N918SW
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
Maintenance disclosures
GEAR DISAGREE WARNING ON TAKEOFF NOSE SHOWED UP AND MAIN GEAR SHOWED DN. ALL GEAR CAME DOWN WITH QRHC: MEL 32-30-1CAT A DUE DATE IS 06/19/2026 SMOD APPROVAL REQUIRED BEFORE RELEASE DUE TO GEAR DISAGREE WARNING "ODI"REF EAML 1916880 (FLIGHT 6055). DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL 32-30-1.
D: FLAP FAIL EVENTC: AD 2009-06-12/10, CREW RESETFULL FLAP AD EVALUATION DUE WITHIN 10 CYCLES DUE 40040 TACFLAP FAIL AT ZERO DEGREES.AT 3000 FT SPEED 195KTS. (FLIGHT 3915) RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL AD COMPLIANCE BY MCC.
ON APPROACH FLAPS 8, FLAPS FAIL CAUTION MESSAGE DISPLAYED (FLIGHT 3360 FILED CLOSED)RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL COMPLIANCE BY MCC
ON APPROACH FLAPS 8, FLAPS FAIL CAUTION MESSAGE DISPLAYED (FLIGHT 3360 FILED CLOSED)RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL COMPLIANCE BY MCC
FLAPS FAIL CAUTION ON APPROACH, WHEN ATTEMPTING TO SET 30 DEGREES FLAPS, FLAPS FAILED AT 20 DEGREES. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26117469 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED THE FLAP CONTROL LEVER IAW CRJ 200 AMM 27-51-01. OPS CHECK GOOD AT THIS TIME. REF CP26117663-1 FOR AD COMPLIANCE."
FOUND LT FLOOR SSUPPORT NR 10 BLEND-OUT, OUT OF LIMITS. PERFORMED A REPAIR TO PRESSURE FLOOR SUPPORT BETWEEN BS 484 - 499, LHS AND PERFORMED REO 601R-53-41-3101, REV -. PRESSURE CHECK GOOD.
FLOOR SILL AT PAX DOOR FWD HANDRAIL CAP HAS INTERGRANULAR CORROSION AND REQUIRES REPLACEMENT. REMOVED AND INSTALLED NEW PAX DOOR FWD HANDRAIL CAP IAW SRM 51-42-06, AND DWG 601R31527, REV AM.
PAX DOOR SILL AFT HANDRAIL CAP BRACKET BETWEEN FS 333.00 TO FS349.00 HAS CORROSION REMOVED AND REPLACED HANDRAIL CUP BRACKET AND CLEAT IAW SRM 51-42-06, 51-45-00, AND DWG 601R31527, REV AM.
PAX DOOR SILL FWD HANDRAIL CAP BRACKET BETWEEN FS 310.00 TO FS319.70 HAS CORROSION. REPLACED PAX DOOR SILL FWD HANDRAIL CAP BRACKET IAW SRM 51-42-06, DWG 601R-31527, REV AM.
FRAME BS 319 HAD MULTIPLE SPOTS OF CORROSION FROM STR 25L TO STR 26. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R32003, REV P. PRESSURE CHECKS GOOD.
R/H FLOOR SILL ANGLE FROM FS310.00 TO FS319.70 HAS AREAS OF CORROSION. REMOVED AND REPLACED THE FLOOR SILL ANGLES WITH NEW IAW SRM 51-42-06, 51-42-13, DWG 601R31148, REV Y.
FRAME BS 310 HAD MULTIPLE SPOTS OF CORROSION FROM S24L TO S24R. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R32002 REV AD.
FORWARD KEEL BEAM PRESSURE BOX, UPPER STIFFENER WAS DENTED WITH POSSIBLE CRACK. EVALUATED DENT ON FORWARD KEEL BEAM PRESSURE BOX, UPPER STIFFENER OUT OF LIMITS. REMOVED AND INSTALLED A NEW FORWARD KEEL BEAM PRESSURE BOX, STIFFENER IAW SRM 51-42-06, SRM 51-23-00, SRM 51-42-21, DWG 601R31060, REV F, AND REO 601R-53-31-1252 REV-. NO LEAKS NOTED.
RIGHT PRESSURE FLOOR SILL FROM BS 409 - 559 HADS AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-21-06. FOUND PARTS TO BE OUT OF LIMITS. COMPLIED WITH ALL STEPS OF REO 601R-53-41-666 REV-C, DISPOSITION 1.2, AND REO 601R-53-41-3102 REV--, NO LEAKS NOTED.
TWO ANGLES FOR INTERCOSTAL AT BS 484 BETWEEN RBL 27 AND RBL 36 ARE CRACKED. REMOVED AND INSTALLED NEW ANGLES IAW SRM 51-42-06, SRM 51-42-21 AND DWG 601R31171, REV B. NO LEAKS NOTED.
SUPPORT FITTING FOR LBL27 FLOOR BEAM AT FS460 HAS A POSSIBLE CRACK. NDT VERIFIED CRACK ON SUPPORT FITTING . REMOVED AND INSTALLED A NEW SUPPORT FITTING WITH REPLACEMENT FASTENERS IAW SRM 51-42-21, AND DWG 600-31143, REV E. NO LEAKS NOTED.
LEFT PRESSURE FLOOR SILL FROM BS409+128 - 559 HAD AREAS OF CORROSION. BLENDED OUT CORROSION AND FOUND AREAS TO BE OUT OF LIMITS. COMPLIED WITH ALL STEPS OF REO'S 601R-53-41-666 REV-C AND REO 601R-53-41-3102 REV-. NO LEAKS NOTED. PERFORMED REPAIR ON BLEND-OUT LOCATION 10.
CORROSION NOTED ON FRAME BS 605 BETWEEN S25R-23L. FOUND OUT OF LIMITS. REMOVED AND INSTALLED A NEW LOWER FRAME IAW DWG 601R36026, REV AF, DWG 601R35005 REV Y, SRM 51-42-06, AND SRM 51-42-21. NO LEAKS NOTED.
TWO ANGLES FOR INTERCOSTAL AT BS 484 BETWEEN FLOORBEAM LBL 27 AND LBL 36 WERE CRACKED. REMOVED AND INSALLED THE TWO ANGLES IAW DWG 601R31171, REV B, AND SRM 51-42-21. NO LEAKS NOTED
PAX DOOR CLEAT COMMON TO FS320.163 FORMER AND MID LWR CHANNEL CORRODED. REMOVED AND REPLACED THE PAX DOOR CLEAT IAW DWG 601R31702, REV N, AND SRM 51-42-06.
