N612QX

Part: SAFETY PIN — INSTALLED (ZONE 700) · airframe 46,091 hrs · 35,135 cycles

GEAR DISAGREE IN AIR RAN QRH. GEAR PINS STILL INSTALLED. (FLIGHT 6218) REMOVED LT/RT AND NLG SAFETY PINS AND INSTALLED THE SAFETY PINS IN THE HOLDER BEHIND THE FOS SEAT AND VERIFIED ALL 4 SAFETY PINS ARE PRESENT. PERFORMED A GVI OF THE LT/RT AND NLG AND ASSOCIATED COMPONENTS. FOUND NO DAMAGE. FOUND NO EICAS MESSAGES. FOUND NO LEAKS. AIRCRAFT CHECKS GOOD FOR CONTINUED SERVICE AT THIS TIME. IAW AMM 32-00-00 FOR EXTERNAL LEAK CHECK OF THE LANDING GEAR. IAW AMM 32-11-00 FOR INSPECTION CHECK OF THE LANDING GEAR & IAW AMM 31-41-00 FOR EICAS.

Part: SKIN — DENTED (ZONE 600 FLAP) · airframe 43,956 hrs · 33,445 cycles

TRANSFER FROM EAML 1516947 : DENTS TO R/H OUTBD FLAP LOWER SKIN (DWG: 601R14536, AL ALLOY 2024-T3, 0.040€? POCKET THICKNESS, 0.050€? PAD-UP THICKNESS, REF). DENTS ARE LOCATED BETWEEN FS235.965- FS254.96 AND 10.00€? FWD OF FLAP TRAILING EDGE (BETWEEN FRONT SPAR DATUM AND INTERCOSTAL SPAR DATUM). (FLIGHT 4937 - FILED CLOSED) REPAIR OF DENTS LOCATED BETWEEN FS235.965- FS254.96 AND 10.00€? FWD OF FLAP TRAILING EDGE (BETWEEN FRONT SPAR DATUM AND INTERCOSTAL SPAR DATUM).CRJ700/900 SRM 57-53-01 TASK 57-53-01-201-001-A01 REPAIR TYPE IIICONTINUED AIRWORTHINESS DAMAGE TOLERANCE INSPECTION REQUIREMENTS FOR TYPE IIIREPAIR HAS THRESHOLD (FLIGHT CYCLES) OF 40000 AT TIME OF INCORPORATION.NDI SURFACE/SUBSURFACEOF FLAP SKIN AND NON-FLUSH REPAIR.CURRENT FC: 33445 DUE AT FC: 73445

Part: UNKNOWN — ODOR (ZONE 200) · airframe 43,752 hrs · 33,300 cycles

BURNING SMELL FOR ABOUT 5 MINS AFTER 30 MINUTES IN FLIGHT. IT CAME ON INTENSELY TWICE DURING THOSE 5 MINUTES. THE WAS NO ANY INDICATION OF SMOKE OR ANY EICAS MESSAGE. THE NEXT 40 MINUTES OF FLYING WAS UNEVENTFUL. (FLIGHT 1300 - FILED CLOSED)COMPLIED WITH FIM 21-21-00 TABLE 201 AND FOUND RH POST MAP LIGHT TO BE EXTREMELY HOT TO THE TOUCH AND EMITTING A HOT SMELL. REMOVED AND REPLACED RH POST MAP LIGHT PER AMM 33-13-03 AND OP CHECK GOOD. ALSO COMPLIED WITH FIM 21-22-00 FIG 210 AND FOUND NO BURNING SMELL WITH PACK OPERATION AND ENGINES RUNNING.

Part: WINDSHIELD — ARCED (ZONE 200) · airframe 43,752 hrs · 33,300 cycles

CA SIDE WINDSHIELD MAY HAVE ARCED. BURNING SMELL IN THE COCKPIT. APPEARS TO BE COMING FROM THE BOTTOM LEFT CORNER OF THE CA SIDE WINDSHIELD. EN-ROUTE AND THE SMELL LASTED ABOUT 5 MINUTES. (FLIGHT 6423 - FILED CLOSED) REMOVED AND REPLACED CA SIDE WINDSHIELD IN REFERENCE WITH CRJ 700 AMM 56-11-01. COMPLIED WITH TASK CARD 8612133. PERFORMED LEAK TEST. LEAK TEST PASSED. AIRCRAFT OK FOR SERVICE AT THIS TIME.

Part: NONE — ODOR · airframe 41,138 hrs · 31,173 cycles

TRANSIENT BRIEF ACRID ODOR SIMILAR TO BURNT RUBBER SMELT BY PASSENGERS IN ROW 6-8. ALL CABIN LIGHTS SELECTED OFF AT TIME OF ODOR. OVERHEAD BINS WERE OPENED AND NO SOURCE OF LION BATTERY RUNAWAY WAS DETECTED. POST FLIGHT INSPECTION OF OVERHEADS BY CREW IN ROW 6-8 DOES NOT SHOW ANY SCORCH/BURN DAMAGE. ONCE SMELL WENT AWAY IT DID NOT RETURN. NO EICAS MESSAGES ASSOCIATED WITH SMOKE/FUMES IN FLIGHT DECK. NO FUMES/SMOKE VISIBLE IN CABIN (FLIGHT #3229 FILED CLOSED) INSPECTED THE PAX COMPARTMENT FROM ROW 6 TO ROW 8 AND DETECTED NO FOUL OR ACRID ODOR. DID FIND NAPKINS STUFFED IN THE SIDEWALL LIGHT ASSY NEXT TO THE LIGHT THAT IS MOST LIKELY THE CAUSE OF THE SMELL.. CHECKED ALL BALLASTS FROM ROW 6 TO ROW 8 AND FOUND NO BURNING OR DISCOLORED AREAS. REMOVED NAPKINS AS NEEDED. OK FOR CONTINUED SERVICE.

Part: NONE — ODOR · airframe 40,636 hrs · 30,762 cycles

FLIGHT CREW AND PASSENGERS REPORT A BURNING SMELL IN THE AREA OF THE 4TH ROW OF SEATS. FLIGHT ATTENDANT REMARKED THAT THE BALLAST DOOR OVER SEATS 4 DC WAS ABNORMALLY HOT COMPARED TO OTHER BALLAST DOORS. ( FLIGHT 3278 - FILED CLOSED) / REFERENCED SERVICE LETTER SL-21-028 DATED 1 JAN, 2013 FOR APPLICABLE TROUBLESHOOTING STEPS. NARROWED THE SEARCH TO THE ROW 4 CD BALLAST PANEL ON THE FLIGHT ATTENDANTS TESTIMONY. NOTED THE CEILING LIGHT BALLAST WAS NOTABLY HOTTER THEN THE SIDEWALL. REMOVED AND PRESENTED THE PS74 BALLAST TO THE FLIGHT CREW IN REFERENCE TO AMM 33-21-03 SO THEY COULD EXAMINE THE AROMA AND THEY AGREED THAT THE BALLAST HAD A SIMILAR ODOR TO THAT THEY WITNESSED IN FLIGHT. REINSTALLED THE PS74 INTO ITS SPOT AND AFTER TURNING ON THE AIRCRAFT THE BALLAST MADE A POP SOUND AND BEGAN TO SMOKE VISIBLY. REMOVED AND REPLACED THE PS74 AND THE PS75 BALLAST IN REFERENCE TO AMM 33-21-03 AND 33-21-09. WHEN THE LIGHTS WERE ACTIVATED NOTED NO CONTINUED ODOR FROM THE BALLASTS. INTERROGATED THE AIRCRAFT'S IN SERVICE LOG ENTRIES GOING BACK 30 DAYS AND IDENTIFIED NO SMOKE EVENTS BUT ON THE 25 OF MAY THE 4 C CEILING LIGHT WAS REPORTED INOPERATIVE. OPS CHECK OF THE CEILING AND SIDEWALL LIGHTS IS GOOD AT THIS TIME.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 38,936 hrs · 29,505 cycles

COPILOT FORWARD WINDSCREEN APPEARS DELAMINATED, UPPER RIGHT CORNER AND LOWER LEADING EDGE. (FLIGHT 2958 - FILED CLOSED) REMOVED AND REPLACED FO WINDSHIELD PER CRJ700 AMM 56-11-01 AND TASK CARD 56-220-1000-SKY. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME. PLEASE REFERENCE AML 713133 FOR APPLICATION OF SPEED TAPE TO AERODYNAMIC SEALANT. PLEASE REFERENCE AML 713265 FOR REINSTALLATION OF FO WINDSHIELD WIPER. AIRCRAFT OK FOR SERVICE. / TORQUE WRENCH: S/N- 0819102467 CAL DUE- 06/30/2022

Part: THRUST REVERSER — DAMAGED (LEFT) · 29,290 cycles

DAMAGE FOUND ON LH LOWER FAN COWL UPON RIGGING OF LH THRUST REVERSERS. (C-CHECK RO 7/5/2021) REPAIRED LH LOWER FAN COWL. REF CRJ-700 SRM 54-14-00-201-004-A01. RESTORED FINISH. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH 51-900-1002-SKY

Part: FLOORBEAM — DAMAGED (BS 280 LBL9) · 29,290 cycles

*MISSING FASTENER HEAD, UNDERSIDE OF FLOOR BEAM RBL9 AFT OF FS 280.00 (C-CHECK RO 7/5/2021) REMOVED AND REPLACED FASTENER WITH MISSING HEAD, LOCATED UNDERSIDE OF FLOOR BEAM RBL 9 AFT OF FS 280.00 REF. CRJ-700 SRM 51-42-13-001-001-A01

Part: SKIN — CORRODED (PAX DOOR) · 29,290 cycles

PAX DOOR OUTER SKIN ( INNER SIDE) FOUND EXFOLIATED CORROSION BETWEEN MID DD3 AND MID DD4 INTERCOSTAL (C-CHECK RO 7/5/2021) BLENDED OUT CORROSION ON PAX DOR OUTER SKIN (INNER SIDE) IAW CRJ700 SRM 51-21-06-001-001-A01, FOUND TO BE WITH IN LIMITS OF REO 670-52-11-1228 REV -- DATED 2021-04-27 , RESTORED FINISH AND APPLIED CIC, COMPLYING WITH REO 670-52-11-1228 REV -- DATED 2021-04-27 STEPS 1. THROUGH 4. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: DOOR FRAME — CORRODED (BS 329) · 29,290 cycles

PAX DOOR FORMER F/S 329.41 IS CORRODED BETWEEN MID DD5 AND MID DD6 INTERCOSTAL (C-CHECK RO 7/5/2021) REMOVED AND REPLACED PAX DOOR FORMER FS329.41 BETWEEN MID DD5 AND MID DD6 INTERCOSTAL PER CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N. RESTORED FINISH AND REAPPLIED CIC TO REPAIR LOCATION. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SW TASK CARD 51-900-1002-SKY.

Part: SKIN — CORRODED (PAX DOOR) · 29,290 cycles

PAX DOOR OUTER SKIN HAS CORROSION BETWEEN MID DD5 AND MID DD6 INTERCOSTAL ( INNNER SIDE) (C-CHECK RO 7/5/2021) REPAIRED PASSENGER DOOR OUTER SKIN BETWEEN DD5 AND DD6. REF REO 670-52-11-1226 REV -- DATED 2021-05-03 ALL STEPS COMPLIED WITH. COMPLIED WITH 51-900-1002-SKY. RESTORED FINISH. LEAK CHECK GOOD.

Part: SKIN — GOUGED (BS 969-985 S26LR) · 29,290 cycles

GOUGE AT APPROX. FS969 €“ FS985 STGR26L €“ STGR26R (C-CHECK RO 7/5/2021) REPAIRED GOUGE AT APPROX. FS969 €“ FS985 STGR26L €“ STGR26R REF REO 670-53-00-290 REV -F DATED 2019/04/26 SOLUTION 2 ALL STEPS COMPLIED WITH. COMPLIED WITH 51-900-1002-SKY RESTORED FINISH. LEAK CHECK GOOD.

Part: DOOR FRAME — CORRODED (BS 328) · 29,290 cycles

PAX DOOR FRAME F/S 327.763 IS CORRODED (C-CHECK RO 7/5/2021) REMOVED AND REPLACED PAX DOOR FRAME FS327.763 PER CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND BOMBARDIER DWG 601R31702 REV. N. RESTORED FINISH AND REAPPLIED CIC TO THE AREA. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY.

Part: SUPPORT ANGLE — CORRODED (PAX DOOR) · 29,290 cycles

PAX DOOR FWD ANGLE SUPPORT IS CORRODED (C-CHECK RO 7/5/2021) REMOVED AND REPLACED PAX DOOR FWD ANGLE SUPPORT WITH A SERVICEABLE UNIT PER CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N. RESTORED FINISH AND REAPPLIED CIC TO REPAIR LOCATION. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SW TASK CARD 51-900-1002-SKY.

Part: SKIN — CHAFED (RT WING TE FLAP) · 29,290 cycles

THE R/H INBOARD FLAP LOWER SKIN IS CHAFED WHERE BOTH THE INBOARD AND OUTBOARD CANOE FAIRING SEALS CONTACT IT. (C-CHECK RO 7/5/2021) COMPLIED WITH THE BLENDOUT REPAIR TO THE R/H INBOARD FLAP LOWER SKIN BETWEEN FLAP STA 48.000 AND FLAP STA 64.000 PER REO 670-57-52-484 REV -- DATED 2021-04-28. COMPLIED WITH SKYWEST FORM M-337 AND TASK 51-900-1002-SKY.

Part: SKIN — CHAFED (LT WING TE FLAP) · 29,290 cycles

THE L/H INBOARD FLAP LOWER SKIN IS CHAFED WHERE THE INBOARD CANOE FAIRING SEAL CONTACTS IT. (C-CHECK RO 7/5/2021) COMPLIED WITH THE BLENDOUT REPAIR TO THE L/H INBOARD FLAP LOWER SKIN BETWEEN FLAP STA 48.000 AND FLAP STA 64.000 PER REO 670-57-52-483 REV -- DATED 2021-04-28. COMPLIED WITH SKYWEST FORM M-337 AND TASK 51-900-1002-SKY.

Part: CLEAT — CORRODED (PAX DOOR) · 29,290 cycles

PAX DOOR FWD CLEAT IS CORRODED COMMON TO DD4 INTERCOSTAL (C-CHECK RO 7/5/2021) REMOVED AND INSTALLED NEW CLEAT COMMON TO AFT DD4 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV. N AND RESTORED FINISH AND APPLY C.I.C AT REPAIRED LOCATION IAW CRJ 700 SRM 51-25-16-001-001-A01 AND SRM 51-21-11-001-001-A01 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 29,290 cycles

PAX DOOR AFT DD4 INTERCOSTAL IS CORRODED (C-CHECK RO 7/5/2021) REMOVED AND REPLACED PAX DOOR AFT DD4 INTERCOSTAL WITH A SERVICEABLE UNIT PER CRJ700 SRM 51-42-06-001-001-A01 & BOMBARDIER DWG 601R31702 REV. N. RESTORED FINISH AND REAPPLIED CIC AT REPAIRED LOCATION. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SW TASK CARD 51-900-1002-SKY.

Part: FORMER — CORRODED (PAX DOOR) · 29,290 cycles

PAX DOOR AFT FORMER HAS CORROSION (C-CHECK RO 7/5/2021) REPLACED PASSENGER DOOR AFT FORMER WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 DRAWING 601R31702 REV N. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — CORRODED (BS 324-327 S20L) · 29,290 cycles

CORROSION ON STGR 20L APPROXIMATELY AT FS 324.00 - 327.00 COMMON TO TRANSPONDER CANNON PLUG AND CABLE BRACKET (C-CHECK RO 7/5/2021) REPLACED STGR 20L WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV Y. COMPLIED WITH 51-900-1002-SKY. RESTORED FINISH. PRESSURE CHECK GOOD.

Part: STRINGER SPLICE — CORRODED (BS 333 S21L) · 29,290 cycles

SPLICE ANGLE AT FS 333.00 ATTACHED TO STGR 21L COMMON TO INTERCOSTAL HAS EVIDENCE OF CORROSION (C-CHECK RO 7/5/2021) REPLACED SPLICE ANGLE AT FS 333.00 ATTACHED TO STGR 21L COMMON TO INTERCOSTAL . REF: CRJ-700 S.R.M. 51-42-06-001-001-A01, DWG SH670-31810 REV-Y. COMPLIED WITH 51-900-1002-SKY.

Part: STRINGER SPLICE — CORRODED (BS 333 S24L) · 29,290 cycles

CORROSION FOUND ON SPLICE STGR 24L FS333.00 (C-CHECK RO 7/5/2021) BLENDED CORROSION REF CRJ 700 SRM 51-12-00-001-001-A01 100% MATERIAL LOSS, AFTER BLEND. SPLICE REQUIRES REPLACEMENT. REF CRJ 700 SRM 53-00-00-101-001-A01 REPLACED STRG 24L SPLICE ATTATCHMENT WITH NEW P/N SH670-32429-1 SPLICE PO: N/A REFERENCE CRJ 700 SRM 51-42-06-001-001-A01 AND DRAWING SH670-32420 REV E. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. COMPLIED WITH SKYWEST FORM M-337.

