N719SK

Part: WINDSHIELD — CRACKED (RIGHT) · airframe 49,031 hrs · 32,693 cycles

RH WINDSHIELD CRACKED AND RH WINDSHIELD HEAT CAUTION MSGDID NOT LAND OVERWEIGHTDID NOT DECLARE EMERGENCY (FLIGHT 6203 FILED CLOSED)REMOVED AND REPLACED R/H WINDSHIELD IAW TASK CARD 05-900-2010-SKY OPS AND LEAK CHECK GOOD

Part: NONE — CRACKED · airframe 45,950 hrs · 30,095 cycles

LH WINDSHIELD POST APPEARS CRACKED RADIATION FORWARD FROM UPPER BARREL NUT HOLE. (C-CHECK RO 6/6/2022) REMOVED L/H WINDSHIELD SIDE POST P/N: 601R33223-1 REF. CRJ-700 SRM 51-42-21-001-001-A01 AND INSTALLED THE NEW LH WINDSHIELD SIDE POST REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG #CC670-33055 REV. -F. OPS AND LEAK CHECKS GOOD. / (NEW POST P/N=601R33223-1) CW 51-900-1002-SKY

Part: NONE — CRACKED · airframe 45,950 hrs · 30,095 cycles

GALLEY SERVICE DOOR - UPPER DOOR STABALIZER-BAR BRACKET IS CRACKED AT UPPER STABALIZER-BAR ATTACH POINT (C-CHECK RO 6/6/2022) REMOVED & INSTALLED THE NEW GALLEY SERVICE DOOR - UPPER DOOR STABILIZER BAR BRACKET REF. CRJ 700 AMM 52-41-27-400-801-A01, COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. ADJUSTMENTS AND OPS CHECKS ARE GOOD.

Part: NONE — CRACKED · airframe 45,950 hrs · 30,095 cycles

CRACKED O/B ANGLE AT APPROX. RBL 9.0 AND FS 280.00 (C-CHECK RO 6/6/2022) REMOVED AND REPLACED CRACKED O/B ANGLE AT APPROX. RBL 9.0 AND FS 280.00 . REF: CRJ-700 SRM 51-42-21-001-001-A01 AND DWG. CC670-34010 REV K. COMPLIED WITH TASK CARD 51-900-1002 SKY

Part: NONE — CRACKED · airframe 45,950 hrs · 30,095 cycles

LH CENTER COCKPIT FLOOR BEAMS LBL12.00 IS CRACKED AT ATTACHING FLANGE, (BELOW FLOOR) FWD SIDE OF FS.280 BULKHEAD. (C-CHECK RO 6/6/2022) PERFORMED REPAIR OF THE LH CENTER COCKPIT FLOOR BEAMS LBL12.00 FWD SIDE OF FS.280 BULKHEAD. REF: CRJ-700 SRM 53-11-43-201-003-A01. ALSO COMPLIED WITH 51-900-1002-SKY.

Part: NONE — CRACKED · airframe 45,950 hrs · 30,095 cycles

RH CENTER COCKPIT FLOOR BEAMS RBL12.00 IS CRACKED AT ATTACHING FLANGE, (BELOW FLOOR) FWD SIDE OF FS.280 BULKHEAD. (C-CHECK RO 6/6/2022) PERFORMED REPAIR OF RH CENTER COCKPIT FLOOR BEAMS RBL12.00 (BELOW FLOOR) FWD SIDE OF FS.280 BULKHEAD. REF: CRJ-700 SRM 53-11-43-201-003-A01, CRJ700 SRM 51-42-06-001-001-A01 & CRJ700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: NONE — CRACKED · airframe 45,950 hrs · 30,095 cycles

LH LOWER TRANSCOWL O/B STAND-OFF APPEARS CRACKED. (C-CHECK RO 6/6/2022) REPLACED LH LOWER TRASNCOWL OB STAND OFF REF CRJ700 SRM 51-42-14-001-001-A01 AND DWG CN624-2001 REV. AG. COMPLIED WITH 51-900-1002-SKY.

Part: NONE — DEPARTED · airframe 45,950 hrs · 30,095 cycles

RH UPPER TRANSCOWL Z ANGLE 1 MISSING FASTENER HEAD AND APPEARS DISBONDED. (C-CHECK RO 6/6/2022) COMPLIED WITH ALL STEPS 1 THRU 25 OF MHIRJ REO 670-54-21-1536 REV -- DATED 2022-05-11 REPAIR FOR CRACK DAMAGE TO THE RH UPPER TRANSCOEL INNER SKIN. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

CORROSION FOUND ON VERTICAL WEB AND ATTACHING FLANGE OF FRAME FS969 BETWEEN STGR 26R AND 26L. (C-CHECK RO 6/6/2022) REPAIRED FRAME AT FS969 BETWEEN STGR 26R AND 26L REF REO 670-53-51-249 REV.-- DATED 04/29/22 AND DWG # SH670-37060 REV. G. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR FURTHER DETAILS.

