N354CA

Part: PRESSURE SWITCH — INOPERATIVE (OIL SYSTEM) · airframe 45,379 hrs · 35,554 cycles

AT CRUISE R OIL PRESS WARNING ILLUMINATED ALONG WITH UNCOMMANDED RUDDER MOVEMENTS TO THE LEFT AND RIGHT. OIL PRESSURE ON RIGHT ENGINE SHOWED 64 AND LEFT WAS 69. DISCONNECTED A/P AND RAN QRH FOR R OIL PRESS. AFTER RIGHT ENGINE WAS AT IDLE R OIL PRESS LIGHT CAME BACK ON WHICH LED TO RIGHT ENGINE SHUTDOWN PER QRH. AFTER SECURING RIGHT ENGINE CONTINUED TO HAVE UNCOMMANDED RUDDER MOVEMENTS. R/R RH ENG OIL PRESSURE SWITCH IAW AMM 79-31-03 OPS CHECK GOOD. PERFORMED OPS CHECK OF RUDDER CONTROL SYSTEM IAW AMM 27-21-00. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: ADC — INOPERATIVE (NR 1) · airframe 42,575 hrs · 32,903 cycles

#1 ADC FAILURE WITH CORRESPONDING UNRELIABLE AIRSPEED INDICATION AND MULTIPLE EICAS MESSAGES. AIR RETURN TO ATL. R/R #1 ADC IAW CRJ 700 AMM 34-13-01. OPS TEST GOOD, LEAK TEST GOOD. PN OFF/ 822-0472-636, SN OFF/ 24GFK, PN ON /822-0372-436, SN ON/ 10HLG

Part: FRAME — CRACKED · airframe 42,509 hrs · 32,836 cycles

L/H FWD OVERWING EXIT DOOR (S/N SBO532) TOP EDGE MEMBER IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR EA CRJ952-14342 REV.IR, DATED 08/26/2022

Part: ANGLE — CORRODED · airframe 42,509 hrs · 32,836 cycles

FRAME (ANGLE) CORRODED AT FS 265.00 BETWEEN STGR 26L AND 27 REMOVED AND REPLACED ANGLE I.A.W. BOMBARDIER CRJ900 SRM 51-42-06-001-001-A01.

Part: FRAME — NONE · airframe 42,509 hrs · 32,836 cycles

L/H AFT OVERWING EXIT (S/N SBO539) TOP EDGE MEMBER IS CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-14340 REV IR DATED 8/26/22

Part: BATTERY — INOPERATIVE · airframe 42,509 hrs · 32,836 cycles

RH OVER WING EMERGENCY LIGHT OUT (AFT OF OVERWING EMERGENCY EXIT DOOR) R&R EMERGENCY BATTERY PACK PS37 IAW AMM 33-51-04. OPS CHECKS GOOD. P/N OFF: 2013-1A, S/N OFF: 119615, P/N ON: 2013-1ASMI, S/N ON: 15022

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

FS280-FS319 STR21R CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED CORRODED STR21R, FROM FS280-FS319 PER CRJ700 SRM 51-42-06.

Part: FLOORBEAM — CORRODED · airframe 42,509 hrs · 32,836 cycles

AFT CARGO FLOOR BEAM CAP AT RBL9.00 FROM FS1041 TO FS1088 HAS SURFACE CORROSION. REMOVED AND REPLACED CORRODED FLOOR BEAM CAP AT RBL9.00 FROM FS976-FS1088 PER CRJ700 SRM 53-00-41.

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

FS379 STR24L HAS TWO SPOTS OF CORROSION REMOVED CORROSION @ FS379 STRG24L. FOUND TO BE OUT OF LIMITS DUE TO NO DAMAGE ALLOWED. CUT OUT DAMAGED PORTION OF STRG24L. FABRICATED NEW ANGLE REPAIR AND INSTALLED. RESTORED FINISH ON WORKED SURFACES. PER. CRJ700 SRM 53-21-03-101-006-A01, 51-42-21-001-001-A01, 53-00-03-201-001-A01, 51-21-11, 51-25-06.

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

FS333-FS349, STR26L STRINGER CORRODED. REMOVED AND REPLACED CORRODED STRINGER STR26L,FS333-FS349 IAW CRJ700 SRM 51-42-06.

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

STGR 21R AT FS 340.00 TO FS 379.00 CORRODED REMOVED CORRODED SECTION OF STRINGER 21R AT FS 340.00 TO FS 379.00 AND REPLACED WITH NEW SECTION OF STRINGER PER CRJ700 SRM 51-42-21 AND SRM 51-42-06

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

CORROSION FOUND ON STGR 19R AT FS 485.00 REMOVED DAMAGED SECTION OF STRINGER 19R FROM FS 479.00 TO FS 491.00 AND REPLACED WITH NEW SECTION OF STRINGER PER CRJ700 SRM 53-00-03

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

STGR 21R FROM FS 394.00 TO FS 477.00 CORRODED REMOVED CORRODED SECTION OF STGR 21R FROM FS 394.00 TO FS 477.00 AND REPLACED WITH NEW SECTION PER CRJ700 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01.

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

CORROSION ON STR19R SECTION FROM FS280 TO FS310. REMOVED AND REPLACED CORRODED STR19R SECTION FROM FS280-FS310 IAW CRJ700 SRM 51-42-06 AND SRM 51-42-21.

Part: SEAT TRACK — CORRODED · airframe 42,509 hrs · 32,836 cycles

SEAT TRACK AT FS 379.00 LBL 9.00 CORRODED REMOVED CORRODED SEAT TRACK AT FS 379.00 LBL 9.00 AND REPLACED WITH NEW SEAT TRACK PER CRJ700 AMM 53-00-49

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

STGR 19R AT FS 476.00 CORRODED REMOVED CORRODED SECTION OF STGR 19R AT FS 421.00 TO FS 479.00 AND REPLACED WITH STRINGER SECTION PER CRJ700 SRM 53-00-03

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

STGR 18R AT FS 437.00 TO FS 453.00 CORRODED REMOVED CORRODED SECTION OF STRINGER 18R AT FS 437.00 TO FS 453.00 AND REPLACED WITH NEW SECTION OF STRINGER PER CRJ700 SRM 53-21-03-101-007-A01

Part: INTERCOSTAL — CORRODED · airframe 42,509 hrs · 32,836 cycles

INTERCOSTAL AT STGR 27(LH) AFT OF AVIONICS BAY DOOR AT FS 364.00 TO FS 379.00 CORRODED REMOVED CORRODED INTERCOSTAL AT STGR 27(LH) AFT OF AVIONICS BAY DOOR AT FS 364.00 TO FS 379.00 AND REPLACED WITH NEW INTERCOSTAL PER CRJ700 SRM 51-42-06

Part: FLOOR SUPPORT — CORRODED · airframe 42,509 hrs · 32,836 cycles

FLOOR BEAM AT FS 1004.00 TO FS 1088.00 LBL 27.00 CORRODED REMOVED CORRODED FLOOR BEAM AND REPLACED WITH NEW FLOOR BEAM

Part: SEAT TRACK — CORRODED · airframe 42,509 hrs · 32,836 cycles

SIDE SEAT RAIL AT FS 711.00 TO FS 761.00 RH SIDE CORRODED REMOVED SIDE SEAT RAIL AT FS 711.00 TO FS 761.00 RH SIDE AND REPLACED WITH NEW SEAT RAIL PER CRJ700 SRM 53-00-49

Part: SEAT TRACK — CORRODED · airframe 42,509 hrs · 32,836 cycles

SIDE SEAT RAIL AT FS 711.00 TO FS 761.00 LH SIDE CORRODED REMOVED SIDE SEAT RAIL AT FS 711.00 TO FS 761.00 LH SIDE AND REPLACED WITH NEW SEAT RAIL PER CRJ700 SRM 53-00-49

Part: INTERCOSTAL — CORRODED · airframe 42,509 hrs · 32,836 cycles

INTERCOSTAL CORRODED FS 364.00 STGR 26L REMOVED CORRODED INTERCOSTAL AT FS 364.00 STGR 26L AND REPLACED WITH NEW INTERCOSTAL PER CRJ700 SRM 51-42-06

