N875AS
Registered owner: CORPORATE FLIGHT MANAGEMENT INC DBA, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Atlantic Southeast Airlines, Inc. | Operator | 2011-09-01 – 2011-09-01 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
WING OVHT WARNING MESSAGE IN CLIMB, FOLLOW QRH, MESSAGE DIDNÃâ¬â¢T CLEAR. / FA REPORTS CABIN SMELLS LIKE RUBBER BURNING. (FLIGHT 5735 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24708232 WITH THE FOLLOWING CORRECTIVE ACTION: "FOR RUBBER BURNING SMELL SEE THE FOLLOWING CPS: / CP 24710772 FOR COMPLETION OF FIM 21-21-00. / CP 24710534 FOR REPLACEMENT OF THE LH AND RH WATER SEPARATOR ASSEMBLY. / CP 24710536 FOR ISOLATING BLEED SOURCES WHILE OPERATING ENGINES AND APU. / FOR THE WING OVHT WARNING MESSAGE SEE THE FOLLOWING CPS: / CP 24708431 FOR THE REPLACEMENT OF THE RH OVERHEAT SENSOR, CONTROL SENSOR, AND STANDBY THERMAL SWITCH. / CP 24708433 FOR LH OVERHEAT AND SUFFICIENT HEAT RESISTANCE CHECKS. / CP 24711747 FOR FUNCTION CHECKS OF THE LH STANDBY THERMAL SWITCH, BACKUP SUFFICIENT HEAT SWITCH, STANDBY OVERHEAT SWITCH. / "
RH BEAM INTERCOSTAL FOUND CRACKED ON RBL9 AND BETWEEN FS559.00+64 - FS559.00+80. (C-CHECK RO 3-25-22) REMOVED AND REPLACED RH BEAM INTERCOSTAL P/N 601R31117-35 AT RBL9 AND BETWEEN FS559.00+64-FS559.00+80 WITH A NEW IDENTICAL UNIT IAW CRJ200 SRM 51-42-06 AND BOMBARDIER DWG 601R31119 REV. H. COMPLIED WITH TASK CARD 51-900-1003-SKY.
* FOUND TWO NICKS ON THE LH TRUNNION OF THE HSTA ATTACH FITTINGS.(AREA MARKED) (C-CHECK RO 3-25-22) BLENDED DAMAGES ON LH TRUNNION OF THE HSTA ATTACH FITTINGS REF CRJ200 SRM 51-12-00. WITHIN LIMITS, RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-55-31-398 REV--, DATED 2022-02-11.
CANN FLIGHT OBSERVERS LOWER SEAT RAIL P/N: 15981-1 FOR USE ON N929SW / SN: 7703. (C-CHECK RO 3-25-22) REMOVED AND REPLACED FLIGHT OBSERVER LOWER SEAT RAIL P/N 15981-1 REF CRJ 200 AMM 25-12-01-400-801
CORROSION FOUND UNDERNEATH GIRT BAR FITTINGS AT SERVICE DOOR LOWER THRESHOLD FS319.70 TO FS349.00 STR17R (C-CHECK RO 3-25-22) REMOVED LOWER THESHOLD ANGLE REF CRJ 200 SRM 51-42-06 AND 51-42-36, INSTALLED LOWER THESHOLD ANGLE REF CRJ 200 SRM 51-42-06, REF CRJ 200 SRM 51-42-36, REF CRJ 200 SRM 51-42-21 & DWG 601R38303 REV AR. SEE CONTINUE CARD FOR MORE DETAIL. COMPLIED WITH TASK CARD 51-900-1003-SKY.
R/H ELEVATOR FITTING LOCATED @ BL15.25 NEEDS TO BE REPLACED DUE TO CORROSION IN THE BEARING BORE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED R/H ELAVATOR FITTING ASSY( BEARING INCLUDED ) @ ES 15-25 P/N 600-24043-1 REF CRJ 200 SRM 51-42-06 AND CRJ 200 DWG# 601R24025 REV G . COMPLIED WITH SKYCARD 51-900-1003.
DEFECTS NOTED IN THE LH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE LH WING DRAIN LOCATED BETWEEN WS0.00 + THE LH BOOST PUMP AND BETWEEN STR5 - STR7. (C-CHECK RO 3-25-22) REPAIRED DEFECTS IN THE LH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE LH WING DRAIN LOCATED BETWEEN WS0.00 + THE LH BOOST PUMP AND BETWEEN STR5 - STR7. REF REO 601R-57-21-3570 REV-A DATED 2022-02-18. COMPLIED WITH TASK CARD 51-900-1003-SKY / LEAK CHECK RESULTS NO LEAKS AT THIS TIME
DEFECTS NOTED IN THE RH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE RH WING DRAIN LOCATED BETWEEN WS0.00 + THE RH BOOST PUMP AND BETWEEN STR5 - STR7. (C-CHECK RO 3-25-22) REPAIRED DEFECTS IN THE RH LWR WING PLANK FWD & AFT ATTACHMENT HOLES FOR THE RH WING DRAIN LOCATED BETWEEN WS0.00 + THE RH BOOST PUMP AND BETWEEN STR5 - STR7. REF REO 601R-57-21-3569 REV A DATED 2022-02-18 / COMPLIED WITH ALL STEPS OF REO 601R-57-21-3569 REV A DATED 2022-02-18 / COMPLIED WITH TASK CARD 51-900-1003-SKY / LEAK CHECK RESULTS NO LEAKS AT THIS TIME
BRACKET COMMON TO PAX DOOR INTERCOSTAL DD6 FOUND CORRODED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED PAX DOOR BRACKET P/N 601R8084-2 WITH A SERVICEABLE UNIT IAW CRJ200 SRM 51-42-06 REVISION 38: JUL 10/2019 AND BOMBARDIER DRAWING 601R31702 REV. -N. COMPLIED WITH TASK CARD 51-900-1003-SKY. PRESSURIZED THE AIRCRAFT IAW CRJ200AMM 21-32-00-863-801. LEAK CHECK GOOD.
* THE LH WING AILERON HINGE FITTING WING SIDE #3 HINGE INBD LUG IS GOUGED. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE ON LH WING AILERON HINGE FITTING WING SIDE #3 HINGE REF CRJ200 SRM 51-12-00. FOUND TO BE WITHIN LIMITS. REF REO 601R-57-51-989 REV--, DATED 2022-02-08. COMPLIED WITH TASK CARD 51-900-1003-SKY.
* THE RH WING AILERON HINGE FITTING WING SIDE #4 HINGE KEEPER BOLT HOLE ON OUTBD SIDE IS GOUGED. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE ON RH WING AILERON HINGE FITTING WING SIDE #4 HINGE REF CRJ200 SRM 51-12-00. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-51-987 REV--, DATED 2022-02-03. COMPLIED WITH TASK CARD 51-900-1003-SKY.
* THE RH WING AILERON HINGE FITTING WING SIDE #3 HINGE IS CHAFFED IN 2EA LOCATIONS. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGES ON RH WING AILERON HINGE FITTING WING SIDE #3 HINGE REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-51-987 REV--, DATED 2022-02-03. COMPLIED WITH TASK CARD 51-900-1003-SKY.
* THE LH OUTBD GROUND SPOILER PCU HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H OUTBOARD GROUND SPOILER PCU ATTACHMENT HARDWARE AND REPLACED WITH NEW HARDWARE TO INCLUDE 3 EA NUTS, 1 EA BOLT, 2 EA WASHERS AND COTTER PINS. ONLY REPALCED ONE NUT AT A TIME IAW CRJ200 AMM 27-63-01-400-801 PROCEDURE 2 STEPS 1 E AND F. CALIBRATED TOOLING TORQUE WRENCH TUC4980 CAL DUE DATE 28-FEB-22.
* THE LH INBD GROUND SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H INBOARD GROUND SPOILER HINGE ATTACHMENT HARDWARE AND REPLACED WITH NEW HARDWARE TO INCLUDE 3 EA NUTS AND COTTER PINS. ONLY REPALCED ONE NUT AT A TIME. IAW CRJ200 AMM 27-65-01-400-801 PROCEDURE 2 STEPS B9,10 AND 11. CALIBRATED TOOLING TORQUE WRENCH TUC4980 CAL DUE DATE 28-FEB-22.
* THE LH INBD GROUND SPOILER PCU HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) L/H INBOARD GROUND SPOILER PCU ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-63-01-400-801 STEPS 2.B.(2)
* THE LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE IS CORRODED AROUND NUTPLATE HOLES. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE AT LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE REF. CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-54-347 REV -- DATED: 2022-02-04.
* THE LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE IS CHAFFED. (MARKED) (C-CHECK RO 3-25-22) BLENDED CHAFFING ON LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-54-347 REV -- DATE 2022-02-04.
* THE LH SPOILERON PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED SURFACE CORROSION FROM L/H SPOILERON HARDWARE, REF. CRJ-200 SRM 51-21-06 STEPS 7. A. [1] (A)-(B).
* THE LH SPOILERON HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW HARDWARE ON L/H SPOILERON, REF. CRJ-200 AMM 27-64-01-400-801. SEE CONTINUATION FOR WORK PERFORMED.
*THE RH FLIGHT SPOILER PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H FLIGHT SPOILER PCU LOWER ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-62-01-400-801 STEPS 2. A THROUGH B / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/22
*THE RH FLIGHT SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H FLIGHT SPOILER HARDWARE FOR HINGE ATTACHMENT REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-64-05-400-801 STEPS 2.B. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/22
*THE RH OUTBD GROUND HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H OUTBOARD GROUND SPOILER HINGE ATTACHMENT CASTLE NUT, WASHER AND COTTER PIN REMOVED FROM INBOARD AND OUTBOARD HINGE AND REPLACED WITH NEW IAW CRJ200 AMM 27-65-01-400-801 STEPS 2.B.(9)(10)(11) / CAL TOOL USED: MACT2256X DUE 3/31/22
*THE RH INBD GROUND PCU HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED R/H INBOARD GROUND SPOILER PCU ATTACHMENT HARDWARE AND REPLACED WITH NEW IAW CRJ200 AMM 27-63-01-400-801 STEPS 2.B.(2)
*THE RH INBD GROUND HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED AND REPLACED CORRODED CASTLE NUTS, WASHERS AND COTTER PINS ON R/H INBOARD GROUND SPOILER HINGE ATTACHMENT OUTBOARD AND INBOARD HINGE IAW CRJ200 27-65-01-400-801 STEPS 2.B.(9)(10)(11) / CAL TOOLS USED: MACT2256X DUE 3/31/22
THE RH SPOILERON HINGES'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H SPOILERON HINGE ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-64-01-400-801 STEPS 2.B. AND C. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/22
* THE LH FLIGHT SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED HARDWARE FROM THE LH FLIGHT SPOILER HINGES REF CRJ200 AMM 27-64-05-000-801 PGS 401-407. INSTALLED NEW HARDWARE FOR THE LH FLIGHT SPOILER HINGES REF CRJ200 AMM 27-64-05-400-801 PGS 408-413. TW#TUC6231 DUE 31JAN23. REPLACED 4 NUTS, 4 COTTER PINS, 11 WASHERS, 2 BOLTS.
* THE LH FLIGHT SPOILER PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REPLACED LH FLIGHT SPOILER PCU'S CORRODED HARDWARE REF CRJ200 AMM 27-64-05-000-801 AND AMM 27-64-05-400-801. REPLACED 2 SCREWS,1 SPLIT WASHER, 1 NUT, 3 WASHERS.
