N440AW

Part: STIFFENER — CRACKED (FS 516.00) · airframe 39,467 hrs · 37,956 cycles

ANGLE STIFFENER AT FS 516, ON RH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE **** REMOVED CRACKED ANGLE STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON RH BL 45.00 IAW ED# AWAC-CRJ 253-01818

Part: NONE — NONE · airframe 39,467 hrs · 37,956 cycles

PREVIOUS BULKHEAD REPAIR, WAS NON-COMPLIANT WITH REO 601R-53-61-1240 NOTE 20 ****AIRCRAFT REMOVED FROM SERVICE **** REPAIRED AFT PRESSURE BULKHEAD IAW 601R-53-61-7793

Part: NONE — CRACKED (FS 516.00) · airframe 39,467 hrs · 37,956 cycles

ANGLE STIFFENER AT FS 516.00, ON LH BL 45.00 IS CRACKED AS MARKED ****AIRCRAFT REMOVED FROM SERVICE*** REMOVED CRACKED STIFFENER AND INSTALLED NEW ANGLE STIFFENER AT FS 516.00 ON LH BL 45.00 IAW ED# AWAC-CRJ253-01817

Part: LINE — DISCONNECTED (WATER SEPARATOR) · airframe 38,453 hrs · 36,906 cycles

CLIMBING THROUGH FL19.5 RECEIVED CABIN ALTITUDE CAUTION. INITIATED DESCENT AND RECEIVED CABIN ALT WARNING, LITTLE TO NO AIRFLOW FELT IN COCKPIT, C/W QRH IN ITS ENTIRETY. ***AIRCRAFT REMOVED FROM SERVICE*** RE-SECURED LINE TO WATER SEPERATOR REF AMM SUP 15-132A, LEAK CHECK GOOD WITH UNPRESSURIZED A/C USING APU.

Part: SEAL — DAMAGED (PAX DOOR) · airframe 38,372 hrs · 36,820 cycles

PASSING THROUGH 8000 MSL CLIMBING, PAX DOOR HAD VERY LOUD NOISE OF AIR RUSHING OUT OF A/C. PRESSURIZATION OF A/C COULD NOT KEEP UP. BELIEVE A/C WAS PRESSURIZING. LOUD NOISE OF AIR CONTINUED THROUGHOUT ARRIVAL. RETURNED TO IAD. ***AIRCRAFT REMOVED FROM SERVICE*** R&R PAX DOOR SEAL IAW AMM 52-11-10 .REF 318911/ 1 FOR OPS AND LEAK CK.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 37,998 hrs · 36,394 cycles

PERFORMED SDI OF AFT PRESSURE BULKHEAD FWD FACE, IAW NDTM AWAC SUPPLEMENT 09-008 REV 41. PERFORMED EDDY CURRENT INSPECTION, IAW NDTM PART 1 51-20-06 REV 41. PERFORMED UT INSPECTION, IAW NDTM PART 4 53-61-153 REV 41. 5 EACH DISCREPANCIES. DISCREPANCY 1: FS 621 LBL 27.5 WL 108.5 TO 109 CRACK LENGTH .5". DISCREPANCY 2: FS 621 BL 00 WL 127.18 TO 135.43 CRACK LENGTH 8.25". DISCREPANCY 3: FS 621 BL 00 WL 112.93 TO 108.43 CRACK LENGTH 4.5". DISCREPANCY 4: FS 621 RBL 18.0 WL 131.93 TO 134.94 CRACK LENGTH 3". DISCREPANCY 5: FS 621 RBL 18.0 WL 110.18 TO 109.43 CRACK LENGTH .75". AIRCRAFT REMOVED FROM SERVICE. MODIFICATION OF AFT PRESSURE BULKHEAD WEB, IAW E.O E17/003/453 REV DATE SEP 28, 2018. TO BE ACCOMPLISHED ON AERSALE W/O002862 CARD NO 4EOAWA21045.

Part: INTERCOSTAL — CRACKED (BS 621 BULKHEAD) · airframe 37,998 hrs · 36,394 cycles

AFT PRESSURE BULKHEAD AT FS 621.00. RT INTERCOSTAL AT RBL 45.70 & S 14R HAS A CRACK. AIRCRAFT REMOVED FROM SERVICE. FABRICATED INTERCOSTAL P/N 601-35012-52 OUT OF .050" 7075 T6, REF SRM 53-61-17 REV 38. INSTALLED RT INTERCOSTAL, REF SRM 51-42-21 REV 38.

Part: SHROUD — CRACKED (RT LEADING EDGE) · airframe 37,998 hrs · 36,394 cycles

TWO CRACKS FOUND ON RT LEADING EDGE PANEL 630KL AT AROUND W/S 314.50. THE FIRST CRACK WAS 8.44" FROM THE INBOARD EDGE THAT MEASURED .7" AND THE SECOND CRACK WAS 6.75" FROM THE OUTBOARD EDGE THAT MEASURED 1.3". AIRCRAFT REMOVED FROM SERVICE. REMOVED SHROUD (PANEL 630KL). FABRICATED NEW SHROUD FROM 2024 T3 .016", REF CRJ 200 SRM 57-41-29 AND 51-40-11 REV 30. TREATED AND PRIMED, REF CRJ 200 SRM 51-21-11 & 51-21-06. INSTALLED SHROUD (PANEL 630KL) ON LEADING EDGE AT W/S 314.50, REF CRJ 200 SRM 51-42-10 REV 38.

Part: SKIN — DENTED (BS 660) · airframe 37,998 hrs · 36,394 cycles

DENT AT FS 660.9 & S22R-2", DENT MEASURED AT .5" L X .5" W X .005" D WITH A W/D=100 ADDITIONAL DENT IDENTIFIED ON AERSALE W/O 002862 CARD NO 453-900-501-N0002 FOUND AT FS 657.80 & S22R+2" THAT MEASURES .7"L X .7"W X .009"D WITH A W/D=77. BOTH DENTS ARE NOT WITHIN ALLOWABLE LIMITS FOR BEING IN ADJACENT BAYS, REF CRJ 200 SRM 53-00-31 FIG 103 SH 3 AND SH 4. AIRCRAFT REMOVED FROM SERVICE. CUT DAMAGE AREA OUT 7" X 4.8" HFEC PERFORMED, NO DEFECTS NOTED. FABRICATED 8"X 8.5" DOUBLER, AND FILLER FROM 2024 T3 .063" INSTALLED PERMANENT REPAIR BETWEEN FS 654.5 TO 672.2 & S22R, REF CRJ 200 SRM 53-00-31 REPAIR 3 REV 38.

Part: SKIN — DENTED (BS 679.8) · airframe 37,998 hrs · 36,394 cycles

DENT AT FS 679.8 & S22R-1 THAT MEASURES .8" L X .8" W X .006" D WITH A W/D=133 AND IS LESS THAN 1" FROM S22R. DENT IS NOT WITHIN ALLOWABLE LIMITS, REF CRJ 200 SRM 53-00-31 FIG 103 SH 3 AND SH 4. AIRCRAFT REMOVED FROM SERVICE. CUT DAMAGE AREA OUT 1.5" X 1.2" W CUTOUT HFEC NO INDICATIONS NOTED AT THIS TIME. FABRICATED REPAIR DOUBLER 4.5" L X 4.5" W FROM 2024 T3 .063". INSTALLED DOUBLER, REF CRJ 200 SRM 53-00-31 REPAIR 3 REV 38.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 37,778 hrs · 36,173 cycles

EN ROUTE TO SAV, THE FLIGHT EXPERIENCED A RH WINDSHEILD HEAT CAUTION MESSAGE. AFTER FOLLOWING THE QRH, THE MESSAGE PERSISTED. THE FLIGHT COULD NOT CONTINUE TO SAV DUE TO ICING CONDITIONS, DIVERTED TO DAY FOR REPAIR. AIRCRAFT REMOVED FROM SERVICE TROUBLESHOT AND REMOVED AND RPELACED RHJ WINDSHIELD TEMP CONTROLLER IA W AMM 30-41-01. OPS CHECK GOOD.

