N451AW

Part: WIRE HARNESS — FAILED (NLG) · airframe 40,256 hrs · 38,506 cycles

RECEIVED STEERING INOP, WOW INPUT, AND WOW OUTPUT FAIL MESSAGES DURING INITIAL CLIMB OUT. GEAR WAS UP AND LOCKED. CW QRH. STEERING SELECTED OFF VIA QRH AND WOW MESSAGES REMAINED. WOW MESSAGES CLEARED WHEN SELECTING GEAR DOWN ON APPROACH. AFTER LANDING RENEGAGED STEERING AND STEERING OPERATED NORMALLY. ***AIRCRAFT REMOVED FROM SERVICE **** R&R OF NLG ELECTRICAL HARNESS IAW AWAC SUP 12-029E. REF 354867-3 FOR OPS CHECKS OF NLG HARNESS.

Part: RELAY — FAILED (APU FUEL) · airframe 40,117 hrs · 38,375 cycles

APU SOV STATUS PRESENT IN-FLIGHT WITH APU OFF. MESSAGE CLEARED AFTER ENGINE SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. R&R FUEL CONTROL RELAY IAW 20-22-00. OPS CHECK GOOD.

Part: PANEL — DENTED (FS700.00+13) · airframe 39,657 hrs · 37,933 cycles

FS700.00+13 STRINGER 20L+5 INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ***AIRCRAFT REMOVED FROM SERVICE ***** DRESSED BACK DENT IAW DISPOSITION INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829 REV DATED 2022-05-17.

Part: PANEL — DENTED (FS654.50 +9 22R) · airframe 39,657 hrs · 37,933 cycles

FS 654.50 TO FS 654.50 + 9 STRINGER 22R +5 2 EA. OUTWARD DENTS C/T EXTERIOR SIDE OF SKIN PANEL. ****AIRCRAFT REMOVED FROM SERVICE ***** REPAIRED FS654.50 TO FS654.50+9 STRINGER 22R DENT REF REO 601R-53-61-7835 REV. DATED 2022-05-24.

Part: NUT PLATE — ELONGATED · airframe 39,657 hrs · 37,933 cycles

TEMPORARY REPAIR TO THE ELONGATED NUT PLATE HOLE IN FUSELAGE STRUCTURE AT STRINGER 19R BETWEEN FS409+80 - FS409+96. ****AIRCRAFT REMOVED FROM SERVICE *** REPAIRED FUSELAGE SKIN NUT PLATE HOLE AT STRINGER 19R BETWEEN FS409+80 TO FS409+96 REF REO 601R-53-31-128 REN. DATED 2022-05-24.

Part: SUPPORT ANGLE — CORRODED (LAV SERVICE POIN) · corrosion level 2 · airframe 39,657 hrs · 37,933 cycles

WIRE SUPPORT ANGLE CORRODED AT THE AFT LAV SERVICE POINT. ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED BRACKET.

Part: PANEL — DENTED (FS605.00+1 23L+3) · airframe 39,657 hrs · 37,933 cycles

FS605.00+1 STRINGER 23L+3 INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ***AIRCRAFT REMOVED FROM SERVICE **** DRESSED BACK DENT AS PER INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829 REV DATED 2022-05-17.

Part: INTERCOSTAL — CRACKED (FS654-FS672) · airframe 39,657 hrs · 37,733 cycles

INTERCOSTAL AT FS654 TO FS672.20 FOUND CRACKED. ***AIRCRAFT REMOVED FROM SERVICE **** REPAIRED INTERCOSTAL IAW AWAC SUPPLEMENT 13-085B DATE ISSUED 2/03/2014 AND REO 601R-53-62-225 REV. DATED 2013-09-19.

Part: PANEL — DENTED (FS625.30+12) · airframe 39,657 hrs · 37,933 cycles

FS625.30+12 STRINGER 22R+4 OUTWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ****AIRCRAFT REMOVED FROM SERVICE **** REPAIRED DENT DAMAGE TO FUSELAGE LOWER SKIN BETWEEN FS625.00 - FS640.00 AND STR 22R - STR 23R REF REO 601R-53-61-7836 REV. DATED 2022-05-25

Part: SKIN PANEL — DENTED (FS605+1 STGR 23L) · airframe 39,657 hrs · 37,933 cycles