Part: INTERCOSTAL — CORRODED · airframe 42,509 hrs · 32,836 cycles

INTERCOSTAL CORRODED FS 364.00 STGR 26R REMOVED CORRODED INTERCOSTAL AT FS 364.00 STGR 26R AND REPLACED WITH NEW INTERCOSTAL PER CRJ700 SRM 51-42-06

Part: STRINGER — CORRODED · airframe 42,509 hrs · 32,836 cycles

STGR 18R AT FS 421.00 TO 437.00 CORRODED REPLACED STGR 18R FROM FS 421.00 TO FS 475.00 PER CRJ700 SRM 51-42-06

Part: FRAME — CORRODED · airframe 42,509 hrs · 32,836 cycles

FRAME SECTION AT FS 565.00 STGR 17L TO STGR 18L CORRODED REMOVED CORRODED FRAME SECTION AT FS 565.00 STGR 17L TO STGR 18L AND REPLACED WITH NEW FRAME SECTION PER CRJ700 SRM 51-42-06-001-001-A01

Part: SEAT TRACK — CORRODED · airframe 42,509 hrs · 32,836 cycles

MAIN CABIN SIDE SEAT TRACK AT FS 785.00 TO FS 855.00 CORRODED CA REMOVED CORRODED SIDE SEAT TRACK AT FS 785.00 TO FS 855.00 AND REPLACED WITH SIDE SEAT TRACK PER CRJ700 SRM 53-41-49 AND AMM 53-00-49

Part: ANGLE — CORRODED · airframe 42,509 hrs · 32,836 cycles

FWD CARGO DOOR CUTOUT AFT UPPER CORNER AT FS 581.00 SIGNS OF CORROSION REMOVED CORROSION ON FWD CARGO DOOR CUTOUT AFT UPPER CORNER PER CRJ700 SRM 51-21-06-001-001-A01

Part: SEAT TRACK — CORRODED · airframe 42,509 hrs · 32,836 cycles

MAIN CABIN SIDE SEAT TRACK AT FS 785.00 TO FS 855.00 CORRODED REMOVED AND REPLACED SIDE SEAT TRACK AT FS 785.00 TO 855.00 PER CRJ700 AMM 53-00-49

Part: INTERCOSTAL — CORRODED · airframe 42,509 hrs · 32,836 cycles

INTERCOSTAL AT STGR 27 FS 364.00 TO 379.00 CORRODED REMOVED CORRODED INTERCOSTAL AT STGR 27 FS 364.00 TO FS 379.00 AND REPLACED WITH NEW INTERCOSTAL PER CRJ700 SRM 51-42-06.

Part: BRACKET — CRACKED · airframe 42,509 hrs · 32,836 cycles

AFT CARGO, AFT LOWER DOOR TRACK SUPPORT HAS CRACK. PNS: MM670-B5552-005 & CC670-58814-1 REMOVED AND REPLACED AFT LOWER DOOR TRACK IAW CRJ700 SRM51-42-06.

Part: BRACKET — CRACKED (FS 1088) · airframe 42,509 hrs · 32,836 cycles

FS 1088.00 STGR 8R SUPPORT BRACKET CRACKED REMOVED CRACKED SUPPORT BRACKET AT FS 1088.00 STGR 8R AND REPLACED WITH NEW SUPPORT BRACKET PER CRJ700 SRM 51-42-06.

Part: NONE — CRACKED · airframe 42,509 hrs · 32,836 cycles

A 1.00 INCH CRACK WAS FOUND IN THE FLOOR BEAM SUPPORT, ADJACENT TO AN EXISTING FASTENER, AT FS 280.00, WL 72.00, LBL 13.50. REPAIRED PER REO 670-53-11-1797.

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 38,104 hrs · 28,656 cycles

AFT EMERGENCY FLOODLIGHT INOP. R&R AFT EMERGANCY EXIT LIGHT IAW CRJ700 AMM 33-51-15. OPS CHECK GOOD.

Part: SEAL — DETACHED (PAX DOOR) · airframe 38,060 hrs · 28,615 cycles

MAIN CABIN DOOR SEAL DETACHED. R&R PAX DOOR SEAL IAW CRJ700 AMM 52-11-07. LEAK CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,126 hrs · 27,755 cycles

CEILING EMERGENCY LIGHT WAS INOPERATIVE AT ROW 6. R & R THE BULB IAW AMM 33-51-09, OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 37,058 hrs · 27,682 cycles

EXIT ROW EMERGENCY LIGHT INOPERATIVE. CONNECTED THE CONNECTOR AND OPS CHECKED GOOD IAW AMM- 33-57-01.

Part: BEAM — CRACKED (PAX DOOR) · airframe 369,213 hrs · 27,568 cycles

PASSENGER DOOR GAS SPRING BEAM IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED GAS SPRING BEAM(PN: 601R318011-1) IAW SRM 51-42-06, 51-40-11, 51-25-16, AND AMM 52-11-17.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 369,213 hrs · 27,568 cycles

PASSENGER DOOR VENT FLAP INTERNAL SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED ANGLE SUPPORT BRACKET(PN: 601R318072-1) IAW SRM 51-42-06, 51-40-11, AND 51-25-16.

Part: FLAP — DENTED (LT WING) · airframe 369,213 hrs · 27,568 cycles

LT I/B FLAP HAS TWO DENTS. REPAIRED DENTS BY FABRICATING AND INSTALLING REPAIR PARTS IAW REO 670-57-52-412 DATED 20 APR 2018.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 36,921 hrs · 27,568 cycles

LEFT SIDE BS 280 FLOORBEAM FOUND CRACKED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-11-41, 51-25-16, 51-21-11, 51-40-11, 51-25-06, 51-42-21, 51-42-13, AMM 20-70-00, AND NDT MANUAL PART 1 51-20-006.

Part: BRACKET — CRACKED (E/E BAY) · airframe 36,921 hrs · 27,568 cycles

AFT EQUIPMENT BAY, LT WING ANTI-ICE DUCT MOUNTING BRACKET CRACKED. REMOVED AND REPLACED THE MOUNTING BRACKET IAW SRM 51-42-21.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 36,921 hrs · 27,568 cycles

LEFT INBD INTERCOSTAL IN THE FWD AVIONICS BAY BETWEEN BS 349 AND 364, HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND SRM 51-42-21.

Part: BRACKET — CRACKED (LT LE SLAT) · airframe 36,921 hrs · 27,568 cycles

LEFT SLAT 1 - 3 SLAT BOX BRACKET CRACKED. CUT AND REMOVED THE DAMAGED AREA, INSTALLED A FABRICATED PART IAW REO 670-57-42-577 REV -, SRM 51-23-00, 51-26-00, AND NDTM PART 01, 51-20-006.

Part: INTERCOSTAL — CORRODED (BS 394-409) · airframe 36,921 hrs · 27,568 cycles

FWD AVIONICS BAY, LEFT INBD INTERCOSTAL, BS 394 - 409 HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.

Part: BRACKET — CRACKED (RT LE SLAT) · airframe 36,921 hrs · 27,568 cycles

RIGHT SLAT 1 - 3 SLAT BOX BRACKET CRACKED. CUT AND REMOVED THE DAMAGED AREA, INSTALLED A FABRICATED PART IAW REO 670-57-42-577, REV -, SRM 51-23-00, AND NDTM PART 01 51-20-006.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 36,921 hrs · 27,568 cycles

AFT CARGO DOOR HANDLE HOUSING IS CRACKED AT AFT BOTTOM CORNER. REMOVED AND REPLACED THE CARGO DOOR HANDLE HOUSING IAW SRM 51-40-11, AND AMM 52-31-03.

Part: RIB — CRACKED (LT WING) · airframe 36,921 hrs · 27,568 cycles

LEFT WING PARTIAL RIB AT WS 58.41 IS CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-42-06, 51-42-13, 51-42-15, 51-40-11, 51-42-21, AND 51-25-06.

