N927SW

Part: FUEL SYS — LEAKING (APU) · airframe 44,315 hrs · 37,677 cycles

JET FUEL SMELL COMING FROM THE VENTS IN FLIGHT DECK AND MADE OUR EYES WATER. THIS HAPPENED ONLY WHEN PACK OUTPUT TEMP WAS MORE THAN 50C. ASKED FA AND HE DID NOT NOTICE ANY SMELL IN THE CABIN. FLIGHT 5104-FILED CLOSED. REF CRJ 200 FIM, FDE-ABNORMAL SMELL FROM FLIGHT DECK OR CABIN. OPENED BOTH ENGINE COWLINGS AND INSPECTED FOR INDICATIONS OF FUEL LEAK AND NONE NOTED. CLOSED AND SECURED BOTH ENGINE COWLINGS AS REQUIRED. GAINED ACCESS TO BOTH PACK COALESCAR BAGS AND NO CONTAMINATION NOTED. CLOSED WATER SEPARATOR COVERS AS REQUIRED. OPENED APU CONTAINMENT CASE AND FOUND BOTTOM OF CASE TO BE COVERED IN FUEL. CLEANED UP FUEL FROM APU CONTAINMENT CASE AND STARTED APU AND FOUND FUEL LEAKING FROM APU FUEL SHUTOFF SOLENOID FITTINGS JUST GOING IN TO FUEL CONTROL. GROUND RAN BOTH ENGINES FOR APPROX 30 MINUTES WITH BOTH PACKS FULL HOT AND NO FUEL SMELL COMING FROM EITHER PACK. SUSPECT THE APU FUEL LEAKING IN CONTAINMENT CASE IS BEING SUCKED IN TO BLEEDS WHEN APU IS USED AS THE BLEED SOURCE FOR BOTH PACKS AND CAUSING FUEL SMELL. PLEASE REFERENCE AML 490182. PLEASE REFERENCE AML 490184 FOR NEW DISCREPANCIES.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAP) · airframe 43,987 hrs · 37,346 cycles

DURING CRUISE AT APPROX .77/290KIAS AND FL320 THE FLAPS DEPLOYED MOMENTARILY WITHOUT MOVEMENT OF THE FLAP LEVER. THE INDICATION DID NOT PASS 8 DEGREES, WITH A MAXIMUM DEPLOYMENT OF APPROX 3-5 DEGREES. SIMULTANEOUSLY THE AIRCRAFT ENTERED A UNCOMMANDED CLIMB OF APPROX 2-300 REQUIRING DISCONNECTION OF THE AUTOPILOT TO RETURN TO STABLE FLIGHT. THE FLAPS RETURNED TO 0 DEGREE STOWED POSITION WITHIN APPROX 5 SECONDS WITHOUT ANY MANIPULATION OF THE FLAP LEVER. SUBSEQUENT ARRIVAL, APPROACH, AND LANDING WAS UNEVENTFUL WITH THE FLAP SYSTEM OPERATING AS EXPECTED AND WITHOUT FURTHER ISSUES. FLIGHT 5981, FILED CLOSED. CYCLED FLAPS ON THE GROUND AND NOTICED LEFT FLAP INDICATION TO BE SLIGHTLY DELAYED COMPARED TO RIGHT SIDE. ALSO NOTE THAT LEFT FLAP TRANSMITTER PROVIDES INDICATION TO EICAS AND STALL PROTECTION SYSTEM POSSIBLE CAUSE FOR UNCOMMANDED FLIGHT MOVEMENT. REPLACED LEFT FLAP POSITION TRANSMITTER WITH SERVICABLE UNIT PER AMM. FLAPS SYSTEM OPERATES NORMAL.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 43,318 hrs · 36,769 cycles

SERVICE DOOR THRESHOLD COVER PLATE CORRODED (C-CHECK) RO:12/14/2019 FOUND TO BE OUT OF LIMITS DUE TO 100 PERCENT CORROSION THROUGH MATERIAL IAW CRJ 200 SRM LOCATED AND DRILLED NEW COVER PLATE / P/N: 601R38957-31 / TAG: B07898

Part: BEARING — CHAFED (RT AILERON) · airframe 43,318 hrs · 36,769 cycles

UPON REMOVAL OF RH AILERON BEARINGS FOUND SEVERE PITTING AND EXCESSIVE CHAMFER IN BORES OF CTR HINGES (C-CHECK) RO:12/14/2019 FOUND CHAMFER AND PITTING OUT OF LIMITS IAW BOMBA CMM. RECEIVED SERVICEABLE AILERON, INSTALL CW ON CP# 19750645 W/O 1017863 6000 0006 SN 7442060. TAG BB4838

Part: BEARING — CHAFED (LT AILERON) · airframe 43,318 hrs · 36,769 cycles

UPON REMOVAL OF LH AILERON BEARINGS FOUND SEVERE PITTING AND EXCESSIVE CHAMFER IN BORES OF CTR HINGES (C-CHECK) RO:12/14/2019 FOUND PITTING AND CHAMFER OUT OF LIMITS IAW BOMBA CMM. RECEIVED SERVICEABLE AILERON, INSTALL C/W ON CP#19750641 W/O 1017863 5000 0006 SN 7442029 TAG BB4839.

Part: SUPPORT ANGLE — CORRODED (BS 349) · airframe 43,318 hrs · 36,769 cycles

AFTER REMOVAL OF BEAM SPACER FOUND CORROSION ON AFT GALLEY SUPPORT ANGLE FS 349 BETWEEN LBL 27-LBL45 (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED GALLEY SUPPORT ANGLE IAW CRJ 200 SRM.

Part: SKIN — CORRODED (BS 559) · airframe 43,318 hrs · 36,769 cycles

FUSELAGE OUTER SKIN HAS NUMEROUS AREAS OF CORROSION BETWEEN FS 559 TO FS 559+64 STR 26L TO STR 26R (C-CHECK) RO 12/14/2019 REMOVED CORROSION BETWWEEN FS 559 TO FS 559 +64 STR 262 TO STR 26R.WITH IN ALLOWABLE LIMITS IAW BOMBA REO.

Part: ANGLE — CRACKED (BS 621-625) · airframe 43,318 hrs · 36,769 cycles

OBLIQUE ANGLE IN AEB AT FS 621-625 STR 14R IS CRACKED (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED ANGLE FS 621-625 STR14R IAW CRJ200 SRM.