F/S 605.00+1, STRINGER 23L+3; INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL ***AIRCRAFT REMOVED FROM SERVICE **** DRESSED BACK DENT AS PER INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829, REV--, DATED 2022-05-17 AND REO 601R-51-00-309 REV. -A DATED 2017-08-23 . GENERATED A PRIORITY 2 CARD SEE JOB 2783235 OP 60

Part: SEAL — MISMANUFACTURED (PAX DOOR) · airframe 38,709 hrs · 36,999 cycles

REF. 342366/4 AND 342667/1- LOUD SQUEAL AT 4,000 FT 250 KNOTS. ABNORMAL CLIMB RATE AT CABIN ALT. AT 10,000 FT, CABIN ALT REMAINED AT 5,000 FT. CABIN ALT INCREASED WITH DECREASED POWER. ON FINAL APPROACH ABNORMALLY HIGH RATE OF DECENT OF CABIN ALT. LANDING WEIGHT APPROX 46,950LBS. SMOOTH LANDING. BTMS READ NORMAL. CREW INDICATED THAT THEY DID NOT BELIEVE IT WAS ONLY THE PAX DOOR CAUSING THE NOISE AND PRESSUIZATION ISSUES. CAPTAIN STATED AT FIRST SHE THOUGHT THE SQUEAL WAS COMING FROM THE RADIO. CREW LEFT IT IN AUTOMATIC THE ENTIRE FLIGHT BECAUSE THE A/C WAS TRYING TO KEEP SOME PRESSUIZATION. WHEN BLEEDS WERE TRANSFERRED BACK TO THE APU FOR DECENT IT GOT MARGINALLY BETTER. NO PAX COMPLAINTS AND CA WAS THE FLYING PILOT. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND PAX DOOR SEAL HAD NO VENT HOLES FOR PRESSURIZATION. C/W AWAC SUP 21-023. OPS CHECK GOOD

Part: SEAL — LEAKING (PAX DOOR) · airframe 38,708 hrs · 36,998 cycles

3930 DURING CLIMBOUT AROUND 13K FEET HEARD LOUD HISSING SOUND COMING FROM BEHIND THE FLIGHT DECK. FA CALLED AND SAID IT WAS FROM THE MAIN CABIN DOOR. AROUND 19K FEET HISSING GOT LOUDER AND CABIN RATE RAPIDLY INCREASED. CABIN ALTITUDE NEVER EXCEEDED 6K FEET. NO MESSAGES REGARDING MAIN CABIN DOOR. DURING DESCENT PRESSURIZATION NORMAL. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND A TEAR IN PAX DOOR SEAL. R&R PAX DOOR SEAL IAW AMM 52-11-10. REF . 342366/3 FOR OPS CHECK

Part: WINDSHIELD — CRACKED (LEFT COCKPIT) · airframe 37,866 hrs · 36,090 cycles

CAPTAIN OUTER SINDSCREEN (WINDSHIELD) CRACKED WHILE ASCENDING THROUGH 19,000FT. C/W QRH AND RETURNED TO DAY. AIRCRAFT REMOVED FROM SERVICE. R & R LT WINDSHIELD, IAW AMM 56-11-01 REF WO 300890 MX WORK CARD NR 3 FOR OPERATIONS AND LEAK CHECK.

Part: FORMER — CRACKED (347) · airframe 37,822 hrs · 36,045 cycles

PAX DOOR AFT FORMER CRACKED. P/N 601R318034-3 AT FS 347.25 THAT MEASURES 2.9'' L. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA OF FORMER 3.0" L, REF REO NR: 601R-52-11-2834 DATED 2020-10-05. PERFORMED HFEC INSPECTION OF CUT OUT AREA AND INNER SKIN, IAW REO NR: 601R-52-11-2834 DATED 2020-10-05 AND CRJ NDTM PART 1 REV 41 51-20-06. NO INDICATIONS NOTED. FABRICATED 2 EA SHIMS AND DOUBLER FROM 0.063'' 7075-T6, REF REO NR: 601R-52-11-2834 DATED 2020-10-05 AND CRJ 200 SRM 51-24-36 AND CRJ 200 SRM 51-24-16. PERFORMED HFEC INSPECTION ON 2 EA SHIMS AND DOUBLE, IAW CRJ NDTM PART 1 REV 41 51-20-06. NO INDICATIONS NOTED. INSTALLED 2 EA SHIMS AND DOUBLER, REF REO NR: 601R-52-11-2834 DATED 2020-10-05 AND CRJ SRM 51-23-00 AND CRJ SRM 51-42-22 REV 38. COMPLIED WITH REO NR: 601R-52-11-2834 DATED 2020-10-05. ALL WORK ACCOMPLISHED ON AERSALE W/O NO: 002943 CARD NO: NR/0001.