Part: ELEVATOR SYSTEM — ABNORMAL

ON TAKE OFF AC REQUIRED EXCESSIVE BACK PRESSURE TO ROTATE. ELEVATOR CONTROLS FEEL HEAVY AND SLOW TO REACT TO CONTROL WHEEL INPUTS. AC CAN BE TRIMMED FOR FLT. DID NOT ENGAGE AUTOPILOT. THERE IS SLACK IN THE CONTROLS (EXCESSIVE HYSTERESIS) COORDINATED WITH DISPATCH AND DECIDED TO DIVERT WITH NO EMERGENCY AND DID NOT LAND OVER WEIGHT.

Part: LANDING — CRACKED (FUSELAGE) · airframe 34,811 hrs · 33,355 cycles

LT TRU DOOR AFT LATCH CUTOUT ON PNL LANDING CRACKED.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,811 hrs · 33,355 cycles

REPAIR FS193-FS202.75 STGR16L COCKPIT LT SIDE SKIN BETWEEN FS193.00 - FS210.0 AND STGR16L-STGR20L (RVSM AREA).

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,811 hrs · 33,355 cycles

STR 15L FS 621-625 INTERCOSTAL MEMBER AT FS 621 BULKHEAD AFT FACE IS CRACKED. REPLACED.

Part: GUIDE — DAMAGED (TE FLAP) · airframe 34,811 hrs · 33,355 cycles

LT WING OUTBD FLAP, INBD FLAP ROLLER GUIDE HAS ABRASION/WEAR. REPLACED

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,811 hrs · 33,355 cycles

FS313 RT FLOOR SILL SPOT OF CORROSION FWD OF SERVICE DOOR.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 34,811 hrs · 33,355 cycles

LT I/B FLAP VANE HAS THREE L/E CHAFES.

Part: GUIDE PLATE — DENTED (TE FLAP) · airframe 34,811 hrs · 33,355 cycles

RIGHT I/B FLAP I/B HINGE ARM I/B FAIRING GUIDE PLATE IS DENTED.

Part: SKIN — CHAFED (RT AILERON) · airframe 34,811 hrs · 33,355 cycles

RIGHT AILERON UPPER CLOSEOUT SKIN CHAFED. REPLACED SKIN IAW SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,811 hrs · 33,355 cycles

STG 15L CLIP INTERCOSTAL AT FS621 BULKHEAD AFT FACE IS CRACKED.

Part: FITTING — CRACKED (COCKPIT) · airframe 34,811 hrs · 33,355 cycles

FLIGHT DECK WINDSHIELD CENTER POST LOWER LT FITTING IS CRACKED. REPLACED WINDSHIELD CENTER POST LOWER LT FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,811 hrs · 33,355 cycles

AT FS 280 AND LBL 9 CRACKED CLIP.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,811 hrs · 33,355 cycles

FS280 RBL9 FRAME HAS A CRACK.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,811 hrs · 33,355 cycles

FS280 LBL9 FWD FLOOR SUPPORT ANGLE CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,811 hrs · 33,355 cycles

LT SIDEWALL SEAT TRACK NR 4 CORRODED. REPLACED SEAT TRACK NR 4 IAW SUPP 13-074 AND AMM 53-01-11.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 34,811 hrs · 33,355 cycles

ELONGATED HOLE IN FLOOR STRAP AT FS559.00, LBL38. REPLACED STRAP IAW SRM 51-45-00, 51-42-06.

Part: SKIN — GOUGED (TE FLAP VANE) · airframe 34,811 hrs · 33,355 cycles

LT WING AT WS264, O/B FLAP FIXED VANE L/E SKIN GOUGED. REPLACED SKIN IAW SRM 51-42-13.

Part: SKIN — DENTED (TE FLAP) · airframe 34,811 hrs · 33,355 cycles

RIGHT O/B FLAP LOWER SKIN IS DENTED. REPAIRED FLAP IAW REO 601R-57-53-1125 REV-B.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 34,811 hrs · 33,355 cycles

RT I/B FLAP VANE, I/B AND O/B LEADING EDGE CHAFED. REPLACED I/B SKIN AND REPAIRED O/B SKIN IAW REO M601R-57-52-004 AND SRM 51-42-13.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 34,473 hrs · 33,010 cycles

DEPARTING TYS GEAR DISAGREE WARNING. NOSE DOOR OPEN. NOSE GEAR DOWN. DID NOT RETRACT. FOLLOWED QRH & MANUAL GEAR EXTENSION. GEAR HANDLE DOWN. GEAR EXTENDED. 3 GREEN. EMERGENCY EXTENSION HANDLE STOWED. LANDED AT 46,500 SMOOTHLY. BTMS READS 3-2-1-2. ADJUSTED NOSE LANDING GEAR PROX SENSOR CENTERING/EXTENDED IAW AMM 32-61-05-05, OPS CHECK GOOD. RETRACTION CHECK GOOD,

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 33,038 hrs · 31,589 cycles

FLOOR EMERGENCY LIGHTS WILL NOT REMAIN ILLUMINATED FROM ROWS 8-12. IT COMES ON THEN FADES OUT. SECURED THE CONNECTOR P40LY IAW 16-371A, OPS CHECKED GOOD.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 32,954 hrs · 31,511 cycles

4031 EMERGENCY LIGHTS NO ILLUMINATING PAST ROW 8 TO THE BACK OF AIRCRAFT ON FLOOR. FOUND CONNECTORS P40LY AND P39LY BAD. REMOVED AND REPLACED BOTH CONNECTORS IAW AMM 16-371A, OPS CHECKED GOOD,

Part: CONTROL HANDLE — FAILED (MLG) · airframe 32,399 hrs · 31,023 cycles

FLT.4127, NO GEAR MOVEMENT AFTER LANDING GEAR LEVER BROUGHT UP. NO GEAR DISAGREE MESSAGE. ALL LANDING GEAR INDICATION LIGHTS STAYED GREEN. PARKING BRAKE SOV CAUTION MESSAGE APPEARED WHEN GEAR LEVER SELECTED UP, CLEARED WHEN GEAR LEVER SELECTED DOWN. ANTISKID INBOARD CAUTION MESSAGE APPEARED WHEN GEAR LEVER SELECTED UP. CLEARED WHEN GEAR LEVER SELECTED DOWN. R & R LANDING GEAR CONTROL HANDLE IAW AMM 32-31-01, REQUIRES LANDING GEAR RETRACTION CHECK IAW AMM TASK32-30-00-720-801. PERFORMED LANDING GEAR RETRACTION FUNCTIONAL TESTED IAW AMM 32-30-00-720-801, OPS CHECKED GOOD. OPS CHECKED PARK BRAKE SOV IAW AMM 32-45-11, OPS CHECKED GOOD. OPS CHECK ANTIISKID CONTROL SYSTEM IAW AMM 32-44-00, OPS CHECKED GOOD

Part: DOOR — STUCK (CABIN) · airframe 31,270 hrs · 29,972 cycles

SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE.

Part: PIN — OUT OF ADJUST (SERVICE DOOR) · airframe 31,131 hrs · 29,843 cycles

SERVICE DOOR OUTER HANDLE PUSH TO RELEASE BUTTON STUCK. ADJUSTED SERVICE DOOR OUTER HANDLE RETENTION PIN AS REQUIRED. OPERATIONS CHECKED GOOD IAW AMM 52-41-03.

Part: SHAFT — CRACKED (SERVICE DOOR) · airframe 31,113 hrs · 29,838 cycles

SERVICE DOOR OUTER HANDLE WILL NOT OPEN FROM OUTSIDE USING PUSHBUTTON. INSPECTED SERVICE DOOR OUTER HANDLE & LUBRICATED IAW SUPP 11-029B, NO FIX. FOUND CRACK IN OUTER SERVICE DOOR OUTER HANDLE SHAFT. DOOR CLOSES, LATCHES & LOCKS NORMALLY.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

FS FRAME 333.00, BETWEEN STRINGER 0 & 1L IS CRACKED. REPLACED FRAME 333.00 IAW SRM 51-40-11, 51-42-06, 51-42-21 & 53-21-15.