Part: HINGE FITTING — GOUGED (PAX DOOR) · 29,290 cycles

* FOUND A GOUGE ON FUSELAGE SIDE OF THE PAX DOOR HINGE LUG(AREA MARKED) (C-CHECK RO 7/5/2021) REPAIRED GOUGE ON FUSELAGE SIDE OF THE PAX DOOR HINGE LUG. BOMBARDIER REO 670-53-21-582 REV -F DATED 2017-08-02. COMPLIED WITH SKYWEST TASK 51-900-1002-SKY.

Part: STRINGER — CORRODED (BS 280-295 S19R) · 29,290 cycles

*CORROSION ON STGR 19R BETWEEN FS 280.00 €“ 295.00, AND FS 310.00 €“ 319.00 (C-CHECK RO 7/5/2021) REMOVED COROSION ON STGR 19 R BETWEEN FS 280.00 - 295.00 AND FS 310.00 - 319.00 REF REO 670-53-21-2060 REV -- DATED 2021-06-05 ALL STEPS COMPLIED WITH. FOUND TO BE WITHIN LIMITS PER MHIRJ REO 670-53-21-2060 REV-- DATED 2021-06-05 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: STRINGER — CORRODED (BS 349-394 S19R) · 29,290 cycles

*CORROSION ON STGR 19R BETWEEN FS 349.00 €“ 394.00. MARKED. (C-CHECK RO 7/5/2021) REPLACED STGR 19R FROM FS349-FS394.00 REF SRM 51-42-06-001-001-A01 DWG SH670-31070 REV J RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY & M-337

Part: DOOR SILL — CORRODED (GALLEY DOOR) · 29,290 cycles

*CORROSION ON GALLEY DOOR SILL. AREA MARKED. (C-CHECK RO 7/5/2021) REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER SILL ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG# SH670-31950 REV.Y. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD. OPS CHECK GOOD.

Part: STRINGER — CORRODED (BS 421-437 S25L) · 29,290 cycles

*CORROSION ON STGR 25L, BETWEEN FS 421.00 €“ 437.00. MARKED. (C-CHECK RO 7/5/2021) REPLACED STRINGER 25L BETWEEN FS409-FS453 REF CRJ 53-00-03-201-001-A01 AND DRAWING SH670-31350 REV A. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. COMPLIED WITH SKYWEST FORM M-337.

Part: STRINGER — CORRODED (BS 319-333 S24L) · 29,290 cycles

*CORROSION ON STGR 24L BETWEEN FS 319.00 €“ 333.00. MARKED. (C-CHECK RO 7/5/2021) REMOVED AND REPLACED STGR24L SECTION F.S.280.00-333.00 IAW CRJ-700 SRM 51-42-06-00-001-A01 REV38 25JULY2020 AND CRJ-700 SRM 51-42-21-00-001-A01 REV38 25JULY2020 AND BOMBARDIER DWG# SH670-31630 REV.-K

Part: STRINGER — CORRODED (BS 333-349 S22L) · 29,290 cycles

*CORROSION ON STGR 22L BETWEEN FS 333.00 €“ 349.00. MARKED. (C-CHECK RO 7/5/2021) REPAIRED STR 22L BETWEEN FS333-FS379. REF CRJ 700 SRM 53-00-03-201-001-A01, CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, DWG SH670-31366 REV NC, DWG SH670-32420 REV E, DWG SH670-31350 REV A . RESTORED FINISH APPLIED CIC. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY. COMPLIED WITH SKYWEST FORM M-337.

Part: INTERCOSTAL — CORRODED (BS 310-349 S21L) · 29,290 cycles

*CORROSION ON INTERCOSTAL ATTACHED TO STGR 21L BETWEEN FS 310.00 €“ 349.00. (C-CHECK RO 7/5/2021) REPLACED INTERCOSTAL BETWEEN F.S. 310.00 - F.S. 349.00 WITH NEW ONE'S P/N SH670-31822-1, SH670-31823-1 REF CRJ 700 SRM 51-42-06-001-001-A01. DWG SH670-31810 REV Y. COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — CORRODED (BS 295-310 S20R) · 29,290 cycles

*CORROSION ON STGR 20R BETWEEN FS 295.00 €“ 310.00 (C-CHECK RO 7/5/2021) REPLACED STR 20RH FROM FS280-FS319.00 WITH NEW. REF CRJ-700 SRM 53-00-03-201-001-A01. 51-42-06-001-001-A01 AND DRAWING SH670-31630 REV K / COMPLIED WITH 51-900-1002-SKY.

Part: STRINGER — CORRODED (BS 319-333 S27L) · 29,290 cycles

*CORROSION ON STGR 27 BETWEEN FS 319.00 €“ 333.00 ON LH AND RH SURFACES. AREA MARKED. (C-CHECK RO 7/5/2021) REMOVED AND REPLACED STGR27 SECTION BETWEEN F.S315.00 AND 333.00 IAW CRJ-700 SRM 51-42-06-001-001-A01 REV.38 25JULY2020 AND BOMBARDIER DWG# SH670-31630 REV.-K, COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — CORRODED (BS 295-310 S19L) · 29,290 cycles

*CORROSION ON STGR 19L, BETWEEN FS 295.00 €“ 310.00. MARKED. (C-CHECK RO 7/5/2021) REPLACED STGR 19L BETWEEN FS295.00-FS310.00 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31550 REV G. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. COMPLIED WITH SKYWEST FORM M-337.

Part: FLOORBEAM — CORRODED (BS 280 L-RBL 9) · 29,290 cycles

*MULTIPLE AREAS OF CORROSION ON FS 280.00 FLOOR SUPPORT BEAM BETWEEN LBL9 €“ RBL9 (C-CHECK RO 7/5/2021) REMOVED AND REPLACED COCKPIT FLOOR SUPPORT BEAM P/N CC670-34095-1 AT FS280 LBL9 - RBL9 REF DWG NO. CC670-33052 REV -G, CRJ700 SRM51-42-06-001-001-A01 AND SRM51-42-21-001-001-A01. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKWEST TASK CARD 51-900-1002-SKY

Part: STRINGER — CORRODED (BS 364-379 S20R) · 29,290 cycles

*CORROSION ON STGR 20R BETWEEN FS 364.00 €“ 379.00. MARKED. (C-CHECK RO 7/5/2021) REMOVED CORROSION ON STGR 20R BETWEEN FS364.00-FS379.00. WITHIN LIMITS. RESTORED FINISH PRESSURE CHECK GOOD. REF REO 670-53-21-2021 REV -- DATED 2021-04-27. COMPLIED WITH 51-900-1002-SKY

Part: FORMER — CORRODED (PAX DOOR) · 29,290 cycles

*PASSENGER DOOR €“ FORWARD FORMER HAS CORROSION ON INNER WEB, UNDER PANEL 832FL. (MARKED) (C-CHECK RO 7/5/2021) REPLACED PASSENGER FOWARD FORMER WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 29,290 cycles

*PASSENGER DOOR - INTERCOSTAL DD6 HAS CORROSION, MULTIPLE AREAS. (MARKED) (C-CHECK RO 7/5/2021) REPLACED PASSENGER DOOR INTERCOSTAL MID DD6 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 CRJ-700 SRM 51-42-21-001-001-A01 AND DRAWING 601R31702 REV N. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 29,290 cycles

*PASSENGER DOOR €“ INTERCOSTAL DD3 HAS CORROSION, MULTIPLE AREAS. (MARKED) (C-CHECK RO 7/5/2021) REPLACED PASSENGER DOOR MID DD3 INTERCOSTAL REF CRJ--700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DRAWING 601R31702 REV N. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (RT WING) · 29,290 cycles

R/H SLAT TRACK 3-2 HAS CORROSION (MARKED WITH RED) (C-CHECK RO 7/5/2021) DAMAGE TO R/H SLAT TRACK 3-2 BLENDED IAW MHI REO 670-57-42-1062 REV -- DATED 2021-04-28 ALL STEPS COMPLIED WITH. RIG CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (LT WING) · 29,290 cycles

L/H SLAT TRACK 2-2 HAS CORROSION (MARKED WITH RED) (C-CHECK RO 7/5/2021) DAMAGE TO L/H SLAT TRACK 2-2 BLENDED IAW MHI REO 670-57-42-1063 REV -- DATED 2021-04-28. ALL STEPS COMPLIED WITH. OPS CHECK GOOD. RIG CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: SLAT TRACK — WORN (LT WING) · 29,290 cycles

SLAT TEACK 3-3 L/H HAS TWO AREAS WORN ON LOWER SIDE (MARKED WITH RED) (C-CHECK RO 7/5/2021) DAMAGE TO L/H SLAT TRACK 3-3 BLENDED IAW MHI REO 670-57-42-1064 REV -- DATED 2021-04-28. OPS CHECK GOOD. RIG CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (RT WING) · 29,290 cycles

R/H SLAT TRACK 2-2 HAS CORROSION ON LWR SIDE (MARKED WITH RED) (C-CHECK RO 7/5/2021) DAMAGE TO R/H SLAT TRACK 2-2 BLENDED IAW MHI REO 670-57-42-1061 REV -- DATED 2021-04-27. ALL STEPS COMPLIED WITH. OPS CHECK GOOD RIG CHECK GOOD. COMPLIED WITH 51-900-1002-SKY.

Part: STRUCTURE — CHAFED (RT NACELLE) · 29,290 cycles

RH ENGINE UPPER CORE COWL CHAFED ON INTERIOR FWD SIDE (MARKED) (C-CHECK RO 7/5/2021) REPLACED INTERIOR GUSSET PN: CN622-0430-205 ON RH ENGINE COWL IAW CRJ700 SRM 51-42-13-001-001-A01 & DWG CN622-0201 REV L FUNCTIONAL CHECK GOOD.

Part: SLAT TRACK — CORRODED (RT WING) · 29,290 cycles

R/H SLAT TRACK 1-3 HAS CORROSION ON LWR SIDE (MARKED WITH RED) (C-CHECK RO 7/5/2021) DAMAGE TO R/H SLAT TRACK 1-3 BLENDED IAW MHI REO 670-57-42-1060 REV -- DATED 2021-04-28 ALL STEPS COMPLIED WITH. OPS CHECK GOOD. RIG CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (RT WING) · 29,290 cycles

R/H SLAT TRACK 1-2 HAS CORROSION ON LWR SIDE (MARKED WITH RED) (C-CHECK RO 7/5/2021) DAMAGE TO R/H SLAT TRACK 1-2 BLENDED IAW MHI REO 670-57-42-1059 REV -- DATED 2021-04-27. ALL STEPS COMPLIED WITH. OPS CHECK GOOD. RIG CHECK GOOD. COMPLIED WITH 51-900-1002-SKY

Part: HINGE FITTING — GOUGED (RT AILERON) · 29,290 cycles

R/H AILERON #2 HINGE FITTING ASSY ACFT SIDE HAS GOUGE (C-CHECK RO 7/5/2021) COMPLIED WITH MHIRJ REO 670-57-51-436 REV -- DATED 2021-04-24 STEPS #1 THRU #2 (SEE CONTINUATION CARD FOR WORK PREFORMED)

Part: SKIN — DENTED (BS 501 S16-17) · 29,290 cycles

DENT FOUND AT FS 501 BETWEEN STRINGERS 16 AND 17 (MARKED) (C-CHECK RO 7/5/2021) REPAIRED DENT FOUND AT FS501.00 BETWEEN STGR 16 AND 17. REF CRJ-700 SRM 53-00-01-201-001-A01. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY.

Part: BUSHING — DAMAGED (RT AILERON) · 29,290 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR PER AMM (C-CHECK RO 7/5/2021) REMOVED AND REPLACED THE BUSHINGS ON THE R/H WING AFT SPAR WHERE THE AILERON ATTACHES REF CRJ 700 AMM 20-31-00-000-801-A01 AND 20-31-00-400-805-A01. ALSO ORDERED AND RECEIVED HARDWARE FOR THE R/H AILERON INSTALLATION. SEE JOB 71004270 OP 584 CAMP 22433748 FOR DETAILS ON THE SPECIFIC ITEMS.

Part: WARNING SYSTEM — ACTIVATED (LAVATORY) · airframe 38,642 hrs · 29,286 cycles

SMOKE AFT LAV WARNING IN FLIGHT. SEE LOGPAGE 483528 DISCREPANCY #1 (FERRIED TO STL)

Part: CONNECTOR — BROKEN (E/E COOLING FAN) · 29,285 cycles

CANNON PLUG ON AVIONICS COOLING FAN FWD OF THE PRESSURE FLOOR AT F.S. 677 HAS A BROKEN SHEILD GROUND ON BACKSHELL. (C-CHECK) RO:1/28/2020REPLACED SHIELDED WIRE GROUND UNINSULATED TERMINAL LUG REF: CRJ 700 ESPM.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 35,525 hrs · 26,251 cycles

AFT CARGO DOOR HANDLE CRACKED. REMOVED AND LOCATED, DRILLED NEW SERVICEABLE AFT CARGO DOOR HANDLE ASSY PER SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE AFT CARGO DOOR HANDLE PER AMM 52-31-03-000-801 A01 & 52-31-03-400-801-A01.

Part: ANGLE — BENT · airframe 35,525 hrs · 26,251 cycles

LEFT AND RIGHT LOWER VISOR PANELS DAMAGED. REMOVED, FABRICATED NEW AND INSTALLED IAW ECTC SNIEO AV670-21200 S01, ECTC AV670-21405 S01 AND DRAWING AV670-21405.

Part: FAIRING — CRACKED (ZONE 400) · airframe 35,525 hrs · 26,251 cycles

LT UPPER AFT HINGE LINE FAIRING IS DENTED. FOUND CRACK DURING NDT AROUND A FASTENER HOLE. CUT OUT SECTION AROUND FASTENER HOLE. APPLIED A DOUBLER AND FILLER PER ECTC REO 670-78-33-998. REPAIRED DENT BY CAREFULLY DRESSING DAMAGED AREAS TO ORIGINAL FORM PER ECTC REO 670-54-21-1029.

Part: SKIN — CORRODED (BS 1031-1051) · airframe 35,525 hrs · 26,251 cycles

RADIO ALTIMETER RECEIVER, NR 2 ANTENNA AND NR 2 TRANSMIT ANTENNA BASE STRUCTURES CORRODED ON THE SKIN. REMOVED AND REPLACED THE ANTENNAS SPACERS AND SHIMS IAW SRM 51-42-06-001-001-AO1, AND DWG MM670-35007.

Part: SKIN — DENTED (ZONE 400) · airframe 35,525 hrs · 26,251 cycles

PANEL 432 AT IS DAMAGED ALONG FORWARD HINGE LINE AREA (BENT EDGE) LT UPPER. REDRESSED THE SKIN TO ORIGINAL FORM PER ECTC REO 670-54-14-1012.

Part: PANEL — CRACKED (PAX DOOR) · airframe 35,525 hrs · 26,251 cycles

UPON REMOVAL OF PAX DOOR DRAG ANGLE OF MODSUM REPAIR IS 670-52-110-107, FOUND AFT RISER CRACKED AT THE POWER ASSIST CABLE CUTOUT AREA. REPAIRED DAMAGED AREA PER REO 670-52-11-0935 REV - DATED 2017-02-20 AND EC/TC REO 670-52-11-935. THIS IS A MAJOR REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,525 hrs · 26,251 cycles

CRACKED FRAME AT FS 333 AND BETWEEN STR'S 1R AND 2R. REPAIRED CRACKED FRAME AT FS 333 AND BETWEEN STR'S 1R AND 2R IAW REO 670-53-21-1400 AND EC/TC REO 670-53-21-1400. THIS IS A MAJOR REPAIR.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,525 hrs · 26,251 cycles

CORROSION AT FS 549 AND FS 581. COMPLIED WITH ECTC AND REO 670-53-00-390 AS FOLLOWS. REMOVED DISCREPANT NUT PLATE. LOCALLY BLENDED OUT DAMAGE TO A SMOOTH SURFACE. VISUALLY INSPECTED FASTENERS ADJACENT TO DAMAGE AREAS FOR PROPER INSTALLATION. IF BLEND DEPTH EXTENDS OVER SOLID RIVET HEADS. MATERIAL REMOVED MUST NOT EXCEED 0.004 DEEP. NO BLENDS ARE ALLOWED OVER FASTENERS . LPI(FLUORESCENT) PER NDTM 51-20-008 OR EDDY CURRENT INSPECT PER NDTM 51-20-006 TO ENSURE REWORKED AREA ARE CRACK FREE. REPLACE NUT PLATES AT DISCREPANT LOCATION. FILL REMOVED MATERIAL CAVITIES WITH SEALANT PER SRM 51-23-00. APPLY CHEMICAL CONVERSION COATING MIL-5541 CLASS 1A FOLLOWED BY ONE COAT OF BAMS565-008 AND 2 COATS OF BAMS 565-009 (SRM 51-25-01)ALTERNATIVELY YOU CAN USE A023( ALODINE PRIMER AND TOP COAT)PER SRM 51-21-16 APPLY CORROSION INHIBITING COMPOUND TO REWORKED AREA PER SRM 51-21-11.

