N514AE

Part: UNKNOWN — ODOR (CABIN) · airframe 48,315 hrs · 37,429 cycles

VERY STRONG CHEMICAL BURNING LIKE SMELL INTERMITTENT IN FLIGHT DECK AND CABIN. NO VISIBLE SMOKE OR OTHER ABNORMAL INDICATIONS. STRONGEST DURING T/O AND 2 TIMES IN CRUISE FLT / T/S PER FIM 21-21-00-810-806-A01/ FIM 21-22-00-810-806-A01, PERFORMED CLEANING OF BOTH ENGINES FOR PERFORMANCE RECOVERY IAW AMM 72-00-00-100-801-A01 SECTION 4 G FROM ITEM 4 THOUGH 19 . NO FUMES OR /AND SMELL ARE NO LONGER PRESENT.

Part: SKIN — DENTED (ZONE 100) · airframe 47,418 hrs · 36,662 cycles

DENTS (2EAS) ON FUSELAGE SKIN LOCATED BTW FS280/ FS310 AND STGR23L / STGR25L. DENTS (2EAS) ON FUSELAGE SKIN LOCATED BTW FS280/ FS310 AND STGR23L / STGR25L WERE REPAIRED PER REO 670-53-21-2608 REV. -- AND REO 670-51-00-085 REV - A.

Part: RETAINER — CORRODED (ZONE 100) · airframe 47,418 hrs · 36,662 cycles

AFTER REMOVAL SEAL IN REFERENCE TO NRC 00025, CORROSION ON RETAINER LOWER AND REATINER SEAL LOWER FWD WAS FOUND. DUE EXCCESIVE DAMAGE ON RETAINER LOWER AND RETAINER SEAL LOWER WERE REPLACED PER CRJ700 SRM 51-10-06-001-001-A01 AND SRM 51-42-06-001-001-A01.

Part: FITTING — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON FITTING PN: 9391251-3 (1EA) UNDER THE FLIGHT ATTENDANT SEAT AT ENTRANCE COMPARTMENT. NEW FITTING PN: 9391251-3 UNDER THE FLIGHT ATTENDANT SEAT AT ENTRANCE COMPARTMENT WAS REPLACED PER SAFRAN CMM 25-23-35

Part: DRAIN PAN — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON DRAIN PLATE OF FLOOR PANEL 232BRF. CORROSION ON DRAIN PLATE OF FLOOR PANEL 232BRF WAS EVALUATED BY EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ/900 AMM 53-00-47-000-802 (CONFIG A19) AND AMM 53-00-47-400-802 (CONFIG A19).

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 47,418 hrs · 36,662 cycles

AFTER SPLICE REMOVAL CORROSION ON SPLICE STGR 26 RH FS 333.00 WAS FOUND. SPLICE STGR 26 RH FS 333.00 WAS EVALUATED OUT OF LIMITS AND REPLACED PER CRJ700 SRM 53-00-00-101-001-A01 AND MUST BE INSTALLED UNDER NRC 00193.

Part: ANGLE — CRACKED (ZONE 100) · airframe 47,418 hrs · 36,662 cycles

CRACK ON ANGLE CAP RH/LH OF FS280 BULKHEAD. ANGLE CAP RH/LH OF FS280 BULKHEAD WERE REPLACED PER CRJ700 SRM 51-42-10-001-001-A01, ANGLE CAP LH WAS INSTALLED UNDER NRC 00194.

Part: HINGE FITTING — CORRODED (ZONE 800) · airframe 47,418 hrs · 36,662 cycles

CORROSION HINGE FITTINGS BORE LH/RH (2E/A) OF NLG DOOR ON FUSELAGE WAS FOUND. EVALUATED, DUE TO EXCESSIVE DAMAGE ON HINGE FITTINGS BORE LH/RH (2E/A) OF NLG DOOR ON FUSELAGE WAS FOUND PER CRJ 700 SRM 53-00-01-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-001-A01.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON FLOOR ANGLE SUPPORTS (3EAS) BTW FS280 TO FS265 AND BTW LBL 12 TO RBL12 AT FLIGHT COMPARTMENT. FLOOR ANGLE SUPPORT (LH AND RH) WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01, MANUFACTURATED PER DWG NO. CC670-33199 AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. PAINT ON FLOOR ANGLE SUPPORT (CENTER) WAS REMOVED PER CRJ700 SRM 51-26-01-001-001-A01, AREA WAS CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND NO DAMAGE CORROSION WAS FOUND AND PAINT WAS RESTORED PER CRJ700 SRM 51-21-11-001-001-A01, CRJ700 SRM 51-25-06-001-001-A01 AND CRJ700 SRM 51-25-16-001-001-A01

Part: ANGLE — CORRODED (ZONE 100) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON SETTLEMENT AREA OF FAIRINGS 195AL, 195BB, 195DL, 196AR AND 196DR BTW FS 847.00 TO FS 977.00 AT AFT FUSELAGE WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01. ON SKIN SETTLEMENT AREA WAS EVALUATED WITHIN LIMITS PER CRJ-700 SRM 53-51-01-101-003-A01, CRJ700 SRM 53-51-01-101-004-A01 AND CRJ700 SRM 53-51-01-101-002-A01. ON SUPPORT STRUCTURE ANGLE LH (FS879), ANGLE RH (FS879), STRAP LH (FS909), STRAP RH (FS909) AND ANGLE M (FS 939) WERE EVALUATED WITHIN LIMITS PER CRJ700 SRM 53-00-00-101-001-A01, ANGLE LH (FS 939), ANGLE RH (FS 939) AND STRAP MID (FS909) WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND WERE REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01

Part: DRAIN PAN — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON DRAIN PLATE AT FLOOR PANEL 232BRF. CORROSION ON DRAIN PLATE AT FLOOR PANEL 232BRF

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON SIDE SEAT RAIL (4 EA) FROM FS 669 TO FS977 LH SIDE. CORROSION ON SIDE SEAT RAIL (4 EA) FROM FS 669 TO FS977 LH SIDE WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-31-49-101-001-A01 AND WERE REPLACED PER CRJ700 AMM 53-00-49 (CONFIG A03).

Part: STRINGER — CORRODED (ZONE 100) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON STGR 27 BTW FS310 TO FS319 AND STGR 25LH BTW FS319 TO FS333 AT MAIN AVIONICS COMPARTMENT. STGR 27 BTW FS310 TO FS319 AND STGR 25LH BTW FS319 TO FS333 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON SIDE SEAT RAIL (4 EA) FROM FS 669 TO FS977 RH SIDE. CORROSION ON SIDE SEAT RAIL (4 EA) FROM FS 669 TO FS977 RH SIDE WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-41-49-101-001-A01 AND WERE REPLACED PER CRJ700 AMM 53-00-49 (CONFIG A03).