Part: STRAP — CORRODED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

SERVICE DOOR SILL T STRAP FS 349.00 HAS CORROSION.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,032 hrs · 29,760 cycles

FLOOR SUPPORT ATTACHMENT FITTING FS 349.00 AT RT SILL HAS CORROSION. REPLACED FLOOR SUPPORT ATTACHMENT FITTING AT FS 349.00 AT RT SILL IAW SRM 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,032 hrs · 29,760 cycles

FRAME 310.00 HAS CORROSION ON THE FWD & AFT SIDES, BETWEEN STRINGER 23R & 22R, IN THE FWD E & E BAY. REPLACED FRAME 310.00 IAW SRM 51-42-21, 51-42-06, 51-42-13, 51-21-11, 51-25-06 & 51-25-16.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,032 hrs · 29,760 cycles

FRAME 333.00 HAS CORROSION ON THE FWD SIDE, BETWEEN STRINGER 23R & 22R, IN THE FWD E & E BAY. REPLACED FRAME 333.00 SECTION, BETWEEN STRINGER 23R & 18R IAW SRM 51-42-06 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

AFT ACCESSORY COMPARTMENT STATION 621.0, BULKHEAD AFT SIDE LT INTERCOSTAL STRINGER 14L, CLIP IS CRACKED. REPAIRED IAW SRM 51-42-01.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

AFT ACCESSORY COMPARTMENT STATION 621, BULKHEAD AFT SIDE LT INTERCOSTAL STRINGER 13L, CLIP IS CRACKED. REPLACED IAW SRM 51-42-21.

Part: RETAINER — CRACKED (LT PYLON) · airframe 31,032 hrs · 29,760 cycles

LEFT PYLON PANEL 412DB HAS A CRACKED SEAL RETAINER. REPLACED SEAL RETAINER ON LT PYLON PANEL 412DB IAW SRM 51-42-06.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

AFT LOWER FUSELAGE SKIN, BETWEEN FS 654.0 & 672.20, STRINGER 26R - 27 HAS A DENT. REPAIRED AFT LOWER FUSELAGE SKIN IAW EA AWAC CRJ253 00359 REV IR DATED 04 16 2016.

Part: PLATE — CRACKED (THRUST REVERSER) · airframe 31,032 hrs · 29,760 cycles

RIGHT THRUST REVERSER PDU CONNECTOR PLUG MOUNTING PLATE IS CRACKED. REPLACED RT THRUST REVERSER PDU MOUNT PLATE IAW SRM 51-42-06.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,032 hrs · 29,760 cycles

PASSENGER DOOR SILL FWD CLEAT HAS CORROSION. REPLACED PAX DOOR FWD CLEAT IAW SRM 51-42-06 & 51-42-10.

Part: ATTACH BRACKET — CRACKED (TE FLAP) · airframe 31,032 hrs · 29,760 cycles

LEFT OTBD FLAP CTR HINGE ARM, OTBD FAIRING ATTACH BRACKET IS CRACKED. R & R ATTACH BRACKET IAW SRM 51-40-11, 51-42-06 & 51-25-16.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

CRACKED BRACKET UNDER PANEL 326CR. REPLACED BRACKET IAW SRM 51-24-21 & 51-11-20.

Part: ANGLE — CRACKED (RT WING) · airframe 31,032 hrs · 29,760 cycles

RIGHT WING INNER SHROUD CRACKED AT WS 143.189. R & R INNER SHROUD ANGLE IAW SRM 51-41-02, 51-42-10 & 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

FS 484.00 CLIP AT LBL 36 IS CRACKED. REPLACED FS 484.00 CLIP AT LBL 36 IAW REO 601R-53-41-059 REV B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

RIGHT OBLIQUE INTERCOSTAL FS 625.00 IS CRACKED. REPLACED RT OBLIQUE INTERCOSTAL IAW SRM 51-42-21.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 31,032 hrs · 29,760 cycles

PASSENGER DOOR AFT RISER SUPPORT ANGLE IS CRACKED. REPLACED DAMAGED SECTION OF PAX DOOR AFT RISER SUPPORT ANGLE IAW REO 601R-52-11-513 REV B.

Part: RETAINER — CRACKED (RT PYLON) · airframe 31,032 hrs · 29,760 cycles

RIGHT PYLON PANEL 422DB HAS A CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW CMM 20-40-11 & 20-42-03.

Part: ATTACH FITTING — CRACKED (COCKPIT) · airframe 31,032 hrs · 29,760 cycles

PILOTS WINDOW SIDE POST LOWER AFT ATTACH FITTING IS CRACKED. REPLACED PILOTS WINDOW LOWER AFT FITTING IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,032 hrs · 29,760 cycles

LEFT SIDE WALL SEAT TRACK STICK NR 8 HAS CORROSION, BETWEEN FS 559+16 & 559+80 IN THE CABIN. REPLACED SEAT TRACK NR 8 ON LT SIDEWALL IAW SRM 51-41-02 & AMM 53-01-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

FS 484.00 CLIP AT LBL 27 IS CRACKED. REPLACED FS 484.00 CLIP AT LBL 27 IAW SRM 51-42-21, 51-40-11, 53-41-43 & REO 601R-53-41-059 REV B.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,032 hrs · 29,760 cycles

SYSTEM 2 HYD ACMP CASE DRAIN FILTER BRACKET IS CRACKED. REPLACED BRACKET FOR NR 2 HYD ACMP CASE DRAIN FILTER IAW SRM 51-42-06.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (RT WING) · airframe 27,737 hrs · 26,565 cycles

ON TAKEOFF ROLL RECEIVED RT WING ANTI-ICE CAUTION MSG. ABORTED TAKEOFF 80KTS. 14TH STAGE ISOLATION VLV WOULD NOT OPEN. STBY MODE IS OPERATIVE.

Part: PRESSURE SWITCH — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 27,737 hrs · 26,565 cycles

IN FLIGHT RECEIVED RT WING ANTI-ICE CAUTION MSG IN STBY MODE. 14TH ISO WAS INTERMITTENT, OPEN & CLOSED. PICKING UP ICE ON RT WING WHILE RT WING ANTI-ICE MSG WAS OUT, WING SHOULD BE HEATING & WING & COWL ADVISORY MSG'S WERE ON NORMAL MODE IS ON MEL. EMER DECLARED. R & R RT PRESS SWITCH IAW AMM 30-12-00. OPERATIONS CHECK OF NORM MODE IS GOOD. PLACARDED & PLACED ON MEL. SN OFF 3018 & SN ON 4785.

Part: SCREW — LOOSE (WINDOW HEAT) · airframe 26,466 hrs · 25,355 cycles

FIRST OFFICER`S WINDSHIELD HEAT TERMINAL BLOCK COVER SMOKING INFLIGHT, WINDSHIELD HEAT OFF SMOKING STOPPED. INSPECTED & FOUND LWR TERMINAL BLOCK SCREW LOOSE CAUSING MOVEMENT & ARCING. SCREW, TERMINAL & TERMINAL BLOCK SHOW EVIDENCE OF DAMAGE FROM ARCING. FOUND ONE WASHER & SPACER MISSING. INSPECTED FIRST OFFICER`S WINDSHIELD & FOUND NO EVIDENCE OF DELAMINATION OR ARCING DAMAGE IAW AMM 56-11-01. PLACED ON MEL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,466 hrs · 25,355 cycles

INTERMITTENT ELEC ODOR DURING CRUISE FLIGHT, ODOR WAS ASSOCIATED WITH COCKPIT AREA ONLY & DECREASED IN INTENSITY AT LWR ALTITUDE. INSPECTED AREA FOR ODORS IN AVIONICS BAY, JUNCTION BOX 1 AREA, COCKPIT, THROUGH BAY & AFT EQUIPMENT BAY. NOTHING UNUSUAL NOTED. RAN AIR CONDITIONING PACKS, BOTH DISPLAY COOL FANS, BOTH ARINC FANS & WINDSHIELD HEATS. NO DEFECTS NOTED. MDC SHOWED NO FAULTS & NO CIRCUIT BREAKERS FOUND TRIPPED. UNABLE TO DUPLICATE PROBLEM.

