N919XJ

Part: WINDOW — CRACKED (ZONE 200) · airframe 38,929 hrs · 27,330 cycles

OUTER PANE OF CABIN WINDOW AT SEAT 9C/D MOSTLY MISSING REPLACED WINDOW ASSEMBLY

Part: SENSOR — INOPERATIVE (BRAKE TEMP) · airframe 37,472 hrs · 26,287 cycles

ON CLIMBOUT @ LGA BRAKE OVERHEAT WARNING POSTED @ APPROX 600 AGL. COMPLIED WITH EMER NON NORMAL CHECK LISTS. DEFERRED IAW MEL 32-46-1D. MX PROCEDURES COMPLIED WITH. MOC NOTIFIED 102658. MMO2 UPDATED AND PLACARD INSTALLED. R&R RHIB THERMOCOUPLE SNSOR IAW CRJ900 AMM 32-46-01. OPS TEST OK. DDL UPDATED. PLACARD REMOVED, MOC NOTIFIED #103486. MAINTENANCE PROCEDURES RESTORED. THIS CLEARS CNTL #4006277-1.

Part: BATTERY PACK — INOPERATIVE (FWD EMERGENCY EX) · airframe 37,399 hrs · 26,232 cycles

DURING LINE CHECK FOUND EMERGENCY LIGHTS OUT FWD OVERWING AND INTERIOR FWD EMERGENCY EXIT R/R EMERGENCY BATTERY IN POSTION PS37 IAW AMM 33-51-17. R/R EMERGENCY OVERWING LIGHT IAW AMM 33-51-15. OPS CHECK GOOD. PN OFF/ON 2013-1ASMI SN OFF 19098 SN ON-19261. LIGHT ON OFF/ON- 8GH005123-06

Part: DRAG ANGLE — CRACKED · airframe 33,242 hrs · 22,956 cycles

VERTICAL STAB. RH FWD DRAG ANGLE HAS POSSIBLE CRACK (FLAGGED) PERFORMED CUT OUT OF RH FWD DRAG ANGLE, BUCKET SKIN, AND COMPLIED WITH ALL STEPS OF REO 690-55-31-071 REV. – DATED: 2022-09-26

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 33,242 hrs · 22,956 cycles

PAX DOOR AFT STAIR WEB DRAG ANGLE HAS CRACK. REMOVED AND REPLACED CRACKED AFT DRAG ANGLE WITH NEW REPLACEMENT DRAG ANGLE USING ALL NEW FASTENERS. REF CRJ900 SRM 51-42-06-001-001 A01

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,242 hrs · 22,956 cycles

FS280 CROSS BEAM CORRODED ON THE UPPER FLANGE UPPER SURFACE BETWEEN LBL 14 & RBL 9. REMOVED AND REPLACED NEW UPPER SPLICE STRAP P/N CC670-34097-1. REF: CRJ-900 SRM 51-42-06-001-001-A01 AND REFERENCED SB 670BA-53-041 REV D FEB 28/2014 PG 162 AND 163

Part: FORMER — CORRODED (PAX DOOR) · airframe 33,242 hrs · 22,956 cycles

PAX DOOR FWD FORMER IS CORRODED IN MULTIPLE AREAS REMOVED AND REPLACED PAX DOOR FWD FORMER WITH NEW P/N 601R318031-5 REF CRJ 900 SRM 51-42-06-001-001-A01, CRJ SRM 51-42-21-001-001-A01 AND DWG.NO. 601R31702 REV.N

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 33,242 hrs · 22,956 cycles

PAX DOOR SILL KICK ANGLE IS CORRODED AROUND FASTENER HOLES INSTALLED NEW SILL KICK ANGLE AND MID CAP ANGLE P/NS SH670-31825-9 & SH670-31875-3 REF. CRJ 900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 & DWG SH670-31810 REV AE

Part: STRINGER — CORRODED (BS 349 S20R) · airframe 33,242 hrs · 22,956 cycles

STRINGER 20R INTERCOSTAL AFT OF FS349 HAS CORROSION BELOW CANNON PLUG BRACKET REMOVED AND REPLACED INTERCOSTAL AT STGR 20R FS349-FS364 REV. CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND DWG SH670-31950 REV. Y

Part: STRINGER — CORRODED (BS 280-295 S25R) · airframe 33,242 hrs · 22,956 cycles

STRINGER 25R BETWEEN FS280 AND 295 HAS CORROSION REMOVED AND REPLACED STR 25R SECTION SH670-31212-2 BETWEEN FS 280- FS 333 REF CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.

Part: WEB — CRACKED (PAX DOOR) · airframe 33,242 hrs · 22,956 cycles

PAX DOOR AFT STAIR WEB HAS CRACK ON LOWER STEP CORNER REMOVED AND REPLACED CRACKED AFT PAX DOOR WEB WITH NEW WEB PER CRJ900 SRM'S 51-42-06-001-001 A01, 51-42-21-001-001 A01 AND 51-42-13-001-001 A01

Part: CLEAT — CORRODED (PAX DOOR) · airframe 33,242 hrs · 22,956 cycles

CORROSION ON PAX DOOR CLEAT COMMON TO INTERCOSTAL DD6 & FORMER, FS329.41 REMOVED AND REPLACED CORRODED PAX DOOR CLEAT WITH NEW PAX DOOR CLEAT (P/N 600-31902-269) AT FS329.41 DD6 WITH NEW FASTENERS. REF DWG 601R31702 REV-N AND CRJ 900 SRM 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,242 hrs · 22,956 cycles

CORROSION ON PAX DOOR INTERCOSTAL DD6 UPPER AND LOWER SIDE REMOVED AND REPLACED INTERCOSTAL AT DD6 FROM FS320-FS338 WITH NEW P/N 601R318057-1 REF DWG 601R31702 REV-N, CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01

Part: DRAG ANGLE — WORN (CARGO DOORWAY) · airframe 33,242 hrs · 22,956 cycles

CENTER BAG BAY DOOR DEFLECTOR WORN THROUGH AT SEVERAL SPOTS CUT AWAY DAMAGED AREA & PERFORMED DRAG ANGLE REPAIR REF CRJ 900 SRM 55-31-00-201-001-A01

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,242 hrs · 22,956 cycles

PAX DOOR INTERCOSTAL (FWD) DD4 IS CORRODED. INSTALLED NEW INTERCOSTAL P/N 601R318093-1 REF CRJ 900 SRM 51-42-06-001-001-A01 AND DWG. NO. 601R31702 REV. N

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 33,242 hrs · 22,956 cycles

VERTICAL STAB RH AFT DRAG ANGLE HAS POSSIBLE CRACK CUT AWAY DAMAGED AREA & PERFORMED DRAG ANGLE REPAIR REF CRJ 900 SRM 55-31-00-201-001-A01

Part: FLOOR SUPPORT — CORRODED (BS 985-1047) · airframe 33,242 hrs · 22,956 cycles

