N461AW

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,247 hrs · 38,904 cycles

RECEIVED LH PACK HI PRESS DURING CLIMB WHILE TRANSFERRING BLEEDS. C/W QRH, MESSAGE REMAINED ON. ALSO HAD LH PACK FAIL ON OVERHEAD. *****AIRCRAFT REMOVED FROM SERVICE. FLT 6274 AIR RETURNED DUE TO MECHANICAL PROBLEMS-DECLARED EMER. ALSO DECLARED EMER DUE TO 2EA PX MEDICAL ISSUES**** R&R OF LH PRSOV FILTER IAW AWAC SUP 06-039A. OPS CHECK GOOD.

Part: FIRE BOTTLE — UNKNOWN (AFT EQUIPMENT BA) · airframe 40,220 hrs · 38,873 cycles

CARGO BOTTLE LOW CAUT MSG RCVD WHEN DESCENDING INTO ORD. CW QRH PROCEDURE LANDED WITHOUT FURTHER INCIDENT ******AIRCRAFT REMOVED FROM SERVICE******* REMOVED AND REPLACED LH CARGO FIRE EXT CONTAINER IAW AWA SUP 10-099B OPS CHECK GOOD S/N OFF 41462D1 S/N ON 47606D1

Part: NONE — NONE · airframe 38,901 hrs · 37,626 cycles

HYD SYSTEM 3 LO PSI INFLIGHT. SYNOPTIC PAGE SHOWED 0 QUANTITY AND 0 PSI WITH EITHER 3A OR 3B PUMPS RUNNING. HYD LEAK NOTED DURING WALK AROUND. NO OTHER HYD3 CAUTION MESSAGES DISPLAYED. ****AIRCRAFT REMOVED FROM SERVICE*** REF 345081/1, 345081/2, 345081,4, AND 345082/1 FOR REMOVAL AND REPLACEMENT OF HYD PUMPS 3A AND 3B SERFVICNING AND BLLED. AC OK FOR SERVICE

Part: NONE — NONE · airframe 38,731 hrs · 37,474 cycles

HYDRAULIC #2 LOW PRESS CAUTION SELECTING 20 DEGREES ON APPROACH. HYD 2 PRESSURE 0, HYD QUANTITY 0. PERFORMED QRH PROCEDURES AND LANDING DISTANCE CORRECTION. UNEVENTFUL LANDING IN ATW. 2010Z TO 2035Z WHEN ENGINE SHUTDOWN ON GROUND. ***AIRCRAFT REMOVED FROM SERVICE*** R&R HYD PUMP #2 REF WORK CARDS 3,4,6,9,11,10,12,1,2, AND 5 OF WO 311644 FOR CORRECTIVE ACTION. OPS AND LEAK CHECKS GOOD.

Part: SELECTOR VALVE — FAULTED (NLG) · airframe 38,249 hrs · 36,986 cycles

DURING APPROACH, WHEN SELECTING GEAR DOWN, RECEIVED GEAR DISAGREE. C/W QRH, MESSAGE CLEARED. ALL GEAR DOWN AND LOCKED BY MANUAL EXTENSION. NLG REMAINED UP INITIALLY. AIRCRAFT REMOVED FROM SERVICE, REF WO 307780 FOR WORK PERFORMED R/R NLG SELECTOR VALVE.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 37,818 hrs · 36,530 cycles

LEFT WING REAR SPAR WS 53.60 VERTICAL SUPPORT/ANGLE HAS CORROSION AT ELECTRICAL CONNECTOR THRU HOLES (2EACH) ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED SUPPORT ANGLE (PN 601R10203-33). UPON REMOVAL OF SUPPORT ANGLE ADDITIONAL CORROSION WAS DISCOVERED ON CHANNEL (PN 601R-10203-27). REMOVED CHANNEL FROM SUPPORT ANGLE. REMOVED CORROSION FROM ANGLE, ORIGINAL THICKNESS 0.080Ï¿½, 4 PLACES. 1) 1.4Ï¿½L X 0.250Ï¿½W X 0.001Ï¿½D 2) 0.450Ï¿½L X 0.400Ï¿½W X 0.003Ï¿½D 3) 2.600Ï¿½L X 0.800Ï¿½W X 0.004Ï¿½D 4) 5.600Ï¿½L X 2.200Ï¿½W X 0.008D. BLENDED DIMENSIONS WITHIN LIMITS IAW ASAP EA# AWAC-CRJ257-01601 REV IR DATED 4/15/2021. REMOVED CORROSION FROM CHANNEL, ORIGINAL THICKNESS 0.050Ï¿½, 1) 1.150Ï¿½L X 0.700Ï¿½W X 0.002Ï¿½D. BLENDED AREA WITHIN LIMITS IAW ASAP EA#AWAC-CRJ257-01602 REV IR DATED 4/15/2021.REINSTALLED SUPPORT ANGLE AND CHANNEL IAW CRJ 200 SRM 51-42-21.

Part: WEB — CORRODED (RWS 48.30) · corrosion level 2 · airframe 37,818 hrs · 36,530 cycles

RIGHT WING REAR SPAR WS 48.30 BATT RIB WEB HAS CORROSION AROUND UPPER LIGHTING HOLE FWD AND AFT SIDES AND AT THE BASE WHERE IT ATTACHES TO LOWER AFT ANGLE. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON RIGHT WING REAR SPAR WS 48.30 BATT RIB WEB, ORIGINAL THICKNESS 0.050", MATERIAL LOSS 0.002". WITHIN LIMITS REF ASAP EA@ AWAC-CRJ253-01600 REV A DATED 4/15/2021

Part: WEB — CORRODED (LWS 48.30) · corrosion level 2 · airframe 37,818 hrs · 36,530 cycles

LEFT WING REAR SPAR WS 48.30 BATT RIB WEB HAS CORROSION AROUND UPPER LIGHTING HOLE FWD AND AFT SIDES AND AT THE BASE WHERE IT ATTACHES TO LOWER AFT ANGLE. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON LH WING REAR SPAR WS 48-30 BATT RIB WEB, ORIGINAL THICKNESS 0.050", MATERIAL LOSS 0.004". WITHIN LIMITS REF ASAP AWAC EA# CRJ257-01599 REV A DATED 4/15/2021.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 37,818 hrs · 36,530 cycles

6 CRACKS WERE FOUND ON FS621.00 BULKHEAD WEB AT FS621.00 AS FOLLOWS: 1. FS 621 WL 91.0 - 91.50, RBL 27.50 CRACK LENGTH .50" 2. FS 621 WL 92.25 - 92.75, RBL 18.00 CRACK LENGTH .50" 3. FS 621 WL 101.50 - 102.00, RBL 27.50 CRACK LENGTH .50" 4. FS 621 WL 109.50 - 110.00, RBL 18.00 CRACK LENGTH .50" 5. FS 621 WL 98.00 Ï¿½ 99.25, LBL 27.50 CRACK LENGTH 1.25Ï¿½ 6. FS 621 WL 109.50 Ï¿½ 110.25, LBL 18.00 CRACK LENGTH .75Ï¿½ ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED BULKHEAD WEB AT FS621.00 WL 91.0 - 91.50, RBL 27.50, WL 92.25 - 92.75, RBL 18.00, WL 101.50 - 102.00, RBL 27.50, WL 109.50 - 110.00, RBL 18.00, WL 98.00 Ï¿½ 99.25, LBL 27.50 AND WL 109.50 Ï¿½ 110.25 LBL 18.00 IAW REO 601R-53-61-1285 REV E DATED 2016-10-31. REPAIRED BULKHEAD WEB AT FS621. WL 91.0 - 91.50, RBL 27.50, WL 92.25 - 92.75, RBL 18.00, WL 101.50 - 102.00, RBL 27.50, WL 109.50 - 110.00, RBL 18.00, WL 98.00 Ï¿½ 99.25, LBL 27.50 AND WL 109.50 Ï¿½ 110.25 LBL 18.00 IAW REO 601R-53-61-1285 REV E DATED 2016-10-31.