Part: SKIN — PUNCTURED (RT JET PIPE) · airframe 26,211 hrs · 25,117 cycles

RIGHT JET PIPE FAIRING OUTER SKIN NEAR UPPER INBD MOUNT IS PUNCTURED. REPAIRED DAMAGE AREA NEAR UPPER INBD MOUNT ACCESS PANEL IAW CMM 78-11-00 REPAIR SRS 062.

Part: SUPPORT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 26,211 hrs · 25,117 cycles

PAX DOOR TOP STEP AFT SUPPORT IS CORRODED. REPAIRED TOP STEP AFT SUPPORT IAW EA 15-2014-077.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,211 hrs · 25,117 cycles

FUSELAGE SKIN CRACKED AT FS 235, RT AFT RADIUS OF NLG CUT OUT. REPAIRED IAW REO 601R-53-11-048 REV C DATED 2008-10-01.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 26,211 hrs · 25,117 cycles

PAX DOOR POWER ASSIST MOTOR LOWER SUPPORT IS CRACKED. R & R PAX DOOR ASSIST MOTOR LOWER SUPPORT BRACKET PN 601R317745-7.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 26,211 hrs · 25,117 cycles

CARGO DOOR FWD TRACK LOWER ATTACH BRACKET IS CRACKED. R & R BRACKET PN 601R35050-25 IAW SRM 51-40-11 & 51-42-06.

Part: SEAL — CRACKED (LT SPOILER) · airframe 26,211 hrs · 25,117 cycles

LEFT FLIGHT SPOILER SPRING SEAL CRACKED. REMOVED UNSERVICEABLE SEAL & INSTALLED SERVICEABLE SEAL IAW SRM 51-42-06 & 51-42-21.

Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 26,211 hrs · 25,117 cycles

CARGO DOOR LOWER SEAL RETAINERS CRACKED & GOUGED. R & R SEAL RETAINERS PN CC670-38742-1 & CC670-38746-1 IAW SRM 51-40-11 & 51-42-06.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,211 hrs · 25,117 cycles

THREE EACH TIE DOWNS ON LBL 27 AT FS 574 TO 559+96 HAVE CORROSION. R & R THREE EACH TIE DOWNS ON LBL 27 AT 574 TO 559+96 IAW AMM 2021-00.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 26,211 hrs · 25,117 cycles

54527-8000-0017 PAX DOOR FWD STAIR SUPPORT PANEL CRACKED AT LOWER RISER. REPAIRED IAW SUPPLEMENT 13-134 DATED 12/9/2013.

Part: RETAINER — CORRODED (E&E BAY) · corrosion level 2 · airframe 26,211 hrs · 25,117 cycles

AVIONICS BAY DOOR SEAL RETAINERS CORRODED. R & R SEAL RETAINERS PN CC670-38662-5, CC670-38663-5, CC670-38674-3 & CC670-38675-3.

Part: BRACKET — CRACKED (RT WING) · airframe 26,211 hrs · 25,117 cycles

RIGHT LE TRANSITION DUCT OTBD BRACKET CRACKED. R & R BRACKET PN 600-12045-12 IAW SRM 51-40-11 & 51-41-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,211 hrs · 25,117 cycles

RIGHT SEAT TRACK HAS CORROSION AT FS 559+96 TO 554.00. REMOVED & INSTALLED NEW SERVICEABLE SEAT TRACK IAW SRM 53-41-49, 51-29-36 & 51-41-02.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 26,211 hrs · 25,117 cycles

54527-8000-0043 PAX DOOR AFT STAIR SUPPORT PANEL CRACKED AT PREVIOUS REPAIR. REMOVED EXISTING DOUBLER & REPAIRED PAX DOOR AFT STAIR SUPPORT PANEL IAW REO 601R-52-11-702 REV C DATED 2010-03-09.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,211 hrs · 25,117 cycles

REPAIR APU INLET DOOR ACT SUPPORT 13-085B. R & R DOOR ACTUATOR SUPPORT INTERCOSTAL IAW SRM 51-41-00, 51-40-11, 51-25-16 & 51-41-04.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 26,211 hrs · 25,117 cycles

CARGO DOOR OUTER HANDLE HOUSING CRACKED. R & R CARGO DOOR OUTER HANDLE HOUSING PN H3415-31 IAW SRM 51-40-11 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,211 hrs · 25,117 cycles

ONE EACH TIE DOWN ON RBL 9 AT FS 559+112 HAS CORROSION. R & R CORRODED SEAT TRACK WITH NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,211 hrs · 25,117 cycles

FLOORBEAM CAP CORRODED, LBL 27 FROM FS 559+112 TO 621. R & R FLOORBEAM CAP SECTION, FS 567 TO 612 IAW SRM 51-40-11 & 51-42-21. REPAIRED CAP END FITTING AT FS 615 ON OTBD FLANGE OF LBL 27 FLOORBEAM CAP IAW EA 15-2014-070 DATED 3/31/2014.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 26,211 hrs · 25,117 cycles

ACFT GND POWER PLUG MOUNT BRACKET CRACKED. R & R BRACKET PN 600-33283-33 IAW SRM 51-40-11 & REO 601R-53-11-009 REV A.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 26,211 hrs · 25,117 cycles

FORWARD FACE OF FS 621 PRESS BULKHEAD HAS SCREW DAMAGE IN TWO PREVIOUSLY BLENDED & DENTED LOCATIONS, RT SIDE BETWEEN RBL 27 & RBL 45 APPROXIMATELY WL 75. REPAIRED TWO LOCATIONS ON FS 621 BULKHEAD IAW REO 601R-53-61-5252 DATED 2014-04-09.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,211 hrs · 25,117 cycles

TIE DOWN TRACK IN CARGO BAY, LBL 9 BETWEEN FS 559+112 & 574 IS CORRODED BEYOND LIMITS. R & R TRACK LBL 9 BETWEEN FS 559+112 & 574 WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-41-02.

Part: POST — CRACKED (FUSELAGE) · airframe 26,211 hrs · 25,117 cycles

FS 409+128 LT VERTICAL POST LOWER OTBD SIDE CRACKED. REPAIRED FS 409+128 VERTICAL POST IAW REO 601R-53-41-056.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,211 hrs · 25,117 cycles

CABIN FLOOR SUPPORT STRUCTURE FS 484 CLIP CRACKED AT RBL 27. R & R CLIP WITH SERVICEABLE CLIP IAW SRM 51-24-36, 51-40-11 & 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,211 hrs · 25,117 cycles

CLIP ON STRINGER 3L AT FS 280 IS CRACKED. R & R CLIP WITH SERVICEABLE PART IAW SRM 51-40-11 & 51-42-06.

Part: FLOOR SKIN — CRACKED (E&E BAY) · airframe 26,211 hrs · 25,117 cycles

54527-2000-0054 FWD EQUIPMENT COMPARTMENT FLOOR SKIN CRACKED AT FRAME FS 193 ON LT OTBD SIDE. REPAIRED IAW REO 601R-53-11-111 REV NC DATED 98 - MAR - 18.

Part: BRACKET — CRACKED (SERVICE DOOR) · airframe 26,211 hrs · 25,117 cycles

SERVICE DOOR INNER HANDLE PROX SWITCH BRACKET CRACKED. R & R BRACKET WITH SERVICEABLE PN 601R38723-17 IAW SRM 51-40-11 & 51-42-20.

