N722EV

Part: FRAME — CORRODED (BS 1000 S20L) · airframe 42,826 hrs · 31,086 cycles

AFT BAGGAGE COMPARTMENT AT FS1000.00 STGR 20L HAS POSSIBLE CORROSION AS MARKED (C-CHECK RO 6/17/2024) REPAIRED CORROSION UNDER AFT CARGO AT APPX FS1000 & STG 20L REO 670-53-61-2265 REV -- DATE 2024-05-02. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. CHECKS GOOD. BLEND ONLY NO WEIGHT CHANGE.

Part: SKIN — ERODED (RT TE FLAP) · airframe 42,826 hrs · 31,086 cycles

EROSION NOTED ON R/H INBD FLAP LOWER SKIN BETWEEN FLS15-FLS38 (MARKED (C-CHECK RO 6/17/2024) R/H I/B FLAP LWR SKIN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01. REF CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.

Part: STAND OFF — CRACKED (LT TRANSCOWL) · airframe 42,826 hrs · 31,086 cycles

L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 6/17/2024) REMOVED CRACKED INBD "A" BRACKET STANDOFF AND INSTALLED 1 EA NEW INBD "A" BRACKET STANDOFF P/N CN624-2082-201 ON L/H UPPER TRANSCOWL REF MHIRJ GREO #670-54-21-971 REV (B) 2023-11-28 STEPS 1-3, AND CRJ 700 SRM 51-42-28-001-001-A01. COMPLIED WITH SKY CARD #51-900-1002-SKY.

Part: SKIN — SCRATCHED (BS 581-597) · airframe 42,826 hrs · 31,086 cycles

DEEP SCRATCHES AND GOUGES ON DOUBLER WHERE FWD ATG ANTENNA MOUNTS (C-CHECK RO 6/17/2024) REMOVED MINOR SCRATCHES AND GOUGES FROM EXTERNAL ( CONTACT ) SURFACE OF ATG FWD ANTENNA DOUBLER REF. CRJ700 SRM TASK 51-12-00-001-001-A01WITH NEW FABRICATED AND DRILLED FWD ATG ANTENNA EXTERNAL DOUBLER SECURED IN THE PLACE AT FUSELAGE SKIN BETWEEN FS.581.00 - FS.597.00 & STR24R & STR25R PERFORMED FIT CHECK AND FOUND STRUCTURALLY AND FUNCTIONALLY ACCEPTABLE REF. AIRCELL ATG FWD ANTENNA INSTALLATION DRAWING D12938-20110 REV. C DATED 06/20/2011 SHEET 5 FIG. 1 & 2COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 42,826 hrs · 31,086 cycles

SCRATCHES AND GOUGES ON DOUBLER WHERE AFT ATG ANTENNA MOUNTS (C-CHECK RO 6/17/2024) REMOVED MINOR SCRATCHES AND GOUGES FROM EXTERNAL ( CONTACT ) SURFACE OF ATG AFT ANTENNA DOUBLER REF. CRJ700 SRM TASK 51-12-00-001-001-A01, WET INSTALLED NEW REPLACEMENT AFT ATG ANTENNA EXTERNAL DOUBLER AT FUSELAGE SKIN BETWEEN FS.1000.00 & FS.1015.00 AND BETWEEN STR25R & STR26R WITH NEW FASTENERS PER CRJ700 SRM 51-23-00-001-001-A01 & SRM 51-42-20-001-001-A01 AND REF AIRCELL ATG ANTENNA INSTALLATION DRAWING D12942-20110 REV. B DATED 06/13/2011, COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY ALL CHECKS GOOD. SEE CONTINUATION TASKS FOR MORE DETAILS.

Part: CHANNEL — GOUGED (ANTENNA) · airframe 42,826 hrs · 31,086 cycles

INTERNAL CHANNEL FOR FWD ATG ANTENNA HAS GOUGES AROUND BOTH CONNECTOR HOLES (C-CHECK RO 6/17/2024) INTERNAL CHANNEL FOR FWD ATG ANTENNA GOUGES HAVE BEEN BLENDED EVALED OUT OF LIMITS, REPAIRED AND REINSTALLED PER CRJ 700 SRM 51-42-20-001-001-A01, EO NO: CL-600-2C10-53-L07965 REV IR DATED 05/17/2024 AND AIRCELL ILLUSTRATED PARTS CATALOG D12710-20110 REV M DATE 10/21/2014 AND COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: FLOOR SUPPORT — CORRODED (BS 985-1000) · airframe 42,826 hrs · 31,086 cycles

LH FLOOR SILL BETWEEN F.S. 1000 AND F.S. 985 HAS CORROSION (C-CHECK RO 6/17/2024) COMPLIED WITHALL STEPS OF REO 670-53-61-2263 REV-- DATED- 2024-04-30, FOR REPLACEMENT/REPAIR OF LH FLOOR SILL AT F.S. 985.00-1000.0 AND COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: HINGE FITTING — CHAFED (LT TE FLAP) · airframe 42,826 hrs · 31,086 cycles

LH WS264.00 OUTBOARD FLAP HINGE FITTING ATTACHMENT POINTS FOR ATTACHMENT BRACKET SH670-14508-1 IS CHAFED. (C-CHECK RO 6/17/2024) REPAIRED CHAFED DAMAGES ON LH WS264.00 OUTBOARD FLAP HINGE FITTING ATTACHMENT POINTS FOR ATTACHMENT BRACKET SH670-14508-1 PER REO 670-57-53-358 REV -- DATED 2024-04-30. ORIGINAL THICKNESS .150" ,REMAINING ON IB HINGE FITTING HALF .137" AND OB HINGE FITTING HALF .127", MATERIAL LOSS ON IB HINGE FITTING HALF .013" AND OB HINGE FITTING HALF .023. C/W TASK CARD 51-900-1002-SKY

Part: HINGE — GOUGED (PAX DOOR) · airframe 42,826 hrs · 31,086 cycles

PASSENGER PIANO HINGE FUSELAGE SIDE, HINGE LAND AFT OF THE 27TH LUG GOUGED. (C-CHECK RO 6/17/2024) REMOVED AND INSTALLED NEW PAX DOOR HINGE ( FUSELAGE SIDE). REF: CRJ-700 SRM 53-21-23-201-010-A01 AND REO 670-53-21-2392 REV -- DATE 2024-04-30 ALL STEPS OF REO COMPLIED WITH. ALSO COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY ALL CHECKS GOOD.

Part: INSERT — BROKEN (THRUST REVERSER) · airframe 42,826 hrs · 31,086 cycles

RH ENGINE UPPER INBOARD T/R NYLON INSERT BROKEN OFF (C-CHECK RO 6/17/2024) REMOVED RH ENGINE UPPER INBOARD T/R NYLON INSERT REF. CRJ700 AMM 78-33-05-960-801-A02,STEPS 1-4A,(1)-(5). REPAIRED ELONGATED SCREW HOLES FOR NYLON INSERT AND INSTALLED NEW RH ENGINE UPPER INBOARD T/R NYLON INSERT PER REO 670-78-30-921 REV B DATED 2014-07-02. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: FRAME — CORRODED (BS 379 S23R) · airframe 42,826 hrs · 31,086 cycles

FRAME AT FS379 STGR23R IS CORRODED (C-CHECK RO 6/17/2024) REMOVED CORROSION ON FRAME AT FS379 STGR23R. REF CRJ700 SRM 51-21-06-001-001-A01EVALUATED. ORIGINAL THICKNESS .063" MINIMUM REMAINING THICKNESS .040" TOTAL MATERIAL LOSS .023" MAXIMUM ALLOWED BLEND .006" (10%). THEREFORE IS OUT LIMITS. REF CRJ700 SRM 53-21-23-001-003-A01 & 53-21-23-101-003-A01. USED TOOL TUC10028 CAL DUE 30-NOV-24INSTALLED NEW FS 379 FRAME SECTION PN SH670-32118-3 REF CRJ 700 SRM 51-42-06-001-001-A01 ,DWG SH670-32050 REV J, DWG SH670-31401 REV A AND DWG SH670-32280 REV H.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: STRINGER — CORRODED (BS 964-979 S23R) · airframe 42,826 hrs · 31,086 cycles

STRINGER 23R BETWEEN FS364-379 HAS AREAS OF CORROSION (C-CHECK RO 6/17/2024) REPAIRED STRINGER 23R BETWEEN FS364-379 REF CRJ700 SRM 53-00-03-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. CHECKS GOOD.

Part: FRAME — CORRODED (BS 578) · airframe 42,826 hrs · 31,086 cycles

FWD SIDE OF SUB FRAME AT FS 578.0 CORRODED AT LOWER GUIDE FITTING (C-CHECK RO 6/17/2024) COMPLIED WITH MHIRJ REO 670-53-31-872 REV-- DATED 2024-04-30 IN REPAIRING OF THE LOWER GUIDE FITTING AT FWD SIDE OF SUB FRAME AT FS578.00 COMPLIED WITH TASK CARD 51-900-1002-SKYCOMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MARJOR REPAIRCOMPLIED WITH FORM M-337

Part: FRAME — CORRODED (BS 535) · airframe 42,826 hrs · 31,086 cycles

AFT SIDE OF SUB FRAME AT FS 535.0 CORRODED AT LOWER GUIDE FITTING (C-CHECK RO 6/17/2024) COMPLIED WITH MHIRJ REO 670-53-31-871 REV-- DATED 2024-05-08 IN REPAIRING OF THE LOWER GUIDE FITTING AT AFT SIDE OF SUB FRAME AT FS535.00. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: FRAME — CORRODED (BS 661 S26L/R) · airframe 42,826 hrs · 31,086 cycles

FORWARD BAGGAGE BAY - CORROSION ON FRAME LOWER FLANGE. FORWARD AND AFT WEB FS661.00 STGR26R - STGR26L. (MARKED IN RED) (C-CHECK RO 6/17/2024) BLENDED CORROSION ON FRAME LOWER FLANGE, FORWARD, AND AFT WEB AT FS661.00 STGR26R - STGR26L IAW CRJ 700 SRM 51-21-06-001-001-A01RECEIVED REO 670-53-31-876 REV --, DATED 2024-05-21 AND COMPLIED WITH ALL STEPS COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: BRACKET — CORRODED (BS 581) · airframe 42,826 hrs · 31,086 cycles

FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS581.00 STGR27 - 26L. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED WITH NEW BRACKET P/N SH670-33389-2 AT FS581.00 STGR27 - 26L. REF. CRJ 700 SRM 51-45-00-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01, DWG SH670-33600 REV AD.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCUTRAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337

Part: SKIN — CORRODED (BS 1031 S27L) · airframe 42,826 hrs · 31,086 cycles

AFT BAGGAGE BAY FS1031.00 STGR27L HAS CORROSION ON SKIN AS MARKED (C-CHECK RO 6/17/2024) REMOVED CORROSION ON AFT BAGGAGE BAY FS1031.00 STGR27L REF CRJ700 SRM 51-21-06-001-001-A01EVALUATED. ORIGINAKL THICKNESS .050" MINIMUM REMAINING THICKNESS .040" TOTAL MATERIAL LOSS .010" MAXIMUM ALLOWED BLEND .005" (10%). THEREFORE IS OUT LIMITS . REF CRJ700 SRMS 51-42-06-001-001-A01 REV 38 DATED 25JULY2020 AND CRJ 700 SRM 51-42-21-001-001-A01 REV 38 DATED 25JULY2020 . REO 670-53-61-2271, REV --, 2024-05-17REPAIRED REF REO 670-53-61-2271, REV --, 2024-05-17. ALL STEPS (1-12) HAVE BEEN COMPLIEDLEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: BRACKET — CORRODED (BS 533 S27) · airframe 42,826 hrs · 31,086 cycles

FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS533.00 STGR27. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED FORWARD BAGGAGE BAY BRACKET FS533.00 STGR27 (PN SH670-33389-1) PER CRJ700 SRMS 51-42-21-001-001-A01, 51-42-22-001-001-A01 AND DWG NO. SH670-33600 REV AD. COMPLIED WITH AL STEPS OF TASK CARD 51-900-1002-SKY

Part: STOP FITTING — CORRODED (SERVICE DOOR) · airframe 42,826 hrs · 31,086 cycles

GALLEY SERVICE DOOR HAS CORROSION AT THE LOWER DOOR STOP FITTINGS AND SILL AS MARKED (C-CHECK RO 6/17/2024) REPLACED LOWER SILL PN# SH670-31996-39 ON GALLEY SERVICE DOOR SURROUND . REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG NO: SH670-31950 REV Y. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: FRAME — CORRODED (BS 645 S26L/R) · airframe 42,826 hrs · 31,086 cycles

FORWARD BAGGAGE BAY - CORROSION ON FRAME WEB AND LOWER FLANGE FS645.00 STGR26R - STGR26L. (MARKED IN RED) (C-CHECK RO 6/17/2024) BLENDED CORROSION ON FRAME WEB AND LOWER FLANGE AT FS645.00 STGR26R - STGR26L IAW CRJ 700 SRM 51-21-06-001-001-A01 RECEIVED REO 670-53-31-876 REV --, DATED 2024-05-21 AND COMPLIED WITH ALL STEPS. AND COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY ALL CHECKS GOOD

Part: BRACKET — CORRODED (BS 581 S22-23L) · airframe 42,826 hrs · 31,086 cycles

FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS581.00 STGR22L - 23L. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND INSTALLED NEW BRACKET P/N SH670-33390-2 REF. CRJ 700 SRM 51-45-00-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01, AND 51-42-28-001-001-A01 AND DWG SH670-33600 REV AD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: BRACKET — CORRODED (BS 533) · airframe 42,826 hrs · 31,086 cycles

FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS533.00 STGR22L 23L. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED MACHINED BRACKET IN FWD CARGO, F.S. 533 STGR 22-23L, WITH NEW, REF CRJ 700 SRM 51-42-20-001-001-A01 REVISION 38: JUL 25/2020, CRJ 700 SRM 51-42-13-001-001-A01 REVISION 38: JUL 25/2020, CRJ 700 SRM 51-42-06-001-001-A01 REVISION 38: JUL 25/2020 & DWG NO. SH670-33600 REV AD. LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR REPAIR & COMPLIED WITH SKYWEST FORM M-337

Part: BRACKET — CORRODED (BS 549-565) · airframe 42,826 hrs · 31,086 cycles

FORWARD BAGGAGE BAY - CORROSION ON BRACKET FS549.00 - FS565.00 STGR25R - 24R. (MARKED IN RED) (C-CHECK RO 6/17/2024) REMOVED AND REPLACED BRACKET BETWEEN F.S. 549 AND F.S. 565 STGR 25R-24R WITH NEW, PN SH670-33852-1, REF CRJ 700 SRM 51-42-06-001-001-A01,51-42-21-001-001-A01 , 51-42-15-001-001-A01 AND DWG # SH670-33600 REV AD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY, COMPLIED WITH SKYWEST FORM M-337