* THE LH OUTBD GROUND SPOILER BONDING JUMPER HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H OUTBOARD GROUND SPOILER BONDING JUMPER ATTACHMENT HARDWARE AND REPLACED WITH NEW HARDWARE TO INCLUDE 2 EA NUTS AND 2 EA SCREWS. IAW CRJ200 AMM 27-65-01-400-801 PROCEDURE 2 STEP E. BONDING CHECK GOOD
* THE LH OUTBD GROUND SPOILER HINGES HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) REMOVED CORRODED L/H OUTBOARD GROUND SPOILER HINGE ATTACHMENT HARDWARE TO INCLUDE 3 EA NUTS AND COTTER PINS. ONLY REPALCED ONE NUT AT A TIME IAW CRJ200 AMM 27-65-01-400-801 PROCEDURE 2 STEPS B9,10 AND 11. CALIBRATED TOOLING TORQUE WRENCH TUC4980 CAL DUE DATE 28-FEB-22.
* THE RH SPOILERON PCU'S HAS CORRODED HARDWARE. (C-CHECK RO 3-25-22) R/H SPOILERON PCU LOWER ATTACHMENT HARDWARE REMOVED AND REPLACED WITH NEW IAW CRJ200 AMM 27-62-01-400-801 STEPS 2. A. THROUGH B. / CAL TOOLS USED: TUC5658 DUE 6/30/22, TUC4822 DUE 6/30/22
PAX DOOR CUT-OUT FRAME AFT ROLLER ATTACHMENT GOUGED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED THE PAX DOOR AFT ROLLER BRACKET REF AMM 53-21-23-400-801 REV 64 SEP 10/2021 AND DWG 600-31469 REV A. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. CHECKS GOOD.
*IN MAIN CABIN, ON PRESSURE FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559, AND RBL9, HAS CORROSION ON MULTIPLE AREAS OF UPPER SURFACE. (MARKED) (C-CHECK RO 3-25-22) PERFORMED REPAIR ON FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559.00, AND RBL9 BY CUTTING THE TOP FLANGES OF THE C CHANNELS AND INSTALLING A HAT EXTRUSION IAW REO 601R-53-41-3021 REV. -- DATE: 2022-02-15, CRJ200 SRM 51-42-21, AND CRJ200 SRM 51-42-22 COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.
PAX DOOR. UPPER STOP BOLT FITTING CORRODED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED BRACKET ASSY P/N 601R38921-13 WITH A NEW SERVICEABLE UNIT IAW CRJ200 SRM 51-42-14.
PAX DOOR. AFT DRAG ANGLE SUSPECTED CRACK BY THE MOTOR ASSIST PULLEY. (C-CHECK RO 3-25-22) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE P/N 601R31772-6 WITH A NEW UNIT IAW CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-14.
PAX DOOR, INTERCOSTAL DD6 AFT END CORRODED. DISCREPANCY VIEWED THRU ACCESS HOLE 832GR. (C-CHECK RO 3-25-22) REMOVED AND REPLACED PAX DOOR DD6 INTERCOSTAL P/N 601R31902-323 WITH A SERVICEABLE UNIT IAW CRJ200 SRM 51-42-06 REVISION 38: JUL 10/2019 AND BOMBARDIER DRAWING 601R31702 REV. -N. PRESSURIZED THE AIRCRAFT IAW CRJ200AMM 21-32-00-863-801. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
*IN MAIN CABIN, ON FLOOR BEAM AT APPROXIMATELY FS409+16 TO FS409+128, AND BETWEEN RBL6 TO RBL8, FLOOR BEAM HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED FLOOR BEAM CAP AT FS409+16 TO FS409+128, AND BETWEEN RBL6 TO RBL8 WITH A NEW IDENTICAL UNIT IAW REO 601R-53-31-1219 REV. -- DATE: 2022-02-04. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.
*IN MAIN CABIN, AT APPROXIMATELY FS409+30 TO FS409+128, AND NEAR LBL6-LBL8, FLOOR BEAM HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED MAIN CABIN FLOOR BEAM CAP AT APPROXIMATELY FS409+30 TO FS409+128, AND NEAR LBL6-LBL8 WITH A NEW UNIT IAW REO 601R-53-31-1223 REV̉‰DATE 2022-02-15 AND DWG 601R31024 REV D AND DWG 601R31117 REV E. COMPLIED WITH TASK CARD 51-900-1003-SKY. SE CONTINUATION CARD FOR DETAILS.
*IN MAIN CABIN, L/H PRESSURE FLOOR SILL MEMBER, FROM APPROXIMATELY 409+128 TO FS559, NEAR STR17L, HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED CORROSION FROM L/H PRESSURE FLOOR SILL FS 409+128-FS 559 STR 17L PER CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-53-41-666 REV-C DATED 2012-11-06, REO 601R-53-41-3018 REV -- DATE 2022-02-09. COMPLIED WITH TASK CARD 51-900-1003-SKY.
PAX. DOOR. CUT-OUT FRAME FS310.00 GOUGED JUST BELOW UPPER PIN STOP. (C-CHECK RO 3-25-22) PERFORMED REPAIR TO PAX DOOR SEAL STRIKER I.A.W. ALL STEPS OF REO 601R-53-22-033 REV-D DATE 2014/02/17 REPAIR TYPE IV. COMPLIED WITH TASK CARD 51-900-1003-SKY. OPS CHECKS GOOD.
*IN MAIN CABIN, ON PRESSURE FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559, AND LBL9, HAS CORROSION ON MULTIPLE AREAS OF UPPER SURFACE. (MARKED) (C-CHECK RO 3-25-22) PERFORMED REPAIR ON FLOOR SUPPORT BEAM, FROM APPROXIMATELY 409+128 TO FS559.00, AND LBL9 BY CUTTING THE TOP FLANGES OF THE C CHANNELS AND INSTALLING A HAT EXTRUSION IAW REO 601R-53-41-3020 REV. -- DATE: 2022-02-15, CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, AND CRJ200 SRM 51-42-22. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS. NO LEAKS NOTED
* THE LH SIDE SEAT TRACK FROM APPROX FS409+16 TO FS409+112 HAS MULTIPLE LOCATIONS OF CORROSION.(MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED LH SIDE SEAT TRACK FROM FS409+16 TO 409+112 REF CRJ200 AMM 53-01-11-000-802 STEPS 1-3.A AND AMM 53-01-11-400-802 STEPS 3.A. TORQUE SCREWDRIVER# TUC7826 DUE 31MAR22.
* THE LH SIDE SEAT RAIL RETAINER TRIM FROM APPROX FS364 TO FS409.00+16 HAS MULTIPLE LOCATIONS OF CORROSION.(MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED LEFT SEAT RAIL RETAINER AND SEAT RAIL FROM APPROX FS364 TO FS409+16 IAW CRJ200 AMM 53-01-11-00/400-802, SEE CONTINUATION FOR WORK ACCOMPLISHED
* THE RH SIDE SEAT TRACK FROM APPROX FS364 TO FS409+16 HAS MULTIPLE LOCATIONS OF CORROSION (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED RH SIDE SEAT TRACK FROM FS364 TO FS409+16 REF CRJ200 AMM 53-01-11-000-802 STEPS 1-3.A AND AMM 53-01-11-400-802 STEPS 3.A. TORQUE SCREWDRIVER# TUC7826 DUE 31MAR22.
* THE RH SIDE SEAT TRACK FROM APPROX FS409+16 TO FS409+112 HAS MULTIPLE LOCATIONS OF CORROSION (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED RH SIDE SEAT TRACK AT FS409+16 TO FS409+112 REF CRJ200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
*GUSSET COMMON TO FS409 FRAME AND INTERCOSTAL AT STR25R HAS CORROSION (MARKED). (C-CHECK RO 3-25-22) REPLACED GUSSET REF DRAWING #601R31049 REV:-F, CRJ200 SRM 51-42-21-00 REV: 38B DATED: 25 NOV 2020. FOR ALL WORK ACCOMPLISHED SEE CONTINUE CARD. COMPLIED WITH 51-900-1002-SKY.
*FRAME AT FS394 HAS GOUGE DAMAGE ON TOPSIDE RADIUS OF THE UPPER FLANGE AT STR27 (MARKED). (C-CHECK RO 3-25-22) BLENDED FRAME AT FS394 UPPER FLANGE AT STR27 PER REF: CRJ-200 SRM 51-12-00, FOUND TO BE WITH IN LIMITS REF CRJ 200 SRM 53-00-00. RESTORED FINISH PER CRJ-200 SRM 51-25-16,
*CORROSION ON FLOOR SILL ATTACHING ANGLE RBL 45 BETWEEN FS 605.00 ̉‰ 621.00 (C-CHECK RO 3-25-22) REMOVED CORROSION FROM FLOOR SILL ATTACHING ANGLE RBL45 F.S.605-621.00 IAW REO 601R-53-61-4690 REV.-- DATED 2012-10-24 FOUND TO BE WITHIN LIMITS.
*CORROSION ON FLOOR SUPPORT BEAM AT FS 589.00 BETWEEN RBL 27 ̉‰ RBL 36 (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AT FS 589.00 BETWEEN RBL 27 ̉‰ RBL 36 REF CRJ200 SRM 51-42-06 REV 38 JUL 10/2019 AND BOMBARDIER DWG 601R35031 REV -AG. COMPLIED WITH TASK CARD 51-900-1003-SKY.
*CORROSION ON FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 9 ̉‰ RBL 18 (C-CHECK RO 3-25-22) REMOVED CORROSION ON FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 9 ̉‰ RBL 18 IAW CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NEW FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 9 ̉‰ RBL 18 REF CRJ200 SRM 51-42-06 AND DWG 601R31025 REV-N. COMPLED WITH TASK CARD 51-900-1003-SKY.
*CORROSION ON FLOOR BEAM RBL 9 BETWEEN FS 559.00 ̉‰ 559.00+96 (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW FABRICATED RBL9 FLOOR BEAM CAP BETWEEN FS 559.00 AND FS 574 .00 REF CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-22, REO 601R-53-51-615 REV -- DATED 2022-02-11 AND DWG 601R-31119 REV H. FOR ALL WORK ACCOMPLISHED SEC CONTINUATION CARD. C/W TASK CARD 51-900-1003-SKY AND MAJOR REPAIR (M-337)
* THE FLOOR BEAM CAP AT RBL27 BETWEEN FS605 AND FS621 APROX HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REPLACED FLOOR BEAM CAP AT RBL27 BETWEEN FS605 AND FS621 REF REO 601R-53-61-3778 REV -B DATE 2016-12-19 AND DRAWING 601R35031 REV AG COMPLIED WITH TASKS CARDS 51-900-1003-SKY, 27-900-1003-SKY, 27-900-1008-SKY AND (M337) MAJOR REPAIR. FOR ALL WORK ACCOMPLISHED SEE CONTINUE CARD. ALL OPS CHECKS GOOD
* THE FLOOR BEAM CAP AT RBL9 BETWEEN FS605 AND FS621 APROX HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED CORRODED FLOOR BEAM CAP AT RBL9 BETWEEN APPROX. FS605 AND FS621 WITH A SERVICEABLE UNIT REF CRJ 200 SRM 51-42-21, REO 601R-53-61-3778 REV -B DATED 2016/12/19, AND DWG 601R35031 REV AG SEE CONTINUATION CARD FOR MORE DETAILS.COMPLIED WITH TASK CARD 51-900-1003-SKY
*IN MAIN CABIN, ON SUPPORT TIE AT APPROXIMATELY FS319 AND STR 17R, CORROSION ON SUPPORT TIE. (MARKED) (C-CHECK RO 3-25-22) : REMOVED CORROSION OF SUPPORT TIE AT APPROX FS319 AND STGR 17R REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW SUPPORT TIE AT FS319 STGR17R REF. CRJ 200 SRM 51-42-21 & DGW: 601R38303 REV. AR. COMPLIED WITH TASK CARD 51-900-1003-SKY.