CRACKED FRAME FS 235.00 BETWEEN STRINGERS 11-12R. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-06, DWG 601R34032, REV V, AND REO 601R-53-11-3810, REV-. PRESSURE CHECKED GOOD.
CRACK ON FRAME BS 235 BETWEEN STRINGERS 11-12L. REMOVED AND INSTALLED A NEW ANGLE IAW SRM 51-42-06, AND DWG 601R34032, REV -V. PRESSURE CHECKS GOOD.
UPON REMOVAL OF LEFT HAND COLLECTOR TANK WATER DRAIN VALVE NOTICED TWO WASHERS UNDER WATER DRAIN VALVE FASTENERS ON WING PLANK SIDE. UPON REMOVAL OF THE WASHERS IDENTIFIED THAT THE LEFT HAND COLLECTOR TANK WATER DRAIN VALVE FASTENER HOLES TWO EACH ARE ELONGATED. PERFORMED REPAIR ON LH COLLECTOR TANK WATER DRAIN SCREW HOLES REF REO 601R-57-21-3660 REV-. NO LEAKS NOTED.
REPAIR DAMAGED UPPER SKIN ON R/H ELEVATOR INBOARD AFT TRAILING EDGE. PERMEANNTLY REPAIRED RT ELAVATOR INBD AFT EDGE IAW SRM 55-20-00.
LEFT MAIN LANDING GEAR WHEEL WELL, BRAKE HYDRAULIC FUSE AFT BRACKET IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06 AND DWG 601R75278 REV-G. NO LEAKS NOTED
LEFT MAIN LANDING GEAR WHEEL WELL, BRAKE HYDRAULIC FUSE FORWARD BRACKET IS CRACKED. REMOVED THE LT MAIN LANDING GEAR WHEEL WELL, HYDRAULIC FUSE FWD BRACKET IAW SRM 51-42-06, INSTALLED A NEW BRACKET IAW SRM 51-42-06 AND DWG 601R75278 REV-G. LEAK CHECK GOOD
UPON REMOVAL FOR BEARING REPLACEMENT, FOUND LT ELEVATOR L/E HINGE FITTING ASSY HAVE PITTING CORROSION IN BEARING BORES OF BOTH HINGE HALVES. REMOVED AND REPLACED THE LT ELEVATOR NR 1 HINGE FITTING ASSY WITH NEW HINGE FITTING ASSY IAW DWG 601R24025, REV G, SRM 51-42-06, AND 51-42-21.
UPON REMOVAL, FOUND RT ELEVATOR L/E HINGE FITTING ASSY TO BE EXCESSIVELY WORN AT BEARING LOCATION. REPLACE HINGE FITTING ASSY IAW DWG 601R24025, REV G, SRM 51-42-06, AND 51-42-21
SMALL DENT ON TOP OF AFT FUSELAGE BETWEEN BS 559+112 AND 574, BETWEEN STR 0 AND STR 1R. COMPLIED WITH PERMANENT REPAIR IAW REO 601R-53-61-7912, REV -., PRESSURE CHECK GOOD.
LEFT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET CRACKED IN TWO PLACES. REMOVED AND INSTALLED A NEW BRACKET IAW SRM 51-42-06, AND DWG 601R31146, REV J. PRESSURE CHECKS GOOD.
RIGHT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER BRACKET CRACKED & BROKEN IN TWO PLACES. REMOVED AND INSTALLED A NEW BRACKET IAW SRM 51-42-06 AND DWG 601R31146 REV J, PRESSURE CHECKS GOOD.
PAX DOOR DD3 AFT INTERCOSTAL CORRODED. REMOVED AND INSTALLED NEW DD3 INTERCOSTAL IAW DWG 601R31702, REV: N, AND SRM 51-42-06. PRESSURE CHECKS GOOD.
PAX DOOR DD4 AFT INTERCOSTAL CORRODED. PAX DOOR DD4 AFT INTERCOSTAL OUT OF LIMITS. REMOVED AND INSTALLED NEW DD4 AFT INTERCOSTAL IAW DWG 601R31702, REV N AND SRM 51-42-06. NO LEAKS NOTED.
PAX DOOR DD3 MID INTERCOSTAL CORRODED. REMOVED AND INSTALLED PAX DOOR DD3 MID INTERCOSTAL IAW SRM 51-42-06 , SRM 51-42-21 AND DWG 601R31702, REV N. PRESSURE CHECKS GOOD
PAX DOOR DD4 MID INTERCOSTAL CORRODED. REMOVED AND INSTALLED PAX DOOR DD4 MID INTERCOSTAL IAW SRM 51-42-06 , SRM 51-42-21 AND DWG 601R31702, REV N. CHECKED GOOD.
PAX DOOR DD6 MID CLEAT COMMON TO FS329.76 FORMER CORRODED. REMOVED AND REPLACED PAX DOOR DD6 MID CLEAT COMMON TO BS 329.76 FORMER IAW DWG 601R31702, REV. N AND SRM 51-42-06.
PAX DOOR DD6 MID INTERCOSTAL CORRODED. PAX DOOR DD6 INTERCOSTAL OUT OF LIMITS. REMOVED AND INSTALLED NEW DD6 INTERCOSTAL IAW DWG 601R31702 REV: N, SRM 51-42-06, SRM 51-42-21. NO LEAKS NOTED.
PAX DOOR CLEAT COMMON TO FS320.163 FRAME AND MID LWR CHANNEL CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT COMMON TO FS320.163 FRAME AND MID LWR CHANNEL IAW DWG 601R31702REV. N AND SRM 51-42-06.
PAX DOOR CLEAT ON DD4 FWD COMMON TO FS313.56 FRAME CORRODED. REMOVED AND REPLACED PAX DOOR CLEAT ON DD4 FWD COMMON TO FS313.56 FRAME REF. DRWG 601R31702 REV. N AND SRM 51-42-06.
PAX DOOR FWD FORMER CORRODED. PAX DOOR FWD FORMER FOUND TO BE CORRODED OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER REF. DRWG 601R31702 REV. N, SRM 51-42-06 AND SRM 51-42-21. NO LEAKS NOTED.
PAX DOOR DD7 FWD INTERCOSTAL DENTED. REMOVED AND INSTALLED A NEW DD7 FWD INTERCOSTAL IN PASSENGER DOOR IAW DWG 601R31702, REV: N, SRM 51-42-06. PRESSURE CHECK GOOD
PAX DOOR DD1 AFT INTERCOSTAL DENTED. PAX DOOR DD1 AFT INTERCOSTAL OUT OF LIMITS. REMOVED AND INSTALLED NEW DD1 INTERCOSTAL IAW DWG 601R31702, REV: N, AND SRM 51-42-06. NO LEAKS NOTED.