Part: STOP FITTING — CRACKED (PAX DOOR) · airframe 36,921 hrs · 27,568 cycles

PASSENGER DOOR UPPER FWD STOP FITTING IS CRACKED. REMOVED AND REPLACED THE STOP FITTING IAW SRM 51-42-21.

Part: WEB — CRACKED (E/E BAY) · airframe 36,921 hrs · 27,568 cycles

RIGHT FLOOR WEB IN FWD EQUIPMENT BAY IS CRACKED. REPIARED THE WEB IAW REO 670-53-11-509, REV D, REO 670-53-11-1386, SRM 51-42-06, AND AMM 20-70-00.

Part: SEAT TRACK — CORRODED (BS 485-677) · airframe 36,921 hrs · 27,568 cycles

RIGHT FLOOR SEAT TRACK, BS 485 - 677 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: SEAT TRACK — CORRODED (BS 485-677) · airframe 36,921 hrs · 27,568 cycles

LEFT SEAT TRACK AT BS 485 - 677 HAVE SIGNS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Part: INTERCOSTAL — CORRODED (BS 319.7-349) · airframe 36,921 hrs · 27,568 cycles

INTERCOSTAL AT STRINGER 20R BETWEEEN BS 319.70 AND 349 FOUND CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 53-00-00, 51-42-06, 51-42-21, 51-40-11, 51-21-11, AND AMM 53-21-23.

Part: WEB — CRACKED (FUSELAGE) · airframe 36,921 hrs · 27,568 cycles

FORWARD EQUIPMENT COMPARTMENT LT SIDE WEB CRACKED. REPAIRED FORWARD EQUIPMENT COMPARTMENT WEB LT SIDE IAW REO 670-53-11-509 REV D DATED 2016-06-29 AND AMM 20-70-00, SRM 51-42-06, NDTM PART 1 51-20-006.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 36,921 hrs · 27,568 cycles

EXTERNAL WING TO FUSELAGE SUPPORT STRUCTURE ANGLE IS CRACKED AT FS 909.00. TRIMMED FWD DIAPHRAGM AND ANGLE TO COMPLETELY ELIMINATE CRACK, FABRICATED AND VERIFIED MATERIALS AND INSTALLED REPAIR PARTS IAW REO 670-53-82-478 REV A DATED 2014-11-12.

Part: TRIPLER — GOUGED (BS 977) · airframe 36,921 hrs · 27,568 cycles

TRIPLER AT BS 977, STRINGER 27, GOUGED. REMOVED AND REPLACED THE TRIPLER IAW REO 670-53-00-290, REV D, AND SRM 51-42-21.

Part: ENGINE — FAILED (LEFT) · airframe 35,624 hrs · 26,384 cycles

LEFT ENGINE FAILED IN FLIGHT.

Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR) · airframe 35,619 hrs · 26,379 cycles

PAX DOOR OUTER HANDLE CAUTION. GAPPED AND SECURED THE PAX DOOR OUTER HANDLE PROXIMITY SWITCH IAW AMM 52-70-04.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 34,782 hrs · 25,653 cycles

PAX DOOR WARNING MESSAGE. PERORMED OPS CHECK OF THE PAX DOOR INDICATION SYS NO FAULTS FOUND AT THIS TIME IAW AMM 52-70-00

Part: DOOR — BINDING (MAIN PAX) · airframe 34,282 hrs · 25,248 cycles

CREW WAS UNABLE TO OPEN PASSENGER DOOR. INSPECTED DOOR TO ENSURE ALL WITNESS MARKS ARE ALIGNED,

Part: HOOK AND LOOP — DAMAGED (ESCAPE ROPE) · airframe 34,181 hrs · 25,171 cycles

ESCAPE ROPE D-RING ACCESS PANEL WILL NOT OPEN ON LEFT EMERGENCY EXIT WINDOW. SECURED THE HOOK AND LOOP FOR THE D RING ACCESS PANEL IAW AMM 25-63-04. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,757 hrs · 24,839 cycles

MID-CABIN EMERGENCY LIGHT HAS BURNED OUT BULBS. RELAMPED LIGHT IAW AMM 33-51-05, OPS CHECKS GOOD AT THIS TIME

Part: ACTUATOR — LEAKING (NR 2 ENGINE) · airframe 33,638 hrs · 24,743 cycles

NR 2 ENGINE FUEL LEAK. R & R PRIMARY VG ACTUATOR IAW AMM 75-30-01, LEAK AND OPS CHECK GOOD.

Part: CAM — LACK OF LUBE (PAX DOOR) · airframe 33,477 hrs · 24,633 cycles

OPS REPORTED PAX DOOR HARD TO CLOSE. CLEANED AND LUBED TOP FWD LOCKING CAM IAW AMM 12-20-52. OPS CHECKED IAW AMM 52-11-00 OPS CHECKED GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 33,388 hrs · 24,567 cycles

MAIN DOOR UNABLE TO OPEN FROM THE OUTSIDE. INSPECTED AND PERFORMED OPS TEST OF MAIN DOOR IAW AMM 52-11-00,OPS CHECKED GOOD AT THIS TIME.

Part: CAM — LACK OF LUBE (PAX DOOR) · airframe 33,384 hrs · 24,561 cycles

PAX DOOR HARD TO CLOSE. CLEANED AND LUBED TOP FWD LOCKING CAM IAW AMM 12-20-52. OPS CHECKED PAX DOOR IAW AMM 52-11-00, OPS CHECKED GOOD AT THIS TIME

Part: FRAME — CORRODED (BS 364) · airframe 33,112 hrs · 24,368 cycles

FRAME BS 364 CORRODED, BETWEEN STRINGER 24L & 24R. ACCOMPLISHED PERMANENT REPAIR TO FRAME 364 BY REMOVING CORRODED SECTION, PERFORMING NDT INSPECTIONS, FABRICATING REPAIR PARTS & INSTALLING THEM IAW REOS 670-53-21-687 REV DATED 2012 08 03, 670-53-21-1305 REV A DATED 2016 06 01 & SRMS 51-51-02, 51-42-06, 51-42-21, 53-21-33, TR-51-0056 & 51-23-00. NDT PERFORMED BY W2XR853X, PO 134624, WO A16-1315 & PO134463 & WO A16-1299.

Part: FITTING — CORRODED (PAX DOOR) · airframe 33,112 hrs · 24,368 cycles

PASSENGER DOOR FWD HANDLE ARM CUP HAS EVIDENCE OF CORROSION. R & R ARM CUP IAW SRM 51-42-06, 51-42-21, 51-21-11, 51-25-16.

Part: CAP — CORRODED (PAX DOOR) · airframe 33,112 hrs · 24,368 cycles

PASSENGER DOOR ENTRY MIDCAP CORRODED AT FASTENER HOLES. REPLACED PAX DOOR MIDCAP IAW SRMS 51-41-02, 51-41-06, 51-42-21, 51-40-11, 51-23-00, TR 51-0056, 51-25-16, 51-21-11 & AMM 52-70-04.

Part: TRIPLER — GOUGED (FUSELAGE) · airframe 33,112 hrs · 24,368 cycles

REPAIR TRIPLER AT FS 977 HAS TWO GOUGES. REPLACED DAMAGED TRIPLER IAW REO 670-53-00-290 REV D DATE 10 SEP 2015. WO 80406, WC 1115.

Part: HINGE — GOUGED (PAX DOOR) · airframe 33,112 hrs · 24,368 cycles

PASSENGER DOOR HINGE LOBES 11, 25, & 27 HAVE GOUGES. REPAIRED HINGE LOBES IAW REO 670-52-11-511 TYPE 1 REV A DATED 06 MAR 2013. WO 80406 & WC 8069.

