N585NN

Part: WINDSHIELD — CRACKED (RH WINSHIELD) · airframe 19,916 hrs · 17,710 cycles

RH WINSHIELD STARTED ARCING CAUSING CRACK. REMOVED AND REPLACED THE RH WINDSHIELD IAW CRJ 900 AMM 56-10-05-000/400-801-A01.

Part: LIFE VEST — UNSERVICEABLE (200) · airframe 19,902 hrs · 17,696 cycles

PFD 1 FAILS WITH ELECTRICAL BURNING SMELL AND PFD 1 CB PANEL 2 V10 POPPED. PILOTS DESCRIBED HOW THEY SMELLED AN €ŒELECTRICAL BURNING SMELL€?. THE LOCATION OF THE SMELL WAS REPORTED IN THE COCKPIT. THE SOURCE OF THE SMELL WAS THE #1 PFD, WHILE THE DURATION OF THE SMELL WAS NO MORE THAN 10 TO 15 MINUTES (SMELL DISSIPATED AFTER CIRCUIT BREAKER POPPED). NO MEDICAL ATTENTION REQUIRED. / REMOVED AND REPLACED PFD 1 IAW CRJ 900 AMM 31-61-01-000/400-801-A02. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49-A12

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA). CORROSION ON LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 THEREFORE LH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (5EA) WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 19,091 hrs · 17,006 cycles

INITIAL INSPECTION: FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO, 2 AND NO, 3 WERE REPLACED PER RIL #2103 REV. B.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS847+16. CORROSION ON SEAT RAILS OF RBL9 BTW FS693.00 TO FS847+16. EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 THEREFORE SEAT RAILS OF RBL9 BTW FS693.00 TO FS847+16 WAS REPLACED PER PER CRJ900 AMM 53-00-49 (CONFIG A12).

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) WERE EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 THEREFORE SEAT RAIL BTW FS744.15 TO FS 969.00 (6EA) WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS677.00 (6EA). CORROSION ON SEAT RAILS OF RBL9 BTW FS349.00 TO FS677.00 (6EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 THEREFORE SEAT RAILS OF RBL9 BTW FS349.00 TO FS677.00 (6EA) WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)

Part: SEAT TRACK — CORRODED (PAX CABIN) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (5EA). LH SIDE SEAT RAIL BTW FS379.00 TO FS677.00 (5EA) WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND CRJ900 SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ-900 AMM 53-00-49-A12

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

DISCREPANCY: CORROSION ON SEAT RAILS OF LBL9 BTW FS708.00 TO FS1000.00. CORROSION ON SEAT RAILS OF LBL9 BTW FS708.00 TO FS1000.00. EVALUATED OUT LIMITS PER CRJ900 SRM 53-41-49-101-001-A02, SEAT RAILS OF LBL9 BTW FS708.00 TO FS1000.00. REPLACED PER AMM 53-00-49 (CONFIG. A12).

Part: FRAME — CORRODED (E/E COMPARTMENT) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON FRAME FS= 310.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) CORROSION ON FRAME FS= 310.00 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED AND EVALUTED WITHIN LIMITS PER CRJ900 SRM 53-00-06-201-005-A01

Part: MOUNT — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON ANGLE, MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE. CORROSION ON ANGLE, MOUNTING BTW FS 319.70 AND FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01

Part: BRACKET — CORRODED (ZONE 100) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-22-001-001-A01

Part: LUG — CORRODED (RT AILERON) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON HOUSING OF LUG 5 AT RH AILERON WAS FOUND. LUG 5 WAS REPAIRED PER REO 670-57-61-237 REV ORIGINAL

Part: FRAME — CORRODED (E/E BAY) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 23LH TO STGR 22RH. CORROSION ON CIRCUMFERENTIAL JOINT FS 280.00 TO FS 282.86 BTW STGR 23LH TO STGR 22RH WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPAIRED PER REO 690-53-21-1790 REV. -

Part: STRAP — CORRODED (E/E BAY) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON JOINT STRAP FS= 333.00 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E). JOINT STRAP FS= 333.00 BETWEEN STRG 27 TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E). WAS REPAIRED PER REO 690-53-21-1789 REV - -