Part: SKIN — DAMAGED (ZONE 100) · airframe 37,822 hrs · 36,045 cycles

NUT PLATE HOLE IN FUSELAGE SKIN AND UNDERLINING DOUBLER AT STR 19R AND FS 409+93 OBLONG/ELONGATED TO 0.297W X 0.294. AIRCRAFT REMOVED FROM SERVICE. OPENED HOLE IN STR 19R TO 0.2055, REF REO 601R-53-31-1145 DATED 2020-10-05. OPENED ELONGATED HOLE IN FUSELAGE SKIN AND UNDERLING DOUBLER TO 0.320 L X 0.304 W, REF REO 601R-53-31-1145 DATED 2020-10-05. PERFORMED HFEC INSPECTION ON REWORKED AREA BETWEEN FS 409+80-FS 409+96 AND STR 19R. EXTERNAL AND INTERNAL SURFACES, IAW REO 601R-53-31-1145 DATED 2020-10-05 AND CRJ 200 NDTM PART 1 REV 41 PROCEDURE 51-20-06. NO INDICATIONS NOTED. COMPLIED WITH REO 601R-53-31-1145 DATED 2020-10-05.

Part: ACCESS PANEL — GOUGED (LT WING TE FLAP) · airframe 37,822 hrs · 36,045 cycles

LT FLAP LOWER INBOARD ACCESS PANEL 584AB GOUGED AT UPPER CENTER LEADING EDGE. GOUGE ON LT FLAP LOWER INBOARD ACCESS PANEL 584AB MEASURES 0.6125''L X 0.30''W X0.011''D. BLENDED GOUGE TO A SMOOTH CONTOUR. DEPTH NOT TO EXCEED ORIGINAL DEPTH OF 0.011'', IAW EA NR: AWAC-CRJ275-01512 DATED 10/02/2020 REV A AND CRJ 200 SRM 51-12-00. AIRCRAFT REMOVED FROM SERVICE. PERFORMED HFEC INSPECTION ON RE-WORKED AREA OF LT FLAP LOWER INBOARD ACCESS PANEL 584AB, IAW EA NR: AWAC-CRJ275-01512 DATED 10/02/2020 REV A AND CRJ 200 NDTM PART 1 REV 41 PROCEDURE 51-20-06. NO INDICATIONS NOTED.

Part: SKIN — GOUGED (BS 409) · airframe 37,822 hrs · 36,045 cycles

2 EACH MISS-DRILLED SCREWS LT FWD WING TO BODY FAIRING ATTACHED POINT (ON FUSELAGE). HOLE NR 1 LOCATED AT FS 409+71.6 AND STR 21L THAT MEASURES 0.307'' W AND 0.25'' L. HOLE NR2 LOCATED AT FS 409+70.45 AND STR 22L THAT MEASURES 0.249'' W AND 0.208'' L. AIRCRAFT REMOVED FROM SERVICE. AT HOLE NR 1 CAREFULLY REMOVED SHARP EDGES IN SKIN AND UNDERLYING STR 21L. AT HOLE NR 2 ENLARGED THE DAMAGED HOLE THROUGH THE SKIN AND UNDERLYING STR 22L, IAW REO 601R-53-31-1146 DATED 2020-09-30. PERFORMED HFEC INSPECTION ON EXTERIOR SKIN AND INTERIOR STRINGER FLANGE AT HOLE NR 1 LOCATED AT FS 409+71.6 AND STR 21L, AND HOLE BR 2 LOCATED AT FS 409+70.45, IAW REO 601R-53-31-1146 AND NDTM PART 1 REV 41 51-20-06. NO INDICATIONS NOTED. ACCOMPLISHED TEMP REPAIR, IAW REO 601R-53-31-1146 DATED 2020-09-30. SUBJECTED TO CONDITIONS IN REO 601R-53-31-1146 DATED 2020-09-30. TEMP REPAIR IS STRUCTURALLY ACCEPTABLE FOR 1850 FLIGHT HOURS FROM TIME OF INCORPORATION OF REO. AIRCRAFT CURRENT HOURS ARE 37,819:22.

