N693BR

Part: RIB — DAMAGED (ZONE 500) · airframe 37,136 hrs · 38,349 cycles

L/H WING TIP HAS ELONGATED HOLES INBD AND OUTBD SIDES OF 600-15107-3 RIB AND 600-15116-11 RIB (C-CHECK RO 04/17/2025)REPLACED LH WING TIP RIB P/N: 600-15116-11 REF CRJ-200 SRM 51-42-21, SRM 51-42-15 AND DWG 600-15110 REV. -E FOR FASTENER CALL OUT COMPLIED WITH ALL STEPS OF REO 601R-57-31-1448 REV. -- DATED: 2025-04-16 AND COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: STRINGER — CORRODED (ZONE 100) · airframe 37,136 hrs · 38,349 cycles

WHILE PERFORMED THE REPAIR FOR EXTERIOR LOWER SKIN FS700 STG21L FOUND STRINGER 21L AT FS 693 CORRODED AND MISSING MATERIAL AT FS 700, (C-CHECK RO 04/17/2025)COMPLIED WITH REPAIR TO STRINGER 21L AT FS 693 REF. CRJ-200, SRM 53-00-03, REV. 39, MAR 10/2021 AND CRJ-200, SRM 51-42-06, REV. 39, MAR 10/2021. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: BRACKET — CORRODED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

BRACKET LOCATED AT INTERCOSTAL AFT DD4 IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW BRACKET LOCATED AT INTERCOSTAL AFT DD4 IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: ANGLE — GOUGED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

AFTER REMOVING SUPPORT PN 601R35210-17 FROM FS672.20 STGR4L IN AFT EQUIPMENT BAY, DISCOVERED CLIP PN 601R35210-37 IS GOUGED. (C-CHECK RO 04/17/2025)REMOVED CLIP PN 601R35210-37 AT FS672.20 STGR4L IN AFT EQUIPMENT BAY PER CRJ200 SRM 51-42-06. AND INSTALLED REPLACEMENT CLIP PN 601R35210-37 AT FS672.20 STGR4L IN AFT EQUIPMENT BAY PER BOMBARDIER ENG DWG 601R35210 REV M, CRJ 200 SRM 51-42-06-00 REV 39 MAR 10/21COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: CLEAT — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

(MX 29800895 ) PAX DOOR CLEAT COMMON TO FRAME F/S 313.56 IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR CLEAT COMMONB TO FRAME F/S 313.56 IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N AND COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SKIN — GOUGED (ZONE 600 FLAP) · airframe 37,136 hrs · 38,349 cycles

GOUGE FOUND AT RH INBD FLAP (MARKED) MX 29796578 (C-CHECK RO 04/17/2025)COMPLIED WITH REO 601R-57-52-2513 REV -- DATE 2025-03-18 REPAIR TO THE RH INBD FLAP.

Part: SUPPORT ANGLE — GOUGED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

UPON REMOVAL OF PAX DOOR FWD PULL-IN LEVER FOUND DEEP GAUGE ON PAX DOOR ANGLE SUPPORT (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR FWD ANGLE SUPPORT IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: ANGLE — CORRODED (ZONE 600) · airframe 37,136 hrs · 38,349 cycles

FOUND CORROSION ON ANGLE P/N 601R10203-34, AT RH BATT RIB, WS53.60. (C-CHECK RO 04/17/2025)ANGLE P/N 601R10203-34. FOUND OUT OF LIMITS IAW CRJ 200 SRM 57-21-12. REMOVED AND INSTALLED NEW ANGLE P/N 601R10203-34, REF.DWG 601R10203, REV -G, CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21. COMPLIED WITH SKYWEST TASK CARD 51-900-1003.

Part: CLEAT — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29790418 ) PAX DOOR QTY 2 CLEATS ARE CORRODED COMMON TO MID DD6 INTERCOSTAL (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED QTY 2 NEW CLEATS COMMON TO MID DD6 INTERCOSTAL IAW CRJ 200 SRM 51-42-06, 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: FITTING — DAMAGED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29783684 ) PAX DOOR AFT MID PIN FITTING PREVIOUSLY REPAIRED QTY 1 OVER SIZE AND ELONGATED FASTENER HOLE (C-CHECK RO 04/17/2025)REPAIRED PAX DOOR AFT MID PIN FITTING IAW REO 601R52-11-3053 REV. -- DATED 2025-03-21 ALL STEPS COMPLIED WITH.

Part: DOUBLER — GOUGED (ZONE 100) · airframe 37,136 hrs · 38,349 cycles

UPON OPENING UPPER SKIN FOR ACCESS TO REPLACE MISSING FASTENER COLLAR (MX 29731975 HN00223848, EXISTING DAMAGE FOUND, THE INNER DOUBLER FOUND GOUGED THROUGH IN SEVERAL SPOTS. (C-CHECK RO 04/17/2025)THE R/H ELEVATOR DOUBLER (PN 601R24026-35) THAT WAS DAMAGED FROM ES8.89 TO ES 48.583, COMMON TO THE UPPER FLANGE OF THE FRONT SPAR HAS BEEN REPAIRED BY WAY OF REO STEPS 1, CUT AWAY DAMAGE, 2, REMOVED BURRS AND SHARP EDGES, 3, NDT PERFORMED ON CUTLINE, 4, FABRICATED REPAIR PARTS, 5, FINISH CODES APPLIED, 6, TOUCH UP CUT LINES, 7AND 8 , MAINTAINED E.D. AND PITCH, 9, INSTALLED FASTENERS REF SRM, 10, MANUFACTURED REPAIR PAT SAME AS ORIGINAL, 11, WET INSTALLED ALL PARTS AND 12, MADE FROM 2024-T3 REF REO# 601R-55-21-605, REV --, DATED 3/25/25.

Part: ANGLE — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29777211 ) PAX DOOR CLIP AT F/S 339.00 IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR CLIP AT F/S 339 IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. LEAK CHECKS PASSED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: ANGLE — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29777052 ) PAX DOOR CLIP AT F/S 321.00 IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR CLIP AT F/S 321.00 IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. LEAK CHECKS PASSED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29776728 ) PAX DOOR AFT DD4 INTERCOSTAL IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW AFT DD4 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29776619 ) PAX DOOR AFT DD5 INTERCOSTAL IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND REPLACED PAX DOOR AFT DD5 INTERCOSTAL REF CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: ANGLE — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29777018 ) PAX DOOR CLIP AT F/S 320.00 IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR CLIP AT F/S 320 IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. LEAK CHECKS PASSED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29776757 ) PAX DOOR AFT DD3 INTERCOSTAL IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR AFT DD 3 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. LEAK CHECKS PASSED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

(MX 29776582 ) PAX DOOR MID DD3 INTERCOSTAL IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND REPLACED PAX DOOR MID DD3 INTERCOSTAL REF CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: ANGLE — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29777177 ) PAX DOOR CLIP AT F/S 338.00 IS CORRODED (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR CLIP AT F/S 338.00 IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. LEAK CHECKS PASSED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: INTERCOSTAL — CRACKED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29771383 ) SUSPECTED CRACK ON PAX DOOR FWD DD1 INTERCOSTAL (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW FWD DD1 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. LEAK CHECKS PASSED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD WITH DETAILS.

Part: DOUBLER — CRACKED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29771555 ) PAX DOOR SUSPECTED CRACK ON FWD PULL IN CAM DOUBLER (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW FWD PULL IN CAM DOUBLER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N AND COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: INTERCOSTAL — CRACKED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29771580 ) PAX DOOR SUSPECTED CRACK ON AFT DD7 INTERCOSTAL (C-CHECK RO 04/17/2025)REMOVED AND REPLACED PAX DOOR AFT DD7 INTERCOSTAL REF CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: INTERCOSTAL — CRACKED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29771444 ) PAX DOOR SUSPECTED CRACK ON AFT DD1 INTERCOSTAL (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR AFT DD1 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. LEAK CHECK PASSED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: DOUBLER — CRACKED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29771567 ) PAX DOOR SUSPECTED CRACK ON AFT PULL IN CAM DOUBLER (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW AFT PULL IN CAM DOUBLER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N AND COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: STOP FITTING — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

AFT CARGO DOOR BOTTOM STOP FITTINGS, 2EA ON THE SILL, ARE CORRODED (MARKED) (C-CHECK RO 04/17/2025)REMOVED CORROSION FROM 2EA LOWER STOP FITTINGS FROM AFT CARGO DOOR SILL.REF CRJ 200 SRM 51-21-06 REPAIRED PER REO 601R-53-61-8310 REV - - DATED 2025-04-03. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. OP CHECK GOOD. FITS AND CLEARANCE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: SUPPORT ANGLE — DAMAGED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

( MX 29761901 ) PAX DOOR AFT ANGLE SUPPORT PREVIOUSLY REPAIRED EXTRA FASTENERS HOLES EXIST REQUIRE REPLACEMENT (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR AFT ANGLE SUPPORT IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: FORMER — DAMAGED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

(MX 29761883 ) PAX DOOR AFT FORMER PREVIOUSLY REPAIRED WITH OVER SIZE FASTENERS HOLES REQUIRE REPLACEMENT (C-CHECK RO 04/17/2025)REMOVED AND REPLACED PAX DOOR AFT FORMER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

