N716EV

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 42,419 hrs · 31,112 cycles

REFERENCE CP27547979 FOR DAMAGED FO'S WINDSHIELD, REMOVE FO'S WINDSHIELD. (FILED CLOSED)REMOVED THE FIRST OFFICER'S WINDSHIELD IAW CRJ 700 AMM 56-11-01. REFERENCE ML 27547979 FOR INSTALLATION OF THE FIRST OFFICER'S WINDSHIELD AND PARTS INFORMATION.

Part: UNKNOWN — MISSING · airframe 41,371 hrs · 30,145 cycles

THE O/B SEAT TRACK AT SEAT 15A IS MISSING. (FILED CLOSED)INSTALLED THE MISSING O/B SEAT TRACK AT SEAT 15A IN REF TO AMM 25-21-02.

Part: NONE — POPPED · airframe 39,002 hrs · 28,238 cycles

AFT CARGO DOOR CAUTION (FLIGHT 3189 - FILED CLOSED) UPON A/C ARRIVAL, FOUND AFT CARGO DOOR HANDLE POPPED OUT. PERFORMED GVI OF AFT CARGO DOOR AND FOUND NO DEFECTS NOTED AT THIS TIME. PERFORMED OPS CHECK OF AFT CARGO DOOR LATCHING AND INDICATION SEVERAL TIMES PER AMM 52-31-00. NO DEFECTS NOTED AT THIS TIME. DOOR HANDLE DOES NOT POP OUT ON ITS OWN WHEN PROPERLY STOWED. INDICATIONS STAY GREEN WHEN DOOR IS TAPPED AROUND HANDLE. SUSPECT AFT CARGO DOOR HANDLE WAS NOT PROPERLY STOWED. AC IS OK FOR SERVICE AT THIS TIME.

Part: DOUBLER — DAMAGED (ZONE 100) · 26,754 cycles

FORWARD VALVE RETAINER DOUBLER P/N KBA670-31630-9SB AT FS280.00 BETWEEN STGR27 AND STGR26R HAS MISLOCATED VALVE HOLE (C-CHECK) RO 2/5/2021 REPAIRED FUSELAGE SKIN BETWEEN FS280.0 - FS333.0 AND STR 26L - STR 26R. REF REO 670-53-21-1914 REV. -- DATED 2021-01-23. COMPLIED WITH 51-900-1002-SKY. ALL CHECKS GOOD COMPLIED WITH M-337

Part: STRINGER SPLICE — CORRODED (ZONE 100) · 26,754 cycles

STGR SPLICE AT STGR 19R F.S. 477.0 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED WITH NEW FROM STOCK STRINGER SPLICE AT 19R AND FS477 PN: SH670-33264-1 REF CRJ700 SRM 51-42-06-001-001-A01, AND DWG SH670-33264 REV NC. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND FORM 337 ACCOMPLISHED.

Part: DOUBLER — DAMAGED (ZONE 100) · 26,754 cycles

(4EA) DOUBLERS HAVE MISLOCATED HOLES (C-CHECK) RO 2/5/2021 FABRICATED 4EA. NEW REPAIR FILLERS REF. MHIRJ REO 670-53-21-1914 REV --(P1) DATED 2020-12-15. LOCATED AND DRILLED DOUBLERS AND INSTALLED REF. MHIRJ REO 670-53-21-1914 REV --(P1) DATED 2020-12-15. RECIEVED FINAL MHIRJ REO 670-53-21-1914 REV -- DATED 2021-01-23. ALL STEPS COMPLIED WITH. PRESSURE CHECKS GOOD. COMPLIED WITH 51-900-1002-SKY.

Part: BRACKET — CORRODED (PAX DOOR AREA) · 26,754 cycles

PAX DOOR BRACKET AT DOOR DATUM 5 TRACE BETWEEN FS347.250 AND FS338.963 IS CORRODED (C-CHECK) RO 2/5/2021 REPLACED PAX DOOR BRACKET AT DOOR DATUM 5 TRACE BETWEEN FS347.250 AND FS338.963REF:CRJ-700 S.R.M. 51-42-06-001-001-A01 & DWG 601R31702 REV N. PRESSURE CHECK GOOD. / COMPLIED WITH SKY CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) / COMPLIED WITH FORM M-337

Part: CLEAT — CORRODED (ZONE 200) · 26,754 cycles

PAX DOOR CLEAT AT DOOR DATUM 5 TRACE BETWEEN FS347.250 AND FS338.963 IS CORRODED (C-CHECK) RO 2/5/2021 REPLACED PAX DOOR CLEAT AT DOOR DATUM 5 TRACE BETWEEN FS347.250 AND FS338.963. REF: CRJ-700 S.R.M. 51-42-06-001-001-A01. / COMPLIED WITH SKY CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) / COMPLIED WITH FORM M-337

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 26,754 cycles

PAX DOOR INTERCOSTAL AT DD3 BETWEEN FS 311.75 AND FS 320.16 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD3 BETWEEN FS 311.75 AND FS 320.16. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · 26,754 cycles

PAX DOOR INTERCOSTAL AT DOOR DATUM 5 TRACE BETWEEN FS 338.96 AND FS 347.25 HAS CORROSION. (C-CHECK) RO 2/5/2021 EVALUATED PAX DOOR INTERCOSTAL AT DATUM 5 RACE BETWEEN FS338.96 AND FS347.25 OUT OF LIMITS. REMOVED AND REPLACED NEW PAX DOOR INTERCOSTAL AT DOOR DATUM 5 FS338.96 ABD FS347.25 REF: CRJ 700 SRM 51-42-06-001-001 (A01), DWG-601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURE CHECK GOOD.

Part: CLEAT — CORRODED (PAX DOOR AREA) · 26,754 cycles

PAX DOOR CLEAT AT FS 320.16 AND DD4 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR CLEAT AT FS 320.16 AND DD4. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTINUATION CARD FOR DETAILS. / COMPLIED WITH SKY CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) / COMPLIED WITH FORM M-337

Part: BRACKET — CORRODED (PAX DOOR) · 26,754 cycles

PAX DOOR BRACKET AT FS 311.75 AND DD6 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR BRACKET AT FS 311.75 AND DD6. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR AND COMPLIED WITH FORM M-337.

Part: CLEAT — CORRODED (PAX DOOR AREA) · 26,754 cycles

PAX DOOR CLEAT AT FS 320.16 AND DD6 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR CLEAT AT FS 320.16 AND DD6. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTINUATION CARD FOR DETAILS. / COMPLIED WITH SKY CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) / COMPLIED WITH FORM M-337

Part: CLEAT — CORRODED (PAX DOOR AREA) · 26,754 cycles

PAX DOOR CLEAT AT FS 311.75 AND DD4 IS CORRODED (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR CLEAT AT FS 311.75 AND DD4. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR AND COMPLIED WITH FORM M-337.

Part: STIFFENER — DAMAGED (LT NACELLE) · 26,754 cycles

LH LWR TRANSCOWL ZED STIFFNER IS HEAVILY CHAFFED AND GOUGED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED LH LWR ZED STIFFNER, REF CRJ 700 SRM 51-40-11-001-001-A01, BOMBARDIER/SHORTS DWG CN624-2038 REV A AND BOMBARDIER REO 670-54-21-1207 REV A DATED 2015-08-27 / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · 26,754 cycles

PAX DOOR FWD FORMER FRAME, UNDER PANEL 832FL, IS CORRODED. (C-CHECK) RO 2/5/2021 REPLACED PAX DOOR FWD FORMER FRAME. REF: CRJ 700 SRM 51-42-06-001-001 (A01), 51-42-21-001-001 (A01), AND DWG 601 R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: SKIN — CRACKED (LT NACELLE) · 26,754 cycles

LH UPPER TRANSCOWL HAS 1EA CRACKED OUT HOLE UNDER "Z" ANGLE ON INNER SKIN (MARKED). (C-CHECK) RO 2/5/2021 REPAIRED CRAKED OUT HOLE ON INNER SKIN OF LH UPPER TRANSCOWL PER MHIRJ REO 670-54-21-1413 REV -- DATED 2020-12-16, REF CRJ 700 SRM 51-42-13-001-001-A01 & 51-23-00-001-001-A01 / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: COAMING — CHAFED (RT NACELLE) · 26,754 cycles

RH ENGINE LWR TRANSCOWLING COAMING HAS EXCESSIVE CHAFFING AT VARIOUS LOCATIONS. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED DAMAGED TRANSCOWL LATCH COAMING P/N CN624-2060-205 AT RH ENGINE LWR TRANSCOWL. REF BOMBARDIER REO 670-54-21-1207 REV A, DATED 2015-08-27. SEE CONTINUE CARD FOR DETAILS. / COMPLIED WITH SKY CARD 51-900-1002-SKY(CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) / COMPLIED WITH FORM M-337

Part: HINGE FITTING — CORRODED (RT ELEVATOR) · 26,754 cycles

UPON REMOVAL ON JOB 71008485 OP 76 CAMP 21903312, FOUND R/H ELEVATOR L/E HINGE FITTING #3, P/N AV670-24136-001, TO HAVE PITTING CORROSION IN THE BEARING BORE. REPLACE HINGE FITTING ASSY. (C-CHECK) RO 2/5/2021 ELEVATOR ASSY REPLACED, NEW ELEVATOR ASSY HAS NEW HINGE FITTING #3 INSTALLED. SEE JOB 71008481 OP 266 CAMP # 21903177 FOR INSTALLATION OF THE ELEVATOR ASSY.

Part: INTERCOSTAL — CORRODED (ZONE 100) · 26,754 cycles

AT F.S. 333.00 STGR 21L, POSSIBLE CORROSION ON THE INTERCOSTAL. (C-CHECK) RO 2/5/2021 REPLACED 21L INTERCOSTAL AT FS333.00 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 DWG SH670-31810 REV Y. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD.

Part: STIFFENER — GOUGED (LT NACELLE) · 26,754 cycles

L/H ENGINE UPPER TRANS COWL, UPON REMOVAL OF Z STIFFNER GOUGE MARKS ON 2 PLACES (C-CHECK) RO 2/5/2021 INSTALLED NEW L/H ENGINE UPPER TRANS COWL Z STIFFENER COMMON TO THE COAMING LATCH DOOR PN-CN624-2038-901. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-54-21-1207 REV A 2015-08-27 / COMPLIED WITH 51-900-1002-SKY

Part: BEARING — CHAFED (TRANS COWL PAD) · 26,754 cycles

L/H ENGINE UPPER TRANS COWL PAD BEARING EXCESSIVE CHAFFING. (C-CHECK) RO 2/5/2021 INSTALLED NEW L/H ENGINE UPPER TRANS COWL PAD BEARING PN-CN624-2130-201. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-54-21-1207 REV A 2015-08-27 / COMPLIED WITH 51-900-1002-SKY

Part: STIFFENER — MISSING (LT NACELLE) · 26,754 cycles

L/H ENGINE UPPER TRANS COWL Z STIFFNER COMMON TO THE COAMING LATCH DOOR HAS 2EA MISSING FASTENER (C-CHECK) RO 2/5/2021 INSTALLED NEW L/H ENGINE UPPER TRANS COWL Z STIFFENER COMMON TO THE COAMING LATCH DOOR PN-CN624-2038-901. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-54-21-1207 REV A 2015-08-27 / COMPLIED WITH 51-900-1002-SKY / COMPLIED WITH FORM M-337

Part: COAMING — CHAFED (LT NACELLE) · 26,754 cycles

L/H ENGINE UPPER TRANS COWL LATCH COAMING HAS HEAVY CHAFFE AROUND HOLE LOCKING AREA (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW L/H ENGINE UPPER TRANS COWL LATCH COAMING PN-CN624-2061-905. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-54-21-1207 REV A 2015-08-27 / COMPLIED WITH 51-900-1002-SKY

Part: DOUBLER — CHAFED (LT NACELLE) · 26,754 cycles

L/H ENGINE UPPER TRANS COWL DOUBLER HAS HEAVY CHAFFE (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW L/H ENGINE UPPER TRANS COWL DOUBLER PN-CN624-2003-997. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-54-21-1207 REV A, DATED 2015-08-27. / COMPLIED WITH 51-900-1002-SKY / COMPLIED WITH FORM M-337

Part: CONTROL UNIT — CORRODED (LT AILERON) · 26,754 cycles

L/H AILERON INBOARD PCU REQUIRES REPLACEMENT DUE TO CORROSION. SEE JOB# 71008484, OPERATION 5, MX TRANS #21851614 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED L/H AILERON INBOARD PCU IAW CRJ-700 AMM 27-14-01-000-801-A01 AND 27-14-01-400-801-A01. OPS TEST GOOD. COMPLIED WITH TASK CARD 27-900-1002-SKY.

