N907SW

Part: BRACKET — CRACKED (CRGO DOOR TRACK) · airframe 43,866 hrs · 41,189 cycles

CARGO COMPARTMENT FWD CARGO DOOR TRACK LOWER U CHANNEL ATTACH BRACKET CRACKED, MARKED. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW FWD CARGO DOOR TRACK LOWER U CHANNEL ATTACH BRACKET P/N 601R35050-25 CRJ200 SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,866 hrs · 41,189 cycles

FS 589.0 FRAME AT STR 26L TO AT 26R HAS CORROSION ON FWD SIDE. C-CHECK RO 11/23/2020. REMOVED CORROSION ON FS 589 FRAME AT STGR 26L TO STGR 26R, REF CRJ200 SRM, FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED.

Part: ANGLE — CRACKED (CROSSBEAM) · airframe 43,866 hrs · 41,189 cycles

LT 280 CROSSBEAM CLIPS ARE CRACKED AROUND LBL 9 FLOORBEAM. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW LT 280 CROSSBEAM CLIPS AT LBL 9 FLOORBEAM, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.

Part: STRAP — CORRODED (CABIN) · airframe 43,866 hrs · 41,189 cycles

LT TOP STRAP AT FS 559.0 FROM LBL 27 TO SILL HAS CORROSION. C-CHECK RO 11/23/2020. REMOVED CORROSION AT LT TOP STRAP AT FS 559.00 LBL 27 TO SILL, REF CRJ200 SRM, FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW LT TOP STRAP AT FS 559.00 LBL 27, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.

Part: ANGLE — CRACKED (CROSSBEAM) · airframe 43,866 hrs · 41,189 cycles

RT 280 CROSSBEAM CLIPS ARE CRACKED AROUND RBL 9 FLOORBEAM. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW RT 280 CROSSBEAM CLIPS AT RBL 9 FLOORBEAM, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (RT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 650AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 650AB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 550DB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550DB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 510BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 510BB, REF REO. FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (RT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 640BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 640BB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 540DB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540DB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: BULKHEAD — GOUGED (AFT) · airframe 43,866 hrs · 41,189 cycles

FS 621 BULKHEAD FWD SIDE HAS 3 GOUGES AT APPROXIMATELY WL 103 & RBL 18, RBL 27, RBL 36, MARKED. C-CHECK RO 11/23/2020. BLENDED OUT DAMAGE TO A SMOOTH SURFACE AT FS 621 WL 103 & RBL 18, RBL 27, RBL 36, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 550FB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550FB, REF REO. FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (RT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 640CB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 640CB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 550EB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550EB, REF REO, FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. TASK CARD COMPLIED WITH. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 540AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540AB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 540FB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540FB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 540EB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540EB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 540BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540BB, REF REO, FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, DATED 2014-02-05, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (RT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 650BB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 650BB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1003-SKY. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (RT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 610AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 610AB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 540CB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 540CB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: ISOLATOR — BENT (PRESSURE BLKHD) · airframe 43,866 hrs · 41,189 cycles

FS 621 BULKHEAD FWD SIDE HAS 14 ISOLATOR BRACKETS BENT/DEFORMED, MARKED. C-CHECK RO 11/23/2020. REMOVED AND REPLACED 14 EA ISOLATOR BRACKET ASSEMBLY FROM FWD SIDE OF FS 621 BULKHEAD, REF CRJ200 SRM, NO LEAKS NOTED.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 550AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550AB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. TASK CARD COMPLIED WITH. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21.

Part: ISOLATOR — LOOSE (PRESSURE BLKHD) · airframe 43,866 hrs · 41,189 cycles

FS 621 BULKHEAD FWD SIDE HAS 3 ISOLATORS LOOSE, MARKED. C-CHECK RO 11/23/2020. REPLACED 6 EA SOLID RIVETS ON FS 621 BULKHEAD FWD SIDE HAS 3 ISOLATORS, REF CRJ200 SRM.

Part: SKIN — CORRODED (RT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 640EB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON RT WING PLANK LAND AT 640EB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. COMPLIED WITH TASK CARD. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 550CB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550CB, REF REO, FOUND TO BE WITHIN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. TASK CARD COMPLIED WITH. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: RIVET — GOUGED (PRESSURE BLKHD) · airframe 43,866 hrs · 41,189 cycles

FS 621 BULKHEAD FWD SIDE HAS 4 GOUGES RIVET HEADS AT APPROXIMATELY WL 87 & RBL 9, RBL 18, RBL 27, RBL 36, MARKED. C-CHECK RO 11/23/2020. REMOVED AND INSTALLED NEW FASTENERS ON FWD SIDE OF FS 621 BULKHEAD AT APPROXIMATELY WL 87 & RBL 9, RBL 18, RBL 27, RBL 36, REF CRJ200 SRM.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 550HB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 550HB, REF REO. FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (LT WING) · airframe 43,866 hrs · 41,189 cycles

