N452AW
Registered owner: SPIRE AVIATION II LLC, NC (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
6058 - AT FL 220 RECEIVED FLAP FAIL CAUTION MESSAGE WITH FLAPS AT 0 DEGREES PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPP 98-018I BOX 12 FLAPS RESET. PLACARDED AND PLACED ON MEL AIRCRAFT REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00. NO FAULTS FOUND. INTERROGATED AND TESTED FECU SYSTEMS IAW AMM 27-51-05. OPS TEST GOOD. REMOVED PLACARD AND REMOVED FROM MEL.
LEFT LOWER WING SKIN PANEL AT WS137.60 - WS148.019 A SMALL CRACK WAS FOUND EMINATING FROM RIVET HOLE. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW MHI REO 601R-57-21-3843 REV (--)
IN FLIGHT, RECEIVED STATUS MSGS FOR L PACK OFF, AND L 10TH ARM OPEN. AC DEPRESSURIZED, MASKS DID NOT DROP. ********AIRCRAFT REMOVED FROM SERVICE******** IN WORK
CLEAT ATTACHED TO FS313.56 FRAME 601R318086-1 IS CORRODED ***AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW CLEAT IAW CRJ200 SRM 51-42-06
****SUPPLEMENTAL INFORMATION *****MULTIPLE SPOTS OF CORROSION NOTED ON AFT PAX DOOR WEB (MARKED) ***AIRCRAFT REMOVED FROM SERVICE **** REPLACED PAX DOOR STAIRS AFT WEB
INTERCOSTAL BETWEEN FS333- FS349 STGR21L HAS CORROSION ****AIRCRAFT REMOVED FROM SERVICE **** REPLACED INTERCOSTAL BETWEEN FS333- FS349 STGR21L
CORROSION NOTED ON R/H FLOOR SEAT TRACK AT RBL9 BETWEEN FS409.00-409.00+120 ***AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW SEAT TRACK AT RBL9 BETWEEN FS409.00 TO FS409.00+120 REF CRJ200 AMM 53-01-11-400-802. TOOL# TUC8612 CAL DUE DATED 31-OCT-22.
RH SIDE SEAT RAIL FS409+16 TO FS409+112 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED A NEW RH SIDE SEAT RAIL FROM FS409.00+16-FS409.00+112 WITH NEW HARDWARE. REF CRJ 200 AMM 53-01-11-400-802 AND REO 601R-53-00-055 REV-C DATED 2017-03-21 REPAIR B STEP 3 TORQUE WRENCH TUC8416 CAL DUE 31-MAY-23
CORROSION NOTED ON L/H FLOOR SEAT RAIL AT LBL9 AND APPROX. BETWEEN FS364.00-FS398 ****AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED SEAT RAIL ON LBL 9 FLOOR BEAM BETWEEN FS 364 AND FS 398 REF CRJ200 AMM 53-01-11-400-802. USED TORQUE WRENCH TUC 8416 CAL DUE DATED: 31-MAY-23
CORROSION NOTED ON R/H FLOOR SEAT RAIL AT RBL9 AND APPROX. BETWEEN FS364.00-FS398] ****AIRCRAFT REMOVED FROM SERVICE **** INSTALLED SEAT RAIL ON RBL 9 FLOOR BEAM BETWEEN FS 364 AND FS 398 REF CRJ200 AMM 53-01-11-400-802
*FS682.00 ÿ½ FS700.00 STRG 21RH ÿ½ 22RH EXTERIOR SKIN DENTED AND WAVY (MARKED) ****AIRCRAFT REMOVED FROM SERVICE **** REPAIRED FS682.00 TO FS 700.00 STR 21 R/H TO STR 22R/H EXTERIOR SKIN REF REO 601R-53-61-7869 REV ( --) DATED 2022-08-15
FWD ANGLE SUPPORT THAT ATTACHES TO FWD FORMER IS CORRODED ***AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW FWD SUPPORT ANGLE (P/N 601R318731-3S) ONTO FWD FORMER USING NEW HARDWARE. REF CRJ200 SRM 51-42-21.
LBL 9 FLOOR BEAM PART # 601R31113-124 COMMON TO THE FS 280 CLIP HAS OVERSIZE FASTENERS HOLES ****AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW FLOOR BEAM WEB P/N 601R31113-124 AT LBL9 BETWEEN FS280.00 - FS295.00 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31113 REV M
LH SIDE SEAT RAIL FS409+16 TO FS409+112 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED NEW SEAT RAIL REF CRJ200 AMM 53-01-11-400-802 AND DWG 601R38312 REV-H
LH SIDE SEAT RAIL FS499 TO FS544 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED NEW LH SIDE SEAT RAIL FS499 TO FS544 REF. REO 601R-53-00-055 REV. C, 2017-03-21 REPAIR "B" STEP 3. TORQUE WRENCH TUC 4980, DUE DATE 28/02/2023.
RH SIDE SEAT RAIL FS449 TO FS409+112 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW SEAT RAIL REF. REO 601R-53-00-055 REV. C, 2017-03-21 REPAIR "B"
RH SIDE SEAT RAIL FS449 TO FS499 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED NEW SEAT RAIL REF. REO 601R-53-00-055 REV. C, 2017-03-21 REPAIR "B"
RH SIDE SEAT RAIL FS499 TO FS544 HAS SEVERAL AREAS WITH CORROSION ****AIRCRAFT REMOVED FROM SERVICE ****** INSTALLED NEW RH SIDE SEAT RAIL FS499 TO FS544 REF. REO 601R-53-00-055 REV. C, 2017-03-21 REPAIR "B"
RH SIDE SEAT RAIL FS559+80 TO FS544 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE *** INSTALLED NEW RH SIDE SEAT RAIL FS559+80 TO FS544 REF. REO 601R-53-00-055 REV. C, 2017-03-21 REPAIR "B" STEP 3. TORQUE WRENCH TUC 4980, DUE DATE 28/02/2023.
LH SIDE SEAT RAIL FS449 TO FS409+112 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED NEW SEAT RAIL REF. REO 601R-53-00-055 REV. C, 2017-03-21 REPAIR "B"
LH SIDE SEAT RAIL FS559+80 TO FS544 HAS SEVERAL AREAS WITH CORROSION ***AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW FLOOR SEAT TRACK REF REO 601R-53-00-055 REV (C) 2017-03-21
RBL 9 FLOOR BEAM (FS559+16 FS559+80) HAS CORROSION IN SEVERAL AREAS ****AIRCRAFT REMOVED FROM SERVICE *** INSTALLED NEW RBL 9 FLOOR BEAM BETWEEN FS559+16 - FS559+80 REF. CRJ200 SRM 51-42-36 & REO 601R-53-51-623 REV -- DATED 2022-08-11.