PAX DOOR AFT FORMER CORRODED. REMOVED AND INSTALLED NEW AFT FORMER IAW SRM 51-42-06, SRM 51-42-21, AND DWG 601R31702, REV N. PRESSURE CHECK GOOD.
LEFT INBOARD FLAP, INBOARD HINGE ARM, INBOARD GUIDE PLATE IS CHAFED. INSTALLED A NEW INBOARD HINGE ARM ,INBD GUIDE PLATE IAW SRM 51-42-06 AND DWG 601R14116, REV H.
LEFT INBOARD FLAP, OUTBOARD HINGE ARM, INBOARD GUIDE PLATE IS CHAFED. REPLACED INBOARD GUIDE PLATE AT LT INBOARD FLAP, OUTBOARD HINGE ARM IAW SRM 51-42-06 AND DWG 601R14116 REV H.
LEFT INBD FLAP VANE HAS CHAFING ON LEADING EDGE AT MID LOCATION AT APPROXIMATELY WS 104.099. (C-CHECK) REMOVED AND INSTALLED NEW LT INBD FLAP VANE CAP, LEADING EDGE MID LOCATION PER DWG 601R14303, REV J AND SRM 51-42-13.
PAX DOOR PIANO HINGE (FUSELAGE SIDE) HAS NUMEROUS ELONGATED HINGE PIN HOLES (C-CHECK) REMOVED AND INSTALLED NEW PAX DOOR HINGE HALF IAW SRM 53-21-23 STEPS 4. R-V AND REO 601R-53-21-656 REV A. NO LEAKS NOTED.
LEFT INBD FLAP VANE HAS CHAFING ON LEADING EDGE AT INBD LOCATION AT APPROXIMATELY WS 56.30. (C-CHECK) UPON BLENDING LT INBD FLAP VANE IB LOCATION, MATERIAL LOSS AT 100%, THROUGH PART AND REQUIRES REPLACEMENT IAW SRM 51-12-00. REMOVED BAD VANE CAP IAW SRM 51-42-10. LOCATE HOLES IN REPLACEMENT CAP IAW SRM 51-42-10. INSTALLED REPLACEMENT VANE CAP IAW SRM 51-42-13, REV 39, AND DWG 601R14302, REV E. COMPLETED CARD 51-900-1003.
REMOVE AND REPLACE PAX DOOR INNER SKIN DUE TO CRACKED. REMOVED AND REPLACED PAX DOOR INNER SKIN IAW SRM 51-42-06, SRM 51-42-10, SRM 51-42-21, AND SRM 51-42-22.
LEFT AILERON LOWER FWD EDGE HAS 3 SPOTS THAT ARE CHAFED. (C-CHECK) BLENDED CHAFING ON LT AILERON LOWER FWD LEADING EDGE SKINS IAW SRM 51-12-00, TWO AREAS FOUND IN LIMITS IAW SRM 57-60-00 AND LOCATION AILS 370 TO 375 FOUND OUT OF LIMITS, REPLACED WITH NEW SKIN IAW SRM 51-42-06 AND SRM 51-42-21 AND DWG CC670-13000 REV D. COMPLIED WITH CARD 51-900-1003. MAJOR REPAIR.
REINSTALL RT AILERON PER AMM IAW AMM 27-15-01-000-801. COMPLY WITH TASK CARD 27-900-1001-SKY (C-CHECK RO 12/17/2022) REMOVED AND REINSTALLED THE RH AILERON WITH NEW HARDWARE - REF CRJ 200 AMM 27-15-01-400-801. RIGGING, BONDING AND OPERATIONAL TESTS ARE GOOD. COMPLIED WITH SKYWEST TASK CARD 27-900-1001-SKY.
REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RT AILERON WING AFT SPAR IAW AMM 20-26-00-910-804. REMOVED, INSTALLED AND SEALED A NEW SERVICEABLE RT AILERON BUSHINGS ON WING AFT SPAR AMM 20-26-00-910-804.
CLIMBING UP, PRESSURE WAS GOOD THEN RECEIVED A OVERBOARD COOL CAUTION MESSAGE AND A INBOARD COOL FAIL STATUS MESSAGE. RAN QRH, PRESSURE WAS STILL GOOD. THEN, CONTINUED ENROUTE CLIMB TO DEN, CABIN RATE AND CABIN ALT WAS INCREASING. RECEIVED CABIN ALT CAUTION ALONG WITH CABIN ALT WARNING. RAN QRC, DECLARED EMERGENCY AND TURNED BACK TO GTF. PAX MASK WERE DEPLOYED, WAS NOT AN OVERWEIGHT LANDING, VSI LESS THAN 100 FT PER MIN, AND CURRENT CREW O2 IS AT 1140. FOUND TO BE THE OVERBOAD EXHAUST SOV TO BE FAULTY. PRESSURIZED AIRCRAFT AS REQUIRED, PER MEL. CABIN HELP PRESSURE. NO OVERWEIGHT LANDING OR HARD LANDING NOTED, REF AML 522207 FOR OVERBOARD COOL CAUTION AND INBOARD COOL STATUS MESSAGE MEL, REF AML 522227 FOR SERVICE CREW OXY SYS. REM AML 522229 FOR DEFERRING PAX OXY SYS MEL.
FS 559 LBL FLOOR STRAP AT PRESSURE FLOOR SILL CORRODED. (C-CHECK) RO: 02/23/2019 REMOVED AND REPLACED THE FS559 LBL27 FLOOR STRAP AT PRESSURE FLOOR SILL IAW SRM. LEAK CHECKS GOOD.
CARGO DOOR SILL CORRODED FROM FS 579 TO FS620. (C-CHECK) RO: 02/23/2019 REMOVED AND REPLACED CARGO DOOR SILL AT FS 579.000-FS620.00 IAW SRM.
REPLACE THE RH INBOARD FLAP LEADING EDGE, INBOARD CAP. (C-CHECK) RO: 02/23/2019 REMOVED AND REPLACED RH INBOARD FLAP LEADING EDGE, INBOARD CAP IAW SRM.
FRETTING DAMAGE ON THE INTERNAL AVIONICS BAY DOOR CUT-OUT SURROUND. (C-CHECK) RO: 02/23/2019 BLENDED INTERNAL AVIONICS BAY DOOR CUT-OUT SURROUND TO A SMOOTH CONTOUR IAW REO.