PILOT WINDSHIELD SIDE POST LOWER AFT ATTACH FITTING IS CRACKED (MARKED) (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED 1EA NEW L/H WINDSHIELD SIDE POST SUPPORT ANGLE P/N 601R33235-3 PER CRJ200SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: CLEAT — CRACKED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

CENTER POST RH LOWER CLEAT CRACKED AS MARKED (C-CHECK RO 04/17/2025)REMOVED AND REPLACED CENTER POST RH LOWER CLEAT WITH A NEW SERVICEABLE UNIT REF CRJ 200 SRM 51-42-21 AND DWG 601R33007 REV U. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: CHANNEL — CRACKED (ZONE 600) · airframe 37,136 hrs · 38,349 cycles

RH WING CHANNEL P/N 601R10203-28 IS CRACKED MX# 29743099 (C-CHECK RO 04/17/2025)REPAIRED RH WING BATT RIB WS53.6 PER REO 601R-57-51-046, REV. -B, DATE: 2002-02-28. COMPLIED WITH SKYWEST TAS CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 37,136 hrs · 38,349 cycles

AFT EQUIPMENT BAY BELOW APU INLET DOOR AT FS 672.20 SUPPORT P/N 601R35210-17 IS CRACKED AT LOWER AFT CORNER (MARKED) (C-CHECK RO 04/17/2025)REMOVED AND REPLACED AEB BELOW APU INLET DOOR AT FS672.20 SUPPORT P/N 601R35210-17 WITH A NEW SERVICEABLE UNIT REF CRJ DWG 601R35210 REV M, AND CRJ 200 SRM 51-42-06. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: HINGE ARM — GOUGED (ZONE 600) · airframe 37,136 hrs · 38,349 cycles

RIGHT OUTBOARD FLAP HINGE ARM AT WS220.00 GOUGED NEAR LOWER ATTACH FITTING AS MARKED (C-CHECK RO 04/17/2025) BLENDED GOUGE AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 601R-57-54-374 REV -- DATE 2025-03-17. SEE CONTINUATION CARD FOR DETAILS.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

PASSENGER DOOR HAS CORROSION ON DD6 BETWEEN FS320.10 - FS329.476 AS MARKED (C-CHECK RO 04/17/2025)REMOVED AND REPLACED PAX DOOR MID DD6 INTERCOSTAL REF CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 37,136 hrs · 38,349 cycles

REAR RIB SUPPORT ANGLE ON AUX SPAR CRACKED IN R/H MLG W/W MARKED (C-CHECK RO 04/17/2025)REPLACED WITH NEW FABRICATED CHANNEL P/N 601R10203-8. REF CRJ200 SRM 51-42-06 , CRJ200 SRM 51-42-21 AND DWG#601R10203 REV-G. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLLIED WITH.

Part: LUG — DAMAGED (ZONE 600) · airframe 37,136 hrs · 38,349 cycles

TOOLING MARKS NOTED AT R/H OTBD FLAP HINGE BOX AT WS178 CENTER LUGS AND ASSY. (MARKED) (C-CHECK RO 04/17/2025)BLENDED DAMAGE AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 601R-57-21-3912 REV -- DATE 2025-03-17. SEE CONTINUATION CARD FOR DETAILS

Part: VANE — CHAFED (ZONE 500 FLAP) · airframe 37,136 hrs · 38,349 cycles

CHAFING NOTED ON L/H INBD FLAP VANE CAP AT INBD CAP ASSY. (MARKED) (C-CHECK RO 04/17/2025)REPLACED L/H INBD FLAP VANE CAP AT INBD CAP ASSY P/N 601R14303-53, REF. DRW 601R14302, REV. E, AND CRJ-200, SRM 51-42-13, REVISION 39, MAR 10/2021. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: SKIN — ERODED (ZONE 500 FLAP) · airframe 37,136 hrs · 38,349 cycles

EROSION NOTED ON L/H INBD FLAP LOWER SKIN BETWEEN FLS15-FLS40.00 (MARKED) (C-CHECK RO 04/17/2025)REMOVED DAMAGE AND EVALUATED WITHIN LIMITS 2EA AREAS REWORKED ON SKIN ONLY AT L/H INBD FLAP LOWER SKIN BETWEEN FLS15-FLS40.00, REF. CRJ-200, SRM 57-52-00 AND REMOVED AND REPLACE 2EA DOUBLER REPAIRS AT L/H INBD FLAP LOWER SKIN BETWEEN FLS15-FLS40.00, REF. CRJ-200, SRM 57-52-00 REPAIR NO. 3 AND SRM 51-42-13. M337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

CORROSION NOTED AT PAX DOOR MID INTERCOSTAL DD4 (MARKED) (C-CHECK RO 04/17/2025)REMOVED AND REPLACED PAX DOOR MID DD4 INTERCOSTAL REF CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: VANE — CHAFED (ZONE 500 FLAP) · airframe 37,136 hrs · 38,349 cycles

CHAFING NOTED ON L/H INBD FLAP VANE CAP AT INBD CAP ASSY. (MARKED) (C-CHECK RO 04/17/2025)REPLACED L/H INBD FLAP VANE CAP AT INBD CAP ASSY P/N 601R14303-53, REF. DRW 601R14302, REV. E, AND CRJ-200, SRM 51-42-13, REVISION 39, MAR 10/2021. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,136 hrs · 38,349 cycles

FS589.0 FORWARD FLANGE HAS MULTIPLE AREAS OF CORROSION BETWEEN STGR19L AND STGR20R (C-CHECK RO 04/17/2025)REPAIRED DAMAGE BY BLENDING AT F.S. 589.00 FRAME BETWEEN STR 19L AND STR 20R REF REO 601R-53-61-8307 REV -- DATED 2025-03-31 COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECKS PASSED. SEE CONTINUE CARD FOR DETAILS.

Part: FRAME — CORRODED (ZONE 100) · airframe 37,136 hrs · 38,349 cycles

CORROSION ON FORWARD SIDE OF FS700 BETWEEN STGR24L AND STGR23L AS MARKED (C-CHECK RO 04/17/2025)REMOVED AND REPLACED SECTION FRAME P/N: 600-36029-9, ON FORWARD SIDE OF FS700 BETWEEN STGR24L AND STGR23L, REF. DRW 600-36029, REV. D AND CRJ-200 SRM 51-42-06, REVISION 39, MAR 10/2021. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH

Part: SKIN — DEFORMED (ZONE 100) · airframe 37,136 hrs · 38,349 cycles

EXTERIOR LOWER SKIN PANEL, FS700 STG21L, PREVIOUS REPAIR IS DEFORMED, HN00223204 (C-CHECK RO 04/17/2025)COMPLETED REPAIR STEPS 1 TO16 FOR DOUBLER REPAIR AND SECTION FRAME OF REF. REO 601R-53-61-8299 REV --, DATE 2025-04-10 AND DWG 600-36029, REV. D. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

SERVICE DOOR FLOOR SUPPORT ANGLE IS CORRODED FS319.00 - 364.00. (MARKED) (C-CHECK RO 04/17/2025)REMOVED AND REPLACED AND INSTALLED NEW SERVICE DOOR FLOOR SUPPORT ANGLE P/N:601R38303-253. PER DWG. 601R38303 REV. AR AND PER REF.CRJ/200 SRM 51-42-06, REF.CRJ/200 SRM 51-42-21 AND REF.CRJ/200 SRM. 51-42-34. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

LH PRESSURE FLOOR SILL ANGLE IS CORRODED IN SEVERAL SPOTS FS409+128 €“ 559 (C-CHECK RO 04/17/2025)REPAIRED LH PRESSURE FLOOR SILL ANGLE AS PER MHIRJ REO 601R-53-41-666 REV C DATED 2012-11-06. SEE CONTINUE CARD FOR DETAILS.

Part: ANGLE — CRACKED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

LH FS484 CLIP IS CRACKED AT LBL36 (C-CHECK RO 04/17/2025)REMOVED AND REPLACED CLIP AT LH FS484 LBL36 REF REO 601R-53-41-059 REV: C DATED: 2020-03-11 STEPS 5-14, CRJ200 SRM 51-42-06, AND CRJ200 SRM 51-42-21. PRESSURE LEAK CHECK PASSED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

RH PRESSURE FLOOR SILL ANGLE IS CORRODED IN SEVERAL SPOTS FS409+128 €“ 559 (C-CHECK RO 04/17/2025)REPAIRED RH PRESSURE FLOOR SILL ANGLE AS PER MHIRJ REO 601R-53-41-666 REV C DATED 2012-11-06. SEE CONTINUE CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

RH PRESSURE FLOOR SIL PNL IS CORRODED IN SEVERAL SPOTS FS409+128 €“ 559 (C-CHECK RO 04/17/2025)BLENDED OUT CORROSION IN MULTIPLE AREAS ON RH SIED PRESSURE FLOOR SILL PANEL BETWEEN FS409+128-FS559.00 DISTANCE BETWEEN BLEND #2 AND #3 IS 3.562" IS OUT-OF-LIMITS IAW REO 601R-53-41-666, REV-C, DATE: 2012-11-06. REPAIRED PER REO 601R-53-41-3297, REV --, DATED 2025-03-13. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