Part: PLATE — CORRODED (FWD CARGO DOOR) · airframe 42,826 hrs · 31,086 cycles

FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE AFT JOINT PLATE IS CORRODED FS581.00 STGR25L. MARKED IN RED. (C-CHECK RO 6/17/2024) REMOVED CORROSION AT FORWARD BAGGAGE BAY DOOR AFTER JOINT PLATE REF. CRJ-700 SRM 51-21-06-001-001-A01ORIGINAL THICKNESS IS .080 REF. DWG SH670-33793 REV. A. REMAINING THICKNESS IS .076". MATERIAL LOSS OF .004" IS OUT OF LIMITS DUE TO NO DAMAGE ALLOWED REF. CRJ 700 SRM 53-31-23-101-001-A01. ENGINEERING SUPPORT REQUIREDRECEIVED REO 670-53-31-873, REV --, 2024-05-08. COMPLIED WITH ALL STEPS OF REO AND REPAIRED AS REQUIRED

Part: FLOORBEAM — CRACKED (BS 280 LBL9) · airframe 42,826 hrs · 31,086 cycles

FS280.00 CROSSBEAM ANGLE CRACKED AT LBL9 AS MARKED (C-CHECK RO 6/17/2024) REMOVED CRACKED CROSSBEAM ANGLE AT FS280.00 LBL9 AND INSTALLED NEW CROSSBEAM ANGLE FS280.00 AT LBL9. REF CRJ700 SRM 51-42-21-001-001-A01 & DWG CC670-34099 REV -- AND COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 42,826 hrs · 31,086 cycles

COCKPIT FLOOR SUPPORT ANGLE AT F.S 280.00 IS HEAVILY CORRODED ON TOP. (C-CHECK RO 6/17/2024) REMOVED CORRODED COCKPIT FLOOR SUPPORT ANGLE AT FS280.00 AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE AT FS280.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01 & DWG. CC670-34010 REV -K. AND COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: ANGLE — CRACKED (BS 1098) · airframe 42,826 hrs · 31,086 cycles

AFT EQUIPMENT COMPARTMENT - FS1098.20 STGR24R INBOARD CLIP IS CRACKED. (MARKED) (C-CHECK RO 6/17/2024) REMOVED FROM FS1098.20 STGR24R CRACKED INBOARD CLIP REF.CRJ-700 SRM 51-42-06-001-001-A01 INSTALLED NEW CLIP REF.CRJ-700 DRAWING MM670-35012 REV. G AND REF. CRJ-700 SRM 53-61-23-001-002-A01 , REF. CR-700 SRM 51-42-06-001-001-A01 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: FITTING — SCRATCHED (RT MLG) · airframe 42,826 hrs · 31,086 cycles

DURING AUDIT OF 1C TASK CARD 32-740-101, (DETAILED INSPECTION OF THE RIGHT MAIN LANDING GEAR (MLG) ATTACHMENT POINTS), FOUND THE SIDE STAY FITTING HAS SEVERAL SCRATCHES ON FACE, O/B SIDE. (C-CHECK RO 6/17/2024) BLENDED AND MEASURED 3 EA BLEND SCRATCHES ON RH MLG SIDE STAY FITTING. INBD BLEND MEASURES L 1.023" X W 0.100 X D 0.003" MID BLEND MEASURES L 1.540" X W 0.054" X D 0.002" OTBD BLEND MEASURES L 1.325" X W 0.0060" X D 0.003". CAPTURED CALIBRATED TOOLING TUC 6721 DUE DATE 31-AUG-2024 TUC10028 DUE DATE 30-NOV-2024. REWORKED CONDITION STRUCTURALLY ACCEPTABLE. REF REO 670-57-11-207 REV-- DATED 2024-05-20. SEE CONTINUATION FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY BLEND REPAIR ONLY. NO WEIGHT CHANGE.

Part: STAND OFF — CRACKED (LT TRANSCOWL) · airframe 42,826 hrs · 31,086 cycles

L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) REMOVED AND REPLACED INBD STAND-OFF P/N CN624-2082-201 ON L/H LOWER TRANSCOWL REF. REO 670-54-21-971 REV. B, 2023-11-28 AND CRJ 700 SRM 51-42-28-001-001-A01. COMPLIED WITH SKY CARD 51-900-1002-SKY.

Part: STAND OFF — CRACKED (RT TRANSCOWL) · airframe 42,826 hrs · 31,086 cycles

R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) INSTALLED 1 EA. NEW STANDOFF P/N CN624-2082-201 ON R/H UPPER TRANS COWL (OTBD.). REF. MHIRJ REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3. COMPLIED WITH MAJOR REPAIR (M337) AND 51-900-1002 SKY.

Part: STAND OFF — CRACKED (RT TRANSCOWL) · airframe 42,826 hrs · 31,086 cycles

R/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) INSTALLED 1 EA. NEW STANDOFF P/N CN624-2082-201 ON R/H UPPER TRANS COWL (OTBD.). REF. MHIRJ REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3. COMPLIED WITH MAJOR REPAIR (M337), AND 51-900-1002 SKY.

Part: STAND OFF — CRACKED (RT TRANSCOWL) · airframe 42,826 hrs · 31,086 cycles

R/H LWR TRANSCOWL INBD " A " BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH M-337 & SKYCARD 51-900-1002-SKY.

Part: STAND OFF — CRACKED (RT TRANSCOWL) · airframe 42,826 hrs · 31,086 cycles

R/H LWR TRANSCOWL OTBD A BRACKET STANDOFF IS CRACKED (C-CHECK RO 6/17/2024) REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-1128. COMPLIED WITH M-337 & SKYCARD 51-900-1002-SKY.

Part: SLIDER — GOUGED (THRUST REVERSER) · airframe 42,826 hrs · 31,086 cycles

R/H UPPER TRANSCOWL INBD SLIDER IS GOUGED (C-CHECK RO 6/17/2024) COMPLIED WITH REO 670-54-21-1631, REV. --, 2024-05-02 ALL STEPS FOR REPAIR TO R/H UPPER TRANSCOWL INBD SLIDER. COMPLIED WITH MAJOR REPAIR FORM 337. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SKIN — GOUGED (RT AILERON) · airframe 42,826 hrs · 31,086 cycles

RIGHT WING AILERON UPPER SKIN LEADING EDGE GOUGED AT APPROXIMATELY WS339.00 AS MARKED (C-CHECK RO 6/17/2024) BLENDED GOUGE DAMAGE ON RH WING AILERON UPPER LEADING EDGE AT WS339.00 IAW CRJ700 SRM 51-12-00-001-001-A01 FOUND OUT OF LIMITS PER CRJ 700 SRM 57-61-01-101-001-A01. AND PERFORMED REPAIRS PER REO 670-57-61-194 REV -C DATE 2019-01-07. ALL STEPS OF REO COMPLIED WITH.

Part: SKIN — DENTED (LT TE FLAP) · airframe 42,826 hrs · 31,086 cycles

LH INBD FLAP LOWER SKIN HAS A CLUSTER OF SMALL DENTS ON INBD SIDE (C-CHECK RO 6/17/2024) L/H I/B FLAP LOWER SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.

Part: SKIN — GOUGED (LT SLAT) · airframe 42,826 hrs · 31,086 cycles

LH INBD SLAT UNDERSIDE GOUGED AT APPROX LOC. WS128 TRAILING EDGE (C-CHECK RO 6/17/2024) REPAIRED GOUGE AT UNDERSIDE OF THE LH INBD SLAT AT APROX WS128 TRAILING EDGE REF MHIRJ REO 670-57-42-909 REV B DATED 2024-04-24. COMPLIED WITH TASK CARD 51-900-1002-SKY AND M-337

Part: PANEL — CORRODED (PAX DOOR) · airframe 42,826 hrs · 31,086 cycles

PAX DOOR PANEL 832DR HAS CORROSION AROUND FASTENER HOLES. (MX-TRANS #28049752) (C-CHECK RO 6/17/2024) ORIGINAL MATERIAL THICKNESS 0.05" AS PER CRJ700 SRM 52-11-32-001-001-A01. DAMAGES MUST BE AT MINIMUM 1.5 D FROM ANY FASTENER, OUT OF LIMITS AS PER CRJ700 SRM 52-11-32-101-001-A01. RECEIVED LOCATED AND DRILLED NEW ACCESS PANEL 832DR. REF CRJ-700 SRM 51-40-11-001-001-A01.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 42,826 hrs · 31,086 cycles

TRANSFER FROM EAML 1061692 : TRANSFERRED FROM CAMP 25898012. COCKPIT FLOOR BEAM RBL12, SUSPECT CRACK IN RADIUS OF THE AFT VERTICAL FLANGE WHERE IT ATTACHES TO THE FWD SIDE FS280 BEAM/WEB. (C-CHECK RO 6/17/2024) REPAIRED CRACKED RBL 12 COCKPIT FLOOR BEAM TO CRJ 700 SRM 53-11-43--201-003-A01 REPAIR TYPE 4, SPLICING IN NEWBEAM SECTION, COMPLIED WITH SKYWESTTASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR, COMPLIED WITHSKYWEST FORM M-337

Part: NOT REPORTED — DAMAGED (NOT REPORTED) · airframe 42,826 hrs · 31,086 cycles

DAMAGE DETERMINED TO BE OUTSIDE SRM LIMITS, DETERMINED TO BE MAJOR REPAIR. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: NOT REPORTED — DAMAGED · airframe 44,694 hrs · 32,601 cycles

DAMAGE DETERMINED TO BE OUTSIDE SRM LIMITS, DETERMINED TO BE MAJOR REPAIR. (FILED CLOSED)TRANSFERRED TO AML 1061696 FOR FERRY FLIGHT.

Part: SKIN — DENTED (BS 1031 S22R) · airframe 42,824 hrs · 31,085 cycles

FUSELAGE SKIN DENTED AT BS 1031.00, S22R JUST AFT OF LP AIR GROUND AIR CONNECTION DOOR. OPEN

Part: SKIN — DENTED (BS 1031 S22R) · airframe 42,826 hrs · 31,086 cycles

FUSELAGE SKIN DINGS AT FS 1031.00, STGR22RH JUST AFT OF LP AIR GROUND AIR CONNECTION DOOR REPAIR OF FUSELAGE SKIN AT FS 1031.00, STGR22RH JUST AFT OF LP AIR GROUND AIR CONNECTION DOOR DONE IN REFERENCE TO REO 670-53-61-2108 REV:- DATE; 2023-01-01

Part: ENGINE — ODOR (RT) · airframe 39,431 hrs · 28,600 cycles

AT 200€™ ON CLIMB OUT RECEIVED SMOKE AFT LAV WARNING MESSAGE, FOLLOWED BY AFT FLIGHT ATTENDANT EMERGENCY CALL CONFIRMING LIGHT SMOKE FROM THE LAV. RETURNED TO FIELD WHILE COMPLYING WITH QRH PROCEDURE OF OPENING APPLICABLE CIRCUIT BREAKERS. UPON LANDING FLIGHT ATTENDANTS CONFIRMED SMOKE HAD DISSIPATED. (FLIGHT 3228 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22765896 WITH THE FOLLOWING CORRECTIVE ACTION: "RAN LT AND RT ENGINES WITH THEIR OWN BLEED SOURCE INDEPENDENTLY OF EACH OTHER. CONFIRMED SMOKE SOURCE AS RT ENGINE BLEED ONLY. WHEN AIR CONDITIONING PACKS RAN FROM ANY OTHER BLEED SOURCE THAN RT ENGINE, NO SMOKE OR SMELL DETECTED. SEE CHILD DISCREPANCIES FOR FURTHER ACTION."

Part: SEAT TRACK — MALFUNCTIONED (CABIN) · airframe 38,232 hrs · 27,681 cycles

MOST AFT (LH INBD) SEAT TRACK REQUIRES REPLACEMENT DUE TO SEAT 17AB NOT LOCKING DOWN PROPERLY. REMOVED AND REPLACED AFT (LH INBD) SEAT TRACK WITH NEWLY FABRICATED ONE REF CRJ700 AMM

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 38,232 hrs · 27,681 cycles

CABIN FLOOR BOARD PANEL 241CLF IS CRACKED. FLOORBOARD 241CLF INSTALLED ON JOB 71012790 OP 7015 CAMP 21083713

Part: ANGLE — CRACKED (HANDLE HOUSING) · airframe 38,232 hrs · 27,681 cycles

CRACK FOUND ON PASSENGER DOOR INNER HANDLE HOUSING ASSY INNER ANGLE P/N# 601R318072-1. (C-CHECK) RO 7/23/2020 REMOVED, DRILLED,LOCATED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INNER HANDLE HOUSING ASSY INNER ANGLE REF CRJ700 SRM.

Part: ANGLE — DAMAGED (BS 349) · airframe 38,232 hrs · 27,681 cycles

IN THE AVIONICS BAY, BELOW FLOORBOARD, FOUND A CLIP WITH AN EXISTING ELONGATED HOLE, AT FS349.0 COMMON TO STR27L (C-CHECK) RO 7/23/2020 REMOVED AND REPLACED CLIP FS349 COMMON TO STR 27L REF CRJ 700 SRM AND DWG. COMPLIED WITH SKY CARD.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CRACK FOUND ON PASSENGER DOOR INTERCOSTAL DD7 P/N# 601R318825-1. (C-CHECK) RO 7/23/2020 REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD7 REF MHIRJ DRAWING AND CRJ700 SRM . COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 38,232 hrs · 27,681 cycles

INBOARD SEAT RAIL AT LBL9 IS CORRODED BETWEEN FS581 & FS677. REMOVED CORROSION ON FABRICATED LBL9 SEAT TRACK FROM FS581 TO FS677 REF CRJ 700 SRM LBL9 SEAT TRACK FROM FS581 TO FS677 FOUND TO BE OUT OF LIMITS IAW SRM.

Part: SUPPORT — CORRODED (WNG-BDY FAIRING) · airframe 38,232 hrs · 27,681 cycles

AFT WING-TO-BODY SUPPORT STRUCTURE- STRAP LOCATED AT LBL 17.63 BETWEEN FS879 AND FS909 IS CORRODED. REMOVED AND INSTALLED 1EA NEW LBL 17.63 STAP BETWEEN F.S. 879 AND 909 AND RESTORED FINISH IAW SRM.

Part: SUPPORT — CORRODED (WNG-BDY FAIRING) · airframe 38,232 hrs · 27,681 cycles

AFT WING-TO-BODY SUPPORT STRUCTURE- STRAP LOCATED AT RBL 17.63 BETWEEN FS879 AND FS909 IS CORRODED (C-CHECK) RO 7/23/2020 REMOVED AND INSTALLED NEW WING TO BODY SUPPORT STRAP LOCATED AT RBL 17.63 BETWEEN FS879 AND FS909 AND RESTORED FINISH IAW CRJ700 SRM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 38,232 hrs · 27,681 cycles

*COCKPIT FLOORBOARD SUPPORT ANGLE JUST FORWARD OF FS280 AND APPROX. BETWEEN LBL12 TO RBL12 HAS CORROSION. (C-CHECK) RO 7/23/2020 REMOVED AND REPLACED COCKPIT FLOORBOARD SUPPORT ANGLE JUST FWD OF FS280 APPROX. BETWEEN LBL12 TO RBL12 DWG CRJ700 SRM AND CRJ700 SRM. SEE CONTINUATION CARD FOR WORK DETAILS.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 38,232 hrs · 27,681 cycles

COCKPIT FLOORBEAM, RBL12, AT FS280: CRACKED IN THE VERTICAL RADIUS ON THE FORWARD SIDE OF THE FS 280 ATTACH FLANGE. NDT VERIFIED NO DEFECT NOTED IN REFERENCE TO THE SUSPECTED CRACK IN THE VERTICAL RADIUS ON THE FORWARD SIDE OF THE FS280 ATTACH FLANGE. SEE CONTINUATION FOR DETAILS.

