N614QX

Part: ANTENNA — DAMAGED (ZONE 100) · airframe 45,762 hrs · 34,909 cycles

COMPLY WITH M-93 CRJ700-53-25-01 AND EA11125 REV A FOR THE MAJOR REPAIR TO THE FUSELAGE VHF ANTENNA, STA 629-645, STR 1L-1R COMPLIED WITH REPAIR PER INTELSAT EA11125 REV. A

Part: ANTENNA — DAMAGED (VHF COMMS) · airframe 45,759 hrs · 34,906 cycles

COMPLY WITH M-93 CRJ700-53-25-01 AND EA11125 REV A FOR THE MAJOR REPAIR TO THE FUSELAGE/VHF ANTENNA/STA 629-645, STR 1L-1R (FILED OPEN)

Part: STEERING SYS — UNCONTROLLABLE (NLG) · airframe 42,162 hrs · 31,972 cycles

CREW REPORTED THAT UPON LANDING AIRCRAFT BEGAN TO SWERVE UNCONTROLABLY (FLIGHT 4939 FILED CLOSED)UPON ARRIVAL TO AIRCRAFT INTERROGATED MDC FOUND NO CURRENT FAULTS AT THIS TIME. PERFORMED VISUAL INSPECTION OF BOTH LEFT AND RIGHT MLG SHOCK STRUT AND UPPER AND LOWER TORQUE LINKS IN REF TO AMM 32-11-05 NO LEAKS NOTED AT THIS TIME NO FURTHER DISCREPANCIES NOTED AT THIS TIME. NO PLAY OR DAMAGE FOUND IN TORQUE LINKS NOTED AT THIS TIME. PERFORMED VISUAL INSPECTION OF MLG SHIMMY DAMPER IN REF TO AMM 32-11-42 NO LEAKS NOTED AT THIS TIME NO FURTHER DISCREPANCIES NOTED AT THIS TIME. PERFORMED VISUAL INSPECTION OF NLG STRUT AND UPPER AND LOWER TORQUE LINKS IN REF TO AMM 32-21-01 NO LEAKS NOTED AT THIS TIME NO FURTHER DISCREPANCIES NOTED AT THIS TIME. NO PLAY OR DAMAGE FOUND IN TORQUE LINKS NOTED AT THIS TIME. PERFORMED OPERATIONAL CHECK OF NWS IN REF TO AMM 32-51-00. OPERATIONAL CHECK GOOD AT THIS TIME. NO LEAKS NOTED AT THIS TIME. PERFORMED VISUAL INSPECT AND OPERATIONAL CHECK OF THE MLG BRAKE SYSTEM IN REF TO AMM 32-33-00. NO DEFECTS NOTED AT THIS TIME. OPERATIONAL CHECK GOOD

Part: SEAT TRACK — BROKEN (CABIN) · airframe 42,030 hrs · 31,880 cycles

SEAT FLOOR TRACK AT 10B IS BROKEN. (FILED CLOSED)REMOVED AND REPLACED FLOOR TRACK AT 10B IAW AMM 25-21-01.

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 41,802 hrs · 31,702 cycles

DURING CLIMB OUT OF AEX AT 8000 FT AND 250KTS RECEIVED BRAKE OVHT WARNING MESSAGE AND ASSOCIATED AURAL WARNING. FO NOTICED BRAKE INDICATOR #4 SHOWED 7 AND THEN JUMPED UP TO 11 THEN RETURNED BACK TO 1. ALL OTHER INDICATORS SHOWED 1. COMPILED WITH QRH AND DETERMINED IT WAS POTENTIALLY AN ERRONEOUS INDICATION. (FLIGHT 3214 FILED CLOSED)UPON ARRIVAL TO AIRCRAFT FOUND #4 BRAKE TEMP MONITORING SYSTEM SENSOR CANON PLUG LOOSE, RETIGHTNED THE CANON PLUG PER CRJ700 AMM 32-46-01. OPS CHECK GOOD AT THIS TIME

Part: WINDOW POST — FAILED INSP (COCKPIT RIGHT) · airframe 38,564 hrs · 29,146 cycles

FO'S WINDOW/WINDSHIELD I POST FAILED LEAK CHECK. REQUIRES REMOVAL, CLEANING, AND PROPERLY RE-SEALING/REINSTALLATION. (FILED CLOSED) REMOVED AND REINSTALLED THE I-STRAP ON THE FO WINDSHEILD AND SIDE WINDOW PER AMM 56-11-07. LEAK CHECK GOOD AT THIS TIME.

Part: WINDSHIELD — CRACKED (COCKPIT LEFT) · airframe 38,564 hrs · 29,146 cycles

CAPTAINS WINDSHIELD IS CRACKED IN THE UPPER LH CORNER NEAR THE TERMINAL BLOCK. (FILED CLOSED) REMOVED AND REPLACED THE CAPTAINS SIDE WINDSHILED PER AMM 56-11-07 AND TASK CARD 56-220-1000-SKY. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME. / TORQE WRENCH TUSCAL 305 S/N 0914804475 CAL DUE 10/2021 / TORQUE WRENCH TUSCAL 201 0120113976 CAL DUE 02/2022

Part: CLEAT — CORRODED (BS 1031 S24R) · 29,134 cycles

STRINGER TO FRAME ATTACHMENT CLEAT AT FS1031 STR24R HAS CORROSION (C-CHECK RO 8/9/2021) REMOVED AND REPLACED CLEAT AT FS1031 STR24R IAW CRJ 700 SRM 51-42-21-001-001-A01, SEE CONTINUATION FOR SPECIFIC WORK ACCOMPLISHED

Part: FRAME — DAMAGED (BS 1047 S22L) · 29,134 cycles

PERFORM FRAME SPLICE REPAIR AT FS1047, STR22L TO PROVIDE ACCESS FOR REPAIR OF STR 25L AT FS 1040 (C-CHECK RO 8/9/2021) INSTALLED NEW FRAME SPLICE AT FS1047 STGR 22L REF-CRJ-700 MHI RJ REO 670-53-61-1921 REV -- DATED 2021-06-26, SRM 51-42-06-001-001 A01 ND SRM 51-42-21-001-001 A01,LEAK CHECK GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: FRAME — DAMAGED (BS 501 S16R) · 29,134 cycles

SPLICE REPAIR OF FRAME SECTOR FS501.00 AT STGR -16R COMMON TO JOB 71004994 OP 63 MX # 22779504 (C-CHECK RO 8/9/2021) PERFORMED SPLICE REPAIR OF THE FRAME SECTOR AT FS501.00 STGR 16R REF REO 670-53-31-671 REV -- DATED 2021-06-05. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SKYWEST FORM M-337 AND SKYWEST TASK 51-900-1002-SKY.

Part: FRAME — DAMAGED (BS 565 S16R) · 29,134 cycles

SPLICE REPAIR OF FRAME SECTOR FS565.00 AT STGR-16R COMMON TO JOB 71004994 OP 61 MX# 22779485 (C-CHECK RO 8/9/2021) PERFORMED SPLICE REPAIR OF FRAME SECTOR FS 565 AT STGR 16R REF REO 670-53-31-671 REV-- DATED 2021-06-05 / COMPLIED WITH TASK CARD 51-900-1002-SKY / LEAK CHECK GOOD

Part: STOP FITTING — CRACKED (BS 310 S4-5L) · 29,134 cycles

PASSENGER DOOR, STOP BRACKET ASSY AT FS310.00 BETWEEN STGR 4LH/5LH CRACKED (C-CHECK RO 8/9/2021) REPLACED PAX DOOR STOPO BRACKET ASSY AT F.S 310.00 BETWEEN STRG 4LH/ 5LH IAW CRJ 700 SRM 51-42-21-001-001-A01

Part: CLEAT — CORRODED (BS 1051 S26R) · 29,134 cycles

CLEAT COMMON TO 1051 FRAME AND STRINGER 26R IS CORRODED (C-CHECK RO 8/9/2021) REMOVED AND REPLACED CLEAT IAW CRJ 700 SRM 51-42-06-001-001-A01, SEE CONTINUATION FOR WORK ACCOMPLISHED. COMPLIED WITH SKYCARD 51-900-1002-SKY.

Part: DOOR — BENT (LT NACELLE) · 29,134 cycles

LH ENGINE UPPER FAN COWL DOOR THE I/B AFT EDGE IS BENT (C-CHECK RO 8/9/2021) REMOVED AND REPLACED 1EA INBOARD EDGE MEMBER ANGLE P/N CN622-0312-209 ON LH ENGINE UPPER FAN COWL DOOR REF : DWG CN622-0101 REV "K", DWG # CN622-0312 REV D. CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01 ANDD CRJ-700 SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUATION FOR DETAILS. / COMPLIED WITH ALL STEPS OF REO 670-54-14-1012 REV A DATED 2011/08/26

Part: DOOR — BENT (RT NACELLE) · 29,134 cycles

RH ENGINE UPPER FAN COWL DOOR I/B AFT EDGE BENT (C-CHECK RO 8/9/2021) REMOVED AND REPLACED 1EA BENT INBOARD EDGE MEMBER P/N CN622-0312-0210 WITH NEW EDGE MEMBER ON THE R/H ENGINE UPPER FAN COWL DOOR REF: DWG# CN622-0201 REV L, CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND CRJ-700 SRM 51-42-13-001-001-A01. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUATION FOR DETAILS.

Part: SKIN — DENTED (RT NACELLE) · 29,134 cycles

RH LOWER TRANSCOWL OUTER SKIN DENT. 6 O€™CLOCK. (C-CHECK RO 8/9/2021) EVALUATED RH LOWER TRANSCOWL OUTER SKIN DENT. 6 O€™CLOCK DEPTH.036" LENGTH .300"WIDTH .300" FOUND TO BE OUT OF LIMITS DUE TO THE FACT ONLY ALLOWED A DEPTH OF .028" TOOL #TUC8531 DUE DATE 31-OCT-2021 REF CRJ 700 SRM 54-21-00-101-001-A01 / INSTALLED REPAIR DOUBLER ON RH LOWER TRANSCOWL IAW MHI RJ REO 670-54-21-1451 REV--(P1) DATED 2021-06-15

Part: RETAINER — CORRODED (PAX DOOR) · 29,134 cycles

PAX DOOR FOWD SEAL RETAINER CORRODED AROUND MORE THAN HALF HOLES AND MATING SURFACE. (C-CHECK RO 8/9/2021) REMOVED AND REPLACED PAX DOOR FWD SEAL RETAINER REF-CRJ-700 SRM 51-42-06-001-001 A01 AND DWG 601R31702 REV N,LEAK CHECK GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: FRAME — CORRODED (BS 1051 S26L-R) · 29,134 cycles

FS 1051 CORRODED BETWEEN STR 26 LH AND 26 RH (C-CHECK RO 8/9/2021) REPAIRED FRAME FS1051 BETWEEN STGR 26LH & 26RH AND COMPLIED WITH ALL STEPS OF REF-CRJ-700 MHI RJ REO 670-53-61-1914 REV -- DATED 2021-06-16. / COMPLIED WITH THE TASK 51-900-1002-SKY

Part: ANGLE — CORRODED (BS 319 S20R) · 29,134 cycles

ANGLE ATTACHED TO INTERCOSTAL FS310 - FS319.70 AT STGR 20R AND FRAME FS310 HAS MULTIPLE AREAS OF CORROSION (C-CHECK RO 8/9/2021) REMOVED AND REPLACED ANGLE P/N SH670-32046-3 AT FRAME FS310 STGR20R INTERCOSTAL REF CRJ700 SRM51-42-06-001-001-A01 REV 38 JUL 25/2020 AND DWG NO. SH670-31950 REV Y. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH MXTRANS#22837804 JOB 71004994 OP 145

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · 29,134 cycles

DURING REMOVEL OF AFT FORMER FOUND AFT SUPPORT ANGLE CORROED (C-CHECK RO 8/9/2021) REMOVED OLD AFT SUPPORT ANGLE & INSTALLED NEW AFT FORMER SUPPORT ANGLE PER CRJ-700-SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 & DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · 29,134 cycles

DURING REMOVAL OF FWD FORMER FOUND FWD SUPPORT ANGLE CORRODED. (C-CHECK RO 8/9/2021) REMOVED OLD ANGLE AND INSTALLED NEW FWD FORMER SUPPORT ANGLE PER CRJ-700 SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 & DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: FORMER — CORRODED (PAX DOOR) · 29,134 cycles

AFT FORMER ON *PAX DOOR HAS CORROSION ON MULTIPLE ELEMENTS (C-CHECK RO 8/9/2021) REMOVED OLD AFT FORMER & REPLACE WITH NEW AFT FORMER PER CRJ-700-SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: INTERCOSTAL — CRACKED (PAX DOOR) · 29,134 cycles

PAX DOOR DD7 INTERCOSTAL BETWEEN F.S.338-347.25 HAS CRACK IN RADIUS. (C-CHECK RO 8/9/2021) REMOVED OLD INTERCOSTAL & REPLACED WITH NEW INTERCOSTAL PER CRJ-700-SRM 51-42-06-001-001-A01 & DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 29,134 cycles

PAX DOOR INTERCOSTAL BETWEEN F.S.338-347.25 BELOW DD3 HAS CORROSION ON MULTIPLE ELEMENTS(AS MARKED) (C-CHECK RO 8/9/2021) REMOVED OLD INTERCOSTAL & REPLACE WITH NEW INTERCOSTAL PER CRJ-700-SRM 51-42-06-001-001-A01 & DWG 601R31702 REV N. LEAK CHK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: INTERCOSTAL — CRACKED (PAX DOOR) · 29,134 cycles

PAX DOOR DD1 INTERCOSTAL HAS CRACK IN RADIUS.(AS MARKED) (C-CHECK RO 8/9/2021) REMOVED AND REPLACED INTERCOSTAL W/NEW PARTS IAW CRJ700 SRM 51-42-06-001-001-A01 & DWG 601R31702 REV N. LEAK CHK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: FORMER — CORRODED (PAX DOOR) · 29,134 cycles

PAX DOOR FWD FORMER HAS CORROSION ON MULTIPLE ELEMENTS. (C-CHECK RO 8/9/2021) REMOVED OLD FWD FORMER & REPLACE WITH NEW FWD FORMER PER CRJ-700-SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01 DWG 601R31702 REV N. LEAK CHK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: HINGE — WORN (PAX DOOR) · 29,134 cycles

*PAX DOOR PIANO HINGE ON DOOR SIDE HAS MULTIPLE LUG LANDINGS WITH WEAR MARKS. (C-CHECK RO 8/9/2021) REMOVED AND REPLACED PIANO HINGE W/NEW PARTS IAW CRJ700 SRM 52-11-01-201-002-A01 & DWG 601R31702 REV .- N. LEAK CHK GOOD. COMPLIED WITH SKY CARD 51-900-1002-SKY

Part: HINGE — WORN (PAX DOOR) · 29,134 cycles

*PAX DOOR PIANO HINGE ON FUSELAGE SIDE, LUG ON FWD PORTION HAS WEAR. MARKED. (C-CHECK RO 8/9/2021) NEW HINGE HALF INSTALLED IAW CRJ700 SRM 53-21-23-201-007-A01 WITH REFERENCE TO DWG #SH670-31810 REV-NC. LEAK CHECK GOOD / 51-900-1002-SKY COMPLIED WITH

Part: CLEAT — CORRODED (PAX DOOR) · 29,134 cycles

SUSPECTED CORROSION IDENTIFIED 2 PLACES ON INNER DOOR STRUCTURE UNDER ACCESS PANEL 832FL - AS MARKED (C-CHECK RO 8/9/2021) REMOVED AND REPLACED 1EA CLEAT IAW CRJ-700 SRM 51-42-06-001-001-A01

Part: SEAT TRACK — CORRODED (BS 364-477 LBL27) · 29,134 cycles

*L/H O/B SEAT TRACK AT LBL 27 FROM APPROX F/S 364 TO 477 HAS MULTIPLE AREAS OF CORROSION (C-CHECK RO 8/9/2021) L/H O/B SEAT TRACK LBL27 FOUND TO BE OUT OF LIMITS DUE TO MULTIPLE DISCREPANT LOCATIONS ONLY ONE TYPE OF DAMAGE IS ALLOWED AT ANY TYPICAL CROSS SECTION ALONG THE LENGTH OF THE TRACK PER CRJ 700 SRM 53-21-49-101-001-A01, REPLACED WITH NEW SEAT TRACK SECTION FABRICATED ON JOB 71004995 OP 124, INSTALLED NEW SEAT TRACK SECTION WET WITH SEALANT PER CRJ 700 AMM 53-00-49-400-801-A02

Part: FLOORBEAM — CORRODED (BS 693 RBL 45) · 29,134 cycles

*RH FLOOR SILL SUPPORT ANGLE ATTACHED TO FWD PRESSURE FLOOR BULKHEAD AT FS 693.00, APPROX. RBL 45 HAS CORROSION (C-CHECK RO 8/9/2021) REPLACED NEW RH FLOOR SILL SUPPORT ANGLE ATTACHED TO FWD PRESSURE FLOOR BULKHEAD AT FS 693.00, APPROX. RBL 45 REF CRJ700 SRM 51-42-06-001-001-A01, REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-31541 REV NC.

Part: FLOORBEAM — CORRODED (BS 333 RBL 18) · 29,134 cycles

*CORROSION ON FLOOR SUPPORT BEAM FS 333.00 AT APPROX. RBL 18. MARKED. (C-CHECK RO 8/9/2021) DAMAGE #1 BLENDOUT DAMAGE PER CRJ 700 SRM 51-21-16-001-001-A01, NO REWORK PERMITTED ON THIS AREA FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 53-21-43-101-001-A01, DAMAGE #2 MATERIAL REMOVED FROM THIS AREA IS .060 , REQUESTED ENGINEERING TO REWORK AREA , RECEIVED REO 670-53-21-2057 REV -- DATED 2021/05/21, FABRICATED REPAIR ANGLE FROM 301-1/2 HARD .063 PO# T-54603 AND FABBED FILLER OUT OF 2024-T3 .100 PO#T-57779 , LOCATED AND DRILLED PER REO 670-53-21-2057 REV -- DATED 2021/05/21 , INSTALLED REPAIR ANGLE AND FILLER PER REO 670-53-21-2057 REV --DATED 2021/05/21 RESTORED FINISH PER REO 670-53-21-2057 REV -- DATED 2021/05/21. COMPLIED WITH 51-900-1002-SKY.

Part: FLOORBEAM — CORRODED (BS 333 RBL9) · 29,134 cycles

*CORROSION ON FLOOR BEAM PACKER SANDWICHED BETWEEN FS 333.00 FLOOR SUPPORT BEAM AND RBL 9 FLOOR BEAM. (C-CHECK RO 8/9/2021) REMOVED AND REPLACE PACKERS (2EA) ON FLOOR BEAM AT FS333.00 RBL9 IAW RJ 700 SRM 51-42-06-001-001-A01

Part: FLOORBEAM — CORRODED (BS 693 LBL 45) · 29,134 cycles

*LH FLOOR SILL SUPPORT ANGLE ATTACHED TO FWD PRESSURE FLOOR BULKHEAD AT FS 693.00, APPROX. LBL 45 HAS CORROSION (C-CHECK RO 8/9/2021) REPLACED NEW L/H FLOOR SILL SUPPORT ANGLE ATTACHED TO FWD PRESSURE FLOOR BULKHEAD AT FS 693.00, APPROX. LBL 45 REF CRJ700 SRM 51-42-06-001-001-A01, REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-31541 REV NC.

Part: PLATE — CORRODED (BS 533 S27) · 29,134 cycles

FWD BAGG FLOOR MOUNT DBLR PLATE CORRODED @ FS 533 STGR 27 (C-CHECK RO 8/9/2021) REMOVED AND INSTALLED NEW FWD CARGO FLOOR MOUNT PLATE SH670-33376-3. REF CRJ-700 SRM 51-42-06-001-001-A01. SEE CONTINUATION CARD FOR DETAILS

Part: SEAT TRACK — CORRODED (BS 830-985 RBL9) · 29,134 cycles

* RH FLOOR SEAT TRACK AT RBL9 BETWEEN FS830.40 AND APROX. FS985.00 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 8/9/2021) REMOVED AND REPLACED RH FLOOR SEAT TRACK AT RBL9 BETWEEN FS830.40 - FS985.00 REF CRJ700 SRM51-41-02-001-001-A01. SEE CONTINUE CARD FOR DETAILS.