Part: PCU — CORRODED (LT AILERON) · 26,754 cycles

L/H AILERON OUTBOARD PCU REQUIRES REPLACEMENT DUE TO CORROSION. SEE JOB# 71008484, OPERATION 5, MX TRANS # 21851614 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED L/H AILERON OUTBOARD PCU IAW CRJ-700 AMM 27-14-01-000-801-A01 AND 27-14-01-400-801-A01. OPS TEST GOOD. COMPLIED WITH TASK CARD 27-900-1002-SKY.

Part: PCU — CORRODED (RT AILERON) · 26,754 cycles

R/H AILERON INBOARD PCU REQUIRES REPLACEMENT DUE TO CORROSION. SEE JOB 7118484, OP4, MX TRANS #21851631 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED R/H AILERON INBOARD PCU IAW CRJ-700 AMM 27-14-01-000-801-A01 AND 27-14-01-400-801-A01. OPS TEST GOOD. COMPLIED WITH TASK CARD 27-900-1002-SKY.

Part: PCU — CORRODED (RT AILERON) · 26,754 cycles

R/H AILERON OUTBOARD PCU REQUIRES REPLACEMENT DUE TO CORROSION. SEE JOB 71008484, OP 4, MX TRANS #21851631 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED R/H AILERON OUTBOARD PCU IAW CRJ-700 AMM 27-14-01-000-801-A01 AND 27-14-01-400-801-A01. OPS TEST GOOD. COMPLIED WITH TASK CARD 27-900-1002-SKY.

Part: FITTING — CORRODED (CARGO DOOR FRAME) · 26,754 cycles

FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE, FWD AND AFT LOWER GUIDE FITTINGS HAVE MOUNTING HARDWARE APPEARS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED FWD BAGGAGE BAY SURROUND STRUCTURE FWD AND AFT LOWER GUIDE FITTING MOUNTING HARDWARE REF CRJ 700 SRM 51-41-02-001-001-A01.

Part: LANDING — CRACKED (LT NACELLE DOOR) · 26,754 cycles

*LEFT ENG LOWER TRANS COWL LATCH DOOR LANDING CRACKED. (MARKED) (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW LATCH COAMING REF BOMBARDIER REO 670-54-21-1207 REV A, DATED 2015-08-27. / COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — CORRODED (ZONE 100) · 26,754 cycles

STGR 25R CORRODED AT F.S. 295 TO F.S. 310.00 (MARKED). (C-CHECK) RO 2/5/2021 REPLACED STGR 25R FROM FS280-FS333 WITH NEW REF CRJ-700 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — CORRODED (ZONE 100) · 26,754 cycles

*CORROSION ON STGR 25L BETWEEN FS 485.00 €“ 501.00 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED STGR 25L F.S. 485.00-501.00, REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH670-33200 REV G, LEAK CHECK GOOD. / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: STRINGER — CORRODED (ZONE 100) · 26,754 cycles

*STGR27 CORRODED FS280.00 - FS295.00. (MARKED) (C-CHECK) RO 2/5/2021 STGR27 FROM FS280-FS313 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01 DWG SH670-31630 REV K. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD.

Part: DOUBLER — CORRODED (DRAIN MAST) · 26,754 cycles

*CORROSION ON DRAIN MAST INTERNAL PLATE/DOUBLER BETWEEN FS 1031.00 €“ 1047.00, RH OF STGR 27 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED DAMAGED AFT DRAIN MAST INTERNAL DOUBLER BETWEEN FS1031.00-1047.00 WITH NEW INTERNAL DOUBLER PN MM670-43255-001 IAW CRJ 700 SRM 51-42-06-001-001-A01. / COMPLIED WITH 51-900-1002-SKY PRESSURE CHECK GOOD.

Part: STRINGER — CORRODED (ZONE 100) · 26,754 cycles

*STGR26R CORRODED FS295.00 €“ FS310.00. (MARKED) (C-CHECK) RO 2/5/2021 REPLACED STGR26R FS280-FS333.00 REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 DWG SH670-31630 REV K COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD.

Part: BRACKET — CORRODED (ZONE 100) · 26,754 cycles

*CORROSION ON FWD CARGO FLOOR MACHINED BRACKET BETWEEN STGR 23L €“ 22L, FS 581.00 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACE BRACKET AT FWD CARGO STGR 23L €“ 22L, FS 581.00 REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM / 51-42-06-001-001-A01, DWG SH670-33600 REV Y / . COMPLETED 51-900-1002-SKY AND M-337.

Part: PLATE — CORRODED (ZONE 100) · 26,754 cycles

*CORROSION ON FWD CARGO FLOOR MOUNT PLATE AT FS 581.00, OVER STGR 27 (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW FWD CARGO FLOOR MOUNT PLATE SH670-33376-4 REF DWG SH670-33376 REV A AND CRJ-700 SRM TASK 51-42-06-001-001-A01 (SOLID RIVETS).

Part: SEAT TRACK — CORRODED (ZONE 200) · 26,754 cycles

*CORROSION ON RH SIE SEAT RAIL BETWEEN FS 565.00 - 661.00. AREAS MARKED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED SEAT RAIL R/H BETWEEN FS 565.00 - FS 661.00 REF CRJ700 AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17

Part: BRACKET — CORRODED (ZONE 100) · 26,754 cycles

*CORROSION ON FWD CARGO FLOOR MACHINED BRACKET BETWEEN STGR 27 -26L, FS 581.00 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED DAMAGED BRACKET AT FWD CARGO FS 581 STR 27-26L REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DRW SH670-33389 REV NC. COMPLIED WITH SKYCARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) COMPLIED WITH FORM M-337

Part: INTERCOSTAL — CORRODED (ZONE 100) · 26,754 cycles

*INTERCOSTAL CORRODED FS310.00 €“ FS319.00, STGR20L. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED DAMAGED INTERCOSTAL (P/N- SH670-31822-1) AT FS 310.00 - FS 319.00, STGR 21LH. . REF CRJ-700 SRM 51-42-06-001-001-A01 & DWG SH670-31822 REV NC. SEE CONTINUE CARD FOR DETAILS. / COMPLIED WITH 51-900-1002-SKY

Part: STRINGER — CORRODED (ZONE 100) · 26,754 cycles

*STGR25L CORRODED BETWEEN FS319.00 €“ FS333.00. (MARKED) (C-CHECK) RO 2/5/2021 REPLACED STGR 25L FROM FS280-FS333 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01, DWG SH670-31630 REV K. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD. / COMPLIED WITH FORM M-337

Part: STRINGER SPLICE — CORRODED (ZONE 100) · 26,754 cycles

*STGR26L STRINGER SPLICE CORRODED JUST FORWARD OF FRAME FS333.00. (MARKED) (C-CHECK) RO 2/5/2021 REPLACED STGR 26L STRINGER SPLICE AT FS333.00 WITH NEW REF CRJ-700 SRM 51-42-06-001-001-A01CRJ 700SRM 51-40-11-001-001-A01 AND DWG SH670-32429 REV A. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD.

Part: BRACKET — CORRODED (ZONE 100) · 26,754 cycles

*CORROSION ON FWD CARGO FLOOR MACHINED BRACKET BETWEEN STGR 25R €“ 24R, FS 549.00 - 565.00 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED BRACKET AT STGR 25R €“ 24R, FS 549.00 - 565.00 FWD CARGO PN SH670-33852-1 REF CRJ700 / SRM 51-42-21-001-001-A01, CRJ700 51-42-06-001-001- / A01, DRW SH670-33852 REV NC COMPLIED WITH 51-900-1002-SKY

Part: BRACKET — CORRODED (ZONE 100) · 26,754 cycles

*CORROSION ON FWD CARGO FLOOR MACHINED BRACKET AT FS 533.00 BETWEEN STGR 23L €“ 22L (C-CHECK) RO 2/5/2021 REPLACED FWD CARGO FLOOR MACHINED BRACKET AT FS533 BETWEEN STGR23L-STGR22L WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD.

Part: PLATE — CORRODED (ZONE 100) · 26,754 cycles

*CORROSION ON FWD CARGO FLOOR MOUNT PLATE ON STGR 25L, FS 533.00 (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW FWD CARGO FLOOR MOUNT PLATE SH670-33376-3 REF DWG SH670-33376 REV A AND CRJ-700 SRM TASK 51-42-06-001-001-A01 (SOLID RIVETS).

Part: SLIDER — WORN (THRUST REVERSER) · 26,754 cycles

R/H LWR TRANS COWL SLIDE HAS WORN AREA (FWD) (C-CHECK) RO 2/5/2021 REPAIRED DAMAGE TO RH LWR TRANSCOWL SLIDE PER MHIRJ REO 670-54-21-1410 REV -- DATED 2020-12-11 AND BOMBARDIER REO 670-78-34-384 REV D DATED 2018-11-27 / COMPLIED WITH SKYWEST TASK CARD 51-900-10032-SKY (CL600-2C10) STRUCTURL MAJOR REPAIR / COMPLIED WITH SKYWEST FORM M-337

Part: SLAT TRACK — CORRODED (ZONE 600) · 26,754 cycles

*RH SLAT TRACK 2-2 HAS 2 AREAS OF CORROSION (MARKED) (C-CHECK) RO 2/5/2021 BLENDED R/H SLAT TRACK 2-2 AND RESTORED AS REQUIRED PER REO 670-57-42-979 REV. -- DATE: 20-12-17 WITHIN LIMITS, ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLIED WITH FORM 337.

Part: SLAT TRACK — CORRODED (RT WING) · 26,754 cycles

*RH SLAT TRACK 1-2 HAS 2 AREAS OF CORROSION (MARKED) (C-CHECK) RO 2/5/2021 BLENDED R/H SLAT TRACK 1-2 AND RESTORED AS REQUIRED PER REO 670-57-42-978 REV.-- DATE: 2020-12-17 ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002 SKY.

Part: SLAT TRACK — CORRODED (LEFT) · 26,754 cycles

LH SLAT TRACK 1-2 HAS 1 AREA OF CORROSION. (C-CHECK) RO 2/5/2021 BLENDED L/H SLAT TRACK 1-2 AND RESTORED AS REQUIRED PER REO 670-57-42-976 REV. -- DATE:2020-12-18 ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: SLAT TRACK — CORRODED (LEFT) · 26,754 cycles

LT SLAT TRACK 2-2 HAS 2 AREAS OF CORROSION (MARKED) (C-CHECK) RO 2/5/2021 BLENDED AREA ON L/H SLAT TRACK 2-2 AND RESTORED AS REQUIRED. BLENDED DAREAS ARE STRUCTURALLY ACCEPTABLE REF. REO 670-57-42-977 REV. -- DATE: 20-12-18 ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLIED WITH FORM M-337

Part: SKIN — DAMAGED (ZONE 200) · 26,754 cycles

RH FUSELAGE SKIN HAS HOLE BELOW STRINGER 11 AT APPROX FS 1151. VISABLE FROM WITHIN AEB (EXTERIOR SKIN IS COVERED BY RH PYLON). (C-CHECK) RO 2/5/2021 FABRICATED REPAIR DOUBLER FROM 2024-T3 .071 PO # T-52592 AND FABRICATED SHIM FROM 2024-T3 .080 PO # T-55606 , LOCATED AND DRILLED TRIMMED TO FIT PER REO 670-53-61-1790 REV -- DATED 2021-01-11 / COMPLIED WITH SKY CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR COMPLIED WITH FORM M-337