Part: STRINGER — CORRODED (ZONE 100) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON STGR 26LH BTW FS310 TO FS349 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR 26LH BTW FS310 TO FS349 AT MAIN AVIONICS COMPARTMENT. WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01

Part: FITTING — CORRODED (GALLEY) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON FLOOR FITTING ACCESS 211 COUNTER AT GALLEY 2. FLOOR FITTING ACCESS 211 COUNTER AT GALLEY 2 WAS REPLACED PER ZODIAC AEROSPACE CMM 25-32-78

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON SEAT TRACK LBL27 (2EA) BTW FS280 TO FS477 AT PAX CABIN. CORROSION ON SEAT RAIL LBL27 (2EA) BTW FS280 TO FS477 AT PAX CABIN WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A01 AND WERE REPLACED PER AMM 53-00-49 (CONFIG A03).

Part: HOUSING — WORN (ZONE 800) · airframe 47,418 hrs · 36,662 cycles

WEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR. WEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 670-52-31-031 REV -B

Part: STRINGER — CORRODED (ZONE 100) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON STGR 23RH BTW FS280 TO FS310 AT MAIN AVIONICS COMPARTMENT. STGR 23RH BTW FS280 TO FS310 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON SPLICES OF STRG (25, 24)RH, FS 333 AT MAIN AVIONICS COMPARTMENT. SPLICES OF STRG (25, 24)RH, FS 333 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01.

Part: TRACK — WORN (ZONE 800) · airframe 47,418 hrs · 36,662 cycles

WEAR AND BEND ON FWD/AFT DOOR TRACKS AT AFT BAGGAGE BAY DOOR. FWD DOOR TRACK AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 670-53-61-2502 REV --. AFT DOOR TRACK AT AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ700 SRM 53-61-58-201-002-A01.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON STGR 19LH AND CONECTOR SUPPORT BTW FS 319 TO FS333 AT MAIN AVIONICS COMPARTMENT. STGR 19L BTW FS 319 TO FS333 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. CORROSION ON CONECTOR SUPPORT BTW FS 319 TO FS333 WAS REMOVED PER SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER SRM 53-00-00-101-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON SEAT RAILS 2 (EAS) AT LBL9 AND LBL 27 FROM FS 847 TO FS977. EVALUATED SEAT RAILS 2 (EAS) AT LBL9 AND LBL 27 FROM FS 847 TO FS977. DUE TO NOT ALLOWABLE DAMAGES PER CRJ-700 SRM 53-41-49-101-001-A01 AND REPLACED PER CRJ-700 AMM 53-00-49-400-801 (CONFIG. A03)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON CENTER SEAT RAILS LBL9/RBL9 (6EAS) BTW STA 280 TO STA 708 AT PAX CABIN. SEAT RAILS LBL9/RBL9 (6EAS) BTW STA 280 TO STA 708 AT PAX CABIN WERE EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A01 AND SRM 53-41-49-101-001-A01 AND REPLACEDPER CRJ-700 AMM 53-00-49-400-801-A03

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 47,418 hrs · 36,662 cycles

AFTER RUDDER REMOVAL, FREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. HINGE FITTING NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WAS REPLACED PER RIL#2103 REV. B.

Part: INTERCOSTAL — CORRODED (E/E BAY) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON INTERCOSTAL AND CLEATS (3 EAS) AT STGR 20R BTW FS319.70 TO FS 349.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-002-A02 AND CORROSION ON CLEATS (3 EAS) AT STGR 20R BTW FS319.70 TO FS 349.00 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND INTERCOSTALWAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND PER CRJ700 SRM 51-42-21-001-001-A01

Part: FITTING — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON 8 EA. FITTINGS BTW FS280 TO FS 310 FROM LBL38 TO RBL38. EXCESSIVE DAMAGE FOUND OUT OF LIMITS 8EA. BTW FS280 TO FS310 FROM LBL38 TO RBL38 REPLACED PER CRJ 700 SRM 51-42-21-001-AO1

Part: DIAPHRAGM — WORN (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CRACK ON DIAPHRAGM LBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE. DIAPHRAGM LBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE WAS REPAIRED PER REO 670-53-82-478 REV. -A.

Part: FRAME — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON FRAME PLATE FS 319.70 AND WL 72 AT PAX CABIN. CORROSION ON FRAME PLATE FS 319.70 AND WL 72 AT PAX CABIN WAS EVALUATED OUT OF LIMITS PER CRJ 700 SRM 53-21-23-101-002-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,662 hrs · 47,418 cycles

AFTER FLOOR SUPPORT ANGLE AT CROSSBEAM REMOVAL, CORROSION FOUND ON WEBS (2 E/AS) AT FS 280.00 BTW LBL 9 AND RBL 9, PREVIOUS REPAIR ON WEBS (2 E/AS) AT FS 280.00 BTW LBL 9 AND RBL 9 WERE REPLACED PER SRM 51-42-13-001-001-A01 AND SRM 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON INTERCOSTALS (1 EAS) STGR 21LH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL AT STGR 21LH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01

Part: ANGLE — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON ANGLE KICKPLATE OF PASSENGER DOOR SURROUND STRUCTURE FROM FS 310 TO FS EN 349 AT PAX CABIN. ANGLE KICKPLATE OF PASSENGER DOOR SURROUND STRUCTURE AT PAX CABIN WAS EVALUATED OUT OF LIMITS PER CRJ700 53-21-23-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND PER CRJ700 SRM 51-42-21-001-001-A01.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

DISCREPANCY: CORROSION ON SEAT RAILS 2 (EAS) AT RBL9 AND RBL 27 FROM FS 847 TO FS977. SEAT RAILS 2 (EAS) AT RBL9 AND RBL 27 FROM FS 847 TO FS977 WERE EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-41-49-101-001-A03 AND REPLACED PER CRJ 700 AMM 53-00-49-400-801 (CONFING A03).

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON STRG 26R BTW FS 333 AND FS 349 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRG 26R BTW FS 333 AND FS 349 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-21-03-101-006-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND PER CRJ700 SRM 51-42-21-001-001-A01

Part: SKIN — DENTED (ZONE 400) · airframe 47,418 hrs · 36,662 cycles

SEVERAL DENTS ON LOWER FAN COWL BTW 5 O'CLOCK TO 8 O'CLOCK POSITION AT LEFT ENGINE. DENT ON LOWER FAN COWL BTW 5 O´CLOCK AT LH ENGINE WAS REPAIRED PER REO 670-54-14-1314 REV. --

Part: DIAPHRAGM — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

CRACK ON DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE. DIAPHRAGM RBL17.63 BTW FS 939.00 TO FS 909.00 AT AFT FUSELAGE WAS REPAIRED PER REO 670-53-82-478 REV. -A.