Part: POST — CRACKED (BS 409) · airframe 43,318 hrs · 36,769 cycles

FS 409+128 POST AT LBL 18 IS CRACKED ON THE O/B SIDE IN THE AFT RADIUS AT APPROX WL68 (C-CHECK) RO 12/14/2019 REPLACED 409+128 O/B STIFFENER AT LBL 18 IAW CRJ200 SRM AND REO. P/N-PLT214-5-4 TAG#B17104 P/N-PLT214-5-5 TAG#A83551 P/N-PLT214-5-7 TAG#B67432 P/N-PLT214-5-6 TAG#A80990 P/N-PLT214-5-3 TAG#B15406 P/N-PLT214-5-8 TAG#B16987 P/N-PLT214-5-2 TAG#A83787 P/N-601R32208-155 TAG#B16829

Part: MOUNT BRACKET — CRACKED (LT WING ENGINE) · airframe 43,318 hrs · 36,769 cycles

LH ENGINE UPPER STANG FAIRING FWD MOUNTING BRACKET ON ENGINE IS CHRACKED (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED LH ENG. UPPER STANG FAIRING FWD MOUNT BRKT IAW BOMBA CMM.

Part: ANGLE — CRACKED (BS 621-625) · airframe 43,318 hrs · 36,769 cycles

OBLIQUE ANGLE IN AEB AT FS 621-FS-625 STR 14L IS CRACKED (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED ANGLE AT AEB FS 621-625 STR 14L IAW CRJ200 SRM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,318 hrs · 36,769 cycles

#2 SEAT TRACK ON RBL 9 HAS CORROSION (C-CHECK) RO:12/14/2019 INSTALLED #2 SEAT TRACK ON RBL 9 IAW CRJ-200 AMM.TAG# A81967 PN# NAS7503-4 / TAG# A83792 PN# NAS7503-3 / AAR31535 CAL DUE 04/09/20

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,318 hrs · 36,769 cycles

#2 SEAT TRACK ON LBL 9 HAS CORROSION (C-CHECK) RO:12/14/2019 INSTALLED #2 SEAT TRACK ON LBL 9 IAW CRJ-200 AMM / TAG# A81967 PN# NAS7503-4 / TAG# A83792 PN# NAS7503-3 / AAR531535 CAL DUE 04/09/20

Part: POST — CRACKED (BS 409) · airframe 43,318 hrs · 36,769 cycles

FS 409+128 RBL 27 I/B POST CRACKED AT THE BOTTOM RADIUS (C-CHECK) RO 12/14/2019 REPAIRED FS 409+128 RBL 27 I/B POST WAS CRACKED AT THE BOTTOM RADIUS IAW: REO.

Part: STRAP — CORRODED (BS 559) · airframe 43,318 hrs · 36,769 cycles

R/H PRESSURE FLOOR STRAP AT FS 559 RBL 28 TO RBL 42 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REPLACED STRAP IAW CRJ 200 SRM. / MATERIAL .050" 7075 T6 #B61485 IAW CRJ 200 SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 43,318 hrs · 36,769 cycles

ANGLE CLIP ON THE AFT SIDE OF BEAM 280 AND O/B OF LBL 9 IS CRACKED IN THE CABIN BELOW THE FLOOR (C-CHECK) RO 12/14/2019 REPLACED THE CRACKED ANGLE ON THE AFT SIDE OF FS280 @ LBL9/OB IAW CRJ200 SRM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,318 hrs · 36,769 cycles

#4 FLOOR SEAT TRACK ON RBL 9 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVED AND INSTALLED NEW SEAT TRACK IAW CRJ200 AMM.

Part: POST — CRACKED (BS 409) · airframe 43,318 hrs · 36,769 cycles

FS 409+128 RBL 18 O/B POST IS CRACKED AT THE BOTTOM (C-CHECK) RO 12/14/2019 REPAIRED FS 409+128 RBL 18 O/B POST WAS CRACKED AT THE BOTTOM IAW: REO.

Part: BRACKET — CRACKED (OVERWING FAIRING) · airframe 43,318 hrs · 36,769 cycles

FS 449 LBL 47 OVERWING FAIRING BRACKET IS CRACKED (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED BRACKET IAW CRJ200 SRM.

Part: BRACKET — CRACKED (OVERWING FAIRING) · airframe 43,318 hrs · 36,769 cycles

FS 461 LBL OVERWING FAIRING BRACKET IS CRACKED (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED BRACKET IAW CRJ200 SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 43,318 hrs · 36,769 cycles

ANGLE CLIP ON THE AFT SIDE OF BEAM 280 AND O/B OF RBL 9 IS CRACKED IN THE CABIN BELOW THE FLOOR (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED ANGLE IAW CRJ-200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 43,318 hrs · 36,769 cycles

L/H PRESSURE FLOOR SILL HAS CORROSION BETWEEN FS 409+128 AND FS 559 (C-CHECK) RO 12/14/2019 REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW CRJ-200 REO.

Part: BRACKET — CRACKED (OVERWING FAIRING) · airframe 43,318 hrs · 36,769 cycles

FS 469RBL 47 OVERWING FAIRING BRACKET IS CRACKED (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED BRACKET IAW CRJ200 SRM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,318 hrs · 36,769 cycles

#4 FLOOR SEAT TRACK ON LBL 9 HAS CORROSION (C-CHECK) RO:12/14/2019 INSTALLED #5 SEAT TRACK ON LBL9 IAW CRJ-200 AMM.

Part: POST — CRACKED (BS 409) · airframe 43,318 hrs · 36,769 cycles

FS 409+128 LBL 27 I/B POST IS CRACKED AT THE BOTTOM (C-CHECK) RO 12/14/2019 REPAIRED FS 409+128 LBL 27 I/B POST IAW BOMBARDIER REO. P/N-HST10AG6-9 TAG# A83645 P/N-HST10AG6-8 TAG#B15795 P/N- HST10AG6-7 TAG# A52147 P/N- KFN587-3 TAG#A52147 P/N-B0203013-08 TAG#A83618 P/N-HST10AG5-3 TAG#A83723

Part: ANGLE — CRACKED (BS 605) · airframe 43,318 hrs · 36,769 cycles

FS 605 CLIP UNDER THE CARGO DOOR SILL IS CRACKED (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED CLIP UNDER THE CARGO DOOR SILL IAW CRJ 200 SRM.

Part: STRAP — CORRODED (BS 559) · airframe 43,318 hrs · 36,769 cycles

L/H PRESSURE FLOOR STRAP AT FS 559 LBL 28 TO LBL 42 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REPLACED STRAP IAW CRJ-200 SRM. / .050" 7075 T-6 #B61485 IAW CRJ-200 SRM.