Part: BRACKET — CRACKED (LT WING) · airframe 26,211 hrs · 25,117 cycles

LEFT WING LE CTR TRANSITION INBD BRACKET CRACKED. R & R BRACKET 600-12045-11 IAW SRM 51-40-11 & 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,211 hrs · 25,117 cycles

FLOOR SUPPORT JUST AFT OF PAX DOOR HAS CORROSION. R & R FLOOR SUPPORT WITH SERVICEABLE SUPPORT IAW SRM 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,211 hrs · 25,117 cycles

FLOOR SUPPORT BEAM RBL 9 INBD & OTBD ATTACH CLIPS AT FS 280 ARE CRACKED. R & R CLIPS IAW REO 601R-53-11-171 & SRM 51-40-11 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,211 hrs · 25,117 cycles

LEFT SEAT TRACK AT FS 364 THROUGH 394 HAS CORROSION. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 & SRM 53-21-49. REMOVED DAMAGED SEAT TRACK & INSTALLED NEW SEAT TRACK IAW SRM 51-41-00 & REO 601R 53-00-485.

Part: ANTENNA — MALFUNCTIONED (RADIO ALTIMETER) · airframe 24,942 hrs · 23,907 cycles

RECEIVED ERRONEOUS GPWS TERRAIN/ TERRAIN/ PULL UP WARNING ON CLIMB OUT. RAD ALT IND 700 FT AT 4000 FT. R & R RADIO ALTIMETER ANTENNA FWD POSITION IAW AMM 34-44-07 AND AWAC SUP 07-035A AND SUP 07-34E. OPS CHECK GOOD AT THIS TIME.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 24,717 hrs · 23,665 cycles

ELECTRICAL ODOR FROM ROWS 1-4 IN CEILING. INSPECTED ROWS 1-5 ABOVE CEILING PANELS FOR EVIDENCE OF ODOR/ANY SIGN OF DISCOLORED AREAS ON WIRES AND INSULATION. FOUND ROWS 2-3 LIGHT BULBS BLOWN SUSPECT BAD BALLAST. R & R BALLAST AND BULBS IAW AMM 33-21-04 AND 33-21-01. OP CHECKED GOOD, NO FURTHER ODOR NOTED NO OTHER DISCREPANCIESNOTED IN AREA. ACFT OK FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 23,360 hrs · 22,391 cycles

AFTER T/O FROM GSO, RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN MSG FLAPS WERE AT 8. RAN QRH. MSG'S WENT AWAY WHEN HANDLE WAS PLACED DOWN. LANDED AT 44600 GROSS, ROLL-OUT AND BRAKING WERE NORMAL. FERRY TO ORF.

Part: SILL — CORRODED (FS 310-349) · corrosion level 2 · airframe 21,473 hrs · 20,536 cycles

SERVICE DOOR LOWER SILL IS CORRODED ON THE AFT & END WHERE SILL IS RIVETED TO THE FLOOR CROSSBEAM. REPAIRED DAMAGED AREA IAW REO 601R-53-21-2283.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 21,473 hrs · 20,536 cycles

PAX DOOR EXTERNAL HANDLE CRACKED. R & R WITH NEW SERVICEABLE HANDLE PN 601R31763-1.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 21,473 hrs · 20,536 cycles

RT MLG DOOR CHAFED ON LOWER T/E. REPAIRED RT MLG DOOR CHAFED AREA AT T/E IAW REO 601R-52-82-334.

Part: FLOOR SUPPORT — CRACKED (FS 589) · airframe 21,473 hrs · 20,536 cycles

FLOOR SILL SUPPORT ANGLE AT LT FLOOR SILL FS 589 CRACKED. REMOVED UNSERVICEABLE SILL SUPPORT ANGLE AT LT FLOOR SILL FS 589 AND REPLACED WITH SERVICEABLE FLOOR SILL SUPPORT ANGLE IAW SRM 51-61-23 AND SRM 51-42-21.

Part: SILL — CORRODED (PAX DOOR) · airframe 21,473 hrs · 20,536 cycles

PAX DOOR CUT OUT LOWER SILL IS CORRODED IN SEVERAL PLACES ALONG THE ENTIRE LENGTH OF THE SILL. REMOVED CORRODED PAX DOOR LOWER SILL THEN FABRICATED NEW LOWER SILL AND INSTALLED IAW SRM 51-24-16, 51-40-02, 51-42-06, 51-42-13.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 21,473 hrs · 20,536 cycles

PAX DOOR CUT OUT LOWER SILL IS CORRODED IN SEVERAL PLACES ALONG THE ENTIRE LENGTH OF THE SILL. REMOVED CORRODED PAX DOOR LOWER SILL THEN FABRICATED NEW LOWER SILL AND INSTALLED IAW SRM 51-24-16, 51-40-02, 51-42-06.

Part: SILL — CORRODED (FS 574) · airframe 21,473 hrs · 20,536 cycles

CARGO DOOR SILL HAS CORROSION AROUND NUT PLATES ON TOP AND BOTTOM SIDES. REMOVED DAMAGED SECTION AND INSTALLED SERVICEABLE SECTION OF SILL IAW REO 601R-53-61-690, REV D IAW SRM 51-42-06, 51-40-11, 51-42-21.

Part: ANGLE — CRACKED (FS 484) · airframe 21,473 hrs · 20,536 cycles

REPAIR ANGLE AT FS 484, LBL 27 CRACKED. REPLACED 484 LBL 27 ANGLE WITH SERVICEABLE IAW REO 601R-53-41-099.

Part: BRACKET — CRACKED (FS 171) · airframe 21,473 hrs · 20,536 cycles

LEFT LOWER NOSE HYD COMPARTMENT AT NR 3 BRAKE ACCUMULATOR HAS A CRACKED FWD BRACKET. REMOVED UNSERVICEABLE BRACKET AND INSTALLED SERVICEABLE BRACKET IAW SRM.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 21,473 hrs · 20,536 cycles

RT MLG DOOR CHAFED ON LOWER L/E. REMOVED, FABRICATED, AND INSTALLED NEW FILLER FORM 412 IAW REO 601R-52-82-034.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 21,473 hrs · 20,536 cycles

LT MLG DOOR CHAFED ON LWR L/E. REMOVED UNSERVICEABLE FILLER AND INSTALLED SERVICEABLE FILLER IAW REO 601R-52-82-034, REV INC.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 16,910 hrs · 15,734 cycles

BRAKE PRESSURE TRANSDUCER BRACKET IN RT WHEEL WELL WALL IS CRACKED. R & R BRACKET PN 601R75262-157 IAW SRM 51-40-11, 51-23-00, 51-42-21, AND 51-21-16.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 16,910 hrs · 15,734 cycles

TOP SIDE OF LT AILERON L/T IS CHAFED. REPAIRED LT AILERON UPPER L/E SKIN IAW REO 601R-57-60-013 AND REO 601R-57-60-071.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 16,910 hrs · 15,734 cycles

NR 2 SYS RETURN FILTER BRACKET IS CRACKED. R & R HYD SUPPORT STRUCTURE INTERCOSTAL PN 600-75221-130 IAW SRM 51-42-06.

Part: COWLING — PUNCTURED (LT ENGINE) · airframe 16,910 hrs · 15,734 cycles

L/N LOWER CORE COWL INNER SKIN PUNCTURED AT 6" INBD OF FWD HINGE. REPAIRED LT LOWER CORE COWL INNER SKIN, 6" INBD OF FWD HINGE IAW CMM 71-12-01, REPAIR NR SRS046.

Part: COWLING — CHAFED (LT NACELLE) · airframe 16,910 hrs · 15,734 cycles

LT LOWER CORE COWL CHAFED IN CTR APPROX 6 " FROM DOME. REPAIRED IAW CMM 71-12-01, REPAIR NO SRS064 & REO 601R-71-12-3976.