Part: CAP — CORRODED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

AFTER REMOVAL MID CAP IN REFERENCE TO NRC 00214, CORROSION ON MID CAP AND FWD CAPANGLE WAS FOUND. CORROSION ON MID CAP AND FWD CAPANGLE WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-001-A01 WERE REPLACED AND MUST BE INSTALLED UNDER NRC0214.

Part: SEAT FRAME — CORRODED (ZONE 200) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON LH SIDE SEAT RAILS BTW FS379.00 TO FS669.40 (3E/A). VALUATED,LH SIDE SEAT RAILS BTW FS379.00 TO FS669.40 (3E/AS). DUE TO NOT ALLOWABLE DAMAGES PER CRJ-700 SRM 53-41-49-101-001-A01 AND REPLACED PER AMM 53-00-49-400-801 (CONFIGA03).

Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 36,662 hrs · 47,418 cycles

CORROSION FOUND ON POSTS (2 E/AS) AT FS 280.00 BTW LBL 9 AND RBL 9. POSTS (2 E/AS) AT FS 280.00 BTW LBL 9 AND RBL 9 WERE REPAIRED PER CRJ 700 SRM 53-11-10-201-006-A01

Part: BRACKET — CORRODED (ZONE 100) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON HYD PLATES ON LH/RH MAIN WHEEL WELL AND RH/LH MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AT MLG WHEEL WELL AREAS, RBL40, RBL 45 AND LBL45, RBL40. CORROSION ON HYD PLATES ON LH/RH MAIN WHEEL WELL AND RH/LH MLG HYDRAULIC LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) AT MLG WHEEL WELL AREAS, RBL40, RBL 45 AND LBL45, RBL40. WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01. HYD PLATES ON LH/RH MAIN WHEEL WELL AND LH MLG HYDRAULIC LINE SUPPORT PLATE WERE EVALUATED WITHIN LIMITS PER CRJ700 SRM 53-00-00-101-001-A01. RH MLG HYDRAULIC LINES SUPPORT PLATE AT MLG WHEEL WELL WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ700 SRM 51-41-02-001-001-A01 AND CRJ700 AMM 20-21-00

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON RH SIDE SEAT RAILS BTW FS379.00 TO FS669.40 (3E/A). EVALUATED,RH SIDE SEAT RAILS BTW FS379.00 TO FS669.40 (3E/A) ARE OUT OFF LIMITS PER CRJ-700 SRM 53-21-49-101-001-A01 AND SRM 53-31-49-101-001-A01 AND REPLACED PER CRJ-700 AMM 53-00-49.

Part: STRINGER — CORRODED (ZONE 100) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON STRG 21R BTW FS 364 AND FS 379 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRG 21R BTW FS 364 AND FS 379 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-21-03-101-006-A01 AND REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01.

Part: HANDLE — CORRODED (SERVICE DOOR) · airframe 47,418 hrs · 36,662 cycles

CORROSION ON R1 HANDLE GUARD. R1 HANDLE GUARD PN: 9329222BK1 ITEM [225] WAS VERIFIED AND REPLACED PER CRJ-700 AIPC 25-26-07.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,662 hrs · 47,418 cycles

CORROSION ON FLOOR SUPPORT ANGLE AT CROSSBEAM FS 280.00 BTW LBL 9 AND RBL 9. CORROSION ON FLOOR SUPPORT ANGLE AT CROSSBEAM FS 280.00 BTW LBL 9 AND RBL 9 WAS EVALUATED OUT OF LIMITS PER SRM 53-00-01-101-001-A01 AND WAS FABRICATED AND REPLACED PER DRAWING CC670-34095 REV. - - AND PER SRM 51-42-06-001-001-A01 AND PER SRM 51-42-21-001-001-A01.

Part: FITTING — DAMAGED (ZONE 400) · airframe 36,662 hrs · 47,418 cycles

TOOL MARK ON FITTING OF SPRING CONTRABALANCE AT LH NACELLE. FITTING OF SPRING CONTRABALANCE AT LH NACELLE WAS REPAIRED PER REO 670-54-20-003 REV --

Part: BRACKET — CRACKED (ZONE 200) · airframe 36,662 hrs · 47,418 cycles

TEMP SIDE POSITION FOR CRACK DAMAGE TO PAX DOOR STOP BRACKET. STOP BRACKET TO PAX DOOR LH WAS REPLACED PER CRJ 700 SRM 51-42-21-00-AO1.

Part: PLATE — WORN (ZONE 100) · airframe 47,418 hrs · 36,662 cycles

WEAR ON EXTERNAL TRIPLER PROTECTOR PLATE BTW FS 893.00 TO FS 909.00, AT STGR 27. EXTERNAL PROTECTOR PLATE BTW FS 893.00 TO FS 909.00, AT STGR 27 WAS REPLACED PER CRJ-700 SRM 51-41-02-001-001-A01

Part: SKIN — WORN (ZONE 500 FLAP) · airframe 47,418 hrs · 36,662 cycles

WEAR ON LWR SKIN OF LH OUTBD FLAP BTW FL168.63 TO WS 262. REPAIRED PER REO 670-57-53-409 REV--.

Part: SKIN — DENTED (ZONE 500 FLAP) · airframe 47,418 hrs · 36,662 cycles

DENT ON LOWER SKIN OF LH INBOARD FLAP BTW FLS92.80 TO FLS101.40. DENT ON LOWER SKIN OF LH INBOARD FLAP BTW FLS92.80 TO FLS101.40 WAS REPAIRED PER REO 670-57-52- 605. REV. - -.

Part: SKIN — WORN (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

PROTUBERANCE ON FUSELAGE SKIN LOCATED BTW FS1000 / FS1015 AND STGR1R / STGR2R. PROTUBERANCE ON FUSELAGE SKIN LOCATED BTW FS1000 / FS1015 AND STGR1R / STGR2R WAS REPAIRED PER REO 670-51-00-085 REV - A AND PER REO 670-53-61-2496 REV. - .