Part: BRACKET — CRACKED (OVRWG FAIRING) · airframe 43,318 hrs · 36,769 cycles

FS 461 LBL 47 OVERWING FAIRING BRACKET IS CRACKED (C-CHECK) RO:12/14/2019 / REMOVED AND REPLACED BRACKET AT FS 461 LBL 47 OVERWING IAW CRJ 200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 43,318 hrs · 36,769 cycles

R/H PRESSURE FLOOR SILL HAS CORROSION BETWEEN FS 409+128 AND FS 559 (C-CHECK) RO 12/14/2019 REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW CRJ-200 REO.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 43,318 hrs · 36,769 cycles

PAX DOOR AFT DRAG ANGLE CRACKED (C-CHECK) RO:12/14/2019 INSTALLED REPAIR ANGLE I.A.W. BOMBA REO.

Part: FRAME — CRACKED (BS 605) · airframe 43,318 hrs · 36,769 cycles

FS605.00 STGR9L FRAME IS CRACKED AT LWR RIVET (C-CHECK) RO 12/14/2019 PERFORMED CUT OUT AND INSTALLED REPAIR DOUBLER IAW CRJ 200 SRM.

Part: FRAME — BENT (BS 682) · airframe 43,318 hrs · 36,769 cycles

AFT ACCY, COMPT. FRAME BENT ON EDGES IN SEVERAL PLACES FORWARD OF THE AFT ACCY DOOR (C-CHECK) RO 12/14/2019 REPAIRED FAIL SAFE ANGLE ON FS 682 BETWEEN STR 24L AND 24R IAW BOMBA REO.

Part: CARGO TRACK — CORRODED (BS 559-617) · airframe 43,318 hrs · 36,769 cycles

CARGO TRACK ON RBL 9 FROM FS 559+116 TO FS 617 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVED AND REPALCED SEAT TRACK IAW CRJ200 AMM.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,318 hrs · 36,769 cycles

#3 FLOOR SEAT TRACK ON LBL 9 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVE AND REPLACED THE #3 SEAT TRACK ON LBL 9 IAW CRJ 200 AMM.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 43,318 hrs · 36,769 cycles

CARGO TRACK ON LBL 27 BETWEEN FS 559+95 AND FS 559+116 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM. / 20276-144-0-0 B08442

Part: SEAT TRACK — CORRODED · airframe 43,318 hrs · 36,769 cycles

#3 FLOOR SEAT TRACK ON RBL 9 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVED CORROSION IAW CRJ200 SRM. FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM.

Part: FLOOR SUPPORT — CORRODED (BS 295-310) · airframe 43,318 hrs · 36,769 cycles

LH FLOOR SILL HAS CORROSION SPOTS BETWEEN FS 295 THRU FS 310 IN THE CABIN (C-CHECK) RO:12/14/2019 REMOVED CORROSION SPOTS BETWEEN FS 295 THRU FS 310 IWA CRJ 200 SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 43,318 hrs · 36,769 cycles

AFT PRESS BULKHEAD HAS MULTIPLE CRACKED / BROKEN ISOLATORS (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED BROKEN ISOLATERS ON THE 621 BULKHEAD IAW CRJ-200 SRM.

Part: ANGLE — CORRODED (BS 319-349) · airframe 43,318 hrs · 36,769 cycles

SERVICE DOOR OPENING LOWER SILL LOWER LONGERON ANGLE STRIP HAS CORROSION SPOTS BETWEEN 319.70 THRU 349 (C-CHECK) RO:12/14/2019 REMOVED DAMAGED SILL STRIKER AND SILL ANGLE AT SERVICE DOOR OPENING LOWER LOCATION AND INSTALLED NEW SILL ANGLE AND SEAL STRIKER IAW CRJ 200 SRM.

Part: CARGO TRACK — CORRODED (BS 589-605) · airframe 43,318 hrs · 36,769 cycles

CARGO TIE DOWN PLATE BETWEEN FS 589 AND FS 605 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVED CORROSION , FOUND TO BE OUT OF LIMITS DUE TO CRACK. INSTALLED NEW CARGO PLATE IAW CRJ-200 SRM.

Part: DOOR SILL — CORRODED (BS 310-349) · airframe 43,318 hrs · 36,769 cycles

PAX DOOR OPENING LOWER SILL LOWER LONGERON ANGLE STRIP HAS CORROSION SPOTS ON THE I/B AND O/B SIDE BETWEEN FS 310 TSHRU FS349 (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED LOWER SILL ANGLE IAW CRJ200 SRM.

Part: ANGLE — CORRODED (BS 319-333) · airframe 43,318 hrs · 36,769 cycles

PAX DOOR OPENING LOWER SILL LOWER LONGERON ANGLE STRIP I/B AWIRE HARNESS MOUNTING BRACKETS ARE BOTH CORRODED BETWEEN FS 319.70 AND FS 333 IN THE CABIN BELOW THE FLOOR (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED MOUNTING BRACKETS IAW CRJ 200 SRM / PN 601R31771-1 TAG B16208 / PN NAS623-3-11 TAG A39092

Part: CARGO TRACK — CORRODED (BS 559-617) · airframe 43,318 hrs · 36,769 cycles

CARGO TRACK ON LBL 27 BETWEEN FS 559+116 AND FS 617 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ-200 SRM. INSTALLED IAW CRJ-200 AMM.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 43,318 hrs · 36,769 cycles

CARGO TRACK ON RBL 9 BETWEEN FS 559+98 TO FS 559+116 HAS CORROSION (C-CHECK) RO:12/14/2019 REMOVED CORROSION FOUND TO BE OUT OF LIMITS, INSTALLED FABRICATED SEAT TRACK IAW CRJ-200 REO.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 43,318 hrs · 36,769 cycles

RH FLOOR SILL HAS CORROSION SPOTS BETWEEN FS 310 THRU FS 319.70 IN THE CABIN (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED RH FLOOR SILL FS 310-319.70 IAW CRJ200 SRM.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 43,318 hrs · 36,769 cycles

CARGO TRACK ON LBL 9 BETWEEN FS 559+95 TO FS 559+116 HAS CORROSION (C-CHECK) RO:12/14/2019 INSTALLED CARGO TRACK ON LBL 9 BETWEEN FS 559+95 TO FS 559+116 IAW CRJ 200 AMM / AAR531535 CAL DUE 04/09/20

Part: STIFFENER — CRACKED (BS 409) · airframe 43,318 hrs · 36,769 cycles

VERTICAL STIFFNER AT RBL 9 AT FS 409+128 IS CRACKED AT THE BOTTOM O/B SIDE, IN THE FWD ECS COMPARTMENT (C-CHECK) RO 12/14/2019 REPARIED VERTICAL STIFFNER AT RBL 9 AT FS 409+128 WAS CRACKED AT THE BOTTOM O/B SIDE, IN THE FWD ECS COMPARTMENT IAW:REO.