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CORROSION INSIDE OF FLOOR PANEL SUPPORT ANGLE WITH THE CROSSBEAM UNION AT FS280.00 BTW RBL 12.00 AND LBL 12.00. FLOOR PANEL SUPPORT ANGLE WITH THE CROSSBEAM UNION AT FS280.00 BTW RBL 12.00 AND LBL 12.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

DISCREPANCY: CORROSION ON SEAT RAILS OF LBL9 BTW FS364.00 TO FS708.00. FLOOR SEAT RAILS OF LBL9 BTW FS364.00 TO FS708.00 (5EA) ARE OUT OFF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01,SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12) AND PER CRJ900 AMM 20-21-00-910-801-A01

Part: POST — CORRODED (BS 280) · airframe 19,091 hrs · 17,006 cycles

IN REF TO: DURING INSPECTION OF THE TASK CARD 53-10-219B, IT WAS DETECTED CORROSION ON BULKHEAD DOOR POST RBL 12 & LBL 12 AT FS280.00. BULKHEAD DOOR POST RBL 12 AND LBL 12 WERE REPAIRED PER CRJ900 SRM 53-11-10-201-006-A01

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

INITIAL INSPECTION: CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN FS= 333.0 TO FS= 349.00 AT MAIN AVIONICS COMPARTMENT. (E/E). INTERCOSTAL ATTACHED TO STRINGER 20RH IN FS= 333.0 TO FS= 349.00 WAS EVALUATED PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01

Part: SKIN — GOUGED (LH WING SLAT) · airframe 19,091 hrs · 17,006 cycles

1211.83FH PERM REPAIR - TEMPORARY FOR LH SLAT NO.3 TE SKIN GOUGE WITHIN 1211.83 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LH SLAT TE SKIN WAS REPAIRED PER REO 690-57-42-1069 REV - - PERMANENT DISPOSITION

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON INTERCOSTAL (2 EAS) BTW FS 349.00 TO FS 364.00, BTW STGR 26LH AND STGR 26RH OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE. (SM). INTERCOSTALS (2EAS) BTW FS349 TO FS364 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-003-A02 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CRACKED CENTER COCKPIT FLOOR BEAM LBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. FLOOR BEAM LBL12 AT FS280.00 FLOOR INTERNAL SUPPORT STRUCTURE WAS REPAIRED PER REO 690-53-11-1790 REV. --

Part: SKIN — WORN (ZONE 500 LOWER) · airframe 19,091 hrs · 17,006 cycles

WEAR ON AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-477 REV - -

Part: FLOORBEAM — CORRODED (FLIGHT COMPARTME) · airframe 19,091 hrs · 17,006 cycles

SECONDARY NRC FROM NRC 00122': AFTER REMOVAL, CORROSION ON RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-13-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01

Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,091 hrs · 17,006 cycles

SECONDARY NRC FROM NRC 00122': AFTER REMOVAL, CORROSION ON LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-13-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

SECONDARY NRC: IN REFERENCE TO JOB TRFKE000YVW3:53-10-303-JIC/001. AFTER REMOVAL FLOOR SUPPORT, CRACK ON FLOOR SUPPORT OF LBL12 BTW FS280 TO FS265 WAS FOUND. FLOOR SUPPORT OF LBL12 BTW FS280 TO FS265 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-13-001-001-A01

Part: SKIN — WORN (RT WING LOWER) · airframe 19,091 hrs · 17,006 cycles

WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB,686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. AREA OF SETTLEMENT OF FAIRINGS (683AB,686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WAS REPAIRED PER REO 690-57-21-478 REV - -.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 19,091 hrs · 17,006 cycles

INITIAL INSPECTION: CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 20.0% FRNT SPAR DATUM TO STGR DATUM TO 25.93% STGR DATUM. FWD DRAG ANGLE BTW 20.0% FRONT SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT WAS REPAIRED PER CRJ-900 SRM-55-31-00-201-001-A01.