Part: PANEL — CHAFED (LT WING TE FLAP) · 26,754 cycles

L/H WING INBOARD FLAP L/E PANEL 584ET , HAS CHAFFING CONDITION (C-CHECK) RO 2/5/2021 REMOVED PNL 584ET, BLENDED DAMAGE, DETERMINED TO EXCEED LIMITS IAW CRJ700 SRM 57-52-01-101-001-A01, ORDERED AND RECIEVED NEW PANEL P/N CC670-14027-3, LOCATED,DRILLED AND COUNTERSUNK SCREW HOLES IAW CRJ700 SRM 51-40-11-001-001-A01. TOP COAT PAINT FINISH TO BE APPLIED ON MX TRANS 21885757 JOB 71008485 OP 65

Part: ANGLE — CORRODED (RT WING) · 26,754 cycles

ANGLE CORRODED ON AIRCRAFT FOR PANEL 642 AZ (C-CHECK) RO 2/5/2021 INSTALLED NEW ANGLE CC670-10338-2 REF DWG CC670-10320 REV F DATE 2015 NOV 5. HI-LITE INSTALLATION REF CRJ-700 SRM TASK 51-42-21-001-001-A01 / COMPLIED WITH SKY CARD 28-900-100-SKY (CL600-2C10) FUEL CELL ACCESS / COMPLIED WITH SKY CARD 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) / COMPLIED WITH FORM M-337

Part: BOLT — CORRODED (LT WING TE FLAP) · 26,754 cycles

* CORROSION DETECTED ON (BOLT HEADS) ON L/H OTBD FLAP, (INBD) HINGE BOX, (FWD) SUPPORT FITTING (WING PLANK SIDE), ATTACHING HARDWARE (MARKED). (C-CHECK) RO 2/5/2021 - INSTALLED 6 NEW BOLTS AND ATTACHING HARDWARE ON TO FLAP HINGE BOX SUPPORT FITTING AT WS178 REF. CRJ-700 AMM 57-54-02-400-810 (A01) STEPS 4.A.(11) TO END. / TUC8498 DUE:31-AUG-21 / LEAK CHECK GOOD. NO DEFECTS NOTED.

Part: SKIN — DAMAGED (ZONE 100) · 26,754 cycles

EVALUATE CREASE @ FS 409 ABOVE STGR 20L. (C-CHECK) RO 2/5/2021 INSTALLED REPAIRED DOUBLER-1 AND REPAIR SHIM-2. REF: REO 670-53-21-1888 REV. -- DATE: 2020-12-14. PRESSURE CHECK GOOD. / COMPLIED WITH ALL STEPS OF REO 670-53-21-1888 REV -- DATED 2020-12-14. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLIED WITH FORM M-337

Part: LIGHT — INOPERATIVE (RWO 4) · airframe 35,860 hrs · 25,753 cycles

DURING MX INSPECTION THE OVERHEAD EMERGENCY LIGHT AT ROW 4 IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-09, CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DIAPHRAGM — CRACKED (FAIRING) · airframe 35,001 hrs · 25,066 cycles

AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE FORWARD DIAPHRAGM P/N SH670-39241-3 AT FS 909.00 LBL 17.63 IS CRACKED AT JOGGLE. REPAIRED WING TO FUSELAGE AFT FAIRING SUP FS 909.00, LBL 17.63 & (OR) RBL 17.63 IAW REO 670-53-82-478 REV A. REO 670-53-82-519 HAS BEEN ACCOMPLISHED.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 35,001 hrs · 25,066 cycles

RT FS280 CROSSBEAM CRACKED APPROX 4" AT RBL 45. REO 670-53-21-1471 HAS BEEN ACCOMPLISHED.

Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 35,001 hrs · 25,066 cycles

REF: CO# 10084617 JOB# 71008468 OP# 28: SERVICE DOOR LOWER SEAL STRIKER IS CORRODED. C/A: REMOVED AND REPLACED SERVICE DOOR LOWER SEAL STRIKER IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01 AND BOMBARDIER REO 670-53-21-1469.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 35,001 hrs · 25,066 cycles

REF: CO# 10084617 JOB# 71008461 OP# 41: PAX DOOR AFT DRAG ANGLE IS CRACKED NEAR POWER ASSIST PULLEY FITTING. C/A: REPAIRED PAX DOOR AFT DRAG ANGLE IAW EXPRESS JET EC/TC REO 670-52-11-072 AND 670-52-11-985.

Part: FLOOR SUPPORT — CORRODED (BS 280-300) · airframe 35,001 hrs · 25,066 cycles

REF: CO# 10084617 JOB# 71008468 OP# 29: RIGHT CABIN FLOOR SILL RBL45 F.S.280-F.S.300 IS CORRODED. C/A: REMOVED AND REPLACED RIGHT CABIN FLOOR SILL IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND EXPRESS JET EC/TC SNIEO SH670-32170 S01

Part: LUG — CHAFED (RT AILERON) · airframe 35,001 hrs · 25,066 cycles

REF: CO# 10084617 JOB# 71008467 OP# 16: RIGHT AILERON OUTBOARD PCU HINGE LUG IS CHAFED. C/A: REPAIRED RIGHT AILERON HINGE LUG IAW BOMBARDIER REO 670-57-61-107 REV A AND EXPRESS JET EC/TC EO700-57-60-00007.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,066 cycles

LEFT SIDEWALL NR 5 SEAT TRACK FROM FS 715-FS 761 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.

Part: HINGE — GOUGED (PAX DOOR) · airframe 35,001 hrs · 25,066 cycles

PASSENGER DOOR HINGE ON DOOR SIDED IS GOUGED AT 2(EA) LOCATIONS ON FORWARD SIDE OF ATTACHMENT LUG. REPAIRED PASSENGER DOOR HINGE IAW REO 670-52-11-511 REV E DATED 2017-08-02 AND EC/TC REO 670-52-11-511 REV E.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 35,001 hrs · 25,066 cycles

MAIN LANDING GEAR FAIRING 194AB CENTER SUPPORT FWD AND AFT ANGLE BRACKETS ARE CRACKED. BROKEN WHERE PANEL MOUNTS. REMOVED AND REPLACED FWD AND AFT ANGLE BRACKETS IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,006 cycles

FLOOR SEAT TRACK AT LBL 9 BETWEEN FS485-FS581 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,066 cycles

FLOOR SEAT TRACK AT LBL 9 BETWEEN FS693-FS847 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,006 cycles

FLOOR SEAT TRACK AT RBL 9 BETWEEN FS847-FS969 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,066 cycles

RT SEAT TRACK AT RBL 9..00 IS CORRODED BETWEEN FS 693 AND FS 847.00. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, DATED 2015-10-22 AND REO 670-53-00-343 REV M, DATED 2015-10-19.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,066 cycles

INTERCOSTAL FROM FS 364-349 BETWEEN STRINGER 27 AND 26L IS CORRODED AT FRONT OF AVIONICS BAY DOOR CUTOUT. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 364 TO 349 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,066 cycles

FS 349 LOWER FRAME SEGMENT IS CORRODED BETWEEN STRINGER 27 AND 26L. REPAIRED FRAME FS 349 IAW REO 670-53-21-1281 DATED 2016-04-11 AND EC/TC REO 670-53-21-1281.

Part: SEAT TRACK — CORRODED (BS 570-677) · corrosion level 2 · airframe 35,001 hrs · 25,066 cycles

LEFT SIDEWALL NR 3 SEAT TRACK FROM BS 570 - 670 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, AND REO 670-53-00-343, REV M.

Part: SEAT TRACK — CORRODED (BS 713-763) · corrosion level 2 · airframe 35,001 hrs · 25,066 cycles

RIGHT SIDEWALL NR 5 SEAT TRACK FROM BS 713 TO 763 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, REV M, AND EC/TC REO 670-53-00-343, REV K.

Part: SEAT TRACK — CORRODED (BS 985-100) · corrosion level 2 · airframe 35,001 hrs · 25,066 cycles

SEAT TRACK, RBL 27 IS CORRODED BETWEEN BS 985 AND 1000. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, AND REO 670-53-00-343, REV M.

Part: SEAT TRACK — CORRODED (BS 785-853) · corrosion level 2 · airframe 35,001 hrs · 25,066 cycles

LEFT SIDEWALL NR 6 SEAT TRACK FROM BS 785 TO 853 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV M, AND EC/TC REO 670-53-00-343, REV K.

Part: SEAT TRACK — CORRODED (BS 675-713) · corrosion level 2 · airframe 35,001 hrs · 25,066 cycles

RIGHT SIDEWALL NR 4 SEAT TRACK, BS 675 TO 713 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, REV M, AND EC/TC REO 670-53-00-343, REV K,

Part: SEAT TRACK — CORRODED (BS 547-985) · corrosion level 2 · airframe 35,001 hrs · 25,066 cycles

LEFT SEAT TRACK AT LBL 9 IS CORRODED BETWEEN BS 847 AND 985. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, AND REO 670-53-00-343, REV M.

Part: SEAT TRACK — CORRODED (BS 485-570) · corrosion level 2 · airframe 35,001 hrs · 25,066 cycles

LEFT SIDEWALL NR 2 SEAT TRACK FROM BS 485 - 570 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, AND REO 670-53-00-343, REV M.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 35,001 hrs · 25,066 cycles

BS 280 FLOORBEAM ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, AND 51-25-00-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 861-961) · corrosion level 2 · airframe 35,001 hrs · 25,066 cycles

RIGHT SIDEWALL NR 8 SEAT TRACK FROM BS 861 TO 961 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW REO 670-53-00-343 REV.M, AND EC/TC REO 670-53-00-343 REV.K,

Part: SEAT TRACK — CORRODED (BS 784-855) · corrosion level 2 · airframe 35,001 hrs · 25,006 cycles

RIGHT SIDEWALL NR 6 SEAT TRACK FROM BS 784 TO 855 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-343, REV M, AND EC/TC REO 670-53-00-343, REV K.

Part: FRAME — CORRODED (BS 310) · airframe 35,001 hrs · 25,066 cycles

BS 310 LOWER FRAME SEGMENT IS CORRODED BETWEEN STRINGERS 25 AND 27L. REPAIRED THE FRAME IAW REO 670-53-21-799, REV A, AND EC/TC REO 670-53-21-799, REV A.

Part: SEAT TRACK — CORRODED (BS 861-961) · airframe 35,001 hrs · 25,066 cycles

LEFT SIDEWALL NR 8 SEAT TRACK FROM BS 861 - 961 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343, REV K, REO 670-53-00-343, REV M, AMM 53-00-49-000-801-A17, AND 53-00-49-400-801-A17.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,066 cycles

LEFT SIDEWALL NR 4 SEAT TRACK FROM FS677-FS715 IS CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EC/TC REO 670-53-00-343 REV K, REO 670-53-00-343 REV M, AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,066 cycles

AVIONICS BAY FLOORBOARD SUPPORT AT FS 280.00 IS CORRODED. REMOVED AND REPLACED WITH NEW SERVICEABLE FLOORBOARD SUPPORT P/N CC670-34256-3 IAW SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 35,001 hrs · 25,066 cycles

SERVICE DOOR STEP PLATE HAS CORROSION ON THE BOTTOM OF THE STEP PLATE. REPLACED CORRODED STEP PLATE P/N SH670-31407-7 WITH NEW SERVICEABLE STEP PLATE P/N SH670-31407-7. DRILLED AND LOCATED STEP PLATE IAW SRMS 51-40-11-001-001-A01 AND 51-45-00-001-001-A01.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 34,486 hrs · 24,686 cycles

UNCOMMANDED RUDDER DEFLECTION TO RIGHT. ACFT RETURNED TO DEPARTURE AFTER T/O. REMOVED AND REPLACED THE ALIERON-RUDDER CONTROL PANEL IAW AMM 27-12-10. OPS TESTED AILERON TRIM SYSTEM IAW AMM 27-11-00. OPS TESTED RUDDER TRIM SYSTEM IAW AMM 27-22-00. OPS TESTED GOOD. NO DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,015 hrs · 24,328 cycles

FUSELAGE DAMAGE BETWEEN FS 265 AND FS 280 BETWEEN STR 15R AND 16R. REPAIRED DAMAGED AREA OF FUSELAGE SKIN IAW REO 670-53-11-1277 REV O.

Part: POST — CRACKED (FUSELAGE) · airframe 33,935 hrs · 24,266 cycles

FS 202 RBL 30 POST, HAS A CRACK INDICATION NOTED AT THE UPPER EDGE OF FLANGE, .200 LONG. FAILED NDT. REPAIRED FS 202 RBL 30 POST IAW SRM 53-11-10-201-005-A01.

