N617NN

ATA 3420

Part: IRU — UNSERVICEABLE (ZONE 100) · airframe 12,722 hrs · 12,039 cycles

PITCH FEEL FAULT STATUS MSG IN FLIGHT AND YD2 INOP, FMS 2 DISPLAYED IRS REVERTED LOST FO'S PFD INDICATION C/A REMOVED AND REPLACED IRU 2 IAW CRJ900 AMM 34-45-01-000/400-801-A01.

ATA 5712

Part: RIB — CRACKED (ZONE 600) · airframe 12,065 hrs · 11,550 cycles

CRACK ON RIB OF FIXED LEADING EDGE STA FS=58.41 (UPPER SIDE) AT RH WING. RIB OF FIXED LEADING EDGE STA FS=58.41 (UPPER SIDE) AT RH WING WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.

ATA 7830

Part: SLIDER — CORRODED (ZONE 400) · airframe 12,065 hrs · 11,550 cycles

CORROSION ON INB SLIDER AT UPPER TRANSCOWL ENG RH. UPPER TRANSCOWL RH WAS REPLACED PER CRJ900 AMM 78-33-01

ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

CORROSION ON SEVERAL POINTS SEAT RAIL BTW FS667 TO FS720.85 AND FS744.15 TO FS761.85 AT RBL15 CAB PAX. CORROSION ON SEVERAL POINTS SEAT RAIL BTW FS667 TO FS720.85 AND FS744.15 TO FS761.85 AT RBL15 CAB PAX WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ900 SRM 53-31-49-101-001-A02 AND SEAT RAILS WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801-A12

ATA 5345

Part: FITTING — CORRODED (ZONE 900) · airframe 12,065 hrs · 11,550 cycles

CORROSION FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-32-02

ATA 5345

Part: FITTING — CORRODED (ZONE 900) · airframe 12,065 hrs · 11,550 cycles

CORROSION ON FWD RH FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV. NEW FWD RH FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV WAS REPLACED SAFRAN CMM 25-40-40 REV. NO. 20

ATA 5320

Part: STRIP — CORRODED (ZONE 100) · airframe 12,065 hrs · 11,550 cycles

CORROSION ON METAL STRIP (LANDING DOOR), BTW STA FS 847 BTW STRINGER 20RH TO STRINGER 20LH, (UPPER/LWR AREA) WAS REWORKED AND FOUND OUT OF ALLOWABLE LIMITS. CORROSION ON METAL STRIP (LANDING DOOR), BTW STA FS 847 BTW STRINGER 20RH TO STRINGER 20LH, (UPPER/LWR AREA) WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ900 SRM 51-42-13-001-001-A01.

ATA 5751

Part: LUG — CORRODED (ZONE 600) · airframe 12,065 hrs · 11,550 cycles

AFTER BUSHINGS REMOVAL CORROSION WAS FOUND ON INTERNAL FACE LUGS R1, R2, R3, R4, R5 AND R6 AT CENTER FITTING RH AILERONON. LUGS R3, R4 AND R6 AT CENTER FITTING RH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND LUGS R1, R2 AND R5 WERE REPAIRED PER REO 670-57-61-237 REV:-- & REO 690-57-61-510 REV:-- -

ATA 5320

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 220.00 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 220.00 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE WAS PER REO 690-53-11-2169 REV -.

ATA 5530

Part: BEARING — EXCESS PLAY (RUDDER) · airframe 12,065 hrs · 11,550 cycles

FREE PLAY IN THE BEARINGS (2EA) OF THE CENTRAL HINGES OF THE RUDDER. FITTING #2 WAS REPLACED PER RIL #2103 REV.B AND BEARING ON FITTING #3 WAS REPLACED PER RIL #1213 REV. A.

ATA 5230

Part: FITTING — WORN (ZONE 800) · airframe 12,065 hrs · 11,550 cycles

WEAR ON FITTING FROM STA FS 1051.30 , STRINGER 12RH OF AFT BAGGAGE-BAY DOOR, WEAR ON FITTING FROM STA FS 1051.30 , STRINGER 12RH WAS REPAIRED REO 690-53-61-1757 REV - -.

ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

CORROSION ON SEAT TRACKS OF AFT BAGGAGE -BAY ,BETWEEN THE COORDINATES RBL9 TO RBL27,AND LBL7 TO LBL27 ,BTW STA FS 1000 TO STA 1069. CORROSION ON SEAT TRACKS OF AFT BAGGAGE -BAY ,BETWEEN THE COORDINATES RBL9 TO RBL27,AND LBL7 TO LBL27 ,BTW STA FS 1000 TO STA 1069 WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND SEAT TRACKS WERE REPLACED PER CRJ-900 AMM 53-00-49-400-802(CONFIG. A03).

ATA 5712

Part: RIB — CRACKED (ZONE 500) · airframe 12,065 hrs · 11,550 cycles

CRACK ON MACHINED RIB OF LEADING EDGE SS 58.41 AT LH WING. CRACK ON MACHINED RIB OF LEADING EDGE SS 58.41 AT LT WING WAS REPAIRED PER REO 690-57-41-240 REV - -.

ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

CORROSION ON SEVERAL POINTS SEAT RAIL BTW 364.00 TO FS409.00 AT LBL09 CAB PAX. CORROSION ON SEVERAL POINTS SEAT RAIL BTW 364.00 TO FS409.00 AT LBL09 CAB PAX WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-21-49-101-001-A01 AND REPLACED PER CRJ900 AMM 53-00-49-400-801(CONFIG A12)

ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

CORROSION ON SEVERAL POINTS SEAT RAIL BTW FS785.15 TO FS847.00+16.00 AND FS847+48.00 TO FS881.00 AT RBL15 CAB PAX. SEAT TRACK BTW FS785.15 TO FS847.00+16.00 AND FS847+48.00 TO FS881.00 AT RBL15 CAB PAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02 AND REPLACED PER AMM 53-00-49 (CONFIG A12).

ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

WEAR ON LH SIDE SEAT RAIL (1EA) ,BTW STA FS 379 TO STA FS 469.00,AND WEAR LH SIDE SEAT RAIL (1EA) BTW STA FS 469.00 TO STA FS 581,ALSO WEAR LH SIDE SEAT RAIL (1EA) BTW STA FS 581 TO STA FS 661+16. AND CORROSION ON WEAR LH SIDE SEAT RAIL (2EA) BTW STA FS 661+16 TO STA FS 669+40. WEAR ON LH SIDE SEAT RAIL (1EA) ,BTW STA FS 379 TO STA FS 469.00,AND WEAR LH SIDE SEAT RAIL (1EA) BTW STA FS 469.00 TO STA FS 581,ALSO WEAR LH SIDE SEAT RAIL (1EA) BTW STA FS 581 TO STA FS 661+16. AND CORROSION ON WEAR LH SIDE SEAT RAIL (2EA) BTW STA FS 661+16 TO STA FS 669+40 WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12).

ATA 5347

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

CORROSION ON SEVERAL POINTS SEAT RAIL BTW FS693 TO FS720.85 AND FS785.15 AT LBL15 CAB PAX. SEAT TRACK BTW FS693 TO FS720.85 AND FS785.15 AT LBL15 CAB PAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 AND REPLACED IAW AMM 53-00-49 (CONFIG A12).

ATA 5320

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

CORROSION ON RH SIDE SEAT RAIL (1EA) BTW STA FS 661+16 TO STA FS 669.40. CORROSION ON RH SIDE SEAT RAIL (1EA) BTW BS 661+16 TO BS 669.40 WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER AMM 53-00-49-400-801-A12.

ATA 5300

Part: SKIN — DENTED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

FUSELAGE SKIN DENT WITHIN 6341.13 FH AFTER SECTION I, REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. DENT DAMAGE ON FUSELAGE SKIN BTW FS942.00 - FS954.00 AND STR21L - STR22L WAS REPAIRED PER CRJ-900 REO 690-53-51-539 REV.--

ATA 5320

Part: WEB — CRACKED (ZONE 100) · airframe 12,065 hrs · 11,550 cycles

CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF ATTACHMENT AREA OF ADG RESTOW PUMP. CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF ATTACHMENT AREA OF ADG RESTOW PUMP WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01

ATA 5344

Part: HINGE — SCRATCHED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

SCRATCHES ON SEVERAL POINTS AT PIANO HINGE LUGS PASSENGER DOOR. PIANO HINGE LUGS PASSENGER DOOR WAS REPAIRED WITH INSPECTION REQUIREMENTS FOR TYPE REPAIR I: THRESHOLD 5,700 FLIGHT CYCLES AND REPEAT WITH 5,700 FLIGHT CYCLES PER REO 670-53-21-582 REV.-G.

ATA 5220

Part: DOOR — CRACKED (ZONE 800) · airframe 12,065 hrs · 11,550 cycles

CRACK ON TOP EDGE MEMBER AT LH AFT EMERGENCY EXIT DOOR. TOP EDGE MEMBER AT LH AFT EMERGENCY EXIT DOOR WAS REPAIRED PER REO 670-52-21-103 REV-.

ATA 5344

Part: HINGE — SCRATCHED (ZONE 200) · airframe 12,065 hrs · 11,550 cycles

WEAR ON LUG LAND AT PIANO HINGE PASSENGER DOOR. LUG LAND AT PIANO HINGE PASSENGER DOOR WAS REPAIRED WITH INSPECTION REQUIREMENTS FOR TYPE REPAIR IV: THRESHOLD 5,700 FLIGHT CYCLES AND REPEAT WITH 5,700 FLIGHT CYCLES PER REO 670-53-21-582 REV.-G.

ATA 5530

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 12,065 hrs · 11,550 cycles

CRACK ON AFT DRAG ANGLE OF LH VERTICAL STABILIZER. CRACK ON AFT DRAG ANGLE OF LH VERTICAL STABILIZER WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01

ATA 5310

Part: CROSSBEAM — DAMAGED (ZONE 200) · airframe 12,056 hrs · 11,547 cycles

REO 690-53-21- 2052 REPAIR TO CROSSBEAM FS 295 BETWEEN RBL 37 AND RBL 45 REQUIRES FINAL DISPOSITION / COMPLETED PERMANENT REPAIR IAW REPAIR ENGINEERING ORDER (REO) 690-53-21-2052. NO ADDITIONAL DEFECTS NOTED AT THIS TIME.

ATA 5311

Part: FRAME — BENT (ZONE 200) · airframe 12,056 hrs · 11,547 cycles

FRAME AT FS280 BENT BETWEEN STR19R AND 20R / COMPLETED PERMANENT REPAIR OF FRAME 280.00 SPLICE REPAIR AT STR22 IAW REPAIR ENGINEERING ORDER (REO) 690-53-11-2071. NO ADDITIONAL DEFECTS NOTED AT THIS TIME.

ATA 5300

Part: NOT REPORTED — NOT REPORTED · airframe 12,056 hrs · 11,547 cycles

FUSELAGE STRUCTURE BETWEEN FS333.0 - FS265.0 AND STR 17R- 26R. / PERFORMED REPAIR IAW REPAIR ENGINEERING ORDER (REO) 690-53-00-638.