Part: ANGLE — CORRODED (BS 319) · airframe 38,232 hrs · 27,681 cycles

CLIP COMMON TO FRAME 319.70 AND STRG20R IS CORRODED. REMOVED AND REPLACED CORRODED CLIP WITH NEW CLIP COMMON TO FRAME 319.70 AND STR 20RH REF DWG AND CRJ 700 SRM. COMPLIED WITH SKYWEST TASK CARD.

Part: ANGLE — CORRODED (BS 349) · airframe 38,232 hrs · 27,681 cycles

CLIP COMMON TO FRAME 349 AND STRG20R IS CORRODED (C-CHECK) RO 7/23/2020 CLIP COMMON TO FRAME 349 AND STRG20R WAS FOUND TO BE OUT OF LIMITS OF CRJ700 SRM, REPLACED CLIP IAW DWG & CRJ700 SRM. COMPLIED WITH SKYWEST TASK CARD.

Part: SUPPORT — CORRODED (WNG-BDY FAIRING) · airframe 38,232 hrs · 27,681 cycles

*AFT WING-TO-BODY SUPPORT STRUCTURE AT LEFT AND RIGHT CENTER STRAPS AT FS879 HAVE CORROSION/FRETTING. (C-CHECK) RO 7/23/2020 REMOVED AND INSTALLED 2EA NEW RBL36 AND LBL36 STAPS AT F.S. 879, AND RESTORED FINISH IAW CRJ700 SRM.

Part: STRINGER — CORRODED (BS 349) · airframe 38,232 hrs · 27,681 cycles

STRG27 HAS CORROSION JUST AFT OF FS349. REMOVED AND REPLACED STR27 JUST AFT OF FS349 TO FS364 REF SRM AND DWG. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (BS 319-349) · airframe 38,232 hrs · 27,681 cycles

INTERCOSTAL AT STRG20R BETWEEN FS 319.70 AND FS 349.00 IS CORRODED (C-CHECK) RO 7/23/2020 REPLACED INTERCOSTAL AT STRG20R BETWEEN FS319.70 & FS349.00 IAW DWG, CRJ700 SRM.

Part: SUPPORT — CORRODED (WNG-BDY FAIRING) · airframe 38,232 hrs · 27,681 cycles

AFT WING-TO-BODY SUPPORT STRUCTURE €“ MID ANGLE AT FS847 HAS CORROSION. REMOVED CORROSION FRM AFT WING TO BODY SUPPORT STRUCTURE-MID ANGLE AT FS847. REF CRJ 700 SRM. PART OUT OF LIMITS. REF CRJ 700 SRM. REMOVED AND REPLACE PART WITH A NEW PART. REF CRJ 700 SRM.

Part: SUPPORT — CORRODED (WNG-BDY FAIRING) · airframe 38,232 hrs · 27,681 cycles

AFT WING-TO-BODY SUPPORT STRUCTURE €“ CENTER FAIRING ATTACH ANGLE AT FS939 HAS CORROSION. BLENDED OUT CORROSION ON THE CENTER FAIRING ATTACH ANGEL AT FS939, AFT WING TO BODY SUPPORT STRUCTURE. REF CRJ 700 SRM. BLEND OUT OF LIMITS. REMOVED AND REPLACED AFT WING TO BODY SUPPORT STRUCTURE, CENTER FAIRING ATTACH ANGLE. REF CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS

Part: FIREWALL — CHAFED (APU BAY) · airframe 38,232 hrs · 27,681 cycles

*APU FIREWALL, AFT FACE HAS A CHAFE (MARKED). (C-CHECK) RO 7/23/2020 REPAIRED APU FIREWALL, AFT FACE IAW CRJ700 SRM.

Part: SUPPORT — CORRODED (WNG-BDY FAIRING) · airframe 38,232 hrs · 27,681 cycles

*AFT WING-TO-BODY SUPPORT STRUCTURE €“ MID STRAP AT FS909 HAS CORROSION. REPLACED CORRODED AFT WING-TO-BODY SUPPORT STRUCTURE MID STRAP AT FS909 WITH NEW STRAP (P/N: SH670-39338-3) REF CRJ-700 SRM, SEE CONTINUATION CARD FOR DETAILS.

Part: RETAINER — BENT (BS 379) · airframe 38,232 hrs · 27,681 cycles

*RH SEAT SIDE TRACK TRIM RETAINER FWD OF FS379.00 IS BENT (MARKED (C-CHECK) RO 7/23/2020 R/H SIDE SEAT TRACK TRIM RETAINER FWD OF FS379 FOUND TO BE OUT OF LIMITS REF CRJ SRM SEE CONTINUATION CARD FOR DETAILS

Part: DOOR FRAME — DAMAGED (PAX DOORWAY) · airframe 38,232 hrs · 27,681 cycles

PAX DOOR LOWER PORTION OF DOOR SURROUND.IS DAMAGED. PAX DOOR LOWER FWD DOOR SURROUND STRUCTURE STRIKER IS DENTED AND GOUGED, NO DENTS ALLOWED IN THIS AREA, OUT OF LIMITS OF CRJ700 SRM. COMPLIED WITH ALL STEPS OF REO.

Part: SEAT TRACK — CORRODED (BS 724-736) · airframe 38,232 hrs · 27,681 cycles

*RH SEAT SIDE TRACK FWD OF FS724.00, AFT OF FS736.05 CORRODED. REMOVED CORROSION ON R/H SIDE SEAT TRACK AT FS713.00 TO FS761.85 REF CRJ 700 SRM R/H SIDE SEAT TRACK AT FS713.00 TO FS761.85 FOUND TO BE OUT OF LIMITS REF CRJ 700 SRM SEE CONTINUATION FOR DETAILS

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 38,232 hrs · 27,681 cycles

* FLOOR SILL R/H SIDE FROM FS280 TO FS 319.70 HAS AREAS OF CORROSION. (C-CHECK) RO 7/23/2020 REMOVED AND INSTALLED NEW RH FLOOR SILL FROM APPROX. F.S 280 TO F.S 319.70 REF. DRAWING. AND CRJ-700 SRM. COMPLIED WITH TASK CARD. LEAK CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 879-953) · airframe 38,232 hrs · 27,681 cycles

*RH SEAT SIDE TRACK FWD OF FS879.00 €“ FWD OF FS953.00 HEAVY CORROSION PITTING ALL OVER THE ENTIRE SEGMENT. RH SEAT SIDE TRACK FWD OF FS879.00 €“ FWD OF FS953.00 INSTALLED REF CRJ 700 AMM

Part: SEAT TRACK — CORRODED (BS 797) · airframe 38,232 hrs · 27,681 cycles

RH SEAT SIDE TRACK AFT OF FS797.00 CORRODED. SEAT SIDE TRACK AFT OF FS797.00 TO FS 855.00 IAW SRM.

Part: SEAT TRACK — CORRODED (BS 863-953) · airframe 38,232 hrs · 27,681 cycles

*LH SEAT SIDE TRACK AFT OF FS863.00 €“ AFT OF FS953.00 HEAVY CORROSION PITTING ALL OVER THE ENTIRE SEGMENT. REMOVED CORROSION ON L/H SIDE SEAT TRACK AT FS868.5 TO FS960.5 REF CRJ 700 SRM L/H SIDE SEAT TRACK AT FS868.5 TO FS960.5 FOUND TO BE OUT OF LIMITS REF CRJ 700 SRM SEE CONTINUATION FOR DETAILS

Part: SEAT TRACK — CORRODED (BS 677-708) · airframe 38,232 hrs · 27,681 cycles

LH SEAT SIDE TRACK FWD OF BS 677 AND AFT OF BS 708 CORRODED IN SEVERAL AREAS. SEAT TRACK FWD REPLACED IAW AMM

Part: SEAT TRACK — CORRODED (BS 533-565) · airframe 38,232 hrs · 27,681 cycles

*RH SEAT SIDE TRACK FS533.00 €“ FS565.00 CORRODED IN SEVERAL AREAS. RH SEAT SIDE TRACK FS533.00 €“ FS565.00 REMOVWD AND INSTALLED WITH NEW. REF CRJ 700 SRM

Part: SEAT TRACK — CORRODED (BS 708) · airframe 38,232 hrs · 27,681 cycles

*RH SEAT SIDE TRACK FWD AND AFT OF FS708.00 IS CORRODED IN SEVERAL AREAS. RH SEAT SIDE TRACK FWD AND AFT OF FS708.00 REPLACED WITH NEW REF CRJ 700 AMM

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 38,232 hrs · 27,681 cycles

AFT CARGO ENTRY FLOOR SILL HAS AREAS OF CORROSION. REMOVED AND INSTALLED NEW CARGO FLOOR SILL REF SRM DWG. LEAK AND OPS CHECK ARE GOOD. SEE CONTINUATION FOR DETAILS. COMPLIED WITH TASK CARD.

Part: DOOR FRAME — DAMAGED (PAX DOORWAY) · airframe 38,232 hrs · 27,681 cycles

PAX DOOR AFT SURROUND STRUCTURE HAS DAMAGE. PAX DOOR UPPER AFT SURROUND STRUCTURE STRIKER IS DENTED AND GOUGED, NO DENTS ALLOWEDIN THIS AREA, OUT OF LIMITS OF CRJ700 SRM. COMPLIED WITH ALL STEPS OF REO.

Part: SEAT TRACK — CORRODED (BS 847) · airframe 38,232 hrs · 27,681 cycles

* INTERNAL FUSELAGE RBL 9.0 FLOOR SEAT RAIL HAS EVIDENCE OF CORROSION FROM FS 847.0 AFT . REMOVED CORROSION FROM SEAT RAIL FROM FS855.4 TO FS977.00 AT RBL 9 REF CRJ 700 SRM SEAT RAIL FROM FS855.4 TO FS977.00 AT RBL 9 OUT OF LIMITS REF CRJ 700 SRM SEE CONTINUATION CARD FOR DETAILS AND JOB 71012795 OP 98 MXTRANS 21152191 FOR FABRICATION

Part: SEAT TRACK — CORRODED (BS 645) · airframe 38,232 hrs · 27,681 cycles

*LH SEAT SIDE TRACK AFT OF FS645.00 CORRODED. REMOVED CORROSION ON L/H SIDE SEAT TRACK AT FS581 TO FS677 REF CRJ 700 SRM L/H SIDE SEAT TRACK AT FS581 TO FS677 FOUND TO BE OUT OF LIMITS REF CRJ 700 SRM 53 SEE CONTINUATION FOR DETAILS

Part: SEAT TRACK — CORRODED (BS 549) · airframe 38,232 hrs · 27,681 cycles

*LH SEAT SIDE TRACK AT FS549.00 CORRODED. LH SEAT SIDE TRACK AT FS549.00 INSTALLED REF CRJ 700 SRM

Part: SEAT TRACK — CORRODED (BS 797) · airframe 38,232 hrs · 27,681 cycles

*LH SEAT SIDE TRACK FWD OF FS797.00 CORRODED. THE SEAT TRACK FWD OF FS797.00 INSTALLED REF CRJ 700 SRM

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 38,232 hrs · 27,681 cycles

AVIONICS BAY IN BETWEEN FS 349.0 AND FS 364.0 BELOW FLOOR BOARD INTERCOSTAL AT 27R HAS AREAS OF CORROSION. REMOVED AND REPLACED INTERCOSTAL AT STRG27R BETWEEN FS349 AND FS364 REF CRJ-700 SRM AND DRAWING. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD.

Part: ATTACH BRACKET — CORRODED (DOOR WINDOW) · airframe 38,232 hrs · 27,681 cycles

* THE GALLEY SERVICE DOOR LOWER ATTACHING BRACKET FOR THE WINDOW HAS CORROSION. FABRICATED REPLACEMENT GALLEY SERVICE DOOR WINDOW LOWER ATTATCH ANGLE PN CC670-38154-7 FREM S6144-14 2024-T3 0.063 P>O> T000051022/13 REF. DRAWING. INSTALLED GALLEY SERVICE DOOR WINDOW LOWER ATTATCH BRACKET REF. CRJ700 SRM.

Part: HAND RAIL — CHAFED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

*PAX DOOR AFT LWR HAND RAIL POST IS CHAFFED. REMOVED AND INSTALLED A NEW SERVICEABLE PAX DOOR AFT LOWER HAND RAIL POST REF CRJ 700 AMM. PERFORMED OPERATIONAL TEST OF THE PAX DOOR REF CRJ 700 AMM OPS TEST GOOD. SEE CONTINUATION FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (BS 379-469) · airframe 38,232 hrs · 27,681 cycles

*RH SEAT SIDE TRACK AFT OF FS379.00 TO FS469.00 CORRODED IN SEVERAL AREAS (MARKED) (C-CHECK) RO 7/23/2020 REMOVED CORROSION ON R/H SIDE SEAT TRACK FROM FS379 TO FS469 REF CRJ 700 SRM R/H SIDE SEAT TRACK FROM FS379 TO FS469 FOUND TO BE OUT OF LIIMITS REF CRJ 700 SRM SEE CONTINUATION CARD FOR DETAILS

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 38,232 hrs · 27,681 cycles

AVIONICS BAY , BELOW FLOORBOARD IN BETWEEN FS 349.0 TO 364.0 AT STR27L INTERCOSTAL HAS AREAS OF CORROSION. REMOVED AND INSTALLED NEW AVIONICS BAY INTERCOSTAL AT APPROX. F.S 349 TO F.S 364 AT STGR 27L REF. DWG AND CRJ-700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: SHAFT — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

*PAX DOOR UPPER LOCK HOUSING INBRD SHAFT ASSY HAS 2EA CORRODED TAPER PIN NUTS. REMOVED AND REPLACED 2 NUTS, 2 WASHERS AND 2 COTTER PINS ON PAX DOOR UPPER LOCK HOUSING INBD SHAFT TAPER PINS REF SRM. TQ WRENCH TUC6228 CAL DUE: 28-FEB-21

Part: HOUSING — CHAFED (DOOR HANDLE) · airframe 38,232 hrs · 27,681 cycles

*PAX DOOR INNER HANDLE SHAFT HOUSING ASSY CHAFFED BY THE ICE BREAK CABLE. PASSENGER DOOR INNER HANDLE HOUSING ASSY TOP SKIN HAS SEVERAL AREA WITH SEVERE CORROSION AND 1 EA PREVIOUSLY BLEND GOUGED IN CUT OUT AREA. NO DAMAGE ALLOWED ON CUT OUT AREA. OUT OF LIMITS REF CRJ700 SRM. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INNER HANDLE ASSY TOP SKIN REF CRJ700 SRM.

Part: WHEEL — CRACKED (PAX DOOR SUPPORT) · airframe 38,232 hrs · 27,681 cycles

*PAX DOOR SUPPORT WHEEL CRACKED (MARKED) (C-CHECK) RO 7/23/2020 REMOVED AND REPLACED PAX DOOR SUPPORT WHEEL PN: 601R38371-13 REF AMM

Part: FORMER — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION FOUND ON PASSENGER DOOR AFT FORMER FS347.25 P/N# 601R318034-3. (C-CHECK) RO 7/23/2020 WHILE REMOVING CORROSION FOUND CRACK ON PASSENGER DOOR AFT FORMER FS347.25 AT POWER ASSIST MOTOR PULLEY BRACKET AREA. OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR AFT FORMER AT FS347.25 REF MHIRJ DRAWING, CRJ700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD. .