WING PLANK LAND AT 510AB HAS FRETTING CORROSION, MARKED. C-CHECK RO 11/23/2020. REMOVED CORROSION ON LT WING PLANK LAND AT 510AB, REF REO, FOUND TO BE WITH IN LIMITS. COMPLIED WITH ALL STEPS OF REO, NO LEAKS NOTED. BONDING TEST GOOD, REF CRJ 200 AMM TUC7801 DUE 28FEB21. COMPLIED WITH TASK CARD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 43,866 hrs · 41,189 cycles

LT INBOARD FLAP VANE LEADING EDGE OUTBOARD SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED CHAFE DAMAGE ON LT INBOARD FLAP VANE LEADING EDGE OUTBOARD SIDE, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW VANE CAP AT LT INBOARD FLAP LEADING EDGE OUTBOARD SIDE, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 43,866 hrs · 41,189 cycles

LT INBOARD FLAP VANE TRAILING EDGE MID UPPER SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED THE CHAFE DAMAGE FROM THE LT INBOARD FLAP VANE UPPER TRAILING EDGE SKIN, REF CRJ200 SRM, FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO. SEE CONTINUATION FOR DETAIL.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 43,866 hrs · 41,189 cycles

RT INBOARD FLAP VANE LEADING EDGE INBOARD SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED CHAFE DAMAGE FROM RT INBOARD FLAP VANE LEADING EDGE, INBOARD SIDE, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RT INBOARD FLAP VANE CAP AT LEADING EDGE INBOARD SIDE, REF CRJ200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD.

Part: STIFFENER — CHAFED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

THE REAR PRESSURE BULKHEAD, VERTICAL STIFFENER AT THE CENTER, IS CHAFED IN THE UPPER PORTION OF ITS HEIGHT, ON THE AFT LEG SURFACE AND AFT CORNER. (C-CHECK) RO:01/25/2019 REPAIRED PRESSURE BULKHEAD VERTICAL STIFFENER AT THE CENTER IAW REO.

Part: FLOOR SKIN — DENTED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

PRESSURE FLOOR SKIN DENT FS516 RBL13. (C-CHECK) RO:01/25/2019 PRESSURE FLOOR SKIN DENT AT FS516 RBL13 IAW REO.

Part: FLOOR SKIN — DENTED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

PRESSURE FLOOR SKIN DENT FS501 RBL15 (C-CHECK) RO:01/25/2019 REPAIRED DENT IAW SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

FLOOR BUTTSTRAP AT FS559.00 FROM LBL27-LBL43 HAS EXFOILIATED CORROSION. (C-CHECK) RO:01/25/2019 REPAIRED FLOOR BUTTSTRAP AT FS559.00 FROM LBL27-LBL43 IAW REO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

RT SIDE STRAP AT FS559.00 BETWEEN RBL 27.0 TO RBL 41.75 IS CORRODED. (C-CHECK) RO:01/25/2019 REPAIRED RT SIDE STRAP AT FS 559.00 BETWEEN RBL 27.0 TO RBL 41.75 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

FLOORBEAM CAP - INBOARD AND OUTBOARD FLANGES ARE CORRODED AROUND THE FASTENER HOLES. LBL27, FS569.5 €“ FS621.00. (C-CHECK) RO:01/25/2019 REMOVED AND REPLACED FLOORBEAM CAP AT LBL27 BETWEEN FS 569.5 TO FS621 IAW SRM AND REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

SEVERAL AREAS OF CORROSION ON FRAME AT FS589 BETWEEN STRG 21L AND 23L. (C-CHECK) RO:01/25/2019 REPAIRED DAMAGED AREA OF FRAME AT FS589 BETWEEN STR 21L AND STR 23L IAW REO.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

LT PRESSURE FLOOR SILL HAS CORROSION IN MULTIPLE PLACES BETWEEN FS 409+128 €“ FS 559 (C-CHECK) RO:01/25/2019 REMOVED CORROSION FROM LT PRESSURE FLOOR SILL IN MULTIPLE PLACES BETWEEN FS 409+128 €“ FS 559.00 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

RBL 9 FLOORBEAM FS 409.00+48 TO 409.00 +112 APPROX. HAS CORROSION. (C-CHECK) RO:01/25/2019 REPAIRED RBL 9 FLOORBEAM AT FS409.00+48 TO FS409+112 IAW REO.

Part: VANE — DAMAGED (TE FLAP) · airframe 41,349 hrs · 38,257 cycles

REPLACE LT INBOARD FLAP CENTER VANE CAP. (C-CHECK) RO:01/25/2019 REPLACED LT IB FLAP CENTER VANE CAP WITH NEW P/N 601R14303-51 IAW REO.

Part: PANEL — CHAFED (LT AILERON) · airframe 41,349 hrs · 38,257 cycles

LEFT HAND AILERON LOWER FIXED LEADING EDGE PANELS HAVE CHAFES. (C-CHECK) RO:01/25/2019 LT AILERON INBD LEADING EDGE PANEL REMOVED AND REPLACED WITH NEW PANEL (P/N CC670-13053-1) IAW SRM.