* THE LH SIDE SEAT TRACK FROM APPROX FS364 TO FS409+16 HAS MULTIPLE LOCATIONS OF CORROSION.(MARKED) (C-CHECK RO 3-25-22) REMOVED AND REPLACED LH SIDE SEAT TRACK FROM FS364 TO FS409+16 REF CRJ200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802 TORQUE SCREWDRIVER# TUC7826 DUE 31MAR22.
*SERVICE DOOR HAS SEVERAL AREAS OF CHAFF DAMAGE ON EXTERIOR SKIN AROUND DOOR HANDLE (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE AT SERVICE DOOR ON EXTERIOR SKIN AROUND DOOR HANDLE PER REF CRJ200 SRM 51-12-00. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-52-41-479 REV -- DATE 2022-02-01.
*IN MAIN CABIN, FLOOR BEAM FRAME TIE AT APPROXIMATELY FS310 & STR 17L, FRAME TIE HAS MULTIPLE AREAS OF CORROSION. (MARKED) (C-CHECK RO 3-25-22) REMOVED CORROSION AT MAIN CABIN FLOOR BEAM FRAME TIE APPROX. FS 310.00 AND STGR. 17L. AS REQUIRED REF: CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-53-21-3530 REV--, DATED 2022-02-07. COMPLIED WITH TASK CARD 51-900-1003-SKY.
R/H STAB CENTER ELEVATOR HINGE FITTING HAS CHAFE AREA @ LWR OTBD MOUNT AREA (C-CHECK RO 3-25-22) BLENDED R/H STAB CENTER ELEVATOR HINGE FITTING AT LWR OTBD MOUNT AREA REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-55-11-713 REV--, DATED 2022-02-09.
R/H STAB OTBD ELEVATOR HINGE FITTING HAS CHAFE AREA LWR SUPPORT (C-CHECK RO 3-25-22) BLENDED R/H STAB OTBD ELEVATOR HINGE FITTING LOWER SUPPORT IAW CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-55-11-713 REV-- DATE 2022-02-09.
*RH MLG TRUNNION STRAP HAS CORROSION AROUND SEVERAL OF THE FASTENER HEADS (MARKED) (C-CHECK RO 3-25-22) CORROSION BLENDED ON RH MLG TRUNNION STRAP HAS CORROSION AROUND FASTENER HEADS REF CRJ200 SRM 51-21-06. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-3572 REV. -- DATE: 2022-02-16. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. SEE CONTINUATION CARD FOR DETAILS.
*LH MLG TRUNNION STRAP HAS CORROSION AROUND SEVERAL OF THE FASTENER HEADS (MARKED) (C-CHECK RO 3-25-22) CORROSION BLENDED ON LH MLG TRUNNION STRAP HAS CORROSION AROUND FASTENER HEADS, WITH DIMENSIONS: L=11.00", W=1.5", THICKNESS REMAINING 0.200" +/- 0.010" TAPERED DOWN TO 0.120" +/- 0.010"; REPLACED AFFECTED HI-LITE FASTENERS AND COMPLIED WITH ALL APPLICABLE STEPS IAW REO 601R-57-21-3571 REV. -- DATE: 2022-02-16. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.
RH ELEVATOR INBD PCU FAILED BEARING BACKLASH CHECK (C-CHECK RO 3-25-22) REMOVE AND INSTALLED NEW HARDWARE TO INCLUDE: QTY1 SPHERICAL BALL, QTY1 BOLT, QTY2 WASHER, QTY1 BUSHING, QTY1 NUT AT RH INBOARD PCU REF. CRJ-200 AMM 27-33-01-400-803. COMPLIED WITH TASK CARD 27-900-1003-SKY. BACKLASH CHECCK GOOD.
LH ELEVATOR MIDDLE PCU FAILED BEARING BACKLASH CHECK (C-CHECK RO 3-25-22) REMOVE AND INSTALLED NEW HARDWAER 1EA BALL SPHERICAL, 1EA BOLT, 2 WASHERS, 1EA BUSHING NUT AND COTTER PIN AT L/H MIDDLE PCU REF,CRJ200 AMM 27-33-01-400-803. BACKLASH CHECK GOOD. COMPLIED WITH TASK CARD 27-900-1003-SKY.
LH ELEVATOR OTBD PCU FAILED BEARING BACKLASH CHECK (C-CHECK RO 3-25-22) REMOVED AND REPLACED L/H OTBD PCU WITH NEW HARDWAER 1EA BALL SPHERICAL, 1EA BOLT, 2 WASHERS, 1EA BUSHING NUT AND COTTER PIN REF,CRJ200 AMM 27-33-01-400-803 TUC 7832 CAL DUE DATE 02/28/2022. BACKLASH CHECK GOOD, OPS CHECK GOOD, RIG GOOD.COMPLIED WITH SKYWEST TASK CARD 27-900-1003-SKY.
RH ELEVATOR MIDDLE PCU FAILED BEARING BACKLASH CHECK (C-CHECK RO 3-25-22) REMOVE AND INSTALLED NEW HARDWARE TO INCLUDE: QTY1 SPHERICAL BALL, QTY1 BOLT, QTY2 WASHER, QTY1 BUSHING, QTY1 NUT. AT R/H MIDDLE PCU REF. CRJ-200 AMM 27-33-01-400-803. BACKLASH CHECK GOOD. COMPLIED WITH TASK CARD 27-900-1003-SKY.
UPPER PIONO HINGE ON TOP STEP #832ET HAS ELONGATED HOLES FOR ATTATCHMENT HARDWARE AND LOWER PIANO HINGE CRACKED AND DAMAGED. (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW UPPER AND LOWER PIANO HINGE ON STEP PANEL # 832ET REF CRJ200 SRM 51-42-06
RIGHT ENGINE FAIL (N1 /N2 DROP) APPROXIMATELY 600 AGL, HIGH ITT, LOUD LOW FREQUENCY VIBRATION. FO SIDE PFD AND MFD MULTIPLE DROP OFFS STOPPED AFTER INFLIGHT SHUTDOWN. NORMAL SINGLE ENGINE LANDING. (FILED CLOSED - FLIGHT 5092) PLEASE REFERENCE AML 806879THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24053839 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED THE R/H ENGINE ASSEMBLY IN REFERENCE TO THE CRJ-200 AMM 71-00-00 AND TASK CARD 71-900-1000-SKY. OPERATINAL CHECK AND LEAK CHECK OF THE R/H ENGINE IS PHENOMENAL AT THIS TIME. / CALIBRATED TOOLING / TORQUE WRENCH-#937-832-3322 S/N-#03051000087 DUE-10/22 / TORQUE WRENCH-#937-832-3322 S/N-#1206100093 DUE-10/22 / TORQUE WRENCH-#937-832-3322 S/N-#52004B DUE-06/22 / DYNOMETER-#937-832-3322 S/N-#E 23462 DUE-03/22"
REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 3-25-22) REMOVED AND REPLACED BUSHINGS ON L/H AILERON WING AFT SPAR, REF. CRJ-200 AMM 20-26-00-910-804. SEE CONTINUATION FOR WORK PERFORMED.
REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 3-25-22) REMOVED AND REPLACED WITH NEW 8EA BUSHINGS FROM THE RH AILERON REAR SPAR HINGE POINTS REF CRJ 200 AMM 20-26-00-910-802 , CRJ200 AMM 20-26-00-910-803 AND CRJ-200 AMM 20-26-00-943-003.
D:GEAR UP DISAGREE COMPLIED WITH QRH 13-3 DIVERTED TO LAX. MAIN GEAR INDICATED UNSAFE UNTIL COMPLETION OF 13-3. LANDING UNEVENTFUL. DEFERRED LANDING GEAR RETRACTION SYSTEM IN ACCORDANCE WITH MEL 32-30-1. COMPLIED WITH MAINTENANCE ACTIONS. INSTALLED AND SAFETY WIRED LANDING GEAR LOCKPINS IN ACCORDANCE WITH AMM 10-11-00. DOWNGRADED CAT II STATUS PER GMM 2-23. / C: MEL 32-30-1 / CAT: A DUE 30OCT21 / *** DUE TO ODI EVENT, AIRCRAFT REQUIRES SMOD APPROVAL TO RTS / ***ODI EVENT. SMOD APPROVAL REQUIRED PRIOT TO RETURN TO SERVICE*** / ******CAT II NOT AUTHORIZED****** (FLIGHT 5326 - FILED CLOSED) OCT 30, 2021 STATION: LAX--DEFERRED LANDING GEAR RETRACTION SYSTEM IN ACCORDANCE WITH MEL 32-30-1. COMPLIED WITH MAINTENANCE ACTIONS. INSTALLED AND SAFETY WIRED LANDING GEAR LOCKPINS IN ACCORDANCE WITH AMM 10-11-00. DOWNGRADED CAT II STATUS PER GMM 2-23. / NOV 01, 2021 STATION: FAT -- REF CP 23747559 FOR TROUBLESHOOTING AND REPLACEMENT OF THE MLG SELECTOR VALVE. CP 23747810 FOR INSPECTION/RIGGING CHECK OF THE UPLOCKS. CP 23747802 AND CP 23748493 FOR PSEU REPLACEMENT AND OPS CHECK. COMPLIED WITH MIP 34-220-1021-SKY CAT II RETURN TO SERVICE TEST. CAT II UPGRADED. RETURN TO SERVICE AUTHORIZED.
RTF- GEAR DISAGREE WARNING FOR NOSEGEAR NOT RETRACTING. IT MADE NO MOTION, BUT MAIN GEAR BOTH CAME UP. HYD 3 CAUTION MESSAGE POSSIBLY ASSOCIATED AFTER RUNNING QRH WITH BOTH HYDRAULIC SYSTEM 3 PUMPS ON (FLIGHT 5507 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 23139055 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP23143423 FOR CORRECTIVE ACTION."
FLOOR MEMBER FS 280.00 HAS A CRACK IN LOWER SIDE AT LBL 9 COMMON TO FLOOR POST. (C-CHECK) RO 01/07/2020 PERFORMED PERMANENT REPAIR TO F.S.280 WEB BETWEEN LBL20.75 AND RBL20.75 IN REF REO. ALL STEPS COMPLETED AT THIS TIME, STRUCTURAL MAJOR REPAIR COMPLETE. SEE CONTINUATION CARD FOR DETAILS.
STRINGER 25 LH CORRODED BETWEEN FS 294.00 TO FS 310.00 (C-CHECK) RO 01/07/2020 PERFORMED STRINGER SPLICE REPAIR TO STGR25 LH FROM FS280-FS240, REF BOMBARDIER REO AND PER BOMBARIDER DWG. COMPLIED WITH TASK CARD
TCAS ANTENNA DOUBLER PLATE BETWEEN FS295.00 - FS310.00 AND BETWEEN STGR27 - STGR26R CORRODED, MARKED, (INSIDE FUSELAGE) (C-CHECK) RO 01/07/2020 EVALUATED ANTENNA DOUBLER PLATE BETWEEN FS 295.00 TO FS 310.00 AND STR 27 TO STR 26 RH FOUND TO BE OUT OF LIMITS MATERIAL LOSS IS 100% REF CRJ 200 SRM. REMOVED ANTENNA DOUBLER REF CRJ 200 SRM. INSTALLED NEW ANTENA DOUBLER PER REF: DWG # 601R31022 REV. B AND CRJ 200 SRM TCAS DOUBLER P/N 601R31022-27. OPERATIONAL AND PRESSURE LEAK CHECKS GOOD. REFERENCE THE CONTINUE CARD FOR DETAILS.
