N856AS

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 44,739 hrs · 41,720 cycles

GEAR DISAGREE (FLT 4680 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26687777 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP26687967 FOR REMOVAL AND REPLACEMENT OF LH MLG SIDE STAY ACTUATOR.REFERENCE CP26688073 FOR LANDING GEAR MECHANICAL AND HYDRAULIC HEALTH CHECK TASK CARD 32-900-1004-SKY.REFERENCE CP 26687914 FOR SMOD APPROVAL"

Part: NONE — PRESSURE LOSS · airframe 44,204 hrs · 41,199 cycles

AFTER T/O CABIN WILL NOT PRESSURIZED AND LEFT PACK OFF WITH THE SWITCH PRESSED ON,STAYED BELOW 10000. QRH WAS PREFORMED DIDN€™T FIX IT. (FLIGHT 5397 - FILED CLOSED) FOUND LEFT 10TH STAGE SOV NOT TO BE OPENING WHEN SELECTED REMOVE AND REPLACED LEFT 10TH STAGE SOV AND FOUND BACK SHELL ON CANNON PLUG BACKED OFF TIGHTENED BACK SHELL AND PREFORMED OPS CHECK PER CRJ 200 AMM 36-11-04 OPS CHECK GOOD. / PREFORMED OPS CHECK OF CABIN PRESSURIZATION PER CRJ 200 AMM 21-30-00 OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (RT ENGINE) · airframe 44,173 hrs · 41,172 cycles

GOT R 14TH DUCT WARNING MESSAGE ON TAKEOFF. CHECKED ANTI-ICE PAGE AND SAW RED LINE GOING UP THE RIGHT SIDE OF THE FUSELAGE. ANTI-ICE WAS OFF, NEVER USED. ABOUT 30 SECONDS LATER GOT BOTH L & R 10TH DUCT WARNING MESSAGES. FOLLOWED QRH, RETURNED TO FIELD WITH RIGHT ENGINE IDLED. (FLIGHT #5659) OPS CHECK OF THE ANTI ICE SYSTEM IS GOOD AT THIS TIME.

Part: NONE — FAILED · airframe 43,616 hrs · 40,690 cycles

D: GEAR DISAGREE ON APPROACH, (AMBER LEFT MAIN) WENT AROUND / PERFORMED QRH, GEAR ALL SHOWED GREEN/DOWN ON THIRD CYCLE. / DEN LINE MX - INTERROGATED PSEU AND FOUND CODES S19 AND S34 FOR THE LH MLG DOWN LOCK. DEFERRING LANDING GEAR RETRACTION SYSTEM REF CRJ200 MEL 32-30-1. MX ACTIONS CW, PLACARDS INSTALLED. / C: MEL 32-30-1 / CAT A DUE WITHIN 1 FLT DAY (6/24?/22) / **SMOD APPROVAL REQ'D TO RTS THIS A/C AFTER MEL CLEARED DUE TO ODI EVENT** / GEAR DISAGREE ON APPROACH, (AMBER LEFT MAIN) WENT AROUND / PERFORMED QRH, GEAR ALL SHOWED GREEN/DOWN ON THIRD CYCLE. / (FLIGHT 5551 - FILED CLOSED) JUN 23, 2022 STATION: DEN--INTERROGATED PSEU AND FOUND CODES S19 AND S34 FOR THE LH MLG DOWNLOCK. DEFERRING LANDING GEAR RETRACTION SYSTEM REF CRJ200 MEL 32-30-1. DOWNGRADED FROM CAT II PER GMM 2-23. MX ACTIONS CW, PLACARDS INSTALLED.

Part: NONE — LEAKING · airframe 43,407 hrs · 40,486 cycles

RIGHT WING 2ND CANOE O/B OF MLG HAS FUEL LEAK AT THE FORWARD BOLTS OF THE BOX FITTING FORWARD HINGE ( REF 57-21-36 ) (FILED CLOSED) REMOVED AND REPLACED FOWARD AND AFT HARDWARE OF FLAP HINGE-BOX FITTING ON RIGHT WING 2ND CANOE IN REFERENCE TO AMM 57-21-36. SEE CP 24702354 FOR LEAK CHECK.

Part: NONE — LEAKING · airframe 43,407 hrs · 40,486 cycles

RIGHT WING 2ND CANOE O/B OF MLG HAS FUEL LEAK. (FILED - CLOSED) REMOVED AND REPLACED THE TWO FORWARD BOLTS, TWO WASHERS, AND TWO NUTS OF R/H WING FWD HINGE-BOX FITTING BY 2ND CANOE OF MLG IN REF TO AMM 57-21-36. SEE CP 24695858 FOR LEAK CHECK.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH ELEVATOR ATTATCHING HARDWARE IS CORRODED AND NEEDS REPLACED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH ELEVATOR ATTATCHING HARDWARE REFERENCE MX TRANS 22021725 FOR INSTALL

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

RH FLIGHT SPOILER INBOARD, IB MID, AND OB MID HINGE POINTS HAVE CORRODED HARDWARE ALONG WITH BOTH PCU LOWER ATTACH BOLT NUTS AND RETAINING PLATES. HARDWARE REQUIRES REPLACEMENT AS NEEDED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED THE RH FLIGHT SPOILER INBD, INBD MID, AND OTBD HINGE POINT CORRODED HARDWARE ALONG WITH BOTH THE PCU LOWER ATTACHMENT BOLTS AND RETAINING PLATE BOLTS IAW CRJ-200 AMM 27-64-05-000-801, 27-64-05-400-801, 27-62-01-000-801, 27-62-01-400-801. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: NONE — DAMAGED · airframe 42,862 hrs · 40,002 cycles

RH OTBD FLAP HINGE BOX AT WS178.00 AFT OTBD HINGE LUG ON THE BOX HAS A BROKEN HAT BUSHING THE HAT IS BROKEN OFF. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED THE RH OTBD FLAP HINGE BOX AT WS178.00 AFT OTBD HINGE LUG ON THE BOX BUSHING IAW CRJ-200 AMM 20-26-00-910-802, 20-26-00-910-804.

Part: NONE — DAMAGED · airframe 42,862 hrs · 40,002 cycles

RH OTBD FLAP HINGE BOX AT WS264.00 AFT OTBD HAT BUSHING IS BROKEN THE HAT IS BROKEN OFF. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED THE RH OTBD FLAP HINGE BOX AT WS264.00 AFT OTBD HAT BUSHING IAW CRJ-200 AMM 20-26-00-910-802, 20-26-00-910-804.

Part: NONE — DAMAGED · airframe 42,862 hrs · 40,002 cycles

LH OTBD FLAP HINGE BOX AT WS178.00 INBD AFT BOX LUG HAT BUSHING HAS THE HAT BROKEN OFF OF IT (C-CHECK- RO 11/11/21) .REMOVED AND REPLACED THE LH OTBD FLAP HINGE BOX AT WS178.00 INBD AFT LUG BUSHINGS IAW CRJ-200 AMM 20-26-00-910-802, 20-26-00-910-804.

Part: NONE — DAMAGED · airframe 42,862 hrs · 40,002 cycles

RH WING OTBD FLAP HINGE BOX AFT MOUNT BUSHINGS HAVE THE HAT BROKEN OFF OF 2 EA HAT BUSHINGS AND REQUIRE REPLACEMENT. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED THE RH WING OTBD FLAP HINGE BOX AT WS220 AFT MOUNT BUSHINGS IAW CRJ-200 AMM 20-26-00-910-802, 20-26-00-910-804.

Part: NONE — DAMAGED · airframe 42,862 hrs · 40,002 cycles

R/H WING O/B FLAP HINGE BOX AFT ATTACH FITTINGS (2 EA) HAVE TOOLING DAMAGE, I/B FITTING O/B LUG O/B AFT CORNER AND O/B FITTING I/B LUG I/B CORNER (C-CHECK- RO 11/11/21) REPAIRED DAMAGE IAW REO 601R-57-21-3524 REV -- DATED 10-4-2021. COMPLETED SKYWEST STRUCTURAL MAJOR REPAIR TASK CARD 51-900-1003-SKY AND ATTACHED 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CRACKED · airframe 42,862 hrs · 40,002 cycles

LH F.S.605 FRAME SECTOR 601R36026-29 IN BAGGAGE BAY JUST BELOW FLOOR LEVEL HAS 2 INCH CRACK. (C-CHECK- RO 11/11/21) REPLACED LH FRAME SECTION AT F.S. 605.00 STGR 17L - 20L IAW CRJ-200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED FORM M-337. NO WEIGHT CHANGE NOTED

Part: NONE — BENT · airframe 42,862 hrs · 40,002 cycles

FLOOR BEAM WEB AT LBL 9 AND FS 559+96 TO 559+112 ON INBOARD SIDE OF BEAM WAS FOUND TO BE BENT ACROSS LIGHTNING HOLES AND REQUIRES REPLACEMENT. (C-CHECK- RO 11/11/21) INSTALLED NEW WEB PN 601R31119-66 AT LBL 9 AND FS. 559 +96 TO FS. 559 +112 ON INBOARD SIDE OF BEAM IAW REO 601R-53-51-599 REV: -- 2021-09-03 AND REF: BOMBARDIER DWG:# 601R31119 REV: H FOR FASTENER CALL OUT AND REF: CRJ 200 SRM 51-42-06 AND SRM 51-40-11 SEE CONTINUATION FOR DETAILS. NO WEIGHT CHANGE RECORDED, PART FOR PART REPLACEMENT, MAJOR REPAIR TASK 51-900-1003-SKY & FORM M337 COMLETED AND ATTACHED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

FOUND SERVICE DOOR LOWER AFT PAN TO BE CORRODED OUT OF LIMITS. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SVC DOOR LOWER AFT PAN IAW CRJ 200 SRM 51-42-06, 51-42-21, AND SNIEO 601R38304 S09. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH ELEVATOR VERTICAL TORQUE TUBE UPPER AND LOWER BEARINGS AND CONTROL ROD BEARINGS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPAIRED LH ELEV VERT SHAFT ATTACHING BEARINGS IAW CRJ 200 AMM 20-26-00-910-806 AND UPPER OB CONTROL ROD IAW CRJ 200 AMM 27-31-35-400-801. RIGS, OPS, AND LEAK CHECK "GOOD."

Part: NONE — GOUGED · airframe 42,862 hrs · 40,002 cycles

W.S. 264.00 FLAP HINGE BOX ATTACH FITTING (OUTBD AFT) FOUND TO BE GOUGED AND REQUIRES REPAIR (C-CHECK- RO 11/11/21) REPAIRED W.S 264.00 FLAP HINGE BOX ATTACH FITTING OUTBD AFT GOUGE IAW MHIRJ REO 601R-57-21-3515 REV -- DATED 2021-09-08 AND SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — NONE · airframe 42,862 hrs · 40,002 cycles

AFTER REMOVAL OF FLOOR BEAM FOUND WEB AT RBL 9 AND F.S 559+16 TO 559+32 ON THE INBOARD SIDE OF FLOOR BEAM TO BE CORRODED WITH A 100% MATERIAL LOSS PART FOUND TO BE UNSERVICABLE AND REQUIRES REPLACEMENT. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED FLOOR BEAM WEB AT RBL 9 F.S. 559+16 TO 559+32 ON THE INBOARD SIDE OF FLOOR BEAM IAW CRJ200 SRM 51-42-06 AND 51-42-21 IN COMPLIANCE WITH MHIRJ REO 601R-53-51-599, REV--, DATE: 2021-09-03. NO WEIGHT CHANGE.M-337, SDR, AND 51-900-1003SKY COMPLIED WITH

Part: TRACK — CORRODED · airframe 42,862 hrs · 40,002 cycles

RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 364 TO F.S. 394. (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802

Part: INTERCOSTAL — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H FLOOR SILL IS CORRODED BETWEEN F.S. 559.0 TO F.S.559.0+16 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH FLOOR SILL FROM FS 559- FS 559+16 IAW CRJ 200 SRM 51-42-06 AND 51-42-21

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H F.S. 513 FRAME IS CORRODED AT STGR 17 (FLOOR LEVEL). (C-CHECK- RO 11/11/21) REPAIRED RH FS 513 FRAME CORROSION AT STGR 17 IAW MHIRJ REO 601R-41-2960 REV -- DATED 2021-09-07 AND SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE REF ATTACHED 337 FORM

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

RBL 9 FLOOR BEAM BETWEEN FS 559 AND FS 559+64 CORRODED OUT OF LIMITS, FROM CAMP 23329338 JOB97404121 OP#293 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RBL9 FLOOR BEAM AT F/S 559 TO 559+64 IAW CRJ 200 SRM 51-42-06, 51-42-36 AND REO 601R-53-51-599 REV -- DATED 2021-09-03. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

L/H WS 53.60 BATT RIB, INBOARD ANGLE IS CORRODED COMMON TO CANNON PLUGS J411 AND J413 ATTCAHING HARDWARE. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH WS 53.60 BATT RIB ANGLES IAW CRJ 200 SRM 51-42-21 AND 51-42-06.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LBL 9 FLOOR BEAM BETWEEN FS 559+9 AND 559+112 CORRODED OUT OF LIMITS, SEE CAMP #23328805 (C-CHECK- RO 11/11/21) REMOVE AND INSTALLED FLOOR BEAM CAP AT LBL 9 FROM FS. 559+9 TO 559+112 IAW MHIRJ REO 601R-53-51-599 REV; -- DATED: 2021-42-36, CRJ 200 SRM 51-42-21, 51-42-22, AND 51-42-36. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED

Part: NONE — DENTED · airframe 42,862 hrs · 40,002 cycles

DURING NDT AND VISUAL INSPECTIONS OF THE FS 621.00 REAR PRESSURE BULKHEAD FOUND THERE TO BE SEVERAL CHAFES, DENTS, AND FAILED NDT INDICATIONS ON THE FWD FACE OF THE BULKHEAD.SEE CONTINUATION CARD FOR TYPE/LOCATION OF DAMAGE. (C-CHECK- RO 11/11/21) REMOVED DAMAGE FROM FS 621 BULKHEAD AND COMPLIED WITH REPAIR IAW REO 601R-53-61-7705 REV -- DATED 2021-10-20 AND REO 601R-53-61-1240 REV.D, DATED 2016-10-31. COMPLIED WITH TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. WEIGHT CHANGE: 33.80 LBS ADDED

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

RBL9 FLOOR SEAT TRACK FS559+86 - FS559+96 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

SERVICE DOOR SILL ANGLE IS CORRODED FS 319.00 TO FS 349.00 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SVC DOOR SILL ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LBL9 FLOOR SEAT TRACK FS559+86 - FS559+96 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LBL9 SEAT TRACK FROM FS559+86 - FS559+96 IAW CRJ 200 AMM 53-01-11-000/400-802 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

RBL27 FLOOR SEAT TRACK FS559+78 - FS559+96 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LBL27 FLOOR SEAT TRACK FS559+78 - FS559+96 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LBL9 FLOOR SEAT TRACK FS559+5 -- 559+86 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL 9 FS 559+5 - FS 559+86 IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

PAX DOOR SILL ANGLE CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACE CORRODED ANGLE (LOWER SILL ANGLE) IAW CRJ-200-SRM 51-42-06, 51-42-13, 51-42-21, 51-40-11, 51-25-00. PERFORMED OP TEST OF DOOR WARNING SYSTEM JIAW CRJ-200-AMM 52-70-04-710-801, OP TEST GOOD AT THIS TIME. / SEE ATTACHED CONTINUATION CARD FOR SIGN-OFF DETAILS.

Part: CUP — CORRODED (DOOR HANDRAIL) · airframe 42,862 hrs · 40,002 cycles

PAX DOOR HANDRAIL CUPS ARE CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED PAX DOOR HAND RAIL CUPS IAW CRJ 200 SRM 51-42-06. COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: SEAT TRACK — CORRODED · airframe 42,862 hrs · 40,002 cycles

RBL9 FLOOR SEAT TRACK FS559+5 - FS559+86 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RBL9 SEAT TRACK FS559+5 - FS559+86 SEAT TRACK SEGMENT IAW CRJ 200 AMM 53-01-11-000/400-802 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: SEAL — CORRODED · airframe 42,862 hrs · 40,002 cycles

L/H EMERGENCY EXIT DOOR FWD AND AFT LOWER INTERNAL CORNERS OF DOOR STRUCTURE IS CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED L/H EMERGENCY EXIT FORWARD AND AFT LOWER INTERNAL BRACKETS I.A.W. BOMBARDIER CRJ 200 SRM 51-42-11 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

SERVICE DOOR LOWER FWD PAN AND SPLICE PLATE ARE CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SVC DOOR LOWER FWD AND SPLICE PLATE IAW CRJ 200 SRM 51-42-06, 51-42-21, AND SNIEO 601R38304 S06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — BENT · airframe 42,862 hrs · 40,002 cycles

PAX DOOR AFT DRAG ANGLE BENT AND 2 RIVETS PULLED OUT WHERE ASSIST CABLE COMES OUT OF DOOR (C-CHECK- RO 11/11/21) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE IAW CRJ 200 SRM 51-42-13.

Part: DOOR SILL — CORRODED (BS 409) · airframe 42,862 hrs · 40,002 cycles

RH FLOOR SILL IS CORRODED BETWEEN FS409 AND FS409+5. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH FLOOR SILL IAW CRJ 200 SRM 51-42-06, 51-42-21, REO 601R-53-21-3500 REV -- DATED 2021-9-14 AND REO 601R-53-21-3501 REV -- DATED 2021-09-24. COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH OB GRND SPOILER PCU LINK HARDWARE IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED OLD LH OB GROUND SPOILER PCU LINK HARDWARE IAW CRJ-200 AMM 27-65-01-000-801 AND INSTALLED NEW HARDWARE IAW CRJ-200 AMM 27-65-01-400-801.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH OB GRND SPOILER PCU WING ATTACHING HARDWARE IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED OLD HARDWARE ON LH OB GROUND SPOILER PCU WING HINGE IAW CRJ-200 AMM 27-65-01-000-801 AND INSTALLED NEW HARDWARE IAW CRJ-200 AMM 27-65-01-400-801.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH IB GRND SPOILER HAS CORRODED HARDWARE AT ALL HINGE POINTS. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH GROUND SPOILER HINGE HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

RBL9 FLOORBEAM IS CORRODED BETWEEN FS409+5 AND FS409+119. (C-CHECK- RO 11/11/21) REMOVED RBL 9 FLOOR BEAM CAP BETWEEN F.S. 409.00 + 5 - F.S. 409.00 + 119 AND INSTALLED NEW SERVICEABLE BEAM CAP IAW CRJ-200 SRM 51-42-06, 51-42-21 AND MHIRJ REO 601R-53-51-599 REV - - DATED 2021-09-03. COMPLETED TASK CARD 51-900-1003-SKY AND M-337. NO CHANGE TO WEIGHT AND BALANCE.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH FLIGHT SPOILER IB PCU IB WING ATTACHING HARDWARE IS CORRODED (C-CHECK- RO 11/11/21) REPLACED L/H FLIGHT SPOILER I/B PCU HARDWARE AND WING ATTACH HARDWARE AS REQUIRED IAW CRJ 200 AMM 27-62-01-400-801. FUNCTIONAL TEST OF SECU'S GOOD IAW CRJ 200 AMM 27-64-05-720-801.SELF TEST OF SECU'S GOOD IAW CRJ 200 AMM27-61-05-740-801 AND OPS TEST OF FLIGHT SPOILER GOOD IAW CRJ 200 AMM27-64-00-710-801. REFERENCE ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH FLOOR SILL FS409+73 -- FS409+128 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH FLOOR SILL FS409+73- FS409+128 IAW CRJ200 SRM 51-42-06 ANF 51-42-21, COMPLIED WITH MHIRJ REO 601R-53-31-1204 REV - - DATED 2021-09-21. REF ATTACHED CONTINUATION FOR WORK PERFORMED. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO WEIGHT AND BALANCE.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

RH FLOOR SILL FS409+73 -- FS409+128 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED R/H FLOOR SILL AT F.S 409+73 TO F.S 409+128 IAW REO 601R-53-31-1203 REV -- DATED 2021-09-20 AND SRM 51-42-06 AND 51-42-21.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH SPOILERON IB PCU WING ATTACH POINT NUTS ARE CORRODED. (C-CHECK- RO 11/11/21) INSTALLED NEW HARDWARE ON L/H SPOILERON I/B PCU TO WING ATTACHING POINT IAW CRJ 200 AMM 27-62-01-400-801 STEP 2.B(4)-(7). REPLACED CORRODED SPOILERON HINGE NUT BEHIND IB PCU WING ATTACH POINT E IAW CRJ 200 AMM27-64-01-400-801. RIG CHECK PERFORMED AND FOUND IN LIMITS IAW CRJ 200 AMM 27-62-01-220-802. - FUNCTIONAL TEST OF SECUS GOOD IAW CRJ / 200 AMM 27-61-05-720-801. OPS TEST OF FLIGHT SPOILER/SPOILERON GOOD IAW CRJ 200 AMM 27-64-00-710-801. REFERENCE ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 42,862 hrs · 40,002 cycles

INTERCOSTAL CLIP ANGLE AT FS484 ON OB SIDE OF LBL27 FLOOR BEAM IS CRACKED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CRACKED INTERCOSTAL CLIP ANGLE WITH NEW AT FS 484 ON OB SIDE OF LBL FLOOR BEAM IAW CRJ 200 BOMBARDIER REO 601R-53-41-059 REV -C DATED 2020-03-11

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

RH FLOOR SILL FS409+5 -- FS409+73 SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REPAIRED RH FLOOR SILL BETWEEN F.S. 409+5 - 409+73 IAW MHIRJ REO 601R-53-31-1206 REV - - DATED 2021-10-06. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LBL9 FLOORBEAM IS CORRODED BETWEEN FS409+5 AND FS409+119 (C-CHECK- RO 11/11/21) REMOVED CORRODED LBL9 FLOORBEAM BETWEEN FS409+5 AND FS409+119 , FABRICATED AND INSTALLED NEW BEAM FROM EXTRUSION P/N N126-1707 IAW REO 601R-53-31-1210 REV - - DATED 2021-10-21 AND CRJ-200 SRM 51-42-21, 51-42-06, AND 51-40-11. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337, NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH IB GRND SPOILER PCU LINK UPPER NUT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH INBOARD GROUND SPOILER PCU LINK UPPER NUT WITH NEW SERVICEABLE HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

RBL9 FS399 --FS409+128 FLOOR SEAT TRACK SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REPLACED FLOOR SEAT TRACK AT RBL9 BETWEEN FS399 AND FS409+128 IAW CRJ200 AMM 53-01-11-000/400-802.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH FLOOR SILL IS CORRODED BETWEEN FS559 AND FS621. (C-CHECK- RO 11/11/21) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE BETWEEN FS 559 AND FS 559+86. REMOVED AND REPLACED LH FLOOR SILL FROM FS 559 TO FS 559+86 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH SPOILERON OB PCU WING ATTACH POINT NUTS ARE CORRODED. (C-CHECK- RO 11/11/21) REPLACED LH SPOILERON OB PCU WING ATTACH NUTS AND IB PCU LOWER MOUNT BOLT ANTI ROTATION PLATE BOLTS AND TEFLON WASHER IAW CRJ-200 AMM 27-62-01-000/400-801 AND 27-64-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

ALL LH FLIGHT SPOILER HINGE NUTS ARE CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED ALL LH FLIGHT SPOILER HINGE NUTS IAW CRJ-200 AMM 27-64-05-000/400-801. OPS TEST OF FLIGHT SPOILER GOOD IAW CRJ 200 AMM 27-64-00-710-801. REFERENCE ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LBL9 FS399 -- FS409+128 FLOOR SEAT TRACK SEGMENT IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL 9 FS 399 - FS 409+128 IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LH SPOILERON HAS CORRODED HARDWARE ON ALL FOUR HINGES. (C-CHECK- RO 11/11/21) REPLACED L'H SPOILERON CORRODED HARDWARE AT ALL 4 HINGES WITH SERVICEABLE HARDWARE IAW CRJ 200 AMM 27-64-01- 400-801 STEP2B (1) THRU (4). OPA TEST OF FLIGHT SPOILER GOOD IAW CRJ 200 AMM 27-64-00-710-801. REFERENCE ATTACHED CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 42,862 hrs · 40,002 cycles

INTERCOSTAL CLIP ANGLE AT FS484 ON OB SIDE OF LBL9 FLOOR BEAM IS CRACKED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED INTERCOSTAL CLIP ANGLE PN: 601R31171-27 AT FS484 ON OB SIDE OF LBL9 IAW CRJ-200 SRM 51-42-06 AND 51-42-21

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

ALL LH SPOILERON HINGE BOLT KEEPERS HAVE CORRODED HARDWARE. (C-CHECK- RO 11/11/21) REPLACED AND INSTALLED NEW HARDWARE ON LH SPOILERON HINGE BOLT KEEPERS IAW CRJ 200 AMM 27-64-01-400-801 STEP 2.C(1)-(3)

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

ALL LH FLIGHT SPOILER HINGE BOLT KEEPERS HAVE CORRODED HARDWARE. (C-CHECK- RO 11/11/21) REPLACED LH FLIGHT SPOILER BOLT RETENTION ANGLE HARDWARE IAW CRJ 200 AMM 27-64-05-400-801

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

STRAP IS CORRODED BETWEEN FLOOR BEAM BL0 TO RBL9 AT F.S.559 (C-CHECK- RO 11/11/21) REMOVED CORROSION ON STRAP AT FS 559 BETWEEN BL0 TO RBL9 ORIGINAL MAT'L THK .050 REMAINING MAT'L THK .047 MAT'L LOSS .003 IS IN LIMITS IAW CRJ 200 SRM 51-21-06, AND 53-00-00 TOOL ID# WVACT204981 CAL DATE 09 FEB 2021 CAL DUE DATE 09 FEB 2022

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

FLOOR BEAM LBL9 UPPER CAP IS CORRODED BETWEEN F.S. 409+128 TO F.S. 559 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED FLOOR BEAM CAP AT LBL 9 FS 409+128 - FS 599 IAW REO 601R-53-41-2952 REV -- DATED 8/24/21, REO 601R-53-00-005 REV B DATED 2011-01-06, 601R-53-00-027 REV D DATED 26-NOV-2009. COMPLIED WITH TASK CARD 51-900-1003-SKY AND ATTACHED COMPETED FORM 337. NO WEIGHT CHANGE NONE.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

FLOOR BEAM RBL 9 UPPER CAP IS CORRODED AT MULTIPLE LOCATIONS BETWEEN F.S.409+128 TO F.S.559 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED FLOOR BEAM CAP AT FS 409+128 - FS 559 AT RBL 9 IAW REO 601R-53-41-2953 REV -- DATED 2021-08-24 & REO 601R-53-00-027 REV D DATED 26-NOV-2009. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

SEAT TRACK SEGMENT IS CORRODED AT LBL 9 BETWEEN F.S.409+128 TO F.S.559 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL 9 FS 409+128 - FS 559 IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

SEAT TRACK SEGMENT RBL 9 IS CORRODED BETWEEN F.S.409+128 TO F.S.559 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED SEAT TRACK SEGMENT FS 409+128 TO FS 559 IAW CRJ 200 AMM 53-01-11-400-802.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 364 TO F.S. 409.0+16. (C-CHECK- RO 11/11/21) REMOVED CORRODED CABIN SIDE SET TRACK F.S. 364.00 - 409.00+16 AND INSTALLED NEW SERVICEABLE TRACK IAW CRJ-200 AMM 53-01-11-000/400-802.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

L/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 499 TO F.S. 544. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED DAMAGED SEAT TRACK IAW CRJ200 AMM 53-01-11-000/400-802

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 364 TO F.S. 394 (C-CHECK- RO 11/11/21) INSTALLED NEW SERVICABLE FLOOR TRACK IAW CRJ200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 409.0+112 TO F.S. 449.85. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 409.0+112 TO F.S. 449.85, IAW CRJ-200 AMM 53-01-11-000/400-802, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

F.S. 280 ANGLE IS CORRODED BETWEEN LBL9 AND RBL9. (C-CHECK- RO 11/11/21) REMOVED CORROSION ON FS 280 ANGLE BETWEEN LBL9 AND RBL 9 IAW CRJ 200 SRM 51-21-06.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

F.S. 280 J ANGLE IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND TREATED CORROSION ON FS 280 J ANGLE IAW: CRJ200-SRM-51-21-06, AND FOUND TO BE WITHIN LIMITS IAW: CRJ200-SRM-53-00-00. REF CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

L/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 544 TO F.S. 559.0+80. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED DAMAGED SEAT TRACK IAW CRJ200 AMM 53-01-11-000/400-802

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 484 TO F.S. 544. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH SIDE SEAT TRACK BETWEEN FS 484 TO FS 554 IAW CRJ 200 AMM 53-01-11-000/400-802 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CRACKED · airframe 42,862 hrs · 40,002 cycles

F.S. 280 RBL 9 INBOARD AND OUTBOARD CLIPS ARE CRACKED. (C-CHECK- RO 11/11/21) REMOVED DAMAGED CLIPS ON I/B AND O/B SIDE OF RBL9 AT FS 280 AND FABRICATED, AND INSTALLED NEW SERVICEABLE CLIPS FROM MATERIAL S6144-14 REFERENCED FROM RE0# 601R-53-11-171, REV D, DATED: 13FEB07 AND CRJ200-SRM-51-40-11, AND CRJ200-SRM-51-42-21. REFERENCE CAMP# 23343186 FOR APPLICATION OF PAINT

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

L/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 409.0+112 TO F.S. 461.0 (C-CHECK- RO 11/11/21) REMOVED L/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 409.0+112 TO F.S.449.85 . INSTALLED NEW FABRICATED SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802. REFERENCE CAMP 23520307 FOR FABRICATION. PERFORMED REPAIR TO SEAT TRACK RETAINER FOR SEAT TRACK. IAW SRM 51-21-06. REFERENCE CONTINUATION CARD FOR ALL WORK PERFORMED.

Part: RAIL — GOUGED · airframe 42,862 hrs · 40,002 cycles

R/H SIDE SEAT TRACK IS GOUGED BETWEEN F.S. 409.0+16 TO F.S. 409.0+31. (C-CHECK- RO 11/11/21) REMOVED CORRODED SIDE SEAT TRACK F.S. 409.00+16 - F.S. 409.00+112 AND INSTALLED NEW SERVICEABLE SIDE SEAT TRACK IAW CRJ-200 AMM 53-01-11-000/400-802.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

L/H SIDE SEAT TRACK IS CORRODED AT F.S. 473. (C-CHECK- RO 11/11/21) REMOVED CORRODED SIDE SEAT TRACK AT F.S. 449.85 - F.S. 500.00 AND INSTALLED NEW SERVICEABLE SIDE SET TRACK IAW CRJ-200 SRM CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR ALL WORK PERFORMED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LEFT FLOOR SILL FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS. (C-CHECK- RO 11/11/21) REMOVED LH FLOOR SILL CORROSION FROM FS 409+128 - FS 559 IAW REO 601R-53-41-666 REV C DATED 2012-11-06, REO 601R-53-41-2963 REV -- DATED 2021-10-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

RIGHT FLOOR SILL ANGLE FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS. (C-CHECK- RO 11/11/21) REMOVED DAMAGE FROM RH FLOOR SILL ANGLE FROM FS 409+128 - FS 559 IAW REO 601R-53-41-666 REV C DATED 2012-11-06, REO 601R-53-41-2959 REV -- DATED 2021-10-07. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — DENTED · airframe 42,862 hrs · 40,002 cycles

EXTERNAL FUSELAGE SKIN HAS SEVERAL DENTS/PRTRUDING DENTS FROM FS 574 TO FS 621, BETWEEN STR 27 AND STR 21L. (C-CHECK- RO 11/11/21) REPAIRED DAMAGE AT FS 574- FS 621 STR 27- STR 21L IAW REO 601R-53-61-7711 REV -- DATED 2021-10-08, REO 601R-53-61-7712 REV L DATED 2021-09-06, AND REO 601R-51-00-309 REV A DATED 2017-08-23. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

FLOOR TENSION STRAP CORRODED AT FS559 BETWEEN LBL45 AND LBL27. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CORRODED TENSION STRAP IAW CRJ200 SRM 51-42-06

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LEFT FLOOR SILL FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS. (C-CHECK- RO 11/11/21) DISCREPANCY SHOULD READ RH FLOOR SILL FROM FS 409+128 TO FS 559 IS CORRODED. REMOVED CORROSION FROM RH FLOOR SILL AT FS 409+128 - FS 559 IAW REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

LEFT FLOOR SILL ANGLE FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS. (C-CHECK- RO 11/11/21) REMOVED DAMAGE FROM LH FLOOR SILL ANGLE FROM FS 409+128 - FS 559 AND REOAIRED IAW REO 601R-53-41-2963 REV A DATED 2021-10-07 AND REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: BRACKET — CRACKED · airframe 42,862 hrs · 40,002 cycles

RH AND LH UPPER OBLEAK ANGLES ON FS.621.00 BULKHEAD AT STR. 14L AND 14R ARE CRACKED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH AND LH UPPER OBLEAK ANGLES ON FS.621.00 BULKHEAD AT STR. 14L AND 14R IAW CRJ 200 SRM 51-42-21-00

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

FWD SIDE OF RIB AT FS.310.00 IS CORRODED BETWEEN STR. 25L AND 25R. (C-CHECK- RO 11/11/21) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE AT FS 319. REMOVED AND REPLACED FRAME SEGMENT AT FS 319 AT STR 25L AND 25R IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

CORROSION ON LOWER FUSELAGE SKIN AROUND DRAIN HOLES AND FASTENERS FS 559+94 TO FS 559+112 AT STR 27. (C-CHECK- RO 11/11/21) REPAIRED LOWER FUSELAGE SKIN AT STGR27 BETWEEN FS559+94 AND FS559+112 IAW MHIRJ REO 601R-53-51-600 REV-- DATED 2021-09-03. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H FLIGHT SPOILER OTBD HINGE NUT AND RETAINING PLATE BOLTS, AND INBD AND OTBD BONDING JUMPER HARDWARE IS CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CORRODED HARDWARE IAW CRJ 200 AMM 27-64-05-000/400-801

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H FLAP BPSU MOUNTING BOLTS ARE CORRODED (C-CHECK- RO 11/11/21) REPLACED AND INSTALLED NEW HARDWARE ON RH FLAP BPSU IAW CRJ 200 AMM 27-51-10-400-801 STEPS 3.B.(4), (6)-(7). REPLACED ONE AT A TIME AND NO ELECTRICAL CONNECTORS WERE DISCONNECTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

CORROSION ON SKIN PANEL AND AROUND FASTENER HEADS AROUND LAV SERVICING POINT FS 559+80 TO FS 559+112 BETWEEN STR 21R AND 24R. (C-CHECK- RO 11/11/21) REMOVED CORROSION FROM SKIN AT FS 559+80 - FS 559+112 AT STR 21R - STR 24R IAW REO 601R-53-61-597 REV -- DATED 2021-09-27. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

#4 R/H FLAP ACTUATOR FWD ATTACH NUT IS CORRODED (C-CHECK- RO 11/11/21) RECIEVED IN A SERVICEABLE FWD ATTACHMENT NUT REFERENCE MX TRANS# 21955104 WVAC JOB 97404125 OP 5527 FOR REMOVAL AND REPLACEMENT.

Part: NONE — CHAFED · airframe 42,862 hrs · 40,002 cycles

L/H AILERON UPPER L/E SKIN SHROUD DEEPLY CHAFFED ACROSS ENTIRE LENGTH (C-CHECK- RO 11/11/21) REMOVED, LOCATED, DRILLED, AND INSTALLED NEW L/H AILERON LEADING EDGE SHROUD IAW CRJ 200 SRM 51-42-06 AND 51-40-11

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H AILERON INBOARD AFT PCU LINK ATTACH NUT, INBOARD CENTER HINGE NUT, AND ATTACHING HARWARE FOR BOTH BONDING JUMPERS ARE CORRODED (C-CHECK- RO 11/11/21) R/H AILERON INBOARD AFT PCU LINK ATTACH NUT, INBOARD CENTER HINGE NUT, AND ATTACHING HARWARE FOR BOTH BONDING JUMPERS WERE REMOVED AND REPLACED IAW CRJ 200 AMM 27-15-01-000/400-801. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

CORROSION ON LOWER FUSELAGE SKIN FS 559+80 BETWEEN STR 26L AND 26R (C-CHECK- RO 11/11/21) REPAIRED LOWER FUSELAGE SKIN AT FS559+80 BETWEEN STGR26L & 26R IAW MHIRJ REO 601R-53-51-600 REV-- DATED 2021-09-03. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H SPOILERON OTBD CENTER HINGE NUT, ALL LOWER ATTACH HARDWARE FOR INBD AND OTBD ACUATORS, INBD AND OTBD CENTER HINGE RETAINER PLATE SCREWS, AND ATTACHING SCREWS FOR BONDING JUMPERS ARE CORRODED. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED R/H SPOILERON OTBD CENTER HINGE NUT, ALL LOWER ATTACH HARDWARE FOR INBD AND OTBD ACUATORS, INBD AND OTBD CENTER HINGE RETAINER PLATE SCREWS, AND ATTACHING SCREWS FOR BONDING JUMPER IAW CRJ 200 AMM 27-61-01-400-801. OPS, BLEEDS, AND RIGS CHECK "GOOD"

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

L/H FLAP OUTBD. BPSU (4 EA.MOUNT BOLTS) RUSTED (C-CHECK- RO 11/11/21) REPLACED AND INSTALLED NEW HARDWARE ON LH FLAP O/B PBSU IAW CRJ 200 AMM 27-51-10-400-801 STEPS 3.B.(4), (6)-(7). REPLACED ONE AT A TIME AND NO ELECTRICAL CONNECTIONS WERE DISCONNECTED

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

R/H SPOILERON INBD HINGE NUT AND RETAINING PLATE BOLTS ARE CORRODED (C-CHECK- RO 11/11/21) REMOVED AND REPLACED RH SPOILERON IB HINGE NUT AND RETAINING PLATE HARDWARE IAW CRJ-200 AMM 27-64-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

BOTH INBD. AND OUTBD. L/H ELEV. FLUTTER DAMPERS , ROD END HARDWARE (2 EA. NUTS AND WASHERS RUSTED) (C-CHECK- RO 11/11/21) REMOVED AND REPLACED LH IB OB FLUTTER DAMPER AFT HARDWARE IAW CRJ200 AMM 27-34-05-400-801 REFERENCE MX TRANS FOR INSTALL AND OPS TEST 23288929

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

HORIZONTAL STAB.TOP CANTED RIB ( FWD. STEADY FITTING) L/H LOWER HARDWAREWARE NUTS CORRODED IN THE MILLED POCKET (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CORRODED HARDWARE IAW CRJ 200 AMM 20-21-00-910-801

Part: NONE — CORRODED · airframe 42,862 hrs · 40,002 cycles

HORIZONTAL STAB. BATHTUB FITTINGS (16 TOTAL JOLL BOLTS CORRODED) (C-CHECK- RO 11/11/21) REMOVED AND REPLACED CORRODED JO-BOLTS IN BATHTUB FITTINGS IAW CRJ 200 SRM 51-42-22

Part: STIFFENER — DAMAGED · airframe 42,862 hrs · 40,002 cycles

FUSELAGE FS409+128 LBL18 INBD VERTICAL POST HAS AN INDICATION .2" LONG BY 50% FSH IN THE AFT RADIUS AT WL69. FAILED NDT INSPECTION. (C-CHECK- RO 11/11/21) REMOVED AND REPLACED VERTICAL POST ASSY AT FS 409+128 LBL 18 WITH NEW IAW CRJ 200 SRM 51-42-02, 51-42-26, AND BOMBARDIER REO 601R-53-41-889 REV -D DATED 2018-10-04. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — DAMAGED · airframe 42,862 hrs · 40,002 cycles

R/H I/B FLAP PANEL 684CB HAS DRILL DAMAGE AROUND FASTENER HOLE, AND STRUCTURE UNDER PANEL ON I/B FLAP. (C-CHECK- RO 11/11/21) COMPLIED WITH REO 601R-27-52-2435 REV -- DATED 2021-09-10 REPAIRED R/H I/B FLAP PANEL 684CB AND UNDERLYING STRUCTURE ON I/B FLAP.COMPLETED TASK CARD 51-900-1003-SKY. 337 AND SDR ATTACHED. NO WEIGHT CHANGE

Part: NONE — CHAFED · airframe 42,862 hrs · 40,002 cycles

R/H I/B FLAP VANE CHAFFED AT W/S 104.099 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED WITH NEW R/H INBOARD FLAP VANE CAP AT WS 104.099 IAW CRJ 200 SRM 51-40-11,51-42-13, & SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED, REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — WORN · airframe 42,862 hrs · 40,002 cycles

PILOTS FLIGHT COMPARTMENT FLOOR SEAT RAILS HAVE EXCESSIVE WEAR (C-CHECK- RO 11/11/21) REMOVED AND REPLACED PILOT SEAT TRACKS IAW CRJ 200 AMM 53-01-05-400-801

Part: NONE — CHAFED · airframe 42,862 hrs · 40,002 cycles

R/H I/B FLAP VANE CHAFFED AT W/S 56.30 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED WITH NEW R/H INBRD L/E FLAP VANE SKIN IAW CRJ 200 SRM 51-40-11 AND 51-42-13

Part: NONE — CHAFED · airframe 42,862 hrs · 40,002 cycles

R/H I/B FLAP VANE CHAFFED AT W/S 139.924 (C-CHECK- RO 11/11/21) FOUND DAMAGE TO BE OUT OF LIMITS OF REO 601R-57-52-004 REV D, DATED 2012-12-19 AND REQUIRES REPLACEMENT. REMOVED AND REPLACED R/H I/B FLAP VANE L/E SKIN AND END CAP RIB AT WS 139.924 AND WS 147 IAW CRJ 200 SRM 51-42-13. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — DAMAGED · airframe 42,862 hrs · 40,002 cycles

L/H I/B FLAP VANE CHAFFED AT W/S 56.30 (C-CHECK- RO 11/11/21) REPLACED CHAFED CAP ON THE LH I/B FLAP VANE AT W/S 56.30 IAW CRJ 200 SRM 51-42-13

Part: NONE — CHAFED · airframe 42,862 hrs · 40,002 cycles

L/H I/B FLAP VANE CHAFFED AT W/S 139.924 (C-CHECK- RO 11/11/21) REPLACED CHAFED CAP LH I/B FLAP VANE AT W/S 139.924 IAW CRJ 200 SRM 51-42-13

Part: NONE — CHAFED · airframe 42,862 hrs · 40,002 cycles

L/H I/B FLAP VANE CHAFFED AT W/S 104.099 (C-CHECK- RO 11/11/21) REPLACED CHAFED CAP AT LH I/B FLAP VANE AT W/S 104.099 IAW CRJ 200 SRM 51-42-13

Part: NONE — DENTED · airframe 42,862 hrs · 40,002 cycles

SMALL DENT JUST FWD OF PAX DOOR JUST BELOW GOLD STRIPE (C-CHECK- RO 11/11/21) REPAIRED DENT AT FS 280 BETWEEN STR 18L AND 17L IAW REO 601R-53-21-3498 REV -- DATED 9/12/21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 42,542 hrs · 39,732 cycles

CA SIDE WINDSHIELD CRACKED IN FLIGHT (FLIGHT 5106 . THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22550210 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED CAPTAIN SIDE WINSHIELD PER TASK CARD 56-220-1000-SKY."

Part: WINDSHIELD — CRACKED (RIGHT) · airframe 42,339 hrs · 39,559 cycles

ON DECENT OUT OF FL250 FIRST OFFICER SIDE WINDSCREEN STARTED TO CRACK AND PROPAGATE. LARGE CRACK ALMOST FULL LENGTH OF WINDSCREEN. FLIGHT 1365 - FILED CLOSED REMOVED AND REPLACED THE RH WINDSHIELD IAW CRJ 200 AMM 56-11-01 AND TASK CARD 56-220-1000-SKY COCKPIT WINDSHIELD AND SIDE WINDOW INSTALLATION. PERFORMED OPS CHECK OF THE WINDSHIELD TEMP CONTROL IAW CRJ 200 AMM 30-41-01, AND PRESSURIZED THE A/C IAW CRJ 200 AMM 21-32-00 TO CHECK FOR LEAKS, NO LEAKS NOTED AND OPS CHECK GOOD AT THIS TIME. A/C OK FOR SERVICE.

Part: NONE — DAMAGED · airframe 42,862 hrs · 40,002 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 11/11/21) COMPLIED WITH REO 601R-53-41-1116 REV. C DATED 2017-03-09 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM 337 COMPLETED AND ATTACHED. WEIGHT CHANGE OF AN ADDED 5.4 POUNDS. . SEE ATTACHED CONTINUE CARD AND TASK CARD FOR DETAILS OF WORK PERFORMED.

Part: BUSHING — DAMAGED · airframe 42,862 hrs · 40,002 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR IAW CRJ-200 AMM 20-26-00-910-803 AND REO 601R-57-51-015 REV NC DATED 95-07-04 . REF ATTACHED CONTINUATION FOR WORK PERFORMED. COMPLETED M-337 AND TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE.

Part: BUSHING — DAMAGED · airframe 42,862 hrs · 40,002 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK- RO 11/11/21) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR IAW CRJ-200 AMM 20-26-00-910-803 AND REO 601R-57-51-015 REV NC DATED 95-07-04 . REF ATTACHED CONTINUATION FOR WORK PERFORMED. COMPLETED M-337 AND TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE.

Part: TRACK — DAMAGED (CARGO DOOR) · airframe 41,514 hrs · 38,792 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA - CARGO DOOR AFT TRACK DAMAGED WHERE LOWER ROLLER RIDES WHEN DOOR IS OPEN. C/W TEMPORARY REPAIR PER REO. PERMANENT REPAIR DUE WITHIN 600 FH BY 41542.9 TAT., THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, A PERMANENT REPAIR COMPLETE, REMOVED AND REPLACED CARGO DOOR AFT TRACK ASSY IAW SRM.

Part: SKIN — CORRODED (WING) · airframe 38,294 hrs · 35,693 cycles

WING PLANK HOLE IS CORRODED. REPAIRED WING PLANK IAW REO.

Part: FLOOR SKIN — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

PRESSURE FLOOR SKIN DAMAGED. REPAIRED PRESSURE FLOOR SKIN IAW REO.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

FUSELAGE SKIN DAMAGED. REPAIRED DAMAGE IAW REO.

Part: FRAME — CORRODED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

FRAME IS CORRODED. R & R THE FRAME IAW SRM.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

FUSELAGE SKIN DAMAGED. REPAIRED FUSELAGE SKIN IAW REO.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

FUSELAGE SKIN DAMAGED. REPAIRED FUSELAGE SKIN IAW REO.

Part: ANGLE — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

CAP ANGLE DAMAGED. REPAIRED CAP ANGLE IAW REO.

Part: BULKHEAD — CRACKED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

PRESSURE BULKHEAD CRACKED. REPAIRED BULKHEAD IAW REO.

Part: BULKHEAD — CRACKED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

PRESSURE BULKHEAD HAS MULTIPLE CRACK INDICATIONS. THE REPAIRED BULKHEAD IAW REO.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 38,294 hrs · 35,693 cycles

PAX DOOR FRAME CRACKED. . REPAIRED THE DOOR FRAME IAW REO.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 38,294 hrs · 35,693 cycles

PAX DOOR FRAME CRACKED. REPAIRED THE DOOR FRAME IAW REO.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,294 hrs · 35,693 cycles

PAX DOOR INTERCOSTAL CORRODED. REPAIRED THE INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,294 hrs · 35,693 cycles

PAX DOOR INTERCOSTAL CORRODED. REPAIRED THE INTERCOSTAL IAW SRM.

Part: DOOR FRAME — CRACKED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

PAX DOOR FRAME CRACKED. REPAIRED THE DOOR FRAME IAW REO.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 38,294 hrs · 35,693 cycles

NLG WHEEL WELL IS CRACKED. REPAIRED IAW REO.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 38,294 hrs · 35,693 cycles

CARGO DOOR SILL CORRODED. REPLACED THE CARGO DOOR SILL IAW REO.

Part: FITTING — CRACKED (ESCAPE HATCH) · airframe 38,294 hrs · 35,693 cycles

ESCAPE HATCH FITTING CRACKED. R&R ESCAPE HATCH FITTING IAW SRM.

Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM.

Part: ACCESS PANEL — CORRODED (WING) · airframe 38,294 hrs · 35,693 cycles

WING ACCESS PANEL IS CORRODED. REPAIRED THE DAMAGE IAW REO.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

FUSELAGE SKIN DAMAGED. REPAIRED SKIN IAW REO.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

SKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

SKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

SKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.

Part: SKIN — DAMAGED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

SKIN PANEL DAMAGED. BLENDED SKIN PANEL IAW REO.

Part: FRAME — CORRODED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

FRAME IS CORRODED. THE REPLACED FRAME SECTOR IAW SRM.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 38,294 hrs · 35,693 cycles

SERVICE DOOR ANGLE IS CORRODED. REPLACED ANGLE IAW SRM.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · airframe 38,294 hrs · 35,693 cycles

PRESSURE FLOOR PANEL CORRODED. BLENDED AREA OF PRESSURE FLOOR PANEL IAW NDTM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,318 hrs · 33,461 cycles

FOUND EMERGENCY LIGHTS SWITCH IN THE ON POSITION, EMERGENCY LIGHTS INOPERATIVE. RECHARGED EMERGENCY LIGHT BATTERY SYSTEM WITH APU GENERATOR SYSTEM FOR 60 MIN SYSTEM RESET NO FURTHER FAULTS NOTED MCC, AC OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,805 hrs · 31,805 cycles

EMERGENCY LIGHTS ARE INOPERATIVE, REQUIRES TROUBLESHOOTING. EMERGENCY LIGHTS ARE INOPERATIVE, TROUBLESHOOTING IS REQUIRED. UPON TROUBLESHOOTING, FOUND EMERGENCY LIGHT CHARGER ASSY NR 4 UNSERVICABLE. REMOVED UNSERVICABLE CHARGER ASSY AND REPLACED WITH SERVICABLE PART IAW AMM 33-51-05-000-801 AND 33-51-05-400-801. OPS TEST GOOD.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND LT SEAT RAIL BETWEEN FS 499.00 AND FS 449.00+85, MARKED AND NEED TO BE EVALUATED. REMOVED LT SEAT RAIL IAW SRM 53-01-11-946-003. INSTALLED 3EA SCREWS IN SEAT RAIL ON LT SIDE FROM FS 449.00+85-499.00 IAW AMM 5-01-11-400-802. INSTALLED SEAT RAIL ON LT WALL AT FS 449.00+85-499 IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO -601R-53-00-055.

Part: SEAT TRACK — CORRODED (BS 364-559) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ALONG SEAT TRACK AT RBL9 BETWEEN FS364, FS409.00+128 AND 559.00 AND 394.00, MARKED AND NEED TO BE EVALUATED. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. CORROSION BLENDED SRM 51-1-06, 53-41-49 STATES TO USE SRM 53-21-49. ALLOWABLE DAMAGE COMPLIED WITH EC/TC REO 601R-53-00-485 BY FABRICATING NEW SEAT RAIL, RBL9, FS 409.00+128 TPO FS 559.00, RAIL REO601R-53-00-485. REMOVED SEAT TRACK AT RL9 BETWEEN FS 409.00+128 -559.00 IAW AMM 53-1-11-000-802. INSTALLED NEW FABRICATED SEAT TRACK AT RBL 9 BETWEEN FS 409.00+128-559.00 IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ALONG RT SEAT RAIL BETWEEN FS 409-00 + 16 & 409.00 + 112, NEED TO BE EVALUATED. REMOVED RT SEAT RAIL BETWEEN FS 409.00+16-409.00+112 IAW AMM 53-01-11-000-802. LOCATED DRILLED AND INSTALLED RT SEAT RAIL AT FS 409.00+16-409.00+112 IAW SRM 51-40-11 AND AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (NOT REPROTED) · airframe 34,805 hrs · 31,805 cycles

CARGO DOOR FLOOR SILL HAS CORROSION AROUND FLOORBOARD SCREW HOLES. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526-REV.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 34,805 hrs · 31,805 cycles

CORROSION AROUND 3 SCREW HOLES ON RBL 9 FLOORBEAM AND PANEL 282LRF SUPPORT STRUCTURE AT FS 559.96. REMOVED CORROSION IAW SRM 51-21-06. EVALAUTED BLEND AREA AND FOUND TO BE WITHIN THE ALLOWABLE LIMITS OF REO 601R-53-00-005, FIGURE 1. COMPLIED WITH REO601R-53-00-005. THIS IS A MAJOR REPAIR. THIS REPAIR HAS BEEN RECLASSIED AS A MAJOR REPAIR IAW EC/TC REO 601R-53-00-005.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ON LT SEAT RAIL BETWEEN FS 409.00+16 & 409.00+112, MARKED & NEED TO BE EVALUATED. REMOVED SEAT RAIL BETWEEN FS 409.00+16-409.00+112 IAW SRM 53-01-11-000-802. LOCATED EVERY OTHER HOLE AND DRILLED AND INSTALLED NEW SERVICABLE SEAT TRACK AT FS 409.00+16-409.00+112 IAW SRM 51-40-11 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ALONG SEAT TRACK AT LBL9 BETWEEN FS 394.00AND 409.00, MARKED AND NEED TO BE EVALUATED. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49, CORROSION BLENDED IAW SRM 51-21-06. COMPLIED WITH EC/TC 601R-53-00-485 BY FABRICATING NEW SEAT RAIL, LBL9 FS394 000-409.00 IAW REO 601R-53-00-485. REMOVED SEAT TRACK AT LBL9 BTW FS 394.00-409.00 IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK AT LBL9 FROM FS 394-FS 409 IAW AMM 53-01-11-400-802. COMPLIED WITH EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ALONG SEAT TRACK AT LBL9 BETWEEN FS 559.00 & 559.00+80, MARKED & NEED TO BE EVALUATED. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION BLENDED IAW SRM 51-21-06, SRM 53-51-49 STATES TO USE SRM 53-21-49 IAW ALLOWABLE DAMAGE LIMITS. REMOVED SEAT TRACK AT LBL9 BETWEEN FS 559.00-559.00+80 IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT RAIL AT LBL9, FROM FS 559- FS 559+80 IAW AMM 53-01-11-400-802. LOCATED & DRILLED 30EA HOLES IN SEAT RAIL IAW SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ALONG SEAT TRACK AT RBL9, BETWEEN FS 394.00 & 409.00+128, MARKED & NEED TO BE EVALUATED. EVALUATED SEAT TRACK CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49, CORROSION REMOVED IAW SRM 51-21-06. COMPLIED WITH EC/TC 601R-53-00-485 STEPS 1-7, 9 BY FABRICATING NEW SEAT RAIL AT RBL 9, FS 394.00-409.00+128 IAW REO 601R-53-00-485. REMOVED SEAT TRACK AT RBL9 BETWEEN FS 394.00-409.00+128 IAW AMM 53-01-11-000-802. INSTALLED SEAT RAIL AT RBL9 FROM FS 394- FS 409.00+128 IAW AMM 53-01-11-400-802. FABRICATED SEAT RAIL IAW GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 34,805 hrs · 31,805 cycles

2 EA SHORT SEAT TRACKS ON LBL9 CORRODED BETWEEN FS 559.80 TO 574. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION REMOVED IAW SRM 51-21-06, SRM 53-51-49, STATES TO USE SRM 53-21-49 FOR ALLOWABLE DAMAGE LIMITS. COMPLIED WITH EC/TC REO 601R-53-00-485 BY FABRICATING 2 SEAT RAILS, LBL9 FS 559+80 TO FS 574 IAW GREO 601R-53-00-485, REV A. REMOVED SEAT TRACKSON LBL9 AT FS 559.80-574 IAW AMM 53-00-49-000-801. INSTALLED NEW FABRICATED SEAT TRACKS LBL9, FS 559.80 TO 574 IAW AMM 53-00-49-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 589-605) · airframe 34,805 hrs · 31,805 cycles

CORROSION AROUND 2 SCREW HOLES ON RBL27 FLOORBEAM BETWEEN FS 589 TO 605 UNDER PANEL 282KRF. REMOVED CORROSION IAW SRM 51-21-06. EVALAUTED BLEND AREAS AROUND 2EA SCREW HOLES ON RBL27 FLOORBEAM FS589 TO 605 AND FOUND THEM TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-61-43 AND 53-00-00, FIG 101. COMPLIED WITH ECTC REO601R-53-00-005.

Part: SEAT TRACK — CORRODED (BS 499-559) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ON LT SEAT RAIL BETWEEN FS 559.00+80 499.00, MARKED & NEED TO BE EVALUATED. EVALAUTED SEAT RAIL AND FOUND TO BE EXFOILATED 100 PERCENT OUT OF LIMITS IAW SRM 53-21-49, 51-21-06. REMOVED UNSERIVCABLE SEAT RAIL FROM LT SIDE BETWEEN FS449-FS559.00+80 IAW AMM 53-01-11-000-802. LOCATED AND DRILLED 46EA HOLES IN NEW SERVICEABLE SEAT RAIL, IAW SRM 51-40-11. INSTALLED NEW SEAT RAIL AT FS 499.00 TO FS 559.00+80 ON LT SIDE WALL IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559-570) · airframe 34,805 hrs · 31,805 cycles

2 EACH SHORT SEAT TRACKS CORRODED ON RBL9 AND BETWEEN FS 559+90 TO FS 570. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION BLENDED IAW SRM 51-21-06 SRM 53-51-49 TO USE SRM 53-21-49 FOR ALLOWABLE DAMAGE LIMITS. COMPLIED WITH EC/TC REO 601R-53-00-485 BY FABRICATION 2 SEAT RAILS RBL9, FS 559+90 TO FS 550 IAW GREO 601R-53-00-485, REV A. REMOVED SEAT TRACKS AT RBL9, FS 559.90-570.00 IAW AMM 53-00-49-000-801. INSTALLED NEW FABRICATED SEAT TRACKS RBL9, FS 559+90-570 IAW AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ALONG SEAT TRACK AT RBL9 BETWEEN FS 364.00 AND 394.00, MARKED AND NEED TO BE EVALUATED. SEAT TRACK AT RBL9 BETWEEN FS 364.00 AND 394.00 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-01. REMOVED CORROSION IAW SRM 51-21-06-00. REMOVED SEAT TRACK AT RBL9 BETWEEN FS 364.00-394.00 IAW AMM 53-01-11-000-802. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. INSTALLED NEW SERIVCABLE SEAT TRACK AT RBL 9, FS 364.00-394.00 IAW AMM 53-01-11-420-001.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 34,805 hrs · 31,805 cycles

CORROSION ON RBL 9 FLOORBEAM AROUND SCREW HOLE AT FS 559+112 UNDER PANEL 281 ALF. REMOVED CORROSION IAW SRM 51-21-06. DURING CORROSION REMOVAL, CORROSION FOUND TO PENETRATE 100 PERCENT OF FLOOR SUPPORT STRUCTURE. COMPLIED WITH SRM 53-00-43-02 FLOOR SUPPORT STRUCTURE REPAIR NR 2 FROM FS 559.00+80 TO FS 559.00+112. RECEIVED AND COMPLIED WITH REO 601R-53-00-610. COMPLIED WITH ECTC REO 601R-53-00-610. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,805 hrs · 31,805 cycles

SHORT SEAT TRACK ON RBL9 CORRODED BETWEEN FS 559+80 TO 559.96. EVALUATED CORROSION ON SEAT TRACK & FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION BLENDED IAW SRM 51-21-06, SRM 53-51-49 TO USE SRM 53-21-49 FOR ALLOWABLE DAMAGE LIMITS. COMPLIED WITH EC/TC REO 601R-53-00-485 BY FABRICATING SEAT RAILS, RBL27 FS 559+80 TO FS 559+96 IAW GREO 601R-53-00-485, REV A. REMOVED SEAT TRACKS AT RBL27 BETWEEN FS 559.80-559+96 IAW AMM 53-00-49-000-801. INSTALLED NEW FABRICATED SEAT TRACKS RBL27, FS 559+80 TO FS 559+96 IAW AMM 53-00-49-400-801.

Part: SUPPORT — CORRODED (BS 559) · airframe 34,805 hrs · 31,805 cycles

CORROSION AROUND SEVERAL SCREW HOLES UNDER PANEL 282ERF SUPPORT STRUCTURE BETWEEN RBL 9 & 27 AND BETWEEN FS 559.80 TO 559.96. BLENDED CORROSION IAW SRM 51-21-06. BLENDED AREAS AT FS 559.80 AND FS 559.96 CROSS-BEAMS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00. AND BEAM CAPS AT RBL 9 & 27 ARE WITHIN LIMITS IAW GREO 601R-53-00-005. COMPLIED WITH GREO 601R-53-00-005, AND COMPLIED WITH ECTC REO 601R-53-00-005. THIS REPAIR IS A MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND LT SEAT RAIL BETWEEN FS 364.00 AND 409.00+64, MARKED AND NEED TO BE EVALUATED. REMOVED LT SEAT RAIL BETWEEN FS 364.00-409.00+64 IAW AMM 53-01-11-000-802. INSTALLED LT SEAT RAIL AT 349.00-409.00 IAW AMM 53-01-11-400-802. LOCATED & DRILLED 15EA REMAINING HOLES IN SEAT TRACK IAW SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ALONG SEAT TRACK AT RBL9 BETWEEN FS 559.00 AND 559.00+80, MARKED AND NEED TO BE EVALUATED. EVALAUTED CORROSION ON SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. CORROSION BLENDED IAW SRM 51-21-06. SRM 53-51-49 STATES TO USE SRM 53-21-49 FOR ALLOWABLE DAMAGE LIMITS. REMOVED SEAT TRACK RBL9 BETWEEN FS559.00-559.00+80 IAW AMM 53-01-11-000-802. DRILLED COUNTER SUNK 40 HOLES IN NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SERVICABLE SEAT RAIL AT RBL9 BETWEEN FS 559.00+ FS 559+80 IAW AMM 53-01-11 400-802.

Part: HINGE — CORRODED (PAX DOOR) · airframe 34,805 hrs · 31,805 cycles

ASD BOTTOM STEP HINGE ASSY CORRODED. REMOVED AND INSTALLED NEW ASD BOTOM STEP HINGE ASSY IAW AMM 52-11-04-000-808, AMM 52-11-00-400-807 DRILLED UP NEW ASD BOTTOM STEP HINGE ASSY IAW SRM 51-40-11, SRM 51-41-00. THIS REPAIR IS CLASSIFIED AS A MAJOR/MINOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 34,805 hrs · 31,805 cycles

CORROSION FOUND ALONG SEAT TRACK AT LBL9, BETWEEN FS 364.00 AND 394.00, MARKED & NEED TO BE EVALUATED. EVALUATED CORROSION ON SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49 CORROSION BLENDED IAW SRM 51-21-06. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT TRACK AT LBL9 BETWEEN FS 364.00-394.00 IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE TRACK IAW AMM 53-01-11-420-001.

Part: ATTACH FITTING — CRACKED (WINDOW FRAME) · airframe 34,805 hrs · 31,805 cycles

LT AND RT LOWER WINDSHIELD CENTER POST ATTACH FITTINGS ARE CRACKED. R & R LT & RT LOWER WINDSHIELD FITTINGS IAW SRM 51-40-11-00 AND 51-42-21-00, DWG 601R33007. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 34,805 hrs · 31,805 cycles

SIDE WALL SEAT RAIL CORRODED AT FS 544.00-559.00+80 LT SIDE. LOCATED AND DRILLED, 42 EA, FASTENER HOLES ON NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. R & R SEAT TRACK AT RT SIDE WALL FS 544.00-559.00+80 IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: LUG — CHAFED (RT WING TE FLAP) · airframe 34,805 hrs · 31,805 cycles

RIGHT INBD FLAP INBD HINGE LUG PLATE CHAFED, GOUGED ON INBD SIDE OF LUG. REMOVED DAMAGE AT RT INBD FLAP HINGE LUG PLATE INBD SIDE OF LUG IAW SRM 51-12-00-00, TR51-31 BLEND LENGTH 0.900" X .0700" X 0.018" D IAW SRM 57-00-00-01 LUG PLATE NOT SPECIFIED ON ALLOWABLE DAMAGE LIMITS. COMPLIED WITH ECTC REO 601R-57-52-1536. BLEND OUT INBD FLAP HINGE ARM ATTCHMENT LUG PLATES AT RT INBD/OTBD LUG, WS80.5 IS COMPLETED IAW REO 601R-57-52-1536 REV A. RESTORED FINISH TO RT INBD. FLAP INBD HINGE LUG PLATE IAW REO 601R-57-52-1536.

Part: ANGLE — CRACKED (BS 625 BULKHEAD) · airframe 34,805 hrs · 31,805 cycles

FS 625.00 RIGHT SIDE PRESSURE BULKHEAD CLIP CRACKED. R & R RT FS 625 PRESSURE BULKHEAD CLIP REF SRM 51-42-21.

Part: ANGLE — CRACKED (BS 625 BULKHEAD) · airframe 34,805 hrs · 31,805 cycles

FS 625.00 LT SIDE PRESSURE BULKHEAD CLIP CRACKED. R & R LT FS 625 PRESSURE BULKHEAD CLIP REF SRM 51-42-21.

Part: PANEL — DAMAGED (UNKNOWN) · airframe 34,805 hrs · 31,805 cycles

LIGHTNING STRIKE PANELS UNDER CABIN FLOORBOARD 231CLF REQUIRES REMOVAL TO C/W INSPECTION. REMOVED 3 LIGHTNING STRIKE PANELS UNDER 231CLF FOR INSPECTION IAW AMM 53-01-01-000-806. INSTALLED 3 LIGHTNING PROTECTION PANELS UNDER CABIN FLOORBOARD 231CLF IAW AMM 53-01-01-410-801, OK TO CLOSE. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: FLASHLIGHT — FAILED (COCKPIT) · airframe 34,784 hrs · 31,785 cycles

F/O FLASHLIGHT INOPERATIVE. REPLACED F/O FLASHLIGHT IAW AMM 25-61-00. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 34,609 hrs · 31,589 cycles

F/A AND SEVERAL PASSENGERS REPORTED ELECTRICAL ODOR AROUND ROW 10 AND 11 ENROUTE, ACFT DIVERTED FOR MAINTENANCE. TURNED LIGHTS ON. COULD NOT SENSE ANY ELECTRICAL ODOR AROUND RO 10/11. ACFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,482 hrs · 31,455 cycles

EMERGENCY LIGHTS DO NOT WORK. CHARGED EMERGENCY LIGHTS, OPS CHECKED GOOD IAW AMM 33-50-01.

Part: SIGN — DAMAGED (CABIN) · airframe 34,120 hrs · 31,067 cycles

LIGHTED EXIT SIGN BY SERVICE DOOR DAMAGED. R & R SIGN IAW AMM 33-51-13. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: TRACK — DIRTY (PAX DOOR) · airframe 33,722 hrs · 30,672 cycles

MAIN CABIN DOOR STICKING AND VERY HARD TO OPEN AND CLOSE. CLEANED TRASH OUT OF PASSENGER DOOR TRACK & CLEANED PASSENGER DOOR SEAL. OPS CHECK GOOD IAW AMM 52-11-00.

Part: ACM — FAILED (NR 2) · airframe 33,274 hrs · 30,215 cycles

ON CLIMBOUT, F/A REPORTED SMOKE IN THE CABIN PULLED UP ECS PAGE AND RT PACK WAS SHOWING 120 IN AUTO MODE. AUTO MODE WOULD NOT CONTROL TEMP SO SWITCHED TO MANUEL MODE. DECREASED TEMP AND SMOKE CLEARED. ACFT RETURNED TO DEPARTURE. R & R NR 2 ACM IAW AMM 21-51-10. AFDL NR FA196521 FOR OPS CHECK. ACM SERVICED IAW AMM 12-13-21. AIPC - 21-51-00. FIG. 10, 45C.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,717 hrs · 28,626 cycles

EMERGENCY LIGHTS WILL NOT ILLUMINATE. ALLOWED FOR THE EMERGENCY LIGHTS BATTERY PACKS TO CHARGE FOR ONE HOUR FROM APU POWER. COMPLIED WITH AN OPS TEST, OPS TESTED GOOD, ALL INTERIOR & EXTERIOR EMERGENCY LIGHTS ILLUMINATED. PROCEDURES DONE IAW AMM 33-51-00. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,018 hrs · 27,903 cycles

RT EXTERIOR OVERWING AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21.

Part: SUPPORT BRACKET — CORRODED (BS 349) · airframe 30,639 hrs · 27,493 cycles

AFT THRESHOLD GUSSET, SUPPORT BRACKET, CORRODED AT LEG JUST AFT OF FS 349 AT SERVICE DOOR. REMOVED AFT THRESHOLD GUSSET, SUPPORT BRACKET AND FOUND OUT OF LIMITS IAW SRM 51-42-21. INSTALLED NEW SUPPORT BRACKET IAW SRM 51-42-21.

Part: SKIN — DAMAGED (BS 574-605) · airframe 30,639 hrs · 27,493 cycles

LOW PRESSURE AIR COVER DAMAGED SKIN AFT OF OPENING BETWEEN FS 574 AND FS 605 AND BETWEEN STRINGERS 21 - 26R. REPAIRED IAW REO 601R-53-61-5005. MAJOR REPAIR.

Part: ANGLE — CORRODED (BS 319.7) · airframe 30,639 hrs · 27,493 cycles

ANGLE CORRODED AT DOOR SILL AT FS 319.7 AND 349. INSTALLED NEW ANGLE IAW SRM 51-42-06, 51-42-13 AND 51-42-21. REPAIR CLASSIFIED AS MAJOR.

Part: STRUCTURE — CORRODED (DOOR FRAME) · airframe 30,639 hrs · 27,493 cycles

CORROSION FOUND ON LOWER SERVICE DOOR SEAL SURROUND AROUND MULTIPLE SCREW HEADS LOWER SEGMENT. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 572. R & R SERVICE DOOR SEAL SURROUND IAW SRM 51-41-02.

Part: SILL — DAMAGED (SERVICE DOOR) · airframe 30,639 hrs · 27,493 cycles

NINE MISDRILLED HOLES AT SERVICE DOOR LOWER SILL REF DWG NR 601R38303 VIEW (BL) REVAN. REPAIRED IAW REO 601R-53-21-2458. REPAIR CLASSIFIED AS MAJOR.

Part: BRACKET — CORRODED (DOOR FRAME) · airframe 30,639 hrs · 27,493 cycles

CORROSION FOUND ON AFT SIDE OF FRAME BRACKET, LOWER, AT BS 310 SERVICE DOOR CUTOUT. REPAIRED IAW 601R-53021-2459.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,639 hrs · 27,492 cycles

REAR PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE CARGO DOOR. REPAIRED IAW GREO 601R-53-61-1541. REPAIR CLASSIFIED AS MAJOR.

Part: CHANNEL — CRACKED (BULKHEAD) · airframe 30,639 hrs · 27,492 cycles

CRACK INDICATION ON VERTICAL BULKHEAD CHANNEL AT BS 409 BL 0. REMOVED CHANNEL AND ISTALLED IAW 51-42-06, 51-42-21, 51-40-06 AND SRM 51-40-11. MAJOR REPAIR.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 30,639 hrs · 27,493 cycles

LOWER SILL AT SERVICE DOOR ENTRY CUT OUT HAS CORROSION. REPAIRED IAW SRM 51-42-06-00, 51-42-06-00, 51-42-34, 51-42-21. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (BS 473.15-499) · airframe 30,639 hrs · 27,493 cycles

RT SIDE FLOOR SUPPORT HAS CORROSION BETWEEN BS 473.15 TO 499. REPAIRED IAW GREO 601R-53-41-666, REO 601R-53-41-1726 & REO 601R-53-41-616.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 30,639 hrs · 27,492 cycles

CORROSION ON LT SIDE FLOOR SUPPORT BETWEEN 559+80 AND 559+64. REPAIRED IAW REO 601R-52-00-526.

Part: FLOOR PANEL — CRACKED (BS 202) · airframe 30,639 hrs · 27,492 cycles

LT FWD HYD BAY FLOOR PANEL CRACKED FWD OF FS 202 AT HYD GAUGE BRACKET. REPAIRED IAW REO 601R-53-11-081.

Part: FLOOR SUPPORT — CORRODED (BS 449.85-473.15) · airframe 30,639 hrs · 27,493 cycles

CORROSION ON LT FLOOR SUPPORT BETWEEN FS 449.85 & 473.15. REPAIRED IAW REO 601R-53-41-666 REV C.

Part: SKIN — DAMAGED (BS 574-605) · airframe 30,639 hrs · 27,493 cycles

LOW PRESSURE AIR COVER DAMAGED SKIN AFT OF OPENING BETWEEN FS 574 - 605 BETWEEN STRINGERS 21 - 26R. REPAIRED IAW REO 601R-53-61-5005 PERMANENT REPAIR. REPAIR CLASSIFIED AS MAJOR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,463 hrs · 27,307 cycles

FOUND CRACK ON PAX DOOR MIDDLE AFT DRAG ANGLE. REPAIRED IAW REO 601R-52-11-1359, REV A.

Part: SIGN — MISSING (CABIN) · airframe 29,919 hrs · 26,754 cycles

"EMERGENCY EXIT" SIGN MISSING FROM MAIN CABIN DOOR.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 29,751 hrs · 26,584 cycles

F/A FLASHLIGHT WILL NOT STAY LIT. R&R FLASHLIGHT. NO FURTHER DEFECT. OPS CHECK TESTED GOOD IAW AMM 25-61-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,664 hrs · 26,490 cycles

F/A'S FLASHLIGHT INOPERATIVE. R & R THE F/A'S FLASHLIGHT IAW AMM 25-61-01. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,454 hrs · 26,266 cycles

RT MIDDLE OVERWING EMERGENCY LIGHT INOPERTAIVE. REPLACED LAMP IAW AMM 33-51-21. OPS TESTED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,403 hrs · 24,012 cycles

NR 7 EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 7 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,358 hrs · 23,964 cycles

EMERGENCY LIGHTS ARE ON WITH THE CORRECT NORMAL SWITCH POSITIONS. RESET AND OPS CHECKED EMERGENCY LIGHTS IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: PLACARD — DETERIORATED · airframe 27,167 hrs · 23,753 cycles

ASD "EXIT" PLACARD IS DETERIORATED. R & R ASD EXIT PLACARD IAW AMM 11-30-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,107 hrs · 23,695 cycles

WARDROBE EXIT LIGHT WIRE SPLICE IS BROKEN. REPLACED SPLICE ON EXIT LIGHT WIRE IAW ESPM 20-16-00. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: FRAME — CRACKED (BS 409) · airframe 27,107 hrs · 23,695 cycles

INDICATION NOTED AT FS 409+128, WL 69.00, RBL 18 INBD CHANNEL 60 PERCENT FSH & OTBD CHANNEL 85 PERCENT FSH AT .040 EDM NOTCH APPROX 10 IN LENGTH, FAILED NDT.REPAIRED IAW REO 601R-53-41-889 REV A.

Part: FLOOR SUPPORT — CORRODED · airframe 27,107 hrs · 23,695 cycles

FLOOR SUPPORT CORRODED ON VERTICAL FACE ON FWD SIDE. REPAIRED IAW SRM 51-42-06 AND 51-42-21.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,107 hrs · 23,695 cycles

CARGO DOOR CUTOUT FLOOR SUPPORT SILL IS CORRODED.

Part: INTERCOSTAL — CORRODED (BS 349) · airframe 27,107 hrs · 23,695 cycles

FS 349.0, LBL 36 TO LBL 45 INTERCOSTAL CORRODED ON END. REPAIRED IAW REO 601R-53-21-2207.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 27,118 hrs · 23,706 cycles

FLOOR SUPPORT SILL AT RBL 36 IS CORRODED BETWEEN 559+96 AND 559+112. C/W STEPS 4 & 5 OF REO 601R-53-51-175. ECTC REQ'D. MFG ISSUED REV 601R-53-51-175, REV--, DATED 10/24/11 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR GMM 3-3 PROCEDURES, PRIOR TO THE ACFT BEING RETURNED TO SERVICE. RII FOUND TO BE SATISFACTORY. (SDR CLOSED)

Part: SUPPORT ANGLE — CORRODED (BS 349) · airframe 27,107 hrs · 23,695 cycles

SUPPORT ANGLE AT FS 349, LBL 38 CORRODED. REMOVED SUPPORT ANGLE IAW SRM 51-42-06. SUPPORT ANGLE IS BEING REPLACED IAW REO 601R-53-21-2207, STEP 12.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,107 hrs · 23,695 cycles

CARGO DOOR CUTOUT FLOOR SUPPORT SILL IS CORRODED.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 27,107 hrs · 23,695 cycles

FLOOR SUPPORT AT LBL 27 FROM FS 559+112 TO 621 CORRODED. REMOVED CORRODED SUPPORT, LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FLOOR SUPPORT IAW REO 601R-53-61-3778 AND GREO 601R-53-61-3778.

Part: POST — CRACKED (BS 409) · airframe 27,107 hrs · 23,695 cycles

CRACK INDICATION NOTED AT FS 409+128, WL 69.00 RBL 18 INBD CHANNEL 60 PERCENT FSH AND OTBD CHANNEL 85 PERCENT FSH AT .040 EDM APPROX .10" LENGTH. FAILED NDT. REMOVED IAW SRM 51-42-06. INSTALLED IAW REO 601R-53-41-889.

Part: POST — CRACKED (BS 409) · airframe 27,107 hrs · 23,695 cycles

CRACK INDICATION NOTED AT FS 409+128, WL 69.00, LBL 18 OTBD CHANNEL IN RADIUS 59 PERCENT FULL SCREEN HEIGHT AT .040 EDM NOTCH. REMOVED POST IAW SRM 51-42-06. DRILLED NEW POST IAW SRM 51-40-11. INSTALLED THE NEW POST IAW SRM 51-42-06 AND REO 601R-53-41-889A.

Part: BEAM — CORRODED (BS 605) · airframe 27,107 hrs · 23,695 cycles

FS 605 TRANSVERSE BEAM AT LBL 40 TO 45 HAS CORROSION ON UPPER AND LOWER SURFACE OF FLANGE. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE WITHIN ACCEPTABLE LIMITS IAW SRM 53-00-00, FIG 102 WITH MAX MATERIAL REMOVED OF 0.004" MAX MATERIAL ALLOWED 0.006" REMAINING MATERIAL IS 0.059". BLENDED AREA IAW SRM 51-25-01.

Part: BEAM — CORRODED (BS 589) · airframe 27,107 hrs · 23,695 cycles

FS 589 TRANSVERSE BEAM AT LBL 40 TO 45 HAS CORROSION ON UPPER AND LOWER SURFACE OF FLANGE. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE WITHIN ACCEPTABLE LIMITS IAW SRM 53-00-00, FIG 102 WITH MAX MATERIAL REMOVED OF 0.003" MAX MATERIAL ALLOWED IS 0.006". REMAINING MATERIAL IS 0.060". BLENDED AREA IAW SRM 51-25-01.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 27,107 hrs · 23,695 cycles

FLOOR SUPPORT AT LBL 9 FROM FS 574-621 IS CORRODED. REMOVED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-42-06, 51-40-11 AND 51-42-21. INSTALLED SERVICEABLE FLOOR SUPPORT IAW REO 601R-53-61-3780.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 27,107 hrs · 23,695 cycles

FS 484 FLOOR SUPPORT AT RBL 27 IS CRACKED. REMOVED FLOOR SUPPORT. LOCATED, DRILLED AND DEBURRED AND INSTALLED NEW SUPPORT IAW SRM 51-40-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,107 hrs · 23,695 cycles

FLOOR SUPPORT CORRODED ON VERTICAL FACE ON FWD SIDE. REMOVED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 27,107 hrs · 23,695 cycles

FS 484 FLOOR SUPPORT AT LBL 36 IS CRACKED. REPAIRED IAW REO 601R-53-41-059.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 27,107 hrs · 23,695 cycles

FS 280 FLOORBEAM CORRODED AROUND 221ALF FASTENER HOLES RBL 9.0 TO LBL 9.0. REPAIRED IAW SRM 51J-42-06 AND 51-41-04. REPAIR IS CLASSIFIED AS A MINOR.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 27,107 hrs · 23,695 cycles

FLOOR SUPPORT AT RBL 36 IS CORRODED BETWEEN 559+96 - +112. REMOVED CORROSION, MAX REMOVED .005", REPAIRED IAW SRM 53-51-43.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 27,107 hrs · 23,695 cycles

FS 621 PRESSURE BULKHEAD HAS ONE CRACKED ISOLATOR AT RBL 27. REPLACED FOUR RIVETS. REPLACED ISOLATOR IAW SRM 51-42-06. REPAIR IS CLASSIFIED AS MINOR.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 27,107 hrs · 23,695 cycles

SEAT TRACK CORRODED AT FS 364, RBL 9. REMOVED CORRODED SEAT TRACK IAW AMM TASK 53-01-11-000-802 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 27,107 hrs · 23,695 cycles

FLOOR SUPPORT AT RBL 9, FS 574 TO 621 CORRODED. BLENDED CORROSION, REMOVED .005" MATERIAL IAW SRM 51-21-06.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,107 hrs · 23,695 cycles

CARGO TRACK AT RBL 8 FS 559+96 CORRODED. REMOVED CORRODED CARGO TRACK IAW SRM 51-41-00. DRILLED NEW CARGO TRACK IAW SRM 51-40-11. INSTALLED NEW CARGO TRACK IAW AMM 53-01-11.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 27,107 hrs · 23,695 cycles

FS 349, LBL 36 TO LBL 45 FLOORBEAM CORRODED OTBD END. REPAIRED IAW SRM 51-42-06 & 51-42-21.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 27,107 hrs · 23,695 cycles

FLOORBEAM BETWEEN LBL 9 & 18 AT FS 589 CORRODED. BLENDED CORROSION, MAX REMOVED MATERIAL .006 IAW SRM 51-21-06. REPAIR CLASSIFIED AS MINOR.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,107 hrs · 23,695 cycles

CARGO TRACK LBL 9 IS CORRODED. (OPEN)

Part: FRAME — CORRODED (BS 319.7) · airframe 27,107 hrs · 23,695 cycles

FRAME CORRODED AT FS 319.70 BETWEEN S25R & S25L. REMOVED CORRODED FRAME SECTION AND INSTALLED NEW FRAME SECTION IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 461) · airframe 27,107 hrs · 23,695 cycles

FS 461 FLOOR SUPPORT AT RBL 9 IS CRACKED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21 & 51-42-22. DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-11. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06, SRM 51-42-22, SRM 51-42-21. REPAIR IS CLASSIFIED AS A MINOR.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,107 hrs · 23,695 cycles

CARGO TRACK AT LBL 27, FS 559+112 IS CORRODED. REMOVED AND REPLACED IAW SRM 51-41-02, 51-40-11 AND 51-41-04.

Part: FLOORBEAM — CORRODED (BS 559-621) · airframe 27,107 hrs · 23,695 cycles

FLOORBEAM CAP AT LBL 27 FROM FS 559+112 TO FS 621 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND OUT OF LIMITS, REPAIRED IAW REO 601R-53-51-174.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 27,107 hrs · 23,695 cycles

FS 484, FLOOR SUPPORT AT LBL 27 IS CRACKED. R & R CRACKED FLOOR SUPPORT IAW SRM 51-40-11, 51-42-06 & 51-42-21. REPAIR IS CLASSIFIED AS A MINOR.

Part: ANGLE — CRACKED (BS 625) · airframe 27,107 hrs · 23,695 cycles

LEFT UPPER OBLIQUE ANGLE CRACKED FS 625. R & R OBLIQUE ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21. MINOR REPAIR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,996 hrs · 19,039 cycles

FS 621 TO FS 625 RT UPPER OBLIQUE ANGLE RBL 45.0 STR 14R CRACKED IN RADIUS 1.25 INCH.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 22,996 hrs · 19,039 cycles

FS 621 FWD PRESSURE BULKHEAD HAS A CRACKED ISOLATOR BRACKET JUST ABOVE WL 106 AT LBL 18.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 22,996 hrs · 19,039 cycles

WHILE PERFORMING HFEC INSPECTION OF FS 460.00 PRESSURE FLOOR MULTIPLE INDICATIONS OF VARYING LENGTHS WERE NOTED APPROX 1.25 INCH FWD OF INTERCOSTALS IN THE THREE BAYS BETWEEN LBL 18.00 AND RBL 9.00. INDICATIONS RANGE FROM 30 - 60 PERCENT FSH. FAILS NDT INSPECTION AT THIS TIME. REPAIRED FS 460 PRESSURE FLOOR IAW REO 601R-53-41-884. COMPLIED WITH EC/TC REO 601R-53-41-884A. PERFORMED TEMPORARY REPAIR PER REO 601R-53-41-884 REVISION C. ALL REQUIREMENTS OF THE REO WERE MET.

Part: SIGN — BROKEN (CABIN) · airframe 23,003 hrs · 19,046 cycles

SERVICE DOOR UPPER SURROUND EXIT SIGN IS BROKE.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 22,996 hrs · 19,039 cycles

RIGHT FS 559 BULKHEAD WEB HAS 2 INDICATIONS NOTED: 1) O/B OF RBL 9.0 WL 58.70 APPROX .2 INCH IN LENGTH 80 PERCENT FSH, 2) I/B OF RBL 18.0 WL 59.10 APPROX .3 INCH IN LENGTH 80 PERCENT FSH. BOTH AREAS FAILED NDT INSPECTION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,996 hrs · 19,039 cycles

FRAME 718.0 HAS A .025 INCH LONG CRACK FROM TOP RIVET TO EDGE OF ATTACHING POINT JUST BELOW STR 11R ON FWD SIDE OF FRAME MEMBER. TRIMMED CRACKED FLANGE PER REO 601R-53-61-193 REV A, VIEW C. C/W LPI OF THE RT FRAME 718.0 REPAIR CUT LINE PER REO 601R-53-61-193 "A" IAW NDTM PT 1, 51-20-08. NO INDICATIONS NOTED AT THIS TIME. FABRICATED -4 ANGLE AND -6 FILLER PER REO 601R-53-61-193 "A". INSTALLED REPAIR -4 ANGLE, AND -6 FILLER PER REO 601R-53-61-193 "A". C/W EO 600-53-0067 REV A.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 22,996 hrs · 19,039 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .1 INCH IN LENGTH 60 PERCENT FSH, FAILED NDT INSPECTION. C/W REO 601R-53-61-1230 STEPS 1-24 REPAIR TO PRESSURE BULKHEAD WEB FS 621 LINTEL REV D.

Part: LIGHT — BROKEN (CABIN) · airframe 22,767 hrs · 18,817 cycles

FLIGHT ATTENDANT WARDROBE OUTBOARD EMERGENCY LIGHT BASE BROKEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,767 hrs · 18,817 cycles

CABIN FLOOR FORWARD MOST EMERGENCY LIGHT STRIP INOP.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,426 hrs · 18,489 cycles

F/O'S WINDSHIELD CRACKED ON DESCENT BELOW 12000 FEET. EMERGENCY DECLARED.

Part: ANCHOR FITTING — CRACKED (ASD) · airframe 22,352 hrs · 18,424 cycles

ASD AFT ANCHOR FITTING CRACKED.

Part: FLAP — FAILED (WING) · airframe 21,755 hrs · 17,847 cycles

FLAP FAIL AT 45 DEGREES. EMERGENCY DECLARED.

Part: SIGN — MISSING (CABIN) · airframe 21,730 hrs · 17,827 cycles

EXIT SIGN MISSING BY MAIN CABIN DOOR.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 21,199 hrs · 17,332 cycles

PAX DR OUTER HANDLE BROKEN

Part: SHEAR PIN — INOPERATIVE (SERVICE DOOR) · airframe 20,933 hrs · 17,077 cycles

SERVICE DOOR SHEAR PIN RELEASE HANDLE INOPERATIVE. FLT 4497. REMOVED AND REPLACED SERVICE DOOR SHEAR PIN OPS CHECKED GOOD. IN ACCORDANCE WITH AMM 42-41-00. OK FOR SERVICE. (B)

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 20,872 hrs · 17,022 cycles

MAIN CABIN DOOR COULD NOT BE OPENED FROM OUTSIDE. COMPLIED WITH INSP OF PAX DOOR HANDLE CLEARED AND LUBE HANDLE OPS CHECK GOOD OK FOR SERVICE PER CRJ200AMM52-10.--[SDR CLOSED](B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,199 hrs · 16,447 cycles

FWD FACING OVERWING EMERGENCY EXIT LIGHTS IN CEILING INOP. RESET SYS C/B.

Part: FLAP — FAILED (WING) · airframe 20,111 hrs · 16,365 cycles

WHEN SELECTING FLAPS FROM 0 DEG TO 8 DEG ON APPROACH, FLAPS FAILED AT 2 DEG. FLAPS FAIL MESSAGE. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,658 hrs · 15,995 cycles

EMERGENCY EXIT CEILING LIGHT INOP.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,066 hrs · 15,502 cycles

CAPTAIN`S FLASHLIGHT INOP. WILL NOT TURN OFF. BATTERY DEAD.

Part: LIGHT — DETACHED (CABIN) · airframe 18,120 hrs · 14,733 cycles

EMERGENCY LIGHT AT TOP OF ENTRY DOOR NEED TO BE REATTACHED. FLT 4568 DEL 69 MINS.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 18,098 hrs · 14,714 cycles

TROUBLESHOT EMERGENCY LIGHTS FOUND NR 1 BATTERY MOUNT CHARGER UNIT DEFECTIVE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,075 hrs · 14,698 cycles

ASD FLOOD LIGHT AND BOTH FWD EXTERIOR EMERGENCY LIGHTS INOP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

LEFT SIDE FS 625 CLIP CRACKED (MARKED). INSTALLED NEW LEFT SIDE 625 CLIP PER CRJ200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 04/16/07.

Part: FRAME — CORRODED (BS 349) · airframe 18,075 hrs · 14,698 cycles

FS 349 FRAME HAS CORROSION DAMAGE IN MAIN AVIONICS BAY CORROSION WAS REMOVED UNDER THE TWO CLIPS ON FS 349 IAW CRJ 200 SRM 51-21-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

RIGHT SIDE FS 625 CLIP CRACKED (MARKED). INSTALLED NEW RIGHT SIDE 625 CLIP PER CRJ200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 04/16/07.

Part: FRAME — CORRODED (BS 333) · airframe 18,075 hrs · 14,698 cycles

FS 333 FRAME HAS CORROSION DAMAGE IN MAIN AVIONICS BAY REMOVED FASTNERS ,BLENDED FS 333 FRAME IAW CRJ 200 SRM 51-21-06.

Part: SUPPORT BRACKET — CRACKED (CARGO BAY) · airframe 18,075 hrs · 14,698 cycles

CARGO DOOR TRACK CROSSBEAM AFT LOWER SUPPORT BRACKET CRACKED (MARKED). REMOVED AND REPLACED CARGO DOOR TRACK CROSSBEAM AFT LOWER SUPPORT BRACKET PER CRJ 200 SRM 51-42-20. SUPPLEMENTAL - SDR CLOSED 04/16/07.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

CORROSION ON LEFT SIDE PRESSURE FLOOR SKIN FROM FS 460 TO FS 513. [SUP 4-23-07] REPAIRED IAW ALL FAA APPROVED DATA.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 18,075 hrs · 14,698 cycles

VERTICAL L/E UPPER CORNER CRACKED ON RIGHT SIDE. CUT AWAY DAMAGED AREA (C/W STEPS 1AND 2) IAW REO 601R-55-32-165 CB7015474. SUPPLEMENTAL - SDR CLOSED 04/16/07.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

CORROSION ON RIGHT PRESSURE FLOOR FROM FS 460 TO FS 513. [SUP 4-23-07] COMPLIED WITH ALL FAA APPROVED DATA.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

MINOR SURFACE CORROSION RT SIDE FLOOR SILL RBL 36 STA 349 (MARKED). REMOVED SURFACE CORROSION IAW CRJ SRM 51-21-06. 04/08/2007. SUPPLEMENTAL - SDR CLOSED 04/16/07.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

STA 280 BULKHEAD WEB CRACKED AT LBL 9.

Part: BEAM — CORRODED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

MINOR SURFACE CORROSION STA 349 TRANSVERSE BEAM LOWER SURFACE LT SIDE AT LBL 36 (MARKED). REMOVED AND BLENDED UNDER TEFLON STRIP AND ON THE UNDERSIDE OF 349 AT LBL 36, FOUND TO BE WITHIN LIMITS, .059 MATERIAL REMAINING PER CRJ 200 SRM 53-00-00. SEALED AND INSTALLED TEFLON STRIP CRJ 200 SRM 51-23-00 AND 51-42-13. SUPPLEMENTAL - SDR CLOSED 04/16/07.

Part: BEAM — CORRODED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

STA 349 TRANSVERSE BEAM RT SIDE CORRODED AT RBL 36 (MARKED). REMOVED CORROSION IAW CRJ200 SRM 51-21-06.

Part: FITTING — CORRODED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

FLOOR SUPPORT STRINGER AFT CLEAT (CUT OUT CUP FOR HANDRAIL ARM) CORRODED. BLENDED AND REMOVED AFT CUP, FOUND TO BE OUT OF LIMITS PER CRJ 200 SRM 53-00-00 BAT 23167. DRILLED UP NEW AFT CUP REF CRJ-200 SRM 51-42-06, AND ADDED NEW NUT PLATES. INSTALLED NEW CUP ON STRINGER PER CRJ 200 SRM 51-42-06, BAT23167 4/14/2007. SUPPLEMENTAL - SDR CLOSED 04/16/07.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

STA 280 BULKHEAD WEB CRACKED AT RBL 9. BEGAN REMOVING FASTENERS THROUGH LT AND RT STA 280 WEB AND RELATED STRUCTURE AS PER CRJ 200 SRM 51-42-00 AND REO 601R-53-11-926. EWB 702040900. CONTINUED REMOVAL OF ASSOCIATED PARTS. MADE CUT AND REMOVED CRACKED / CORRODED CENTER SECTION OF WEB AT LBL 7 THRU RBL 7. REMOVED IAW REO 601R-53-11-926. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES PER REO 601R-53-11-926 IAW CRJ 200 NDTM PART 1, 51-20-06. NO DEFECTS NOTED. STARTED TRIMMING AND LOCATED EXISTING HOLES IN -1 AND -2 DOUBLER, TRIMMED -3 FILLER AND LOCATED EXISTING HOLES. TRIMMED -5 AFT FLOORS SUPPORT ANGLE TO SIZE IAW CRJ 200 SRM 601R-53-11-926 MS 7022223. FABRICATED -13, -18 SHIM FROM 2024 T3 .050" B

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

STA 280 RBL 9 AND LBL 9 INBOARD CLIPS CRACKED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

STA 280 FWD AND AFT FLOOR SUPPORT ANGLES CORRODED AT BL 0. REMOVED FWD FLOOR SUPPORT ANGLE REF CRJ200SRM 51-42-06, AFT FLOOR SUPPORT ANGLE WILL BE REPAIRED ON N/R-00090 W/O 55779. PSP19749 10APR07. INSTALLED NEW FWD FLOOR SUPPORT ANGLE PER CRJ 200 SRM 51-42-06. SUPPLEMENTAL - SDR CLOSED 04/16/07.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 18,075 hrs · 14,698 cycles

FLOOR SUPPORT STRINGER AT PAX DOOR SILL CORRODED AND MISSING NUT PLATES (MARKED). BLENDED AND REMOVED STRINGER AND AFT CUP BOTH FOUND TO BE OUT OF LIMITS PER CRJ 200 SRM 53-00-00. DRILLED UP NEW PAX DOOR SILL REF CRJ-200 SRM 51-42-21, AND CRJ-200 SRM 51-42-06. ACCOMPLISHED NUTPLATE MOD AND STARTED INSTALLING SILL ON A/C PER REO 601R-52-11-577, CRJ200 SRM 51-42-21, AND 51-42-06. INSTALLED UPPER ANGLES ON ASD SILL PLATE IAW CRJ 200 SRM 51-42-06. INSTALLED DOOR PROX SWITCH AND OPS CK GOOD IAW CRJ 200 AMM 52-70-04.