Part: PLATE — CORRODED (BS 517 S26-27R) · 29,134 cycles

FWD BAGG FLOOR PLATE CORRODED @ FS 517 BTWN STGRS 26R/27 (C-CHECK RO 8/9/2021) BLENDED THEN REPLACED CORRODED OUT OF LIMITS FLOOR PLATE WITH NEW FABRICATED PART AT FS 517 BETWEEN STGRS 26R/27 REF CRJ700 SRM 51-42-06-001-001-A01

Part: STRINGER — CORRODED (BS1031-1047 S26R) · 29,134 cycles

*CORROSION ON STGR 26R BETWEEN FS 1031.00 €“ 1047.00 (C-CHECK RO 8/9/2021) REMOVED CORROSION ON STGR 26R BETWEEN FS 1031.00 €“ 1047.00 REF. CRJ700 AMM 53-00-03-201-001-A01. EVALUATED AND FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR REF. CRJ700 AMM 51-21-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD, NO DEFECTS FOUND.

Part: STRINGER — CORRODED (BS 485-501 S20R) · 29,134 cycles

STGR 20R CORRODED 3 PLACES BTWN FS'S 485/501 (C-CHECK RO 8/9/2021) PERFORMED A SPLICE REPAIR TO STGR 20R BETWEEN FS485-501 REF REO 670-53-31-665 REV A DATED 2021-06-11. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SKYWEST FORM M-337 AND SKYWEST TASK 51-900-1002-SKY.

Part: SEAT TRACK — CORRODED (BS 860-985 LBL9) · 29,134 cycles

* LH SEAT TRACK AT LBL9 BETWEEN FS830.40 AND FS985.00 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 8/9/2021) REMOVED AND INSTALLED NEW SEAT TRACK LBL9 BETWEEN FS830 AND FS985 REF-CRJ-700 SRM 51-41-02-001-001 A01

Part: STRINGER — CORRODED (BS 485-501 S19R) · 29,134 cycles

STGR 19R CORRODED BTWN FS'S 485/501 (C-CHECK RO 8/9/2021) REMOVED AND REPLACED CORRODED STGR19R BETWEEN FS485 TO FS501 REF CRJ 700 SRM 53-00-03-201-001-A01.LEAK CHECK GOOD / COMPLIED WITH TASK 51-900-1002-SKY

Part: DOUBLER — CORRODED (BS 1031-1051) · 29,134 cycles

*CORROSION ON DOUBLER FOR DRAIN MAST BETWEEN FS 1031.00 €“ 1051.30, STGR 27 €“ 26R (C-CHECK RO 8/9/2021) REPLACED DOUBLER AT DRAIN MAST BETWEEN FS1031-1051 STGR 27-26R REF- DWG MM670-43200 REV-N AND CRJ-700 SRM 51-42-06-001-001 A01,LEAK CHECK GOOD,NO LEAKS NOTED. / COMPLIED WITH TASK 51-900-1002-SKY

Part: MOUNT — CORRODED (BS 556 S22-23L) · 29,134 cycles

FWD BAGG TIE DOWN MOUNT PLATE CORRODED @ FS 533 BTWN STGRS 22L/23L (C-CHECK RO 8/9/2021) REMOVED AND INSTALLED NEW FWD CARGO FLOOR MACHINED BRACKET (P/N SH670-33390) AT FS533.00 BETWEEN STGR 22L/23L. REF CRJ-700 SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01 AND DWG SH670-33600 REV Y / COMPLIED WITH SKY CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**)

Part: STRIKER — CORRODED (SERVICE DOOR) · 29,134 cycles

* SERVICE DOOR BOTTOM SILL SEAL STRIKER HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 8/9/2021) REMOVED AND REPLACED NEW SERVICE DOOR SEAL STRIKER P/N SH670-31412-1 REF- CRJ700 SRM 51-42-06-001-001-A01 AND DRAWING NO. SH670-31950 REV Y. SEE CONTINUE CARD FOR DETAILS. / COMPLIED WITH TASK 51-900-1002-SKY

Part: STRINGER CLIP — CORRODED (BS 1000 S26L) · 29,134 cycles

*CORROSION ON CLIP ATTACHED TO STGR 26L AND FS 1000.00 (C-CHECK RO 8/9/2021) REMOVED AND REPLACED CLIP IAW CRJ700 SRM 51-42-06-001-001-A01, DRAWING# MM670-36061 REV D, SEE CONTINUATION FOR WORK ACCOMPLISHED. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: BULKHEAD — CORRODED (BS 693 S26L-R) · 29,134 cycles

FS 693 FWD PRESSURE BLKHD CORRODED @ BOTTOM ANGLE BTWN STGRS 26L/26R (C-CHECK RO 8/9/2021) REPAIRED LOWER MACHINED FRAME AT FS693 FWD PRESSURE BULKHEAD BTW STGR 26L-STGR 26R AND ALL STEPS COMPLETED OF REF-CRJ-700 MHI RJ REO 670-53-41-530 REV -- DATED 2021-07-07. LEAK CHECK GOOD. / COMPLIED WITH TASK 51-900-1002-SKY. ALL REPAIR/FABRICATED PARTS INSTALLED PER CRJ-700 MHI RJ REO 670-53-41-530 REV -- DATED 2021-07-07

Part: STRINGER — CORRODED (BS 565-581 S20R) · 29,134 cycles

STGR 20R CORRODED BTWN FS'S 565/581 (C-CHECK RO 8/9/2021) PERFORMED SPLICE REPAIR TO STGR 20R BETWEEN FS565-581 REF REO 670-53-31-665 REV A DATED 2021-06-11. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SKYWEST FORM M-337 AND SKYWEST TASK 51-900-1002-SKY.

Part: STRINGER — CORRODED (BS 310-319 S20R) · 29,134 cycles

* STR.20R BETWEEN FS 310.00 AND 319.70 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 8/9/2021) REMOVED AND REPLACED INTERCOSTAL P/N SH670-32074-1 AT FS310-319 STGR20R REF CRJ700 SRM51-42-06-001-001-A01 AND SRM51-42-21-001-001-A01 REV 38 JUL 25/2020 AND DWG NO. SH670-31950 REV Y. SEE CONTINUE CARD FOR DETAILS. / COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**)

Part: STRINGER — CORRODED (BS1088-1051 S25L) · 29,134 cycles

*CORROSION ON STGR 25L BETWEEN FS 1088.00 €“ 1051.00. AREAS MARKED. (C-CHECK RO 8/9/2021) REPAIRED DAMAGED STRINGER 25L BETWEEN FS 1051 AND FS1088 IAW CRJ700 SRM 53-00-03-201-001-A01 FIG 53-00-03-991-805 SHT 2, C/W TACK CARD 51-900-1002-SKY, SEE CONTINUATION FOR WORK ACCOMPLISHED

Part: SKIN — CHAFED (LT WING TE FLAP) · 29,134 cycles

* LH INBOARD FLAP UPPER SKIN IS CHAFED UNDER PANEL 584CB (C-CHECK RO 8/9/2021) BLENDED DAMAGE AREA FROM UPPER SKIN UNDER PANEL 584CB PER CRJ 700 SRM 51-12-00-001-001-A01,NO DAMAGE ALLOW AREA , RECIEVED REO 670-57-52-352 REV -- DATE 2017-03-28 , NDT AREA FOR CRACKS FREE AND NO DEFFECTS AND RESTORED FINISH AREA PER REO AND CRJ 700 SRM 51-21-16-001-001-A01 AND MARKED REWORK AREA PER REO STEP #6 " 670-57-52-352 ".

Part: SKIN — CHAFED (BS 977-985 S27) · 29,134 cycles

* FUSELAGE EXTERIOR SKIN CHAFED IN 3 LOCATIONS BETWEEN FS977 €“ FS985 STGR27 (C-CHECK RO 8/9/2021) PERFORMED REPAIR TO THE FUSELAGE EXTERIOR SKIN CHAFED AREAS BETWEEN FS977-985 AT STGR 27 REF REO 670-53-00-660 REV -- DATED 2021-05-31AND REO 670-53-00-290 REV F DATED 2019/04/26. PRESSURE LEAK CHECK GOOD. COMPLIED WITH SKYWEST FORM M-337 AND SKYWEST TASK 51-900-1002-SKY.

Part: FITTING — CHAFED (FWD CARGO) · 29,134 cycles

* FWD CARGO DOOR SURROUND, UPPER FWD GUIDE FITTING CHAFED/GOUGED (C-CHECK RO 8/9/2021) REPLACED FWD CARGO DOOR SURROUNG UPPER FWD GUIDE FITTITNG IAW CRJ 700 AMM 53-31-23-400-801-A01 / OPS TEST GOOD

Part: BRACKET — LOOSE (SERVICE DOOR) · 29,134 cycles

* SERVICE DOOR HOLD OPEN BRACKET IS LOOSE (C-CHECK RO 8/9/2021) REMOVED AND REPLACED AFT STRGR 14 IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. INSTL'D SERVICE DOOR HOLD OPEN BRACKET IAW CRJ700 SRM 51-42-13-001-001-A01, LEAK CHK GOOD SEE CONT CARD. COMPLIED WITH 51-900-1002-SKY. COMPLIED WITH SKYWEST FORM M-337. / REF DWG CC670-38103 REV C

Part: STOP FITTING — CORRODED (DOOR FRAME) · 29,134 cycles

* PASSENGER DOOR LOWER STOP BOLT FITTING CORRODED (C-CHECK RO 8/9/2021) REMOVED AND REPLACED PAX DOOR LOWER STOP FITTING IAW CRJ-700 AMM 52-11-02-000-806-A01 AND 52-11-02-400-806-A01

Part: LUG — CORRODED (LT WING TE FLAP) · 29,134 cycles

* L/H #3 FLAP MECHANISM FWD LUG FITTING HAS CORRODED HARDWARE (C-CHECK RO 8/9/2021) REPLACED MOUNTING HDWR ON L/H # 3 FLAP MECHANISM FWD LUG FITTING PER REF CRJ700 AMM TASK 57-54-02-400-810 CONFIG A01 LEAK CHECK GOOD

Part: SEAT TRACK — CORRODED (BS 863-969) · 29,134 cycles

R/H SIDE SEAT RAIL AT APPROX. FS863.00-FS969.00 HAS MULTIPLE SPOTS OF CORROSION ,SCRATCHES AND GOUGES (C-CHECK RO 8/9/2021) REMOVED AND REPLACED R/H SIDE SEAT RAIL AT APPROXIMATELY FS863.00 - FS969.00 IAW REF CRJ700 SRM 53-00-49-000-801-A01 AND SRM 53-00-49-400-801-A03

Part: SEAT TRACK — CORRODED (BS 379-485) · 29,134 cycles

*R/H SIDE SEAT RAIL AT APPROX. FS379.00-FS485.00 HAS MULTIPLE SPOTS OF CORRROSION ,SCRATCHES AND GOUGES (C-CHECK RO 8/9/2021) NO DAMAGE ALLOWED ON SIDE SEAT RAIL FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 53-21-49-101-001-A01, REPLACED BY NEW SECTION FABRICATED ON JOB 71004995 OP 119 , INSTALLED NEW SIDE SEAT RAIL WET WITH SEALANT PER CRJ 700 AMM 53-00-49-400-801-A02

Part: SEAT TRACK — CORRODED (BS 879-953) · 29,134 cycles

*L/H SIDE SEAT RAIL AT APPROX. FS879.00-FS953.00 HAS MULTIPLE SPOTS OF CORRODE HARDWARE ,SCRATCHES AND GOUGES (C-CHECK RO 8/9/2021) NO DAMAGE ALLOWED ON SIDE SEAT RAIL FS 879-953 FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 53-51-49-101-001-A01, FABRICATED NEW SECTION OF SIDE SEAT RAIL ON JOB 71004995 OP 120, INSTALLED NEW SECTION OF SIDE SEAT RAIL WET WITH SEALANT PER CRJ 700 AMM 53-00-49-400-801-A02

Part: FITTING — CORRODED (DOOR FRAME) · 29,134 cycles

PASSENGER DOOR SURROUND STRUCTURE FITTING. LOCATED TOWARD FWD AT THE MID SECTION HAS CORRODED FASTENER AND NUTPLATE. IDENTIFIED WITH TAPE. (C-CHECK RO 8/9/2021) REPLACED HARDWARE AND NUTPLATES ON PAX DOOR SURROUND STRUCTURE FITTING IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-15-001-001-A01

Part: FITTING — CORRODED (DOOR FRAME) · 29,134 cycles

PASSENGER DOOR SURROUNDING STRUCTURE FITTING. LOCATED TOWARD AFT AT THE MID SECTION HAS CORRODED FASTENER (1) AND NUTPLATE. IDENTIFIED WITH TAPE. (C-CHECK RO 8/9/2021) REMOVED AND REPLACED NUTPLATE AT PAX DOOR SURROUND STRUCTURE MID LOCATION REF CRJ700 SRM51-42-15-001-001-A01. SEE CONTINURE CARD FOR DETAILS.

Part: SLAT TRACK — CORRODED (LT WING) · 29,134 cycles

L/H SLAT TRACK 3-2 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 3-2 REF-CRJ-700 MHIRJ REO 670-57-42-1097 REV --, DATED 2021-05-17 AND CRJ 700 SRM 51-21-06-001-001-A01 ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (LT WING) · 29,134 cycles

L/H SLAT TRACK 1-2 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 1-2 REF-CRJ-700 MHIRJ REO 670-57-42-1093 REV --, DATED 2021-05-17 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (LT WING) · 29,134 cycles

L/H SLAT TRACK 1-3 HAS WORN AREA AND PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 1-3 REF-CRJ-700 MHIRJ REO 670-57-42-1094 REV --, DATED 2021-05-17 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (RIGHT) · 29,134 cycles

R/H SLAT TRACK 2-2 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) REMOVED PITTING CORROSION ON RH SLAT TRACK 2-2 IN 2 AREAS IAW CRJ700 SRM 51-21-06-001-001-A01 / ORIGINAL THICKNESS IS .250" / AFT TRACK L= 1.6" W= 1" REMAINING THICKNESS IS .247" MATERIAL LOST .003" / FWD TRACK L= 1.6" W= .5" REMAINING THICKNESS IS .249" MATERIAL LOST .001" NO ALLOWABLE LIMITS DIVEN IAW DWG CC670-12051 REV -C TOOL# TUC6260 DUE30-SEP-21 / RECIEVED ENGINEERING REO-670-57-42-1082 REV -- DATE 2021-05-10. / REMOVED SIDE SURFACE WEAR MARKS ON RH SLAT TRACK 2-2 REF CRJ 700 SRM 51-12-00-001-001-A01 / COMPLIED WITH STEPS 1,2 & 4 OF REO 670-57-42-1082 REV -- DATED 2021-05-10 / R/H SLAT TRACK 2-2 CANNED FOR USE ON N720EV JOB 71011585 OP 202 MX TRANS #22612319 / INSTALLATION OF NEW R/H SLAT TRACK FOR N614QX ACCOMPLISHED ON JOB 71004995 OP 108 MX TRANS #22766481 / COMPLIED WITH SKY CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR

Part: SLAT TRACK — CORRODED (LT WING) · 29,134 cycles

L/H SLAT TRACK 2-2 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 2-2 REF-CRJ-700 MHIRJ REO 670-57-42-1096 REV --, DATED 2021-05-17 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: VANE — CORRODED (LT WING TE FLAP) · 29,134 cycles

L/H INBD FLAP MOVEABLE VANE UPPER MOUNTING HARDWARE CORRODED (C-CHECK RO 8/9/2021) REMOVED LHIB FLAP MOVABLE VANE UPPER MOUNTING HARDWARE REF CRJ700 AMM 27-52-23-000-801-A01 STEP 4.A.(3)(A)(B). INSTALLED NEW MOUNTING HARDWARE REF CRJ700 AMM 27-52-23-400-801-A01 STEP 4.A.(4)(A)(B).

Part: SLAT TRACK — CORRODED (LT WING) · 29,134 cycles

L/H SLAT TRACK 2-1 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 2-1 REF-CRJ-700 MHIRJ REO 670-57-42-1095 REV --, DATED 2021-05-17 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (LT WING) · 29,134 cycles

L/H SLAT TRACK 1-1 HAS PITTING CORROSION (MARKED WITH RED) (C-CHECK RO 8/9/2021) BLENDED DAMAGE AT LH SLAT TRACK 1-1 REF-CRJ-700 MHIRJ REO 670-57-42-1091 REV --, DATED 2021-05-14 AND ALL STEPS COMPLETED, OPS TEST GOOD. / COMPLIED WITH TASK 51-900-1002-SKY

Part: BRACKET — CRACKED (SERVICE DOOR) · 29,134 cycles

GALLEY SERVICE DOOR - STABILIZER BAR BRACKET CRACKED @ UPPER STABILIZER BAR ATTACH POINT (C-CHECK RO 8/9/2021) REMOVED AND REPLACED STABILIZER BAR BRACKET P/N CC670-38380-3 WITH A NEW ONE IAW CRJ700 SRM TASK 51-41-02-001-001-A01.

Part: SKIN — CHAFED (RT WING) · 29,134 cycles

*RH WING LOWER EXTERNAL SKIN HAS CHAFING FROM CANOE FAIRING PANEL 695AB BETWEEN FS 797.00 €“ 847.00, APPROX. WS 202.67 (C-CHECK RO 8/9/2021) DAMAGE BLENDED-OUT IAW REO 670-57-21-913 REV -- (DATED 2021-05-12) & CRJ700 SRM 51-12-00-001-001-A01. LEAK CHK C/W NO LEAKS NOTED. REPAIR WAS BLEND OUT ONLY WITH NO INCRESE/DECREASE IN WEIGHT AND BALANCE. / COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: SKIN — DENTED (BS 485 S21R) · 29,134 cycles

EXTERNAL FUSELAGE - SEVERAL SMALL DENTS FS 485 STGR 21R (C-CHECK RO 8/9/2021) DUE TO THE PROXIMITY OF THE SEVERAL SMALL DENTS TO EACH OTHER AT FS485 STGR 21R, THEY WERE TREATED IN EFFECT AS ONE DENT AND REWORKED REF REO 670-53-31-673 REV -- DATED 2021-06-16 AND REO 670-51-00-085 REV A DATED 2017-08-23.

Part: ANGLE — CRACKED (BS 202 BULKHEAD) · airframe 36,812 hrs · 27,539 cycles

FOUND THE BS 202.75 BULKHEAD CAP ANGLE HAS A CRACK INDICATION AT STRINGER 13AR. 1 INCH LONG, 100%FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 670-53-11-1353 AND REO 670-53-11-1353.

Part: ANGLE — CRACKED (BS 202 BULKHEAD) · airframe 36,812 hrs · 27,539 cycles

FOUND THE BS 202.75 BULKHEAD CAP ANGLE HAS A CRACK INDICATION IN THE RADIUS AT STRINGER 13A . REPAIRED THE DAMAGE IAW REO 670-53-11-1351.

Part: STIFFENER — CRACKED (BS 202 BULKHEAD) · airframe 36,812 hrs · 27,539 cycles

FOUND THE BS 202.75 BULKHEAD FWD STIFFENER, AFT INBD RADIUS, LBL 30, WL 100 HAS A CRACK INDICATION, .200 INCH LONG, 80% FSH, FAILED NDT INSPECTION. REPAIRED THE STIFFENER IAW SRM 53-11-10-201-005-A01.

Part: STIFFENER — CRACKED (BS 202 BULKHEAD) · airframe 36,812 hrs · 27,539 cycles

FOUND THE BS 202.75 BULKHEAD FWD VETICAL STIFFENER BL 0, WL 100 HAS A CRACK INDICATION NOTED ON THE RT SIDE FWD RADIUS APPROXIMATELY 1 INCH LONG, 70% FSH FAILED NDT. REPAIRED THE DAMAGE IAW REO 670-53-1354, AND REO 670-53-11-1354.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

LT FLOORSILL AT FS 349 IS CORRODED. REPAIRED FLOORSILL IAW EA 25-2017-028 AND EC/TC EA 25-2017-028 REV 0.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 35,329 hrs · 26,027 cycles

DURING C CHECK, FOUND PASSENGER DOOR LOWER SILL MID CAP ANGLE CORRODED. R & R PASSENGER DOOR LOWER SILL MID CAP ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

CORROSION ON FLOORBEAM AT LBL 27.00 BETWEEN FS 1000 AND FS 1051. REPAIRED FLOORBEAM IAW EO 700-53-10-00012.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

CORROSION ON FLOORBEAM AT LBL 9.00 BETWEEN FS 1015.00 AND FS 1051.30. CONTINUATION FROM OP 74 FOUND DAMAGED CLIP AT LBL9 FS 985. REPAIRED CLIP IAW EA 26-2017-024.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 35,329 hrs · 26,027 cycles

DURING C CHECK, FOUND CORROSION ON THE TCAS OMNI DIRECTIONAL ANTENNA DOUBLER. R & R THE DOUBLER.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

CORROSION ON AVIONICS BAY INTERCOSTAL AT FS 364.00 STR 26L. REMOVED AND INSTALLED NEW SERVICEABLE INTERCOSTAL AT FS 364.00 STR 26L IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FRAME — CORRODED (BS 295) · airframe 35,330 hrs · 26,027 cycles

CORROSION ON BS 295 FRAME BETWEEN STRINGERS 25L-25R. REPAIRED THE FRAME SECTOR IAW EC/TC REO 670-53-21-799 AND REO 670-53-21-799 REV A.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 35,330 hrs · 26,027 cycles

CO-PILOTS WINDSHIELD SIDE POST LOWER AFT SUPPORT ANGLE IS CRACKED AT RADIUS. REMOVED AND INSTALLED A NEW SUPPORT FITTING IAW SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SERVICE DOOR LOWER SILL, LOWER SILL ANGLE IS CORRODED. REMOVED AND REPLACED SILL ANGLE IAW SRM 51-42-06-001-001-A01.