FLOOR TRACK AT FS559+80 ON RBL27 HAS CORROSION ****AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND INSTALLED NEW SEAT TRACK SECTION REF CRJ200 AMM 53-01-11-400-802 AND DWG 601R38312 REV-H
*PANEL 163AB TRAILING EDGE ATTACH ANGLE INNER SIDE CORRODED IN THE WHEEL WELLS (MARKED) ****AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED NEW STIFFENER P/N 601R32026-131 AT AFT FAIRING (WING-TO-FUSELAGE) FS559.00 BETWEEN RBL38 - LBL38. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, C
L/H INBD COCKPIT FLOOR SEAT RAIL MISSING FASTENERS AND HAS NICKS AND WEAR MARKS ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND REPLACED L/H INBD COCKPIT FLOOR SEAT RAIL, REF REO 601R-53-11-3792, REV -A, 2022-08-04 , DWG 600-33100 REV AB, DWG 601R41080 REV -B, CRJ 200 SRM 51-42-21 AND CRJ 200 SRM 51-42-20
PAX DOOR HINGE, FUSELAGE SIDE, HOLES ARE WORN/OUT OF ROUND ON SEVERAL LOBES, PIN IN EXCESSIVELY LOOSE WHEN INSTALLED ****AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW PAX DOOR HINGE (FUSELAGE SIDE) PN 600-31529-15 PO# 7835-00002 AND TOUCHED UP REPAIR AREA REF CRJ 200 SRM 53-21-23 STEP 4.R THRU 4.V , BOMBARDIER DWG 601R31527 REV AM AND DWG 601R31020 REV F.
CORROSION NOTED ON PAX DOOR FWD FORMER AT FS311.75 BETWEEN DD6-DD5 ****AIRCRAFT REMOVED FROM SERVICE *** INSTALLED NEW PAX DOOR FWD FORMER P/N 601R318031-5S REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-13, CRJ 200 SRM 51-42-21 AND DWG. NO. 601R31702 REV.N
UPPER SEAL SURROUND FOR THE SERVICE DOOR HAS SEVERAL GOUGES ****AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW MID UPPER AND UPPER FWD SERVICE DOOR SURROUND IAW CRJ200 SRM 51-42-06 AND DWG 601R38340 REV B
TOP PLATE FS559+80 SCRATCHED. BETWEEN RBL27 AND RBL9 ****AIRCRAFT REMOVED FROM SERVICE **** INSTALLED FLOOR SUPPORT PLATE ON FS559+80 BETWEEN RBL27 AND RBL9 REF CRJ200 SRM 51-42-06. & DRAWING # 601R38203 REV. NC
CORROSION NOTED AT 280 CROSSBEAM BETWEEN LBL9-RBL9 ***AIRCRAFT REMOVED FROM SERVICE **** FS 280 BULKHEAD WEB AND FLOOR SUPPORT ANGLE BETWEEN LBL 27 AND RBL 27 IS REPAIRED WITH FULL FS 280 BULKHEAD WEB REPAIR ON JOB 2783541 OP 360
MULTIPLE SPOTS OF CORROSION NOTED ON FWD PAX DOOR WEB (MARKED) ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND INSTALLED NEW FWD PAX DOOR WEB REF CRJ 200 SRM 51-42-06 AND DWG.NO. 601R317071 REV.E
CORROSION NOTED ON FLOOR SUPPORT STRUCTURE COMMON TO 280 BULKHEAD BETWEEN RBL9-RBL27 (MARKED) ****AIRCRAFT REMOVED FROM SERVICE *** FS 280 BULKHEAD WEB AND FLOOR SUPPORT ANGLE BETWEEN LBL 27 AND RBL 27 IS REPAIRED WITH FULL FS 280 BULKHEAD WEB REPAIR ON JOB 2783541 OP 360
LH MLG WHEEL WELL APPROX WS48.30 BATT ANGLE IS CRACKED (MARKED) ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AND INSTALLED NEW BATT ANGLE P/N 600-10204-27 AT LH MLG WHEEL WELL APPROX WS48.30 REF CRJ200 SRM 51-42-06, AND CRJ200 SRM 51-42-21 AND DWG 600-10204 REV M
FS621.00 BULKHEAD FORWARD FACE ABOVE FLOOR - VERTICAL STIFFENER REPAIR ON RIGHT BL35 HAS GOUGING DAMAGE FROM A SCREW. (CIRCLED IN RED) ****AIRCRAFT REMOVED FROM SERVICE **** REPAIRED FS 621 BULKHEAD FORWARD FACE ABOVE FLOOR VERTICAL STIFFENER REPAIR ON R/H BL 35 REF REO 601R-53-61-1285 REV E DATED 2016-10-31
FS621 BULKHEAD FORWARD FACE ABOVE FLOOR VERTICAL STIFFENER REPAIR ON RIGHT BL 35 HAS GOUGING DAMAGE FROM A SCREW ***AIRCRAFT REMOVED FROM SERVICE *****REMOVED AND INSTALLED NEW REPAIR DOUBLER AT RBL 36 ON FS 621 BULKHEAD REF REO 601R-53-61-1285 REV E DATED 2016-10-31
LEFT WING INBOARD FLAP LOWER SKIN HAS TWO DENTS. BOTH ARE 10.0ÿ½ FROM THE INBOARD EDGE OF FLAP AND 12.0ÿ½ & 14.0ÿ½ FROM THE TRAILING EDGE WITH APPROXIMATELY 2.0ÿ½ BETWEEN THE DENTS. ****AIRCRAFT REMOVED FROM SERVICE ***** REPAIRED L/H WING INBOARD FLAP LOWER SKIN REF REO 601R-57-52-1544 REV-- DATED 2010/01/07
LEFT WINDSHIELD LOWER SIDE POST ASSY. IS CRACKED BELOW WL110.00 AND FWD OF FS236.75 (MARKED)***AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED NEW ANGLE AT LH WINDSHIELD LOWER SIDE POST ASSY JUST BELOW WL 110.00 AND FWD OF FS 236.75 PER CRJ 200 SRM 51-42-06 AND BOMBARDIER DWG 601R34032 REV V & DWG 601R33010 REV J.