Part: FRAME — CORRODED (BS 409) · airframe 43,318 hrs · 36,769 cycles

FRAME 409 HAS CORROSION SPOTS ON THE FWD SIDE BETWEEN STGR 26L THRU 26R IN THE FWD E&E BAY (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED FLOOR SUPPORT IAW SRM.

Part: SKIN — CORRODED · airframe 43,318 hrs · 36,769 cycles

A/C BELLY INNER SKIN HAS CORROSION AND PITS ALL THE WAY AROUND THE FWD E&E BAY DOOR OPENING (C-CHECK) RO:12/14/2019 REPAIRED INNER SKIN DAMAGE IAW CRJ-200 REO .

Part: BRACKET — CRACKED (DOOR SENSOR) · airframe 43,318 hrs · 36,769 cycles

SERVICE DOOR, SENSOR BRACKET IS CRACKED AND LOOSE. (C-CHECK) RO:12/14/2019 REMOVED DAMAGED SERVICE DOOR SENSOR BRACKET AND INSTALLED A NEW BRACKET PER CRJ 200 SRM. / PERFORMED AN OPERATIONALTEST - WITH SATISFACTORY RESULTS - IAW CRJ 200 AMM.

Part: ANGLE — CORRODED (559) · airframe 43,318 hrs · 36,769 cycles

COMPLY WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK) RO:12/14/2019 COMPLIED WITH REO 601R-53-41-1116 REV. C. IAW BOMBARDIER REO.

Part: FLOORBEAM — CRACKED (BS 605) · airframe 38,688 hrs · 32,675 cycles

A CRACK WAS FOUND ON THE BS 605 FLOORBEAM ANGLE LT END UNDER CARGO DOOR SILL. REPAIRED THE FLOORBEAM ANGLE IAW REO.

Part: FLOOR SUPPORT — CRACKED (BS 589-605) · airframe 38,688 hrs · 32,675 cycles

CARGO FLOOR SUPPORT AT BS 589 - 605 CRACKED. INSTALLED A NEW FLOOR SUPPORT IAW SRM AND REO.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,688 hrs · 32,675 cycles

CORROSION FOUND ON PAX DOOR INTERCOSTAL DD5. REMOVED AND INSTALLED A NEW INTERCOSTAL IAW SRM. OPS AND LEAK CHECKED GOOD.

Part: ACTUATOR — FAILED (NLG DOOR) · airframe 36,317 hrs · 30,460 cycles

IN-FLIGHT NLG DOOR OPEN WARNING. DIVERTED, R & R NLG DOOR ACTUATOR IAW AMM. SWUNG GEAR MULTIPLE TIMES WITH NO FAULTS FOUND, OPS CHECKED GOOD.

Part: SKIN — CHAFED (RT AILERON) · airframe 34,202 hrs · 28,547 cycles

RIGHT AILERON L/E UPPER SKIN PANEL CHAFED BEYOND LIMITS. REPLACED RT AILERON UPPER L/E SKIN IAW SRM.

Part: FRAME — DAMAGED (BS 333) · airframe 34,202 hrs · 28,547 cycles

FRAME AT BS 333 STRINGERS 1-4L DAMAGED. R & R THE FRAME SECTION FROM STR 1-4L IAW SRM.

Part: TAB — CHAFED (LT AILERON) · airframe 34,202 hrs · 28,547 cycles

LEFT AILERON L/E OTBD TAB HAS CHAFING. R & R PANEL, IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,973 hrs · 27,419 cycles

UPON REPLACEMENT OF PAX DOOR ANCHOR FITTING, CORROSION FOUND ON STRINGER. REPAIRED IAW SRM.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 31,673 hrs · 26,331 cycles

LOWER EMERGENCY EXIT SIGN AT RT OVERWING EXIT NOT WORKING. R & R THE LOWER EXIT SIGN AT THE LT WING EMERGENCY EXIT AND THE NR 3 EMERGENCY LIGHT INVERTER IAW AMM, OPS CHECK GOOD AT THIS TIME.(2014NM060066)

Part: DUCT — DETACHED (MIXING MANIFOLD) · airframe 31,445 hrs · 26,162 cycles

THE ACFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL. MX FOUND THE MIXING CHAMBER UNDER CARGO FLOOR HAS ONE SIDE DETACHED. R & R THE MIXING MANIFOLD AND DUCT IAW AMM. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 31,036 hrs · 25,852 cycles

ONE BULB BURNED OUT ON GALLEY EXIT SIGN. R & R BULB.

Part: CABIN PRESSURE — FAILED · airframe 30,966 hrs · 25,803 cycles

DURING CLIMBOUT, CABIN FAILED TO PRESSURIZE. RETURNED TO FIELD. INSPECTED ALL DOOR SEALS, NO DEFECTS NOTED. INSPECTED OUTFLOW VALVES AND PERFORMED PRESSURIZATION OF ACFT ON GROUND. NO DEFECTS OR LEAKS NOTED. REPLACED PSEU, CABIN PRESSURE SELECTOR PANEL AND RELAYS IN JB11 IAW ESPM. PERFORMED PRESSURIZATION OF ACFT ON GROUND IAW AMM.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 30,952 hrs · 25,795 cycles

CABIN ALT CAUTION MESSAGE RAN QRH, CABIN KEPT CLIMBING IN AUTO AND MANUAL. PERFORMED EMERGENCY DESCENT, DEPLOYED PAX OXYGEN MASKS, DECLARED EMERGENCY AND DIVERTED. REPLACED CPC1, CPC 2 AND CPAM IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,700 hrs · 25,607 cycles

LT FWD OVER WING EMERGENCY LIGHT IS BURNED OUT. REPLACED LAMP.

Part: VANE — CHAFED (TE FLAP) · airframe 29,878 hrs · 24,958 cycles

REPLACED LT INBD FLAP VANE OTBD CAP DUE TO BEING CHAFFED OUT OF LIMITS. C-CHECK LOCATED, DRILLED & INSTALLED NEW OTBD VANE CAP, PN 601R14303-43S IAW CRJ 200 SRM.