LH PRESSURE FLOOR SIL PNL IS CORRODED IN SEVERAL SPOTS FS409+128 €“ 559 (C-CHECK RO 04/17/2025)REMOVED CORROSION BY BLENDING AT BLENDS #3, #4, #5, #6. FOUND TO BE WITHIN LIMITS. REF REO 601R-53-41-666 REV C DATED 2012-11-06. REPAIRED BLENDS #1 AND #2. REF REO 601R-53-41-3297, REV --, DATED 2025-03-13. PERFORMED PRESSURE LEAK CHECK OF THE LH SIDE PRESSURE FLOOR SILL PANEL BETWEEN FS409+128-FS559.00. LEAK CHECK PASSED. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: CAM — CHAFED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

PASSENGER DOOR SURROUND PULL IN CAM AT FS310 CHAFED (C-CHECK RO 04/17/2025)REMOVED AND REPLACED PASSENGER DOOR SURROUND PULL-IN CAM P/N 600-31688-17 AT FS310 PER DWG NO 600-31900 REV K, AND CRJ200 SRM 51-42-21. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: STOP FITTING — GROOVED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

AFT CARGO DOOR OPENING ON FS574.00 UPPER AND LOWER STOPS GROOVED. (C-CHECK RO 04/17/2025) REMOVED DAMAGE AT AFT CARGO DOOR OPENING ON FS574.00 UPPER AND LOWER STOPS,. FOUND OUT OF LIMITS. REPAIRED PER REO 601R-53-61-8306, REV --, 2025-03-17. FITS AND CLEARANCE CHECK GOOD. OP CHECK GOOD. ADJUSTMENT CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: CAM — GOUGED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

PASSENGER DOOR SURROUND PULL IN CAM AT FS349 GOUGED (C-CHECK RO 04/17/2025)REMOVED AND INSTALLED NEW PAX DOOR SURROUND PULL IN CAM FITTING AT 349 REF DWG 600-31900 REV K AND CRJ 200 SRM 51-42-21. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 37,136 hrs · 38,349 cycles

LBL9 FLOOR BEAM IS CORRODED ON THE INBD AND OTBD FLANGES IN SEVERAL LOCATIONS FS417 €“ 513 (C-CHECK RO 04/17/2025)REPAIRED LBL 9 FLOOR BEAM CORROSION ON FLANGES AS PER REO 601R-53-41-3298 REV -- DATED 2025-03-28. ALL STEPS OF REO COMPLIED WITH. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS.

Part: CUP — CORRODED (ZONE 800) · airframe 37,136 hrs · 38,349 cycles

FWD AND AFT PAX DOOR HANDRAIL CUPS ARE CORRODED (C-CHECK RO 04/17/2025)REMOVED AND REPLACED FWD AND AFT PAX DOOR HANDRAIL CUPS P/N: 601R31527-217 REF CRJ200 SRM 51-42-06 AND 51-42-10 DWG 601R31527 REV. AM. COMPLIED WITH ATTATCHED SKYCARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: FORMER — CRACKED (PAX DOOR) · airframe 36,221 hrs · 37,382 cycles

CRACK APPROX. 3" LONG ON PASSENGER DOOR OUTER FORMER AT FS347.25 JUST AFT OF POWER ASSIST PULLEY WHEEL BRAKET. DAMAGE MEETS THE CRITERIA CLASSIFYING IT AS A MAJOR REPAIR. (FILED CLOSED)COMPLIED WITH REO 601R-52-11-3008 REV -- DATED 2024-02-12 MAJOR REPAIR OF THE PAX DOOR FORMER FS347.25 UNDER PULLEY MOUNTING BRACKET AND. COMPLIED WITH MAJOR REPAIR.

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 35,995 hrs · 37,134 cycles

WHEN SELECTING THE GEAR UP AFTER TAKEOFF RECEIVED NOSE DOOR OPEN WARNING FOLLOWED BY A GEAR DISAGREE WARNING MESSAGE. QRH CLEARED MESSAGES. RETURN TO FIELD. (FLIGHT 4739 FILED CLOSED)C/W PSEU FAULT LOG AND FOUND S23 FAR IN FLIGHT. INSPECTED NLG AND FOUND S23 (NLG OLEO CENTERED/EXTEND) SENSOR AND MOUNTING BRACKET DAMAGED. REMOVED AND REPLACED WOFFW #2 HARNESS ASSEMBLY AS WELL AS THE NLG OLEO CENTERED/EXTEND SENSOR MOUNTING BRACKET PER CRJ200 AMM 32-61-05 AND AMM 32-61-05. COMPLIED WITH RETRACTION AND EXTENSION OF THE NLG PER CRJ200 AMM 32-30-00. NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECKS OF THE PROXIMITY SENSOR SYSTEM PER CRJ200 AMM 32-61-00 AND OPERATIONAL CHECKS OF THE NOSEWHEEL STEERING SYSTEM CRJ200 AMM 32-51-00. ALL OPERATIONAL CHECKS GOOD AT THIS TIME.

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 35,785 hrs · 36,919 cycles

STEARING INOP FOLLOWED BY GEAR DISAGREED AFTER TAKEOFF. CHECKLIST RESOLVED. RETURNED TO AIRPORT. (FLIGHT 5178 FILED CLOSED)

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 35,781 hrs · 36,916 cycles

STEARING INOP FOLLOWED BY GEAR DISAGREED AFTER TAKEOFF. CHECKLIST RESOLVED. RETURNED TO AIRPORT. (FLIGHT 5178 FILED OPEN)

Part: NOT REPORTED — CRACKED (NOT REPORTED) · airframe 34,596 hrs · 35,765 cycles

AFTER TAKEOFF OUT OF ORD A CRACK STARTED IN THE UPPER RIGHT HAND CORNER OF FIRST OFFICER€™S FORWARD WINDSHIELD. THERE IS ALSO A CONSIDERABLE AMOUNT OF DELAMINATION ON THE UPPER PORTION OF THE RIGHT FORWARD WINDSHIELD WITH ANOTHER CRACK BEGINNING TO DEVELOP. (FILED CLOSED)REMOVED AND REPLACE FO FORWARD WINDSHIELD IN REF WITH AMM 56-11-01. COMPLIED WITH TASK CARD 56-220-1000-SKY.LEAK CHECK GOOD AT THIS TIMEPLEASE REFERENCE AML 1075795

Part: NONE — SHUTDOWN · airframe 34,117 hrs · 35,318 cycles

IN CRUISE LEFT ITT IMMEDIATELY INCREASE 900+ FLASHING RED, LEFT ENGINE SPUTTERS, N1 DROPS TO ABOUT 30% AND STAYS. LEFT ENGINE WARNING MESSAGE APPEARS. RUN QRC/QRH FOR LEFT ENGINE SHUT DOWN. NO SMOKE. NO VISIBLE DAMAGE. (FLIGHT 5730 - FILED CLOSED) DUE TO ANALYZED FDR DATA SHOWING ITT OVER 900 C FOR 169 SECS WITH MAX OF 1160 C. ENGINE CHANGE REQUIRED PER AMM 72-00-00-200-801. SEE AML 1010152 FOR ENGINE CHANGE.

Part: NONE — BROKEN · airframe 32,956 hrs · 34,280 cycles

LEFT ELEVATOR FLUTTER DAMPER REAR BOLT ACCESS PANEL, ON FORWARD LOWER EDGE OF THE LEFT ELEVATOR, OUTBOARD FORWARD SCREW NUTPLATE MOUNTING TAB BROKEN. (FILED CLOSED) REPLACED LH ELEVATOR ASSY IN REFERENCE TO CRJ200 AMM 27-34-01 AND 27-900-1004-SKY / TORQUE WRENCH SN: 218034073 CAL DUE: 11/30/2022 / TORQUE WRENCH SN: 0618101471 CAL DUE: 11/30/2022 / TORQUE WRENCH SN: 0314802037 CAL DUE: 08/31/2022

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 32,159 hrs · 33,593 cycles

SCRATCH /GOUGE IN LH LOGO NEAR MED (C-CHECK RO 8/5/2021) REMOVED DAMAGE BY BLENDING AND REMOVING DENT IAW BOMBARDIER REO 601R-51-00-309 REV -A DATED 2017-08-23 AND MHIRJ REO 601R-53-21-3476 REV -- DATED 2021-08-04. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: RIB — CRACKED (RT NACELLE) · airframe 32,159 hrs · 33,593 cycles

RIB OF RH PYLON AT F.S. 605.00 IS CRACKED IN UPPER O/B CORNER. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED RH PYLON RIB IAW CRJ200 SRM 51-42-06 AND REF BOMBARDIER DRAWING #601-37004 REV R. / FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: STIFFENER — CRACKED (BS 621) · airframe 32,159 hrs · 33,593 cycles

ANGLE COMMON TO F.S 621 BULKHEAD AT LBL36, APROX WL 75 FOUND TO BE CRACKED. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED STIFFENER IAW CRJ200 SRM 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: TRUNNION — CRACKED (RT MLG) · airframe 32,159 hrs · 33,593 cycles