Part: CAGE — DAMAGED (SMOKE DETECTOR) · airframe 35,330 hrs · 26,027 cycles

CARGO PANEL 281 ALC,S SMOKE DETECTOR CAGE IS BENT AND HAS ONE PIECE BROKEN OFF AND MISSING. REPAIRED CAGE IN ACCORDANCE WITH ECTC CARD NR REO 670-25-52-006 REV B DATED 2017-01-27 AND REO 670-25-52-006 REV E DATED 2016-09-09.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 6 FS 785-FS 863 HAS CORROSION AT MULTIPLE LOCATIONS. REPLACED SEAT TRACK SEGMENT IAW AMM 53-00-49-400-801-A02.

Part: SKIN — CHAFED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

FUSELAGE EXTERNAL SKIN CHAFED AT STRINGER 27 BETWEEN FS 969 - 1000, (3) AREAS TOTAL. REPAIRED DAMAGED AREA REPAIRED IAW REO 670-53-00-290 REV D, DATED 09/10/2015 AND EC/TC REO 670-53-00-290.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

STRINGER 27 FS 280.00-295.00 HAS CORROSION. REMOVED AND REPLACED STRINGER IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (BS 1144-1162) · airframe 35,329 hrs · 26,027 cycles

DURING C CHECK, FOUND LT INTERCOSTAL INBD FLANGE HAS CHAFE DAMAGED FROM BONDING WIRE CLAMP. CHAFE IS LOCATED A FWD END OF INTERCOSTAL. REPAIRED INTERCOSTAL IAW EA 30-2017-020.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

CARGO DOOR SURROUND STRUCTURE LOWER SILL CORRODED BETWEEN FS 1000.00-1047.00 STR 17L. REMOVED AND REPLACED LOWER SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: WEB — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

ALL 4 SERVICE DOOR STEP PLATE SUPPORTS CORRODED (WEB PROTECTORS). REMOVED AND REPLACED ALL 4 GALLEY DOOR PROTECTORS MACHINED WEBS SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

RT FS 280 WEB ANGLE HAS FILIFORM CORROSION AROUND FLOORBOARD FASTENER. UPON REMOVAL OF WEB ANGLE, NO CORROSION FOUND. CORROSION WAS FOUND ON RT FS 280 CROSS BEAM. REMOVED AND REPLACED CROSS BEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

RIGHT SIDE SEAT TRACK SEGMENT FROM FS 713-763 HAS CORROSION IN MULTIPLE PLACES. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW EC/TC REO 670-53-00-343 AND AMM 53-00-49-400-801-A02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

PASSENGER DOOR LOWER SILL KICK PLATE ANGLE CORRODED. REMOVED AND REPLACED PASSENGER DOOR LOWER SILL KICK PLATE IAW SRM 51-42-13-00-00-A01 AND 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 7, FS 863-969 HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 2, FS 485-565, HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 4, FS 677-713 HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 3, FS 565-677 HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 4, FS 677-713 HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

CORROSION ON AVI BAY INTERCOSTAL AT FS 364.00, STR 25L. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 5, FS 713-761 HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: FRAME — CORRODED (FAIRING) · airframe 35,330 hrs · 26,027 cycles

FUSELAGE FAIRING FRAMES ARE CORRODED AROUND FASTENER HOLES FROM FS 879 TO FS 939.00. REPAIRED DAMAGED AREA IAW SRM 51-21-06-001-001-A01 AND 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SEAT TRACK SEGMENT NR 2 AT RBL 9.00 IS CORRODED AT MULTIPLE PLACES BETWEEN FS 485 TO 581. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

RIGHT SIDE SEAT TRACK SEGMENT NR 7, FS 863-969 HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 6, FS 785-863 HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SEAT TRACK SEGMENT NR 1 IS CORRODED AT FS 477.00. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 3, FS 565 - FS 677 HAS CORROSION AT MULTIPLE LOCATIONS. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SEAT TRACK SEGMENT NR 4 LBL 9.00 IS CORRODED AT MULTIPLE PLACES. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

LEFT SIDE SEAT TRACK SEGMENT NR 2 IS CORRODED AT FS 485-565. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SEAT TRACK SEGMENT NR 2 AT LBL 9 IS CORRODED MULTIPLE PLACES BETWEEN AT FS 485-581. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SEAT TRACK SEGMENT 3 AT LBL 9 IS CORRODED AT MULTIPLE PLACES BTW FS 581.00-677.00. REMOVED AND REPLACED SEAT TRACK SEGMENT IAW REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

RT SIDE CABIN FLOOR SILL IS CORRODED FROM FS 280 TO FS 319. REMOVED AND REPLACED RT SIDE SILL P/N SH670-32172-3, SPLICE ANGLE P/N SH670-31543-1, LIGHTNING DIVERTER ANGLE P/N SH670-31547-1, ANGLE ASSY SH670-31546-1 AND RING DOUBLER P/N SH670-31524-1 IAW SRM 51-40-06-001-001-AO1, 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SEAT TRACK SEGMENT 3 AT RBL 9 IS CORRODED MULTIPLE PLACES BTW FS 581.00-677.00. REMOVED AND REPLACED SEAT TRACK SEGMENT IAW REO 670-53-00-343 REV M DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SEAT TRACK SEGMENT 1 AT LBL 9 IS CORRODED BTW FS 376.00-380.00. REMOVED AND REPLACED SEAT TRACK SEGMENT IAW REO 670-53-00-343 REV M DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SERVICE DOOR LOWER SILL MOUNTING ANGLE IS CORRODED. REMOVED AND REPLACED SERVICE DOOR LOWER SILL MOUNTING ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SEAT TRACK SEGMENT NR 4 AT RBL 9.00 IS CORRODED AT MULTIPLE PLACES. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,330 hrs · 26,027 cycles

SEAT TRACK SEGMENT NR 1 AT RBL 9 AT FS 349.00-485.00 IS CORRODED AND GOUGED. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M DATED 2015-10-19 AND EC/TC REO 670-53-00-343.

Part: RUB STRIP — DETERIORATED (LT AILERON) · airframe 34,443 hrs · 25,338 cycles

RUB STRIP ON LT AILERON HAS SEPARATED FROM AILERON. PERFORMED PERMANENT REPAIR OF LT AILERON RUB STRIP.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 34,294 hrs · 25,204 cycles

EMERGENCY LIGHTS ALL OVER THE ACFT CAME ON AND STAYED ON FOR TEN MINTUES AND THEN SELF EXTINGUISHED. LIGHTS ARE NOT ON NOW. SYSTEM SELF RESET FAULT NO LONGER EXIST IAW NO FURTHER ACTION IS REQUIRED.

Part: DOOR — NONE · airframe 32,979 hrs · 24,144 cycles

PASSENGER DOOR HARD TO OPEN. PERFORMED OPS CK OF PASSENGER DOOR IAW AMM 52-11-00, OPS CK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 31,297 hrs · 22,872 cycles

EMERGENCY LIGHTS ON STATUS MESSAGE. MESSAGE DISAPEARRED AFTER LANDING. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS TESTED GOOD. CAN NOT DUPLICATE FAULT. ACFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 30,944 hrs · 22,597 cycles

EMERGENCY LIGHT LEFT ON BY CLEANERS, ALL EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERIES ON BOARD IAW AMM 25-60-3. OPS CK GOOD.

Part: NUT PLATE — BROKEN (RT WING) · airframe 30,905 hrs · 22,571 cycles

RT WINGLET PANEL 671BT HAS A BROKEN NUTPLATE. R & R NUTPLATE ON WINGLET PANEL 671BT IAW SRM 51-42-15-001-001-A01.

Part: BRACKET — DAMAGED (BS 280) · airframe 30,905 hrs · 22,571 cycles

ALTERNATE EXTENSION CABLE BRACKET AT FS 280.00 HAS ELONGATED HOLES. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED ALTERNATE EXT CABLE BRACKET AT FS 280 DUE TO HOLES OUT OF DWG SPECIFICATIONS IAW SRM 51-42-06-001-001. INSTALLED SERVICEABLE ALT EXTENSION CABLE BRACKET, PN CC670-85101-1 AT FS 280.00 AS NEEDED REF SRM 51-42-00-001-001-A01 AND DWG CC670-85020. OBTAINED, LOCATED AND OPEN HOLES AS REQUIRED. DEBURR HOLES AND COATING OF NEW ALTERNATE EXTENSION CABLE BRACKET IAW SRM 51-40-11-001-001-A01, 51-25-06-001-001-A01.

Part: STIFFENER — CRACKED (BS 280 BULKHEAD) · airframe 30,905 hrs · 22,571 cycles

VERTICAL STIFFNER LOCATED AT BS 280, RBL 70, IS CRACKED. REMOVED VERTICAL STIFFNER ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED IAW DWG CC670-33050 AND SRM 51-42-06-001-001-A01.

Part: GUSSET — DAMAGED (BS 280) · airframe 30,905 hrs · 22,571 cycles

RIGHT GUSSET LOCATED AT BS 280, RBL 9,HAS ELONGATED HOLES. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED RT GUSSETT LOCATED AT FS 280.00, RBL9 AS NEEDED REF: SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED RT GUSSETT AT FS280, LBL9 AS NEEDED REF: DRG CC670-33052 AND SRM 51-40-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-40-11-001-001-A01.

Part: ANGLE — DAMAGED (FLOORBEAM) · airframe 30,905 hrs · 22,571 cycles

LEFT FLOORBEAM ANGLE AT BS 2800, LBL 9 HAS ELONGATED HOLES. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01, DWG CC670-33052, SRM 51-40-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-40-11-001-001-A01.

Part: ANGLE — BUCKLED (PAX DOOR) · airframe 30,905 hrs · 22,571 cycles

ASD TOP AFT SIDE STRUCTURE IS BUCKLED. COMPLIED WITH REO 670-52-11-072. INSTALLED REPAIR PARTS IAW REO 670-52-11-072. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REPAIRED AIR STAIR DOOR SIDE STRUCTURE IAW EC/TC AND REO 670-52-11-072.

Part: ANGLE — CRACKED (FLOORBEAM) · airframe 30,905 hrs · 22,571 cycles

FLIGHT DECK FLOORBEAM ANGLE RT SIDE IS CRACKED. REMOVED RT FLIGHT DECK FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED FLOORBEAM ANGLE IAW DWG CC670-33199, DWG CC670-33052, SRM 51-40-06-001-001-A01, SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01.

Part: BRACKET — DAMAGED (BS 280) · airframe 30,905 hrs · 22,571 cycles

MOUNTING BRACKET FOR THE STICK PUSHER, LOCATED AT FS 280.00, HAS ELONGATED HOLES. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. OBTAINED, LOCATED AND OPEN HOLES AS REQUIRED, DEBURR HOLES AND COATING OF NEW MOUNTING BRACKET IAW SRM 51-46-11-001-001: 51-25-06-001-001-A01. INSTALLED NEW SERVICEABLE STICK PUSHER CAPTAN BRACKET ONTO RT FS 280 WEB SRM 51-42-06-001-001 AND DWG CC670-94641.

Part: ANGLE — CRACKED (FLOORBEAM) · airframe 30,905 hrs · 22,571 cycles

COCKPIT FLOORBEAM ANGLE, LT SIDE, CRACKED. REMOVED LT FLT DECK FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED FLOORBEAM ANGLE IAW DWG CC670-33199, DWG CC670-33052, SRM 51-42-06-001-001-A01, SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 30,905 hrs · 22,571 cycles

LEFT BULKHEAD AT FS 280 LOWER WEB CORRODED. REMOVED SPLICE PLATE & WEB, FABRICATED NEW WEB IAW REO 670-53-11-594. COMPLIED WITH REMAIN REO 670-53-11-594 AND ECTC REO 670-53-11-594. REPAIR CLASSIFIED AS MAJOR.

Part: BEAM — CORRODED (BS 280) · airframe 30,905 hrs · 22,571 cycles

BS 280 BEAM IS CORRODED TOP SURFACE, AT COCKPIT DOOR ENTERANCE. BEAM REPLACED IAW SB 670BA-53-041.

Part: BULKHEAD — CORRODED (BS 280) · airframe 30,905 hrs · 22,571 cycles

RT COCKPIT BULKHEAD FS 280 IS CORRODED. SEVERAL LOCATIONS ALONG FLOOR LEVEL. COMPLIED WITH REO 670-53-11-594-01 AND ECTC IAW REO 670-53-11-594-01.

Part: SKIN — BUCKLED (PAX DOOR) · airframe 30,905 hrs · 22,571 cycles

ASD TOP AFT SIDE STRUCTURE IS BUCKLED. COMPLIED WITH PERMANENT REPAIR OF ASD TOP AFT SIDE STRUCTURE IAW EC/TC REO 670-52-11-072. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED AFT ASD SKIN IAW SRM 51-42-06-001-001-A01. DRILLED NEW AFT SKIN FOR ASD IAW SRM 51-42-06-001-001. INSTALLED SKIN TO ASD INSTALL STIFFENERS TO SKIN IAW SRM 51-42-06-001-001. INSTALLED HAND RAIL BRACKET, STEP AND COUNTER BALANCE BRACKET TO SKIN IAW SRM 51-42-66-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,018 hrs · 21,958 cycles

AFT DRAG ANGLE ON PAX DOOR CRACKED. REMOVED DAMAGED AFT DRAG ANGLE AND SPLICES IAW SRM 51-42-13 AND SRM 51-42-06. STEPPED UP DISCREPANT HOLES IN PAX DOOR AFT SIDE PANEL AND WEB TO REMOVE DAMAGE IAW SRM 51-40-11. SUBMITTED DAMAGE REPORT TO MFG IAW SRM 51-13-01. INSTALLED NEW DRAG ANGLE IAW REO 670-52-11-735, REV B.

Part: MEGAPHONE — UNKNOWN (CABIN) · airframe 28,422 hrs · 20,802 cycles

F/A MEGAPHONE INOPERATIVE. PERFORMED OPS CHECK OF MEGAPHONE IAW AMM25-61-14. OPS CHECKED GOOD AT THIS TIME NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 26,985 hrs · 19,755 cycles

ON 1ST FLT CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. RECHARGED EMERGENCY LIGHT BATTERY PACK, PERFORMED OPS CHECK IAW AMM 35-51-01, OPS CHECKED GOOD,

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,903 hrs · 19,701 cycles

EMERGENCY LIGHTS IN GALLEY LIFT IN ON POSITION CAUSING EMERGENCY LIGHTS TO NOT FUNCTION FOR FIRST FLIGHT. RECHARGED CABIN EMERGENCY BATTERY PACK, OPS CHECKED GOOD, NO DEFECT NOTED, IAW AMM 33-51-01.

Part: SEAT TRACK — CORRODED (BS 863-785.15) · airframe 26,457 hrs · 19,376 cycles

RIGHT SIDEWALL SEAT TRACK AT FS 863 TO FS 785.15 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-19-101-001-A01 AND 53-51-19-101-001-A01. R & R SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 26,457 hrs · 19,376 cycles

DURING REMOVAL OF THE BS 280.00 CROSSBEAM REPLACEMENT, FOUND COCKPIT FLOOR SUPPORT LAND CRACKED. INSTALLED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: FLOORBEAM — DAMAGED (BS 280) · airframe 26,457 hrs · 19,376 cycles

ON REMOVAL OF RT 280 FLOORBEAM, FOUND 1 HOLE ROUTED OUT AT FLOOR SILL AT 280. REPAIRED IAW REO 670-53-21-139.

Part: ATTACH FITTING — CORRODED (BS 320.1-388) · airframe 26,457 hrs · 19,376 cycles

FOUR 90 DEGREE ATTACH ANGLE AT ENDS OF DOOR FRAMES AT BOTTOM OF DOOR CORRODED FWD FRAME, FS 320.1, AFT FS 388. INSTALLED ATTACH ANGLES IAW SRM 51-42-06-001-001-A01.

Part: WEB — CORRODED (BS 280) · airframe 26,457 hrs · 19,376 cycles

LEFT BS 280 WEB CORRODED. FOUND TO BE OUT OF LIMITS IAW 53-11-10-201-003-A01. REPAIRED IAW REO 670-53-11-594.

Part: VERTICAL SUPPORT — CRACKED (BS 280) · airframe 26,457 hrs · 19,376 cycles

VERTICAL ANGLE FS 280.00 AT BL 26.00 CRACKED. INSTALLED SERVICABLE ANGLE IAW AMM SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — DAMAGED (BS 661-752) · airframe 26,457 hrs · 19,376 cycles

LEFT SIDE WALL SEAT TRACK AT FS 661 TO 752 CHAFED AND CORRODED. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED DAMAGED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — DAMAGED (BS 469-565) · airframe 26,457 hrs · 19,376 cycles

LT SIDE WALL SEAT TRACK AT APROX FS 469 - 565 CHAFED AND CORRODED. FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 26,457 hrs · 19,376 cycles

ASD LOWER STEP NUTPLATE ANGLE CRACKED AT WD SECTION. INSTALLED NEW ANGLE IAW SRM 51-42-13-001-001-A01, 52-42-15-001-001-A01

Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 26,457 hrs · 19,376 cycles

RIGHT SIDE WALL SEAT TRACK AT FS 581 TO 661 CORRODED. REMOVED DAMAGE FROM SEAT TRACK IAW SRM 51-21-06-001-001. FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01.

Part: SEAT TRACK — CORRODED (BS 469-565) · airframe 26,457 hrs · 19,376 cycles

RIGHT SIDE WALL SEAT TRACK AT FS 469 TO 565 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001. FOUND TO BE OUT OF LIMITS FOR SRM 53-31-490991-804. R & R DAMAGED SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 677-693) · airframe 26,457 hrs · 19,376 cycles

RIGHT SIDE WALL SEAT TRACK AT FS 677 TO 693 CORRODED. REMOVED CORROSION IAW SRM 51-12-00-001-001. FOUND TO BE WITHIN LIMITS IAW SRM 53-31-49-101-001-A01.

Part: RISER — CRACKED (PAX DOOR) · airframe 26,457 hrs · 19,376 cycles

ASD FWD RISER CRACKED LOWER CORNER. REMOVED RISER DRAG ANGLE SUPPORT ANGLES UPPER RAIL & BOX FITTING & NUT PLATES IAW SRM 51-42-06-001-001-A01. LOCATED NEW RISER ON FWD ASD DRILLED UP RISER FOR THE DRAG ANGLE SUPPORT ANGLES UPPER RAIL BOX FITTING & NUT PLATES IAW SRM 51-40-11-001-001-A01. ASSEMBLE PARTS ON ASD FWD SIDE PANEL. INSTALLED RISER SKIN TO ALL SUPPORT ANGLES, DRAG ANGLE UPPER RAIL BOX FITTING & NUT PLATES SRM 51-42-06-00 & 51-42-15-00. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED ASA MAJOR/MINOR REPAIR IAW ASA SOP 5702. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)

Part: SEAT TRACK — CORRODED (BS 597-677) · airframe 26,457 hrs · 19,376 cycles

LBL 9 SEAT TRACK CORRODED FROM FS 597 TO 677. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 26,457 hrs · 19,376 cycles

LBL 9 SEAT TRACK CORRODED FROM FS 485 TO 581. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801 (A02) AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 693) · airframe 26,457 hrs · 19,376 cycles

RBL 9.00 SEAT TRACK CORRODED AT FS 693. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND TO BE WITHIN LIMITS IAW SRM 53-41-49, FIG 53-41-49-991-804.

Part: SEAT TRACK — CORRODED (BS 485-565) · airframe 26,457 hrs · 19,376 cycles

RBL 9 SEAT TRACK CORRODED FROM FS 485 TO 565. SEAT TRACK FOUND TO BE CORRODED BEYOND ALLOWABLE DAMAGE IAW SRM 53-41-49. R & R WITH SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 364-565) · airframe 26,457 hrs · 19,376 cycles

LBL 9 SEAT TRACK CORRODED FROM FS 364 TO 565. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01. R & R CORRODED SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 26,457 hrs · 19,376 cycles

RBL 9 SEAT TRACK CORRODED FROM 349 TO 409. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801(A02) AND 53-00-49-400-801(A02).