Part: NONE — CRACKED · airframe 45,950 hrs · 30,095 cycles

PAX DOOR INNER SKIN CRACKED AT ACCESS PANEL 832AL (C-CHECK RO 6/6/2022) COMPLIED REO 670-52-11-1291, REV-- DATE 2022-04-29 STEPS 1 TO 17. REPAIR TO PAX DOOR INNER SKIN BETWEEN FS310.00-FS320.163 AND ABOVE DATUM #1. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

SERVICE DOOR- LOWER SILL ANGLE HAS EVICENDCE OF CORROSION (C-CHECK RO 6/6/2022) SERVICE DOOR LOWER SILL ANGLE IS OUT OF LIMITS REF CRJ-700 SRM 53-21-23-101-002-A01. REMOVED SERVICE DOOR LOWER SILL ANGLE P/N: SH670-31986-1 REF CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICE DOOR LOWER SILL ANGLE REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# SH670-31950 REV-Y. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: NONE — DAMAGED · airframe 45,950 hrs · 30,095 cycles

DURING REMOVAL OF L/H INBD FLAP LOWER SKIN, 2 EA. RIBS WERE DAMAGED AT FLS84.20 AND FLS92.80. (C-CHECK RO 6/6/2022) REMOVED 3 EA. DAMAGED RIBS AND INSTALLED NEW 1 EA. RIB P/N CC670-14169-1 (FLS84.20), NEW 1 EA. RIB P/N CC670-14170-3 (FLS92.80) & 1 EA. NEW RIB P/N CC670-14173-1 (FLS112.30) ON L/H I/B FLAP, REF. CRJ700 SRM 51-41-06-001-001-A01 & DWG. CC670-14050, REV. L. COMPLIED WITH 51-900-1002-SKY

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

SERVICE DOOR- SEAL STRIKER HAS EVIDENCE OF CORROSION (C-CHECK RO 6/6/2022) SERVICE DOOR BOTTOM SEAL STRIKER IS OUT OF LIMITS REF CRJ-700 SRM 53-21-23-101-002-A01.REMOVED DAMAGED SERVICE DOOR BOTTOM SEAL STRIKER REF CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED NEW BOTTOM SEAL STRIKER AT SERVICE DOOR REF DWG# SH670-31950 REV-Y AND SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: NONE — CRACKED · airframe 45,950 hrs · 30,095 cycles

* L/H WING SLAT CAN 1/3 HAS A CRACK IN THE AFT ATTACH TAB, MARKED. (C-CHECK RO 6/6/2022) COMPLIED WITH ALL STEPS OF REO 670-57-42-577 REV-- DATED: 2016-12-02. COMPLIED WITH 51-900-1002-SKY SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

* AVIONICS BAY CIRCUMFERETIAL FRAME AT FS.295.00 FROM STR.26L TO STR.26R CORRODED (MARKED). (C-CHECK RO 6/6/2022) REMOVED AND REPLACED DAMAGED FRAME SECTOR ON FS 295 FROM STR 25L TO STR 25R REF CRJ 700 SRM 53-00-06-201-006-A01. LEAK CHECK GOOD.

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

* FS.280.00 CROSSBEAM BETWEEN LBL9 AND RBL9 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 6/6/2022) REMOVED DAMAGED AND INSTALLED NEW FS280.00 BETWEEN LBL9-RBL9 UPPER SPLICE STRIP P/N: CC670-34097-1 REF CRJ-700 SRM 51-42-13-001-001-A01 AND USED DWG. CC670-34010 REV.-J / SEE CONTINUATION CARD FOR DETAILS / COMPLIED WITH 51-900-1002-SKY.

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

* AVIONICS BAY FLOOR BOARD MOUNT ANGLE AT FS.280.00 FROM LBL9 TO RBL9 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 6/6/2022) REMOVED AND REPLACED NEW AVIONICS BAY FLOOR BOARD MOUNT ANGLE AT FS.280.00 FROM LBL9 TO RBL9. REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV K. COMPLETED WITH TASK CARD 51-900-1002-SKY AND FORM M-337. SEE CONTINUE CARD FOR MORE DETAILS

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

* COCKPIT FLOOR BOARD MOUNT ANGLE AT FS.280.00 FROM LBL9 TO RBL9 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 6/6/2022) REMOVED AND INSTALLED NEW FLOOR PANEL SUPPORT ASSY REF: CRJ-700 S.R.M. 51-42-06-001-001-A01,51-42-21-001-001-A01, ALSO COMPLIED WITH 51-900-1002-SKY

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

* LH FLOOR SILL FROM FS.533.00 TO FS.565.00 CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 6/6/2022) INSTALLED NEW SILL ASSY, ON LH FLOOR FS533-FS581 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-32170 REV.V. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — ELONGATED · airframe 45,950 hrs · 30,095 cycles

PAX DOOR PIANO HINGE (DOOR SIDE) LUGS HOLES ARE ELONGATED. (C-CHECK RO 6/6/2022) AFTER TO ACCOMPLISH MEASUREMENT ON DAMAGED LUG HOLES AND EVALUATE, IT WAS FOUND WITHIN LIMITS PER REF BOMBARDIER GENERIC REO# 670-52-11-511, REV -E, DATED ON 2017-08-02. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