LEFT WING INBOARD FLAP LOWER SKIN HAS TWO DENTS, BOTH ARE 10.0" FROM INBOARD EDGE OF FLAP AND 12.0"&14.0" FROM TRAILING EDGE WITH APPROXIMATELY 2.0" BETWEEN THE DENTS ***AIRCRAFT REMOVED FROM SERVICE ***** REPAIRED L/H WING INBOARD FLAP LOWER SKIN REF REO 601R-57-52-1544 REV -- DATED 2010/01/07
WHILE LOADING BAGGAGE, THE CARGO DOOR CLOSED AND WAS STUCK CLOSED WHILE A PERSON WAS INSIDE THE CARGO BAY. THE A/C WAS OPERATING UNDER MEL 52-31-01-00 (CARGO BALANCE SPRING MEL) ON-CALL MX RESPONDED BUT PERSONNEL WAS REMOVED BEFORE ARRIVAL. ***AIRCRAFT REMOVED FROM SERVICE*** R&R CARGO DOOR BALANCE SPRING ASSEMBLY FOR BOTH CABLES IAW AWAC SUP 11-025A. OPS CHECKS GOOD, AC OK FOR RTS PN: 601R35218-4 S/N OFF: 55862 S/N ON: 56834 SMG PN: 601R35218-4 S/N OFF: 56765 S/N ON: 56728 SMG
APPROXIMATELY 10 SECONDS AFTER GEAR SELECTED UP RECEIVED GEAR DISAGREE. NLG SHOWED DOWN AND LOCKED. MAINS WERE UP. DUE TO NR 3A ACMP ON MEL. WAITED 20 PLUS SECONDS. NO CHANGE TO INDICATIONS. CW QRH. PULLED EMERGENCY LEVER GEAR EXTENDED AND INDCATED LOCKED DOWN. BURNED OFF FUEL. AIRCRAFT REMOVED FROM SERVICE. R & R NLG PRIORITY VALVE, REF AMM 32-33. OPERATIONS CHECK/LEAK CHECK GOOD. REMOVED PLACARD, REMOVED FROM MEL.
CABIN FLOOR SEAT TRACK CORRODED AT LBL 9 FROM FS 409+128 TO FS 559+10. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CORRODED CABIN FLOOR SEAT TRACK AT LBL 9 FROM FS 409+128 TO FS 559+10, IAW 601R-53-00-764.
FLOOR SUPPORT CAP CORRODED AT FS 589 FROM LBL 9 TO LBL 27. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORRODED CAP STRIP FS 589 FROM LBL 9 TO LBL 27 AND INSTALLED NEW CAP STRIP, IAW SRM 51-42-00 AND DRW 601R35031.
LAVATORY AFT WALL FLOOR FITTING AND ASSOCIATED SEAT TRACK REQUIRE CLEANING AND EVALUATION. FOUND SEAT TRACK AT 559 RBL 27 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORRODED SEAT TRACK AT FS 559 AT RBL 27, IAW REO 601R-53-00-764.
CABIN FLOOR SEAT TRACK AT RBL 9 FROM FS 409+128 TO 559 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CORRODED CABIN FLOOR SEAT TRACK AT RBL 9 FROM FS 409+128 TO 559, IAW REO 601R-53-00-764.
T CAP CORRODED AT NUTPLATE LOCATION LBL 27 AND FS 589+14. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CORRODED T CAP AT NUTPLATE LOCATION LBL 27 AND FS 589+14, IAW DRW 601R35031.
TRANSFER RECTIFIER COMPARTMENT LEFT SIDE SKIN CRACKED AT FS 193.00 OUTBOARD OF HYDRAULIC SYSTEM NR 2. AIRCRAFT REMOVED FROM SERVICE. REPAIRED LEFT SIDE SKIN CRACK FS 193.00, IAW REO 601R-53-11-111 AND SRM 51-42-00.
RT WING ANTI-ICE CAUTION MESSAGE CLEARED IN STNDBY WITH 14TH STAGE ISOL VLAVE OPEN. REAPPEARED AND WOULD NOT CLEAR. DIVERTED TO CID. "AIRCRAFT REMOVED FROM SERVICE" R&R LH 14TH STAGE MSOV REF AMM 30-11, BOTH LH, AND RH WING ANTI ICE SYST OPERATE NORMALLY AT THIS TIME IN NORMAL AND STBD MODE
RECEIVED NWS INOP CAUTION RAN QRH MSG DID NOT RESET. MSG CLEARED UPON LANDING WHEN NWS SELECTED AIRCRAFT REMOVED FROM SERVICE SERVICED NLG STRUT PER AMM 12-12-32. CW OPERATIONAL CHECK OF NWS PER AMM 32-51 CHECKED GOOD NO AMBER CAUTION MSGS DISPLAYED
AFTER TAKEOFF CREW SELECTED GEAR UP AND IMMEDIATELY RECEIVED A GEAR DISAGREE, NOSE LANDING GEAR DOOR OPEN, STEERING INOP, AND WEIGHT OFF WHEELS CAUTION MSG. PER QRH THE FLIGHT RETURNED TO KORD AND LANDED WITHOUT FURTHER ISSUES. FLIGHT DID NOT DECLARE EMERGENCY AND WAS ABLE TO TAXI TO THE GATE WITHOUT ASSISTANCE. NO PASSENGER ISSUES REPORTED. AIRCRAFT REMOVED FROM SERVICE FOUND NLG STRUT SERVICED INCORRECTLY. SERVICED NLG STRUT PER AMM 12-12-32. CW LANDING GEAR OPS CHECK PER AMM 32-30-00. CHECKS GOOD. ALL MESSAGES CLEARED AT THIS TIME NO AMBER CAUTION MSG NOTED. NWS OPS CHECK GOOD PER AMM 32-51
DURING CLIMB OUT, FELT VIBRATION, AND AIRCRAFT DID NOT PERFORM NORMALLY FOR BEING EMPTY. UPON LANDING IN ORD, FOUND THE UPPER TRANSLATING COWL ON THE RT ENGINE TO BE OPEN. SUSPECTED TO BE OPEN ENTIRE FLIGHT.
W/O 275590 MX WORK CARD #3, DURING EMERGENCY LIGHT CHECK, FOUND AFT MOST EXTERNAL EMERGENCY LIGHTS, AND MID-CABIN INTERIOR EMERGENCY LIGHT OUT.
REF WO 275079 JOB CARD NR/0002 - REF 257951/1 RIVET FS185 & FS295 NOT FLUSH.