Part: HINGE — SCRATCHED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

PAX DOOR HINGE FUSELAGE SIDE HAS MULTIBLE SCRATCH'S AND NICKS. (C-CHECK) RO:01/25/2019 / REMOVED AND REPLACED WITH NEW FUSELAGE SIDE PAX DOOR HINGE IAW REO.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,349 hrs · 38,257 cycles

STRAP AT FS349.00 STR 3L HAS CORROSION AT MULTIPLE PLACES. (C-CHECK) RO:01/25/2019REMOVED AND INSTALLED NEW STRAP AT FS349.00 STGR 3L IAW SRM.

Part: SKIN — DENTED (BS 605-621) · airframe 38,204 hrs · 34,797 cycles

LEFT SIDE OF FUSELAGE SKIN HAS A DENT BETWEEN BS 605 AND 621, STRINGERS 21 - 22L. PERFORMED PERMANENT REPAIR IAW REO AND SRM.

Part: VANE — UNSECURE (RAM AIR EXHAUST) · airframe 34,140 hrs · 30,079 cycles

LEFT RAM AIR EXHAUST DUCT VANE IS MISSING ADHESIVE. CLEANED AND REAPPLIED ADHESIVE TO LT RAM AIR EXHAUST DUCT VANE IAW REO.

Part: VANE — UNSECURE (RAM AIR EXHAUST) · airframe 34,140 hrs · 30,079 cycles

RIGHT RAM AIR EXHAUST DUCT VANE IS MISSING ADHESIVE, C-CHECK, RO 12/13/14, CLEANED AND REAPPLIED ADHESIVE TO RT RAM AIR EXHAUST DUCT VANE IAW REO.

Part: NUT — UNSECURE (CONTROL COLUMN) · airframe 34,140 hrs · 30,079 cycles

CO-PILOTS AILERON CONTROL COLUMN HAS CLICKING. RETORQUED COPILOTS CONTROL COLUMN NUT ON FWD SIDE OF THE CONTROL WHEEL SHAFT REF REO AND AMM.

Part: RADOME — OUT OF TOLERANCE · airframe 34,140 hrs · 30,079 cycles

CLEARANCE BETWEEN FUSELAGE SKIN AND RADOME FAILED GAP CHECK. TRIMMED RADOME TO ACHIEVE PROPER CLEARANCE IAW REO.

Part: ANGLE — GOUGED (BS 621 BULKHEAD) · airframe 34,140 hrs · 30,079 cycles

AFT PRESSURE BULKHEAD FORWARD FACE REINFORCEMENT ANGLE, 47 INCHES ABOVE FLOOR IS GOUGED ON UPPER FLANGE EDGE. REPAIRED THE BS 621 BULKHEAD REINFORCEMENT ANGLE. REPAIR IS WITHIN LIMITS IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 534) · airframe 34,140 hrs · 30,079 cycles

FLOOR SUPPORT CORRODED AT BS 534, RBL 39. REMOVED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 489) · airframe 34,140 hrs · 30,079 cycles

LEFT FLOOR SUPPORT HAS CORROSION AT BS 489, LBL 39. REMOVED CORROSION IAW REO.

Part: CONNECTOR — MISSING (WIRE HARNESS) · airframe 34,140 hrs · 30,079 cycles

FWD GALLEY AREA, WIRE BUNDLE AT BS 314, JUST ABOVE FLOOR, FWD OF SERVICE DOOR, IS MISSING FLEXIBLE CONDUIT AT CONNECTOR, INSTALLED NEW TUBING FOR SERVICE DOOR WARNING SYSTEM IAW REO. PERFORMED OPS TEST OF THE SERVICE DOOR WARNING SYSTEM TEST GOOD IAW AMM.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 34,140 hrs · 30,079 cycles

FLOOR SUPPORT ANGLE FROM BS 409.128 - 559 CORRODED. REMOVED CORROSION IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 34,140 hrs · 30,079 cycles

FLOOR SUPPORT ANGLE FROM BS 409.128 - 559 CORRODED. REMOVED THE CORROSION IAW REO.

Part: FLOOR PANEL — CRACKED (BS 459) · airframe 34,140 hrs · 30,079 cycles

PRESSURE FLOOR SKIN PANEL HAS A CRACK AT BS 459, RBL 5. REPAIRED PRESSURE FLOOR PANEL IAW REO.

Part: BULKHEAD — GOUGED (BS 621) · airframe 34,140 hrs · 30,079 cycles

AFT PRESSURE BULKHEAD FORWARD FACE GOUGED . REPAIRED AFT PRESSURE BULKHEAD. REPAIR AREAS ARE WITH IN LIMITS IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,140 hrs · 30,079 cycles

LEFT WING INBD FLAP VANE HAS CHAFE DAMAGED. REPAIRED LT WING INBD FLAP VANE IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 34,140 hrs · 30,079 cycles

RIGHT WING INBD FLAP VANE CHAFED AT APPROXIMATELY WS 56.30. REPAIRED RT WING INBD FLAP VANE IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,140 hrs · 30,079 cycles

LEFT WING I/B FLAP VANE HAS CHAFE DAMAGE. REPAIRED IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 34,140 hrs · 30,079 cycles

LEFT WING INBD FLAP VANE HAS CHAFE DAMAGE ON OTBD L/E CAP. , REPAIRED LT WING INBD FLAP VANE CHAFE DAMAGE ON OTBD L/E CAP, IAW REO.