LH FLOOR SILL FROM FS 985 TO FS 1047 HAS MULTIPLE SPOTS OF CORROSION REMOVED AND REPLACED LH LOWER SILL MM670-35655-003 FS 1000 - 1047 WITH NEW P/N MM670-35655-003 REF CRJ 900 SRM 51-42-06-001-001-A01 , SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01. COMPLIED WITH ALL STEPS OF EA CRJ953-14614 REV IR DATED 09/28/2022 FOR REWORKED AREAS ON LH FLOOR INTERCOSTAL FS985 - 1000

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 33,242 hrs · 22,956 cycles

RIGHT FLOOR SILL FS280.00 - FS319.00 IS CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED RH FLOOR SILL BETWEEN FS280.00 AND FS319.00 WITH NEW P/N SH670-32172-9 REF CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01

Part: FLOORBEAM — CORRODED (BS 280 RBL 9-24) · airframe 33,242 hrs · 22,956 cycles

CORROSION FOUND ON CAP AT FS 280.00 RH CROSS BEAM AT RBL 9 TO RBL 24. REMOVED AND REPLACED FS 280.00 RH CROSS BEAM AT BL0-RBL42.00 WITH NEW P/N CC670-34094-2 REF CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-22-001-001-A01, CRJ900 SRM 51-42-13-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01

Part: ANGLE — CORRODED (BS 280 RBL 9-39) · airframe 33,242 hrs · 22,956 cycles

RH FS280.00 BULKHEAD WEB CAP ANGLE CORRODED. REMOVED AND INSTALLED NEW CAP ANGLE COMMON TO RH FLOOR BEAM AT FS280 AND RH LOWER WEB RBL9.0-RBL39 REF CRJ900 SRM 51-42-006-001-A01, 51-42-13-001-001-A01 AND SRM 51-42-15-001-001-A01

Part: ANGLE — CORRODED (BS 280) · airframe 33,242 hrs · 22,956 cycles

CAP ANGLE (PN CC670-34096-1) COMMON TO FS280.00 FLOOR BEAM AND FS280.00 BULKHEAD LOWER WEB FROM LBL39 TO LBL9 HAS CORROSION IN MULTIPLE AREAS ON FAYING SURFACES REMOVED AND REPLACED CAP ANGLE COMMON TO LH FLOOR BEAM AT FS280 AND LH LOWER WEB LBL9.0-LBL39 WITH NEW P/N CC670-34096-1 REF CRJ900 SRM 53-11-10-201-004-A01

Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 33,242 hrs · 22,956 cycles

LH FS280.00 BULKHEAD LOWER WEB (PN CC670-34170-7) AFT SIDE FROM LBL39 TO LBL9 HAS CORROSION IN MULTIPLE AREAS REMOVED AND REPLACED LH BULKHEAD LOWER WEB COMMON TO LH FS280.00 FLOOR BEAM AND BUTTSTRAP AT LBL 12.00-LBL45.00 WITH NEW PARTS REF CRJ900 SRM 53-11-10-201-004-A01, SRM 53-11-10-201-003-A01, SRM 51-42-06-001-001-A01, 51-42-13-001-001-01,AND SRM 51-42-21-001-001-A01

Part: NONE — CORRODED · airframe 33,242 hrs · 22,956 cycles

CORROSION FOUND LH SIDE SEAT RAIL BETWEEN FS 379-483 INSTALLED NEW SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801-A07.

Part: NONE — CORRODED · airframe 33,242 hrs · 22,956 cycles

CORROSION FOUND ON LH SIDE SEAT RAIL CHANNEL BETWEEN FS 903.00-961.00 INSTALLED NEW SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801-A07.

Part: SEAT TRACK — CORRODED · airframe 33,242 hrs · 22,956 cycles

LBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 847+48 TO F.S. 985. INSTALLED FABRICATED SEAT TRACK AT LBL 9 F.S 847+48 TO F.S. 985.IAW CRJ 900 AMM 53-00-49-400-801-A07

Part: ANGLE — CRACKED · airframe 33,242 hrs · 22,956 cycles

VERTICAL STAB. LH AFT DRAG ANGLE HAS POSSIBLE CRACK REPLACD ANGLE PER CRJ 900 SRM 55-31-00-201-001-A01

Part: NONE — CORRODED · airframe 33,242 hrs · 22,956 cycles

CORROSION FOUND ON RH SIDE SEAT RAIL BETWEEN FS 847.00+14-867.00. INSTALLED NEW SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801-A07.

Part: NONE — CHAFED · airframe 33,242 hrs · 22,956 cycles

RH I/BD FLAP PANEL 684ET IS CHAFED REPLACED PANEL PER CRJ900 SRM 51-40-11-001-001-A01

Part: FLAP — CHAFED · airframe 33,242 hrs · 22,956 cycles

LEFT WING INBOARD FLAP LEADING EDGE PANEL 584ET IS CHAFED. REPLACED PANEL PER CRJ900 SRM 51-40-11-001-001-A01

Part: CLEAT — CORRODED · airframe 33,242 hrs · 22,956 cycles

PAX DOOR CLEAT COMMON TO INTERCOSTAL DD6 AND FORMER, FS320 IS CORRODED. REPLACED CLEAT AND FORMER PER CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-15-001-001-A01

Part: PANEL — CHAFED · airframe 33,242 hrs · 22,956 cycles

TRANSCOWL PANEL 443BT IS CHAFED REPLACED PANEL PER CRJ900 SRM 51-12-00-001-001-A01

Part: ACTUATOR — TRIPPED (SLATS) · airframe 28,096 hrs · 18,604 cycles

SLATS FAIL" CAUTION MESSAGE ON APPROACH TO MKE. RAN QRH. MESSAGE REMAINED. SLATS STUCK AT 0, FLAPS FUNCTIONED NORMALLY. NOTED SLAT ACTUATORS NR 3, 4, AND 6 ON LH SIDE AND 5 ON RH SIDE TRIPPED. SUSPECTED WATER IN LH NR 3 SLAT ACTUATOR. REMOVED AND REPLACED LH NR 3 SLAT ACTUATOR IAW AMM 27-81-09. RESET TRIPPED ACTUATORS LH NR 4 AND 6 AND RH 5 IAW AMM 27-81-09 OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,803 hrs · 18,380 cycles

EMERGENCY TRACK LIGHTING DAMAGED AT ROW 9. REMOVED AND REPLACD DAMAGE FLOOR TRACK LIGHTING IAW AMM 33-51-01. FLOOR TRACK LIGHTING OK FOR SVC IF NECESSARY. P/N OFF/ON - PL1100LH07 P/N OFF/ON - PLI315LH00

Part: STRINGER — CORRODED (FUSELAGE) · airframe 26,336 hrs · 17,245 cycles

INITIAL INSPECTION. CORROSION ON STRINGER 27 FROM FS= 280 TO FS= 295, ALSO ON STRINGER 27 FROM FS= 333 TO FS= 353 AT MAIN AVIONICS COMPARTMENT. (E/E) (TCI: 100-09)COMPLETE: SUMMARY OF NRC 00101: CORROSION LEVEL 2 ON STRINGER 27 FROM FS= 280 TO FS= 295, ALSO ON STRINGER 27 FROM FS= 333 TO FS= 353 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED AND FINDING IT OUT OF LIMITS PER SRM 53-21-03-101-002-A04, STRINGER WAS REPLACED PER SR M 51-42-06-001-001-A01. STRINGER 27 FROM FS= 333 TO FS= 353 WAS INSPECTED PER 51-11-00-001-001-A01 AND NOT DAMAGE WAS FOUND.