Part: COLLAR — MISSING (DOOR FRAME) · airframe 33,112 hrs · 24,368 cycles

PASSENGER DOOR SURROUND MISSING 1 EACH LOCK FASTENER COLLAR AT FS 333 & WL 72. INSTALLED LOCK FASTENER COLLAR IAW SRM 51-42-21. WO 80406 & WC 8078

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,112 hrs · 24,368 cycles

RIGHT FWD FLOOR SEAT TRACK SEGMENT HAS SIGNS OF CORROSION. R & R SEAT TRACK IAW SRM 53-00-49. WO 80406 WC 2162.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 32,985 hrs · 24,279 cycles

PASSENGER DOOR RED EICAS MSG. PERFORMED GVI OF ACFT TO ENSURE IT IS SAFE FOR A ONE TIME FERRY FLIGHT. ENSURED WHEN DOOR WAS CLOSED & LOCKED THAT ALL GREEN MARKS ARE LINED UP.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 32,982 hrs · 24,278 cycles

FLOORBEAM AT LBL 9.00, BS 1031 CORRORED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,235 hrs · 23,701 cycles

FRAME AT STATION 319.00, STRINGER 0 IS CRACKED. REPAIRED FRAME AT STATION 319.00, STRINGER 0, BY FABRICATING REPAIR PARTS & INSTALLING IAW REO 670-53-21-1248 DATED 05 DEC 2015, & REO 670-53-21-1248, DATED 05 DEC 2015.

Part: STIFFENER — CRACKED (BS 202 BULKHEAD) · airframe 32,191 hrs · 23,668 cycles

FWD SIDE OF BULKHEAD AT FS 202.75, FOUND INDICATION ON TOP OF STIFFNER AT LBL30.0 APPROXIMATELY 0.125" LONG. STIFFNER FAILED NDT INSPECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,177 hrs · 23,656 cycles

EMERGENCY LIGHT OUT AT ROW 9. DEFERRED CEILING LIGHT AT ROW 9 IAW MEL 33-51-01B CAT C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,169 hrs · 23,651 cycles

EMERGENCY LIGHT OUT AT ROW 9. DEFERRED EMER LIGHT IAW MEL 33-51-01B CAT C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,901 hrs · 23,445 cycles

CEILING LIGHT EMER OVERHEAD BIN FLOODLIGHT INOPERATIVE AT ROW 17. DEFERRED IAW MEL 33-51-01B.

Part: DOOR — UNKNOWN (CABIN) · airframe 31,826 hrs · 23,388 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. VERIFIED PAX DOOR CLOSED & LOCKED PRIOR TO FLIGHT. EVALUATED & INSPECTED ACFT, FOUND TO BE SAFE FOR A ONE TIME FERRY FLIGHT.

Part: HANDLE — BROKEN (SERVICE DOOR) · airframe 31,209 hrs · 22,926 cycles

SERVICE DOOR OUTER HANDLE BROKE OFF. PERFORMED INSPECTION OF ACFT, VERIFIED SERVICE DOOR CLOSED & LATCHED. NO SERVICE DOOR INDICATIONS NOTED IAW AMM 52-10-00. ACFT GOOD FOR ONE TIME FERRY FLIGHT.

Part: DOOR SEAL — CONTAMINATED (PAX DOOR) · airframe 30,753 hrs · 22,586 cycles

PASSENGER DOOR STICKS WHEN OPENING. CLEANED GLUE SUBSTANCE OFF MAIN CABIN DOOR SEAL & C TRACK. PERFORMED OPERATIONS CHECK IAW AMM 52-11-00. NO DISCREPANCIES NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,747 hrs · 22,580 cycles

ROW 16 EMER LIGHTS INOPERATIVE. DEFERRED IAW MEL 33-51-01B CAT C.

Part: CABLE — DEFECTIVE (PAX DOOR) · airframe 30,610 hrs · 22,468 cycles

PASSENGER DOOR SQUEALS. R & R PAX DOOR ICE BREAKER CABLE IAW AMM 52-11-15. OPERATIONS CHECKED GOOD.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 30,571 hrs · 22,437 cycles

EMERGENCY CEILING FLOODLIGHT AT ROW 17 INOPERATIVE. ADJUSTED ROW 17 EMER FLOODLIGHT BULB. PERFORMED OPERATIONS CHECK IAW AMM 33-51-09. OPERATIONS CHECKED GOOD.

Part: BALLAST — HOT (LAVATORY) · airframe 30,550 hrs · 22,419 cycles

AFT LAVATORY SMOKE WARNING IN FLIGHT. VISUALLY INSPECTED ALL ELEC COMPONENTS IN LAVATORY & FOUND LAVATORY VANITY BALLAST TO BE UNUSUALLY HOT. R & R LAVATORY VANITY BALLAST IAW AMM 33-25-05. R & R LAVATORY VANITY LIGHT BULBS IAW AMM 33-25-03. OPERATIONS CHECKED GOOD AT THIS TIME. PERFORMED OPERATIONS CHECK ON LAVATORY SMOKE DETECTOR WITH NO DEFECTS NOTED.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 30,503 hrs · 22,377 cycles

SMOKE IN AFT LAVATORY WARNING MSG. NO VISIBLE SMOKE NOTED. DEFERRED AFT LAVATORY SMOKE DETECTION SYS IAW MEL 26-16-01 CAT C.

Part: INDICATION SYS — FALSE ACTIVATION (COCKPIT) · airframe 30,333 hrs · 22,256 cycles

PASSENGER DOOR OUTER HANDLE CAUTION MSG. DEFERRED PAX DOOR INDICATION IAW MEL 52-70-01 CAT A.

Part: DOOR — NOISY (CABIN) · airframe 30,256 hrs · 22,199 cycles

EXCESSIVE SQUEAL FROM PAX DOOR IN FLIGHT. PERFORMED GVI ON ACFT FOR ONE TIME FERRY FLIGHT. ACFT SAFE FOR A ONE TIME FLIGHT.

Part: GLOWSTRIP — MISSING (SERVICE DOOR) · airframe 29,908 hrs · 21,942 cycles

SERVICE DOOR MISSING PHOTO LUMINESCENT STRIP ON LT SIDE. FOUND SERVICE DOOR TRIM PANEL LOOSE. SECURED IAW AMM 25-26-07.

Part: DOOR — STUCK (CABIN) · airframe 29,804 hrs · 21,857 cycles

PAX DOOR STUCK. DEACTIVATED & DEFERRED PAX DOOR ASSIST ON DMI IAW MEL 52-11-01A.

Part: DOOR — DAMAGED (CABIN) · airframe 29,804 hrs · 21,857 cycles

PAX DOOR DAMAGE AT PULLEY ATTACH POINT. CLOSED & SECURED PAX DOOR, VERIFIED LATCHED. INSPECTED ACFT & FOUND SAFE FOR ONE TIME FERRY FLIGHT.

Part: TRIM PANEL — PEELING (SERVICE DOOR) · airframe 29,506 hrs · 21,612 cycles

TRIM INSIDE SERVICE DOOR PEELING OFF. SECURED SERVICE DOOR TRIM IAW AMM 25-25-00.

Part: VALVE — STUCK (FUEL SYSTEM) · airframe 29,285 hrs · 21,436 cycles

LEFT WING LEAKING FUEL IN FLIGHT. FOUND LT WING VENT VLV STUCK OPEN, RESET VLV. PERFORMED OPERATIONS CHECK, OPERATIONS CHECKED GOOD IAW AMM 28-12-06.

Part: FASTENER — LOOSE (PAX DOOR) · airframe 29,203 hrs · 21,371 cycles

PASSENGER DOOR STEP HAS LOOSE HARDWARE. TIGHTENED PAX DOOR STEP HARDWARE IAW AMM 20-21-00.

Part: SPLICE — UNSECURE (PAX DOOR) · airframe 29,093 hrs · 21,282 cycles

PASSENGER DOOR OUT HANDLE CAUTION MSG. SECURED SPLICE FOR SENSOR PX107, OPERATIONS CHECKED GOOD IAW ESPM 20-44-00 & AMM 52-11-00. CLEARED DMI 33905.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,963 hrs · 21,180 cycles

NR 3 LT EMERGENCY LIGHT INOPERATIVE. RELAMPED OUTSIDE LT NR 3 EMERGENCY LIGHT IAW AMM 33-51-15, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 28,760 hrs · 21,011 cycles

RED LIGHT FWD FACING ON EMERGENCY EXIT SIGN ON CEILING AT ROW 12 INOPERATIVE. R & R BULB IAW CRJ700 33-51-07, OPERATIONS CHECKED NO GOOD. DEFERRED LIGHT IAW MEL 23-40-01J CAT B.