Part: FLOOR SUPPORT — CORRODED (BS 1088.2) · airframe 35,525 hrs · 26,251 cycles

CORROSION ON THE FLOOR SUPPORT ATBS 1088.2 AND LBL 35. COMPLIED WITH ECTC AND REO 670-53-00-390.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1041) · airframe 35,525 hrs · 26,251 cycles

FLOOR SUPPORT LBL 9 CORRODED, BS 1031 - 1041. REMOVED CORROSION IAW SRM 51-21-06-001-001 A01. REPAIRED THE FLOOR SUPPORT IAW EO 700-53-10-0022 AND COMPLIED WITH REO 670-53-61-133 AND ECTC REO 670-53-61-1333.

Part: CHANNEL — CORRODED (BS 295-310) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND CORROSION AROUND ANTENNA BASE HOLE ON STRINGER 27 AND BETWEEN BS 295 - 310. R & R TCAS CHANNEL.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND FLOORBEAM CORRODED. REMOVED CORROSION & PERFORMED UT AND EC NDT INSPECTIONS.

Part: FLOOR SUPPORT — CORRODED (BS 1088.20) · airframe 35,525 hrs · 26,251 cycles

CORROSION ON THE FLOOR SUPPORT BS 1088.20 AND LBL 35. COMPLIED WITH ECTC AND REO 670-53-00-390.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 35,525 hrs · 26,251 cycles

CORROSION THE FLOOR SUPPORT AT BS 349 AND 364. COMPLIED WITH ECTC AND REO 670-53-00-390.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE RT SIDE WALL SEAT TRACK CORRODED. REMOVED, FABRICATED, AND INSTALLED A NEW SIDE WALL SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE LT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE AREAS. REMOVED, FABRICATED, AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 701-761) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND LT SIDEWALL SEAT TRACK CORRODED IN SEVERAL AREAS. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE SEAT TRACK CORRODED IN SEVERAL AREAS. R & R THE SEAT TRACK.

Part: ANGLE — CRACKED (BS 909) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND ATTACH RIB ANGLE CRACKED AS VIEWED FROM UNDER PANEL 195AL. REPAIRED WING TO FUSELAGE AFT FAIRING SUPPORT.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,525 hrs · 26,251 cycles

CENTER CAP ANGLE AT PAX DOOR SURROUND HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH NEW CENTER CAP ANGLE PER SRM 51-42-06-001-A01 AND 51-42-06-001-A01.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND SEAT TRAC CORRODED IN SEVERAL AREAS. R & R THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 37,813 hrs · 28,367 cycles

DURING C CHECK, FOUND THE BS 581-677, LBL 9 SEAT TRACK CORRODED IN MULTIPLE AREAS. R & R THE SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND AFT FLOOR SUPPORT ANGLE FOR FLOOR PANEL 221ALF CORRODED. R & R THE FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 37,813 hrs · 28,367 cycles

DURING C CHECK, FOUND THE LT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE AREAS. R & R SEAT TRACK.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE RT BS 280 FLOORBEAM CORRODED AT FLOOR LEVEL. R & R THE FLOORBEAM.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED IN SEVERAL AREAS. R & R THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 647-847) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 847-1000) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK FOUND SEAT TRACK CORRODED IN SEVERAL AREAS. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 847-1000) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE SEAT TRACK CORRODED. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK.

Part: DOOR SILL — CORRODED (ZONE 100) · airframe 35,525 hrs · 26,251 cycles

LOWER SILL AT PAX DOOR SURROUND HAS CORROSION DAMAGE. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06-001-A01, AND 51-42-06-001-A01.

Part: SEAT TRACK — CORRODED (BS 377-701) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND LT SIDEWALL SEAT TRACK CORRODED IN SEVERAL AREAS. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE LT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE AREAS. FABRICATED AND INSTALLED A NEW SEAT TRACK.

Part: ANGLE — CORRODED (ZONE 100) · airframe 35,525 hrs · 26,251 cycles

CENTER CAP ANGLE T PAX DOOR SURROUND HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH NEW CENTER CAP ANGLE IAW SRM 51-42-06-001-A01 AND 51-42-06-001-A01.

Part: SEAT TRACK — CORRODED (BS 677-847) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND SEAT TRACK CORRODED. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE RT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE AREAS. FABRICATED AND INSTALLED A NEW SEAT TRACK.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,525 hrs · 26,251 cycles

LOWER SILL AT PAX DOOR SURROUND HAS CORROSION DAMAGE. REMOVED AND REPLACED LOWER SILL PER SRM 51-42-06-001-A01 AND 51-42-06-001-A01.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE SEAT TRACK CORRODED IN SEVERAL AREAS. R & R THE SEAT TRACK.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 30,876 hrs · 22,205 cycles

DURING C CHECK, FOUND FLOORBEAM CORRODED. REMOVED CORROSION AND PERFORMED UT THICKNESS CHECK AND REPAIRED CORRODED AREA.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND FWD FLOOR SUPPORT ANGLE AND PAX DOOR CORRODED. R & R FLOOR SUPPORT .

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE RT FLOOR SUPPORT CORRODED. R & R THE FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (BS 677-701) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE RT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE AREAS. REMOVED, FABRICATED, AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE LT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE AREAS. REMOVED, FABRICATED, AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE RT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE AREAS. REMOVED, FABRICATED, AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE RT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE AREAS. REMOVED, FABRICATED, AND REPLACED THE SEAT TRACK.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,525 hrs · 26,251 cycles

CORROSION ON FLOORBEAM AT BS 280. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-15-001-001-A01, 51-42-13-001-001-A01, 51-42-15-001-001-A01 AND 51-42-21-001-001-A01.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 35,525 hrs · 26,251 cycles

CORROSION ON FLOORBOARD 141ALF SUPPORT ANGLE AT FS 280. REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 51-42-15-001-001-A01, 51-42-13-001-001-A01, 51-42-15-001-001-A01 AND 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 701-761) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE RT SIDEWALL SEAT RAIL CORRODED IN MULTIPLE AREAS. REMOVED, FABRICATED, AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 35,525 hrs · 26,251 cycles

DURING C CHECK, FOUND THE RT SIDEWALL SEAT TRACK CORRODED IN MULTIPLE AREAS. REMOVED, FABRICATED, AND REPLACED SEAT TRACK.

Part: SKIN — DENTED (RUDDER) · airframe 35,525 hrs · 26,251 cycles

DENTS ON RT SIDE OF RUDDER EXTERNAL SKIN. RS 148.86 - 151.51 BY CUT OUT DAMAGE AND INSTALLED A DOUBLER IAW ECTC REO 670-55-41-051.

Part: SKIN — CORRODED (PAX DOOR) · airframe 35,525 hrs · 26,251 cycles

ASD CUTOUT FOR PANEL 832DL HAS CORROSION. REMOVED CORROSION. CORROSION OUT OF TOLERANCE. REPLACED PAX DOOR INNER SKIN PER SRM 51-42-06-001-001-AO1, ECTC REO 670-52-11-933, 51-42-21-001-001-A01.

Part: DOOR — CORRODED (MAIN PAX) · airframe 35,525 hrs · 26,251 cycles

ASD CUTOUT FOR PANEL 832DL HAS CORROSION. REMOVED THE CORROSION AND OUT OF TOLERANCE. REPLACED PAX DOOR INNER SKIN PER CRJ 700 SRM 51-42-06-001-001-AO1, ECTC REO 670-52-11-933, 51-42-21-001-001-A01.

Part: LIGHT — LOOSE (CABIN) · airframe 35,234 hrs · 26,040 cycles

F/A REPORTS AT 11B THE EMERGENCY FLOOR LIGHTING STRIP IS PULLED UP. REPLACED LT SIDE FLOOR TRACK LIGHTING COVER APROXIMATELY 3 FT SECTION NEAR 11/B IAW AMM 33-50-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,989 hrs · 25,852 cycles

RIGHT OVERWING FWD EMERGENCY LEFT INOPERATIVE. R & R THE BULB. OPS CHECK GOOD IAW AMM 33-51-15.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 34,989 hrs · 25,852 cycles

12CD LOWER EXIT SIGN HAVE 2 LIGHT BULBS BURNED OUT. R & R 12CD EXIT SIGN LIGHT BULBS IAW AMM 33-51-05. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 34,989 hrs · 25,852 cycles

MAIN ENTRANCE, BOTTOM LOWER EXIT SIGN HAVE 1 LIGHT BULB BURNED OUT. R & R MAIN ENTRANCE BOTTOM LOWER EXIT SIGN LIGHT BULB IAW AMM 33-51-05. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 34,989 hrs · 25,852 cycles

12AB LOWER EXIT SIGN HAVE 3 LIGHT BULBS BURNED OUT. R & R 12AB EXIT SIGN LIGHT BULBS IAW AMM 33-51-05. OPS CHECK GOOD.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 34,811 hrs · 25,699 cycles

ALL EMERGENCY LIGHTS INOPERATIVE. IAW MCC, SYS SELF RESET. FAULT NO LONGER EXISTS. NO FURTHER ACTION REQUIRED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 33,884 hrs · 24,957 cycles

12 AB AND 12CD LOWER EXIT SIGN HAVE 2 LIGHT BULBS BURNED ON EACH SIGN. R & R LIGHT BULBS IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,850 hrs · 24,928 cycles

ROW 4, EMERGENCY LIGHT. REPLACED THE LAMP IAW AMM 33-51-09.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,850 hrs · 24,928 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 4 IS OUT. REPLACED THE LAMP IAW AMM 33-51-09.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,714 hrs · 24,812 cycles

FORWARD FACING EXIT ROW LIGHT IS BURNED OUT ON SIGN OVERHEAD. R & R NR 2 BATTERY PACK IAW AMM 33-51-17. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,433 hrs · 24,599 cycles

NR 5 EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. 03-23-2015, RELAMPED CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,496 hrs · 23,874 cycles

SEVERAL INTERIOR EMERGENCY EXIT LIGHT BULBS INOPERATIVE. R & R THE BULBS IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 31,996 hrs · 23,475 cycles

MULTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK NR 1, NR 3, NR 4 AND BATTERY CHARGER ASSY NR 2 IAW AMM 33-51-17.

Part: BRACKET — MISSING (BS 752) · airframe 30,943 hrs · 22,691 cycles

FOUND FOUR MISSING BRACKETS FOR THE BLEED LOOPS IN AREA OF BS 752 LT AND RT. . FABRICATED BRACKETS IAW EO KBA670-35550, STEP 1. INSTALLED BRACKETS, IAW EO DWG KBA670-35550. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 30,943 hrs · 22,691 cycles

INTERCOSTAL CORRODED AT FS 364 AND S27R. REMOVED CORROSION IAW SRM 51-21-03-001-001-A01.

Part: BULKHEAD WEB — CANNING (BS 280) · airframe 30,943 hrs · 22,691 cycles

REMOVAL OF THE RT 280 BULKHEAD WEB FOUND TO BE OIL-CANNED APPROX 1 INCH ABOVE BUTT STRAP. COMPLIED WITH ECTC REO 670-53-11-906 AND REO 670-53-11-906 REV DATED 2014-1-30. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 30,943 hrs · 22,691 cycles

INTERCOSTAL CORRODED AT BS 364 AND S27L. REMOVED CORROSION IAW SRM 51-21-03-001-001-A01.

Part: STRINGER — CORRODED (BS 319-333) · airframe 30,943 hrs · 22,691 cycles

CORROSION AROUND RIVETS ON STRINGER 26R BETWEEN BS 319.7 - 333. REMOVED CORROSION IAW SRM 51-21-06-001-001 AND 51-42-06-001-001. COMPLIED WITH EA 20-2014-017 AND EC/TC EA 20-2014-017. COMPLIED WITH EC/TC REO 670-53-21-1071 AND REO 670-53-21-1071.

Part: STRAP — CORRODED (BS 280) · airframe 30,943 hrs · 22,691 cycles

CORROSION ON FS 280 STRAP BETWEEN S26L TO 25R. REMOVED CORROSION IAW SRM 51-21-06-001-001. REPAIRED IAW REO 670-53-21-1069.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,943 hrs · 22,691 cycles

FLOOR PANEL 221ALF AFT SUPPORT ANGLE THAT ATTACHES TO FS 280 CROSSBEAM IS CORRODED. R & R SUPPORT ANGLE.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 30,943 hrs · 22,691 cycles

RT LOWER WEB AT FS 280 IS CORRODED. COMPLIED WITH REO 670-53-11-594. INSTALLED WEB IAW REO 670-53-11-594. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,943 hrs · 22,691 cycles

FS 280 FLOORBEAM IS CORRODED. FLOORBEAM R & R IAW SB670BA-53-041.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 30,943 hrs · 22,691 cycles

RT FLOORBEAM BS 280 IS CORRODED. REMOVED RT FLOORBEAM IAW SRM 51-42-06-001-001 AND SRM 51-42-21-001-001. INSTALLED RT FLOORBEAM IAW DWG SH670-32170. MAJOR REPAIR.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 30,943 hrs · 22,691 cycles

LT LOWER WEB IAW FS 280 IS CORRODED AT DOOR POST. COMPLIED WITH REO 670-53-11-594. MAJOR REPAIR.

Part: WIRE — CHAFED (LT IDG) · airframe 30,943 hrs · 22,691 cycles

LEFT ENGINE IDG T1 LEAD IS CHAFING ON THE EXHAUST COWL. WRAPPED WIRES WITH PROTECTIVE TAPE TIED WIRES & REPOSITIONED THEM TO PREVENT CHAFING IAW REO 670-24-21-001. MAJOR REPAIR.

Part: WIRE — DAMAGED (IDG) · airframe 30,943 hrs · 22,691 cycles

RT ENGINE IDG LEAD PROTECTION SHEATHS ARE TORN AND MISSING IN SEVERAL PLACES. WRAPPED WIRES WITH PROTECTIVE TAPE IAW REO 670-24-21-001. NO DEFECTS NOTED AT THIS TIME. MAJOR REPAIR.

Part: WARNING MESSAGE — ILLUMINATED (ANTI-ICE SYSTEM) · airframe 30,882 hrs · 22,644 cycles

ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT. COMPLIED QRH, EMERGENCY DECLARED AS A PRECAUTION. NO FAULT FOUND WHEN ACFT POWERED UP. PERFORMED BLEED LEAK TEST IAW FIM 36-21-03.

Part: RETAINER — DAMAGED (PAX DOOR) · airframe 30,004 hrs · 22,001 cycles

RAISED METAL ON SEAL RETAINER FOR ASD AFT UPPER AREA. REPAIRED IAW SRM IAW SRM 51-12-00. CLASSIFIED AS MAJOR.

Part: SKIN — CRACKED (PAX DOOR) · airframe 28,605 hrs · 20,993 cycles

PASSENGER DOOR CRACKED IN OUTER SKIN FWD BOTTOM CORNER FORWARD OF DOOR HINGE. REPAIRED IAW REO 670-52-11-698 AND SRM 51-21-16.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 27,672 hrs · 20,309 cycles

MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE IAW AMM 25-51-14. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 813.7-847) · airframe 26,236 hrs · 19,255 cycles

LEFT SEAT TRACK CORRODED BEWTEEN FS 813.70 AND 847. REMOVED CORROSION AND FOUND TO DAMAGE TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 708-761.85) · airframe 26,236 hrs · 19,255 cycles

RIGHT SEAT TRACK HAS CORROSION BETWEEEN FS 708 TO 761.85. REMOVED AND INSTALLED SEAT TRACK IAW SRM 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 711-761.85) · airframe 26,236 hrs · 19,255 cycles

LEFT SEAT TRACK HAS CORROSION BETWEEN FS 711 AND 761.85. REPAIRED IAW REO 670-53-00-343 AND GREO 670-53-00-343.

Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 26,236 hrs · 19,255 cycles

VERTICAL ANGLE AT RBL 26 IS CRACKED ON 280 BULKHEAD. FABRICATED ANGLE IAW DWG CC670-34117 AND LOCATED IAW SRM 51-40-11-001-001. INSTALLED ANGLE IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 26,236 hrs · 19,255 cycles

VERTICAL ANGLE AT LBL 26 IS CRACKED ON 280 BULKHEAD. FABRICATED ANGLE IAW DWG CC670-34117 AND LOCATED IAW SRM 51-40-11-001-001. INSTALLED ANGLE.