Part: RIB — CHAFED (TE FLAP) · airframe 29,878 hrs · 24,958 cycles

1.3" CHAFE TO LT INBD FLAP AT INBD RIB ON FWD SIDE OF RIB. C-CHECK REPLACED NEW 601R14125-3 RIB IAW CRJ200 SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 29,878 hrs · 24,958 cycles

FS 409.0 +128 VERTICAL POST AT BL 0.0 HAS CRACKS ON BOTH LT & RT POST. C-CHECK REPLACED FS 409.0 +128 VERTICAL POST AT BL 0.0 IAW CRJ-200-SRM & REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,878 hrs · 24,958 cycles

LT INBD FLAP VANE CTR LE CHAFFING. C-CHECK BLENDED LT INBD FLAP VANE CTR LE WITHIN LIMITS IAW REO

Part: VANE — CHAFED (TE FLAP) · airframe 29,878 hrs · 24,958 cycles

RT INBD FLAP VANE CTR OF THE LE CHAFFING. C-CHECK BLENDED RT INBD FLAP VANE CTR LE IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,878 hrs · 24,958 cycles

RT INBD FLAP VANE INBD LE CHAFFING. C-CHECK BLENDED RT INBD FLAP VANE LE, WITHIN LIMITS IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,878 hrs · 24,958 cycles

RT INBD FLAP VANE OTBD LE CHAFFING. C-CHECK BLENDED RT INBD FLAP VANE OTBD LE WITHIN LIMITS IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,878 hrs · 24,958 cycles

LT INBD FLAP VANE INBD LE CHAFFING. C-CHECK BLENDED LT INBD FLAP VANE INBD LE WITHIN LIMITS IAW REO.

Part: LEVER — CHAFED (PAX DOOR) · airframe 29,878 hrs · 24,958 cycles

PAX DOOR FWD PULL IN LEVER CHAFFED. C-CHECK REPAIRED PAX DOOR FWD PULL IN LEVER IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,093 hrs · 23,564 cycles

FORWARD EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 6237) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,496 hrs · 22,399 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6338) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — FAILED (CABIN) · airframe 26,192 hrs · 22,158 cycles

AFT EMERGENCY FLOOR LIGHT STRIP WILL NOT TEST. (FLT 5641) REPLACED INVERTER ABOVE AFT LAVORATORY FOR AFT EMERGENCY FLOOR LIGHT SECTION IN REFERENCE TO CRJ AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 26,192 hrs · 22,158 cycles

LAST 4 EMERGENCY FLOOR LIGHT STRIPS WILL NOT TEST. (FLT 6285) DISCONNECTED WIRE CONNECTIONS AT ROW 13 AND RECONNECTED.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 25,924 hrs · 21,943 cycles

STRONG BURNING SMELL NOTICED IN FRONT SECTION OF PAX CABIN. (FLT 6424) REPLACED BALLAST AT STORAGE BIN 4AB.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 25,776 hrs · 21,831 cycles

EMERGENCY LIGHTS ON RIGHT WING ARE OUT. (FLT 5426) RELAMPED EMERGENCY LIGHTS.

Part: CONNECTOR — LOOSE (CABIN) · airframe 25,603 hrs · 21,697 cycles

FLOOR LEVEL EMERGENCY LIGHTS FROM ROW 2 FORWARD DO NOT ILLUMINATE WHEN TESTED. (FLT 6409) RE-SECURED LOOSE CONNECTOR ON FLOOR LEVEL STRIP AT ROW 2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,491 hrs · 21,612 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5467) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,338 hrs · 21,494 cycles

(C-CHECK) CRACK ON THE RIGHT FS 559.0 PRESSURE BULKHEAD. REPAIRED RIGHT FS 559.0 PRESSURE BULKHEAD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,098 hrs · 21,297 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. (FLT 6212) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 24,432 hrs · 20,736 cycles

EMERGENCY LIGHTS POWERED BY BATTERY PACK 4 ILLUMINATED WITHOUT COMMAND. (SERVICE) REPAIRED WIRE LF1G20 TO NR 4 EMERGENCY LIGHT BATTERY PACK.

Part: RELAY — FAILED (CABIN) · airframe 24,394 hrs · 20,706 cycles

ALL EMERGENCY LIGHTS WILL NOT ILLUMINATE. (FLT 6459) REPLACED RELAY K1XD.

Part: RELAY — FAILED (ELECTRICAL SYS) · airframe 24,394 hrs · 20,706 cycles

AFTER EXTENDING THE LANDING GEAR, EMERGENCY LIGHTS CAME ON TWICE IN THE CABIN. (FLT 5440) REPLACED RELAY KIXD AC ESSENTIAL BUS SENSOR RELAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,331 hrs · 20,652 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,331 hrs · 20,652 cycles

MIDDLE RIGHT EXTERNAL EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DIRTY (CABIN) · airframe 24,331 hrs · 20,652 cycles

EMERGENCY LIGHTS WERE COMING ON & OFF. (FLT 6306) CLEANED CONNECTORS AT JB12.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,262 hrs · 20,602 cycles

LEFT OVERWING EXTERIOR MIDDLE EMERGENCY LIGHT IS OUT. (FLT 5258) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,262 hrs · 20,602 cycles

THE 2ND AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5133) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,262 hrs · 20,602 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. (FLT 6486) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,078 hrs · 20,456 cycles

THE 2ND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6532) REPLACED NR 3 EMERGENCY BATTERY PACK, BATTERY PACK CHARGER, AND SECOND TO AFT EMERGENCY LIGHT FIXTURE. P/N: AD-2013-1A S/N OFF: 77254.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,013 hrs · 20,395 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5428) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,691 hrs · 20,143 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6534) RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,150 hrs · 18,054 cycles

FS 280 FLOORBEAM IS CRACKED. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,164 hrs · 18,068 cycles

FS 621.0 BULKHEAD CRACKED NEAR CARGO TRACK. (C-CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,224 hrs · 18,117 cycles

FS 621 BULKHEAD HAS .25 INCH CRACK AT TOP OF CARGO DOOR TRACK. (C-CHECK) REPAIRED PER REO.

Part: BEAM — CRACKED (FUSELAGE) · airframe 21,224 hrs · 18,117 cycles

FS 280 BEAM IS CRACKED ON LOWER FLANGE. (C-CHECK) REPAIRED PER REO.

Part: ACM — FAILED (AC BAY) · airframe 21,120 hrs · 18,028 cycles

LEFT PACK FELL OFFLINE DURING CLIMB AND FOUL SMELL CAME THROUGH AIR VENTS. (FLT 6477) REPLACED LEFT AIR CYCLE MACHINE PER AMM.

Part: YOKE — CORRODED (LT ENGINE) · airframe 21,120 hrs · 18,028 cycles

LEFT ENGINE YOKE LINK ASSEMBLY CORRODED. (ENGINE CHANGE) REPLACED YOKE LINK ASSEMBLY PER AMM.