Part: SEAT TRACK — CORRODED (BS 597-677) · airframe 26,457 hrs · 19,376 cycles

RBL 9 SEAT TRACK CORRODED FROM FS 597 TO 677. REMOVED CORROSION AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 26,457 hrs · 19,376 cycles

LBL 9.00 SEAT TRACK CORRODED FROM FS 863 TO 969. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49-101-001-A01. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 53-11-49-000-801(A01) AND 53-00-49-400-801(A02).

Part: SEAT TRACK — CORRODED (BS 693) · airframe 26,457 hrs · 19,376 cycles

LBL 9 SEAT TRACK CORRODED AT FS 693. REMOVED CORROSION FROM SEAT TRACK, FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49.

Part: SEAT TRACK — CORRODED (BS 847-939) · airframe 26,457 hrs · 19,376 cycles

RBL 9.00 SEAT TRACK CORRODED FROM FS 847 TO 939. SEAT TRACK IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 26,457 hrs · 19,376 cycles

FS 280, LBL 9 FLOORBEAM CRACKED. REPAIRED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 26,457 hrs · 19,376 cycles

FS 280 CROSSBEAM CORRODED. REPAIRED IAW REO 670-53-11-697.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 26,457 hrs · 19,376 cycles

FWD EQUIPMENT BAY FLOOR CRACKED ON LT SIDE JUST OTBD OF BRAKE ACCUMALATOR GAUGES. COMPLIED WITH REO 670-53-11-509 AND REO 670-53-11-509 REV.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,457 hrs · 19,376 cycles

FS 280, RBL 9 FLOORBEAM CRACKED. REPAIRED.

Part: ANGLE — CORRODED (BS 1015 S5-19R) · airframe 26,457 hrs · 19,376 cycles

ANGLE AT S5-19R, FS 1015 HAS CORROSION. REMOVED CORRODED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE SRM 51-42-06-001-001A-01.

Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 26,457 hrs · 19,376 cycles

FWD EQUIPMENT FLOOR CRACKED ON RT SIDE NEXT TO ADG PUMP. COMPLIED WITH REO 670-53-11-509 AND REO 670-53-11-509 REV.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 26,457 hrs · 19,376 cycles

FLOOR LEVEL GLOW STRIP IS MISSING IN FRONT OF WARDROBE CLOSET. INSTALLED MISSING GLOW STRIP IAW AMM 33-51-00. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,058 hrs · 19,100 cycles

ELECTRICAL BURNING ODOR COMING FROM ROW 16D. SIDE PANEL WAS WARM TO THE TOUCH. INSPECTED ACFT WIRING ROW 16D IAW ESPM 20-12-00, NO FAULTS FOUND.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 25,401 hrs · 18,654 cycles

AFT MEGAPHONE INOPERATIVE. R & R AFT MEGAPHONE IAW AMM 25-65-14. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,248 hrs · 18,546 cycles

CABIN CEILING EMERGENCY LIGHT THIRD FROM FRONT INOP. RELAMPED CABIN NR3 CEILING EMERGENCY LIGHT IAW AMM 33-51-09. OPS CHECK GOOD.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 24,873 hrs · 18,285 cycles

RECEIVE GEAR DISAGREE WARNING MSG AFTER SELECTING GEAR DOWN NO INDICATION OF GEAR CYCLE PERFORM GEAR DISAGREE QHR PROCEDURE AND EMERGENCY GEAR EXTENSION LANDED AFTER OBTAINING 3 GREEN. (EMERGENCY DECLARED AS A PRECAUTION). R & R LANDING GEAR SELECTOR VALVE IAW IWA AMM 32-32-10. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,821 hrs · 18,249 cycles

NR4 INTERIOR CEILING EMERGENCY LIGHT INOP. RELAMPED NR4 INTERIOR CEILING EMERGENCY LIGHT AS REQUIRED. OPS CHECKED GOOD IAW AMM 33-51-00. RELAMPED NR4 INTERIOR CEILING EMERGENCY LIGHT AS REQUIRED. OPS CK GOOD IAW AMM 33-51-00.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 24,727 hrs · 18,185 cycles

EMERGENCY LIGHTS CYCLE ON AND OFF WHEN IN THE ARM POS. R & R ALL 4 EMERGENCY BATTERY PACK IAW AMM 33-51-17. NO HELP.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 24,671 hrs · 18,144 cycles

MEGAPHONE INOP. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 708) · airframe 24,070 hrs · 17,716 cycles

FS 708 RT SIDEWALL SEAT TRACK HAS CORROSION BEYOND SRM LIMITS. REMOVED SEAT TRACK IAW TASK 53-00-49-000-801. INSTALLED NEW TRACK IAW TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 581) · airframe 24,070 hrs · 17,716 cycles

FS 581 RT SIDEWALL SEAT TRACK HAS CORROSION BEYOND SRM LIMITS . REMOVED SEAT TRACK IAW AMM 53-00-49-400-800. INSTALLED NEW TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 420) · airframe 24,070 hrs · 17,716 cycles

FS 420 RT SIDEWALL SEAT TRACK HAS CORROSION BEYOND SRM LIMITS. 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 420-490) · airframe 24,070 hrs · 17,716 cycles

REF NR 2534N00020, CUSTOMER REQUEST CORROSION ON RT SIDEWALL SEAT TRACK, FS 420 AND 490. DURING EVALUATION, DETERMINED THE CORROSION TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-21-49.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 24,070 hrs · 17,716 cycles

CORROSION ON RT SIDEWALL SEAT TRACK, AT SEAT POSITIONS 7CD AND 11CD. DETERMINED THE CORROSION TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49.

Part: FLOOR PANEL — CRACKED (BS 810) · airframe 23,858 hrs · 17,568 cycles

DURING NDT INSPECTION, FOUND ONE CRACK INDICATION, APPROX .5" LONG ON THE PRESSURE FLOOR, LT SIDE, AT FS 810 BETWEEN LBL9 AND LBL18. MAPPED CRACK AND VERFIED. REPAIRED AREA IAW REO 670-53-41-125/3.

Part: BALLAST — OVERHEATED (CABIN LIGHTS) · airframe 23,863 hrs · 17,527 cycles

NOTICED ELECTRICAL ODOR IN ROW 6-7 OVERHEAD BIN AREA DURING CABIN WALK-THRU. INSPECTED, FOUND BALLAST IN OVERHEAD BIN FOR CEILING LIGHT AT ROW 6-7 ED OVERHEATED. REMOVED BALLAST IAW AMM TASK 33-23-00-000-801, INSTALLED NEW BALLAST FROM STOCK IAW AMM TASK 33-23-00-400-801. ALSO RE-LAMPED LIGHT BULBS ABOVE ROW 6-7 ED. OPS CHECK GOOD. RETURNED TO SERVICE.

Part: FAN — FAILED (ZONE 200) · airframe 22,584 hrs · 16,612 cycles

DISPLAY COOL CAUTION AFTER T/O, RETURN TO FIELD. LANDING UNEVENTFUL. REPLACED NR 1 DISPLAY SUPPLY FAN AND CHECK VALVE IAW AMM TASKS 21-24-12-000-801 & 21-24-12-400-801, OPS CHECK GOOD. RETURNED TO SERVICE.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 21,732 hrs · 15,982 cycles

C CHECK - PAX DOOR MIDCAP ANGLE HAS CORROSION ON IT. REMOVED PAX DOOR MIDCAP ANGLE IAW SRM 51-41-02-001-001-A01. RECEIVED NEW MIDCAP ANGLE AND LOCATED NEW HOLES IAW SRM 51-40-11-001-001-A01. INSTALLED NEW MIDCAP ANGLE IAW SRM 51-41-00-001-001-A01. APPLIED AV-8 IAW SRM 51-21-11-001-001-A01.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · airframe 21,732 hrs · 15,982 cycles

C CHECK - SERVICE DOOR MOUNTING ANGLE HAS CORROSION ON IT. REMOVED CORROSION FROM MOUNTING ANGLE ON SILL IAW SRM 51-21-06-001-001, FOUND BLEND TO BE OUT OF LIMITS IAW SRM 51-12-00-001-001 AND 53-21-23-101-002-A01. REMOVED MOUNTING ANGLE AND LOCATED FASTENER HOLES IN NEW ANGLE IAW SRM 51-42-06-001-001-A01. TREATED AND PRIMED HOLES IAW SRM 51-21-11-001-001-A01. INSTALLED NEW MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01.

Part: STRAP — CORRODED (BS 280 S27R) · airframe 21,732 hrs · 15,982 cycles

C-CHECK DURING INSP FOUND CORRODED ON FS 280 JOINT STRAP AT STRINGER 27RBL 3". REMOVED 2 RIVETS AND BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREA IS A NO-DAMAGE ALLOWED AREA IAW SRM 53-21-01-101-002-A01. PERFORMED ECI ON BLENDED AREA . NO CORROSION OR CRACKS FOUND IAW NDTM ECI 51-20-006. SENT FOR ENGINEERING. RECEIVED ENGINEERING. BLEND IS W/IN LIMITS OF REO 670-53-21-559. ALLODINED IAW SRM 51-21-11-001-001-A01. PRIMED AREA IAW CRJ700 51-21-06-001-001-A01. INSTALLED RIVETS IAW SRM 51-42-06-001-001-A01. PAINTED IAW SRM 51-25-16-001-001. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01. ALL WORKS IS IN CONFORMITY WITH REO 670-53-21-559/3.

Part: FITTING — CORRODED (BS 265-280) · airframe 21,732 hrs · 15,982 cycles

C-CHECK FOUND CORROSION ON FWD JACK FITTING BETWEEN FS 265-FS280 AND STRINGER 26L AND 26R. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED CORROSION BETWEEN FS265-FS280 ON FWD JACK FITTING IAW SRM 51-21-06-001-001-A01. BLENDED CORRODION BETWEEN FS 265-FS280 ON FWD TRACK FITTING IAW SRM 51-21-06-001-001-A01. PERFORMED ECI. NO CRACKS NOTED AT THIS TIME IAW NDTM 51-20-006. ALL BLENDING DONE W/IN LIMITS IAW SRM 53-00-00-101-001-A01. TREATED , PRIMED, AND TOP-COATED IAW SRM 51-21-11-001-001-A01. MAXIMUM MATERIAL REMOVED .004 6" LONG .65 WIDE ON FLANGE OF JACK-FITTING SUPPORT. NO ALLOWABLE LIMITS IAW SRM. SENT DAMAGE REPORT TO MFG. COMPLETED WORK IAW REO 670-53-11-498. ALL WORKS ABOVE IS IN CONFORMITY WITH REO 670-53-11-498.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 21,732 hrs · 15,982 cycles

C-CHECK SUSPECT CORROSION ON LT SIDE SEAT TRACK FS379-485. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW REO 670-53-03-013. REMOVED LT SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW LT SEAT TRACK IAW AMM53-00-49-400-801.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 21,732 hrs · 15,982 cycles

C-CHECK SERVICE DOOR STRIKER SEAL HAS CORROSION. REMOVED CORROSION IAW CXRJ700 SRM 51-21-06-001-001-A01. PERFORMED LPI IAW NDTM LPI 51-20-008-230-A01. STRIKER SEAL FOUND TO BE OUT OF LIMITS OF SRM 53-21-23-101-001-A01. REMOVED SERVICE DOOR STRIKER SEAL AND LOCATED FASTENER HOLES IN NEW STRIKER SEAL FITTING IAW CRJ700 SRM 51-42-06-001-001-A01. TREATED AND PRIMED HOLE IAW CRJ700 SRM 51-21-11-001-001-A01. INSTALLED STRIKER SEAL IAW CRJ700 SRM 51-42-06-001-001-A01. COMPLETED REPAIR IAW REO 670-53-21-557. PERFORMED LEAK CHECK IAW CRJ700 AMM 52-00-00-790-801.

Part: STRINGER — CORRODED (BS 280 S26R) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - DURING INSP FOUND CORROSION ON STR 26 RT JUST AFT OF FS 280 JOINT STRAP ON STRINGER ATTACH FLANGE. BLENDED AREA OF CORROSION ON STRINGER IAW SRM 51-21-06-001-001-A01. BLENDED AREA FOUND TO BE A "NO DAMAGE ALLOWED" AREA IAW SRM 53-21-03-101-002-A01. SENT DAMAGE REPORT TO MFG ENGINEERING. PERFORMED ECI, NO CRACKS NOTED AT THIS TIME IAW NDTM ECI 51-00-006-250-A01, REO 670-53-21-558. DURIING INSTALL FOUND ADDITIONAL CORROSION ON AFT SECTION OF STRINGER, NO DAMAGE ALLOWED IAW SRM 53-21-03-101-002-A01. SUBMITTED TO ENGINEERING. REMOVED OLD STRINGER, FABRICATED NEW STRINGER IAW SRM 53-21-03-001-002-A01. FABRICATED DOUBLER IAW REO670-53-21-559. PERFORMED ECI ON FRAME CUTLINE. NO CRACK FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01. ETCHED ALODINE IAW SRM 51-21-11-001-001-A01. TOPPED COAT IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. INSTALLED REPAIR IAW REO 670-53-21-559 AND SRM 53-00-03-201-001-A01. TOP COATED FASTENERS IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: ATTACH ANGLE — CORRODED (ZONE 100) · airframe 21,732 hrs · 15,982 cycles

C-CHECK ATTACHED ANGLE CORRODED IN AVIONICS BAY UNDER FLOORBOARDS 141ALF. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 53-00-00-001-A01. LOCATED HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01. TOP COATED ALL FASTENERS IAW SRM 51-25-06-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 784-863) · airframe 21,732 hrs · 15,982 cycles

C-CHECK EVIDENCE OF CORROSION ON RT SIDE SEAT TRACK FROM FS 784 TO FS 863. FOUND CORROSION OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801A2. INSTALLED SEAT TRACK IAW RJ700 AMM 53-00-49-400-801-A02.

Part: SILL — CHAFED (CARGO DOORWAY) · airframe 21,732 hrs · 15,982 cycles

C-CHECK DURING INSP FOUND AFT CARGO DOOR SILL TO BE CHAFED AND CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED ECI IAW NDTM ECI 51-20-006. FOUND BLEND OUT OF LIMITS SENT TO ENGINEERING TREATED AND PRIMED AND PAINTED AS REQUIRED IAW REO 670-53-61-585. APPLIED AV8 CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01. ALL WORK DONE IN CONFORMITY WITH TASK CARDS REO 670-53-61-585/3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 21,732 hrs · 15,982 cycles

RFD C-CHECK INNER SIDE OF FUSELAGE SKIN AROUND AVIONICS DOOR CUT-OUT HAS CORROSION. REMOVED CORROSION IAW REO670-53-21-242. PERFORMED LPI. NO CRACKS OR CORROSION FOUND IAW NDTM LPI-51-20-008-230-A01, REO670-53-21-242. COMPLETED REPAIR IAW SRM 51-21-16-001-001-A01 AND REO 670-53-21-242.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 21,732 hrs · 15,982 cycles

C-CHECK SERVICE DOOR MID CAP ANGLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-12-001-001-A01 AND 53-21-23-101-002-A01. REMOVED MID CAP ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED , DRILLED, AND DE-BURRED NEW MID CAP-ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED MID CAP ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. PRIMED AND PAINTED FASTENERS IAW SRM 51-25-00-001-001-A01.

Part: ATTACH ANGLE — CORRODED (BS 364 S26R) · airframe 21,732 hrs · 15,982 cycles

C-CHECK DURING INSP, FOUND CORROSION ON ATTACH ANGLE 26R FWD OF FS364 ON ITS OTBD SIDE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-12-00-001-001 AND SRM 53-21-23-101-001-A01. LOCATED HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ATTACH ANGLE IAW SRM 51-42-21-001-001-A01. TOP COATED FASTENERS IAW SRM 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-801-A01.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 21,732 hrs · 15,982 cycles

C-CHECK. DURING INSP FOUND CORRODED ANGLE FWD CAP AT PAX DOOR. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SILL — CORRODED (FUSELAGE) · airframe 21,732 hrs · 15,982 cycles

C-CHECK-PAX DOOR LOWER SILL HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED DOOR SILL IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SILL IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 21,732 hrs · 15,982 cycles

RFD C-CHECK EVIDENCE OF CORROSION ON LT SIDE SEAT TRACK FROM FS 677 TO FS 708. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW LT SIDE SEAT TRACK FROM 677 TO 708 IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 708-762) · airframe 21,732 hrs · 15,982 cycles

RFD C-CHECK EVIDENCE OF CORROSION ON RT SEAT TRACK FROM FS 708 TO FS 762. BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED RT SEAT TRACK IAW AMM 53-00-49-000-801-A02. INSTALLED NEW SEAT TRACKS IAW AMM 53-00-49-000-801-A02.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 21,732 hrs · 15,982 cycles

C-CHECK CORROSION FOUND ON SECTION OF THE LT FLOOR SEAT TRACK FROM FS379 TO FS485. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK FROM FS 379 TO 485 IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SKIN — DAMAGED (WING) · airframe 21,732 hrs · 15,982 cycles

C-CHECK. COMPLY WITH HORIZON TASK CARD REO 670-57-52-134/3. DRILLED OUT ALL BLIND RIVETS IAW REO 670-57-52-134. REMOVED DAMAGED SKIN IAW REO 670-57-52-138. PERFORMED LPI ON CUT LINES. NO CRACKS FOUND. IAW NDTM LPI 51-20-008-230-A01. REO 670-57-52-138. FABRICATED THE DOUBLER IAW REO 670-57-52-138. TREATED, PRIMED IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01. PERFORMED ECI ON CUT LINES USING ECI NDTM 51-20-006-250-A01. REO 670-57-52-134 NO CRACKS FOUND AT THIS TIME. INSTALLED REPAIR IAW REO 670-57-52-134/3. TOP COATED ALL FASTENERS IAW SRM 51-25-01-001-001-A01.

Part: SKIN — CORRODED (FUSELAGE) · airframe 21,732 hrs · 15,982 cycles

C-CHECK CORROSION ON BELLY SKIN LOCATED WHERE ADF ANTENNA IS LOCATED. BLENDED AREAS IAW SRM 51-21-06-001-001-A01. FOUND BLEND OUT OF LIMITS IAW SRM 53-31-01-101-003. PERFORMED ECI, NO CRACKS OR CORROSION FOUND AT THIS TIME IAW NDTM ECI 51-20-006-250-A01 AND REO 670-53-31-158. ALODINED IAW SRM 51-21-11-001-001-A01. TOP COATED IAW CRJ700 SRM 51-25-21-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01. ALL WORK DONE IAW REO 670-53-31-158.

Part: PANEL — CHAFED (LE FLAP) · airframe 21,732 hrs · 15,982 cycles

C-CHECK CHAFE ON L/E OF FLAP PANEL 584EB. BLENDED CHAFED DAMAGE IAW SRM 51-12-00-001-001-A01. FOUND BLEND TO BE OUT OF LIMITS IAW SRM 57-52-01-101-001-A01. TREATED, PRIMED, TOP-COATED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 708-762) · airframe 21,732 hrs · 15,982 cycles

C-CHECK EVIDENCE OF CORROSION ON LT SIDE SEAT TRACK FROM FS 708 TO FS 762. BLENDED CORROSION, FOUND BLEND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A02. DRILL HOLES AND COUNTERSUNK NEW TRACK IAW SRM 51-40-11-001-001-A01. INSTALLED SREAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 21,732 hrs · 15,982 cycles

C-CHECK CORROSION FOUND ON SECTION OF RT FLOOR SEAT TRACK FROM FS 349 TO FS 485. BLENDED CORROSION, FOUND BLEND OUT OF LIMITS IAW REO 670-53-00-13. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A02. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A02.