Part: WEB — CORRODED (BS 280) · airframe 26,236 hrs · 19,255 cycles

RT 280 WEB CORRODED. REPAIRED IAW REO 670-53-11-594. PERFORMED EDDY CURRENT INSPECTION OF CUTLINE ON LOWER WEB IAW REO 670-53-11-594 & NDTM PART1, 51-20-006. NO INDICATIONS NOTED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,236 hrs · 19,255 cycles

FLIGHT DECK FWD FS 280 CROSSBEAM CRACKED UNDER LBL9 AND RBL9 AT TEE BRACKETS.

Part: SEAT TRACK — CORRODED (BS 677-693) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK CORRODED BETWEEN FS 677-693 LBL 9. REMOVED CORROSION AND FOUND DAMAGE TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 708-761.85) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 708 AND 761.85. REMOVED CORROSION AND FOUND DAMAGE TO BE OUT OF LIMITS REO670-53-00-013. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 711-761.85) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 711 AND 761.85. REMOVED CORROSION AND FOUND DAMAGE TO BE OUT OF LIMITS IAW REO670-53-00-013. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,236 hrs · 19,255 cycles

FS 280.00 FLOORBEAM CORRODED. REPAIRED IAW REO 670-53-11-047 AND REO 670-53-11-047 REV E.

Part: SEAT TRACK — CORRODED (BS 485-549) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 485 AND 549. REMOVED CORROSION IAW SRM 53-31-49-101-001-A01. DAMAGE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A02. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED NEW SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 677-693) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 677-693 LBL 9. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785.15-813.7) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 785.15 AND 813.70. REMOVED CORROSION AND FOUND DAMAGE TO BE OUT OF LIMITS REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801 AND INSTALLED IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK CORRODED BETWEEN FS 485-581, LBL 9. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01 AND 51-41-02. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001-A01. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 813.7-847) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 813.70 AND 847. REMOVED CORROSION IAW SRM 53-51-51-101-001-A01. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A02 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-621) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 581 AND 621. FABRICATE SEAT TRACK IAW REO 670-53-00-343. R & R SEAT TRACK IAW AMM 53-00-04-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 396) · airframe 26,236 hrs · 19,255 cycles

LEFT SEAT TRACK HAS CORROSION AT FS 396. REPAIRED IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 613-645) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION AT FS 613 AND 645. REMOVED CORROSION IAW SRM 53-31-49-101-001-A01. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PRODCEDURE UT-3. FOUND TO BE WITHIN LIMITS IAW SRM 53-31-45-101-001-A01. BLEND AREA REQUIRE TREAT. TREATED BLENDED AREAS IAW SRM 51-12-00-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 533-549) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 533 - 549 LBL 9. REMOVED AREA OF CORROSION IAW SRM 53-31-49-101-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PRODCEDURES UT-3. MIN MATERIAL REMAINING IS .368" ORIGINAL IS .370' MATERIAL REMOVED IS .002" VJ161730. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-31-45-101-001-A01. TREATED BLENDED AREA SRM 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 677 AND 708. REMOVED CORROSION AND FOUND DAMAGE TO BE OUT OF LIMITS REO 670-53-00-013. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT SIDE RAIL LT SIDE AT FS675 TO FS713 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 461) · airframe 26,236 hrs · 19,255 cycles

LEFT SEAT TRACK HAS CORROSION AT FS 461. REPAIRED IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 519) · airframe 26,236 hrs · 19,255 cycles

LEFT SEAT TRACK HAS CORROSION AT FS 519. REMOVED CORROSION AND FOUND DAMAGE TO BE OUT OF LIMITS IAW REO 670-53-00-013. R & R SIDE SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK CORRODED BETWEEN FS 349 RBL 9. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. REMOVED SEAT TRACK IAW SRM 51-41-02-001-001-A01. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK CORRODED BETWEEN FS 581-677 LBL 9. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. FABRICATED SEAT TRACK IAW REO 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,236 hrs · 19,255 cycles

FS280.00, LBL 9 FLOORBEAM TEE CRACKED. REPLACED WITH THE INCORPARATION OF IS670531100026.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,236 hrs · 19,255 cycles

RBL 9, FS 280.00 FLOORBEAM TEE CRACKED . REPLACED TEE.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION BETWEEN FS 581-677 LBL 9. REMOVED CORROSION AND FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 429) · airframe 26,236 hrs · 19,255 cycles

LEFT SEAT TRACK HAS CORROSION AT FS 429. FOUND BLEND AREA AND OUT OF LIMITS IAW REO 670-53-00-013. R & R SEAT TRACK IAW AMM 53-00-04-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 26,236 hrs · 19,255 cycles

RIGHT SEAT TRACK HAS CORROSION BETWEEN FS 379 AND 485. REMOVED CORROSION AND FOUND DAMAGE TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-00-801. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED NEW SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 551) · airframe 26,236 hrs · 19,255 cycles

SEAT TRACK HAS CORROSION AT FS 551. REMOVED CORROSION AND FOUND TO DAMAGE TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK FROM FS 477-573 IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT RAIL IAW REO 670-53-00-343. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOOR PANEL — CRACKED · airframe 26,236 hrs · 19,255 cycles

FORWARD EQUIPMENT COMPARTMENT BAY FLOOR CRACKED ON LT SIDE OF BRAKE ACCUMALATOR GOUGED. COMPLY WITH EC/TC REO 670-53-11-509. COMPLIED WITH EC/TC REO 670-53-11-509 AND GENERIC REO 670-53-11-509 REV. RII FOUND TO BE SATISFACTORY.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 26,236 hrs · 19,255 cycles

FORWARD EQUIPMENT COMPARTMENT BAY FLOOR CRACKED ON RT SIDE UNDER ADS STOW PUMP. COMPLY WITH EC/TC REO 670-53-11-505. COMPLIED WITH EC/TC REO 670-53-11-509 AND GENERIC REO 670-53-33-509 REV. RII FOUND TO BE SATISFACTORY.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,236 hrs · 19,255 cycles

CRAWLWAY FLOOR SUPPORT CORRODED. CORROSION BEYOND ALLOWABLE LIMITS IAW SRM 53-00-00-161-001-A01. R & R SUPPORT ANGLE REF SRM 51-42-06-001-001 AND SRM 51-42-21-001-001.

Part: SEAL — LACK OF LUBE (EMERGENCY EXIT) · airframe 26,236 hrs · 19,255 cycles

LEFT OVERWING EMERGENCY EXIT FAILED, THE PULL FUNCTIONAL TEST PULLED 50 POUNDS. MAXIMUM LIMIT IS 40 POUNDS. CHECKED AND LUBRICATED SEAL, HATCH NOW OPENS AT 20LBS. ACCOMPLISHED IAW AMM 52-21-05-720-801.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED · airframe 25,982 hrs · 19,062 cycles

ANTI-ICE DUCT RED WARNING IN FLIGHT FOLLOWED QRH AND ICING CONDITIONS. EMERGENCY DECLARED. RESET ANTI-ICE SYS IAW FIM 30-11-00. NO DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 25,928 hrs · 19,023 cycles

EMERGENCY LIGHTS WOULD NOT COME ON. CHARGED BATTERY PACKS BY RUNNING APU, OPS CHECKED GOOD, IAW AMM33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,710 hrs · 18,172 cycles

EMERGENCY LIGHTS IN GALLEY INOP. R & R EPSU BATTERY PACK IAW AMM 33-51-17, OPS CHECK GOOD NO DEFECTS NOTED.

Part: PROXIMITY SENSOR — FAILED (CARGO DOOR) · airframe 24,190 hrs · 17,829 cycles

AT 8.3 DELTA P "AFT CARGO DOOR" CAUTION WITH PROX SYS FAULT 2 STATUS MESSAGE. DURING DESCENT MESSAGE EXTINGUISHED & REAPPEARED AT 4.0 DELTA P STAYED ON TILL AFT CARGO DOOR OPENED. DIVERT. LANDING UNEVENTFUL. R & R AFT CARGO DOOR PX39 & PX102. ALSO, REPLACED MATRIX SPLICES SP121,SP126, SP122. MAINT PERFORMED IAW WDM 52-70-01, AMM TASKS 52-70-02-000-801-A02, 52-70-02-400-801-A02, 52-70-02-000-802-A01, 52-710-02-400-802-A01. ALL OP'S CHECKS ARE GOOD. RETURNED TO SERVICE.

Part: ELEMENT — MALFUNCTIONED (FIRE DETECTION) · airframe 23,722 hrs · 17,488 cycles

FIRE SYS FAULT STATUS MESSAGE. REPLACED AS A PRECAUTION THE NR 4 ELEMENT A241 LOOP "B" ON THE LT ENGINE IAW AMM TASK 26-11-11-00-801-A01. OPS CHECK OF THE FIRE EX SYS CKS GOOD. NO MESSAGES ON THE MDC.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION) · airframe 23,509 hrs · 17,337 cycles

FIRE SYS FAULT STATUS MESSAGE. PLACED SYS ON MEL 26-00-1. 11/29 CLEARED BY: R & R CONTROL UNIT IAW AMM 26-10-01-000 (400) -801. OPS CHECKS GOOD. RETURNED TO SERVICE.

Part: SENSING ELEMENT — MALFUNCTIONED (FIRE WARNING) · airframe 23,444 hrs · 17,287 cycles

FIRE SYS FAULT STATUS MESSAGE. PLACED ON MEL 26-00-1. MDC FAULT HISTORY INDICATES LT ENG FIRE LOOP B, SHORTED, FAULT IS NOT CURRENT. REMOVED LT ENG LOWER FIRE DETECTION RAIL IAW MM 26-11-03-000-801 AND INSTALLED NEW SERVICEABLE LOOP A239. REINSTALLED RAIL IAW 26-11-03-400-801. OPS CK GOOD, CLEAR MEL. RETURNED TO SERVICE.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 22,531 hrs · 16,588 cycles

RT V-STAB TO FUSELAGE ATTACHMENT DRAG ANGLE IS POSSIBLY CRACKED. APPROX STA 1240 HFEC INSPECTED SUSPECTED CRACK IAW NDTM PART 6, 53-00-000-250-A01. CRACK INDICATION NOTED, APPROX 1.2" LONG. REMOVED FASTENERS AND CUT OUT DAMAGE ON ATTACHMENT DRAG ANGLE IAW REO 670-55-31-018. HFEC INSPECTED AT CUT OUT FOR CRACK IAW NDTM PART 1, 51-20-006, NO CRACK NOTED. FABRICATED FILLER ANGLE AND ANGLE DOUBLER IAW REO 670-55-31-018. FAY SEALED FILLER AND DOUBLER AND INSTALLED NEW DOUBLER IAW REO 670-55-31-018.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 21,830 hrs · 16,065 cycles

ON TAXI IN THE FLAPS FAIL CAUTION ILLUMINATED. ACFT DOWN FOR REPAIRS.

Part: FITTING — CORRODED (JACK POINT) · airframe 21,629 hrs · 15,922 cycles

RFD - NOSE GEAR JACK POINT FITTINGS BOTH RIGHT AND LEFT HAVE MINOR SURFACE CORROSION. REMOVED RIVETS TO GAIN ACCESS. BLENDED CORROSION. NO CRACKS FOUND. AREA REMOVED WITHIN LIMITS. INSTALLED RIVETS AND PRIMED AND PAINTED AREA.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · airframe 21,629 hrs · 15,922 cycles

RFD - CORROSION ON THE FORWARD INBOARD SIDE OF THE GALLEY SERVICE DOOR. BLENDED CORROSION. BLENDED AREA WITHIN LIMITS IAW SRM 53-21-23-002-A01. TREATED AREA AND PRIMED AND PAINTED.

Part: SKIN — CORRODED (E/E DOOR) · airframe 21,629 hrs · 15,922 cycles

RFD - CORROSION ON AVIONICS DOOR CUT OUT (INNER SKIN). BLENDED AREA FOR A SMOOTH FINISH. REMOVED MATERIAL IS WITHIN LIMITS IAW REO 670-53-21-242. PERFORMED PRESSURIZATION CHECK WITH NO DEFECTS NOTED.

Part: ATTACH ANGLE — CORRODED (SERVICE DOOR) · airframe 21,629 hrs · 15,922 cycles

RFD - CORROSION FOUND ON GALLEY SERVICE DOOR MID CAP ATTACH ANGLE. REMOVED AFT DOOR STOP FITTINGS AND LOWER SILL ANGLE. ANGLE IS CORRODED BEYOND LIMITS. INSTALLED NEW ANGLE AND HARDWARE.

Part: SEAT TRACK — CORRODED (BS 570-672) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - RT SIDE SEAT TRACK FROM FS 570.00 TO 672.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED RT SIDE SEAT TRACK, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 21,629 hrs · 15,922 cycles

PAX DOOR MID CAP ANGLE IS CORRODED. REMOVED CORRODED ANGLE, FOUND TO BE CORRODED THROUGHOUT AND BEYOND LIMITS IAW SRM 53-21-23-001-A01 PG 101, ALL WORK DONE IAW SRM 51-42-02-001-001-A01. LOCATED AND DRILLED NEW MID CAP ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED MID CAP ANGLE ON SILL IAW SRM 51-41-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - LT SIDE SEAT TRACK FROM FS 379-485.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED LT SIDE SEAT TRACK. FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 711-761) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - RT SIDE SEAT TRACK FROM FS 711.00 TO 761.85 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED RT SIDE SEAT TRACK FROM FS 711.00 TO 761.85 , FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 711-761) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - LT SIDE SEAT TRACK FROM FS 711-761.85 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED LT SIDE SEAT TRACK, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK FROM FS 711 TO 761.85 IAW AMM 53-00-49-000-801. INSTALLED NEW LT SIDE SEAT TRACK FROM FS 711 TO 761.85 IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 855-977) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - RT FLOOR SEAT TRACK FROM FS 855.40 TO 977.00 IS CORRODED. FOUND THAT TRACK IS CORRODED BEYOND LIMITS IAW REO 670-53-00-013. REMOVED RT FLOOR SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW TASK 53-00-49-400-801-A02 AT FS 855.40 TO 977.00 RT SIDE.

Part: SEAT TRACK — CORRODED (BS 855-977) · airframe 21,629 hrs · 15,922 cycles

C-CHECK, LT FLOOR SEAT TRACK FROM FS 855.40 TO 977.00 IS CORRODED. FOUND THAT TRACK IS CORRODED BEYOND LIMITS IAW REO 670-53-00-013. REMOVED LT FLOOR SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW LT FLOOR SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 785-860) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - RT SIDE SEAT TRACK FROM FS 785.15 TO 860.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED RT SIDE SEAT TRACK, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: STRIKER — CORRODED (PAX DOOR) · airframe 21,629 hrs · 15,922 cycles

C CHECK - PAX DOOR STRIKER ANGLE IS CORRODED. FOUND STRIKER ANGLE TO BE CORRODED THROUGHOUT AND IS BEYOND LIMITS IAW SRM 53-21-23-001-001-A01 PAGE 101. REMOVED STRIKER ANGLE, LOCATED AND DRILLED NEW ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED STRIKER ANGLE IAW SRM 51-40-06-001-001-A01 AND 51-42-21-001-001-A01. APPLIED TOP COAT AS REQUIRED IAW SRM 51-25-16-001-001-A01. APPLIED AV-8 IAW SRM 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 677-711) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - RT SIDE SEAT TRACK FROM FS 677.00 TO 711.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED RT SIDE SEAT TRACK, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 185-581) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - LT FLOOR SEAT TRACK FROM FS 185.00 TO FS 581.00 IS CORRODED. FOUND SEAT TRACK TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED TRACK IAW AMM 53-00-49-000-801-A02. INSTALLED NEW TRACK IAW AMM TASK 53-00-49-400-801.

Part: STRINGER — CORRODED (BS 319-333 S25L) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - CORROSION ON STR 25L BETWEEN FS 333.00 AND 319.00. BLENDED AREA IS NO DAMAGE AREA IAW SRM 53-21-03-101-002-A01. MATERIAL REMAINING ON STR IS .046 AND .060 ON DOUBLER. SENT DAMAGE REPORT TO MFG FOR AN REO. PERFORM ECI ON BLENDED AREA, NO CRACKS OR CORROSION FOUND AT THIS TIME, IAW NDTM 51-20-006. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED AV-8 IAW SRM 51-21-11-001-001-A01. WORK PERFORMED IS IN CONFORMITY WITH TASK CARD REO 670-53-21-533.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - AFT CARGO DOOR SILL CORRODED AROUND NUT PLATE HOLES AND AT ANGLES OF RADIUS. BLENDED CORROSION IAW 51-21-06-001-001-A01. PERFORMED ECI ON BLENDED AREAS, NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM 51-20-006. MAPPED OUT DAMAGE AND SENT TO MFG FOR REO. TREATED AND PRIMED AREA IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01. WORK PERFORMED IN CONFORMITY WITH TASK CARD REO 670-53-61-559.