Part: SKIN — DENTED (BS 640 S23L) · airframe 37,818 hrs · 36,530 cycles

OUTWARD DENT ON FUSELAGE AT LEFT HAND FS 640.0+3 LEFT HAND STR 23-1. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED REPAIR ON FS 640.0+5 STR 23LH-1 REF ASAP EA# AWAC-CRJ253- 01596 REV A DATED 4/12/2021

Part: TRACK — GOUGED (CARGO DOOR) · airframe 37,818 hrs · 36,530 cycles

CARGO DOOR AFT UPPER TRACK HAS GOUGES AT LOWER END. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE, 1.2"L X 0.150"W X 0.025" D, WITHIN LIMITS, PERFORMED HFEC, NO INDICATIONS REF AWAC EA CRJ253-01597 REV IR DATED 4/10/2021.

Part: SKIN — DENTED (BS 672. S24R) · airframe 37,818 hrs · 36,530 cycles

OUTWARD DENT ON FUSELAGE AT RT HAND FS672.0+8 S24R+3. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED FUSELAGE AT FS 672.2+8 RT AND S24R+3 IAW ASAP EA# AWAC-CJ253-01598 REV A DATED 4/17/2021.

Part: WINGLET — DAMAGED (WS407.08) · airframe 37,818 hrs · 36,530 cycles

JOB CARD 4DMI23824 REPAIR LH WINGLET T/E REF GREO 601R-57-30-001 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED L.H WINGLET T/E, REPAIRED, REINSTALLED AND RESTORED PROTECTIVE FINISH REF GREO 601R-57-30-001 REV B DATED2019-07-16 AND AWAC EA# CRJ257-01595 REV IR DATED 4-7-2021

Part: SKIN — DENTED (FS 682) · airframe 37,818 hrs · 36,530 cycles

3 EACH OUTWARD DENTS WITHIN 1 INCH AT RIGHT HAND FS682.0+7.5 STR RIGHT 22, AIRCRAFT REMOVED FROM SERVICE. EVALUATED DENTS AT RH FS 682.00+7.5 STR 22R+3 AND FOUND OUT OF LIMITS REF CRJ200 SRM 53-00-31 REV 38. PERFORMED EXTERNAL NON-FLUSH PERMANENT REPAIR REF CRJ 200 SRM 53-00-31 REPAIR #3, REV 38. THIS REPAIR DOES NOT REQUIRE ADDITIONAL TOLERANCE INSPECTIONS. THE CURRENT INSPECTION PROGRAM IS NOT AFFECTED BY THE INSTALLATION OF THIS REPAIR.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 37,818 hrs · 36,530 cycles

REF 4DMI22779. REPAIR PAX DOOR SPRING HOLE REF 601R52-11-2715. AIRCRAFT REMOVED FROM SERVICE. TEMP REPAIR PERFORMED, REF REO 601R-52-11-2715 ON AAR WORK ORDER 1017223 JN 7130264, WAS FOUND TO BE STRUCTURALLY ACCEPTABLE AS A PERMANENT DISPOSITION REPAIR REF MHIRJ REO 601R-51-11-2866 REV -- DATED 2021-04-12

Part: SKIN — DAMAGED (BS 409 S1-2) · airframe 37,818 hrs · 36,530 cycles

SCRIBE MARKS ON TOP OF FUSELAGE AT FS 409.0+64 TO FS 409.0+80 STR L0+2 TO STR L1 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED SCRIBE MARKS ON TOP OF FUSELAGE AT FS 409.0+64 TO FS 409.0+80 STR R1 TO STR L1. WHERE ORIGINAL MATERIAL IS 0.058" THE LOWEST REMAINING THICKNESS IS 0.045, WHERE THE ORIGINAL MATERIAL IS 0.45" THE LOWEST REMAINING THICKNESS IS 0.042". ALL BLENDED AREAS WITHIN LIMITS IAW ASAP A# AWAC-CRJ253-01603 REV IR DATED 4/15/2021.

Part: ECU — FAILED (NLG STEERING) · airframe 37,634 hrs · 36,328 cycles

RECEIVED NOSE WHEEL STEERING INOPERABLE CAUTION MESSAGE IN FLT. CW QRH MESSAGE PERSISTS AFTER CYLLING NWS STEERING SW. GEAR WAS UP. AFTER LANDING SELECTED STEERING ON MESSAGE RETURNED. AIRCRAFT REMOVED FROM SERVICE. AC WAS TOWED TO THE REMOTE PAD. R & R NWS ECU, IAW AMM 32-51-10. SN OFF: 02-810 SN ON: 04-1039. R & R NLG STEERING HARNESS, IAW AMM 32-61-25. OPERATIONS CHECK GOOD.

Part: FILTER — DIRTY (COCKPIT DISPLAY) · airframe 36,671 hrs · 35,335 cycles

WHILE OPERATING WITH DISPLAY FAN #1 ON MEL CREW RECEIVED DISPLAY COOL CAUTION. C/W QRH AND MESSAGE DID NOT CLEAR. PERFORMED AIR RETURN TO FSD. AIRCRAFT REMOVED FROM SERVICE REMOVED FO PFD & MFD & CLEANED AIR FILTER IAW AMM 31-61-01. PERFORMED OPS CHECK OF DISPLAYS AND DISPLAY FANS IAW AMM 31-61-01 & 21-24-00. OPS CHECKS GOOD, COULD NOT DUPLICATE FAULT.

Part: NOT REPORTED — MALFUNCTIONED (AC BAY) · airframe 35,990 hrs · 34,700 cycles

IN CLIMB, AFTER TRANSFERRING TO ENGINE BLEEDS, NOTICED LIMITED AIRFLOW FROM COCKPIT GASPERS AND NO AIRFLOW FROM CABIN GASPERS. TURNED OFF LEFT PACK AND AIRFLOW IMPROVED SIGNIFICANTLY. AFTER LEVELING OFF AT FL250 RECEIVED RIGHT PACK HI-TEMP CAUTION. WHILE C/W QRH NOTICED CABIN ALTITUDE CLIMBING APPROX 1400 FT/MIN. PERFORMED EMERGENCY DESCENT WITH BOTH PACKS OFF. ON APPROACH TURNED RIGHT PACK BACK ON, AIRFLOW RETURNED TO NORMAL. AFTER LANDING RECEIVED RIGHT PACK HI-TEMP CAUTION AGAIN. LANDED AT APPROX 48,000LBS, LANDING WAS SMOOTH AND UNEVENTFUL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,654 hrs · 34,369 cycles

DURING APPROACH TO KORD, WHEN SELECTING FLAPS 30, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND LANDED WITHOUT FURTHER INCIDENT. ARFF ESCORTED THE AIRCRAFT TO THE GATE WHERE THE PASSENGERS DEPLANED NORMALLY WITH NO ADVERSE PASSENGER REACTIONS NOTED.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 3,558 hrs · 34,305 cycles

ON DEPARTURE SWAPPING BLEED RECEIVED R PACK HI PRESSURE MESSAGE. C/W QRH MSG CLEARED. CLIMBING THROUGH 17,000 FT R PACK AND R 10TH STAGE SOV DID NOT RESPOND TO 1ST RESET. ON 2ND ATTEMPT PACK RESET AND OPERATED APPROPRIATELY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,447 hrs · 34,169 cycles

DURING APPROACH TO KCHS, WHEN SELECTING FLAPS, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE WITH FLAPS AT 5 DEGREES. THEY CANCELED THE APPROACH, REQUESTED VECTORS FROM ATC, DECLARED AN EMERGENCY AS A PRECAUTION AND COMPLETED THE QRH. AIRCRAFT LANDED WITHOUT INCIDENT.

Part: HINGE — DAMAGED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

PAX DOOR FUSELAGE SIDE HINGE PIN HOLES ELONGATED. REPLACED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 35,444 hrs · 34,167 cycles

RT INBD FLAP VANE LEADING EDGE AT WS 60.0 IS CHAFFED. REPLACED.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 34,167 cycles

FS 280 WEB BETWEEN LBL 9 AND RBL 9 CORRODED. REPAIRED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

NOSE WHEEL WELL STATION 202 VERTICAL POST RBL 9 HAS CRACKED CLIP AT TOP OF POST REMOVED AND REPLACED NOSE WHEEL WELL STATION 202 VERTICAL POST RBL 9 CLIP AT TOP OF VERTICAL POST IAW SRM 51-42-06.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 34,167 cycles

FS 295 TO FS 310 STRINGER 16L INTERCOSTAL HAS CORROSION REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 34,167 cycles

FS 280 LBL 9 TO RBL 9 FWD ANGLE HAS CORROSION REMOVED ADN REPLACED FWD ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.