Part: SEAT TRACK — CORRODED (BS 572-669) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - SUSPECT CORROSION ON LT SIDE SEAT TRACK FROM FS 572 TO 669.40. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FRAME — CORRODED (BS 549 S26-27L) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - CORROSION ON THE ATTACH FLANGE AT FRAME FS 549.00 BETWEEN STR 27 AND 26L. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .059" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01. PAINTED AREA IAW SRM 51-25-16-001-001-A01. APPLIED AV8 CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 517 S26L/R) · airframe 21,732 hrs · 15,982 cycles

C CHECK -CORROSION ON THE FWD FREE FLANGE ON FRAME FS 517.00 BETWEEN STR 26L AND 26R. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .048" AND WITHIN LIMITS OR SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01. PAINTED AREA IAW SRM 51-25-16-001-001-A01. APPLIED AV8 CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 517 S26-27R) · airframe 21,732 hrs · 15,982 cycles

C CHECK - CORROSION ON THE ATTACH FLANGE AT FRAME FS 517.00 BETWEEN STR 27 AND 26R. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .045" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01. PAINTED AREA IAW SRM 51-25-16-001-001-A01. APPLIED AV8 CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 517 S25-26L) · airframe 21,732 hrs · 15,982 cycles

C CHECK - CORROSION ON THE ATTACH FLANGE AT FRAME FS 517.00 BETWEEN STR 26L AND 25L. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .067" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01. PAINTED AREA IAW SRM 51-25-16-001-001-A01. APPLIED AV8 CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: WEB — CORRODED (BS 280) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - CORROSION FOUND ON R/H WEB AT FS 280.00. BLENDED CORROSION, FOUND BLENDS TO BE OUT OF LIMITS IAW SRM 53-11-10-991-805. REMOVED WEB IAW SRM 57-42-06-001-001-A01 AND 51-42-13-001-001-A01. LOCATED ALL FASTENER HOLES IN NEW WEB IAW SRM 51-40-11-001-001-A01 AND TASK 53-11-10-201-003-A01. INSTALLED NEW WEB IAW SRM 51-42-06-001-001-A01 AND 53-11-10-003-A01. TOPCOATED ALL FASTENERS IAW 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 517 S26-27L) · airframe 21,732 hrs · 15,982 cycles

C CHECK - CORROSION ON THE ATTACH FLANGE AT FRAME FS 517.00 BETWEEN STR 27 AND 26L. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .068" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01. PAINTED AREA IAW SRM 51-25-16-001-001-A01. APPLIED AV8 CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 517 S22-23L) · airframe 21,732 hrs · 15,982 cycles

C CHECK -CORROSION ON THE ATTACH FLANGE AT FRAME FS 517.00 BETWEEN STR 23L AND 22L. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IS .069" AND WITHIN LIMITS OF SRM 53-31-06-101-003-A01. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01. PAINTED AREA IAW SRM 51-25-16-001-001-A01. APPLIED AV8 CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,732 hrs · 15,982 cycles

C CHECK- COCKPIT PANEL FLOOR SUPPORT ANGLE AT FS 280 SHOWS SIGNS OF CORROSION. BLENDED CORROSION, FOUND CORROSION OUT OF LIMITS IAW SRM5300-00-001-A01 PAGE 3. LOCATED FASTENER HOLE IN NEW ANGLE IAW SRM51-40-11-001-001-A01. INSTALLED NEW A IAW SRM 51-42-21-001-001-A01. PRIMED, TOP-COATED FASTENERS IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 629 S26-27R) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - CORROSION ON THE ATTACH FLANGE OF FRAME FS 629.00 BETWEEN STR 27 AND 26R. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED .003", REMAINING MATERIAL THICKNESS IS .060" AND WITHIN LIMITS OR SRM 53-31-06-101-003-A01. ALODINED IAW 51-21-11-001-001-A01. PRIMED IAW SRM 51-21-11-001-001-A01. PAINTED AREA IAW SRM 51-25-16-001-001-A01. APPLIED AV8 CORROSION PREVENTATIVE COMPOUND IAW SRM 51-21-11-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 21,732 hrs · 15,982 cycles

C CHECK -LT AND RT SIDE OF 280 BEAM SHOWS SIGNS OF CORROSION. BLENDED CORROSION RT 280 BEAM IAW SRM 51-11-00-001-001-A01. FOUND BEAM TO BE CRACKED. REMOVED BEAM IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. CUT NEW 280 BEAM. PERFORMED LPI ON CUTLINE, NO CRACKS NOTED IAW NDTM LPI 51-20-008-230-A01. LOCATED, DRILLED AND DEBURRED ALL HOLES IN THE NEW BEAM IAW SRM 51-40-11-001-001-A01. INSTALLED 280 BEAM IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. TREATED, PRIMED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-06-001-001-A01. COMPLETED BEAM INSTALLATION IAW REO 670-53-11-047. PRIMED & TOP-COATED IAW SRM51-25-06-001-001-A01. APPLIED CORROSION PREVENTATIVE COMPOUND IAW SRM51-21-11-001-001-A01.

Part: FRAME — CORRODED (BS 295 S26R) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - CORROSION FOUND ON FWD WEB SIDE OF FRAME 295.00 AROUND STGR 26R CUTOUT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, BLENDS WITHIN LIMITS IAW SRM 53-21-06-101-002-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-21-06-001-001-A01, 51-25-16-001-001-A01.

Part: STRUCTURE — CHAFED (BS 977 S27) · airframe 21,732 hrs · 15,982 cycles

C CHECK - CHAFING AT STR 27 FS 977.00 UNDER PANEL DL. BLENDED OUT DAMAGED AREA IAW SRM 51-12-00-001-001-A01. BLEND FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-14. PERFORMED LPI IAW NDTM LPI 51-20-008-230-A01. ETCHED AND ALODINED IAW SRM 51-21-11-001-001-A01. PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, AND REO 670-53-00-014.

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 21,732 hrs · 15,982 cycles

C CHECK - EVIDENCE OF CORROSION ON RT SIDE SEAT TRACK FROM FS 677.00 TO FS 708.00. BLENDED OUT ALL CORROSION AND FOUND TO BE WITHIN LIMITS OF REO 670-53-00-13. TREATED IAW REO 670-53-00-13.

Part: SEAT TRACK — CORRODED (BS 784-863) · airframe 21,732 hrs · 15,982 cycles

C CHECK - EVIDENCE OF CORROSION ON LT SIDE SEAT TRACK FROM FS 784.00 TO FS 863.00. BLENDED OUT ALL CORROSION AND FOUND TO BE WITHIN LIMITS OF REO 670-53-00-13. ETCHED AND ALODINED LT SIDE SEAT TRACK IAW SRM 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 572-669) · airframe 21,732 hrs · 15,982 cycles

C CHECK - SUSPECT CORROSION ON SIDE SEAT TRACK RT FROM FS 572-669.4. BLENDED OUT ALL CORROSION FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-13. TREATED IAW REO 670-53-00-13.

Part: SEAT TRACK — CORRODED (BS 485-572) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - SUSPECT CORROSION ON LT SIDE SEAT TRACK FROM FS 485 TO 572. BLENDED LT SIDE SEAT TRACK FS 485 TO 572 CORROSION. ORIGINAL THICKNESS .110, BLENDED .020 MAX ALLOWABLE .035", REMAINING MATERIAL .090" FOUND TO BE WITHIN LIMITS IAW REO 670-53-00-013. ETCHED, ALODINED AREA IAW SRM 51-21-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 458-572) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - SUSPECT CORROSION ON SIDE SEAT TRACK FROM FS 485 TO 572 FURTHER INVESTIGATION REQUIRED ON RT SIDE. BLENDED OUT ALL CORROSION TO .024" DEEP BY .375 WIDE BY 2" LONG. ORIGINAL MATERIAL THICKNESS IS .105", REMAINING MATERIAL AFTER BLENDING .081" CORROSION REMOVED FOUND TO BE WITHIN LIMITS OF REO 670-53-00-013. TREATED IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - SUSPECT CORROSION ON SIDE SEAT TRACK FROM FS 379 TO 485 FURTHER INVESTIGATION REQUIRED ON RT SIDE. BLENDED OUTT ALL CORROSION TO .031" DEEP BY 1.0" WIDE BY 1.0" LONG. ORIGINAL MATERIAL THICKNESS IS .105" REMAINING MATERIAL AFTER BLAND .074" CORROSION REMOVED, FOUND TO BE WITHIN LIMITS OF REO 670-53-00-13. TREATED IAW REO 670-53-00-13.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - RT LOWER L/E OF AILERON HAS CHAFING ON SKIN. BLENDED DAMAGE ON THE RT LOWER L/E SKIN AT AILS 330.68 AND AILS 370.66 TO A SMOOTH AND DAMAGE FREE CONDITION IAW SRM 51-12-00-001-001-A01. ALL BLENDS ARE WITHIN LIMITS IAW SRM 57-61-01-101-001-A01. ETCHED, ALODINED, PRIMED AND PAINTED AREA IAW CRJ700 SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-21-16-001-001-A01.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 21,732 hrs · 15,982 cycles

C-CHECK - LT UPPER L/E OF AILERON HAS CHAFING ON SKIN. BLENDED CHAFE DAMAGE ON UPPER L/E AT AILS 365.00 IAW SRM 51-12-00-001-001-A01. BLEND IS A MAX 2.0 INCH LONG AND .75 INCH WIDE. REMAINDER MAX OF .005 OUT OF ORIGINAL .090. BLEND IS WITHIN LIMITS IAW SRM 57-61-01-101-001-A01. ETCHED AND ALODINED AREA IAW SRM 51-21-11-001-001-A01. PRIMED AND PAINTED AREA IAW SRM 51-25-06-001-001-A01, AND 51-21-16-001-001-A01.

Part: PANEL — HOT (SEAT ROW 18E) · airframe 21,473 hrs · 15,801 cycles

PASSENGER COMPLAINS THAT THE SIDEWALL AT ROW 18E WAS TO HOT TO TOUCH DURING APPROACH. FOUND SIDEWALL TEMP AT ROW 18AB & 18DE BOTH FOLLOW DEMAND TEMPERATURE, AIR CONDITIONING DUCTS RUN BEHIND SIDEWALL IN THAT LOCATION. NO DEFECTS FOUND AIR FLOW TO GASPERS IS NORMAL. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CONTROLLER — MALFUNCTIONED (ANTISKID SYS) · airframe 20,518 hrs · 15,085 cycles

INBD GROUND SPOILER FAULT STATUS MESSAGE AFTER LIFTOFF. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. INTERROGATED MDC, FOUND FAULT IN HISTORY, "SSCU 1/NO ASCU-1, BUS INPUT". C/W FIM ISOLATION IAW FIM 27-61-05-810-839-A02. REMOVED AND REPLACED ANTI-SKID CONTROL AS A PRECAUTIONARY MEASURE IAW AMM TASK 32-44-06-000-801-A01, 32-44-06-400-801-A01. OPS CHECK GOOD, NO FAULTS NOTED. RETURNED TO SERVICE.

Part: WIRE HARNESS — MALFUNCTIONED (CARGO DOOR) · airframe 20,426 hrs · 15,008 cycles

WHILE AT CRUISE "AFT CARGO FOOR" CAUTION AND "PROX SYS FAULT2" STATUS MESSAGE. DIVERTED AND ACCOMPLISHED A UNEVENTFUL LANDING. INSPECTED AFT CARGO DOOR UPON ARRIVAL AT GATE, FOUND DOOR CLOSED AND LOCKED. INSPECTED MDC MESSAGE - AFT CARGO DOOR COVER, INPECTED WIRING, NO DEFECTS FOUND. REINSTALLED COVER AND CHECKED WIRING FROM CONNECTOR AT DOOR TO FUSELAGE. NO DEFECTS FOUND. REMOVED AND REPLACED AFT DOOR PROX SENSOR IAW MM TASK 52-70-02-000-803 AND 52-70-02-400-803. OPS CHECK OF BAGGAGE DOOR WARNING SYS GOOD. RETURNED TO SERVICE.

Part: TRANSDUCER — FAILED (STALL WARNING) · airframe 18,998 hrs · 13,860 cycles

PDX - RIGHT AFTER T/O STALL FAIL CAUTION LIGHT CAME ON. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. IN MDC HISTORY FOUND "SPC L/R AOA DISAGREE". PERFORMED FUNCTIONAL TEST OF STALL PROTECTION COMPUTER PER CRJ700 AMM TASKS 27-35-01-720-801, FUNCTIONAL TEST GOOD. REMOVED & REPLACED LT ANGLE-OF-ATTACK TRANSDUCER PER CRJ700 AMM TASKS 27-35-05-000-801 & 27-35-05-400-801 AS A PRECAUTIONARY MEASURE, RT WAS REMOVED AND REPLACED 3-24-09. OPS TEST GOOD. RETURNED TO SERVICE.

Part: WIRE HARNESS — CHAFED (STATIC INVERTER) · airframe 17,946 hrs · 12,932 cycles

PDX - WIRE HARNESS TO STATIC INVERTER ON AFT RT SIDE OF REAR PRESSURE HAS CHAFED THRU HYDRAULIC LINE AND DAMAGED WIRES TO STATIC INVERTER. REPAIRED WIRE RHB0878-20 AT STATIC INVERTER BY SPLICING IAW CRJ 700 WM 74-00-01. INSTALLED STATIC INVERTER WITH A SERVICEABLE PART FROM STOCK IAW CRJ 700 AMM TASK 74-31-03-400-801-A01. OP'S CHECKED GOOD. RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK CORROSION FOUND UNDER LOWER TCAS ANTENNA ON STRUCTURE. REMOVED ANTENNA IAW CRJ 700 AMM 34-43-07-000-801. BLENDED CORROSION .008 MATERIAL REMOVED IAW REO670-53-21-362. PERFORMED ECI NO DEFECT NOTED IAW REO670-53-21-362. TREATED AREA AND INSTALLED ANTENNA IAW REO 670-53-21-362 AND CRJ AMM 34-43-07.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK FS 280 SHOWS SIGNS OF CORROSION. BLENDED CORROSION FROM LT FS 280 BULKHEAD. .002 MATERIAL REMOVED, IAW CRJ 700 SRM 53-11-10. BLENDED CORROSION FROM RT FS 280 BULKHEAD, .003 MATERIAL REMOVED. IAW CRJ 700 SRM 53-11-10. TREATED IAW CRJ 700 SRM 51-21-11, PRIMED IAW SRM 51-25-06 TOPCOAT APPLIED IAW SRM 51-25-00.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 675 TO 713. REMOVED CORROSION FROM SEAT TRACK AT FS 675 TO 713. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 675 TO 713. REMOVED CORROSION FROM SEAT TRACK AT FS 675 TO 713. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 573 TO FS 675. REMOVED CORROSION FROM SEAT TRACK AT FS 573 TO FS 675. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16.

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 784 TO 861. REMOVED CORROSION FROM SEAT TRACK AT FS 784 TO 861. .015 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 713 TO 784. FOUND OUT OF LIMITS AFTER BLEND. REMOVED CORRODED SEAT TRACK FROM FS 713 TO 784 IAW CRJ 700 SRM 51-41-02. INSTALLED NEW SEAT TRACK IAW CRJ 700 SRM 51-41-00, 51-41-02 AND 51-23-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK CORROSION FOUND UNDER UPPER TCAS ANTENNA ON STRUCTURE. REMOVED ANTENNA IAW CRJ 700 AMM 34-43-04-000-801. BLENDED CORROSION, .013 MATERIAL REMOVED IAW REO670-53-21-362. PERFORMED ECI NO DEFECTS NOTED IAW REO 670-53-21-362. TREATED AREA AND INSTALLED ANTENNA IAW REO 670-53-21-362 AND CRJ AMM 34-43-04-400-801.

Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 379 TO FS 483. REMOVED CORROSION FROM SEAT TRACK AT FS 379 TO FS 483. .015 MATERIAL REMOVED TREATED IAW REO 670-53-00-013 AND SRM 51-21-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK. NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 379 TO FS 483. REMOVED CORROSION FROM SEAT TRACK AT FS 379 TO 483. .15 MATERIAL REMOVED IAW REO670-53-00-013. TREATED IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 861 TO 985. REMOVED CORROSION FROM SEAT TRACK AT FS 861 TO 985. .015 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK PAX DOOR MID CAP ANGLE CORRODED. REMOVED CORRODED MID CAP ANGLE IAW CRJ 700 SRM 51-41-00. LOCATED HOLES IN NEW ANGLE ATTACHED 5 NUTPLATES. TRANSFERRED BRACKETS FROM OLD TO NEW PART IAW CRJ 700 SRM 51-42-06. INSTALL MID CAP ANGLE IAW CRJ 700SRM 51-41-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 483 TO 573. REMOVED CORROSION FROM SEAT TRACK AT FS 483 TO 573. .015 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 573 TO 675. REMOVED CORROSION FROM SEAT TRACK AT FS 573 TO 675. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 483 TO FS 573. REMOVED CORROSION FROM SEAT TRACK AT FS 483 TO FS 573. .040 MATERIAL REMOVED, OUT OF LIMITS IAW REO 670-53-00-013. REMOVED CORRODED SEAT TRACK IAW CRJ 700 SRM 51-41-02 AND INSTALLED NEW SEAT TRACK IAW 51-41-02 AND 51-23-00.

Part: SILL — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK FOUND CORROSION ON SILL OF AFT CARGO BAY DOOR. BLENDED IAW REO 670-53-61-373, .002 MATERIAL REMOVED. PERFORMED ECI IAW REO 670-53-61-373 NO DEFECTS NOTED. TREATED, PRIMED AND PAINTED IAW REO 670-53-61-373.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 861 TO 985. REMOVED CORROSION FROM SEAT TRACK AT FS 861 TO 985. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 713-784) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 713 TO 784. REMOVED CORROSION FROM SEAT TRACK AT FS 713 TO 784. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK LT SECTION OF THE 280 CROSSBEAM IS CORRODED. BLENDED CORROSION FROM LT FS 280 CROSSBEAM. .020 MATERIAL REMOVED, BLEND IS OUT OF LIMITS IAW REO 670-53-11-046. REMOVED LT SECTION OF 280 CROSSBEAM IAW CRJ 700 SRM 51-42-06. CUT NEW CROSSBEAM IAW REO 670-53-11-047. PERFORM LPI IAW CRJ NDTM 51-20-008 NO DEFECT NOTED. INSTALLED NEW 280 CROSSBEAM IAW CRJ 700 SRM 51-40-11, REO 670-53-11-046. PRIMED AND APPLIED TOP COAT IAW CRJ 700 SRM 51-25-06 AND 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL RS 784 TO 861. REMOVED CORROSION FROM SEAT TRACK AT FS 784 TO 861. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,954 hrs · 12,090 cycles

RFD C4 CHECK BURN MARK FOUND ON FUSELAGE SKIN BETWEEN FS 592 AND FS 613. REMOVED RIVET FORWARD OF BURN MARK IAW CRJ 7000 SRM 51-42-06. BLENDED DAMAGE REMOVED .025 MATERIAL IAW REO 670-53-31-101. PERFORMED ECI ON BLENDED AREA IAW REO 670-53-31-101 NO DEFECTS NOTED. TREATED IAW CRJ 700 SRM 51-21-11. INSTALLED RIVET AND PRIMED AND PAINTED IAW CRJ 700 SRM 51-21-11, REO 670-53-31-101.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 16,053 hrs · 11,435 cycles

PDX - FLIGHT 2533, NOTICED A ELECTRICAL SMELL AROUND ROW 7 IN THE CABIN. MAINTENANCE FOUND THE BALLAST FOR THE OVERHEAD LIGHTS AT ROW 6 A/B VERY HOT. REPLACED BALLAST. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (ANTI ICE SYS) · airframe 15,694 hrs · 11,156 cycles

PDX - FLIGHT 9820 - UPON SELECTING WING ANTI-ICE TO ON RECEIVED A SENSOR MESSAGE. MAINTENANCE REPLACED THE J814 CONNECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 15,693 hrs · 11,154 cycles

PDX - FLIGHT 2591 - GOING THROUGH 8000 FEET, FLIGHT ATTENDANT CALLED TO SAY THAT THERE WAS AN EXHAUST ODOR IN THE BACK OF THE AIRCRAFT. STRONGEST AFTER TAKEOFF, BUT DISSIPATED BY THE TIME SHE CALLED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE PERFORMED A INSPECTION OF THE APU AND ENGINE GROUND RUN, WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: WARNING LIGHT — ILLUMINATED (BRAKE OVERHEAT) · airframe 15,625 hrs · 11,101 cycles

FLIGHT 2553. EXPERIENCED ON CLIMB, A BRAKE OVERHEAT WARNING MESSAGE. NR 4 BRAKE INDICATED 20. AFTER 1 MINUTE THE INDICATION WENT TO GREEN. BTMS RESET. MAINTENANCE COMPLIED WITH SL 32-033. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SLEEVE — MISSING (THRUST REVERSER) · airframe 15,588 hrs · 11,075 cycles

BIL- FLIGHT 2549 - ON TAXI OUT, CYCLING THE THRUST REVERSERS RESULTED IN A REVERSER UNLOCKED CAUTION MESSAGE. RETURNED TO THE GATE. AFTER PARKING THE REVERSER APPEARS TO BE FULLY DEPLOYED. MAINTENANCE FOUND THE INBOARD TRANS COWL SLIDING SLEEVE TO BE HALF MISSING AND TWISTED, PREVENTING RETRACTION OF THE RIGHT THRUST REVERSER. ADJUSTED REMAINING PORTION OF SLEEVE AND REINSTALLED THE TRANS COWLS. LOCKED OUT THE RIGHT THRUST REVERSER AND PLACED ON MEL 78-33-01. ACFT RETURNED TO SERVICE. REPLACED THE NR 2 ENGINE UPPER TRANSCOWL NYLON INSERT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — FAILED (STARTER) · airframe 15,332 hrs · 10,896 cycles

