 36,102 cycles

FRETTING DAMAGE ON THE INTERNAL AVIONICS BAY DOOR CUT-OUT SURROUND. (C-CHECK) RO: 02/23/2019 BLENDED INTERNAL AVIONICS BAY DOOR CUT-OUT SURROUND TO A SMOOTH CONTOUR IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 42,879 hrs · 36,102 cycles

RH AILERON UPPER LEADING EDGE CHAFED ALONG ENTIRE LENGTH. (C-CHECK) RO: 02/23/2019 REMOVED AND REPLACED RH AILERON LE EDGE SKIN WITH NEW IAW SRM AND REO.

Part: SKIN — DENTED (RT WING) · airframe 42,879 hrs · 36,102 cycles

RH WING LOWER SKIN DENT, RHWS377 - 1.5 INCHES FWD OF AFT EDGE OF SKIN. (C-CHECK) RO: 02/23/2019 COMPLIED WITH ALL APPLICABLE STEPS IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 42,879 hrs · 36,102 cycles

LH INBD FLAP VANE UPPER SKIN TRAILING EDGE CHAFED 5 INCHES OTBD OF INBOARD END. (C-CHECK) RO: 02/23/2019 BLENDED CHAFE ON THE LH INBD FLAP VANE UPPR SKIN TRAILING EDGE IAW REO.

Part: GUSSET — CORRODED (BS 310) · airframe 42,879 hrs · 36,102 cycles

GUSSET ON FS310.00 FRAME STGR13L IS CORRODED. (C-CHECK) RO: 02/23/2019 REMOVED AND INSTALLED NEW GUSSET P/N 600-31109-57 IAW SRM.

Part: HINGE — CHAFED (SERVICE DOOR) · airframe 42,879 hrs · 36,102 cycles

SERVICE DOOR HINGE HAS CHAFING DAMAGE. (C-CHECK) RO: 02/23/2019 BLENDED CHAFFED AREAS ON SERVICE DOOR HINGE. COMPLIED WITH ALL STEPS IAW REO.

Part: FRAME — CORRODED (BS 349) · airframe 42,879 hrs · 36,102 cycles

FS349 FRAME, STGR25L TO STGR25R, ON BOTH FORWARD AND AFT SIDE IS CORRODED. (C-CHECK) RO: 02/23/2019 REMOVED AND INSTALLED THE NEW BOTTOM FRAMES SECTION AT FS349.00 BETWEEN STGR25L AND STGR25R. IAW SRM.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 41,852 hrs · 35,168 cycles

FLAPS FAIL MESSAGE AT CRUISE. FAILED IN 0 POSITION. (FLT 5311) FO: 07/31/2018 CLOSED. RESET AND OPERATED FLAPS. OK TO CONTINUE SERVICE FOR 10 FLIGHT CYCLES. C/W FIM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,286 hrs · 31,907 cycles

FRETTING ON THE UPPER FUSELAGE WHERE THE ADF ANTENNA CONTACTS THE AIRCRAFT. (C-CHECK) RO: 02/09/2017 COMPLIED WITH ALL STEPS OF REO.

Part: WEB — CORRODED (PAX DOOR) · airframe 38,286 hrs · 31,907 cycles

PAX DOOR AFT WEB HAS CORROSION UNDER PANEL 832HR. COMPILED WITH REO.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 38,286 hrs · 31,907 cycles

PAX DOOR ACCESS PANEL 832AR HAS CORROSION AROUND FASTNER HOLES. REPLACED THE ACCESS PANEL IAW SRM.

Part: PANEL — CORRODED (DOOR) · airframe 38,286 hrs · 31,907 cycles

DOOR PANEL 832GR HAS CORROSION AROUND FASTNER HOLES. REPLACED PANEL IAW SRM.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 38,286 hrs · 31,907 cycles

PAX DOOR ACCESS PANEL 832AL HAS CORROSION AROUND FASTNER HOLES. REPLACED THE ACCESS PANEL IAW SRM.

Part: PANEL — CORRODED (DOOR) · airframe 38,286 hrs · 31,907 cycles

DOOR PANEL 832HL HAS CORROSION AROUND FASTNER HOLES.REPLACED THE PANEL IAW SRM.

Part: SKIN — DENTED (CARGO DOOR) · airframe 38,286 hrs · 31,907 cycles

DENT ON LOWER RIGHT CORNER FOR CARGO DOOR. COMPLIED WITH REO.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 38,286 hrs · 31,907 cycles

LEFT WING INBOARD GROUND SPOILER DENTED. REPAIRED IAW REO.