Part: PANEL — FAILED · airframe 34,140 hrs · 30,079 cycles

VISOR PANEL 326AR FAILED GAP CHECK. REPAIRED IAW REO.

Part: PANEL — OUT OF TOLERANCE · airframe 34,140 hrs · 30,079 cycles

VISOR PANEL 326AL FAILED GAP CHECK. RECONTOURED VISOR PANEL 326AL, REF REO.

Part: PANEL — FAILED · airframe 34,140 hrs · 30,079 cycles

VISOR PANEL 326BR FAILED GAP CHECK. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 571-589) · airframe 34,140 hrs · 30,079 cycles

FUSELAGE SKIN DENTED BELOW THE CARGO DOOR BETWEEN BS 574 - 589 AND S20-21L. REPAIRED THE DAMAGE IAW EA.

Part: TIRE — FAILED (RT MLG) · airframe 33,447 hrs · 29,294 cycles

DURING POST FLIGHT INSPECTION, FOUND RT INBD TIRE BLEW OUT ON LANDING. R & R INBD & OTBD ON RT SIDE MAIN TIRES.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,335 hrs · 29,167 cycles

FWD EMERGENCY LIGHT ON RT OF FUSELAGE OVER WING INOPERATIVE. R & R BURNED OUT BULB, FWD EMERGENCY LIGHT ON RT OF FUSELAGE WITH A SERVICEABLE UNIT. OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 32,971 hrs · 28,783 cycles

EMERGENCY EXIT LIGHT, FLOOR BLUE STRIP DOES NOT ILLUMINATE AT ROW 6-7. RECONNECTED EMERGENY EXIT STRIP TOGETHER BY ROW 6-7.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 32,251 hrs · 27,959 cycles

LOST HYD 3 FLUID DOWN TO 5%. MANUALLY EXTENDED GEAR. FLT 2965 REPLACED HYD FLEX LINE FROM 3A PUMP TO DAMPENERS. NO LEAKS NOTED. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,259 hrs · 26,941 cycles

EMERGENCY OVERHEAD LIGHT BURNED OUT. FLT#2989 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,388 hrs · 26,004 cycles

LAST OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 2930) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,263 hrs · 25,864 cycles

AFT EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 2974) RELAMPED EMERGENCY LIGHT.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,127 hrs · 25,727 cycles

CARGO DOOR BEAM HAS CRACKED ANGLE AT FS 621 BULKHEAD. (C-CHECK) REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,127 hrs · 25,727 cycles

FS 574 TO FS 621 LBL 27 FLOORBEAM HAS CORROSION ON OUTBOARD NUT PLATE HOLES. (C-CHECK) REPAIRED FLOORBEAM FROM FS 574 TO FS 621 ON LBL 27 ON OUTBOARD SIDE IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 30,127 hrs · 25,727 cycles

FOUND CRACK ON FS 409+128 VERTICAL POST AT RBL 18 OUTBOARD POST ON AFT LOWER FLANGE AT LOWER FASTENER HOLE. (C-CHECK) INSTALLED FS 409+128 VERTICAL POST AT RBL 18 OUTBOARD POST IAW SRM AND REO.

Part: POST — CRACKED (FUSELAGE) · airframe 30,127 hrs · 25,727 cycles

CRACK NOTED ON FS 409.0+128 VERTICAL POST AT LBL 18.00 WL 69.00 OUTBOARD AFT RADIUS. (C-CHECK) REMOVED AND INSTALLED LBL 18 POST AT FS 409+128 REFERENCE IAW SRM AND REO.

Part: POST — CRACKED (FUSELAGE) · airframe 30,127 hrs · 25,727 cycles

CRACK NOTED ON FS 409.0+128 VERTICAL POST AT RBL 18.00 WL 69.00 INBOARD AFT RADIUS. (C-CHECK) REPLACED FS 409+128 POST AT RBL 18.00 IAW SRM AND REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,127 hrs · 25,727 cycles

CRACK NOTED AND MARKED ON FS 621 AFT PRESSURE BULKHEAD FWD FACE AT BL 0.00 WL 110.43. (C-CHECK) REPAIRED FS 621.0 BULKHEAD AT APPROXIMATELY BL 0.00 AND WL 110.43 IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,127 hrs · 25,727 cycles

PASSENGER DOOR LOWER SILL AREA - CORROSION ON ANGLE AT 3 LOCATIONS, AROUND CONNECTOR AND PROX SENSOR LOCATIONS. (C-CHECK) REPLACED PAX DOOR SILL, IAW SRM.

