N900EV

Part: NONE — FAILED · airframe 40,828 hrs · 39,139 cycles

DEPARTING ACV, CREW REPORTS DURING GEAR RETRACTION RECEIVED GEAR DISAGREE WARNING. NLG DID NOT RETRACT. (FLIGHT 5341 - FILED CLOSED) FOUND NLG SELECTOR VALVE CONNECTOR DISCONNECTED. RESECURED CONNECTOR AND VERIFIED TO BE LOCKED AND SECURED IN REF TO CRJ200 AMM 32-22-20 . REATTACHED HARNESS CLAMP ASSY AT NLG SELECTOR VALVE ASSY. COMPLIED WITH OPERATIONAL CHECK OF NOSE DOOR SELECTOR VALVE IN REF TO CRJ200 AMM TASK 32-22-01-720-801. COMPLIED WITH EXTENSION AND RETRACTION OF NLG IN REF TO CRJ200 AMM 32-33-00. ALL INDICATIONS NORMAL NO DISCREPANCIES NOTED.

Part: NONE — CRACKED · airframe 39,829 hrs · 38,231 cycles

CRACK FORMING IN UPPER LEFT HAND CORNER OF CA SIDE WINDSHIELD. (FLIGHT 4688 - FILED CLOSED) REMOVED CA SIDE WINDSHIELD AND WINDSHIELD WIPER DRIVE ARM REF AMM 56-11-01 / PLEASE REFERENCE AML 769130 FOR INSTALL.

Part: WINDOW — CRACKED (LEFT) · airframe 38,238 hrs · 36,845 cycles

CRACK IN LEFT WINDOW. FLIGHT 5889-FILED CLOSED. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 21870767 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LT WINDOW ASSEMBLY, IAW CRJ200 AMM AND TASK CARD. OPERATIONS AND LEAK CHECKS GOOD AT THIS TIME. TORQUE WRENCH: S/N: 1018916975 DUE-11/20S/N: 0814054098 DUE-10/21.

Part: SUPPORT — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

RH SILL HAS CORROSION AT FS 559+4 (C-CHECK) RO 1/28/2020 EVALUATED FOUND TO BE OUT OF LIMITS IAW BOMBA REO. WORK TO BE ACCOMPLISHED ON SN 7507203 AAR WO 1018024 1000 0117 CAMP 20064949

Part: FLOOR SUPPORT — DAMAGED (BS 559) · airframe 37,401 hrs · 35,934 cycles

REPAIR FLOOR SUPPORT STRUCTURE RBL9 FS 559+80 - 559+96 (C-CHECK) RO 1/28/2020 REPAIRED FLOOR SUPPORT STRUCTURE RBL 9, F.S. 559+80 - 559+96 IAW REO.

Part: FITTING — DAMAGED (HORIZ STAB) · airframe 37,756 hrs · 36,376 cycles

STEADY FITTING HAS 6 LOOSE BOLTS, WASHERS ON RIGHT HAND OUTBOARD BOLT CAN BE TURNED BY HAND. REPAIRED V/STAB STEADY FITTING ELONGATED HOLES AND LOOSE HDWR IAW REO. THIS SDR FOR T/STEADY FITTING IS BEING SUBMITTED AS A PART OF VDR_2020NM064006.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 37,401 hrs · 35,934 cycles

FOUND CARGO DOOR BRACKET FOR SPRING BOX ATTACHED TO 621 BULKHEAD CRACKED AFTER REMOVAL (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED SPRING BOX ATTACHMENT BRACKET IAW CRJ 200SRM.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

FLOOR SUPPORT STRUCTURE RBL 9 HAS CORROSION BTWEEN FS 559.00+80 AND FS 559.00+96 (C-CHECK) RO 1/28/2020 REMOVED CORROSION IAW CRJ200 SRM 51-21-06. OUT OF LIMITS IAW CRJ200 SRM. WORK TO BE ACCOMPLISHED ON W/O 1018024 1000/0184 SN 7507374

Part: FRAME — CORRODED (BS 589) · airframe 37,401 hrs · 35,934 cycles

FRAME 589 HAS CORROSION SPOTS ON THE FWD AND AFT SIDE BETWEEN STGR 22R AND 20R IN THE CARGO BAY BELOW THE FLOOR (C-CHECK) RO 1/28/2020 TRIMED OUT OUTER FLANGE FRAME AND PERFORMED REPAIR IAW CRJ200 SRM T.063 7075-T6 TAG B33959 S1710-1 TAG B13723 MS20420AD5-5 B18237 B0205019AD5-75 B27974

Part: ATTACH BRACKET — DAMAGED (LT WING) · airframe 37,401 hrs · 35,934 cycles

R/H STUB FAIRING FWD ATTAC BRACKET IS DAMAGED (C-CHECK) RO 1/28/2020 AFTER FUTHER EVALUATION STUB FAIRING AND BRACKET FOUND TO BE OUT OF LIMITS. RECEAVED, LOCATED, DRILLED AND ASSEMBLED NEW FAIRING AND BRACKET IAW CRJ 200 SRM.

Part: SUPPORT BRACKET — CRACKED (ACCESS PANEL) · airframe 37,401 hrs · 35,934 cycles

LH OVERWING ACCESS PNL SUPPORT BRACKET AT FS 449.85 IS CRACKEDREMOVED CRACKED BRACKET AND INSTALLED NEW BRACKET IAW CRJ 200 SRM.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 37,401 hrs · 35,934 cycles

LBL 9 FLOOR SEAT TRACK BETWEEN FS 409.0+128 AND FS 559.0 HAS CORROSION (C-CHECK) RO 1/28/2020 SEAT TRACK FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-21-49. REMOVED AND REPLACED IAW BOMBA REO.

Part: FLOOR SUPPORT — CRACKED (BS 513) · airframe 37,401 hrs · 35,934 cycles

INTERCOSTAL AT FS 513.0 BETWEEN LBL 9 AND LBL 27 IS CRACKED AT INBD CLIP (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED INBD CLIP AT FS513 BETWEEN LBL9 AND LBL27 REF CRJ200 SRM.

Part: FLOOR SUPPORT — CRACKED (BS 513) · airframe 37,401 hrs · 35,934 cycles

INTERCOSTAL AF FS 513.0 BETWEEN OTBD SILL NAD LBL 27 IS CRACKED AT INBD CLIP (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED INBD CLIP AT FS513 LBL27 REF CRJ200 SRM.

Part: FLOOR SUPPORT — CRACKED (BS 513) · airframe 37,401 hrs · 35,934 cycles

INTERCOSTAL AT FS 513.0 BETWEEN LH OTBD PRESS SILL AND LBL 27 IS CRACKED OTBD CLIP (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED OTBD CLIP AT FS513 LH OTBD PRESSURE SILL AND LBL27 REF CRJ200 SRM

Part: FLOOR SUPPORT — CRACKED (BS 513) · airframe 37,401 hrs · 35,934 cycles

FS 513.0 INTERCOSTAL BETWEEN RH PRESSURE SILL AND RBL 27 HAS CRACKED CLIP ON OTBD END (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED ANGLE AT FS513 BETWEEN RH PRESSURE SILL AND RBL 27 REF CRJ 200 SRM.

Part: FLOOR SUPPORT — CRACKED (BS 513) · airframe 37,401 hrs · 35,934 cycles

FS 513.0 INTERCOSTAL BETWEEN RH PRESSURE SILL AND RBL 27 IS CRACKED ON INBD CLIP (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED INBD CLIP AT FS513 BETWEEN RH PRESSURE SILL AND RBL27 REF CRJ200 SRM.

Part: SUPPORT BRACKET — CRACKED (ACCESS PANEL) · airframe 37,401 hrs · 35,934 cycles

LH WING OVERWING ACCESS PNL SUPPORT BRACKET AT FS 461.0 IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED BRACKET AND INSTALLED NEW BRACKET IAW CRJ 200 SRM.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

LBL 9 CARGO FLOOR SEAT TRACK HAS CORROSION AT FF 559.0+94 (C-CHECK) RO 1/28/2020 REMOVED CORROSION IAW CRJ 200 SRM FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM REMOVED AND REPLACED IAW CRJ 200 AMM. N126-2075 B17426

Part: FLOORBEAM — DAMAGED (BS 559) · airframe 37,401 hrs · 35,934 cycles

PERFORM LOCAL REPAIR TO RBL 9 FLOORBEAM CAP AT FS 559+4 IAW S/N SPECIFIC REO. (C-CHECK) RO 1/28/2020 REPAIRED FLOOR BEAM CAP AT FS 559+4 IAW BOMBA REO. P/N-KFN587-3 TAG#A84011 P/N-HST11AG6-4 TAG#A80240 P/N-KFN587-3 TAG#A83571 P/N-HST11AG5-6 TAG#B99244 P/N-HST10AG6-4 TAG#A84986 P/N-HST11AG5-3 TAG#B11376 P/N-HST11AG6-2 TAG#B13673 P/N-B0203013-08 TAG#A83729 P/N-BN360PB1032DU4 TAG#B00123

Part: FLOOR SUPPORT — DAMAGED (BS 559) · airframe 37,401 hrs · 35,934 cycles

REPAIR OR REPLACE RBL 27 FLOORBEAM CAP THAT HAS DAMAGE BETWEEN FS 559+80 AND FS 559+112 (C-CHECK) RO 1/28/2020 REPAIRED FLOORBEAM ON RBL 27 BETWEEN FS 559+80 AND FS 559+112 IAW CRJ 200 SRM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 37,401 hrs · 35,934 cycles

L/H WINDSHIELD SIDE POST SUPPORT FITTING IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED L/H WINDSHIELD SIDE POST SUPPORT FITTING IAW CRJ-200 SRM 51-42-21.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 37,401 hrs · 35,934 cycles

R/H WINDSHIELD SIDE POST SUPPORT FITTING IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED R/H WINDSHIELD SIDE POST SUPPORT FITTING IAW CRJ-200 SRM.

Part: FRAME — CRACKED (BS 333) · airframe 37,401 hrs · 35,934 cycles

FRAME 333 IS CRACKED AT TOOLING HOLE JUST I/B OF STGR 2L IN THE CABIN (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED FRAME SECTION IAW CRJ-200 SRM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 37,401 hrs · 35,934 cycles

L/H WINDSHIELD SIDE POST WEB IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED L/H WINDSHIELD SIDE POST WEB IAW CRJ-200 SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 37,401 hrs · 35,934 cycles

AFT PRESSURE BULKHEAD WEB IS CRACKED AT BLO APPROX WL 112 (C-CHECK) RO 1/28/2020 REPAIRED AFT PRESSURE BULKEAD AT BL 0 WL 112 IAW BOMBARDIER REO. FILLER TO BE INSTALLED ON AND REO WILL BE SCANNED ON CAMP # 19794163

Part: ANGLE — CRACKED (STRINGER 3L) · airframe 37,401 hrs · 35,934 cycles

I/B AND O/B ANGLE CLIPS ON STGR 3L JUST AFT OF FRAME 280 ARE CRACKED IN THE CABIN (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED I/B AND O/B ANGLE CLIPS IAW CRJ-200 SRM 51-42-06 AND SRM

Part: SEAT TRACK — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

RBL9 TRACK AT FS559.0+112 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED CORRODED TRACK ( CORRODED BEYOND SRM LIMITS), FABRICATED AND INSTALLED NEW TRACK IAW BOMBARDIER REO.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 37,401 hrs · 35,934 cycles

PASSENGER DOOR HAS AFT CLOSING PLATE MOUNTING BRAKET CRACKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED PANEL MOUNTING BRACKET, FABRICATED NEW BRACKET IAW CRJ-200 SRM AND INSTALLED NEW BRACKET IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

LBL9 #4 FLOOR SEAT TRACK BETWEEN FS 559.0+4 AND FS559.0+80 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED LBL#9 FLOOR SEAT TRACK BETWEEN FS559.0+4 AND FS559.0+80 IAW:CRJ 200 AMM.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

LH SILL HAS CORROSION BETWEEN FS559.0 TO FS599.0+80 (C-CHECK) RO 1/28/2020 REPAIRED FLOOR SILL IAW REO.