Part: SKIN — CRACKED (PAX DOOR) · airframe 37,822 hrs · 36,045 cycles

PASSENGER DOOR INTERNAL STRUCTURE ENTRY DOOR/STAIRS AFT SIDE FOUND CRACK IN SKIN AT 2ND TO TOP STEP. AIRCRAFT REMOVED FROM SERVICE. REPAIRED PASSENGER DOOR STAIRS AFT SIDE AT 2ND STEP, REF AIR WISCONSIN SUPPLEMENT NO: 14-162 DATE OF ISSUE JULY 21, 2014. REMOVED STEP FOR ACCESS, IAW CRJ 200 MM 52-11-04 REV 41. CUT OUT CRACK AREA .9''W X 1.85''L, IAW AIR WISCONSIN SUP. NO: 14-162 DATE OF ISSUE JULY 21, 2014. PERFORMED HFEC AROUND CUTOUT. NO INDICATIONS NOTED, REF BOMBARDIER REO PL601R-52-11-702 REV C SHEET 4 NOTE NR 2 AND CRJ 200 NDTM PART 1 PROCEDURE 51-20-06 REV 41. FABRICATED AND INSTALLED FILLER AND EXTERNAL DOUBLER OUT OF 7075-T6 .032 AND 7075-T6 .040 (REP DOUBLER 6.2''L X 3.0''W) RESPECTIVELY PER AIR WISCONSIN SUPP. NO: 14-162 DATE ISSUE JULY 21, 2014.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 37,718 hrs · 35,955 cycles

AFTER T/OFF ON CLIMB, RECEIVED GEAR DISAGREE AFTER 6 SECS FROM SELECTION. NLG SHOWS DOWN AND NLG DOOR OPEN. BOTH MLG SHOW UP AND LOCKED. ALSO RECEIVED NWS INOP, WOW INPUT CAUTION, WOW OUTPUT FAIL MESSAGES. RAN QRH AND STEERING MESSAGE CLEARED. EXTENDED GEAR AND ALL THREE INDICATED DOWN AND LOCKED. LANDED AT APPROX. 130 KNOTS SMOOTH AND NOT OVERWEIGHT. AFTER LANDING WOW MESSAGES CLEARED AND NWS OPERATED NORMALLY. NORMAL BRAKING USED. "AIRCRAFT REMOVED FROM SERVICE" R+R NLG ASSY IAW AWA MTCM 12-07-2. OPS AND LEAK CHECK GOOD. S/N OFF DCL870/03 S/N ON DCL918/03

Part: WIRE HARNESS — NOT REPORTED (NLG) · airframe 37,488 hrs · 35,737 cycles

AFTER TAKE OFF, RECEIVED A GEAR DISAGREE, NOSE GEAR REMAINED DOWN. COMPLIED WITH QRH. MANUAL GEAR EXTENSION ACCOMPLISHED, RECEIVED 3 GREEN. ON TAXI IN, RECEIVED A HYD 3 HIGH TEMP AND NWS INOPERATIVE CAUTION. COMPLIED WITH QRH. MESSAGES CLEARED. AIRCRAFT REMOVED FROM SERVICE. INSPECTED NLG, NO VISIBLE DEFECTS FOUND. REMOVED AND REPLACED NLG OLEO CENTERING BRACKET IAW CMM 32-20-04. REMOVED AND REPLACED NLG HARNESS IAW SUPP 12-069D. PERFORMED GEAR SWINGS OPS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 36,871 hrs · 35,156 cycles

NOSE DOOR OPEN (W) MSG RECEIVED WHEN PUTTING GEAR UP ON DEPARTURE GEAR DISAGREE(W) ALSO RECEIVED. RAN QRH FOR NOSE DOOR OPEN. MSG APPEARED IMMEDIATELY AFTER HANDLE MOVEMENT.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 35,950 hrs · 34,277 cycles

DURING CLIMB, AT APPROXIMATELY 15,000 FEET, THE FLIGHT CREW RECEIVED A RIGHT THRUST REVERSER UNLOCKED CAUTION MESSAGE. THE CREW COMPLETED THE APPROPRIATE CHECKLISTS, DECLARED AN EMERGENCY. THE FLIGHT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 35,710 hrs · 34,038 cycles

DURING APPROACH, THE FLIGHT CREW IDENTIFIED A AIR DATA COMPUTER 2 ISSUE (INDICATED AIRSPEED AND ALTITUDE) AND ABANDONED THE APPROACH. THE CREW COMPLETED THE APPROPRIATE CHECKLISTS, DECLARED AN EMERGENCY AND ATTEMPTED AN APPROACH FOR THE SECOND TIME. AFTER RECEIVING A WIND SHEAR WARNING ALERT FROM ATC DURING THE SECOND APPROACH, THE CREW ABANDONED THE APPROACH AND DIVERTED WITHOUT FURTHER INCIDENT.