RH AILERON UPPER LEADING EDGE CHAFED ALONG ENTIRE LENGTH. (C-CHECK) RO: 02/23/2019 REMOVED AND REPLACED RH AILERON LE EDGE SKIN WITH NEW IAW SRM AND REO.
FUSELAGE SKIN DENTED AT APPROX FS627 BETWEEN STR27 AND STR26R. (C-CHECK) RO: 02/23/2019 DRESSED BACK FUSELAGE SKIN DENT AT APPROX. FS627 BETWEEN STR27 AND STR26R TO ORIGINAL CONTOUR IAW REO. NO FURTHER DEFECTS NOTED.
SERVICE DOOR HINGE HAS CHAFING DAMAGE. (C-CHECK) RO: 02/23/2019 BLENDED CHAFFED AREAS ON SERVICE DOOR HINGE. COMPLIED WITH ALL STEPS IAW REO.
GUSSET ON FS310.00 FRAME STGR13L IS CORRODED. (C-CHECK) RO: 02/23/2019 REMOVED AND INSTALLED NEW GUSSET P/N 600-31109-57 IAW SRM.
FS349 FRAME, STGR25L TO STGR25R, ON BOTH FORWARD AND AFT SIDE IS CORRODED. (C-CHECK) RO: 02/23/2019 REMOVED AND INSTALLED THE NEW BOTTOM FRAMES SECTION AT FS349.00 BETWEEN STGR25L AND STGR25R. IAW SRM.
RH WING LOWER SKIN DENT, RHWS377 - 1.5 INCHES FWD OF AFT EDGE OF SKIN. (C-CHECK) RO: 02/23/2019 COMPLIED WITH ALL APPLICABLE STEPS IAW REO.
LH INBD FLAP VANE UPPER SKIN TRAILING EDGE CHAFED 5 INCHES OTBD OF INBOARD END. (C-CHECK) RO: 02/23/2019 BLENDED CHAFE ON THE LH INBD FLAP VANE UPPR SKIN TRAILING EDGE IAW REO.
FLAPS FAIL MESSAGE AT CRUISE. FAILED IN 0 POSITION. (FLT 5311) FO: 07/31/2018 CLOSED. RESET AND OPERATED FLAPS. OK TO CONTINUE SERVICE FOR 10 FLIGHT CYCLES. C/W FIM.
FRETTING ON THE UPPER FUSELAGE WHERE THE ADF ANTENNA CONTACTS THE AIRCRAFT. (C-CHECK) RO: 02/09/2017 COMPLIED WITH ALL STEPS OF REO.
PAX DOOR AFT WEB HAS CORROSION UNDER PANEL 832HR. COMPILED WITH REO.
PAX DOOR ACCESS PANEL 832AR HAS CORROSION AROUND FASTNER HOLES. REPLACED THE ACCESS PANEL IAW SRM.
DOOR PANEL 832HL HAS CORROSION AROUND FASTNER HOLES.REPLACED THE PANEL IAW SRM.
DOOR PANEL 832GR HAS CORROSION AROUND FASTNER HOLES. REPLACED PANEL IAW SRM.
PAX DOOR ACCESS PANEL 832AL HAS CORROSION AROUND FASTNER HOLES. REPLACED THE ACCESS PANEL IAW SRM.
LEFT WING INBOARD GROUND SPOILER DENTED. REPAIRED IAW REO.
DENT ON LOWER RIGHT CORNER FOR CARGO DOOR. COMPLIED WITH REO.
RIGHT PACK FAILED FOLLOWED QRH, DESCENDED TO 25FL THEN LT PACK FAILED, LOST PRESSURIZATION. DIVERTED. DECLARED AN EMERGENCY AND DEPLOYED OXYGEN MASKS. CLEANED CABIN TEMPERATURE SENSOR FAN IAW AMM. RAN BOTH PACKS, WITH ENGINES AND PRESSURIZED A/C IAW AMM. OPS CHECK GOOD NO FAULTS FOUND.
RT WING FUEL PANEL CUTOUT FOR PANEL 650FB HAS PITTING ON LOWER BONDING SURFACE. C-CHECK, RO 2/28/15. PITTING, FRETTING CORROSION, UNDER FUEL PANEL 650FB, HOLE NR 14 AT WS 274.319 WAS BLENDED MORE THAN 50 PERCENT OF THE HATCH AREA AND ALSO IN THE CRITICAL AREAS. NDT ENSURED A CRACK FREE CONDITION. ORIGINAL THICKNESS AROUND THE HOLE VARIED FROM .185"? TO .192"?. MINIMUM REMAINING MATERIAL THICKNESS WAS .184"?. MINIMIM ALLOWABLE THICKNESS WITHOUT REPEAT INSPECTION IS .182"?. MATERIAL LOSS RANGED FROM.001"? TO .002"?. BLENDED AREAS WITHIN LIMITS. BLENDED AREA WAS ROTO PEENED. REF FOR BLENDING AND LIMITS: REO. ADDITION ENGINEERING FOR BLENDING MORE THAN 50 PERCENT OF HATCH AREA AND WITHIN THE CRITICAL AREAS: REO STATES BLEND IS ACCEPTABLE AS IS, AS LONG AS MEETING ALL OTHER REQUIREMENTS OF REO.
RT WING FUEL PANEL CUTOUT FOR PANEL 650EB HAS PITTING ON LOWER BONDING SURFACE. C-CHECK, RO 2/28/15. PITTING, FRETTING CORROSION, UNDER FUEL PANEL 650EB, HOLE NR 13 AT WS 253.022 WAS BLENDED MORE THAN 50 PERCENT OF THE HATCH AREA AND ALSO IN THE CRITICAL AREAS. NDT ENSURED A CRACK FREE CONDITION. ORIGINAL THICKNESS AROUND THE HOLE VARIED FROM .188"? TO .192"?. MINIMUM REMAINING MATERIAL THICKNESS WAS .187"?. MINIMIM ALLOWABLE THICKNESS WITHOUT REPEAT INSPECTION IS .182"?. MATERIAL LOSS RANGED FROM.001"? TO .002"?. BLENDED AREAS WITHIN LIMITS. BLENDED AREA WAS ROTO PEENED. REFERENCE FOR BLENDING AND LIMITS: REO. ADDITION ENGINEERING FOR BLENDING MORE THAN 50 PERCENT OF HATCH AREA AND WITHIN THE CRITICAL AREAS: REO, STATES BLEND IS ACCEPTABLE AS IS, AS LONG AS MEETING ALL OTHER REQUIREMENTS OF REO.