Part: HARNESS — BINDS (FO SEAT) · airframe 28,480 hrs · 24,048 cycles

FIRST OFFICER'S SHOULDER HARNESS BINDS. (FLT 2850) REPLACED FIRST OFFICER'S RESTRAINT SYSTEM ASSEMBLY PER AMM. P/N OFF: 5001-1-001-2396

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,234 hrs · 23,786 cycles

RIGHT OVERWING MIDDLE EXIT EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,205 hrs · 23,758 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2952) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — OUT OF ADJUST (CABIN) · airframe 28,136 hrs · 23,687 cycles

NR 7 EMERGENCY LIGHT STRIP IS OUT. (SERVICE) ADJUSTED CONNECTOR.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,729 hrs · 23,312 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6216) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,672 hrs · 23,261 cycles

NR 2 OVERHEAD AND NR 1 EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 6517) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,592 hrs · 23,201 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6249) RELAMPED EMERGENCY LIGHT.

Part: SHOULDER BELT — BINDS (COCKPIT) · airframe 27,289 hrs · 22,932 cycles

F/O REPORTS LEFT SHOULDER STRAP LOCKS UP WHEN MOVING FORWARD. (FLT 6440) REPLACED F/O'S SHOULDER STRAP HARNESS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,220 hrs · 22,882 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6206) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,130 hrs · 22,818 cycles

SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 6521) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,130 hrs · 22,818 cycles

LEFT WING AFT EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 6521) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,101 hrs · 22,798 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6360) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,580 hrs · 22,401 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6930) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,498 hrs · 22,333 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 6532) RELAMPED EMERGENCY LIGHT.

Part: CAM — OUT OF ADJUST (MAIN DOOR) · airframe 26,462 hrs · 22,303 cycles

MCD WOULD NOT OPEN. (FLT 6245) ADJUSTED THE AFT SPIGOT AND LATCH CAM MECHANISMS.

Part: LINKAGE — LACK OF LUBE (CABIN DOOR) · airframe 26,462 hrs · 22,303 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6962) CLEANED AND LUBED INNER DOOR LINKAGE.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 26,383 hrs · 22,238 cycles

PAX DOOR WILL NOT OPEN. (FLT 7036) RE-RIGGED PASSENGER DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,360 hrs · 22,215 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: ROLLER CAM — LACK OF LUBE (CABIN DOOR) · airframe 26,360 hrs · 22,215 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. (FLT 6350) CLEANED AND LUBED UPPER ROLLER CAM ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,177 hrs · 22,043 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6919) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,177 hrs · 22,043 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6585) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,728 hrs · 21,667 cycles

FS 559 PRESSURE BULKHEAD IS CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.

Part: WEB — CRACKED (FUSELAGE) · airframe 26,085 hrs · 21,966 cycles

FS 280 LOWER FLANGE OF WEB CRACKED IN RADIUS. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,661 hrs · 20,776 cycles

BULB BURNED OUT IN EMERGENCY LIGHT "EXIT" CLUSTER ADJACENT TO SERVICE DOOR ON GALLEY. (FLT 6220) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,563 hrs · 20,684 cycles

THE FIRST CABIN EMERGENCY FLOOD LIGHT IN THE CEILING IS BURNED OUT. (FLT 6279) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,511 hrs · 19,792 cycles

EMERGENCY CEILING LIGHT NR 3 INOP. (FLT 5843) RELAMPED EMERGENCY LIGHT.

Part: FUEL CONTROL — MALFUNCTIONED (RT ENGINE) · airframe 22,049 hrs · 18,576 cycles

FLT 6175, RIGHT ENGINE OVERTEMPED AND LOST OIL PRESSURE IN CRUISE. FUEL CONTROL REPLACED, ALL INSPECTIONS AND BOROSCOPE FOUND NORMAL CONDITIONS, ENGINE RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,153 hrs · 17,854 cycles

CEILING LEVEL EMERGENCY LIGHT AT ROW 2 INOP. (FLT 6760) RELAMPED EMERGENCY LIGHT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,502 hrs · 18,137 cycles

REAR PRESSURE BULKHEAD CLIPS BROKEN. (C CHECK) REPAIRED PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,502 hrs · 18,137 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,502 hrs · 18,137 cycles

FORWARD BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,502 hrs · 18,137 cycles

FS 280 BEAM ANGLE CRACKED. (C CHECK) REPAIRED PER REO.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 21,502 hrs · 18,137 cycles

FS 280 BEAM SUPPORT CRACKED. (C CHECK) REPLACED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,919 hrs · 16,890 cycles

FLT 5838 - LEFT WING AFT EMERGENCY EXIT LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,919 hrs · 16,890 cycles

FLT 5838 - MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED.

Part: SHUTOFF VALVE — INOPERATIVE (RIGHT) · airframe 17,856 hrs · 15,086 cycles

FLT 6590 - DURING CLIMB-OUT, THE CABIN WOULD NOT PRESSURIZE. REPLACED RIGHT PRSOV PER AMM 21-52-43 AND PRESSURE TRANSDUCER IAW MM 21-51-40. OPS CHECK GOOD AT THIS TIME.