Part: FAN — DIRTY · airframe 37,821 hrs · 31,462 cycles

RIGHT PACK FAILED FOLLOWED QRH, DESCENDED TO 25FL THEN LT PACK FAILED, LOST PRESSURIZATION. DIVERTED. DECLARED AN EMERGENCY AND DEPLOYED OXYGEN MASKS. CLEANED CABIN TEMPERATURE SENSOR FAN IAW AMM. RAN BOTH PACKS, WITH ENGINES AND PRESSURIZED A/C IAW AMM. OPS CHECK GOOD NO FAULTS FOUND.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 33,692 hrs · 27,840 cycles

RT WING FUEL PANEL CUTOUT FOR PANEL 650FB HAS PITTING ON LOWER BONDING SURFACE. C-CHECK, RO 2/28/15. PITTING, FRETTING CORROSION, UNDER FUEL PANEL 650FB, HOLE NR 14 AT WS 274.319 WAS BLENDED MORE THAN 50 PERCENT OF THE HATCH AREA AND ALSO IN THE CRITICAL AREAS. NDT ENSURED A CRACK FREE CONDITION. ORIGINAL THICKNESS AROUND THE HOLE VARIED FROM .185"? TO .192"?. MINIMUM REMAINING MATERIAL THICKNESS WAS .184"?. MINIMIM ALLOWABLE THICKNESS WITHOUT REPEAT INSPECTION IS .182"?. MATERIAL LOSS RANGED FROM.001"? TO .002"?. BLENDED AREAS WITHIN LIMITS. BLENDED AREA WAS ROTO PEENED. REF FOR BLENDING AND LIMITS: REO. ADDITION ENGINEERING FOR BLENDING MORE THAN 50 PERCENT OF HATCH AREA AND WITHIN THE CRITICAL AREAS: REO STATES BLEND IS ACCEPTABLE AS IS, AS LONG AS MEETING ALL OTHER REQUIREMENTS OF REO.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 33,692 hrs · 27,840 cycles

RT WING FUEL PANEL CUTOUT FOR PANEL 650EB HAS PITTING ON LOWER BONDING SURFACE. C-CHECK, RO 2/28/15. PITTING, FRETTING CORROSION, UNDER FUEL PANEL 650EB, HOLE NR 13 AT WS 253.022 WAS BLENDED MORE THAN 50 PERCENT OF THE HATCH AREA AND ALSO IN THE CRITICAL AREAS. NDT ENSURED A CRACK FREE CONDITION. ORIGINAL THICKNESS AROUND THE HOLE VARIED FROM .188"? TO .192"?. MINIMUM REMAINING MATERIAL THICKNESS WAS .187"?. MINIMIM ALLOWABLE THICKNESS WITHOUT REPEAT INSPECTION IS .182"?. MATERIAL LOSS RANGED FROM.001"? TO .002"?. BLENDED AREAS WITHIN LIMITS. BLENDED AREA WAS ROTO PEENED. REFERENCE FOR BLENDING AND LIMITS: REO. ADDITION ENGINEERING FOR BLENDING MORE THAN 50 PERCENT OF HATCH AREA AND WITHIN THE CRITICAL AREAS: REO, STATES BLEND IS ACCEPTABLE AS IS, AS LONG AS MEETING ALL OTHER REQUIREMENTS OF REO.

Part: FRAME — CRACKED (BS 333) · airframe 33,692 hrs · 27,840 cycles

FRAME AT STR 0-1L AND FS 333 HAS POSSIBLE CRACK AT TOOLING HOLE, MARKED. C-CHECK, RO 2/28/15. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER, PN; " EA 24-2015-55-1 DOUBLER", STS EA . ALL STEPS AND ITEMS COMPLIED WITH. COMPLIED WITH ST, WEIGHT OF PARTS, REMOVED 0.00 LBS. WEIGHT OF PARTS INSTALLED 0.02 LBS. NET WEIGHT GAIN 0.02LBS.

Part: FRAME — CORRODED (BS 333) · airframe 33,692 hrs · 27,840 cycles

FS 333 FRAME, LOWER SECTION FORWARD OF AVIONICS BAY DOOR, SUSPECTED CORROSION ON FWD FACE BL 0-RBL15. BUBBLING PAINT, C-CHECK, RO 2/28/15. REPLACED LOWER SECTION FRAME AT FS 333, LBL15-RBL15, PN 601R32004-55, FWD OF AVIONICS BAY DOOR, REF SRM. COMPLIED WITH ST LEAK CHECK GOOD.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 33,692 hrs · 27,840 cycles

LEFT INBD FLAP VANE CENTER L/E CHAFED OUT OF LIMITS REF CAMP MAINTENANCE TRANS NR 11850984. C-CHECK 2/28/15, REMOVED LT INBD FLAP VANE CENTER L/E AND INSTALLED NEW CENTER L/E PN 601R14303-51, REF SRM. COMPLIED WITH ST.