Part: MOTOR — FAILED (PAX DOOR) · airframe 28,742 hrs · 20,997 cycles

PASSENGER DOOR HIT THE GND UPON OPENING. R & R PAX DOOR ASSIST MOTOR IAW CRJ700 AMM 52-11-08, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

CORROSION FOUND ON FRAME AT FS 333 BL 0. BLENDED CORRODED AREA. NO REJECT INDICATIONS NOTED AT THIS TIME.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

INTERCOSTAL NR 2 FWD OF AVIONICS DOOR AT FS 364 CORRODED. R & R NR 2 INTERCOSTAL WITH NEW SERVICEABLE PART, PART SH670-3207-3 IAW CRJ700 SRM 51-42-06, 51-42-21, 51-40-11 & CRJ700 AMM 20-70-00.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

CORROSION FOUND ON STRINGER 26L BETWEEN FS 333.00 & FS 364.00. REMOVED CORRODED SECTION OF STRINGER 26L & REPLACED WITH NEW FABRICATED PART, PART SH67-21332-2 IAW REO 670-53-21-1082. NDT ACCOMPLISHED INSPECTIONS ON 10 MAR 2014.

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

CORROSION FOUND AT FS 333, BL 0. BLENDED CORRODED AREA IAW REO 670-53-21-1079. NO REJECT INDICATIONS NOTED AT TIME OF INSPECTION.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

LEFT FS 280 CROSSBEAM CORRODED. R & R CROSSBEAM WITH NEW PN CC670-34175-7S. FABRICATED LT & RT BULKHEAD LOWER WEBS & INSTALLED IAW CRJ 700 SRM CHAPTERS 51 & 53.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 28,695 hrs · 20,963 cycles

INTERCOSTAL FWD OF AVIONICS DOOR AT FS 364 CORRODED. R & R INTERCOSTAL IAW SRM 51-42-21, 51-42-06, 51-40-11, 51-42-13 & AMM 20-70-00.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

CORROSION FOUND ON FRAME AT FS 295 STRINGER 27. BLENDED CORRODED AREA. NO REJECT INDICATIONS NOTED AT TIME OF INSPECTION.

Part: SKIN — GOUGED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

GOUGES DISCOVERED ON FUSELAGE AT FS 980 STRINGER 27. CUT OUT TWO DAMAGED SECTIONS, FABRICATED FILLERS, DOUBLERS & TAPERED SHIMS FOR REPAIR, INSTALLED IAW REO 670-53-00-290 REV C DATED 03/21/2014. NDT ACCOMPLISHED INSPECTIONS K9QR554B 02 MAR 2014.

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

LEFT INNER DOORWAY SKIN AT FS 280.00 CORRODED. REMOVED DAMAGE, FABRICATED REPAIR PARTS & INSTALLED IAW REO 670-53-11-745 DATED 2012-09-08. NDT PERFORMED, NO INDICATIONS NOTED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

LINTEL STRINGER 3 CRACKED. PERMANENTLY REPAIRED LINTEL STRINGER 3 BY CUTTING AWAY DAMAGE, FABRICATING REPAIR PARTS & INSTALLING IAW REO 670-53-21-493 REV C DATED 2011-12-08 & SERVICE BULLETIN 670BA-53-040 REV C DATED 20 SEPT 2012. NDT PERFORMED BY K & B INSPECTION SERVICES CRS K9QR554B ON 6 MARCH 2014, NO INDICATIONS NOTED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

CORROSION FOUND ON STRINGER 26R BETWEEN FS 333.0 & 364.00. CUT OUT CORRODED SECTION OF STRINGER 26R. FABRICATED & INSTALLED NEW PART, PART SH670-31372-4 & SHIM IAW REO 670-53-21-1082, DATED 2014-O3-O7. NDT ACCOMPLISHED INSPECTIONS K9QR554B ON 3/10/14 & JOB AV0310148J, PO 120087. NO DEFECTS FOUND.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

LEFT HAND STATION 280 LOWER BULKHEAD WEB CORRODED. R & R LOWER WEB & STRAP WITH FABRICATED PARTS IAW REO 670-53-11-594, DATED 27 APR 2014.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

ENTRY STOWAGE & FLIGHT ATTENDANT CABINET FWD INBD MOUNT FITTING CORRODED. REPLACED FITTING WITH NEW PN CDSP2024-1-700 IAW CMM 25-23-37 REV 8 DATED 08-01-03.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

RIGHT BULKHEAD LOWER WEB AT FS 280.00 CORRODED. REMOVED DAMAGE, FABRICATED REPAIR PARTS & INSTALLED IAW REO 670-53-11-594 DATED 2011-04-27.

Part: SILL — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

RIGHT FLOOR SILL AT FS 280.00 - 319.7 IS CORRODED. REPLACED RT FLOOR SILL AT FS 280.00 - 319.7 WITH NEW PN SH 670-32172-3 IAW CRJ 700 SRM 51-21-11, 51-25-16, 51-42-06, 51-40-11, 51-41-00 & 51-42-10.

Part: PROTECTOR — CORRODED (SERVICE DOOR) · airframe 28,695 hrs · 20,963 cycles

GALLEY SERVICE DOOR MID CAP CORRODE. R & R SERVICE DOOR MID CAP FLOOR PROTECTOR IAW CRJ 700 SRM 51-42-21, 51-42-06, 51-45-00, 51-40-11, 51-25-21 & CRJ 700 AMM 20-70-00. AVMAX WORK ORDER 80205 & WORK CARD 8036.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

AVIONICS COMPARTMENT FWD CRAWL WAY FLOORBOARD ATTACH ANGLE CORRODED. R & R FWD CRAWL WAY FLOORBOARD ATTACH ANGLE IAW CRJ 700 SRM 51-42-06, 51-42-21, 51-21-11, 51-25-06, 51-40-11 & 51-42-10. AVMAX WORK ORDER 80205 & WORK CARD 1057.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

TCAS OMNIDIRECTIONAL ANTENNA MOUNTING CHANNEL CORRODED. R & R CORRODED OMNIDIRECTIONAL ANTENNA MOUNTING CHANNEL IAW CRJ 700 AMM 34-43-07, CRJ 700 SRM 51-21-11, 51-25-16, 51-40-11, 51-42-06 & 51-42-21.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

FLOOR BEAM AT FS 1036, LBL 27 CORRODED. CUT OUT CORRODED SECTION OF FLOOR BEAM. INSTALLED NEW PART IAW REO 670-53-00-029 REV A, CRJ 700 AMM 20-70-00, CRJ 700, SRM 51-24-36, 51-40-11, 51-21-11, 51-25-06 & 51-25-16.

Part: PROTECTOR — CORRODED (FUSELAGE) · airframe 28,695 hrs · 20,963 cycles

GALLEY SERVICE DOOR WEB FLOOR PROTECTORS X 4 CORRODED. REPLACED GALLEY SERVICE DOOR WEB FLOOR PROTECTORS X 4 WITH NEW PN SH670-32040-1, SH670-32040-2 & RECEPTACLE ASSEMBLY PN KBA670-30024-13 IAW CRJ 700 SRM 51-42-21, 51-42-13, 51-40-11, 51-21-11 & 51-25-16.

Part: PROTECTOR — CORRODED (SERVICE DOOR) · airframe 28,695 hrs · 20,963 cycles

FOUR GALLEY SERVICE DOOR WEB FLOOR PROTECTORS CORRODED. R & R GALLEY SERVICE DOOR WEB FLOOR PROTECTORS PN SH670-32040-1, SH670-32040-2 IAW CRJ700 SRM 51-42-21, 51-42-13, 51-40-11, 51-21-11 & 51-25-16.