Part: CARGO TRACK — CORRODED (BS 570) · airframe 37,401 hrs · 35,934 cycles

CARGO TRACK ON LBL9 HAS CORROSION AT FS570.0 (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED CARGO TRACK AT LBL9 FS570.0 IAW:CRJ200-AMM.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

RBL27 CARGO TRACK HAS CORROSION BETWEEN FS559.0+80 TO FS559.0+96 (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED RBL27 CARGO TRACK BETWEEN FS559.0+80 TO FS559.0+96 IAWCRJ200- AMM

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 37,401 hrs · 35,934 cycles

PASSENGER DOOR CUT-OUT HAS CORROSION AT LOWER AFT CORNER BY DRAIN HOLE (C-CHECK) RO 1/28/2020 REPAIRED LOWER AFT CORNER OF PASSENGER DOOR CUT-OUT IAW BOMBA REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

RBL9 #4 FLOOR SEAT TRACK BETWEEN FS559.0+4 AND FS559.0+80 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM. TOOL# AAR519954 CAL DUE: 05/09/20

Part: FRAME — CRACKED (BS 605) · airframe 37,401 hrs · 35,934 cycles

FS605.0 IS CRACKED AT STGRL9 (C-CHECK) RO 1/28/2020 REPAIRED FRAME 605 AT STGR 9L REF REO

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 37,401 hrs · 35,934 cycles

LH MLG W/W GEAR PROX WIRE HARNESS SUPPORT ANGLE AT AUX SPAR RIB WS 6.0 CRACKED ABOVE CONNECTOR J411 (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED SUPPORT ANGLE AT AUX SPAR RIB WS 6.0 L/H MLG IAW CRJ200SRM.

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 37,401 hrs · 35,934 cycles

LH MLG W/W AUX SPAR RIB SUPPORT ANGLE CRACKED FWD OF INBD DRAG ANGLE. BL 45L (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED L/H AUX SPAR RIB SUPPORT ANGLE AT BL 45L IAW CRJ200 SRM.

Part: NOT REPORTED — CORRODED (BS 589-621) · airframe 37,401 hrs · 35,934 cycles

RBL27 HAS CORROSION BETWEEN FS589.0 TO FS621.0 (C-CHECK) RO 1/28/2020 EVALUATED AND FOUND TO BE OUT OF LIMITS IAW REO. WORK TO BE ACCOMPLISHED ON CP 20065025, AAR NON-ROUTINE 1018024/1000/0120 S/N: 7507206

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 37,401 hrs · 35,934 cycles

LBL9 HAS CORROSION ON FLOOR SUPPORT BETWEEN FS589.0 TO FS621.0 (C-CHECK) RO 1/28/2020 EVALUATED AND FOUND TO BE OUT OF LIMITS IAW REO. WORK TO BE ACCOMPLISHED ON CP 20064973, AAR NON-ROUTINE 1018024/1000/0119 S/N: 7507205

Part: CARGO TRACK — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

RBL9 CARGO TRACK HAS CORROSION AT FS559.0+94 (C-CHECK) RO 1/28/2020 REMOVED AND INSTALLED RBL9 CARGO TRACK AT FS559.0+94 IAW: CRJ200-AMM. TORQUE GUN: AAR531535 DATE:4/9/2020

Part: NOT REPORTED — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

RBL27 HAS CORROSION BETWEEN FS559.0+80 TO FS559.0+112 (C-CHECK) RO 1/28/2020 EVALUATED AND FOUND TO BE OUT OF LIMITS IAW REO. WORK TO BE ACCOMPLISHED ON CP 20064968, AAR NON-ROUTINE 1018024/1000/0118 S/N: 7507204

Part: BRACKET — CRACKED (LT MLG WW) · airframe 37,401 hrs · 35,934 cycles

LH MLG W/W, BRAKE HYD PRESSURE TRANSDUCER BRACKET CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED L/H MLG BRAKE HYD. PRESSURE TANSDUCER BRACKET IAW CRJ200 SRM.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

LBL27 CARGO TRACK BETWEEN FS559.0+80 TO FS559.0+96 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED LBL27 SEAT TRACK BETWEEN FS559+80 TO FS559+96 IAW CRJ 200 AMM.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 37,401 hrs · 35,934 cycles

LBL 27 HAS CORROSION ON FLOOR SUPPORT BETWEEN FS559.0+80 TO FS559.0+112 (C-CHECK) RO 1/28/2020 EVALUATED AND FOUND TO BE OUT OF LIMITS IAW REO. WORK TO BE ACCOMPLISHED ON CP 20072407 AAR NON-ROUTINE 1018024-1000-0127 S/N: 7507217.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 37,401 hrs · 35,934 cycles

LH SIDE SEAT RAIL #5 BETWEEN FS449.85 AND FS499.0 HAS CORROSION (C-CHECK) RO 1/28/2020 BLENDED CORROSIONFOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW CRJ-200 AMM. NAS1580A3T17/BB4980, NAS517-3-5/A64793

Part: SEAT TRACK — CORRODED (BS 409) · airframe 37,401 hrs · 35,934 cycles

LH SIDE SEAT RAIL #3 BETWEEN FS409.0+16 AND 409.0+112 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED CORROSION FOUND TO BE OUT OF LIMITS, INSTALLED NEW SEAT TRACK IAW CRJ-200 AMM PN 601R38312-29S TN B99057

Part: PIN — CRACKED (PAX DOOR) · airframe 37,401 hrs · 35,934 cycles

PASSENGER DOOR UPPER FWD PANEL 832BL, 832BR, AND 832ER SIGHT LENSE RETAINERS ARE CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED PASSENGER DOOR PANEL 832BL, 832BR, AND 832ER SIGHT LENS RETAINERS IAW CRJ200 AMM PN: 601R319021-7 TAG#B18479,B20587,B20074 RMITCHELL32218

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 37,401 hrs · 35,934 cycles

LH SIDE SEAT RAIL #7 BETWEEN FS544.0 TO FS559.0+112 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACE IAW REO.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 37,401 hrs · 35,934 cycles

RH SIDE SEAT RAIL #5 BETWEEN FS449.85 ADN FS499.0 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 37,401 hrs · 35,934 cycles

RH SIDE SEAT RAIL #7 BETWEEN FS544.0 AND FS559.0+112 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED RH SIDE SEAT RAIL #7 IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 37,401 hrs · 35,934 cycles

LH SIDE SEAT RAIL #2 HAS BETWEEN FS364.0 AND FS409.0+16 CORROSION (C-CHECK) RO 1/28/2020 / REMOVED AND REPLACED SIDE SEAT TRACK IAW CRJ200 AMM.

Part: DRAG ANGLE — CRACKED (RT MLG WNG ROOT) · airframe 37,401 hrs · 35,934 cycles

RH MLG BAY WING ROOT DRAG ANGLE CRACKED.REMOVE AND REPLACED DRAG ANGLE IAW CRJ200 SRM B0203013-08 A82854 / HST10AG5-3 A82608, HST11AG6-3 A78606 ,HST11AG6-5 AB18333, 600-10389-2S B95647

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 37,401 hrs · 35,934 cycles

LH SIDE SEAT RAIL #4 BETWEEN FS409+112 AND FS449.85 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM. MAX ALLOWABLE MATERIAL REMOVAL IS .020", REMOVED .026", NOMINAL THICKNESS IS .105", REMAINING THICKNESS IS .079". TOOL# AAR531287, CAL DUE DATE: 06-27-2020. REMOVED AND REPLACED SIDE SEAT TRACK IAW REO, PART NUMBER 20276-288-0-0, TAG NUMBER B15443.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 37,401 hrs · 35,934 cycles

RH SIDE SEAT RAIL #2 BETWEEN FS364.0 AND FS409+16 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED SIDE SEAT TRACK IAW CRJ200 AMM.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 37,401 hrs · 35,934 cycles

LH SIDE SEAT RAIL #6 BETWEEN FS499.0 AND FS544.0 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED #6 SIDE SEAT RAIL DUE TO CORROSION AND FABRICATED NEW TRACK AND INSTALLED IAW CRJ-200 AMM.

Part: SEAT TRACK — CORRODED (BS 449-544) · airframe 37,401 hrs · 35,934 cycles

RH SIDE SEAT RAIL #6 BETWEEN FS499.0 TO FS544.0 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED CORROSION FOUND OUT OF LIMITS. INSTALLED NEW SEAT TRACK IAW CRJ 200 AMM. PN601R38312 TNB17188

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 37,401 hrs · 35,934 cycles

RH SIDE SEAT RAIL #4 BETWEEN FS409+112 AND FS449.85 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED RHS SEAT RAIL #44 BETWEEN FS409+112 ABD FS449.85 IAW:CRJ200*AMM

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 37,401 hrs · 35,934 cycles

RH MLG BAY BRAKE PRESSURE TRANSDUCER SUPPORT BRACKET CRACKED AT LWR SURFACE OF PRESSURE FLOOR SKIN. (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED BRACKET IAW CRJ-200 SRM.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 37,401 hrs · 35,934 cycles

RH SIDE SEAT RAIL #3 BETWEEN FS409.0+16 ADN FS409+112 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED RH SIDE SEAT RAIL # 3 BETWEEN FS409.0+16 AND FS409+112 IAW:CRJ200-AMM.

Part: FRAME — CORRODED (BS 319) · airframe 37,401 hrs · 35,934 cycles

FRAME 319.70 HAS CORROSION SPOTS ON THE FWD SIDE BETWEEN STGR 25L THRU 26R IN THE FWD E&E BAY (C-CHECK) RO 1/28/2020 REMOVED CORROSION IAW CRJ200 SRM. OUT OF LIMITS IAW CRJ200 SRM. WORK TO BE ACCOMPLISHED ON W/O 1018024 1000/0166 SN 7507330.

Part: ATTACH BRACKET — CRACKED (SERVICE PANEL) · airframe 37,401 hrs · 35,934 cycles

EXTERNAL SERVICING PANEL LOWER ATTACH BRACKET CRACKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED ELECTRICAL SERVICE PANEL LOWER BRACKET (FS 193 - FS 202.75), AND INSTALLED NEW BRACKET IAW CRJ 200 SRM.

Part: TRIM PANEL — CRACKED (ESCAPE HATCH) · airframe 37,401 hrs · 35,934 cycles

CREW ESCAPE HATCH HAS OUTER TRIM PANEL CRACKED AT FASTENER HOLES (C-CHECK) RO 1/28/2020 RECIEVED NEW CREW ESCAPE HATCH P/N601R41295-73, TAG NUMBER BB4986. LOCATED AND DRILLED NEW PANEL AND INSTALLED SEAL AND RETAINERS IAW CRJ-200 SRM. INSTALLED PLACARD IAW AMM.