Part: SKIN — DENTED (ZONE 200) · airframe 47,418 hrs · 36,662 cycles

DENTS (6EAS) ON FUSELAGE SKIN LOCATED BTW FS349/ FS421 AND STGR18R / STGR19R. PREVIOUS BLEND OUT ON AREA (1 EA) BTW FS 364 TO FS349 STGR 18R TO STGR 19R AND AREAS (3 EAS) BTW FS379 TO FS 394 STGR18R TO STGR 19R WERE EVALUATED WITHIN LIMITS PER CRJ700 SRM 53-21-01-101-007-A01 AND DENTS BTW FS409.00 - 421.00 AND BTWN SGTR18R - 19R WERE REPAIRED PER REO 670-53-21-2610 REV.--

Part: WINDSHIELD — SMOKE (ZONE 200) · airframe 46,611 hrs · 36,012 cycles

CLIMBING THROUGH 1000FT, RECEIVED A LH WINDSHIELD HEAT CAUTION MSG AND BEGAN TO SMELL FUMES. A LITTLE BIT OF SMOKE PUFFED FROM THE LH WINDSHIELD TERMINAL BLOCK. SMOKE AND FUMES WENT AWAY AFTER THE HEAT WAS TURNED OFF. THE LOCATION OF THE FUMES WAS THE COCKPIT AND CAME FROM THE LH WINDSHIELD TERMINAL BLOCK. THE DURATION OF THE SMOKE LASTED NO MORE THAN 5 MINUTES, AND NO MEDICAL ATTENTION WAS REQUIRED; HOWEVER, THE CREW OXYGEN WAS USED. / REMOVED AND REPLACED LH WINDSHIELD IAW CRJ 700 AMM 56-11-01-000/400-801-A01. REMOVED AND REPLACED LH WINDSHIELD TEMP CONTROLLER IAW CRJ700 AMM 30-41-06-000/400-801-A01 AND PERFORMED OPERATIONAL TEST OF WINDSHIELD TEMPERATURE CONTROLLER IAW CRJ700 30-41-06-710-801 FOUND GOOD AND PERFORMED LEAK TEST BY PRESSURING THE AIRCRAFT IAW CRJ700 AMM 21-31-00-910-801/802 AND NO LEAK DETECTED AT THIS TIME.

Part: FILTER — DIRTY (ZONE 200) · airframe 46,495 hrs · 35,897 cycles

BURNING SMELL IN COCKPIT DURING FLIGHT. TURNED OFF UNNECESSARY LIGHTING, SMELL DISSIPATED. / INVESTIGATED SMOKE SMELL IN COCKPIT IAW CRJ 700 FIM 21-21-00-810-806. COULD NOT REPLICATE. FOUND DIRTY FLIGHT COMPARTMENT DISPLAY COOLING AIR FILTER. REMOVED AND REPLACED FILTER IAW CRJ 700 AMM 21-24-10-000/400-801.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,120 hrs · 34,734 cycles

AFTER LANDING AND STARTING THE APU, VERY STRONG FUEL SMELL IN COCKPIT AND PAX CABIN / REMOVED AND REPLACED APU IAW CRJ 700 AMM 49-10-00-000/400-801-A02-PSA. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME, NO FUEL SMELL PRESENT IN AIRCRAFT AT THIS TIME. NO CURRENT DEFECTS AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 44,846 hrs · 34,502 cycles

AFTER LANDING TOWER OBSERVED SIGNIFICANT SMOKE COMING FROM RIGHT ENGINE. FIRE TRUCK ALSO SAW FUEL LEAKING FROM DRAIN TUBE LEAVING LARGE SPOT. INSPECTED AND FOUND RH ENGINE SCVGA ROD END HOSE LOOSE AND LEAKING. RETORQUED AND PERFORMED WET MOTOR AND ENGINE EXTERNAL FUEL/OIL LEAK CHECK. NO FURTHER EXTERNAL LEAKS NOTED. PERFORMED ENGINE OILE LEVEL CHECK IAW CRJ 700 AMM 12-13-79-610-801 AND 12-13-79-612-801. NO OIL SERVICING REQUIRED AT THIS TIME

Part: NONE — UNSERVICEABLE (700) · airframe 44,223 hrs · 33,968 cycles

STEERING INOP IN FLIGHT (AFTER GEAR EXTENSION). TROUBLESHOOT B1 CODE 006931 IAW CRJ 700 FIM 32-51-01-810-802-A01 FOUND PILOT HANDWHEEL CONTROLLER TO BE FAULTY. REMOVED AND REPLACED PILOT HANDWHEEL CONTROLLER IAW CRJ 700 AMM 32-51-01-000/400-801-A01. OP CHECKED GOOD AT THIS TIME.

Part: ELEVATOR SYSTEM — OUT OF ADJUST

DURING CLIMBOUT OUT OF SGF THE ELEVATOR SPLIT CAUTION MSG OCCURRED AT APPROXIMATELY 9,000 TO 10,000 FT. THE CREW RAN THE QRH AND HELD TO BURN FUEL BEFORE LANDING FOR STRUCTURAL CONCERNS. THE A/C DID NOT LAND OVERWEIGHT AND THE PAX DID NOT BRACE FOR LANDING. EMERGENCY VEHICHLES WERE ROLLED UPON LANDING. ELEVATOR SPLIT CAUTION MSG IN FLIGHT / INSPECTED AND FOUND A PHYSICAL SPLIT BETWEEN LH AND RH ELEVATOR CONTROL SURFACES. TROUBLESHOT IAW CRJ700 FIM 27-31-00-810-803. PERFORMED ELEVATOR CABLE CIRCUIT TENSION CHECK IAW CRJ700 AMM 27-31-00-220-812. TENSION CHECK GOOD. PERFORMED FUNCTIONAL CHECK OF THE ELEVATOR CONTROL SYSTEM IAW CRJ700 AMM 27-31-00-720-801. COMPLETED TAP# 0373 FOR ELEVATOR SPLIT MESSAGE. FOUND TB6 JUST UNDER SPEC TENSION. ADJUSTED IAW CRJ-700 AMM 27-31-00-820-808. COMPLETED RIGGING OF THE ELEVATOR CONTROL COLUMN STOPS PER AMM 27-31-01-820-803. FOUND BACK STOPS HITTING FIRST. ADJUSTED STOPS IAW AMM 27-31-01-820-803. / ELEVATORS NOW TRAVEL FULL RANGE. OPS CHECK GOOD."

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYSTEM) · airframe 42,707 hrs · 32,622 cycles

CREW RECEIVED A SLATS FAIL CAUTION MESSAGE. THEY DECIDED TO GO AROUND AND CONSULT THE QRH. UPON LANDING THE FLAPS DEPLOYED BUT THE SLATS DID NOT. SLATS FAIL CAUTION MESSAGE WHEN LOWERING FLAPS TO 8 DEGREES MSG DID NOT GO AWAY DURING QRH PROCEDURE HAPPENDED DURING LANDING/APPROACH PHASE. PERFORMED VISUAL INSPECTION OF SLATS NO DEFECTS NOTED. PERFORMED OPS CHECK OF FLAP AND SLAT SYSTEM IAW CRJ 700 AMM 27-50-00-710-801-A01. OPS CHECK GOOD AT THIS TIME.