Part: POST — CRACKED (FUSELAGE) · airframe 33,935 hrs · 24,266 cycles

FS 202 LBL 30 POST, HAS A CRACK INDICATION NOTED AT THE UPPER EDGE OF FLANGE, .250 INCHES LONG. FAILED NDT. REPAIRED FS 202 LBL 30 POST IAW SRM 53-11-10-201-005-A01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,935 hrs · 24,266 cycles

FS 202.75 RT CAP ANGLE HAS A CRACK 1.1 INCHES LONG IN THE RADIUS AT STRINGER 13R. FAILED NDT. REPAIRED FS 202.75 CAP ANGLE IAW BOMBARDIER REO 670-53-11-1264.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,935 hrs · 24,266 cycles

FS 280 STRINGER 3L WAS FOUND TO BE CRACKED. REO 670-53-21-493 AND SERVICE BULLETIN 670BA-53-040 PART A & B INCORPORATED.

Part: FITTING — CORRODED (BS 310) · airframe 31,903 hrs · 22,641 cycles

CLOSING FITTING AT FS 310, LBL42, WL72 IS CORRODED BEYOND ALLOWABLE LIMITS. R & R FWD CLOSING FITTING REF SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-45-00-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 1030) · airframe 31,903 hrs · 22,641 cycles

FLOORBEAM CORRODED AT LBL9, FS 1030, WL 72 BEYOND ALLOWABLE LIMITS. NO CORROSION ALLOWED ON FLOORBEAM, LBL 9 AT FS 1030, WL72 IAW SRM 53-61-43-001-A01. INSTALLED ALL REPAIR PARTS AND C/W REO IN ITS ENTIRETY REF REO 670-53-00-029, REV A 201-08-31, FIG 13. REPAIR ITEMS PN:670-53-00-029-21, QTY 4, -25 QTY 2, -19 QTY, 4, -12 AND -16. FABRICATED IAW REO 670-53-00-029, REV A 8/31/2010. TRIMMED, LOCATED AND DRILLED 1EA BEAM SECTION, PN: 670-53-00-029-164-1, REF REO 670-53-00-029, REV A 2010/08/31, FIGURE 13. PERFORMED CUTOUT OF DAMAGED SECTION OF BEAM REF REO 670-53-00-029, REV A 2010/08/31, FIGURE 13. REPAIR ITEMS, PN: 670-3-00-029-21, QTY 4, -5 QTY 2 AND -19, QTY 4, TRIMED, DRILLED AND LOCATED IAW REO 670-53-00-029, REV A 8-31-2010.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 31,903 hrs · 22,641 cycles

AFT CARGO DOOR SILL CORRODED BEYOND ALLOWABLE LIMITS. AFT CARGO DOOR SILL CORRODED BEYOND LIMITS IAW SRM 53-61-23-101-001-A01. REMOVED AFT CARGO DOOR SILL, FWD, MID AND AFT CHORDS' AND TIE DOWN CLEATS IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. LOCATED AND DRILLED NEW AFT CARGO DOOR SILL REF SRM 51-40-11-001-001-A01. INSTALLED FWD, MID AND AFT CHORDS REF SRM 51-42-06-001-001-A01. INSTALLED AFT CARGO DOOR SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED CARGO DOOR LWR COMING REF SRM 51-41-02-001-001-A01. INSTALLED CARGO DOOR LOWER COMING REF SRM 51-41-02-001-001-A01. INSTALLED 3 EA TIE DOWN CLEATS REF SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (BS 1030) · airframe 31,903 hrs · 22,641 cycles

FLOORBEAM CORRODED AT FS 1030, LBL 27, WL 72. REPAIR ITEMS PN 670-53-00-029-21 QTY 4, -25 QTY , 2, -12, -16 FABRICATED IAW REO 670-53-00-029, REV A 8/31/10. REPAIR ITEMS PN 670-53-00-029-25 QTY, 2, -21 QTY, 4, AND -16 TRIMED, DRILLED AND LOCATED IAW REO 670-53-00-029, REV A 8/31/10. SHIMS QTY 4, PN 670-53-00-029-19. FABRICATED IAW REO 670-53-00-029, REF VA 8/31/10. NO CORROSION ALLOWED ON BEAM IAW SRM 53-61-43-001-A01. COMPLIED WITH REO 670-53-00-029, REV A 8/31/10, FIG 13 IN ITS ENTIRETY. ALL PARTS INSTALLED. CUTOUT BEAM SECTION FROM FS 1021.0 TO FS 1038.0, LBL 27 FLOORBEAM IAW REO 670-53-00-029, REV A 08/31/10. C/W EC/TC EO 700-53-0302 AND GREO 670-53-00-029, REV A DATED 8/31/2010 OR THE FLOORBEAM CORROSION LOCATED AT LBL27.0 AT FS 1013.0 AS WRITTEN.

Part: LIGHT — MISSING (CABIN) · airframe 31,683 hrs · 22,464 cycles

12 CD FWD, EXIT SIGN, EMERGENCY LIGHT STRIP, ARROWS MISSING. REMOVED WORN LIGHT STRIP AND INSTALLED NEW STRIP IAW AMM 33-51-00.

Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 30,758 hrs · 21,729 cycles

FWD CARGO BAY DOOR SEAL RETAINER DAMAGE AT FWD LWR CORNER. COMPLIED WITH EC/TC REO 670-52-35-127, PERMANENT REPAIR. REFER TO EC/TC FOR WORK ACCOMPLISHED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,307 hrs · 21,349 cycles

FOUND SEVERAL OVERWING EXIT LIGHTS INOPERATIVE. REPLACED THE LAMPS AND R & R NR 3 BATTERY PACK AS REQUIRED IAW AMM 33-51-04. OPS CHECKED GOOD AT THIS TIME.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 29,344 hrs · 20,565 cycles

EMERGENCY EXIT LIGHT ON AFT SIDE OF GALLEY 2 FAILS OPS TEST. REMOVED PANEL 232DZ IAW AMM 25-26-07-000-801-A01. SECURED ELECTRICAL CONNECTOR TO GALLEY 2 OK TO CLOSE 232DZ QC55 CLOSED PANEL 232DZ IAW AMM 25-26-07-400-801-A01.

Part: BEAM — CRACKED (LT MLG WW) · airframe 29,349 hrs · 20,571 cycles

ACTUATOR BEAM HOLE HAS CRACK INDICATION, LT MLG. RECEIVED AND COMPLIED WITH REO 670-57-21-759. RECEIVED AND COMPLIED WITH EC/TC 670-57-21-759.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 29,344 hrs · 20,565 cycles

PAX DOOR UPPER SILL ANGLE CORRODED. REMOVED CORRODED MID CAP ANGLE FROM PAX DOOR SURROUND IAW SRM 51-42-21-001-001-A01. INSTALLED NEW MID CAP ANGLE IAW SRM 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 29,344 hrs · 20,565 cycles

PAX DOOR LOWER SILL ANGLE CORRODED. PAX DOOR LWR SILL ANGLE CORRODED BEYOND LIMITS IAW SRM 51-12-00-001-001-A01/TR51-0050 R & R. REMOVED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SILL ANGLE IAW SRM 51-40-11-001-01-A01 TRANSFERED NEW NUTPLATES IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SILL AND, LOWER, TO PAX DOOR THRESHOLD OPENING, REF SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 & DWG SH670-31810, REV Y.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 29,344 hrs · 20,565 cycles

LBL9 SEAT RAIL SEGMENT BS 581-677 CORRODED SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A03, AMM 53-00-49-400-801 AND REO 670-53-00-434.

Part: INTERCOSTAL — CORRODED (BS 319-340) · airframe 29,344 hrs · 20,565 cycles

INTERCOSTAL CORRODED AT STRINGER 20R BETWEEN BS 319.70-340. IAW STRUCTURE INDENTICATION SRM 53-21-23-001-002-A01 INTERCOSTAL ATTACHES TO STR 20RT REMOVE CORROSION AND ENSURE WITHIN LIMITS IAW SRM 53-21-23-101-002-A01. INTERCOSTAL OUT OF LIMITS DUE TO MORE THAN 30 PERCENT OF ITS LENGTH DAMAGED IAW SRM 53-21-23-101-002-A01. REMOVED STR 20R, INTERCOSTAL, 3EA ATTACH CLIPS IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. LOCATED AND STARTED INSTALLING INTERCOSTAL AND STRINGER 20R IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950. INSTALLED INTERCOSTAL AND 3 EA ATTACH CLIPS AT STR 20 IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 374-485) · airframe 29,344 hrs · 20,565 cycles

LBL 9 SEAT RAIL SEGMENT 374-485 CORRODED AT FWD SECTION OF TRACK. REMOVED BAD SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A03. STARTED FABRICATING NEW SEAT TRACK FROM N126-2075 EXTRUSION IAW REO 670-53-00-343, STEP NR 1. COMPLETED FABRICATION OF SEAT TRACK IAW REO 670-53-00-343. INSTALLED SEAT TRACK IAW REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV G.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 29,344 hrs · 20,565 cycles

SERVICE DOOR LOWER SILL UPPER CAP ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. LWR SILL CAP ANGLE FOUND TO BE OUT OF LIMITS IAW SRM 51-12-00-001-001-A01 TR51-0050. REMOVED SERVICE DOOR LWR SILL UPPER CAP ANGLE. INSTALLED UPPER CAP ANGLE TO LWR SILL ANGLE IAW SRM 51-42-06-001-001-A01. COATED, DRILLED, AND DEBURRED ON UPPER CAP ANGLE ON SERVICE DOOR LOWER SILL IAW SRM 51-42-06-001-001-A01. INSTALLED UPPER CAP ANGLE TOP THE LWR SILL ANGLE IAW SRM 51-42-06-001-001-A01.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 29,344 hrs · 20,565 cycles

SERVICE DOOR SILL LOWER ANGLE CORRODED. SERVICE DOOR LWR SILL ANGLE CORRODED OUT OF LIMITS IAW SRM 51-12-00-001-001-A01, TR0050. REMOVED LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED DRILLED & DEBURRED HOLES IN NEW LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01 & SRM 51-40-11-001-001-A01. INSTALLED SERVICE DOOR LWR SILL ANGLE IAW SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 710-761) · airframe 29,344 hrs · 20,565 cycles

LT SIDE SEAT TRACK CORRODED FS 710-761. REPAIRED IAW SRM 53-41-49-101-001-A01.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,344 hrs · 20,565 cycles

LT 280 FLOORBEAM CORRODED. R & R THE FLOORBEAM IAW SB670BA-53-041.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,344 hrs · 20,565 cycles

LT BULKHEAD WEB CORRODED AT BS 280. EVALUATED DAMAGE AND FOUND IT TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A0. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, REV.

Part: DOUBLER — CORRODED (BS 295-310) · airframe 29,344 hrs · 20,565 cycles

LOWER TCAS ANTENNA DOUBLER CORRODED, BS 295 - 310. STRINGER 27. REMOVED LOWER TCAS ANTENNA DOUBLER FS 295-310, STR27, REMOVED STR27, DRILLED UP NEW DOUBLER OK TO INSTALL NEW TCAS DOUBLER INSTALLED TCAS DOUBLER INSTALLED STR27 IAW SRM 51-42-06-001-001-A01 DWG SH670-32364. REMOVED TCAS IAW AMM 34-43-07-000-801-A03. REINSTALLED LOWER TCAS ANTENNA IAW AMM 34-43-07-400-801-A01, BOND CHECK GOOD. PERFORMED OPS TEST OF THE TCAS IAW AMM 34-43-00-710-801-A01. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 29,344 hrs · 20,565 cycles

RT SIDE SEAT TRACK CORRODED, BS 785.15-863. REPAIRED THE SEAT TRACK IAW SRM 53-41-49-101-001-A01.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 29,344 hrs · 20,565 cycles

COCKPIT FLOOR SUPPORT CORRODED. R & R THE FLOOR SUPPORT IAW SB670BA-53-041.