Part: ACTUATOR — MALFUNCTIONED (NLG STEERING) · airframe 17,640 hrs · 14,903 cycles

FLT 5966 - NOSE GEAR FAILED TO SHOW UP AND LOCKED. REPLACED LEFT AND RIGHT STEERING ACTUATORS PER 32-52-01 AND REPACKED NOSE STRUT AND SERVICED PER 32-21-25.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 17,610 hrs · 14,877 cycles

FLT 5983 - STEERING INOP CAUTION MESSAGE APPEARED AFTER TAKEOFF FOLLOWED BY A GEAR DISAGREE WARNING MESSAGE. REPLACED NLG PRIORITY VALVE ASSEMBLY REF CRJ 200 AMM 32-33-15 AND NLG SELECTOR VALVE IAW CRJ 200 AMM 32-33-10. OPS CHECK AND LEAK CHECK GOOD, PN 4622 SN/OFF 1609A PN 750006000, SN/OFF 0221T.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 16,596 hrs · 14,022 cycles

RIGHT THRUST REVERSER NR 4 MAIN TRACK IS CRACKED, FOUND AT C-CHECK. REPLACED NR 4 THRUST REVERSER TRACK PER CRJ200 AMM 70-34-11-400-801.

Part: FITTING — CORRODED (RT ENGINE) · airframe 16,596 hrs · 14,022 cycles

RIGHT ENGINE THRUST FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED ENGINE THRUST FITTING PER CRJ200 AMM 71-22-01-400-801.

Part: FITTING — CORRODED (LT ENGINE) · airframe 16,596 hrs · 14,022 cycles

FOUND AT C-CHECK, LEFT ENGINE THRUST FITTING IS CORRODED. INSTALLED NEW ENGINE THRUST FITTING PER CRJ200 AMM 71-22-01-400-801.

Part: WEB — CRACKED (PAX DOOR) · airframe 16,596 hrs · 14,022 cycles

PAX DOOR FORWARD AND AFT WEB IS CRACKED, FOUND AT C-CHECK. INSTALLED WEB REPAIR PARTS PER CRJ200 REO 601R-52-11-702 (REV A).

Part: FRAME — DAMAGED (FUSELAGE) · airframe 16,596 hrs · 14,022 cycles

FRAME BELOW RIGHT MAIN GEAR UPLOCK ACTUATOR IS DAMAGED FROM DOOR ROD, FOUND AT C-CHECK. PERFORMED REPAIR PER REO 601R-53-41-568.

Part: NUT CLIP — CRACKED (BS 484) · airframe 16,596 hrs · 14,022 cycles

FOUND AT C-CHECK, FLOORBEAM CLIP AT FS484 LBL36 IS CRACKED. INSTALLED REPAIR ANGLES PER CRJ200 REO 601R 53-41-059 STEPS 8, 11, 12 AND 14.

Part: FRAME — DEFORMED (FUSELAGE) · airframe 16,596 hrs · 14,022 cycles

FRAME BELOW LEFT MAIN GEAR UPLOCK ACTUATOR HAS DAMAGE FROM DOOR ROD, FOUND AT C-CHECK. INSTALLED ALL REPAIR PARTS ON LEFT MAIN GEAR SUPPORT STRUCTURE PER REO 601R-53-41-568 REV- A.

Part: WEB — CRACKED (PAX DOOR) · airframe 16,596 hrs · 14,022 cycles

PAX DOOR FORWARD WEB UPPER CORNER IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS ON PAX DOOR PER REO NO 601R-52-11-1299.

Part: CONTROLLER — MALFUNCTIONED (AUTO DEPLOY) · airframe 16,042 hrs · 13,541 cycles

FLT 6020 - ON ROTATION AND WEIGHT OFF WHEELS, THE ADG DEPLOYED. REPLACED ADG AUTO DEPLOY CONTROLLER IAW MM 24-23-15, P/N 82046-5 S/N OFF 1149.

Part: ACM — SMOKE (LEFT) · airframe 15,646 hrs · 13,185 cycles

LEFT PACK TEMPERATURE IS HOT. NOT CONTROLLABLE IN AUTO OR MANUAL MODES. SMOKE CAME THROUGH COCKPIT VENTS UNTIL LEFT PACK WAS TURNED OFF. REPLACED LEFT ACM AND LEFT PRSOV. OPS CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,024 hrs · 12,638 cycles

AN EMERGENCY LIGHT INOP IN MAIN CABIN CEILING. RELAMPED EMERGENCY LIGHT BETWEEN ROW 4 AND 5 AS REQUIRED, OPS CHECK GOOD.

Part: TRANSMITTER — INOPERATIVE (RUDDER) · airframe 12,005 hrs · 10,080 cycles

RUDDER INDICATION DOES NOT WORK. REPLACED RUDDER POSITION TRANSMITTER IAW MM 27-24-05. OPERATIONAL CHECK GOOD IAW MM 27-24-05.