Part: CHARGER — FAILED (CABIN) · airframe 39,861 hrs · 30,057 cycles

LH OVERWING EMERGENCY EXIT SIGN FWD OF DOOR INOP. MX REMOVED AND REPLACED #3 EPSU BATTERY CHARGER IAW CRJ700 AMM. OPS CHECK GOOD AT THIS TIME.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,706 hrs · 29,929 cycles

STRINGER 25R IS CORRODED AT RIVSTS BETWEEN FS 319.70 AND FS.333

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,706 hrs · 29,929 cycles

3 INTERCOSTALS BETWEEN FS.349 AND FS.364 BETWEEN STGR 25L AND STGR 26R ARE CORRODED

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,706 hrs · 29,929 cycles

STRINGER 26R IS CORRODED AT RIVETS BETWEEN RS295 AND FS310

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,706 hrs · 29,929 cycles

FUSELAGE FRAME FS.333 BETWEEN STGR26R AND STGR 26L IS CORRODED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 39,714 hrs · 29,937 cycles

PNL 196DR AT STRUCTURAL ANGLE IS CRACKED.REMOVED AND REPLACED DAMAGED AFT STRUCTURAL SUPPORT ANGLE AND STRAP IAW CRJ 700 SRM 51-42-13-001-001-A01 AND 51-40-11-001-001-A01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 39,714 hrs · 29,937 cycles

REMOVED LEFT AND RIGHT JACK PAD INTERCOSTALS IAW CRJ700 SRM 51-42-21-001-001-A01. INSTALLED NEW INTERCOSTALS CC670-32179-1, CC670-32179-2 IAW CRJ700 SRM 51-42-21-001-001-A01.

Part: ACCESS PANEL — DETACHED (100) · airframe 37,708 hrs · 28,167 cycles

ON CLIMBOUT OUT, #3 HYDRAULIC ACCESS PANEL 195AB DEPARTED THE A/C. THE A/C CONTINUED TO DESTINATION WHERE THE CREW DISCOVERED THE PANEL WAS MISSING. THE A/C FERRIED WHERE MX PERFORMED A DETAILED INSPECTION. MX REWORKED DAMAGED AREA AND REPLACED MISSING PANEL.

Part: GUIDE — LOOSE (PAX DOOR) · airframe 32,871 hrs · 23,785 cycles

PASSENGER DOOR WILL NOT OPEN. REMOVED AND INSTALLED PASSENGER DOOR AFT ANCHOR FITTING GUIDE SHAFT AND SWIVEL LEVER.

Part: MANIFOLD — DEFECTIVE (NLG STEERING) · airframe 32,846 hrs · 23,755 cycles

STEERING INOPERATIVE CAUTION MESSAGE. REMOVED AND REPLACED THE STEERING MANIFOLD.

Part: DOOR FRAME — CORRODED (BS 311) · corrosion level 2 · airframe 32,834 hrs · 23,741 cycles

PASSENGER DOOR FORWARD FORMER AT BS 311.75 IS CORRODED UNDER PANEL 832FL. REMOVED AND REPLACED FORWARD FORMER.

Part: SKIN — CORRODED (PAX DOOR) · corrosion level 2 · airframe 32,834 hrs · 23,741 cycles

PASSENGER DOOR IS CORRODED ON THE INNER SKIN UNDER PANELS 832EL, 832BL, 832FL, 832HL, AND 832DL INNER SKIN HAS MULTIPLE AREAS OF CORROSION ON OUTER AND INNER SURFACES. REMOVED, FABRICATED AND INSTALLED INNER SKIN.

Part: ATTACH ANGLE — CORRODED (BS 319 - 349) · corrosion level 2 · airframe 32,834 hrs · 23,741 cycles

SERVICE DOOR STEP PLATE SUPPORT BRACKET ATTACH ANGLES ARE CORRODED. REMOVED AND REPLACED THE ATTACH ANGLES.

Part: DOOR SILL — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 32,834 hrs · 23,741 cycles

CARGO DOOR SILL IS CORRODED BETWEEN BS 1000 AND 1047. REMOVED AND REPLACE CARGO DOOR SILL.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,834 hrs · 23,741 cycles

SERVICE DOOR STEP PLATE SUPPORT BRACKET ATTACHMENT ANGLES CORRODED. REMOVED AND REPLACED SERVICE DOOR STEP PLATE SUPPORT BRACKET ATTACHMENT ANGLES.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,834 hrs · 23,741 cycles

SERVICE DOOR SILL LOWER MOUNTING ANGLE IS CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL LOWER MOUNTING ANGLE.

Part: BELLOWS — LEAKING (PNEUMATIC SYS) · airframe 32,208 hrs · 23,151 cycles

CLIMBING OUT OF 24500, THE CREW RECEIVED A RT RED BLEED DUCT CASS MESSAGE FOLLOWED BY AN AMBER RT DUCT BLEED MESSAGE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LEAKING BELLOWS AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: SIGN — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 32,094 hrs · 23,051 cycles

CABIN OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE INSPECTED, CYCLED SYSTEM SWITCH AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACM — ODOR (AC BAY) · airframe 31,653 hrs · 22,666 cycles

LEFT PACK HIGH TEMP AND BURNING ELECTRICAL ODOR IN COCKPIT. MAINTENANCE TROUBLESHOT, DEFFERED THE LT PACK AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE. MAINTENANCE R&R LT ACM IAW AMM, OPS CHECK GOOD, LEAK CHECK GOOD. MEL CLEARED.

Part: MOTOR — FAILED (WIPER SYSTEM) · airframe 30,346 hrs · 21,496 cycles

AFTER TAKEOFF, CREW REPORTED CAPTAIN’S WINDSHIELD WIPER WOULD NOT STOP. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT WINDSHIELD WIPER MOTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 30,312 hrs · 21,460 cycles

UPON CLIMB AT APPROXIMATELY 22,000 FT, CREW NOTICED SPARK ON RT WINDSHIELD AND SHORTLY AFTER GOT A RT WINDSHIELD HEAT MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WINDSHIELD — SPARKS (COCKPIT) · airframe 30,312 hrs · 21,460 cycles

UPON CLIMB AT APPROXIMATELY 22,000 FT, CREW NOTICED SPARK ON RT WINDSHIELD AND SHORTLY AFTER GOT A RT WINDSHIELD HEAT MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CHECK VALVE — BROKEN (BLEED AIR SYSTEM) · airframe 30,161 hrs · 21,311 cycles

CREW REPORTED LT ENGINE DEGRADED MESSAGE FOLLOWED BY LT ENGINE FLAMEOUT AT FL 360. CREW DECLARED AN EMERGENCY, DIVERTED AND LANDED SAFELY. MAINTENANCE TROUBLESHOT, R & R LT ENGINE 6TH STAGE BLEED AIR CHECK VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 30,019 hrs · 21,176 cycles

FUSELAGE EXTERIOR SKIN IS GOUGED, BETWEEN FS 969.00 - 985.00 ALONG STRINGER 27. REPAIRED FUSELAGE EXTERIOR SKIN GOUGE IAW ERS-CR-53MR-1599.