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 29,344 hrs · 20,565 cycles

LT SIDE SEAT TRACK CORRODED FS 379-485. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 29,344 hrs · 20,565 cycles

RT BS 280 FLOORBEAM CORRODED. R & R THE FLOORBEAM IAW SB670BA-53-041.

Part: FLOOR SUPPORT — CORRODED · airframe 29,344 hrs · 20,565 cycles

MAIN AVIONICS BAY CRAWLWAY FLOOR SUPPORT CORRODED AT AFT SIDE OF BS 280 LOWER FRAME. EVALUATED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. R & R THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001, 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 29,344 hrs · 20,565 cycles

LT SIDE SEAT TRACK CORRODED BS 863-969. REPAIRED IAW SRM 53-51-49-101-001-A01.

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 29,344 hrs · 20,565 cycles

RT BULKHEAD WEB CORRODED AT BS 280. EVALUATED DAMAGE AND FOUND IT TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV.

Part: SKIN — DENTED (LT NACELLE) · airframe 29,349 hrs · 20,571 cycles

LEFT NOSE INLET COWL HAS A DENT JUST FWD OF FADEC ACCESS PANEL. COMPLIED WITH PERMANENT REPAIR IAW SRM 54-11-01. CLEANED AREA OF DENT AND MEASURE DAMAGE 2.0" LONG X 1.6" WIDE X 0.075" DEEP FOUND DENT OUT OF LIMITS IAW SRM 54-11-01-101-001-A01.

Part: SKIN — DENTED (BS 169-173) · airframe 29,344 hrs · 20,565 cycles

DENT ON FUSELAGE RT SIDE BETWEEN BS 169-173 STR 1R. REPLACED THE SKIN IAW SRM 51-42-06-001-001-A01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,538 hrs · 19,966 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,754 hrs · 19,366 cycles

EMERGENCY LIGHT BATTERIES DISCHARGED. FOUND EMERGENCY LIGHT SWITCH IN 'ON' POSITION, HAD BEEN SITTING AT GATE FOR 3 HRS. TRIED CHARGING THEM FOR ABOUT 30 MIN. RESULTED IN ONLY ABOUT 15 SEC OF EMERGENCY LIGHT POWER. RESET EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,300 hrs · 19,038 cycles

NR 2 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS & OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 26,572 hrs · 18,516 cycles

EMERGENCY LIGHTS & EXTERIOR EMERGENCY LIGHTS COME ON THEN OFF AFTER ACTIVATION. EMERGENCY BATTERIES CHARGED FOR 30 MINS., OPS CHECKED GOOD IAW AMM 33-51-17.

Part: RETAINER — DENTED (CARGO DOOR SEAL) · airframe 26,309 hrs · 18,313 cycles

FWD CARGO DOOR RETAINER FOR SEAL DENTED ON FWD LOWER CORNER. REPAIRED IAW REO 670-52-35-127 ( REV B ). MAJOR REPAIR IAW GMM 5-3.

Part: LIGHT — UNKNOWN · airframe 25,964 hrs · 18,052 cycles

CEILING EMERGENCY LIGHT OVER ROW 9 INOPERATIVE. PERFORMED OPS CHECK OF EMERGENCY CEILING LIGHTS OF ROW 9 IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,959 hrs · 18,050 cycles

CEILING EMERGENCY LIGHT ABOVE ROW 9 INOPERATIVE. PERFORMED OPS CHECK OF EMERGENCY CELING LIGHTS OF ROW 9 IAW AMM 33-51-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,967 hrs · 17,361 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FWD F/A FLASHLIGHT IAW AMM 25-61-00 AND AIPC 25-61-02, OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED · airframe 24,710 hrs · 17,185 cycles

FLOOR SUPPORT AT FS 280 & RBL 11.16 IS CORRODED AT FLOOR LEVEL. REMOVED RT FLOOR SUPPORT POST AT FS 280 IAW SMR 51-42-21-001-001-A01, 51-42-21-001-001-A01. LOCATED AND DRILLED NEW, SERVICABLE FLOOR POST IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW FLOOR SUPPORT POST AT FS 280 RT SIDE IAW SRM 51-42-06-001-001 AND 51-42-21-001-001.

Part: FLOOR SUPPORT — CRACKED (BS 265-280) · airframe 24,710 hrs · 17,185 cycles

COCKPIT FLOOR SUPPORT AT BS 265-280 & FS 11.16 IS CRACKED IN THE RADIUS. REMOVED FLOOR SUPPORT ANGLE ON RT SIDE AT FS 280 IAW SRM 51-42-006-001-001. LOCATED & DRILLED NEW SUPPORT PN CC670-33199-4 IAW SRM 51-40-11-001-001. INSTALLED NEW SUPPORT PN CC670-33199-4 IAW SRM 51-40-11-001-001.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 24,710 hrs · 17,185 cycles

CRAWL SPACE FLOOR SUPPORT AT FS 280 IS CORRODED. REMOVED CORRODED FLOOR SUPPORT AT 280. DRILLED UP NEW FLOOR SUPPORT BRACKET AT 280 WITH A SERVICEABLE PART IAW SRM 51-42-06-001-001-A01, 51-42-20-001-001-A01. INSTALLED NEW FLOOR SUPPORT BRACKET IAW SRM 51-42-06-001-001-A01 & 51-42-20-001-001-A01.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 24,710 hrs · 17,185 cycles

ASD ICE BREAKER ASSY SUPPORT AFT INTERCOSTAL ANGLE BRACKET CRACKED. REMOVED BRACKET IAW SRM 51-42-06-001-001. PICKED UP ALL EXISTING FASTENER HOLES IN NEW ANGLE BRACKET AND INSTALLED SERVICEABLE ANGLE BRACKET FOR ASD IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-25-16-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 24,710 hrs · 17,185 cycles

SEAT TRACK BS 708 LBL9 IS CORRODED. REMOVED CORROSION AND BLENDED OUT AREA IAW SRM 51-12-00 AND 51-21-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,710 hrs · 17,183 cycles

BS 280 FLOOR BEAM CORRODED IN TEN AREAS. INSTALLED NEW FLOORBEAM AND REPAIR PARTS IAW REO 670-53-11-047.

Part: SEAT TRACK — CORRODED (BS 572-672) · airframe 24,710 hrs · 17,185 cycles

RT SIDEWALL SEAT TRACK BS 572-672 CORRODED IN SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND AMM 53-00-49-400-801 A03.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 24,710 hrs · 17,183 cycles

FLOOR PANEL 221ALF AFT FLOORBEAM ANGLE CORRODED. REMOVED FLOORBEAM ANGLE AT FS 280 IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW FLOOR SUPPORT ANGLE AT FS 280 IAW SRM 51-40-11-001-001-A01. INSTALLED FLOORBEAM ANGLE AT FS 280 IAW SRM 51-42-06-001-001 AND SRM 51-42-21-001-001.

Part: SEAT TRACK — CORRODED (BS 713-761.85) · airframe 24,710 hrs · 17,185 cycles

RT SIDEWALL SEAT TRACK BS 713-761.85 CORRODED SEVERAL AREAS. 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 860-969) · airframe 24,710 hrs · 17,185 cycles

RT SIDEWALL SEAT TRACK BS 860-969 CORRODED SEVERAL AREAS. REMOVED RT SIDEWALL SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 785.15-860) · airframe 24,710 hrs · 17,185 cycles

LT SIDEWALL SEAT TRACK BS 785.15-860 CORRODED AT SEVERAL AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 833.4-976) · airframe 24,710 hrs · 17,185 cycles

SEAT TRACK RBL 9 BS 833.4-976 CORRODED AT SEVERAL AREAS. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 379-466) · airframe 24,710 hrs · 17,185 cycles

RT SIDEWALL SEAT TRACK BS 379-466 CORRODED AT SEVERAL AREAS. REMOVED RT SIDEWALL SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK AT IAW 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (349-485) · airframe 24,710 hrs · 17,184 cycles

SEAT TRACK RBL9 BS 349-485 CORRODED AT FWD AND AFT SECTIONS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 833.4-988) · airframe 24,710 hrs · 17,184 cycles

SEAT TRACK 833.4-988 CORRODED AT SEVERAL AREAS. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 785-860) · airframe 24,710 hrs · 17,185 cycles

RT SIDEWALL SEAT TRACK BS 785.15-860 CORRODED SEVERAL AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 682-833.4) · airframe 24,710 hrs · 17,184 cycles

SEAT TRACK LBL 9 BS 682-833.4 CORRODED AT SEVERAL AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW SRM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 682-833.4) · airframe 24,710 hrs · 17,185 cycles

SEAT TRACK RBL 9 BS 682-833.4 CORRODED AT SEVERAL AREAS. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 708) · airframe 24,710 hrs · 17,185 cycles

LT SIDEWALL SEAT TRACK CORRODED FS 708. REMOVED SEAT TRACK IAW AMM 53-00-49. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 665) · airframe 24,710 hrs · 17,185 cycles

SEAT TRACK RBL CORRODED AT FS 665. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 24,710 hrs · 17,185 cycles

SEAT TRACK RBL 9 BS 485-581 CORRODED AT SEVERAL AREAS. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICEALBE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,710 hrs · 17,183 cycles

FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT IAW 51-42-06-001-001. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06-001-001 & 51-42-21-001-001.

Part: SEAT TRACK — CORRODED (BS 581-682) · airframe 24,710 hrs · 17,183 cycles

SEAT TRACK LBL 9 FS 581 - 682 CORRODED AT SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 693-713) · airframe 24,710 hrs · 17,185 cycles

RT SIDEWALL SEAT TRACK BS 693-713 CORRODED SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND AMM 53-00-49-400-801 A03.

Part: BULKHEAD — CORRODED (BS 280) · airframe 24,710 hrs · 17,183 cycles

LT BS 280 BULKHEAD CORRODED. INSTALLED LT LOWER BULKHEAD WEB AT FS 280 IAW REO 670-53-11-594.

Part: SEAT TRACK — CORRODED (BS 988-1005) · airframe 24,710 hrs · 17,184 cycles

SEAT TRACK LBL9 BS 988 - 1005, CORRODED AT SEVERAL AREAS. SEAT TRACK WORN BEYOND LIMITS. REMOVED AND INSTALLE SEAT TRACKS IAW RIL 2803, REV B.

Part: SEAT TRACK — CORRODED (BS 466-572) · airframe 24,710 hrs · 17,185 cycles

RT SIDEWALL SEAT TRACK BS 466-572 CORRODED AT SEVERAL AREAS. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 1000-1051.3) · airframe 24,710 hrs · 17,183 cycles

RT FLOOR SUPPORT CORRODED BETWEEN FRAMES 1000.00 AND 1051.30. BLENDED AREAS OF CORROSION RT FLOOR SUPPORT BETWEEN FRAMES 1000 & 105130, REF 51-21-06-001-001. COMPLIED WITH REO 670-53-61-930,

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 24,710 hrs · 17,183 cycles

AFT CARGO DOOR LOWER SILL ANGLE CORRODED FROM FS 1000.00 TO 1047.00. REMOVED CORROSION ON LOWER SILL ANGLE IAW SRM 51-21-06-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (BS 1051.3-1070.7) · airframe 24,710 hrs · 17,183 cycles

RT FLOOR SUPPORT CORRODED BETWEEN FS 1051.30 AND FS 1070.70. BLENDED AREAS OF CORROSSION ON RT FLOOR SUPPORT BETWEEN FS 1051.30 & FS 1070.70 REF SRM 51-21-06-001-001. RECEIVED AND COMPLIED WITH REO 670-53-61-930.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 24,394 hrs · 16,933 cycles

CEILING EMERGENCY FLOOD LIGHT MISSING FROM ROW 1 AND 2. REPLACED CEILING EMERGENCY FLOOD LIGHT LENSE IAW 33-51-09.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 23,868 hrs · 16,541 cycles

FWD CABIN FLASHLIGHT INOPERATIVE. REPLACED BATTERIES OF FWD CABIN FLASHLIGHT IAW AMM 25-61-00. NO FURTHER DEFECTS NOTED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,399 hrs · 16,169 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPLACED OF PASSENGER DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,685 hrs · 15,674 cycles

4TH CEILING EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED EMERGENCY FLOODLIGHT. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,685 hrs · 15,674 cycles