Part: INTERCOSTAL — CRACKED (BS 625 S14L) · airframe 12,467 hrs · 10,456 cycles

FS 625.00, STR 14L INTERCOSTAL CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW REO 601R-53-61-100 REV NC AND 601R-53-61-422 REV NC.

Part: INTERCOSTAL — CRACKED (BS 625 S14R) · airframe 12,467 hrs · 10,456 cycles

FS 625.00 STR 14R INTERCOSTAL CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW REO 601R-53-61-100 REV NC AND 601R-53-61-422 REV NC.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,467 hrs · 10,456 cycles

FUSELAGE, PULLEY INTERCOSTAL HAS A CRACKED I/B ANGLE & O/B FLANGE, FS 484.00, RBL 27 + RBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV A.

Part: FRAME — CRACKED (BS 654 S13-14R) · airframe 12,467 hrs · 10,456 cycles

AFT EQUIP BAY FS 654.5 BETWEEN STR 13R-14R, FRAME WORN ON AFT I/B EDGE FROM APU EXHAUST DUCT. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED AS PER REO 610R-53-61-1731 REV NC.

Part: MCU — MALFUNCTIONED (HORIZONTAL STAB) · airframe 11,665 hrs · 9,792 cycles

"STAB CH 1 INOP" STATUS MSG CAME ON EN ROUTE TO ORD AND REMAINED ON AFTER SHUTDOWN. REPLACED HORIZONTAL STABILIZER TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01, 27-42-05 AND CAPT'S HORIZONTAL STAB TRIM SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD, P/N MOTOR CONTROL UNIT: 7062-3 S/N OFF: 216 P/N HSTA: 8396-3 S/N OFF: 778.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZONTAL STAB) · airframe 11,590 hrs · 9,726 cycles

STAB CHANNEL 1 KEEPS KICKING OFF. REPLACED HSTCU IAW AMM 27-41-01 AND REPLACED FO'S PITCH DISCONNECT SWITCH IAW AMM 27-41-30. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,924 hrs · 8,350 cycles

FOUR OF THE 12 EMERGENCY FLOOR LEVEL LIGHTING INOPERATIVE. REPLACED CABLE ADAPTER FOR EMERGENCY FLOOR LEVEL LIGHTING AT SEAT 12CD. OPERATIONAL CHECK GOOD.

Part: SWITCH — INOPERATIVE (PITCH TRIM) · airframe 9,758 hrs · 8,206 cycles

F/O TRIM MOSTLY INOPERATIVE. REPLACED F/O'S PITCH TRIM SWITCH IAW CRJ MM 27-41-05. OPERATIONAL CHECKS GOOD.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 8,879 hrs · 7,463 cycles

WHILE LEVEL AT FL350 LEFT WINDSHIELD SHATTERED. REMOVED AND REPLACED LEFT WINDSHIELD IAW 56-11-01. P/N OFF 601R33033-13, S/N OFF 61030H8727.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,735 hrs · 7,316 cycles

OVERHEAD EMERGENY LIGHT INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AS NEEDED, OPERATIONAL CHECK GOOD.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 7,929 hrs · 6,686 cycles

SHORTLY AFTER DISCONNECTING THE AUTOPILOT THE ELEVATOR JAMS. COULD NOT DUPLICATE PROBLEM WITH AUTOPILOT SYSTEM. OPS CHECKS GOOD IAW MM 32-11-00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,424 hrs · 7,068 cycles

LEFT FS 625 OBLIQUE ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND INSTALLED NEW ANGLE P/N: 601-35012-51 IAW CRJ 200 SRM 51-42-06.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 8,424 hrs · 7,068 cycles

SUPPORT ANGLES CRACKED RBL 9.0 AND LBL 9.0 FS 280.0 WL 73.5. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED SUPPORT ANGLES AT FS 280.00, WL 73.5, RBL 9, LBL 9, IAW CRJ 200 SRM 51-42-06 AND 51-42-20.

Part: BPSU — MALFUNCTIONED (LEFT) · airframe 7,411 hrs · 6,204 cycles

EN ROUTE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. LANDED FLAPS 0 AT SLC. REPLACED LEFT SIDE BPSU PER CRJ MM 27-51-10. OPS CHECK GOOD.

Part: TURBINE BLADES — TORN (RT ENGINE) · airframe 7,166 hrs · 5,977 cycles

NUMEROUS RIGHT ENGINE 7TH STAGE ROTOR BLADES DAMAGED, TORN. REMOVED AND REPLACED RIGHT ENGINE IAW RII 71-401.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,109 hrs · 5,913 cycles

RIGHT WING CENTER EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED RT WING CENTER EMERGENCY LAMP AS REQUIRED. OPS CHECK GOOD.