RIGHT FLOOR SILL IS CORRODED. FS1031.00 €“ FS1059.00. (MARKED) (C-CHECK RO 6/6/2022) INSTALLED NEW RH FLOOR SILL AT BETWEEN FS1031.00 €“ FS1059.00 REF CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG MM670-35052 REV K. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

* SEVICE DOOR LOWER SILL CAP ANGLE FORM FS319.7 TO FS.349.00 CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 6/6/2022) EVALUATED CORROSION ON SERVICE DOOR LOWER SILL CAP ANGLE FS319.7 TO FS349.00 AND FOUND 100% MATERIAL LOSS. OUT OF LIMITS. REPLACED PART. INSTALLED NEW SERVICE DOOR LOWER SILL CAP ANGLE FROM FS319.7 TO FS349.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# SH670-31950 REV-Y. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

STGR26L IS CORRODED MULTIPLE AREAS. FS953.00 €“ FS969.00. (MARKED) (C-CHECK RO 6/6/2022) INSTALLED NEW STRINGER SECTION REF. REO 670-53-00-690 REV. -- DATED 2022-05-09, AND DWG. SH670-37060 REV. G. LEAK CHECK GOOD AT THIS TIME. COMPLIED WITH 51-900-1002-SKY

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

* PAX DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 6/6/2022) BLENDED CORROSION ON PAX DOOR LOWER SILL REF. CRJ-700 SRM, 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS REF. CRJ-700 SRM ,53-21-23-101-001-A01. REMOVED AND REPLACED WITH NEW KICKPLATE ANGLE (P/N: SH670-31875-7) REF DWG SH670-31810 REV AE AND CRJ-700 SRM, 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

RH MAIN LANDING GEAR WHEEL WELL SUPPORT ANGLE ON WING REAR SPAR FOR PANEL 642BZ HAS CORROSION. (C-CHECK RO 6/6/2022) REMOVED AND REPLACED R/H MLG WHEEL SUPPORT ANGLE P/N CC670-10338-2 REF. CRJ700 SRM 51-42-21-001-001-A01 DATE SEP 20/2007 REV. 20, DRAWING # CC670-10320 REV. -F. NO LEAKS NOTED. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND MAJOR REPAIR M-337.

Part: NONE — CORRODED · airframe 45,950 hrs · 30,095 cycles

LH MLG WHEEL WELL BETWEEN WS14.50 AND WS 24.50 SUPPORT ANGLE FOR 542BZ HAS CORROSION. (C-CHECK RO 6/6/2022) REMOVED AND REPLACED L/H MLG WHEEL SUPPORT ANGLE P/N CC670-10338-1 REF. CRJ700 SRM 51-42-21-001-001-A01 DATE SEP 20/2007 REV. 20, DRAWING # CC670-10320 REV. -F. NO LEAKS NOTED. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND MAJOR REPAIR M-337.

Part: NONE — CHAFED · airframe 45,950 hrs · 30,095 cycles

*AFT BAG BAY DOOR HANDLE HOUSING CHAFFED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/6/2022) INSTALLED NEW AFT BAGGAGE DOOR HANDLE HOUSING IAW CRJ 700 SRM 51-42-21-001-001-A01 / DRAWING # 601R35027 REV Y SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: NONE — CRACKED · airframe 45,950 hrs · 30,095 cycles

*EVALUATE POSSIBLE CRACK ON RIGHT VERTICAL STAB DRAG ANGLE. (MARKED) (C-CHECK RO 6/6/2022) REPLACED RIGHT VERTICAL STAB DRAG ANGLE REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG# BA670-35002 REV F. ALSO COMPLIED WITH 51-900-1002-SKY. ALL CHECKS GOOD AT THIS TIME.

Part: NONE — CHAFED · airframe 45,950 hrs · 30,095 cycles

EVALUATE CHAFE ON SKIN DOUBLER JUST AFT OF FS977, STGR 27. (MARKED) (C-CHECK RO 6/6/2022) EVALUATED. ORIGINAL MATERIAL THICKNESS IS 0.063" REF. REO # 670-53-00-290, REV. -F DATED: 2019-04-26, MATERIAL LOST 0.020", REMAINING MATERIAL IS 0.043" NO DAMAGE ALLOWED ON AREA.REF. CRJ700 SRM 53-00-00-101-001-A01. REPAIRED CHAFE DAMAGE ON SKIN DOUBLER AFT OF FS977 STR 27 IAW REO 670-53-00-290 REV -F DATED 2019-04-26. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: WINDOW — OVERHEATED (COCKPIT LEFT) · airframe 44,458 hrs · 28,979 cycles

DUE TO WINDOW HEAT CAUTION MESSAGE LH FLIGHT COMPARTMENT SIDE WINDOW REQUIRES REPLACEMENT. (FILED CLOSED) REMOVED LH FLIGHT COMPARTMENT SIDE WINDOW IAW CRJ 700 AMM 56-12-01-000-801-A01. SEE CP23072910 FOR INSTALLATION OF NEW SIDE WINDOW.