Part: BULKHEAD — CRACKED (BS 621) · airframe 37,401 hrs · 35,934 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL(J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7608, POSITION: (C-CHECK) RO 1/28/2020 COMPLIED WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND; MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. COMPLIED WITH SERIAL NUMBER 7608.

Part: AXLE — FAILED (NLG) · airframe 35,712 hrs · 34,015 cycles

ON DEPARTURE WHEN RETRACTING GEAR, NOSE GEAR DID NOT GO UP AND LOCK. RECEIVED GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH AND WARMING MESSAGE WENT AWAY. GEAR CAME DOWN AND LOCKED. RETURNED TO FIELD LANDED NORMALLY. (FLT 7429) CLOSED REMOVED AND REPLACED NLG PISTON AXLE ASSEMBLY IAW AMM. PERFORMED NLG STRUT EXTENSION CHECK AND RETRACTION/EXTENSION CHECK. NO FAULTS FOUND.

Part: RIB — CRACKED (RT AILERON) · airframe 33,849 hrs · 31,935 cycles

AILERON RIB AT A/STA 324.459 CRACKED AT TRAILING EDGE. (C-CHECK) REMOVED AND REPLACED RT AILERON RIB AT STA 324.459 IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,849 hrs · 31,935 cycles

DENT FOUND ON EXTERNAL FUSELAGE SKIN AT FS297 BETWEEN STR22R AND STR23R. (C-CHECK) COMPLIED WITH ALL STEPS OF PERMANENT REPAIR IAW REO.

Part: SKIN — DENTED (RT AILERON) · airframe 33,849 hrs · 31,935 cycles

RT AILERON LOWER SKIN AND TRAILING EDGE DENTED. (C-CHECK) REMOVED AND REPLACED THE TRAILING EDGE BAR ASSEMBLY P/N 601R13040-24 WITH A FACTORY NEW PART. AND PERFORMED REPAIR TO THE DAMAGED SKIN SECTION ON THE RT AILERON LOWER SKIN IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,849 hrs · 31,935 cycles

DENT ON FUSELAGE SKIN BETWEEN FS625-FS640 AND STR21L-STR22L. (C-CHECK) COMPLIED WITH PERMANENT REPAIR FOR DENT DAMAGE TO FUSELAGE SKIN BETWEEN FS 621.00 & FS640.00 AND STRINGERS 20 & 23 L. PERFORMED CUT OUT OF DAMAGED AREA, REPAIRED STRINGER STR22L FROM FS625 TO FS647, AND INSTALLED FILLER DOUBLER AND TRIPLER REPAIR PARTS IAW REO.

Part: HANDLE — BINDING (PAX DOOR) · airframe 31,844 hrs · 29,758 cycles

PAX DOOR INSIDE LEVER IS HARD TO MOVE. PERFORMED OPS TEST OF THE PAX DOOR IAW AMM 52-11-00. OP CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE / [SDR CLOSED].

Part: HANDLE — STUCK (PAX DOOR) · airframe 31,500 hrs · 29,384 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. THE HANDLE WAS STUCK IN THE 3/4 OPEN POSITION. OPS. TEST OF PASSENGER DOOR SEVERAL TRANSITS WITH F/A PERSONNEL. OPS GOOD AT THIS TIME IAW AMM 52-11-21. ACFT GOOD FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 409-424) · airframe 30,262 hrs · 28,093 cycles

FLOOR SUPPORT AT FS 409-116 TO 424.00 HAS 3 NUTPLATES CORRODED WITH 100 PERCENT MATERIAL LOSS. COMPLIED WITH REO 601R-53-41-1955, FINAL REV REMOVED DAMAGED SECTION IAW REO 601R-53-41-1955. REINSTALLED FABRICATED SECTION IAW REO 601R-53-41-1955, REV P2. COMPLIED WITH FABRICATION OF REO 601R-53-41-1599. RECEIVED AND COMPLIED WITH REO 601R-53-41-1955(P2) DATED 10/21/2015. RECEIVED AND COMPLIED WITH ECTC REO 601R-53-41-1955.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 30,262 hrs · 28,093 cycles

SEAT TRACK AT FS 409+126 TO 559+4 IS CORRODED. COMPLIED ECTC FABRICATED SEAT TRACK IAW GREO 601R-53-00-425, REV A. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED PASSENGER FLOOR SEAT TRACK IAW AMM 53-01-11-400-802.

Part: RISER — DAMAGED (PAX DOOR) · airframe 30,262 hrs · 28,093 cycles

PAX DOOR AFT RISER DAMAGED. REMOVED AFT RISER IAW SRM 51-42-06. LOCATED HOLES IN NEW RISER AND ATTACHED ALL STIFFENERS IAW SRM 51-42-06. INSTALLED AFT RISER ON PAX DOOR IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: ANGLE — CRACKED (BS 625) · airframe 30,262 hrs · 28,093 cycles

LT AND RT ANGLES CRACKED AT STR 15L AND 15R AND FS 625.30. REMOVED LT AND RT CLIP ANGLES AT STR 15L & 15R AND FS 625.30 IAW SRM 51-42-21-00. INSTALLED NEW SERVICEABLE LT & RT CLIP ANGLES AT STR 15L & 15R AND FS 625.30 IAW SRM 51-42-21-00 & DWG #601-35012.

Part: RIB — CRACKED (RT MLG WW) · airframe 30,262 hrs · 28,093 cycles

RT MLG W/W AREA BATTERY RIB CRACKED. RECEIVED AND COMPLIED WITH GREO 601R-57-51-0045 REV B. REPAIRED BATTERY RIB ASSEMBLY IAW REO 601R-57-51-043, REV B.

Part: ISOLATOR — CRACKED (AFT PRESS BLKHD) · airframe 30,262 hrs · 28,093 cycles

CRACKED ATTACHMENT ARM ON ISOLATOR ON ISOLATOR ON AFT PRESSURE BULKHEAD. REPLACED ISOLATOR IAW SRM 51-42-03.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,262 hrs · 28,093 cycles

CRACK FOUND ON FLOOR ANGLE BETWEEN RBL 9 AND INBD SIDE OF FS 280.00. COMPLIED WITH EC/TC REO 601R-53-11-923 01.

Part: ANGLE — CORRODED · airframe 30,262 hrs · 28,093 cycles

CORROSION FOUND ON INBD SIDE OF ASD SILL TOP ANGLE AROUND AND BY FLOOR NUT PLATES. CORROSION ON MID ANGLE FOUND TO BE CORRODED COMPLETLY THROUGH PART OUT OF LIMITS IAW SRM 53-00-00. R & R MID ANGLE IAW SRM 51-42-06, 51-42-21, 51-42-13. LOCATED AND DRILLED NEW SERVICABLE MID CAP ANGLE IAW SRM 51-40-11-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,262 hrs · 28,093 cycles

CRACK FOUND ON FLOOR CLIP BETWEEN RBL 9 AND OTBD SIDE AT BS 280. COMPLIED WITH EC/TC REO 601R-53-11-923 01.

Part: FLOOR SUPPORT — CRACKED (BS 605) · airframe 30,262 hrs · 28,093 cycles

LT CARGO FLOOR SILL CRACKED AT FS 605.00. REPAIRED CRACK IAW REO 601R-53-61-433. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH EC/TC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 30,262 hrs · 28,093 cycles

CORROSION FOUND ON SEAT TRACK LBL9 AT BS 364, 409+128. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED & FABRICATED SEAT TRACK IAW AMM 53-01-11, GREO 601R-53-00-485, REV A. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 30,262 hrs · 28,093 cycles

LEFT FLOOR SILL CORRODED AROUND SCREW HOLES BETWEEN FRAMES 574 - 621. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526. BLENDED AREAS ARE WITHIN ALLOWABLE LIMITS IAW REO 601R-53-00-526.

Part: STRUCTURE — CORRODED (BS 349-) · airframe 30,262 hrs · 28,093 cycles

CORROSION FOUND ON SILL EDGE AT BS 349 AND RBL 40. REMOVED FLOOR SILL AT 349.00 DUE TO 100 PERCENT MATERIAL LOSS OUT OF LIMITS IAW SRM 51-42-06-001-001-A01. RECEIVED AND COMPLIED WITH EC/TC REO 601R-53-21-326.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 30,262 hrs · 28,093 cycles

FLOORBEAM AT BS 589 UNDER FLOOR PANEL 282KRF IS CORRODED. BLENDED CORROSION IAW SRM 51-21-06. R & R FLOORBEAM CAP IAW SRM 51-42-06 AND 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 30,262 hrs · 28,093 cycles

RBL9 LONGIITUDINAL FLOOR SUPPORT HAS VARIOUS FLOORBOARDS SCREW HOLES CORRODED FROM BS 409 - 409+128. EVALUATED AND FOUND CORROSION AROUND VARIOUS FLOORBOARD SCREW HOLES FROM FS 409 - 409+128 TO BE BEYOND REPAIRABLE LIMITS REF SRM 53-00-43 VARIOUS SCREW HOLES COMPLETELY CORRODED THROUGH. REMOVED CORRODED LONGITUDINAL FLOOR SUPPORT , RBL 9, FS 409.00-409+128 & INSTALLED NEW SERVICEABLE BEAM IAW SRM 51-42-21, REO 601R-53-31-852. COMPLIED WITH EC/TC REO 601R-53-31-852, REV: O.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 30,262 hrs · 28,093 cycles

CORROSION FOUND ON SEAT TRACK AT FS 364 - 409+128 AND RBL9. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM, 53-21-49. REMOVED SEAT TRACK AT FS 364-404.00 +128, RBL9 IAW AMM 53-01-11. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485, REV A. INSTALLED SEAT TRACK AT F/S 364.00-409.00+128 AT RBL9. REF: AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00- 485, REV A FABRICATED SEAT TRACK IAW GREO 601R-53-00-485, REV A.

Part: FRAME — CORRODED (BS 605) · airframe 30,262 hrs · 28,093 cycles

FRAME 605 FROM STR 25R TO STR 20L IS CORRODED IN MULTIPLE AREAS. BLENDED MULTIPLE AREAS OF CORROSION AT FR 605 IAW SRM 51-21-06 & 51-12-00. RECEIVED REPAIR AND COMPLIED WITH EA 32-2015-385. RECEIVED AND COMPLIED WITH EC/TC EA 32-2015-385.

Part: FLOOR SUPPORT — CORRODED (BS 424) · airframe 30,262 hrs · 28,093 cycles

LT PRESSURE FLOOR SUPPORT FS 424 IS CORRODED. BLENDED CORROSION IAW SRM 51-21-06. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SO 5702. .

Part: FLOOR SUPPORT — CORRODED (BS 621-559) · airframe 30,262 hrs · 28,093 cycles

FLOORBEAM TOP CAP AT LBL 27 FROM BS 621 - 559.00+64 IS CORRODED IN MULTIPLE AREAS AND AT NUT PLATE LOCATIONS. BLENDED CORROSION IAW SEM 51-21-06, FOUND TO BE OUT OF LIMITS DUE TO 100 PERCENT MATERIAL LOSS AT MULTIPLE NUTPLATE LOCATIONS. REMOVED THE FLOOR BEAM TOP CAP BETWEEN FS 621-FS 559+64 AT LBL 27 IAW SRM 541-42-06, 51-42-21. COMPLIED WITH ECTC REO 601R-53-61-3778 AND GREO 601R-53-61-3778, REV A, DATED: 07/15/2011 AS WRITTEN. LOCATED FASTENERS HOLES TO MATCH EXISTING HOLE SIZE IN NEW BEAM CAP, FS 559+64 TO FS 621 AT LBL27 IAW SRM 51-40-11. INSTALLED NEW SEAT RAIL BEAM, CAP SECTIONAL IAW REO 601R-53-61-3778.