RH MLG TRUNION HAD 3 INDICATIONS NOTED WHILE PERFORMING BOMBARDIER SB 601R-57-046 AT THE 3RD, 4TH AND 5TH HOLES AFT OF THE FWD HOLE ALL AT 55% FULL SCREEN HEIGHT FAILING NDT. (C-CHECK RO 8/5/2021) REPAIRED RH MLG TRUNNION 3 INDICATIONS IAW REO 601R-57-21-3477 REV -- DATED 2021-06-19 & SKY CARD 51-900-1003-SKY, NO WEIGHT CHANGE, FORM 337 IS ATTACHED

Part: TRUNNION — FAILED (LT MLG) · airframe 32,159 hrs · 33,593 cycles

LHS MLG TRUNION FITTING HAS 3 INDICATIONS NOTED WHILE PERFORMING BOMBARDIER SB 601R-57-046 AT THE 4TH, 5TH AND 8TH HOLE AFT OF THE FWD HOLE ALL AT 55% FULL SCREEN HEIGHT FAILING NDT. (C-CHECK RO 8/5/2021) PERFORMED REPAIR TO LHS MLG TRUNION FITTING BY COMPLETING ALL REPAIR STEPS FOR DISCREPANT HOLE AT THE 4TH, 5TH AND 8TH AFT OF THE FWD HOLE THAT ARE IDENTIFIED AS HOLE #15, #18 & #19 IAW REO 601R-57-21-3476 REV -- DATED 2021-06-05 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: BULKHEAD — DAMAGED (BS 621) · airframe 32,159 hrs · 33,593 cycles

ACCESS REQUIRED AT FS 621 FOR UNDERFLOOR REPAIRS (C-CHECK RO 8/5/2021) PERFORMED ACCESS AT FS621 BY REMOVING AND REINSTALLING LBL 9 FLOOR BEAM FITTING ASSY AT FS62 AND REMOVING AND INSTALLING WEB AT FS 610 BETWEEN LBL 9 AND RBL 9 IAW CRJ 200 SRM 51-41-02, 51-42-06, AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED 337. NO WEIGHT CHANGE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: FLOORBEAM — CORRODED (BS 589 LBL 9-27) · airframe 32,159 hrs · 33,593 cycles

CROSSBEAM CAP AT FS 589, LBL9 TO LBL 27 IS CORRODED BEYOND LIMITS, REQUIRES REPLACEMENT. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED CROSSBEAM CAP AT FS 589 LBL 9 TO LBL 27 IAW CRJ 200 SRM 51-40-11, 51-42-06, 51-42-15, AND 51-42-21 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: ANCHOR FITTING — CRACKED (AFT PAX DOOR) · airframe 32,159 hrs · 33,593 cycles

AFT ANCHOR FITTING AT PAX DOOR CUT-OUT IS CRACKED ON AFT SIDE (C-CHECK RO 8/5/2021) REMOVED AND REPLACED AFT ANCHOR FITTING IAW CRJ200 AMM 52-11-17-400-804, ADJUSTMENT AND OPS CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: HINGE — GOUGED (PAX DOOR) · airframe 32,159 hrs · 33,593 cycles

PAX DOOR PIANO HINGE FUSELAGE SIDE HAS 12 LANDS GOUGES IN MID SECTION AND MOST AFT LAND HAS GOUGE FROM ROLL PIN (AS MARKED) (C-CHECK RO 8/5/2021) AFT LUG LLAND ON PAX DOOR FUSE SIDE HINGE FOUND TO BE OUT OF LIMITS PER GREO 601R-53-21-814 REV C DATED 2017-08-02 TYPE IV REPAIR, STEP 2 AND ALSO DUE TO DAMAGE NOTED ON CP 22707200 (WVAC 5/168). REFER TO CP 22708181, WVAC 5/169, FOR REPLACEMENT FO THE FUSE SIDE HINGE.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 32,159 hrs · 33,593 cycles

PASSENGER DOOR FUSELAGE SIDE HINGE REQUIRES REPLACEMENT DUE TO DAMAGE TO THE AFT MOST LUG LAND AND ELONGATED HOLES AT THE FWD END AND AFT END OF THE HINGE THAT ARE BEYOND THE LIMITS OF GREO 601R-53-21-8814 REV C DATED 2017-08-02. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED PAX DOOR FUSELAGE SIDE HINGE IAW CRJ 200 SRM 53-21-23 & REO 601R-53-21-656 REV A DATED 2017/03/06, PRESSURE CHECK GOOD, REFER TO CONTINUE CARD FOR WORK PERFORMED. MAJOR REPAIR TASK 51-900-1003-SKY AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NEEDED, PART FOR PART REPLACEMENT.

Part: ANGLE — CRACKED (BS 280 S3L) · airframe 32,159 hrs · 33,593 cycles

STR 3L AT FS 280 IS CRACKED. (C-CHECK RO 8/5/2021) REMOVED DAMAGED ANGLE ON STRGR 3L AT FS 280. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE ANGLE IAW: CRJ200-SRM-51-42-06, 51-42-21, AND 51-40-11

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 32,159 hrs · 33,593 cycles

RH FLOOR SILL MULTIPLE SPOTS OF CORROSION FROM FS559.00+112 TO FS621.00 (C-CHECK RO 8/5/2021) REPAIRED RH FLOOR SILL MULTIPLE SPOTS OF CORROSION FROM FS559.00+112 TO FS621.00 IAW REO 601R-53-61-7662 REV.--, DATED 6/19/21, REO 601R-53-00-526 REV. --, DATED 5/22/13 AND REO 601R-53-61-5376 REV. A, DATED 10/25/18. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 32,159 hrs · 33,593 cycles

LH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS574.00 TO FS621.00 (C-CHECK RO 8/5/2021) REPAIRED LH FLOOR SILL, FS574-FS621 IAW REO 601R53-61-1574 REV. B, DATED 04/15/2012, CRJ200 SRM 51-42-06, 51-40-11 AND 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (BS 605-621) · airframe 32,159 hrs · 33,593 cycles

FLOOR BEAM AT RBL27 HAS CORROSION BETWEEN FS605.00 AND FS621.00 (C-CHECK RO 8/5/2021) REMOVED AND REPLACED FLOOR BEAM PN: 601R35031-263 WITH NEW FLOOR BEAM AT RBL 27 F.S 569-608 IAW MHIRJ REO 601R-53-61-7659 REV:-- DATE: 2021-6-4 STEPS 1-3 COMPLETED SEE CONTINUATION CARD FOR DETAILS. 51-900-1003 SKY COMPLIED WITH. COMPLETED SKYWEST M-337 AND M-131 FOR MAJOR REPAIR. NO CHANGE TO WEIGHT AND BALANCE.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 32,159 hrs · 33,593 cycles

CROSSBRAM CAP AT FS559.00+112 IS CORRODED IN MULTIPLE SPOTS BETWEEN RBL27 AND RBL45 (C-CHECK RO 8/5/2021) REMOVED AND REPLACED CROSSBEAM CAP AT FS559.00+ 112 BETWEEN RBL27 AND RBL45 IAW CRJ200 SRM 51-42-06 AND 51-42-15. TOPCOATED NEW CROSSBEAM CAP IAW CRJ200 SRM 51-25-16.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 32,159 hrs · 33,593 cycles

STRAP FROM FLOOR SILL TO PRESSURE FLOOR BEAM IS CORRODED AT FS 559. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED CORRODED STRAP WITH SERVICEABLE STRAP, IAW CRJ 200 SRM 51-42-06, 51-40-11. / NO DEFECTS NOTED BY MX

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 32,159 hrs · 33,593 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS 2 INDICATIONS NOTED 1) LBL9.5 WL76 1.5 INCHES LONG 100 FSH AND 2) LBL18 WL76 1 INCH LONG 90%FSH BOTH FAILED NDT INSPECTION (C-CHECK RO 8/5/2021) REPAIRED DAMAGE IAW MHIRJ REO 601R-53-61-7644 REV -- DATED 2021-06-14. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. WEIGHT CHANGE +.90LBS. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 32,159 hrs · 33,593 cycles

L/H FLOOR SILL IS CORRODED IN VARIOUS LOCATIONS FROM FS 409+128 TO FS 559. (C-CHECK RO 8/5/2021) BLENDED CORROSION, NDT INSPECTED, FOUND TO BE WITHIN LIMITS, RE FINISHED BLENDED AREAS. / ALL WORK ACCOMPLISHED IAW BOMBARDIER REO 601R-53-41-666, REV -C, DATED 2012-11-06.