Part: DOOR SILL — DAMAGED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

FS 548.5 RBL 39 PRESSURE FLOOR SILL HAS ELONGATED FLOOR BOARD FASTENER HOLE REPAIRED PRESSURE FLOOR SILL AT FS 54835 RBL39 IAW 601R-53-41-2477.

Part: POST — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

409+128 VERTICAL POST AT BL18 LEFT SIDE IS CRACKED AT JOGGLE ON BOTH INBOARD AND OUTBOARD SIDES IN THE AFT RADIUS OF UPPER POST AREA REMOVED AND REPLACED BOTH INBOARD AND OUTBOARD VERTICAL POST AT 409+128 LBL 19 IAW REO# 601R-53-41-889.

Part: POST — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

409+128 VERTICAL PAST AT BL18 LEFT SIDE IS CRACKED AT JOGGLE ON BOTH INBOARD AND OUTBOARD SIDES IN AFT RADIUS OF UPPER POST AREA REMOVED AND REPLACED BOTH INBOARD AND OUTBOARD VERTICAL POST AT 409+128 LBL 18 IAW REO# 601R-53-41-889.

Part: ANGLE — CRACKED (RT WING) · airframe 35,444 hrs · 34,167 cycles

WING STATION 139.54 HAS CRACKED ANGLE ON THE LEADING EDGE PANEL 620JL REPLACED WS 139.54 ANGLE ON RH PANEL 620JL IAW SRM 51-41-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

FUSELAGE SKIN IS CRACKED AT THE NLG SPADE DOOR CUT OUT, RT AFT CORNER REPAIRED FUSELAGE SKIN AT THE NLG SPADE DOOR CUT OUT RH AFT CORNER IAW REO 601R-53-11-048.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 35,444 hrs · 34,167 cycles

RT MLG WHEEL WELL Z ANGLE ATTACHED TO PRESSURE FLOOR SKIN IS CRACKED IN RADIUS. REMOVED CRACKED RT MLG WHEEL WELL Z-ANGLE AND INSTALLED NEW Z-ANGLE IAW SRM 51-42-06, TR 51-42.

Part: SKIN — CHAFED (RT AILERON) · airframe 35,444 hrs · 34,167 cycles

RT AILERON LWR CENTER L/E CHAFFED. REMOVED & REPLACED RT AILERON LWR CENTER L/E SKIN IAW SRM 51-42-06 & 51-42-21.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

HYDRAULIC SYSTEM 2 PRESSURE AND RETURN MANIFOLD MOUNTING BRACKET CRACKED AT AFT LOWER CORNER. REPAIRED MOUNTING BRAKCET IAW REO 601R-53-62-031 REV A.

Part: BEAM — CHAFED (CARGO DOOR) · airframe 35,444 hrs · 34,167 cycles

AFT CARGO DOOR BEAM MEMBER GROOVED DUE TO CONTACT WITH DOOR CABLES REMOVED AND REPLACED AFT CARGO DOOR BEAM MEMBER IAW SRM 51-42-21.

Part: SKIN — CHAFED (LT AILERON) · airframe 35,444 hrs · 34,167 cycles

LT AILERON LWR CENTER L/E CHAFFED. REMOVED AND REPLACED LT LWR AILERON CENTER L/E SKIN IAW SRM 51-42-06 & 51-42-21.

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

TRU LT ACCESS PNL HAS CRACK UNDER AFT LATCH CUTOUT. REPAIRED IAW SUPP 19-016B.

Part: SKIN — CHAFED (LT AILERON) · airframe 35,444 hrs · 34,167 cycles

LT AILERON LWR CENTER L/E CHAFFED. REMOVED AND REPLACED LT LWR AILERON CENTER L/E SKIN IAW SRM 51-42-06 & 51-42-21.

Part: ANGLE — CRACKED (RT WING) · airframe 35,444 hrs · 34,167 cycles

WING STATION 143.189 HAS CRACKED ANGLE ON LEADING EDGE PANEL 630JL. REMOVED AND REPLACED CRACKED ANGLE IAW SRM 51-42-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,444 hrs · 34,167 cycles

LT FLOOR SEAT TRACK STICK 1 ON LBL 9 HAS CORROSION. REMOVED AND REPLACED LT FLOOR SEAT TRACK STICK #1 IAW SMM 53-01-11.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

AEB STR 15L OBLIQUE ANGLE IS CRACKED. REPLACED OBLIQUE ANGLE IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

FS 280 RBL 9 INBD CLIP CRACKED. REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

FS 280 BEAM AFT ANGLE AT RBL 12 CRACKED. REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,444 hrs · 34,167 cycles

AEB STR 13L INTERCOSTAL IS CRACKED. REMOVED AND REPLACED AEB STRINGER 13L INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG) · airframe 33,497 hrs · 32,268 cycles

AFTER GEAR RETRACTION, RECEIVED A NOSE GEAR DISAGREE INDICATED, RED ON SYNOPTIC PAGE. COMPLIED WITH QRH, MESSAGE CLEARED AFTER LANDING GEAR MANUAL RELEASE WAS USED AND LANDING GEAR LEVER SELECTED DOWN. MAX AIRPSEED WITH GEAR EXTENDED 200 KNOTS, ICING CONDITIONS WERE PRESENT. TROULBESHOT IAW SUPP 08-067, SWUNG GEAR MULTIPLE TIMES, NO FAULTS NOTED. ANALYZED FDR DOWNLOAD FOR ANY DISCREPANCIES, OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (LT NLG) · airframe 32,429 hrs · 31,196 cycles

AFTER TAKEOFF RECEIVED NWS INOPERATIVE CAUTION FOLLOWED BY WOW INPUT CAUTION. TRIED QRH FOR STEERING, NO SUCCESS. RAN QRH FOR WOW. AFTER LANDING CYCLED NOSE WHEEL STEERING, STEERING BECAME OPERATIVE. EMERGENCY WAS DECLARED, LANDING WAS SMOOTH, INTEROGATED PSEU FOUND FAULT FOR LT NLG WOW PROXIMITY SWITCH. INSPECTED LT NLG WOW PROXIMITY SWITCH IAW AMM 32-61-05 AND FOUND OUT OF ADJUSTMENT. PERFORMED RIGGED LT NLG WOW SWITCH PS13GA IAW AMM 32-61-05, OPS CHECKED GOOD AND GEAR SWINGS GOOD.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 32,138 hrs · 30,918 cycles

EMERGENCY LIGHTS ROW 8 AND AFT WILL NOT ILLUMINATE. FOUND COVER CRACKED AND WIRES CUT AT ROW 12. REPAIRED THE WIRES AND R & R THE CONNECTORS V77890 AND CABLE V32890 IAW ESPM 20-17 AND AMM 33-51-01. OPS CHECKED GOOD.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 32,137 hrs · 30,918 cycles

FRAME BS 333 HAS CORRODED AREAS ON THE FWD AND AFT SIDES BETWEEN STRINGERS 24L AND 24R

Part: STIFFENER — CRACKED (BS 280) · airframe 32,137 hrs · 30,918 cycles

STIFFENER CRACKED FWD SIDE OF BS 280, LBL 20, BELOW THE FLIGHT DECK FLOOR

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 32,137 hrs · 30,918 cycles

INTERCOSTAL CRACKED AT BS 621 TO 625, STRINGER 14L. REPLACED THE INTERCOSTAL IAW SRM 51-40-11.

Part: STRINGER — CRACKED (BS 379) · airframe 32,137 hrs · 30,918 cycles

STRINGER 3L, BS 379 IS CRACKED. REPLACED THE SECTION OF THE STRINGER IAW SRM 53-00-03.

Part: STIFFENER — CRACKED (JET PIPE FAIRING) · airframe 32,137 hrs · 30,918 cycles

RT JET PIPE FAIRING 446AL FWD STIFFENER IS CRACKED. REPAIRED THE STIFFENER IAW CMM 78-11-00.