Part: SEAT TRACK — CORRODED (BS 570-677) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - LT SIDE SEAT TRACK FROM FS 570.00 TO 677.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED LT SIDE SEAT TRACK FROM FS 570.00 TO 677.00, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: STRINGER — CORRODED (BS 319-333 S25R) · airframe 21,629 hrs · 15,922 cycles

CORROSION ON STRINGER 25R BETWEEN FS 333.00 AND 319.00. BLENDED AREA IS NO DAMAGE AREA YAW SUM 53-21-03-101-002-A01. MATERIAL REMAINING ON STIR IS .046 AND .060 ON DOUBLERS. SENT DAMAGE REPORT TO MFG FOR AN REO. PERFORM EKE ON BLENDED AREA, NO CRACKS FOUND AT THIS TIME, YAW NET 51-20-006. TREATED, PRIMED AND PAINTED YAW SUM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED AV-8 YAW SUM 51-21-11-001-001-A01. WORK PERFORMED IS IN CONFORMITY WITH TASK CARD REO 670-53-21-533.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - LT SIDE SEAT TRACK FROM FS 863.00 TO 969.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED LT SIDE SEAT TRACK, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - LT SIDE SEAT TRACK FROM FS 863.00 TO 969.00 HAS NUMEROUS SPOTS OF CORROSION. EVALUATED LT SIDE SEAT TRACK, FOUND CORROSION ON SEAT TRACK SCREW COUNTERSINK. COUNTERSINK IS A NO ALLOWABLE DAMAGE AREA IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SILL — CORRODED (BS 280-319) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - CORROSION ON RT FLOOR SILL FROM FS 319.00 TO FS 280.00. BLENDED MINOR SUFACE CORROSION, MATERIAL THICKNESS IS .050. BLENDED MATERIAL MEASURES AT .004 DEPTH WITH .046 REMAINING. BLEND IS WITHIN LIMITS IAW SRM 53-21-43-001-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, AND 51-25-16-001-001-A01. APPLIED AV-8 TO THE AREA IAW SRM 51-21-11-001-001-A01.

Part: ATTACH BRACKET — GOUGED (FUSELAGE) · airframe 21,629 hrs · 15,922 cycles

C CHECK - DURING INSP FOUND GOUGES ON LT LOWER CASCADE ATTACHMENT BRACKET. BLENDED 2 GOUGES SMOOTH IAW SRM 51-12-00-001-001-A01. PERFORMED LPI ON BLENDS, NO CRACKS NOTED AT THIS TIME IAW NDTM LPI 51-20-008. TREATED, PRIMED IAW SRM 51-21-11-001-001-A01 AND 51-25-16-001-001-A01. ALL WORK PERFORMED IAW REO 670-78-34-970.

Part: FITTING — DAMAGED (RT MLG) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - RT MLG SIDE STAY FITTING DAMAGED 2 PLACES ON OTBD UPPER FLANGE. BLENDED OUT DAMAGE AND WITHIN LIMITS IAW REO 670-57-11-043. PERFORMED LPI ON BLENDED AREAS, NO CRACKS NOTED AT THIS TIME, IAW LPI NDTM 51-20-08, REO 670-57-11-043. PERFORMED ROTO PEEN IAW REO 670-57-11-043. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. ALL WORK PERFORMED IS IN CONFORMITY WITH REO 670-57-11-043.

Part: DOOR FRAME — DAMAGED (CARGO DOOR)

C CHECK - FWD CARGO BAY DOOR SURROUND STRUCTURE HAS GOUGES IN FWD LOWER CORNER AND AFT LOWER CORNER OF STRIKER SEAL. REMOVED DAMAGE IAW SRM 51-12-00-001-001-A01. BLENDED AREAS ARE WITHIN LIMITS IAW SRM 53-31-23-101-001-A01 AND 53-00-00-101-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: DOOR FRAME — GOUGED (CARGO BAY) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - FWD CARGO BAY DOOR SURROUND STRUCTURE HAS GOUGES IN FWD LOWER CORNER AND AFT LOWER CORNER OF SEAL RETAINER. DAMAGE FOUND TO BE DENTS NOT GOUGES. REMOVED DAMAGE IAW SRM 51-12-00-001-001-A01. BLENDED AREAS ARE WITHIN LIMITS IAW REO 670-52-35-127. PERFORMED ECI ON BLENDED AREA IAW NDTM 51-20-006 AND REO 670-52-35-127. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. ALL WORK PERFORMED IS IN CONFORMITY WITH REO 670-52-35-127.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - CHAFE DAMAGE FOUND ON RT ENG LOWER TRANSCOWL SLIDER INBD. BLENDED DAMAGED AREA IAW AND WITHIN TOLERANCE OF REO 670-78-34-384. TREATED AND PRIMED IAW SRM 51-21-11-001-001, 51-25-06-001-001. ALL WORK WAS PERFORMED IAW REO 670-78-34-384.

Part: SKIN — CHAFED (BS 977) · airframe 21,629 hrs · 15,922 cycles

C-CHECK- 2 BELLY SKINS CHAFED AT FS 977 FROM PANELS 195DL/196DR. BLENDED CHAFED AREA IAW REO 670-53-00-014. PERFORMED LPI ON BLENDED AREAS, NO CRACKS NOTED AT THIS TIME, IAW REO 670-53-00-014 NDTM 51-20-08. ALL BLENDED AREAS ARE WITHIN LIMITS IAW REO 670-53-00-014. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: FITTING — DAMAGED (LT MLG) · airframe 21,629 hrs · 15,922 cycles

C-CHECK -LT MLG SIDE STAY FITTING DAMAGED AT UPPER OTBD FLANGE EDGE. BLENDED OUT DAMAGE AND WITHIN LIMITS IAW REO 670-57-11-043. PERFORMED LPI ON BLENDED AREAS, NO CRACKS NOTED AT THIS TIME, IAW LPI NDTM 51-20-08, REO 670-57-11-043. PERFORMED ROTO PEEN IAW REO 670-57-11-043. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. ALL WORK PERFORMED IS IN CONFORMITY WITH REO 670-57-11-043.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - CORROSION ON RT FLOOR SEAT TRACK FROM FS 349.00 TO FS 485. FOUND CORROSION TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801, PREPPED NEW TRACK FOR INSTALL IAW SRM 51-40-11-001-001-A01, TREATED TRACK IAW SRM 51-21-11-001-001. INSTALLED TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 581-691) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - CORROSION ON RT FLOOR SEAT TRACK FROM FS 581.00 TO FS 691.50. FOUND CORROSION TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A01, PREPPED NEW TRACK FOR INSTALL IAW SRM 51-40-11-001-001, ETCHED AND ALODINED TRACK IAW SRM 51-21-11-001-001. INSTALLED TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 21,629 hrs · 15,922 cycles

C CHECK -CORROSION ON LT FLOOR SEAT TRACK FROM FS 349.00 TO FS 485.00. FOUND CORROSION TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED LT FLOOR TRACK IAW AMM 53-00-49-000-801. PREPARED NEW SEAT TRACK IAW SRM 51-40-11-001-001-A01, TREATED IAW SRM 51-21-11-001-001. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 485-570) · airframe 21,629 hrs · 15,922 cycles

C CHECK - NUMEROUS SPOT OF CORROSION ON LT FLOOR SEAT TRACK FROM FS 485.00 TO FS 570. FOUND CORROSION TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801, DRILLED NEW TRACK FOR INSTALL IAW SRM 51-40-11-001-001, ETCHED AND ALODINED TRACK IAW SRM 51-21-11-001-001-A01. INSTALLED TRACK IAW AMM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,629 hrs · 15,922 cycles

C-CHECK -SURFACE CORROSION FOUND ON TOP FLANGE OF FS 280.0 BEAM. BLENDED SURFACE CORROSION, REMOVED .002" MATERIAL IAW SRM 53-21-43-101-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-06-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,629 hrs · 15,922 cycles

C-CHECK -FLOORBEAM ANGLE ON FWD SIDE OF 280.0 IS CORRODED. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-21-001-001-A01. INSTALLED NEW NUTPLATES USING CR3214-4 FASTENERS, ALL WORK IAW SRM 51-42-13-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - LT AND RT LOWER BULKHEAD AT FS 280, SHOWS EVIDENCE OF CORROSION. BLENDED LIGHT SURFACE CORROSION IAW SRM 53-11-10-201-003-A01. TREATED, PRIMED & PAINTED WORKED AREAS IAW SRM 51-21-06-001-001-A01, 51-21-11-001-001-A01, AND 51-25-16-001-001-A01.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 21,629 hrs · 15,922 cycles

C-CHECK - FWD AND AFT ATTACH CLIP ANGLES SHOW SURFACE CORROSION AT INNER DOOR SECTION UPPER HINGE AREA. REMOVED CLIPS IAW SRM 51-42-06-001-001-0A01. REMAINING MATERIAL ON ALL CLIPS MEET CRITERIA IAW SRM 53-21-43-101-001-A01. TREATED, PRIMED AND PAINTED WORKED AREAS IAW SRM 51-21-06-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01, AND 51-21-16-001-001-A01. INSTALLED CLIPS IAW SRM 51-42-06-001-001-A01, APPLIED HARDCOAT IAW SRM 51-21-11-001-001-A01.

Part: FIRE DETECTOR — MALFUNCTIONED · airframe 21,280 hrs · 15,664 cycles

"FIRE SYS FAULT" STATUS MESSAGE. (INTERMITTENT ON & OFF). PLACED ON MEL 26-00-1 REF TO PAST T/S IN TRAX AND NO CURRENT FAULTS IN MDC OR STATUS MSG. R & R RT ENG UPPER AND LWR FIRE DETECT RAILS AS A PRECAUTIONARY MEASURE IAW AMM 26-11-01-000/400-802 AND 26-11-03-000/400-802. FIRE DETECT SYS TEST GOOD, NO STATUS MSG SHOWN. MEL CLEARED. RETURNED TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE DETECTION) · airframe 21,218 hrs · 15,616 cycles

FIRE SYS FAULT STATUS MESSAGE ON INTERMITTENT DURING FLIGHT. PLACED ON MEL 26-00-1. RETURNED TO SERVICE.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 20,194 hrs · 15,524 cycles

FWD CABIN DOOR UPPER DOOR STOP BRACKET CRACKED. REF. W/O 90683, N/R-00001. REMOVED AND REINSTALLED SAME BRACKET. ALLOWED IAW REO 670-53-21-518/1. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BRAKE ASSY — OUT OF ALIGNMENT (NR 1) · airframe 20,839 hrs · 15,339 cycles

PDX- WHEN BRAKES APPLIED DURING TAXI, LOUD SQUEAL HEARD IN COCKPIT AND CABIN. C/W VISUAL INSPECTION AND FOUND NR 1 MAIN WHEEL DRIVE KEYS NOT ALIGNED WITH BRAKE SLOTS. REMOVED MAIN WHEEL ASSY. AND VISUALLY INSPECTED BRAKE AND WHEEL ASSYS. NO DEFECTS NOTED. REALIGNED BRAKE SLOTS AND REINSTALLED WHEEL REF TASK CARD R324101. A/C O.K. FOR SERVICE. NO PARTS REPLACED.

Part: FIRE WARNING — MALFUNCTIONED · airframe 20,631 hrs · 15,174 cycles

FIRE SYST FAULT STATUS MSG CYCLES ON AND OFF. SYS PLACED ON MEL 26-00-1. RETURNED ACFT TO SERVICE.

Part: WIRE — DAMAGED (CARGO DOOR) · airframe 20,420 hrs · 14,995 cycles

PDX - PROX SYS FAULT 2 STATUS MSG. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. REPAIRED THE AFT CARGO DOOR INDICATION WIRING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACM — FAILED (AC BAY) · airframe 20,412 hrs · 14,987 cycles

MFR - THERE WAS A SMOKE SMELL IN CABIN / COCKPIT, TURNED OFF PACK 2 SMOKE SUBSIDED. RT PACK WILL NOT HEAT A/C IN AUTO OR MAN MODE. DIVERTED TO MFR AND ACCOMPLISHED A UNEVENTFUL LANDING. CFR MET AIRCRAFT. CHECKED MDC AND FOUND NO AIR CONDITIONING RELATED FAULTS. REPLACED NR 2 AIR CYCLE MACHINE IAW CRJ-700 MM TASK NUMBERS 21-51-08-000-801-A01 AND 21-51-08-400-801-A01. AIR CONDITIONING TEMPERATURE CONTROL SYSTEM OPERATIONAL TEST GOOD IAW CRJ-700 MM TASK 21-60-00-710-801. NO UNUSUAL ODORS NOTED IN FLIGHT DECK OR CABIN DURING OPERATIONAL TEST. RETURNED TO SERVICE.

Part: AIR DUCT — CONTAMINATED · airframe 19,360 hrs · 14,168 cycles

PDX - SMOKE AFT LAVATORY MESSAGE, MASTER WARNING, AFTER TAKEOFF. PERFORMED CHECKLIST AND PULLED APPLICABLE CB'S. RETURNED TO FIELD, NO FURTHER PROBLEMS NOTED. INSPECTED A/C, NOTICED STRONG ODOR OF SOAP IN CABIN BLEED SYS GROUND RAN IAW TASK 72-00-00-100-801 PAR H STEP 25. OP CHECK GOOD, NO DEFECTS NOTED. NOTE: ACFT ENGINES NR 1 AND NR 2 HAD PRESSURE WASH THE NIGHT BEFORE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — FALSE INDICATION · airframe 19,195 hrs · 14,033 cycles

SEA- "GLD UNSAFE" CAUTION MSG AFTER ADDING THRUST. ABORTED T/O, RETURNED TO THE GATE. PERFORMED GVI OF "RAD ALT" ANTENNA, FOUND NO DAMAGE OR DISTORTION. PERFORMED "RAD ALT" TEST IAW AMM TASK 34-44-01-740-801 (CONFIG A01) OPS TEST GOOD. PERFORMED OPS TEST OF "GLD" MAN ARM/ DISARM IAW AMM TASK 27-61-00-710-801 (CONFIG AO1) OPS TEST GOOD. NO FAULTS FOUND IN MDC "GLD UNSAFE" CAUTION DID NOT RE OCCUR. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: PLUNGER — MALFUNCTIONED (DOOR HANDLE) · airframe 18,403 hrs · 13,341 cycles

LAX - SERVICE DOOR EXIT IS HARD TO OPEN AND CLOSE. OPEN MIDDLE ACCESS PNL ON SERVICE DOOR EXIT, FOUND AND RESET CENTER PLUNGER ON DOOR HANDLE. OPS CHECK GOOD. CLOSED MIDDLE ACCESS PNL. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,606 hrs · 12,671 cycles

PDX - C4 - LT OUTBOARD SEAT TRACK HAS CORROSION ON TRACK AT APPROX FS 708.00. BLENDED OUT CORROSION AND FOUND TO BE OUT OF LIMITS PER REO 670-53-00-013. REMOVED TRACK IAW CRJ 700 MM 53-00-49-000-801-A02 PARA 3A-D (1) (B). INSTALLED NEW TRACK IAW CRJ 700 AMM 53-00-49-400-801A02 PARA 6A-D (1) (B) & E (1).