Part: CONTROL UNIT — FAILED (GROUND SPOILERS) · airframe 6,607 hrs · 5,474 cycles

OUTBOARD GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT STATUS MESSAGE ON GROUND. RETURNED TO GATE. REPLACED NR 1 SECU. OPS CHECKS GOOD IAW 27-00-00. P/N: 44-164-05, S/N OFF: 1244.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 6,109 hrs · 5,072 cycles

AFTER TAKEOFF, UPON GEAR RETRACTION, EICAS WARNINGS ''NOSE DOOR OPEN'' AND ''GEAR DISAGREE'' ILLUMINATED. RETURNED TO LAX. REMOVED AND REPLACED NLG SELECTOR VALVE AND REPLACED PROX SENSOR. SWUNG GEAR, ALL CHECKS GOOD. NO LEAKS NOTED IAW MM 32-33-00.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 5,985 hrs · 4,950 cycles

HORIZONTAL STAB TRIM FAILS CHANNEL 2 ON PREFLIGHT TEST. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT. OPS CHECK GOOD IAW RII 27-415. MOTOR CONTROL UNIT PN: 7062-3 SN OFF: 961 SN ON: 218.

Part: ANGLE — CRACKED (INTERCOSTAL) · airframe 4,248 hrs · 3,527 cycles

FS 625.0 RIGHT INTERCOSTAL ANGLE AT STR 14R CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06. P/N: 601-35012-52.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,248 hrs · 3,527 cycles

FS 621.0 RT & LT FLOOR SUPPORT ANGLES CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREAS IAW CRJ REO 601R-53-61-117 REV A. ANGLE P/N: 601R-53-61-117-2, REPAIR ANGLE P/N: 601R-53-61-117-4.

Part: CHANNEL — CRACKED (CARGO DOOR STR 1) · airframe 4,314 hrs · 3,568 cycles

CARGO DOOR FORWARD TRACK CHANNEL STR 16L IS CRACKED. FOUND DURING C CHECK INSPECTION. REPAIRED DAMAGED CHANNEL IAW CRJ SRM 53-61-23, 51-24-16, 51-40-11, 51-25-06, 51-25-00, 51-42-06 & 51-24-11.

Part: SILL — CRACKED (CARGO BAY) · airframe 4,248 hrs · 3,527 cycles

CARGO DOOR FLOOR SILL FS 575.5 CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-620 'NC'. NDT-HFEC CARRIED OUT IAW REO 601R-53-61-620. NO CRACKS NOTED.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 3,754 hrs · 3,175 cycles

STAB AND MACH TRIM DISENGAGED AT THE GATE WITH A CAUTION MESSAGE. REENGAGED SYSTEM AND STAB CHANNEL 2 WOULD NOT REENGAGE. REPLACED HORIZONTAL STAB ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01. OPS CHECKED GOOD.

Part: SERVICE DOOR — OPEN (ELECTRICALF) · airframe 3,075 hrs · 2,533 cycles

LOUD WHINE COMING FROM FRONT OF THE AIRCRAFT AFTER TAKEOFF. NOISE INCREASED WITH SPEED INCREASE. RETURNED TO LAX. FOUND NOSE ELECTRICAL SERVICE PANEL DOOR OPEN. INSPECTED DOOR, FOUND NO DAMAGE. ALL CHECKS GOOD.

Part: DOOR — UNLATCHED (AVIONICS BAY) · airframe 2,132 hrs · 1,701 cycles

AFTER TAKEOFF THE CREW HEARD A "POP" AND THE AVIONICS BAY DOOR WARNING LIGHT ILLUMINATED. RETURNED TO BOI. FOUND AVIONICS DOOR LATCH NOT SECURED. INSPECTED AND LATCHED AVIONICS BAY DOOR. NO DEFECTS FOUND.

Part: BPSU — MALFUNCTIONED (LEFT) · airframe 1,770 hrs · 1,346 cycles

ON APPROACH FLAPS FAILED WHEN FLAPS SELECTED 8 DEGREES. FLAPS FAILED AT 0 DEGREES. RAN QRH. REPLACED LEFT BPSU AND PERFORMED RIGGING PER CRJ MM 27-51-10 AND CYCLED FLAPS SEVERAL TIMES. OPS CHECK GOOD. S/N OFF: 1241B

Part: GASKET — DEFECTIVE (RT COWL) · airframe 1,455 hrs · 1,014 cycles

CLIMBING THROUGH 2,000 FT R 14TH STAGE WARNING MESSAGE WAS GENERATED. RETARD THRUST LEVER PER QRH. MESSAGE WENT OUT. RETURNED TO AIRPORT PER QRH. RT ENGINE DUCT FAIL LIGHT, R 14TH DUCT LIGHT ILLUMINATED WITH RED EICAS MESSAGE FLOW LINE BETWEEN RT BLEED SOV, NOSE COWL AND WING SOV AT POWER ABOVE 80 PERCENT N1. RETURNED TO FIELD. REMOVED AND REPLACED A DEFECTIVE GASKET FOR THE RIGHT ENGINE COWL ANTI-ICE DUCT AT THE PYLON DISCONNECT. OPERATED THE RIGHT ENGINE AT T/O POWER FOR 20 MINUTES WITH NO FURTHER PROBLEMS. NO LEAKS NOTED.