STRINGER 26 LH CORRODED BETWEEN FS 295.00 TO FS 310.00 (C-CHECK) RO 01/07/2020 REOMVED AND REPLACED STRINGER 26 LH. REF CRJ200 SRM BOMBARDIER DWG. NO LEAKS NOTED.
HORIZONTAL STABILIZER STEADY FITTING BOLT NUMBER 2 RHS AS REFERENCED IN REO LOOSE. COMPLETED REPAIR FOR ELONGATED HOLES IN V-STAB STEADY FITTING REF REO. PERFORMED GAP CHECK BETWEN V-SATB STEADY FITTING AND SLIDER BLOCK REF REO, GAP CHECK GOOD. GAP CHECK GOOD. THIS SDR FOR T/STEADY FITTING IS BEING SUBMITTED AS A PART OF VDR_2020NM064006.
STRINGER 27 CORRODED BETWEEN FS 349.00 AND 333.00 (C-CHECK) RO 01/07/2020 PERFORMED STRINGER REPAIR ON STGR27 BETWEEN FS280 - FS364 REF BOMBARDIER DWG, CRJ-200 SRM. COMPLIED WITH TASK CARD.
INTERCOSTAL BETWEEN FRAMES FS364.00 AND FS349.00 AND BETWEEN STRGRS. 27 TO 26L COMMON TO SKIN HAS CORROSION. (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM INTERCOSTAL BETWEEN FRAMES FS364.00 AND FS349.00 AND BETWEEN STRGRS. 27 AND 26L AND COMMON TO LOWER SKIN REF: CRJ200 SRM. EVALUATED BLENDS ORGINAL .080 REMOVED .002 REMAINING .078 FOUND TO BE OUT OF LIMITS DUE TO THE FACT MORE THEN 30% OF THE INTERCOSTAL IS DAMAGE REF CRJ 200 SRM. REMOVED INTERCOSTAL BETWEEN FS 364.00 TO FS 349.00 AND BETWEEN STR 27 AND 26 LH REF CRJ 200 SRM.- INSTALLED NEW INTERCOSTAL BETWEEN FS 364.00 TO 349.00 BETWEEN STR 27 AND 26 LH REF CRJ 200 SRM. RESTORED FINISH AND CIC. REFERENCE THE CONTINUE CARD FOR DETAILS. NO LEAKS NOTED.
L/H AND R/H FITTINGS P/N 601R38343-2,-3 COMMON TO FRAME FWD. SIDE FS. 364.00 STRGR.26L AND 26R HAVE CORROSION (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM LH & RH FITTINGS P/N 601R38343-2, -3 COMMON TO FRAME FWD SIDE SIDE FS354.00 STGR 26L AND 26R REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO DAMAGE NOT ALLOWED REF CRJ 200 SRM. REMOVED CORRODED FITTINGS AND INSTALLED NEW FITTINGS 2EA. P/N 601R38343-1 REF CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.
SUSPECT CRACK FOUND ON LOWER FRAME FLANGE AT FS605.00 AND O/B OF STGR 24L. (MARKED) (C-CHECK) RO 01/07/2020 REMOVED AND REPLACED FRAME AT FS605.00 P/N 601R36026-27R. PER BOMBARDIER DWG 601R36026 REV AF AND REF CRJ200 SRM. NO LEAKS NOTED. COMPLIED WITH SKYWEST TASK CARD.
* PASSENGER DOOR HINGE HALF ON THE FUSELAGE HAS ALL LUG LANDS CHAFED DUE TO CONTACT WITH DOOR SIDE HINGE HALF LUGS. ALL LUGS ALSO HAVE ELONGATED HOLES. (C-CHECK) RO 01/07/2020 REMOVED PAX DOOR FUSELAGE HINGE REF. CRJ 200 SRM. INSTALLED THE NEW PAX DOOR FUSELAGE HINGE REF. CRJ 200 SRM. BOMBARDIER DWG AND REF. BOMBARDIER REO. OPERATIONAL CHECKS GOOD.
* L/H FLIGHT SPOILER OBD PCU LOWER ATTACHMENT BOLT HAS CORRODED NUT AND IS MISSING COTTER PIN. (C-CHECK) RO 01/07/2020 REMOVED AND INSTALLED NEW LH WING ATTACHING HARDWARE @ FLIGHT SPOILER OTBD PCU TO REAR SPAR REF CRJ200 AMM. PERFORMED OPERATIONAL TEST OF FLILGHT SPOILERS REF CRJ200 AMM. OPERATIONAL TEST GOOD, NO FAULT NOTED.
CARGO SEAT TRACK AT LBL9, FS559+112 - FS570.00 HAS CORROSION (C-CHECK) RO 01/07/2020 CARGO SEAT TRACK AT LBL9, FS559+112 - FS570.00 FOUND TO BE OUT OF LIMITS REF CRJ200 SRM. INSTALLED NEW SEAT TRACK PER BOMBARDIER REO. ALL STEPS COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS.
AVIONICS BAY FS333.00 FWD AND AFT SIDE FRAME CORRODED BETWEEN STGR26L - STGR26R, MARKED (C-CHECK) RO 01/07/2020 BLENDED CORROSION. OUT OF LIMITS. REPLACED FS333 FRAME SECTOR WITH NEW FRAME REF CRJ-200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD
AVIONICS BAY FS349.00 FWD AND AFT SIDE FRAME CORRODED BETWEEN STGR26L - STGR25R, MARKED (C-CHECK) RO 01/07/2020 REPLACED FS349 FRAME SECTOR WITH NEW FRAME SECTORE REF CRJ-200 SRM AND DWG. COMPLIED WITH TASK CARD
FLOOR BEAM STRAP AT FS589.00 BETWEEN LBL9 AND LBL27 CORRODED, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION IN REF CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM. MEASURED THICKNESS .088" ORIGINAL THICKNESS .100". MATERAL LOSS .012" MAX ALLOWED .010". REMOVED AND REPLACED FLOOR BEAM STRAP IN REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.
RH FLOOR STRAP AT FS559.00 AFT OF PRESSURE FLOOR SILL CORRODED, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM RH FLOOR STRAP AT FS559.00 AFT OF PRESSURE FLOOR SILL REF CRJ200 SRM. ORIGINAL MATERIAL THICKNESS RH OUTBOARD FLOOR SUPPORT STRAP AT FS559 .050", REFERENCE CRJ200 SRM. MINIMUM REMAINING THICKNESS .044". DEPTH REMOVED .006". MINIMUM ALLOWED .045" (.050"X10%=.005", .050"-.005"=.045") REFERENCE CRJ200 SRM. CORROSION REMOVAL IS NOT ALLOWABLE AND NOT WITHIN LIMITS. REMOVED AND REPLACED STRAP WITH (1) NEW STRAP PN # 601R31025-29. REF BOMBARDIER DRAWING & CRJ200 SRM. COMPLIED WITH SKYWEST TASK CARD. LEAK CHECK GOOD
FLOOR SEAT RAIL, RBL9 AT FS559.00 - FS559+80 HAS MULTIPLE AREAS OF CORROSION (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON CARGO SEAT TRACK AT RBL9 FS559.00 - FS559.00+80 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS REF CRJ200 SRM AND BSM.TOOL #7498 CAL DUE 31-DEC-19. REMOVED CARGO SEAT TRACK AT RBL9 FS559.00- FS559.00+80 REF CRJ200 AMM. FABRICATED INSTALLED NEW SEAT TRACK USING N126-2075, PO# T51210, AS WELL AS APPLIED FINISH AND ID'D PER BOMBARDIER REO. ALL STEPS COMPLIED WITH.
FLOOR SEAT RAIL, LBL9 AT FS559.00 - FS559+80 HAS MULTIPLE AREAS OF CORROSION (C-CHECK) RO 01/07/2020 REMOVED CORROSION FLOOR SEAT RAIL SECTION LBL9 FS559 TO FS599+80, REFERENCE CRJ200 SRM. CORROISON REMOVAL NOT WITHIN LIMITS, REFERENCE CRJ200 SRM. REMOVED AND REPLACED WITH NEW (FABRICATED) SEAT TRACK SECTION CRJ200 AMM. REPLACEMENT SEAT RAIL SECTION FABRICATED REFERENCING REO.
CARGO SEAT TRACK AT RBL9, FS559+112 - FS570.00 HAS CORROSION (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON CARGO SEAT TRACK AT RBL9 FS559+112 - FS570.00 REF CRJ200 SRM. ORIGINAL THICKNESS IS 0.110", REMAINING THICKNESS IS 0.87" MATERIAL LOSS IS 0.023" MAXIMUM ALLOWABLE MATERIAL LOSS IS 0.020Ãâ¬? FOUND TO BE OUT OF LIMITS REF CRJ200 SRM AND BSM. TOOL #7498 CAL DUE 31-DEC-19. REMOVED CARGO SEAT TRACK AT RBL9 FS559+112 - FS570.00 REF CRJ200 AMM. FABRICATED AND INSTALLED NEW SEAT TRACK USING N126-2075, PO# T51210, AS WELL AS APPLIED FINISH AND ID'D PER BOMBARDIER REO. ALL STEPS COMPLIED WITH.
AVIONICS BAY FS310.00 FWD AND AFT SIDE FRAME CORRODED BETWEEN STGR25L - STGR25R, MARKED (C-CHECK) RO 01/07/2020 BLENDED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED NEW LOWER FRAME SECTOR FS310.00 REF CRJ-200 SRM AND BOMBARDIER. COMPLIED WITH TASK CARD.
TOP OTBD CORNER OF FLOOR BEAM NEXT TO RH SIDE SILL AT FS349.00 CORRODED, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON TOP OUTBOARD CORNER OF FLOOR BEAM RH AT FS 349.00 AND FOUND TO BE OUT OF LIMITS. REPAIRED PER REO. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR DETAILS.
FUSELAGE DENT LOCATED NEAR UPPER FLANGE OF STGR24L AT 3.50" AFT OF FS 202.75 CANNOT BE DRESSED-BACK TO ORIGINAL COUNTOUR REFERENCING REO AS IT GOES INTO NON-MILLED SKIN UNDER, OR COMMON TO, STGR24L. (C-CHECK) RO 01/07/2020 PERFORMED PATCH REPAIR TO FUSELAGE DENT LOCATED FS 202.75 NEAR STGR24L REF BOMBARDIER REO. COMPLIED WITH TASK CARD.
RIGHT SIDE FLOOR SILL ANGLE AT FS319.00 HAS CORROSION, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION OH RH SIDE FLOOR SILL ANGLE AT FS319.00 REF CRJ 200 SRM. EVALUATED AND FOUND FLOOR SILL OUT OF LIMITS, REF CRJ 200 SRM. REPLACED RH SIDE FLOOR SILL ANGLE WITH NEW ANGLE P/N 601R31148-79 REF BOMBARDIER DWG, CRJ 200 SRM. SEE CONTINUSTION CARD FOR DETAILS. COMPLETED SKYWEST TASKCARD.
TOP OF INTERCOSTAL CORRODED AT STGR21L BEWTEEN FS333.00 AND FS349.00, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM TOP OF INTERCOSTAL AT STR 21 LH BETWEEN FS 333.00-349.00 REF CRJ 200 SRM. ORIGINAL MATERIAL THICKNESS IS 0.063" REF BOMBARDIER DWG. MINIMUM REMAINING THICKNESS IS 0.048" FOR A LOSS OF 0.015" FOUND TO BE OUT OF ALLOWABLE LIMITS REF CRJ200 SRM. INSTALLED REPLACEMENT INTERCOSTAL BETWEEN FS333.00 AND FS349.00 AT STR 21L REF: BOMBARDIER DWG, CRJ200 SRM.