Part: WIRE — NOT SEATED (EMERGENCY LIGHT) · airframe 20,346 hrs · 17,381 cycles

EMERGENCY FLOOR LIGHTING AFT OF EXIT ROW INOP. (FLT 6897) RESEATED WIRING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,581 hrs · 16,739 cycles

CRACK ON FORWARD PRESSURE BULKHEAD BL 23.71. (A CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,826 hrs · 16,080 cycles

OVERHEAD EMERGENCY LIGHT IN CABIN INOP. (FLT 6404) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,632 hrs · 15,926 cycles

EMERGENCY OVERHEAD LIGHT IN CABIN AT STATION NR 3 INOP. (FLT 5897) RELAMPED EMERGENCY LIGHT.

Part: ADC — FAULTY (NR 1) · airframe 18,632 hrs · 15,926 cycles

CAPTAINS ALTIMETER READING ERRATIC. (FLT 5791) REPLACED NR 1 ADC PER AMM.

Part: ADC — UNRELIABLE (NR 2) · airframe 18,451 hrs · 15,780 cycles

CAPTAIN ALTIMETER AND COPILOT ALTIMETER DIFFER BY 75 FEET AT CRUISE. (FLT 6756) REPLACED NR 2 ADC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,397 hrs · 15,744 cycles

LEFT WING CENTER EMERGENCY EXIT LIGHT INOP. (FLT 6251) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 16,789 hrs · 14,479 cycles

FLT 6533 - EMERGENCY LIGHT IN GALLEY INOP. RESEATED CONNECTOR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 16,915 hrs · 14,587 cycles

DURING C-CHECK, LINTEL FITTING TO AFT PRESSURE BULKHEAD CRACKED. REPAIRED PER REO.

Part: SPHERICAL BEARIN — CORRODED (RT ENGINE) · airframe 16,915 hrs · 14,587 cycles

RIGHT ENGINE AFT THRUST FITTING SPHERICAL BEARING CORRODED (C CHECK). REPLACED PER AMM.

Part: SPHERICAL BEARIN — CORRODED (LT ENGINE) · airframe 16,915 hrs · 14,587 cycles

LEFT ENGINE AFT THRUST FITTING SPHERICAL BEARING CORRODED (C CHECK). REPLACED PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,567 hrs · 14,310 cycles

FLT 6735 - LEFT OVERWING EXIT EMERGENCY LIGHT INOP. CLEANED MOISTURE FROM TRACK AND LIGHTS.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 16,513 hrs · 14,269 cycles

FLT 6399 - LESS THAN 50 PERCENT OF FLOOR STRIP LIGHTS INOP. REPLACED NR 2 INVERTER.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,971 hrs · 13,855 cycles

FLT 6526 - FLOOR EMERGENCY LIGHTS FROM ROW 2 THROUGH 5 INOP. REPLACED NR 1 BATTERY POWER SUPPLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,906 hrs · 13,801 cycles

FORWARD EMERGENCY FLOOD LIGHT INOP (FLT 5970). RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 15,519 hrs · 13,479 cycles

EXTENDED LANDING GEAR ON APPROACH AND RECEIVED A NOSE GEAR DISAGREE MESSAGE. WENT AROUND AND RECEIVED NORMAL GEAR DOWN INDICATIONS. FLIGHT 6831. REPLACED NOSE GEAR SELECTOR VALVE PER AMM 32-22-20. OPS AND LEAK CHECK GOOD. P/N 750006-000, S/N OFF 2029.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 15,285 hrs · 13,298 cycles

ELECTRICAL SMOKE ODOR IN CABIN. (FLIGHT NR 5933) REPLACED OVERHEAD LIGHT BALLAST NEAR ROW 4 IAW AMM 33-21-00. OPS CHECK GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 15,285 hrs · 13,298 cycles

02 MASKS DROPPED WHEN HYDRAULICS WERE SELECTED ON USING GPU AT THE GATE. RESTOWED ALL 02 MASKS IAW MM 35-13-00. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,220 hrs · 13,246 cycles

FLOOR EMERGENCY LIGHTING IS INOPERATIVE. (FLIGHT NR 6103) REPLACED EMERGENCY LIGHT CHARGER ASSEMBLY IAW AMM 33-51-01.

Part: OXYGEN MASK — UNWANTED DEPLOY (PAX CABIN) · airframe 14,595 hrs · 12,679 cycles

FLT 6689 - DURING INITIAL POWER-UP, THE PAX O2 MASKS DEPLOYED. INSPECTED AND RESTOWED MASKS PER AMM 35-21-09. MASKS REMAINED SECURE.

Part: ACM — SMOKE (RIGHT) · airframe 14,475 hrs · 12,577 cycles

FLT 5991 - SMELLED SMOKE IN CABIN. REPLACED RIGHT PACK IAW 21-51-10. OPS CHECK GOOD.

Part: WIRE HARNESS — FAILED (MLG) · airframe 14,475 hrs · 12,577 cycles

FLT 6495 - RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN MESSAGES. REPLACED RIGHT GEAR INBOARD ELECTRICAL HARNESS PER AMM 32-61-20. OPS CHECK GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 13,827 hrs · 12,044 cycles

FLT 5881 - AFTER RETRACTING LANDING GEAR, RECEIVED A NOSE DOOR OPEN AND GEAR DISAGREE WARNING MESSAGE. REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW CRJ 200 AMM 32-33-10, P/N 750006000, S/N OFF 2032.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,115 hrs · 11,439 cycles

FLT 6024 - PAX DOOR FLOOR LEVEL EMERGENCY FLOOD LIGHT IS INOP. REPLACED FLOOR LEVEL EMERGENCY LIGHT ASSEMBLY IAW CRJ 200 MM 33-51-19.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 13,043 hrs · 11,376 cycles

FIRST OVERHEAD EMERGENCY LIGHT IS BURNED OUT, FLIGHT NR 5901. REPLACED LAMP. OPS CHECK GOOD.

Part: TORQUE LINK — DISCONNECTED (NLG STEERING) · airframe 12,833 hrs · 11,194 cycles

AFTER TAKEOFF, RECEIVED A GEAR DISAGREE, NOSE WHEEL STEERING INOP, AND WOW INPUT. DIVERTED TO SFO, FLIGHT NR 6507. CONNECTED NOSE GEAR TORQUE LINKS AND PERFORMED A VISUAL INSPECTION. REPLACED BOTH NOSE TIRES AND SWUNG GEAR SEVERAL TIMES. ALL OPS CHECKS GOOD.