Part: FITTING — DAMAGED (NLG LINK) · airframe 19,091 hrs · 17,006 cycles

PERM REPAIR BEFORE 19,411.07 FH - TEMPORARY REPAIR FOR BURR DAMAGE TO NLG LOCK LINK FITTING BOLT HOLE THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 3650 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV - -. NLG LOCK LINK FITTING WAS REPAIRED PER REO 690-53-11-1794 REV. --

Part: SEAT TRACK — DAMAGED (FLIGHT DECK) · airframe 19,091 hrs · 17,006 cycles

TEMP/PERM REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS PERMANENT REPAIR PILOT/CO-PILOT SEAT TRACK WEAR STRIP DUE TO MISSING OR LOOSE FASTENERS SEE INDIVIDUAL WO OR LB AND REO 670-53-11-210-C FOR DETAILS. PILOT/CO-PILOT SEAT TRACKS WERE REPAIRED PER REO 670-53-11-210 REV. -D PERMANENT REPAIR.

Part: BULKHEAD WEB — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON LH LOWER WEB AT BULKHEAD FS 280.00 LBL 12 ABOVE FLOOR. CORROSION ON LH LOWER WEB AT BULKHEAD FS 280.00 LBL 12 ABOVE FLOOR WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-11-10-201-003-A01 AND WAS REPAIRED PER CRJ-900 SRM 53-11-10-201-003-A01.

Part: STRAP — CORRODED (ZONE 100) · airframe 19,091 hrs · 17,006 cycles

INITIAL INSPECTION: CORROSION ON STRAP, INNER (2EAS) FS 319.70 AND FS 349.00 OF STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE. STRAP, INNER (2EAS) FS 319.70 AND FS 349.00 OF STGR 17RH AT SERVICE DOOR SURROUND STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.

Part: FIRESHIELD — DAMAGED (RT NACELLE) · airframe 19,091 hrs · 17,006 cycles

RH ENGINE LWR FWD CORE COWL FIRE SHIELD WITHIN 2,566.78 FLIGHT HOURS FROM IR (BEFORE 19,384.43FH) REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. FIRESHIELD LWR FWD CORE COWL RH ENGINE WAS REPAIRED PER REO 690-54-23-384 REV - -

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 220.00 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE. FLOOR SUPPORT RBL 12.00 BTW FS 220.00 TO FS 229.00 WAS REPAIRED PER REO 690-53-11-1797 REV. - -

Part: ANGLE — CORRODED (ZONE 100) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON ANGLE, LOWER SILL (4EAS) BTW FS 319.70 TO FS 349.00 AT SERVICE DOOR SURROUND STRUCTURE. ANGLE, LOWER SILL (4EAS) BTW FS 319.70 TO FS 349.00 WERE EVALUATED OUT OF LIMITS PER CRJ 900 SRM 53-00-00-101-001 -A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.

Part: FITTING — CORRODED (ZONE 200) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON SETTLEMENT FITTING (1EA) FS 310 ( LBL37) OF ENTRANCE COMPARTMENT AT FUSELAGE FLOOR STRUCTURE. SETTLEMENT FITTING AT FS310 LBL37 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01

Part: WEB — CRACKED (ZONE 100) · airframe 19,091 hrs · 17,006 cycles

CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB RH FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.

Part: CANISTER — CRACKED (ZONE 500) · airframe 19,091 hrs · 17,006 cycles

SETTLEMENT FITTING AT FS310 LBL37 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01. CANISTER OF SLAT TRACK 1-3 AT RH FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV. - -

Part: PLATE — CORRODED (ZONE 100) · airframe 19,091 hrs · 17,006 cycles

INITIAL INSPECTION: CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT. CORROSION ON UPPER/LOWER FACE OF PLATE LBL 3.4 BTW FS533.00 AND FS 549.00 AT FWD CARGO COMPARTMENT.