Part: BALLAST — FAULTY (CABIN) · airframe 29,762 hrs · 20,969 cycles

ELECTRICAL BURN SMELL IN GALLEY. R & R GALLEY LIGHTING BALLAST PS88 & PS89 IAW AMM CH 33-26-03. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 29,096 hrs · 20,439 cycles

AFT FLIGHT ATTENDANT FLASHLIGHT WILL NOT STAY IN CRADLE. R & R AFT EMER FLASHLIGHT ASSEMBLY IAW AMM 25-61-02.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 28,858 hrs · 20,240 cycles

AT FL 230 GOT CABIN A/T ON EO2 COMPLIED WITH POMI PROCEDURES DESCENDED TO FL 100 COULD NOT CONTROL. CABIN ALTITUDE CONTINUED FLIGHT UNPRESSURIZED. COMPLIED WITH PRESSURIZATION CHECK IAW AMM 21-31-00. NO DEFECTS NOTED. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — SMOKE (LT MLG) · airframe 28,369 hrs · 19,874 cycles

ON LANDING EXCESSIVE SMOKE REPORTED BY TOWER FROM LT MLG. INSPECTED MLG & DOOR IAW AMM CH 32-10-00, NO DEFECTS NOTED.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,113 hrs · 19,663 cycles

FORWARD CABIN FLASHLIGHT CRADLE BROKEN. R & R FLASHLIGHT ASSEMBLY IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.

Part: ECU — FAILED (NLG STEERING) · airframe 27,080 hrs · 18,951 cycles

STEERING INOPERATIVE IN FLIGHT. R & R ECU IAW AMM 37-51-10. PERFORMED OPERATIONS CHECK OF RVDT RIGGING IAW AMM 32-50-00. OPERATIONS CHECKED GOOD. STEERING INOPERATIVE MSG CLEARED. .

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,632 hrs · 18,660 cycles

DECLARED EMERGENCY LG ISSUE FLIGHT CXL. DURING MAINTENANCE INSPECTION ON FLIGHT 3313 FOUND EICAS GEAR DISAGREE ON TAKEOFF. AIRCRAFT WAS REMOVED FROM SERVICE. COMPLY WITH THE EXTENSION AND RETRACTION OF THE LANDING GEAR. COULD NOT DUPLICATE FAULT. OPS CHECK GOOD IAW CRJ 700 AMM 32-30-00.

Part: BRACKET — DEFECTIVE (FLASHLIGHT) · airframe 26,218 hrs · 18,401 cycles

FIRST OFFICER`S FLASHLIGHT WILL NOT STAY IN CRADLE. R & R FIRST OFFICER`S FLASHLIGHT BRACKET IAW CRJ MM 25-61-02, OPERATIONS CHECKED GOOD.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 25,980 hrs · 18,237 cycles

LEFT VERTICAL STABILIZER TO FUSELAGE FWD DRAG ANGLE HAS A 1.5 INCH CRACK ALONG T/E OF ANGLE. LT VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE REPAIRED IAW EO CR-55MR-038.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 25,980 hrs · 18,237 cycles

RT VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE HAS 1 INCH CRACK ALONG L/E OF ANGLE. REPAIRED THE RT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE IAW EO CR-53MR-164R1 PART B.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,980 hrs · 18,237 cycles

FOUND FLOORBEAM AT FS 280 CRACKED ON LT AND RT SIDES. REPLACED FLOORBEAM IAW SRM 51-42-06. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CRACKED (BS 280) · airframe 25,980 hrs · 18,237 cycles

LEFT INBD FLOORBEAM ANGLE AT FS 280 CRACKED. FABRICATED REPAIR IAW EO 53EP-115. AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — TORN (RT OVERWING EXIT) · airframe 25,980 hrs · 18,237 cycles

RT OVERWING EMERGENCY EXIT CENTER HANDLE HAS A TEAR IN IT. R & R RT OVERWING EMERGENCY EXIT CENTER HANDLE IAW AMM 25-26-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,980 hrs · 18,237 cycles

LT AFT SECTON OF AISLE EMERGENCY FLOOR PROXIMITY STRIP IS CRACKED. R & R THE LT AFT SECTION OF AISLE EMERGENCY FLOOR PROXIMITY STRIP IAW AMM 33-51-01-400-801 AND ETN CR-33-004.

Part: ELECTRICAL SYS — OVERHEATED · airframe 25,620 hrs · 18,017 cycles

FOUND STRONG ODOR OF ELECTRICAL SMOKE IN COCKPIT. OVERTEMP MESSAGE DISPLAYED ON ED 1 AND ED 2, CIRCUIT BREAKER C9 WAS FOUND TO BE TRIPPED. CIRCUIT BREAKER E-14 WAS ALSO TRIPPED. ACFT WAS SUSPECTED TO BE POWERED FOR 15 PLUS HOURS WITH NO AIR CONDITIONING PACK RUNNING OR PCA CART HOOKED TO ACFT. REMOVED POWER FROM THE ACFT TO ALLOW ACFT TO COOL. PERFORMED AN OPS TEST OF THE COCKPIT ELECTRINIC FLIGHT DISPLAYS EICAS DISPLAY NR 1 AND EICAS DISPLAY NR 2 IAW AMM 31-61-01.

Part: CONTROL UNIT — FAILED (FLAP/SLATS) · airframe 25,334 hrs · 17,838 cycles

THE CREW REPORTED THAT DURING THE CLIMB THEY RECEIVED A STALL FAIL AND SLATS FAIL CAUTION MESSAGE. THE CREW COMPLIED WITH AOM VOL 1 PROCDURES AND DECLARED AN EMERGENCY. THE CREW RETURNED TO ORD AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 2 SLATS/FLAPS ELECTRONIC CONTROL UNIT IAW AMM 27-51-05. THE OPS CHECK WAS GOOD, NO DEFECTS NOTED. R & R THE STALL PROTECTION COMPUTER IAW MM 27-35-01. COMPUTER, STALL PROTECTION, PN: C12851CA01, SN 252. THE OPS CHECK WAS GOOD NO DEFECTS NOTED. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,997 hrs · 17,636 cycles

DURING B-INSPECTION FOUND THE NR 4 EMERGENCY BATTERY WILL NOT POWER LIGHTS. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 4 EMERGENCY BATTERY PACK AND CHARGER IAW WC 33-002. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,306 hrs · 17,188 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT RECHARGEABLE FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT RECHARGEABLE FLASHLIGHT AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,931 hrs · 16,320 cycles

FOR FLIGHT 3724 THE CREW REPORTED THE EXTERIOR EMERGENCY LIGHTS DEAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. NR 1 EMERGENCY LIGHT BATTERY PACK INOPERABLE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK IAW WORK CARD 33-002. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,931 hrs · 16,320 cycles