UPON REMOVAL OF SKIN PANEL (FS 193.00 TO FS 280.00) FOUND SEVERAL OVERSIZED HOLES.
RT ICE DETECTOR DOUBLER P/N 600-33010-126 IS DEFORMED/WRINKLED.
RT ICE DETECTOR DOUBLER P/N 600-33010-128 IS DEFORMED.
RT KIDNEY PANEL (DOOR 132AL) HAS 3 EA. FASTENER HOLES THAT HAVE LOOSE/MISSING FREEZE PLUGS.
STR 19R BETWEEN FS 193 AND FS 202 HAS SEVERAL ELONGATED HOLES.
3 EACH STRINGERS DAMAGED BETWEEN FS 202 AND FS 220 STRG 19R, STRG 20R, AND STRG 21R.
RIGHT AILERON LOWER LEADING EDGE SKIN IS CHAFED. REPLACED RIGHT AILERON LOWER LEADING EDGE SKIN IAW SRM 51-42-21, 51-42-06.
FUSELAGE SKIN AT AFT NLG DOOR CUTOUT RT SIDE CRACKED. REPAIRED.
LEFT I/B FLAP LOWER SKIN HAS NICKS AND DENTS. REPLACED LOWER SKIN IAW SRM 51-42-13.
AFT PRESSURE BULKHEAD HAS A CRACK IN THE WEBB AT BL0, WL110.00. REPAIRED CRACK IAW REO 601R-53-61-1285 REV-E.
CARGO DOOR BEAM LOWER AFT ANGLE AT APB IS CRACKED. REPLACED AFT ANGLE ON CARGO DOOR BEAM AT APB IAW SRM 51-42-21.
CARGO DOOR FWD TRACK LOWER CHANNEL CRACKED. REPLACED
PAX DOOR HAS CRACKED INTERCOSTAL.
FLOOR SUPPORT I/B AND O/B TOP FLANGES HAVE CORROSION AT LBL 27 AND BS 605 - 621.
PAX DOOR WEB UNDER TOP FOLDING STEP IS CRACKED ON AFT SIDE.
RIGHT INBD FLAP DAMAGED AT OB LOWER EDGE.
PAX DOOR AFT RISER DRAG ANGLE CRACKED BY CABLE ASSIST PULLEY. REPAIRED.
ATTACH ANGLE AT BS 280 AND STRINGER 3L IS CRACKED.
BS 621 AFT PRESSURE BULKHEAD GOUGED.
RIGHT FLOOR SUPPORT HAS CORROSION AT BS 317 - 320.
LEFT SIDE OVERWING FAIRING ATTACHMENT BRACKET AT BS 469 IS CRACKED
FWD CLEAT AT PAX DOOR LOWER SILL HAS CORROSION.
AFT CLEAT AT PAX DOOR LOWER SILL HAS CORROSION.
RIGHT SIDE OVERWING FAIRING ATTACHMENT BRACKET AT BS 469 IS CRACKED
PRESSURE FUELING BRACKET IS CRACKED
RIGHT SIDE OVERWING FAIRING ATTACHMENT BRACKED AT BS 449 IS CRACKED
LEFT FUSELAGE STRINGER 3L IS CRACKED AT BS 379.
LEFT SIDE OVERWING FAIRING ATTACHMENT BRACKET AT BS 461 IS CRACKED
LEFT SIDE OVERWING FAIRING ATTACHMENT BRACKET AT BS 449 IS CRACKED
RIGHT SIDE OVERWING FAIRING ATTACHMENT BRACKET AT BS 461 IS CRACKED
CENTER WINDSHIEL POST LT SIDE LOWER BRACKET CRACKED. REPLACED THE WINDOW FRAME.
CENTER WINDSHIELD POST, RT SIDE LOWER BRACKET CRACKED.
FLT DECK FLOOR LANDING ANGLE ON THE FWD SIDE OF BEAM BS 280 IS CORRODED AT THE BOTTOM SIDE AND IS CRACKED BETWEEN RBL 12 AND LBL 12
PAX DOOR AFT RISER IS CRACKED AT BOTTOM FIXED STEP
LEFT FUSELAGE FRAME BS 333 IS CRACKED BETWEEN STRINGERS 1 AND 2L.
RIGHT INBD FLAP INBD LOWER SKIN DENTED AND GOUGED IN THE CENTER LOCATED AT WS 57.
PAX DOOR WEB UNDER TOP FOLDING STEP IS CRACKED ON FWD SIDE.
LEFT IB FLAP LOWER SKIN DENTED AT WS 53.
UPON LANDING, APPLIED NORMAL BRAKES, LT BRAKE FELT SPONGY AND TOOK MORE TOE PRESSURE THAN RT BRAKE. UNUSUAL SQUEAL WITH LT BTMS 6, 5 AND RT 2, 2.
SMOKE TOILET CAUTION ON TAXI INTO GATE. INVESTIGATED, NO SMOKE IN LAVATORY. INSPECTED LAVATORY, CABIN & CARGO BAY, NO EVIDENCE OF SMOKE OR FIRE. RAN APU & ENGS WITH BOTH PACKS ON, NO SMOKE OR FUMES. R & R LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPERATIONS CHECKED GOOD. REMOVED PLACARD & REMOVED MEL.
LEFT INBD FLAP, INBD HINGE ARM GOUGED.
LEFT MLG WW BATTERY RIB DRAG ANGLE STIFFENER IS CRACKED.
STIFFENER BATTERY RIB DRAG ANGLE IN RT MLG WW IS CRACKED.
LT & RT OBLIQUE ANGLES CRACKED BETWEEN FS 621 & 625 NEAR STRINGER 14L & 14R.
PAX DOOR AFT STAIR SUPPORT PANEL DRAG ANGLE CRACKED.
RIGHT CLIP CRACKED AT FS 484 & RBL 27.
RIGHT MLG WW VOLUMETRIC FUSE BRACKET IS CRACKED.
RIGHT OTBD CLIP AT INTERCOSTAL FS 484 IS CRACKED.
EXTERNAL POWER RECEPTACLE SUPPORT BRACKET CRACKED.
CARGO BAY TIE DOWN TRACKS ON LBL 9 CORRODED FS 559+112 - 559+125.
RIGHT MLG WW BRAKE TRANSDUCER MOUNT BRACKET IS CRACKED.
55065-2000-0039 FLOOR SEAT TRACKS AT LBL & RBL 9, FS 364 TO 394 CORRODED.