Part: STIFFENER — CRACKED (JET PIPE FAIRING) · airframe 32,137 hrs · 30,918 cycles

RIGHT JET PIPE FAIRING 446AL, SECOND STIFFENER FROM FWD END IS CRACKED. REPAIRED THE STIFFENER IAW CMM 78-11-00.

Part: ATTACH BRACKET — CRACKED (BS 467) · airframe 32,137 hrs · 30,918 cycles

RIGHT WING TO BODY ATTACH BRACKET CRACKED AT BS 467. REPLACED ATTACH BRACKET IAW SRM 51-42-06, AND 51-42-21.

Part: ATTACH BRACKET — CRACKED (WING TO BODY) · airframe 32,137 hrs · 30,918 cycles

RIGHT WING UPPER WING TO BODY ATTACH BRACKET CRACKED AT BS 475. REPLACED THE ATTACH BRACKET IAW SRM 51-42-06, AND 51-42-21.

Part: ATTACH BRACKET — CRACKED (WING TO BODY) · airframe 32,137 hrs · 30,918 cycles

LEFT WING UPPER WING TO BODY FAIRING ATTACH BRACKET CRACKED AT BS 461. REPLACED THE ATTACH BRACKET IAW SRM 51-42-06, AND 51-42-02.

Part: ATTACH BRACKET — CRACKED (BS 449) · airframe 32,137 hrs · 30,918 cycles

RIGHT WING, UPPER WING TO BODY ATTACH BRACKET CRACKED AT BS 449. REPLACED THE ATTACH BRACKET IAW SRM 51-42-06.

Part: ATTACH BRACKET — CRACKED (WNG-BDY FAIRING) · airframe 32,137 hrs · 30,918 cycles

LEFT WING UPPER WING TO BODY ATTACH BRACKET CRACKED. REPLACED THE ATTACH BRACKET IAW SRM 51-41-02, AND 51-41-06.

Part: ATTACH BRACKET — CRACKED (BS 449) · airframe 32,137 hrs · 30,918 cycles

LEFT WING UPPER WING TO BODY ATTACH BRACKET CRACKED AT BS 449. REPLACED THE ATTACH BRACKET IAW SRM 51-41-02, AND 51-42-06.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,770 hrs · 30,572 cycles

BURNING ODOR NOTED IN CABIN BETWEEN ROWS 8 & 9.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 31,110 hrs · 29,977 cycles

PASSENGER DOOR WILL NOT CLOSE. ATTEMPTED TO CYCLE DOOR. DOOR WOULD NOT OPEN.

Part: UNKNOWN — MALFUNCTIONED (PAX DOOR) · airframe 30,847 hrs · 29,735 cycles

3974 PASSENGER DOOR DIFFICULT TO OPEN, F/O OPENED SERVICE DOOR AND WENT TO PASSENGER DOOR AND OPENED IT. EXTERNAL HANDLE HARD TO OPERATE ON PASSENGER DOOR.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 30,786 hrs · 29,683 cycles

F/A REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN, CLOSES FINE.

Part: CABLE — OUT OF POSITION (PAX DOOR) · airframe 30,702 hrs · 29,601 cycles

PAX DOOR DIFFICULT TO CLOSE, UNABLE TO LATCH. UPON INVESTIGATION FOUND LOWER CABLE OFF TRACK. RESECURED CABLE ON TRACK AS REQUIRED. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,606 hrs · 27,639 cycles

FLOOR EMER LIGHTS ROW 8 & BACKWARDS INOPERATIVE.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,530 hrs · 27,555 cycles

FLIGHT 3943, EMERGENCY LIGHTS BEYOND ROW 8 INOPERATIVE. R & R THE EMERGENCY LIGHT POWER CABLE IAW 33-51-01. OPS CHECKED GOOD.

Part: STALL WARNING — FALSE ACTIVATION (COCKPIT) · airframe 28,055 hrs · 27,082 cycles

ON CLIMB OUT AT 400FT AGL, RECEIVED STALL FAIL CAUTION MESSAGE. RAN QRH, SELECTED RIGHT SWITCH OFF. COMPLIED WITH FIM RESET, MESSAGE CLEARED.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 27,761 hrs · 26,796 cycles

LIGHTED PAX SIGN ON BULKHEAD FWD OF SEAT 1C, DETTACHED. R & R THE EMERGENCY EXIT SIGN IAW AMM 33-20-00. OPS CHECKED GOOD.

Part: DOOR SILL — CRACKED (FUSELAGE) · corrosion level 2 · airframe 27,458 hrs · 26,517 cycles

PAX DOOR LOWER SILL HAS CORROSION AROUND 2 NUTPLATES ON INBD SIDE.

Part: SKIN — CHAFED (LT AILERON) · airframe 27,458 hrs · 26,517 cycles

LEFT AILERON UPPER LE SKIN CHAFED.

Part: HEAT SHIELD — CRACKED (RT EXHAUST) · airframe 27,458 hrs · 26,517 cycles

RIGHT ENG EXHAUST FAIRING INNER HEAT SHIELD HAS TWO EACH CRACKS NEAR DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,458 hrs · 26,517 cycles

LBL 27 FLOORBEAM FITTING JUST FWD OF 621 BULKHEAD IS CORRODED.

Part: STIFFENER — CRACKED (RT EXHAUST) · airframe 27,458 hrs · 26,517 cycles

RIGHT ENG EXHAUST NOZZLE FAIRING SECOND STIFFENER FROM LE IS CRACKED.

Part: BRACKET — CRACKED (MLG WW) · airframe 27,458 hrs · 26,517 cycles

BRACK PRESS TRANSDUCER HYD LINE BRACKET IN WW IS CRACKED.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 27,458 hrs · 26,517 cycles

LEFT SIDE DRAG ANGLE COMMON TO RIB IS CRACKED AT FWD END.

Part: MOUNT — CRACKED (RT WING) · airframe 27,458 hrs · 26,517 cycles

RIGHT WING MIDDLE LE INBD MOUNT IS CRACKED AT TOP & BOTTOM.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,458 hrs · 26,517 cycles

LBL 27 FS 621 THROUGH 559+112 HAS CORROSION.

Part: SKIN — CHAFED (TE FLAP VANE)

LEFT INBD FLAP VANE SKIN CHAFED IN 3 SPOTS.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 27,248 hrs · 26,517 cycles

280 BULKHEAD RBL 11 20" FROM FLOOR HAS CHAFES.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 27,458 hrs · 26,517 cycles

NUMBER 1 HYD SYS PRESS FILTER MOUNT IS CRACKED FS 718.00.

Part: SKIN — DENTED (RT SPOILER) · airframe 27,458 hrs · 26,517 cycles

RIGHT FLIGHT SPOILER LOWER SKIN HAS DENT.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 27,458 hrs · 26,517 cycles

RIGHT SIDE DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 27,458 hrs · 26,517 cycles

COPILOT’S SIDE WINDOW POST LOWER OTBD SUPPORT FITTING IS CRACKED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,458 hrs · 26,517 cycles

FS 280 FLOOR SUPPORT BEAM HAS CRACK AT LBL 12.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 27,458 hrs · 26,517 cycles

PILOT'S SIDE WINDOW LOWER OTBD SUPPORT FITTING IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,458 hrs · 26,517 cycles

BATH TUB FITTING ON RBL 9 AT FS 461 CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,458 hrs · 26,517 cycles

LEFT & RIGHT FLOOR SEAT TRACK HAVE CORROSION ON FWD ENDS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,458 hrs · 26,517 cycles

LEFT OTBD 484 CLIP IS CRACKED.

Part: MOUNT BRACKET — CRACKED (RT WING) · airframe 27,458 hrs · 26,517 cycles

SPOILER MOUNT BRACKET CRACKED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 27,458 hrs · 26,517 cycles

FS 280 STRINGER L3 CLIPS ARE CRACKED.

Part: TIE DOWN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,458 hrs · 26,517 cycles

RIGHT 9G TIE DOWN ON RBL 27 HAS CORROSION.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 27,458 hrs · 26,517 cycles

LEFT MLG HYD TRANSDUCER BRACKET TOP CTR IN SIDE OF WW CRACKED.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,458 hrs · 26,517 cycles

THREE EACH TIE DOWNS ON LBL 9 AT FS 621 THROUGH 574 HAS CORROSION.