6TH CEILING EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED EMERGENCY FLOODLIGHT, OPS CHECKED GOOD IAW AMM 33-51-00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,217 hrs · 15,354 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. PAX DOOR REPLACED IAW REO 670-52-11-619.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,217 hrs · 15,354 cycles

PAX DOOR CRACK AT DRAG ANGLE AFT SIDE CENTER. REPAIRED IAW REO 670-52-11-619.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,056 hrs · 15,241 cycles

PAX DOOR DRAG ANGLE CRACKED AFT SIDE CENTER. COMPLIED WITH REO 670-52-11-287 REV A, SHEET 5, ZONE 3, ITEMS 1-7. CRACK MEASURED 1 INCH.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,050 hrs · 15,237 cycles

PAX DOOR DRAG ANGLE CRACKED, AFT SIDE CENTER. REPAIRED IAW REO 670-52-11-287, REV A, SHEET 5.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,050 hrs · 15,237 cycles

PAX DOOR DRAG ANGLE CRACKED, AFT SIDE, CENTER. COMPLIED WITH REO 670-52-11-287, REV A, SHEET 5, ZONE 3, ITEMS 1-7 CRACK MEASURES 1INCH.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 20,755 hrs · 14,333 cycles

MEGAPHONE IN OVERHEAD BIN INOP. R & R MEGAPHONE IAW AMM 25-61-14. R & R MEGAPHONE IAW AMM 25-61-14. (CLOSED)

Part: CROSSBEAM — CORRODED (BS 280) · airframe 19,869 hrs · 13,734 cycles

CROSSBEAM CORRODED. INSTALLED 280 CROSSBEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

CORROSION FOUND AT FS 364.00 AND LBL2. REMOVED CORRORSION. REPAIRED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-23-101-003-A01 AND 51-12-00-001-001-A01. PERFORMED LIQUID PENRTRANT INSP TYPE I, METHOD C REPAIR AREA FS 364.00 AT LBL 2 IAW SRM 51-12-00-001-001-A01 AND MAC NDT INSP PROCEDURES PT-1 NO INDICATIONS FOUND AT THIS TIME. MINOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

CORROSION FOUND ON FRAME FS 319.70 AT STR 27. REMOVED CORROSION. REPAIRED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-A01 AND 51-12-00-001-001-A01. PERFORMED FLUORESCENT LIQUID PENETRANT INSP ON REPAIR AREA FS 319.70 AT STR27 IAW SRM 51-12-00-001-001-A01 AND NDT INSP PROCEDURES PT-1. NO INDICATIONS NOTED AT THIS TIME. MINOR REPAIR.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

FS 349 CROSSBEAM HAS TWO CORRODED NUTPLATES/RIVETS ON RT SIDE AND ONE ON THE LEFT SIDE. R & R NUTPLATE ON CROSSBEAM FS 349 AT RBL 17 AND LBL 17 IAW SRM 51-45-00-001-001-A01. THIS IS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

SIDE SEAT RAIL STGR 15L, LT WALL SEAT TRACK, CORRODED FROM FS 379.00 TO FS 761.85. REMOVED SIDE SEAT RAILS IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49.

Part: WEB — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

FS 280.00 RT WEB, LOWER LT SECTION CORRODED. BLENDED CORROSION ON FS 280 RT WEB, DAMAGE FROM CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. INSTALLED RT LOWER WEB AT FS250 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

FRAME FLANGE HAS CORROSION FS 295, STR 27. REPAIR AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-A01 AND 51-12-00-001-001-A01. (LT) 2 NDT REQUIRED INSTALL RIVETS AND RESTORE FINISH. PERFORMED FLUORESCENT LIQUID PENETRANT INSP ON FRAME FLANGE FS 295.00, STR 27 IAW SRM 5112-00-001-001-A01 AND NDT INSP PROCEDURES PT-1 NO INDICATIONS NOTED AT THIS TIME. INSTALLATION OF RIVETS AND RESTORATION OF FINISH REQUIRED. INSTALLED RIVETS AND RESTORED FINISH IAE SRM 51-42-06-001-001-A01 & 51-25-16-001-001-A01. THIS IS A MINOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

FRAME FLANGE HAS CORROSION FS 310, STR 27. REPAIRED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-A01 AND 51-12-00-001-001-A01. PERFORMED FLUORESCENT LIQUID PENETRANT INSP ON FRAME FLANGE FS 310.00, STR 27 IAW SRM 51-12-00-001-001-A01 AND MAC NDT INSP PROCEDURES PT-1 NO INDICATIONS NOTED AT THIS TIME.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

LT FLOORBEAM FWD SECTION AT FS 280.00 JOINT HAS CORROSION.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

CROSSBEAM AT FS 409 HAS ONE CORRODED NUTPLATE/RIVETS RT SIDE NEAR WALL. REMOVED NUTPLATE & RIVETS, INSPECTED AREA, FOUND NO FURTHER CORROSION, INSTALLED NEW RIVETS AND EXISTING NUTPLATE IAW SRM 51-42-10-001-001-A01. THIS IS A MINOR REPAIR.

Part: WEB — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

FS 280.00 LT WEB, LOWER RT SECTION CORRODED. WEB IS CORRODED OUT OF ALLOWABLE DAMAGE LIMITS SRM 53-11-10-201-003-A01. REMOVED LT LOWER 280 WEB AND TRANSFERRED HOLES TO NEW SERVICABLE PART IAW SRM 51-42-06-001-001-A01. INSTALLED LT LOWER 280 WEB IAW SRM 51-42-06-001-001-A01, 51-42-13-00-001-001-A01, 51-42-21-00-001-001-A01.

Part: SUPPORT — CORRODED (DOOR) · airframe 19,869 hrs · 13,734 cycles

FS 280 RT DOOR SUPPORT CORRODED. REMOVED LIGHT CORROSION ON RT DOOR SUPPORT IAW SRM 51-21-06-001-001-A01. MINOR REPAIR IAW SOP 5702.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 19,869 hrs · 13,734 cycles

FS 280 CROSS BEAM CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-06-101-008-A01. REMOVED 280 CROSS BEAM IAW SRM 51-42-06-001-001-A01. INSTALLED IAW SRM 51-40-11-001-001-A01.

Part: SUPPORT — CORRODED (PAX DOOR) · airframe 19,869 hrs · 13,734 cycles

FS 280 LT DOOR SUPPORT CORRODED. REMOVED LIGHT CORROSION ON LT DOOR SUPPORT IAW SRM 51-21-06-001-001-A01. MINOR REPAIR.

Part: PLACARD — MISSING (ESCAPE HATCH) · airframe 19,869 hrs · 13,734 cycles

CREW ESCAPE HATCH EXTERNAL PAINT PEELING AND PLACARDS ARE WORN AND MISSING. APPLIED GREY & WHITE TOP COAT TO ESCAPE HATCH EXTERNAL SKIN IAW AMM 11-22-01-992-801-AO1. INSTALLED NEW SILKSCREEN PLACARDS ON CREW ESCAPE HATCH IAW AMM 11-20-60-11-400-801-A01.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 18,627 hrs · 12,823 cycles

MAIN CABIN INTERIOR; FORWARD LT CLOSET, AFT FACE OF EMERGENCY EXIT SIGN HAS CRACKED LENS. INSTALLED A SERVICABLE LENS IAW AMM CHAP 33-27-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,627 hrs · 12,823 cycles

FUSELAGE EXTERIOR- LT ESCAPE HATCH EMERGENCY LIGHT INOP AFT OF HATCH. REMOVED AND REPLACED LAMP ON LT ESCAPE HATCH EMERGENCY LIGHT AFT OF HATCH REMOVED AND CHECKED BATTERY PACK AND FUSES OPS CHECK OF IAW AMM 33-50-00.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 18,600 hrs · 12,805 cycles

MAIN CABIN-L1 DOOR THRESHOLD ANGLE HAS CORROSION. R & R ANGLE PART NR SH670-31825-7 IAW SRM 51-41-02 OPS CHECK GOOD IAW SRM MM 52-11-00.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 18,478 hrs · 12,707 cycles

EMERGENCY LIGHT CYCLING ON AND OFF.

Part: BLADE — LACK OF LUBE (LT ENGINE) · airframe 18,193 hrs · 12,487 cycles

EXESSIVE VIBRATION IN LT ENGINE DURING CLIMB OUT. ( 1.8 ) AT CLIMB POWER . VIBRATION COULD BE FELT IN COCKPIT (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) REMOVED AND REINSTALLED NR 1 ENG. FAN BLADES IAW AMM 72-21-02. LUBED FAN BLADES IAW ESM 72-00-21. OPS CHECK AND ENGINE VIBRATION CHECK IAW MM ENGINE RUN, OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,865 hrs · 12,255 cycles

NR 1 CABIN EMERGENCY CEILING LIGHT INOP. (CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS). REMOVED AND REPLACED NR 1 EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-17 OPS CHECK GOOD OK FOR SERVICE DEFER CLEARED PLACARD REMOVED.

Part: PLACARD — MISSING (PAX DOOR) · airframe 17,648 hrs · 12,090 cycles

"EXIT" PLACARD ON MAIN BOARDING DOOR MISSING.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,986 hrs · 11,578 cycles

LEFT AND RIGHT OVERWING EMERGENCY EXIT LWR FLOOD LIGHTS HAVE SEVERAL BULBS BURNED OUT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 15,398 hrs · 10,366 cycles

F/A REPORTS FLASHLIGHTS NEED BATTERIES.

Part: STRUCTURE — CORRODED (CARGO BAY) · airframe 15,320 hrs · 10,304 cycles

CORROSION FOUND AROUND NUTPLATES IN AFT CARGO BELOW FLOOR BOARD AT DOOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

CORROSION ON FS 501 TO FS 517 ON LBL FLOORBEAM. BLENDED OUT CORROSION ON FLOORBEAM CAP FS 501 - FS517 LBL9 PER CRJ 700 SRM 51-21-06. LBL9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00391 FOR THE REMOVAL AND REPLACEMENT OF LBL9 FLOORBEAM FS485-565.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

CORROSION FOUND FS 517 TO FS 533 LBL 9 FLOOR BEAM CAP. BLENDED CORROSION ON FLOORBEAM CAP FS517 - FS533 LBL9 PERCRJ 700 SRM 51-21-06. LBL9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00391 FOR THE REMOVAL AND REPLACEMENT OF LBL9 FLOORBEAM FS485-565.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOOR SUPPORT CAP HAS CORROSION AT LBL 9 BETWEEN FS 485.00 AND FS 501.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS485.00 & FS501.00 IAW CRJ 700 SRM 51-21-06. REQUIRES THICKNESS CHECK. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00391 FOR BEAM REPLACEMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT RBL 9 BETWEEN FS 517.00 AND FS 533.00. BLENDED CORROSION ON FLOORBEAM CAP ON RBL 9 BETWEEN FS 517.00 & FS 533.00 IAW CRJ 700 SRM 51-21-06. REQUIRES THICKNESS CHECK. RBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00390 FOR BEAM REPLACEMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 469.00 AND FS 485.00. REMOVED AND REPLACED FLOORBEAM AT FS 477 TO 573 PER REO 670-53-00-172 REV A, CRJ 700 SRM 51-21-06, CRJ 700 SRM 51-11-00, REO 670-53-00-029, CRJ 700 NDTM 51-20-006, CRJ 700 51-40-11, CRJ 700 SRM 51-21-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 565.00 AND FS 581.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS565.00 & 581.00 IAW CRJ 700 SRM 51-21-06. FWD & AFT LBL9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00391 + N/R-00395 FOR BEAM REPLACEMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 AT FS 708.00. COMPLIED WITH (BLENDING, NDT, AND FINISH RESTORATION) OF REO 670-52-00-172 ON FLOOR SUPPORT BEAM LOCATED AT FS 708, LBL9, WL73 REFER TO ATTACHED M-234 FOR WORK ACCOMPLISHED. BLENDED FLOORBEAM CAP LBL 9 FS 708.00 IAW CRJ 700 SRM 51-21-06. PERFORMED EDDY CURRENT INSPECTION OF BLEND AREA AT LBL9, FS 708 PER REO 670-53-00-172 I/A/W CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOOR SEAT TRACKS AT LBL AND RBL 9 BETWEEN FS 581.00 AND FS 677.00 BOTTOM SIDE CORRODED. REPLACED LBL 9 FLOOR SEAT TRACKS BETWEEN FS581.00 AND FS677.00 IAW CRJ700 AMM 53-00-49-400-801. NO DEFECTS NOTED. REWORKED AND REINSTALLED RBL 9 FLOOR SEAT TRACKS BETWEEN FS581.00 AND FS677.00. REWORK WITHIN ALLOWABLE DAMAGE LIMITS PER CRJ 700 SRM 53-31-49. REINSTALLATION IAW CRJ700 AMM 53-00-49-400-801. NO DEFECTS NOTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 533.00 AND FS 549.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS533.00 & FS549.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOOR BEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R -00391 FOR BEAM REPLACEMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 597.00 AND FS 613.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS597.00 & FS613.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00395 FOR BEAM REPLACEMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 645.00 AND FS 661.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS 645.00 & FS 661.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMITS CORROSION. REFER TO W/O 105591 N/R-00395 FOR BEAM REPLACEMENT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT 280 FRAME UPON FURTHER INVESTIGATION FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED RT FS280 BEAM IAW CRJ 700 SRM 51-20-006, 51-24-28, 51-21-00, 51-42-06, 51-42-00, 51-42-21, 51-42-13, IS670531120026 AND IS670531100026, AD KMT ORD 10048994, BAT 372037 REF TO M-234 FORM FOR WORK ACCOMPLISHED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT 280 FRAME UPON FURTHER INVESTIGATION FOUND CORROSION TO BE OUT OF LIMITS. LT 280 BEAM REMOVED AND REPLACED PER CRJ700 SRM 51-42-06 AND 51-42-21, PER MODSUM IS67053110026,SRM 51-42-13, SB670BA-53-026, CRJ 700 SRM 51-21-16 AND CRJ 700 SRM 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