55065-1000-0023 BATH TUB FITTING CRACKED AT RBL 9 & FS 461.
55065-7000-0005 LEFT MLG WW BRAKE TRANSDUCER BRACKET IS CRACKED.
LEFT INBD FLAP VANE LE CHAFED.
RIGHT INBD FLAP VANE LE CHAFED, INBD END.
PAX DOOR LOWER SILL SUPPORT ANGLE CORRODED.
FS 280 FLOOR SUPPORT OTBD OF LBL 9 IS CRACKED AT LOWER SIDE.
ONE EACH TIE DOWN TRACK CORRODED AT RBL 27 & FS 559+80.
55065-2000-0036 TWO EACH TIE DOWN TRACKS CORRODED ON RBL 9 FROM FS 559+80 TO 574.
FUSELAGE LOWER SKIN CRACKED IN AFT LT RADIUS OF NLG WW.
LBL 9 & RBL 9 INBD & OTBD FLOORBEAM ATTACH CLIPS AT FS 280 ARE CRACKED.
EMERGENCY LIGHT FLOOR LIGHTING ROW 6 - 8 OUT & ELECTROLUMINESCENT EXIT IDENTIFIER SIGN AT RT OVERWING EXIT, KNEE HIGH, INOPERATIVE.
REF 276847/2 WHILE COMPLYING WITH NEF 25-70-20-23 FOUND LAST THREE INCHES OF EMER FLOOR LIGHTING INOPERATIVE, FWD PORTION. PLACARDED & PLACED ON MEL. NO CM ACTION REQUIRED.
ENTIRE ACFT VIBRATION OF MODERATE INTENSITY FOLLOWED BY UN-COMMANDED YAW MOTION IN BOTH DIRECTIONS. FOLLOWED BY AILERON CAUTION ON PFD-"AILERON MISS-TRIM". AND TWO SHARP LEFT BANKS WITH AUTO PILOT ON. DECLARED EMERGENCY AND LANDED FLAPS 8. R & R FCC 2 IAW AMM 22-12-14, OPS CHECK FAILED. ELEVATOR FLAG WITH AUTOPILOT ENGAGED ALL INDICATIONS NORMAL WITH AUTOPILOT DISENGAGED REF 252701/4 FOR MEL.
FRAME AT FS 574 BELOW CARGO FLOOR LT SIDE DAMAGED. REPAIRED IAW STS EA 15-2013-284.
STRINGER 21L, FS 559 +112 TO 621 DAMAGED. R & R STRINGER IAW SRM 51-42-06 & 51-42-21.
FRAME AT FS 589, BELOW CARGO FLOOR, LT SIDE DAMAGED. REPAIRED IAW EA 15-2013-285.
SKIN DAMAGED FROM FS 574-605 UNDER CARGO FLOOR LT SIDE. REPAIRED IAW EA 15-2013-286, REV A.
NR 2 HYD MANIFOLD BRACKET CRACKED ON LOWER AFT CORNER. COMPLIED WITH REO 601R-53-62-031 REV A.
FASTENER HOLE ON ACCESS HOLE FOR PANEL 132AL HAS DAMAGE. OPEN HOLE TO .330 AND MANUFACTURE FREEZE PLUG AND INSTALL.
DENT BETWEEN FS 625.3 AND 640 RIGHT AFT FUSELAGE. REPAIRED IAW BOMBARDIER REO 601R-53-61-4685 REV A.
INBOARD FLAP ACCESS PANEL 684 AB & 684 BB HAVE CHAFE DAMAGE. BLENDED DAMAGE IAW REO 601R-57-52-1980 REV.
RIGHT ENGINE LOWER CORE COWL HAS DENT PUNCTURE ON INTERIOR SKIN PROTRUDING TO EXTERIOR. COMPLIES WITH REO 601R-71-12-4140 REV A BY CUTTING REMOVING DAMAGE AND INSTALLING EXTERNAL DOUBLER.
RIGHT MLG DOOR IS GOUGED AND CHAFED IN SEVERAL PLACES. REMOVED DAMAGED UPPER INNER SKIN AND INSTALLED SERVICEABLE INNER SIN IAW CRJ 200 SRM 51-42-13.
DURING COLD WORKING OF FASTENERS HOLES OF MLG TRUNNION FLANGE FOUND 2 EA OVERSIZED HOLES (1 EA LT & 1EA RT ). REAMED 2EA HOLES TO START HOLE DIA. COLD WORKED HOLES AND REAMED TO FINAL HOLE DIAMETER AND INSTALLED 2EA HI LITE PINS AND NUTS PER REO 601R-57-21-1789.
RIGHT MLG DOOR HAS CHAFE MARKS ON THE INNER SKIN AND ON THE INNER TRAILING EDGE. REMOVED DAMAGED LOWER INNER SKIN AND INSTALLED NEW SERVICEABLE INNER SKIN IAW CRJ 200 SRM 51-42-13.
RIGHT ENGINE LOWER CORE COWL L/E INBOARD HAS BENT CRUSHED COMPOSITE. REPAIRED RIGHT ENGINE LWR CORE COWL L/E INBOARD CORNER IAW BOMBARDIER CMM 71-12-01 SRS 118.
SYSTEM NR 3 BRAKE ACCUMULATOR FORWARD O/B MOUNT BRACKET IS CRACKED. REMOVED DISCREPANT BRACKET AND INSTALLED SERVICEABLE P/N 601R75250-55 BRACKET IAW CRJ 200 SRM 51-42-21.
FS 484 CLIP RIGHT SIDE O/B IS CRACKED AT RIGHT UNDERFLOOR LONGERON. REMOVED AND INSTALLED WITH REPLACEMENT SERVICEABLE 484 CLIP IAW CRJ 200 SRM 51-42-21.
SEAT TRACKS ARE CORRODED FROM FS 559+80 TO 559+96 AT RBL 9. REMOVED CORRODED SEAT TRACKS LOCATED AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW BOMBARDIER REO 601R-53-60-485.
CORROSION FOUND AT FLOORBEAM CAP AT LBL 27 BETWEEN FS 574 & FS 621 AROUND SCREW HOLES. FLOORBEAM CAP REQUIRES REPLACEMENT.
CORROSION FOUND ON LEFT FLOOR SILL FROM FS 559+80 TO 621.00. LEFT SILL REQUIRES REPLACEMENT.
CARGO BOTTLE LOW CAUTION MESSAGE. R & R CARGO FIRE BOTTLE REF SUP 10-099. OPS CHECKED GOOD.