AFT COCKPIT FLOOR SUPPORT ANGLE CORRODED AT FS280.00 (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM AFT FLOOR SUPPORT ANGLE AT F.S.280.00 IN REF CRJ200 SRM. MEASURED DEPTH OF BLEND OUT AT .028" WITH MICROMETER: TUC3939, DUE: 30-APR-20. ORIGINAL MATERIAL THICKNESS .040", MATERIAL LOSS OF .012" AND REMAINING MATERIAL THICKNESS OF .028" IS OUT OF THE 10% LIMIT, REF.CRJ-200 SRM. REMOVED AND REPLACED PART IN REF DWG, CRJ200 SRM. STRUCTURAL MAJOR REPAIR COMPLET. SEE CONTINUATION CARD FOR DETAILS.
FS280.00 BEAM BETWEEN RBL9 AND LBL9 CORRODED ACROSS THE TOP, MARKED (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON TOP OF FS280.00 BEAM (FLOOR ANGLE) BETWEEN RBL9 AND LBL9, FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW F.S.280.00 BEAM FILLER ANGLE P/N 600-34017-595 BETWEEN APPROX LBL20.75 AND RBL 20.75 IN REF DWG, CRJ200 SRM. SEE CONTINUATION FOR DETAILS. COMPLIED WITH TAST CARD.
RIGHT FLOOR SEAT RAIL FROM FS364.00 TO FS401.00 CORRODED MULTIPLE AREAS (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM FLOOR SEAT RAIL FROM RH SIDE FS364.00 TO FS401.00 REF CRJ200. FOUND TO BE OUT OF LIMITS REF CRJ200 SRM AND BSM. FABRICATED NEW SEAT TRACK REF REO. INSTALLED SEAT TRACK RAIL FROM FS364.00 TO FS401.00 REF CRJ200 AMM. SEE CONTINUE CARD FOR DETAILS.
LEFT FLOOR SEAT RAIL FROM FS364.00 TO FS401.00 CORRODED MULTIPLE AREAS (C-CHECK) RO 01/07/2020 REMOVED CORROSION FROM FLOOR SEAT RAIL FROM FS364.00 TO FS401.00 ON L/H SIDE REF CRJ 200 SRM FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK USING N126-2075, PO# T51210, AS WELL AS APPLIED FINISH AND ID'D PER BOMBARDIER REO. INSTALLED FLOOR SEAT TRACK FROM FS 364.00 TO FS 401.00 ON LH SIDE TOOL # TUC8606 CAL 28-OCT-2019 DUE 31-OCT-2020 REF CRJ 200 SRM
RIGHT FLOOR SEAT RAIL FROM FS401.00 TO FS409+128 CORROSION IN MULTIPLE AREAS (C-CHECK) RO 01/07/2020 REMOVED CORROSION ON CARGO SEAT TRACK AT RBL9 FS559+112 - FS570.00 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS REF CRJ200 SRM (TOOL #8544 CAL DUE 30-SEP-20). REMOVED CARGO SEAT TRACK AT RBL9 FS401.00- FS409+128 REF CRJ200 AMM. FABRICATED NEW REPLACEMENT SEAT TRACK, MATERIAL I.D. N126-2075, PO# T51210, AND INSTALLED TRACK REFERENCE BOMBARDIER REO. ALL STEPS COMPLIED WITH.
* L/H PRESSURE FLOOR SILL PANEL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 409.00 + 128 AND FS 559.00. (C-CHECK) RO 01/07/2020 PERFORMED THE REPAIRS ON THE LH PRESSURE FLOOR SILL PANEL BETWEEN FS 409.00 + 128 AND FS 559.00. REF BOMBARDIER REO AND REO.
*PAX DOOR SIIL FS349.00 AFT IS CORRODED. FLAGGED (C-CHECK) RO 01/07/2020 BLENDED PAX DOOR SILL FROM FS 349.00 TO FS 409.00+5.00 REF CRJ200 SRM. FOUND BLENDED AREA TO BE OUT OF LIMITS REF REO AND DWG. REMOVED AND REPLACED FLOOR SILL SECTION WITH NEW SILL SECTION REF BOMBARDIER DWG, CRJ-200 SRM. SEE CONTINUE CARD FOR DETAILS. COMPLETED SKYWEST TASKCARD.
*PAX DOOR AFT HANDLE RAIL CUP IS CORRODED. FLAGGED (C-CHECK) RO 01/07/2020 REMOVED AND REPLACED THE AFT HANDRAIL CUP WITH NEW LOCATED REF. CRJ 200 AND BOMBARDIER DWG. COMPLIED WITH SKY WEST M-337 FORM AND SKY WEST STRUCTURAL MAJOR REPAIR CARD.
*PAX DOOR LOWER SILL AREA IS CORRODED BETWEEN FS310.00 THROUGH FS349.00. FLAGGED (C-CHECK) RO 01/07/2020 REMOVED AND REPLACED THE LOWER ANGLE AT PAX DOOR FUSELAGE CUT OUT LOWER SILL AREA BETWEEN FS.310 AND FS.349 WITH NEW REF. CRJ 200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.
* R/H PRESSURE FLOOR SILL PANEL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 409.00 + 128 AND FS 559.00. (C-CHECK) RO 01/07/2020 REPAIRED THE R/H PRESSURE FLOOR SILL PANEL BETWEEN FS 409.00 + 128 AND FS 559.00. REF BOMBARDIER REO.
* LEFT HAND WING INBOARD GROUND SPOILER ACTUATOR HARDWARE IS CORRODED. (C-CHECK) RO 01/07/2020 REMOVED AND INSTALLED NEW ATTACHING HARDWARE ON LH WING INBD GROUND SPOILER PCU TO LINK REF CRJ200 AMM. / PERFORMED OPERATIONAL CHECK OF GROUND SPOILERS REF CRJ200 AMM; OPERATIONAL TEST GOOD, NO FAULTS FOUND.
* RIGHT HAND WING OUTBOARD GROUND SPOILER ACTUATOR HARDWARE IS CORRODED. (C-CHECK) RO 01/07/2020 REPLACED CORRODED RH GROUND SPOILER ACTUATOR HARDWARE REF CRJ200 AMM. PERFORMED OPERATIONAL TEST OF GROUND SPOILERS REF CRJ200 AMM. OPERATIONAL TEST GOOD, NO FAULT NOTED
* RIGHT HAND WING INBOARD GROUND SPOILER ACTUATOR HARDWARE IS CORRODED. (C-CHECK) RO 01/07/2020 REPLACED CORRODED NUT WASHER AND COTTER PIN WITH NEW HARDWARE. REF CRJ200. PERFORMED OPERATIONAL TEST OF GROUND SPOILERS REF CRJ200 AMM. OPERATIONAL TEST GOOD, NO FAULT NOTED
* LEFT HAND WING OUTBOARD GROUND SPOILER ACTUATOR HARDWARE IS CORRODED. (C-CHECK) RO 01/07/2020 REWMOVED AND INSTALLED NEW LH WING OTBD GROUND SPOILER ACTUATOR TOP ATTACHING HARDWARE @ PCU LINK TO SPOILER SURFACE REF CRJ200 AMM. PERFORMED OPERATIONAL TEST OF GROUND SPOILERS REF CRJ200 AMM. OPERATIONAL TEST GOOD, NO FAULT NOTED
* RIGHT HAND WING FLIGHT SPOILER INBOARD AND OUTBOARD HINGE BOLT KEEPER HARDWARE IS CORRODED. (C-CHECK) RO 01/07/2020 REMOVED AND INSTALLED NEW HARWARE ON R/H WING FLIGHT SPOILER INBOARD AND OUTBOAED HINGE BOLT KEEPERS (4EA BOLTS, 4EA WASHERS) REF CRJ 2OO SRM.
* RIGHT HAND WING SPOILERON INBOARD HINGE BOLT KEEPER HARDWARE IS CORRODED. (C-CHECK) RO 01/07/2020 REMOVED AND INSTALLED NEW HARWARE ON R/H WING SPOILERON INBOARD HINGE BOLT KEEPER (2EA BOLTS, 2EA WASHERS) REF CRJ 2OO SRM.
* ATTACH FITTING FOR FORWARD LOWER FUSELAGE FAIRING 193AB HAS CORRODED HARDWARE. (C-CHECK) RO 01/07/2020 REMOVED AND INSTALLED NEW, P/N NAS428-3A12, BOLT, MS21042-3, NUT & NAS73-3E015, BUSHING ON THE L/H O/B ATTACH FITTING FOR FORWARD LOWER FUSELAGE FAIRING 193AB. REMOVED, CLEANED AND REINSTALLED HARDWARE ON OTHER ATTACH FITTINGS (3EA) FOR FORWARD LOWER FUSELAGE FAIRING 193AB. REF. CRJ200 AMM. / TORQUE WRENCH TUC5656, CAL DUE 30-APR-20
CORROSION ON INTERCOSTAL INSIDE PAX DOOR BETWEEN FS327.763 AND FS338.90 AT DD6 ON TOP, BOTTOM FLANGE AND POSSIBLY THE BOTTOM ALLSO, MARKED (C-CHECK) RO 01/07/2020 CORROSION FOUND ON MULTIPLE ELEMENTS (FLANGE ELEMENT, WEB ELEMENT AND ATTACHMENT ELEMENT) THEREFORE FOUND OUT OF LIMITS IN REF CRJ200 SRM. REMOVED AND REPLACED PAX DOOR DD6 INTERCOSTAL P/N 601R318057-1S PO# T52166 IN REF DWG, CRJ200 SRM CRJ200 SRM. LEAK CHECK GOOD AT THIS TIME. TASK CARD COMPLETED. SEE CONTINUATION CARD FOR DETAILS. ALL OPS TESTS AND ADJUSTMENTS GOOD
LH INBD FLAP VANE OTBD CAP CHAFE, FLAGGED (C-CHECK) RO 01/07/2020 CHAFE ON L/H INBD FLAP VANE CAP̉‰OTBD SIDE FOUND TO BE OUT OF LIMITS REF. CRJ200 SRM, REMOVED OUT OF LIMITS VANE CAP REF. CRJ200 SRM, LOCATED, DRILLED FULL SIZE AND COUNTERSUNK ALL HOLES COMMON TO REPLACEMENT VANE CAP REF. CRJ200 SRM AND INSTALLED REPLACEMENT VANE CAP REF. BOMBARDIER DWG AND CRJ200 SRM. FILLET SEALED REPLACEMENT L/H INBD FLAP VANE CAP̉‰OTBD SIDE REF. CRJ200 SRM AND RESTORED FINISH REF. CRJ200 SRM.
LH INBD FLAP VANE MIDDLE CAP CHAFE, FLAGGED (C-CHECK) RO 01/07/2020 REMOVED AND REPLACED CHAFED LH INBD FLAP VANE MIDDLE CAP WITH NEW (P/N 601R14303-51S) WITH NEW FASTENERS, REF BOMBARDIER DWG AND CRJ200 SRM. / SKYCARD COMPLIED WITH IN ITS ENTIRITY.
COMPLY WITH SCHEDULED MAINTENANCE CODE: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7559, POSITION: COMPLIED WITH DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. / (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO).AND, MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE.