Part: FLOOR PANEL — CRACKED (BS 432) · airframe 33,692 hrs · 27,840 cycles

PRESSURE FLOOR CRACKED AT FS 462 AND LBL 4.0 TO LBL 6.0, MARKED. (C-CHECK RO 2/28/15)REPAIRED PRESSURE FLOOR CRACKED AT FS 462 AND LBL 4.0 TO LBL 6.0, REF REO. NO LEAKS NOTED, COMPLIED WITH ST.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,692 hrs · 27,840 cycles

LEFT INBD FLAP VANE L/E HAS CHAFING AT THE ONBD BUMPER LOCATION. C-CHECK, RO 2/28/15, LT INBD FLAP VANE L/E CHAFE AT THE OTBD BUMPER OUT OF LIMITS REF REO, REPLACED CAP REF SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,692 hrs · 27,840 cycles

LEFT INBD FLAP VANE L/E HAS CHAFING AT THE INBD BUMPER LOCATION. C-CHECK, RO 2/28/15, BLENDED CHAFE DAMAGE ON THE LT INBD FLAP, INBD VANE CAP IAW REO. FOUND PART TO HAVE 100 PERCENT MATERIAL LOSS. R & R LT INBD FLAP, INBD VANE CAP REF SRM. VANE CAP FINISH WAS RESTORED ON JOB 2764575, OP 103, MX TRANS: 11880909.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 33,692 hrs · 27,840 cycles

LEFT INBD FLAP VANE L/E HAS CHAFING AT THE CENTER BUMPER LOCATION. C-CHECK, RO 2/28/15, BLENDED LT INBD FLAP, FLAP VANE CENTER L/E SKIN REF REO, BLEND OUT OF LIMITS. REF CAMP MAINTENANCE TRANS 11857280 FOR REPLACEMENT OF LT INBD FLAP, FLAP VANE CENTER L/E SKIN .

Part: SKIN — DENTED (RT WING) · airframe 33,692 hrs · 27,840 cycles

ONE DENT LOCATED ON THE RT WING LOWER WING BOX EXTENSION. COMPLIED WITH TEMPORARY REPAIR IAW REO. PERMANENT REPAIR DUE WITHIN 1800 FLT HRS BY TAT: 34626.1. C-CHECK, RO 2/28/15. COMPLIED WITH PERMANENT REPAIR OF 1 DENT LOCATED ON THE RT WING LOWER WING BOX EXTENSION REF STS EA DENT WITHIN LIMITS.

Part: DISPLAY — FAILED (EICAS) · airframe 32,072 hrs · 26,572 cycles

RETURN TO THE FIELD WHEN A EICAS SCREEN WENT BLANK. REPLACED DISPLAY. CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,031 hrs · 26,535 cycles

RT NR 4 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. R & R THE RT NR 4 EXTERIOR EMERGENCY LIGHTS IAW AMM.

Part: BULB — INOPERATIVE (INDICATOR) · airframe 31,986 hrs · 26,501 cycles

FLIGHT DECK EMERGENCY LIGHT OFF LIGHT HAS TWO OUT OF FOUR BULBS INOPERATIVE. REPLACED THE ANNUNCIATOR LIGHT CAP. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,517 hrs · 26,137 cycles

LT EXTERIOR NR 1 EMERGENCY LIGHT IS BURNED OUT. REPLACED LAMP.

Part: SKIN — DENTED (BS 230-235) · airframe 31,303 hrs · 25,959 cycles

DENT IN NOSE FUSELAGE BELOW CAPTAIN'S WINDOW BETWEEN BS 230 - 235, WL 110, S12L. REPAIRED IAW REO.

Part: CARBON SEAL — FAILED (ENGINE) · airframe 31,032 hrs · 25,760 cycles

SLOW LOSS OF OIL PRESS IN FLIGHT. COMPLETED QRH PROCEDURE. IN FLIGHT ENGINE SHUTDOWN. FLT 5561 REPLACED HYD ENG DRIVEN PUMP, AIR TURBINE STARTER & IDG CARBON SEALS ON RT ENG. PERFORMED OIL CONSUMPTION CHECK IAW AMM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 29,616 hrs · 24,754 cycles

LT STRINGER 11A IS GOUGED & TORN. C-CHECK REPLACED IAW STS. PN 601R31018-45

Part: SILL — CORRODED (FUSELAGE) · airframe 29,616 hrs · 24,754 cycles

CARGO DOOR SILL HAS CORROSION ON TOP SURFACE AT FS589. C-CHECK REPLACED IAW SRM & REO.

Part: FLOORBOARD — CRACKED (COCKPIT) · airframe 29,616 hrs · 24,754 cycles

COCKPIT FLOOR BOARD AT FS 279.5 RBL 10 IS CRACKED. C-CHECK REPLACED COCKPIT FLOOR BOARD AFT FLOOR SUPPORT IAW SRM. PN 600-34017-351.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,616 hrs · 24,754 cycles

LT 202 BULKHEAD AT PARKING BRAKE ROD LOCATION IS CRACKED. C-CHECK REPAIRED IAW REO.

Part: DOOR — CORRODED (CABIN) · airframe 29,616 hrs · 24,754 cycles

CORROSION FOUND ON AIRCRAFT MAIN CABIN DOOR UNDER PANEL 832GL. C-CHECK REPAIRED IAW STS.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 27,795 hrs · 23,334 cycles

LEFT PACK HIGH PRESSURE WHEN THROTTLES ARE ADVANCED. (FLT 5322) PERFORMED OPERATIONAL CHECK OF LEFT ENGINE PRSOV AND LEFT PACK IAW AMM. NO FAULTS FOUND.