FRAME AT STR 0-1L AND FS 333 HAS POSSIBLE CRACK AT TOOLING HOLE, MARKED. C-CHECK, RO 2/28/15. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER, PN; " EA 24-2015-55-1 DOUBLER", STS EA . ALL STEPS AND ITEMS COMPLIED WITH. COMPLIED WITH ST, WEIGHT OF PARTS, REMOVED 0.00 LBS. WEIGHT OF PARTS INSTALLED 0.02 LBS. NET WEIGHT GAIN 0.02LBS.
FS 333 FRAME, LOWER SECTION FORWARD OF AVIONICS BAY DOOR, SUSPECTED CORROSION ON FWD FACE BL 0-RBL15. BUBBLING PAINT, C-CHECK, RO 2/28/15. REPLACED LOWER SECTION FRAME AT FS 333, LBL15-RBL15, PN 601R32004-55, FWD OF AVIONICS BAY DOOR, REF SRM. COMPLIED WITH ST LEAK CHECK GOOD.
LEFT INBD FLAP VANE CENTER L/E CHAFED OUT OF LIMITS REF CAMP MAINTENANCE TRANS NR 11850984. C-CHECK 2/28/15, REMOVED LT INBD FLAP VANE CENTER L/E AND INSTALLED NEW CENTER L/E PN 601R14303-51, REF SRM. COMPLIED WITH ST.
PRESSURE FLOOR CRACKED AT FS 462 AND LBL 4.0 TO LBL 6.0, MARKED. (C-CHECK RO 2/28/15)REPAIRED PRESSURE FLOOR CRACKED AT FS 462 AND LBL 4.0 TO LBL 6.0, REF REO. NO LEAKS NOTED, COMPLIED WITH ST.
LEFT INBD FLAP VANE L/E HAS CHAFING AT THE INBD BUMPER LOCATION. C-CHECK, RO 2/28/15, BLENDED CHAFE DAMAGE ON THE LT INBD FLAP, INBD VANE CAP IAW REO. FOUND PART TO HAVE 100 PERCENT MATERIAL LOSS. R & R LT INBD FLAP, INBD VANE CAP REF SRM. VANE CAP FINISH WAS RESTORED ON JOB 2764575, OP 103, MX TRANS: 11880909.
LEFT INBD FLAP VANE L/E HAS CHAFING AT THE ONBD BUMPER LOCATION. C-CHECK, RO 2/28/15, LT INBD FLAP VANE L/E CHAFE AT THE OTBD BUMPER OUT OF LIMITS REF REO, REPLACED CAP REF SRM.
LEFT INBD FLAP VANE L/E HAS CHAFING AT THE CENTER BUMPER LOCATION. C-CHECK, RO 2/28/15, BLENDED LT INBD FLAP, FLAP VANE CENTER L/E SKIN REF REO, BLEND OUT OF LIMITS. REF CAMP MAINTENANCE TRANS 11857280 FOR REPLACEMENT OF LT INBD FLAP, FLAP VANE CENTER L/E SKIN .
ONE DENT LOCATED ON THE RT WING LOWER WING BOX EXTENSION. COMPLIED WITH TEMPORARY REPAIR IAW REO. PERMANENT REPAIR DUE WITHIN 1800 FLT HRS BY TAT: 34626.1. C-CHECK, RO 2/28/15. COMPLIED WITH PERMANENT REPAIR OF 1 DENT LOCATED ON THE RT WING LOWER WING BOX EXTENSION REF STS EA DENT WITHIN LIMITS.
RETURN TO THE FIELD WHEN A EICAS SCREEN WENT BLANK. REPLACED DISPLAY. CHECKED GOOD.
RT NR 4 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. R & R THE RT NR 4 EXTERIOR EMERGENCY LIGHTS IAW AMM.
FLIGHT DECK EMERGENCY LIGHT OFF LIGHT HAS TWO OUT OF FOUR BULBS INOPERATIVE. REPLACED THE ANNUNCIATOR LIGHT CAP. OPS CHECKED GOOD.
LT EXTERIOR NR 1 EMERGENCY LIGHT IS BURNED OUT. REPLACED LAMP.
DENT IN NOSE FUSELAGE BELOW CAPTAIN'S WINDOW BETWEEN BS 230 - 235, WL 110, S12L. REPAIRED IAW REO.
SLOW LOSS OF OIL PRESS IN FLIGHT. COMPLETED QRH PROCEDURE. IN FLIGHT ENGINE SHUTDOWN. FLT 5561 REPLACED HYD ENG DRIVEN PUMP, AIR TURBINE STARTER & IDG CARBON SEALS ON RT ENG. PERFORMED OIL CONSUMPTION CHECK IAW AMM.
CARGO DOOR SILL HAS CORROSION ON TOP SURFACE AT FS589. C-CHECK REPLACED IAW SRM & REO.
COCKPIT FLOOR BOARD AT FS 279.5 RBL 10 IS CRACKED. C-CHECK REPLACED COCKPIT FLOOR BOARD AFT FLOOR SUPPORT IAW SRM. PN 600-34017-351.
LT STRINGER 11A IS GOUGED & TORN. C-CHECK REPLACED IAW STS. PN 601R31018-45
LT 202 BULKHEAD AT PARKING BRAKE ROD LOCATION IS CRACKED. C-CHECK REPAIRED IAW REO.
CORROSION FOUND ON AIRCRAFT MAIN CABIN DOOR UNDER PANEL 832GL. C-CHECK REPAIRED IAW STS.
LEFT PACK HIGH PRESSURE WHEN THROTTLES ARE ADVANCED. (FLT 5322) PERFORMED OPERATIONAL CHECK OF LEFT ENGINE PRSOV AND LEFT PACK IAW AMM. NO FAULTS FOUND.
AT FLAPS 45 PLANE ROLLS UNCOMMANDED. (FLT 6450) REMOVED PAINT RUNS FROM ALL FOUR FLAP TRAILING EDGE UNDERSIDES AND UPPER LEADING EDGE SURFACES IN REFERENCE TO CRJ MM.
EMERGENCY EXIT SIGN AT 8 C/D IS INOPERATIVE. (FLT 6276) REPLACED EMERGENCY LIGHT POWER INVERTER NR 3 IAW AMM.
FLT 6242, NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6204) RELAMPED EMERGENCY LIGHT.
NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5914) RELAMPED EMERGENCY LIGHT.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6218) RELAMPED EMERGENCY LIGHT.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5384) RELAMPED EMERGENCY LIGHT.