Part: A/C PACK — ODOR (LEFT) · airframe 11,687 hrs · 10,214 cycles

FUEL ODOR FROM LEFT PACK WHILE ON THE GROUND AS WELL AS INFLIGHT. INSPECTED LEFT ACM OIL LEVEL AND FOUND TO BE OVER SERVICED. REMOVED EXCESS OIL AND CHECKED COMPRESSOR INLET AND DISCHARGE LINES FOR DISCREPANCIES BUT FOUND NOTHING. PACK FUNCTIONS NORMALLY.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 11,912 hrs · 10,400 cycles

PAX DOOR ASSIST MOTOR BRACKET IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED PAX DOOR ASSIST MOTOR BRACKET PER SRM 51-42-06.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 11,912 hrs · 10,400 cycles

FOUND CRACK IN DOUBLER FRAME ON RIGHT SIDE OF FS 640, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS 601R 36001-4 AND 601R 36002-4 PER SB 601R53-061.

Part: WEB — CRACKED (PAX DOOR) · airframe 11,912 hrs · 10,400 cycles

PAX DOOR - THE PAX DOOR FORWARD WEB IS CRACKED IN THE RADIUS BETWEEN THE 3RD AND 4TH FIXED STEPS, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS ON FORWARD WEB OF PAX DOOR PER REO 601R-52-11-1235.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 11,912 hrs · 10,400 cycles

PAX DOOR HAS CRACKED BRACKET INSIDE ACCESS HOLE (832BR) ON AFT SIDE OF DOOR, DISCOVERED AT C-CHECK. INSTALLED NEW INTERCOSTAL P/N 601R-31902-3185 IAW CRJ200 SRM 51-42-06 PG 11.

Part: WEB — CRACKED (PAX DOOR) · airframe 11,912 hrs · 10,400 cycles

PAX DOOR AFT WEB IS CRACKED IN THE RADIUS BETWEEN THE 3RD AND 4TH FIXED STEPS, DISCOVERD AT C-CHECK. INSTALLED ALL REPAIR PARTS ON AFT SIDE OF PAX DOOR PER REO 601R 52-11-702 REV 'A'.

Part: SUPPORT BEAM — CRACKED (LT ENGINE) · airframe 11,912 hrs · 10,400 cycles

ENGINE SUPPORT BEAM LOWER WEB HAS CRACK ON CORNER OF LEFT ACCESS PANEL CUT OUT, DISCOVERED AT C-CHECK. INSTALLED FABRICATED REPAIR PARTS ON LEFT ENGINE BEAM LOWER WEB IAW CRJ200 REO 601R-53-61-358, REV A.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,912 hrs · 10,400 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS ON AFT SIDE OF PAX DOOR PER REO 601R-52-11-513 REV A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,609 hrs · 10,142 cycles

THIRD OVERHEAD EMERGENCY FLOODLIGHT IS INOP. REPLACED OVERHEAD EMERGENCY LIGHT IAW AMM 33-51-16.

Part: SEAL — LEAKING (NLG STRUT) · airframe 11,267 hrs · 9,841 cycles

UPON ROTATION GOT NOSE GEAR DOOR WARNING AND GEAR DISAGREE. CYCLED GEAR WITH NO CHANGE. RETURNED TO DEN REPACKED NOSE STRUT SEALS PER CRJ 200 MM 32-21-20 AND SERVICED STRUT IAW 12-12-32. OPERATIONAL CHECKS GOOD.

Part: ANCHOR — CRACKED (PAX DOOR) · airframe 11,126 hrs · 9,723 cycles

AFT PAX DOOR ANCHOR CRACKED, DISCOVERED DURING SERVICE CHECK. REPLACED AFT PAX DOOR ANCHOR AND SWIVEL IAW CRJ200 MM 52-11-17. OPERATIONAL CHECKS GOOD.

Part: MCU — MALFUNCTIONED (STAB) · airframe 8,693 hrs · 7,612 cycles

CREW REPORTS STAB CHANNEL 1 WILL NOT ENGAGE. REPLACED MCU REF AMM 27-42-05. REPLACED HSTCU REF AMM 27-41-01. OPERATIONAL CHECK GOOD, PN 1 ON/OFF 7062-3 SN 1 OFF 1300, PN 2 ON/OFF 7060-9 SN 2 OFF 203.

Part: LIGHT — UNKNOWN (CABIN) · airframe 8,693 hrs · 7,612 cycles

ONE OF THE RED LIGHTS ON THE CABIN EMERG EXIT SIGN APPEARS NOT TO ILLUMINATE. REPLACED RED LIGHT COVER ON EMERG EXIT SIGN AT ROW 8A. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (RUDDER TRIM) · airframe 8,651 hrs · 7,579 cycles

AILERON TRIM WOULD NOT MOVE LEFT WING DOWN. REPLACED AIL/RUD TRIM CONTROL PANEL. OPERATIONAL CHECK GOOD.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZONTAL STAB) · airframe 8,516 hrs · 7,455 cycles

STAB TRIM CH2 WILL NOT STAY ENGAGED. REPLACED HSTA AND MCU IAW CRJ MM 27-40-00, 27-42-01 AND 27-42-05. OPERATIONAL TEST GOOD. P/N: 8396-3, S/N OFF: 1074, P/N: 7062-3, S/N OFF: 1107.

Part: CAPSTAN — MALFUNCTIONED (STALL WARNING) · airframe 8,516 hrs · 7,455 cycles

WHILE PERFORMING STALL TEST LOUD NOSE WAS HEARD FROM F/O SEAT (UNDER). REPLACED STICKS PUSHER CAPTSTAN IAW 27-35-20 2, OPERATIONAL CHECK SATISFACTORY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,291 hrs · 7,244 cycles

TWO LIGHT BULBS BURNT OUT ON LOWER EMERGENCY LIGHT FOR SERVICE CABIN DOOR. RELAMPED IAW 33-51-21, OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 7,839 hrs · 6,825 cycles

SPOILERONS FAULT, STATUS WOULD NOT CLEAR. REPLACED RIGHT SPOILERON NR 2 PCU OPERATIONAL CHECK GOOD, PN ON 27000-7 OFF 5830.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 7,839 hrs · 6,825 cycles

SPOILERON FAULT STATUS MSG. REPLACED NR 2 SECU PER 27-61-05, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,789 hrs · 6,790 cycles

FLOOR STRIP EMERGENCY LIGHTS ROWS 2-6 DO NOT ILLUMINATE. REPLACED POWER STRIP FLOOR LIGHTS ROWS 2-6. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 33-50-00.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,411 hrs · 7,355 cycles

CABIN FLOOR FS 484 RT INTERCOSTAL INBD CLIP RBL 27 CRACKED ITEM FOUND AT C CHECK INSPECTION. CLIP REPLACED IAW CRJ REO 601R-53-41-059 REV "A" AND AMM 20-24-00.