Part: DOUBLER — CHAFED (RT NACELLE) · airframe 43,985 hrs · 28,641 cycles

FABRICATED DOUBLER FOR PREVIOUS REPAIR DOUBLER AT ACCESS PANEL RH LOWER CORE COWL FOUND CHAFED THROUGH (FILED CLOSED)REMOVED EXISTING REPAIR DOUBLER AND FABRICATED NEW DOUBLER AT ACCESS PANEL RH LOWER CORE COWL IAW SRM 54-23-00-201-005-A01 STEPS A(1) THRU (3) (J)

Part: UNKNOWN — SMOKE (CABIN) · airframe 39,925 hrs · 25,411 cycles

DURING TAXI IN TO GATE WE GOT A SMOKE TOILET WARNING. SMOKE WAS FILLING CABIN FROM VENTS. NO OTHER MESSAGES WHERE DISPLAYED. (FLT#2961) CLOSED PERFORMED VISUAL INSPECTION OF PASSENGER CABIN AND LAV, NO OBVIOUS SIGNS OF DEFECTS, PERFORMED VISUAL INSPECTION OF APU ASSY, NO SIGNS OF DEFECT. REMOVED APU BLEED DUCT AND INSPECTED FOR SIGNS OF OIL, NO OIL FOUND RE-INSTALLED APU BLEED DUCT IAW AMM. INSPECTED RECIRC FANS IN AFT CARGO IAW AMM. NO SIGNS OF DEFECTS AND NO SMELL OF SMOKE. INSPECTED AVIONICS BAY NO SIGNS OF DEFECT. INSPECTED AFT EQUIPMENT BAY AREA AND BOTH ACM'S AND ACM DUCTING NO SIGNS OF DEFECTS FOUND. INTERROGATED MDC NO CURRENT FAULTS FOUND. PERFORMED APU RUN WITH BLEEDS FOR AN EXTENDED TIME, NO SMOKE OR SMELL NOTED. PERFORMED ENGINE RUNS WITH BLEEDS ON FOR SEVERAL MINUTES WITH NO SMOKE OR SMELL NOTED.

Part: FAN — FAILED (RECIRCULATION) · airframe 39,742 hrs · 25,252 cycles

DURING TAXI IN TO GATE, AFT LAV SMOKE WARNING MSG DISPLAYED WITH REPORT SMOKE FROM FA AND BURNING SMELL IN FLIGHT DECK. EMERGENCY DECLARED AND PROCEEDED WITH EXPEDITED EVACUATION. (FLT#3018) CLOSED FOUND #2 RECIRC FAN RUNNING HOT. REMOVED AND REPLACED #2 RECIRC FAN IAW AMM. PERFORMED OPS TEST OF ACM SYSTEM IAW AMM. RAN ENGINE AND APU BLEED SOURCES FOR AN EXTENDED AMOUNT OF TIME. NO FURTHER SMELLS OR SMOKE NOTED AT THIS TIME.

Part: APU — CONTAMINATED (APU BAY) · airframe 39,418 hrs · 25,000 cycles

WHILE TAXIING, WE RECEIVED A SMOKE AFT LAV WARNING MSG. THE FLIGHT ATTENDANT CONFIRMED SMOKE IN THE CABIN. THE AFT FA VERIFIED THAT THE SMOKE DETECTOR WENT OFF. THERE WAS A SMELL OF BURNED PLASTIC AND THE FORWARD FA DECIDED TO OPEN THE MAIN CABIN DOOR. WE PROCEEDED WITH AN EXPEDITED DEPLANING. (FLT 3050) CLOSED / FOUND NO SIGNS OR EVIDENCE OF FIRE. RAN AIR CONDITIONING SYSTEM SMELL WAS PRESENT WHEN ONLY APU RUNNING. SUSPECT APU AS SOURCE OF SMELL AND SMOKE, IN THE CABIN. OPENED APU COMPARTMENT, FOUND EXCESSIVE AMOUNTS OF DE-ICE FLUID IN AND AROUND THE APU, CLEANED OFF EXCESS DE-ICING FLUID FROM APU AND APU COMPARTMENT IAW AMM. RAN APU TILL SMELL DISSIPATED AND LEFT OVER SMOKE DISSIPATED. SMOKE AND SMELL NO LONGER PRESENT AT THIS TIME. REMOVED AND REPLACED THE LT & RT RECIRCULATION FAN FILTER.

Part: ANGLE — CORRODED (BS 319-349) · airframe 37,957 hrs · 23,650 cycles

TWO ANGLES LOCATED AT BS 319.7 AND 349, STRINGER 20R, COMMON TO INTERCOSTAL, FOUND TO BE CORRODED. INSTALLED THE TWO ANGLES IAW SRM.

Part: STRINGER — CORRODED (BS 319-349) · airframe 37,957 hrs · 23,650 cycles

CORROSION FOUND ON STRINGER 20R BETWEEN BS 319 - 349. REPAIRED IAW REO.

Part: INTERCOSTAL — CORRODED · airframe 37,957 hrs · 23,650 cycles

INTERCOSTAL AT STRINGER 20R CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.