Part: SKIN — DENTED (LT SPOILER) · airframe 27,459 hrs · 26,517 cycles

LEFT OTBD GND SPOILER LOWER SKIN DENTED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,276 hrs · 26,344 cycles

EXTERNAL AC POWER CONNECTOR RECEPTACLE SURROUND SKIN & LANDING DAMAGED.

Part: LIGHT — INOPERATIVE (ROW 1) · airframe 27,244 hrs · 26,314 cycles

EMERGENCY LIGHTS AT ROW 1 INOPERATIVE. R & R THE EMERGENCY LIGHTS IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: ACARS — MALFUNCTIONED (COCKPIT) · airframe 24,324 hrs · 23,558 cycles

ACARS SCREEN WENT BLANK ACCOMPANIED WITH STRONG ELEC BURNING ODOR. SUSPECT BURNING SMELL COMING FROM ACARS UNIT. PULLED & COLLARED CB P2 - K5 NO ODOR PRESENT IAW 253131 1 FOR MEL.

Part: HINGE — DAMAGED (PAX DOOR) · airframe 22,897 hrs · 22,173 cycles

PAX DOOR HINGE ON DOOR SIDE ROLL PIN HOLE IS ELONGATED. REPAIRED IAW K00601K-5 LT .258.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 22,897 hrs · 22,173 cycles

ACFT GROUND POWER HAS CRACKS IN STRUCTURE AROUND POWER PLUG. R & R ACFT GROUND POWER SUPPORT IAW SRM 51-42-06, 51-42-21, 51-42-13.

Part: STRUCTURE — CHAFED (THRUST REVERSER) · airframe 22,897 hrs · 22,173 cycles

COWL 434 AT GAS CHAFE ON INBD END THAT FITS INTOP CENTER PART OF STANG FAIRING. REPAIRED LT UPPER TRANS COWL 434 INBD END IAW REO 601R-78-33-4017.

Part: SKIN — DENTED (THRUST REVERSER) · airframe 22,897 hrs · 22,173 cycles

DENTS ON OUTER SKIN OF LT UPPER TRANS COWL ON OTBD END. BLENDED SMOOTH IAW REO 601R-78-33-4018.

Part: STRUCTURE — CRACKED (BS 559-682) · airframe 22,897 hrs · 22,173 cycles

LEFT SEPARATOR ON PANEL 412DB WAS CRACKED FROM OTBD CORNER TO 1ST FASTENER HOLE. R & R SEPARATOR ON PANEL 412 DB IAW SRM 51-42-06 AND 51-42-13.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 22,897 hrs · 22,173 cycles

CARGO TRACK BS 559 CORRODED. CARGO TRACK R & R WITH NEW.

Part: SKIN — DENTED (THRUST REVERSER) · airframe 22,897 hrs · 22,173 cycles

LEFT UPPER TRANS COWL HAS 1 DENT OUT OF LIMITS ON OUTER SKIN JUST FWD OF OIL PLACARD PLACED ON OTBD END. CUT OUT DAMAGE & REPAIR IAW REO 601R-78-33-4018.

Part: STIFFENER — CRACKED (BS 201) · airframe 22,897 hrs · 22,173 cycles

STIFFENER IN ADG COMPARTMENT NEAR FS 201, RBL 6 HAS CRACK. REPAIRED NLG WHEEL WELL CHANNEL NEAR FS 202.75 WL 67.60, RBL 6 IAW REO 601R-53-11-2522.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 22,897 hrs · 22,173 cycles

AEB RT NR 2 HYD RETURN MANIFOLD FWD ATTACH BOLT IS PULLING THRU THE HYD RACK MOUNTING BRACKET, BRACKET IS CRACKED. R & R BRACKET.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 22,897 hrs · 22,173 cycles

PAX DOOR INTERCOSTAL IS CRACKED ON THE AFT LOWER SIDE OF DOOR. REMOVED UNSERVICEABLE INTERCOSTAL AND INSTALLED SERVICEABLE INTERCOSTAL ON THE AFT LOWER SIDE OF THE PAX DOOR IAW SRM 51-42-06, 51-42-13, 51-42-21, 51-42-11 AND 51-41-00.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 22,897 hrs · 22,173 cycles

CARGO TRACK BS 559+90 CORRODED. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-21-49 AND WERE REPLACED WITH NEW SEAT TRACK.

Part: STRIKER — CHAFED (PAX DOOR SEAL) · airframe 22,897 hrs · 22,173 cycles

PAX DOOR FWD SEAL STRIKER IS CHAFED NEAR UPPER LATCH. EDGE BLENDED AND FOUND TO BE WITHIN LIMITS FOR SRM TR 53-27.

Part: ANGLE — CRACKED (BS 484) · airframe 22,897 hrs · 22,173 cycles

AT FS 484, LBL 27 THE ANGLE ON INBD SIDE FOR THE FLIGHT CONTROL CABLE GUIDES IS CRACKED IN TOP CORNER TO FIRST FASTENER HOLE. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-42-20.

Part: ANGLE — CRACKED (BS 484) · airframe 22,897 hrs · 22,173 cycles

ANGLE AT FS 484 RBL 36 HAS A CRACK TOP OTBD SIDE. FABRICATED NEW ANGLE & INSTALLED IAW SRM 51-42-20.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 22,897 hrs · 22,173 cycles

BRAKE PRESSURE TRANSDUCER BRACKET IN RT MLG WW CRACKED. R & R BRACKET.

Part: FAIRING — CRACKED (TAIL PIPE) · airframe 22,897 hrs · 22,173 cycles

RIGHT TAIL PIPE FAIRING HAS TWO SMALL CRACKS FROM THE 4TH DRAIN HOLE FROM AFT. REMOVED 2 SMALL CRACKS BY INCREASING SIZE OF DRAIN HOLE BY 0.040, NO EO WAS AFFECTED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 21,994 hrs · 21,305 cycles

FLAP FAIL ZERO DURING APPROACH. PERFORMED FLAP FLAP RESET PROCEDURE IAW AWAC SUP 98-18E BOX 12, FLAPS RESET PLACARD AND PLACED ON MEL.

Part: PANEL — CRACKED (PAX DOOR) · airframe 21,515 hrs · 20,836 cycles

CRACKS FOUND ON PAX DOOR AFT SIDE PANEL BETWEEN DATUM 4 AND 5. CRACK FOUND ON PAX DOOR AFT DRAG ANGLE. REPAIRS DONE IAW REO 601R-52-11-702C, REO 601R-52-11-573, REO 601R-52-11-2115. REFER TO EMERY AIR W/O RJ-00385.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 21,465 hrs · 20,788 cycles

STAB AND MACH TRIM CAUTION MSG AFTER FLAPS SELECTED TO 20 DEGREES. COMPLIED WITH QRH. ENGAGED STAB AND MACH TRIM APPROX 60 SEC TO 120 SECONDS LATER, NOTED UNCOMMANDED NOSE DOWN TRIM AND MAC TRIM DISPLAY. COMPLIED WITH STAB TRIM RUN AWAY IAC & QRH. NOTED TRIM AT 402. TRIM RAN ITSELF DOWN TO 4.2. REMOVED AND REPLACED HSTCU PER AMM 27-41-01-04. OPS CHECK PER 27-41-00-05. OPS GOOD. INSPECTED MOUNT FOR MOISTURE. NONE FOUND.

Part: WIRE — SHORTED · airframe 119,150 hrs · 18,461 cycles

AT FL250 RECEIVED LT 10TH STAGE DUCT MESSAGE, RAN QRH, MESSAGE PERSISTED UNTIL ARRIVAL TO GATE. SYNOPTIC PAGE FROM APU LCV TO LT PACK SHOWED YELLOW. PERFOMRED A CONDUCTIVE TEST IAW CMM 26-14-12, LOOP A50WK WAS FOUND TO BE SHORTED. RESISTANCE BTW CONDUCTOR AND OUTSIDE HAS BEEN FOUND TO BE 14 OHMS. REMOVED AND REPLACED LOOP A50WK IAW AMM 36-21-04.