AT 2700 AGL, 180 KTS, SELECTED GEAR DOWN, NOSE INDICATED DOWN AND LOCKED BOTH MAINS INDICATED UP. RAN QRH AND USE MANUAL RELEASE, MANUAL EXTENSION. ALL GEAR INDICATED DOWN AND LOCKED. NO OTHER ABNORMAL. R & R RT MLG SELECTOR VALVE REF AMM 32-32-10. OP CK GOOD AT THIS TIME.
GALLEY FAN APPEARS TO HAVE ELECTRICAL ODOR WHEN ON. INSPECTED GALLEY FAN MOTOR WIRING AND SURROUNDING COMPONENTS. NO SIGN OF FAILURE OR FIRE CONDITION FOUND. THE ODOR NOTED, COULD NOT BE DUPLICATED.
ACFT FUSELAGE SKIN IS GOUGED ON LT SIDE AT 409.00 + 64 ABOVE 4TH LT PAX WINDOW BETWEEN STR 13L & 10L. REPAIRED FUSELAGE SKIN BETWEEN FS 409.00 +57 AND FS 409.00 +67 BETWEEN STR4 AND STR BL IAW SRM 53-00-31 REPAIR NR 8.
PAX DOOR STAIR STRUCTURE IS CRACKED ON AFT SIDE AT 4TH STEP CUT OUT. CRACKED SECTION ON AFT SIDE AT 4TH STEP, AND FABRICATED NEW SECTION IAW B/A REO 601R-52-11-702, REV C.
PAX DOOR STAR STRUCTURE IS CRACKED NEX TO FWD HANDRAIL BRACKET 4TH STEP CUTOUT CRACKED SECTION ON FWD SIDE PANEL AT 4TH STEP AND FABRICATED NEW SECTION IAW BA REO 601R-52-11-702, REV C.
PAX DOOR STAIR STRUCTURE IS CRACKED NEX TO AFT HANDRAIL BRACKET 4TH STEP CUTOUT CRACKED SECTION ON AFT SIDE PANEL AT 4TH STEP, AND FABRICATED NEW SECTION IAW B/A REO 601R-52-11-702, REV C.
PANEL 434BT (STANG FAIRING) CRACKED TOP R/B SIDE. REPLACED WITH NEW PART.
BACK SIDE OF PAX DOOR BLOW OUT DOOR IS CHAFED. BLENDED CHAFED AREA IAW SRM 51-12-00 & REO 601R-52-11-1040.
RT MLG BATT RIB CRACKED CUTOUT DAMAGE INSTALLED FILLER AND DOUBLER.
PAX DOOR FWD CENTERING PLATE IS CHAFED. REPAIRED DAMAGED PAX DOOR FWD AFT CENTERING PLATE IAW SRM 52-00-31.
LT MLG DOOR L/E IS CHAFED. APPLIED REO 601R-52-82-033, REV A, AND REO 601R-52-82-034, REV NC REPAIR MLG DOOR FOR RETURN TO SERVICE.
PAX DOOR AFT CENTERING PLATE IS CHAFED. REPAIRED DAMAGED PAX DOOR AFT CENTERING PLATE IAW SRM 52-00-31.
ACCESS HOLE FOR PANEL 132 HAS 4 DAMAGED FASTENER HOLES IN FUSELAGE SKIN. REPAIRED 4 EA HOLES IAW REO 601R-53-11-162, REV B.
LT BATT RIB CRACKED CUT OUT DAMAGED AND INSTALLED FILLER AND DOUBLER.
RT EXHAUST FAIRING HAS BROKEN FIRE LOOP ATTACHMENT BRACKET. R & R 2 EA FIRE LOOP ATTACHMENT BRACKETS IAW SRM 51-42-06 AND SRM 51-40-11.
RT INBD FLAP VANE L/E SKIN HAS CHAFING DAMAGE IN (3 EA) AREAS FROM STOPS. REPAIRED RT INBD FLAP L/E IAW REO 601R-57-52-004.
PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED AFT CRACKED DRAG ANGLE SECTION, THEN SPLICED IN NEW SECTION USING PN 601R31772-5 AND IAW BA REO 601R-52-11-513, REV A.
LT FS 621.00 OBLIQUE ANGLE CRACKED. R & R WITH SERVICEABLE OBLIQUE ANGLE, PN 601-35012-51 IAW SRM 51-42-06 AND REO 601R-53-61-422, REV NC.
LT AILERON UPPER L/E SKIN HAS CHAFING DAMAGE IN SEVERAL AREAS. REPAIRED LT AILERON UPPER L/E SKIN IAW REO 601R-57-60-013.
LT AILERON LWR SKIN HAS CHAFING DAMAGE ON L/E IN 2 EA AREAS. REPAIRED DAMAGED AREAS IAW REO 601R-57-60-020.
LT WING OTBD FLAP ROLLER FITTING HAS CHAFING DAMAGE. REPAIR CHAFING DAMAGE ON LT WING OTBD FLAP ROLLER FITTING IAW REO 601R-57-53-850.
LT INBD FLAP VANE INBD ACTUATOR SEAM HAS WEAR FROM LOWER ROLLERS. REMOVED CHAFING DAMAGE ON LT INBD FLAP VANE INBD ACTUATOR BEAM IAW REO 601R-51-52-1683.
LT INBD FLAP VANE CENTER ACTUATOR BEAM HAS WEAR FROM LOWER ROLLERS. REMOVED CHAFING DAMAGE ON LT INBD FLAP VANE CENTER ACTUATOR BEAM IAW REO 601R-51-52-1683.
RT OTBD FLAP HAS 2 LOOSE RIVETS ON TOP SKIN IN THE CENTER OF THE FLAP. REMOVED UNSERVICEABLE LOOSE RIVETS ON RT OTBD FLAP TOP SKIN IN THE CENTER OF THE FLAP AND INSTALLED SERVICEABLE RIVETS IAW REO 601R-57-53-849.
BULKHEAD FS 202 CRACKED AROUND PARKING BRAKE CABLE. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71, WL 69.684 IAW REO 601R-53-11-563.
LT WING OTBD FLAP ROLLER GUIDE FITTING HAS CHAFING DAMAGE. REPAIRED LT OTBD FLAP ROLLER GUIDE FITTING IAW REO 601R-57-51-143.
L/E OF RT INBD FLAP VANE JAS CHAFE DAMAGE. REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN.