Part: LIGHT — LOOSE (PAX DOORWAY) · airframe 28,675 hrs · 20,948 cycles

PASSENGER DOOR ESCAPE PATH LIGHT PEELING OFF ON STEPS 3 & 4. R & R EMERGENCY PATH LIGHT ON PAX DOOR STEPS IAW AMM 20-60-04.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 28,544 hrs · 20,852 cycles

AFT SMOKE LAVATORY MASTER WARNING. INSPECTED LAVATORY ACCESS PANELS & INSPECTED SURROUNDING AREA, NO DEFECTS NOTED IAW AMM 25-41-02. OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: LENS — CRACKED (PAX DOOR) · airframe 28,538 hrs · 20,847 cycles

PASSENGER DOOR EMERGENCY LIGHT LENS CRACKED. DEFERRED IAW MEL 33-51-01E CAT C.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,448 hrs · 20,780 cycles

LEFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R EXTERIOR EMERGENCY LIGHT BULB OVER LT WING FWD IAW IAW CRJ700 AMM 33-51-15. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: HINGE — DAMAGED (AIRSTAIRS) · airframe 28,422 hrs · 20,763 cycles

TOP STEP OF AIR STAIRS SEPARATED FROM AIRCRAFT. R & R TOP STEP HINGE IAW CRJ700 AMM 52-11-04.

Part: INDICATOR — MISSING (CABIN DOOR) · airframe 28,192 hrs · 20,591 cycles

GREEN LINE MISSING ON MAIN CABIN DOOR. REMARKED GREEN INDICATION & PERFORMED OPERATION CHECK OF PAX CABIN DOOR INDICATION IAW CRJ700 AMM 52-11-00. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,174 hrs · 20,578 cycles

CEILING EMERGENCY LIGHT INOPERATIVE OVER SEAT ROW 15. R & R LIGHT BULB IAW CRJ700 AMM 33-51-09.

Part: PLACARD — WORN (PAX DOOR) · airframe 28,287 hrs · 20,510 cycles

PAX DOOR OPEN PLACARD IS WORN. R & R PAX DOOR OPEN PLACARD IAW AMM 20-60-04.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,062 hrs · 20,493 cycles

LOWER EMERGENCY EXIT LIGHT BY PAX DOOR HAS A BULB OUT. R & R BULB IAW AMM 33-51-05, OPS CHECKED GOOD.

Part: SEAL — LACK OF LUBE (EMERGENCY EXIT) · airframe 27,196 hrs · 19,809 cycles

LEFT WING OVERWING EMERGENCY EXIT SQUEALS IN FLIGHT. LUBRICATED LT OVERWING EMERGENCY DOOR SEAL IAW AMM 12-20-52. GOOD AT THIS TIME.

Part: PLACARD — MISSING (CABIN) · airframe 26,738 hrs · 19,465 cycles

EMERGENCY EXIT PLACARD ON BACK OF SEAT 11D MISSING. OPEN

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 2,571,705 hrs · 18,967 cycles

GLD UNSAFE CAUTION ON TAKEOFF. RESET SYS, OP'S CHECKED GOOD IAW AMM 27-61-00, OP'S CHECKED GOOD ST THIS TIME.

Part: LIGHT — NO TEST (CABIN) · airframe 25,209 hrs · 18,326 cycles

EMERGENCY LIGHTS WILL NOT TEST. OP'S CHECKED IAW AMM 33-51-00, OP'S CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,245 hrs · 17,623 cycles

EMERGENCY LIGHT INOPERATIVE. PERFORMED EMERGENCY LIGHT CHECK IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 22,599 hrs · 16,411 cycles

F/A REPORTS MEGAPHONE INOP. PERFORMED OPS CHECK OF MEGAPHONE IAW AMM 25-61-14. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 22,542 hrs · 16,378 cycles

F/A FLASHLIGHT INOPERATIVE, REPLACED FLASHLIGHT BATTERIES IAW AMM 25-60-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 21,860 hrs · 15,889 cycles

LT REAR EMERGENCY LIGHT LENSE BROKEN LOCATED OUTSIDE FUSELAGE JUST ABOVE FLAP. R & R LT AFT EMERGENCY LIGHT LENSE COVER IAW CMM 33-52-07. OPS CK GOOD ACFT OK FOR SERVICE. (SDR CLOSED)

Part: HOUSING — CRACKED (EMERGENCY LIGHT) · airframe 19,662 hrs · 14,332 cycles

MAIN PASSENGER CABIN EMERGENCY LIGHT ON WARDROBE BASE ASSY CRACKED. R & R MAIN PAX CABIN EMERGENCY LIGHT ASSY ON WARDROBE OPS CHECK GOOD IAW GS 5600128 / P238 5600149.

Part: COUPLING — DISCONNECTED (FUEL SYSTEM) · airframe 19,263 hrs · 14,026 cycles

FUEL IMBALANCE DURING CLIMBOUT. COMPLIED WITH QRH, MAX IMBALANCE LT WING 2000LBS. RT ENGINE SHUTDOWN. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) FOUND COUPLING IN RT COLLECTET TANK FOR THE LT FUEL/DEFUEL VALVE BOSS DISCONNECTED. INSTALLED COUPLING IAW AMM 28-25-09-400-801. OPS AND LEAK CHECK GOOD.

Part: PLACARD — WORN (ESCAPE HATCH) · airframe 19,215 hrs · 13,990 cycles

CREW ESCAPE HATCH 831 PLACARDS ARE ILLEGIBLE. INSTALLED SILKSCREEN PRINT TO CREW ESCAPE HATCH (3) REF AMM 20-60-11-400-801.

Part: SEAT TRACK — CORRODED (BS 477-669) · airframe 19,215 hrs · 13,990 cycles

SEAT TRACKS ON FS477 TO FS669 RBL & LBL 9.0 ARE CORRODED BEYOND LIMITS AND REQUIRE REPLACING. REMOVED CORRODED SEAT TRACK IAW STANDARD PRACTICE SRM 51-42-02-001-001-A01. LOCATED SEAT TRACK IAW SRM 51-40-11-001-001-A01. INSTALLED SEAT TRACK IAW SRM 51-23-00-001-001-A01 & 51-40-11-001-001-A01.

Part: SEAT TRACK — CORRODED (BS 855.40-977) · airframe 19,215 hrs · 13,990 cycles

SEAT TRACKS ON FS 855.40 TO FS 977.00, RBL 9.0 & LBL 9.0 ARE CORRODED. BLENDED SEAT TRACKS FROM FS855.40 TO 977.00 IAW REO 670-53-00-013 ECTC ATTACHED, REO 670-53-00-013.

Part: SEAT TRACK — CORRODED (BS 669-855) · airframe 19,215 hrs · 13,990 cycles

SEAT TRACKS ON FS669.40 TO FS855.40 RBL & LBL 9.0 ARE CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03 PARA 4B. INSTALLED AT SEAT TRACK IAW AMM 53-00-49-400-801-A03.

Part: INTERCOSTAL — CORRODED (BS 319 S6-20R) · airframe 19,215 hrs · 13,990 cycles

RIGHT FUSELAGE, ST6R 20R, AT FS319.70 CONNECTION CORRODED (FLAGGED). REMOVED ANGLE IAW SRM 51-42-11. REMOVED GROUND ASSY IAW AMM 51-80-00. REMOVED CORROSION IAW AMM 51-21-06 REMOVED .003 FROM INTERCOSTAL THICKNESS. PAINTED AND TREATED IAW SRM 51-25-00. FABRICATED PART P/N SH 670-32045-1 P/O 107559 MATERIAL 7075-T6 DRILL EXISTING HOLE INSTALLED BRACKET IAW SRM 51-42-10. BONDING CHECK OK IAW AMM 51-80-00-760-802.

Part: SEAT TRACK — CORRODED (BS 280-477) · airframe 19,215 hrs · 13,990 cycles

SEAT TRACKS ON FS280 TO FS477 RBL & LBL 9.0 ARE CORRODED BEYOND LIMITS AND REQUIRE REPLACING. REMOVED CORRODED SEAT TRACK IAW STANDARD PRACTICE SRM 51-42-02-001-001-A01. LOCATED SEAT TRACK IAW SRM 51-40-11-001-001-A01. INSTALLED SEAT TRACK IAW SRM 51-23-00-001-001-A01.