Part: FLOORBEAM — CRACKED (CRACKED) · airframe 8,411 hrs · 7,355 cycles

FS 280 RT FLOORBEAM RBL 9.0 I/B AND O/B ATTACH ANGLES CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED ANGLES AT FS 280, RBL 9 I/B AND O/B IAW CRJ SRM 51-42-06, 51-23-00, 51-40-11 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,411 hrs · 7,355 cycles

FS 280 LT FLOORBEAM LBL 9.0 I/B AND O/B ATTACH ANGLES CRACKED, ITEM FOUND AT C CHECK INSPECTION. ANGLES AT FS 280, LBL 9 I/B AND O/B REPLACED IAW CRJ SRM 51-42-06, 51-23-00, 51-40-11 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 8,411 hrs · 7,355 cycles

MAIN FUSELAGE; FS 280, LBL 9.0, UPPER FLANGE CRACKED ON TRANSVERSE BEAM, ITEM FOUND AT C CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-138 REV NC.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 8,411 hrs · 7,355 cycles

RT INTERCOSTAL (CLIP) CRACKED AT FS 625 AND STRINGER 14R, ITEM FOUND AT C CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 8,411 hrs · 7,355 cycles

LT INTERCOSTAL (CLIP) CRACKED AT FS 625 AND STRINGER 14L, ITEM FOUND AT C CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,411 hrs · 7,355 cycles

CABIN FLOOR FS 484 LT INTERCOSTAL LBL 27 AND LBL 36 CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-059 REV "A".

Part: FLOOR SUPPORT — CRACKED (BS 460) · airframe 8,411 hrs · 7,355 cycles

CABIN FLOOR RT SUPPORT FITTING FS 460 RBL 9.0 CRACKED, ITEM FOUND AT C CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11.

Part: CONTROL UNIT — MALFUNCTIONED (MOTOR) · airframe 7,656 hrs · 6,654 cycles

DURING CRUISE AND DESCENT AP PITCH TRIM CAUTION MSG ILLUMINATED FOLLOWED BY STAB TRIM CH 1 STATUS MSG. REPLACED STAB MCU IAW CRJ 200 MM 27-43-05 AND 27-41-00. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 7,527 hrs · 6,530 cycles

AP PITCH TRIM CAUTION MSG INFLIGHT DURING DESCENT. REPLACED 1 H/RF CARD AND HORIZONTAL STAB CONTROL UNIT. OPERATIONAL CHECK GOOD IAW 22-11-00, 22-12-00 AND 27-41-00, PN: 7060-9 SN: OFF 1218.

Part: TRIM SWITCH — MALFUNCTIONED · airframe 7,475 hrs · 6,488 cycles

RECEIVED "STAB TRIM" AND "MACH TRIM" CAUTION MSG'S SHORTLY AFTER ROTATION. REPLACED PILOT'S PITCH TRIM DISC SWITCH. OPERATIONAL CHECK GOOD IAW CRJ 200 MM 27-41-30.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZONTAL STAB) · airframe 7,383 hrs · 6,409 cycles

DURING DESCENT INTO DEN "AP STAB TRIM CAUTION MSG ILLUMINATED. REPLACED HSTCU REF AMM 27-41-01 AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 6,164 hrs · 5,412 cycles

CAPTAIN'S SIDE WINDOW CRACKED. REPLACED CAPTAIN'S SIDE WINDOW IAW CRJ MM 56-12-01. OPERATIONAL CHECK GOOD. PN NP139322-9 SN/OFF 02163H7998.

Part: PCU — MALFUNCTIONED (FLT SPOILER) · airframe 6,082 hrs · 5,340 cycles

SPOILERON FAULT STATUS MESSAGE EN ROUTE. REPLACED RIGHT SPOILERON OUTBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 6,069 hrs · 5,330 cycles

STAB TRIM CH1 INOP STATUS MESSAGE WILL NOT EXTINGUISH. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR (HSTA) AND MOTOR CONTROL UNIT (MCU) IAW MM 27-40-01. OPERATIONAL CHECK GOOD.

Part: SWITCH — STUCK (TRIM) · airframe 5,961 hrs · 5,228 cycles

CAPTAIN`S TRIM SWITCH STICKS. REMOVED AND REPLACED CAPTAIN'S SIDE TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 4,851 hrs · 4,232 cycles

FLT SPOILERS FAULT STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED SPOILER ELECTRONIC CONTROL UNIT IAW 27-60-00, OPERATIONAL CHECK GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 3,982 hrs · 3,437 cycles

FS 621 LEFT FLOOR SUPPORT ANGLE LBL 41 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV A AND RII53-401.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 3,982 hrs · 3,437 cycles

FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601RR-53-61-117 REV A AND RII53-401.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 3,982 hrs · 3,437 cycles

CARGO PIT TRANSVERSE BEAM TO LANDING PLATE ATTACH ANGLE IS CRACKED FOR DOOR STOP FITTING FS 589.00 LBL 43.0. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-21-11, 51-42-02, AND RII53-401.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 3,106 hrs · 2,659 cycles

FLOOR LEVEL ESCAPE PATH LIGHTING ROWS 1-5 IS ENTIRELY INOPERATIVE. REMOVED NR 1 EMERGENCY LIGHT BATTRY PACK AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: POWER SUPPLY — FAILED (TE FLAPS) · airframe 1,469 hrs · 1,250 cycles

''FLAP FAIL'' CAUTION MESSAGE AFTER FLAP RETRACTION AFTER LANDING IN SLC. REMOVED AND REPLACED RIGHT BPSU IAW 27-51-10. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG STRUT) · airframe 675 hrs · 534 cycles

ON GEAR RETRACTION GEAR DISAGREE WARNING ACCOMPANIED BY NOSE DOOR OPEN AND NOSE GEAR DOWN INDICATION. RETURNED TO SFO. ADJUSTED NLG STRUT EXTENSION PROX SENSOR. OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 87 hrs · 67 cycles

FIRST OFFICER'S SIDE WINDOW IS CRACKED. REMOVED AND REPLACED FIRST OFFICER'S RIGHT SIDE WINDOW. OPS CHECK GOOD OF WINDOW HEAT AND PRESSURIZATION IAW CRJ MM 56-00-00.