Part: SEAT TRACK — CORRODED (BS 629) · airframe 17,606 hrs · 12,671 cycles

PDX-C4 CHECK - CORROSION ON RT INBOARD SEAT TRACK AT STATION 629. REMOVED CORROSION BY BLENDING AFFECTED AREA. MATERIAL REMOVED WITHIN LIMITS OF REO 670-53-00-013. NO CRACKS NOTED. ALODINED SEAT TRACK. (A)

Part: SEAT TRACK — CORRODED (BS 565) · airframe 17,606 hrs · 12,671 cycles

PDX-C4 CHECK. LT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES AT STATION 565.00. BLENDED CORROSION AND GOUGES. MATERIAL REMOVED IS WITHIN LIMITS. HFEC FOR CRACKS, NONE FOUND. ALODINE AREA IAW REO 670-53-00-013. (S)

Part: SEAT TRACK — CORRODED (BS 427) · airframe 17,606 hrs · 12,671 cycles

PDX - C4 CHECK. LT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES AT STATION 427.00. BLENDED CORROSION AND GOUGES. MATERIAL REMOVED IS WITHIN LIMITS. HFEC FOR CRACKS, NONE FOUND. ALODINE AREA IAW REO 670-53-00-013. (S)

Part: SEAT TRACK — CORRODED (BS 677) · airframe 17,606 hrs · 12,671 cycles

PDX-C4 CHECK - CORROSION AT RT INBOARD SEAT TRACK AT STATION 677.00. BLENDED AREA. MATERIAL REMOVED WITHIN LIMITS OF REO 670-53-00-012. ALODINED TRACK. (A)

Part: SEAT TRACK — CORRODED (BS 667) · airframe 17,606 hrs · 12,671 cycles

PDX - C4 CHECK - CORROSION AT RT INBOARD SEAT TRACK AT STATION 667.00 BLENDED AREA. MATERIAL REMOVED WITHIN LIMITS OF REO 670-53-00-012. ALODINED TRACK. (A)

Part: SEAT TRACK — GOUGED (BS 909) · airframe 17,606 hrs · 12,671 cycles

PDX-C4 CHECK. GOUGE ON RT INBOARD SEAT TRACK AT STATION 909.00. REMOVED GOUGE BY REO 670-53-00-013. REMOVED MATERIAL IS IN LIMITS. HFEC AREA WITH NO CRACKS FOUND. ALODINE AREA. (S)

Part: SEAT TRACK — CORRODED (BS 460) · airframe 17,606 hrs · 12,671 cycles

PDX - C4 CHECK. LT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES AT STATION 460.00. BLENDED CORROSION AND GOUGES. MATERIAL REMOVED IS WITHIN LIMITS. HFEC FOR CRACKS, NONE FOUND. ALODINE AREA IAW REO 670-53-00-013. (S)

Part: SEAT TRACK — CORRODED (BS 645) · airframe 17,606 hrs · 12,671 cycles

PDX-C4 CHECK - CORROSION AND A GOUGE AT THE RT SEAT TRACK AT STATION 645.00. BLENDED CORROSION. MATERIAL REMOVED IS WITHIN LIMITS OF REO 670-53-00-013. ALODINED TRACK. (A)

Part: SEAT TRACK — CORRODED (BS 613) · airframe 17,606 hrs · 12,671 cycles

PDX-C4 CHECK. CORROSION ON INBOARD RT SEAT TRACK AT STATION 613.00. REMOVED CORROSION BY BLENDING. REMOVED MATERIAL WITHIN LIMITS. HFEC FOR CRACKS, NONE NOTED. ALODINED AREA IAW REO 670-53-013. (S)

Part: SEAT TRACK — CORRODED (BS 572) · airframe 17,606 hrs · 12,671 cycles

PDX-C4 CHECK. CORROSION ON INBOARD RT SEAT TRACK AT STATION 572.00. REMOVED CORROSION BY BLENDING. REMOVED MATERIAL WITHIN LIMITS. HFEC FOR CRACKS, NONE NOTED. ALODINED AREA. (S)

Part: CHANNEL — CORRODED · airframe 17,028 hrs · 12,228 cycles

PDX C4 CHECK, ABOVE 280 BEAM AT COCKPIT ENTRY, CAMLOCS AND CAMLOC SUPPORT ARE CORRODED. REMOVED ATTACHMENT ANGLE AT COCKPIT ENTRY IAW SRM 51-40-11. DRILLED UP NEW ANGLE IAW SRM 51-40-11. INSTALLED NEW CAMLOC CHANNEL IAW CRJ 700 SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,028 hrs · 12,228 cycles

PDX C4 CHECK - 280 BEAM HAS 2 CRACKS AT APPROX LBL 9 AND RBL 9. REMOVED 280 BEAM IAW CRJ 700 SRM 51-40-11. HFEC AT CUTOUT AREA IAW NDTM PT 1, 51-20-006 NO CRACKS NOTED. INSTALLED 280 BEAM IAW CRJ 700 SRM 51-42-06 AND 51-42-21.

Part: WARNING MESSAGE — ILLUMINATED · airframe 16,054 hrs · 11,520 cycles

FLIGHT 2503. FIRE SYSTEM FAULT MESSAGE RECEIVED. MAINTENANCE PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — OPEN (AC POWER) · airframe 16,001 hrs · 11,479 cycles

PDX - FLIGHT 2586 - LOUD NOISE HEARD FROM LOWER FLIGHT DECK AREA JUST AFTER TAKEOFF ON RIGHT SIDE. MAINTENANCE FOUND THE A/C POWER DOOR LEFT OPEN. INSPECTED DOOR AND FOUND NO DEFECTS AND CLOSED DOOR. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: RELAY — UNKNOWN (LT ENGINE) · airframe 15,935 hrs · 11,433 cycles

BOI - FLIGHT 2592 - ON TAXI RECEIVED A ENGINE DEGRADE CAUTION FOR THE LEFT ENGINE. RETURNED TO THE GATE. MAINTENANCE REPLACED THE K19 AND K21 RELAYS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE LOOP — MALFUNCTIONED · airframe 15,715 hrs · 11,272 cycles

PDX - FLIGHT 2555 - AFTER ENGINE START RECEIVED A INTERM FIRE SYSTEM FAULT MESSAGE. RETURNED TO THE GATE, MAINTENANCE PLACED THE SYSTEM ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE. TROUBLESHOOTING SHOWED A SHORT IN LOOP "A" ON THE LEFT SIDE MEL CONTINUED. REPLACED LOOP ELEMENT "A". OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION) · airframe 15,701 hrs · 11,263 cycles

PDX - FLIGHT 2586 - INTERMITTENT FIRE SYSTEM FAULT MESSAGE. PLACED ON MEL 26-00-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE REPLACED THE FIDEEX CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FLAP SYSTEM — FALSE INDICATION (TE FLAPS) · airframe 15,473 hrs · 11,113 cycles

BOI - FLIGHT 2590, RECEIVED A FLAP HALF-SPEED STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE CHECKED THE MDC AND RAN THE SFECU 1/2 TEST. TEST PASSED AND CLEARED INHIBITS. FLAPS OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: FILTER — UNKNOWN (APU FUEL) · airframe 14,510 hrs · 10,490 cycles

PDX - AFTER TAKEOFF ON FLIGHT 2527, THE APU FAULT CAUTION ILLUMINATED ALONG WITH AUTO SHUTDOWN OF THE APU. DUE TO ONE IDG ALREADY BEING ON MEL, RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE APU FUEL FILTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ELEMENT — MALFUNCTIONED (B FIRE LOOP) · airframe 14,145 hrs · 10,233 cycles

PDX - FIRE SYSTEM FAULT MESSAGE DISPLAYED. MAINTENANCE FOUND THE UPPER DETECT LOOP B TO BE AT FAULT. REPLACED DETECTION LOOP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION · airframe 14,093 hrs · 10,202 cycles

SEA - FIRE SYSTEM FAULT MESSAGE DISPLAYED INTERMITTENT. MAINTENANCE PERFORMED CONTINUITY CHECK OF SYSTEM. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE WITH NO PARTS REPLACED.

Part: VALVE — MALFUNCTIONED (APU BLEED) · airframe 13,883 hrs · 10,070 cycles

SEA- FLIGHT 2531 - AFTER ENGINE START RECEIVED A APU BLEED CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE FOUND CODE MPE 46 IN THE MDC. REPLACED THE LOAD CONTROL VALVE IAW CRJ-700 AMM 49-51-05-000-801-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PANEL — DAMAGED (LT WING) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - LEFT WING PANEL 522CB HAS DAMAGE ON TABS. REPAIRED IAW SRM 57-52-01, 51-20-00.

Part: PANEL — DAMAGED (TE FLAP) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - FLAP PANEL 684GB HAS MINOR DAMAGE ON FACE OF PANEL. REPAIRED IAW SRM 57-61-01, 57-52-01.

Part: SKIN — CORRODED (FUSLEAGE) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - LOWER FUSELAGE SKIN AROUND OMNI DIRECTIONAL TCAS ANTENNA CORRODED AFT OF NOSE JACKING POINT. REPAIRED IAW SRM 53-00-01, 51-21-06.

Part: PANEL — DAMAGED (TE FLAP) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - FLAP VANE PANEL HAS MINOR DAMAGE ON FACE OF PANEL. REPAIRED IAW SRM 57-61-01, 57-52-01, 51-21-06.

Part: PANEL — DAMAGED (TE FLAP) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - FLAP PANEL 584JB HAS MINOR DAMAGE ON FACE OF PANEL. REPAIRED IAW SRM 51-21-06, 57-61-01.

Part: PANEL — DAMAGED (TE FLAP) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - FLAP PANEL 584EB HAS MINOR DAMAGE ON FACE OF PANEL. REPAIRED IAW SRM 57-61-01, 51-13-00, AND 57-52-01.

Part: PANEL — CHAFED (WING) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - PANEL 684JB IS CHAFED. REPAIRED IAW SRM 57-61-01, 51-13-00, ND 51-25-06.

Part: PANEL — DAMAGED (TE FLAP) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - FLAP PANEL 684DB HAS MINOR DAMAGE ON FACE OF PANEL. REPAIRED IAW SRM 57-61-01 AND 57-52-01.

Part: SKIN — DAMAGED (LE SLAT) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - LEFT OUTBOARD SLAT LOWER SURFACE DAMAGED AT SS446.86. REPAIRED IAW SRM 51-21-06, 57-42-01, 51-21-11, AND 51-21-16.

Part: SKIN — GOUGED (BS 677-693) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - RIGHT SIDE FUSELAGE BETWEEN FS 677.00 TO FS 693.00 JUST ABOVE WING FUSELAGE SKIN GOUGED. REPAIRED IAW SRM 51-21-06, 51-21-11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,771 hrs · 9,311 cycles

C3 OKC - FORWARD PASSENGER DOOR CUTOUT FORWARD LOWER CORNER HAS SEVERAL NICKS IN SKIN. REPAIRED IAW SRM 53-00-01, 53-21-01, AND 51-21-11.

Part: WARNING SYSTEM — MALFUNCTIONED (FUEL SYSTEM) · airframe 12,240 hrs · 8,957 cycles

BOI - FLIGHT 2517 - XFLOW PUMP CAUTION MESSAGE RECEIVED. RETURNED TO THE GATE. MAINTENANCE CLEARED THE CAUTION MESSAGE IAW SERVICE LETTER SL-28-007C. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 11,730 hrs · 8,575 cycles

PDX - EMERGENCY LIGHTS INOP. REMOVED THE 4 EPSU BATTERY PACKS AND INSTALLED SERVICEABLE ONES IAW CRJ-700 AMM TASK 33-51-17-400-801-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 11,590 hrs · 8,476 cycles

PDX - FIRE SYSTEM FAULT STATUS MESSAGE RECEIVED. MAINTENANCE REPLACED THE AFT CARGO COMPARTMENT SMOKE DETECTOR (AFT). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — CHAFED (FIRE WARNING) · airframe 11,554 hrs · 8,450 cycles

PDX- INTERMITTANT FIRE SYSTEM FAULT STATUS MESSAGE. MAINTENANCE FOUND WIRES CHAFING AT CONNECTOR A222P1. REPAIRED WIRES IAW CRJ-700 WIRING DIAGRAM WDM26-15-01 PAGE 1. RECONNECTED WIRE AND INTERROGATED MDC. NO FAULTS FOUND. COMPLIED WITH FIRE SYSTEM SELF TEST. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: ROD — DETACHED (SERVICE DOOR) · airframe 11,554 hrs · 8,450 cycles

PDX - UNABLE TO OPEN GALLEY SERVICE DOOR FROM THE INSIDE. MAINTENANCE FOUND THE GALLEY SERVICE DOOR OUT OF SEQUENCE. RE-ATTACHED THE LIFTING ROD AND OPERATIONAL CHECK PERFORMED OF THE DOOR. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: O-RING — DAMAGED (FUEL SUMP) · airframe 10,214 hrs · 7,517 cycles

PDX - ON POST FLIGHT 2466, NOTICED FUEL DRIPPING FROM AROUND A FUEL DRAIN UNDER THE RIGHT WING ROOT. REPLACED O-RING ON RT FWD INBD FUEL TANK WATER DRAIN (SUMP). NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 10,183 hrs · 7,496 cycles

FAT - ON TAXI FOR FLIGHT 2453 SPLR/STAB FAULT & RUD LIMIT FAULT STATUS MSGS KEEP CYCLING ON AND OFF. RETURNED TO THE GATE. REMOVED AND REPLACED ISI PER CRJ700 AMM 34-12-01-000-801-A01 AND 34-12-01-400-801-A01. PERFORMED PITOT LIN P3 CONTAMINATION REMOVAL PER TR 34-0089 34-11-00-100-803-A02. REMOVED STATIC LINE S3 CONTAMINATION PER 34-11-00-100-806-A01, NO CONTAMINATION NOTED ON S3 OR P3. PERFORMED OPS TEST OF ISI PER CRJ-700 AMM 34-12-01-710-801-A01, NO DEFECTS NOTED. PERFORMED MTC R341101 PITOT/STATIC LEAK CHECK, NO LEAKS NOTED. PERFORMED SPOT TESTS SPLR/STAB FAULT CLEARED AND RUD LIMIT FAULT. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — INOPERATIVE (NR 1 A/C PACK) · airframe 10,149 hrs · 7,468 cycles

PDX - ON TAXI FOR FLIGHT 2475 RETURNED TO THE GATE WITH NR 1 AIR CONDITIONING PACK NOT ON-LINE. PLACED ON MEL 21-51-1(A). RETURNED TO SERVICE. ON 12/20 MDC INDICATES LEFT FLOW CONTROL VALVE NO RESPONSE TO COMMAND. REMOVED AND REPLACED LEFT FLOW CONTROL VALVE IAW CRJ AMM TASK 21-53-14-000-801-A01 AND 21-53-14-400-801-A01. OPS CHECK GOOD, NO LEAKS NOTED. PERFORMED SEVERAL ENGINE STARTS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 9,660 hrs · 7,155 cycles

SJC - ON FLIGHT 2528 RETURNED TO THE GATE FOR A RIGHT AIR CONDITIONING PACK CAUTION MESSAGE. MAINTENANCE PLACED THE RIGHT PACK ON MEL 21-51-1 B- RSI NUMBER 353012. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (RT A/C PACK) · airframe 9,618 hrs · 7,119 cycles

PDX - ON TAXI OUT FOR FLIGHT 2456 RECEIVED A RIGHT PACK CAUTION MESSAGE. FLIGHT RETURNED TO THE GATE. MAINTENANCE PLACED THE RIGHT AIR CONDITIONING PACK ON MEL. MEL CLEARED ON 10/23 BY PERFORMING TROUBLESHOOTING IAW FIM 21-53-14, WITH NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK IAW AMM 21-51-00, NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 9,459 hrs · 7,015 cycles

ON TAXI OUT FOR FLIGHT 4310, RECEIVED A LT AIR CONDITIONING PACK FAULT. FLIGHT RETURNED TO THE GATE. MAINTENANCE PLACED ON MEL 21-51-1(A) RSI NR 352561. CLEARED LATER IN THE DAY BY CYCLING THE LT PACK SWITCH. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 9,408 hrs · 6,983 cycles

PDX- ON TAXI OUT FOR FLIGHT 2509, RECEIVED A SPOILER STAB AND RUDDER LIMIT FAULT MESSAGE. FLIGHT RETURNED TO THE GATE. MAINTENANCE DETERMINED MESSAGE WAS DUE TO A ISI AND ADI MISMATCH. PURGED THE PITOT STATIC SYSTEM. NO FAULTS OR MOISTURE FOUND. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED.

Part: ACTUATOR — MALFUNCTIONED (VARIABLE SLAVE) · airframe 8,947 hrs · 6,650 cycles

PDX - FUEL LEAK NOTED ON NR 1 ENGINE. MAINTENANCE REPLACED THE VARIABLE SLAVE ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE LOOP — SHORTED (RT ENGINE) · airframe 8,399 hrs · 6,264 cycles

FIRE SYSTEM FAULT STATUS MESSAGE OCCURRED INTERMITTENTLY DURING DESCENT. MAINTENANCE INTERROGATED MDC SHOWS RT ENGINE LOOP INTERMITTENT SHORT. DEFERRED. ACFT RETURNED TO SERVICE.

Part: FASTENER — LOOSE (HORIZ STAB) · airframe 7,843 hrs · 5,885 cycles

YYC - HORIZONTAL STABILIZER CENTERING TRACK ALL ATTACHED FASTENERS LOOSE. REPAIRED IAW HORIZON AIR EA R-55-32A AND REO 670-55-31-004.

Part: SKIN — DENTED (LT COWLING) · airframe 7,843 hrs · 5,885 cycles

YYC - LEFT LOWER TRANSCOWL HAS A DENT 9 INCHES AFT OF FORWARD EDGE AT BOTTOM OF COWL. REPAIRED IAW REO 670-54-21-350 AND CRJ 700 SRM 51-25-16-001-001-A01.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE EXTERIOR HAS AREAS OF NICKS ABOVE AFT CARGO DOOR BETWEEN FUSELAGE STATION 1015 AND 1031 ON FUSELAGE SKIN. REPAIRED IAW CRJ700 SRM 51-25-01, PAGE 7, PARAGRAPH B AND SRM 51-25-01-001-001-A01.