Part: SUPPORT — CRACKED (REFUEL/ DEFUEL) · airframe 19,091 hrs · 17,006 cycles

AFTER REMOVAL OF LOWER FUSELAGE FAIRINGS, CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM). REFUEL DUCT MOUNTING SUPPORT WAS REPAIRED PER REO 690-28-25-022 REV.--

Part: SKIN — CORRODED (ZONE 100) · airframe 19,091 hrs · 17,006 cycles

CORROSION ON JOINT PLATE UPPER LONGERON AND AFT HINGE BTW FS549.00 AND FS565.00 AT FWD BAGGAGE BAY DOOR SURROND STRUCTURE. JOINT PLATE UPPER LONGERON WAS REPAIRED PER REO 690-53-31-847 REV. -- AND AFT HINGE BTW FS549.00 AND FS565.00 AT FWD BAGGAGE BAY DOOR SURROND STRUCTURE WAS REPLACED PER CRJ900 AMM 20-21-00-910-801-A01

Part: PIN — UNSERVICEABLE (FAN BLADE) · airframe 18,242 hrs · 16,262 cycles

INSPECTED LH FAN BLADES FOR STIFFNESS, NO DEFECTS FOUND, VIBE CHECK GOOD IAW CRJ 900 AMM 72-21-02-200-803-A01. HIGH TORQUE PIN T/S DUE WITHIN 15 CYCLES. / REMOVED AND REPLACED LH ENGINE FAN BLADE PINS IAW CRJ 900 AMM 72-21-02-000/400-801-A01-PSA. PERFORMED VIBE CHECK IAW CRJ 900 AMM 71-00-00-720-806. ENGINE RUN GOOD. VIBE CHECK GOOD. L/H VIBE .2 R/H VIBE .3. GOOD VIBES.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,080 hrs · 16,086 cycles

PAX DOOR WARNING MSG IN FLIGHT, PEFORMED QRH FOLLOWED BY CABIN ALT, ALSO FOLLOWED BY PROX SYSTEM FAULT ONE STATUS MSG+MANAULLY DEPLOYED MASKS FA NOTED WHISTLINGS SOUND COMING FROM PAX / C/W FULL RIG CHECK OF PAX DOOR IAW CRJ900 AMM 52-11-00-720-802-A01. NO OUT OF RIG CONDITIONS NOTED NEUTRAL RIG MAINTAINED. C/W OPS CHECK OF PAX DOOR IAW CRJ900 AMM 52-11-00-710-801-A02, PAX DOOR OPERATION AND INDICATION ALL CHECKED GOOD.

Part: FMU — UNSERVICEABLE (400) · airframe 16,365 hrs · 14,636 cycles

L ENGINE FLAMEOUT CAUTION MESSAGE IN FLIGHT, N1 AND N2 BOTH DECREASED MOMENTARILY THEN CAME BACK TO NORMAL INDICATIONS L ITT EXCEED C MESSAGE FOLLOWED / COMPLIED LH ENGINE BORESCOPE INSP. OF THE STAGE 1 AND 2 HPT, COMBUSTION LINER AND TURBINE NOZZLE IAW CRJ 900 AMM 72-44-00-290-801 AND 72-51-01-290-801. NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED LH FUEL METERING UNIT IAW CRJ 900 AMM 73-21-03-000/400-801. LEAK AND OPS CHECK GOOD.

Part: SENSOR — UNSERVICEABLE (700) · airframe 14,836 hrs · 13,268 cycles

RTF-LH OB BTMS WENT TO 2O IN FLIGHT / FOUND #1 MLG BTMS CONNECTER SLIGHTLY LOOSE. DEFERRED #1 MLG BTMS PER CRJ900 MEL 32-46-01 OPTION 4 CAT C. C/W M FUNCTION BY CAPPING CONNECTER WITH METAL DUST CAP AND SECURING TO HARNESS. REMOVED AND REPLACED #1 BRANK TEMP SENSOR IAW CRJ 900 AMM 32-46-01-000/400-801-A01. OP CHECK GOOD, MEL CLEARED."