FOR FLIGHT 3724 THE CREW REPORTED THE EXTERIOR EMERGENCY LIGHTS DEAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. NR 4 EMERGENCY LIGHT BATTERY PACK INOPERABLE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK IAW WORK CARD 33-002. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,931 hrs · 16,320 cycles

FOR FLIGHT 3724 THE CREW REPORTED THE EXTERIOR EMERGENCY LIGHTS DEAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. NR 2 EMERGENCY LIGHT BATTERY PACK INOPERABLE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK IAW WORK CARD 33-002. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,931 hrs · 16,320 cycles

FOR FLIGHT 3724 THE CREW REPORTED THE EXTERIOR EMERGENCY LIGHTS DEAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. NR 3 EMERGENCY LIGHT BATTERY PACK INOPERABLE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY PACK IAW WORK CARD 33-002. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,563 hrs · 16,057 cycles

FLIGHT 3761, THE CREW REPORTED THAT AFTER LANDING, WERE ASKED TO SHUTDOWN THE RIGHT ENGINE SO GROUND CREW COULD INSPECT ACFT. WHEN CLEARED TO TAXI THE CREW STARTED THE RIGHT ENGINE FOR BETTER CONTROL. AFTER IT STABILIZED THE CREW SMELLED SOMETHING ABNORMAL. THE CREW SHUT DOWN ENGINE IMMEDIATELY IN CASE OF FOD. NO START ABNORMALITIES JUST AN ODD ODOR. AIRCRAFT REMOVED FROM SERVICE. GROUND RAN ACFT IAW MM 72-00-00. OPERATED BLEED SYSTEM IAW AMM 36-10-00, NO DEFECTS NOTED. REMOVED AND REPLACED NR 3 MAIN TIRE ASSEMBLY, NR 1 MAIN LANDING GEAR WHEEL ASSEMBLY AND THE NR 4 WHEEL ASSEMBLY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — FAILED (MLG) · airframe 22,563 hrs · 16,057 cycles

FLIGHT 3761, AT ROTATION, A STRONG VIBRATION STARTED. CONTINUED TAKEOFF WITH NO OTHER ABNORMALITIES. ALL ENGINE PARAMETERS NORMAL. DURING CLIMB, CREW ASCERTAINED THAT TIRE MATERIAL WAS FOUND ON THE RUNWAY AFTER TAKEOFF. CONTINUED TO MONITOR ALL ENGINE AND SYSTEM PARAMETERS AND LANDED AT DESTINATION. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ON INSPECTION, NR 3 MAIN WHEEL WAS DAMAGED BUT STILL INFLATED. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AIRCRAFT AND DETERMINED VIBRATION CAUSED BY TREAD LOSS TO NR 3 MAIN LANDING GEAR TIRE. REMOVED AND REPLACED NR 3 MAIN TIRE ASSEMBLY IAW AEAI WORK CARD 32-002. NR 1 TIRE ASSEMBLY WORN AS PER MANAGEMENT. REMOVED AND REPLACED NR 1 MAIN LANDING GEAR WHEEL ASSEMBLY IAW CRJ-700 MTX W/C 32-002. REMOVED AND REPLACED THE NR 4 WHEEL ASSY IAW CRJ-700 MTX W/C 32-002. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — INOPERATIVE (LT BLEED) · airframe 22,215 hrs · 15,826 cycles

FLT 9804, CREW REPORTED, CLIMBING THRU 31,600 FT, RECEIVED A LT BLEED DUCT WARNING MESSAGE. BOTH PACKS SHUTOFF. PERFORMED AN EMERGENCY DESCENT TO 10,000 FT. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FWD CLAMP IAW MM 21-53-14. OPERATED BOTH PACKS FOR 90 MINUTES AND COULD NOT DUPLICATE BLEED LEAK. REMOVED AND REPLACED THE VENTILATED TEMPERATURE SENSOR (FWD) IAW AMM 21-61-06. OPERATED PACK ON AUTO IAW AMM 21-51-00. OPS CHECKED GOOD. REMOVED AND REPLACED NR 2 PACK DISCHARGE PRESSURE SENSOR IAW AMM 21-51-24. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 22,214 hrs · 15,825 cycles

FLIGHT 4639 - DURING THE CLIMB AT FLIGHT LEVEL 280, RECEIVED A LT BLEED DUCT WARNING MESSAGE. EMERGENCY CHECKLIST EXECUTED. LT BLEED DUCT WARNING MESSAGE WENT OUT. THEN RECEIVED A CABIN ALTITUDE WARNING MESSAGE AT APPROXIMATELY FL 310. CABIN ALTITUDE ROCKETED FROM APPROXIMATELY 9900 TO IN EXCESS OF FL 190 CABIN ALTITUDE PAX OXYGEN ILLUMINATED AND MASKS DEPLOYED. ALL EMERGENCY, ABNORMAL AND NORMAL CHECKLIST FOLLOWED. NO STRUCTURAL INTEGRITY COMPROMISE NOTED. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CPC NR 2 IAW MM 21-31-04. PERFORMED OPERATIONAL CHECK OF CABIN PRESSURE SYSTEM IAW 21-31-00. NO EICAS OR MDC MESSAGES NOTED. AIRCRAFT OK FOR SERVICE FOR FERRY FLIGHT.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 21,821 hrs · 15,581 cycles

FLIGHT 3682, CREW REPORTED OVERHEAD EMERGENCY LIGHT ROW 5 WAS INOPERATIVE. TROUBLESHOT SYSTEM PER WM 33-50-04, FOUND BROKEN CONNECTOR J357-1 SPLICE WIRE IAW EEC SPM 20-16-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,924 hrs · 15,050 cycles

ON FLIGHT 3824 THE CREW REPORTED THE RIGHT LOWER OVERWING EMERGENCY EXIT "EXIT" LIGHT HAS 2 BULBS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT LOWER OVERWING EMERGENCY EXIT "EXIT" LIGHT BULBS IAW CRJ 700 AMM 33-51-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 20,765 hrs · 14,960 cycles

ON FLIGHT 3753 THE CREW REPORTED THE EMERGENCY LIGHT STRIP ON RIGHT SIDE OF INTERIOR SERVICE DOOR IS PEELING OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESECURED EMERGENCY LIGHT STRIP ON RIGHT SIDE OF SERVICE DOOR AS REQUIRED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,111 hrs · 14,515 cycles

DURING MAINTENANCE BASE VISIT FOUND BOTH HALVES OF BEAM AT FRAME 280 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH HALVES AT BEAM FRAME 280 IAW AE EO#CR-53MR-219. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,111 hrs · 14,515 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT COCKPIT BULKHEAD WEBS CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AND RIGHT COCKPIT LOWER BULKHEAD WEBS IAW EO#CR-53MR-174. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,038 hrs · 12,530 cycles