DEN - FLIGHT 2507 - DURING ENGINE START AFTER PUSHBACK RECEIVED A LEFT ENGINE STARTER VALVE CAUTION. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 80-11-3. AIRCRAFT RETURNED TO SERVICE. REPLACED THE STARTER CONTROL VALVE. OPERATIONAL CHECKS GOOD MEL CLOSED. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (ANTI ICE SYS) · airframe 15,320 hrs · 10,889 cycles

PDX - FLIGHT 2571 - RIGHT WING ANTI ICE CAUTION MESSAGE RECEIVED WITH CHECKLIST ACCOMPLISHED, MESSAGE DID NOT RE-APPEAR. MAINTENANCE PLACED THE SYSTEM ON MEL 30-12-4B. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CRACKED (PAX DOOR) · airframe 14,782 hrs · 10,554 cycles

PDX - MAIN CABIN DOOR INNER SKIN CRACKED AT FUSELAGE STATION 335 NEXT TO INTERCOSTAL DD6. MAINTENANCE REPAIRED IN ACCORDANCE WITH REO 670-52-11-277. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 14,782 hrs · 10,544 cycles

DEN - MAIN CABIN DOOR OUTER HANDLE HAS A 1/2 INCH CRACK IN THE CIRCULAR BOSS (KEYHOLE REINFORCEMENT AREA). MAINTENANCE REPLACED THE MAIN CABIN DOOR OUTER HANDLE IAW AMM 52-11-03-400-801-A01. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — UNKNOWN (MLG) · airframe 14,522 hrs · 10,379 cycles

DEN - FLIGHT 4325, ON TAXI OUT, THE RIGHT OUTBOARD (NR 4) BRAKE TEMP WENT FROM 4 IN THE GREEN TO 8 IN THE WHITE. RETURNED TO THE GATE. BRAKE WAS NOT DRAGGING. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE INDICATION ON MEL 32-46-1. THE MEL WAS CLEARED BY REPLACING THE NR 4 BRAKE AND THE THERMOCOUPLE SENSOR FOR THE TEMP INDICATION. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (ANTI SKID SYS) · airframe 14,181 hrs · 10,154 cycles

PDX - LEFT BRAKES SEEM MUSHY AND SEEM TO GET HOT QUICKLY. MAINTENANCE REPLACED THE ANTI-SKID CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: VALVE — MALFUNCTIONED (RT BRAKE) · airframe 14,153 hrs · 10,138 cycles

PDX - RIGHT BRAKE WEAK. MAINTENANCE REPLACED THE ANTI-SKID CONTROL VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BRAKE — WEAK (MLG) · airframe 13,995 hrs · 10,033 cycles

PDX - ON LANDING IN PDX, THE RIGHT BRAKE WAS VERY WEAK, HAD TO PUSH IT A LOT FURTHER TO GET ANY RESPONSE. MAINTENANCE BLED NR 3 AND NR 4 BRAKES. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: CHARGER — MALFUNCTIONED (APU) · airframe 13,640 hrs · 9,789 cycles

PDX - FLIGHT 2561 - RETURN TO THE GATE FOR A APU BATTERY CHARGER STATUS MESSAGE. MAINTENANCE REPLACED THE BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BLEED VALVE — LEAKING (NR 2 ENGINE) · airframe 13,620 hrs · 9,778 cycles

PDX - FUEL LEAKING FROM NR 2 ENGINE. MAINTENANCE REPLACED THE OBV VALVE IAW 75-31-01-000-801-A01 AND 75-31-01-400-801-A01. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (FUEL QTY) · airframe 13,461 hrs · 9,670 cycles

PDX - FLIGHT 2565 - RECEIVED A XFLOW PUMP CAUTION MESSAGE AFTER XFLOW OVERRIDE SELECTED (NO CROSS FLOW ACTIVE). RESET SYSTEM WITH NO HELP. RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL QUANTITY GAUGING COMPUTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHARGER — FAILED (APU BATTERY) · airframe 13,400 hrs · 9,625 cycles

PDX - FLIGHT 2575, ON TAXI RECEIVED A APU BATTERY CHARGER STATUS MESSAGE. RETURNED TO THE GATE. MAINTENANCE REPLACED THE APU BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSDUCER — INOPERATIVE (AOA SENSOR) · airframe 12,829 hrs · 9,219 cycles

BUR - FLIGHT 2552 - AFTER ACTIVATION OF THE PROBE HEAT SWITCHES, THE LEFT AOA HEAT CAUTION MESSAGE APPEARED AND CIRCUIT BREAKER POPPED. RESETTING THE CIRCUIT BREAKER HAD THE SAME EFFECT. RETURNED TO THE GATE. MAINTENANCE REPLACED THE AOA TRANSDUCER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DAMAGED (RUDDER) · airframe 12,540 hrs · 9,018 cycles

C3 - RUDDER RIGHT SIDE HAS WEAR MARKS ALONG LEADING EDGE, RS 40.0 - 150.0. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-55-42-001.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 12,540 hrs · 9,018 cycles

C3 - VERTICAL STAB LEFT SIDE OUTER SKIN HAS SCRATCH AT ACCESS PANEL 325EL, TOP EDGE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01 AND 51-25-01-001-001-A01.

Part: SKIN — DAMAGED (BS 980) · airframe 12,540 hrs · 9,018 cycles

YYC C3 - FUSELAGE EXTERNAL SKIN AT FS980 CENTER BELLY AFT END OF FAIRING STRAP ASSEMBLY HAS WORN A BROOVE INTO FUSELAGE SKIN. REPAIRED IAW CRJ700 SRM 51-42-20-001-001-A01, 53-00-47-000-803-A01 AND REO 670-53-51-015.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,540 hrs · 9,018 cycles

C3 - FUSELAGE EXTERNAL SKIN AFT OF AFT BAGGAGE DOOR HAS SEVERAL NICKS. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, PAGE 12, PARAGRAPH D, 51-12-00-001-001-A01 AND REO 670-53-61-301.

Part: ATTACH FITTING — CRACKED (VERTICAL STAB) · airframe 12,540 hrs · 9,018 cycles

YYC C3 - VERTICAL STAB LOWER LEFT SIDE, FUSELATE TO STAB ATTACH CHORD HAS SUSPECT CRACK IN RADIUS AFT END BELOW REAR SPAR. REPAIRED IAW REO 670-55-31-013.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,540 hrs · 9,018 cycles

C3 - FUSELAGE EXTERNAL SKIN ABOVE AFT BAGGAGE DOOR HAS MANY NICKS. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, PAGE 12, PARAGRAPH D, 51-12-00-001-001-A01 AND REO 670-53-61-301.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 12,540 hrs · 9,018 cycles

C3 - FUSELAGE EXTERNAL SKIN FORWARD OF AFT BAGGAGE DOOR HAS SEVERAL NICKS. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, PAGE 12, PARAGRAPH D, 51-12-00-001-001-A01 AND REO 670-53-61-301.

Part: DOOR FRAME — DAMAGED (BS 319) · airframe 12,540 hrs · 9,018 cycles

C3 - EXTERNAL GALLEY SERVICE DOOR SURROUND, STATION FS 319.00, TOP 3 STOP FITTINGS HAVE WEAR MARKS FROM THE DOOR. REPAIRED IAW REO 670-53-21-238.

Part: SKIN — DAMAGED (LT AILERON) · airframe 12,540 hrs · 9,018 cycles

C3 - LEFT AILERON LEADING EDGE HAS WEAR UNDER PANEL 598BT, W319, TOP SURFACE. REPAIRED IAW CRJ 700 AMM 57-52-32-000-809-A01 AND CRJ700 SRM 57-61-01-101-001-A01.

Part: SKIN — WORN (RT AILERON) · airframe 12,540 hrs · 9,018 cycles

C3 - RIGHT AILERON HAS WEAR ON TOP LEADING EDGE UNDER PANELS 698AT, 698BT AND 698CT. REPAIRED IAW CRJ700 SRM 57-61-01-101-001-A01 AND AMM 57-52-32-001-801-A01.

Part: ATTACH ANGLE — LOOSE (VERTICAL STAB) · airframe 12,540 hrs · 9,018 cycles

YYC C3 - VERTICAL STAB HAS AREA OF LOOSE RIVETS ON RIGHT SIDE, LOWER ATTACH ANGLE BELOW RUDDER. REPAIRED IAW CRJ 700 SRM 51-42-10-001-001-A01.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - RIGHT HORIZONTAL STABILIZER, EXTERIOR LOWER SKIN OUTBOARD RIB HAS 4 RIVETS PULLED WITH IMPROPER LENGTHS. REPAIRED IAW SRM 51-42-10.

Part: SKIN — DAMAGED (BS 2047) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - AFT BAGGAGE BAY DOOR SURROUND, AFT FRAME HAS LOOSE RIVETS AT FS 2047, 8" UP FROM FLOOR. REPAIRED IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - FUSELAGE INTERIOR, FS 280 FLOOR CROSS BEAM IS CORRODED ALONG THE TOP FLANGE. REPAIRED IAW SRM 51-42-21 AND 51-42-13.

Part: SEAT TRACK — CORRODED (BS 784-861) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 784.0-861.0, RIGHT OUTER SEAT RAIL HAS AREAS OF CORROSION. REPAIRED IAW REO670-53-00-013.

Part: SKIN — DENTED (TE FLAP) · airframe 12,540 hrs · 9,018 cycles

YYC C3 - LEFT INBOARD FLAP AREA BETWEEN INBOARD END AND STATION 38.00 HAS SEVERAL DENTS IN SKIN. REPAIRED IAW CRJ700 SRM 57-52-01-001-001-A01 AND 51-12-00-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 573.0-675.0, RIGHT OUTER SEAT RAIL HAS AREAS OF CORROSION. REPAIRED IAW REO670-00-013.

Part: SEAT TRACK — CORRODED (BS 573-675) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 573.0-675.0, LEFT OUTER SEAT RAIL HAS AREAS OF NICKS AND CORROSION. REPAIRED IAW REO670-53-00-013.

Part: ATTACH ANGLE — LOOSE (VERTICAL STAB) · airframe 12,540 hrs · 9,018 cycles

YYC C3 - VERTICAL STAB HAS 3 LOOSE RIVETS ON LEFT SIDE LOWER ATTACH ANGLE BELOW RUDDER. REPAIRED IAW CRJ700 SRM 51-42-10-001-001-A01, 51-21-11-001-001-A012 AND 51-25-01-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 675.0-713.0, LEFT OUTER SEAT RAIL HAS AREAS OF CORROSION. REPAIRED IAW REO670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 713.0-763.0, RIGHT OUTER SEAT RAIL HAS AREAS OF CORROSION. REPAIRED IAW REO670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 379.0 - 483.0, LEFT OUTER SEAT RAIL HAS AREAS OF NICKS AND CORROSION. REPAIRED IAW REO670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 781-861) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 781.0-861.0, LEFT OUTER SEAT RAIL HAS AREAS OF NICKS AND CORROSION. REPAIRED IAW REO670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 675-713) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 675-713.0, RIGHT OUTER SEAT RAIL HAS AREAS OF CORROSION. REPAIRED IAW REO670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS483.0 - 573.0, LEFT OUTER SEAT RAIL HAS AREAS OF NICKS AND CORROSION. REPAIRED IAW REO670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 379-483) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 379.0 - 483.0, RIGHT OUTER SEAT RAIL HAS AREAS OF CORROSION. REPAIRED IAW REO670-00-013.

Part: SEAT TRACK — CORRODED (BS 483-573) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 483.0-573.0, RIGHT OUTER SEAT RAIL HAS AREAS OF CORROSION. REPAIRED IAW REO670-53-00-013.

Part: SKIN — CHAFED (BS 1126-1162) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - FUSELAGE EXTERIOR SKIN BETWEEN FS 1126 - FS 1162 AND STRINGER 10R - 12R CHAFED BY SEALS ON PYLON AFT FAIRING. REPAIRED IAW SRM 53-61-01.

Part: SKIN — CHAFED (BS 1126-1162) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - FUSELAGE EXTERIOR SKIN BETWEEN FS 1126 AND FS 1162 AND STRINGER 10L - 12L CHAFED BY SEALS ON PYLON AFT FAIRING. REPAIRED IAW SRM 53-61-01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 FLOORBEAM IS CORRODED ALONG THE TOP FLANGE. REPAIRED IAW REO670-53-11-047, SRM 51-42-21.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 12,540 hrs · 9,018 cycles

YYC C3 - FUSELAGE INTERIOR COCKPIT FLOORBOARD SUPPORT ANGLE AT FS 280 RBLK TO LBLK IS CORRODED AT CAMLOC LOCATIONS. REPAIRED IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.

Part: FASTENER — LOOSE (LT WING) · airframe 12,540 hrs · 9,018 cycles

C3 - LEFT WING LOWER SURFACE HAS SMOKING RIVETS AT TRAILING EDGE WS147. REPLACED RIVETS IAW CRJ700 SRM 51-12-06-001-001-A01.

Part: STOP FITTING — LOOSE (CARGO DOOR) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - AFT BAGGAGE BAY DOOR, FORWARD UPPER STOP FITTING HAS LOOSE RIVETS. REPAIRED IAW SRM 51-42-10.

Part: SEAT TRACK — CORRODED (BS 713-763) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - INTERNAL FUSELAGE, FS 713.0-763.0, LEFT OUTER SEAT RAIL HAS AREAS OF CORROSION. REPAIRED IAW REO670-53-00-013.

Part: SILL — CORRODED (BS 1015) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - AFT BAGGAGE BAY DOOR SURROUND, LOWER SILL HAS CORROSION AT FS 1015. REPAIRED IAW SRM 51-21-06 AND 51-25-01.

Part: SKIN — DAMAGED (LT WING) · airframe 12,540 hrs · 9,018 cycles

C3 - LEFT WING UPPER SURFACE HAS SMOKING RIVET AT TRAILING EDGE WS 170. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: SKIN — DAMAGED (RT WING TE) · airframe 12,540 hrs · 9,018 cycles

C3 - RIGHT WING TRAILING EDGE TOP SURFACE INBOARD AND OUTBOARD OF MFS, TRAILING EDGE SURFACE HAS SEVERAL LOOSE SOLID RIVETS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: SKIN — DAMAGED (RT INTAKE) · airframe 12,540 hrs · 9,018 cycles

C3 YYC - RIGHT ENGINE INTAKE LEADING EDGE HAS ONE LOOSE RIVET INSIDE LIP OF REPAIR 11:00. REPAIRED IAW SRM 51-42-13, 54-11-05.

Part: RELAY — MALFUNCTIONED (RT ENGINE) · airframe 12,516 hrs · 9,004 cycles

PDX - ON TAXI FOR FLIGHT 2501, RECEIVED A RIGHT ENGINE DEGRADE CAUTION MESSAGE. RETURNED TO THE GATE. MAINTENANCE REPLACED THE K20 AND K22 RELAYS ON PCB 3 IN THE JB-10 REF FIM 73-21-02. GROUND ENGINE AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. RELAY PART NUMBERS M210D4N AND M220D4N

Part: DOOR — OPEN (CARGO BAY) · airframe 12,417 hrs · 8,937 cycles

BUR - FLIGHT 2554, AFTER TAKEOFF AIRCRAFT FAILED TO PRESSURIZE, NO DOOR STATUS MESSAGES RECEIVED. DIVERTED TO SMF AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND AFT BAGGAGE DOOR AJAR. INSPECTED DOOR AND AREA AND FOUND NO DEFECTS. OPERATIONAL TEST OF DOOR CHECKS GOOD IAW CRJ-700 AMM 52-31-00-710-801-A01. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BRAKE ASSY — CONTAMINATED (NR 3 & 4) · airframe 11,732 hrs · 8,466 cycles

PDX- RIGHT BRAKES ARE SPONGY DURING LANDING ROLL. BRAKE TEMPERATURE SHOWS 03 FOR THE LEFT BRAKES, 02 AND 01 FOR THE RIGHT. MAINTENANCE BLED NR 3 AND NR 4 BRAKES IAW CRJ-700 AMM TASK 32-43-00-870-801-A01. TAXI CHECKS GOOD, NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: BRAKE — MALFUNCTIONED (NR 2) · airframe 11,637 hrs · 8,393 cycles

AIRCRAFT PULLS TO THE LT ON BRAKE APPLICATION. IB BRAKE ON LT SIDE SHOWS A TEMP OF 7, AND OB BRAKE SHOWS A TEMP OF 5. MAINTENANCE REPLACED THE NR 2 BRAKE ASSEMBLY. OPERATIONAL AND TAXI CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHARGER — FAILED (MAIN BATTERY) · airframe 11,318 hrs · 8,158 cycles

SFO - ON APPLYING POWER FROM THE JETWAY, A BURNING ELECTRICAL ODOR WAS NOTICED IN THE COCKPIT AND SPU BAY WITH THE FOLLOWING FAULTS, TAT HEAT, STBY PROBE HEAT, R FADEC FAULT, L FADEC FAULT, APU BATTERY CHARGER, MAIN BATTERY CHARGER, WINDSHIELD FAIL. MAINTENANCE REPLACED THE APU BATTERY CHARGER IAW CRJ-700 AMM TASK 24-32-07-000-801-A02. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 11,194 hrs · 8,062 cycles

PDX - AFTER TAKEOFF AUTO PRESSURE CONTROLLER WENT TO MANUAL MODE AND IT WOULD NOT CONTROL THE CABIN PRESSURE. DURING DESCENT IT BEGAN TO WORK. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 2 SAFETY OUTFLOW VALVE. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 11,088 hrs · 7,992 cycles

PDX - MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE FOUND THE INNER HANDLE STICKING A LITTLE ON THE OPEN CYCLE. LUBED INNER HANDLE AND ADJUSTED THE INNER HANDLE DETENT ASSEMBLY IAW CRJ-700 AMM TASK 52-11-02-400-831-A01. OPERATIONAL CHECKS GOOD. HANDLE NO LONGER STICKS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: SOCKET — SHORTED (LAV SERVICE) · airframe 10,689 hrs · 7,725 cycles

SEA - ON FLIGHT 2299, RETURNED TO GATE, ELECTRICAL SHORT NEAR LAV SERVICE PORT AFTER SPILL OF BLUE JUICE DURING LAV SERVICE. MAINTENANCE FOUND LAV SERVICE INDICATOR SOCKET SHORTED. REMOVED TERMINAL CAPS FROM WIRES AND INSTALLED NEW SERVICE INDICATOR LIGHT IN AFT WASTE SERVICE COMPARTMENT. OPERATIONAL TEST GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — FAILED (COCKPIT) · airframe 10,548 hrs · 7,616 cycles

CAPTAIN SIDE CONSOLE FLOOD LIGHT TURNED ON SMOKE CAME FROM AREA OF LIGHT FIXTURE. SMOKE ACCOMPANIED BY ODOR OF BURNING ELECTRICAL INSULATION. SMOKE STOPPED WHEN FLOODLIGHT RHEOSTAT TURNED ALL THE WAY DOWN. INSPECTED & FOUND CAPTAINS SIDE FWD FLOOD LIGHT TO BE SOURCE OF BURNING ODOR. REMOVED LIGHT ASSY & INSPECTED SURROUNDING AREA FOR DAMAGE TO WIRING, NO DEFECTS NOTED. ISOLATED DAMAGE JUST TO SOCKET ASSY. REINSTALLED FLOOD LIGHT ASSY & DEACTIVATED FLOOD LIGHT ASSY PULLING & COLLARING U2 CB. NO FIRE OR SPARKS REPORTED. ALL INSTRUMENT FLOOD LIGHTING INOP. R & R CAPTAINS SIDE CONSOLE FLOOD LIGHT ASSY. OPS CHECK GOOD. R & R CAPTAINS LIGHTNING CONTROL PANEL. OPS CHECK GOOD. CLEARS RSI NR 355795. ACFT RTS.

Part: COMPUTER — INOPERATIVE (NR 2) · airframe 10,412 hrs · 7,516 cycles

PDX - ON FLIGHT 2505, RETURNED TO FIELD. FO'S PFD SHOWED AMBER IAS AND INDICATED AIRSPEED WAS VARING INCORRECTLY. MAINTENANCE REMOVED AND REPLACED NR 2 DADC. PERFORMED OPERATIONAL TEST OF NR 2 DADC, OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: APU — MALFUNCTIONED · airframe 10,417 hrs · 7,516 cycles

PDX - ON FLIGHT 2515, AFTER TAKEOFF, AFT LAV SMOKE WARNING. HOT ODOR IN CABIN, WENT AWAY AFTER 1.5 MINUTES. EMERGENCY DECLARED. RETURNED TO PDX, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED APU. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FADEC — MALFUNCTIONED (COCKPIT) · airframe 10,164 hrs · 7,349 cycles

PDX- ON TAXI FOR FLIGHT 2525 MOMENTARY "L ITT EXCEEDENCE C" STATUS MESSAGE FOLLOWED BY ABNORMAL ITT INDICATIONS (WITHIN GREEN RANGE) BUT MUCH HIGHER THAN NORMAL DURING TAXI. RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 ENGINE FADEC, LUBRICATED IGV BELLCRANK ASSY, INSPECTED IGV ACCTUATOR ATTACHMENT HARDWARE. BOROSCOPED ENGINE. C/W POWER ASSURANCE RUN NO DISCREPANCIES NOTED. NO ABNORMAL VISUAL SIGNS NOTED ON NR 1 ENGINE. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR — NOISY (MAIN PAX) · airframe 10,144 hrs · 7,338 cycles

DEN - ON FLIGHT 4438 HEARD A CLICKING NOISE FROM THE MAIN CABIN DOOR ON TAXI. RETURNED TO THE GATE. INSPECTED MCD INTERNAL MECHANISM. NO DEFECTS NOTED. INSPECTED EXTERNAL MCD WITH NO DEFECTS NOTED. CYCLED MCD WITH NO DEFECTS. VERIFIED MCD HAS POSITIVE LOCK WHEN CLOSED. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED.