REMOVE CABIN FLOOR SEAT TRACKS FROM FS 581.00 AND AFT (CORROSION FOUND UNDER ALL SEAT TRACKS FWD OF FS 581.00 WITH ALLUM CAPS). REMOVED CABIN FLOOR SEAT TRACKS FROM FS581.00 AND AFT IAW CRJ 700 AMM 53-00-49. VK7025976. REINSTALLED FLOOR SEAT TRACKS LEFT SIDE OF CENTER AISLE FROM VICINITY OF FS830 AFT, AND ALL TRACKS RIGHT SIDE OF CENTER AISLE FROM FS581.00 AFT IAW CRJ700 AMM 53-00-49. INSTALLED CABIN SEAT FLOOR TRACKS ON LT SIDE OF CENTER AISLE FROM FS581.00 AFT TO FS830.40 IAW CRJ700 AMM 53-00-49.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 581.00 AND FS 597.00. LBL 9 FLOORBEAM REPLACED BETWEEN FS 572.00 & 686. WORK DONE IAW CRJ 700 SRM 51-21-06, CRJ 700 SRM 51-11-00. LBL 9 FLOOR BEAM REPLACED REFER TO W/O 105591 N/R-00401 FOR WORK ACCOMPLISHED .

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 661.00 AND FS 677.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS 661.00 & FS 677.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00395 FOR BEAM REPLACEMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 613.00 AND FS 629.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS613.00 & FS629.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION . REFER TO W/O 105591 N/R-00395 FOR BEAM REPLACEMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 629.00 AND FS 645.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS629.00 & FS645.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00395 FOR BEAM REPLACEMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FLOORBEAM CAP HAS CORROSION AT RBL 9 BETWEEN FS 485.00 AND FS 501.00. FLOORBEAM RBL 9 FS 485 THRU 565 REMOVED AND REPLACED PER REO 670-53-00-172, REO 670-53-00-029, CRJ 700 SRM 51-21-06, CRJ 700 SRM 51-11-00, CRJ 700 NDTM 51-20-006, REO 670-53-31-124.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

CORROSION DAMAGE FS 280 BULKHEAD LOWER ANGLE AT ENTRANCE TO FLT COMPT RBL 10. CORROSION AREAS OF RBL 10 OF FS 280 BULKHEAD WERE TREATED IAW REO 670-53-11-370,REO 670-53-11-369,REO 670-53-11-3698 SRM 51-42-06,51-11-00 .025, NDTM 51-20-06.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

CORROSION ON FS 280 BEAM CENTER SPLICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

CORROSION DAMAGE FS 280 BULKHEAD LOWER ANGLE AT ENTRANCE TO FLT COMPT LBL 10. CORROSION LBL 10 OF FS 280 BULKHEAD WAS TREATED BY ACCOMPLISHING DAMAGE 1 SPOT A OF REO 670-53-11-370. REINSTALLED RIVETS AT LBL 10 280 DOOR POST 13" FROM 280 BEAM, ALL WORK IAW CRJ 700 SRM 51-42-06. MEASURED BLENDED AREA OF FOUND TO BE .010" OF MATERIAL REMOVED. WORK DONE IAW CRJ 700 SRM 51-11-00, NDTM 51-20-06 SUBMITTED DAMAGE TO CRC.

Part: FRAME — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

CORROSION AT FWD SIDE OF THE BELLY FRAME LOWER FLANGE AT FS 317.00 BETWEEN STR 27 AND 26R. REMOVED CORROSION AT FWD SIDE OF THE BELLY FRAME LOWER FLANGE AT FS 317.00 BETWEEN STR 27 AND 26R IAW SRM 51-21-06 SKIN THICKNESS WITHIN LIMITS. ALODINED PRIMED AND PAINTED REWORKED AREA IAW SRM 51-21-16. WORK COMPLETED RG7026456.

Part: FRAME — CORRODED (BS 349) · airframe 15,320 hrs · 10,304 cycles

CORROSION AT AFT SIDE OF THE BELLY FRAME LOWER FLANGE AT FS 349.00 BETWEEN STR 27 AND 26R. REMOVED CORROSION AT AFT SIDE OF THE BELLY FRAME LOWER FLANGE AT FS 349.00 BETWEEN STR 27 AND 26R IAW SRM 51-21-06 SKIN THICKNESS WITHIN LIMITS. ALODINED, PRIMED AND PAINTED REWORKED AREA IAW SRM 51-21-16. WORK COMPLETED RG7026456.

Part: STRAP — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

CORROSION AT BELLY STRAP JUST AFT OF FS 280.00 BETWEEN STR 26L TO 26R. STARTED TO REMOVE PAINT AND SOLID RIVITS FROM STRAP JUST AFT OF FS280 FRAME IN BELLY OF A/C AT STR 27 TO STR 26R ALL WORK IAW CRJ 700 SRM 51-42-06 AND 51-21-06, CRJ 700 NDTM 51-20-004, REO 670-53-21-421 PER CRJ 700 NDTM 51-20-006, CRJ 700 SRM 51-21-16, CRJ 700 SRM 51-21-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT FLOOR SEAT RAIL FS 379.00 TO 485.00 HAS CORROSION DAMAGE (MARKED). REMOVED LHS FLOOR SEAT RAIL FS379.00 TO 485 WORK DONE IAW CRJ 700 SRM 51-41-02. INSTALLED NEW SEAT RAIL PER CRJ 700 AMM 53-00-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT FLOOR SEAT RAIL FS 581.00 TO FS 693.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .011, WITHIN LIMITS PER SRM 53-31-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT SIDEWALL SEAT RAIL FS 785.15.00 TO FS 863.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .011, WITHIN LIMITS PER SRM 53-41-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT SIDEWALL SEAT RAIL FS 708.00 TO FS 761.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .005 WITH IN LIMITS PER SRM 53-41-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT SIDEWALL SEAT RAIL FS 485.00 TO FS 565.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .008, WITHIN LIMITS PER SRM 53-31-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT SIDEWALL SEAT RAIL FS 565.00 TO FS 661.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .010, WITH IN LIMITS PER SRM 53-31-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT SIDEWALL SEAT RAIL FS 677.00 TO FS 708.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .015, WITHIN LIMITS PER SRM 53-41-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT FLOOR SEAT RAIL FS 830.40 TO 985.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009 WITHIN LIMITS PER SRM 53-51-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT SIDEWALL SEAT RAIL FS 565.00 TO FS 661.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .005,WITHIN LIMITS PER SRM 53-31-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT FLOOR SEAT RAIL FS 581.00 TO FS 693.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009, WITHIN LIMITS PER SRM 53-31-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT SIDEWALL SEAT RAIL FS 863.00 TO FS 969.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION, MAX DEPTH .006 WITH IN LIMITS PER SRM 53-51-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT FLOOR SEAT RAIL FS 830.40 TO 985.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .010, WITHIN LIMITS PER SRM 53-51-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT SIDEWALL SEAT RAIL FS 379.00 TO FS 485.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009, WITHIN LIMITS PER SRM 53-31-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT SIDEWALL SEAT RAIL FS 708.00 TO FS 761.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .013, WITHIN LIMITS PER SRM 53-41-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT FLOOR SEAT RAIL FS 693.00 TO FS 847.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .014 , WITHIN LIMITS PER SRM 53-41-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT SIDEWALL SEAT RAIL FS 863.00 TO FS 969.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .007, WITH IN LIMITS PER SRM 53-51-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT SIDEWALL SEAT RAIL FS 785.15.00 TO FS 863.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .010 WITHIN LIMITS PER SRM 53-41-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT FLOOR SEAT RAIL FS 349.00 TO 485.00 HAS CORROSION DAMAGE (MARKED). INSTALLED SEAT TRACK P/N SH670-32159-1 PER AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT FLOOR SEAT RAIL FS 485.00 TO FS 581.00 HAS CORROSION DAMAGE (MARKED). REPLACED SEAT TRACK P/N SH670-33426-1 PER AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT SIDEWALL SEAT RAIL FS 379.00 TO FS 485.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .015, WITHIN LIMITS PER SRM 53-21-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT SIDEWALL SEAT RAIL FS 485.00 TO FS 565.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .005, WITHIN LIMITS PER SRM 53-31-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT FLOOR SEAT RAIL FS 693.00 TO FS 847.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .015 , WITHIN LIMITS PER SRM 53-41-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT SIDEWALL SEAT RAIL FS 677.00 TO FS 708.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009, WITHIN LIMITS PER SRM 53-41-49.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT FLOOR SEAT RAIL FS 485.00 TO FS 581.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009 ,WITH IN LIMITS PER SRM 53-31-49.

Part: MECHANISM — BINDING (PAX DOOR) · airframe 10,790 hrs · 7,243 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE AND FEELS AS THOUGH LOCKING MECHANISM IS BINDING.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 15,320 hrs · 10,304 cycles

PAX DOOR INNER FRAME DOUBLER (PN 600-31922-4) AT FS 338.90 CRACKED (INBD OF 318 FRAME, ACCESS PNL 832AR)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

FWD FLOOR ANGLE OF FS 280 LBL9 - RBL 9 CORRODED. REMOVED FWD FLOOR ANGLE OF FS280 LBL9-RBL9 DUE TO CORROSION BEING OUT OF LIMITS. ALL WORK DONE IAW CRJ 700 SRM 51-42-06, SB670-53-026, CRJ 700 51-42-21

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,320 hrs · 10,304 cycles

LT 280 FLOORBEAM, UPPER SURFACE HAS MINOR CORROSION. REMOVED SURFACE CORROSION ON LT 280 FLOORBEAM, UPPER SURFACE PER SRM 51-12-00. PERFORMED UT THICKNESS MEASUREMENT OF BLEND AREA ON LEFT 280 FLOORBEAM IAW NDTM 51-20-004.

Part: WEB — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT 280 WEB, AFT SIDE HAS MINOR CORROSION. STARTED REMOVING CORROSION ON AFT SIDE OF RT BS 280 WEB PER SRM 51-12-00 AND REMOVED 4 FASTENERS FROM AFT INBOARD CORNER. REMOVED REMAINING CORROSION ON AFT FACE OF RT BS 280 WEB IAW SRM 51-12-00. MECHANICALLY MEASURED BLENDED AREAS ABOVE BS 280 FLOORBEAM, .005 MAX MATERIAL REMOVED. ALL BLENDS WITHIN LIMITS ON RT AFT SIDE OF BS 280 WEB PER SRM 53-11-10. REPLACED REMOVED RIVETS ON RT FS 280 WEB AND RESTORED A023 FINISH IAW SRM 51-42-06, SRM 51-42-16.