Part: BULKHEAD WEB — CRACKED (CRACKED) · airframe 34,669 hrs · 33,083 cycles

AFT PRESSURE BULKHEAD ABOVE AFT CARGO DOOR, AFT OF THE TRACK WAS CRACKED. REPAIRED THE BULKHEAD WEB.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,669 hrs · 33,083 cycles

RIGHT INBD FLAP, LOWER INBD SKIN PANEL HAD MULTIPLE AREAS OF DENTS, DINGS, AND PITS. REPLACED THE FLAP SKIN IAW SRM 51-42-13.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,669 hrs · 33,083 cycles

LEFT INBD FLAP, LOWER OTBD SKIN PANEL HAD TWO DENTS. REPLACED THE FLAP SKIN PANEL IAW SRM 51-42-13

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 34,669 hrs · 33,083 cycles

BS 280 FLOORBEAM OTBD ANGLE AT LBL 9 WAS CRACKED. REPLACED THE FLOORBEAM ANGLE.

Part: BEAM — CRACKED (BS 574-621) · airframe 34,669 hrs · 33,083 cycles

CARGO DOOR BEAM CUT BY BOTH DOOR ASSIST CABLE, LOWER OTBD FLANGE, AT TWO PLACES. REPLACED THE CARGO DOOR BEAM LOWER OTBD FLANGE IAW SRM 51-42-21, AND SRM 51-42-06.

Part: WEB — CRACKED (ASSIST YOKE) · airframe 34,669 hrs · 33,083 cycles

ON REMOVAL OF A CRACKED DRAG ANGLE REPAIR, AFT RISER WEB FOUND TO BE CRACKED BY THE ASSIST MOTOR YOKE. REPAIRED PAX DOOR AFT WEB RISER IAW SUPP 15-310

Part: SKIN — CRACKED (PAX DOOR) · airframe 34,669 hrs · 33,083 cycles

ON REMOVAL OF THE PAX DOOR AFT RISER DRAG ANGLE, THE INNER SKIN HAD A CRACK UNDER THE DRAG ANGLE SLPICE. REPAIRED PAX DOOR INNER SKIN IAW 18-225.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,669 hrs · 33,083 cycles

RIGHT INBOARD FLAP LOWER OTBD SKIN PANEL WAS DENTED. REMOVED AND REPLACED THE SKIN IAW SRM 51-42-13.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 34,669 hrs · 33,083 cycles

FLOORBEAM STRAP AT BS 559 HAD CORROSION BETWEEN RBL 27 AND THE RT FLOOR SUPPORT, IN THE CABIN. REMOVED AND REPLACED THE FLOORBEAM STRAP IAW SRM 51-42-06, 51-40-11, 53-41-43, AND 53-00-00

Part: STRAP — DAMAGED (SEAL STRIKER) · airframe 34,669 hrs · 33,083 cycles

PAX DOOR FWD SEAL STRIKER REPAIR STRAP DAMAGED. REPLACED PAX DOOR FWD SEAL STRIKER REPAIR STRAP IAW SUPP 17-009.

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 34,669 hrs · 33,083 cycles

LT INBD FLAP LOWER INBD SKIN PANEL HAS MULTIPLE AREAS WITH DAMAGE. REPLACED LT INBD FLAP LOWER INBD SKIN PANEL IAW SRM 51-42-13.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,669 hrs · 33,083 cycles

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

Part: WEB — CRACKED (PAX DOOR) · airframe 34,669 hrs · 33,083 cycles

PAX DOOR UPPER STEP WEB BELOW TOP FOLDING STEP IS CRACKED. REPAIRED IAW REO 601R-52-11-279 REV-NC.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 34,669 hrs · 33,083 cycles

PAX DOOR AFT DRAG ANGLE WAS CRACKED. REPAIRED THE AFT DRAG ANGLE IAW REO 601R-52-11-513 REV B.