Part: FLOOR SUPPORT — CORRODED (BS 424) · airframe 30,262 hrs · 28,093 cycles

RT SIDE PRESSURE FLOOR SUPPORT AT BS 424 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 30,262 hrs · 28,093 cycles

FLOORBEAM AT FS 589 BETWEEN LBL 9 AND LBL 27 TOP CAP IS CORRODED IN MULTIPLE AREAS. BLENDED CORROSION IAW SRM 51-21-06. R & R FLOORBEAM ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: SCAVENGE PUMP — FAILED (ENGINE OIL) · airframe 29,968 hrs · 27,764 cycles

DURING CLIMBOUT, AT ABOUT 1400 FT, RECEIVED A MASTER WARNING LT ENGINE OIL PRESSURE. OIL PRESSURE WAS FLUCTUATING FROM 15 PSI TO 66 PSI, RAN QRH DID NOT SHUTDOWN THE ENGINE KEEP ENGINE AT IDLE. ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY DECLARED. R & R LT ENGINE LUBE AND SCAVAGE ASSY IAW AMM 79-21-01, AIPC 79-21-11, FIG 1, ITEM 335G. SERVICE LT ENGINE OIL TANK, AND LEAK AND OPS CHECKS.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 29,707 hrs · 27,487 cycles

FLASHLIGHT INOPERATIVE, CAPTAIN SIDE. R & R BATTERIES IAW AMM 25-61-02. OPS CK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 29,074 hrs · 26,819 cycles

EXIT LENS COVER ON CABIN EXIT SIGN MISSING. CREW FOUND EXIT SIGN INSTALLED EXIT SIGN IAW AMM 33-51-13.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,906 hrs · 25,659 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS IAW AMM 33-51-04 AND AIPC 33-51-04, ITEM 17. OPS TESTED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,262 hrs · 25,024 cycles

EMERGENCY LIGHTS NOT WORKING, CREW REPORT F/A EMERGERCY LIGHT PANEL WAS LEFT ON, ALLOWED EMERGENCY LIGHTS TO CHARGE & PERFORMED OPS CHECK IAW AMM 33-51-00. OPS CHK GOOD, ACFT OK FOR SERVICE.

Part: COUNTERBALANCE — FAILED (PAX DOOR) · airframe 26,887 hrs · 24,628 cycles

PAX DOOR FAILED FUNCTIONAL CHECK, DOOR OPENS TOO HARD. ADJUSTED PASSENGER DOOR COUNTER BALANCE REF AFT AMM TASK 52-11-17-820-802 FASTENED CHECK FAILED. REPLACED PASSENGER-DOOR COUNTER BALANCE GAS SPRINGS IAW AMM 52-11-17-400-802. OPS CHECKED GOOD. ADJUSTED FORWARD COUNTER BALANCE ANCHOR SWIVEL AMM TASK 52-11-17-820-802. FUNCTIONAL TESTED GOOD IAW AMM TASK 52-11-00-720-802.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,887 hrs · 24,628 cycles

EMERGENCY LIGHT AT LT AND RT EMERGENCY EXITS UNSERVICEABLE. REPLACED EMERGENCY LIGHT IAW 33-51-01 01.

Part: PLATE — DENTED (CARGO DOOR) · airframe 26,887 hrs · 24,628 cycles

TWO DENTS ON LOWER RT SIDE OF CARGO SKID PLATE. COMPLIED WITH EC/TC REO601R-53-61-5084.

Part: SKIN — CRACKED (RT WING) · airframe 26,887 hrs · 24,628 cycles

CRACK INDICATION IN RT WING LOWER PLANK NR 2 HOLE. COMPLIED WITH REO 601R-57-21-2033, REV.(P1) DATED NOV.9, 2013. MAJOR REPAIR.

Part: TRUNNION — DAMAGED (LT WING) · airframe 26,887 hrs · 24,628 cycles

WHILE PERFORMING SB601R-57-046, FOUND AFT HOLE ON LT WING TRUNNION STRAP OVERSIZED TO .3405. COMPLIED WITH REO 601R-57-21-2033, REV (P1). MAJOR REPAIR.

Part: TRUNNION — DAMAGED (RT WING) · airframe 26,887 hrs · 24,628 cycles

WHILE PERFORMING SB601R-57-046, FOUND AFT HOLE ON RT WING TRUNNION STRAP OVERSIZED TO .3400. COMPLIED WITH REO 601R-57-21-2033, REV P1. MAJOR REPAIR.

Part: SKIN — CRACKED (RT WING) · airframe 26,887 hrs · 24,628 cycles

CRACK INDICATION IN RT WING LOWER PLANK NR 3 HOLE. COMPLIED WITH REO 601R-52-21-2033, REV (P1). MAJOR REPAIR.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 26,887 hrs · 24,628 cycles

PSD AFT WALL DISCOVERED FIVE OVERSIZE HOLES WHILE ACCOMPLISHING REPAIR ON DRAG ANGLE. COMPLIED WITH REO 601R-52-11-2195. FABRICATED AND INSTALLED FILLER 601R-52-11-2195-2 AND FILLER 601R-52-11-2192-1 IAW REO 601R-52-11-2195. MAJOR REPAIR.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 26,887 hrs · 24,628 cycles

FS 621 BULKHEAD HAS BROKEN ISOLATOR AT RBL 9.0 SECOND ONE FROM FLOOR. R & R ISOLATOR IAW AMM 51-42-13.

Part: SKIN — CORRODED (WING) · airframe 26,887 hrs · 24,628 cycles

LOWER PLANK ACCESS OPENING FOR PANEL 550DB HAS CORROSION. COMPLIED WITH ECTC 600-57-81, IAW SRM 51-24-11, ROTO PEENED REWORKED AREA.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,887 hrs · 24,628 cycles

FOUND CRACK ON AFT SIDE DRAG ANGLE CENTER OF PAX DOOR. COMPLIED WITH EC/TC REO 601R-52-11-513.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 26,887 hrs · 24,628 cycles

VERTICAL BEAM AT FS 409+128, RBL27 IS CRACKED AT INBD AFT FLANGE AT THE BOTTOM. COMPLIED WITH EC/TC REO 601R-53-41-056. MAJOR REPAIR.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 26,887 hrs · 24,628 cycles

VERTICAL BEAM AT FS 409+128, LBL 27 IS CRACKED AT INBD AFT BOTTOM FLANGE. COMPLIED WITH EC/TC REO 601R-53-41-056 AND REO 601R-53-41-056. MAJOR REPAIR.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 26,887 hrs · 24,628 cycles

VERTICAL BEAM AT FS 409 + 128 RBL 18 IS CRACKED AT OTBD AFT FLANGE AT THE BOTTOM. COMPLIED WITH EC/TC REO 601R-53-41-056. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 400-404) · airframe 26,887 hrs · 24,628 cycles

SECOND SEGMENT OF SEAT TRACK ON RBL 9.0 FROM FS 400 TO 404+128 CORRODED IN MULTIPLE LOCATIONS. R & R SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 26,887 hrs · 24,628 cycles

FLOOR SUPPORT HAS CORROSION FROM FS 589 - 621 LBL 27. REMOVED CORROSION IAW SRM 51-26-06.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 26,887 hrs · 24,628 cycles

FIRST SEGMENT OF SEAT TRACK ON LBL 9.0 FROM FS 364 TO 400 IS CORRODED IN MULTIPLE LOCATIONS. R & R SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 26,887 hrs · 24,628 cycles

FIRST SEGMENT OF SEAT TRACK ON RBL 9.0 FROM FS 364 TO 400 CORRODED IN MULTIPLE LOCATIONS. R & R SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SKIN — CORRODED (BS 559) · airframe 26,887 hrs · 24,628 cycles

MULTIPLE AREAS OF CORROSION ON EXTERNAL SKIN AT LAV DUMP PORT MARKED BETWEEN BS 559 + 80 TO 559 + 112 STRINGERS 23R AND 24R UNDER RIVET HEADS DOUBLER AND AFT FAIRING SUPPORT. REMOVED CORROSION FROM SKIN IAW SRM 51-21-06-00 & EVAL IAW SRM TR 53-33. REMOVED CORROSION FORM FS 559+80 TO FS 559+112 STRINGERS 23 AND 24 DOUBLER AND AFT FAIRING SUPPORT IAW SRM 51-21-05-00.

Part: ANGLE — CRACKED · airframe 26,887 hrs · 24,628 cycles

LAVATORY FLOOR ASSY METAL ATTACHMENT PLATE BENT AND CRACKED. R & R METAL ANGLE IAW AMM 20-21-0-910-801.

Part: ANGLE — CRACKED (BS 625) · airframe 26,887 hrs · 24,628 cycles

ANGLE CRACKED AT BS 625.30, S9L. REMOVED & INSTALLED NEW ANGLE IAW SRM 51-40-06 & 51-42-20 & DWG 601-36012.

Part: HOUSING — CHAFED (CARGO DOOR) · airframe 26,887 hrs · 24,628 cycles

CARGO DOOR HANDLE HOUSING CHAFED ON EXTERIOR, LOWER, FWD CORNER. COMPLIED WITH REO 601E-52-31-086. MAJOR REPAIR.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 26,887 hrs · 24,628 cycles

CARGO DOOR SKIN CHAFED. COMPLIED WITH REO 601R-52-31-198. MAJOR REPAIR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,887 hrs · 24,628 cycles

FOUND CRACK ON AFT SIDE DRAG ANGLE CENTER OF PAX DOOR. COMPLIED WITH PERMANENT REPAIR OF PAX DOOR AFT DRAG ANGLE IAW EC/TC REO 601R-52-11-513. MAJOR REPAIR.

Part: PLATE — DENTED (CARGO DOOR) · airframe 26,887 hrs · 24,628 cycles

RAMP REPORTED TWO DENTS ON LOWER RT SIDE OF CARGO SKID PLATE. COMPLIED WITH PERMANENT REPAIR OF FUSELAGE DENTS AT FS 605-621, S18-19L IAW EC/TC REO 601R-53-61-5084. MAJOR REPAIR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,417 hrs · 24,147 cycles

NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21.

Part: SKIN — BURNED (BS 409) · airframe 26,259 hrs · 23,991 cycles

BURN AT 7 O`CLOCK POSITION ON EDGE OF WINDOW BETWEEN FS 409+16 AND FS 409+32. REPAIRED IAW REO 601R-53-31-796. MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 409) · airframe 26,259 hrs · 23,991 cycles

BURN AT 7 O`CLOCK POSITION ON EDGE OF WINDOW BETWEEN FS 409+48 AND FS 409+64. REPAIRED IAW REO 601R-53-31-796. MAJOR REPAIR IAW GMM 5-3.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,173 hrs · 23,903 cycles

FOUND CRACK ON AFT SIDE DRAG ANGLE CENTER OF PAX DOOR. REPAIRED IAW REO 601R-52-11-1360 (REV B).