Part: SEAT TRACK — CORRODED (BS 409-559 RBL 9) · airframe 32,159 hrs · 33,593 cycles

SEAT TRACK AT RBL 9 FROM FS 409+128 TO FS559 IS CORRODED (C-CHECK RO 8/5/2021) REMOVED AND REPLACED CABIN FLOOR SEAT TRACK AT RBL 9 FROM FS 409+128 TO FS559 IAW CRJ 200 AMM 53--01-11-000/400-802 REF CAMP #22876406 FOR FABRICATION OF THE TRACK REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: SEAT TRACK — CORRODED (BS 409-559 LBL 9) · airframe 32,159 hrs · 33,593 cycles

SEAT TRACK AT LBL9 IS CORRODED FROM FS 409+128 TO FS559. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED CABIN FLOOR SEAT TRACK AT LBL9 BETWEEN FS 409+128 TO FS 559.00 IAW CRJ 200 AMM 53-01-11-400-802 NOTE SEAT TRACK WAS FABRICATED UNDER CAMP # 22876411 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: STRAP — CORRODED (BS 559) · airframe 32,159 hrs · 33,593 cycles

STRAP FROM FLOOR SILL TO PRESSURE FLOOR BEAM IS CORRODED AT FS 559 RBL 36. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED STRAP IAW CRJ200 SRM 51-40-11 AND 51-42-06. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 32,159 hrs · 33,593 cycles

R/H FLOOR SILL HAS CORROSION IN VARIOUS LOCATIONS FROM 409+128 TO 559. (C-CHECK RO 8/5/2021) REMOVED CORROSION AND EVALUATED. REMAINING MATERIAL FOUND TO BE WITHIN LIMITS. IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 & SKY CARD 51-900-1003-SKY, NO WEIGHT CHANGE, FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 32,159 hrs · 33,593 cycles

FS 621 REAR PRESSURE BULKHEAD FWD FACE FOUND 6 INDICATIONS 1 BL 0 WL 134-128 50% FSH, 2 RBL 27 WL 107-111 40% FSH, 3RBL 18 WL 108-111 50% FSH, 4 RBL 18 WL 98-100 55% FSH, 5 BL 0 WL 97-116 100% FSH, 6 BL 0 WL 93-95 100% FSH FAILED NDT MARKED ON SKIN (C-CHECK RO 8/5/2021) REPAIRED DAMAGE IAW MHIRJ REO 601R-53-61-7644 REV -- DATED 2021-06-14 AND BOMBARDIER REO 601R-53-61-1240 REV D DATED 2016-10-31. REFERENCE CAMP 21955207 FOR COMPLETION OF REO 601R-53-61-1240 REV D DATED 2016-10-31 AND WEIGHT CHANGE. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (BS 349) · airframe 32,159 hrs · 33,593 cycles

FS 349 INTERCOSTAL RIVETS ARE CORRODED FROM LBL 27 - LBL 36 (C-CHECK RO 8/5/2021) REMOVED 9EA CORRODED RIVETS FROM THE FS 349 CROSSBEAM BETWEEN LBL 27 ANDLBL 36 AND INSTALLED 9EA NEW SERVICEABLE RIVETS IAW CRJ-200 SRM 51-42-13, APPLIED FINISH TO THE REPAIR AREA IAW CRJ-200 SRM 51-25-00

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 32,159 hrs · 33,593 cycles

SEAT TRACK AT LBL 9 FROM FS 394 TO FS 409+128 IS CORRODED. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED SEAT TRACK SEGMENT IAW CRJ200 AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: ANGLE — CORRODED (BS 280) · airframe 32,159 hrs · 33,593 cycles

FS 280 FWD "J" ANGLE IS CORRODED. (C-CHECK RO 8/5/2021) REMOVED DAMAGED FS 280 FWD 'J' ANGLE AND INSTALLED WITH NEW SERVICEABLE ANGLE IAW: CRJ200-SRM-51-42-06, AND 51-40-11

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,159 hrs · 33,593 cycles

RBL 9 BOTH INBD AND OUTBD CLIPS ARE CRACKED AT FS 280. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED CLIPS IAW CRJ-200-SRM-51-42-21

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 32,159 hrs · 33,593 cycles

SEAT TRACK AT RBL 0 FROM FS 394 TO FS 409+128 IS CORRODED. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED SEAT TRACK SEGMENT IAW CRJ200 AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 32,159 hrs · 33,593 cycles

LBL 9 BOTH INBD AND OUTBD CLIPS ARE CRACKED AT FS 280. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED CLIPS IAW CRJ-200-SRM-51-42-21

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 32,159 hrs · 33,593 cycles

SEAT TRACK AT RBL 9 FROM FS 364 TO FS 394 IS CORRODED. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED SEAT TRACK SEGMENT IAW CRJ200 AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 32,159 hrs · 33,593 cycles

SEAT TRACK AT LBL 9 FROM FS 364 TO FS 394 IS CORRODED. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED SEAT TRACK SEGMENT IAW CRJ200 AMM 53-01-11-400-802. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: WEB — CORRODED (PAX DOOR) · airframe 32,159 hrs · 33,593 cycles

PAX DOOR AFT SIDE WEB HAS MULTIPLE AREAS OF CORROSION ON THE FWD SIDE FROM TOP TO BOTTOM (C-CHECK RO 8/5/2021) REMOVED AND REPLACED PAX DOOR AFT WEB IAW CRJ 200 SRM 51-42-06.

Part: ANGLE — CRACKED (BS 621-625) · airframe 32,159 hrs · 33,593 cycles

R/H UPPER AND LOWER OBLIQUE ANGLES FS 621.00 TO FS 625.00 RBL 45.0 STR 14 AND 15 ARE CRACKED. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED R/H UPPER ANGLE FS 621.00 TO 625.00 RBL 45.0 STR 14 IAW REO 601R-53-61-422 REV NC DATE 2001-08-23 & SKY CARD 51-900-1003- SKY NO WEIGHT CHANGE, FROM 337 IS ATTACHED & REMOVED AND REPLACED R/H LOWER ANGLE FS 621.00 TO 625.00 RBL 45.0 STR 15 IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-20

Part: ANGLE — CRACKED (BS 621-625) · airframe 32,159 hrs · 33,593 cycles

L/H UPPER AND LOWER OBLIQUE ANGLES FS 621.00 TO 625.00 LBL 45 STR 14 AND 15 ARE CRACKED. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED L/H UPPER OBLIQUE ANGLE FS 621.00 LBL 45 STR 14 IAW BOMBARDIER REO 601R-53-61-422 REV NC DATED 2001-08-23 & SKY CARD 51-900-1003- SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED.REMOVED AND REPLACED L/H LOWER OBLIQUE ANGLE FS 621.00 LBL45 STR 15 IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-20

Part: BOLT — CORRODED (RT AILERON) · airframe 32,159 hrs · 33,593 cycles

RH AILERON OB HINGE ANTI MIGRATION BRACKET BOLTS 4EA ARE CORRODED. (C-CHECK RO 8/5/2021) REMOVED AND REPLACED R/H AILERON O/B HINGE ANTI MIGRATION BRACKET BOLTS 4EA WITH SERVICEABLE HARDWARE I.A.W. CRJ-200 AMM TASKS 20-21-00-910-801 AND 20-24-00-910-803.

Part: HINGE FITTING — CORRODED (RT AILERON) · airframe 32,159 hrs · 33,593 cycles

RH AILERON OB HINGE FITTING ON AFT SPAR IS CORRODED. (C-CHECK RO 8/5/2021) INSTALLED NEW SERVICABLE RH AILERON OB HINGE SACRIFICIAL PLATES IAW SNIEO 601R10064S06, CRJ-200 SRM 51-42-06 AND 51-41-02. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NUT PLATE — BROKEN (BELLY FAIRING) · airframe 32,159 hrs · 33,593 cycles

AFT BELLY FAIRING 196AL HAS 1EA BROKEN NUT PLATE. REPLACEMENT REQUIRED. (MARKED W/ TAPE) (C-CHECK RO 8/5/2021) PERFORMED REPAIR TO FUSELAGE SKIN AT BROKEN NUTPLATE AREA IAW MHIRJ REO 601R-53-51-589 REV. --, DATED 06/15/2021. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FAIRING — CHAFED (RT WING TE FLAP) · airframe 32,159 hrs · 33,593 cycles

RH FLAP STUB FARING IS CHAFED AND SEALS ARE WORN (C-CHECK RO 8/5/2021) REMOVED AND REPLACED R/H STUB FAIRING SKIN AND SEALS IAW CRJ200 SRM 51-42-06.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 32,159 hrs · 33,593 cycles

SERVICE DOOR THRESHOLD IS CORRODED BEYOND REPAIRABLE LIMITS ON THE THE UPPER FLANGE. NEEDS REPLACED (C-CHECK RO 8/5/2021) LOCATED , DRILLED AND INSTALLED NUTPLATES ON NEW SERVICE DOOR SILL THRESHOLD IAW CRJ 200 SRM 51-40-11 AND 51-42-06 . REFERENCE CONTINUE CARD FOR WORK PERFORMED . REFERENCE CP# 22291359 FOR INSTALL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,159 hrs · 33,593 cycles

EXTERIOR LOWER SKIN JUST AFT OF PNL 195 BB HAS CORROSION (C-CHECK RO 8/5/2021) REMOVED CORROSION ON EXTERIOR SKIN AFT OF PANEL 195BB IAW MHIRJ REO 601R-53-61-7653 REV -- DATED 2021-06-01 AND COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED FORM 337. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: BUSHING — CORRODED (SPOILER ACTUATOR) · airframe 32,159 hrs · 33,593 cycles

R/H WING O/B GROUND SPOILER ACTUATOR HAS CORRODED HARDWARE (C-CHECK RO 8/5/2021) REMOVED AND REPLACED THE RH OTBD GROUND SPOILER ACTUATOR HARDWARE IAW CRJ-200 AMM 27-63-01-000-801, 27-63-01-400-801. OPERATIONAL TEST IS GOOD AT THIS TIME.REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: BEARING — CORRODED (SPOILER ACTUATOR) · airframe 32,159 hrs · 33,593 cycles