Part: BRACKET — CRACKED (CARGO BAY) · airframe 34,669 hrs · 33,083 cycles

AFT CARGO DOOR TRACK, LOWER AFT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 33,318 hrs · 31,744 cycles

FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE FROM ROWS 9 AFT. SECURED THE EMERGENCY LIGHT CONNECTOR AT ROW 12, OPS CHECKED GOOD IAW AMM 33-51-01.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,087 hrs · 31,523 cycles

EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW AMM 33-51-10, OPS CHECKED GOOD.

Part: BRACKET — BROKEN (BS 605) · airframe 30,983 hrs · 29,550 cycles

LEFT NOSE COWL PDU WIRE HARNESS BRACKET BROKEN. REPLACED BRACKET IAW CMM 20-42-06.

Part: STRINGER CLIP — CRACKED (BS 621) · airframe 30,983 hrs · 29,550 cycles

STRINGER CLIP BS 621 STRINGER 13L AFT SIDE IS CRACKED

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 30,983 hrs · 29,550 cycles

FRAME BS 333 HAS CORROSION ON THE FWD SIDE BETWEEN STRINGERS 22 - 23R IN THE FWD E&E BAY. REMOVED CORROSION AND INSTALLED DOUBLERS AS REQUIRED IAW REO 601R-53-21-2733 REV-A.

Part: SKIN — CRACKED (RT WING LE) · airframe 30,983 hrs · 29,550 cycles

RT I/B L/E INNER SKIN IS CRACKED 24 INCHES FROM I/B EDGE. REPAIRED DAMAGE IAW EA AWAC-CRJ257-00423 REV-IR AND AWAC SUPPLEMENT 16-188.

Part: FITTING — CRACKED (BS 621) · airframe 30,983 hrs · 29,550 cycles

BS 621 SEAT TRACK ATTACHMENT LBL 27 HAS CORROSION. REPAIRED ATTACH FITTING IAW EA AWAC-CRJ 253-00421 REV-IR.

Part: LUG — CHAFED (RT WING TE FLAP) · airframe 30,983 hrs · 29,550 cycles

RIGHT O/B FLAP, CENTER HINGE ARM FWD ATTACH POINT, O/B LUG IS CHAFED. REPAIRED IAW REO 601R-57-53-1048 REV.

Part: FLOOR SUPPORT — GOUGED (BS 559) · corrosion level 2 · airframe 30,983 hrs · 29,550 cycles

RIGHT FLOOR SUPPORT BETWEEN BS 559+48 AND 559+64 IS GOUGED BY THE TOILET DUMP FITTING. REPAIRED THE FLOOR SUPPORT IAW EA AWAC-CRJ253-00422 REV- IR.

Part: RIB — CRACKED (JET PIPE) · airframe 30,983 hrs · 29,550 cycles

JET PIPE FAIRING 446AL FWD RIB IS CRACKED. REPAIRED THE RIB IAW CMM 78-11-00-300-810-A01.

Part: FITTING — CRACKED (COCKPIT) · airframe 30,983 hrs · 29,550 cycles

RIGHT WINDSHIELD SIDEPOST SUPPORT, AFT FITTING IS CRACKED. REPLACED RT WINDSHIELDS SIDEPOST AFT FITTING IAW SRM 51-42-21.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 30,983 hrs · 29,550 cycles

STR 14L CLIP AT FS 621.00 AFT SIDE IS CRACKED. REPLACED STR 14L CLIP AT FS 621.00 AFT SIDE IAW SRM 51-42-06, 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 30,983 hrs · 29,550 cycles

LEFT OBLIQUE INTERCOSTAL AT STRINGER 14L BS 625 IS CRACKED. REPLACED THE INTERCOSTAL.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,983 hrs · 29,550 cycles

CARGO TIE DOWN FITTINGS AT LBL9 ARE CORRODED. REPLACED CARGO TIE DOWN FITTINGS AT LBL9 IAW AMM 53-00-49-000-801, 53-00-49-400-801.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 30,983 hrs · 29,550 cycles

STR 15L CLIP AT FS 621.00 AFT SIDE IS CRACKED. REPLACED STR 15L CLIP ON AFT SIDE OF FS 621.00 IAW SRM 51-42-06, 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 30,983 hrs · 29,550 cycles

LEFT OBLIQUE INTERCOSTAL STRINGR 15L, BS 625 IS CRACKED. REPLACED THE INTERCOSTAL.