Part: STRINGER — CORRODED (BS 280-330) · airframe 26,336 hrs · 17,245 cycles

CORROSION ON STRINGER 26L AND 26R FROM FS= 280 TO FS= 330 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2 ON STRINGER 26L AND 26R FROM FS= 280 TO FS= 330 WAS EVALUATED AND FINDING IT OUT OF LIMITS PER SRM 53-21-03-101-002-A04 AT MAIN AVIONICS COMPARTMENT. STRINGER WAS REPLACED PER SRM 51-42-06-001-001-A01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,336 hrs · 17,245 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 572 TO FS= 661+16, STR 15L/R ] [ FS= 661+16 TO FS= 661+90, STR 15L/R ] [ FS=661+90 TO FS=720, STR 15R ] AT PAX CABIN. (CPAX) (TCI: 53-20-217). COMPLETE: SUMMARY OF NRC 00116 : NEW SIDE SEAT RAILS IN SECTIONS [ FS= 572 TO FS= 661+16, STR 15L/R ] [ FS= 661+16 TO FS= 661+90, STR 15 L/R ] [ FS=661+90 TO FS=720, STR 15R ] AT PAX CABIN WERE REPLACED PER SRM 51-41-02-001-001-A01 PAR. 6D AND AMM 53-00-49-400-801 (CONFIG. A07).

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,336 hrs · 17,245 cycles

CORROSION ON FLOORBEAM LBL27 STA FS=1032 AT AFT CARGO COMPARTMENT. FLOORBEAM LBL27 STA FS=1032 AT AFT CARGO COMPARTMENT WAS REPAIRED PER REO 670-53-00-029 REV "A".

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,336 hrs · 17,245 cycles

CORROSION ON FLOORBEAM LBL9 STA FS 1033 AT AFT CARGO COMPARTMENT. FLOORBEAM LBL9 STA FS=1033 AT AFT CARGO COMPARTMENT WAS REPAIRED PER REO 670-53-00-029 REV "A" .

Part: STRIKER — CORRODED (FUSELAGE) · airframe 26,336 hrs · 17,245 cycles

CORROSION ON LOWER EDGE AT SERVICE DOOR SURROUND STRUCTURE. DUE TO EXCESSIVE DAMAGE WERE REPLACE ANGLE AND STRIKE SEAL PER SRM 51-42-06-001-001-A01 PAR 6C, SRM 51-42-20-001-001-A01 PAR 6C AND SRM 53-21-23-101-002-A02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,336 hrs · 17,245 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 749 TO FS= 761, STR 15L/R ] [ FS= 785 TO FS= 847+16, STR 15L/R ] AT PAX CABIN. (CPAX) (TCI: 53-20-233) COMPLETE: SUMMARY OF NRC 00117 : NEW SIDE SEAT RAILS IN SECTIONS [ FS= 749 TO FS= 761, STR 15L/R ] [ FS= 785 TO FS= 847+16, STR 15L/R ] AT PAX CABIN WERE REPLACED PER SRM 51-41-02-001-001-A01 PAR. 6D AND AMM 53-00-49-400-801 ( CONFIG.A07 ).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,336 hrs · 17,245 cycles

INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 847+16 TO FS= 905, STR 15L ] [ FS= 847+16 TO FS= 867, STR 15R ] AT PAX CABIN. (CPAX) (TCI: 53-20-233) COMPLETE: SUMMARY : NEW SIDE SEAT RAILS IN SECTIONS [ FS= 847+16 TO FS= 905, STR 15L ] [ FS= 847+16 TO FS= 867, STR 15R ] AT PAX CABIN WERE REPLACED PER SRM 51-41-02-001-001-A01 PAR. 6D AND AMM 53-0 0-49-400-801 ( CONFIG.A07 )

Part: OXYGEN MASK — BROKEN (CAPTAIN'S) · airframe 25,193 hrs · 16,442 cycles

CAPTAIN`S OXYGEN MASK RED LEVER BROKEN. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12.

Part: OXYGEN MASK — BROKEN (FIRST OFFICER'S) · airframe 24,759 hrs · 16,124 cycles

FIRST OFFICER`S OXYGEN MASK HAS A BROKEN OR DISCONNECTED HOSE ON THE HEAD HARNESS. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS AND LEAK TESTED GOOD. NO FURTHER DEFECTS NOTED

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 24,253 hrs · 15,763 cycles

F/A REPORTS STRAP ON FLASHLIGHT BROKEN. REMOVED AND REPLACED THE FLASHLIGHT TAMPER SEAL. VERIFIED FLASHLIGHT SERVICEABLE IAW AMM 25-61-02.

Part: FLASHLIGHT — INOPERATIVE (MAIN CABIN) · airframe 24,030 hrs · 15,607 cycles

FLASHLIGHT BY SPARE FA JUMPSEAT INOP REMOVED AND REPLACED FLASHLIGHT IAW CRJ 900 AMM 25-61-02. OPS CHECK GO OD AT THIS TIME.

Part: KNOB — BROKEN (MEGAPHONE) · airframe 24,016 hrs · 15,595 cycles

VOLUME KNOB IS MISSING ON MEGAPHONE REMOVED AND REPLACED MEGAPHONE IAW CRJ900 AMM 25-61-14. OPS CHECK GOOD NO DEFECTS NOTED

Part: OXYGEN MASK — BROKEN (FLIGHT DECK) · airframe 23,691 hrs · 15,630 cycles

DURING PREFLIGHT FIRST OFFICER`S OXYGEN MASK RED LEVER BROKE DURING TESTING. REMOVED AND REPLACED FO OXYGEN MASK IAW AMM 35-11-12, OP CHECKED.

Part: STOWAGE BOX — NO TEST (OXYGEN MASK) · airframe 22,964 hrs · 14,827 cycles

CAPTAIN`S OXYGEN MASK PRESS TO TEST AND RESET BUTTON IS INOPERATIVE. REMOVED AND REPLACED THE OXYGEN MASK STORAGE BOX IAW AMM 35-11-15, PERFORMED OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,007 hrs · 14,172 cycles

EMERGENCY LIGHTS NOT TURNING ON. R&R EPSU BATTERY PACKS IAW AMM 33-51-17. OPS CHECK GOOD IAW AMM 33-51-00. OK FOR SERVICE.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 21,940 hrs · 14,132 cycles

CAPTAIN SIDE O2 MASK BROKEN. HARNESS FEELS LIKE IT SNAPPED. SWAPPED CAPT O2 MASK WITH OBSV MASK. DEFERRED OBSV SEAT IAW MEL 35-10-1. REMOVED AND REPLACED OBSERVER O2 MASK IAW 35-11-12 PERFORMED LEAK TEST. OPS TEST PF THE CREW O2 AND OPS TEST OF THE OBSERVER O2 MICROPHONE IAW 35-10-00 AND 23-51-00.