L/H WING O/B GROUND SPOILER ACTUATOR HAS CORRODED HARDWARE (C-CHECK RO 8/5/2021) REMOVED AND REPLACED L/H WING O/B GROUND SPOILER ACTUATOR HARDWARE IAW CRJ 200 AMM 27-63-01-000-801, 27-63-01-400-801

Part: BUSHING — CORRODED (SPOILER ACTUATOR) · airframe 32,159 hrs · 33,593 cycles

R/H WING I/B GROUND SPOILER ACTUATOR HAS CORRODED HARDWARE (C-CHECK RO 8/5/2021) REMOVED AND REPLACED THE RH INBD GROUND SPOILER ACTUATOR HARDWARE IAW CRJ-200 AMM 27-63-01-000-801, 27-63-01-400-801. OPERATIONAL TEST IS GOOD AT THIS TIME. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: BEARING — CORRODED (SPOILER ACTUATOR) · airframe 32,159 hrs · 33,593 cycles

L/H WING I/B GROUND SPOILER ACTUATOR HAS CORRODED HARDWARE (C-CHECK RO 8/5/2021) REMOVED AND REPLACED THE LH INBD GROUND SPOILER ACTUATOR HARDWARE IAW CRJ-200 AMM 27-63-01-000-801, 27-63-01-400-801. OPERATIONAL TEST IS GOOD AT THIS TIME. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: FLAP SYSTEM — FAILED · airframe 31,876 hrs · 33,335 cycles

COMPLY WITH FULL FLAP EVAULATION PER CRJ 200 FIM AND FLAP FAIL AD 2009-06-12. FLAPS FAIL CAUTION ON FINAL APPROACH. FLAPS FAIL MESSAGE AFTER FLAPS SELECTED FROM 20 TO 30 AT 2400€™. RAN CHECKLIST AND LANDED WITH FLAPS 20.FEB 06, 2021 STATION: DSM--€ŒRESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 MCI CREATED FOR FULL AD COMPLIANCE BY MCC / FEB 08, 2021 STATION: COS--COMPLIED WITH PARAGRAPH (H)(6) OF THIS AD BY PERFORMING THE APPLICABLE MAINTENANCE ACTIONS SPECIFIED IN FAULT ISOLATION MANUAL (FIM) A-009, SECTION 27-50-00 OF VOLUME 1, REVISION 38, DATED JANUARY 10, 2008.

Part: ANGLE — WEAK (BS 559) · airframe 32,159 hrs · 33,593 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK RO 8/5/2021) COMPLIED WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS, REFERENCE CONTINUATION CARD , COMPLIED WITH 27-900-1008-SKY , 27-900-1000-SKY. TOTAL WEIGHT CHANGE +4.30 USING SCALE WVACTT#205055 CAL DATE 31MAR2022

Part: BULKHEAD — CRACKED (BS 621) · airframe 32,159 hrs · 33,593 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B€“AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7761, POSITION: (C-CHECK RO 8/5/2021) COMPLIED WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B€“AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. AND; MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. / COMPLIED WITH SERIAL NUMBER 7761.

Part: PRESSURE SWITCH — INACCURATE (APU OIL PRESSURE) · airframe 29,964 hrs · 31,607 cycles

APU OIL PRESS CAUTION IN FLIGHT. RAN QRH. RETURN TO FIELD PER QRH AND EXISTING GENERATOR DEFERRAL. INTERROGATED APU ECU AND FOUND 'LOP SDN' FAULT 129 TO BE FLAGGED IN ECU. VERIFIED OIL LEVEL WAS SUFFICIENT AND REMOVED AND REPLACED APU LOW OIL PRESSURE SWITCH IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: BYPASS VALVE — FAILED (NLG) · airframe 27,264 hrs · 29,207 cycles

GEAR DISAGREE WARNING MESSAGE FOR NOSE GEAR DURING GEAR RETRACTION. RAN QRH. DIVERTED TO NEAREST SUITABLE AIRPORT. REMOVED AND REPLACED NLG MANUAL RELEASE BYPASS VALVE IAW AMM. INSTALLED NEW SEAL IN NLG STRUT PISTON UPPER CAM ASSY IAW AMM. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 27,238 hrs · 29,179 cycles

AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. GEAR DISAGREE WARNING MESSAGE. RETURNED TO FIELD. REMOVED AND REPLACED NLG UPLOCK PROXIMITY SENSOR IAW AMM. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,212 hrs · 29,157 cycles

GEAR DISAGREE UPON TAKE OFF. DIVERTED. (FLT 5775) FO: 08/02/2018 CLOSED T/S NLG DISAGREE, NO DEFECTS NOTED AT THIS TIME. PERFORMED SEVERAL GEAR EXTENSIONS/RETRACTIONS WITH NO DEFECTS NOTED IAW AMM.

Part: FLOOR PANEL — CORRODED (BS 610) · airframe 26,655 hrs · 28,625 cycles

LBL 27 FLOOR SUPPORT CORRODED AT BS 610. REPAIRED IAW REO.

Part: DOOR SILL — CORRODED (BS 574-621) · airframe 26,655 hrs · 28,625 cycles

CARGO DOOR SILL CORRODED FROM BS 574 TO 621. REPLACED THE CARGO DOOR SILL IAW REO.

Part: FLOOR PANEL — CORRODED (BS 409-559) · airframe 26,655 hrs · 28,625 cycles

LEFT SIDE PRESSURE FLOOR PANEL HAS SEVERAL AREAS OF CORROSION. BLENDED THE CORROSION, BS 409+128 - 559. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 26,655 hrs · 28,625 cycles

LBL 27 FLOOR SUPPORT CORRODED FROM BS 574 TO 621. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 26,655 hrs · 28,625 cycles

RIGHT AILERON UPPER LEADING EDGE SKIN CHAFED. REPAIRED THE AILERON SKIN IAW REO.

Part: SKIN — DENTED (BS 605-621) · airframe 26,655 hrs · 28,625 cycles

FUSELAGE SKIN BETWEEN BS 605 - 621, STRINGERS 20L AND 21L DENTED. INSTALLED A REPAIR DOUBLER IAW REO.

Part: STRUCTURE — DENTED (RT AILERON) · airframe 22,910 hrs · 24,642 cycles

DENT FOUND ON RT AILERON. COMPLIED WITH REO AND ALL STEPS COMPLETED PERMANENT REPAIR IAW REO.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 22,910 hrs · 24,642 cycles

DENT ON UPPER SKIN, RT INBD FLAP. COMPLIED WITH EA AND ALL STEPS COMPLETED OF PERMANENT REPAIR.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 22,910 hrs · 24,642 cycles

DENT ON UPPER SKIN, LT OTBD FLAP. COMPLIED WITH EA AND ALL STEPS COMPLETED OF PERMANENT REPAIR. NO DEFECTS NOTED.

Part: SKIN — DENTED (BS 624) · airframe 22,910 hrs · 24,642 cycles

DENT ON BS 624, STR 20R. COMPLIED WITH EA AND ALL STEPS COMPLETED OF PERMANENT REPAIR.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 22,910 hrs · 24,642 cycles

CHAFE AT CENTER OF LT FLAP VANE L/E. R & R IAW SRM AND REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 22,910 hrs · 24,642 cycles

RIGHT INBD FLAP CENTER L/E VANE CAP IS CHAFED. REPLACED RT INBD FLAP L/E VANE CAP IAW REO AND SRM.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 22,910 hrs · 24,642 cycles

SEVERAL DENTS LOCATED ON THE UPPER SURFACE OF THE LT WING INBD FLAP ASSY. REPAIRED DENTS IAW EA.

Part: SKIN — DAMAGED · airframe 21,309 hrs · 23,208 cycles

LIGHTNING STRIKE ON NOSE, FOUND DURING INSPECTION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,373 hrs · 21,577 cycles

THE FORWARD LT EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R THE LT FORWARD EXTERNAL EMERGENCY LIGHT WITH A SERVICEABLE UNIT, OPS CHECKED GOOD.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 19,314 hrs · 21,538 cycles

GEAR DISAGREE WARNING MESSAGE. NOSE GEAR MADE CYCLING NOISES WITH GEAR UP. REMOVED AND REPLACED PSEU AND LANDING GEAR HANDLE. SWUNG GEAR OPS CHECKED GOOD IAW AMM.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 19,126 hrs · 21,382 cycles

BOTH FLIGHT DECK FLASHLIGHT BATTERIES ARE INOPERATIVE. F/O REPLACED BOTH FLASHLIGHT BATTERIES. CHECKED GOOD.

Part: SHUTOFF VALVE — FAILED (PARKING BRAKE) · airframe 19,057 hrs · 21,322 cycles

PARK BRAKE SHUTOFF VALVE CAUTION IN FLIGHT. RAN QRH NO CHANGE. RETURNED TO FIELD. R & R PARKING BRAKE SHUTOFF VALVE IAW AMM. OPS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 18,850 hrs · 21,141 cycles

NR 2 ENGINE INDICATION FLUCTUATION AND UNCOMMANDED ACCELERATION ON CLIMBOUT.