Part: SUPPORT FITTING — CRACKED (COCKPIT) · airframe 30,983 hrs · 29,550 cycles

LEFT WINDSHIELD SIDE POST SUPPORT CLIP BELOW WINDOW IS CRACKED. REPLACED LT WINDSHIELD SIDE POST SUPPORT CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,983 hrs · 29,550 cycles

LEFT WINDSHIELD SIDE POST SUPPORT AFT FITTING IS CRACKED. REPLACED LT WINDSHIELD SIDE POST AFT FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,983 hrs · 29,550 cycles

CLIP ON AFT SIDE OF FS 280.00 AND STR 3L IS CRACKED. REPLACED CLIP ON AFT SIDE OF FS 280.00 AND STR 3L IAW SRM 51-42-21.

Part: RETAINER — CRACKED · airframe 30,983 hrs · 29,550 cycles

PANEL 422BB HAS CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-40-11.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 30,983 hrs · 29,550 cycles

RIGHT WING TO BODY FAIRING SUPPORT CRACKED AT FS 424.00. REPLACED SUPPORT ANGLE AT FS 424.00, RT SIDE IAW SRM 51-42-06.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 30,983 hrs · 29,550 cycles

LEFT WING TO BODY FAIRING SUPPORT CRACKED AT FS 424.00. REPLACED ANGLE AT FS 424.00 LT IAW SRM 51-42-06.

Part: INVERTER — INOPERATIVE (E&E BAY) · airframe 30,731 hrs · 29,304 cycles

ROW 1 & GALLEY LOWER SERVICE DOOR & LOWER PAX DOOR EMER EXIT LIGHTING FAILED TO TEST. INVERTER FAILED & INVERTER WAS R & R. REMOVED FROM SERVICE FOR RON MX.

Part: FCU — FAULTY (RT ENGINE) · airframe 30,528 hrs · 29,113 cycles

AFTER LEVELING OFF & REDUCING POWER BELOW 79 PERCENT N1 NOTICED THE FOLLOWING INDICATIONS ON RT ENG, FF 1150-1210, N1 70-70.6, N2 83-83.5. ALL INDICATIONS NORMAL ABOVE 79 PERCENT N1, COMPLIED WITH QRH, SPEED SWITCH OFF, NO EFFECT ON INDICATION, AT IDLE ALL INDICATIONS STILL ERRATIC. DID NOT FEEL ANYTHING PHYSICALLY IN FLIGHT FROM ENG. R & R RT FCU.

Part: LIGHT — INOPERATIVE (ROWS 2-5) · airframe 29,887 hrs · 28,533 cycles

FLOOR TRACK LIGHTING INOPERATIVE ROW 2 - 5.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 28,095 hrs · 26,791 cycles

ON TAXI IN RECEIVED, AP TRIM NU, CTN MSG. FOUND STAB TRIM 11 DEG NOSE UP, HEARD TRIM WARNING, CENTERED TRIM & MSG CLEARED.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 27,598 hrs · 26,327 cycles

FLAP FAIL CAUTION MSG DURING CLIMB WITH FLAPS AT ZERO. PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18F, BOX 12, FLAPS RESET.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 26,341 hrs · 25,133 cycles

AT FLIGHT LEVEL 350, SMOKE CARGO INDICATION. COMPLIED WITH QRH DISCHARGED CARGO BOTTLE. FOUND AFT CARGO SMOKE DETECTOR FAILED OPS CHECK IAW AMM 26-15-00. R & R AFT SMOKE DETECTOR IAW AMM 26-15-01. OPS CHECKED GOOD.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 26,339 hrs · 25,131 cycles

PAX DOOR STAIRS CRACKED AT UPPER PAX DOOR ASSIST MOTOR MOUNT BRACKET .

Part: TRUNNION — DAMAGED (LT MLG) · airframe 26,339 hrs · 25,131 cycles

DURING PERFORMANCE OF MLG TRUNNION FASTENER HOLES COLD WORKING, FOUND 10 TOTAL OVERSIZE HOLES ON THE LT LOWER FLANGE.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 26,339 hrs · 25,131 cycles

RIGHT MLG WW DRAG ANGLE CRACKED AT FWD END.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,339 hrs · 25,131 cycles

RIGHT OBLIQUE ANGLE CRACKED FS 625.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 26,339 hrs · 25,131 cycles

RIGHT INBD FLAP VANE CHAFED INBD LE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,339 hrs · 25,131 cycles

INBD & OTBD CLIPS CRACKED AT FS 280 FLOORBEAM, LBL 9.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,339 hrs · 25,131 cycles

CORROSION ON SEAT TRACK RBL 27, FS 559.80.