Part: COWLING — PUNCTURED (LT ENGINE) · airframe 16,910 hrs · 15,734 cycles

LT LOWER CORE COWL INNER SKIN PUNCTURED IN CTR REPAIRED BY CUTOUT FILLER AND DOUBLER IAW CMM 71-12-01. REPAIR SRS046 AND REO 601R-71-12-3976, REV A.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 16,910 hrs · 15,734 cycles

RT AILERON UPPER SKIN L/E CHAFED. REPAIRED CHAFE DAMAGE IAW REO 601R-57-60-013, REV NC AND REO 601R-57-60-072 REV. ORIGINAL.

Part: SUPPORT BRACKET — CRACKED (LT MLG WW) · airframe 16,910 hrs · 15,734 cycles

BRAKE PRESSURE TRANSDUCER SUPPORT BRACKET IN LT MLG W/W IS CRACKED BRACKET. R & R IAW SRM 51-42-06.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 16,910 hrs · 15,734 cycles

FS 484, CLIP LBL 35" CRCKED. R&R CRACKED CLIP AT FS 484, LBL 35 WITH SERVICEABLE CLIP IAW REO 601R-53-41-059.

Part: PLATE — CRACKED (BS 589) · airframe 16,910 hrs · 15,734 cycles

CARGO FLOOR LANDING PLATE CRACKED AT FS 589. REPAIRED IAW REO 601R-53-61-433, REV B.

Part: DOOR — CHAFED (RT MLG) · airframe 16,910 hrs · 15,734 cycles

RT MLG DOOR CHAFED ON L/E. REPAIRED IAW REO 601R-52-82-102 SECTION A-A CUT IN Z MEMBER ONLY.

Part: BULKHEAD — DAMAGED (BS 280) · airframe 16,910 hrs · 15,734 cycles

DEEPLY GOUGED PN 2 PLACES APPROX 2` ABOVE FLOOR AT APPROX RBL 9 AFT SIDE COCKPIT ENTRY WAY. REPAIRED DAMAGED AREA AT 280 BULKHEAD APPROX 2` ABOVE FLOOR APPROX RBL 9 AFT SIDE COCKPIT ENTRY IAW REO 601R-53-11-1727, REV C.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,910 hrs · 15,734 cycles

FLOOR SUPPORT CRACKED AT FS 280 APPROX LBL 9 BY MLG MANUAL RELEASE CABLE PULLEY BRACKET REO 601R-53-11-138 CARRIED OUT.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 16,910 hrs · 15,734 cycles

FLOOR SUPPORT CRACKED AT FS 280 APPROX LBL 9 BY MLG MANUAL RELEASE CABLE PULLEY BRACKET REO 601R-53-11-137 CARRIED OUT.

Part: ATTACH FITTING — CHAFED (LT WING) · airframe 16,910 hrs · 15,734 cycles

LT OTBD FLAP OTBD HINGE BOX ATTACH FITTING IS CHAFED. REPAIRED LT OTBD FLAP HINGE BOX AFT FITTING BY BLENDING IAW REO 601R-57-21-1264 ORIGINAL ISSUE.

Part: CARBON SEAL — FAILED (STARTER) · airframe 15,591 hrs · 14,431 cycles

RT LOW OIL PRESS ON DESCENT. PRESS BELOW 25 PSI, RAN QRH. ACCOMPLISHED PRECAUTIONARY ENGINE SHUTDOWN. DECLARED EMERGENCY LANDING. REF MAINT W/O 142728 FOR ALL WORK PERFORMED. LEAK CHECK GOOD ON GROUND AT THIS TIME. REMOVED AND REPLACED IDG, EDP, AND AIR TURBINE STARTER CARBON SEALS IAW SUPP 05-018A. (K)

Part: WASHER — MISINSTALLED (WIRE LOCK RING) · airframe 15,364 hrs · 14,210 cycles

DURING ALL PHASES OF FLT FELT OCCASSIONAL ELEVATOR BINDING AND GRAB DURING PITCH CHANGES SPECIFICALLY WHEN PULLING BACK ON YOKE. BINDS/ GRABBING OCCURRED WITH A/P ON OR OFF. WHEN A/P ON THE BINDING/ GRABBING WAS VISIBLE BUT NO CHANGE IN PITCH OR ATTITUDE OCCURRED. BINDING/ GRABBING OCCURRED AT ALL ALTITUDES AND AIRSPEEDS AND DIDN`T VARY IN FORCE. NOTED BINDING OF YOKE IN NOSE UP POS FOUND WASHERS ON WIRE LOCK RING TO BE INSTALLED IMPROPERLY CAUSING WASHERS TO BIND AGAINST PITCH A/PILOT SERVO. PROPERLY INSTALLED HARDWARE FOR EFFECTIVITY IAW CMM 22-10-84. OPS CK GOOD. (K)

Part: ELEVATOR SYSTEM — STICKING · airframe 15,347 hrs · 14,193 cycles

DURING CLIMBOUT EXPERIENCED ELEVATOR STICKING AT 8,000 FT INTERMITTENTLY. UNAFFECTED BY ALTITUDE OR SPEED CHANGES OR AUTOPILOT ENGAGED OR DISENGAGES. NOT PRESENT BELOW 10,000 FT OR ON GROUND. (K)

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 15,275 hrs · 14,128 cycles

IN CRUISE AT 33000 FT, RECEIVED LT WINDSHIELD HEAT CAUTION MSG WINDSHIELD SHATTERED PRIOR TO COMPLETION OF QRH. REMOVED LT WINDSHIELD IAW AMM 56-11-01. REF LOG 191089/6 COMPLETED LT WINDSHIELD INSTALLATION IAW AMM CH 56-11, OPS AND LEAK CHECK GOOD. REF MX M/C NR 3 FOR INSTALLATION OF LT WIPER ARM. (K)

Part: EXTINGUISHER — DISCHARGED (CARGO BAY) · airframe 12,342 hrs · 11,349 cycles

CARGO BOTTLE LOWER MESSAGE IN FLIGHT. COMPLIED WITH QRH. R&R LT CARGO FIRE BOTTLE IAW AMM 26-25-01. CHECKS GOOD. NO AIR LEAKS FOUND AND NO SMOKE PRESENT IN CARGO BAY. OK FOR SERVICE.

Part: SWITCH — MALFUNCTIONED · airframe 12,047 hrs · 11,062 cycles

CPLT ROLL CMD MESSAGE ON ED2 INFLIGHT. GREEN CPLT ROLL LIGHT ILLUMINATED ON GLARESHIELD. ALL FLIGHT CONTROL RESPONDED NORMAL. REPLACED CO-PILOT ROLL PRIORITY SWITCH PER AMM 27-61-20. OPS TEST GOOD. ALSO, PERFORMED OPS TEST OF ROLL PRIORITY SYSTEM PER AMM TASK 27-61-20-710-810. NO DEFECTS NOTED. OK FOR SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY DOOR) · airframe 12,029 hrs · 11,042 cycles

RIGHT EMERGENCY DOOR OVERWING CAUTION MESSAGE IN CRUISE. COMPLIED WITH QRH MESSAGE DISAPPEARED AFTER LANDING AND AIRCRAFT DEPRESSURIZED. CLEARED PSEU FAULTS REF AMM 32-60-00 AND PRESSURIZED AIRCRAFT, NO DEFECTS NOTED AT THIS TIME, AIRCRAFT OK TO CONTINUE SERVICE. (M)

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY DOOR) · airframe 12,029 hrs · 11,042 cycles

RIGHT EMERGENCY DOOR CAUTION MESSAGE ON CLIMB-OUT AT 13,000 FT, NORMAL PRESSURIZATION. COMPLIED WITH QRH. (M)

Part: RETAINER — CRACKED (PANEL SEAL) · airframe 12,016 hrs · 11,029 cycles

RIGHT ENGINE, PYLON PANEL 422 DB SEAL RETAINER IS CRACKED. REPLACED IAW CRJ 200 SRM 51-42-06. (M)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 12,016 hrs · 11,029 cycles