RT AILERON LOWER L/E IS CHAFED IN 2 PLACES. REPAIRED CHAFED AREAS ON RT LOWER L/E 2 PLACES IAW 601R-57-60-020, REV NC.
RT T/R LOWER OTBD AND INBD MAIN TRACKS CHAFED. REPAIRED CHAFE ON RT T/R LOWER OTBD AND INBD MAIN TRACK.
AFT FACE OF RT NOSE INLET HAS CRACKED BRACKET AT 4 O`CLOCK POSITION. R & R BRACKET IAW SRM 51-42-06, 51-21-11, 51-25-16.
LT INBD FLAP VANE SKIN L/E HAS CHAFING DAMAGE FROM STOPS IN 3 EA AREAS. REPAIR LT INBD FLAP VANE IAW REO 601R-57-52-004.
RT MLG DOOR L/ECHAFED. REMOVED DAMAGE, INSTALLED DOUBLER AND FILLER.
PAX DOOR EXTERNAL HANDLE CRACKED. REMOVED CRACKED HANDLE THEN INSTALLED NEW HANDLE PN 601252-119.
RT MAIN GEAR WOULD NOT COME UP AFTER T/O. RETURNED AND LANDED. REMOVED RT MLG DOWNLOCK PIN AS REQUIRED. (K)
AFTER TAKEOFF WITH 2600 LBS PER SIDE, FUEL IMBALANCE ON ED1, QTY 3000 IN LT, 2000 IN RT. RT WING LOWERING AND CENTER TANK WAS INCREASING. REMOVED AND REPLACED FUEL SYS COMPUTER IAW AMM 28-41-16. OPS CHECK GOOD. (K)
MWC 132399-121 - MID CABIN FLOOR STRUCTURE, INTERCOSTAL CRACKED AT FS 484, RBL 35. MID CABIN FLOOR STRUCTURE INTERCOSTAL AT FS 484, RBL 35, REPAIRED IAW REO 601R-53-41-059, REV A. (K)
MID CABIN FLOOR STRUCTURE, ANGLE CRACKED (.500 LENGTH) AT FS 484 AND RBL 28. MID CABIN FLOOR STRUCTURE, ANGLE REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)
TOOL DAMAGE ON FLOORBEAM AT FS 484, RBL 36.00, WL 72.00 AND INTERCOSTAL AT FS 484.00 BTW RBL 36 AND RBL 45, WL 72.00. FLOORBEAM AT FS 484.00, RBL 36.00, WL 72 AND INTERCOSTAL FS 484.00, RBL 36-45 WL 72 REPAIRED IAW REO 601R-53-41-916. (K)
PAX DOOR OUTER HANDLE FLAP IS CRACKED. PAX DOOR OUTER HANDLE REPLACED IAW SRM 51-42-06. (K)
MWC 132399-119- MID CABIN FLOOR STRUCTURE, ANGLE CRACKED (.400 INCH LENGTH) AT FS 484, LBL 28. MID CABIN FLOOR STRUCTURE, ANGLE REPLACED AT FS 484, LBL 28 IAW SRM 51-42-06 AND 51-42-21. (K)
MWC 132400-69- UPPER ANGLE ALONG CROSSBEAM AT FS 280.00, LBL 10.00, WL 72 IS CRACKED. UPPER ANGLE ALONG CROSSBEAM AT FS 280.00 LBL 10.00, WL 72.00 REPAIRED IAW REO 601R-53-11-138. (K)
MWC 132399-120 - INTERCOSTAL AT FS 484 LBL 36.00, WL 70.00 IS CRACKED. INTERCOSTAL AT FS 484.00, LBL 36.00, WL 70.00 REPAIRED IAW REO 601R-53-41-059, REV A. (K)
MWC 132400-83 - RT INBD ANGLE AT FS 280.00, RBL 8.00, WL 72.00 CRACKED, CRACK LENGTH .350 INCH RT INBD ANGLE AT FS 280.00, RBL 8.00, WL 72.00. REMOVED AND REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)
OTBD ANGLES CRACKED AT FS 280.00, LBL 9.0, WL 72.00 (L+.200 INCH AND .300 INCH) OTBD + INBD ANGLES AT FS 280.00, LBL 9.0, WL 72, INSTALLED IAW SRM 51-42-21. (K)
MWC 132399-41 - FWD FUSELAGE ASSESS PANEL DOOR SURROUND SKIN QTY (2) ELONGATED FASTENER HOLES AT FS 228.00 BTW STR 19-20 RT SIDE FWD FUSELAGE ACCESS PANEL DOOR SURROUND SKIN QTY (2) ELONGATED FASTENER HOLES AT FS 228.00 BTW STR 19-20. REPAIRED IAW REO 601R-53-11-162, REV B. (K)
FLAP FAIL MSG ON TAXI OUT WHEN FLAPS SELECTION TO FLAPS 8 DEGREES. COMPLIED WITH RESET PROCEDURE FOR SDS AND FLAP SYS IAW FIM 27-00. OPS CHECK GOOD. (K)
FLAPS FAILED WHEN SELECTING FROM 8 DEGREES TO 20 DEGREES, AIRSPEED 180 KNOTS. OAT APPROXIMATELY 5 DEGREES CELSIUS. CW FIM 27-50 FOUND FLAP CONTROL LEVER FAULT ON FECU. REPLACED FLAP CONTROL LEVER IAW AMM 27-50. RESET FLAP SYSTEM IAW AWAC SUP 98-018B. OPS CHECK GOOD AT THIS TIME.
LOG 192018/1 ON APPROACH HAD FLAPS FAIL MSG. WHEN FLAPS SELECTED TO 8 FLAP INOPERATIVE CAUTION MSG DISPLAYED. COMPLIED WITH FIM 27-50-00. FAULTS FOUND LEAD TO INTERNAL FECU/BPSU MISS RIG. R&R FECU IAW AMM 27-51-05. OPS CHECK GOOD. RIG CHECK GOOD AT THIS TIME REF AMM 27-51-10.
LOG 192011/1 PAX DOOR WILL NOT LOWER COMPLETELY. HELD DOOR DOWN TO UNLOAD PASSENGERS, POWER ASSIST MOTOR FAILED. ASSIST SPRINGS ALSO BAD. R&R PAX DOOR ACTUATOR IAW AMM 52-10-00, OPS CHECK OK.