AFT CEILING EMEREGENCY LIGHT IS OUT. (FLT 5483) RELAMPED EMERGENCY LIGHT.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5612) RELAMPED EMERGENCY LIGHT.
NR 1 AND NR 4 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. (FLT 6525) RELAMPED EMERGENCY LIGHTS.
LEFT INBOARD FLAP LOWER SKIN HAS A DENT. (C-CHECK) REPAIRED PER REO.
LEFT FS 559.0 PRESSURE BULKHEAD HAS DAMAGE. (C-CHECK) REPAIRED PER REO.
F/O SEATBELT DOESN'T RELEASE PROPERLY. (FLT 5441) REPLACED F/O'S BUCKLE ASSEMBLY.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6306) RELAMPED EMERGENCY LIGHT.
NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5347) RELAMPED EMERGENCY LIGHT.
LEFT CENTER OVERWING EMERGENCY LIGHT IS OUT. (FLT 5519) RELAMPED EMERGENCY LIGHT.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 6350) RELAMPED EMERGENCY LIGHT.
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6251) RELAMPED EMERGENCY LIGHT.
AFT SECTION OF FLOOR EMERGENCY LIGHTS ARE OUT. (FLT 6860) RECONNECTED WIRE ON AFT FLOOR EMERGENCY LIGHT.
CEILING EMERGENCY LIGHT IS OUT. (FLT 6552) RELAMPED EMERGENCY LIGHT.
LAST SEGMENT OF THE EMERGENCY LIGHT FLOOR STRIP IS NOT ILLUMINATING DURING TEST. (FLT 7022) RE-SECURED CONNECTOR ON AFT FLOOR STRIP LIGHT.
AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6565) RELAMPED EMERGENCY LIGHT.
NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6424) RELAMPED EMERGENCY LIGHT.
OVERHEAD EMERGENCY LIGHT AT ROW 13 IS OUT. (FLT 6917) RELAMPED EMERGENCY LIGHT.
LEFT EMERGENCY EXIT FORWARD EXTERIOR LIGHT IS OUT. (FLT 6262) RELAMPED EMERGENCY LIGHT.
SERVICE DOOR AFT EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6262) RELAMPED EMERGENCY LIGHT.
EMERGENCY LIGHT OVER ROW 2 IS OUT. (FLT 6472) RELAMPED EMERGENCY LIGHT.
NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6506) RELAMPED EMERGENCY LIGHT.
RIGHT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
NR 4 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
NR 2 CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6408) RELAMPED NR 2.
NR 4 EMERGENCY POD LIGHT INOPERATIVE. (FLT 6274) RELAMPED EMERGENCY LIGHT.
MOST AFT, INTERIOR EMERGENCY LIGHT INOPERATIVE. (FLT 6737) RELAMPED EMERGENCY LIGHT.
NR 1 EMERGENCY LIGHT INOPERATIVE. (FLT 6749) RELAMPED EMERGENCY LIGHT.
NR 4 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. (FLT 6655) RELAMPED EMERGENCY LIGHT.
LAST EMERGENCY CEILING LIGHT IS BURNT OUT. (FLT 6693) RELAMPED EMERGENCY LIGHT.
NR 1 CEILING EMERGENCY LIGHT INOP. (FLT 6816) RELAMPED EMERGENCY LIGHT.
PRESSURE BULKHEAD AT FS 559 CRACKED. (C CHECK) REPAIRED PER REO.
FS 621 AFT PRESSURE BULKHEAD WEB CRACKED AT LINTEL FITTING AND AT TOP OF AFT CARGO DOOR TRACK. (C CHECK) REPAIRED PER REO.
FS 621 FORWARD AFT PRESSURE BULKHEAD CRACKED AT SPLICE. (C CHECK) REPAIRED PER REO.
FS 621 PRESSURE BULKHEAD WEB CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.
FS 484 LEFT INTERCOSTAL CRACKED AT CABLE SUPPORT MOUNT BOLT HOLE. (C CHECK) REPAIRED PER SRM.
FS 621 PRESSURE BULKHEAD CRACKED AT SPLICE. (C CHECK) REPAIRED PER REO.
FS 621 FORWARD AFT PRESSURE BULKHEAD CRACKED AT TOP OF AFT CARGO DOOR TRACK. (C CHECK) REPAIRED PER REO.
FS 621 BULKHEAD CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.
CABIN OVERHEAD EMERGENCY LIGHT NR 2 INOP. (FLT 5778) RELAMPED EMERGENCY LIGHT.
EMERGENCY CEILING LEVEL LIGHT AT ROW 13 INOP. (FLT 6580)RELAMPED.
AFT MOST EMERGENCY CEILING FLOOD INOP. (FLT 6137) RELAMPED EMERGENCY LIGHT.
EMERGENCY EXIT LIGHT NR 2 ON CEILING INOP. (FLT 6728) RELAMPED EMERGENCY LIGHT.
EXTERIOR EMERGENCY EXIT LIGHTS INOP. (FLT 5835) RELAMPED EMERGENCY LIGHTS.
PLASTIC STRIP COVERING EMERGENCY FLOOR STRIP HAS BROKEN OFF FROM ABOUT ROW 12 BACK TO LAVATORY. (FLT 6014) REMOVED & REPLACED AFT EMERGENCY TRACK LIGHT COVER IAW AMM 33-51-00.
FOURTH OVERHEAD EMERGENCY LIGHT AFT IS BURNED OUT. (FLT 6189) REMOVED AND REPLACED 4TH AFT EMERGENCY OVERHEAD BULB PER AMM CH 33-51-16.
EMERGENCY EXIT LIGHT BY MAIN DOOR INOP. (FLT 6639) RE-SEATED CONNECTOR.
NR 2 AFT CEILING EMERGENCY LIGHT INOP. (FLT 5849) RELAMPED EMERGENCY LIGHT.
EMERGENCY FLOOR LIGHTING AFT STRIP DAMAGED. (FLT 6510) REPLACED LIGHT STRIP SECTION.
CABIN EMERGENCY LIGHT IN CEILING INOP. (FLT 6484) RELAMPED EMERGENCY LIGHT.
GEAR DISAGREE DISPLAYED. (FLT 6589) REPLACED NLG SELECTOR VALVE (GEAR DOORS).
FLT 6562 - EMERGENCY EXIT LIGHT BY CABIN DOOR NOT ILLUMINATING. RESEATED CONNECTOR.