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION FOUND ON PASSENGER DOOR INTERCOSTAL DD3 P/N# 601R318056-1. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 40 % OF LENGTH OF THE PART . OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD3 REF DRAWING, SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CRACK FOUND ON PASSENGER DOOR INTERCOSTAL DD7 P/N# 601R318826-1 (C-CHECK) RO 7/23/2020 REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD7 P/N# 601R318826-1 REF MHIRJ DRAWING AND CRJ700 SRM. COMPLIED WITH TASK CARD.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

PASSENGER DOOR HINGE ON DOOR SIDE HAS ELONGATED HOLES AND GOUGES. PASSENGER DOOR HINGE DOOR SIDE FWD HOLE HAS A INSIDE DIAMETER OF 0.300" MAXIMUM ALLOWED IS 0.295" . OUT OF LIMITS REF REO.. USED TUC8562 CAL DUE DATE 31-OCT-20 REPLACED HINGE. COMPLIED WITH ALL STEPS OF CRJ700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: PCU — CORRODED (LT WING SPOILER) · airframe 38,232 hrs · 27,681 cycles

* THE LH OUTBOARD MULTI-FUNCTION SPOILER PCU'S ANTI-MIGRATION PLATE ATTACH BOLT HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED 1 EA LH OUTBOARD MULTI-FUNCTIONAL SPOILER PCU ANTI MIGRATION PLATE BOLT, 1 NUT, AND 2 WASHERS REF AMM. NO OTHER DISCONNECTIONS PERFORMED. NO OPS TESTS REQUIRED

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CRACK FOUND ON PASSENGER DOOR PULL IN CAM DOUBLER P/N# 601R318094-1. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR PULL IN CAM DOUBLER REF SRM.

Part: FORMER — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION FOUND ON PASSENGER DOOR FORMER FS329.41 BETWEEN DD5 AND DD6 P/N# 601R318078-3. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR FORMER AT FS329.41 BETWEEN DD5 AND DD6 REF DRAWING AND SRM . COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CRACK FOUND ON PASSENGER DOOR INTERCOSTAL DD1 P/N# 601R31902-318. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD1 REF MHIRJ DRAWING AND CRJ700 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION FOUND ON PASSENGER DOOR INTERCOSTAL P/N# 601R31902-317 COMMON TO DD4. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 40 % OF LENGTH OF THE PART . OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL P/N# 601R31902-317 COMMON TO DD4 REF MHIRJ DRAWING AND SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION FOUND ON PASSENGER DOOR INTERCOSTAL DD6 P/N# 601R318057-1. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD6 REF DRAWING, SRM. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION FOUND ON PASSENGER DOOR INTERCOSTAL DD4 P/N# 601R318081-1. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD4 REF DRAWING, CRJ700 SRM. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION FOUND ON PASSENGER DOOR INTERCOSTAL DD2 P/N# 601R318053-3. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 40 % OF LENGTH OF THE PART . OUT OF LIMITS REF CRJ200 SRM AND REO.REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD2 REF DRAWING, COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: STOP FITTING — BROKEN (FWD CARGO DOOR) · airframe 38,232 hrs · 27,681 cycles

FWD CARGO DOOR, FWD AND AFT OTBD DOOR STOP BOLTS DEFORMED AND SAFETIES BROKEN FROM REPEATED IMPACTS (C-CHECK) RO 7/23/2020 REMOVED AND REPLACED WITH NEW FWD AND AFT OTBD DOOR STOP BOLTS ON FWD BAGGAGE DOOR REF. CRJ700 AMM. TOOL ID TUC4238 CAL DUE 31-MAY-21

Part: FORMER — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION FOUND ON PASSENGER DOOR FORMER AT FS311.75 P/N# 601R318031-3. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR FWD FORMER FS311.75 REF CRJ700 SRM AND DRAWING. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: HINGE — NICKED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

THE PASSENGER DOOR HINGE HALF, FUSELAGE SIDE, HAS NICKS, SCRATCHES AND GOUGES IN LUG LANDS #8 THROUGH #27. (NUMBERED FROM FWD POSITION 1, TO AFT POSITION 27) COMPLIED WITH ALL STEPS OF TYPE IV. REF REO SEE CONTINUE CARD FOR DETAILS. COMPLETED SKYWEST SKYCARD ATTACHED. ALL BLENDS WITHIN LIMITS.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION FOUND ON PASSENGER DOOR CLEAT COMMON TO DD5 P/N# 600-31902-269. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR CLEAT AT DD5 REF CRJ700 SRM.

Part: WEB — CORRODED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

CORROSION ON PASSENGER DOOR FWD WEB. CORROSION IS PRESENT ON MULTIPLE ELEMENTS AND COVERS MORE THAN 50% OF THE LENGTH OF PART OUT OF LIMITS REF CRJ200 SRM AND REO. REMOVED AND INSTALLED SERVICEABLE PASSENGER DOOR FWD WEB DRAG ANGLE, EXISTING DOUBLERS, GAS SPREING MOUNT BRACKET AND HANDRAIL CUP REF CRJ700 SRM.

Part: STRUCTURE — DAMAGED (LT NACELLE) · airframe 38,232 hrs · 27,681 cycles

2EA LH PYLON UPPER LOCK FASTENER HOLES, LOCATIONS 5 AND 7 COUNTING FROM FWD TO AFT, WERE FOUND OVERSIZED AND WITH DEFECTS UPON INCORPORATION OF SB 670BA-54-007 (MARKED) (C-CHECK) RO 7/23/2020 REPAIRED LH PYLON OVERSIZED AND DEFECTIVE HOLES REF. MHIRJ REO. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD.

Part: SKIN — DENTED (RUDDER TE) · airframe 38,232 hrs · 27,681 cycles

* THE RUDDER'S TRAILING EDGE IS DENTED. REPAIRED RUDDER TRAILING EDGE DENT TO REF MHIRJ REO.

Part: HINGE — CRACKED (PAX DOOR) · airframe 38,232 hrs · 27,681 cycles

PASSENGER DOOR AFT HINGE COVER ON FUSELAGE SIDE IS CRACK. REMOVED AND REPLACED WITH NEW PN# 601R31895-12PP, PASSENGER DOOR AFT HINGE COVER FAIRING REF CRJ700 AMM PRESSURE CHECKS GOOD

Part: DOUBLER — CHAFED (BS 969) · airframe 38,232 hrs · 27,681 cycles

APPROX. F.S 969 LOWER FUSELAGE DOUBLER HAS TWO CHAFES AT STGR 27. PERFORMED DOUBLER REPAIR AT APPROX. F.S 969 STRINGER 27 REF. REO . COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: STRUCTURE — CHAFED (FUSELAGE) · airframe 38,232 hrs · 27,681 cycles

* THE CENTER WING FRONT SPAR'S LOWER ANGLE IS CHAFED ON ITS UPPER SURFACE AT BL0.00. BLENDED CENTER WING FRONT SPAR REF MHIRJ REO. WITHIN LIMITS.

Part: SKIN — GOUGED (RT AILERON) · airframe 38,232 hrs · 27,681 cycles

RH AILERON UPPER SURFACE LEADING EDGE GOUGED. (C-CHECK) RO 7/23/2020 REMOVED DAMAGE TO R/H AILERON UPPER SURFACE LEADING EDGE, PART IS OUT OF LIMITS PER BOMBARDIER REO. REPLACED R/H AILERON UPPLER SURFACE LEADING EDGE WITH NEW REF CRJ 700 SRM AND BOMBARDIER DWG. SEE CONTINUATION FOR DETAILS.

Part: SKIN — WORN (LT NACELLE) · airframe 38,232 hrs · 27,681 cycles

LEFT ENGINE UPPER TRANS COWL HAS COWL SLIDER WEAR AND RIDGES WORN. (C-CHECK) RO 7/23/2020 REPAIRED LEFT SIDE ENGINE UPPER TRANS COWL SLIDER REF MHI REO AND REO. . SEE CONTINUATION FOR DETAILS.

Part: SUPPORT FITTING — DAMAGED (LT WING FLAP) · airframe 38,232 hrs · 27,681 cycles

L/H INBOARD FLAP INBOARD SUPPORT FITTING HAS VISIBLE TOOLING MARK. (C-CHECK) RO 7/23/2020 REMOVED DAMAGE ON THE L/H INBOARD FLAP INBOARD SUPPORT FITTING REF CRJ700 SRM. REPAIRED FITTING REF MHI RJ REO. COMPLETED SKYWEST ST ATTACHED. SEE CONTINUATION FOR DETAILS.

Part: ATTACH BRACKET — CRACKED (CARGO DOOR TRACK) · airframe 38,232 hrs · 27,681 cycles

* AFT CARGO DOOR, AFT TRACK LOWER ATTACH BRACKET IS CRACKED. MARKED. INSTALLED NEW BRACKET ASSY COMMON TO LINTEL PN MM670-35699-029. REF CRJ700 SRM.

Part: WEB — CRACKED (BS 939) · airframe 38,232 hrs · 27,681 cycles

WEB AT FS939.00 - LOWER/AFT BOTTOM CORNER IS CRACKED. AFT FAIRING ATTACHMENT. CRACK IS VERIFIED TO BE ON WEB AT FS909.00 LOWER/AFT BOTTOM CORNER. COMPLIED WITH ALL STEPS (1-13) IN THE BOMBARDIER REO SEE CONTINUE CARD FOR DETAILS

Part: SLAT TRACK — WORN (RT WING) · airframe 38,232 hrs · 27,681 cycles

R/H SIDE LEADING EDGE SLAT DRIVEN TRACK 1-1 HAS WEAR MARKS ON OUTER SECTION OF TRACK.(MARKED) (C-CHECK) RO 7/23/2020 REPAIRED RH SIDE LEADING EDGE SLAT DRIVE TRACK 1-1 PER MHIRJ REO. ALL CHECKS AND RIGS ARE GOOD AT THIS TIME.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 38,232 hrs · 27,681 cycles

* R/H SIDE EXTERNAL FUSELAGE ARE VARIOUS SMALL SCRATCHES JUST AFT AND BELOW A/C SERVICE CONNECTION FS 1031.0 (C-CHECK) RO 7/23/2020 BLENDED VARIOUS SCRATCHES ON RH SIDE EXTERNAL FUSELAGE SKIN JUST AFT AND BELOW A/C CONNECTION AT FS 1031.0. REF CRJ 700 SRM. WITHIN LIMITS REF MHI RJ REO. COMPLETED SKYWEST ST CARD ATTACHED. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DENTED (BS 265) · airframe 38,232 hrs · 27,681 cycles

DENT ON FUSELAGE SKIN FWD OF FS 265.00 BETWEEN STGR 24R - 25R (C-CHECK) RO 7/23/2020 REPAIRED FUSELAGE SKIN DENT FWD OF F.S 265 BETWEEN STGR 24R - 25R REF. MHIRJ REO. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD.

Part: BEARING — DAMAGED (LT AILERON) · airframe 38,232 hrs · 27,681 cycles

ROUTE LT AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBD, MID, OUTBD) ON LH AILERON PER AMM (C-CHECK) RO 7/23/2020 REMOVED AND REPLACED WORN BUSHINGS AND BEARINGS REF,CRJ 700 AMM FOR BEARINGS AND REO FOR BUSHINGS

Part: SKIN — DENTED (BS 985-1000) · airframe 38,232 hrs · 27,681 cycles

RH SIDE FUSELAGE BETWEEN FS 985 AND FS1000 IN BETWEEN STGR12 AND 13 HAS A SCRATCH/GOUGE MEASURING 6 IN X 1.3 IN AND A MAX DEPTH OF .007 IN. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-61-1475 REV A. PERMANENT REPAIR DUE WITHIN 6700 FH FROM ORIGINAL ISSUE OF REO (AT TAT 34592.5). DUE BY TAT: 41292.5., PART NUMBER: - , SERIAL NUMBER: 10127, POSITION: (C-CHECK) RO 7/23/2020 REPAIRED RH FUSELAGE DENT DAMAGE AREA BETWEEN F.S 985 TO F.S 1000 BETWEEN STRINGERS 12R AND 13R REF. REO.

Part: CONTROL PANEL — FAILED (TRIM SYSTEM) · airframe 35,682 hrs · 25,642 cycles

EXPERIENCED FULL LEFT RUDDER DEFLECTION DURING DESCENT. RUDDER TRIM FOUND TO BE ALMOST FULL NL POSITION. RESET RUDDER TRIM TO CENTER AND LANDED WITH NO FURTHER ISSUES. (FLT#3290) CLOSED REMOVED AND REPLACED RUDDER TRIM/AILERON TRIM PANEL. PERFORMED OP CHECK OF RUDDER TRIM SYSTEM RUDDER TRIM OP CHECKS GOOD IAW AMM.

Part: VANE — CHAFED (TE FLAP) · 24,690 cycles

LT INBOARD FLAP VANE MIDDLE LEADING EDGE PANEL HAS CHAFE DAMAGE. (C-CHECK) 07/08/2018 REPAIRED LT INBOARD FLAP VANE, MIDDLE LEADING EDGE IAW REO.

Part: VANE — CHAFED (TE FLAP) · 24,690 cycles

RT INBOARD FLAP VANE MIDDLE LEADING EDGE PANEL HAS CHAFE DAMAGE. (C-CHECK) 07/08/2018 REPAIRED RT INBOARD FLAP VANE, MIDDLE LEADING EDGE CAP IAW REO.

Part: NOT REPORTED — DENTED (FUSELAGE) · 24,690 cycles

THERE IS A DENT ABOVE FWD POT WATER DOOR CUTOUT. (C-CHECK) 07/08/2018 REPAIRED DENT ABOVE FWD POT WATER DOOR CUTOUT IAW REO.

Part: NOT REPORTED — DENTED (FUSELAGE) · 24,690 cycles

THERE IS A DENT BELOW THE PAX DOOR CUTOUT. (C-CHECK) 07/08/2018 REPAIRED DENT BELOW THE PAX DOOR CUTOUT IAW REO.

Part: CONNECTOR — NOT SEATED (SMOKE DETECTOR) · airframe 33,796 hrs · 24,142 cycles

PILOT REPORTED THAT DURING ARROACH AT 4000FT, RECEIVED A SMOKE MASTER WARNING FOR THE AFT LAVATORY. STAYED ON EVEN AFTER LANDING, COMPLIED WITH QRH. RESET THE CONNECTOR AND PERFORMED AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

STG 26L CORRODED 363.00. REMOVED AND REPLACED CORRODED STG 26L BTW FRAMES 363.00 IAW SRM 51-42-06-001-001-A01. ALL DEFECTS CORRECTED. P/N-SH670-31372-3 DRAWING SH670-31372-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

CRAWLWAY FLOOR SUPPORT ANGLE CORRODED AT FS 280.00. REMOVED AND REPLACED FLOOR SUPPORT ANGLE FS 280.00 PER SRM 51-40-11-001-001-A01. P/N-CC670-35256-3 DRAWING CC670-35256.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

INSIDE AVIONICS BAY BULKHEAD AT FS 235.00 HAS (1) EA FASTENER CORRODED AND POSSIBLE STRUCTURE AROUND FASTENER CORRODED AT RBL3, APPOX 6"HIGH FROM LOWER SKIN. COMPLIED WITH EC/TC REO 670-53-11-1307 AND REO 670-53-11-1307.