Part: BUTT JOINT — LEAKING (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE EXTERIOR, HAS AREAS OF SUSPECT PRESSURE LEAKS ON BUTT JOINT FUSELAGE STATION 669, STRINGER 15R TO 15L. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-23-03-001-001-A01.

Part: SKIN — DAMAGED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - CENTER FUSELAGE RIGHT SIDE AT STATION 477 AND STRINGER 21X HAS EVIDENCE OF PRESSURE LEAK AT SKIN BUTT JOINT. REPAIRED IAW CRJ SRM 51-23-00-001-001-A01 AND CRJ700 AMM 21-31-00-910-801.

Part: TORQUE BOX — CHAFED (RT COWLING) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND ENGINE LOWER FAN COWL HAS CHAFE DAMAGE IN THE TORQUE BOX AT THE 4 O'CLOCK AND 7 O'CLOCK POSITIONS. REPAIRED IAW REO 670-78-34-355 AND HORIZON AIR EA R-78-31.

Part: PANEL — CORRODED (RT WING) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND WING FUEL LID REBATE PANEL 641BB HAS MINOR FRETTING CORROSION. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01 AND TASK 51-80-00-760-802-A01.

Part: PANEL — CORRODED (RT WING) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHT HAND WING FUEL LID PANEL 641BB HAS FRETTING CORROSION. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-57-12-002, ISSUE 1.

Part: SLAT — GOUGED (LT WING) · airframe 7,843 hrs · 5,885 cycles

YYC - LEFTHAND WING LEADING EDGE SLAT NR 1 TRAILING EDGE IS GOUGED AT SS60. REPAIRED IAW HORIZON AIR EA R-57-100 AND REO 690-57-42-001.

Part: STIFFENER — DAMAGED (FUSELAGE FAIRING) · airframe 7,843 hrs · 5,885 cycles

YYC - CENTER FUSELAGE, LOWER FAIRING PANEL, PANEL STIFFENER REQUIRES REWORK DUE TO CONTACT WITH FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA R-53-287 AND MOD SUM 1S67053820021, REV A-1.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE EXTERIOR HAS SCRATCH AT STATION 1031 AND STRINGER 5R. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01 AND CRJ700 SRM 53-61-01-101-A01.

Part: ATTACH FITTING — SCORED (ZONE 600) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND AILERON INBOARD PCU LINK OUTBOARD LUG BORE FOR BUSHINGS SCORED. REPAIRED IAW REO 670-57-01-022 AND HORIZON AIR EA R-57-112.

Part: HINGE — BROKEN (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE RIGHT SIDE SERVICE DOOR AT STATION 379.0 HAS UPPER HINGE BROKEN. REPLACED IAW SRM 51-41-00-001-001-A01.

Part: HINGE — CHAFED (ZONE 600) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND INBOARD FLAP LOWER SURFACE INBOARD HINGE AREA HAS CHAFED MARKS FROM FAIRING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND INBOARD FLAP LOWER SURFACE HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-12-00-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 57-52-01-101-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X350 TO X402, HAS MODERATE TO SEVERE PITTING CORROSION ON TOP AND INSIDE SURFACES. REMOVED AND REPLACED IAW CRJ700 SRM 51-41-02-001-001-A01 AND SRM 53-00-49-400-801-A02.

Part: ATTACH FITTING — CORRODED (ZONE 500) · airframe 7,843 hrs · 5,885 cycles

YYC - LT WING FORWARD MAIN LANDING GEAR ATTACHMENT POINT AREA SURFACE CORROSION ON RIVET HEADS/SURROUNDINGS. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01, PARAGRAPH 6 AND SRM 51-25-00-001-001-A01.

Part: FASTENER — CORRODED (RT WING) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND WING LOWER SURFACE INBOARD MAIN LANDING GEAR DOUBLER PLATE ATTACHMENT FASTENERS ARE RUSTY. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01 AND SRM 51-25-00-001-001-A01.

Part: ANGLE — CRACKED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 AT LBL9 AND RBL9 TEE ANGLES ARE CRACKED. REPAIRED IAW CRJ700 SRM 51-42-20-001-001-A01 AND SRM 51-40-11-001-001-A01.

Part: SKIN — DAMAGED (T/E FLAP) · airframe 7,843 hrs · 5,885 cycles

YYC - LEFTHAND INBOARD FLAP LOWER SURFACE GRAVEL DAMAGED. REPAIRED IAW CRJ 700 SRM 51-25-01-001-A01.

Part: HINGE — BROKEN (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE RIGHT POTABLE WATER SERVICE DOOR HAS UPPER HINGE ASSEMBLY BENT AND BROKEN. REPLACED IAW CRJ700 SRM 51-41-00-001-001-A01.

Part: SKIN — WORN (LT AILERON) · airframe 7,843 hrs · 5,885 cycles

YYC - LEFTHAND AILERON HAS SEVERAL AREAS OF WEAR ON TOP AND LOWER LEADING EDGE SKIN. REPAIRED IAW CRJ 700 SRM 51-41-02-001-001-A01.

Part: SKIN — NICKED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE LOWER SKIN FROM STATION 310 TO 319.7 AND STRINGER 25P TO 26P HAS FOUR SMALL NICKS IN SKIN. REPAIRED IAW CRJ700 SRM 51-12-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: SKIN — NICKED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - CENTER FUSERLAGE LOWER LEFT SIDE SKIN, STATION 517 TO 533 AND STRINGER 24 TO 26 PORT HAS FOUR NICKS. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: SKIN — NICKED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - CENTER FUSELAGE LOWER SKIN LEFT SIDE HAS TWO SKIN NICKS STATION 521 TO 517 AND BETWEEN STRINGERS 24 AND 25 PORT. REPAIRED IAW CRJ700 SRM 51-25-01, PAGE 7, PARAGRAPH B AND SRM 51-25-01-001-001-A01.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD LOWER FUSELAGE SKIN AT STATION 260 AND RBL 6.0 HAS A TWO INCH LONG SCRATCH. REPAIRED IAW CRJ700 SRM 51-25-01-001-A01.

Part: SKIN — NICKED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - CENTER FUSELAGE LEFT SIDE SKIN LOWER HAS SKIN NICKS AND STATION 501 BETWEEN STRINGER 22 AND 29 PORT. REPAIRED IAW CRJ700 SRM 51-21-00-001-001-A01 AND SRM 51-25-001-001-A01.

Part: SKIN — GOUGED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - CENTER FUSELAGE, LOWER FUSELAGE SKIN GOUGED AT FUSELAGE STATION 975.00 AND STRINGER 27.0. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01 AND HORIZON AIR EA R-53-787.

Part: SKIN — NICKED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - CENTER FUSELAGE LEFT SIDE LOWER SKIN AT STATION 565.0 AND UPPER EDGE OF DOOR CUTOUT HAS SKIN NICKED. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01.

Part: ANGLE — CRACKED (ZONE 800) · airframe 7,843 hrs · 5,885 cycles

YYC - PASSENGER DOOR AFT SIDE OF STAIR ANGLE AT DOOR PANEL CRACKED AT ASSIST MOTOR. REPAIRED IAW REO 670-52-11-072.

Part: SKIN — NICKED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE LOWER SKIN FROM STATION 295-310 AND STRINGER 25P TO 27 HAS SMALL NICKS IN SKIN. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01, 51-12-00-001-A01.

Part: CYLINDER — CORRODED (NLG) · airframe 7,843 hrs · 5,885 cycles

YYC - CORROSION FOUND ON NOSE LANDING GEAR OUTER CYLINDER. REPAIRED IAW HORIZON AIR EA R-32-184 AND REO 670-32-21-0041.

Part: SKIN — SCRATCHED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE LOWER SKIN FROM 319.7 TO 333.0 AND STRINGER 25 TO 27 PORT HAS THREE SMALL NICKS. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND 51-25-01-001-001-A01.

Part: RIVET — SMOKE (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE EXTERIOR HAS FOUR SMOKING RIVETS AT STATION 745 AND STRINGER 16R. REPLACED RIVETS IAW CRJ7800 SRM 51-42-06-001-001-A01.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE EXTERIOR SKIN AT PASSENGER DOOR SURROUND HAS SCRATCHES AT STATION 310 AND 349, STRINGER 15L. REPAIRED IAW CRJ700 SRM 51-25-01, PAGE 7, PARAGRAPH B AND SRM 51-25-01-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR COCKPIT FLOORBOARD SUPPORT ANGLE AT FUSELAGE STATION 280 IS CORRODED AND CRACKED. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: HINGE — GOUGED (FAN COWLING) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND NACELLE FAN COWL DOOR HINGES, UPPER AND LOWER, ARE GOUGED AT STATION 1069.75 ON HINGE LUGS. REPAIRED IAW CRJ 700 SRM 51-12-001-001-A01 AND HORIZON AIR EA R-78-23.

Part: BRACKET — CRACKED (ZONE 800) · airframe 7,843 hrs · 5,885 cycles

YYC - PASSENGER DOOR AFT SIDE CRACKED AT BASE OF TOP RISER AND BACK OF TREAD AT HANDRAIL STOWAGE BRACKET. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01 REO 670-52-11-104.

Part: PLATE — CHAFED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE, GALLEY SERVICE DOOR FRAME SEAL SKIN SPLICE PLATE CHAFED. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 51-12-01-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 53-21-23-101-001-A01.

Part: SKIN — CRACKED (ZONE 400) · airframe 7,843 hrs · 5,885 cycles

YYC - LEFT ENGINE TRAILING EDGE TRANSCOWL FORWARD EDGE WORN ON BOTTOM CRACKED ON TOP AT 2 O'CLOCK AND 4 O'CLOCK POSITIONS. REPAIRED IAW REO 670-78-33-347 AND HORIZON AIR EA R-78-26.

Part: SCREW — LOOSE (ZONE 600) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND WINGLET INBOARD AND OUTBOARD SURFACES HAVE MANY LOOSE SCREWS. RETORQUED IAW CRJ700 MM 57-30-84, PAGE 422/425.

Part: COWLING — WORN (LT ENGINE) · airframe 7,843 hrs · 5,885 cycles

YYC - LEFT HAND ENGINE AFT ENGINE OF FAN COWL STATION, ENGINE STATION 157.00 HAS WEAR MARKS FROM TRANS COWL AT 2 O'CLOCK AND 4 O'CLOCK POSITION. REPAIRED IAW REO 670-78-33-347

Part: SKIN — CHAFED (ZONE 600) · airframe 7,843 hrs · 5,885 cycles

YYC - RT WING AILERON UPPER LEADING EDGE SURFACES HAVE CHAFE MARKS. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01.

Part: STRIKER — GOUGED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE PASSENGER DOOR SEAL STRIKE GOUGED BESIDE FORWARD TOP PRESSURE STOP. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 51-21-16-001-001-A01 AND SRM 53-21-23-101-001-A01.

Part: SKIN — GOUGED (ZONE 300) · airframe 7,843 hrs · 5,885 cycles

YYC - VERTICAL STABILIZER, SKIN BELOW BOTTOM AFT CORNER OF PANEL 325FR IS GOUGED IN TWO PLACES. REPAIRED IAW CRJ700 SRM 51-25-01-001-01-A01.

Part: SKIN — GOUGED (RT NACELLE) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND NACELLE LIPSKIN GOUGED BETWEEN 3 AND 5 O'CLOCK POSITIONS. REPAIRED IAW CRJ700 SRM 51-21-11-001-A01.

Part: CARGO TRACK — DAMAGED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT RETREVIAL TRAY RAILS, FORWARD RIGHTHAND INBOARD RAIL HARD ANODIZED COATING COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01 AND SRM 51-21-06-001-00-A01.

Part: RAIL — DAMAGED (CARGO BAY) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT RETRIEVAL TRAY RAILS, RIGHTHAND AFT INBOARD RAIL HAS ANODIZED COATING COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01 AND SRM 51-21-06-001-001-A01.

Part: SKIN — SCRATCHED (ZONE 400) · airframe 7,843 hrs · 5,885 cycles

YYC - LEFT NACELLE, AFT CORE COWL, UPPER INBOARD SIDE HAS NUMEROUS SCRATCHES. REPAIRED IAW CRJ700 SRM 54-13-00-101-001-A01 AND SRM 51-12-00-001-001-A01.

Part: RAIL — DAMAGED (CARGO BAY) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT, RETRIEVAL TRAY RAILS, CENTER AFT RAIL HAD ANODIZED COATING COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01.

Part: STRUCTURE — SCRATCHED (RT NACELLE) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHTHAND NACELLE, AFT CORE COWL SCRATCHED ON OUTBOARD. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01.

Part: RAIL — DAMAGED (ZONE 100) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT CARGO RETRIEVAL BIN RAILS, FORWARD LEFTHAND INBOARD ANODIZED COATING COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01 AND SRM 51-21-06-001-001-A01.

Part: STRUCTURE — WORN (THRUST REVERSER) · airframe 7,843 hrs · 5,885 cycles

YYC - RIGHT ENGINE, UPPER AND LOWER THRUST REVERSER COWLS HAVE WEAR ON STOW RAMP AND STRIKER PLATES AS FOLLOWS UPPER, 3 EACH INBOARD, LOWER 1 EACH INBOARD. REPAIRED IAW HORIZON AIR EA R-78-24M R-78-25 ABD REO 670-78-34-351.

Part: RAIL — DAMAGED (CARGO BAY) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE, FORWARD CARGO COMPARTMENT RETRIEVAL TRAY RAILS, FORWARD RIGHTHAND OUTBOARD SEVERAL SMALL AREAS OF HARD ANODIZED SURFACE COMING OFF. REPAIRED IAW CRJ700 SRM 51-21-11-001-001-A01 AND 51-21-06-001-001-A01.

Part: RIVET — LOOSE (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE UPPER EXTERIOR HAS SEVERAL SMOKING RIVETS AT STRINGER 7L, BETWEEN FUSELAGE STATION 893 TO 939. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: RIVET — LOOSE (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE UPPER EXTERIOR HAS SEVERAL SMOKING RIVETS AT STRINGER 3L AND BETWEEN FUSELAGE STATION 345 TO 379. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: RIVET — SMOKE (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE EXTERIOR HAS SMOKING RIVET AT FUSELAGE STATION 485. REPAIRED IAW CRJ700 SRM 51-25-001-001-A01.

Part: RIVET — SMOKE (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE EXTERIOR HAS SEVERAL SMOKING RIVETS AT FUSELAGE STATION 677, STRINGER 3L TO STRINGER 6L. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X431 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: RIVET — PULLED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - CENTER FUSELAGE AT STATION 770.0, WL 725, RBL 9.0-17.0 HAS RIVETS PULLED ON FLAT STRAP. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR FLOOR SUPPORT CROSSBEAM AND FUSELAGE STATION 280 IS CORRODED ALONG UPPER FLANGE. REPAIRED IAW CRJ700 SRM 51-26-21-001-001-A01 AND REO 670-53-11-047.

Part: HOUSING — GOUGED (ZONE 800) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE, AFT BAGGAGE DOOR HANDLE HOUSING HAS GOUGE ON FORWARD TOP OUTER FACE. REPAIRED IAW CRJ700 SRM 51-12-00-991-802 AND SRM 51-21-01-001-001-A01.

Part: ATTACH BRACKET — CRACKED (ZONE 800) · airframe 7,843 hrs · 5,885 cycles

YYC - PASSENGER DOOR AFT SIDE INTERNAL Z FOR ASSIST MOTOR ATTACH IS CRACKED. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, LEFTHAND OUTBOARD SEAT RAIL AT STATION X709 HAS PITTING CORROSION ON INSIDE AND MOST INBOARD SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND SRM 51-21-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL, AT STATION X417, HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RT OUTBOARD SEAT RAIL AT STATION X712 HAS PITTING CORROSION ON INSIDE SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAGH 3E AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X448 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X584, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/90-0 SRM 51-21-06-001-001-A01, PARAGRAPH 3E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEATRAIL, AT STATION X584, HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X646 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X479 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND OUTBOARD SEAT RAIL AT STATION X708 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-0101-A01, PARAGRAPH 3E AND SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X678 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC FUSELAGE INTERIOR LEFT OUTBOARD SEAT RAIL AT STATION X795 HAS PITTING CORROSION ON INSIDE AND MOST INBOARD SURFACES. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL, AT STATION X523 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR RIGHTHAND OUTBOARD SEAT RAIL AT STATION X810 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPHA 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X665 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC FUSELAGE INTERIOR, LEFT OUTBOARD SEAT RAIL AT STATION X740 HAS PITTING CORROSION ON ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND OUTBOARD SEAT RAIL AT STATION X785, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR LEFT OUTBOARD SEAT RAIL AT STATION X810 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ 7--/9-- SRM 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X603 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHT HAND OUTBOARD SEAT RAIL AT STATION X739, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH A 3E AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X616 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X553 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X479 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND INBOARD SEAT RAIL AT STATION X540 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHTHAND OUTBOARD SEAT RAIL AT STATION 753, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X522 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRN 51-21-06-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, RIGHT OUTBOARD SEAT RAIL AT STATION X613, HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X460 HAS PITTING CORROSION ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, LEFTHAND INBOARD SEAT RAIL AT STATION X647 HAS PITTING CORROSION ON TOP SURFACE. REPAIRED IAW CRJ700/900 SRM 51-21-06-001-001-A01, PARAGRAPH 3E, REO 670-53-00-013 AND CRJ700 SRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR LEFT OUTBOARD SEAT RAIL AT STATION X615 HAS PITTING CORROSION ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01, PARAGRAPH 3E AND CRM 51-21-16, CODE A044.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, LEFT OUTBOARD SEAT RAIL AT STATION X785 HAS PITTING CORROSION AND TOOL MARKS ON MOST INBOARD SURFACE. REPAIRED IAW CRJ700 SRM 51-21-06-001-001-A01 AND REO 670-53-00-013.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 BULKHEAD LEFTHAND LOWER WEB IS CORRODED ALONG THE FLOOR CROSSBEAM. REPAIRED IAW REO 670-53-110-052, REV A.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 BULKHEAD RIGHTHAND LOWER WEB IS CORRODED ALONG THE FLOOR CROSSBEAM. REPAIRED IAW REO 670-53-11-052, REV A.