FLT 6503 - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. ADJUSTED NOSE GEAR PROX SENSOR BRACKET.
FLT 5855 - EMERGENCY LIGHTS INOP. REPLACED ALL FOUR EMERGENCY LIGHT BATTERIES.
C-CHECK, THREE ISOLATORS FORWARD SIDE OF AFT PRESSURE BULKHEAD CRACKED. REPLACED PER SRM.
C-CHECK, FS 280 LEFT BRACKET, RIGHT SIDE OF COCKPIT FLOOR OPENING, CRACKED. REPAIRED PER REO.
C-CHECK, FS 280 LBL 9 SUPPORT CLIP CRACKED. REPAIRED PER REO.
C-CHECK, FS 280 RBL 9 SUPPORT CLIPS CRACKED. REPAIRED PER REO.
C-CHECK SUPPORT AND CLIP AT FS 625 CRACKED. REPLACED PER SRM.
FLT 6006 - RECEIVED A PACK HI TEMP CAUTION MESSAGE ALONG WITH REPORTED LIGHT SMOKE IN CABIN. REPLACED RIGHT PACK AIR CYCLE MACHINE IAW AMM 21-12-00. OPS AND LEAK CHECK GOOD, P/N 782790-15, S/N OFF 200106038.
ADG DEPLOYED DURING FLIGHT. RESTOWED ADG AS REQUIRED.
FLT 6670 - SYSTEM 2 HYDRAULIC QUANTITY DROPPED TO 0 PERCENT IN FLIGHT. REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-01. OPS CHECK AND LEAK CHECK GOOD.
RIGHT WING RIB AT WS389 IS DAMAGED. REPLACED RIGHT WING RIB AT WS 389 IAW REO 601R-57-21-899.
FORWARD OUTBOARD WING SPAR ON RIGHT WING HAS DAMAGE AT WS 339. REPAIRED WING SPAR DAMAGE AT WS 335-353 IAW CRJ 200 REO 601R-57-21-898.
LEFT PACK BRIEFLY HAS AN ODOR OF SMOKE, MADE A LOUD NOISE AND THEN OVERTEMPED. REPLACED LEFT AIR CYCLE MACHINE IAW AMM 21-51-10-401.
AFT RED EMERGENCY EXIT SIGN IS MISSING. REPLACED AFT RED EMERGENCY EXIT SIGN IAW AMM 33-51-00.
DESCENDING THRU 9,000 FT RIGHT WINDOW CRACKED. REPLACED RIGHT SIDE WINDOW IAW CRJ MM 53-12-01 AND RII 56-220-1000, PN OFF: NP139322-001 SN OFF: 02014H6515.
UPON GEAR EXTENSION GOT A GEAR DISAGREE AND TOWER CONFIRMED THAT THE NOSE GEAR WAS STILL UP. PERFORMED MANUAL RELEASE GEAR EXTENSION AND RECEIVED THREE GREEN INDICATIONS. REPLACED NLG SELECTOR VALVE ASSY IAW CRJ 200 MM 32-33-10. OPERATIONAL CHECKS GOOD.
UPON GEAR EXTENSION, GOT A GEAR DISAGREE WITH THE NOSE GEAR REMAINING UP. EXTENDED GEAR MANUALLY WITH ALL GEAR EXTENDING NORMALLY. REPLACED NLG SELECTOR VALVE ASSY IAW CANDAIR REGIONAL SET MM 32-22-25 PG 401.
AFTER SELECTING GEAR DOWN NOSE GEAR DID NOT COME DOWN. RECYCLED GEAR HANDLE THREE TIMES, NO HELP. MANUALLY EXTENDED NOSE GEAR. REPLACED NLG PRIORITY VALVE IAW RJ 200 MM 32-33-15. OPERATIONAL CHECKS GOOD, P/N; 4622.
FS 280 LBL9 LOWER FRAME/EVIDENCE OF CRACKS ON FLOOR SUPPORT BEAM AND LBL9 I/B AND O/B 280 CLIPS ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED I/B AND O/B CLIPS AND FILLERS.
FS 280 LBL9 LOWER ANGLE CRACKED ON FLOOR SUPPORT BEAM AND RBL9 I/B AND O/B 280 CLIPS ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AND CLIPS AT STA 280 RBL9 LOWER PER CRJ200 REO 601R 53-171 REV 'C' REPAIR SCHEME 'B' .
CREW REPORTS NR 2 STAB TRIM SWITCH INOP. REPLACED NR 2 STAB TRIM SWITCH REF AMM 27-41-05, OPERATIONAL CHECKS GOOD.
ON APPROACH "FLAPS HALFSPEED" STATUS MESSAGE CAME ON. REPLACED FLAP PDU PER CRJ MM 27-51-00. OPERATIONAL CHECK GOOD.
L-BRACKET (CLIP) AT OUTBOARD LEFT HAND 9' LBL ATTACHMENT TO 280 FS BEAM IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIP LEFT HAND INBOARD STA 280.00 LBL 9 IAW CRJ200 SRM 51-42-06 PG 1-4.
MAIN CABIN OVER PRESSURE FLOOR AT STA 461.00 BL 9 FLOORBEAM ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. FLOORBEAM INSTALLED AS REQUIRED IAW EO 600-31068 AND SRM 51-42-06; 51-42-21.
CRACKED SUPPORT ANGLE FS 621; LBL 45; WL 73.5. ITEM FOUND AT C-CHECK INSPECTION. REPAIR PARTS INSTALLED AS REQUIRED AND ALL WORK DONE IAW REO 601R-53-61-004 SRM 51-42-06 AND 51-42-21.
L-BRACKET CLIP AT INBOARD RIGHT HAND 9' LBL ATTACHMENT TO 280 FS FLOORBEAM IS CRACKED AT TOP RADIUS. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIP STA 280 INBOARD RBL 9 IAW CRJ200 SRM 51-42-06 PG 1-17.
DURING FLIGHT FROM ORD, CAPTAIN`S ALTIMETER JUMPED ERRATICALLY BETWEEN 22.00 - 32.00. UNABLE TO RESET WITH BARO KNOB TO PROPER SETTING. DIVERT TO CAK. REMOVED AND REPLACED NR 1 ADC IAW AMM 34-11-00. OPERATIONAL CHECK GOOD. A/C REMAINS CAT II & RVSM.
ON SHORT FINAL RECEIVED SPOILERONS FAULT AND OUTBOARD GROUND SPOILER FAULT STATUS MESSAGES. REMOVED AND REPLACED ANCP LOW PSI SWITCH 1B. PERFORMED SECU CHECKS IAW 27-61-05. OPERATIONAL CHECK GOOD.