Part: STRINGER SPLICE — CORRODED (BS 238-338) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

STRINGER SPLICE 25R CORRODED BS 328 - 338. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-06-001-001-A01 AND DRAWING SH670-32429.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

FRAME 310 CORRODED FWD SIDE BTW STGRS 25L-25R. REPAIRED FRAME AT 310 FWD SIDE BTW STGRS 25L-25R IAW EC/TC REO 670-53-21-799 01 AND REO 670-53-21-799 01.

Part: STRINGER — CORRODED (BS 363) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

STRINGER 26R CORRODED AT BS 363. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

CRAWLWAY FLOOR SUPPORT ANGLE CORRODED AT FS 280.00. REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT FS 280.00 PER SRM 51-40-11-001-001-A01. P/N-CC670-35256-3 DRAWING CC670-3525.

Part: FRAME — CORRODED (BS 295) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

FRAME BS 295 CORRODED FWD & AFT SIDES BETWEEN STRINGERS 24R - 25L. COMPLIED WITH EC/TC REO 670-53-21-799, AND REO 670-53-21-799 .

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

FRAME 364 CORRODED FWD & AFT SIDES BTW STGRS 25R-25L. COMPLIED WITH EC/TC REO 670-53-21-687 AND REO 670-53-21-687.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

FRAME BS 333 CORRODED FWD & AFT SIDES BETWEEN STRINGERS 24R - 25L. COMPLIED WITH EC/TC REO 670-53-21-799-03, AND REO 670-53-21-799-03.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

STR 26R SPLICE JOINT SEGMENT CORRODED BTW FS 328-338. REMOVED AND REPLACED STR SPLICE SEGMENT PER SRM 51-42-06-001-001-A01 AND 51-25-00-001-001 A01 P/N-SH670-32429-4 DRAWING SH670-32429

Part: HANDLE — CHAFED (SERVICE DOOR) · airframe 33,199 hrs · 23,679 cycles

SERVICE DOOR OUTER HANDLE HOUSING CHAFED AT THE FWD UPPER CORNER. REMOVED AND REPLACED HANDLE ASSEMBLY IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, DRAWINGS CC670-38171, AND CC670-38255.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

PAX DOOR ICE BREAKER DOOR CUTOUT INTERCOSTALS CORRODED. REPAIRED THE INTERCOSTALS IAW EC/TC EA 43-2017-128 &129, AND EA 43-2017-128-29,

Part: WIRE — MELTED (LT IDG) · airframe 33,199 hrs · 23,679 cycles

LEFT ENGINE IDG SHRINK WRAP MELTED. REPAIRED THE LT IDG CABLE IAW EC/TC REO 670-24-21-001 AND REO 670-24-21-001.

Part: FRAME — CORRODED (BS 319.7) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

FRAME BS 319.7 CORRODED FWD SIDE BETWEEN STINGERS 25L-25R. REPAIRED THE FRAME IAW EC/TC REO 670-53-21-799-02, AND REO 670-53-21-799-02.

Part: SKIN — CORRODED (BS 364-394) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

MAIN AVIONICS DOOR SURROUND HAS CORRISION.. REMOVED AND REPLACED IAW MODSUM IS67053210097, EC/TC REO 670-53-21-242, AND REO 670-53-21-242.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · corrosion level 2 · airframe 33,199 hrs · 23,679 cycles

CORRODED FLOOR SUPPORT BETWEEN BS 349 - 364, RBL 2. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 33,199 hrs · 23,679 cycles

CORRODED FLOOR SUPPORT BETWEEN BS 349 - 364, LBL 2. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, AND 51-40-11-001-001-A01

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 33,199 hrs · 23,679 cycles

RT CABIN FLOOR SILL CORRODED AT FS 282.00 RBL 42. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390.

Part: FRAME — CORRODED (FUSELAGE) · airframe 33,199 hrs · 23,679 cycles

FRAME 349 FWD & AFT SIDES CORRODED BTW STR 24R-25L. REMOVED AND REPLACED FRAME 349.00 IAW SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01 AND DRAWING SH670-31357.

Part: SEAT TRACK — CORRODED (BS 581 & 613) · airframe 33,199 hrs · 23,679 cycles

LEFT SIDE SEAT TRACK CORRODED AT BS 581 AND 613. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17, EC/TC REO 670-53-00-343, AND REO 670-53-00-343.

Part: FLOOR SUPPORT — CORRODED (BS 394-409) · airframe 33,199 hrs · 23,679 cycles

CORRODED FLOOR SUPPORT BETWEEN BS 394 & 409, LBL 2. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 394-409) · airframe 33,199 hrs · 23,679 cycles

CORRODED FLOOR SUPPORT BETWEEN FRAMES BS 394 & 409, RBL 2. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.

Part: STRINGER — CORRODED (BS 339-349) · airframe 33,199 hrs · 23,679 cycles

STRINGER 25R CORRODED BS 339 - 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 736.05) · airframe 33,199 hrs · 23,679 cycles

RIGHT SIDE SEAT TRACK WAS CORRODED AT BS 736.05. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, ECTC REO 670-53-00-343, REO 670-53-00-343, AND AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (BS 785-853) · airframe 33,199 hrs · 23,679 cycles

LEFT SIDE SEAT TRACK BS 785.15 - 853 CORRODED AND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, ECTC REO 670-53-00-343, REO 670-53-00-343, AND AMM 53-00-49-400-801-A17.

Part: STRINGER — CORRODED (BS 280-328) · airframe 33,199 hrs · 23,679 cycles

STRINGER 25R CORRODED AT SEVERAL AREAS BETWEEN BS 280 - 328. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 785-853) · airframe 33,199 hrs · 23,679 cycles

RIGHT SIDE SEAT TRACK FROM BS 785.15 - 853 IS CORRODED AND OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A17, ECTC REO 670-53-00-343, REO 670-53-00-343, AMM 53-00-49-400-801-A17.

Part: STRINGER — CORRODED (BS 280-300) · airframe 33,199 hrs · 23,679 cycles

STRINGER 27, BS 280 - 300 CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, AND DRAWING SH670-31642.

Part: SEAT TRACK — CORRODED (BS 581-613) · airframe 33,199 hrs · 23,679 cycles

LEFT SIDE SEAT TRACK SEGMENT IS CORRODED AT BS 581 AND 613. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17, EC/TC REO 670-53-00-343, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,199 hrs · 23,679 cycles

SEAT RAIL SEGMENT FROM F.S. 581-682 RBL9 IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 581-682 RBL9 IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17 AND EC/TC REO 670-53-00-343 AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 675-712) · airframe 33,199 hrs · 23,679 cycles

RIGHT SIDE SEAT TRACK SEGMENT FROM BS 675 - 712 IS CORRODED AND OUT OF LIMITS. REMOVED THE SEAT IAW AMM 53-00-49-000-801-A17. FABRICATED A NEW SEAT TRACK IAW ECTC REO 670-53-00-343, AND REO 670-53-00-343. INSTALLED THE NEW SEAT TRACK IAW AMM 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (BS 549) · airframe 33,199 hrs · 23,679 cycles

LEFT SIDE SEAT TRACK SEGMENT IS CORRODED BS 549. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17, EC/TC REO 670-53-00-343, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 693-708) · airframe 33,199 hrs · 23,679 cycles

SEAT TRACK SEGMENT RBL9 IS CORROSION AT BS 693 AND 708. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17, EC/TC REO 670-53-00-343, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 33,199 hrs · 23,679 cycles

SEAT TRACK FROM BS 349 - 485, RBL 9 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17, EC/TC REO 670-53-00-343, AND REO 670-53-00-343.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 33,199 hrs · 23,679 cycles

TCAS INTERNAL SKIN CORRODED, STRINGER 27 BETWEEN BS 295 - 310. REMOVED AND REPLACED TCAS DOUBLERS I/A/W CRJ 700 SRM 51-42-06-001-001-A01. P/N SH670-32364-7 DRAWING # SH670-32364..

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,199 hrs · 23,679 cycles

SEAT RAIL SEGMENT FROM F.S. 581-682 RBL9 IS CORRODED. REMOVED AND REPLACED SEAT TRACK AT FS 581-682 RBL9 IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17 AND EC/TC REO 670-53-00-343 AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 33,199 hrs · 23,679 cycles

SEAT TRACK SEGMENT FROM BS 485-581, LBL 9 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17, EC/TC REO 670-53-00-343, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 517 & 549) · airframe 33,199 hrs · 23,679 cycles

RT SIDE SEAT TRACK CORRODED AT BS 517 AND 549. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17, EC/TC REO 670-53-00-343, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (BS 581 & 613) · airframe 33,199 hrs · 23,679 cycles

RIGHT SIDE SEAT TRACK CORRODED AT BS 613 AND 581. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, 53-00-49-400-801 A17, EC/TC REO 670-53-00-343, AND REO 670-53-00-343.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,199 hrs · 23,679 cycles

FLOOR SEAT TRACK SEGMENT FROM FS 485-581 ON RBL9 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801 A03. FABRICATED SEAT TRACK BY COMPLYING WITH EC/TC REO 670-53-00-343 AND BOMBARDIER REO 670-53-343 REV M AND INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801 A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,199 hrs · 23,679 cycles

FLOOR SEAT TRACK SEGMENT FROM FS 830.40-987 ON LBL9 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801 A03. FABRICATED SEAT TRACK BY COMPLYING WITH EC/TC REO 670-53-00-343 AND REO 670-53-343 REV M AND INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801 A03.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,776 hrs · 23,361 cycles

NOTICED PLASTIC BURNING ODOR ON ARRIVAL. MX OPENED AND INSPECTED CEILING PANELS AND PCU'S IN CABIN. NO FAULTS FOUND. ACFT OK FOR SERVICE.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 32,572 hrs · 23,206 cycles

PATCH REPAIR REQUIRED DUE TO SKIN DAMAGE. COMPLIED WITH EC/TC REO 670-53-61-1359 FS 1051 STRINGER 18R.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 32,575 hrs · 23,207 cycles

DURING C CHECK SKIN DAMAGE AT FS 1051 AND STR 18R REQUIRED A PATCH REPAIR. SKIN PANEL REPAIRED IAW EC/TC REO 670-53-61-1359.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,572 hrs · 23,206 cycles

DURING C CHECK THE FLOORBEAM AT LBL9 FS 1031 WAS CORRODED. REMOVED CORROSION ON AND FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM IAW SRM 53-00-41-201-001-A01 AND EO700-53-10-00050.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,572 hrs · 23,206 cycles

CORRODED FLOORBEAM LBL 27 FS 1031. REMOVED CORROSION ON FLOORBEAM FS 1031.0 LBL 27, FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM FS 977.0 AND 1037.0 LBL 27 REF SRM 53-00-41-201-001-A01, EO 700-53-10-00051 SRM 51-21-06-001-A01 AND 53-61-43-101-001-A01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,572 hrs · 23,206 cycles

CORRODED FLOORBEAM NEAR FS 1031.0 LBL 9. REMOVED CORROSION ON FLOORBEAM FS 1031.0 LBL 9, FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM FS 977.0 AND 1037.0 LBL 27 REF SRM 53-00-41-201-001-A01, EO 700-53-10-00050 SRM 51-21-06-001-A01 AND 53-61-43-101-001-A01.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 32,572 hrs · 23,206 cycles

DURING C CHECK, THE FLOORBEAM AT RBL 9 BS 1031 WAS CORRODED. REMOVED CORROSION ON AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM IAW SRM 53-00-41-201-001-A01, AND EO700-53-10-00049.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,572 hrs · 23,206 cycles

DURING C CHECK THE FLOORBEAM AT LBL27 FS 1031 WAS CORRODED. REMOVED CORROSION ON AND FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM IAW SRM 53-00-41-201-001-A01 AND EO700-53-10-00051.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,270 hrs · 21,390 cycles

12 CD LOWER EXIT SIGN HAVE 1 LIGHT BULB BURNED OUT. R & R THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,270 hrs · 21,390 cycles

MAIN ENTRANCE EXIT SIGN BELOW FLASHLIGHT HAS 1 LIGHT BULB BURNED OUT. R & R BURNED OUT BULBS ON EXIT SIGH BY MAIN DOOR BELOW FLASHLIGHT IAW AMM 33-51-05. OPS CHECK GOOD.

Part: STRINGER — CRACKED (BS 193) · airframe 28,710 hrs · 20,167 cycles

LT ELECTRIC BAY AT 193.00. REPAIR FOUND STRINGER UNDER REPAIR AREA TO BE CRACKED. CRACK INDICATION NOTED AT AFT SECTION OF STRINGER SEGMENT. R & R STR IAW SRM 51-42-06-001-001-AO1.

Part: DOOR — OUT OF ADJUST (RT EMER EXIT) · airframe 28,710 hrs · 20,167 cycles

RT EMERGENCY EXIT FAILED FUNCTION CHECK TOOK 60LBS TO OPEN. ADJUSTED THE STEP FIT STOP SCREWS IAW 52-21-00-820-801. ADJUSTED RT OVERWING PROX SENSOR BRACKET AT TOP OF DOOR EMERGENCY EXIT PUSH PULL TEST WITHIN LIMITS FUNCTIONAL CHECK GOOD IAW AMM 52-21-00-720-801-A01. OPS CHECK GOOD ON RT WING EMERGENCY EXIT IAW AMM 52-21-00-710-801-A01. REBONDED STRIKER PLATE ON RT EMERGENCY DOOR PROXIMITY LEVER IAW AMM 51-31-00-992-801-A01.

Part: CONNECTOR — BROKEN (CABIN LIGHT) · airframe 28,710 hrs · 20,167 cycles

LT CABIN LIGHT AT E/EXIT CONNECTOR BROKEN, R & R LT CABIN LIGHT CONNECTOR AT E/EXIT , CONNECTOR PS9P2, IAW AMM 33-21-07-400-801, ESPM 20-26-06, ESPM 20-26-00 WM 25-28-01. PERFORMED OPS TEST OF THE PASSENGER COMPARTMENT LIGHTING IAW AMM 33-21-00-710-801-A01 TEST PASSED.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 28,710 hrs · 20,167 cycles

SERVICE DOOR SEAL STRIKER IS CORRODED. REMOVED SERVICE DOOR SEAL STRIKER LOWER IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE SERVICE DOOR LOWER SEAL STRIKER IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950. SDR CLOSED.

Part: LENS — DETERIORATED (EMERGENCY LIGHT) · airframe 28,710 hrs · 20,167 cycles

ENTRANCE STOWAGE COMPARTMENT EMERGENCY EXIT LIGHT LENS YELLOWED. INSTALLED LIGHT LENS ENTRANCE STOWAGE COMPARTMENT EMERENCY EXIT LIGHT BY PUSHING INTO PLACE.

Part: POST — CORRODED (COCKPIT DOOR) · airframe 28,710 hrs · 20,167 cycles

RT COCKPIT DOOR POST CORRODED ON LOWER INBD SIDE. REMOVED CORROSION AT RT COCKPIT DOOR POST IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 32-2015-31, DATED 7/29/2015.

Part: FLOOR SUPPORT — NOT REPORTED · airframe 28,710 hrs · 20,167 cycles

COCKPIT FLOOR SUPPORT ANGLE AT LBL 12 CAM LOC FASTENERS. R & R COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-00.