Part: CHARGER — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 25,789 hrs · 23,506 cycles

OVERHEAD EMERGENCY LIGHT IN CABIN IS OUT. R & R BATTERY CHARGER ASSY, IAW AMM 33-51-05, OPS CHECKED GOOD, OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,861 hrs · 22,560 cycles

NR 7 EXTERIOR EMERGENCY LIGHT INOPERATIVE. LAMPED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD.

Part: DETECTOR — FAILED (TE FLAPS) · airframe 24,498 hrs · 22,173 cycles

FLAPS FAIL MESSAGE AT 18000FT. NEVER WENT AWAY. LANDED FLAPS ZERO. EMERGENCY DECLARED AS A PRECAUTION, TOWER HAD EQUIPMENT STANDING BY. R & R SKEW DETECTION UNIT IAW AMM 27-51-15. CLEARED. SDR CLOSED.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 24,424 hrs · 22,099 cycles

ON GEAR EXTENSION BOTH MAIN GEARS DID NOT COME DOWN, PERFORMED QRH, AND MANUAL RELEASE, THEN GEAR CAME DOWN. EMERGENCY DECLARED. R & R MLG SELECTOR VALVE IAW 32-32-10. LEAK AND FUNCTIONAL CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,626 hrs · 21,224 cycles

EXTERIOR NR 3 EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EXTERIOR NR 3 EMERGENCY FLOOD LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SENSOR — FAILED (TE FLAPS) · airframe 23,233 hrs · 20,814 cycles

FLAPS FAIL MESSAGE AT FL 310, FLAPS 0 SAT -41C TAT -16C. ACFT RETURNED TO DEPARTURE. EMERGENCY DECLARED. R & R RT FLAP BPSU IAW AMM 27-51-10, OPS CHECKED GOOD IAW AD 2009-06-12.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 23,045 hrs · 20,616 cycles

FS 349.0 RBL 27 SILL FLOOR SUPPORT CORRODED. REPAIRED IAW REO 601R-53-21-2222, DATED 11/11/2011.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 23,045 hrs · 20,616 cycles

FS 349.00, RBL 27 SILL FLOOR SUPPORT CORRODED. PERFORMED EDDY CURRENT INSPECTION IAW NDTM 51-20-06. NO INDICATIONS NOTED. REPAIRED IAW REO 601R-53-21-22222.

Part: SKIN — CORRODED (BS 343-364) · airframe 22,998 hrs · 20,566 cycles

FUSELAGE EXTERNAL SKIN CORRODED FS 343 AND 364 STR 17-19L. REMOVED CORROSION IAW SRM 51-21-06. SKIN .063, MATERIAL REMOVED .004, REMAINING .059. DAMAGE IS OUT OF LIMITS OF SRM IAW SRM 53-00-31. REPAIRED IAW REO 601R-53-21-2215.

Part: BULKHEAD WEB — CRACKED · airframe 22,998 hrs · 20,566 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION.

Part: BULKHEAD — CRACKED · airframe 22,998 hrs · 20,566 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 36.20 WL 80 APPROX .750" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1285 REV B.

Part: FRAME — CORRODED (BS 333) · airframe 22,998 hrs · 20,566 cycles

FUSELAGE FRAME IS CORRODED AT ACFT BELLY CENTER LINE FS 333.

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,998 hrs · 20,566 cycles

FUSELAGE EXTERNAL SKIN HAS AREAS OF CORROSION UNDER THE FWD DOOR HINGE FAIRING. REPAIRED IAW REO 601R-53-21-2223.

Part: SKIN — CORRODED (BS 343-364) · airframe 22,998 hrs · 20,566 cycles

FUSELAGE EXTERNAL SKIN HAS SEVERAL AREAS OF CORROSION BETWEEN FS 343 AND 364 BETWEEN STR 17 AND 19 LEFT. REMOVED CORROSION IAW SRM 51-21-06 TO WITHIN ALLOWABLE DAMAGE LIMITS OF SRM 53-00-31.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 22,998 hrs · 20,566 cycles

RT FLOOR SUPPORT SILL AT FS 559+16 - 559+32 CORRODED. REMOVED CORROSION IAW SRM 51-21-06. REPAIR WITHIN THE LIMITS. APPLIED TREATMENT & PAINT IAW SRM 51-21-00.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 22,998 hrs · 20,566 cycles

LT FLOOR SUPPORT SILL FROM FS 559 - 559+112 CORRODED. BLENDED DAMAGE IAW SRM 51-42-00. APPLIED TREATMENT & PAINT IAW SRM 51-21-00.

Part: BULKHEAD WEB — CRACKED · airframe 22,998 hrs · 20,566 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .5" IN LENGTH 70 PERCENT FSH, FAILED NDT INSPECTION.

Part: WEB — CRACKED (BS 280) · airframe 22,998 hrs · 20,566 cycles

FS 280 WEB CRACKED OTBD LBL9 AFT J ANGLE CRACKED. REPAIRED IAW REO 601R-53-11-826 & REO 601R-53-11-926, REV B.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 22,998 hrs · 20,566 cycles

FS 349.00, RBL 27 TO SILL FLOORBEAM CORRODED. REMOVED CORROSION IAW REO 601R-53-21-2222. FOUND OUT OF LIMITS.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 22,998 hrs · 20,566 cycles

RT FLOOR SUPPORT AT FS 559+80 - 621 CORRODED. REMOVED CORROSION IAW SRM 53-00-00 & 51-21-06. ALODINED, PRIMED & PAINTED IAW SRM 51-21-06.

Part: SILL — CORRODED · airframe 22,998 hrs · 20,566 cycles

RT SILL FLOOR SUPPORT CORRODED. SERVICEABLE SILL PLATE INSTALLED IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 22,998 hrs · 20,566 cycles

FLOORBEAM RBL 9 AT FS 484 IS CRACKED IN UPPER RADIUS. R & R FLOORBEAM IAW SRM 51-42-06 & REO 601R-53-41-1514, STEPS 1 & 2.

Part: FRAME — CORRODED (BS 333) · airframe 22,998 hrs · 20,566 cycles

FUSELAGE FRAME IS CORRODED AT ACFT BELLY CENTERLINE FS 333. REMOVED FRAME IAW SRM 51-42-06. LOCATED, DRILLED & INSTALLED FRAME IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 349) · airframe 22,998 hrs · 20,566 cycles

FUSELAGE FRAME IS CORRODED AT ACFT BELLY CENTERLINE FS 349. REMOVED AND INSTALLED FRAME IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 22,998 hrs · 20,566 cycles

RIGHT SILL FLOOR SUPPORT FITTING IS CORRODED FS 319.70, RT BL 46. REPAIRED IAW SRM 51-42-06, 51-41-11 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 22,998 hrs · 20,566 cycles

FLOORBEAM RBL 27 AT FS 484 IS CRACKED IN UPPER RADIUS. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-21.

Part: BULKHEAD WEB — CRACKED · airframe 22,998 hrs · 20,566 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 80 APPROX .750" IN LENGTH 50 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 AND 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,998 hrs · 20,566 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED APPROX .70" LONG. INSTALLED NEW DRAG ANGLE IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 621-625) · airframe 22,998 hrs · 20,566 cycles

FS 621- 625 LT & RT OBLIQUE ANGLES CRACKED. REMOVED ANGLES. FITTED, DRILLED AND DEBURRED AND INSTALLED NEW ANGLES IAW SRM 51-42-21.

Part: SKIN — CORRODED (BS 564) · airframe 22,998 hrs · 20,566 cycles

CORROSION ON FUSELAGE EXTERNAL SKIN AT FS 564.00+8 BETWEEN STRS 22R AND 21R. FOUND TO BE WITHIN ALLOWABLE LIMITS OF 53-61-31, 53-00-31. BLENDED IAW SRM 51-12-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,742 hrs · 19,186 cycles

RT EXTERIOR NR 1 EMERGENCY EXIT LIGHT INOP. RELAMPED RT EXTERIOR NR 1 EMERGENCY LIGHT IAW AMM 33-51-21. OP'S CHECK GOOD. RELAMPED RT EXTERIOR NR 1 EMERGENCY LIGHT IAW AMM 33-51-21. OP'S CHECK GOOD. (CLOSED)

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 20,667 hrs · 17,969 cycles

RT EXTERIOR NR1 EMERGENCY LIGHT IS INOP. RELAMPED RT EXTERIOR NR1 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD. RELAMPED RT EXTERIOR NR1 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,287 hrs · 17,547 cycles

GALLEY FWD WARDRODE LOWER EMERGENCY FLOODLIGHT HAS SEVERAL LAMPS BURNED OUT. RELAMPED GALLEY FWD WARDROBE LOWER EMERGENCY FLOODLIGHT IAW AMM 33-51-19. OPS CK GOOD. RELAMPED GALLEY FWD WARDROBE LOWER EMERGENCY FLOODLIGHT IAW AMM 33-51-19. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,851 hrs · 17,044 cycles

EMERGENCY LIGHT IS INOP. R & R PAX DOOR EXIT, OPEN AND OPEN ARROW PLACARDS IAW AMM 11-30-00. ITEM: 1 03-29-2010 R & R PAX DOOR EXIT, OPEN AND OPEN ARROW PLACARDS IAW AMM 11-30-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,851 hrs · 17,044 cycles

NR 6 EXTERIOR EMERGENCY LIGHT IS INOP. RELAMPED NR 6 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD ITEM: 1, 03-29-2010 RELAMPED NR 6 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD.

Part: LIGHT — INOPERATIVE · airframe 19,270 hrs · 16,393 cycles

FWD RT EMERGENCY LIGHT ON EXTERIOR INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,203 hrs · 16,321 cycles

EMERGENCY LIGHTS ON GALLEY AND WARDROBE INOP.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 19,203 hrs · 16,321 cycles

FLOOR SUPPORT LOCATED AT RBL 9 FS 559+16 TO 559+80 IS CORRODED. REMOVED FLOOR SUPPORT AT RBL 9 FS 559+16 TO 570 IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED NEW FLOORBEAM SUPPORT IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE SUPPORT IAW REO 601R-55-00-337 AND MEETS ALL ITS REQUIREMENTS. LOCATED AND INSTALLED BLIND NUTS IAW SRM 51-42-34. LOCATED AND DRILLED NUTPLATES ON BEAM SUPPORT IAW SRM 51-42-15. INSTALLED NUTPLATES IAW SRM 51-45-00.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 19,203 hrs · 16,321 cycles

LT MLG DOOR OUTER SKIN IS CRACKED AND GOUGED BETWEEN DOOR MOUNT LUGS. NEW LT MLG DOOR REQUIRES PAINTING TO MATCH THE ORIGINAL DOOR. PAINTED NEW DOOR IAW SRM 51-25-01 PART B1 SECTION 8 A-G AND PART A SECTION 9 1-3. INSTALLED SERVICEABLE LT MLG DOOR IAW AMM 32-12-01-400-801 STEPS 1-2(9). PERFORMED ADJUSTMENT OF LT MLG IAW AMM 32-12-01-400-801 PARA 3A CHECKS GOOD AT THIS TIME. LT MLG DOOR WAS REMOVED ON 8760811, OP 236.

Part: SEAT TRACK — DAMAGED (BS 559.80) · airframe 19,203 hrs · 16,321 cycles

CARGO BAY SEAT TRACK SEGMENT LBL 27 FS 559.80 AND 559+96 FITTING ASSY FOR BULKHEAD ATTACHMENT BROKEN PN CDSP1900-509. REMOVED AND REPLACED FITTING ASSY FOR BULKHEAD ATTACHMENT AT LBL 27, FS 557.80 AND 559+96 IAW SRM 51-41-04.