Part: FLAP — DEFECTIVE (WING) · airframe 27,251 hrs · 22,884 cycles

AT FLAPS 45 PLANE ROLLS UNCOMMANDED. (FLT 6450) REMOVED PAINT RUNS FROM ALL FOUR FLAP TRAILING EDGE UNDERSIDES AND UPPER LEADING EDGE SURFACES IN REFERENCE TO CRJ MM.

Part: INVERTER — FAILED (CABIN) · airframe 26,106 hrs · 21,992 cycles

EMERGENCY EXIT SIGN AT 8 C/D IS INOPERATIVE. (FLT 6276) REPLACED EMERGENCY LIGHT POWER INVERTER NR 3 IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,926 hrs · 21,843 cycles

FLT 6242, NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,850 hrs · 21,787 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6204) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,752 hrs · 21,704 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,713 hrs · 21,675 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5914) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,644 hrs · 21,621 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6218) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,266 hrs · 21,318 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5384) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,008 hrs · 21,102 cycles

AFT CEILING EMEREGENCY LIGHT IS OUT. (FLT 5483) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,008 hrs · 21,102 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5612) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,943 hrs · 21,048 cycles

NR 1 AND NR 4 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. (FLT 6525) RELAMPED EMERGENCY LIGHTS.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 26,440 hrs · 22,254 cycles

LEFT FS 559.0 PRESSURE BULKHEAD HAS DAMAGE. (C-CHECK) REPAIRED PER REO.

Part: SKIN — DENTED (TE FLAP) · airframe 26,440 hrs · 22,254 cycles

LEFT INBOARD FLAP LOWER SKIN HAS A DENT. (C-CHECK) REPAIRED PER REO.

Part: BUCKLE — DEFECTIVE (COCKPIT) · airframe 24,884 hrs · 20,998 cycles

F/O SEATBELT DOESN'T RELEASE PROPERLY. (FLT 5441) REPLACED F/O'S BUCKLE ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,713 hrs · 20,872 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6306) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,412 hrs · 20,613 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5347) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,376 hrs · 20,569 cycles

LEFT CENTER OVERWING EMERGENCY LIGHT IS OUT. (FLT 5519) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,186 hrs · 20,427 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,981 hrs · 20,265 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 6350) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,674 hrs · 20,014 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6251) RELAMPED EMERGENCY LIGHT.

Part: WIRE — DISCONNECTED (CABIN) · airframe 23,626 hrs · 19,958 cycles

AFT SECTION OF FLOOR EMERGENCY LIGHTS ARE OUT. (FLT 6860) RECONNECTED WIRE ON AFT FLOOR EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,626 hrs · 19,958 cycles

CEILING EMERGENCY LIGHT IS OUT. (FLT 6552) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 23,600 hrs · 19,938 cycles

LAST SEGMENT OF THE EMERGENCY LIGHT FLOOR STRIP IS NOT ILLUMINATING DURING TEST. (FLT 7022) RE-SECURED CONNECTOR ON AFT FLOOR STRIP LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,307 hrs · 19,691 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6565) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,291 hrs · 19,679 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6424) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,081 hrs · 19,502 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 13 IS OUT. (FLT 6917) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,994 hrs · 19,425 cycles

LEFT EMERGENCY EXIT FORWARD EXTERIOR LIGHT IS OUT. (FLT 6262) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,994 hrs · 19,425 cycles

SERVICE DOOR AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6262) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,994 hrs · 19,425 cycles

EMERGENCY LIGHT OVER ROW 2 IS OUT. (FLT 6472) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,932 hrs · 19,377 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6506) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,872 hrs · 19,329 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,872 hrs · 19,329 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,295 hrs · 18,885 cycles

NR 2 CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6408) RELAMPED NR 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,133 hrs · 18,753 cycles

NR 4 EMERGENCY POD LIGHT INOPERATIVE. (FLT 6274) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,934 hrs · 18,579 cycles

MOST AFT, INTERIOR EMERGENCY LIGHT INOPERATIVE. (FLT 6737) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,820 hrs · 18,489 cycles

NR 1 EMERGENCY LIGHT INOPERATIVE. (FLT 6749) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,356 hrs · 18,099 cycles

NR 4 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. (FLT 6655) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,079 hrs · 17,858 cycles

LAST EMERGENCY CEILING LIGHT IS BURNT OUT. (FLT 6693) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,471 hrs · 17,347 cycles

NR 1 CEILING EMERGENCY LIGHT INOP. (FLT 6816) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,280 hrs · 17,187 cycles

PRESSURE BULKHEAD AT FS 559 CRACKED. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,280 hrs · 17,187 cycles

FS 621 PRESSURE BULKHEAD WEB CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,280 hrs · 17,187 cycles

FS 621 AFT PRESSURE BULKHEAD WEB CRACKED AT LINTEL FITTING AND AT TOP OF AFT CARGO DOOR TRACK. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,280 hrs · 17,187 cycles