Part: SKIN — DAMAGED (BS 494) · airframe 18,800 hrs · 21,100 cycles

BURNED SKIN AT BS 494, ONE INCH BELOW S10L. C-CHECK, REPAIRED IAW REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,572 hrs · 20,941 cycles

MULTIPLE MINIATURE LAMPS ARE BURNED OUT INSIDE FWD AND AFT FACING REAR INTERIOR EMERGENCY EXIT CEILING SIGNS, REPLACED THE LAMPS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,599 hrs · 20,957 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS BURNED OUT, REPLACED THE LAMP.

Part: STRUT — CHAFED (LT MLG DOOR) · airframe 18,325 hrs · 20,763 cycles

LEFT MLG DOOR STRUT CHAFED. C-CHECK, R & R LT MLG DOOR STRUT IAW AMM.

Part: SKIN — CORRODED (LT WING) · airframe 18,325 hrs · 20,763 cycles

LEFT WING LOWER FUEL ACCESS PANEL OPENING ON WING AT BL 0 HAS CORROSION IN THREE AREAS. C-CHECK, TREATED CORROSION ON LT WING FUEL ACCESS PANEL OPENING 510AB IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,325 hrs · 20,763 cycles

FS 280, INBD SIDE AT LBL9, FLOOR BOX STRUCTURE TO FS 280, INBD ANGLE IS CRACKED. C-CHECK, R & R CRACKED ATTACH ANGLE AT FS 280 INBD SIDE OF LBL 9 IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,325 hrs · 20,763 cycles

FS 280, FLOOR BOX STRUCTURE TO 280 ATTACH ANGLE ON OTBD SIDE, LBL 11 IS CRACKED. C-CHECK, R & R CRACKED ATTACH ANGLE AT FS 280, LBL 11 OTBD SIDE IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,325 hrs · 20,763 cycles

FS 280 AT RBL 8, FLOOR BOX STRUCTURE TO 280, ATTACH ANGLE CRACKED. C-CHECK, R & R CRACKED ATTACH ANGLE AT FS 280, RBL 8 IAW SRM.

Part: PULLEY BRACKET — CRACKED (BS 484) · airframe 18,325 hrs · 20,763 cycles

PULLEY BRACKETS LT AT FS 484, AT BL 27 LT AND 36 LT ARE BOTH CRACKED. C-CHECK, FABRICATED AND REPLACED BOTH CLIPS ON PULLEY BRACKET AT LT FS484, BL27 AND BL36 IAW REO AND SRM.

Part: PULLEY BRACKET — CRACKED (BS 484) · airframe 18,325 hrs · 20,763 cycles

PULLEY BRACKET RT AT FS 484, BL 27 RT IS CRACKED. C-CHECK, FABRICATED AND REPLACED CLIP ON PULLEY BRACKET AT RT FS484, BL27 IAW REO AND SRM.

Part: SKIN — GOUGED (BS 621) · airframe 18,325 hrs · 20,763 cycles

FS 621.00 FWD SIDE HAS GOUGE ON SKIN AT LBL 9.0 APPROX 6" FROM TOP. C-CHECK, BLENDED GOUGE AT FS 621.00 ON SKIN OF FWD BULKHEAD AT LBL 9.0 APPROX 6" FROM TOP IAW REO.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 18,325 hrs · 20,763 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 621.00, BULKHEAD NEAR CARGO DOOR OPENING. C-CHECK, R & R FLOOR SUPPORT ANGLE AT FS 621 BULKHEAD NEAR CARGO DOOR OPENING IAW SRM.

Part: STRUCTURE — CHAFED (BS 621) · airframe 18,325 hrs · 20,763 cycles

FWD SIDE OF FS 621 CHAFED FROM ACCESS PANEL SCREWS AT LBL 35.0, 27.0 AND 17.0, 30" ABOVE FLOOR SUPPORT ANGLES. C-CHECK, BLENDED CHAFED AREAS OF FS 621 AT LBL 17,27, AND 35 AT 30" ABOVE FLOOR IAW REO.

Part: LEVER — GOUGED (PAX DOOR) · airframe 18,325 hrs · 20,763 cycles

PAX DOOR INTERIOR, THE FWD PULL-IN LEVER IS GOUGED. C-CHECK, REPAIRED THE PAX DOOR FWD PULL IN LEVER IAW REO AND AMM.

Part: SUPPORT BEAM — CRACKED · airframe 18,325 hrs · 20,763 cycles

CARGO DOOR NET SUPPORT BEAM LOWER AFT ATTACHMENT ANGLE CRACKED. C-CHECK, R & R A NEW ANGLEAT AFT LOWER CARGO DOOR NET SUPPORT BEAM IAW SRM.

Part: SKIN — CHAFED (LT AILERON) · airframe 18,325 hrs · 20,763 cycles

LEFT AILERON UPPER L/E SKIN CHAFED. C-CHECK, REPLACED LEFT AILERON UPPER L/E SKIN WITH NEW SKIN IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 18,325 hrs · 20,763 cycles

RIGHT INBD FLAP VANE L/E SKIN CHAFED AT INBD END. C-CHECK, REPAIRED RT INBD FLAP VANE L/E SKIN IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 18,325 hrs · 20,763 cycles

LEFT INBD FLAP VANE L/E SKIN CHAFED AT CENTER. C-CHECK, REPAIRED LT FLAP VANE L/E SKIN IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 18,325 hrs · 20,763 cycles

RIGHT INBD FLAP VANE L/E SKIN CHAFED AT CENTER. C-CHECK, REPAIRED RT FLAP VANE L/E SKIN AT CENTER IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 18,325 hrs · 20,763 cycles

RIGHT AILERON UPPER L/E SKIN CHAFED SEVERAL AREAS. C-CHECK, REMOVED CHAFING FROM RT AILERON UPPER L/E SKIN IAW REO.

Part: PLATE — CHAFED (LT WING TE FLAP) · airframe 18,325 hrs · 20,763 cycles

LEFT INB FLAP INBD HINGE ARM AFT INBD LUG PLATE CHAFED ON INB SIDE. C-CHECK, REPAIRED LT INBD HINGE ARM AT INBD LUG PLATE IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 18,325 hrs · 20,763 cycles

LEFT INBD FLAP VANE L/E SKIN CHAFED AT OTBD END. C-CHECK, REPAIRED LT INBD FLAP VANE L/E SKIN AT OUTBD END IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 18,325 hrs · 20,763 cycles

LEFT INB FLAP VANE L/E SKIN CHAFED AT INBD END. C-CHECK, REPAIRED CHAFED LT FLAP VANE L/E SKIN AT INBD END IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 18,325 hrs · 20,763 cycles

RIGHT INBD FLAP VANE L/E SKIN CHAFED AT OTBD END. C-CHECK, REPAIRED RT INBD FLAP VANE L/E SKIN AT OTBD END IAW REO.

Part: LUG — CHAFED (MLG DOOR) · airframe 18,325 hrs · 20,763 cycles

LEFT MLG DOOR LOWER CONTROL ARM ATTACHMENT LUG CHAFED AFT SIDE. C-CHECK, REMOVED CHAFING FROM LT MLG DOOR LOWER CONTROL ARM ATTACHMENT LUG IAW REO.

Part: BELLCRANK — CHAFED (LT MLG DOOR) · airframe 18,325 hrs · 20,763 cycles

LEFT MLG DOOR CONTROL BELLCRANK CHAFED AT OTBD END. C-CHECK, R & R LT MLG DOOR BELLCRANK IAW AMM.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 18,325 hrs · 20,763 cycles

LEFT MLG DOOR INNER SKIN CHAFED AT OTBD L/E. C-CHECK, REPAIRED DAMAGE AT LT MLG DOOR OTBD L/E IAW REO.

Part: BELLCRANK — CHAFED (RT MLG DOOR) · airframe 18,325 hrs · 20,763 cycles

RIGHT MLG DOOR CONTROL BELLCRANK CHAFED AT OTBD END. C-CHECK, R & R RT MLG DOOR BELLCRANK IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 18,165 hrs · 20,643 cycles

EMERGENCY EXTERIOR LIGHT BURNED OUT, REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,595 hrs · 20,234 cycles

NR 2 CEILING EMERGENCY LIGHT IS BURNED OUT. FLT 5243 RELAMPED.