Part: SEAL — LACK OF LUBE (EMERGENCY EXIT) · airframe 19,215 hrs · 13,990 cycles

LT OVERWING EMERGENCY EXIT DOOR STICKS WHEN OPERATING HANDLE TO OPEN, FORCE TO COMPLETELY OPERATE EXCEEDS MAXIMUM ALLOWED. LUBED DOOR SEAL & PERFORMED FUNCTIONAL TEST IAW AMM 52-21-00-720-801.

Part: INDICATOR — INOPERATIVE (NLG) · airframe 18,917 hrs · 13,759 cycles

UPON GEAR RETRACTION, GEAR DISAGREE MSG, NOSE GEAR INDICATOR WAS RED (A/C RETURNED TODAY AFTER T/O -- EMERGENCY DECLARED). PERFORMED EXTENTION/ RETRACTION OF NLG AND MLG IAW AMM 32-30-00. OPS CHECKED GOOD.

Part: LANDING GEAR — UNKNOWN · airframe 18,916 hrs · 13,759 cycles

PERFORMED EXTENTION/ RETRACTION OF NLG AND MLG IAW AMM 32-30-00. OPS CHECKED GOOD. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,721 hrs · 13,617 cycles

EMERGENCY LIGHTS INOP, FOUND SWITCH ON F/A PANEL ON THE "ON" POSITION. ACFTJUST ARRIVED AT THE GATE FROM THE HANGAR AFTER A LC-2 CHECK.

Part: PLACARD — TORN (PAX DOOR) · airframe 16,133 hrs · 11,660 cycles

EXIT STICKER ON PAX DOOR TORN.

Part: COVER — BROKEN (CABIN) · airframe 15,609 hrs · 11,269 cycles

CEILING LIGHT COVER AT 15AB BROKEN. LIGHT LENS/COVERS, INCLUDING EMERGENCY LIGHT. REPLACED LIGHT COVER AT SEAT 15AB IAW CRJ 700 AMM 33-21-00. DML CLEARED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 1,494,729 hrs · 10,796 cycles

BURNING SMELL IN FLT ACCOMPANIED BY RADIO ATL AT 20 FT GEAR HORN SINK RATE AND PULL UP AURAL. FLT 4268 DEL 104 MINS. (SERVICE LIGHTS) REMOVED AND REPLACED PYLON SERVICE LIGHT ASSY IAW CRJ700 AMM33-31. CBP2M7 PUSH IN, STAYS CLOSED, NO SMOKE, NO POPPING. OPERATION CHECKED GOOD, NO OTHER DEFECTS NOTED AT THIS TIME. INSPECTED CBP-2 AROUND CB-M7 PER CRJ700 AMM 05-21-00-210-801-A01. NO DEFECTS NOTED. REMOVED AND REPLACED PYLON SERVICE LIGHT ASSY IAW CRJ700 AMM 33-31. CBP2 M7 PUSH IN, STAYS CLOSED, NO SMOKE, NO POPPING, OPERATION CHECKED GOOD. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: STRIP — DAMAGED (CABIN) · airframe 14,301 hrs · 10,354 cycles

FLOOR EMERGENCY LIGHT STRIPS REMOVED DUE TO DAMAGE.

Part: LENS — CRACKED (CABIN) · airframe 14,292 hrs · 10,345 cycles

RIGHT EMERGENCY WING LIGHT LENS CRACKED. REMOVED AND REPLACED LENS IAW CRJ 700 AMM 33-51-21. SUPPLEMENTAL SDR CLOSED 3/11/08.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 14,292 hrs · 10,345 cycles

CORROSION DAMAGE IN MAIN AVIONICS BAY JUST FWD OF DOOR CUTOUT FS 364.00 AT STR 27 (MARKED). C/W REPAIR ON CORROSION DAMAGE IN MAIN AVIONICS BAY FWD OF DOOR CUT OUT.

Part: PLACARD — MISSING (SERVICE DOOR) · airframe 14,292 hrs · 10,345 cycles

SERVICE DOOR MISSING EMERGENCY EXIT INSTRUCTION PLACARD.

Part: ATTACH ANGLE — CRACKED (RT PYLON) · airframe 14,291 hrs · 10,345 cycles

RT PYLON INBD ATTACH ANGLE CRACKED FS 1108.0. C/W REPAIR ON RT PYLON INBOARD ATTACH ANGLE AT FS 1108.0.

Part: FRAME — CORRODED (BS 280) · airframe 14,291 hrs · 10,345 cycles

CORROSION DAMAGE IN FWD MAIN AVIONICS BAY JUST FWD OF FS 280 FRAME AT NOSE JACK PAD SUPPORT STRUCTURE LHS (MARKED). REMOVED DIRT PRIMER AND PAINT, AT MARKED LOCATION, NO CORROSION FOUND INSPECTED LOCAL AREA NO CORROSION FOUND AT THIS TIME AT NOSE JACK PAD AREA.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,291 hrs · 10,345 cycles

CORROSION DAMAGE ON FLOORBOARD SUPPORT ANGLE IN MAIN AVIONICS BAY AT FS 280.00 (MARKED). REMOVED PRIMER AND PAINT BLENDED MILD CORROSION PER SRM 53-00. REMOVED APPROX .002 ". REPRIMED AND PAINTED PER SRM 51-25-00.

Part: SILL — CORRODED (BS 295) · airframe 14,291 hrs · 10,345 cycles

CORROSION AT LT FLOOR SILL AT FS 295. BLENDED CORROSION AT FS 295 MEASURED THICKNESS, ALL WORK DONE IAW SRM 53-21-43.

Part: FRAME — CORRODED (FUSELAGE) · airframe 14,291 hrs · 10,345 cycles

CORROSION DAMAGE IN MAIN AVIONICS BAY BETWEEN FS 295.00 AND 310.00 FRAMES (MARKED). BLENDED CORROSION ON FS 295 FRAME IN LIMITS, .047 MATERIAL REMAINING IAW CRJ 700 SRM 53-21-06. SUPPLEMENTAL SDR CLOSED 3/7/08.

Part: SILL — CORRODED (FUSELAGE) · airframe 14,292 hrs · 10,345 cycles

RT FLOOR SILL AT FS 280 CORRODED. REPAIRED IAW W/O 84336 EC/TC 670-53-21-139.

Part: SILL — CORRODED (BS 319) · airframe 14,291 hrs · 10,345 cycles

FOUND CORROSION AT RT FLOOR SILL AT FS 319.

Part: HANDLE — CRACKED (E/E BAY DOOR) · airframe 14,291 hrs · 10,345 cycles

MAIN AVIONICS BAY DOOR HANDLE CRACKED AT BASE. REMOVED AND REPLACED MAIN AVIONICS BAY DOOR HANDLE IAW AMM 51-42-03 AND SRM 51-42-06 SG7020421

Part: FLOOR PANEL — BROKEN (COCKPIT) · airframe 14,291 hrs · 10,345 cycles

AFT LAND OF CENTER COCKPIT FLOOR BADLY CORRODED. REMOVED AND REPLACED AFT FLOOR LAND OF CENTER COCKPIT PER SRM 51-42-21.

Part: BEAM — CORRODED (FUSELAGE) · airframe 14,291 hrs · 10,345 cycles

THE 280 BEAM CORRODED BEYOND LIMITS. REFER TO E/C FOR REPLACEMENT REFER TO M-234 FORM ATTACHED TO N/R FOR WORK ACCOMPLISHED SM7017032. REPAIR MADE IAW ASA EO700-53-0061. SUPPLEMENTAL SDR CLOSED 3/7/08.

Part: DRAG ANGLE — CRACKED (STAB TO FUSE) · airframe 14,291 hrs · 10,345 cycles

RT VERTICAL STAB-TO-FUSELAGE DRAG ANGLE CRACKED AT AFT END.

Part: PANEL — CRACKED (SPOILER) · airframe 14,291 hrs · 10,345 cycles

RT MULTIFUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBD AFT CORNER. REPAIRED SHROUD IAW EO 700-57-065, REO 670-57-51-153A AND 51-75-18.