Part: ANGLE — CRACKED (BS 672) · airframe 18,476 hrs · 17,733 cycles

AEB DOOR CUTOUT HAS 1 EA CRACKED ANGLE. R & R 1 EA ANGLE AT AEB CUTOUT LT SIDE IAW SRM 53-61-23.

Part: SEAL — CRACKED (LT ENG NACELLE) · airframe 18,476 hrs · 17,733 cycles

LT TRANSCOWL TORQUE BOX UPPER AND LOWER SEALS ARE CRACKED. R & R IAW SRM 51-42-13.

Part: STRUCTURE — CRACKED (THRUST REVERSER) · airframe 18,476 hrs · 17,733 cycles

RT UPPER THRUST REVERSER CASCADE CRACKED IN 4 PLACES. REPAIRED CRACKS IN RT UPPER THRUST REVERSER CASCADE IAW AWAC PROCESS SPEC 1.

Part: ANGLE — CRACKED (BS 625) · airframe 18,476 hrs · 17,733 cycles

RT OBLIQUE ANGLE CRACKED AT FS 625. R & R RT OBLIQUE ANGLE AT FS 625 IAW REO 601R-53-61-100.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 18,476 hrs · 17,733 cycles

CLIP CRACKED AT INTERCOSTAL FS 484, LBL 36. REMOVED UNSERVICEABLE CLIP AND INSTALLED SERVICEABLE CLIP AT INTERCOSTAL FS 484, LBL 36 IAW REO 601R-53-41-059.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 18,476 hrs · 17,733 cycles

BRACKET FOR HORIZONTAL STAB FAIRING CRACKED ON LT SIDE. R & INSTALLED BRACKET PN 60021137-5 IAW SRM 52-42-21.

Part: STRUCTURE — CRACKED (RT NACELLE) · airframe 18,476 hrs · 17,733 cycles

RT LWR CORE COWL HAS CRACK ON FIREWALL OTBD OF DRAIN. REPAIRED UNSERVICEABLE DAMAGE ON RT LOWER CORE COWL OTBD OF DRAIN IAW CMM 71-12-01 SRS046. RESTORED TO ORIGINAL FINISH, ( ALODINED, PRIME PAINT) IAW SRM 51-21-11, 51-25-06, 51-25-16.

Part: ANGLE — CRACKED (LT PYLON) · airframe 18,476 hrs · 17,733 cycles

PYLON PANEL ANGLE CHAFED, R & R ANGLE .

Part: SKIN — CHAFED (LT AILERON) · airframe 18,476 hrs · 17,733 cycles

LT AILERON LWR OTBD SKIN AND LWR REMOVABLE PANELS CHAFED. WORKED IAW REO 601R-57-60-020 TO BLEND NDT ALODINE, PRIME AND PAINT TOP COAT.

Part: SKIN — CHAFED (RT AILERON) · airframe 18,476 hrs · 17,733 cycles

RT AILERON UPPER L/E SKIN CHAFED. REMOVED CHAFE DAMAGE ON RT AILERON UPPER L/E SKIN DAMAGE FOUND TO BE WITHIN SERVICEABLE LIMITS (.008 MATERIAL LOSS) RETREATED BLENDED AREA TO ORIGINAL THICKNESS IAW SRM 51-21-11, 51-25-06, 51-25-16 AND REO 601R-57-60-013.

Part: SKIN — CHAFED (LT AILERON) · airframe 18,476 hrs · 17,733 cycles

LT AILERON UPPER SKIN CHAFED. WORKED REO 601R-57-60-013 TO BLEND, NDT, ALODINE, PRIMED AND TOP COAT.

Part: STIFFENER — CHAFED (BS 621) · airframe 18,476 hrs · 17,733 cycles

REAR PRESSURE BULKHEAD CENTER VERTICAL STIFFENER CHAFED, BLENDED, MEASURED, NDT, ALODINED, PRIMED, AND PAINTED IAW REO 601R-53-61-1523.

Part: HINGE — GOUGED (PAX DOOR) · airframe 18,476 hrs · 17,733 cycles

PASSENGER DOOR PIANO HINGE HALF ON ACFT SIDE IS GOUGED ON AFT LUG. BLENDED GOUGE, TREATED, PRIMED AND TOP COATED IAW REO 601R-53-21-814.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 18,476 hrs · 17,733 cycles

CLIP IS CRACKED AT INTERCOSTAL F/S 484, RBL 28. FABRICATED NEW CLIP, REMOVED UNSERVICEABLE CLIP AND REPLACED WITH SERVICEABLE CLIP IAW CRJ200.

Part: ANGLE — CRACKED (BS 625) · airframe 18,476 hrs · 17,733 cycles

LT OBLIQUE ANGLE CRACKED AT FS 625. R & R LT OBLIQUE ANGLE FS 625 IAW REO 601R-53-61-100.

Part: RIB — CRACKED (RT WING) · airframe 18,476 hrs · 17,733 cycles

BATTERY RIB ON RT WHEEL WELL CRACKED. REPAIRED BATTERY RIB IAW REO 601R-57-51-046.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 18,476 hrs · 17,733 cycles

FS 280, RBL 9 CLIP CRACKED. R & R CLIP IAW SRM 51-42-21.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 18,476 hrs · 17,733 cycles

FS 280, LBL 9 INBD CLIP CRACKED. R & R CLIP IAW SRM 51-42-21.

Part: RIB — CRACKED (LT WING) · airframe 18,476 hrs · 17,733 cycles

LT BATT RIB CRACKED. REPAIRED LT BATT RIB IAW REO 601R-57-51-046. REPAIRED REPAIR NR 2.

Part: STRUCTURE — UNKNOWN (BS559) · airframe 16,844 hrs · 16,024 cycles

PERMORMED REO 601R-53-41-1116. COMPLIED WITH REPAIR OF REINFORCEMENT OF THE FS 559 LOWER CAP ANGLES AT BL 9.00 & 18.00, LT SIDE & RT SIDE IAW REO 601R-53-41-1116, REV B.

Part: POST — CRACKED (BS 559 BULKHEAD) · airframe 16,844 hrs · 16,024 cycles

PERFORM GREO 601R-53-41-260 FOR CRACKED LBL 9. COMPLIED WITH REPAIR OF CRACKED LBL9 ON FS559 BULKHEAD BY FULL INCORPORATION OF REO 601R-53-41-260 REV E & 601R-53-41-609, REV B, DEVIATION E.

Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 16,844 hrs · 16,024 cycles

GARGO DOOR TRACK SUPPORT BEAM AFT LOWER ATTACH ANGLE CRACKED AT 621 BULKHEAD. REMOVED DAMAGED ATTACH ANGLE, FABRICATED AND INSTALLED SERVICEABLE BRACKET.

Part: TRIM PANEL — FAULTY (COCKPIT) · airframe 16,289 hrs · 15,434 cycles

ON CLIMBOUT AT 4000`, RUDDER TRIM (NOSE LT) AND AILERON (LWD) RUNAWAY. R & R TRIM PANEL ASSY IAW AMM 27-12-01.

Part: YOKE — DIRTY (FLT CONTROLS) · airframe 15,237 hrs · 14,312 cycles

AT GATE, DURING FLT CONTROL CHECK, RATCHETING SOUND COMING FROM F/O`S YOKE DURING ELEVATOR CHECK. INSPECTED AND CLEANED DEBRIS FROM YOKE ASSY AND COVER PANEL. NO FURTHER DEFECTS NOTED AT THIS TIME IAW AMM 27-31.

Part: IDG — MALFUNCTIONED (NR 1) · airframe 14,345 hrs · 13,430 cycles

ABORTED TAKEOFF AT 60 KNOTS DUE TO IDG NR 1 CAS MESSAGE. UPON CLEARING RUNWAY. GEN NR 1 OFFLINE. BRAKE TEMP 3,3,3,4. SERVICED IDG IAW AMM 12-13-24-610-801 AND OPS TEST GOOD.