FS 621 FORWARD AFT PRESSURE BULKHEAD CRACKED AT SPLICE. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,746 hrs · 17,576 cycles

FS 621 BULKHEAD CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 20,746 hrs · 17,576 cycles

FS 484 LEFT INTERCOSTAL CRACKED AT CABLE SUPPORT MOUNT BOLT HOLE. (C CHECK) REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,746 hrs · 17,576 cycles

FS 621 FORWARD AFT PRESSURE BULKHEAD CRACKED AT TOP OF AFT CARGO DOOR TRACK. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,746 hrs · 17,576 cycles

FS 621 PRESSURE BULKHEAD CRACKED AT SPLICE. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,468 hrs · 16,514 cycles

CABIN OVERHEAD EMERGENCY LIGHT NR 2 INOP. (FLT 5778) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,305 hrs · 16,394 cycles

EMERGENCY CEILING LEVEL LIGHT AT ROW 13 INOP. (FLT 6580)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,127 hrs · 16,247 cycles

AFT MOST EMERGENCY CEILING FLOOD INOP. (FLT 6137) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,068 hrs · 16,201 cycles

EMERGENCY EXIT LIGHT NR 2 ON CEILING INOP. (FLT 6728) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,068 hrs · 16,201 cycles

EXTERIOR EMERGENCY EXIT LIGHTS INOP. (FLT 5835) RELAMPED EMERGENCY LIGHTS.

Part: COVER — BROKEN (CABIN) · airframe 18,950 hrs · 16,115 cycles

PLASTIC STRIP COVERING EMERGENCY FLOOR STRIP HAS BROKEN OFF FROM ABOUT ROW 12 BACK TO LAVATORY. (FLT 6014) REMOVED & REPLACED AFT EMERGENCY TRACK LIGHT COVER IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,950 hrs · 16,115 cycles

FOURTH OVERHEAD EMERGENCY LIGHT AFT IS BURNED OUT. (FLT 6189) REMOVED AND REPLACED 4TH AFT EMERGENCY OVERHEAD BULB PER AMM CH 33-51-16.

Part: CONNECTOR — LOOSE (CABIN) · airframe 18,907 hrs · 16,085 cycles

EMERGENCY EXIT LIGHT BY MAIN DOOR INOP. (FLT 6639) RE-SEATED CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,723 hrs · 15,941 cycles

NR 2 AFT CEILING EMERGENCY LIGHT INOP. (FLT 5849) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — DAMAGED (CABIN) · airframe 18,558 hrs · 15,812 cycles

EMERGENCY FLOOR LIGHTING AFT STRIP DAMAGED. (FLT 6510) REPLACED LIGHT STRIP SECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,512 hrs · 15,774 cycles

CABIN EMERGENCY LIGHT IN CEILING INOP. (FLT 6484) RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 18,435 hrs · 15,716 cycles

GEAR DISAGREE DISPLAYED. (FLT 6589) REPLACED NLG SELECTOR VALVE (GEAR DOORS).

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 17,414 hrs · 14,936 cycles

FLT 6562 - EMERGENCY EXIT LIGHT BY CABIN DOOR NOT ILLUMINATING. RESEATED CONNECTOR.

Part: BRACKET — OUT OF ADJUST (NLG PROX SENSOR) · airframe 17,387 hrs · 14,919 cycles

FLT 6503 - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. ADJUSTED NOSE GEAR PROX SENSOR BRACKET.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,112 hrs · 14,711 cycles

FLT 5855 - EMERGENCY LIGHTS INOP. REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 16,515 hrs · 14,259 cycles

C-CHECK, THREE ISOLATORS FORWARD SIDE OF AFT PRESSURE BULKHEAD CRACKED. REPLACED PER SRM.

Part: SUPPORT — CRACKED (BS 280) · airframe 16,515 hrs · 14,259 cycles

C-CHECK, FS 280 RBL 9 SUPPORT CLIPS CRACKED. REPAIRED PER REO.

Part: SUPPORT — CRACKED (BS 625) · airframe 16,515 hrs · 14,259 cycles

C-CHECK SUPPORT AND CLIP AT FS 625 CRACKED. REPLACED PER SRM.

Part: SUPPORT — CRACKED (BS 280) · airframe 16,515 hrs · 14,259 cycles

C-CHECK, FS 280 LBL 9 SUPPORT CLIP CRACKED. REPAIRED PER REO.

Part: BRACKET — CRACKED (BS 280) · airframe 16,515 hrs · 14,259 cycles

C-CHECK, FS 280 LEFT BRACKET, RIGHT SIDE OF COCKPIT FLOOR OPENING, CRACKED. REPAIRED PER REO.

Part: ACM — FAILED (RIGHT) · airframe 15,606 hrs · 13,525 cycles

FLT 6006 - RECEIVED A PACK HI TEMP CAUTION MESSAGE ALONG WITH REPORTED LIGHT SMOKE IN CABIN. REPLACED RIGHT PACK AIR CYCLE MACHINE IAW AMM 21-12-00. OPS AND LEAK CHECK GOOD, P/N 782790-15, S/N OFF 200106038.