Part: ANGLE — CORRODED (BS 280) · airframe 28,710 hrs · 20,167 cycles

ANGLE AT LBL 11.00, WL 71.10, FS 280.00, CORRODED. R & R CORRODED ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-10-001-001-A01, DWG CC670-34-101.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 28,710 hrs · 20,167 cycles

SERVICE DOOR FLOOR PROTECTOR MACHINED ANGLE CORRODED, UPPER CAP ANGLE. CORROSION FOUND TO BE OUT OF LIMITS AS IT AFFECTS BOTH CROSS SECTION IAW SRM 53-21-23-101-002-A01. REMOVED SERVICE DOOR LOWER SILL ANGLE, CAP ANGLE, IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE LOWER SILL CAP ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01, REF DWG SH670-31950. LOCATED AND DRILLED HOLES IN NEW SERVICIBLE PART IAW SRM 51-40-11-001-001-A01.

Part: POST — CORRODED (COCKPIT DOOR) · airframe 28,710 hrs · 20,167 cycles

LEFT COCKPIT DOOR POST CORRODED ON LOWER INBD SIDE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 32-2015-315, DATED 7/29/2015.

Part: SEAT TRACK — CORRODED (BS 350-485) · airframe 28,710 hrs · 20,167 cycles

SEAT RAIL AT RBL9 BETWEEN BS 350-485, CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: ANGLE — CORRODED (BS 280) · airframe 28,710 hrs · 20,167 cycles

ANGLE AT RBL 11, BS 280, WL71 CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-10-001-001-A01. INSTALLED A NEW ANGLE AT RBL11, FS 280, WL 71 IAW SRM 51-42-06-001-001-A01 AND 57-42-10-001-001-A01.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 28,710 hrs · 20,167 cycles

FOUR ANGLES AT SERVICE DOOR LOWER SILL FLOOR PROTECTOR CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01 INTERGRANULA CORROSION. REMOVED 4 EA SERVICE DOOR CLIP ANGLES AT WEB PROTECTORS IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE CLIP ANGLES AT SERVICE DOOR WEB FLOOR PROTECTORS IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED AND DRILLED HOLES IN NEW SERVICIBLE FLOOR PROTECTOR CLIPS 4 EACH IAW SRM 51-40-11-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 28,710 hrs · 20,167 cycles

RT FLOOR SILL CORRODED JUST AFT OF FS349, COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390, REV DATED 1/22/2014 AS WRITTEN.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 28,710 hrs · 20,167 cycles

SERVICE DOOR LOWER MOUNTING ANGLE CORRODED. CORROSION FOUND TO BE OUT OF LIMITS AS IT AFFECTS BOTH CROSS SECTION IAW SRM 53-21-23-101-002-A01. REMOVED SERVICE DOOR LOWER SILL ANGLE, CAP ANGLE, IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE LOWER SILL CAP ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REF DWG SH670-31950. LOCATED AND DRILLED HOLES IN NEW SERVICIBLE PART IAW SRM 51-40-11-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 28,710 hrs · 20,167 cycles

RT FLOOR SILL CORRODED AROUND NUT PLATEHOLES BETWEEN FS 280 - FS 319. DAMAGE OUT OF LIMITS OF EC/TC REO 670-53-00-390. R & R SILL FS 280-FS 319, EC/TC REO 670-53-00-390 NOT REQUIRED. DAMAGE IS BEYOND REO 670-53-00-390. AREA IS OUT OF LIMITS IAW REO 670-53-00-390. DAMAGE OUT OF LIMITS OF EC/TC REO670-53-00-390. REMOVED RT FLOOR SILL AT FS280-319 IAW SRM 51-42-10-001-01-A1, 51-42-13-001-001-A01. LOCATED AND DRILLED HOLES IN NEW FLOOR SILL AT FS 280-319 IAW SRM 51-40-11-001-001-A01, DWG SH670-32127. INSTALLED NEW RT FLOOR SILL AT FS 280-319 IAW DWG SH 670-32172, SRM 51-42-10-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 374-485) · airframe 28,710 hrs · 20,167 cycles

SEAT TRACK AT LBL9 BETWEEN BS 374-485, CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 28,710 hrs · 20,167 cycles

COCKPIT FLOOR SUPPORT ANGLE AT RBL 12 CORRODED AT FWD END AND AROUND CAMLOC FASTENERS. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE AT RBL12 IAW SRM 51-42-06-001-001-A01, DWG CC670-33199.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 28,710 hrs · 20,167 cycles

RT FS 280 WEB CORRODED, COMPLIED WITH EC/TC REO 670-53-11-59401, GREO 670-53-21-594, REV A, DATED 4/27/2011.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 28,710 hrs · 20,167 cycles

LT BS 280 WEB CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, REV A DATED 4/27/111.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 28,710 hrs · 20,167 cycles

FWD EQUIPMENT COMPLARTMENT FLOOR PANEL CRACKED LT SIDE AT FS 193.00. COMPLIED WITH ECTC REO 670-532-11-509 AND GREO 670-53-11-509, REV B, DATED 1/28/2014.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 28,710 hrs · 20,167 cycles

EMERGENCY LIGHT LENS CRACKED ABOVE LT OVER WING EMERGENCY EXIT. REMOVED AND INSTALLED NEW SERVICEABLE EMERGENCY LIGHT LENS FWD OF LT OVER WING EXIT IAW AMM 33-51-05-000-801-A01 & 33-51-05-400-801-A01.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 28,710 hrs · 20,167 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED EMERGENCY EXIT LENS ASSEMBLY INSTALLED NEW EMERGENCY EXIT LENS ASSEMBLY BY PRESSING PLASTIC LENS ONTO TABS.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 28,709 hrs · 20,166 cycles

LEFT FLOOR SILL CORRODED AROUND NUTPLATE HOLES BETWEEN BS 280- 319. COMPLIED WITH EC/TC REO 670-00-390 AND REO 670-53-00-390, REV DATED, 01/22/2014 AS WRITTEN.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,439 hrs · 19,935 cycles

ROW 15 EXIT CEILING LIGHT INOPERATIVE. R & R THE BULB IAW AMM 33-51-09, OPS CHECKED GOOD.

Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 28,195 hrs · 19,743 cycles

FWD CARGO DOOR SEAL RETAINER BENT AT FWD LOWER CORNER. COMPLIED WITH EC/TC REO 670-52-35-127 01, PERMANENT REPAIR. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,473 hrs · 18,447 cycles

WHITE OVERHEAD CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPED AND OPS CHECKED GOOD IAW AMM 33-51-09.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 26,320 hrs · 18,332 cycles

F/O FLASHLIGHT INOPERATIVE. CLEANED CONTACTS ON FLASHLIGHT. INSTALLED NEW BATTERIES IAW AMM 25-61-04. ALL CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,301 hrs · 18,316 cycles

FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 25,153 hrs · 17,493 cycles

PAX DOOR HARD TO OPEN. LUBED PAX DOOR INNER HANDLE IAW AMM 52-10-00. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,468 hrs · 16,996 cycles

AFT F/A FLASHLIGHT INOPERATIVE, R & R AFT F/A'S FLASHLIGHT IAW AMM 25-61-02.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,357 hrs · 16,918 cycles

EMERGENCY LIGHTS WILL NOT TURN ON. REMOVED AND INSTALLED SERVICEABLE NR 2 & NR 3 BATTERIES IAW AMM 33-51-17-000-801, 33-51-17-400-801, OPS CHECKED GOOD.

Part: RIB — DAMAGED (LT WING) · airframe 24,343 hrs · 16,905 cycles

WHILE REMOVING FASTENER, DAMAGE TO RIB OCCURED AT WS 49.00 ON LT WING FASTENER NR 23 ON ATTACHED ILLISTRATION. REPAIRED IAW REO 670-57-21-579.

Part: BEARING — CRACKED (LT WING) · airframe 24,357 hrs · 16,918 cycles

LEFT AFT WING LINK UPPER AND LOWER BEARINGS ARE CRACKED AND TOUCHING ATTACH FITTING. REPAIRED IAW REO 670-57-27-398-01 AND SB 670BA-57-016, REV B, DEC 07/2012. REPAIR CLASSIFIED AS MAJOR.

Part: LINK — CRACKED (RT WING) · airframe 24,357 hrs · 16,918 cycles

RT AFT WING LINK UPPER AND LOWER BEARINGS ARE CRACKED AND TOUCHING ATTACH FITTING. REPAIRED IAW SB 670BA-57-016, REV B. REPAIR CLASSIFIED AS MAJOR.

Part: STRAP — MISMANUFACTURED (WING) · airframe 24,357 hrs · 16,918 cycles

RT SIDE LOWER STRAP FOR SB670BA-57-02001 HAS ONE HOLE MISCOUNTERSUNK. REPAIRED IAW OF REO 670-57-21-576. MAJOR REPAIR.

Part: FITTING — DAMAGED (TE FLAP) · airframe 24,343 hrs · 16,905 cycles

OVERSIZED HOLES ON LT & RT FWD FLAP FITTING ASSY. REPAIRED IAW REO 670-57-21-575, REV P1. REPAIR CLASSIFIED AS MAJOR.

Part: ANGLE — CORRODED (BS 280) · airframe 24,343 hrs · 16,905 cycles

ON REMOVAL OF BS 280 BEAM, FOUND FWD FLOORBEAM, BACK-UP ANGLE LT SIDE DAMAGED AND CORRODED. REMOVED LT SIDE BACK UP ANGLE. LOCATED AND DRILLED NEW SERVICABLE LT FITTING IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERIVCABLE BACKUP ANGLE IAW SRM 51-42-22-001-001-A01 AND 51-42-21-001-001.

Part: CROSSBEAM — CORRODED (BS 349) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON CROSSBEAM AT BS 349, APPROX RBL 9. REPAIRED IAW SRM 53-21-43-101-001-A01, 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,343 hrs · 16,905 cycles

COCKPIT FLOOR PANEL 221ALF, AFT SUPPORT ANGLE AT FS 280 CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED HOLES IN NEW AFT FLOOR SUPPORT IAW SRM 51-40-06 AND 51-40-11 & DWG CC670-33292. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21 & DWG CC670-33292. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (BS 295) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON FRAME BS 295 BETWEEN S26L AND 26R. REPAIRED IAW SRM 51-21-06-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (BS 379-500) · airframe 24,343 hrs · 16,905 cycles

RT SIDE WALL SEAT TRACK CORRODED IN MULTIPLE SPOTS FROM FS379-500 APPROX. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 700-760) · airframe 24,343 hrs · 16,905 cycles

RIGHT SIDE WELL SEAT TRACK CORRODED BETWEEN BS 700-760 IN NUTPLATE SPOTS. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A03 & AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 379-500) · airframe 24,343 hrs · 16,905 cycles

LEFT SIDE WALL SEAT TRACK FWD SEGMENT CORRODED IN MULTIPLE AREAS APPROX FS 379-500. R & R SEAT RAIL AT LT SIDEWALL FS 379 IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.

Part: FRAME — CORRODED (BS 349) · airframe 24,343 hrs · 16,905 cycles

FRAME IS CORRODED AT FRAME BS 349 BETWEEN S26-27L. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-972. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT BRACKET — CRACKED (LOCKING MECH) · airframe 24,343 hrs · 16,905 cycles

CRACKED ANGLE SUPPORT BRACKET ON ASD INNER LOCKING MECH BRACKET AFT OF ICE BREAKER DOOR. R & R ANGLE BRACKET IN REF SRM 52-11-06-991-801, 51-42-06. LOCATED & DRILLED NEW SERVICEABLE ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERIVCABLE ANGLE IAW REO 670-52-11-719 AND SRM 51-42-21. RECEIVED AND COMPLIED WITH ECTC REO 670-52-11-719.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 24,343 hrs · 16,905 cycles

PAX DOOR LOWER SILL RECESSED, FWD FLOOR SUPPORT FITTING HAS CORROSION ON SEVERAL PLACES AROUND FASTENERS. REMOVED CORROSION FROM FWD SUPPORT FITTING DAMAGE FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 51-21-06-001-001-A01 AND 53-21-23-101-001-A01. INSTALLED NEW SERVICEABLE FITTING AT FWD FLOOR SUPPORT AREA IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 & DWG SH670-31840.

Part: FRAME — CORRODED (BS 333) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON FRAME BS 333 AT S25L. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-972. REPAIR CLASSIFIED AS MAJOR.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 24,343 hrs · 16,905 cycles

PAX DOOR LOWER SILL RECESSED AFT FLOOR SUPPORT FITTING HAS CORROSION ON SEVERAL PLACES AROUND FASTENERS. REMOVED SUPPORT FITTING THAT WAS FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE FITTING IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 DWG SH670-32475.

Part: FRAME — CORRODED (BS 310) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON FRAME BS 310 BETWEEN S26L AND 26R. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-972. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,343 hrs · 16,905 cycles

PAX DOOR LOWER SILL AFT FLOOR SUPPORT ANGLE HAS CORROSION AROUND FASTENERS AND 1 FASTENER HAS CORRODED AWAY, REMOVED AFT ANGLE THAT WAS FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED UP NEW SERVICEABLE PART (AFT FLOOR SUPPORT ANGLE) IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE AFT ANGLE IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 & DWG SH670-31821. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: FLOOR SUPPORT — CORRODED (AVIONICS BAY) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON FLOOR SUPPORT IN AVIONICS BAY. R & R FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & DWG CC670-34256. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (BS 319) · airframe 24,343 hrs · 16,905 cycles

CORROISON ON FRAME BS 319 BETWEEN S26-27L. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-972. REPAIR CLASSIFIED AS MAJOR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON INTERCOSTAL AT FWD END OF AVIONICS BAY DOOR CUTOUT FRAME BS 364 AT S26L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-972. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,357 hrs · 16,918 cycles

FLOORBEAM CORRODED AT FS 280 AT RBL 45 TO SERVICE DOOR. REMOVED IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-45-00-001-001-A01. INSTALLED IAW SRM 51-42-06-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON INTERCOSTAL AT FWD END OF AVIONIC BAY DOOR CUTOUT FRAME BS 364 AT S27L. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-42-06-001-001-A01. LOCATED DRILLED AND DEBURED NEW INTERCOSTAL IAW SRM 51-40-06-001-001-A01, ALSO, 51-40-11-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, ALSO 51-42-21-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: BRACKET — DAMAGED (CARGO DOOR) · airframe 24,343 hrs · 16,905 cycles

AFT CARGO DOOR FWD AFT CABLE CUTTING INTO SUPPORT BRACKET. REPAIRED IAW EO CL600-2C10-53-100359. REPAIR CLASSIFIED AS MAJOR.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON PASSENGER DOOR LOWER SILL. REPAIRED IAW SRM 51-21-06-001-001-A01. REPAIR CLASSIFIED AS MAJOR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,357 hrs · 16,918 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED DAMAGED PART 1 IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND DEBURRED NEW DRAG ANGLE AND SPLICES IAW SRM 51-40-056-001-001-A01 ALSO 51-40-11-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,343 hrs · 16,905 cycles

BS 280 FLOORBEAM CORRODED FROM LBL9 TO RBL45. REMOVED, LOCATED, DRILLED AND INSTALLED NEW FLOORBEAM IAW SRM 53-11-41-201-003-A01. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (BS 349) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON FRAME BS 349 BETWEEN S25-27R. REPAIRED IAW SRM 51-21-06-001-001-A01 AND REO 670-53-21-972. REPAIR CLASSIFIED AS MAJOR.