Part: HINGE — CHAFED (PAX DOOR) · airframe 37,957 hrs · 23,650 cycles

PASSENGER DOOR HINGE LUGS AIRCRAFT SIDE SCRATCHED AND CHAFED. INSTALLED A NEW DOOR HINGE IAW SRM.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 37,957 hrs · 23,650 cycles

SERVICE DOOR UPPER SILL ANGLE HAS CORROSION UNDER FITTINGS. THE DOOR SILL ANGLE WAS REPLACED WITH NEW IAW SRM.

Part: FLOOR SUPPORT — CORRODED (AFT) · airframe 37,957 hrs · 23,650 cycles

AFT FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.

Part: FRAME — CORRODED (BS 295) · airframe 37,957 hrs · 23,650 cycles

FRAME AT BS 295 BETWEEN STRINGERS 26L TO 26R CORRODED. REMOVED THE CORROSION IAW SRM.

Part: FRAME — CORRODED (BS 333) · airframe 37,957 hrs · 23,650 cycles

FRAME AT BS 333 BETWEEN STRINGERS 26L TO 25R CORRODED. COMPLIED WITH FRAME SECTION REPLACEMENT IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 37,957 hrs · 23,650 cycles

INTERCOSTAL AT STRINGER 27L BETWEEN BS 349 AND 364 CORRODED. REPLACED THE INTERCOSTAL IAW SRM.

Part: STRINGER — CORRODED (BS 333-349) · airframe 37,957 hrs · 23,650 cycles

STRINGER 26R BETWEEN BS 333 TO 349 CORRODED. INSTALLED A NEW STRINGER IAW REO AND SRM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 37,957 hrs · 23,650 cycles

INTERCOSTAL AT STRINGER 27R BETWEEN BS 349 AND 364 CORRODED. REMOVED AND REPLACED THE INTERCOSTAL SRM.

Part: FRAME — CORRODED (BS 349) · airframe 37,957 hrs · 23,650 cycles

FRAME AT BS 349 BETWEEN STRINGERS 26L TO 26R CORRODED. INSTALLED A NEW SERVICEABLE FRAME IAW SRM AND REO.

Part: SUPPORT — CORRODED (BS 597-693) · airframe 37,957 hrs · 23,650 cycles

FORWARD FUSELAGE BS 597 TO 693 HAS EVIDENCE OF CORRSION AT NUMEROUS SPOTS ON THE FUSELAGE AT PANEL 191AB, 191BB, AND 192BB ATTACH POINTS. REMOVED CORROSION IAW SRM.

Part: SUPPORT — CORRODED (BS 597-693) · airframe 37,957 hrs · 23,650 cycles

FORWARD FUSELAGE, BS 597 TO 693, HAS EVIDENCE OF CORROSION AT NUMEROUS SPOTS ON FAIRING SUPPORT STRUCTURE FOR PANELS 191AB, 191BB, AND 192BB. REMOVED CORROSION AND REPLACED OUT OF LIMITS PARTS FAIRING SUPPORT STRUCTURE ON FWD FUSELAGE FROM BS 597 TO 693 IAW SRM.

Part: HOUSING — GOUGED (CARGO DOOR) · airframe 37,957 hrs · 23,650 cycles

AFT CARGO BAY DOOR HANDLE HOUSING HAS A DEEP GOUGE WORN INTO EDGE AT THE HANDLE ALIGNMENT PIN. REMOVED AND INSTALLED AFT BAGGAGE BAY DOOR HANDLE HOUSING IAW SRM.

Part: HOUSING — GOUGED (GALLEY DOOR) · airframe 37,957 hrs · 23,650 cycles

GALLEY SERVICE DOOR OUTER HANDLE HAS A WORN TEFLON PAD AT THE PIVOT POINT.CAUSING GOUGING AT AREA OF ROTATION. REPLACED THE OUTER HANDLE HOUSING AND TEFLON PADS IAW SRM.

Part: STRUT — DISCHARGED (NLG) · airframe 37,737 hrs · 23,478 cycles

GEAR DISAGREE AFTER TAKE OFF, MAIN GEAR LIGHTS WENT GREEN MOMENTARILY, THEN STARTED FLICKERING BETWEEN RED AND AMBER, NLG DIDN'T GO GREEN AT ALL AND FLUCTUATED BETWEEN RED AND AMBER. RETURNED TO FIELD. PERFORMED AN OPS CHECK OF THE LANDING GEAR SYSTEM IAW AMM. SWUNG GEAR MULTIPLE TIMES. OPS CHECKED GOOD. SERVICE NLG STRUT IAW AMM. NO LEAKS NOTED.

Part: NOT REPORTED — OUT OF ADJUST (NLG) · airframe 37,737 hrs · 23,478 cycles

NOSE GEAR DISAGREE. FOUND THE PX11 OUT OF RIG. ADJUSTED THE PX11. OPS CHECKED GOOD.

Part: FLOOR PANEL — WORN (NOT REPORTED) · airframe 33,608 hrs · 20,114 cycles

PANEL, 522JZ HAS 2 NUTPLATES WITH EXCESSIVE PLAY CAUSING PANEL WEAR. PANEL 522JZ, REPLACED DUE TO .1562 NUTPLATE ATTACHMENT HOLES OUT OF LIMITS IAW SRM.