Part: PANEL — CRACKED (SPOILER) · airframe 14,291 hrs · 10,345 cycles

LT MULTIFUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBD AFT CORNER. REPAIRED SHROUD IAW EO 700-57-065, REO 670-57-51-153A AND 51-75-18.

Part: DRAG ANGLE — CRACKED (STAB TO FUSELAGE) · airframe 14,291 hrs · 10,345 cycles

LHS VERTICAL STAB-TO-FUSELAGE DRAG ANGLE CRACKED AT AFT END. REPAIRS PERFORMED IAW REO 670-55-31-018, REO 670-55-31-031, AND REO 670-55-31-031A

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 14,291 hrs · 10,345 cycles

EMERGENCY EXIT LIGHT ON WARDROBE JUST BELOW FLASHLIGHT, LENS COVER CRACKED. REMOVED AND REPLACED EXIT LIGHT LENS COVER IAW 33-51-01.

Part: COVER — MISSING (CABIN) · airframe 14,248 hrs · 10,316 cycles

EMERGENCY LIGHTING COVER MISSING, LAST 20 INCHES LEFT FWD CABIN. EMERGENCY FLOOR LIGHT COVER.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 12,908 hrs · 9,391 cycles

FLIGHT ATTENDANTS MEGAPHONE INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,411 hrs · 9,056 cycles

FWD F/A FLASHLIGHT INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,371 hrs · 9,024 cycles

F/A REPORTED, REAR FLASHLIGHT INOP.

Part: UNKNOWN — UNKNOWN (SPOILERS) · airframe 11,718 hrs · 8,572 cycles

OUTBOARD SPOILERONS & OUTBOARD FLT SPLRS CAUTION MSG. EMERGENCY DECLARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 11,586 hrs · 8,479 cycles

HYD SYS NR 1 HIGH TEMP MSG. AIR RETURN, AIRCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED.

Part: COWL DOOR — CHAFED (LEFT NACELLE) · airframe 11,189 hrs · 8,204 cycles

LEFT UPPER FAN COWL DOOR IS GOUGED AND RIB IS CHAFED FROM THE THRUST REVERSER FLEX DRIVE CABLE. REPAIRED DAMAGE IAW COMAIR EA 70-5414-01485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,189 hrs · 8,204 cycles

NUMEROUS FLOOR AND SIDE SEAT TRACKS ARE CORRODED. BLENDED WITHIN LIMIT SEAT TRACKS IAW REO 670-53-00-013, AND REPLACED 2 EA OUT OF LIMIT TRACKS IAW SRM 53-41-51.

Part: DOOR — MISSING (LT MLG) · airframe 8,214 hrs · 6,267 cycles

FLIGHT 5855 - LT MLG DOOR IS MISSING. REPAIRED COLLATERAL DAMAGE FROM IN FLIGHT SEPARATION AND DEFERRED GEAR DOOR PER CDL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 7,765 hrs · 5,917 cycles

FLIGHT 5186 - COPILOT SIDE WINDOW SHATTERED. REPLACED WINDOW.

Part: BULKHEAD — CORRODED (FS 280) · airframe 7,620 hrs · 5,804 cycles

FS 280 BULKHEAD LOWER WEBS ARE CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED THE FS 280 BULKHEAD LOWER WEBS IAW BOMBARDIER REO 670-53-11-052 REV A REPAIR 2.

Part: CYLINDER — CORRODED (NLG) · airframe 7,620 hrs · 5,804 cycles

NLG OUTER CYLINDER P/N 52101-1 S/N BA0027 IS CORRODED. CORROSION REPAIRED IAW BOMBARDIER REO 670-32-21-062 AND GOODRICH SCR 0008-04 REV C.

Part: STRINGER — DENTED (FUSELAGE) · airframe 7,620 hrs · 5,804 cycles

AFT RT FUSE AT FS1057 STR 14R-15R HAS 2.6L X 1.6W X .040D DENT. TRIMMED OUT DAMAGED AREA, LPI OR EDDY CURRENT TO ENSURE NO CRACKS EXIST. FABRICATE AND INSTALL DOUBLER (2024-T3 .063) IAW BRAS EO 601R-53-6952.

Part: CROSSBEAM — CORRODED · airframe 7,620 hrs · 5,804 cycles

THE TRANSVERSE BEAM AT FS 280 IS CORRODED. REMOVED AND REPLACED TRANSVERSE BEAM P/N CC670-34175-7-01 I/A/W BOMBARDIER REO 670-53-11-047 REV C.

Part: ENGINE — FLAMED OUT (LEFT) · airframe 5,525 hrs · 4,194 cycles

FLIGHT 5655 LT ENGINE FLAMED OUT DURING DESCENT FROM FL 410. NO FAULTS IN MDC, RAN ENGINE, NO DEFECTED NOTED.

Part: PUMP — UNRELIABLE (HYD SYSTEM) · airframe 4,859 hrs · 3,675 cycles

FLIGHT 5020 NR 2 HYDRAULIC SYSTEM HIGH TEMP WARNING. REPLACED THE RIGHT ENGINE HYDRAULIC PUMP.

Part: SENSOR — MALFUNCTIONED (RT MLG) · airframe 4,751 hrs · 3,597 cycles

FLT 5524 BRAKE OVERHEAT WARNING. REPLACED THE RT OUTBOARD BRAKE TEMP SENSOR.

Part: CONTROL UNIT — MALFUNCTIONED (ASCU) · airframe 4,750 hrs · 3,597 cycles

FLIGHT 5524 BRAKE OVERHEAT MASTER WARNING. COULD NOT DUPLICATE. RESET THE ASCU.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 4,529 hrs · 3,422 cycles

FLIGHT 5086 LEFT THRUST REVERSER UNSAFE MESSAGE DURING T/O. DEFERRED MAINT PER MEL.

Part: FITTING — CRACKED (SPOILER) · airframe 3,963 hrs · 2,986 cycles

DMI 34502 RIGHT OUTBOARD MULTI FUNCTION SPOILER SHROUD FITTING P/N CC670-17083-5 IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW SERVICEABLE FITTING P/N CC670-17083-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4857.

Part: FITTING — CRACKED (SPOILER) · airframe 3,963 hrs · 2,986 cycles

DMI 34502 RIGHT OUTBOARD MULTI FUNCTION SPOILER SHROUD FITTING P/N CC670-17083-5 IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED NEW SERVICEABLE FITTING P/N CC670-17083-5 IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES EO 601R-57-4857.

Part: OXYGEN BOTTLE — DISCHARGED (CABIN) · airframe 3,907 hrs · 2,935 cycles

FLIGHT 5641 FWD CABIN 02 BOTTLE EMPTY. SERVICED 02 BOTTLE.

Part: DOOR — UNSECURE (CARGO BAY) · airframe 3,533 hrs · 2,666 cycles

FLIGHT 5075 CABIN ALTITUDE CAUTION, AIRCRAFT WOULD NOT PRESSURIZE. FOUND CARGO DOOR NOT CLOSED PROPERLY. INSPECTED DOOR, NO DEFECTS NOTED. SECURED DOOR CLOSED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 2,599 hrs · 1,955 cycles

FS 1098.20 BULKHEAD RT WEB BETWEEN STRINGERS 8R AND 9R ARE CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B AND REO 670-53-61-089.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 2,599 hrs · 1,955 cycles

FS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPAIRED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 2,599 hrs · 1,955 cycles

FS 1098.20 BULKHEAD RIGHT WEB BETWEEN STRINGERS 8R AND 9R IS CRACKED. REPLACED BY REMOVING DAMAGE AND INSTALLING A BATHTUB FITTING IAW BOMBARDIER, INC REO 670-53-61-034 REV B.

Part: LINE — LEAKING (NR 2 HYD SYS) · airframe 930 hrs · 694 cycles

FLIGHT 5741 - NR 2 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPAIRED CHAFED HYDRAULIC TUBING IN AFT EQUIP BAY.

Part: WINDSHIELD — BROKEN (R/H) · airframe 781 hrs · 576 cycles

FLIGHT 5899 CO-PILOTS WINDSHIELD BROKEN DURING TAXI.REPLACED THE CO-PILOTS WINDSHIELD.