Part: NONE — NONE · airframe 14,601 hrs · 13,056 cycles

PERMANENT REPAIR DUE TO FUSELAGE SKIN BETWEEN FS 364.00 AND FS 379.00 AND STR 22R- STR 23R / COMPLIED WITH EDDY CURRENT OF CUT OUT SECTIONS OF REPAIR AREA SURROUNDING FS 364.00, FS 379.00, AND STR 22R-23R USING REO 690-53-21-1520 REV. P2 AND CRJ900 NDTM 51-20-006. AREA FOUND TO BE FREE OF CRACKS. SEE REMAINING LABOR ROWS OF TASK FOR COMPLETION OF PERMANENT REPAIR. PERFORMED RII INSPECTION OF PERMANENT REPAIR COMPLETED BY MHIRJ TECHNICIAN FOR REO 690-53-21-1520 IAW REO INSTRUCTIONS. REPAIR HAS BEEN FOUND TO BE SATISFACTORY AND AIRCRAFT IS APPROVED FOR RETURN TO SERVICE. FINAL REO AND MHIRJ AIRCRAFT STATEMENT OF WORK FORMS STILL NEED RECEIVED AND DOCUMENTED. FAA FORM 337 NEEDS COMPLETED. RECEIVED THE FINAL REO APPROVAL AND THE STATEMENT OF WORK. COMPLETED AND SEND FORM 337. COMPLIED WITH THE NEW WEIGHT AND BALANCE. AIRCRAFT IS APPROVED FOR RETURN TO SERVICE."

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,384 hrs · 10,270 cycles

RIGHT SIDE RBL 9 SEAT TRACK CORRODED AT FS 349.0.

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,384 hrs · 10,270 cycles

CROSS BEAM AT FS 280.0 HAS CORROSION.

Part: RIB — CRACKED (LT WING ZONE 500) · airframe 11,384 hrs · 10,270 cycles

LT WING INBOARD LEADING EDGE MACHINED RIB AT WS 58.41 CRACKED.

Part: SEAT TRACK — CORRODED (ZONE 200 - CABIN) · corrosion level 2 · airframe 11,015 hrs · 10,012 cycles

CABIN SEAT TRACK RBL 9 STA 485-501 AREAS OF CORROSION.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 10,361 hrs · 9,343 cycles

BURNING SMELL ON TAKEOFF, SMELL IN FLT DECK, SMELL ONLY AT HIGH POWER APU OFF. MX INSPECTED. PERFORMED ENGINE RUN UP AT HIGH POWER IAW CRJ 900 AMM 71-00-00-866 CONFIG A02. PACKS OPERATED SEPARATELY AND AT THE SAME TIME, WITH HYDRAULIC POWER LOADING THE SYSTEM. NO BURNING SMELL DETECTED AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 10,312 hrs · 9,301 cycles

BURNING SMELL IN COCKPIT AND CENTER CARGO. MX INSPECTED AND BELIEVE GROUND AIR CART TO BE SOURCE OF SMELL. ATTEMPTED TO DUPLICATE ACFT CONFIG. COULD NOT DUPLICATE BURNING SMELL IN/AROUND ACFT. NO FURTHER DEFECTS NOTED AT THIS TIME

Part: COUPLING — DAMAGED (FUEL SYSTEM) · airframe 8,640 hrs · 7,811 cycles

FUEL SPILL OVER FIVE GALLONS, FIRE TRUCKS CALLED FOR PRECAUTION. REMOVED AND REPLACED NEW O-RING RUBBER AND NEW BOOT RE/DE FUEL COUPLING IAW AMM 28-25-11-000/400-801 OPS CK GOOD NO FUTHER DEFECTS NOTED AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,147 hrs · 5,668 cycles

CREW DECLARED AN EMERGENCY FOR L BLEED DUCT WARNING WHICH SHUT DOWN THE LT PACK, THE APU AND RT PACK ARE ON DEFERRAL. THE CREW DIVERTED INTO PHL. INSP BLEED LOOPS MT142 & MT225 NO DEFECTS NOTED. C/W ALIC BITE CHECK SYS CHECK GOOD, C/W BLEED AIR LEAK DETECTION & WARNING SYSTEM TEST SYS OPS CHECK GOOD. RAN ENG INSP LOOPS FOR BLEED LEAKS NONE FOUND.