Part: FLOOR PANEL — CRACKED (BS 193) · airframe 33,608 hrs · 20,114 cycles

LEFT TRU BAY FLOOR IS CRACKED AT APPROXIMATELY FS 193.00. REPAIRED CRACK IN LT TRU BAY FLOOR IAW REO.

Part: SKIN — WORN (LE FLAP) · airframe 33,608 hrs · 20,114 cycles

PANEL 684AB IS WORN ALMOST ALL THE WAY THROUGH ON THE INBD L/E. REPLACED FLAP PANEL NR 684AB WITH NEW PANEL, PN: CC670-14051-2, P/O: T-34051/6 IAW SRM.

Part: TRACK — CHAFED (CARGO DOOR) · airframe 33,608 hrs · 20,114 cycles

BRACKET ON LT LOWER AFT CARGO DOOR TRACK SHOWS SIGNS OF CHAFING. REPLACED OUT OF LIMITS AFT CARGO DOOR AFT TRACK, ROLLER GUIDE UP AFT BRACKET, PN CC670-38810-2 AND AFT CARGO DOOR AFT TRACK, ROLLER GUIDE UP AFT SUPPORT BRACKET, PN CC670-38814-1 IAW SRM.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 29,685 hrs · 17,678 cycles

PILOT REPORTED UNCOMMANDED RUDDER MOVEMENT IN FLIGHT, DIVERTED. REMOVED AND REPLACED NR 1 AND 2 YAW DAMPNER ACTUATORS.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 28,850 hrs · 17,217 cycles

RT INBD FLAP PANEL 684AB CHAFED. R & R FLAP PANEL IAW SRM.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 28,850 hrs · 17,217 cycles

REPAIR ANGLE ON AFT WEB OF PAX DOOR IS CRACKED. C-CHECK, FABRICATED NEW REPAIR ANGLE IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 364) · airframe 28,850 hrs · 17,217 cycles

CORROSION ON INBD AND OTBD SIDES OF INTERCOSTAL, STRINGER 27 RT, FORWARD OF AVIONICS BAY DOOR FS 364. C-CHECK, R & R INTERCOSTAL FWD OF AVIONICS BAY DOOR AT FS 364.00, STRINGER 27R IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 364-349) · airframe 28,850 hrs · 17,217 cycles

CORROSION ON INBD AND OTBD SIDES OF INTERCOSTAL, STRINGER 27 LT, FORWARD OF AVIONICS BAY DOOR FS 364 TO 349. C-CHECK, REMOVED AND INSTALLED NEW LATCH PIN INTERCOSTAL AT STRG 27L IAW SRM.

Part: WEB — CRACKED (PAX DOOR) · airframe 28,850 hrs · 17,217 cycles

PASSENGER DOOR AFT STAIRWELL WEB CRACKED UNDER MOTOR MOUNT. REPAIRED PASSENGER DOOR AFT STAIRWELL WEB IAW REO.

Part: STRUCTURE — CHAFED (BS 967) · airframe 28,850 hrs · 17,217 cycles

CHAFING FOUND AT BS 967, STRINGER 27. REPAIRED IAW REO.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 28,631 hrs · 17,096 cycles

THE WHITE LENS COVER ON THE EMERGENCY EXIT OVERHEAD LIGHT IS MISSING. REPLACED THE WHITE LENS COVER IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 28,517 hrs · 17,023 cycles

EMERGENCY LIGHTS WERE LEFT ON. AFTER CHARGING THE EMERGENCY LIGHTS, OPS CHECKED GOOD IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,263 hrs · 16,874 cycles

EMERGENCY RED LIGHT IS BURNED OUT. REPLACED LAMP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,195 hrs · 16,833 cycles

CABIN EMERGENCY INDICATOR LIGHT IS BURNED OUT. REPLACED THE LAMP.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 27,827 hrs · 16,626 cycles

EMERGENCY EXIT SIGN LT OVERWING EXIT IS BURNED OUT. FLT 5162 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,547 hrs · 15,954 cycles

EMERGENCY OVERHEAD LIGHT AT ROW 14 IS BURNED OUT. FLT#5161 RELAMPED.

Part: STRINGER — CRACKED (PAX DOOR) · airframe 24,634 hrs · 14,868 cycles

FS 280/FS 295 PASSENGER DOOR LINTEL STRINGER 3 CRACKED. (C-CHECK) REPAIRED FS 280.00 TO FS 295.00 - LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, IAW REO.

Part: AXLE — CORRODED (LT MLG) · airframe 24,634 hrs · 14,868 cycles

FOUND CORROSION ON LEFT MLG NR 1 AXLE. (C-CHECK) REPAIRED CORROSION ON LEFT MLG NR 1 AXLE IAW REO.

Part: AXLE — CORRODED (LT MLG) · airframe 24,634 hrs · 14,868 cycles

FOUND CORROSION ON LEFT MLG NR 2 AXLE. (C-CHECK) REPAIRED CORROSION ON LEFT MLG NR 2 AXLE IAW REO.