UPON ENGINE START GROUND SPOILER DEPLOY ADVISORY MESSAGE. ALL SPOLERS CONFIRMED UP VISUALLY AND ON FLIGHT CONTROL PAGE. INTERROGATED LT AND RT SECU`S FOR FAULTS, NO FAULTS FOUND. CHECKED MDC FOR FAULTS/DIAGNOSTICS, NO FAULTS FOUND GROUND RAN AIRCRAFT, RE CHECKED MDC NO FAULTS FOUND OPS CHECK NORMALLY IAW AMM 27-60-00. (A)
AFTER SELECTING GEAR DOWN GOT GEAR DISAGREE MESSAGE, RT MLG DID NOT EXTEND. COMPLIED WITH QRH, ALL THREE GEAR EXTENDED DOWN AND LOCKED AND ALL GREEN. DURING GEARDOWN SELECTION, HEAVY SIDE WIND GUST. (M)
ON CLIMBOUT AFTER TAKEOFF, APROX 600 MSL, CARGO DOOR MESSAGE ED1 AND CAUTION LIGHT ILLUMINATED. CABIN CLIMBING APPROX 1400 FT PER MIN. C/W QRH. AFTER LANDING NOTED CARGO DOOR HANDLE POPPED. FOUND CARGO DOOR HANDLE EXTENDED UPON ARRIVAL AT GATE. STOWED CARGO DOOR HANDLE, PRESSURIZED AIRCRAFT, NO DEFECTS NOTED W/ CARGO DOOR WARNING SYS, OPS CHECK OF CARGO DOOR HANDLE GOOD IAW AMM 52-31-03. OK FOR CONTINUED SERVICE. (K)
RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG IN OB RADIUS. (K) [07-17-07] MAINTENANCE REPAIRED IAW BOMBARDIER AEROSPACE REO 601R-53-61-117. (M)
LT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. (K) [07-17-07] MAINTENANCE CUT AWAY DAMAGED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R53-61-117 REV C. (M)
PASSENGER DOOR AFT DRAG ANGLE CRACKED APPROX .5 INCHES LONG AT DOOR ASSIST CABLE PULLEY BRACKET. (K) [07-17-07] MAINTENANCE CUT AWAY CRACKED ANGLE AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R52-11-513 REV A. (M)
STRONG BURNING SMELL IN GALLEY AREA. SMELL LESSENS WHEN GALLEY HEATERS TURNED OFF. PERFORMED SELF TEST OF GALLEY HEATING SYSTEM, FOUND SYSTEM ONE FAILED. PERFORMED SELF TEST OF GALLEY HEAT SYSTEM, FOUND SYSTEM ONE FAILED. COMPLIED WITH CM ACTION, REF 142284/2 FOR MEL. REMOVED AND REPLACED GALLEY HEATER PER AMM 21-23-05. OPERATIONAL CHECK GOOD. REMOVED PLACARD AND REMOVED OFF MEL. (M)
RIGHT REVERSER UNLOCKED CAS MESSAGE IN FLIGHT FOLLOWED QRH PROCEDURE. COMPLIED WITH MAINTENANCE ACTION AND DEACTIVATION OF THRUST REVERSER REF 142277/4 FOR MEL. PERFORMED OPS CHECK OF RT REVERSER SYSTEM PER MM 78-30-00, OK FOR SERVICE REMOVED FROM MEL. (M)
TRANSVERSE BEAM AT FS 250, RBL 30, NEAR STRINGER 16 IS BENT AND CRACKED .3 INCH INBOARD OF STRINGER 16. MAINTENANCE REPAIRED TRANSVERSE BEAM IAW EO 601R-53-9822. (M)
AIRCRAFT BLOWN INTO FUEL TRUCK. DAMAGED ON RIGHT FUSELAGE BELOW F/O`S WINDOW. MAINTENANCE REPAIRED DAMAGE TO FWD FUSELAGE STRUCTURE FS 235 TO FS 280, STRINGER 17 TO 23, REO 601R-53-11-1062. (M)
RT IB FLAP LOWER SKIN HAS A DENT 2 INCHES X 2.5 INCHES AND .077 INCH DEEP. DENT IS 24 INCHES FROM IB EDGE AND 2 INCHES FROM TRAILING EDGE. REPAIRED RT IB FLAP LOWER SKIN BY INSTALLING FLUSH REPAIR IAW BRAS EO. (K)
RT AFT FUSELAGE SKIN AT FS 590, 11 INCHES BELOW LOW PRESSURE EXT AIR DOOR HAS DENT AND GOUGE. REPAIRED LOWER AFT FUSELAGE SKIN AT FS 590 BETWEEN STRINGERS 21L AND 25R BY REMOVING EXISTING REPAIR AND INSTALLING A LARGER EXTERNAL DOUBLER IAW BRAS EO. (K)
DOOR SEAL IS LOUD ABOVE 6 DP. VIBRATION NOISE STARTS AT 270 KNOTS IAS. REMOVED AND REPLACED PASSENGER DOOR SEAL. PRESSURE CHECK GOOD. (M)
ENGINE 2 VIBRATION EXCEEDED LIMITS AT V1 WITH CONSTANT AIRFRAME VIBRATION INDICATION GOT OVER 3. REMOVED AND REPLACED NR 2 ENGINE DUE TO HIGH VIBRATION IAW AMM 72-10. (M)
FUSELAGE SKIN DAMAGED AT FS 621 BETWEEN STRINGERS 22L AND 25L. RE-CONTOURED SKIN, PERFORMED EDDY CURRENT INSPECTION AND RETURNED EXTERIOR FINISH TO THE ORIGINAL OPERATING CONFIGURATION IAW WVAC EO 601R-53-4350A. (M)
FUSELAGE SKIN DAMAGED AT FS 605 BETWEEN STRINGERS 24L TO 25L. RECONTOURED SKIN, PERFORMED EDY CURRENT INSPECTION AND RETURNED EXTERIOR FINISH TO THE ORIGINAL OPERATING CONFIGURATION IAW WVAC EO 601R-53-435OA. (M)
FOUND FRAME AT FS 589 SKIN FLANGE BETWEEN STRINGERS 24L AND 25L IS DAMAGED AND FLANGE BETWEEN STRINGERS 25L AND 26L IS DAMAGED. REMOVED FLANGE, FABRICATED REPAIR FLANGES FROM 2024 T3 .050 INCH WVAC PO NR 29699/1, FABRICATED FILLER SHIMS FROM 2024 T3 .090 INCH WVAC PO NR 25026/1, AND INSTALLED REPAIR PARTS WET USING PR1422B 1/2 AND FASTENERS MS20426AD-S IAW CRJ200 SRM 53-00-51 REPAIR NR 2. (M)