Part: LIGHT — UNSECURE (CABIN) · airframe 19,591 hrs · 12,549 cycles

RUBBER FLOOR STRIP IN FRONT OF GALLEY CART, ACROSS FROM LAVATORY. SECURED FLOOR LIGHT STRIP IAW MM 3-51-01-400-801-A21.

Part: LIFE VEST — DAMAGED (COCKPIT) · airframe 19,053 hrs · 12,198 cycles

FIRST OFFICERS LIFE VEST IS DAMAGED. R & R FIRST OFFICERS LIFE VEST IAW AMM 25-61-03.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 19,053 hrs · 12,198 cycles

MEGA PHONE ALARM INOPERATIVE. R & R MEGA PHONE IAW AMM 25-61-14. OPERATIONS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 18,828 hrs · 12,034 cycles

EMERGENCY LIGHT OPERATIONS TEST FAILS. R & R EPSU NR 3 BATTERY CHARGER IAW MM 33-51-17-000-802 & 400-802-A02. NR 3 EPSU OPERATIONS TEST CHECKED OK IAW MM 33-51-17-710-801-A02.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,828 hrs · 12,034 cycles

COPILOT'S FLASHLIGHT BATTERY INOPERATIVE. REMOVED & INSTALLED SERVICEABLE COPILOT'S EMER FLASHLIGHT BATTERY BY UNSCREWING CAP ON FLASHLIGHT & SCREWING CAP BACK ON.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 18,828 hrs · 12,034 cycles

GALLEY AREA AISLE FLOOR PATH EMER LIGHTS REQUIRE TO BE REMOVED & INSTALLED CORRECTLY IAW AMM TASK 33-51-01-400-801. BOTH GALLEY AREA FLOOR PATH LIGHTS FOUND TO BE TAPED ON TOP OF THE FLOOR MAT. REMOVED & INSTALLED GALLEY AREA AISLE FLOOR PATH EMER LIGHTS IAW AMM 38-51-01-400-801.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,828 hrs · 12,034 cycles

CORROSION WAS FOUND ON STRINGER 27 AT FS 258.00. THE CORROSION MEASURES 3.00” X 0.600” X 0.026” MAX DEPTH. REPAIRED IAW EA CRJ953-03722.

Part: HOUSING — CHAFED (SERVICE DOOR) · airframe 18,828 hrs · 12,034 cycles

SERVICE DOOR EXTERNAL HANDLE HOUSING IS CHAFED. LOCATED & DRILLED NEW HOUSING IAW SRM 51-42-06-001-001-A01 & INSTALLED IAW SRM 51-42-06-001-001-A01. OPERATIONS TESTED GOOD IAW AMM 52-41-00-710-801. REFERENCE LINE ITEMS 1 - 6 FOR DETAILS OF WORK PERFORMED. REFERENCE OP 254.

Part: CROSSBEAM — CHAFED (CAARGO DOOR) · airframe 18,828 hrs · 12,034 cycles

AREA OF CHAFING ON THE AFT CARGO DOOR CROSSBEAM. THE CHAFED AREAS MEASURE .500” X .075” X .050” DEEP. REPAIRED IAW EA CRJ953-03705.

Part: SPACER — CORRODED (RADIO ALTIMETER) · airframe 18,828 hrs · 12,034 cycles

TRANSMIT ANTENNA 1 E8 & 2 E19 SPACER PLATES HAVE CORROSION, ALTERNATIVE RADIO ALTIMETER ANTENNA. R & R SPACERS FOR TRANSMIT ANTENNAS 1 E8 & 2 E19 IAW SRM 51-06-001-001-A01. REF LINE ITEM 1 OF JOB 81516311 OP 150.

Part: SUPPORT CHANNEL — CHAFED (CARGO DOOR) · airframe 18,828 hrs · 12,034 cycles

AFT CARGO DOOR AFT SUPPORT CHANNEL CHAFED FROM BALANCE SPRING CABLE, APPROX .063 X .063 DEEP. REPAIRED AFT CARGO BAY DOOR AFT SUPPORT CHANNEL IAW EA CRJ953-03705. REF LINE ITEMS 1 - 5 FOR DETAILS.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

CORROSION ON FWD RT JACKING FITTING SUPPORT. REPAIRED CORROSION BY R & R FITTING & SUPPORT STRUCTURE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & 51-40-11-001-001-A01. REF LINE ITEMS 1 - 6 ON MWC JOB 81516311 OP 57 FOR DETAILS.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

CORROSION ON LT OVERWING SILL ANGLE AT FS 708.00 & FS 797.00 AROUND FASTENER HOLE. REPAIRED CORROSION ON LT OVERWING SILL ANGLE IAW SRM 53-41-51-101-001-A02 & EA REPAIR NR CRJ953-03720. REFERENCE CONTINUATION ON OP 178.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FS 280 CROSSBEAM IS CORRODED. INSTALLED NEW SERVICEABLE LT & RT FS 280 CROSSBEAMS IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01 & 51-42-22-001-001-A01. REFERENCE OPS 91, 104, 149.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT AT FS 349, BETWEEN STRINGERS 26L - 25R, THE FRAME ATTACHMENT ANGLES ARE CORRODED. LOCATED & DRILLED NEW SERVICEABLE FRAME IAW SRM 51-40-11-001-004-A01. INSTALLED NEW SERVICEABLE FRAME SECTION PN SH670-31357-5 AT FS 349 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. REF CO 15163115 JOB 81516311 OP 72 FOR DETAIL OF WORK PERFORMED.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 319.70 - 333.00, STRINGER 25L, SPLICE IS CORRODED. R & R STRINGER SPLICE PN SH670-31197-1 IAW SRM 51-40-11-001-001-A01 & 51-42-06-001-0014-A01. REFERENCE CO 15163115 JOB 81516311 OP 70 FOR DETAIL OF WORK PERFORMED.

Part: SUPPORT CHANNEL — LOOSE (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

RIGHT MLG FAIRING SUPPORT CHANNEL ASSEMBLY AT FS 797 IS LOOSE AT FAIRING BRACKET, JUST BELOW INBD PINTLE PIN, SIDE STAY ASSEMBLY CONNECTION POINT. R & R RT MLG FAIRING SUPPORT CHANNEL IAW SRM 51-42-21-001-001-A01 & AMM 20-21-00-910-801.

Part: SUPPORT CHANNEL — LOOSE (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

LEFT MLG FAIRING SUPPORT CHANNEL ASSEMBLY AT FS 797 IS LOOSE AT FAIRING BRACKET, JUST BELOW INBD PINTLE PIN SIDE STAY ASSEMBLY CONNECTION POINT. R & R LT MLG FAIRING SUPPORT CHANNEL IAW SRM 51-42-21-001-001-A01 & AMM 20-21-00-910-801.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 333 - 349, STRINGER 26R, SPLICE & STRINGER ARE CORRODED. R & R STRINGER 26R, PN SH670-31372-4, FROM FS 333 - 349 IAW SEM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01. REFERENCE CO 15163115 JOB 81516311 OP 72 FOR DETAILS OF WORK PERFORMED.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 349 - 364 AT STRINGER 27 LOCATION, RT SIDE, THE INTERCOSTAL ATTACHMENT ANGLE IS CORRODED. R & R INTERCOSTAL, PN SH670-32075-4, FS 349 - 364, STRINGER 27 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01. REFERENCE CO 15163115 JOB 81516311 OP 72 FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

CORROSION ON SEAT RAILS AT LBL 9, FS 364.00 & RBL 9, FS 349.00 - FS 379.00. R & R SEAT RAILS IAW AMM 53-00-49-400-801 A07. REF LINE ITEMS 1 & .

Part: STRINGER — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

PITTING CORROSION FOUND ON FLANGE OF STRINGER 26L, BETWEEN FS 333.00 - 349.00. R & R STRINGER 26L, PN SH670-31372-3 IAW SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01. REFERENCE CO 15163115 JOB 81516311 OP 126 FOR DETAILS OF WORK PERFORMED.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 333 - 349, THE STRINGER SPLICE IS CORRODED. R & R STRINGER SPLICE & STRINGER IAW SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

PASSENGER COMPARTMENT UNDER FLOORBOARDS, BETWEEN FS 310.00 - 319.70 AT STRINGER 20R LOCATION, THE INTERCOSTAL IS CORRODED. R & R INTERCOSTAL, PN SH670-32047-1, AT STRINGER 20R, FS 310 - 319.70 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01. REFERENCE CO 15163115 JOB 81516311 OP 71 FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 349 - 364 AT STRINGER 26R, THE INTERCOSTAL IS CORRODED. R & R INTERCOSTAL, PN SH670-32077-4, IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 349 - 364 AT STRINGER 27 LT SIDE, THE INTERCOSTAL IS CORRODED. R & R INTERCOSTAL, PN SH670-32077-3, IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 319.70 - 333.00, STRINGER 26L SPLICE & FASTENERS ARE CORRODED. R & R STRINGER SPLICE P N SH670-31197-1 IAW SRM 51-42-06-001-001-A01, REFERENCE CO 15163115 JOB 81516311 OP 70 FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

PASSENGER COMPARTMENT UNDER FLOORBOARD, BETWEEN FS 310 - 333.00 AT STRINGER 20L LOCATION, THERE ARE 2 EACH INTERCOSTALS CORRODED. R & R INTERCOSTAL, PN 670-31823-1, BETWEEN FS 310 - 333 IAW SRM 51-42-06-001-001-A01, 51-40-14-001-001-A01 & 51-42-21-001-001-A01. REFER TO CO 15163115 JOB 81516311 OP 70 FOR DETAILS OF WORK PERFORMED.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

PASSENGER COMPARTMENT UNDER FLOORBOARDS, BETWEEN FS 319.70 - 333.00 AT STRINGER 20R, THE INTERCOSTAL ATTACHMENT ANGLE IS CORRODED. R & R INTERCOSTAL ATTACH ANGLE, PN SH670-32045-1, BETWEEN FS 319.70 - 333 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01. REFERENCE CO 15163115 JOB 81516311 OP 71 FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

CABIN FLOOR SEAT TRACKS, LT & RT, HAVE CORROSION FS 477.40 - 693.00. R & R LT & RT CABIN FLOOR SEAT TRACKS IAW AMM 53-001-49-000 4001-801 & REO 670-53-00-343 REV L DATED 2015 05 05.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT AT FS 319.70, BETWEEN STRINGERS 26L - 26L, THE FRAME ATTACHMENT ANGLES ARE CORRODED. REPAIRED LOWER FRAME SECTOR AT FS 319.70 IAW GREO 670-53-21-799, DATED 2012 01 30 REV, REFERENCE CO 15163115 JOB 81516311 OP 69 FOR DETAILS OF WORK PERFORMED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 319.70 - 333.00, STRINGER 25R & FASTENERS ARE CORRODED. R & R STRINGER SEGMENT, PN SH670-31212-2, STRINGER 25R, FROM FS 280 - 333 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. REFERENCE CO 15163115 JOB 81516311 OP 70 FOR DETAILS OF WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 349 - 364 AT STRINGER 26L, THE INTERCOSTAL IS CORRODED. R & R INTERCOSTAL, PN SH670-32075-4 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT FLOORBOARD ATTACHMENT ANGLE AT FS 280 AFT, IS CORRODED BETWEEN STRINGER 25L - 25R. R & R FLOORBOARD SUPPORT ANGLE, PN CC670-34256-3 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01, REFERENCE MWC CO 15163115 JOB 81516311 OP 69 FOR DETAILED OF WORK PERFORMED.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

STRINGER SPLICE AT STRINGER 25R, BETWEEN FS 319.70 - 333.00 HAS PITTING CORROSION. R & R STRINGER SPLICE, PN SH670-31197-1, IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FOUND CORROSION ON INTERCOSTAL ATTACH ANGLE FWD AT FS 310.00, STRINGER 20R. FABRICATED INTERCOSTAL ATTACHMENT ANGLE, PN SH670-32046-3 IAW SAMPLE REFERENCING DWG FOR MATERIAL TYPE & THICKNESS LOCATED & DRILLED IAW SRM 51-40-11-001-001-A01 & INSTALLED IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

CORROSION ON LT OVERWING SILL ANGLE AT FS 708.00 & FS 797.00 AROUND FASTENER HOLE. REPAIRED CORROSION IAW SRM 53-41-51-101-001-A02 & EA REPAIR NR CRJ953-03720.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 319.70 - 333.00, STRINGER 26R & STRINGER SPLICE ARE CORRODED. R & R STRINGER 26R, PN SH670-31634-2 & STRINGER SPLICE, PN SH670-31197-1, IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01. REFERENCE CO 15163115 JOB 81516311 OP 70 FOR DETAILS OF WORK PERFORMED.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

FORWARD AVIONICS COMPARTMENT, BETWEEN FS 295 - 310.00 AT STRINGER 27 LOCATION, THE ANTENNA DOUBLER IS CORRODED. R & R ANTENNA DOUBLER, PN SH670-32364-7 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01, REFERENCE CO 15163115 JOB 81516311 OP 69 FOR DETAILS OF WORK PERFORMED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,828 hrs · 12,034 cycles

PASSENGER DOOR, AFT DRAG ANGLE CRACKED, PREVIOUS REPAIR. REPAIRED CRACKED PAX DOOR IAW SRM 52-11-04-201-002-A01.

Part: FAIRING — CRACKED (LT ENGINE) · airframe 18,828 hrs · 12,034 cycles

LEFT ENG LOWER AFT HINGE LINE FAIRING 433BB HAS APPROX 1" CRACK THROUGH FASTENER HOLE. REINSTALLED CLIP & C CHANNELS TO CN 24-4230-206 IAW SRM 51-42-06-001-001-A01 & SRM 51-42-10-001-001-A01. EXTERIOR PAINT ON FAIRING 433BB IAW REO 670-78-33-998.

Part: PANEL — CHAFED (WING) · airframe 18,828 hrs · 12,034 cycles

PANEL 599AB HAS A DEEP GOUGE ON THE INBD EDGE OF THE PANEL. RECEIVED NEW PANEL 599AB, REFER TO MASTER PANEL BOOK M-212 PG 74 FOR REMOVAL & INSTALLATION. LOCATED, DRILLED & COUNTERSUNK NEW PANEL 599AB, PN 601R13440-1 IAW SRM 51-40-11-001-001-A01.

Part: PANEL — CHAFED (TE FLAP) · airframe 18,828 hrs · 12,034 cycles

PANEL 584EB IS CHAFED AT CUT OUT FOR FLAP VANE ACT ROD. RECEIVED NEW PANEL 584JB, PN CC670-14178-1. REFERENCE MASTER PANEL M212 PG 75 FOR REMOVAL & INSTALLATION. LOCATED, DRILLED & COUNTERSUNK NEW PANEL 584EB, PN CC670-14177-1, IAW SRM 51-40-11-001-001-01.

Part: PANEL — CHAFED (TE FLAP) · airframe 18,828 hrs · 12,034 cycles

PANEL 584JB IS CHAFED AT CUT OUT FOR FLAP VANE ACT ROD. RECEIVED NEW PANEL 584JB, PN CC670-14178-1, REFERENCE MASTER PANEL BOOK M212 PAGE 76 FOR REMOVAL & INSTALL OF PANEL 584JB. LOCATED, DRILLED & COUNTERSUNK NEW PANEL 584JB, PN CC670-14178-1, IAW SRM 51-40-11-001-001-A01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 18,828 hrs · 12,034 cycles

CORROSION ON SERVICE DOOR SURROUND STRUCTURE, LOWER AFT SILL FROM FS 349.00 - 364.00. REO:670-53-00-390, REV DATED 01/22/14 COMPLIED WITH IN ITS ENTIRETY.

Part: MECHANISM — BINDING (EMERGENCY EXIT) · airframe 18,828 hrs · 12,034 cycles

RIGHT FWD, AFT OVERWING EMER EXITS FAIL THE DOOR HANDLE FUNCTIONAL TEST. DOORS OPEN AT 55 LBS, SHOULD BE UNDER 40 LBS. REMOVED FWD EMER EXIT DOOR LINER FOR ACCESS IAW AMM 25-26-09-000-801 A02. LUBRICATED FWD OVERWING EXIT IAW AMM 12-20-52-640-816 A01, DOOR STILL FAILS FUNCTIONAL CHECK. FURTHER TROUBLESHOOTING REQUIRED. UPON FURTHER INVESTIGATION FOUND LINK RODS ON LATCH MECHANISM TO BE BINDING & NOT TORQUED IAW AMM 52-21-02-400-801 A02. RE-TORQUED LINK RODS IAW AMM 52-21-02-400-801 A02. OPERATIONS CHECKED GOOD. REMOVED PANEL 845AZ IAW CRJ 900 AMM 25-26-09-000-801 FOR ACCESS. FOUND LINK RODS TO BE BINDING & REMOVED PINS FROM ROD ENDS IAW AMM 52-21-00-000-801 A02. REINSTALLED PINS & LUBRICATED EMER EXIT DOOR IAW AMM 52-21-00-400-801 A02 & 12-20-52-640-816 A01. OPERATIONS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (ESCAPE HATCH) · airframe 18,828 hrs · 12,034 cycles

CREW HATCH EXTERNAL HANDLE WILL NOT POP OUT WHEN ENGAGING PUSH BUTTON. LUBRICATED CREW ESCAPE HATCH & SUCCESSFULLY DISENGAGED & RE-ENGAGED EXTERNAL HANDLE TEN TIMES IAW AMM 12-20-525-640-804 A01.

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 17,880 hrs · 11,336 cycles

DURING CLIMB OUT AT 296KTS AT F190 LOUD BANG RT ENG FLAME OUT, VIB N2, FOLLOWED BY ENG OIL P-199, FOLLOWED CHECK LIST. R & R RT ENG IAW 900-72-430-902 & 900-72-430-906. REFER TO 527345 NON-ROUTINE WORK CARD. EMER WAS DECLARED, ACFT LANDED SAFELY WITHOUT INCIDENT. ON THE CLIMB THROUGH 19,000’ AT 290 KTS, EXPERIENCED A LOUD BANG WITH SIGNIFICANT VIBRATION THROUGH THE ACFT. THE RT ENG N1 BEGAN TO DETERIORATE WITH ASSOCIATED YAW & THE N2 SHOWED A VIB MSG. SHORTLY AFTER, THE RT ENG FLAME OUT & OIL PRESS MSGS APPEARED. THE ACFT WAS LEVELED OFF & AN EMER DECLARED. CHECKLISTS COMPLETED & ENG ENGINE SECURED. YELLOW LEVEL EMER DECLARED & PA MADE TO THE CUSTOMERS. COMPLETED APPROACH WITH NORMAL LANDING. CABIN REPORTED TO THE CREW THAT MOST OF THE CUSTOMERS REMAINED CALM WITH ONLY A FEW QUESTIONS OF CONCERN. APPLAUSE AFTER LANDING & CREW COMMENDED DURING THE DEPLANING.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,734 hrs · 11,276 cycles

DURING FLIGHT ATTENDANT PREFLIGHT INSPECTION, THE OVERHEAD, EMER EXIT SIGN & 2 SEAT LEVEL SIGNS AT ROW 13 DO NOT ILLUMINATE. R & R EPSU BATTERY PACK & CHARGER IAW 33-51-17. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,726 hrs · 11,273 cycles

NOTED EMER LIGHT AT SEAT 10 & 11 ARE INOPERATIVE. REPLACED BATTERY PACK AT PS37 PN ON & OFF AD-2013-1A IAW AMM CH 33-51-17. XN OFF 145968, SN ON 79988 IAW JC 33-900-701. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 17,625 hrs · 11,207 cycles

PILOT SIDE FLASHLIGHT INOPERATIVE. R & R PILOT FLASHLIGHT IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 17,473 hrs · 11,101 cycles

LUMINESCENT STRIPING FOR EXIT LIGHTING ON FLOOR IN GALLEY UNSECURED. RESECURED FLOOR STRIP AS REQUIRED OK FOR SERVICE.

Part: DOOR FRAME — OBSTRUCTED (PAX DOOR) · airframe 17,069 hrs · 10,827 cycles

MAIN BOARDING DOOR WOULD NOT OPEN. TRIED BOTH INSIDE AND OUTSIDE HANDLES. COULD NOT GET THEM TO BUDGE. MAINTENANCE APPLIED FORCE ON BOTH INSIDE AND OUTSIDE SIMULTANEOUSLY, WHICH RESULTED IN A LOUD, SHARP, BANG, AND THE DOOR OPENING. CLEARED DEBRIS FROM DOOR FRAME AND PERFORMED OPS CHECK OF PASSENGER DOOR IAW AMM 52-11-00. OPS CHECKED GOOD, ACFT OK TO RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 16,311 hrs · 10,341 cycles

UPPER FWD FACING OVERWING EMER EXIT SIGN DOES NOT LIGHT. REPLACED PS43 IAW 33-51-17. OPERATIONS CHECKED GOOD.

Part: PANEL — CHAFED (TE FLAP VANE) · airframe 14,965 hrs · 9,415 cycles

RIGHT WING INBD FLAP NR 3 VANE PANEL 684ET CHAFFED. LOCATED & DRILLED PANEL RECEIVED IAW CRJ900 SRM 51-42-06-001-001-A01.

Part: STRAP — CRACKED (FUSELAGE) · airframe 14,965 hrs · 9,415 cycles

JOINT STRAP AT PANEL 195DL & 196DR AFT LOWER FUSELAGE CTR SEAM CRACKED AFT END R & R JOINT STRAP ON PANEL 196DR & 195DL IAW NR 5670538200021. NO FURTHER DAMAGE FOUND.

Part: FIRESHIELD — CHAFED (RT COWLING) · airframe 14,965 hrs · 9,415 cycles

RIGHT LOWER COWL ENG DRAINS FIRE SHIELD IS CHAFED AT THE FWD OTBD CORNER. REPAIR IAW EO R540490 USING ONE CORNER FROM A NEW FIRE SHIELD PN CN624-3170-203. RT LOWER TR IS PN CN 624-0104-003 & SN SB087. REPAIRED CHAFE ON RT LOWER COWL ENG DRAIN FIR SHIELD IAW CRJ900 EO RS4090. NO FURTHER DAMAGE FOUND.

Part: SKIN — CHAFED (FUSELAGE) · airframe 14,965 hrs · 9,415 cycles

FUSELAGE SKIN & RIVET CHAFED AT FS 918.5, STRINGER 27 FROM EXCESSIVELY LONG SCREW BODY FAIRING 196DR. REPAIRED CHAFED IN FUSELAGE SKIN AT FS 918.5 AT STRINGER 27 IAW CRJ900 EO R3528.

Part: PANEL — CHAFED (TE FLAP) · airframe 14,965 hrs · 9,415 cycles

LEFT INBD FLAP INBD VANE PANEL 684ET CHAFED. OBTAINED NEW LT INBD FLAP INBD VANE PANEL 684ET. BACK DRILLED & COUNTERSUNK PANEL 684ET IAW CRJ 900 SRM 51-40-11. APPLIED PRIMER & TOP COAT IAW CRJ 900 SRM 51-25-06 7 CRJ 900 SRM 51-25-16.

Part: PANEL — CHAFED (TE FLAP) · airframe 14,965 hrs · 9,415 cycles

RIGHT INBD WING FLAP PANEL 684JB HAS CHAFE DAMAGE. REPLACED RT INBD WING FLAP PANEL 684JB WITH PN CC670-14178-1. DRILL & COUNTERSUNK HOLES IAW CRJ 900 SRM 51-40-11-001-001-A01 IAW CRJ900 IPC 57-51-32.

Part: PIN — BACKED OUT (EMERGENCY LIGHT) · airframe 14,965 hrs · 9,415 cycles

LEFT WING, AFT OVER WING EMERGENCY LIGHT WIRE, PULLED OUT. RECEDED PIN INTO CONNECTOR IAW CRJ 900 ESPM 20-16-05. PERFORMED OPERATIONAL TEST OF EXTERIOR EMERGENCY LIGHTS IAW CRJ 900 AMM 33-51-15-710-801-A01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: TARGET — DEFECTIVE (LANDING GEAR) · airframe 14,762 hrs · 9,393 cycles

AFTER TAKEOFF WE PUT THE LG HANDLE TO THE UP POSITION & THEN WE GOT THE GEAR DISAGREE MASTER WARNING MESSAGE & THE PROX SYS FAULT 1 STATUS MESSAGE. RAN THE NON-NORMAL LIST & LANDED AT DSM, THE GEAR NEVER CAME UP. ALL THE GEAR PINS WERE OUT. INSTALLED TARGET FOR PROX SENSOR PX37 RIG, OPERATIONS CHECKED GOOD IAW CRJ900 32-61-05.

Part: LIGHT — MISSING (GALLEY) · airframe 14,473 hrs · 9,114 cycles

EMERGENCY LIGHT STRIP IN GALLEY IS MISSING. REPLACED EMERGENCY LIGHT IAW AMM 33-51-01.

Part: A/C PACK — ODOR (CABIN) · airframe 14,177 hrs · 8,926 cycles

AFTER TAKEOFF, STRONG SULFUR ODOR NOTICED. LEFT PACK OAT 65C AND WOULDN'T COOL OFF. SELECTED MANUAL MODE TEMP CONT TEMP COOLED OFF. ODOR WENT AWAY. INSPECTED LEFT DUCT FOR PROBLEMS. NO ODOR DETECTED.

Part: FUEL NOZZLE — LEAKING · airframe 13,906 hrs · 8,773 cycles

F/A REPORT A STRONG ODOR IN CABIN. ODOR BEGAN WHEN PACKS STARTED. STRONG "OILY" ODOR. ODOR IMPROVED AFTER A TIME, BUT REMAINED IN THE CABIN. ODOR SEEMED STRONGER IN SOME AREAS. PRIMARILY AROUND ROWS 5 AND 6. WHEN PACKS WERE OFF, ODOR WENT AWAY. FOUND LEAK AT THE 5 O`CLOCK POSITION OF FUEL NOZZLES.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 13,113 hrs · 8,259 cycles

PHOTO LUMINESCENT STRIP IS MISSING FROM ROW 7AB. OK TO DEFER PHOTO LUMINESCENT STRIP AT 7AB PER MEL 33-51-1G. MOC NOTIFIED. PLACARD INSTALLED MM02 UPDATED. REPLACED PHOTO LUMINESCENT STRIP AT SEAT 7AB IAW 33-51-01. P/N PL88-900LH00. ITEM REMOVED FROM MM02. MXC NOTIFIED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,218 hrs · 7,098 cycles

ALL EMERGENCY LIGHTS AFT OF EMERGENCY EXITS ARE INOPERATIVE. REMOVED AND REPLACED EPSU BATTERY PACK PS38 IAW 33-51-17. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,257 hrs · 6,534 cycles