Part: DOOR — DEPARTED (NR 2) · airframe 6,918 hrs · 5,220 cycles

THE NR 2 INBOARD GEAR DOOR BROKE OFF DURING CLIMBOUT OF MFR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE INBOARD DOOR MISSING, AND THE CONNECTING ROD BROKEN OFF AT THE MOUNT BOLT. DAMAGE TO THE INBOARD FLAP WAS ALSO FOUND. MAINTENANCE REMOVED THE REMAINDER OF THE INBOARD DOOR AND PLACED ON RSI.

Part: WARNING LIGHT — ILLUMINATED (ZONE 100) · airframe 5,695 hrs · 4,282 cycles

SFO FLIGHT 2475, LEFT ENGINE BLEED CAUTION MESSAGE CAME ON AFTER LANDING AND STAYED ON FOR 3-5 MINUTES. MESSAGE WENT AWAY BEFORE ABNORMAL CHECKLIST WAS ACCOMPLISHED. MAINTENANCE INTERROGATED MDC. NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: CARTRIDGE — FAULTY (RT WING) · airframe 5,635 hrs · 4,237 cycles

SJC - FLIGHT 2572 - THE CREW REPORTED A RIGHT TRANSFER SHUT OFF VALVE CAUTION MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT FUEL TRANSFER SHUT OFF VALVE CARTRIDGE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROD — OUT OF ADJUST (SERVICE DOOR) · airframe 5,421 hrs · 4,067 cycles

SEA - FLIGHT 2455 - CREW REPORTED THAT THE SERVICE DOOR WILL NOT OPEN. MAINTENANCE INSPECTED THE DOOR AND REPOSITIONED THE ROD ASSEMBLY FOR VERTICAL MOVEMENT. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHIMNEY — TORN (CARGO BAY) · airframe 5,354 hrs · 4,019 cycles

FORWARD BAGGAGE COMPARTMENT ENTRY-WAY OVERHEAD CHIMNEY HAS A TEAR IN THE METAL WEBBING. REMOVED AND REPLACED CHIMNEY ASSEMBLY.

Part: CHIMNEY — DAMAGED (ZONE 200) · airframe 4,506 hrs · 3,404 cycles

FORWARD CARGO COMPARTMENT CHIMNEY IS DAMAGED. REMOVED AND REPLACED CHIMNEY. OPEATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (ZONE 300) · airframe 4,476 hrs · 3,380 cycles

BIL- ON FLIGHT 2508 AFTER TAKEOFF AUTOPILOT TRIM IS SHOWING A CAUTION MESSAGE. DISCONNECTED AUTOPILOT, RETRIMMED, THEN RECONNECTED PER CHECKLIST. NO FURTHER INCIDENTS. COMPLIED WITH AUTOPILOT SYSTEM OPERATIONAL CHECK IAW CRJ AMM 22-11-00-710-802 AND 22-11-24-710-801. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FADEC — INOPERATIVE (ZONE 400) · airframe 4,453 hrs · 3,363 cycles

SJC-ON FLIGHT NUMBER 2457, JUST AFTER TOUCHDOWN THE RIGHT FADEC CAUTION MESSAGE CAME ON FOLLOWED BY THE RIGHT ENGINE FLAME OUT CAUTION MESSAGE. AFTER STOWING THE REVERSER LEVERS THE RIGHT REVERSER UNLOCKED CAUTION MESSAGE APPEARED. AFTER ENGINE SHUTDOWN THE RIGHT IGNITION-B FAULT STATUS MESSAGE CAME ON. REMOVED AND REPLACED NR 2 FADEC. OPERATED ENGINE AT SEVERAL POWER SETTINGS, SEVERAL TIMES AND DEPLAYED THRUST REVERSERS SEVERAL TIMES. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — LEAKING (BLEED AIR SYS) · airframe 3,863 hrs · 2,929 cycles

SEA-ON FLIGHT NUMBER 2508, DURING CLIMB A WARNING MESSAGE APPEARED AND DISAPPEARED TO QUICKLY TO READ. THIS WAS FOLLOWED BY A RT BLEED DUCT CAUTION MESSAGE. PACK 2 ON THE SYNOPTIC PAGE CONTINUOUSLY FLICKERED BETWEEN GREEN AND WHITE. THE SHUTOFF VALVE REMAINED CLOSED. AFTER COMPLETING THE RT BLEED DUCT AND MANUAL CHECKLISTS, RIGHT BLEED DUCT PRESSURE INDICATES 25 PSI. FOUND BLEED LEAK. INSTALLED NEW SEALS AT STUB DUCT. PERFORMED OPERATIONAL TEST OF THE BLEED AIR LEAK DETECTION. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 3,837 hrs · 2,914 cycles

CKB- PERFORMED EDDY CURRENT INSPECTION OF RIGHT HAND PYLON SHEAR DECK LUNCH BOX. NOTED INDICATION OF CRACK APPROXIMATELY 2 INCHES LONG AT AFT FITTING IN CARGO BAY. REPAIRED IAW CRJ SRM 51-42-06 AND SRM 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 3,837 hrs · 2,914 cycles

CKB- DURING DNT INSPECTION OF THE PRESSURE BULKHEAD AT FS 1098.20 RIGHT HAND SIDE SHOWS INDICATIONS OF CRACK. REPAIRED IAW BOMBARDIER EO 670-53-61-034, AND HORIZON AIR EO 53-44B.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 3,837 hrs · 2,914 cycles

CKB- DURING INSPECTION OF THE PRESSURE BULKHEAD LEFT HAND SIDE, NDT SHOWED INDICATIONS OF CRACK. REPAIRED IAW BOMBARDIER EO 670-53-61-034 AND HORIZON AIR EO 53-44B.

Part: VANE — CHAFED (T/E FLAP) · airframe 3,837 hrs · 2,914 cycles

CKB- LEFT AFT OUTBOARD FLAP VANE ASSEMBLY HAS A CHAFE .003 INCH DEEP AND .250 INCH LONG APPROXIMATELY 2 INCHES FROM OUTBOARD EDGE. REPAIRED IAW WVAC EO 601R-57-4319A AND HORIZON AIR EO R-57-50.

Part: VANE — CHAFED (RT FLAP)

RT OUTBOARD FLAP VANE IS CHAFED ON THE OUTBOARD LEADING EDGE OF THE VANE CAP APPROXIMATELY 2 INCHES FROM THE END. THE CHAFE IS .025 INCHES X .003 INCHES DEEP. CHAFING AGAINST THE BUTE DOORS WHEN FLAPS EXTEND AND RETRACT. RECOMMENDATION: BLEND CHAFED AREA TO SMOOTH THE SURFACE, PERFORM EDDY CURRENT TO ENSURE THAT NO CRACKS EXIST ALODINE, PRIME, AND PAINT TO MATCH SURROUNDING STRUCTURE IAW EA R57-50.(K)

Part: INDICATOR — MALFUNCTIONED (ZONE 100) · airframe 3,767 hrs · 2,883 cycles

YEG- ON FLIGHT 2462 EFIS CAUTION LIGHT CLIMBING THROUGH 15,000, COMPLIED WITH EMEREGNCY CHECKLIST. CAUTION LIGHT WENT OUT. FIVE MINUTES LATER RECEIVED ANOTHER EFIS CAUTION. DETERMINED FIRST OFFICER'S HEADING INDICATOR DIFFERED FROM STANDBY COMPASS. COMPLIED WITH EMERGENCY CHECKLIST. COMPLIED WITH CRJ-700 AMM TASK 34-21-00-720-801-A01. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHIMNEY — TORN (ZONE 200) · airframe 3,725 hrs · 2,828 cycles

FORWARD CARGO BAY CENTER FIRE DETECTION CHIMNEY IS TORN. REMOVED AND REPLACED CHIMNEY.

Part: WARNING LIGHT — ILLUMINATED (ZONE 200) · airframe 3,641 hrs · 2,760 cycles

ON FLT 2504 ON LANDING ROLLOUT GOT 'DISPLAY COOL' AMBER CAUTION MESSAGE. PERFORMED CHECKLIST, WENT TO GROUND ALTERNATE ON DISPLAY FAN AND 'DISPLAY COOL' MESSAGE EXTINGUISHED. INTEROGATED MDC WITH NO FAULTS FOUND. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE WARNING — FALSE INDICATION (COCKPIT) · airframe 3,219 hrs · 2,444 cycles

ON FLIGHT 2494 FIRE SYSTEM FAULT AMBER. CYCLED SHIPS POWER AND FIRE SYSTEM FAULT CLEARED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (ZONE 200) · airframe 3,219 hrs · 2,444 cycles

ADG DEPLOY AUTO CB (2N6) OPENED PER PROXIMITY SYSTEM CHANNEL MESSAGE CHECKLIST AND SHUTDOWN APU. CLOSED ADG DEPLOY AUTO CB. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CAGE — DAMAGED (CARGO BAY) · airframe 3,214 hrs · 2,440 cycles

PDX- FORWARD CARGO BAY CHIMNEY AT DOOR ENRTY HAS A TEAR IN THE WEBBING. REMOVED AND REPLACED FORWARD CARGO BAY CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT) · airframe 3,205 hrs · 2,433 cycles

MSO- ON FLIGHT 2429 FIRE SYSTEM FAULT CAUTION MESSAGE. CYCLED SHIPS POWER AND COMPLIED WITH FIRE SYSTEM TEST. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 2,958 hrs · 2,246 cycles

SJC-ON FLIGHT NUMBER 2456, TRANSFER PUMP CAUTION LIGHT ON TAXI OUT. RESET FUEL SYSTEM CONTROL CIRCUIT BREAKERS. NO FURTHER CAUTION OR FAULT NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE HARNESS — FAULTY (RT MLG) · airframe 2,958 hrs · 2,246 cycles

PDX-ON FLIGHT NUMBER 2438, MAIN LANDING GEAR FAULT STATUS MESSAGE. REMOVED AND REPLACED RIGHT GEAR DOWNLOCK HARNESS ASSEMBLY. REPAIRED IAW CRJ MM, 32-61-05 AND CRJ MM 32-61-00-710-801-A01. AIRCRAFT RETURNED TO SERVICE.

Part: TRU — BURNED (ZONE 200) · airframe 2,710 hrs · 2,055 cycles

SEA-STRONG ELECTRICAL SMELL EMITTING AROUND NOSE AREA. TRANSFORMER RECTIFIER UNIT 2 BURNED INTERNALLY. REMOVED AND REPLACED TRANSFORMER RECTIFIER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — FAILED (ZONE 200) · airframe 2,669 hrs · 2,026 cycles

PDX - FLIGHT 2402 - CREW REPORTED THE NUMBER 3 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE NUMBER 3 HYDRAULIC PUMP. OPERATIONAL CHECKS AND GEAR SWINGS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STOP FITTING — WORN (FUSELAGE) · airframe 7,843 hrs · 5,885 cycles

YYC - FORWARD FUSELAGE, RIGHTHAND GALLEY SERVICE DOOR, DOOR STOP FITTING PAD WORN. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 51-25-00-001-001-A01, SRM 53-21-23-101-002-A01 AND CRJ700 AMM 52-00-00-790-801.

Part: SKIN — DENTED (ZONE 200) · airframe 2,257 hrs · 1,727 cycles

PDX- DENT BELOW RIGHT SIDE STATIC PORT. REPAIRED IAW CRJ SRM 51-25-16 AND HORIZON AIR EA R-53-81/REO 670-53-21-032.

Part: BLADE — MISSING (ZONE 400) · airframe 2,082 hrs · 1,606 cycles

PDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE MISSING AND FOUR BLADES HAVE TRAILING EDGE DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT1 DAMPNER (ALONG WITH RE-WORK OF THE ACCELERATOR) IS THE CORRECTIVE ACTION FOR THE REMOVED ENGINE. A PLAN HAS BEEN DEVISED TO INCORPORATE THIS MOD IN THE NEXT FEW QUARTERS.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 1,837 hrs · 1,424 cycles

SEA- LEFT FUEL PRESSURE LOW CAUTION MESSAGE. REMOVED AND REPLACED NR 1 FUEL LOW PRESSURE SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CAGE — DAMAGED (CARGO BAY) · airframe 1,803 hrs · 1,399 cycles

PDX- FORWARD CARGO BAY CHIMNEY IS DAMAGED. REMOVED AND REPLACED CHIMNEY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 1,713 hrs · 1,341 cycles

PDX-ENROUTE, FLIGHT ATTENDANTS COMPLAINED OF AN ODOR TOWARDS THE REAR OF THE CABIN CAUSING THEIR EYES TO BURN AND FELT SICK. GROUND RAN BOTH ENGINES. NO SMELLS NOTICED IN BLEED SYSTEM. HAD LAVATORY SERVICED, NO SMELLS NOTICED AT THAT TIME. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — LEAKING (FUEL SYSTEM) · airframe 1,489 hrs · 1,182 cycles

BOI - FUEL LEAK NOTED IN FRONT OF LEFT WHEEL WELL. MAINTENANCE INSPECTED AND REPLACED THE ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 1,352 hrs · 1,086 cycles

LAX - CREW RECEIVED A LEFT FUEL LOW PRESSURE WHILE EN ROUTE AT FL 390. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE ENGINE FUEL FEED SWITCH. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — OUT OF ADJUST (CARGO DOOR) · airframe 1,297 hrs · 1,044 cycles

PDX - CREW RETURNED TO FIELD WHEN AFTER TAKE-OFF, THE AFT CARGO DOOR CAUTION ILLUMINATED WITH A STATUS MESSAGE THAT READ PROX SYSTEM FAULT 2. PSI DIFFERENTIAL WAS SEVEN. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJUSTED THE PROX SENSOR AND LUBED THE AFT CARGO DOOR HANDLE. AN OPERATIONAL CHECK AND GROUND PRESSURIZATION WAS PERFORMED. NO DISCREPANCIES WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCREEN — DAMAGED (FIRE SUPPRESSION) · airframe 1,250 hrs · 1,004 cycles

PDX- FORWARD CARGO COMPARTMENT FIRE SUPPRESSION CHIMNEY SCREEN IS TORN. REMOVED AND REPLACED CHIMNEY ABOVE FORWARD CARGO DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — OBSTRUCTED (MAIN FUEL SYS) · airframe 1,216 hrs · 981 cycles

BOI - ABORTED TAKEOFF. TAKEOFF RPM (N1) ON NR 1 ENGINE APPROXIMATELY 10 PERCENT BELOW REQUIRED INDICATION, FADEC CALLED FOR 88.2 PERCENT, N1 INDICATOR SHOWED APPROXIMATELY 76.3 PERCENT. REMOVED OBSTRUCTION FROM MAIN FUEL PUMP INLET AND REINSTALLED. GROUND RAN, ALL INDICATIONS NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: CAGE — DAMAGED (CARGO BAY) · airframe 954 hrs · 772 cycles

BOI- FORWARD CARGO COMPARTMENT CHIMNEY IN ENTRYWAY DAMAGED. REMOVED AND REPLACED CARGO COMPARTMENT FIRE DETECTOR CHIMNEY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (COCKPIT) · airframe 131 hrs · 108 cycles

SMF- ON DESCENT INTO SMF, THERE WAS A HOT PLASTIC SMELL IN THE CABIN AND THOUGH AIR VENTS IN COCKPIT. SMELL DISSIPATED AFTER 5 MINUTES. INSPECTED AIR VENTILATION AND AVIONICS COOLING. NO PARTS REPLACED. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE.