N909EV
Registered owner: SKYWEST AIRLINES INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
GEAR DISAGREE WARNING MESSAGE. FIXED WITH QRH. (FLIGHT 6022). CP 31854923 FOR FUNCTION TEST OF THE GEAR EXTENSION/RETRACTION SYSTEM SEE CP 31854883 FOR INSPECTION OF NLG OLEO CENTERING SENSOR, HARNESS, AND BRACKET SEE CP 31854876 FOR CHECKING AND RIGGING ALL GEAR PROXIMITY SENSORS.SEE CP 31855741 FOR REMOVAL AND INSTALLATION OF NLG UPLOCK ASSEMBLY AND TASK CARD. OPS CHECK GOOD."
DENT ON FUSELAGE SKIN BETWEEN BS 409+80 - 409+96, S18 - 19L, PERMANENT REPAIR OF LT FUSELAGE SKIN IAW REO 601R-53-31-1363, REV CP 31597873 FOR STEP 1, CP 31599706 FOR STEP 2, 31596075 FOR STEP 3, 31599715 FOR STEP 4, 31596400 FOR STEP 5, 31599965 FOR STEPS 7,8,11,12,13,AND 14, CP31599991 FOR STEPS 6,9,AND 10. SEE CP 31599859 FOR PRESSURIZATION CHECK. COMPLIED WITH RII TASK CARD 51-900-1003-SKY.
DURING CRUISE AT FL320 GOT A STRONG BURNING SMELL FROM THE FLIGHT DECK VENTS. AT ONE POINT WE HAD A BURNING SMOKE SMELL. (FLIGHT 5021 - FILED CLOSED)MAY 23, 2025 STATION: CID--PREVIOUS TROUBLESHOOTING NOTED, TROUBLESHOT IN REFERENCE TO FIM 21-21-00, PERFORMED BOROSCOPE ON LH ENGINE CORE INLET AREA OF THE FAN BLADES AND FWD STAGES OF COMPRESSOR IN REFERENCE TO AMM 72-20-00, INSPECTED 1 AND 2 STAGE COMPRESSOR BLADES IN REFERENCE TO 72-32-00, FOUND NO SIGNS OF WETTING AT THIS TIME. INSPECTED THE CENTER VENT AIR SEAL PACKING BY REMOVING FWD SPINNER IN REFERENCE TO TASK 72-20-00-000-801, FOUND NO SIGNS OF OIL IN THE FAN FRONT SHAFT CAVITY. REINSTALLED LH ENG. FWD SPINNER. ACCESSED REAR OF CBP-1 AND CBP-2 FOR SIGNS OF BURNING OR HEAT DAMAGE, NO DEFECTS NOTED. SAT IN COCKPIT AND OPERATED LH PACK WITH APU BLEED AND ISOL VALVE CLOSED, OPERATED ARNIC AND DISPLAY FANS SWITCHING FORM NORM GROUND ALT AND FLT SWITCHED ALL COCKPIT LIGHTS ON. AFTER APPROX 10 MINUTES NO BURNING SMELLS NOTED. OPERATED LH AND RH WINDSHIELD HEAT ON HIGH. AFTER APPROX. 15 MINUTES BEGAN TO NOTICE A SMELL FROM RH WINDSHIELD POWER TERMINAL BLOCK, CONFIRMED SMELL WITH LH PACK OFF, LIGHTS OFF, A
DURING CRUISE AT FL320 GOT A STRONG BURNING SMELL FROM THE FLIGHT DECK VENTS. AT ONE POINT WE HAD A BURNING SMOKE SMELL. (FLIGHT 5021 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
STRONG BURNING SMELL DURING FLIGHT. NO SMOKE. NO INDICATION. FA COULD NOT SMELL IT. PARTIALLY DISSIPATED DURING FLIGHT THEN CAME BACK STRONGER. SMELL WENT AWAY DURING DECENT. REFERENCE AML 1607385, 1607510, 1607516 AND 1607525. (FLIGHT 5435) TROUBLESHOT BURNING SMELL IN THE COCKPIT PER FIM 21-21-00. SEE AML# 1607620 FOR INSPECTION OF LH ENGINE COMPRESSOR SECTION BLADES AND VANES WITH BOROSCOPE FOR SIGNS OF OIL LEAKAGE AND OIL COKING. SEE AML# 1607623 FOR INSPECTION OF RH ENGINE COMPRESSOR SECTION BLADES AND VANES WITH BOROSCOPE FOR SIGNS OF OIL LEAKAGE AND OIL COKING. SEE AML# 1607621 BOROSCOPE INSPECTION OF LH ENGINE BEHIND THE FAN DISC TO VERIFY NO WETTING NEAR THE CORE INLET AREA, FAN VANES, AND FIRST FORWARD STAGES OF THE COMPRESSOR. SEE AML# 1607624 FOR BOROSCOPE INSPECTION OF RH ENGINE BEHIND THE FAN DISC TO VERIFY NO WETTING NEAR THE CORE INLET AREA, FAN VANES, AND FIRST FORWARD STAGES OF THE COMPRESSOR. SEE AML# 1607634 FOR APU BOROSCOPE INSPECTION. SEE AML# 1607665 FOR OPERATIONAL CHECKS OF LEFT AND RIGHT ACM'S WITH APU, LEFT ENGINE AND RIGHT ENGINE BLEEDS INDIVIDUALLY AND VERIFIED NO SMOKE OR SMELL IS PRESENT. SEE AML# 1607659 FOR VISUAL INSPECTION OF THE INLET FACE AND CORE OF THE LEFT DUEL HEAT EXCHANGER AND FAN SECTION. SEE AML# 16
FLOOR BEAM JOINTS AT FS 409.00 TO FS 409.00 + 10 LBL 27.0, LBL 9.0, RBL 9.0, AND RBL 27.0 MISSING FASTENERS. (FILED CLOSED) COMPLIED WITH REO 601R-53-21-3722, REV--, DATED 2025-02-13 FOR DISPOSITION FOR MISSING FASTENERS TO FLOOR BEAM INSTALLATION BTW FS409.00 -FS409.00+16.00 AT LBL27.00, LBL9.00, RBL9.00 AND RBL27.00. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED FORM M-337. ALL NDTS COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME.
FLOOR BEAM FLOOR BOARD LANDING BETWEEN FS 409.00 TO FS 409.00 + 37 AT RBL 9.0 BEYOND LIMITS OF REO 601R-53-00-005. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
FLOOR BEAM FLOOR BOARD LANDING BETWEEN FS 409.00 TO FS 409.00 + 37 AT RBL 9.0 BEYOND LIMITS OF REO 601R-53-00-005. (FILED CLOSED) PERFORMED REPAIR OF FLOOR BEAM FROM FS 409.00 TO FS 409.00 + 37 WITH REFERENCE TO REO 601R-53-00-027 REV "D" DATED 26-NOV-2009. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.
AFT PRESSURE BULKHEAD (FS621), INTERCOSTAL CRACKED INLINE WITH STINGER 14L. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
AFT PRESSURE BULKHEAD (FS621), INTERCOSTAL CRACKED INLINE WITH STINGER 14L. (FILED CLOSED) REMOVED AND REPLACED THE INTERCOSTAL INLINE WITH STINGER 14L ON THE AFT SIDE OF THE AFT PRESSURE BULKHEAD FS621.00. WORK DONE IN REFERENCE WITH THE CRJ-200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.
CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT BALANCE SPRING MOUNTING BRACKET WITH REFERENCE TO CRJ-200 SRM 51-42-06. PERFORMED EDDY CURRENT INSPECTION OF FASTENER BORES THROUGH ENTIRE STACK UP WITH REFERENCE TO NDTM PART 6 53-00-097 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. REFERENCE CP 104895 FOR LEAK CHECK.
CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET CRACKED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
CORROSION FOUND ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES. (FILED CLOSED) BLENDED CORROSION ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS WITH REFERENCE TO SRM 53-21-23 AND SRM 53-00-00. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. RESTORED SURFACE FINISH WITH REFERENCE TO SRM 51-21-16. COMPLETED CORROSION FINDINGS REPORT.
PAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 HAS BEEN REMOVED TO FOM (FILED CLOSED) INSTALLED THE PAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 IN REFERENCE WITH THE CRJ-200 SRM 51-42-06. COMPLETED FORM M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY.
CORROSION FOUND ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
PAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 HAS BEEN REMOVED TO FOM (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
PAX DOOR SILL LOWER ANGLE (REF SRM 53-21-23 ITEM 56B) CORRODED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
PAX DOOR SILL LOWER ANGLE (REF SRM 53-21-23 ITEM 56B) CORRODED. (FILED CLOSED) REMOVED AND REPLACED THE PAX DOOR SILL LOWER ANGLE IN REFERENCE WITH THE CRJ-200 SRM 51-42-06, SRM 51-42-21, SRM 51-42-13 AND SRM 53-21-23. COMPLETED FORM M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED THE CORROSION FINDINGS REPORT.
FLOOR BEAM, FLOOR BOARD LANDING HAS SURFACE CORROSION BETWEEN FS 409.00 TO 409.00 +112 @ RBL 9.00. (FILED CLOSED) REMOVED CORROSION ON FLOOR BEAM FLOOR BOARD LANDING BETWEEN FS409.00 TO FS409.00 + 112 @ RBL 9.0 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT THICKNESS MEASUREMENT OF BLEND WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS OF REO 601R-53-00-005 REV "-B" DATED 2011/01/06 BETWEEN FS 409.00 + 37 TO FS 409.00 + 112. FS 409.00 TO FS 409.00 + 37 FOUND TO BE OUT OF LIMITS AND REQUIRES REPAIR - SEE CHILD CAMP FOR CONTINUATION. PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREAS AND WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.
CARGO DOOR UPPER AFT CORNER SEAL RETAINER GOUGED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
FLOOR SUPPORT FLOOR BOARD LANDING HAS SURFACE CORROSION BETWEEN FS 409.00 TO 409.00 +112 @ RBL 9.00.
CARGO DOOR UPPER AFT CORNER SEAL RETAINER GOUGED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR UPPER AFT CORNER SEAL RETAINER WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY. REFERENCE CHILD CAMP FOR LEAK CHECK.
RH ELECTRIC BOOST PUMP SATELLITE HOLE # 9 ON LOWER AFT WING PLANK HAS TOO MUCH NOISE INDICATION DURING EDDY CURRENT OPEN HOLE INSPECTION. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
RH ELECTRIC BOOST PUMP SATELLITE HOLE # 9 ON LOWER AFT WING PLANK HAS TOO MUCH NOISE INDICATION DURING EDDY CURRENT OPEN HOLE INSPECTION. (FILED CLOSED) REPAIRED RH ELECTRIC BOOST PUMP SATELLITE HOLE #9 ON LOWER AFT WING PLANK WITH REFERENCE TO REO 601R-57-21-169 REV "D" DATED 2008-06-23 REPAIR #2. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 6 53-00-097 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
CORROSION ON RH CABIN FLOOR SILL ASSY WL73.00 BETWEEN FS559.00 TO FS 559.00 + 16 AND BETWEEN RBL 41.75 (FILED CLOSED) COMPLIED WITH REO 601R-53-51-699 DATED: 2025-01-15 REV - - TEMPORARY DISPOSITION FOR BLENDED CORROSION DAMAGE TO FLOOR SILL STRUCTURE BTW FS559.00 FS559.00+16 AND AT BL41.75, RHS. REFERENCE CHILD FOR MCI'S CREATED FOR PERMANENT REPAIR AND VISUAL REINSPECTS. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M337.
CORROSION ON LH PRESSURE FLOOR ASSY WL73.00 BETWEEN FS409 + 128 -TO FS559.00 AND BETWEEN LBL36.00 AND LBL47.00.
CORROSION ON LH PRESSURE FLOOR ASSY WL73.00 BETWEEN FS409 + 128 -TO FS559.00 AND BETWEEN LBL36.00 AND LBL47.00. (FILED CLOSED) BLENDED CORROSION ON LH PRESSURE FLOOR SILL ASSY WL73.00 BETWEEN FS409 + 128 TO FS559.00 AND BETWEEN LBL36.00 AND LBL47.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE ACCEPTABLE PER REO 601R-53-41-666 REV "-C" DATED 2012-11-06. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH REO 601R-53-41-666 REV "-C" DATED 2012-11-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.
IN CRUISE TO DEN RECEIVED L/H 14TH STAGE DUCT WARNING FOLLOWED QRH TO LAND AT NEAREST SUITIBLE AIRPORT (FLIGHT 4741 FILED CLOSED)UPON ARRIVAL TO AIRCRAFT FOUND 14TH STAGE DUCT WARNING TO BE HARD FAULTED AND PYLON LOOP SECTION OF A/ICE PAGE OF THE EICAS TO BE ILLUMINATED RED. PERFORMED RESISTANCE CHECK OF THE LT PYLON LOOP AND FOUND TO BE SHORTED, REMOVED AND REPLACED LOOP A59WK WITH SERVICEABLE UNIT REF AMM 36-21-04.
D: FLAP FAIL CAUTION FLAPS STUCK AT 8 OUT OF RNO ON FLAP RETRACT / C: MCI / CAT: "A" DUE IN 10 FC FROM TAC 37285 (DUE AT TAC 37295) / FLAP FAIL CAUTION FLAPS STUCK AT 8 OUT OF RNO ON FLAP RETRACT (FLIGHT 5998 - FILED CLOSED) APR 18, 2022 STATION: SFO--RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 MCI CREATEDFOR FULL AD COMPLIANCE BY MCC
THE BRAKET OUTBOARD OF THE FORWARD LOWER ROLLER TRACK FOR THE CARGO DOOR IS CRACKING FROM TWO RIVET HEADS. (FILED - CLOSED) REMOVED AND REPLACED DAMAGED BRACKET O/B OF THE FWD LOWER ROLLER TRACK FOR THE CARGO DOOR IN REFERENCE TO CRJ200 SRM 51-42-21.
RH ENGINE AFT MOUNT THRUST FITTING APPEARS TO BE WORN (FILED CLOSED) REMOVED AND REPLACED THE RH ENGINE AFT THRUST FITTING IN REFERENCE TO AMM: 71-22-01. / TORQUE WRENCH INFO: / S/N: 1021102692 DUE: 7/2022
COMPLY WITH SCHEDULED MAINTENANCE CODE: NDT ENG MOUNT SHAFT - ENGINE MOUNT THRUST SHAFT DUE NDT INSPECTION. REMOVE AND REPLACE ENGINE THRUST MOUNT SHAFT IN REFERENCE TO AMM 71-00-00 AND 71-430-603 AND 71-440-603. SEND TO VENDOR FOR COMPLIANCE OF NDT (MRB 71-21-104), PART NUMBER: 601-37020-7 - SHAFT, THRUST, SERIAL NUMBER: CLA0789, POSITION: RIGHT (FILED-CLOSED) REMOVED AND REPLACED THE RH ENGINE AFT THRUST SHAFT IN REFERENCE TO AMM: 71-00-00 AND CARD MIP TASK CARD 71-900-1000-SKY. / TORQUE WRENCH INFO: / S/N: DQF28192 DUE: 9/2022 / S/N: MD 45343 DUE: 1/2023
GEAR DISAGREE WARNING MESSAGE ON TAKEOFF OUT OF RNO WHEN SELECTING GEAR UP. NOSE WHEEL DOOR WARNING MESSAGE AND NOSE WHEEL STEERING INOP CAUTION ASSOCIATED. COMPLIED WITH QRH GEAR DOWN THREE GREEN AFTERWARDS. (FLIGHT 5899 - FILED CLOSED) INTERROGATED PSEU FOUND FAULT CODES FOR CURRENT LEG TO BE S30 FAR(LEFT NOSE DOOR CLOSED),S31 FAR(RT NOSE DOOR CLOSED),DI14 ON(LEFT GEAR DOOR OPEN)PERFORMED 10 COMPLETE GEAR SWINGS PER AMM 32-30-00 WITH NO DEFECTS AND PERFORMED CHECK OF NWS PER AMM 32-51-00 WITH NO FAULTS. REVIEWED FDR DOWNLOAD SUMMARY AND REMOVED AND REPLACED NLG DOOR SELECTOR VALVE IN REF TOO AMM 32-22-20 ALL CHECKS GOOD AT THIS TIME.NO LEAKS NOTED.
LH FLOOR SILL FROM FS559+80 TO FS574 HAS MULTIPLE BROKEN NUTPLATES. REPLACEMENT REQUIRED. (C-CHECK RO 7/24/2021) REPLACED 13EA NUTPLATES ON LH FLOOR SILL BETWEEN FS559+80 AND FS574 IAW CRJ200 SRM 51-45-00. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
RH SPOILERON I/B AND O/B PCUS OUT OF RIG. TRAILING EDGE SURFACE EXCEEDS 0.120 ABOVE THE FLAP SURFACE. (C-CHECK RO 7/24/2021) REMOVED, REPLACED, AND RIGGED RH SPOILERON IB PCU AND RIGGED RH SPOILERON OB PCU IAW CRJJ 200 AMMS 27-62-01-830-801 & 27-62-01-400-801. ALL REQUIRED OPS, FUNCTIONAL, RIG AND LEAK CHECKS PASS. REFER TO CONTINUE CARD FOR WORK PERFORMED.
FOUND DENT ON L/H ELEVATOR LOWER SKIN. (C-CHECK RO 7/24/2021) REPAIRED LH ELEVATOR LOWER SKIN IAW CRJ200 SRM 55-20-00 REV. 38, DATED 07/10/20419. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. WEIGHT CHANGE 0.5 LBS. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
RIGHT LOWER WING PLANK AT WS 45 IS CHAFED AT THE AFT EDGE ALONG WITH TWO FASTENER HEADS. (C-CHECK RO 7/24/2021) RIGHT LOWER WING PLANK AT WS 45 IS CHAFED AT THE AFT EDGE ALONG WITH TWO FASTENER HEADS WAS REPAIRED IAW BOMBARDIER REO 601R-57-21-880 REV-D DATED 2017/03/06. MATERIAL REMOVED WAS .038" AS MEASURED AND DOCUMENTED ON ATTACHED CONTINUATION CARD. AREA WAS ROTO PEENED, PRIMED, PAINTED IAW BOMBARDIER REO 601R-57-21-880 REV-D. COMPLIED WITH TASK CARD 51-900-1003-SKY, M-337 COMPLETED. WEIGHT AND BALANCE NOT AFFECTED.
R/H OUTBOARD FLAP OUTBOARD HNIGE BOX HAS CHAFE/GOUGE DAMAGE AT THE AFT ATTACHMENT POINT (C-CHECK RO 7/24/2021) REPAIRED R/H OUTBOARD FLAP OUTBOARD HNIGE BOX AT W.S 264.00 CHAFE/GOUGE DAMAGE AT THE AFT ATTACHMENT POINT IAW MHIRJ REO 601R-57-21-3466 REV-- DATE 2021-04-30, REFERNCE CONTIUATION CARD FOR DETAILS OF WORK PERFOMED
RIGHT WING UPPER SKIN ACCESS HOLE AT PANEL 640AT CUTOUT HAS SEVERAL AREAS OF MINOR CORROSION AROUND CUTOUT. (C-CHECK RO 7/24/2021) REPAIRED RH WING UPPER SKIN IAW REO 601R-57-21-3464 REV -- DATED 2021-04-29 BOND CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED,
SERVICE DOOR LOWER CLOSE OUT FWD AND AFT LOWER PANS ARE HEAVILY CORRODED (C-CHECK RO 7/24/2021) REMOVED AND REPLACED SERVICE DOOR LOWER CLOSE OUT FWD AND AFT LOWER PANS IAW CRJ 200 SRM 51-42-06, 51-42-21,51-42-10 AND SNIEO 60138304S05 AND S06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
LEFT WING UPPER SKIN ACCESS HOLE AT PANEL 540AT CUTOUT HAS MINOR CORROSION IN SEVERAL AREAS AROUND CUTOUT. (C-CHECK RO 7/24/2021) REMOVED CROSSION FROM PANELS 540AT, 540BT, AND 540 CT PANEL LANDING IAW CRJ 200 SRM 51-21-06. COMPLIED WITH MHIRJ REO 601R-57-21-3465 REV-- DATED 2021-04-29 FOR FINISH.
PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. (C-CHECK RO 7/24/2021) REMOVED AND REPLACED PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING IAW CRJ 200 SRM- 51-42-21, 51-40-11 AND DWG 601R33007. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE.
CO-PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. (C-CHECK RO 7/24/2021) REMOVED AND REPLACED CO-PILOTS WINDSHIELD SIDE POST LOWER AFT FITTING IAW CRJ 200 SRM- 51-42-21, 51-40-11 AND DWG 601R33007. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE.
LH UPPER OBLIQUE ANGLE CRACKED AT FS621.00 TO FS625.00 LBL45 STRGR 14L AND WL97.5 (C-CHECK RO 7/24/2021) REMOVED AND REPLACED LH UPPER OBLIQUE ANGLE AT FS621,00 TO 625.00 LBL45 STRG14L AND WL97.5 IAW CRJ200 SRM 51-42-21
RH UPPER OBLIQUE ANGLE CRACKED AT FS621.00 TO FS625.00 RBL45 STRGR 14R AND WL97.5 (C-CHECK RO 7/24/2021) REMOVED AND REPLACED RH UPPER OBLIQUE ANGLE AT FS621.00 TO FS625.00 RBL45 STRG14R AND WL97.5 IAW CRJ200 SRM 51-42-21
SEAT RAIL RIGHT SIDE FORWARD OF FS409.0 +128 NINE PLACES GOUGED (C-CHECK RO 7/24/2021) SEAT RAIL RIGHT SIDE FORWARD OF FS409.0 +128 NINE PLACES GOUGED, FOUND TO BE OUT OF LIMITS. REFERENCE CAMP# 22737342 FOR FABRICATION AND INSTALL OF NEW SEAT RAIL
BAGGAGE DOOR AFT UPPER "TEE" IMPACT DAMAGE @ FS621.0 (C-CHECK RO 7/24/2021) REMOVED AND REPLACED AFT UPPER T FITTING IAW CRJ 200 AMM 52-31-00-820-801 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
L/H OUTBOARD FLAP HINGE ARM AT FLAP ATTACH POINT IS DAMGAGED ON INNER FLANGE FROM COUNTER SUNK SCREW BEING LEFT IN HINGE ARM AREA. (C-CHECK RO 7/24/2021) REPAIRED LH OUTBOARD FLAP OB HINGE ARE AT WS 264.00 IAW MHIRJ REO 601R-57-21-3468 DATED 2021-05-02 AND SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
BAGGAE DOOR SURROUND AT FS577.0 LOWER FWD BELOW "TEE" IS WORN (C-CHECK RO 7/24/2021) REMOVED AND REPLACED BAGGAGE DOOR SURROUND FS 577.00 LOWER DOOR COAMING IAW CRJ 200 SRM 51-42-06,51-42-21, 51-41-02 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
F.S. 409.00+128 VERTICAL BEAM AT RBL 27 IS CRACKED AT I/B AFT BOTTOM RADIUS. (C-CHECK RO 7/24/2021) REPAIRED FS 409.00+128 VERTICAL BEAM AT RBL 27 CRACK AT I/B AFT BOTTOM RADIUS IAW BOMBARDIER REO 601R-53-41-056 REV F DATED 2011-09-02, MHIRJ REO 601R-53-41-2924 REV -- DATED 5/17/2021 & SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
FS559.00+112 FRAME CORRODED BETWEEN STRGR 26L AND 26R. (C-CHECK RO 7/24/2021) REMOVED AND REPLACED SPLICE ANGLE FRAME AT FS559.00+112 STR 26L-26R IAW CRJ 200 SRM 51-42-06 REV. 38B, DATED 11/25/2020 AND CRJ200 SRM 51-42-21 REV. 38B, DATED 11/25/2020. COMPLIED WITH SKYWEST M-337 AND M-131. SKYWEST MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLIED WITH. NO CHANGE TO WEIGHT AND BALANCE.
LH FLOOR SILL AT LBL36 IS CORRODED AT F.S. 409.00+128. (C-CHECK RO 7/24/2021) REPAIRED LH FLOOR SILL AT LBL36 FS409+128 IAW BOMBARDIER REO 601R-53-00-530 REV-A DATE 2014-10-07 & SKYCARD 51-900-1003-SKY FORM 337 IS ATTACHED NO WEIGHT CHANGE REFERENCONTINUATION CARD FOR WORK PERFORMED.
LH PRESSURE FLOOR SILL IS CORRODED AROUND FASTENER HOLES BETWEEN F.S. 513.00 AND F.S. 529.00. (C-CHECK RO 7/24/2021) REPAIRED LH PRESSURE FLOOR SILL BETWEEN FS513 AND FS529 IAW BOMBARDIER REO 601R-53-41-666 REV-C DATE 2012-11-06. & SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
SEAT RAIL CORRODED AT RBL9 FROM FS559.00+80 TO FS559.00+96. (C-CHECK RO 7/24/2021) REMOVED AND REPLACED SEAT RAIL AT RBL 9 559+80 TO 559+ 96 IAW CRJ 200 AMM 53-00-49-400-801 REF CONTINUATION CARD FOR WORK COMPLETED
3 EA. SEAT RAILS CORRODED AT LBL9 FROM FS559.00+80 TO FS559.00+96, FS559.00+112 TO FS574.00 AND FS605.00 TO FS621.00 (C-CHECK RO 7/24/2021) REMOVED AND REPLACED 3 EACH SEAT RAILS IAW CRJ 200 AMM 53-00-49-400-801 REFERENCE COTINUATION CARD FOR WORK PERFORMED.
INTERCOSTAL AT F.S. 310.00 JUST ABOVE THE FLOOR IS CORRODED (C-CHECK RO 7/24/2021) INSTALLED NEW SERVICEABLE INTERCOSTAL AT FS 310.00. REFERENCE CONTINUATION CARD FOR WORK PREFORMED.
RH PRESSURE FLOOR SILL FASTENER HOLE BETWEEN F.S. 461.00 AND F.S. 473.00 HAS CORROSION. (C-CHECK RO 7/24/2021) REPAIRED RH PRESSURE FLOOR SILL BETWEEN FS461 AND FS473 IAW BOMBARDIER REO 601R-53-41-666 REV-C DATE 2012-11-06, SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE. FORM 337 ATTACHED. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
RH PRESSURE FLOOR SILL IS CORRODED JUST AFT OF F.S. 449.85. (C-CHECK RO 7/24/2021) REPAIRED RH PRESSURE FLOOR SILL CORROSION JUST AFT OF FS 449.85 IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06 AND MHIRJ REO 601R-53-41-2914 REV -- DATED 2021-05-18 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
RH PRESSURE FLOOR SILL IS CORRODED AROUND FASTENER HOLE AT F.S. 424.00. (C-CHECK RO 7/24/2021) REPAIRED RH PRESSURE FLOOR SILL CORROSION AROUND FASTENER HOLE FS 424.00 AND TWO AREAS BETWEEN FS 424.00 AND FS439.00 IAW MHIRJ REO 601R-53-41-2922 REV -- DATED 2021-05-12, REO 601R-53-41-666 REV C DATED 20212-11-06 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED
LH PRESSURE FLOOR SILL IS CORRODED AROUND FASTENER HOLE JUST AFT OF F.S. 449.85. (C-CHECK RO 7/24/2021) REPAIRED LH PRESSURE FLOOR SILL JUST AFT OF FS449.85 IAW BOMBARDIER REO 601R-53-41-666 REV-C DATE 2012-11-06.& SKY CARD 51-900-SKY NO WEIGHT CHANGE REF ATTACHED FORM 337 REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
LH PRESSURE FLOOR SILL IS CORRODED AROUND FASTENER HOLES BETWEEN F.S. 439.00 AND F.S. 449.85. (C-CHECK RO 7/24/2021) REPAIRED LH PRESSURE FLOOR SILL BETWEEN FS439.00 AND FS449.85 IAW BOMBARDIER REO 601R-53-41-666 REV-C DATE 2012-11-06 & SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE REF ATTACHED FORM 337 . REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
INTERCOSTAL BETWEEN F.S. 349.00 AND F.S. 364.00 STGR 26L TO 27 IS CORRODED AROUND GROUND STUD. (C-CHECK RO 7/24/2021) REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 349.00 AND FS 364.00 STGR 26L TO 27 IAW CRJ 200 ARM 51-42-21, 51-42-06 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
FLOOR SUPPORT CROSSBEAM IS CORRODED AT LBL 36 F.S. 349.00. (C-CHECK RO 7/24/2021) REPAIRED FLOOR SUPPORT CROSSBEAM AT LBL 36 FS 349.00 IAW MHIRJ REO 601R-53-21-3442 REV -- DATED 2021-05-17 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED
FOUND 4 DENTS UNDER FWD FUSELAGE BETWEEN STGRS 26L-25R, AND FUSELAGE STATIONS FS250.0-FS280.0 REFERANCE CP 18607833 AND REO (SPECIFIC) 601R-53-11-3418 REV -- FOR ALL DAMAGE COVERED 600 FLIGHT HOUR VISUAL REINSPECT PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES (C-CHECK RO 7/24/2021) REPAIRED 4 DENTS UNDER FWD FUSELAGE BETWEEN STGRS 26L-25R AND FUSELAGE STATIONS FS250.00 -FS 280.00 IAW BOMBARDIER REO 601R-51-00-309 REV A DATED 8/23/2017 AND MHIRJ REO 601R-53-11-3690 REV -- DATED 2021-06-08 & SKYCARD 51-900-1003-SKY ,FORM M-337 IS ATTACHED. WEIGHT CHANGE +3.23LBS, ARM 117.00, MOMENT 377.91 LBIN.
STOP DRILL AT LEFT TRU DOOR LATCH EVALUATE. (C-CHECK RO 7/24/2021) REMOVED AND REPLACED THE LEFT TRU DOOR LANDING IAW CRJ 200 SRM 51-42-06, 51-40-11 AND 51-42-13 REV 38B DATED 25 NOV 2020, REO 601R-53-11-3694 REV -- DATED 2021-05-19 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA55520-601R-57-21-3224 REV 909EV MXCODEID50314-PR - RH I/B LOWER WING SKIN HAS THREE DENTS JUST AFT OF RH LANDING LIGHT WS50.54- WS65.75. COMPLIED TEMPORARY REPAIR PER REO 601R-57-21-3224 REV. VALID FOR 1750 FH. PERMANENT REPAIR DUE BY 40187.3 TAT., PART NUMBER: - , SERIAL NUMBER: 7658, POSITION: (C-CHECK RO 7/24/2021) REPAIRED RH I/B LOWER WING SKIN THREE DENTS JUST AFT OF RH LANDING LIGHT WS50.54- WS65.75 IAW REO 601R-57-21-3461 REV. A, DATED 5/4/21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
HAD SMOKE IN THE CABIN. SMOKE WAS THICK AND GRAY. HAPPENED RIGHT AT AROUND 1000 ABOVE FIELD. PASSENGERS AND CREW ALL SAY IT SMELLS LIKE BURNING PLASTIC. FLIGHT 5698 CLOSEDFOLLOWED FIM FOR SMOKE IN THE CABIN. INSPECTED BALLAST FOR ALL OVERHEAD CEILING LIGHTS AND SIDEWALL LIGHTS AND FOUND NO EVIDENCE OF BURNING OR CHARRING. REMOVED AND REPLACED COALESCER BAGS WITH REFERENCE TO AMM. LEAK CHECK GOOD AT THIS TIME. SPOKE WITH RAMP CREW AND WAS INFORMED THAT THE AIRCRAFT HAD TYPE 1 AND TYPE 4 DEICING ON ENTIRE BODY OF AIRCRAFT. THE RAMPER MENTIONED THAT THE TYPE 4 DEICING FLUID HAS A BIT OF A PLASTIC SMELL AND IF THIS DEICING FLUID GOT INTO THE AIR CONDITIONING SYSTEM IT COULD CAUSE THE SMELL THAT WAS DESCRIBED. COMPLIED WITH THE ENGINE AND ECS DRY OUT PROCEDURE WITH REFERENCE TO AMM AND FOUND NO SMELL OF SMOKE PRESENT AFTER. AIRCRAFT IS OK FOR SERVICE,
GEAR DISAGREE WARNING ON FINAL FOR RIGHT MLG. THE RIGHT GEAR DID FINALLY GO GREEN AFTER WE INITIATED A GO-AROUND. NO FURTHER ISSUE UPON LANDING. (
FUSELAGE OUTER SKIN HAS TWO DENTS BETWEEN FS 574 AND FS 589 BETWEEN STRINGERS 24L AND 25L. REPAIRED DENTS IN FUSELAGE SKIN BETWEEN FS 574 AND FS 589 AND STRINGERS 24L AND 25L IAW SRM 53-00-31 REPAIR NR 1 AND EC/TC EO200-53-30-00001.
DURING CLIMB, RECEIVED A GEAR DISAGREE WARNING AND NLG DOOR WARNING MESSAGE. USED MANUAL EXTENSION, RECEIVED THREE GREENS AND LANDED NORMALLY. REPLACED THE BRACKET ON THE BACK OF NOSE GEAR AND ADJUSTED SENSOR PS14GA. OPS CHECKED GOOD.
PANEL 832AL HAS CORROSION. INSTALLED A NEW PANEL 832AL AND NEW GASKET IAW SRM.
MAIN CABIN DOOR DIFFICULT TO OPEN. LOUD THUMP NOISE OBSERVED DURING EXTENSION. ADJUSTED FWD PAX DOOR TENSION TIE AND ANCHOR STOP BOLT ADJUSTMENT. PERFORMED OPS CHECK OF PAX DOOR. PAX DOOR OPS CHECKS GOOD IAW AMM'S 52-11-00 AND 52-11-17.
AT GEAR UP, "NOSE DOOR" MESSAGE AND "GEAR DISAGREE" WARNING MSG, DURING QRH PRECEDURE, NOSE GEAR RETRACTED ON IS OWN. GEAR LOWERED DURING QRH PROCEDURE NORMALLY. ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED AS A PRECAUTION. LANDING GEAR RETRACTION SYS, RESOLUTION DESCRIPTION: R & R NLG WOW NR 2 AND GR CENTERING PROXIMITY SENSOR HARNESS AND BRACKET IAW AMM 32-61-25. OPS CHECK GOOD. DMIL CLEARED PLACARD REMOVED.
LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED AT RT WATER DRAIN, NEAR BOOST PUMP, IN BARE METAL BONDING AREA 60 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION. RECEIVED REO 601R-57-21-2317. C/W REO 601R-57-21-2317. ROTO PEENED REWORKED AREA IAW REO 601R-57-21-2317. REO 601R-57-21-2317 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A WC.
LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED AT LT WATER DRAIN, NEAR BOOST PUMP, IN BARE METAL BONDING AREA 60 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION. RECEIVED AND COMPLIED WITH REO 601R-57-21-2317. C/W REO 601R-57-21-2317. ROTO PEENED REWORKED AREA IAW REO 601R-57-21-2317. REO 601R-57-21-2317 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A WC.
TWO AREAS DAMAGED ON PAX DOOR SILL RETAINER BTM UNDER FOLDING STEP .75 L X .125 W X .063 DEEP. REMOVED PAX DOOR SEAL RETAINER IAW SRM 1-42-06. REPLACED PAX DOOR SEAL RETAINER IAW SRM 51-42-13 AND REO 601R-52-16-915. C/W ECTC REO 601R-52-11-915 IAW REO 601R-52-11-915. REMOVED SEAL, COMMON TO STATIC RETAINER BEING REPLACED IAW AMM 52-11-10-000-803. REINSTALLED SAME SEAL INTO SEAL RETAINER IAW AMM 52-11-10-400-803.
INTERCOSTAL JUST OTBD OF STR 27 AFT OF BS 394 IS CORRODED WITH FILIFORM CORROSION. REMOVED INTERCOSTAL IAW SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-40-11. FOUND CORROSION TO BE OUT OF LIMITS WITH OVERLAPPING ELEMENTS IAW SRM 51-21-23 AND 53-00-00, FIG 102, SHEET 2. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.
INBD AND OTBD ANGLES ON STRINGER 3L AT BS 280 ARE CRACKED. R & R THE ANGLES.
AFT EQUIPMENT BAY, RT SIDE BS 621-625, OBLIQUE ANGLE CRACKED. R & R CRACKED ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21.
AFT EQUIPMENT BAY LT SIDE FUSELAGE BS 621-625 OBLIQUE ANGLE CRACKED. R & R CRACKED ANGLE WITH NEW SERVICEABLE ANGLE IAW SRM 51-42-21. SDR CLOSED.
ENTRY FLOOR LEVEL "EXIT" SIGN DOES NOT ILLUMINATE. R & R EXIT SIGN, IAW AMM 33-51-10. OPS CHECKED GOOD.
LIGHTED FLOOR-LEVEL EXIT SIGN AT RT EMERGENCY EXIT INOPERATIVE. R & R WIRE SPLICE CONNECTORS IAW SPM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
AT 20000 FT DURING A CLIMB TO 23000 FT, CABIN ALTITUDE BEGAN TO CLIMB AT BETWEEN 600-800 FPM. THIS WAS WITH A LOUD SQUEAL FROM MAIN PAX DOOR AT 23000 FT, ALTITUDE CAUTION MESSAGE, BEGAN QRH AND CABIN QUICKLY CLIMBED, BEGAN DESCENT AND AT 20000 FT AND RECEIVED CABIN ALTITUDE WARNING. PAX OXYTEN MASKS DEPLOYED AND F/A COMMAND USE PORTABLE O2 BOTTLE WAS USED FOR 3B BECAUSE MASK DID NOT DEPLOY. ENROUTE, ACFT DIVERTED.
FWD EXTERIOR EMERGENCY LIGHT ABOVE RT WING INOPERATIVE. R & R BULB IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
WARDROBE EMERGENCY FLOODLIGHT AND MID CABIN CEILING EXIT LIGHT INOP. R & R WARDROBE EMERGENCY FLOODLIGHT IAW AMM 33-51-19-400-801. R & R NR 2 BATTERY POWER SUPPLY ASSY IAW AMM 33-51-05-000-801 AND AMM 33-51-05-400-801. OPS TEST OF THE EMERGENCY LIGHTS IS DUE IAW AMM 33-51-00-710-801. OPS CHECK OF EMERGENCY LIGHTS C/W IAW AMM 33-51-00-710-801. OPS CHECK GOOD AT THIS TIME.
LT ENGINE PYLON RIB AT FS 605.00 IS CRACKED ON OTBD END ADJACENT TO NUTPLATE HOLE APPROX .2500" LONG. REPAIRED IAW EO CL600-2B19-54-I00338, DATED 7/2/2013. MAJOR REPAIR.
CRACK IN BS 202 BULKHEAD AROUND PARKING BRAKE CABLE. COMPLIED WITH EC/TC REO 601R-53-11-563 AND REO 601R-53-11-563, REV C.
FLOORBEAM CAP CORRODED BETWEEN FS 559.00+64 AND FS 559.00+80 AT RBL 9. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-51-43. REMOVED FLOORBEAM CAP RBL 9 FS 559 TO FS 574 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW FLOORBEAM CAP, PN 601R-31119-9S IAW SRM 51-40-11. INSTALLED FLOORBEAM CAP IAW REO 601R-53-61-4951.
FS 621 BULKHEAD AT RBL 36-20 REQUIRES REPAIR IAW EC/TC REO 601R-53-61-1285. REPAIRED IAW REO 601R-53-61-4942.
FS 621 BULKHEAD AT LBL 9 REQUIRES REPAIR IAW EC/TC REO 601R-53-61-1289. REPAIRED IAW REO 601R-53-61-4942.
FS 621 BULKHEAD AT RBL 9 REQUIRES REPAIR IAW EC/TC REO 601R-53-61-1285. REPAIRED IAW REO 601R-53-61-4942.
RT LOWER WING PLANK LANDING FOR ACCESS PANEL 640FB HAS AN INDICATION NOTED ON THE FWD INBD AREA APPROX 8" LONG X .250" X 60 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030, REV J.
LT LOWER WING PLANK LANDING FOR ACCESS PANEL 550GB HAS AN INDICATION NOTED IN THE FWD INBD AREA APPROX 1.5" LONG X .250" X 60 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030, REV J.
LT LOWER WING PLANK LANDING FOR ACCESS PANEL 550DB HAS AN INDICATION NOTED IN THE AFT OTBD AREA APPROX 12" LONG X .250" X 50 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030, REV J.
FS 621 BULKHEAD, RBL 18 FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT BETWEEN WL 111 TO 94. REPAIRED IAW REO 601R-53-61-49-42.
FS 621, BULKHEAD LBL 27.5 FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT BETWEEN WL 111.0 TO 97.0. REPAIRED IAW REO 601R-53-61-4942.
FS 621 BULKHEAD RBL 27.5 FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT BETWEEN WL 111 TO 83. REPAIRED IAW REO 601R-53-61-4942.
FS 621 BULKHEAD, LBL 28 FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT BETWEEN WL 111 TO 97.0. REPAIRED IAW SRM 51-24-36, 51-24-16. REO 601R-53-61-4942.
FS 621 BULKHEAD, LBL 36.20 FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT BETWEEN WL 82.0 AND 78.0. REPAIRED IAW REO 601R-53-61-4942.
FS 621 BULKHEAD BL 0 FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT BETWEEN WL 102 TO 117. REPAIRED IAW REO 601R-53-61-4942.
SEAT TRACK CORRODED FROM FS 559+80 AT RBL 9.0. REMOVED SEAT TRACK IAW 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485.
CARGO DOOR TIE DOWN MOUNTING PLATE CORRODED. LOCATED, DRILLED IAW SRM 51-42-06 AND 51-40-11. INSTALLED IAW SRM 51-42-06 AND 51-42-21.
BS 473.15 AT LBL 45.0, WING TO FUSE FITTING CORRODED AT FLOOR LEVEL. REPAIRED IAW SRM 53-00-00, TR 53-27 AND IAW SRM 51-12-00.
CARGO DOOR LOWER FWD "C" CHANNEL CRACKED AT FASTENER HOLE. R & R CRACKED CHANNEL WITH NEW CHANNEL IAW SRM 51-42-06.
FRAME BS 605 CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED IAW REO 601R-53-61-4938, REV, DATED 2013-06-19. MAJOR REPAIR.
PRESSURE FLOORBEAM AT FS 559.00 BETWEEN RBL 27.0 AND RBL 45.00 CORRODED. REPAIRED IAW SRM 51-21-06.
SEAT TRACK CORRODED AT RBL 9.0 FROM FS 409+128 TO 559. REMOVED SEAT TRACK IAW SRM 51-41-02. INSTALLED NEW SEAT TRACKS IAW SRM 51-41-027, AND REO 601R-53-00-485.
PRESSURE FLOORBEAM AT FS 559.00 BETWEEN LBL 27.0 AND LBL 45.0 CORRODED. REPAIRED IAW SRM 51-21-06.
PRESSURE FLOOR SUPPORT BETWEEN FS 473.15 AND 559 AT RBL 36 TO RBL 45 HAS AREAS OF MINOR CORROSION. REPAIRED IAW REO 601R-53-41-666, REV C.
PRESSURE FLOOR SUPPORT HAS AREAS OF CORROSION FROM FS 409+128 TO FS 559 BETWEEN LBL 36 AND LBL 45.0. REPAIRED IAW REO 601R-53-41-666, REV C.
CARGO DOOR LOWER SILL HAS CORROSION AROUND FASTENER HOLES. R & R CORRODED CARGO DOOR SILL IAW REO 601R-53-61-1574.
FS 621, BULKHEAD FWD FACE APPROX 30" ABOVE FLOOR HAS SCREW MARKS .20 DIAMETER, NO DEEPER THAN .003 AT RBL 9, 18, 27, 36 AND LBL 9, 18 AND 27. REPAIRED IAW REO 601R-53-61-2155. MAJOR REPAIR.
FS 484, OTBD SUPPORT ANGLE CRACKED AT LBL 36.0. REPAIRED IAW SRM 51-41-06, 51-42-06, 51-40-11 & REO 601R-53-41-059.
FS 484.00, RT FLOORBEAM ANGLES ARE CRACKED INBD AND OTBD. REMOVED INBD AND OTBD SUPPORT ANGLE FROM INTERCOSTAL IAW SRM 51-42-06. INSTALLED NEW IAW SRM 51-42-06 & REO 601R-53-41-059.
FLOOR SUPPORT HAS MINOR CORROSION AT LBL 45.0 FROM FS 559 TO 559+80. REPAIRED IAW GREO 601R-53-00-526, REV.
FLOOR SUPPORT HAS CORROSION IN VARIOUS AREAS FROM FS 349 TO 379 AT LBL 45.0. REPAIRED IAW SRM 51-12-00 AND REO 601R-55-00-530.
FRAME BS 349 CORRODED BETWEEN STRINGERS 26L AND 26R. REMOVED LOWER FRAME SECTOR IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE LWR FRAME SECTOR IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FRAME SECTOR LOWER IAW SRM 51-42-06 AND 51-42-21.
EMERGENCY LIGHT HAS DAMAGE ON LT AND RT SIDE PROTECTIVE COVERS AND PHOTOLUMINESCENT INSERTS. REPLACED DAMAGED PROTECTIVE COVERS AND PHOTOLUMINESCENT INSERTS ON LT & RT SIDES IAW STC ST02687AT.
FRAME 319.70 CORRODED BETWEEN STRINGERS 26L AND 26R. REMOVED LWR FRAME SECTOR AT FS 319.70 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW FRAME SECTION 319.70 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FRAME SECTOR AT FS 319.70 IAW SRM 51-42-06 AND 51-42-21.
SEAT TRACK CORRODED AT RBL 9.0 BETWEEN FS 409 TO 409+112. R & R SEAT TRACK IAW SRM 51-40-11 AND 51-41-02. INSTALLED NEW SEAT TRACK IAW SRM 51-40-11 AND 51-41-02.
SEAT TRACK CORRODED AT RBL 9.0 FROM FS 364 TO 379. R & R CORRODED SEAT TRACK IAW AMM 53-01-11-400-802.
LEFT AFT GUIDE FITTING ON AVIONICS DOOR SURROUND STRUCTURE IS CRACKED. REMOVED AND REPLACED GUIDE FITTING, LT AFT AT AVIONICS DOOR OPENING IAW AMM 20-21-00-910-801 & 20-24-00-910-803.
FRAME BS 333 CORRODED BETWEEN STRINGERS 26L AND 26R. REMOVED FRAME SECTOR IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED FRAME SECTOR IAW SRM 51-40-11. REMOVED DRAG ANGLE FROM FRAME SECTOR LWR IAW SRM 51-42-06. LOCATED AND DRILLED DRAG ANGLE TO MATCH FRAME SECTOR IAW SRM 51-40-11.
SUPPORT ANGLE ATTACHED TO AFT WEB OF PAX DOOR VENT FLAP STRUCTURE IS CRACKED. R & R INNER ANGLE ATTACHED TO AFT WEB OF PAX DOOR VENT FLAP STRUCTURE, PN 601R318072-1 IAW SRM 51-42-06.
FS 280.00 RBL 9.0 INBD AND OTBD ANGLES ARE CRACKED. REMOVED INBD AND OTBD ANGLES RBL 9.0 IAW REO 601R-53-11-171. INSTALLED INBD AND OTBD ANGLES IAW REO 601R-53-11-171. FABRICATED ANGLES IAW REO 601R-53-11-171.
LT INBD FLAP, INB HINGE, AFT INBD LUG PLATE IS CHAFED. DAMAGE APPROX .100"L X .030"W X .015"D. REPAIRED IAW REO 601R-57-52-1536 IAW SRM 51-12-00. MAJOR REPAIR.
FRAME BS 310 CORRODED BETWEEN STRINGERS 26L AND 26R. REMOVED LWR FRAME SECTOR AT FS 310.00 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW FRAME SECTOR PN 601R32002-69 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FS 310 FRAME SECTOR PN 601R32002-69 IAW SRM 51-42-06 AND 51-42-21.
FOUND FS 409+128 RBL 18 INBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .250" LONG X 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 & 51-42-22 & REO 601R-53-41-889, REV A.
FOUND LBL 18 INBD POST AT FS 409+128 HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .250" LONG X 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED LBL 18 409+128 POST IAW SRM 51-42-06 & 51-42-22. LOCATED & DRILLED NEW SERVICEABLE INBD FS 409+128 LBL 18 POST IAW SRM 51-40-11. INSTALLED FS 409+128 LBL 18 POST ASSY IAW REO 601R-53-41-889, REV A.
NR 2 EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R BULB. IAW AMM 33-51-21. OP'S CHECKED GOOD.
NR 2 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. R & R NR 2 CEILING EMERGENCY FLOOD LIGHT ASSY IAW AMM 33-51-16.
ELECTRICAL BURNING ODOR IN LAVATORY. FOUND LAVATROY VANITY LIGHT BALLAST TO BE SOURCE OF ODOR, DISCONNECTED BALLAST IAW AMM 33-25-02. (
HYDRAULIC LOW PRESSURE MESSAGE DURING APPROACH, RAN QRH. GEAR SLOW COMING DOWN. WENT AROUND AND CONTINUED NORMAL LANDING. EMERGENCY DECLARED. R & R NR 3A HYDRAULIC PUMP ASSY IAW AMM-29-12-03, OPS AND LEAK CHECKED GOOD,
EMERGENCY EXIT SIGN FLOOR LEVEL NEAR PASSENGER DOOR, MISSING LENS. REPLACED LENS IAW AMM 33-51-19. NO FURTHER DEFECTS FOUND.
WHEN SELECTING GEAR DOWN, RECD HYD 3 LOW PRESS CAUTION MESSAGE. EXECUTED QRH PROCEDURE, HYD SYS SHOWED 0 PERCENT SYS QUANTITY, PERFORMED ALTERNATE GEAR EXTENSION, ON POST FLIGHT FOUND HYD FLUID ON UNDERSIDE OF FUSELAGE. UNABLE TO STOW ALTERNATE EXTENSION HANDLE. EMERGENCY DECLARED AS A PRECAUTION. R & R NR 3A HYD PUMP PRESSURE HOSE IAW AMM 29-12-03. LEAK AND OPS CHECKED GOOD. ACFT OK FOR SERVICE.
SERVICE DOOR SURROUND STRUCTURE LOWER SILL HAS MODERATE CORROSION LOCATED BETWEEN FS 349 AND FS 364 ON UPPER AND LOWER SURFACES. WORST AREA IS AT FWD NUTPLATE HOLE AND MEASURES APPROX 1.8" DIA X .005" DEEP ON TOP SURFACE AND .7 DIA X .002" DEEP ON LOWER SURFACE. REPAIRED IAW REO 601R-53-61-1303, REV.
PAX DOOR AFT DRAG ANGLE CRACKED AT DOOR ASSIST CABLE PULLEY. C/W EC/TC REO 601R-52-11-513 REPAIR OF PAX DOOR AFT DRAG ANGLE. RII FOUND TO BE SATISFACTORY.
FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT LBL 27.50 INBD FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1541.
FOUND VERTICAL POST FS 409.0+128, BL 0.0 LT AND RT SIDES HAVE INDICATIONS NOTED APPROX .2" IN LENGTH 80 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. BOTH FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06 AND 51-42-21. INSTALLED POST ASSY IAW REO 601R-53-41-889.
FOUND FS 409.0+128 LBL 18.0 OTBD VERTICAL POST HAS INDICATION NOTED APPROX .2" IN LENGTH, 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REPAIRED IAW AMM 51-23-00-390-804.
FOUND FS 409.0+128, RBL 18.0 OTBD VERTICAL POST HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSHF AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED POST IAW SRM 51-42-06. INSTALLED NEW POST ASSY IAW REO 601R-53-41-889 AND SRM 51-42-06.
RT FS 621 TO 625 OBLIQUE ANGLE IS CRACKED, R & R ANGLE IAW SRM 51-42-21.
LT FS 621 TO FS 625 OBLIQUE ANGLE IS CRACKED. R & R ANGLE IAW SRM 51-42-21.
CABIN FLOOR SUPPORT TRANSVERSE BEAM AT FS 349 HAS CORROSION ON RT SIDE AT OTBD END, TOP SURFACE, MEASURES APPROX 1.1" LONG X .5" WIDE X .003" DEEP. REMOVED CORROSION IAW SRM 51-21-06, TREATED IAW 51-21-11 AND PRIMED AND PAINTED IAW 51-25-00.
FOUND FS 559 BULKHEAD WEB HAS 3 INDICATIONS NOTED ALL APPROX .2" IN LENGTH, LT FS 559 WEB INDICATIONS AT WL 51.70 50 PERCENT FSH, RT FS 559, WEB 70 PERCENT FSH OTBD OF RBL 9.0, WL 58.70 AND RT FS 559 WEB 50 PERCENT FSH INBD OF RBL 18.0 AT WL 59.10 LT AND RT SIDES FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-41-260 AND REO 601R-53-41-260, REV E.
CARGO SEAT TRACK LBL 9 FS 559+112 CORRODED. REMOVED CORRODED TRACK & INSTALLED NEW TRACK IAW SRM 51-40-11, 51-41-02 & AMM 20-21-00-910-801.
CARGO SEAT TRACK RBL 9, FS 559+96 CORRODED. REMOVED CORRODED TRACK. INSTALLED NEW TRACK IAW SRM 51-40-11, 51-41-02 AND AMM 20-21-00-910-801.
CARGO SEAT TRACK RBL 9, FS 559+112, CORRODED. REMOVED CORRODED TRACK. INSTALLED NEW TRACK IAW SRM 51-40-11, 51-41-02 & AMM 20-21-00-910-801.
CARGO SEAT TRACK, RBL 27, FS 559+96 CORRODED. REMOVED CORRODED TRACK AND TRACK FITTING. LOCATED AND INSTALLED NEW TRACK IAW SRM 51-40-11, 51-41-02 AND AMM 20-21-00-910-801.
FS 280, RBL 9 OTBD FLOOR SUPPORT ANGLE CRACKED. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW REPLACEMENT SUPPORT ANGLE S6144-13 IAW SRM 51-42-21 AND SRM 51-42-06.
FS 484, RBL 36 FLOOR SUPPORT ANGLE CRACKED. R & R FLOOR SUPPORT ANGLE AT FS 484, RBL 36 IAW REO 601R-53-41-059.
FS 621 BULKHEAD FWD SIDE ISOLATOR CRACKED. R & R ISOLATOR IAW SRM 51-42-13.
CARGO SEAT TRACK LBL 27, FS 559+112 CORRODED. INSTALLED NEW TRACK IAW SRM 51-40-11, 51-41-02 & AMM 20-21-00-910-801.
CARGO SEAT TRACK LBL 9 JUST AFT OF FS 559+96 CORRODED. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK IAW SRM 51-40-11, 51-41-02 & AMM 20-21-00-910-801.
EMERGENCY EXIT FLOODLIGHT ON GALLEY SIDE CLOSEOUT PANEL IS CRACKED. INSTALLED SERVICEABLE LIGHTED FLOOR LEVEL EXIT SIGN IAW AMM 33-51-10-400-801. OPS TESTED GOOD IAW AMM 33-51-00-710-801.
EMERGENCY FLOOR LIGHTING IS DISCOLORED AND CRACKED ON THE LT & RT FWD SECTIONS OF LIGHT TRACK. REPLACED LIGHT.
AFTER RAISING GEAR AFTER T/O WE HAD A NOSE DOOR OPEN WARNING MSG AND A GEAR DISAGREE WARNING MSG. MAINS RETRACTED NORMALLY NOSE STAYED DOWN AND LOCKED GREEN INDICATION. RAN QRH AND RETURNED TO DEPARTURE. (LANDING GEAR RETRACTION SYS ) (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) FOUND NLG CTR/EXTENTED PROX SWITCH S23 NOT WITHIN LIMITS PERFORMED NLG PROX SWITCH S23 ADJUSTMENT IAW AMM-32-61-05, PERFORMED NLG EXTENTSION RETRACTION SWING IAW AMM-32-61-00. OPS CHECKS GOOD DEFER CLEARED PLACARD REMOVED.
AFTER RAISING GEAR AFTER TAKEOFF, WE HAD GEAR DISAGREE WARNING MSG AND NOSE DOOR OPEN WARNING MSG. C/W QRH AND LANDED IN CHS. MAIN GEAR RETRACTED NORMALLY, NOSE GEAR REMAINED DOWN. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED, ARFF RESPONDED ADJUSTED NLG OLEO CENTERED / EXTENDED PROXIMITY SENSOR IAW AMM 32-61-05. OP'S CHECK GOOD.
RT FIRE FAIL CAUTION MESSAGE INTERMITTENT DURING FLIGHT. R & R THE FIRE CONTROL UNIT IAW AMM 26-10-01.
ON TAKEOFF HAD A GEAR DISAGREE AND FOLLOWED QRH. MANUAL EXTENSION PULLED AND COULD NOT STOW BACK. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. R & R CENTERED/EXTENDED PROX SENSOR BRACKET AND RE-RIGGED PROX SWITCH IAW AMM 32-61-05. OPS CK GOOD, DEFER CLEARED PLACARD REMOVED ACFT OK FOR SERIVCE. PERFORMED INSPECTION OF BRACKET INSTALLED AND OPS CHECKED. GEAR SWING, NO DEFECTS NOTED.
REPLACED PAX DOOR EXIT PLACARD IAW AMM 11-30-00. ITEM: 1 01-02-2010 REPLACED PAX DOOR EXIT PLACARD IAW AMM 11-30-00. (CLOSED)
PAX DOOR EXIT PLACARD PEELING.
RECEIVED LT 14TH DUCT MSG IN FLIGHT. C/W QRH, MSG PERSISTED, DIVERTED TO CAE. EN ROUTE TO ILM, A/C DIVERTED TO CAE DUE TO MTC.
OPERATION 367/CONTINUATION OF JOB 8765821 OP 264, FLOOR BEAM AT LBL 27 OTBD FLANGE IS CORRODED AROUND NUTPLATE FOR FLOORBOARD SCREWS FS 559+80 TO FS 621.0.
PAX DOOR AFT SUPPORT BRACKET AT FS 343 IS CORRODED AND REQUIRES REPLACEMENT. REMOVED DAMAGED BRACKET & INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-42-06. APPLIED TOPCOAT AND SEALANT IAW AMM 51-23-00 AND 51-25-16.
FS 280 TRANSVERSE BEAM IS CRACKED O/B APPROX 1.5 INCH FROM RBL 9.00 JUST ABOVE LOWER RADIUS.
FS 280 FWD FLOOR ANGLE HAS SEVERE CORROSION IN SEVERAL AREAS.
FS 280 TRANSVERSE BEAM IS CRACKED O/B APPROX 3FT FROM LBL 9.00 JUST ABOVE LOWER RADIUS. FABRICATED 1 REPAIR ANGLE FROM 2075-0 .050 HEAT TREATED TO T62 IAW REO 601R-53-11-171. REPAIRED TRANSVERSE BEAM IAW EO 600-53-90 C/W AND REO 601R-53-11-171 REV D.
OPERATION 299/PAX DOOR AFT WEB IS CRACKED AT TOP OF STEP 832BT, APPROX 15 INCHES LONG.
FS 621 PRESSURE BULKHEAD WEB HAS MULTIPLE HFEC INDICATIONS BETWEEN 50 PERCENT AND 80 PERCENT FSH AND APPROX .2 INCH IN LENGTH EXTENDING FROM BOTH I/B CORNERS OF THE LINTEL FITTING FAILS NDT INSP AT THIS TIME. REPAIRED PER EC/TC REO 601R-53-61-1230.
CARGO DOOR SUPPORT BEAM LOWER AFT BRACKET IS CRACKED APPROX .25 INCH.
JOB 8765821 OPERATION 268 / INBOARD WING PLANK AT FUEL PNL 550HB HAS CORROSION IN NON-CRITICAL AREA. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW BOMBARDIER REO 601R-57-21-030, REV G.
JOB 8765821 OPERATION 267 / FWD PLANK AT FUEL PNL 510AB HAS CORROSION APPROX 40 PERCENT OF WING PLANK IN CRITICAL AND NON-CRITICAL AREAS. COMPLIED WITH EC/TC EO 600-57-81 & REPAIRED IAW REO 601R-57-21-030, REV G.
JOB 8765821 OPERATION 266 / INBOARD AND OUTBOARD WING PLANK AT FUEL PNL 540BB HAS CORROSION IN NON-CRITICAL AREA. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV G.
FLOORBEAM AT LBL 27 OUTBOARD FLANGE IS CORRODED AROUND NUT PLATES FOR FLOORBOARD SCREWS FS 559+80 TO FS 621.0. REMOVED FLOORBEAM CAP IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW CAP IAW SRM 51-42-06. REMOVED BEAM FITTING STA 605-621 IAW SRM 51-42-06 & 51-42-21. LOCATED AND DRILLED NEW BEAM FITTING IAW SRM 51-42-06 & 51-42-51. BEAM CAP AND BEAM FITTING REQUIRES INSTALLATION. INSTALLED BEAM FITTING P/N 601R35289-1 IAW SRM 51-42-06 & 51-42-21. INSTALLED FLOORBEAM CAP IAW SRM 51-42-06, 51-42-22 & 51-42-21.
FS 349 CAP DOUBLERS THAT FLOORBOARDS LAY ON FROM LBL 40 TO RBL 40 (5 EA) HAVE AREAS OF CORROSION ON RIVET HEADS.
FS 280 ATTACH CLIPS FOR FLOORBEAMS ARE CRACKED AT O/B SIDE OF LBL 9 AND O/B SIDE OF RBL 9. REMOVED & REPLACED PER REO 601R-53-11-171 STEP 9 ON MWC 8765821.
FS 280 AFT J-ANGLE IS CRACKED 1.5 INCH IN RADIUS O/B OF LBL 9. C/W EC/TC EO 600-53-91 C/W IAW REO 601R-53-11-136 REV A.
RIGHT SIDE FS 621 FLOOR SUPPORT ANGLE IS CRACKED AT RBL 49, WL 73. COMPLIED WITH REPAIR TO FLOOR SUPPORT ANGLE FS 621 RT IAW REO 601R-53-61-117 REV C AND ECTC 601R-53-61-117.
LEFT SIDE FS 621 FLOOR SUPPORT ANGLE IS CRACKED AT LBL 40, WL 73. REPAIRED LT FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117.
FS 484 FLOOR SUPPORT INTERCOSTAL HAS A CRACKED ATTACH ANGLE AT THE O/B SIDE OF RBL 27. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-06.
JOB 8765821 OPERATION 212 / LT BATT RIB CRACKED AROUND TOP FASTENER.
PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED AFT DRAG ANGLE AND 2 EA PREVIOUS REPAIR SPLICES IAW SRM 51/42/06. COMPLIED WITH EC/TC REO 601R-52-11-513 AND ALL WORK WAS PERFORMED IAW REO 601R-53-11-513 REV A.
PAX DOOR BOTTOM FOLDING STEP IS CRACKED IN SEVERAL PLACES. REMOVED DAMAGED STEP IAW AMM 52-11-04-000-802 AND INSTALLED A SERVICEABLE STEP IAW AMM 52-11-04-400-802. CONNECTED ROD ASSY TO BOTTOM FOLDING STEP IAW AMM 52-11-04-400-802. PERFORMED OPS CHECK OF BOTTOM FOLDING STEP IAW AMM 52-11-04-710-803. OPS CHECK GOOD.
JOB 8765821 OPERATION 144 PAX DOOR AFT WEB IS CRACKED AT HANDRAIL BRACKET AND STEP JUST BELOW. COMPLIED WITH EC/TC REO 601R-52-11-702 AND MET ALL THE REQUIREMENTS OF REO 601R-52-11-702 REV A.
OPERATION 143/ PAX DOOR FWD WEB IS CRACKED AT HANDRAIL BRACKET AND JUST BELOW.
EXTERIOR EMERGENCY LIGHT NR 3 ON LEFT SIDE OUT.
ENGINE BOX BEAM CRACKED MIDDLE AFT WEB, COMING FROM THE FIRE LOOP SUPPORT BRACKET. COMPLIED WITH REO 601R-53-61-345 AND EO600-53-72-0001.
FLAPS FAILED AT ZERO IN FLT, EMERGENCY DECLARED. FLT 4916, 5325 CX.
FWD LT OVERWING EMERGENCY LIGHT IS INOP.
EXIT PLACARD ON MAIN CABIN DOOR PARTIALLY MISSING ALONG WITH EMERGENCY DIRECTIONAL ARROW. FLT 4250 DEL 15 MINS. REPLACED EXIT AND ARROW ON PAX DOOR IAW AMM. (K)
CEILING EMERGENCY FLOOD LIGHT OVER ROW 10 INOPERATIVE. RELAMPED CEILING EMERGENCY FLOOD LIGHT OVER ROW 10 IAW CRJ200 AMM33-51-16. OPS CHECK GOOD. (K)
EMERGENCY LIGHTS INOP.
EMERGENCY EXIT SIGN OVER THE AISLE IS BROKEN.
LEFT SIDE FWD EMERGENCY EXIT LIGHT INOP.
FOUND FS 484 LBL 27.0 O/B ANGLE CRACKED.
EXTERIOR PAX DOOR HANDLE IS CRACKED. REPAIRED IAW SRM 52-11-03.
FOUND FS 484 RBL 36.00 O/B ANGLE CRACKED.
CABIN EMERGENCY ESCAPE HATCH EXTERIOR INSTRUCTION PLACARD MISSING, RESOLVED ON W/O: 61271 TASKCARD: N/R-00122. REMOVED AND REPLACED CABIN EMERGENCY ESCAPE HATCH EXTERIOR INSTRUCTION PLACARD WITH NEW SERVICEABLE PLACARD P/N S1859, PO NR ASA115 IAW CRJ 200 AMM 11-20-01.
FLAP FAIL AT ZERO DEGREES ON APPROACH. EMERGENCY EQUIPMENT ROLLED AS A PRECAUTION.
FLAPS FAIL WHEN SELECTING FLAPS 20 DEGREES ON APPROACH. LEFT AT 8 DEGREES, RIGHT AT 10 DEGREES. EMERGENCY DECLARED.
FLAP HALF SPEED FOLLOWED BY FLAP FAIL. EMERGENCY DECLARED. FLT 4879 CX. REMOVED AND REPLACED PDU IAW AMM OPS CHECK GOOD.
RIGHT FS 640 DOUBLER HAS 1 .5 INCH LONG CRACK AT STRINGER 10.
FLOORBEAM ATTACH CLIPS AT FS 280, LBL 9 I/B AND O/B, RBL 9 I/B AND O/B CRACKED.
LT BOX BEAM CRACK LOWER WEB C/W REO601R-53-61-366. REPAIRED LEFT HAND LOWER BOX BEAM WEB REF REO 601R-53-61-366 (CLOSED 11/01/06)
LT FS 640 DOUBLER HAS .7500 INCH CRACK AT STRINGER 10. REPAIRED & MODIFIED FRAME 640 BETWEEN STR 9 AND 12 ON LT & RT SIDE REF: SB601R-53-061 APP B. REPAIRED THE BONDED SKIN DOUBLER AT FRAME 640 REF REO: 601R-53-61-506. REPAIRED RIGHT SIDE LOWER BOX BEAM WEB AT ACCES PANEL REF REO: 601R-53-61-366. (CLOSED 11/01/06)
RT FS 640 DOUBLER HAS 1.5 INCH LONG CRACK AT STRINGER 10, FLT 4844 CX.
ENGINE BOX BEAM HAS A CRACK AT RT LOWER ACCESS PANEL FORWARD IB CORNER. CRACK IS APPROXIMATELY 1.5- 2 INCHES LONG. REPAIRED RIDE SIDE LOWER BOX BEAM WEB AT ACCES PANEL REF REO 11/01/06 01R-53-61-366 (CLOSED 11/01/06)
DURING CRUISE, AT APPROXIMATELY 30,000 FEET, THE CREW HEARD A LOUD NOISE AND SAW THAT THE CAPTAINS NR 2 WINDSHIELD HAD SHATTERED. THE CREW DECLARED AN EMERGENCY AND DESCENDED TO 25, 500 FT. THE REMAINDER OF THE FLIGHT WAS UNEVENTFUL, AND THE AC LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN`S NR 2 WINDSHIELD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
DURING A HANGAR INSPECTION, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE FORWARD EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
DURING A GROUND INSPECTION, THE EMERGENCY LIGHT STRIP HOUSING, NEAR THE PASSENGER DOOR ENTRANCE, WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K)
DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING A GROUND INSPECTION IN ATL, THE EXIT SIGN, NEAR THE GALLEY, WAS FOUND TO HAVE A MISSING COVER. MAINTENANCE REPLACED THE EXIT SIGN COVER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
FLT 4500 - DURING A GROUND INSPECTION IN SHV, THE FLOOR LEVEL EMERGENCY LIGHT, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE FLOOR LEVEL EMERGENCY LIGHT, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING A C-CHECK IN HOT, THE FS 621 RIGHT BEAM WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 621 RT BEAM IAW ASA EO 600-53-0105. (M)
DURING A C-CHECK IN HOT, THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M)
DURING A C-CHECK IN HOT, THE FS 621 LEFT/RIGHT OBLIQUE ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 621 LT/RT OBLIQUE ANGLE IAW CRJ SRM
DURING A GROUND INSPECTION, THE 2ND OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE LAMP IN THE 2ND OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD. AC OK FOR SERVICE. (K)
FLT 4571 - DURING APPROACH INTO YUL FROM ATL, UPON SELECTING THE FLAPS TO EIGHT DEGREES A FLAP FAIL CAUTION MESSAGE WAS RECEIVED WITHT THE FLAP INDICATOR SHOWING ZERO DEGREES. THE QRH WAS COMPLIED WITH AND THE CREW REQUESTED EMERGENCY VEHICLES TO BE ROLLED AS A PRECAUTION. A ZERO FLAP LANDING WAS ACCOMPLISHED WITH THE AIRCRAFT LANDING SAFELY. MAINTENANCE INSPECTED THE FLAPS AND RESET THE FLAPS SYSTEM IAW ASA EO 600-27-0004. NO DEFECTS WERE NOTED AND SYSTEM OPERATIONS WERE GOOD. UPON FURTHER INSPECTION MAINTENANCE FOUND THE LEFT AND RIGHT NR 1 AND THE RIGHT NR 4 FLEX SHAFTS DAMAGED. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT NR 1 AND THE RIGHT NR 4 FLEX SHAFTS. OPERATIONAL CHECKS GOOD. AIRCRAFT
FLT 4118 - DURING A GROUND INSPECTION IN MGM, THE NR 4 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE NR 4 EMERGENCY CEILING LIGHT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING CRUISE, AT APPROXIMATELY 37,000 FT, CREW RECEIVED A RT PACK HIGH TEMP MASTER CAUTION. CREW REQUESTED DESCENT TO 25,000 FT WHILE COMPLYING WITH CHECKLIST FOLLOWED BY THE RT PACK HIGH TEMP MASTER CAUTION GOING OUT. PACK DID NOT RESET OR COME ON. UPON LEVELING TO 25,000 FT A LT PACK HIGH PRESSURE MASTER CAUTION WAS RECEIVED. CREW REQUESTED EMERGENCY DESCENT TO 10,000 FT WITH THE FIRST OFFICER COMPLYING WITH THE CHECKLIST. AN EMERGENCY WAS DECLARED WITH THE TOWER INSTRUCTING THE AIRCRAFT TO DIVERT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED RT PRESSURE REGULATING VALVE AND ALSO GROUND RAN LT PACK WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
DURING AN A-CHECK, THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
DURING HANGAR MAINTENANCE, THE LT INTERIOR EMERGENCY EXIT LIGHT FORWARD OF THE WING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE LT INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY FORWARD OF THE WING AND CLEANED THE CONNECTORS; THEN REINSTALLED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.
DURING DESCENT, AT APPROXIMATELY 11,000 FEET, THE CREW NOTICED A STRONG BURNING SMELL IN THE COCKPIT AND CABIN WITH THE LT PACK GOING TO FULL HOT WHICH BECAME UNCONTROLLABLE IN EITHER AUTOMATIC OR MANUAL MODES. AN AUTOMATIC SHUTDOWN OF THE PACK OCCURRED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT AIR CYCLE MACHINE AND ALSO THE COMPRESSOR DISCHARGE OVERTEMP SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.
DURING HANGAR MAINTENANCE IN MCN, THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR WERE FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE TOP AND BOTTOM STEPS ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
FLT 4486 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 10. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING A GROUND INSPECTION IN ATL, THE AFT OVERWING EMERGENCY EXIT LIGHT ON THE RIGHT SIDE WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OVERWING EMERGENCY EXIT LIGHT LAMP ON THE RIGHT SIDE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING HANGAR MAINTENANCE, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY CEILING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING APPROACH INTO DFW FROM HSV, TEH CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE WHEN SELECTING THE FLAPS TO 30 DEGREES FOR LANDING. QRH PROCEDURES WERE COMPLIED WITH AND A NORMAL LANDING ACHIEVED WITH FLAPS SELECTED AT 20 DEGREES. EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE FLAPS CONTROL UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING GROUND INSPECTION, WHEN THE EMERGENCY LIGHT SWITCH IS IN THE OFF POSITION AND THE AIRCRAFT POWER IS TURNED OFF, EMERGENCY LIGHTS COME ON. ALSO WHEN THE AIRCRAFT POWER IS TURNED ON AND THE EMERGENCY LIGHT SWITCH IN THE COCKPIT IS TURNED ON, THE EMERGENCY LIGHTS DO NOT COME ON. MAINTENANCE RESECURED A LOOSE WIRE ON THE EMERGENCY LIGHTS CONNECTOR. OPERATIONS CHECK GOOD. AIRCRAFT OK FOR SERVICE.