Part: POST — CRACKED (BS 409) · airframe 19,203 hrs · 16,321 cycles

FOUND FS 409.0+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS A INDICATION NOTED AT WL 69.0 APPROX .2 IN LENGTH 50 PERCENT FSH FAILED NDT INSP AREA MARKED ON ACFT. REMOVED FS 409.0+128 VERTICAL POST LBL 18.0 IAW SRM 51-42-06. LOCATED AND DRILLED NEW FS 409+128 VERTICAL POST LBL 18 OTBD SIDE IAW SRM 51-40-11. INSTALLED VERTICAL POST AT LBL 18 ASSY IAW REO 601R-53-41-889 EC/TC 601R-53-41-889. FILLET SEALED REPAIR AREA AT FS 409+128 LBL 18.0 AND APPLIED CORROSION INHIBITOR IAW SRM 51-25-00 AND 51-21-11. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 19,203 hrs · 16,321 cycles

FOUND FS 409.0+128 VERTICAL POST BL 0.0 LT/RT HAVE INDICATIONS NOTED AT WL 69.0 APPROX .2" IN LENGTH 90 PERCENT FSH FAILED NDT INSP, AREAS MARKED ON ACFT. REMOVED INBD EXHAUST VALVE AIR DUCT PN X9064 FOR ACCESS IAW SRM 51-41-00. AIR DUCT X9064 NEEDS INSTALLED AFTER REPLACEMENT OF POST AT BL 0.0 409H28. REMOVED VERTICAL POST AT BL 0 LT AND RT IAW SRM 51-42-06. LOCATED AND DRILLED BL 0.0. LT AND RT 409+128 POST. RIVETED POST TOGETHER IAW SRM 51-42-06 AND 51-42-21. BL 0.0. POST REQUIRES INSTALL. INSTALLED BL 0.0. POST AT FS. 409+128 IAW SRM 51-42-06 + 51-42-21. INSTALLATION OF THE POST AT FS 409+128, BL 0 USING PLT 214-5 OR PLT 214-6 IS COMPLETED IAW REO 601R-53-41-1105 AND MEETS WITH ALL ITS REQUIREMENTS.

Part: LIGHT — BROKEN (GALLEY) · airframe 19,203 hrs · 16,321 cycles

G1 GALLEY TRIM PANEL HAS BROKEN EMERGENCY EXIT LIGHT. REMOVED AND REPLACED EMERGENCY LIGHT ON G1 GALLEY TRIM PNL IAW AMM 33-51-10-000-801 AND 33-51-10-400-801. OPS CHECK DUE. OPS TEST IS GOOD IF THE SERVICE DOOR FLOOR-LEVEL FLOODLIGHT ON GALLEY TRIM PANEL IAW AMM TASK 33-51-00-710-801.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 19,202 hrs · 16,321 cycles

CARGO BAY SEAT TRACK SEGMENT RBL 27.0 FS 559+80 TO FS 559+96 CORRODED. REMOVED CORRODED SEAT TRACK IAW SRM 51-41-02. LOCATED, DRILLED, AND COUNTERSUNK NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE SEAT TRACK IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 19,203 hrs · 16,321 cycles

CARGO BAY SEAT TRACK SEGMENT RBL 9.0, FS 559+95 TO FS 567.0 IS CORRODED. REMOVED CARGO BAY SEAT TRACK IAW SRM 51-41-02. LOCATED, DRILLED, AND COUNTERSUNK NEW TRACK SEGMENT IAW SRM 51-40-11. INSTALLED NEW TRACK SEGMENT RBL 9 FS 559+96 TO FS 567.0 IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 19,203 hrs · 16,321 cycles

CARGO BAY SEAT TRACK SEGMENT LBL 9.0 FS 559+95 TO FS 567.0 CORRODED. REMOVED CORRODED TRACK IAW SRM 51-41-02. LOCATED, DRILLED, AND COUNTERSUNK HOLES IN NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE SEAT TRACK IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (BS 618-621) · airframe 19,203 hrs · 16,321 cycles

CARGO SEAT TRACK SEGMENT LBL 9.0, FS 618.0 TO FS 621.0 IS CORRODED. REMOVED CARGO BAY SEAT TRACK SEGMENT LBL 9 FS 618.0 TO FS 621.0 IAW SRM 51-41-02. LOCATED, DRILLED, AND COUNTERSUNK NEW TRACK SEGMENT IAW SRM 51-40-11. INSTALLED NEW CARGO SEAT TRACK SEGMENT LBL 9 FS 618.0 TO FS 621.0 IAW SRM 51-41-02.

Part: ANCHOR FITTING — CORRODED (FUSELAGE) · airframe 19,202 hrs · 16,321 cycles

CARGO BAY ANCHOR FITTINGS (3) ON LBL 27.0 (2) ON LBL 9.0 ARE CORRODED. REMOVED THE ANCHOR FITTINGS ON LBL 9. INSTALLED NEW SERVICEABLE FITTINGS IAW SRM 51-41-02. ANCHOR FITTINGS 3EA ON LBL 27.0 REQUIRE REPAIR OR REPLACEMENT. REMOVED UNSERVICEABLE ANCHOR FITTINGS 3 EA LBL 27 AND REPLACED WITH SERVICEABLE ANCHORS 3 EA IAW SRM 51-41-02-51-41-01.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,203 hrs · 16,321 cycles

CABIN SEAT TRACK FS 559 TO 559+84 RBL 9.0 BADLY CORRODED. REMOVE CABIN SEAT TRACK AND LOCATED AND COUNTERSUNK NEW SERVICEABLE CABIN SEAT TRACK IAW AMM 53-01-11-000-802 AND SRM 51-41-02. INSTALLED NEW SERVICABLE SEAT RAIL IAW AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (BS 559) · airframe 19,203 hrs · 16,321 cycles

FOUND FS 559 HAS 3 INDICATIONS NOTED: AT LT WEB WL 51.70 O/B OF LBL 9.0 APPROX .2" IN LENGTH 50 PERCENT FSH, AT RT WEB WL 58.70 OTBD OF RBL 9.0 APPROX .2" IN LENGTH 90 PERCENT FSH, AND 3) AT RT WEB WL 59.10 INBD OF RBL 18.0 APPROX .4" IN LENGTH 70 PERCENT FSH. ALL FAILED NDT INSP. LT WEB AT WL 51.70 OF LBL 9.0 REPAIRED ON 8760815 OP 120 AND CO NR 7608109. CONTINUE FS 559 REPAIR IAW REO 601R-53-41-260 REV D. REPAIRED PRESSURE BULKHEAD STRUCTURE FS 559 BL FROM 23L TO 23R IAW REO 601R-53-41-260 REV D. C/W EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 19,203 hrs · 16,321 cycles

CARGO DOOR SUPPORT BEAM LWR AFT ANGLE IS CRACKED APPROX 1.5" IN LENGTH. REMOVED CARGO DOOR SUPPORT BEAM LWR AFT ANGLE, LOCATED AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,203 hrs · 16,321 cycles

CARGO BAY SEAT TRACK SEGMENT LBL 9.0 FS 559+84 TO 559+96 IS CORRODED. REMOVED IAW SRM 51-41-02. LOCATED, DRILLED, AND COUNTERSUNK NEW TRACK SEGMENT IAW SRM 51-40-11. INSTALLED NEW TRACK SEGMENTS LBL 9 FS 559+84 TO FS 559+96 IAW SRM 51-41-02.

Part: SEAT TRACK — DAMAGED (BS 559) · airframe 19,202 hrs · 16,321 cycles

REMOVED SEAT TRACK FS 559+80 TO FS 559+96 LBL 27 SRM 51-41-02. LOCATED, DRILLED, AND COUNTERSUNK NEW TRACK SEGMENT IAW SRM 51-40-11. INSTALLED NEW TRACK SEGMENTS FS 559+80 TO FS 559+96 LBL 27 IAW SRM 51-41-02.

Part: ISOLATOR — CRACKED (PRESSURE BLKHEAD) · airframe 19,202 hrs · 16,321 cycles

FOUND 6 ISOLATORS CRACKED ON REAR PRESSURE BULKHEAD BRACKETS, 4 LOCATED OTBD OF RBL 36.0 BETWEEN WL 73 AND WL 120.43, 1 LOCATED RBL 9.0 APPROX WL 100 AND 1 LOCATED LBL 9.0 APPROX WL 100. REMOVED AND REPLACED 6 ISOLATORS ON REAR PRESSURE BULKHEAD BRACKETS 4 LOCATED OTBD OF RBL 36.0 BETWEEN WL 73 AND WL 120.43.1 LOCATED AT RBL 9.0 APPROX WL 100 AND 1 LOCATED AT LBL 9.0 APPROX WL 100 IAW SRM 51-42-10 STEPS 6, 7, 8, AND 9 AND 51-42-13 STEPS 3, 6, 7, 8, AND 11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 19,202 hrs · 16,321 cycles

CARGO BAY SEAT TRACK SEGMENT RBL 9.0, FS 559+84 TO 559+46 IS CORRODED. REMOVED CORRODED SEAT TRACK IAW SRM 51-41-02. LOCATED AND DRILLED AND COUNTERSUNK NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE SEAT TRACK IAW SRM 51-41-02.

Part: PLATE — CORRODED (CARGO DOOR SEAL) · airframe 19,203 hrs · 16,321 cycles

ENTIRE LENGTH OF CARGO DOOR SEAL PLATE HAS MINOR CORROSION.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 19,203 hrs · 16,321 cycles

FS 484 LBL 27.0 INTERCOSTAL ANGLE CRACKED. REMOVED AND REPLACED FS 484, LBL 27.0 INTERCOSTAL ANGLE IAW SRM 51-42-06 AND REO 601-R53-41-1106.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,203 hrs · 16,321 cycles

BULKHEAD REPAIR REQUIRES DEVIATION, DUE TO CRACK AT WEB LT WL 51.7" OTBD OF LBL 9 APPROX .2" LONG, DEVIATION FROM REO 601R-53-41-260. C/W F.S. 559 BULKHEAD REPAIR DEVIATION TO LT WEB AREA IAW REO 601R-53-41-609 DEVIATION B C/W EC/TC 601R-53-41-609 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-609 REV A.

Part: PRESSURE BLKHD — DAMAGED (BS 621) · airframe 19,202 hrs · 16,321 cycles

REPAIRED FS 621 REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1230 REV D. REPAIR IAW EC/TC REO 601R-53-61-1230 HAS BEEN COMLETED AND THE REPAIR C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.

Part: INTERCOSTAL — CRACKED (BS 621-625 S14R) · airframe 19,203 hrs · 16,321 cycles

RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED IN RADIUS APPROX .7" LONG. REMOVED DAMAGED INTERCOSTAL FROM STR 14R COMMON TO FS 621.00 - FS 625.30 AND REPLACED WITH NEW SERVICEABLE PART IAW SRM 51-42-21 AND PAINTED.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 19,203 hrs · 16,321 cycles

LT SIDE, FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED IN RADIUS APPROX 1.1" LONG. REMOVED INTERCOSTAL FROM STR 14L COMMON TO FS 621.00 AND 625.30 AND REPLACED WITH NEW SERVICEABLE PART IAW SRM 51-42-21 AND PAINTED IAW SRM 51-21-16.