Part: STEP — DENTED (PAX DOOR) · airframe 13,698 hrs · 12,793 cycles

DENT EXIST ON PASSENGER DOOR STEP NR 2 AND NR 3. PASSENGER DOOR STEP NR 2 AND NR 3 REPAIRED IAW REO 601R-52-11-652. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,698 hrs · 12,793 cycles

CROSSBEAM LWR FLANGE CRACKED AT FS 280, RBL12.00. CROSSBEAM LWR FLANGE AT FS 280, RBL 12.00. REPAIRED IAW REO 601R-53-11-171, REV D. (K)

Part: FAIRING — DENTED (EXHAUST NOZZLE) · airframe 13,698 hrs · 12,793 cycles

LT ENG EXHAUST NOZZLE FAIRING DENTED AT 6 O’CLOCK CLOSE TO DRAINS. LT ENG EXHAUST NOZZLE FAIRING AT 6 O`CLOCK. REPAIRED IAW CMM78-11-00-300-805-401. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 13,698 hrs · 12,793 cycles

CLIP CRACKED AT FS 484 AND RBL 27 UNDER FLOOR. CLIP AT FS 484 AND RBL 27 UNDER FLOOR REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: SILL — CRACKED (BS 574) · airframe 13,698 hrs · 12,793 cycles

CRACK ON LT FLOOR SILL AT FS 574 UNDER STOP BRACKET. LT FLOOR SILL AT FS 574 UNDER STOP BRACKET REPAIRED IAW REO 601R-53-61-1741. (K)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 13,698 hrs · 12,793 cycles

OTBD CLIP CRACKED AT FS 280 AND LBL 9.00. OTBD CLIP AT FS 280 LBL, 9.0 REPLACED IAW SRM 51-42-20. (K)

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 13,698 hrs · 12,793 cycles

PASSENGER DOOR ASSIST MOTOR STIFFENER CRACKED (.200 " LONG). PASSENGER DOOR ASSIST MOTOR STIFFENER REPLACED IAW SRM 51-42-06. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,698 hrs · 12,793 cycles

PASSENGER DOOR AFT STAIR PANEL CRACKED IN ZONE NR 2 (REF REO 601R-57-11-702) (REV A) PASSENGER DOOR AFT STAIR PANEL IN ZONE NR 2 REPAIRED IAW REO 601R-52-11-702, REV A. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,698 hrs · 12,793 cycles

PASSENGER DOOR FWD STAIR PANEL CRACKED IN ZONE NR 2 (REF 601R-52-11-702, REV A). .250" LONG. PASSENGER DOOR FWD STAIR PANEL REPAIRED IN ZONE NR 2 IAW REO 601R-52-11-702, REV A. (K)

Part: HANDLE — CRACKED (PAX DOOR) · airframe 13,698 hrs · 12,793 cycles

PAX DOOR HANDLE CRACKED 2 PLACES (.100" AND .300" LONG) PAX DOOR OUTER HANDLE REPLACE IAW AMM 51-11-03-400-802. (K)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,698 hrs · 12,793 cycles

FS 280 UPPER AFT ANGLE CRACKED AT LBL 12.00, FS 280 UPPER AFT ANGLE AT LBL 12.00 REPAIR CARRIED OUT IAW REO 601R-53-11-138. (K)

Part: CARGO TRACK — CORRODED (BS 559-567) · airframe 13,698 hrs · 12,793 cycles

CORROSION ON BOTH BAGGAGE RAILS BTWN FS 559+95.01 TO FS 567 AT LBL 9.00 AND REB 9.00. BAGGAGE RAILS BTWN FS559+95.01 TO FS 567 AT LBL 9 AND RBL 9, REPLACED IAW AMM 20-21-00-910-801. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 13,698 hrs · 12,798 cycles

PASSENGER DOOR AFT STAIRS PANEL, DRAG ANGLE CRACKED (.500 LONG).

Part: PRESSURE BLKHD — CRACKED (BS 202) · airframe 13,698 hrs · 12,793 cycles

CRACK FOUND ON FWD PRESSURE BULKHEAD WEB FS 202.75, LBL 23.71 PARKING BRAKE CABLE LOCATION. REPAIR PERFORMED ON FWD PRESSURE BULKHEAD WEB FS 202.75 LBL 23.71 ON PARKING BRAKE LOCATION IAW REO 601R-53-11-563, REV NC. (K)

Part: RIB — CRACKED (LT PYLON) · airframe 13,698 hrs · 12,793 cycles

ON LT PYLON, FIRE SHIELD RIB FOUND CRACKED ON FS 654.00 ON LT PYLON, NEW FIRE SHIELD RIB INSTALLED IAW SRM 51-42-06. (K)

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 13,698 hrs · 12,793 cycles

AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING LOCATION. LINTEL REPAIR AT AFT PRESSURE BULKHEAD CARRIED OUT IAW REO 601R-53-61-1230, REV D. (K)

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 13,698 hrs · 12,793 cycles

CRACK FOUND ON REAR PRESSURE BULKHEAD WEB FS 621.00, LBL 27.00, WL 130.00. ON REAR PRESSURE BULKHEAD WEB 621.00, LBL 27.00, WL 130.00. REPAIR CARRIED OUT IAW REO 601R-53-61-154, REV B. (K)

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 13,148 hrs · 12,272 cycles

FLAPS FAIL AT 8 DEGREES DURING FLAP EXTENSION, COMPLIED WITH RESET PROCEDURE IAW SUPPLEMENT 98-018B, STEPS 1.3 AND 1.4. FLAP SYS RESET, OK. (K)

Part: ADC — MALFUNCTIONED (NR 2) · airframe 13,000 hrs · 12,128 cycles

LOST DIR CONTROL AT V1, TOOK PLANE AIRBORNE, DID A FLYBY THEN LANDED. RT WING LIFTED SUDDENLY AND LOST 15 KTS IND AIRSPEED ON F/O SIDE, MORE BRISK THAN A WIND DIRECTION SPEED, WAKE TURBULENCE WAS NOT AN ISSUE. REMOVED AND REPLACED ADC 2 FOR VAR CIRCUITRY 350 WORD BITS 13,14, 21 = 1 350 WORD 18, 26, 25 = 1 PERFORM REMOVED AND REPLACED AND LEAK CHECK IAW AMM 34-11-00. OPS CHECK GOOD. (K)

Part: SHAFT — SHEARED (STARTER) · airframe 11,565 hrs · 10,763 cycles

STARTER ON ENGINE NR 1 WILL NOT STAY ENGAGED. NO ROTATION N1 OR N2. STARTER SHAFT SHEARED. R&R NR 1 ENG ATS PER MM 80-11-01. OPS CHECK GOOD.

Part: RVDT — MALFUNCTIONED (NLG STEERING) · airframe 10,349 hrs · 9,602 cycles

STEERING INOPERATIVE CAUTION MESSAGE INFLIGHT. COMPLIED WITH QRH BUT MESSAGE RETURNED. THE GEAR AND FLAP ICONS ARE STILL ON ED-1. DIVERTED TO ORF. REMOVED AND REPLACED LT NOSE WHEEL STEERING RVDT IAW AMM 32-51-20. OPS CHECK GOOD. (M)

Part: SKIN — DENTED (BS 589 S23-26L) · airframe 8,719 hrs · 8,022 cycles

LT SIDE LOWER FUSELAGE DENTS FWD OF FS 589 BETWEEN STRINGERS 23L AND 24L APPROX 5 INCHES LONG X 4 INCHES WIDE .035 INCH DEEP AND ABOVE STRINGER 26L APPROX 2.9375 LONG X 3.9375 INCHES WIDE X .023 DEEP. (K) MAINTENANCE REPAIRED LEFT SIDE LOWER FUSELAGE DAMAGE IAW SRM 53-00-31 REPAIR NR 1. (M)

Part: SKIN — DAMAGED (BS 602) · airframe 8,719 hrs · 8,022 cycles

LT SIDE LOWER FUSELAGE SKIN DAMAGED 3 INCHES AFT OF FS 605 BETWEEN STRINGERS 24L AND 25L. DENT MEASURES 4.25 X 4.75 INCHES AND CREASE MEASURES 4.25 INCHES X 0.095 INCHES DEEP. (K) MAINTENANCE REPAIRED LT LOWER SKIN DAMAGE USING EXTERNAL DOUBLER IAW BSC EO 601R-53-12317. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625 S14L) · airframe 8,719 hrs · 8,022 cycles

LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.5 INCH LONG. (K) REMOVED AND REPLACED FS 621 TO 625.30 INTERCOSTAL IAW BOMBARDIER AERO SPACE REO 601R-53-61-422 AND CRJ SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 8,719 hrs · 8,022 cycles

RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14 IS CRACKED NEAR RADIUS APPROX 1.5 INCH L. (K) MAINTENANCE REMOVED AND REPLACED RT FS 621-625.30 INTERCOSTAL IAW BOMBARDIER AEROSPACE REO 601R-53-61-422 AND SRM 51-42-06. (M)

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 8,719 hrs · 8,022 cycles

CARGO DOOR FWD SLIDE RAIL LOWER BRACKET CRACKED. (K) MAINTENANCE REMOVED AND REPLACED CHANNEL IAW CRJ SRM 51-42-06. (M)

Part: PANEL — CORRODED (RT WING) · airframe 8,719 hrs · 8,022 cycles

RT FUEL PANEL 640BB HAS CORROSION DAMAGED IN THE NON-CRITICAL AREA, COMPLY WITH E06/21/457 (WING PLANK CUTOUT) (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,719 hrs · 8,022 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED APPROX 1.0 INCH LONG NEAR PULLEY BRACKET. (K) MAINTENANCE REPAIRED BY REMOVING DAMAGED SECTION, FABRICATING AND INSTALLING A SPLICE REPAIR IAW BOMBARDIER REO 601R-53-11-513 REV A. (M)

Part: PANEL — CORRODED (LT WING) · corrosion level 1 · airframe 8,719 hrs · 8,022 cycles

LT FUEL PANEL 510AB HAS CORROSION DAMAGE IN THE NON-CRITICAL AREA COMPLY WITH E06/21/457 (WING PANEL CUTOUT) (K) MAINTENANCE REPAIRED WING PLANK IAW BOMARDIER REO 601R-57-21-030. (M)

Part: PANEL — CORRODED (LT WING) · corrosion level 1 · airframe 8,719 hrs · 8,022 cycles

LT FUEL PANEL 540BB HAS CORROSION DAMAGE IN THE NON-CRITICAL AREA COMPLY WITH E06/21/457 (WING PLANK CUTOUT) (K) MAINTENANCE REPAIRED WING PLANK IAW BOMBARDIER REO 601R-57-21-030. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,719 hrs · 8,022 cycles

LT 484 ANGLE IS CRACKED APPROX .2500 INCH AT LBL 36. (K) MAINTENANCE REMOVED FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A. FABRICATED AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-1-059 AND BSC SR 601R-53-0030A. (M)

Part: STRINGER CLIP — CRACKED (FS 280)

RIGHT INBOARD AND OUTBOARD 280 CLIPS ARE CRACKED APPROX .25 INCH AT RBL 9. MAINTENANCE REMOVED RIGHT INBOARD AND OUTBOARD 280 CLIPS AT RBL 9 AND INSTALLED 2 NEW SERVICEABLE 280 CLIPS IAW BSC REPAIR 601R-53-0037A. (M)

Part: STRINGER CLIP — CRACKED (BS 280)

LEFT INBOARD 280 CLIP IS CRACKED APPROX .25 INCH L AT LBL 9. MAINTENANCE REMOVED DAMAGED LEFT INBOARD 280 CLIP AT LBL 9 AND INSTALLED NEW SERVICEABLE CLIP AT LBL IAW BSC REPAIR 601R-53-0057A. (M)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,719 hrs · 8,022 cycles

LT FS 621 FLOOR SUPPORT ANGLE CRACKED, 2 INCH LONG. (K) MAINTENANCE REPAIRED LEFT FLOOR SUPPORT ANGLE AT FS 621 IAW BOMBARDIER REO 601R-53-61-117. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,719 hrs · 8,022 cycles

RT 484 ANGLE IS CRACKED APPROX .5 INCH LONG AT RBL 27. (K) MAINTENANCE REMOVED FLANGE IAW BOMBARDIER REO 601R-53-41-059 REV A. FABRICATED AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,719 hrs · 8,022 cycles

LT 484 ANGLE IS CRACKED APPROX .5 INCH L AT LBL 27. (K) MAINTENANCE REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. FABRICATED AND INSTALLED REPAIR ANGLE IAW BSC SR 601R-53-0039B. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,719 hrs · 8,022 cycles

RT 484 ANGLE IS CRACKED APPROX .2500 INCH LONG AT RBL36. (K) MAINTENANCE REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,719 hrs · 8,022 cycles

RT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .2 INCH LONG. (K) MAINTENANCE REPAIRED RIGHT FLOOR SUPPORT ANGLE AT FS 621 IAW BOMBARDIER REO 601R-53-61-117. (M)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 7,996 hrs · 7,309 cycles

FLAPS FAIL CAUTION MESSAGE ON DEPARTURE. INSPECTED FLAPS, NO EVIDENCE OF SKEW FOUND. RESET FLAP SYSTEM IAW AMM SUPPLEMENT 98-018B. FLAPS OPS CHECK OK. (K)

Part: ACM — MALFUNCTIONED (RIGHT) · airframe 7,846 hrs · 7,167 cycles

CABIN FILLED WITH VISIBLE SMOKE. SHUTDOWN PACKS, SMOKE DISSIPATED. TROUBLESHOT SYSTEM FOUND RT AIR CYCLE MACHINE BAD. REMOVED AND REPLACED RT AIR CYCLE MACHINE IAW 21-51-10. OPS CHECK GOOD. (K)

Part: FLAP SYSTEM — OUT OF RIG (TE FLAPS)

UNCOMMANDED ROLL TO LEFT ON FINAL IN LANDING CONFIGURATION. LANDING GEAR DOWN, FLAPS 45, A/P DISENGAGED, NO SPOILER MESSAGES, NEEDED RT AILERON TRIM. LEFT WING INBOARD FLAP, INBOARD AND OUTBOARD ACTUATORS REQUIRE OVERTRAVEL STOP RIG. RT WING OUTBOARD FLAP, INBOARD ACTUATOR REQUIRES OVERTRAVEL STOP RIG. RIGGED LEFT OUTBOARD FLAP, INBOARD FLAP ACTUATORS. RIGGED RIGHT WING OUTBOARD FLAP INBOARD ACTUATOR. OPS CHECK GOOD. (M)

Part: FIRE — DETECTED (APU BAY) · airframe 5,908 hrs · 5,265 cycles

TAXIING TO RW27L, TAXIIED INTO POSITION, ANOTHER AIRCRAFT STATED OVER THE RADIO, (IT LOOKS LIKE FIRE COMING OUT OF THE APU EXHAUST), DECIDED TO TAXI DOWN THE RUNWAY AND TURN OFF THE APU. NO FIRE INDICATIONS WERE NOTED IN THE COCKPIT UNTIL I SET THE BRAKE AND PARKED, THEN GET AN APU FORE FAIL MSG, FOLLOWED BY AN APU FIRE WARNING. CALLED FOR THE IAC AND BLEW THE APU FIRE BOTTLE, FIRE INDICATIONS WENT AWAY. AT THAT POINT FIRE TRUCKS ARRIVED AND WE OPENED THE DOOR . FIREMAN STILL SAW SMOKE FROM THE APU SO WER EVACUATED THE AIRCRAFT. (K) REMOVED AND REPLACED APU IAW CRJ AMM 49-10-00. OPS AND LEAK CHECK GOOD. (M)

Part: SKIN — CORRODED (RT WING)

MWC 59 WING PLANK, RT WING, UNDER FUEL ACCESS PANEL 650EB IS SEVERLY CORRODED AROUND ENTIRE CIRCUMFERENCE OF OPENING, .150 INCH WIDE X .005 INCH DEEP. BLENDED LOWER WING PLANK IAW MFG REO. (K)

Part: SKIN — DENTED (FUSELAGE) · airframe 3,731 hrs · 3,221 cycles

MWC 1 DENT IN AFT FUSELAGE AT FS 672 BETWEEN STRINGERS 26L AND 27L. CUT OUT DAMAGED AREA AND INSTALLED FABRICATED FILLER PARTS IAW EO. (K)