Part: SKIN — CHAFED (FUSELAGE) · airframe 24,634 hrs · 14,868 cycles

EXTERNAL SKIN CHAFED AT FS 977.00 STR 27.00 IN APPROXIMATELY TWO PLACES. (C-CHECK) REPAIRED CHAFED AREA IAW REO.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 24,634 hrs · 14,868 cycles

TOP OF 280 CROSSBEAM CRACKED AT LBL 9 AND RBL 9. (C-CHECK) REPLACED FS 280.0 CROSSBEAM IAW REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 24,634 hrs · 14,868 cycles

LIGHT SURFACE CORROISON ALONG INNER SKIN OF AVIONICS DOOR CUT-OUT, AT AVIONICS DOOR SEAL. (C-CHECK) REPAIRED INNER SKIN OF AVIONICS BAY DOOR CUT-OUT IAW REO.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,067 hrs · 14,541 cycles

EMERGENCY OVERHEAD LIGHTS NR 2, 3 AND LEFT WING AND EXIT LIGHTS INOPERATIVE. (FLT 6531) REPLACED NR 2 EMERGENCY LIGHT BATTERY PACK.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 23,940 hrs · 14,456 cycles

ROW 12 EMERGENCY EXIT SIGN LIGHT BULBS BURNED OUT. (FLT#5196) RELAMPED EMERGENCY LIGHTS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 23,798 hrs · 14,377 cycles

IN CRUISE FIRST OFFICER'S WINDSHIELD CRACKED. (FLT 5581) REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD IAW AMM.

Part: HARNESS — JAMMED (FA JUMPSEAT) · airframe 23,438 hrs · 14,165 cycles

FORWARD FLIGHT ATTENDANT JUMPSEAT HARNESS JAMMED. (FLT 5203) RE-POSITIONED HARNESS ON FLIGHT ATTENDANTS FORWARD JUMPSEAT.

Part: SIGN — MISSING (CABIN DOOR) · airframe 23,066 hrs · 13,954 cycles

EMERGENCY EXIT SIGN ON THE MAIN CABIN DOOR HANDLE IS MISSING. (FLT 5176) REPLACED EMERGENCY EXIT SIGN ON MAIN CABIN DOOR INNER HANDLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,823 hrs · 13,770 cycles

ROW 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5363) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,458 hrs · 13,582 cycles

LEFT WING EMERGENCY EXIT LIGHT IS OUT. (FLT 5401) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,928 hrs · 13,290 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,737 hrs · 13,176 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5391) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,422 hrs · 13,007 cycles

NR 3 LEFT EXTERIOR EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 21,097 hrs · 12,848 cycles

HYDRAULIC NR 2 LOW PRESSURE. (FLT 5309) REPLACED THE NR 2 ENGINE HYDRAULIC PUMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,800 hrs · 10,417 cycles

AFT CEILING EMERGENCY LIGHT INOP. (FLT 6289) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,321 hrs · 10,119 cycles

REAR EMERGENCY CEILING LIGHT INOP. (FLT 6858) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,321 hrs · 10,119 cycles

OVERHEAD EMERGENCY CEILING LIGHT NR 6 INOP. (FLT 6080) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — NOT SEATED (CABIN) · airframe 15,665 hrs · 9,727 cycles

OVERHEAD EMERGENCY EXIT LIGHT SIGN INOP AT ROW 11. (FLT 6443) RESEATED BULBS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,665 hrs · 9,727 cycles

AFT MOST OVERHEAD EMERGENCY LIGHT INOP. (FLT 6219) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,251 hrs · 9,477 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 5776) RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,629 hrs · 9,707 cycles

FS 280 FLOORBEAM CRACKED. (C CHECK) REPAIRED PER REO.

Part: ROD — LOOSE (SERVICE DOOR) · airframe 14,759 hrs · 9,189 cycles

SERVICE DOOR WILL NOT OPEN. (FLT 6573) RE-SECURED DOOR LIFTING ROD.

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 14,146 hrs · 8,819 cycles

LEFT ENGINE YOKE LINK BOLT BUSHING CORRODED. (ENG CHG) REPLACED BOLT BUSHING PER AMM.

Part: CABLE — WORN (CABIN DOOR) · airframe 14,054 hrs · 8,766 cycles

MAIN CABIN DOOR WILL NOT CLOSE. (FLT 6061) REPLACED OUTER HANDLE FLAP CABLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,016 hrs · 8,744 cycles

ONE (1) OF THE EXIT LIGHTS AT LEFT OVERWING EXIT, DOES NOT ILLUMINATE. (FLT 6478) RELAMPED LIGHT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,283 hrs · 8,326 cycles

FLT 6033, RIGHT WINDSHIELD CRACKED IN CRUISE. REPLACED WINDSHIELD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,509 hrs · 7,876 cycles

FLT 6732 - EMERGENCY EXIT SIGN ABOVE FA FLASHLIGHT INOP. RELAMPED.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 10,599 hrs · 6,713 cycles

EMERGENCY EXIT LIGHT COVER IS MISSING NEAR SERVICE DOOR. FLIGHT 6343. REPLACED LENS FOR SERVICE DOOR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,348 hrs · 4,773 cycles