FLOOR SUPPORT ANGLES AT FS 621, WL 73, LBL 40 AND RBL 40 ARE CRACKED. REPAIRED IAW REO 601R-53-61-117 REV C. (M)

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 12,016 hrs · 11,029 cycles

SERVICE DOOR SILL PLATE CORRODED. SERVICE DOOR SILL PLATE REPLACED IAW CRJ 200 SRM 51-41-04. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,016 hrs · 11,029 cycles

PAX DOOR AFT WEB DRAG ANGLE IS CRACKED. REPAIRED IAW REO 601R-52-11-513 REV A. (M)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 12,016 hrs · 11,029 cycles

CLIPS CRACKED ON INTERCOSTALS AT FS 484, RBL 27 AND RBL 36. INBOARD CLIP REPLACED IAW SRM 51-42-21, OUTBOARD CLIP, REPLACED IAW REO 601R-53-41-059. (M)

Part: SKIN — CRACKED (RT WING) · airframe 12,016 hrs · 11,026 cycles

RIGHT WING LE, 620AT, AT WS 140 EDGING IS CRACKED IN RADIUS. RIGHT WING INBOARD L/E (620AT) WS 140 SHROUD CRACK REMOVED IAW REO 601R-57-41-502. (M)

Part: STEP — CRACKED (PAX DOOR) · airframe 12,016 hrs · 11,029 cycles

PAX DOOR AFT SIDE PANEL, QTY TWO CRACKS EXIST AT 4 AND 5 STEP. PAX DOOR AFT SIDE PANEL REPAIRED IAW 601R-52-11-702 REV A. (M)

Part: CHANNEL — CRACKED (BS 574) · airframe 12,016 hrs · 11,029 cycles

AT FS 574 WL 73 QTY ONE CHANNEL OF CARGO DOOR SURROUND STRUCTURE IS CRACKED. CHANNEL AT FS 574, WL 73, REMOVED IAW CRJ SRM 51-42-06 CHANNEL FABRICATED AND TREATED IAW CRJ SRM 51-24-16 AND 51-21-11, 51-25-06 CHANNEL INSTALLED IAW CRJ SRM 51-42-06. (M)

Part: STEP — PUNCTURED (PAX DOOR) · airframe 12,016 hrs · 11,029 cycles

TOP STAIR ASSY IS PUNCTURED IN THE TREAD AREA. TOP STAIR ASSY PUNCTURED AREA REPAIRED IAW REO 601R-52-11-1457. (M)

Part: CARGO TRACK — CORRODED (BS 567) · airframe 12,016 hrs · 11,029 cycles

ONE CARGO TRACK CORRODED IN CARGO BAY AT FS 567 LBL 9. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06 OUT OF LIMITS IAW CRJ 200 SRM 53-61-49 THEREFORE SEAT RAIL AT FS 567 RBL 9. REPLACED IAW CRJ 200 SRM 51-40-11 AND 51-41-02. (M)

Part: SILL — CORRODED (BS 559-621) · airframe 12,016 hrs · 11,029 cycles

BTW FS 621 TO FS 559 PLUS 112, WL 73, FLOOR SILL IS CORRODED AT NUT PLATES LOCATION. CORROSION BETWEEN FS 559 PLUS 112 TO 621 WL 73 FLOOR SILL REMOVED IAW CRJ200 SRM 51-21-06 AND WITHIN LIMITS IAW SRM 53-61-23. (M)

Part: SHAFT — CORRODED (HATCH HANDLE) · airframe 12,016 hrs · 11,029 cycles

CREW ESCAPE HATCH OUTER HANDLE CORRODED ON SHAFT DURING C-CHECK. REPLACED HANDLE ASSEMBLY. (M)

Part: BRACKET — CRACKED (FUSELAGE) · airframe 12,016 hrs · 11,029 cycles

CARGO POST NET BRACKET COMMON TO FORWARD FACE CRACKED, LOWER BRACKET. BRACKET REMOVED IAW SRM 51-42-06, BRACKET FABRICATED IAW SRM 51-24-21 AND FABRICATED BRACKET INSTALL IAW SRM 51-42-06. (M)

Part: MANIFOLD — CRACKED (HYD SYSTEM) · airframe 12,016 hrs · 11,029 cycles

NR 2 HYDRAULIC MANIFOLD CRACKED ON AFT LOWER CORNER P/N 600-75221-130. NR 2 HYDRAULIC MANIFOLD SUPPORT BRACKET REPAIRED. (M)

Part: HINGE — CORRODED (DOOR STEP) · airframe 12,016 hrs · 11,029 cycles

PAX DOOR FOLDING STEP UPPER HINGE FOUND CORRODED. PAX DOOR FOLDING STEP UPPER HINGE REPLACED WITH SERVICEABLE ITEM IAW CRJ 200 SRM 51-40-11 AND 51-41-04. (M)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 12,016 hrs · 11,029 cycles

CRACKS ON FORWARD AND AFT ON PAX DOOR UNDER STEP PLATE. REPAIRED IAW REO 601R-52-11-279. (M)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,016 hrs · 11,029 cycles

CRACK FOUND ON FS 280 LBL 9 ON FLOOR STRUCTURE. REPAIRED IAW CRJ200 REO 601-53-11-171 REV D ON FS 280 LBL 9. (M)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,016 hrs · 11,029 cycles

CRACKS FOUND ON FS 280 RBL 9 ON FLOOR STRUCTURE. REPAIRED IAW REO 601R-53-11-1366 REV A. (M)

Part: DOOR — FAULTY (SERVICE DOOR) · airframe 11,751 hrs · 10,780 cycles

REQUEST INSPECTION FOR OPERATION OF SERVICE DOOR. (DOOR OPENS ABNORMALLY). (K)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 9,604 hrs · 8,719 cycles

SMOKE TOILET CASS MESSAGE AFTER TAKEOFF WITH LAV SMOKE ALARM ACTIVATED RAN QRH, MESSAGE EXTINGUISHED ALARM OFF F/A REPPORTED NO INDICATION OF SMOKE OR FIRE ON INSPECTION. RAN ENGINE WITH APU AIR SWITCH OVER TO BLEED AIR AND NO SMOKE CAUTION MESSAGE WITH EITHER APU OR ENGINE SUPPLYING PACKS NO EXTERNAL ENGINE OIL LEAKS NOTED. SUSPECT FAULTY LAV SMOKE DETECTION SYSTEM. REMOVED AND REPLACED SMOKE DETECTOR UNIT, OPS CHECK GOOD. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 8,783 hrs · 7,945 cycles

FLAPS FAILED TO EXTEND WHEN SELECTED ON APPROACH. COMPLIED WITH SUPPLEMENT 98-018A, FLAP RESET AND OPERATE NORMALLY. (K)

Part: COALESCER BAG — DIRTY · airframe 8,667 hrs · 7,831 cycles

DURING POST DE-ICING RUN UP, RECEIVED LAV SMOKE MESSAGE. COMP;IED WITH QRH AND MESSAGE CLEARED. PERFOMED LAV SMOKE DE4TECTOR TEST IAW AMM. OPPS CHECKED GOOD. REMOVED AND REPLACED COALESCER BAGS IAW AMM, OPS CHECK GOOD. NO MESSAGE OR SMOKE SMELL FOUND. (K)

Part: WIRE — LOOSE (MAP LIGHT) · airframe 8,757 hrs · 7,915 cycles

ENROUTE, SPARKS OBSERVED COMING FROM F/O`S YOKE MAP LIGHT. CB2U6 POPPED. LOOSE CONNECTION ON F/O`S MAP LIGHT FOUND. RESECURED LOOSE CONNECTION. OPS CHECK GOOD IAW 33-13-13. (K)

Part: DOUBLER — CRACKED (BS 640)