Part: CONNECTOR — LOOSE (SELECTOR VALVE) · airframe 17,163 hrs · 19,892 cycles

NOSE GEAR OPEN WARNING MESSAGE AFTER GEAR SELECTED UP. FLT#5554 TIGHTENED A LOOSE CONNECTOR ON THE SELECTOR VALVE.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 17,139 hrs · 19,875 cycles

ASYMMETRIC ROLL NOTED IN FLIGHT WHEN FLAPS SELECTED TO 45 DEGREE. PAINT RIDGES NOTICED ON TOP OF FLAP LE. FLT#5553 INSPECTED ALL FLIGHT CONTROLS & FLAPS FOR ANY DEFECTS, NO DEFECTS NOTED. RAN ALL FLIGHT CONTROLS TO FULL TRAVELS & RAN FLAPS FROM 0 DEGREE TO 45 DEGREE SEVERAL TIMES, NO DEFECTS NOTED. OPERATIONS CHECKED GOOD. PRC PAINT RIDGES ARE NORMAL PART OF FLAP JOINT LE, NO DEFECTS.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 15,893 hrs · 18,765 cycles

AFTER TAKEOFF AND GEAR RETRACTION ATTEMPT, GEAR DISAGREE WARNING AND NOSE DOOR OPEN WARNING MESAGE ILLUMINATED. NOSE GEAR REMAINED DOWN. (FLT 4522 REPLACED NLG SELECTOR VALVE, PERFORMED OPS CHECK OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM, BLED NR 3 HYDRAULIC SYSTEM IAW AMM. P/N: 750006000 S/N ON: 1807 S/N OFF: 0063T

Part: ACM — CONTAMINATED (AC BAY) · airframe 15,423 hrs · 18,352 cycles

STRONG DRY ACRID SMELL IN COCKPIT, NOT NOTICEABLE IN CABIN, COMING FROM GASPERS WITH BLEEDS CLOSED AND APU RUNNING. (FLT 4559) CLEANED GLYCOL OFF ACM OUTLET PIPE, SMELL IS GONE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,770 hrs · 17,798 cycles

LEFT FORWARD 2 EMERGENCY EXTERNAL LIGHTS ARE OUT. (FLT 6257) RELAMPED EMERGENCY LIGHTS.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 14,443 hrs · 17,528 cycles

AFTER SELECTING GEAR LEVER DOWN RECEIVED GEAR DISAGREE WARNING MESSAGE. (FLT 4793) REPLACED NLG PRIORITY VALVE IN REFERENCE TO AMM. P/N: 4622 S/N OFF: 1553A.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,704 hrs · 16,860 cycles

FLT 5354, AFT OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: WIRE — CHAFED (E&E BAY) · airframe 13,436 hrs · 16,643 cycles

ARCING IN AFT EQUIPMENT BAY. CHAFING WIRE AND CABLE ON FRAME AT FUSE STATION FS 672/00R. FRAME HAS ELECTRICAL ARCING DAMAGE AND SHIELD DAMAGE. (FLT 5535) REPLACED THE WIRES CD7C20WHT, CD8C20BLU, CD9C20DRN AND SHIELD. REPAIRED FRAME SECTION IAW REO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,289 hrs · 16,520 cycles

RIGHT WING EMERGENCY EXIT EXTERIOR MIDDLE LIGHT IS OUT. (FLT 5517) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,289 hrs · 16,520 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5517) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,289 hrs · 16,520 cycles

EMERGENCY LIGHTS AT GSD AND LEFT REAR OVERWING EXIT ARE OUT. (FLT 5488) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,289 hrs · 16,520 cycles

NR 2 LEFT OVERWING EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6463) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 13,215 hrs · 16,462 cycles

AFT HALF OF EMERGENCY STRIP FLOOR LIGHTS ARE OUT. (FLT 4748) CONNECTION ON FLOOR STRIP IN FRONT OF LAVATORY DISCONNECTED. RECONNECTED STRIP AS NEEDED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 13,110 hrs · 16,379 cycles

NR 3 LEFT EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,975 hrs · 16,283 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 5514) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,695 hrs · 16,054 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 6485) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,367 hrs · 15,759 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 6350) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,247 hrs · 15,661 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5454) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,962 hrs · 15,435 cycles

EXTERIOR EMERGENCY LIGHT FORWARD OF PAX BOARDING DOOR IS OUT. (FLT 5624) RELAMPED EMERGENCY LIGHT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 11,893 hrs · 15,375 cycles

GALLEY EMERGENCY EXIT LIGHT & BOTH FORWARD EMERGENCY EXTERIOR LIGHTS ARE OUT. (FLT 6273) REPLACED THE NR 1 ELBP BATTERY CHARGER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,842 hrs · 15,339 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6241) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 11,449 hrs · 15,028 cycles

EMERGENCY FLOOR LIGHTING STRIP IS OUT FROM ROW 9 AFT TO ROW 12. (FLT 6393) RE-SECURED AFT FLOOR EMERGENCY LIGHT CONNECTOR.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,356 hrs · 14,954 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: BRAKE ASSY — LOCKED (LT MLG) · airframe 11,299 hrs · 14,904 cycles

LEFT OUTBOARD MAIN BRAKE LOCKED UP ON TAXI. (FLT 6690) INSTALLED SERVICEABLE BRAKE ASSEMBLY AND MAIN WHEEL ASSY AT NR 1 POSITION. P/N 5010520-1, S/N OFF DEC97-1158, P/N 5010571-1, S/N OFF AUG01-4285.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,276 hrs · 14,888 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6916) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,118 hrs · 14,748 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6957) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,096 hrs · 14,731 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6394) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,980 hrs · 14,646 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5820) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,838 hrs · 14,506 cycles

EXTERIOR EMERGENCY LIGHT FORWARD OF MAIN CABIN DOOR IS OUT. (FLT 3060) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,662 hrs · 14,346 cycles

MOST AFT EMERGENCY CEILING LIGHT IS OUT. (FLT 6393) RELAMPED EMERGENCY LIGHT.

Part: FITTING — CORRODED (ENGINE MOUNT) · airframe 9,937 hrs · 13,751 cycles

RIGHT ENGINE AFT THRUST MOUNT FITTING ASSEMBLY HAS CORROSION. (C-CHECK) INSTALLED NEW RIGHT AFT THRUST MOUNT FITTING ASSEMBLY.

Part: BPSU — OUT OF RIG (T/E FLAP) · airframe 9,902 hrs · 13,709 cycles

ASH FLT 1908 HNL- OVERNIGHT - FLAPS FAIL CAUTION OCCURRED ON EXTENSION BETWEEN 20 AND 30 DEGREES WITH THE HANDLE SELECTED TO 30 DEGREES. MX COMPLIED WITH THE FLAPS FAIL PARTS A AND B PROCEDURES AND RIGGED THE BPSU UNITS.

Part: GEARBOX — WORN (THROTTLE) · airframe 9,891 hrs · 13,685 cycles

FOUND WEAR ON THE ENGINE THROTTLE CONTROL GEARBOX, WEAR GREATER THAT .010 INCH. REMOVED AND REPLACED NR 1 ENGINE THROTTLE CONTROL GEARBOX.

Part: LIFE VEST — MISSING (CABIN) · airframe 9,574 hrs · 12,987 cycles

ASH FLT 1040 HNL-ITO. SEAT 10A LIFE VEST WAS MISSING. MX INSTALLED A NEW LIFE VEST.

Part: LIFE VEST — OPEN · airframe 8,989 hrs · 11,724 cycles

ASH FLT 1017 HNL-OGG, INFANT LIFE VEST OPENED. MX REPLACED THE LIFE VEST.

Part: FITTING — UNKNOWN (TE FLAP) · airframe 8,673 hrs · 11,028 cycles

REPAIR TO O/B FLAP LUG FITTING WS 178 AND 264.

Part: FIRST AID KIT — OPEN (CABIN) · airframe 8,245 hrs · 10,095 cycles

ASH 1030 HNL-KOA. FIRST AID KIT WAS OPENED. MX REPLACED THE FIRST AID KIT.

Part: CONTROL PANEL — FAILED (STAB CHANNEL 2)

ASH 1022 HNL - STAB CHANNEL 2 FAILED. MX REPLACED THE TRIM CONTROL PANEL.

Part: LIFE VEST — MISSING (CABIN) · airframe 7,228 hrs · 7,852 cycles

ASH 1007 HNL. SEATS D AND F WERE MISSING LIFE VESTS. MX INSTALLED NEW LIFE VESTS.

Part: PRESSURE SWITCH — FAILED (EDP) · airframe 7,142 hrs · 7,684 cycles

ASH 1027 HNL. PILOT REPORTED INBOARD AND OUTBOARD SPOILER FAULT IN FLIGHT. MX REPLACED THE EDP 1 LOW PRESSURE SWITCH.

Part: ECU — MALFUNCTIONED (SPOILER SYS) · airframe 6,583 hrs · 6,449 cycles

ASH 1024 HNL - INBRD GROUND SPOILER CTN MESSAGE. MX RESET SECU'S.

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 6,545 hrs · 6,531 cycles

ASH 1011 KOA - SPOILERON FAULT CAUTION MESSAGE. MX RESET THE SECU. NO FURTHER ACTION REQURIED.

Part: STATUS MESSAGE — FALSE ACTIVATION · airframe 6,282 hrs · 5,746 cycles

ASH 1036 OGG - INBD GROUND SPOILER/FLIGHT SPOILER FAULT STATUS MESSAGE. MX RESET THE SECUS AND THE SYSTEM OP CHECKED GOOD.

Part: STATUS MESSAGE — NONE · airframe 6,257 hrs · 5,728 cycles

ASH 1006 HNL - GROUND SPOILER STATUS FAULT. MX RESET SYSTEM.

Part: CONTROL UNIT — INOPERATIVE (STABILIZER)

STAB TRIM/MACH TRIM MSG. RESET HSTCU. NO FAULTS FOUND NOTED. FUNC IAW 27-40-00.

Part: LIGHT — INOPERATIVE (CABIN)

DURING INSPECTION THE LT FORWARD OVERWING EMERGENCY LAMP WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.