COMPLY WITH SCHEDULED MAINTENANCE CODE: RA47263-601R57-21-138 875AS-PR - LEFT WING HAS INDICATION OF CRACK AT WS 148.019 JUST O/B OF WING JACK POINT APPROX. 4 INCHES AND APPROX. 7.25 INCHES FORWARD OF TRAILING EDGE. COMPLIED WITH TEMPORARY REPAIR PER REO 601R57-21-138 REV A DATED 2003-03-17. PERMANENT REPAIR IS DUE IN 1 YEAR BY 3/21/2020., PART NUMBER: - , SERIAL NUMBER: 7559, POSITION: (C-CHECK) RO 01/07/2020 COMPLIED WITH PARAGRAPH (B) OF AD BY REPAIRING CRACK ON THE LEFT SIDE LOWER WING PLANK BEFORE FURTHER FLIGHT PER A METHOD APPROVED BY EITHER THE MANAGER, NEW YORK AIRCRAFT CERTIFICATION OFFICE (ACO), FAA; OR TRANSPORT CANADA CIVIL AVIATION (OR ITS DELEGATED AGENT). (SKYWEST HAS DETERMINED TO USE REO.) COMPLIED WITH PERMANENT REPAIR OF THE LEFT WING PLANK AT WS 148.019 BY INCORPORATING REO. COMPLIED WITH SKYWEST TASK CARD. SEE CONTINUATION CARD FOR DETAILS.
LT WING FLAP STUB FAIRING CHAFED. REMOVED AND REPLACED LT STUB FLAP FAIRING WITH NEW IAW AMM AND SRM.
RT WING FLAP STUB FAIRING CHAFED. REMOVED AND REPLACED RT STUB FLAP FAIRING WITH NEW IAW AMM AND SRM.
GEAR DISAGREE, PERFORMED GO AROUND. NOSE AND RT MAIN GEAR NOT SHOWING DOWN. RAN QRH AND GEAR CAME DOWN. LANDED WITHOUT INCIDENT. REPLACED PSEU IAW AMM. OPS CHECKED GOOD.
RIGHT FORWARD TRU BAY LANDING CRACKED, FS 193. REPAIRED CRACK ON RT FWD TRU BAY LANDING FS 193 IAW GREO.
AVIONICS BAY FWD FRAME AT FS 364 HAS CORROSION JUST ON FWD FACE OF FRAME. REPAIRED FRAME IAW EA. PERFORMED PRESSURIZATION LEAK CHECK IAW SRM. LEAK CHECK GOOD.
AVIONICS BAY, BELOW FLOORBOARD, IN BETWEEN FS 364.0 TO FS 349.0 INTERCOSTAL AT STR 27R, HAS CORROSION AT FLANGE. R & R INTERCOSTAL BETWEEN FS 349.00 AND 364.00, STR 27R IAW SRM. PERFORMED PRESSURIZATION LEAK CHECK IAW SRM. LEAK CHECK GOOD.
GEAR DISAGREE. LT MLG WASN`T COMING DOWN, RAN QRH ALL GEAR WENT DOWN. SECURED MLG SELECTOR VALVE CONNECTOR PLUG. SWUNG GEAR MULTIPLE TIMES NO FAULTS FOUND, EMERGENCY ALTERNATE EXTENSION WITH NO DEFECTS NOTED. OPS CHECKS GOOD IAW AMM.
CREW REPORTED LT MLG WOULD NOT COME DOWN DURING INITIAL TRY DURING APPROACH. CHANGED THE MLG SELECTOR VALVE AND THE SIDE STAY ACTUATOR. LEAK AND OPS CHECKED GOOD.
RETURNED TO FIELD. BOTH TRANSPONDERS FAILED IN FLIGHT. FOUND A LOOSE CONNECTOR, AND TIGHTENED.
EMERGENCY LIGHT HOUSING AND LENS AT THE FORWARD SERVICE DOOR ARE BROKEN. R & R EMERGENCY LIGHT HOUSING AND LENS IAW AMM.
DURING EXTENTION OF FLIGHT SPOILERS INFLIGHT, RECEIVED FLIGHT SPOILERS FAULT STATUS MESSAGE FOLLOWED BY SLIGHT UNCOMMANDED ROLL AND YAW. RESET SECU AND PERFORMED SPOILER OPS CHECK IAW AMM.
MULTIPLE LIGHTS INOPERATIVE INTERIOR REAR FWD/AFT FACING CEILING EMERGENCY EXIT AND RT/ LT EMERGENCY EXIT SIGNS. R & R ALL INOPERATIVE LIGHTS IN THE REAR FWD/AFT FACING CEILING EMERGENCY EXIT AND RT/ LT EMERGENCY EXIT SIGNS, OPS CHECK GOOD AT THIS TIME.
ON APPROACH, WHEN GEAR HANDLE PLACE IN DOWN POSITION RECEIVED GEAR DISAGREE WARNING. FLT 2909 INTERROGATED PSEU WITH NO FAULTS FOUND IAW AMM. PERFORMED VLV PRIORITY TEST IAW AMM WITH NO FAULTS FOUND. PERFORMED OPERATIONS TEST & FUNCTIONAL TEST OF PSEU IAW AMM WITH NO FAULTS FOUND. PERFORMED EMERGENCY EXTENSION WITH NO FAULTS FOUND IAW AMM. SWUNG LG MULTIPLE TIMES WITH NO FAULT FOUND.
RT APRON SKIN PANEL CHAFED COMMON TO WING UPPER SKIN SEAL. C-CHECK REPLACED RT APRON SKIN PANEL IAW STS EA & SRM.
RT BATT RIB AT WS 53.6 IS CRACKED AT UPPER RADIUS. C-CHECK REPAIRED RT BATT RIB AT WS 53.6 IAW REO.
LT MLG WW BATT RIB ASSEMBLY AT WS 53.6 HAS A CRACK ON UPPER AFT FLANGE. C-CHECK REPAIRED LT BATT RIB AT WS 53.6 IAW REO.
LT APRON SKIN PANEL CHAFED COMMON TO WING UPPER SKIN SEAL. C-CHECK REPLACED LT APRON SKIN PANEL IAW STS EA & SRM.
EVALUATE CORROSION ON LT PRESS FLOOR STRAP FS 559.00, LBL 37. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 559.00, LBL 37 STRAP IAW REO.
EVALUATE CORROSION ON RT PRESS FLOOR FS 475.00, RBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 475.00, RBL 42 FLOOR ANGLE IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 559.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 559.00, LBL 42 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 526.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 526.00, LBL 42 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 522.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 522.00, LBL 42 CHEM-MILLED AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 518.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 518.00, LBL 42 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 510.00, LBL 38. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 510.00, LBL 38 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 510.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 510.00, LBL 42 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 502.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 502.00, LBL 42 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 493.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 493.00, LBL 42 PAD UP AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 479.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 479.00, LBL 42 CHEM-MILLED AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 477.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 477.00, LBL 42 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 470.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 470.00, LBL 42 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 461.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 461.00, LBL 42 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 448.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 448.00, LBL 42 FLOOR ANGLE AREA IAW REO.
EVALUATE CORROSION ON LT PRESS FLOOR FS 441.00, LBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 441.00, LBL 42 CHEM-MILLED AREA IAW REO.
EVALUATE CORROSION ON RT PRESS FLOOR FS 501.00, RBL 42. C-CHECK BLENDED & EVALUATED REPAIR AREA AT FS 501.00, RBL 42 ON PAD UP AREA IAW REO.
GEAR DISAGREE WARNING UPON LANDING. RECYCLED GEAR & ALL INDICATIONS WERE NORMAL. RT MLG WAS THE REASON FOR THE GEAR DISAGREE. FLT 9458 FOUND MLG SELECTOR VLV CONNECTOR NOT FULLY ENGAGED ON VLV. CONNECTED CONNECTOR PROPERLY ON MLG SELECTOR VLV. SWING GEAR NO FAULTS FOUND.
INTERIOR RT OVERWING EMERGENCY EXIT LIGHT OUT. FLT 2921 RELAMPED.
NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 2965 RELAMPED.
GEAR DISAGREE WARNING MESSAGE WHEN GEAR SELECTED DOWN. RT MAIN TOOK LONGER THAN THE REST, GEAR CAME DOWN & MESSAGE CLEARED. FLT 2911 REPLACED NR 3 HYD RESERVOIR IAW AMM.
GEAR DISAGREE WARNING MESSAGE WHEN MLG DEPLOYED. LT MAIN DID NOT COME DOWN UNTIL AFTER 5 SECONDS & LOCKED INTO PLACE. FLT 2923 REPLACED MLG PRIORITY VALVE FOR TROUBLESHOOTING IAW AMM. SWUNG GEAR SEVERAL CYCLES. OPERATIONS CHECKED GOO. PN'S 4619-3 SN ON 1088B SN OFF 1490B
ON APPROACH RECEIVED A GEAR DISAGREE MASTER WARNING. THE LT MAIN WAS STILL SHOWING IN TRANSIT BUT THEN SHOWED DOWN & GREEN & THE MESSAGE WENT AWAY. FLT#2977 FREED STUCK UPLOCK ROLLER ON LT MAIN GEAR IAW AMM.
FIRST EMERGENCY OVERHEAD LIGHT BURNED OUT. FLT#2941 REPLACED NR 2 EMERGENCY OVERHEAD LIGHT.
GEAR DISAGREE. FLT#2902 PERFORMED PSEU SELF TEST & PASSED. TESTED ALL GEAR SENSORS WITH THE AIRCRAFT IN A GEAR DOWN & GEAR UP POSITION, ALL SENSORS GOOD. PERFORMED AN EMERGENCY EXTENSION OF THE LANDING GEAR SYSTEM. SWUNG THE GEAR WITH FLAPS AT 20, COULD NOT DUPLICATE FAULT. CHECK THE GAP AT THE GEAR WOW, UPLOCK & NLG DOOR SENSORS ALL GAPS ARE CORRECT. LANDING GEAR OPERATIONS CHECKED GOOD AT THIS TIME. NO FAULT FOUND.
RECEIVED A CARGO BOTTLE LOW CAUTION MESSAGE. FLT#2976 REPLACED SMALL CARGO BOTTLE IAW AMM. PN: 36500018-3, SN: 51708D1, SN OFF: 46535D, PN: 30903870, SN: 07303, SN OFF: 05972, PN: 30903870, SN: 07388, SN OFF: 05978
PASSENGER DOOR FORWARD COUNTERBALANCE ANCHOR FITTING IS CRACKED. C-CHECK REPLACED FORWARD COUNTERBALANCE ANCHOR FITTING IAW REO.
NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT, RELAMPED.
EMERGENCY OVERHEAD LIGHT AT ROW 9 BURNED OUT. (FLT 2980) RELAMPED EMERGENCY LIGHT.
FELT A BIG BANG - LEFT ENGINE N1 WENT TO 30 PERCENT AND ITT WAS AROUND 920ðC, SHUT DOWN THE LEFT ENGINE. (FLT 2958) REPLACED LEFT ENGINE IAW AMM P/N: CF34-3B1 S/N ON: 873869 S/N OFF: 873127 P/N: 755469E S/N ON: 1832/4738.
MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE. (FLT 2969) CLEANED AND LUBED UPPER LINKAGE ON MAIN CABIN DOOR.
NR 1 EMERGENCY OVERHEAD LIGHT IN CABIN BURNED OUT. (FLT 2934) RELAMPED EMERGENCY LIGHT.
CAPTAIN'S SIDE WINDOW CRACKED. (FLT 2982) REPLACED CAPTAIN'S SIDE WINDOW IN REFERENCE TO AMM. P/N: NP-139322-11 S/N OFF: 05297H5509.