CAPTAINS SIDE WINDOW HAS MULTIPLE CRACKS THAT SPAN THE LENGTH OF WINDOWS. REMOVED AND REPLACED LT SIDE WINDOW IAW AMM 56-12-01. P/N NP139322-5, S/N OFF 01352H5316.
STAB TRIM AND MACH TRIM CAUTION ILLUMINATED AFTER TAKEOFF. REMOVED AND REPLACED HSTCU IAW CRJ 200 MM 27-41-01. OPERATIONAL CHECK GOOD.
RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EXTERIOR EMERGENCY EXIT DOOR LIGHT IAW CRJ MM 33-51-21. OPERATIONAL CHECK GOOD.
BACK EMERGENCY LIGHTS INOPERATIVE. REMOVED BATTERY AND CLEANED CONTACTS. OPERATIONAL CHECK GOOD.
EMERGENCY LIGHTS AFT OF EXIT ROW INOPERATIVE. REMOVED EMERGENCY BATTERY AND CLEANED CONTACTORS, RE-INSTALLED AFT BATTERY. OPERATIONAL CHECK GOOD.
FLAPS FAIL MESSAGE ON APPROACH TO LANDING. REMOVED AND REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD.
NR 2 STAB TRIM FAILED TO ENGAGE. REMOVED AND REPLACED HSTA, IAW CH. 27-42-01 AND REPLACED MCU IAW MM CH. 27-42-05. OPERATIONAL CHECK GOOD. P/N: 7062-3 S/N OFF: 117.
ON APPROACH STAB TRIM CHANNEL 1 DISENGAGED. REMOVED AND REPLACED CAPTAINS STAB TRIM SWITCH AND STAB TRIM/MACH TRIM POND ASSY IAW MM 27-41-00 AND 27-41-25. OPERATIONAL CHECK GOOD.
INFLIGHT, MACH TRIM AND CHANEL 1 STAB DISENGAGED. REMOVED AND REPLACED STAB TRIM/MACH TRIM PANEL FOR IAW CRJ 200 MM 27-41-20. OPERATIONAL CHECK GOOD.
FLIGHT SPOILERS FAULT STATUS MESSAGE DISPLAYED ON ED2. RESECURED NR 1 SECU IN RACK. OPERATIONAL CHECK GOOD.
FLT SPOILERS FAULT STATUS MSG CYCLES ON AND OFF, TAXIED BACK TO GATE. PERFORMED FAULT ISOLATION PROCEDURES OF FLIGHT SPOILERS SYSTEM. NO DEFECTS NOTED.
FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED POWER DRIVE UNIT FOR FLAPS IAW 27-52-01. OPS CHECKS GOOD.
MAIN CABIN DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED BULB, OPS CHECK GOOD.
FLAPS FAIL CAUTION MESSAGE ON WHEN FLAPS SELECTED AT APPROXIMATELY 13,000 FT. REMOVED AND REPLACED RIGHT NR 1 AND LEFT NR 1 ACTUATOR (FLAP), IAW 27-53-01, 27-53-05, AND RII 27-412. OPS CHECKS GOOD. S/N OFF RIGHT: 3392.
FLAPS FAIL AT -0- WHEN SELECTED. REMOVED AND REPLACED RIGHT AND LEFT FLAP BPSU, LEFT FLAP ACTUATOR IN THE NUMBER 3 POSITION AND THE RIGHT NR 3 FLAP ACTUATOR. RIGHT BPSU S/N OFF: 0801, ACTUATOR P/N: 853D100-19, LEFT S/N OFF: 1945. RIGHT S/N OFF: 1941. OPS CHECKS GOOD.
CARGO PIT FS 621.00 RBL 42.0 FLOORBEAM ANGLE IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV-A.
CABLE FAIRLEAD INTERCOSTAL AT FS 484 RBL 36.0 IS CRACKED AT O/B FLANGE. DISCOVERED DURIING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-41-059 REV-A.
CABLE FAIRLEAD INTERCOSTAL AT FS 484 LBL 36.0 IS CRACKED AT FLANGE. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-41-059 REV-A.
MAIN CABIN I/B AND O/B ATTACH CLIPS ARE CRACKED ON LBL 9.0 FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11.
MAIN CABIN INBOARD AND OUTBOARD ATTACH CLIPS ARE CRACKED ON RBL 9.0 FS 280.00. DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIPS IAW CRJ SRM 51-40-11.
STALL FAIL MESSAGE AFTER TAKEOFF. REPLACED STALL COMPUTER. OPS CHECK GOOD. S/N OFF: 887
PILOT REPORTS L SPOILER FAULT ON INBOUND FLIGHT. REPLACED NR 1 SECU. OPS CHECK GOOD AT THIS TIME.
WITH BOTH ENGINES RUNNING AND NORMAL HYDRAULIC PRESSURE ON ALL 3 SYSTEMS, FLT SPLICER FAULT AND INBOARD GROUND SPOILER FAULT MESSAGES ON ED2 (STATUS). RETURNED TO THE GATE. REMOVED AND REPLACED NR 2 SECU. OPS CHECK GOOD.
DURING FLIGHT TO SFO AT 16,000 FT, NR 2 ENGINE N1 FLUCTUATIONS OF 8 TO 10 PERCENT WITH ASSOCIATED N2 FUEL FLOW & ITT FLUCTUATIONS. WITH THRUST BACK AT 68 PERCENT, FLUCTUATIONS STOPPED. REMOVED AND REPLACED RIGHT ENGINE BLUE AND YELLOW HARNESS. ENGINE RUN OF SYSTEM OPS CHECKS GOOD ON THE GROUND.
AFTER ESTABLISHING CLIMB POWER AFTER DEPARTURE FROM FAT, RIGHT SIDE N1 FLUCTUATIONS OF +/- 10 PERCENT AND FUEL FLOW OF +/- 500 PPH CAUSED A/C TO YAW UP TO 20K FT. REDUCED POWER AND RIGHT ENGINE STABILIZED. NO FURTHER FLUCTUATIONS WERE OBSERVED. RETURNED TO FAT. REPLACED NR 2 N1 AMPLIFIER. OPS CHECK GOOD IAW MM 73-21-03.
STAB CH1 WILL NOT ENGAGE. REMOVED AND REPLACED TRIM UNIT, HORIZONTAL STAB IAW CRJ MM 27-41-05. PERFORMED OPS AND FUNCTIONAL CHECK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO CAT II STATUS.