Part: ADG — DEPLOYED · airframe 15,364 hrs · 13,327 cycles

ADG DEPLOYED DURING FLIGHT. RESTOWED ADG AS REQUIRED.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 14,248 hrs · 12,365 cycles

FLT 6670 - SYSTEM 2 HYDRAULIC QUANTITY DROPPED TO 0 PERCENT IN FLIGHT. REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-01. OPS CHECK AND LEAK CHECK GOOD.

Part: RIB — DAMAGED (RWS 389) · airframe 14,248 hrs · 12,365 cycles

RIGHT WING RIB AT WS389 IS DAMAGED. REPLACED RIGHT WING RIB AT WS 389 IAW REO 601R-57-21-899.

Part: SPAR — DAMAGED (RWS 339) · airframe 14,248 hrs · 12,365 cycles

FORWARD OUTBOARD WING SPAR ON RIGHT WING HAS DAMAGE AT WS 339. REPAIRED WING SPAR DAMAGE AT WS 335-353 IAW CRJ 200 REO 601R-57-21-898.

Part: ACM — FAILED (LEFT) · airframe 12,447 hrs · 10,818 cycles

LEFT PACK BRIEFLY HAS AN ODOR OF SMOKE, MADE A LOUD NOISE AND THEN OVERTEMPED. REPLACED LEFT AIR CYCLE MACHINE IAW AMM 21-51-10-401.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 12,216 hrs · 10,624 cycles

AFT RED EMERGENCY EXIT SIGN IS MISSING. REPLACED AFT RED EMERGENCY EXIT SIGN IAW AMM 33-51-00.

Part: WINDOW — CRACKED (COCKPIT) · airframe 11,589 hrs · 10,045 cycles

DESCENDING THRU 9,000 FT RIGHT WINDOW CRACKED. REPLACED RIGHT SIDE WINDOW IAW CRJ MM 53-12-01 AND RII 56-220-1000, PN OFF: NP139322-001 SN OFF: 02014H6515.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 11,509 hrs · 9,975 cycles

UPON GEAR EXTENSION GOT A GEAR DISAGREE AND TOWER CONFIRMED THAT THE NOSE GEAR WAS STILL UP. PERFORMED MANUAL RELEASE GEAR EXTENSION AND RECEIVED THREE GREEN INDICATIONS. REPLACED NLG SELECTOR VALVE ASSY IAW CRJ 200 MM 32-33-10. OPERATIONAL CHECKS GOOD.

Part: SELECTOR — MALFUNCTIONED (MLG) · airframe 11,509 hrs · 9,975 cycles

UPON GEAR EXTENSION, GOT A GEAR DISAGREE WITH THE NOSE GEAR REMAINING UP. EXTENDED GEAR MANUALLY WITH ALL GEAR EXTENDING NORMALLY. REPLACED NLG SELECTOR VALVE ASSY IAW CANDAIR REGIONAL SET MM 32-22-25 PG 401.

Part: VALVE — MALFUNCTIONED (NLG) · airframe 11,509 hrs · 9,975 cycles

AFTER SELECTING GEAR DOWN NOSE GEAR DID NOT COME DOWN. RECYCLED GEAR HANDLE THREE TIMES, NO HELP. MANUALLY EXTENDED NOSE GEAR. REPLACED NLG PRIORITY VALVE IAW RJ 200 MM 32-33-15. OPERATIONAL CHECKS GOOD, P/N; 4622.

Part: FRAME — CRACKED (BS 280) · airframe 11,426 hrs · 9,901 cycles

FS 280 LBL9 LOWER FRAME/EVIDENCE OF CRACKS ON FLOOR SUPPORT BEAM AND LBL9 I/B AND O/B 280 CLIPS ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED I/B AND O/B CLIPS AND FILLERS.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,426 hrs · 9,901 cycles

FS 280 LBL9 LOWER ANGLE CRACKED ON FLOOR SUPPORT BEAM AND RBL9 I/B AND O/B 280 CLIPS ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AND CLIPS AT STA 280 RBL9 LOWER PER CRJ200 REO 601R 53-171 REV 'C' REPAIR SCHEME 'B' .

Part: TRIM SWITCH — INOPERATIVE (NR 2 STAB) · airframe 9,118 hrs · 7,890 cycles

CREW REPORTS NR 2 STAB TRIM SWITCH INOP. REPLACED NR 2 STAB TRIM SWITCH REF AMM 27-41-05, OPERATIONAL CHECKS GOOD.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 8,828 hrs · 7,634 cycles

ON APPROACH "FLAPS HALFSPEED" STATUS MESSAGE CAME ON. REPLACED FLAP PDU PER CRJ MM 27-51-00. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 461) · airframe 8,443 hrs · 7,305 cycles

MAIN CABIN OVER PRESSURE FLOOR AT STA 461.00 BL 9 FLOORBEAM ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOORBEAM INSTALLED AS REQUIRED IAW EO 600-31068 AND SRM 51-42-06; 51-42-21.