ON FLIGHT 3478 THE CREW REPORTED THE SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND TO BE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR EMERGENCY EXIT LIGHTED SIGN ASSEMBLY IAW CRJ-700 AMM 33-51-05. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — BROKEN (CABIN) · airframe 15,994 hrs · 11,806 cycles

DURING THE PREFLIGHT FOR FLIGHT 4128 THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR WAS NOT ATTACHED OR FELL OFF THE BRACKET. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY SIGN ABOVE THE SERVICE DOOR IAW CRJ-700 MM 33-51-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CRACKED (COWL) · airframe 15,171 hrs · 11,146 cycles

DURING MAINTENANCE INSPECTION FOUND THE OUTBOARD TRANS COWL EXTRUSION CRACKED. AIRCRAFT REMOVED FROM SERVICE.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 1,517 hrs · 11,146 cycles

DURING MAINTENANCE INSPECTION FOUND THE OUTBOARD TRANSCOWL EXTRUSION CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT ENGINE LOWER OUTBOARD CASCADE IAW CRJ 700 AMM 78-34-01. ALSO PERFORMED A FUNCTIONAL CHECK OF THE THRUST REVERSERS, CHECKED GOOD IAW CRJ 700 AMM TASK 78-30-00-720-801. AIRCRAFT RETURNED TO SERVICE.

Part: FAIRING — CRACKED (LT OVERWING) · airframe 15,171 hrs · 11,146 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OVERWING FAIRING 172CL CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED LEFT OVERWING FAIRING 171CL IAW CRJ 700 ETA CR-5300-088. RESTORED PROTECTIVE FINISH IAW SRM 51-25-01, 51-25-06 AND ETN GN-51-002R3. AIRCRAFT RETURNED TO SERVICE.

Part: FAIRING — CRACKED (RT OVERWING) · airframe 15,171 hrs · 11,146 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT OVERWING FAIRING 172CR CRACKED. AIRCRAFT REMOVED FROM SERVICE.

Part: FAIRING — CRACKED (RT OVERWING) · airframe 15,171 hrs · 11,146 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT OVERWING FAIRING 172CR CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED RIGHT OVERWING FAIRING 172CR IAW CRJ 700 ETA CR-5300-088. AIRCRAFT RETURNED TO SERVICE.

Part: FAIRING — CRACKED (LT OVERWING) · airframe 15,171 hrs · 11,146 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OVERWING FAIRING 172CL CRACKED. AIRCRAFT REMOVED FROM SERVICE.

Part: STAND OFF — CRACKED (THRUST REVERSER) · airframe 15,171 hrs · 11,146 cycles

DURING MAINTENANCE INSPECTION FOUND THE INBOARD STANDOFF CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INBOARD STANDOFF IAW ENT CR-54-015RT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,171 hrs · 11,146 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT SIDE SERVICE DOOR SILL TO BE CORRODED AT FS 319. AIRCRAFT REMOVED FROM SERVICE. REPAIRED RIGHT SERVICE DOOR SILL AT FS 319 IAW EO CR-53MR-171. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FS 319) · airframe 15,171 hrs · 11,146 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT SERVICE DOOR TO BE CORRODED AT FS 319. THE AIRCRAFT HAS BEEN REMOVED FROM SERVICE.

Part: VALVE — MALFUNCTIONED (NR 1) · airframe 10,891 hrs · 7,903 cycles

CREW REPORTED THAT AUTO PRESS HALF FAIL IN CLIMB. REMOVED AND REPLACED NUMBER 1 SAFETY VALVE IAW AMM 21-32-03. OPS CHECK IAW AMM 21-32-03. NO DEFECTS NOTED PRESSURIZED AIRCRAFT IAW AMM 21-31-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: OVERHEAT SENSOR — FAILED (ZONE 700) · airframe 9,792 hrs · 7,117 cycles

"SUP" BRAKE OVERTEMP MESSAGE IN FLIGHT, DECLARED EMERGENCY. DIVERTED TO BNA. REMOVED AND REPLACED RIGHT OUTBOARD BRAKE TEMPERATURE SENSOR IAW CRJ AMM 32-46-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 9,417 hrs · 6,861 cycles

EMERGENCY LIGHTS STATUS MESSAGE CYCLING ON AND OFF WITH LIGHTS FOLLOWING. REMOVED AND REPLACED RELAY K135 ON PCB NR 5 OF JB11 IAW CRJ AMM 24-06-11. OPERATIONAL CHECK GOOD.

Part: ENGINE — VIBRATION (NR 2) · airframe 8,378 hrs · 6,084 cycles

ENGINE 2 VIBRATION INDICATION WENT TO 2.2 WHILE IN CRUISE, REDUCED THROTTLES AND VIBRATION LOWERED AND THEN RETURNED TO 2.2.INDICATION, DIVERTED TO CMH. COMPLIED WITH ENGINEERING TECHNICAL NOTICE CR-72-002R1. PERFORMED FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — DIRTY (LAVATORY)

AFT LAVATORY SMOKE WARNING ILLUMINATED AFTER TAKEOFF. FUMES PRESENT THROUGHOUT AIRCRAFT. REPLACED LT AND RT RECIRCULATION FAN FILTERS. REPLACED LAVATORY SMOKE DETECTOR. GROUND RAN AIRCRAFT AT SEVERAL POWER SETTINGS WITH NO LAVATORY SMOKE DETECTED OR SMELL NOTED. ACCOMPLISHED SATISFACTORY FUNCTIONAL CHECK FLIGHT. AIRCRAFT RETURNED TO SERVICE. LAVATORY RECIRCULATION FILTER PN CA01131B UNSERIALIZED. (K)

Part: COMPUTER — FAILED (FUEL SYS)

NOTIFIED BY DISPATCH, AIRCRAFT DIVERSION, DUE TO FUEL CHANNEL 1 FAIL EICAS MESSAGE. CREW FOLLOWED AOM PROCEDURES AND LANDED. RAI FQGC OPS CHECK GOOD. (K)

Part: SENSOR — INOPERATIVE (HORIZONTAL STAB)

CREW RECEIVED STABILIZER FAULT STATUS MESSAGE IN CRUISE. REPLACED HORIZONTAL STABILIZER ACTUATOR POSITION SENSOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: APU — LEAKING (APU BAY)

ON TAXI TO THE GATE WITH PACKS AND APU ON SMOKE ENTERED THE CABIN AND CREW RECEIVED LAVATORY SMOKE WARNING. FOUND APU LEAKING OIL INTO THE BLEED SYSTEM REPALCED APU. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K)

Part: RELAY — INOPERATIVE (EMERGENCY LIGHT)

CLE - FLT 4341 - MAINTENANCE FOUND THAT ALL EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED RELAY K135. OPERATIONAL CHECK GOOD. (M)