Part: SUPPORT BEAM — CRACKED (RT ENGINE) · airframe 18,075 hrs · 14,698 cycles

RT ENGINE SUPPORT BEAM LOWER WEB CRACKED AT FWD INBD NUT PLATE FOR ACCESS PANEL [SUP 4-23-07] REPAIRED IAW ALL FAA APPROVED DATA.

Part: SUPPORT BEAM — CRACKED (LT ENGINE) · airframe 18,075 hrs · 14,698 cycles

LT ENGINE SUPPORT BEAM LOWER WEB CRACKED AT FWD IB NUT PLATE FOR ACCESS PANEL. [SUP 4-23-07] COMPLIED WITH ALL FAA APPROVED DATA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,739 hrs · 14,443 cycles

AFT EMERGENCY FLOOR LIGHT INOP.

Part: UNKNOWN — UNKNOWN (NLG STEERING) · airframe 17,634 hrs · 14,366 cycles

AFTER ROTATION -STEERING INOP- CAUTION. AFTER LANDING ROLLOUT TURNED ON NWS PER MX CTL. STEERING INOP MSG CAME ON AGAIN. EMERGENCY EQUIPMENT ON STANDBY. FLTS 4785, 4762 CX.

Part: LIGHT — BROKEN (CABIN) · airframe 17,534 hrs · 14,303 cycles

FLOOR LEVEL LIGHTS BETWEEN 6CD BROKEN.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 17,117 hrs · 14,002 cycles

ON TAKEOFF RECEIVED STEERING INOP MSG. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY EQUIP ON STANDBY AS A PRECAUTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,827 hrs · 13,001 cycles

LT EXT EMERGENCY LIGHT FWD OF EMERGENCY DOOR INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,705 hrs · 12,913 cycles

FOUND ROW 5 SEAT EMERGENCY FLOOR LIGHT INOP AND PLASTIC COVER BROKEN.

Part: BULB — BURNED OUT (GALLEY) · airframe 15,705 hrs · 12,913 cycles

GALLEY SERVICE DOOR EMERGENCY LIGHT HAS BULBS OUT.

Part: ACTUATOR — MALFUNCTIONED (NLG)

DURING APPROACH, CREW RECEIVED A RED GEAR DISAGREE MESSAGE ON EICAS ALONG WITH A MASTER WARNING INDICATING THE NOSE GEAR WAS NOT DOWN. THE TOWER CONFIRMED THE NOSE GEAR WAS NOT DOWN WHILE PERFORMING A GO AROUND. THE CREW COMPLIED WITH THE QRH AND CYCLED THE MANUAL RELEASE HANDLE, WITH THE NOSE GEAR STILL NOT INDICATING DOWN. THE CREW CYCLED THE GEAR HANDLE TO THE DOWN POSITION AND THE NOSE GEAR THEN INDICATED IT WAS DOWN AND LOCKED. THE CREW DECLARED AN EMERGENCY AND REQUESTED THE EMERGENCY VEHICLES BE DISPATCHED AS A PRECAUTION. THE AIRCRAFT LANDED SAFETY IN RIC. MAINTENANCE REMOVED AND REPLACED THE NLG DOOR SELECTOR VALVE AND NLG UPLOCK ACTUATOR. OPS CHECK GOOD, AC OK FOR SERVICE. (K)

Part: SELECTOR VALVE — MALFUNCTIONED (NLG DOOR)

DURING APPROACH, CREW RECEIVED A RED GEAR DISAGREE MESSAGE ON THE EICAS ALONG WITH A MASTER WARNING INDICATING THE NOSE GEAR WAS NOT DOWN. TOWER CONFIRMED THE NOSE GEAR WAS NOT DOWN WHILE PERFORMING A GO AROUND. CREW COMPLIED WITH THE QRH AND CYCLED THE MANUAL RELEASE HANDLE, WITH NOSE GEAR STILL NOT INDICATING DOWN. THE CREW CYCLED THE GEAR HANDLE TO THE DOWN POSITION AND THE NOSE GEAR THEN INDICATED IT WAS DOWN AND LOCKED. CREW DECLARED AN EMERGENCY AND REQUESTED THE EMERGENCY VEHICLES BE DISPATCHED. MX REMOVED & REPLACED NLG DOOR SELECTOR VALVE AND THE NLG UPLOCK ACTUATOR. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K)

Part: PLACARD — WORN (CABIN)

DURING AN A-CHECK, THE EXIT PLACARD ON THE PASSENGER DOOR WAS FOUND NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE EXIT PLACARD ON THE PASSENGER DOOR. (K)

Part: WARNING LIGHT — ILLUMINATED (NLG)

DURING APPROACH, UPON SELECTING THE GEAR DOWN AND FLAPS TO 30 DEGREES, THE CREW RECEIVED A GREEN GEAR DOWN INDICATION FOR THE MLG FOLLOWED BY A NOSE GEAR DISAGREE WARNING MESSAGE ON EICAS. AT APPROX 1,000 FT, THE CREW INITIATED A GO AROUND AND DECLARED AN EMERGENCY. UPON COMPLIANCE WITH THE QRH, 3 GREEN INDICATION FOR THE LANDING GEAR WERE RECEIVED AND THE AIRCRAFT THEN LANDED SAFELY. MAINT TESTED AND INSPECTED THE NLG EXTENSION SYSTEM AND CYCLED NLG NUMEROUS TIMES IAW MM AND COULD NOT DUPLICATE THE DISCREPANCY. NO DEFECTS WERE NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE, THE RT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK GOOD. AC OK FOR SERVICE. (K)

Part: SWITCH — JAMMED (MACH TRIM)

DURING CLIMB-OUT, EN ROUTE, AT APPROXIMATELY 7000 FT, THE CREW REPORTED STAB AND MACH TRIM FAILURE. AFTER COMPLYING WITH THE QRH THE TRIMS STILL COULD NOT BE ENGAGED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AFTER RETURNING. MAINTENANCE INTERROGATED THE MDC AND FOUND THE FIRST OFFICERS STAB DISCONNECT SWITCH JAMMED. MAINTENANCE REMOVED AND REPLACED THE JAMMED DISCONNECT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB)

DURING DESCENT THROUGH APPROX 18,000 FT, THE STAB TRIM (BOTH CHANNELS) AND THE MACH TRIM DISENGAGED. THE CREW COMPLIED WITH THE QRH BY ATTEMPTING TO RESET THE STAB AND MACH TRIM WITH NO SUCCESS. THE CREW REQUESTED EMERGENCY VEHICLES BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY WITH THE FLAPS SELECTED TO 20 DEGREES. MAINT RESET THE HORIZONTAL STAB TRIM CONTROL UNIT AND STAB TRIM CHANNELS. MAINT ALSO DISENGAGED AND RE-ENGAGED THE STAB TRIM AND MACH TRIM SYSTEM NUMEROUS TIMES. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE)

DURING CLIMB OUT, WHEN PASSING THROUGH 14,500 FEET THE CREW NOTICED A DROP IN THE LT ENGINE OIL PRESSURE TO 27 PSI, IT THEN BEGAN FLUCTUATING BETWEEN 27 PSI AND 40 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE AIR TURBINE STARTER CARBON SEAL ASSEMBLY. OPERATIONAL AND OIL CONSUMPTION CHECKS GOOD. AIRCRAFT OK FOR SERVICE. THE AIRCRAFT WAS PUT ON DAILY CHECK FOR LT ENGINE HIGH OIL CONSUMPTION DURING NEXT FIVE DAYS.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE IB CLIPS AT THE FLOOR SUPPORT, FS484, LBL27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE IB CLIPS AT THE FLOOR SUPPORT, FS 484, LBL 27 AND RBL 27 IAW EO 600-53-0098.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CLIPS AT FS280, LBL9 AND RBL9 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL9 AND RBL 9 ON THE LT AND RT SIDES IAW SRM51-00.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM. (ASOA04334)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIPS AT FS 625 BELOW THE BOX BEAM.

Part: RIB — CRACKED (WING)

DURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT MLG BATT RIB ASSEMBLIES AT WS 53.60 IAW EO60057039A.

Part: SILL — CRACKED (CARGO BAY)

DURING A C-CHECK, THE CARGO BAY FLOOR SILL AT FS 562.72 TO FS 589.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72 TO FS 589.00 IAW EO600530095.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT SIDE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT SIDE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 IAW EO 600530105.

Part: RIB — CRACKED (CENTER WING)

DURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CLIPS AT FS 280, LBL9 AND RBL9 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS 280, LBL 9 AND RBL 9 ON THE LT AND RT SIDES IAW SRM. (ASOA04344)

Part: RIB — CRACKED (CENTER WING)

DURING A C-CHECK, THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT MAIN LANDING GEAR BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO.

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, THE AFT EQUIPMENT BAY CLIPS AT FS640 BELOW THE BOX BEAM WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AFT EQUIPMENT BAY CLIPS AT FS640, BELOW THE BOX BEAM.

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, THE IB CLIPS AT THE FLOOR SUPPORT, FS 484, LBL 27 AND RBL27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE IB CLIPS AT THE FLOOR SUPPORT, FS 484, LBL27 AND RBL27 IAW EO. (ASOA04345)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW EO600530072.

Part: LIGHT — BROKEN (CABIN)

DURING C-CHECK, THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D. OPERATIONAL CHECKS GOOD. (ASOA04343)

Part: LIGHT — BROKEN (CABIN)

DURING A C-CHECK, THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP NEAR ROW 12 C/D. OPERATIONAL CHECKS GOOD.

Part: CABLE — DAMAGED (FUSELAGE)

FLT 4740 - DURING A GROUND INSPECTION IN ICT, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SUPPORT WHEEL RETRACT CABLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — BROKEN (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT ASSEMBLY AT THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STRIKER — CRACKED (PAX DOOR SEAL)

FLT 4308 - DURING FLIGHT FROM CLT-ATL, THE FILGHT ATTENDANT NOTICED AN AIR RUSH ON THE TOP LEFT CORNER OF THE PASSENGER DOOR. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REPAIRED THE PASSENGER DOOR SEAL STRIKER IAW ASA EO 600-52-0008C. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

FLT 4807 - DURING A GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE FORWARD EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A GROUND INSPECTION IN MTY, THE PASSENGER DOOR BOTTOM STEP BRACKET WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (COCKPIT)

FLT 4680 - DURING CRUISE FROM ROA-ATL, WHILE LEVELING OFF AT 23,000 FEET A STRONG FUEL SMELL OCCURRED IN THE COCKPIT AND THEN DISAPPEARED WITHIN APPROXIMATELY FIVE MINUTES AFTER SWITCHING THE BLEEDS TO THE AUXILIARY POWER UNIT. THE AICRAFT LANDED SAFELY IN ATL. MAINTENANCE RAN EACH ENGINE BLEED INDEPENDENTLY WITH THE PACK AND AUXILIARY POWER UNIT SEPARATELY. NO DEFECTS WERE NOTED. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANTENNA — INOPERATIVE (FUSELAGE)

DURING CLIMB-OUT FROM VPS-DFW, THE RADAR BECAME UNSTABLE PAINTING RED AT ALL RANGES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO VPS, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR ANTENNA. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (CABIN)

FLT 4382 - DURING A GROUND INSPECTION AT MGM, THE NR 1 AND NR 3 CEILING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 3 CEILING EMERGENCY EXIT LIGHT LAMPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

DURING CRUISE FLIGHT FROM RDU TO DFW, AT APPROXIMATELY FL350, THE CAPTAINS WINDSHIELD SHATTERED ACCOMPANIED BY A LOUD BANG. AN EMERGENCY WAS DECLARED AT THIS TIME. PRESSURIZATION REMAINED NORMAL, BUT CAPTAIN HAD AIRCRAFT DESCEND TO 10,000 FEET AND 250 KNOTS AS A PRECAUTION. AIRCRAFT DIVERTED TO THE NEAREST AVAILABLE AIRPORT, TXK, AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS SHATTERED WINDSHIELD. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4511 - DURING GROUND INSPECTION IN ATL, THE RIGHT FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD EMERGENCY LIGHT BULB. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTACTOR — DIRTY (CABIN)

DURING GROUND INSPECTION IN ATL, THE FORWARD SECTION OF THE EMERGENCY TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE CLEANED CONTACTORS ON BOTH LIGHT ASSEMBLIES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PRIORITY VALVE — MALFUNCTIONED (NLG)

FLT 4477 - ON TAKEOFF FROM HPN TO ATL, WHEN GEAR HANDLE WAS SELECTED UP THE NOSE GEAR DID NOT RETRACT. GEAR POSITION INDICATOR SHOWED YELLOW GEAR INTRANSIT AND RED GEAR DISAGREED WITH CHIME. COMPLIED WITH QRH. CAPTAIN DECLARED AND EMERGENCY FOR AN UNSAFE LANDING GEAR INDICATION. WHEN GEAR WAS SELECTED DOWN, ALL THREE POSITION INDICATORS SHOWED DOWN AND LOCKED. AIRCRAFT DIVERTED AND LANDED SAFELY AT JFK. GEAR PINS WERE INSTALLED AND SAFETIED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. BLEEDS LEAK AND OPERATIONAL CHECKS GOOD. GEAR PINS WERE REMOVED. AIRCRAFT RETURNED TO SERVICE. (M)