NOTED MULTIPLE INTERIOR AND EXTERIOR EMERGENCY LIGHTS ARE INOP. REPLACED BATTERIES AT PS38 AND PS43. REF CRJ900 AMM CH 33-51-17. P/N 2013-1A. S/N ON AT PS38 74272. S/N ON AT PS43 84841. ALL CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (BS 354) · airframe 9,404 hrs · 6,022 cycles

INTERCOSTAL AT FS 364.00 STRINGER 27 LT HAS CORROSION. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 9,404 hrs · 6,022 cycles

COCKPIT FLOORBEAM ANGLE CORRODED ON FWD SIDE OF BS 280, MARKED DOT 68A004. R & R FLIGHT DECK FLOORBEAM ANGLE AT FS 280 IAW SRM 51-42-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,404 hrs · 6,022 cycles

CABIN FLOOR SUPPORT AT SERVICE DOOR CORRODED, MARKED DOT 68A008. REMOVED CORROSION FROM CABIN FLOOR SUPPORT IAW SRM 51-21-06, SUPPORT IS WITHIN LIMITS IAW SRM 53-21-23 RE APPLIED FINISH IAW SRM 51-25-16.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 9,404 hrs · 6,022 cycles

SERVICE DOOR THRESHOLD CORRODED, MARKED DOT 68A009. R & R SERVICE DOOR THRESHOLD IAW SRM 51-42-06.

Part: WEB — CRACKED · airframe 9,404 hrs · 6,022 cycles

FWD EQUIPMENT BAY RT SIDE WEB IS CRACKED NEXT TO ADG PUMP. FABRICATED & INSTALLED A TITANIUM REPAIR DOUBLER IAW REO 670-53-11-509.

Part: SILL — CORRODED (BS 280) · airframe 9,404 hrs · 6,022 cycles

CABIN FLOOR SILL CORRODED ON AFT SIDE OF 280 BEAM RT SIDE AT RBL 43, MARKED DOT 68A005. REMOVED LIGHT SURFACE CORROSION ON AFT SIDE OF 280 BEAM RT SIDE AT RBL 43, SRM 51-21-06 AND FINISH COATS SRM 51-21-16.

Part: BULKHEAD — CORRODED (BS 280) · airframe 9,404 hrs · 6,022 cycles

STATION 280 BULKHEAD CORRODED ON LT SIDE OF FLT DECK ENTRANCE ON UPPER SIDE OF 280 BEAM, MARKED DOT 68A006. REMOVED 3 BLIND RIVETS TO FACILITATE THE REMOVAL OF CORROSION. REMOVED CORROSION FROM STA 280 BULKHEAD IAW SRM 51-21-06. UT INSPECTION SHOWED A MATERIAL LOSS OF .001 USING UT TESTER AAR 521401 DUE DATE 04/11/12. REMAINING MATERIAL IS WITHIN LIMITS IAW SRM 53-00-00. REMAINING MATERIAL IS .031. REINSTALLED 3 BLIND RIVETS PN CR3223-5-2. TAG NR B84867 IAW SRM 51-42-00. REAPPLIED FINISH TO AREA IAW SRM 51-21-16.

Part: LIGHT — DAMAGED (CABIN) · airframe 8,379 hrs · 5,392 cycles

FWD GALLEY AREA EMERGENCY FLOOR PATH LIGHTING DAMAGED. REPLACED FWD GALLEY AREA FLOOR PATH LIGHTING IAW AMM 33-51-01.

Part: STRINGER — DAMAGED (BS 1155 S8R) · airframe 7,972 hrs · 5,147 cycles

FOUND DAMAGED STRINGER NR 8R AT STA 1155 DAMAGE DEPTH .053, W .2958, L .622. DAMAGE REMOVED FROM STR 8R ES 1162,00 AND TEMPORARY REPAIRED IAW REO 690-53-61-161. ALSO, INITIATED PWI TO COMPLETE PERMANENT REPAIR WITHIN 1200 FLT HRS.

Part: LIGHT — MISSING (CABIN) · airframe 7,937 hrs · 5,125 cycles

EMERGENCY FLOOR PATH LIGHT STRIP FWD LT GALLEY MISSING TOP PIECE. INSTALLED EMERGENCY FLOOR PATH STRIP PIECE AND FILM BY FWD GALLEY IAW MM 33-51-01.

Part: MOUNT — CRACKED (PAX DOOR) · airframe 7,733 hrs · 5,007 cycles

NOTED CRACK THRU TOP RIVET ON AFT DOOR MOTOR MOUNT. REPAIRED DAMAGE IN ZONE 4 ON PAX AFT STAIR SIDE PANEL USING REO 670-52-11-104 AS REF. ACCOMPLISHED EDDY CURRENT INSPECTION OF REPAIRED AREA AND CUTOUT EDGES PER NDTM 51-20-006 CRACK FREE AT THIS TIME.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,733 hrs · 5,007 cycles

NOTED 1,5 INCH CRACK IN RADIUS OF AFT DRAG ANGLE NEAR THE SUPPORT WHEEL PULLEY BRACKET AREA ON FWD PAX DOOR. REPAIRED AFT DRAG ANGLE USING SRM 52-11-04 & REO 690-52-11-026 AS REF.

Part: LIGHT — DETACHED (CABIN) · airframe 6,288 hrs · 4,179 cycles

F/A REPORTS LUMINESCENT STRIP IN FRONT OF GALLEY TRASH CAN IS DETACHED. REPLACED LUMINESCENT STRIP, FRONT GALLEY LT SIDE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 6,112 hrs · 4,064 cycles

UPON INSP FOUND EMERGENCY FLOOD LIGHT IN ROW 2 TO BE INOP. REPOSITIONED PIN ON CONNECTOR.

Part: LIGHT — MISSING (GALLEY) · airframe 4,633 hrs · 3,219 cycles

FLOORTRACK LIGHTING MISSING FROM GALLEY 2. REPLACED EMERGENCY FLOOR TRACK LIGHTING IN GALLEY 2.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 4,343 hrs · 3,057 cycles

GLOW STRIP ON FLOOR BY FRONT GALLEY GARBAGE CAN NEEDS TO BE RESECURED. REPLACED EMERGENCY FLOOR PATH MARKING AT LT GALLEY.

Part: LIGHT — LOOSE (CABIN) · airframe 3,900 hrs · 2,747 cycles

FA REPORTED THAT THE FLOOR TRACK LIGHTING STRIP WAS LOOSE. REPLACED FLOOR LIGHTING STRIP.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 106 hrs · 77 cycles

HOT PLASTIC SMELL NOTED IN FLIGHTDECK DURING DESCENT, LANDING ,TAXI IN DTW. ARRIVED AT A/C COULD NOT SMELL ANYTHING. RAN PACK'S FULL NOT COULD NOT SMELL ANYTHING JUST THE NEWNESS OF THE A/C COULD NOT DUPLICATE THE SMELL. INSPECTED THE VENT'S COULD NOT SEE ANYTHING.