Part: ANGLE — CRACKED (BS 621) · airframe 8,443 hrs · 7,305 cycles

CRACKED SUPPORT ANGLE FS 621; LBL 45; WL 73.5. ITEM FOUND AT C-CHECK INSPECTION. REPAIR PARTS INSTALLED AS REQUIRED AND ALL WORK DONE IAW REO 601R-53-61-004 SRM 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,443 hrs · 7,305 cycles

L-BRACKET CLIP AT INBOARD RIGHT HAND 9' LBL ATTACHMENT TO 280 FS FLOORBEAM IS CRACKED AT TOP RADIUS. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIP STA 280 INBOARD RBL 9 IAW CRJ200 SRM 51-42-06 PG 1-17.

Part: CLIP — CRACKED (BS 280) · airframe 8,443 hrs · 7,305 cycles

L-BRACKET (CLIP) AT OUTBOARD LEFT HAND 9' LBL ATTACHMENT TO 280 FS BEAM IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIP LEFT HAND INBOARD STA 280.00 LBL 9 IAW CRJ200 SRM 51-42-06 PG 1-4.

Part: ADC — MALFUNCTIONED (COCKPIT) · airframe 6,888 hrs · 6,046 cycles

DURING FLIGHT FROM ORD, CAPTAIN`S ALTIMETER JUMPED ERRATICALLY BETWEEN 22.00 - 32.00. UNABLE TO RESET WITH BARO KNOB TO PROPER SETTING. DIVERT TO CAK. REMOVED AND REPLACED NR 1 ADC IAW AMM 34-11-00. OPERATIONAL CHECK GOOD. A/C REMAINS CAT II & RVSM.

Part: PRESSURE SWITCH — MALFUNCTIONED (SPOILERS) · airframe 6,512 hrs · 5,725 cycles

ON SHORT FINAL RECEIVED SPOILERONS FAULT AND OUTBOARD GROUND SPOILER FAULT STATUS MESSAGES. REMOVED AND REPLACED ANCP LOW PSI SWITCH 1B. PERFORMED SECU CHECKS IAW 27-61-05. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 6,420 hrs · 5,640 cycles

CAPTAINS SIDE WINDOW HAS MULTIPLE CRACKS THAT SPAN THE LENGTH OF WINDOWS. REMOVED AND REPLACED LT SIDE WINDOW IAW AMM 56-12-01. P/N NP139322-5, S/N OFF 01352H5316.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 6,330 hrs · 5,568 cycles

STAB TRIM AND MACH TRIM CAUTION ILLUMINATED AFTER TAKEOFF. REMOVED AND REPLACED HSTCU IAW CRJ 200 MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 5,976 hrs · 5,247 cycles

RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EXTERIOR EMERGENCY EXIT DOOR LIGHT IAW CRJ MM 33-51-21. OPERATIONAL CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,930 hrs · 5,203 cycles

BACK EMERGENCY LIGHTS INOPERATIVE. REMOVED BATTERY AND CLEANED CONTACTS. OPERATIONAL CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,774 hrs · 5,073 cycles

EMERGENCY LIGHTS AFT OF EXIT ROW INOPERATIVE. REMOVED EMERGENCY BATTERY AND CLEANED CONTACTORS, RE-INSTALLED AFT BATTERY. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 5,767 hrs · 5,067 cycles

FLAPS FAIL MESSAGE ON APPROACH TO LANDING. REMOVED AND REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORZ STAB TRIM) · airframe 5,518 hrs · 4,834 cycles

NR 2 STAB TRIM FAILED TO ENGAGE. REMOVED AND REPLACED HSTA, IAW CH. 27-42-01 AND REPLACED MCU IAW MM CH. 27-42-05. OPERATIONAL CHECK GOOD. P/N: 7062-3 S/N OFF: 117.

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 5,401 hrs · 4,730 cycles

ON APPROACH STAB TRIM CHANNEL 1 DISENGAGED. REMOVED AND REPLACED CAPTAINS STAB TRIM SWITCH AND STAB TRIM/MACH TRIM POND ASSY IAW MM 27-41-00 AND 27-41-25. OPERATIONAL CHECK GOOD.