Part: WEB — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

LT 280 WEB, AFT SIDE HAS MINOR CORROSION. REMOVED MINOR CORROSION ON LT WEB AFT SURFACE PER CRJ700 SRM 51-12-00. REMOVED 4 RIVETS ON LOWER INBOARD CORNER. MEASURED BLENDED AREA OF 280 WEB AT 2 TO 6 INCHES OUTBOARD OF LBL 9 DEPTH AT .005 IAW SRM 53-11-10. RE-MEASURED BLENDED AREAS OF THE LT 280 WEB AFT SIDE MECHANICALLY. MAX MATERIAL REMOVED IS .005. BLENDED AREA WITH IN LIMITS PER SRM 53-11-10. REPLACED REMOVED RIVETS ON LT FS 280 WEB AND RESTORED A023 FINISH IAW SRM 51-42-06, SRM 51-42-16.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,320 hrs · 10,304 cycles

RT 280 BEAM HAS MINOR CORROSION ON UPPER SURFACE. REMOVED MINOR CORROSION ON UPPER SURFACE OF RT 280 FLOORBEAM PER SRM 51-12-00. PERFORMED UT THICKNESS MEASUREMENT OF BLEND AREA ON RT 280 FLOORBEAM IAW NDTM 51-20-004.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 15,320 hrs · 10,304 cycles

RT VERTICAL FWD DRAG ANGLE APPEARS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF RIGHT FORWARD VERTICAL STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE CONFIRMED CRACKED AND MARKED. RT DRAG ANGLE REPAIRED PER REO 670-55-31-018.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 15,320 hrs · 10,304 cycles

LT VERTICAL FWD DRAG ANGLE APPEARS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF LEFT FORWARD VERTICAL STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE CONFIRMED CRACKED AND MARKED. LT DRAG ANGLE REPAIRED PER REO 670-55-31-018. REMOVED PAINT IAW CRJ SRM 51-12-00, VERIFIED CORROSION TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-00-00 FIG 102. REPAIR OR REPLACEMENT REQUIRED. REMOVED FLOOR LANDING PLATE, LOCATED AND DRILLED NEW PLATE FS 559+112 - 621 IAW CRJ 200 SRM 51-42-06. CUT NEW FLOOR LANDING PLATE IAW BOMBARDIER REO 601R-53-61-593A STEPS 1 AND 2.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,300 hrs · 9,521 cycles

CEILING EMERGENCY LIGHTS NR 4 AND 5 INOPERATIVE. REMOVED AND REPLACED CEILING EMERGENCY LIGHTS NR 4 AND 5 LIGHT BULBS. OPS CHECK GOOD. (B)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,300 hrs · 9,521 cycles

EMERGENCY LIGHT FWD OF RT OVERWING EMERGENCY EXIT HAS SEVERAL INOP BULBS. REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT FWD FLOOR LEVEL EMERGENCY FLOOD LIGHT BULBS. OPS CHECK GOOD. (B)

Part: PLACARD — WORN (PAX DOOR) · airframe 11,898 hrs · 7,846 cycles

PAX DOOR EXIT PLACARD WORN PER FA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,794 hrs · 7,774 cycles

AFTMOST CABIN CEILING EMERGENCY LIGHT INOP.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,410 hrs · 7,478 cycles

LEFT LOWER FS 280 WEB HAS CORROSION. REPAIRED IAW EO670-53-11-052, REO 670-53-11-052, AND CRJ SRM 51-25-16.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,410 hrs · 7,478 cycles

AFT DRAG ANGLE ON PAX DOOR IS CRACKED.

Part: INTERCOSTAL — CRACKED (WING) · airframe 11,410 hrs · 7,478 cycles

RIGHT I/B SLAT CLOSING PLATE AND INTERCOSTAL CRACKED. LOCATED NEW SERVICEABLE INTERCOASTAL AND INSTALLED WITH SOLID FASTENERS TO SERVICEABLE CLOSING PLATE IAW CRJ 700 SRM 51-42-06. TRIMMED SERVICEABLE CLOSING PLATE TO FIT. OKAY TO PAINT. PRIME AND PAINTED, IAW CRJ SRM 51-25-16. REQUIRES INSTALLATION; CLEARANCE FIT, TO COMPLETE. INSTALLED RT TELESCOPIC DUCT CLOSING PLATE IAW CRJ 700 AMM 27-81-00. CLEARENCE AND FIT CHECK GOOD.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 11,410 hrs · 7,478 cycles

OUTER PAX DOOR HANDLE IS CRACKED. [07-24-07] REPAIRED IAW AMM 52-11-03, AMM 52-11-02, AND AMM 52-11-03. NO DEFECTS NOTED AT THIS TIME.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,410 hrs · 7,478 cycles

RIGHT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REPAIRED IAW ALL SRM`S AND REO`S.

Part: WEB — CORRODED (FUSELAGE) · airframe 11,410 hrs · 7,478 cycles

RIGHT LOWER FS 280 WEB HAS CORROSION. REPAIRED IAW EO670-53-11-052, REO 670-53-11-052, AND CRJ SRM 51-25-16.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 11,410 hrs · 7,478 cycles

LEFT FS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. [SUP 06-07-07] REPAIRED IAW ALL SRM`S AND REO`S.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,410 hrs · 7,478 cycles

FS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. REPAIRED IAW ALL SRM`S AND REO`S.

Part: MECHANISM — LACK OF LUBE (SERVICE DOOR) · airframe 11,410 hrs · 7,478 cycles

SERVICE DOOR FAILS PULL CHECK FOR FORCE REQUIRED TO OPEN DOOR. FORCE EXCEEDS 35LB MAXIMUM FORCE. LUBRICATED GALLEY SERVICE DOOR IAW CRJ 700 AMM 12-20-52. RECHECK - FUNCTIONAL TEST FOR FORCE REQUIRED. OPS CHECK GOOD, WITHIN LIMITS IAW CRJ 700 AMM 52-41-00. SUPPLEMENTAL- SDR CLOSED 06/05/07.

Part: DOOR — UNKNOWN (EMERGENCY EXIT) · airframe 11,410 hrs · 7,478 cycles

FOUND LEFT OVERWING EMERGENCY EXIT DIFFICULT TO OPEN WHILE PERFORMING FUNCTIONAL TEST OF LEFT OVERWING EMERGENCY EXIT. [SUP 06-07-07] PERFORMED LUBE TASK IAW CRJ 700 AMM 12-20-52-640-802-A01 PERFORMED. OPS CHECK IAW CRJ 700 AMM 52-21-00. NO DEFECTS FOUND AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,218 hrs · 6,708 cycles

THE MOST AFT, RT OVERWING EMERGENCY LIGHT IS INOP. (EXTERIOR EMERGENCY LIGHTS - DAY OPERATIONS ONLY).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,016 hrs · 5,962 cycles

AFT CEILING EMERGENCY LIGHT IS INOP

Part: PLACARD — UNKNOWN (CABIN) · airframe 8,607 hrs · 5,701 cycles

ASD EXIT PLACARD NEEDS REPLACED.

Part: LAMP — BURNED OUT (FUSELAGE)

DURING A GROUND INSPECTION, THE RT SIDE CENTER OVER WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT SIDE CENTER OVER WING EMERGENCY LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: HANDLE — CORRODED (ESCAPE HATCH)

DURING A HANGAR INSPECTION IN MCN, THE CREW ESCAPE HATCH OUTER HANDLE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CREW ESCAPE HATCH OUTER HANDLE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT SIDE WALL SEAT TRACKS, FROM FS 349 TO FS 985, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED CORROSION FROM THE LEFT SIDE WALL SEAT TRACKS, FROM FS 349 TO 985, IAW BOMBARDIER REO 670-53-00-013. REMOVED AND REPLACED THE LEFT SIDE WALL SEAT TRACKS FROM FS 784 THROUGH FS 861 IAW BOMBARDIER REO 670-53-00-013. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE, AT THE PASSENGER DOOR, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT ANGLE, AT THE PASSENGER DOOR IAW CRJ SRM 51-41-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK, THE SEAT TRACKS, FROM FS349 TO FS 985, RBL 9, WERE FOUND TO BE CORRODED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MATENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: SEAT TRACK — CORRODED (BS 349-985)

DURING A C-CHECK IN MCN, THE SEAT TRACKS AT FS 349-985, LBL 9, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS AT FS 349-985, LBL 9, IAW CRJ 700 AMM 53-00-49. (M)

Part: SEAT TRACK — CORRODED (BS 349-985)

DURING A C-CHECK IN MCN, THE RIGHT SIDEWALL SEAT TRACKS, FROM FS 349 TO FS 985, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED CORROSION FROM THE RIGHT SIDEWALL SEAT TRACKS, FROM FS 349 TO FS 985, IAW BOMBARDIER REO 670-53-00-013. (M)

Part: LENS — CRACKED (CABIN)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS, OVER THE SERVICE DOOR, WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LENS IN THE EMERGENCY EXIT LIGHT, OVER THE SERVICE DOOR. (K)

Part: LAMP — BURNED OUT (CABIN)

DURING A C-CHECK, THE AFT GALLEY FLOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE WILL REMOVE AND REPLACE THE LAMP IN THE AFT GALLEY FLOOR EMERGENCY EXIT LIGHT. (K)

Part: BULKHEAD — CORRODED (BS 280)

DURING A C-CHECK IN MCN, THE LEFT SIDE AND RIGHT SIDE FS 280 BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT SIDE AND RIGHT SIDE FS 280 BULKHEAD WEB IAW BOMBARDIER REO 670-53-11-052. (M)

Part: STEP — MISSING (COCKPIT SEAT)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY STEP ON THE CO-PILOT'S SEAT BACK WAS FOUND MISSING. MAINTENANCE REPLACED THE EMERGENCY STEP ON THE CO-PILOTS SEAT BACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: TORQUE LINK — DISCONNECTED (NLG)

DURING CLIMB OUT, THE CREW SELECTED GEAR UP AND THE GEAR HANDLE WOULD NOT MOVE FROM THE DOWN POSITION. SEVERAL SECONDS LATER THEY RECEIVED A WEIGHT ON WHEELS INPUT CAUTION MESSAGE FOLLOWED BY A NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT RETURNED TO PHF. NORFOLK APPROACH DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY BACK IN PHF. MAINTENANCE FOUND THE (NLG) UPPER AND LOWER TORQUE LINK ASSEMBLIES DISCONNECTED AND RECONNECTED THEM. OPERATIONAL CHECKS GOOD DURING GROUND TAXI CHECK. AIRCRAFT OK FOR SERVICE.

Part: CONTROLLER — FAILED (SLATS)

DURING APPROACH THE CREW SELECTED SLATS TO 8 DEGREES AND THEN RECEIVED SLAT FAIL CAUTION AND SLATS MECHANICAL JAMMED MESSAGES. AN EMERGENCY WAS NOT DECLARED. THE AIRCRAFT DIVERTED TO ONT AND LANDED SAFELY. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE SLATS WITHOUT ANY DEFECTS NOTED AND HAD THE CREW POWER DOWN AND UP THE AIRCRAFT WHICH CLEARED THE FAULT MESSAGES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: MOUNT — CRACKED (PICCOLO TUBE)

DURING A GROUND INSPECTION IN ATL, THE LT INBOARD TELESCOPIC LEADING EDGE ANTI-ICE SUPPLY MOUNT ON THE PICCOLO TUBE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT INBOARD TELESCOPIC LEADING EDGE ANTI-ICE SUPPLY MOUNT ON THE PICCOLO TUBE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHT)

FLT 4712 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS WHEN THE SWITCH WAS IN THE ARMED POSITION, TURNED ON AND OFF INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS RELAY AT JUNCTION BOX ELEVEN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDOW — CRACKED (COCKPIT)

DURING DESCENT INTO ATL FROM PHF, AT APPROXIMATELY 30,000 FT, THE CAPTAIN'S SIDE WINDOW CRACKED. THE CREW COMPLIED WITH QRH PROCEDURES, REDUCED AIR SPEED AND DESCENDED TO 10,000 FT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S SIDE WINDOW. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)