Part: PLACARD — MISSING (PAX DOOR) · airframe 17,592 hrs · 14,708 cycles

F/A REPORTS EXIT PLACARD MISSING FROM PAX DOOR. FLT 5032 DEL 19 MINS.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 17,303 hrs · 14,453 cycles

F/A REPORTED EMERGENCY LIGHT FLOOR LEVEL LIGHT STRIP (REAR 1/2) ORANGE STRIP "EXIT DIRECTION" IS AT ROW 12 NOT BY AN EXIT.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 16,960 hrs · 14,142 cycles

SERVICE DOOR REALLY HARD TO CLOSE. LUBED SERVICE DOOR HANDLE IAW CRJ200, AMM 52-41-01.

Part: FLAP — MALFUNCTIONED (WING) · airframe 15,093 hrs · 12,550 cycles

FLAPS FAILED AT 0 DEGREES, LANDED IN MOBILE 0 DEGREES FLAPS 165KTS, 42000 LBS, HIGHEST BREAK TEMP 05. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY.

Part: FLAP — MALFUNCTIONED (WING) · airframe 15,093 hrs · 12,550 cycles

FLAPS FAILED AT ZERO WHEN SELECTING 8 ON DESCENT. EMERGENCY EQUIPMENT ON STANDBY. FLT 4257 DEL 115 MINS.

Part: FLAP SYSTEM — WARNING LIGHT (TE FLAPS) · airframe 14,926 hrs · 12,400 cycles

OBSERVED FLAPS FAIL MSG ON APPROACH WHEN FLAP HANDLE AT 8*, EMERGENCY DECLARED.

Part: TIP CAP — CRACKED (HORIZ STAB) · airframe 14,898 hrs · 12,377 cycles

AAR - RIGHT HORIZONTAL STABILIZER TIP HAS CRACK ON LEADING EDGE TIP.

Part: TIP CAP — CRACKED (HORIZ STAB) · airframe 14,898 hrs · 12,377 cycles

AAR - LEFT HORIZONTAL STABILIZER TIP HAS CRACK ON LEADING EDGE TIP.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,892 hrs · 12,370 cycles

SEAT TRACK NR 2 FROM FWD ON RIGHT SIDE FLOOR HAS CORROSION (MARKED). 10-30-07 REMOVED CORROSION FROM SEAT TRACK NR 2 FROM FWD ON RT SIDE FLOOR IAW CRJ 200 SRM 51-21-06. APPLIED CHEMICAL CORROSION COATING TO REPAIRD AREA IAW CRJ 200 SRM 51-21-11. THE CORROSION REMOVED WAS WITHIN THE ALLOWABLE LIMITS OF CRJ 200 SRM 53-31-49. REMOVED .003 THICKNESS FROM SEAT TRACK THICKNESS.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 14,892 hrs · 12,370 cycles

FS 280 HAS CRACKED CLIP AT 19.5 LBL POSITION. 10-30-07 REMOVED DAMAGED CLIP AT FS 280 LBL 9 O/B POSITION AND DUPLICATED PER CRJ SRM 53-21-43 FIG 1 ITEM 6, IAW CRJ SRM 51-24-21, 51-40-11, 51-26-16 AND INSTALLED IAW CRJ SRM 51-23-00 AND 51-42-21 AT FS 280 LBL 9 O/B POSITION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,892 hrs · 12,370 cycles

FLOOR SUPPORT ANGLE AT PAX DOOR ENTRANCE HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT ANGLE AT PAX DOOR ENTRANCE IAW CRJ 200 SRM 51-21-06. OK TO ALODINE, PRIME AND TOPCOAT. ALODINE REPAIR AREA IAW CRJ 200 SRM 51-21-11. APPLIED PRIME TO REPAIR AREA IAW CRJ 200 SRM 51-25-06 AND APPLIED TOPCOAT TO REPAIR AREA IAW CRJ 200 SRM 51-25-16. THE CORROSION REMOVED WAS WITHIN THE ALLOWABLE LIMITS OF THE CRJ 200 SRM 53-00-00. REMOVED .003 THICKNESS FROM ANGLE.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 14,892 hrs · 12,370 cycles

FS 280 HAS CRACKED CLIP AT 10.25 RBL POSITION. 10-30-07 REMOVED DAMAGED CLIP AT FS 280 LBL 9 I/B POSITION AND DUPLICATED PER CRJ SRM 53-21-43 FIG. 1 ITEM 6, IAW CRJ SRM 51-24-21, 51-40-11, 51-21-16 AND INSTALLED IAW CRJ SRM 51-23-00 AND 51-42-21 AT FS 280 LBL 9 I/B POSITION.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 14,892 hrs · 12,370 cycles

CLIP CRACKED AT FS 484 I/B OF RBL 36. 10-30-07 CUT AWAY DAMAGED ATTACHMENT FLANGE OF 601R31171-15 REF AS SHOWN IN SHEET 3 OF REO 601R-53-41-059 REV A. PERFORMED LPI OF CUTLINE PER DNTM 51-20-08 IAW ASA REO 601R-53-41-059 REV A SHEET 3 STEP 2. NO DEFECTS NOTED. OK TO TOUCH UP CUT EDGE TOUCH UP FINISH A023 PER CRJ SRM 51-21-16 FABRICATED ANGLE, INSTALLED ANGLE IAW ASA REO 601R-53-41-059.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 14,892 hrs · 12,370 cycles

PAX DOOR OUTER HANDLE IS CRACKED. 11-01-07 REMOVED UNSREVICEABLE PAX DOOR OUTER HANDLE ASSY IAW CRJ 200 AMM 52-11-03-020-007. INSTALLED NEW SERVICEABLE SLEX HANDLE ON NEW SERVICEABLE HANDLE IAW CRJ 200 SRM 51-42-06. INSTALLED THE REMAINDER OF HARDWARE ON NEW SERVICEABLE HANDLE IAW CRJ 200 AMM 52-11-03. OK TO ISTALL ON PAX DOOR. INSTALLED NEW SERVICEABLE PAX DOOR OUTER HANDLE. COLLARS, WASHERS IAW CRJ 200 AMM 52-11-03-420-003. INSTALLED PLACARD, TO OUTER HANDLE IAW CRJ 200 AMM 11-20-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,892 hrs · 12,370 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 280, O/B OF LBL 9.00. 10-30-07 COMPLIED WITH ASA CARD NR REO 601R-53-11-138.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 14,892 hrs · 12,370 cycles

FS 280 CLIP CRACKED RBL 9.0 O/B. 10-30-07 REMOVED UNSERVICEABLE CLIP FS 280 O/B OF FS 9. INSTALLED NEW CLIP.

Part: SKIN — CRACKED (PAX DOOR) · airframe 14,892 hrs · 12,370 cycles

PAX DOOR STAIRS FWD SKIN IS CRACKED IN RADIUS UNDER STEP 832DT. 10-30-07 REMOVED DAMAGE SECTION OF PAX DOOR STAIRS SKIN UNDER FWD STEP 832 DT IAW REO 601R-52-11-702. CUTOUT REQUIRES LPI OF THE EDGES. PERFORMED LPI OF THE PAX DOOR STAIRS FWD SKIN UNDER STEP 832 DT REPAIR CUTOUT IAW CRJ 200 NDTM 51-20-08, NO DEFECTS NOTED. REPAIR COMPLETED IAW REO 601R-52-11-702.

Part: SUPPORT BEAM — CRACKED (BS 280) · airframe 14,892 hrs · 12,370 cycles

AFT FS 280 SUPPORT BEAM CRACKED AT 12 O'CLOCK RBL POSITION ON LOWER RADIUS. 10-30-07 COMPLIED WITH REO 601R-53-11-171 IAW ASA EO 600-53-0090.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 14,892 hrs · 12,370 cycles

FS 280 CLIP CRACKED, RBL 9.0 I/B. 10-30-07 REMOVED DAMAGED CLIP AT FS 280 RBL 9 I/B POSITION AND DUPLICATED PER CRJ SRM 53-21-43 FIG. 1 ITEM 6. IAW CRJ SRM 51-24-21, 51-40-11, 51-21-16 AND INSTALLED IAW CRJ SRM 51-23-00 AND 5142-21 AT FS 280 RBL 9 I/B POSITION.

Part: SKIN — CRACKED (PAX DOOR) · airframe 14,892 hrs · 12,370 cycles

PAX DOOR STAIRS AFT SKIN IS CRACKED IN RADIUS UNDER STEP 832DT. 10-30-07 REMOVED DAMAGE SECTION OF AFT PAX DOOR STAIRS SKIN UNDER STEP 832DT IAW REO 601R-52-11-702. CUTOUT REQUIRES LPI OF THE EDGES. PERFORMED LPI ON THE PAX DOOR STAIRS AFT SKIN UNDER STEP 832DT REPAIR CUTOUT IAW CRJ 200 NDTM 51-20-08. NO DEFECTS NOTED, REPAIR COMPLETED IAW REO 601R-52-11-702.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 14,892 hrs · 12,370 cycles

CLIP CRACKED AT FS 484 O/B OF RBL 27. 10-30-07 REMOVED CRACKED CLIP AT FS 484. LOCATED AND DRILLED NEW ANGLE IAW REO 601R-53-41-057. OK TO TREAT AND PRIME. TREATED PRIMED AND TOPCOATED IAW CRJ SRM 51-21-11 51-25-06 51-25-16. OK TO INSTALL NEW ANGLE. INSTALLED CLIP IAW CRJ SRM 51-42-21 AND REO 601R-53-41-059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,892 hrs · 12,370 cycles

RIGHT I/B BATH TUB FITTING CRACKED. 10-30-07 REMOVED 2 ACCESS PANELS JUST O/B OF BATHTUB FITTING IAW CRJ 200 SRM 51-41-02. LOCATED HOLES IN SERVICEABLE FITTING P/N 600-31068-19 IAW CRJ 200 SRM 51-40-11. OK TO INSTALL. INSTALLED ALL LOCK FASTENERS THROUGH SERVICEABLE FITTING P/N 600-31068019 IAW CRJ 200 SRM 51-42-21. REQUIRES INSTALLATION OF SOLID RIVETS. ISNTALLED SOLID RIVETS IAW CRJ SRM 51-42-06. OK TO REINSTALL TWO EA INSP PNLS O/B OF FILLING. REINSTALLED 2EA PNLS IAW CRJ SRM 51-41-02. REINSTALLED PREVIOUS REMOVED 4EA WIRE BUNDLE TIE DOWN BRACKETS. IAW CRJ SRM 51-41-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 14,892 hrs · 12,370 cycles

LT UPPER ENGINE BEAM O/B ATTACH ANGLE OF AFT RADIUS, CRACKED. 10-30-07 REMOVED CRACKED LT UPPER ENGINE BEAM O/B ATTACH ANGLE. LOCATED NEW SERVICEABLE ANGLE. OK TO INSTALL. INSTALLED ANGLE IAW CRJ SRM 51-42-21. OK TO TOPCOAT FASTENERS. APPLIED TOPCOAT TO FASTENERS IAW CRJ SRM 51-21-16.