STA 280 FLOORBEAM SUPPORT IS CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS AND BEAM AT STA 280 PER CRJ7/9 SRM 51-42-06-001-001 AND REO:670-53-11-242.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 7,348 hrs · 4,773 cycles

AFT COCKPIT FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. REPLACED COCKPIT FLOOR SUPPORT PER SB670-53-026.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 6,065 hrs · 3,975 cycles

FLOOR-LEVEL LIGHTED EXIT SIGN AT ROW 18 ON RIGHT SIDE IS OUT. REPLACED BATTERY CHARGER PER AMM 33-51-17. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 5,945 hrs · 3,895 cycles

FOUND RIGHT MID FUSELAGE LOWER EMERGENCY LIGHT PLACARD WON`T ILLUMINATE. REPLACED NR 4 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD IAW CRJ 200 MM 33-51-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 5,119 hrs · 3,364 cycles

3RD BACK CABIN EMERGENCY LIGHTS CEILING FLOOD LIGHT OUT. RELAMPED 3RD BACK CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: WIRE — DISCONNECTED (CABIN) · airframe 3,690 hrs · 2,455 cycles

EMERGENCY LIGHTS ON FORWARD RIGHT WIND SCREEN ARE INOP. RECONNECTED WIRES TO FORWARD RIGHT WINDSCREEN. OPERATIONAL CHECKS GOOD PER MM 33-51-01.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 4,316 hrs · 2,849 cycles

PAX DOOR AFT DRAG ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS TO AFT DRAG ANGLE ON PAX DOOR PER CRJ700 SRM 51-42-11 PG 4; 51-42-06 PG 7 AND RII52-401.

Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 3,319 hrs · 2,213 cycles

FLAPS HALFSPEED STATUS MSG. REPLACED LT I/B SKEW DETECTOR PER CRJ MM 27-52-45. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 2,524 hrs · 1,661 cycles

EMERGENCY LIGHTS EXIT SIGNS DON'T LIGHT ON BULKHEAD 1ST CLASS AND ON CEILINGS ROW 12. REPLACED NR 2 EMERGECNY BATTERY IAW 33-51-17. OPERATIONAL CHECKS GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,129 hrs · 1,376 cycles

CABIN EMERGENCY LIGHTS BETWEEN BUSINESS CLASS AND COACH ON BULKHEAD BOTH INOP. INSTALLED NEW FUSE FOR BATTERY PACK 2 CHARGER. OPERATIONAL CHECK GOOD IAW CRJ 700 AMM 33-51-00; 33-51-17.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 1,727 hrs · 1,103 cycles

"SSCU 1 FAULT" AND "SPL/STAB FAULT" STATUS MSGS. REPLACED NR 1 SSCU IAW CRJ MM 27-41-00. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NR 2) · airframe 1,683 hrs · 1,075 cycles

FLAPS FAILED AT 20 DEGREES. REPLACED LEFT NR 2 ACTUATOR PER CRJ MM 27-52-09. OPERATIONAL CHECK GOOD.

Part: DETECTOR — MALFUNCTIONED (FLAPS) · airframe 1,541 hrs · 974 cycles

FLAPS HALFSPEED STATUS MESSAGE DURING TAXI. REPLACED RIGHT WING OUTBOARD FLAP SKEW DETECTOR FOR NR 1 SFCU IAW MM 27-52-45. OPERATIONAL CHECK GOOD.

Part: FLAP SYSTEM — OUT OF RIG (TE FLAPS) · airframe 1,470 hrs · 934 cycles

FLAPS FAIL MESSAGE ON CLIMB-OUT. CLEARED INHIBITS. ELECTRICALLY RIGGED FLAPS. OPERATIONAL CHECK GOOD.

Part: SPRING — MALFUNCTIONED (FLAP ACTUATOR) · airframe 1,363 hrs · 854 cycles

"FLAPS FAIL" MESSAGES. RESET FLAP ACTUATOR (RT) SPRING TYPE INDICATOR IAW CRJ MM 27-52-09-610-802-A01. OPERATIONAL CHECK GOOD.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 1,270 hrs · 790 cycles

FLAPS FAIL CAUTION MESSAGE ON GROUND. REPLACED FLAP PDU IAW MM 27-52-37. OPERATIONAL CHECK GOOD, PN 766359B, SNOFF 0543.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 838 hrs · 497 cycles

RUDDER LIMIT FAULT STATUS MESSAGE ON CLIMBOUT. REPLACED NR 1 SSCU IAW 27-61-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 781 hrs · 463 cycles

STAB/SPOILER FAULT WILL NOT CLEAR. REPLACED NR 2 SSCU WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD AMM 27-61-05.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 332 hrs · 189 cycles

RUDDER LIMIT FAULT STATUS MESSAGE. REPLACED NR 1 RUDDER LIMITER ACTUATOR (A203) IAW CRJ MM 27-25-03. OPERATIONAL CHECK GOOD. P/N BA670-93490-3, S/N OFF 0513.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 124 hrs · 55 cycles

STAB CH 2 INOP STATUS MESSAGE. REPLACED NR 2 SSCU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. P/N C13045BA03, S/N OFF 826.