Part: ATTACH ANGLE — CORRODED (BS 364) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON INTERCOSTAL ATTACH ANGLE AT FWD END OF AVIONICS BAY DOOR CUTOUT FRAME BS 364 S26R. REMOVED ATTACH ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED DRILLED AND DEBURRED NEW ATTACH ANGLE IAW SRM 51-40-06-001-001-A01 & 51-40-11-001-001-A01. INSTALLED NEW ATTACH ANGLE IAW SRM 51-42-06-001-001 & DWG SH670-32077. REPAIR CLASSIFIED AS MAJOR.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 24,343 hrs · 16,905 cycles

CORROSION ON INTERCOSTAL AT FWD END OF AVIONICS BAY DOOR CUTOUT FRAME BS 364 S27R. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND DEBURRED NEW INTERCOSTAL IAW SRM 51-40-06-001-001-A01, & 51-40-11-001-001-A01. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG SH670-32075. REPAIR CLASSIFIED AS MAJOR.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 24,343 hrs · 16,905 cycles

PAX DOOR LOWER SILL PROXIMITY SENSOR ANGLE HAS CORROSION ON SEVERAL PLACES. REMOVED ANGLE IAW SRM 51-41-02-001-001-A01. LOCATED, DRILLED & DEBURRED HOLES IN NEW SILL ANGLE ALSO ATTACHED NUT PLATES IAW SRM 51-40-06-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-45-00-001-001-A01 DWG SH670-31825, REV A. INSTALLED CAP ANGLE MID STA 330 WITH NEW SERVICEABLE PART IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 24,343 hrs · 16,905 cycles

FS 193.00, ELECTRICAL BAY FLOOR CRACKED ON RT SIDE UNDER ADG STOW PUMP, FWD OTBD CORNER. REPAIR IS CLASSIFIED AS MAJOR. COMPLIED WITH EC/TC REO 670-53-11-509 AND GREO 670-57-11-509.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 23,134 hrs · 16,047 cycles

F/A WARDROBE EMERGENCY LIGHT COVER MISSING. REPLACED F/A WARDROBE FLOOR LEVEL EMERGENCY FLOOD LIGHT LENS IAW AMM 66-51-11. OPS CHECKED GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 22,810 hrs · 15,815 cycles

ROW 12AB FWD EMERGENCY LIGHTING PHOTO ILLUMINESCENT STRIP MISSING. INSTALLED EMERGENCY FLOOR PATH PHOTO ILLUMINESCENT MARKING AT ROW 12AB FWD IAW AMM 33-51-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,786 hrs · 15,019 cycles

CEILING EMERGENCY LIGHT OUT AT ROW 6. RELAMPED CEILING EMERGENCY LIGHT AT ROW 6 IAW AMM 33-51-09. RELAMPED CEILING EMERGENCY LIGHT AT ROW 6 IAW AMM 33-51-09.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,686 hrs · 14,946 cycles

CABIN THIRD FROM FRONT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY CEILING LIGHT FIXTURE IAW AMM 33-51-09.

Part: MEGAPHONE — OUT OF ADJUST (CABIN) · airframe 21,158 hrs · 14,576 cycles

MEGAPHONE DOES NOT WORK. PERFORMED ADJUSTMENT TEST OF MEGA PHONE IAW AMM 25-61-14. OPS CHECKED GOOD.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,652 hrs · 13,530 cycles

SURROUND STRUCTURE LOWER SILL HAS CORROSION. REMOVED LOWER SILL ANGLE IAW SRM 51-42-06-001-001, LOCATED AND DRILLED FASTENER HOLES IN NEW LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01. INSTALL LOWER ANGLE. OK TO INSTALL LOWER ANGLE, INSTALLED ASD LOWER SILL ANGLE IAW SRM 51-42-06-001-001 AND 51-42-20-001-001. EM161737 CORROSION AFT SIDE OF ASD LOWER SILL. OUT OF SEQUENCE. UPON REMOVEAL OF PAX DOOR DAMAGED MID CAP ANGLE FOUND CORROSION ON AFT SIDE OF ASD LOWER SILL AT PROX SWITCH LOCATION ASD LOWER SILL IS OUT OF ALLOWABLE LIMITS. REFER TO ITEMS 6 AND 7 FOR REMOVAL AND INSTALLATION. INSTALL ASD ROD ASY ACTUATOR HANDRAIL BRACKETS. REMOVED AND INSTALLED ASD ROD ASY ACTUATOR, HANDRAIL FWD AND AFT BRACKETS IAW SRM 51-42-20-001-001. RII FOUND TO BE SATISFACTORY. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 785) · airframe 19,652 hrs · 13,530 cycles

RT SIDEWALL SEAT RAIL CORRODED AT FS 785. RECEIVED EC/TC FROM REPS REO 670-53-00-332, ALL STEPS COMPLIED WITH. RII FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 19,652 hrs · 13,530 cycles

LEFT SIDEWALL SEAT TRACK CORRODED AT BS 785. REMOVED AND REPLACED IAW SRM 51-42-02-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 736) · airframe 19,652 hrs · 13,530 cycles

LEFT SIDEWALL SEAT TRACK CORRODED AT FS 736. REPAIRED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,652 hrs · 13,530 cycles

CORROSION ON FLANGE OF LOWER SILL ANGLE. REMOVED AND DRILLED NEW MID ANGLE IAW SRM 51-41-02-001-001 AND 51-42-06-001-001. INSTALLED ANGLE IAW SRM 51-41-02-001-001-A01.

Part: FIREWALL — CRACKED (NR 1 NACELLE) · airframe 19,652 hrs · 13,530 cycles

NR 1 SYS LT PYLON FIREWALL 2ND FROM AFT UPPER ACCESS HOLE ELONGATED (NR 1 SYS PRESSURE LINE). APPEARS TO BE CRACKED AT FWD SIDE. COMPLIED WITH STEPS 1-2 OF REO 670-54-51-018. COMPLIED WITH NDT IAW STEP 3 OF REO 670-4-51-018 NDTM PART 1, 51-20-006. NO INDICATIONS NOTED. COMPLIED WITH STEPS 4 AND 5 OF REO 670-54-51-018. COMPLIED WITH STEPS 6-9 OF REO 670-54-51-018. REMOVED FIREWALL ASSY IAW SRM 51-42-06. INSTALLED FIREWALL ASSY IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 752) · airframe 19,652 hrs · 13,530 cycles

LEFT BS 752 SIDEWALL SEAT TRACK CORRODED. REMOVED CORROSION, THICKNESS IS .355, REMOVED .011, AND IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49. PERFORMED LPI, TYPE 1, METHOD C ON BLENDED AREA IAW NDT PROCEDURE PT-1. NO CRACK NOTED. REPAIRED IAW SRM 53-41-49-101-001-A01. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 736) · airframe 19,652 hrs · 13,530 cycles

LT SIDEWALL SEAT TRACK CORRODED AT BS 736. REMOVED CORROSION. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 19,652 hrs · 13,530 cycles

LEFT SIDEWALL SEAT TRACK CORRODED AT BS 708. REMOVED CORROSION, ORIGINAL THICKNESS IS .355, REMOVED .030 MATERIAL , REMAINING THICKNESS IS .325, WITHIN LIMITS IAW SRM 53-41-49.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 19,652 hrs · 13,530 cycles

RIGHT SIDEWALL SEAT TRACK CORRODED BS 785. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801.

Part: SEAT TRACK — CORRODED (BS 813) · airframe 19,652 hrs · 13,530 cycles

LEFT BS 813 SIDEWALL SEAT TRACK CORRODED. REMOVED CORROSION, THICKNESS IS .355, REMOVED .013 AND IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49. PERFORMED LPI, TYPE 1, METHOD C ON BLENDED AREAS IAW NDT INSPECTION PROCEDURES PT-1. NO CRACK NOTED. REPAIRED IAW 670-53-00-013 IAW SRM 53-41-49-101-001-A01. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 19,652 hrs · 13,530 cycles

RIGHT SIDEWALL SEAT TRACK CORRODED AT BS 708. REMOVED CORROSION, ORIGINAL THICKNESS .355, REMOVED .037 MATERIAL, REMAINING THICKNESS IS .318. FOUND OUT OF LIMITS IAW SRM 53-41-49. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 19,652 hrs · 13,530 cycles

LEFT BS 785 SIDEWALL SEAT TRACK CORRODED. REMOVED CORROSION, THICKNESS IS .355, REMOVED .015 AND IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREA IAW NDT INSPECTION PROCEDURES PT-1. NO CRACK NOTED. REMOVED SEAT TRACK IAW SRM 53-00-49. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-332, STEPS 1 THRU 4. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 785) · airframe 19,652 hrs · 13,530 cycles

LT SIDEWALL SEAT RAIL CORRODED AT FUS STA 785. REMOVED CORROSION FROM LT SIDE WALL SEAT RAIL AT FS 785 SEAT TRACK THICKNESS IS .355, REMOVED .015 REMAINING THICKNESS IS .340 AND IS WITHIN ALLOWABLE LIMITS IAW SRM 53-41-49. THIS IS A MINOR REPAIR. BLEND AREA REQUIRES LPI IAW SRM 51-12-00-001-001-A01. PERFORMED LPI, TYPE 1, METHOD C ON BLEND AREA IAW MAC NDT INSP PROCEDURE PT-1. NO INDICATION NOTED AT THIS TIME. BRUSH ALODINE BLEND AREA AND IDENTIFY SEAT TRACK IAW SRM 53-41-49-101-001-001-A01. ALODINE BLEND AREA AND INDENTIFY SEAT TRACK IAW SRM 670-53-00-013 IAW SRM 53-41-49-101-001-A01. THIS IS A MINOR REPAIR. REMOVED SEAT TRACK IAW SRM 53-00-49. FABRICATE NEW TRACK. FABRICATED NEW SEAT TRACK IAW REO 670-53-00-332, STEPS 1 THRU 4. INSTALLED SEAT TRACK. OK TO INSTALL MAC3QC, INSTALLED LT SIDE WALL SEAT TRACK AT FS 785 IAW AMM 53-00-49-400-801-A03. RII FOUND TO BE SATISFACTORY.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,652 hrs · 13,530 cycles

FS 280 FWD FLOORBEAM ANGLE CORRODED. ANGLE CORRODED BEYOND REPAIR, REMOVED ANGLE, DRILLED NEW ANGLE, AND INSTALLED IAW SRM 51-42-06-001-001-A01. MINOR REPAIR.

Part: STRINGER — CORRODED (BS 295-310 S26R) · airframe 19,652 hrs · 13,530 cycles

CORROSION ON STRINGER 26 RIGHT, BETWEEN FRAMES 295.00-310.00. FOUND TO BE OUT OF LIMITS REF SRM 53-21-03-101-002-A01. REMOVED AND REPLACED STRINGER IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,652 hrs · 13,530 cycles

BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED LOWER SILL AND UPPER ANGLE TO BE REPLACED IAW SRM 51-42-06-001-001-A01. PARTS DAMAGED BEYOND LIMITS IAW SRM. INSTALL NEW PARTS. INSTALLED NEW LOWER SILL AND UPPER ANGLE IAW SRM 51-40-11, 51-40-00 & 51-42-00. MINOR REPAIR.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 19,652 hrs · 13,530 cycles

PAX DOOR ASSIST MOTOR LOWER VERTICAL STIFFENER CRACKED APPROX .3750" LEFT IN RADIUS. REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-42-06-001-001-A01.

Part: BULKHEAD — CORRODED (BS 280) · airframe 19,652 hrs · 13,530 cycles

LT BULKHEAD AT FS 280.00 IS CORRODED. REMOVED CORROSION, A LONG WL 72.5 IAW SRM 53-11-10-201-003-A01. DAMAGE EXCEEDED LIMITS. REMOVED DAMAGED WEB IAW REO 670-53-11-594. PERFORMED ET INSPECTION IAW NDT PROCEDURE ET-2. NO INDICATIONS NOTED. FABRICATED WEB AND SPLICE PLATE IAW REO670-53-11-594 INSP. INSTALLED WEB AND SPLICE PLATE IAW REO 670-53-11-594.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,652 hrs · 13,530 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. DRAG ANGLE WAS REPAIRED IAW SRM 52-11-04-201-002-A06.

Part: DOOR — OBSTRUCTED (EMERGENCY EXIT) · airframe 19,652 hrs · 13,530 cycles

LEFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST IAW AMM 52-21-00-991-805. TRASH FOUND ON LOCK PINS, CLEANED AND REINSTALLED DOOR, PERFORMED FUNCTIONAL TEST IAW AMM 52-21-00-720-801, TESTED GOOD.

Part: BULKHEAD — CORRODED (BS 280) · airframe 19,652 hrs · 13,530 cycles

BULKHEAD AT FS 280.00 IS CORRODED. REMOVED CORROSION IAW SRM 53-11-10-201-003-A01. FOUND OUT OF LIMITS. REMOVED DAMAGED BULKEHEAD WEB IAW REO 670-53-11-594 01. PERFORMED ET IAW NDT PROCEDURE ET-2. NO INDICATIONS NOTED. FABRICATED NEW WEB AND SPLICE PLATE IAW REO670-53-11-594. INSTALLED WEB AND SPLICE PLATE IAW REO 670-53-11-594.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,652 hrs · 13,530 cycles

CORROSION DAMAGE EXCEEDS GENERAL ALLOWABLE DAMAGE LIMITS OF SRM 53-00-00-101-001-A01, REMOVED FS 280 BEAM WL 72 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01. CUT CROSSBEAM IAW REO 670-53-11-047. NDI IAW REO 670-53-11-047, ITEM 5. NO INDICATIONS NOTED. COMPLIED WITH STEPS NR 6-9 OF ECTC REO 670-53-11-047. INSTALLED BEAM IAW ECTC REO 670-53-11-047.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 18,618 hrs · 12,820 cycles

ON CLIMBOUT GEAR DISAGREE MESSAGE WITH ASSOCIATED WOW INPUT AND NOSE STEER INOP, COMPLIED WITH QRH. LANDED W/O INCIDENT, TOUCHDOWN VREF 135+5 VSI +500 MINIMAL BRAKING WEIGHT ON TOUCHDOWN 64K ONLY NOSE WHEEL CYCLED. ACFT RETURNED TO DEPARTURE AFTER TAKE OFF -- EMERGENCY DECLARED. ADJUSTED NLG WOW SENSORS PX 06 AND PX 11 IAW AMM 32-61-05. PERFORMED OPS TEST OF LANDING GEAR EXTENSION IAW AMM 32-30-00. OPS CHECK GOOD. COMPLIED WITH GENERAL VISUAL INSP AFTER HARD/OVERWEIGHT LANDING IAW AMM 05-51-01 NO DISCREPANCIES NOTED.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,828 hrs · 11,564 cycles

LEFT ESCAPE HATCH FWD LOWER EMERGENCY LIGHT 3EA BULBS BURNED OUT. RELAMPED CABIN EMERGENCY LIGHT AT LT ESCAPE HATCH LOWER FWD 5EA BULBS OPS CHECK GOOD IAW AMM 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,828 hrs · 11,564 cycles

ERMERGENCY LIGHT BULB INOP RT ESCAPE HATCH LOWER FWD. RELAMPED CABIN EMERGENCY LIGHT AT RT ESCAPE HATCH LOWER FWD BULB OPS CHECK GOOD IAW AMM 33-51-00.