Part: PLACARD — DAMAGED (PAX DOOR) · airframe 14,892 hrs · 12,370 cycles

PAX DOOR EXIT PLACARD IS DAMAGED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 14,892 hrs · 12,370 cycles

AAR - PAX DWR AFT DRAG ANGLE CRACKED. 10-30-07 CUT AWAY DAMAGED SECTION OF AFT DRAG ANGLE AND REMOVED BURRS AND SHARP EDGES IAW BOMBARDIER REO 601R-52-11-513, PERFORMED LPI PER NDTM 51-20-08 ON REORKED AREAS AND CUTOUT EDGES OF PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513, NO DEFECTS NOTED. TOUCHED UP CUT EDGES IAW REO 601R-52-11-513. FABRICATED REPAIR ANGLE AND SPLICE ANGLES IAW REO 601R-52-11-513. OK TO INSTALL. INSTALLED REPAIR ANGLE AND SPLICE ANGLES, SANDED FARING SURFACES, FILLET SELECTED EDGES, APPLIED TOPCOAT IAW BOMBARDIER REO 601R-52-11-513.

Part: PLACARD — UNKNOWN (ESCAPE HATCH) · airframe 14,892 hrs · 12,370 cycles

PLACARDS ON EMERGENCY ESCAPE HATCH REQUIRES REPLACEMENT. 10-25-07 REMOVED EMERGENCY ESCAPE HATCH PLACARDS IAW CRJ 200 AMM 11-10-03. INSTALLED SERVICEABLE PLACARDS OPEN P/N S1875, CLOSED P/N S1874, CURVED ARROW P/N S1887, EMERG. EXIT PUSH AND P/N S1859 IAW CRJ 200 AMM 11-20-00.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 14,892 hrs · 12,370 cycles

PAX DOOR FWD ANCHOR FITTING IS CRACKED. 11-01-07 REMOVED UNSERVICEABLE PAX DOOR FWD ANCHOR FITTING IAW CRJ 200 AMM 52-11-17-400-803. OK TO INSTALL. INSTALLED FWD ANCHOR FITTING P/N 601R38074-6 PO 95-1202 IN SERVICEABLE CONDITION IAW CRJ 200 AMM STILL REQUIRES PIN FOR CABLE. INSTALLED SERVICEABLE UPPER PIN ON PAX DOOR FWD CABLE (PIN P/N MS20392-3C23) AS PER CRJ 200 52-11-17. REQUIRES OPS CHECK. PERFORMED OPS CHECK OF PAX DOOR COUNTERBALANCE AS PER CRJ 200 AMM 52-11-17. TESTED GOOD. PERFORMED THE ADJUSTMENT OF PAX DOOR COUNTER BALANCE SYSTEM AS PER CRJ 200 AMM 52-11-17.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 14,770 hrs · 12,276 cycles

BRACKET AFT OF ASD BOTTOM STEP IS CRACKED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 14,531 hrs · 12,070 cycles

STAB TRIM, MACH TRIM CAUTION MSG. EMERGENCY DECLARED. EMERGENCY EQUIP ON STANDBY.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,414 hrs · 11,982 cycles

PILOT REPORT GARBAGE LIKE SMELL IN COCKPIT DURING DESCENT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 14,257 hrs · 11,867 cycles

AFTER DEPARTING BTR, RECEIVED -GEAR DISAGREE, WOW INPUT GEAR UNSAFE, NOSE WHEEL STEERING INOP- MSG. IN THE COCKPIT VERIFIED THROUGH NOISE AND VIBRATION THAT THE NOSE GEAR WAS NOT UP AND LOCKED. COMPLIED WITH QRH. A/C RETURNED TO BTR AFTER T/O. EMERGENCY DECLARED. RELATED TO DEFECT NR 317576-2. FLT 4703 CX.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 13,152 hrs · 11,016 cycles

FLAP FAIL AT ZERO ON APPROACH. EMERGENCY DECLARED.

Part: SKIN — CRACKED (BS 169) · airframe 12,974 hrs · 10,884 cycles

ETNRC 2000-13 LOWER SKIN AT FS 169.00 BETWEEN LBL 12.00 AND RBL 12.00 IS CRACKED. LOWER SKIN AT FS 169.00 BTW LBL 12.00 AND RBL 12.00 REMOVED AND REPLACED IAW SRM 51-42-06.

Part: FRAME — CRACKED (BS 171) · airframe 12,974 hrs · 10,884 cycles

ETNRC 2000-16 LOWER FRAME AND SUPPORT CLIPS AT FS 171.00 BETWEEN LBL 12.00 AND RBL 12.00 ARE BENT, CRACKED. LOWER FRAME AND SUPPORT CLIPS AT FS 171.00 BTW LBL12.00 AND RBL 12.00 REMOVED AND REPLACED IAW SRM 51-42-06.

Part: SHEAR TIE — CRACKED (BS 169) · airframe 12,974 hrs · 10,884 cycles

ETNRC 2000-15 LOWER LLEFT SKIN ANGLE AT FS 169.00 LBL 12.00 IS CRACKED. LOWER LT SKIN ANGLE AT FS 169.00 LBL12.00 REMOVED AND REPLACED IAW SRM 51-42-06.

Part: FLAP — FAILED (WING) · airframe 12,896 hrs · 10,825 cycles

FLAPS FAIL ON APPROACH. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,676 hrs · 9,878 cycles

VERY AFT FLOOR EMERGENCY LIGHT INOP.

Part: RIB — CRACKED (LT WING) · airframe 11,324 hrs · 9,597 cycles

FOUND LT BATT RIB CRACKED. REPAIRED LT BATT RIB IAW REO 601R-57-51-046. KW 10175.

Part: HINGE — CORRODED (PAX DOOR) · airframe 11,324 hrs · 9,597 cycles

FOUND PAX DOOR UPPER STEP HINGE CORRODED. REMOVED AND REPLACED HINGE 601R 31980-41, IAW CRJ SRM 51-40-11 AND 51-41-02.

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENGINE)

DURING DESCENT FROM ATL-CAK, AT APPROXIMATELY 20,000 FEET, THE FIRE WARNING SYSTEM FOR THE RIGHT ENGINE SOUNDED. THE CREW SHUTDOWN THE RIGHT ENGINE AND FIRED BOTH FIRE BOTTLES. AN EMERGENCY WAS DECLARED, WITH ALL EMERGENCY VEHICLES DISPATCHED. THE AIRCRAFT PERFORMED A SINGLE ENGINE LANDING IN CAK, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED BOTH FIRE BOTTLES. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOOR — OBSTRUCTED (MAIN PAX)

DURING A GROUND INSPECTION, THE PAX DOOR WAS FOUND DIFFICULT TO CLOSE. MAINTENANCE REMOVED AND OBJECT FROM THE BOTTOM OF THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: DOOR — OVERSERVICED (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND TO BE DIFFICULT TO CLOSE. MAINTENANCE CLEANED THE EXCESS GREASE FROM THE LOCKING LUGS ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR FORWARD ANCHOR FITTING WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR FORWARD ANCHOR FITTING (P/N 601R380742) AND LEVER (P/N 601R319742). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: RESERVOIR — OVERHEATED (NR 1 HYD SYSTEM)

DURING CRUISE FROM ATL-YUL, AT APPROXIMATELY 33,000 FEET, THE CREW RECEIVED A NR 1 HYD TEMP HIGH EICAS MESSAGE. THE QRH WAS COMPLIED WITH AND UPON CHECKING THE NR 1 HYD TEMP THE CREW OBSERVED IT HOVERING APPROXIMATELY 110 DEGREES CELSIUS, BUT THEN ROSE TO 150 DEGREES C AND QUICKLY TO 191 DEGREES CELSIUS. THE CREW THEN SHUTDOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO SYR, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYDRAULIC RESERVOIR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: TRANSDUCER — FAILED (NR 1 HYD SYSTEM)

FLT 4620 - DURING CRUISE FROM ABE-ATL, AT APPROX 28,000 FEET THE CREW RECEIVED A HYD NR 1 HI TEMP MESSAGE. THE QRH WAS COMPLIED WITH AND THE CREW SHUTDOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO GSP, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYDRAULIC SYSTEM TRANSDUCER AND CONNECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: RESERVOIR — MALFUNCTIONED (HYD SYSTEM)

FLT 4292 - DURING CRUISE FROM ATL-SAT, AT APPROXIMATELY 30,000 FEET, THE CREW RECEIVED A HYD HI TEMP NR 1 CAUTION MESSAGE. THE QRH WAS COMPLED WITH, AN EMERGENCY WAS DECLARED AND THE CREW SHUTDOWN THE LEFT ENGINE. THE AIRCRAFT DIVERTED TO IAH AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC RESERVOIR AND HEAT EXCHANGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 7,363 hrs

DURING A C-CHECK, THE LT AND RT SIDE ENGINE SUPPORT BEAMS AT BL36.20 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT SIDE ENGINE SUPPORT BEAMS AT BL36.20 IAW EO600-53-0070.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 IAW EO 601R-53-61-1179.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK, RT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 IAW EO 600-53-0105.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CLIPS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS625.

Part: CLIP — CRACKED (FLOORBEAM)

DURING A C-CHECK, THE LT OB CLIP ON THE FLOORBEAM AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT OB CLIP ON THE FLOORBEAM AT FS 484, LBL 36 IAW EO 600-53-0098.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT CARGO AFT WALL TO FLOOR SUPPORT ANGLE AT FS 621 IAW EO. (K)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4512 - DURING A GROUND INSPECTIN IN BTR, THE EXTERIOR RIGHT MIDDLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR RIGHT MIDDLE EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 9773 - DURING A GROUND INSPECTION IN DFW, THE NR 2 EXTERIOR EMERGENCY LIGHT ON THE RIGHT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EXTERIOR EMERGENCY LIGHT LAMP ON THE RIGHT SIDE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR TRACK LIGHTS BETWEEN SEATS 10-C/D AND 11-C/D WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LAMP STRIP BETWEEN SEATS 10-C/D AND 11-C/D. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STRIKER — DEFECTIVE (EMERGENCY EXIT)

DURING GROUND INSPECTION AT BHM, THE LEFT OVERWING EMERGENCY EXIT INDICATED AN AMBER CAUTION MESSAGE WITH THE DOOR INSTALLED. DEFERRED IAW MEL 52-70-03. MAINTENANCE DETERMINED THE MICROSWITCH STRIKER PLATE IS NEEDED TO CLEAR THIS DEFERRAL. THE DEFERRAL WAS CLEARED BY MAINTENANCE REMOVING AND REPLACING THE MICROSWITCH STRIKER PLATE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (COCKPIT)

DURING TAKEOFF, BLEEDS OPEN AND APU DEFERRED, PILOT NOTED SMELL OF SOMETHING BURNING THAT WENT AWAY. ON ROTATION, SMELL CAME BACK VERY STRONG OUT OF VENTS ALONG WITH TRACE AMOUNTS OF SMOKE. PILOT SHUTOFF LEFT PACK WHICH STOPPED SMELL AND SMOKE COMING FROM VENTS. RT PRES GAUGE SHOWED 120 PSI AND LEFT SHOWED 138 PSI. AC RETURNED TO AIRPORT FOR A SAFE BUT OVERWEIGHT LANDING. MAINTENANCE PERFORMED AN OVERWEIGHT LANDING INSP WITH NO DEFECTS NOTED AT THAT TIME. MAINTENANCE RAN THE AC AT TAKEOFF POWER. 10TH STAGE BLEED PRESSURE WAS AT 118 PSI AND PACK PRESS READ 32 PSI. THERE WAS NO EVIDENCE OF SMELL OF SMELL OR SMOKE ONLY MINOR CONDENSATION FROM VENTS WAS OBSERVED. NO DEFECTS WERE NOTED. AC OK FOR SERVICE.