Part: TRIM PANEL — MALFUNCTIONED (STAB TRIM) · airframe 5,288 hrs · 4,646 cycles

INFLIGHT, MACH TRIM AND CHANEL 1 STAB DISENGAGED. REMOVED AND REPLACED STAB TRIM/MACH TRIM PANEL FOR IAW CRJ 200 MM 27-41-20. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — LOOSE (E/E BAY) · airframe 5,035 hrs · 4,384 cycles

FLIGHT SPOILERS FAULT STATUS MESSAGE DISPLAYED ON ED2. RESECURED NR 1 SECU IN RACK. OPERATIONAL CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (FLT SPOILERS) · airframe 4,877 hrs · 4,244 cycles

FLT SPOILERS FAULT STATUS MSG CYCLES ON AND OFF, TAXIED BACK TO GATE. PERFORMED FAULT ISOLATION PROCEDURES OF FLIGHT SPOILERS SYSTEM. NO DEFECTS NOTED.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 4,693 hrs · 4,081 cycles

FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED POWER DRIVE UNIT FOR FLAPS IAW 27-52-01. OPS CHECKS GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,241 hrs · 3,643 cycles

MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED BULB, OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 4,038 hrs · 3,450 cycles

FLAPS FAIL CAUTION MESSAGE ON WHEN FLAPS SELECTED AT APPROXIMATELY 13,000 FT. REMOVED AND REPLACED RIGHT NR 1 AND LEFT NR 1 ACTUATOR (FLAP), IAW 27-53-01, 27-53-05, AND RII 27-412. OPS CHECKS GOOD. S/N OFF RIGHT: 3392.

Part: BPSU — MALFUNCTIONED (BRAKE POSITION) · airframe 3,998 hrs · 3,414 cycles

FLAPS FAIL AT -0- WHEN SELECTED. REMOVED AND REPLACED RIGHT AND LEFT FLAP BPSU, LEFT FLAP ACTUATOR IN THE NUMBER 3 POSITION AND THE RIGHT NR 3 FLAP ACTUATOR. RIGHT BPSU S/N OFF: 0801, ACTUATOR P/N: 853D100-19, LEFT S/N OFF: 1945. RIGHT S/N OFF: 1941. OPS CHECKS GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,013 hrs · 3,430 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,013 hrs · 3,430 cycles

CABLE FAIRLEAD INTERCOSTAL AT FS 484 RBL 36.0 IS CRACKED AT O/B FLANGE. DISCOVERED DURIING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-41-059 REV-A.

Part: CLIP — CRACKED (FUSELAGE) · airframe 4,013 hrs · 3,430 cycles

MAIN CABIN INBOARD AND OUTBOARD ATTACH CLIPS ARE CRACKED ON RBL 9.0 FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11.

Part: CLIP — CRACKED (FUSELAGE) · airframe 4,013 hrs · 3,430 cycles

MAIN CABIN I/B AND O/B ATTACH CLIPS ARE CRACKED ON LBL 9.0 FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,013 hrs · 3,430 cycles

CABLE FAIRLEAD INTERCOSTAL AT FS 484 LBL 36.0 IS CRACKED AT FLANGE. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-41-059 REV-A.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 3,492 hrs · 2,925 cycles

STALL FAIL MESSAGE AFTER TAKEOFF. REPLACED STALL COMPUTER. OPS CHECK GOOD. S/N OFF: 887

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 2,972 hrs · 2,478 cycles

PILOT REPORTS L SPOILER FAULT ON INBOUND FLIGHT. REPLACED NR 1 SECU. OPS CHECK GOOD AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (NR 2) · airframe 2,140 hrs · 1,727 cycles

WITH BOTH ENGINES RUNNING AND NORMAL HYDRAULIC PRESSURE ON ALL 3 SYSTEMS, FLT SPLICER FAULT AND INBOARD GROUND SPOILER FAULT MESSAGES ON ED2 (STATUS). RETURNED TO THE GATE. REMOVED AND REPLACED NR 2 SECU. OPS CHECK GOOD.

Part: WIRE HARNESS — FAULTY (NR 2 ENGINE) · airframe 840 hrs · 675 cycles

DURING FLIGHT TO SFO AT 16,000 FT, NR 2 ENGINE N1 FLUCTUATIONS OF 8 TO 10 PERCENT WITH ASSOCIATED N2 FUEL FLOW & ITT FLUCTUATIONS. WITH THRUST BACK AT 68 PERCENT, FLUCTUATIONS STOPPED. REMOVED AND REPLACED RIGHT ENGINE BLUE AND YELLOW HARNESS. ENGINE RUN OF SYSTEM OPS CHECKS GOOD ON THE GROUND.

Part: AMPLIFIER — MALFUNCTIONED (NR 2 ENGINE) · airframe 758 hrs · 615 cycles

AFTER ESTABLISHING CLIMB POWER AFTER DEPARTURE FROM FAT, RIGHT SIDE N1 FLUCTUATIONS OF +/- 10 PERCENT AND FUEL FLOW OF +/- 500 PPH CAUSED A/C TO YAW UP TO 20K FT. REDUCED POWER AND RIGHT ENGINE STABILIZED. NO FURTHER FLUCTUATIONS WERE OBSERVED. RETURNED TO FAT. REPLACED NR 2 N1 AMPLIFIER. OPS CHECK GOOD IAW MM 73-21-03.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 330 hrs · 294 cycles

STAB CH1 WILL NOT ENGAGE. REMOVED AND REPLACED TRIM UNIT, HORIZONTAL STAB IAW CRJ MM 27-41-05. PERFORMED OPS AND FUNCTIONAL CHECK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO CAT II STATUS.