LOUD NOISE FROM GALLEY SERVICE DOOR AND GALLEY SERVICE DOOR DIFFICULT TO OPEN AND CLOSE. (FLT 2979) REPLACED SERVICE DOOR RUBBER SEAL WITH A SERVICABLE UNIT PER AMM.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2954) RELAMPED EMERGENCY LIGHT.
ALL EMERGENCY LIGHTS ARE INOPERATIVE. (FLT 2956) REPLACED ALL EMERGENCY BATTERIES. P/N: AD-2013-1A S/N OFF: 77235, 70601, 71648, 81149.
NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2972) RELAMPED EMERGENCY LIGHT.
LEFT GEAR DISAGREE WHEN GEAR SELECTED UP. (FLT 2908) ADJUSTED LEFT MLG UPLOCK PROXIMITY SENSOR TARGET.
LEFT GEAR DISAGREE AFTER TAKEOFF. (FLT 2908) REPLACED LEFT SIDE STAY ACTUATOR AND LEFT MLG SELECTOR VALVE. P/N OFF: 750005000 S/N OFF: 0340 P/N OFF: 17008-115 S/N OFF: 01183.
(C-CHECK) RIGHT CENTER LEADING EDGE DAMAGED BETWEEN WS 158.52 AND 167.46. REPAIRED RIGHT CENTER LEADING EDGE BETWEEN WS 158.52 AND 167.46.
EMERGENCY LIGHT AT TOP OF AIRSTAIR ON LT BROKEN. R & R EMERGENCY LIGHT ASSY IAW AMM 33-51-10. OPS CHECKED GOOD.
FOUND 2 CRACKS ON THE LT SIDE OF L/E RIB AT WS58.00. (REF ISE-STR-11-080 REV NC DETAILED DAMAGE 6.9) PERFORMED ET INSPECTION OF AFFECTED AREA ON L/E RIB AT WS 58.00 IAW NDTM PART 1, 51-20-06. NO CRACKS NOTED AT THIS TIME. PERFORMED ET INSP OF AFFECTED AREA ON L/E RIB AT WS58.00 IAW NDTM PART 1, 51-20-06. NO CRACKS NOTED AT THIS TIME. 09-29-2011.
SKIN AND DOUBLER DAMAGED ON LT WING EXTENSION AND WINGLET. R & R SKIN IAW SRM 57-31-31, DWG NR 600-10380, AND REO 601R-57-31-1161.
FOUND LT WINGLET FRAMING STRUCTURES BENT/CHAFED/GOUGED DUE TO DIRECT CONTACT WITH RUNWAY. REPLACED DAMAGED RIBS AND ANGLES IAW DWGS 600-10382, AND 600-10384. REPAIRED GOUGES IAW SRM 51-12-00. REPLACED DAMAGED RIBS AND ANGLES IAW DWGS 600-10382, AND 600-10384. REPAIRED GOUGES IAW SRM 51-12-00.
GOUGES FOUND ON ALL FLAP HINGE BOXES IN VARIOUS LOCATIONS. REPAIRED GOUGES IAW SRM 51-12-00. 09-28-2011.
GOUGES FOUND ON FWD AND AFT WING FITTINGS FOR FLAP HINGE BOXES AND FLAP ACTUATORS (REF ISE-STR-11-080 REV NC, DETAILED DAMAGE 6.4.) REPAIRED GOUGES FOUND ON FWD AND AFT WING FITTINGS FOR FLAP HINGE BOXES AND FLAP ACTUATORS IAW SRM 51-12-00. REPAIRED GOUGES FOUND ON FWD AND AFT WING FITTINGS FOR FLAP HINGE BOXES AND FLAP ACTUATORS IAW SRM 51-12-00.
LT WING TIP FAIRING REMOVED DUE TO DAMAGE. R & R LT WING TIP FAIRING IAW AMM 57-30-01. REMOVED LT WING TIP FAIRING IAW AMM 57-30-01. REPLACED LT WING TIP FAIRING IAW AMM 57-30-01.
LEFT MLG DISAGREE ILLUMINATED. EMERGENCY DECLARED. R & R LT MLG UPLOCK ASSY WITH NEW HARDWARE IAW AMM 32-32-05. OPS AND LEAK CHECK GOOD.
RT SIDE EXIT EMERGENCY LIGHT MOST FWD IS INOP. RELAMPED RT SIDE EXIT EMERGENCY LIGHT MOST FWD, OPS CHK GOOD IAW AMM 33-51-00.
GEAR DISAGREE AFTER PUTTING THE GEAR HANDLE IN THE DOWN POSITION ON APPROACH. BOTH MAINS WERE NOT DOWN AND LOCKED. NOSE GEAR INDICATED DOWN AND LOCKED. FOLLOWED QRH. PULLED MANUAL GEAR EXTENSION RECEIVED 3 GREEN. EMERGENCY DECLARED - TOWER HAD EQUIPMENT STANDING BY AS A PRECAUTION. FLT 5534. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10, OPS CHECKED GOOD.
NR 6 (RIGHT SIDE) EXTERNAL EMEREGENCY LIGHT WILL NOT ILLUMINATE. R & R NR 6 EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-51-21. OPS CHECK GOOD.
(2) CEILING FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULBS IAW AMM 33-51-16 OPS CK GOOD
FOUND OVERHEAD EMERGENCY LIGHT BETWEEN SEATS 10AB AND 10CD DIM.
PASSENGER DOOR GOT STUCK CLOSED. IT OPENED AFTER SEVENTH OR EIGHTH ATTEMPT BUT IT STILL FELT LIKE IT WAS NOT FREE TO MOVE 100 PERCENT. ( PASSENGER DOOR POWER ASSIST SYS )
LEFT AND RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS AT THE FWD POSITION WILL NOT ILLUMINATE.
CENTER LIGHTED CEILING LIGHT EXIT SIGN AFT DIRECTION WILL NOT ILLUMINATE.
CARGO SEAT TRACK LBL 9.0 FS 615 IS CORRODED. REMOVED CORRODED SEAT TRACK FROM FS 615.00, LBL 9.00 AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-04.
SEAT TRACK RBL 9.0, 409+128 TO 559.0 HAS AN AREA OF CORROSION. REMOVED SEAT TRACK AND TRANSFERRED HOLE LOCATIONS ONTO NEW SEAT TRACK IAW MM 53-01-11-000-802, SRM 51-40-11. INSTALLED SEAT TRACK IAW SRM 51-41-02 PGS 1 AND 2 AND AMM 53-01-11-400-802.
CARGO BAY SEAT TRACK LBL 27.0 FS 559+84 TO 559+96 IS CORRODED. REMOVED & REPLACED CARGO BAY SEAT TRACK LBL 27.0 FS 559+84 TO FS 559.+96 IAW SRM 51-41-02.
PAX DOOR LOWER SILL LONGERON, ANGLE, AND BOTH HANDRAIL BRACKETS ARE CORRODED BEYOND REPAIRABLE LIMITS PER SRM 53-00-31. REMOVED LOWER SILL ANGLE AND FWD AND AFT HANDRAIL CLEATS IAW SRM 51-42-06, 51-42-13, 51-42-21. FABRICATED REPLACEMENT LOWER SILL IAW SRM 51-24-21, REF. DWG 601R31527. INSTALLED LOWER SILL IAW SRM 51-42-06, 51-42-11 AND 51-42-21. INSTALLED CLEATS & PRIMED AND PAINTED ALL REPAIR PARTS IAW SRM 51-42-11 & 51-25-00. OPS CHECK GOOD IAW MM 33-45-00-710-801, 52-11-08-710-802 AND 52-70-04-710-803.
CARGO BAY SEAT TRACK RBL 27.0 FS 559+84 TO 559+96 IS CORRODED. REMOVED & REPLACED CARGO BAY SEAT TRACK RBL 27.0 FS 559.+84 TO FS 559.+96 IAW SRM 51-41-02.
CARGO BAY SEAT TRACK FS 559+95 TO FS 567.0 RBL 9.0 IS CORRODED. REMOVED SEAT TRACK FS 559.95-FS 567.0 RBL 9.0 IAW CRJ 200 SRM 51-41-02. INSTALLED NEW TRACK IAW SRM 51-41-02.
CARGO BAY SEAT TRACK FS 559+95 TO FS 567 LBL 9.0 IS CORRODED. REMOVED DAMAGED SEAT TRACK FS 559+95 TO FS 567 LBL 9-0 IAW SRM 51-41-02. INSTALLED NEW SEAT TRACK IAW SMR 51-41-02.
CARGO SEAT TRACK FS 559+85 TO FS 559+96 LBL 9.0 IS CORRODED. REMOVED CARGO SEAT TRACK FS 559+85 TO FS 559+96 LBL 9.0 IAW SRM 51-41-02. SEAT TRACK NEEDS INSTALLED. INSTALLED CARGO SEAT TRACK IAW CRJ 200 SRM 51-41-02.
CARGO SEAT TRACK FS 559+85 TO FS 559+96 RBL 9.0 IS CORRODED. REMOVED CORRODED SEAT TRACK FROM FS 615.00, LBL 9.00 AND INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-41-04.
PAX DOOR INTERIOR "EXIT" PLACARD IS DETERIORATED.
REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS A INDICATION NOTED APPROX .2 INCH IN LENGTH 90 PERCENT FSH FAILED NDT INSP. REPAIRED PER EC/TC REO 601R-53-61-1230, C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.
CARGO DOOR SUPPORT BEAM LOWER BRACKET IS CRACKED APPROX .3 INCH IN LENGTH. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER BRACKET IAW SRM 51-42-21.
FS 409+128 VERTICAL POST BL 0.0 RT SIDE FWD FLANGE FIRST FASTENER AFT SIDE HAS A INDICATION NOTED APPROX .2 INCH IN LENGTH 100 PERCENT FSH FAILED NDT INSP. REMOVED DAMAGED VERTICAL POST AT FS 409+128 BL 0 PER SRM 51-42-06 AND 51-42-21. FABRICATED REPLACEMENT POST AND REINFORCEMENT ANGLE IAW SRM 51-24-21. REF DWG 601R32208. INSTALLED IAW EC/TC REO 601R-53-41-1056 AND SRM 51-42-06.
LBL 27.0 FLOORBEAM CAP CORRODED ON FLANGES AROUND NUT PLATE HOLES, FS 574.0 - FS 621. REMOVED AND REPLACED LBL 27.0 FLOORBEAM CAP AT FS 574-0 - FS 621 IAW SRM 51-42-06, 51-42-21, 51-42-22, AND 51-42-34. DISPOSITION FOR ALTERNATE FASTENERS FOR AFT FUSELAGE FLOORBEAM CAP INSTALLATION IS COMPLETED IAW REO 601R-53-61-3322 AND MEETS WITH ALL THE REQUIREMENTS OF REO 601R-53-61-3322 AND DRAWINGS NR 601R31030 AND 601R35031.
EMERGENCY EXIT LIGHT LENS CRACKED.
WHILE PERFORMING HFEC INSPECTION OF FS 559.00 BULKHEAD WEB AND CAP ANGLE, A 50% FSH INDICATION APPROX 0.5" IN LENGTH WAS NOTED ON THE WEB AT RBL 19.00 AND WL 59.10. FAILS NDT AT THIS TIME. C/W EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV C. REF CO 7559109 JOB 8755915/241 FOR FABRICATION OF REPAIR KIT PARTS.
FLOOR SUPPORT ANGLE AT FS 280 OUTBOARD SIDE OF RBL 9 IS CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-42-21. FABRICATED NEW ANGLE IAW REO 601R-53-11-171, STEP 9 AND EC/TC EO 600-53-90 C/W. INSTALLED NEW ANGLE PER REO 601R-53-11-171, EC/TC EO 600-53-90 C/W AND SRM 51-42-21.