Part: FAN — FAILED (NR 2 DISPLAY) · airframe 8,945 hrs · 6,550 cycles

DEN - ON FLIGHT 2457, AFTER TAKEOFF RECEIVED A DISPLAY COOL CAUTION MESSAGE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE FOUND THE NR 2 DISPLAY FAN FAILED. PLACED ON MEL 21-24-2, RSI 351876. AIRCRAFT RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 8,909 hrs · 6,520 cycles

DEN - ON FLIGHT 2457, AFTER STARTING FUEL BOOST PUMP TEST, A STRONG SMELL OF JET A WAS NOTICED IN THE BACK OF THE AIRCRAFT. INSPECTED AFT EQUIPMENT BAY AND FOUND A STRONG ODOR OF JET FUEL, BUT NO NOTICEABLE LEAKS. MAINTENANCE INSPECTED THE APU AND FUEL LINES IN THE AFT EQUIPMENT AREA WITH NO DEFECTS NOTED. RAN BOTH ENGINES, NO SMELLS OR LEAKS NOTED. WITH BOOST PUMPS BOTH ON AND OFF NO SMELL OR LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.

Part: TORQUE BOX — CHAFED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC - LT ENGINE UPPER AND LOWER FAN COWLS HAVE CHAFE/WEAR DAMAGE ON THE TORQUE BOX STRUCTURE. REPAIRED IAW REO 670-78-34-304 AND HORIZON AIR EA R-71-103.

Part: STRIKER — NICKED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE AT PASSENGER DOOR OPENING FORWARD BOTTOM SKIN NICKED AND PRESSURE SEAL STRIKER ROUGH IN CONTACT AREA. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01 AND HORIZON AIR EA R-53-313.

Part: ARM — GOUGED (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHTHAND WING INBOARD FLAP INBOARD HINGE ARM IS GOUGED ON OUTBOARD SIDE OF THE ATTACH LUG RADIUS. REPAIRED IAW REO 67-57-54-005, HORIZON AIR EA R-57-117, CRJ700 SRM 51-24-11-001-001-A01 AND SRM 51-21-16.

Part: ARM — GOUGED (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RT WING INBOARD FORWARD FLAP HINGE ARM AFT EDGE IS GOUGED. REPAIRED IAW REO 57-54-005, HORIZON AIR EA R-57-117 AND CRJ700 SRM 51-24-11-001-001-A01.

Part: CYLINDER — CORRODED (ZONE 700) · airframe 7,596 hrs · 5,611 cycles

YYC - CORROSION FOUND ON NOSE LANDING GEAR OUTER CYLINDER. REPAIRED IAW HORIZON AIR EA R-32-186 AND REO 670-32-21-00-13.

Part: FLANGE — CHAFED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT ENGINE LOWER TRANSCOWL FORWARD FLANGE IS CHAFING ON THE TORQUE BOX AT APPROXIMATELY 7:00 POSITION. REPAIRED IAW HORIZON AIR EA R-78-38 AND REO 670-78-33-362.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE INTERIOR LEFT FLOOR SEAT RAIL AT STATION 399.0 IS GOUGED. REPAIRED IAW REO 670-53-00-013.

Part: COWLING — CHAFED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC - LEFTHAND ENGINE TRANSLATING COWL IS CHAFING ON FORWARD COWL WHEN STOWED AT UPPER ANDL LOWER COWLS. REPAIRED IAW HORIZON AIR EA R-78-39, EA R-78-40 AND REO 670-78-33-363.

Part: STOP FITTING — WORN (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE GALLEY SERVICE DOOR STOP FITTINGS HAVE WEAR MARKS ON END AND AFT INNER FACE. REPAIRED IAW HORIZON AIR EA R-53-310 AND REO 670-53-21-098.

Part: COWLING — CHAFED (THRUST REVERSER) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT ENGINE UPPER TRANSCOWLING FORWARD FLANGE IS CHAFING ON TORQUE BOX STRUCTURE IN TWO PLACES AND 11:00 AND 1:00 O'CLOCK POSITIONS. REPAIRED IAW HORIZON AIR EA R-78-37 AND REO 670-78-33-362.

Part: STRUCTURE — CHAFED (THRUST REVERSER) · airframe 7,596 hrs · 5,611 cycles

YYC - RT ENGINE UPPER AND LOWER FAN COWLS HAVE CHAFE/WEAR DAMAGE ON THE TORQUE BOX STRUCTURE. REPAIRED IAW REO 670-78-34-364 AND HORIZON AIR EA R-71-104.

Part: BEAM — GOUGED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC - LEFT PYLON HINGE BEAM AT PYLON TIE BAR HAS GOUGES ON HINGE, TOP AND LOWER LOCATION FROM TIE BAR BRACKETS RUBBING. REPAIRED IAW CRJ700 MM 78-36-05-000-801-A01, PAGE 402, PARAGRAPH C, STEPS 1-4, REO 670-78-34-360 AND CRJ700 SRM 51-25-06-001-001-A01.

Part: COWLING — CHAFED (THRUST REVERSER) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT ENGINE, UPPER COWLING AREA, TRANSCOWL ASSEMBLY, FOUR EACH RETAINERS ARE CHAFING ON THE TORQUE BOX ASSEMBLY. REPAIRED IAW HORIZON AIR EA R-78-42 AND REO 670-78-34-361.

Part: DOOR — CHAFED (THRUST REVERSER) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT ENGINE, TRANS COWL LATCH DOOR ASSEMBLY, CHAFING ON TRANS COWL STRUCTURE AT AFT EDGE. REPAIRED IAW CRJ700 SRM 54-21-00-101-001-A01 AND SRM 51-25-01-001-001-A01.

Part: RETAINER — CHAFED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC - RT ENGINE, LOWER TRANSCOWLING HAS THREE RETAINERS THAT ARE CHAFING ON THE TORQUE BOX ASSEMBLY (4:00, 6:00 AND 8:00 O'CLOCK POSITIONS). REPAIRED IAW HORIZON AIR EA R-78-4 AND REO 670-78-34-361.

Part: SKIN — NICKED (CARGO DOOR) · airframe 7,596 hrs · 5,611 cycles

YYC - AFT BAGGAGE BAY DOOR HAS SCRATCHES AND NICKS ON TOP SURFACE OF OUTER SKIN. REPAIRED IAW CRJ700 SRM 52-31-01-101-001-A01, SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: HOUSING — GOUGED (ZONE 500) · airframe 7,596 hrs · 5,611 cycles

YYC - LT WING TRAILING EDGE OUTBOARD FLAP GUIDE ROLLER HOUSING GOUGED AT WING STATION 147.50. REPAIRED IAW CRJ700 SRM 57-51-02-201-001-A01 AND 51-24-11-001-001-A01.

Part: SKIN PANEL — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 295 TO 310 BETWEEN STRINGER 25R AND STRINGER 26L. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 53-21-01-101-002-A01, 51-12-00-001-001-A01, AND 51-25-01-001-001-A01.

Part: COWLING — WORN (THRUST REVERSER) · airframe 7,596 hrs · 5,611 cycles

YYC - LEFT ENGINE, THRUST REVERSER, TRANSLATING UPPER COWL, INBOARD "TR CLOSED" RAMPS AND STARTERS ARE WORN. REPAIRED IAW HORIZON AIR EA R-78-41, REO 670-78-34-361.

Part: SKIN — GOUGED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC-RIGHT NACELLE LIP SKIN HAS GOUGES BETWEEN 3 AND 5 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 54-11-05-101-001-A01, AND 51-21-11-001-001-A01.

Part: SKIN — DAMAGED (ZONE 500) · airframe 7,596 hrs · 5,611 cycles

YYC - LT INBOARD FLAP LOWER SKIN HAS GRAVEL DAMAGE. REPAIRED IAW HORIZON AIR EA R-57-113, REO 670-57-52-024 AND CRJ700 SRM 51-25-101-001-001-A01.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE UPPER SKIN AT STATION 300 AND STRINGER 0 HAS SCRATCHES UNDER TCAS ANTENNA. REPAIRED IAW CRJ700 SRM 51-12-00, SRM 51-21-11-001-001-A01, REO 670-53-21-099, HORIZON AIR EA R-53-314

Part: SKIN PANEL — CHAFED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL CHAFING DAMAGE BY POTABLE WATER SERVICE DOOR STATION 349 TO 364 BETWEEN STRINGER 21R AND STRINGER 24R. REPAIRED IAW HORIZON AIR EA R-53-312 AND REO 670-53-21-095.

Part: SKIN PANEL — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 349 TO 379 BETWEEN STRINGER 24R AND STRINGER 23L. REPAIRED IAW HORIZON AIR EA R-53-311 AND REO 670-53-21-097.

Part: BEAM — NICKED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT PYLON, HINGE BEAM HAS NICK 6" FORWARD OF PYLON TIE BAR NR 3 HINGE POSITION. REPAIRED IAW HORIZON AIR EA R-78-36 AND REO 670-78-34-260.

Part: SKIN — CHAFED (ZONE 500) · airframe 7,596 hrs · 5,611 cycles

YYC- LEFT INBOARD FLAP LOWER EXTERNAL SURFACE HAS CHAFE MARKS UNDER INBOARD HINGE ARM FAIRING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 57-52-01-101-001-A01, AND 51-25-01-001-001-A01.

Part: ATTACH FITTING — DAMAGED (ZONE 800) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD BAGGAGE DOOR AFT TOP LUG FOR ROLLER ATTACH TO COUNTER BALANCE HAS NICKS AND SCRATCHES. REPAIRED IAW CRJ700 SRM 52-35-06-101-001-A01, 51-12-00-001-001-A01, AND 51-25-01-001-001-A01.

Part: DOOR — WORN (RT NACELLE DOOR) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT ENGINE TRANS COWL LATCH DOOR ASSEMBLY AREA, DOOR LATCH CONTACT POINT WORN. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: SKIN — DAMAGED (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT INBOARD FLAP LOWER SKIN HAS GRAVEL DAMAGE. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: STRINGER — CHAFED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE - FORWARD BAGGAGE BAY OPENING FUSELAGE STATION 565.00 TO 533.0 EDGE OF LOWER DOOR OPENING CUTOUT CHAFED AT STRINGER 25L. REPAIRED IAW REO 670-53-31-036, HORIZON AIR EA R-53-305 AND CRJ700 SRM 51-25-01-001-001-A01.

Part: SKIN PANEL — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE, STATION 421 TO 437, BETWEEN STRINGER 26R AND STRINGER 27C AND STRINGER 23L AND 22L. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 53-21-01-101-006-A01, 51-12-00-001-001-A01, AND 51-25-01-001-001-A01.

Part: FASTENER — LOOSE (ZONE 500) · airframe 7,596 hrs · 5,611 cycles

YYC - LEFTHAND WING UPPER SKIN TRAILING EDGE, INBOARD OF INBOARD MULTI SPOILER HAS LOOSE FASTENERS. REPAIRED IAW CRJ700 SRM 51-62-06-001-001-A01.

Part: SKIN — GOUGED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC - LEFT NACELLE LIPSKIN HAS GOUGES BETWEEN 6 AND 8 O'CLOCK POSITION. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 54-11-08-101-001-A01, AND 51-21-11-001-001-A01.

Part: FITTING — CORRODED (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT OUTBOARD FLAP INBOARD ROLLER FITTING HAS FRETTING CORROSION. REPAIRED IAW REO 670-57-53-015, SRM 51-25-16-001-001-A010 AND SRM 51-24-11.

Part: HINGE — GOUGED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT PYLON HINGE BEAM AT PYLON TIE BAR HAS GOUGES ON HINGE TOP AND LOWER LOCATIONS FROM TIE BAR BRACKETS RUBBING NR 3 HINGE POSITION. REPAIRED IAW REO 670-78-34-360 AND HORIZON AIR EA R-78-36.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE INTERIOR, COCKPIT FLOOR PANEL SUPPORT ANGLE IS CORRODED. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 FLOOR SUPPORT CROSSBEAM IS CORRODED ON TOP FLANGE FROM LBL30 TO RBL30. REPAIRED IAW REO 670-53-11-047.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE EXTERIOR HAS SCRATCHES AT STATION 310 AND STRINGER 13L. REPAIRED IAW CRJ700 SRM 53-21-01-101-001-A01, SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: STRIKER — WORN (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC - LEFT HAND ENGINE, CORE COWL LOWER, BELOW OF DOOR LATCH STRIKER PLATE IS WORN. REPAIRED IAW CRJ700 SRM 51-24-16-001-001-A01, 51-42-06-001-001-A01, AND 51-42-13-001-001-A01.

Part: SKIN — DAMAGED (ZONE 400) · airframe 7,596 hrs · 5,611 cycles

YYC-RIGHT PYLON, TOP SIDE, CENTER SECTION MISSING AREA OF PAINT. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01.

Part: SKIN — TOOL DAMAGE (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE LOWER SKIN PANEL TOOLING DAMAGE TO THE LOWER SKIN AT FUSELAGE STATION 549.00 AND 565.00 BETWEEN STRINGER 24R AND 25R. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 53-31-01-101-003-A01 AND SRM 51-25-01-001-001-A01.

Part: SKIN PANEL — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, FORWARD FUSELAGE LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 319.70 TO 333 BETWEEN STRINGER 26R AND STRINGER 25R. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 53-21-01-101-002-A01, AND 51-25-01-001-001-A01.

Part: FASTENER — BROKEN (ZONE 500) · airframe 7,596 hrs · 5,611 cycles

YYC - LEFTHAND WING UPPER SKIN, TRAILING EDGE, OUTBOARD SIDE OF OUTBOARD MULTI SPOILER HAS TWO BROKEN FASTENERS. REPLACED IAW CRJ700 SRM 51-62-06-001-001-A01.

Part: SKIN — NICKED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE EXTERIOR HAS AREAS OF NICKS ABOVE AFT CARGO DOOR AT STATION 1031 ON FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA R-53-315, REO 670-53-61-166, CRJ700 SRM 51-25-01-001-001-A01 AND SRM 51-21-16-001-001-A01.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

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

Part: SKIN — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL FS 469 TO 477 BETWEEN STRINGER 24L AND 25L ROCK CHIP PITTING DAMAGE. REPAIRED IAW REO 670-53-21-094 AND HORIZON AIR EA R-53-308.

Part: SKIN — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL ROCK CHIP PITTING DAMAGE FS 437 TO 453 BETWEEN STRINGER 25R AND 25L. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 51-12-00-001-001-A01, AND 53-21-01-101-006-A01.

Part: SKIN — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE BELOW FORWARD BAGGAGE BAY OPENING AT STATION 517.00 BETWEEN STRINGER 25L AND 26L ROCK CHIP IN SKIN PANEL. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 53-31-01-101-003-A01 AND SRM 51-25-01-001-001-A01.

Part: SILL — CORRODED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - AFT BAGGAGE BAY DOOR STRUCTURE SURROUND HAS FRETTING DAMAGE ON LOWER SILL PLATE AND PAINT/PRIMMER MISSING. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, SRM 51-21-11-001-001-A01 AND SRM 51-25-01-001-001-A01.

Part: SKIN PANEL — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 394 TO 409 BETWEEN STRINGER 24R AND STRINGER 25L. REPAIRED IAW REO 670-53-21-096, AND HORIZON AIR EA R-53-309.

Part: FITTING — CORRODED (ZONE 500) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHTHAND OUTBOARD FLAP INBOARD ROLLER FITTING HAS FRETTING CORROSION. REPAIRED IAW REO 670-57-53-015 AND CRJ700 SRM 51-25-16-001-001-A01.

Part: SKIN — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE - BELOW FORWARD BAGGAGE BAY OPENING FUSELAGE STATION 549.00 TO 533.00 BETWEEN STRINGER 25L AND 25R ROCK CHIP PITTING. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, SRM 51-25-01-001-001-A01 AND SRM 53-31-01-101-003-A01.

Part: SKIN — CORRODED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, BELOW FORWARD BAGGAGE BAY OPENING FS 581 TO FS 594 BETWEEN STRINGER 27R AND STRINGER 26R ROCK CHIP PITTING IN SKIN PANEL. REPAIRED IAW CRJ700 SRM 53-31-01-101-003-A01, 51-12-00-001-001-A01, 51-25-16-001-001-A01, AND 51-25-01-001-001-A01.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

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

Part: STRUCTURE — CHAFED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - LOWER FUSELAGE IN WHEEL WELL HAS LOOSE DIAPHRAGM AT UPPER ATTACH SCREWS AND CHAFING DAMAGE. REPAIRED IAW CRJ700 SRM 51-42-001-001-A01, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.

Part: SKIN — GOUGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - LOWER FUSELAGE SKIN AT STATION 981 AND STRINGER 27 HAS TWO GOUGES. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01 AND HORIZON AIR EA R-53-307.

Part: SKIN — CORRODED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, BELOW FORWARD BAGGAGE BAY OPENING FS 565 TO FS 581, BETWEEN STRINGER 26L AND STRINGER 27L ROCK CHIP PITTING IN SKIN PANEL. REPAIRED IAW CRJ700 SRM 53-31-01-101-003-A01, 51-25-16-001-001-A01, AND 51-25-01-001-001-A01.

Part: SKIN PANEL — DAMAGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD FUSELAGE, FORWARD LOWER SKIN PANEL HAS ROCK CHIP PITTING DAMAGE AT STATION 333 TO 349 BETWEEN STRINGER 25R AND STRINGER 26R. REPAIRED IAW CRJ700 SRM 51-26-00-001-001-A01, 53-21-01-101-006-A01, 51-12-00-001-001-A01, AND 51-25-01-001-001-A01.

Part: SKIN — CHAFED (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT AILERON UPPER SKIN LEADING EDGE HAS CHAFE MARKS. REPAIRED IAW CRJ700 SRM 57-52-32-400-808-A01, 57-52-32-400-809-A01, 57-52-32-400-810-A01 AND SRM 57-52-32-400-811-A01.

Part: SKIN — CHAFED (ZONE 500) · airframe 7,596 hrs · 5,611 cycles

YYC-LEFT WING BOTTOM SKIN HAS CHAFE MARK UNDER FAIRING 586AB. REPAIRED IAW CRJ700 SRM 57-00-01-101-001-A01, 51-12-00-04-001-A01, AND 51-25-16-001-001-A01.

Part: SKIN — NICKED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE EXTERIOR SKIN AT STATION 1000, BETWEEN STRINGER 14L AND 15L HAS NICK ON SKIN. REPAIRED IAW HORIZON AIR EA R-53-306, REO 670-53-61-165 AND CRJ700 SRM 51-25-01-001-001-A01.

Part: CHANNEL — WORN (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - LOWER FUSELAGE AFT WING TO BODY FAIRING HAS CENTRAL C-CHANNEL WORN. REPAIRED IAW HORIZON AIR EA R-53-307.

Part: RETAINER — CHAFED (ZONE 800) · airframe 7,596 hrs · 5,611 cycles

YYC - FORWARD BAGGAGE DOOR BOTTOM SEAL RETAINER HAS CHAFE MARKS AT FORWARD AND AFT ENDS FROM SEAL STRIKE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, AND 51-25-01-001-001-A01.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 7,596 hrs · 5,611 cycles

YYC - PASSENGER DOOR AFT SIDE STRINGER TO DOOR PANEL ATTACH ANGLE HAS POSSIBLE CRACK AT ASSIST MOTOR. REPAIRED IAW REO 670-52-11-072.

Part: SKIN — GOUGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - AFT FUSELAGE SKIN GOUGED AT STATION 5.00 BETWEEN STRINGER 26R AND 25R. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01, 53-00-01-101-001-A01 AND CRJ700 SRM 51-25-01-001-001-A01.

Part: STRINGER — CRACKED (ZONE 800) · airframe 7,596 hrs · 5,611 cycles

YYC - PASSENGER DOOR AFT STRINGER CRACKED AT RISER AT HANDRAIL STOWAGE BRACKET. REPAIRED IAW REO 670-52-11-104.