FOUND RIGHT SIDE FS 640 FRAME DOUBLER IS CRACKED AT STRINGER 10R APPROX 1 INCH LONG. MAINTENANCE REPAIRED BY PERFORMING JOB CARD 4EOMFG08415 AWAC EO E02/087/453 REV A INSPECTION AND MODIFICATION OF AFT FUSELAGE FRAME AT FS 640 BL 45 BETWEEN STRINGERS 9 AND 12. (M)

Part: SKIN — DENTED · airframe 7,060 hrs · 6,311 cycles

DENT FWD AND LT OF NOSE JACK POINT .8 INCH X 14 INCH AND .2500 INCH DEEP. CORRECTIVE ACTION IN PROGRESS. (K) MAINTENANCE REPAIRED FUSELAGE SKIN AT FS 272 STRINGER.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

FS 484 ANGLE CRACKED AT LBL 27 APPROX .5 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED CLIP IAW BSC STANDARD REPAIR 601R-53-0029A AND SRM 51-42-06, 51-42-21. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

FS 484 ANGLE CRACKED AT LBL 36 APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED FLANGE AT FS 484, LBL 36 IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

FS 280, LBL 9, IB CLIP IS CRACKED. (K) MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

FS 280, RBL 9 OB CLIP IS CRACKED. CA IN PROGRESS. (K) MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-42-13, AND BOMBARDIER STANDARD REPAIR 601R-53-0057A. (M)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

FS 280, LBL 9 OB CLIP IS CRACKED. (K) MAINTENANCE CRACKED CLIP AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ200 SRM 51-42-06, 51-42-21. (M)

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

FS 280, RBL 9 IB CLIP IS CRACKED. (K) MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-06, 51-42-21. (M)

Part: SKIN — CORRODED (RT WING) · airframe 7,060 hrs · 6,311 cycles

RT LWR WING PLANK HOLE NR 16, WS 303.861 HAS CORROSION AROUND ENTIRE CIRCUMFERENCE .002 INCH-.003 INCH DEEP. (K) MAINTENANCE REPAIRED RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT BY REMOVING CORROSION AND TREATING AREA AT PANEL 650HB, WS 303.861, HOLE NR 16 MAX DEPTH OF REPAIR WAS .003 INCH DEEP BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING) · airframe 7,060 hrs · 6,311 cycles

LT LWR WING PLANK, HOLE NR 11, WS 209.040, HAS CORROSION ON AFT OB SIDE 8.5 INCH L X .002 INCH, .003 INCH DEEP. (K) MAINTENANCE REPAIRED LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT PANEL 550CB, WS 209.040, HOLE NR 11 OUTBOARD EDGE BY REMOVING CORROSION TO A MAX DEPTH OF .003 INCH IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING) · airframe 7,060 hrs · 6,311 cycles

LT LWR WING PLANK HOLE NR 2, WS 12.245, HAS CORROSION AT IB SIDE 3.5 INCH L X .002 INCH-.003 INCH DEEP. (K) MAINTENANCE REPAIRED LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT PANEL 510AB, WS 12.245, HOLE NR 2 BY REMOVING CORROSION ON INBOARD EDGE TO A MAX DEPTH OF .003 INCH IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING) · airframe 7,060 hrs · 6,311 cycles

LT WING, LWR WING PLANK, HOLE NR 1, WS 54.897, HAS CORROSION AT IB SIDE 12 INCH L X .002 INCH-.003 INCH DEEP AND OB FWD SIDE 1 INCH L X .001 INCH - .002 INCH DEEP AND AT OB FWD SIDE 1 INCH L X .001 INCH- .002 INCH DEEP. (K) MAINTENANCE REPAIRED LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT PANEL 540BB, WAS 54.897 HOLE NR 1 INBOARD AND OUTBOARD EDGES BY REMOVING CORROSION TO A MAX DEPTH OF .003 INCH IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

LT LWR WING PLANK, HOLE NR 16, WS 303.861, HAS CORROSION AROUND ENTIRE CIRCUMFERENCE, .002 INCH- .003 INCH DEEP. (K) MAINTENANCE LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OUT AT PANEL 550HB, WS 303.861, HOLE NR 16 BY REMOVING CORROSION TO A MAX DEPTH OF .003 INCH IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)

Part: INTERCOSTAL — CRACKED (STR 14R) · airframe 7,060 hrs · 6,311 cycles

RT SIDE FS 621.0 TO FS 625.3 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. CORRECTIVE ACTION IN PROGRESS. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

LT SIDE FS 621.0 TO FS 625.3 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED FS 621 TO 625.3 INTERCOSTAL AT STRINGER 14L IAW CRJ SRM 51-42-06. (M)

Part: WEB — CRACKED (AFT FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

ENGINE SUPPORT BEAM LOWER WEB CRACKED LT SIDE FROM ACCESS PANEL NUTPLATE, APPROX FS 628, LBL 39, WL 111.09. (K) MAINTENANCE REPAIRED LOWER WEB BY INCORPORATION AWAC E02/081/453 MODIFICATION OF THE ENGINE SUPPORT BEAM (BOMBARDIER SERVICE BULLETIN A601R-53-059 REV D). (M)

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 7,060 hrs · 6,311 cycles

RT SIDE FS 640 FRAME DOUBLER IS CRACKED AT STRINGER 10R APPROX 1.0 INCH LONG. CORRECTIVE ACTION IN PROGRESS. (K)

Part: STRINGER — DAMAGED (S26L, FS280) · airframe 7,060 hrs · 6,311 cycles

STRINGER 26L, 10 INCHES FWD OF FS 280 IS DAMAGED. (K) MAINTENANCE REMOVED DAMAGED SECTION OF STRINGER 26L FROM FS 257 TO FS 272. FABRICATED SECTION OF REPAIR STRINGER AND SPLICES FROM P/N 600-33011-161. INSTALLED REPAIRED STRINGER AND SPLICES IAW BSC EO 601R-53-8695. (M)

Part: SKIN — DENTED (RT IB FLAP)

RT IB FLAP BOTTOM SKIN IS DENTED APPROX .7500 INCH LONG X .6250 INCH WIDE AND .040 DEEP WITH GOUGES IN CENTER OF DENT. DENT IS 1.7500 INCH FORWARD OF AFT EDGE AND 8 INCH OB FROM IB ENGINE. PERFORMED A MAJOR REPAIR BY CUTTING OUT DAMAGED SKIN AND INSTALLING DOUBLER AND FILLER IAW REO 601R-57-52-058, REV A.

Part: BUSHING — MIGRATED (MLG TRUNNION)

LT MAIN LANDING GEAR AFT TRUNNION BUSHING MIGRATED 0.005 INCH. REMOVED LT AFT MLG TRUNNION BUSHING IAW AMM 20-26-00-910-803. INSTALLED A NEW OVERSIZE (2ND) BUSHING PN 601R5721003-23. IAW REO 601R57-21-003B. REAMED INSIDE DIA TO 2.4384 IAW DWG 601R85007RWC.

Part: ENGINE — FAILED (NR 1)

UPON TAKEOFF NOTED NR 1 ENGINE ITT AT 900. DURING CLIMB NOTED ITT AT 858-874. AT FL280 HEARD THUMP AND NR 1 ENGINE SPOOLED DOWN. SECURED PER QRH AND COMPLIED WITH SINGLE ENGINE OPERATIONS. REMOVED AND REPLACED NR 1 ENGINE. SHOP REPORT REMARKS, REPLACED NR 3 BEARING AND FAN DRIVE SHAFT. TESTED ENGINE PER SEI - 756. (M)

Part: LINE — FAILED (OXYGEN MASK)

OXYGEN MASK SUPPLY LINE FAILED. COCKPIT 02 SUPPLY DEPLETED. INSTALLED NEW SUPPLY HOSE FROM OBSERVERS OXYGEN STORAGE BOX AND RECHARGED OXYGEN SYTEM TO 1520 PSI. NO FURTHER LEAKS NOTED. (M)