PNL 232DZ EXIT SIGN HOUSING ASSY AND LENS CRACKED. REMOVED AND REPLACED EXIT SIGN HOUSING ASSY AND LENS IAW AMM 33-51-13-400-801. OPS TEST OF PNL 232DZ EXIT SIGN GOOD AT THIS TIME IAW AMM 33-51-00-76-801.
LEFT FS 621-625 INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL AT FS 621-625 AND INSTALLED SERVICEABLE INTERCOSTAL IAW SRM 51-42-21.
CO PILOT SIDE WINDOW FRONT SEAL UNSEATED. TOWER DECLARED AN EMERGENCY & PUT EMERGENCY VEHICLES ON STANDBY AS A PRECAUTION. REMOVED SPEED TAPE FROM F/O'S SIDE WINDOW IAW REO 601R-56-00-001
LOADED PASSENGER ON AIRCRAFT AND MAIN DOOR WON`T CLOSE. FLT 5224.
PAX DOOR WON'T CLOSE. FLT 5358 DEL 30 MINS.
FLT 4999 - RADIO ALTIMETER FAULT FOLLOWED BY GPWS FAIL, WINDSHEAR FAIL, TCAS FAIL, SPOILERONS FAULT, FLT SPOILERS FAULT, OTBD GND SPOILERS FAULT, INBD GND SPOILERS FAULT, EMERGENCY VEHICLES ROLLED AS A PRECAUTION.
SERVICE DOOR LATCH WILL NOT RELEASE DOOR TO CLOSE. C/N/D DOOR (SERVICE) WORKS PROPERLY NOT DEFECT FOUND AT THIS TIME OK FOR SERVICE. IAW 52-45-01.
LT 1ST EMERGENCY LIGHT ON FUSELAGE INOP.
PAX DOOR FWD ANCHOR FITTING IS CRACKED. REPAIRED IAW AMM 52-11-17, SRM 51-40-11, MM 52-11-17, AND MM 52-11-17. NO DEFECTS NOTED.
AAR - CRACKS ON FLOOR SILL AT FS 589 AND 605 UNDER FLOORBOARD 281 LLF IN CARGO BAY.
AAR - LEFT O/B CLIP AT FS 280 AND LBL 9.0 IS CRACKED. REMOVED LEFT O/B CLIP AT FS 280 AND LBL 9.0 AND INSTALLED NEW CLIP P/N 601R31113-57 IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 09/12/07.
AAR - LEFT I/B CLIP AT FS 280 AND LBL 9.0 IS CRACKED. REMOVED LEFT I/B CLIP AT FS 280 AT LBL 9.0 AND INSTALLED NEW SERVICEABLE CLIP P/N 601R31113-57 IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 9/12/07.
AAR - CLIP CRACKED AT FS 484, RBL 27 OUTBOARD.
AAR - CLIP CRACKED AT FS 484, LBL 36 INBOARD.
AAR - WEB DOOR CUT OUT HAS A CRACKED CLIP ON LEFT CENTER SIDE AT FS 700. REPAIRED IAW CRJ 200 SRM 53-61-23.
AAR - UPPER WEB OF ENGINE BEAM, APPROXIMATELY CENTERED IN AFT EDGE AT MARKED RIVET, SUSPECT A CRACK. REPAIRED IAW EO 600-53-0169.
AAR - RIGHT I/B CLIP AT FS 280 AND RBL 9.0 IS CRACKED. REMOVED RIGHT I/B CLIP AT FS 280 AND RBL 9.0. INSTALLED NEW SERVICEABLE CLIP P/N 601R31113-58 IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 09/12/07.
AAR - FS 280 AFT FLOOR ANGLE 600-34017-595 IS CRACKED AT LBL 9.0 AND RBL 9.0. COMPLIED WITH REO 601R-53-11-136. 14031 9-8-07. REPAIRED J-ANGLE ON THE PILOT'S BULKHEAD AT FS 280.0 FROM LBL 9.0 TO RBL 9.0 IAW ASA EO 600-53-0091. SUPPLEMENTAL - SDR CLOSED 09/14/07.
AAR - RIGHT O/B CLIP AT FS 280 AND RBL 9.0 IS CRACKED. REMOVED RIGHT O/B CLIP AT FS 280 AT RBL 9.0. FABRICATED NEW CLIP FROM S6144-4 AND INSTALLED SERVICEABLE CLIP IAW REO 601R-53-11-171. SUPPLEMENTAL - SDR CLOSED 09/14/07.
AAR - FS 280 BULKHEAD HAS CRACK AT RBL 12.0 JUST ABOVE LOWER ANGLE RADIUS. COMPLIED WITH REO 601R-53-11-171. REPAIRED PILOTS BULKHEAD AT FS 280 FROM LBL 9.0 TO RBL 9.0 IAW ASA EO 600-53-0090. 13341. SUPPLEMENTAL - SDR CLOSED 09/14/07.
AAR - BATH TUB FITTING CRACKED AT FS 472, RBL 9 OUTBOARD. REPAIRED IAW CRJ 200 SRM 51-40-11.
AAR - CLIP CRACKED AT FS 484, RBL 36 INBOARD.
SERVICE DOOR WILL NOT CLOSE.
SERVICE DOOR WON'T CLOSE PROPERLY.
AFTER TAKEOFF, RECEIVED A WING OVERHEAT WARNING MSG, CYCLES CONTINUOUSLY. RETURNED TO ATL. REPEAT WRITE-UP. EMERGENCY DECLARED. FLT 4257 CX.
RIGHT ENGINE OIL PRESSURE FLUX. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLTS 4084, 4401 CX.
LEFT SIDE FS 640 DOUBLER CRACKED. REPAIRED LT SIDE FR 640 IAW SRM (CLOSED 11/01/06).
FOUND RT SIDE FS 640 DOUBLER CRACKED. CW RT SIDE FS 640 REPAIR IAW S.B 601R-53-061 (CLOSED 11/01/06).
FOUND CAPT'S FLASHLIGHT DIM.
DURING CLIMB OUT, ON GEAR RETRACTION, THE CREW RECEIVED A STEERING INOPERATIVE MESSAGE FOLLOWED BY A GEAR DISAGREE WARNING. THE EICAS INDICATED THE MAIN GEAR RETRACTED AND THE NOSE POSITION WAS NOT INDICATING. THE CREW COMPLIED WITH THE QRH AND MANUALLY EXTENDED THE GEAR. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED, WHERE A SAFE LANDING WAS PERFORMED. MAINTENANCE REMOVED AND REPLACED THE NLG PRIORITY VALVE AND RIGGED THE FEEDBACK RVDT`S. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
DURING CLIMB OUT, THE CREW RECEIVED A GEAR DISAGREE MESSAGE. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO DEPARTURE, WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR SELECTOR VALVE ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)
DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR OUTER HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR OUTER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT ANGLE, ABOVE THE ASSIST PULLEY, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR AFT ANGLE, ABOVE ASSIST PULLEY, IAW REO 601R-52-11-513. (K)
DURING A GROUND INSPECTION IN ATL, THE SERVICE DOOR WAS FOUND DIFFICULT TO OPEN. MAINTENANCE RIGGED THE SERVICE DOOR AND ADJUSTED THE CENTER INTERNAL STABILIZER ROD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
FLT 4447 - DURING CRUISE FROM ATL-VPS, AT APPROXIMATELY 30,000 FEET, THERE WAS AN ILLUMINATING GLOW FROM THE ANTI-ICE VEIN, FOLLOWED BY A LOUD SHATTERING OF THE NR 2 WINDSHIELD. THE CREW COMPLIED WITH THE QRH AND DIVERTED INTO MGM, AFTER DECLARING AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN MGM. MAINTENANCE REMOVED AND REPLACED THE NR 2 WINDSHIELD IAW CRJ AMM 56-11-01. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
FLT 4508 - DURING CLIMB-OUT FROM TUP-ATL, AT APPROX 18,000-19,000 FT, THE CREW RECEIVED AN INTERMITTENT ENG OIL PRESSURE AURAL AND A R ENG OIL PRESSURE WARNING FOR APPROXIMATELY TEN SECONDS. IT THEN WENT OUT AND REOCCURRED THREE TIMES WITH THE OIL PRESSURE FLUCTUATING FROM 32-75 PSI. THE CREW LEVELED THE AIRCRAFT OFF AND MOVED THE RIGHT ENGINE POWER LEVER TO IDLE AND THE OIL PRESSURE STABILIZED BETWEEN 32-38 PSI. THE QRH HAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT PERFORMED A SINGLE ENGINE LANDING SAFELY INTO ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE HYDRAULIC PUMP AND STARTER CARBON SEALS, RUNNERS, PACKINGS AND O-RINGS. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SER
DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY FLASHLIGHT. OPERATIONAL CHECKS GOOD. (M)
STARTER CARBON SEAL, WORN. (K)
DURING CLIMB OUT, CREW NOTICED FLUCTUATION IN RT ENG OIL PRESS OF 45-80 PSI WITH ALL OTHER INSTRUMENTS INDICATING NORMAL. AS CLIMB OUT PROGRESSED, OIL PRESS FLUCTUATIONS BEGAN DROPPING TOWARD 25 PSI ACCOMPANIED BY RT ENG OIL PRESS MESSAGE. QRH WAS COMPLIED WITH AND PWR LEVER REDUCED TO IDLE, STABILIZING OIL PRESSURE AT 27-32 PSI. CREW SHUTDOWN RT ENG AND DECLARED AN EMERGENCY. AC RETURNED AND LANDED SAFELY. INSP LUBE SYST AND TIGHTENED LINE TO OIL PRESS TRANSDUCER, PRESS SWITCH. ALSO, CHANGED LUBE ELEMENT, FLUSHED OIL TANK AND SUP LINE, INSPECTED, CLEANED SCREEN FOR CHIP DETECTOR. OPS AND LEAK CHECK GOOD. AC WAS PLACED ON OIL CONSUMPTON CK FOR 5 DAYS. AC OK FOR SERVICE.
DURING A GROUND INSPECTION, THE MAIN PASSENGER DOOR WAS HARD TO CLOSE USING THE HANDLE. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.
DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT LATCH. THE PASSENGERS WERE DEPLANED AND THE AIRCRAFT REPOSITIONED ON THE RAMP. MAINTENANCE INSPECTED THE PASSENGER DOOR INTERNALLY AND EXTERNALLY. NO FAULTS OR DEFECTS WERE FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.
DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT LATCH. MAINTENANCE REPOSITIONED THE PASSENGER DOOR CONNECTOR HARNESS AND TRIMMED EXCESS HEAT SHRINK OFF THE WIRE HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.
DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT LATCH FROM THE INSIDE. MAINTENANCE ADJUSTED THE LOWER FORWARD PIN STOP FITTING IAW THE AMM 52-11-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.
FLT 4612 - DURING A GROUND INSPECTION IN VPS, THE EMERGENCY EXIT SIGN AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN LAMP AT THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M)
DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP ACTUATING ROD WAS FOUND BROKEN FROM THE BOTTOM STEP. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT SIGN COVER AT ROW 11 A/B WAS FOUND MISSING. MAINTENANCE LOCATED THE MISSING EMERGENCY EXIT SIGN COVER AND RE-INSTALLED IT AT ROW 11 A/B. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
DURING A SCHEDULED INSPECTION, THE RIGHT EXTERNAL EMERGENCY LIGHT AFT OF THE WING WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNT OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.