Part: STRINGER — CRACKED (ZONE 800) · airframe 7,596 hrs · 5,611 cycles

YYC - PASSENGER DOOR FORWARD STRINGER CRACKED AT RISER AT HANDRAIL STOWING BRACKET. REPAIRED IAW REO 670-52-11-104.

Part: SKIN — NICKED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE EXTERIOR HAS NICK AT STATION 823 BELOW STINGER 15R. REPAIRED IAW HORIZON AIR EA R-53-301, REO 670-53-41-013 AND CRJ700 SRM 51-25-01-001-001-A01.

Part: STRAP — BROKEN (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - LOWER FUSELAGE AFT WING TO BODY FAIRING HAS STRAP BROKEN. REPAIRED IAW CRJ700 SRM 53-82-83-400-803-A01 AND HORIZON AIR EA R-53-307.

Part: RIVET — LOOSE (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - LOWER FUSELAGE STATION 1098 TO 1108 STRINGER 18 TO 19 RT SKIN HAS FOUR LOOSE RIVETS SMOKING. REPAIRED IAW CRJ700 SRM 51-25-01-001-001-A01, SRM 51-23-00-001-00-A01 AND SRM 51-42-06-001-001-401.

Part: PANEL — CHAFED (ZONE 500) · airframe 7,596 hrs · 5,611 cycles

YYC - LEFT WING INBOARD FLAP VANE LEADING EDGE PANEL HAS CHAFED MARK. REPAIRED IAW CRJ700 SRM 57-52-02-101-001-A01, 51-21-11-001-001-A01, AND 51-25-01-001-001-A01.

Part: SKIN — NICKED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE EXTERIOR UPPER SKIN HAS THREE NICKS AT FASTENERS BETWEEN STATION 295 TO 322 AND STRINGER 6R. REPAIRED IAW CRJ700 SRM 51-40-00-001-001-A01, REO 670-53-00-045.

Part: SKIN — NICKED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE EXTERIOR UPPER SKIN HAS NICK AT STATION 364 AND STRINGER 4R. REPAIRED IAW CRJ700 REO 670-53-00-045 AND SRM 51-25-01-001-001-A01.

Part: SKIN — NICKED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE EXTERIOR AT STATION 310 AND STRINGER 11R HAS TWO NICKS AT FASTENERS. REPAIRED IAW CRJ700 REO 670-53-00-045 AND SRM 51-25-01-001-001-A01.

Part: SKIN — CHAFED (AILERON) · airframe 7,596 hrs · 5,611 cycles

YYC - LEFT HAND AILERON UPPER SKIN LEADING EDGE HAS CHAFE MARKS. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01, 57-61-01-101-001-A01, 51-25-01-001-001-A01, AND 57-52-32-700-810-A01.

Part: RIVET — LOOSE (ZONE 300) · airframe 7,596 hrs · 5,611 cycles

YYC - VERTICAL STABILIZER, RIGHT SIDE, BOTTOM AFT SKIN HAS NINE SMOKING RIVETS. REPLACED IAW CRJ7000 SRM 51-42-13-001-001-A01.

Part: SKIN — NICKED (ZONE 800) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE GALLEY SERVICE DOOR OUTER SKIN HAS NICK BELOW CLOSE HANDLE. REPAIRED IAW CRJ700 SRM 51-12-00-001-001-A01, 53-00-01-101-001-A01,AND 51-25-01-001-001-A01.

Part: SILL — CORRODED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE GALLEY SERVICE DOOR SILL PLATE HAS SPOTS OF CORROSION ON UNDER SIDE. REPAIRED IAW CRJ700 SRM 53-21-23-101-002-A01 AND 51-25-00-001-001-A01.

Part: BRACKET — CRACKED (ZONE 800) · airframe 7,596 hrs · 5,611 cycles

YYC - PASSENGER DOOR ASSIST MOTOR MOUNT BRACKET HAS SMALL CRACK AT OUTBOARD END. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: FASTENER — LOOSE (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHTHAND WING MULTI FUNCTION SPOILER LOWER COMPOSITE SHROUD TWO FASTENERS FOUND LOOSE AT CENTER HINGE OF INBOARD SPOILER AND OUTBOARD HINGE OF OUTBOARD SPOILER. REPAIRED IAW CRJ700 SRM 51-42-13-001-001-A01.

Part: FASTENER — LOOSE (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RT WING UPPER SKIN TRAILING EDGE INBOARD OF INBOARD MULTI FUNCTION SPOILER HAS LOOSE FASTENERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: FASTENER — BROKEN (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHTHAND WING UPPER SKIN TRAILING EDGE, OUTBOARD OF OUTBOARD MULTI FUNCTION SPOILER HAS BROKEN FASTENERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE INTERIOR LEFT SIDE SEAT RAIL AT STATION 553.0 IS GOUGED. REPAIRED IAW REO 670-53-00-013.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE INTERIOR, RIGHT INBOARD SEAT TRACK AT STATION 665 HAS GOUGES ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16-001-001-A01.

Part: SKIN — NICKED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE EXTERIOR HAS NICK AT STATION 1060 AND STRINGER 13L. REPAIRED IAW CRJ700/900 SRM 53-61-01-001-002-A01 AND CRJ700 SRM 51-25-01-001-001-A01.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE INTERIOR, RIGHT INBOARD SEATRAIL AT STATION 571 HAS GOUGES ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16-001-001-A01.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE INTERIOR LEFT FLOOR SEAT RAIL AT STATION 539 IS GOUGED. REPAIRED IAW CRJ700 SRM 51-21-16-001-001-A01 AND REO 670-53-00-013.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE INTERIOR, RIGHT INBOARD SEAT RAIL AT STATION 539 HAS GOUGES ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 670-53-00-013 AND CRJ700 SRM 51-21-16-001-001-A01.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 7,596 hrs · 5,611 cycles

YYC - FUSELAGE INTERIOR, RIGHT INBOARD SEAT TRACK AT STATION 632 TO 637 HAS GOUGES ON TOP AND INSIDE SURFACES. REPAIRED IAW REO 70-53-00-013 AND CRJ700 SRM 51-21-16-001-001-A01.

Part: FLAP TRACK — GOUGED (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHT WING OUTBOARD FLAP INBOARD GUIDE ROLLER TRACK GOUGED. REPLACED IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: SKIN — GOUGED (ZONE 100) · airframe 7,596 hrs · 5,611 cycles

YYC - LOWER FUSELAGE SKIN AT FS 975 AND STRINGER 27 HAS GOUGE CAUSED BY WING/FUSELAGE FAIRING CENTRAL CHANNELS. REPAIRED IAW CRJ700 SRM 51-42-21-001-001-A01 AND SRM 51-25-16-001-001-A01.

Part: FASTENER — LOOSE (ZONE 600) · airframe 7,596 hrs · 5,611 cycles

YYC - RIGHTHAND WING UPPER SKIN, TRAILING EDGE HAS LOOSE FASTENERS BETWEEN TWO MULTI FUNCTION SPOILERS. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.

Part: SWITCH — FAILED (ZONE 700) · airframe 7,213 hrs · 5,350 cycles

SEA - FLIGHT 2467 - THE FLIGHT RETURNED TO THE GATE AFTER RECEIVING A STEERING INOP CAUTION MESSAGE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE STEERING ARMING SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SELECTOR VALVE — INOPERATIVE (ZONE 100) · airframe 6,352 hrs · 4,904 cycles

PDX - ON FLIGHT NUMBER 2507, 10 MINUTES INTO FLIGHT, RECEIVED A GEAR DISAGREE WARNING MESSAGE WHEN GEAR WAS SELECTED UP. AN EMERGENCY CHEKLIST WAS PERFORMED. EMERGENCY GEAR EXTENSION WAS PERFORMED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR SELECT VALVE. OPERATIONAL CHECK GOOD. NO DAMAGE OR DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: DCU — INOPERATIVE (ZONE 600) · airframe 4,931 hrs · 3,610 cycles

SBA - FLIGHT 2455 - AILERON TRIM MOVING RIGHT WING DOWN SIMULTANEOUSLY WITH RUDDER TRIM MOVING NOSE RIGHT, WITHOUT PILOT INPUT. ON GROUND, CANNOT MOVE AILERON TRIM TO FULL LEFT WING DOWN OR RUDDER TRIM TO FULL NOSE LEFT. AFTER SHUTDOWN AILERON TRIM CONTINUES TO MOVE AT A VERY SLOW RATE. RIGHT WING DOWN AND RUDDER TRIM CONTINUES TO MOVE AT A VERY SLOW RATE, NOSE RIGHT. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED NR 2 DCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: EXHAUST LOUVER — MISSING (ZONE 200) · airframe 4,598 hrs · 3,353 cycles

RT ACM EXHAUST LOUVER MISSING FROM EXHAUST DUCT. INSTALLED RIGHT HAND ACM EXHAUST DUCT POUVER ASSEMBLY IAW CRJ SRM 51-42-06.

Part: EJECTOR — LEAKING (FUEL TANK) · airframe 4,195 hrs · 3,076 cycles

PDX - FLIGHT 2555 - CREW NOTED THE CENTER TANK FILLING WITH FUEL. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEM AND FOUND THE LEFT PRIMARY EJECTOR BAD. THE LEFT PRIMARY EJECTOR WAS REPLACED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOTOR — FAILED (HORIZ STAB) · airframe 4,098 hrs · 3,010 cycles

TUS - FLIGHT 2571 - IN FLIGHT, THE STAB CHANNEL INOP STATUS MESSAGE APPEARED WITH RUNAWAY TRIM CLACKER. MAINTENANCE INTERROGATED THE MAINTENANCE DIAGNOSTICS COMPUTER AND FOUND THE H-STAB RESOLVER FAILED. THE HSTA MOTOR WAS THEN REPLACED, OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHIMNEY — TORN (ZONE 200) · airframe 4,009 hrs · 2,952 cycles

PDX - FORWARD CARGO COMPARTMENT CENTER CHIMNEY AND FORWARD CENTER CHIMNEY METAL MESH IS TORN. REMOVED AND REPLACED CHIMNEY.

Part: POWER SUPPLY — FAILED (ZONE 100) · airframe 3,875 hrs · 2,855 cycles

SEA - FLIGHT 2462 - THE AILERON AND RUDDER TRIM INDICATORS SHOW VERY SLOW UNCOMMANDED TRIM MOTION. MAINTENANCE REPLACED THE RUDDER/AILERON TRIM POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULKHEAD — CRACKED (AFT CARGO BAY)

LT PRESSURE BULKHEAD WEB AT FS1098, BL3441, STR8-9, FOUND TO BE CRACKED. CUT OUT DAMAGED WEB. PERFORMED AN EDDY CURRENT INSPECTION TO ENSURE ALL DAMAGE WAS REMOVED AND NO CRACKS EXIST. NO INDICATIONS FOUND. WET INSTALLED FABRICATED FITTING PN 670-53-61-026-1 AND FASTENERS. RESTORED ELECTRICAL CONTINUITY SURFACE. RESTORED BONDING SURFACE. PRESSURIZATION CHECK GOOD IAW CRJ700 AMM 21-31-00-910-801-A01. ALL WORK PERFORMED IAW MFG REO NR 670-53-61-034, DATED 2003-09-05. (EA09200601238)

Part: FASTENER — LOOSE (LT ENG NACELLE)

LT ENGINE PYLON HAS A TOTAL OF 8 LOCK FASTENERS THAT ARE LOOSE. PYLON IS SUSCEPTIBLE TO STRESS AND VIBRATION FROM THE ENGINE. REMOVE EXISTING FASTENERS AND ENLARGE THE HOLES TO A .2606 INCH - .26636 INCH IN DIAMETER. INSTALL HST111AG8XX LOCK FASTENERS INTO THE ENLARGED HOLE USING HST1488TP8 COLLARS IAW EA R-54-42 AND EO 601R-54-4444 DATED 12/03/03. (EA09200401171)

Part: FASTENER — LOOSE (RT ENG NACELLE)

RT ENGINE PYLON HAS A TOTAL OF 8 LOCK FASTENERS THAT ARE LOOSE. PYLON IS SUSCEPTIBLE TO STRESS AND VIBRATION FROM THE ENGINE. REMOVE EXISTING FASTENERS AND ENLARGE THE HOLES TO A .2606 INCH-.026636 INCH DIAMETER. INSTALL HST111AG8XX HI-LITE INTO THE ENLARGED HOLE USING HST1488TP8 COLLARS IAW EA R5442 AND EO 601R544444 DATED 12/03/03. (EA09200401173)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 3,589 hrs · 2,643 cycles

PDX- ON FLIGHT 2523 ABORTED TAKEOFF DUE TO CONFIGURATION AILERON WARNING MESSAGE DURING TAKEOFF ROLL. AILERON TRIM INDICATORS CENTERED AND GREEN. TAKEOFF CONFIGURATION OK ADVISORY MESSAGE DISPLAYED PRIOR TO TAKEOFF ROLL. TROUBLESHOOT WARNING IAW FIM 27-12-00. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — FAILED (COCKPIT) · airframe 3,536 hrs · 2,604 cycles

PDX- ON FLIGHT 2436 DISPLAY COOL CAUTION MESSAGE APPEARED AFTER TAKEOFF. COMPLIED WITH CHECKLIST SELECTION TO FLIGHT ALT FAN. MESSAGE EXTINGUISHED. REMOVED AND REPLACED COCKPIT DISPLAY FAN 1. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PITOT HEAD — OBSTRUCTED (ZONE 100) · airframe 3,409 hrs · 2,510 cycles

FLIGHT 2452 ABORTED TAKEOFF DUE TO LARGE A/S SPLIT, FIRST OFFICERS A/S INDICATED APPROXIMATELY 80 KTS, CAPTAINS INDICATED APPROXIMATLEY 50 KTS. ALSO INDICATED MASTER CAUTION WITH/EFIS COMPUTER MON AND MACH MESSAGES. FOUND OBSTRUCTION IN PILOTS PITOT TUBE. REPLACED PILOTS PITOT STATIC HEAD. PERFORMED P/S LEAK TEST OF PILOTS SYSTEM ALL TEST GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: YOKE — GOUGED (RT ENGINE) · airframe 2,808 hrs · 2,063 cycles

PDX- RIGHT HAND ENGINE YOKE HAS GOUGE ON FORWARD CENTER. REPAIRED IAW HORIZON AIR EA R-71-51 AND REO 670-71-21-004.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,802 hrs · 2,058 cycles

PDX-ON FLIGHT NUMBER 2437, CONFIG AILERON WARNING MESSAGE APPEARED. ABORTED TAKEOFF AND MESSAGE DISAPPEARED AFTER 1-2 SECONDS. MDC HAS NO REPORTS FOR AILERON TRIM SYSTEM. PERFORMED FAULT CONFIRM OF AILERON TRIM SYSTEM. OPERATIONAL TEST OF AILERON SYSTEM GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.

Part: STRINGER — DAMAGED (ZONE 200) · airframe 2,215 hrs · 1,632 cycles

PDX- DAMAGED RIVET 2 INCHES AFT OF STATION 533.00 ON STRINGER R7 ABOVE RIGHT HAND WINDOW 6. REPAIRED IAW CRJ-700 SRM 51-42-06 AND 51-25-16.

Part: RIVET — DAMAGED (ZONE 200) · airframe 2,215 hrs · 1,632 cycles

PDX- DAMAGED RIVET ON STRINGER 9R ONE INCH AFT OF FUSELAGE 409.00 ABOVE RIGHT HAND WINDOW 2. REPAIRED IAW HORIZON AIR EA R-53-106, REO 670-53-00-036, CRJ SRM 51-25-16 AND 51-12-00.

Part: LATCH — DAMAGED (RADOME) · airframe 2,215 hrs · 1,632 cycles

PDX- DAMAGED RIVET AT STATION 169.00 ON BOTTOM, ONE INCH LEFT OF LOWER RADOME LATCH .5 INCH AFT OF FRAME FRONT. REPAIRED IAW CRJ-700 SRM 51-25-16 AND 51-42-13.

Part: STRINGER — DAMAGED (ZONE 200) · airframe 2,215 hrs · 1,632 cycles

PDX- DAMAGED RIVET ON STRINGER 7 BETWEEN STATION 565.00 AND 581.00 BETWEEN RIGHT HAND WINDOWS 7 & 8. REPAIRED IAW CRJ-700 SRM 51-42-06 AND 51-25-16.

Part: RIVET — DAMAGED (ZONE 200) · airframe 2,215 hrs · 1,632 cycles

PDX-DAMAGED RIVET AT STATION 613.00 TWO INCHES BELOW STRINGER 6R ON RIGHT HAND SIDE ABOVE WINDOW 9. REPAIRED IAW CRJ-700 SRM 51-42-06 AND 51-25-16.

Part: RIVET — DAMAGED (ZONE 200) · airframe 2,215 hrs · 1,632 cycles

PDX- DAMAGED RIVET 10 INCHES AFT OF FIRST OFFICERS SIDE WINDOW ON STRINGER 11AR. REPAIRED IAW HORIZON AIR EA R-53-106 AND REO 670-53-00-036.

Part: PRESSURE SWITCH — LEAKING (ZONE 100) · airframe 1,908 hrs · 1,412 cycles

BOI - MAINTENANCE DISCOVERED A FUEL LEAK ON THE CENTER BELLY SECTION OF THE AIRCRAFT. THE NR 1 ENGINE INLET FUEL PRESSURE SWITCH WAS REMOVED AND REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — INOPERATIVE (ZONE 300) · airframe 1,637 hrs · 1,231 cycles

SEA ON FLIGHT 2516- ABORTED TAKEOFF DUE TO TAKEOFF ROLL CONFIG/AILERON WARNING AND AURAL WARNING. TAKEOFF CONFIG OKAY. ADVISORY MESSAGE WAS PRESENT. REMOVED AND REPLACED AILERON TRIM ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (ZONE 200) · airframe 1,565 hrs · 1,177 cycles

PDX ON FLIGHT 2536- APU FAULT FOLLOWED BY APU SHUTDOWN PER CHECKLIST. REMOVED AND REPLACED OIL FILTER DELTA PRESSURE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 1,542 hrs · 1,161 cycles

PDX-BOOST PUMPS CYCLING INFLIGHT. MAINTENANCE INSPECTED AND REPLACED THE ENGINE INLET PRESSURE SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BLADE — BROKEN (ZONE 400) · airframe 1,496 hrs · 1,126 cycles

PDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE BROKEN OFF. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. NVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. IT HAS BEEN CONCLUDED THAT MODIFICATION TO THE HPT 1 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: LINE — RUPTURED (ANTI-ICE SYS) · airframe 1,321 hrs · 995 cycles

SUP SEA ON FLIGHT 2461- ABORTED TAKEOFF DUE TO WING ANTI-ICE FAULT MESSAGE. FOUND A LINE RUPTURED. REMOVED AND REPLACED LINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 1,312 hrs · 990 cycles

SUP PDX ON FLIGHT 2490- INTERMITTENT FIRE SYSTEM FAULT STATUS MESSAGE. REMOVED AND REPLACED NR 3 CARGO SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (FIRE DETECTION) · airframe 1,082 hrs · 830 cycles

BIL ON FLIGHT 2481- FIRE SYSTEM FAULT STATUS MESSAGE. TESTED FIRE SYSTEM AND ALL STATUS MESSAGES CLEARED. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — FAILED (FUEL SYSTEM) · airframe 984 hrs · 752 cycles

PDX- LEFT HAND AND RIGHT HAND FUEL PUMPS ON DURING TAXI, FUEL PUMP SWITCHES CYCLED OFF AND ON. RIGHT MAIN EJECTOR CAUTION MESSAGE CAME ON. AFTER CYCLING PUMP SWITCHES SEVERAL TIMES, THE FUEL PUMPS STAYED OFF, BUT A RIGHT FUEL LOW PRESSURE CAUTION MESSAGE CAME ON AND STAYED ON. REMOVED AND REPLACED PRIMARY EJECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (AILERON) · airframe 945 hrs · 725 cycles

SEA - CREW ABORTED TAKEOFF WHEN THEY RECEIVED AN AILERON CONFIGURATION WARNING. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE AILERON TRIM ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CAGE — DAMAGED (CARGO BAY) · airframe 843 hrs · 653 cycles

PDX - THIS SDR IS BEING REPORTED PER REQUEST OF FSDO-09 ASI. FORWARD CARGO BAY CENTER CHIMNEY ASSEMBLY IS DAMAGED. MAINTENANCE REMOVED AND REPLACED CENTER CHIMNEY IN THE FORWARD CARGO BAY. OPERATIONAL CHECK AND SECURITY IS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (LT ENGINE) · airframe 250 hrs · 197 cycles

PDX- LEFT FIRE FAIL CAUTION MESSAGE ON TWICE DURING TAXI OUT. RETURNED TO GATE. TIGHTENED LOOSE CONNECTION ON LEFT HAND ENGINE B-LOOP. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.