Part: STEP — CRACKED (DOOR) · airframe 16,535 hrs · 11,337 cycles

TOP A/S/D STEP BROKEN. REPLACED THE TOP ASD STEP IAW AMM 52-11-04, ITEM: 1, REPLACED THE TOP ASD STEP IAW AMM 52-11-04.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 16,238 hrs · 11,124 cycles

F/O'S FLASHLIGHT INOP. REMOVED AND REPLACED F/O'S FLASHLIGHT IAW AMM 25-61-00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,684 hrs · 9,964 cycles

ANGLE AT FS 280, LBL 26, WL 68-78 FOUND TO BE CRACKED ON LOWER EDGE (16052 6-28-09 AAR349 PG6). REMOVED OLD AND INSTALLED NEW ANGLE IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,684 hrs · 9,964 cycles

RT PAX COMP FLOOR SEAT RAIL HAS CORROSION FROM FS 450.00 TO FS 469.00 (13259 6-24-09 AAR363 PG102). BLENDED ON RT SEAT TRACK FROM FS 450.00 TO FS 469.00 TO DETERMINE SEVERITY OF CORROSION. CORROSION ON SEAT TRACK FOUND TO BE OUT OF LIMITS FOR BLENDING IAW SRM 53-31-49-101-001-A01. REMOVED SEAT TRACK IAW SRM 51-41-02. LOCATED & DRILLED SERVICEABLE SEAT TRACK IAW SRM 51-40-11. COUNTER SUNK HOLES IAW SRM 51-40-11. ALODINED OPEN HOLES IAW SRM 51-21-11. INSTALLED SERVICEABLE RT SIDE FLOOR SEAT TRACK IAW AMM 53-00-49-400-801-A01.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 14,684 hrs · 9,964 cycles

FLT DECK FLOOR SUPPORT ANGLE AT FS 280 CORRODED. REMOVED UNSERVICEABLE FLOOR SUPPORT ANGLE. LOCATED DRILLED AND PREPARED NEW SERVICEABLE ANGLE P/N CC670-33-292-13S FOR INSTALLATION IAW SRM 51-40-11. INSTALLED SERVICEABLE FLIGHT DECK FLOOR SUPPORT ANGLE P/N CC670-33292-13S, PO 959654 IAW SRM 51-42-06 AND 51-42-21. APPLIED PRIMER TO FASTENERS IAW SRM 51-25-06. APPLIED TOPCOAT TO PRIMED AREA IAW SRM 51-25-21.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 14,684 hrs · 9,964 cycles

FS 280 BULKHEAD RT LWR WEB CORRODED. REMOVED FASTENERS AS REQUIRED. BLENDED WEB TO REMOVE SURFACE CORROSION. MAX DEPTH .005 INCH (.005" ALLOWED) IAW SRM 53-11-10-201-003 REPAIR A. OK TO RESTORE FINISH, APPLIED ALODINE PRIMER AND TOPCOAT TO RESTORE FINISH CODE IAW SRM 51-21-16. STILL REQUIRES RE-INSTALLATION OF PREVIOUSLY REMOVED FASTENERS. INSTALLED PREVIOUSLY REMOVED FASTENERS IAW SRM 51-42-06. REMOVED CORROSION ON RT LOWER WEB IAW SRM 51-21-06.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 14,684 hrs · 9,964 cycles

FS 280 FLOOR SUPPORT CROSSBEAM CORRODED. RECEIVED SERVICEABLE CROSSBEAM. FABRICATED AND INSTALLED CROSSBEAM SPLICES. C/W EO 700-53-0061.

Part: BULKHEAD WEB — CORRODED (FUSELAGE) · airframe 14,684 hrs · 9,964 cycles

FS 280 BULKHEAD LT LWR WEB CORRODED. REMOVED FASTENERS AS REQUIRED. BLENDED WEB TO REMOVE SURFACE CORROSION. MAX DEPTH .003 (.005 INCH ALLOWED) IAW SRM 53-11-10-201-003 REPAIR "A". REMOVED EDGE DAMAGE 1 INCH IN LENGTH AT I/B WEB EDGE JUST ABOVE FLOOR LEVEL IAW SRM 53-00-00-101-001. APPLIED ALODINE, PRIMER, AND TOPCOAT TO RESTORE FINISH CODE IAW SRM 51-21-16. INSTALLED PREVIOUSLY REMOVED FASTENERS IAW SRM 51-42-06. REMOVED CORROSION ON BULKHEAD LT LWR WEB IAW SRM 51-21-06.

Part: SILL — CORRODED (FUSELAGE) · airframe 14,684 hrs · 9,964 cycles

RT FLOOR SILL CORRODED AROUND NUT PLATE AT FS 282. BLENDED DISCREPANT AREA AT FS 282 ON RT FLOOR SILL, FOUND TO BE WITHIN SERVICEABLE LIMITS IAW SRM 53-00-01.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 14,684 hrs · 9,964 cycles

F/O'S FLASHLIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,536 hrs · 9,842 cycles

NR 2 AND NR 3 CABIN CEILING EMERGENCY FLOOD LIGHTS INOP.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 14,536 hrs · 9,842 cycles

EMERGENCY LIGHTS COME ON SPONTANEOUSLY WITH WITCH IN "ARM POSITION . SEE PREVIOUS LIGHTING STRIKE WRITE-UP

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 14,377 hrs · 9,727 cycles

FLIGHT ATTENDANT MEGA PHONE INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,147 hrs · 8,764 cycles

EMERGENCY LIGHT JUST AFT OF SERVICE DOOR HAS SEVERAL INOP BULBS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,685 hrs · 7,012 cycles

EXIT LIGHT AT 1A + B IS OUT.

Part: CHARGER — READS LOW (CABIN) · airframe 10,687 hrs · 7,013 cycles

EMERGENCY BATTERY CHARGER NR 1 READING LOW VOLTAGE.

Part: BATTERY — READS LOW (CABIN) · airframe 10,687 hrs · 7,013 cycles

EMERGENCY BATTERY NR 3 AND NR 4 READING LOW VOLTAGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,687 hrs · 7,013 cycles

FOUND EXIT LIGHT AT 1 A + B IS OUT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,351 hrs · 6,789 cycles

LEFT FLOOR SEAT TRACK FS 485.00 TO FS 581.00 HAS SURFACE CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,351 hrs · 6,789 cycles

LEFT FLOOR SEAT TRACK FS 581.00 TO FS 677.00 HAS SURFACE CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,351 hrs · 6,789 cycles

RIGHT FLOOR SEAT TRACK FS 581.00 TO FS 677.00 HAS SURFACE CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,351 hrs · 6,789 cycles

RIGHT FLOOR SEAT TRACK FS 485.00 TO FS 581.00 HAS SURFACE CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,351 hrs · 6,789 cycles

LEFT FLOOR SEAT TRACK FS 374.00 TO 485.00 CORRODED AND BENT (MARKED).

Part: STRUCTURE — CORRODED (COCKPIT FLOOR) · airframe 10,351 hrs · 6,789 cycles

AFT COCKPIT FLOOR LAND AT FS 280 IS CORRODED. 10-24-07 REMOVED AFT COCKPIT FLOOR LAND AT FS 280 IAW CRJ 700 51-42-06 AND 1-42-21. DRILLED UP NEW AFT COCKPIT FLOOR LAND WORK DONE IAW CRJ 700 SRM 51-42-06. INSTALLED AFT COCKPIT FLOORBOARD ANGLE AND CAMLOCK RECEPTACLES (2) PER CRJ 700 SRM 51-42-06. COMPLIED WITH RII INSPECTION OF AFT COCKPIT FLOOR LAND INSTALLATION AT FS 280 PER ASA SP 607 AND CRJ 700 SRM 51-42-06.

Part: WEB — CORRODED (FUSELAGE) · airframe 10,351 hrs · 6,789 cycles

RIGHT AND LEFT 280 WEBS HAVE SIGNS OF SURFACE CORROSION JUST ABOVE 280 TRANSVERSE BEAM. REMOVED SURFACE CORROSION ON LT AND RT 280 WEBS PER CRJ700 SRM 53-11-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,351 hrs · 6,789 cycles

RBL 9 SEAT TRACK CORRODED AT FS 349.00.

Part: HINGE FITTING — CRACKED (LT WING) · airframe 10,351 hrs · 6,789 cycles

LT MFS HINGE FITTING OUTBOARD AT WS 216.95 CRACKED. 10-29-07 R & R LT MFS FITTING IAW CRJ 700 SB 670-BA-57-010. REMOVED BUTTE DOORS FROM LT WING. BEGAN REMOVING HINGE FITTING IAW BOMBARDIER SB 70BA-57-010. INSTALLED LT WING MFS PCU PER CRJ 700 AMM 27-62-01-400-801-A01. INSTALLED LT WING FLAP TORQUE TUBE IAW CRJ 700 AMM 27-52-01. INSTALLED LT WING AILERON CIRCUIT CABLES IAW CRJ 700 AMM 27-11-13. LT WING AILERON CABLES TENSIONED IN MLG BAY IAW CRJ AMM CHAPTER 27-11-00. REATTACHED LT WING WIRE HARNESS FROM WS 178.00 TO 231.00 FOLLOWING S/M REPAIR IAW SB 670-BA-57-010. TRANSFERED HOLES & DEBUFED NEW PART & INSTALLED LOCK FASTENERS THRU TANK IAW SB 670-BA-57-010. COMPLETED INSTALLATION OF CENTER HINGE FITTING IAW SB 670-BA-57-010. COMPLIED WITH RIG. LEAK & OPS CHECK IAW CRJ 700 AMM 27-64-00. RIGGED LT WING AILERON CONTROL CABLES IAW CRJ 700 AMM 27-11-00 TASK 27-11-00-820-801-A01. COMPLIED WITH OPS CHECK OF FLAP IAW CRJ 700 AMM 27-50-00 OPS CHECK GOOD. FOUND & INSTALLED MISSING FLAP TORQUE TUBE CONTAINMENT RING ON LT WING IAW CRJ 700 AMM 27-52-01. PERFORMED OPS TES OF AILERON CONTROL SYS IAW CRJ 700 MM TASK 27-11-00-710-801. OP CHECKS GOOD.

Part: BEAM — CORRODED (FUSELAGE) · airframe 10,351 hrs · 6,789 cycles

SURFACE CORROSION ON 280 TRANSVERSE BEAM ON UPPER SURFACE. 10-24-07 REMOVED SURFACE CORROSION ON 280 TRANSVERSE BEAM ON UPPER SURFACE IAW SRM 51-21-06. RT OUT OF LIMITS. REMOVE RT 280 FRAME & RBL 19 AND 27 INTERCOSTAL IAW CRJ 700 SRM 51-42-06 AND 51-42-21. REMOVED RT PITOT STATIC LINE IAW CRJ 700 AMM 34-11-00. CUT NEW 280 FRAME & DRILLED FASTNER HOLES LABELS DONE IAW IS67053110026. INSTALLED RT 280 FRAME IAW IS67053110026 & 280 FRAME SPLICE IAW REO 670-53-11-047. INSTALLED FASTENERS IN ITANIUM DOUBLERS PER MODSUM IS67053110026 CONTINUE INSTALLATION OF FASTENERS THROUGH UPPER PORTION OF TITANIUM. FINISHED INSTALLATION OF RT SIDE OF 280 TRANSVERSE BEAM PER IS67053110026 AND REO 670-53-11-045.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 10,351 hrs · 6,789 cycles

LT AND RT EMERGENCY LIGHT LUMINESCENT STRIP PROTECTORS DAMAGED MID WAY THROUGH CABIN.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 10,351 hrs · 6,789 cycles

ASD EXTERNAL HANDLE CRACKED. 10-26-07 REMOVED AND REPLACED ASD EXTERNAL HANDLE IAW CRJ SRM 51-40-11, 51-25-06,51-25-16 AND CRJ 700 MM 25-11-03.

Part: DRAG BRACE — CRACKED (FUSELAGE) · airframe 10,351 hrs · 6,789 cycles

DRAG BRACE FOR FUSELAGE TO VERTICAL STAB, T/E CRACKED. 10-29-07 REPAIRED DRAG BRACE ANGLE IAW REO 670-55-31-018.

Part: PLACARD — MISSING (PAX DOOR) · airframe 8,549 hrs · 5,553 cycles

PASSENGER ENTRY DOOR -EXIT- PLACARD MISSING.

Part: ATTACH ANGLE — CORRODED (BS 279) · airframe 7,092 hrs · 4,620 cycles

FOUND COCKPIT CENTER FLOOR AFT ATTACH ANGLE CORRODED, FS 279.

Part: ANGLE — CORRODED (DOOR) · airframe 7,092 hrs · 4,620 cycles

FOUND ASD CENTER DOOR ANGLE CORRODED.

Part: STRUCTURE — CRACKED (AIRSTAIR DOOR) · airframe 7,093 hrs · 4,620 cycles

ASD CRACKED UNDER UPPER STEP AFT SIDE

Part: WARNING MESSAGE — ILLUMINATED · airframe 7,000 hrs · 4,563 cycles

FIRE SYSTEM FAULT STATUS MSG.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, EMERGENCY LIGHTING WOULD NOT ILLUMINATE. MAINTENANCE CHARGED THE EMERGENCY LIGHTING SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BATTERY — DAMAGED (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE LEFT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND RESCURED A RECESSED PIN IN THE NR4 EMERGENCY BATTERY TERMINAL BLOCK. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K)

Part: COMPRESSOR — DAMAGED (RT ENGINE)

DURING TAKEOFF, CREW EXPERIENCED A RUMBLE AND YAW IN A/C ACCOMPANIED BY A COMPRESSOR STALL ON RT ENGINE ALONG WITH TOWER ADVISING OF FLAMES COMING OUT OF ENGINE. CREW REDUCED RT ENGINE TO IDLE WITH ALL PARAMETERS REMAINING AT NORMAL, NO FIRE INDICATIONS PRESENT. EMERGENCY WAS DECLARED AND A/C RETURNED, LANDING SAFELY WITH FLAPS SELECTED AT 20 DEGREES. MAINT FOUND FOD DAMAGE TO RT ENG COMPRESSOR STAGES 1-5. REMOVED AND REPLACED RT ENGINE. TEARDOWN REPORT CONCLUDED THAT FOREIGN OBJECT WAS INJECTED INTO RT ENG. OBJECT WAS IDENTIFIED AS LOW ALLOY STEEL NOT COMMON FOR ENGINE AIRFLOW MATERIAL , RESULTING IN DAMAGES TO FAN BLADES, COMPRESSOR ROTOR, STATOR, COMBUSTION CHAMBER, HIGH AND LOW PRESS TURBINE SECTIONS.

Part: ENGINE — FOD (RIGHT)

DURING TAKEOFF, CREW EXPERIENCED A RUMBLE AND YAW IN AIRCRAFT ACCOMPANIED BY A COMPRESSOR STALL ON THE RT ENGINE ALONG WITH THE TOWER ADVISING OF FLAMES COMING OUT OF ENGINE. CREW REDUCED RT ENGINE TO IDLE WITH ALL PARAMETERS REMAINING AT NORMAL AND NO FIRE INDICATIONS PRESENT. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED, LANDING SAFELY WITH FLAPS SELECTED AT 20 DEGREES. MAINTENANCE FOUND FOD DAMAGE TO THE RT ENGINE COMPRESSOR STAGES 1 THROUGH 5. MAINTENANCE REMOVED AND REPLACED RT ENGINE. MRR WILL REMAIN OPEN, PENDING ENGINE TEARDOWN REPORT.