Part: ATTACH BRACKET — CRACKED (RT MLG WW) · airframe 26,339 hrs · 25,131 cycles

RIGHT MLG WW BRAKE TRANSDUCER HYD LINES ATTACHED BRACKET CRACKED AT OTBD SIDE.

Part: FITTING — CRACKED (FUSELAGE)

RIGHT INBD & OTBD 484 CLIPS ARE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,339 hrs · 25,131 cycles

RBL 18 FLOOR SUPPORT STRUCTURE LOWER INBD ANGLE CRACKED AT FS 559.00 +32.

Part: ATTACH BRACKET — BROKEN (LT INLET) · airframe 26,339 hrs · 25,131 cycles

LEFT ENG INLET HAS TWO EACH BROKEN T2 LINE ATTACH BRACKETS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,339 hrs · 25,131 cycles

INBD & OTBD CLIPS ARE CRACKED AT FS 280 FLOORBEAM RBL 9.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,339 hrs · 25,131 cycles

FS 280 FLOOR SUPPORT AFT ANGLE CRACKED OTBD OF RBL 9.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,339 hrs · 25,131 cycles

FLOOR SUPPORT CROSSBEAM AT FS 349 HAS CORROSION ON TOP FROM RBL 36 TO 43.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 26,339 hrs · 25,131 cycles

RIGHT MLG WW TRANSDUCER BRACKET IS CRACKED.

Part: SEAL — CRACKED (SPOILER) · airframe 26,339 hrs · 25,131 cycles

LEFT WING, UPPER TE, CTR SPRING SEAL COMMON TO FLIGHT SPOILER IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,339 hrs · 25,131 cycles

LEFT INBD & OTBD FS 484 CLIPS ARE CRACKED.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,339 hrs · 25,131 cycles

FS 310 FRAME TO SERVICE DOOR LOWER SILL ATTACH BRACKET CORRODED.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 26,339 hrs · 25,131 cycles

OTBD SUPPORT BRACKET FOR SINGLE POINT REFUELING AT RT WING IS CRACKED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,339 hrs · 25,131 cycles

FLOOR SILL IS CORRODED BETWEEN FS 307 & 309 AT RBL 43, SERVICE DOOR AREA.

Part: SKIN — DENTED (LT ELEVATOR)

LEFT ELEVATOR SKIN DENTED.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 26,339 hrs · 25,131 cycles

CARGO DOOR TRACK SUPPORT ASSEMBLY CLIP CRACKED AT FS 621 BULKHEAD.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 26,339 hrs · 25,131 cycles

LEFT ENG THRUST REVERSER STOW SWITCH BRACKET CRACKED.

Part: SKIN — DENTED (FUSELAGE)

DENT IN EXTERNAL SKIN FS 282, BETWEEN STRINGER 24R & 25R.

Part: BPSU — FAULTY (TE FLAP) · airframe 26,213 hrs · 25,017 cycles

FLAP FAIL CAUTION MSG DURING FINAL APPROACH WHEN FLAPS SELECTED FROM ZERO TO EIGHT. FLAPS STILL INDICATED ZERO. FOUND LT BPSU FAULTS. REPLACED LT WING BPSU IAW AMM CH 27-51, OPERATIONS CHECKED GOOD. REMOVED PLACARD & REMOVED FROM MEL SN OFF 2079 & ON 2383 CLM.

Part: FLAP — MALFUNCTIONED (WING) · airframe 26,205 hrs · 25,011 cycles

FLAPS FAILED AT 45 DEG AFTER LANDING WHEN SELECTING FLAPS FROM 45 TO 0. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-018F BOX 12. FLAPS RESET, PLACARDED & PLACED ON MEL.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 26,199 hrs · 25,005 cycles

3720 FLAPS FAIL CAUTION MSG RECEIVED OUT OF FL 220. FLAPS HAD ALREADY BEEN AT 0 FOR A WHILE. PERFORMED RESET PROCEDURE IAW SUPP 98-18F, BOX 12. FLAPS RESET, PLACARD & PLACED ON MEL. R & R LT FLAP BRAKE & POSITION SENSOR UNIT IAW AMM 27-51-10. OPERATIONS & RIG CHECKED GOOD. REMOVED PLACARD & FROM MEL.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 24,601 hrs · 23,490 cycles

FLAPS FAIL AT 30 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW SUPPLEMENT 98-018F BOX 12. FLAPS RESET.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 24,501 hrs · 23,392 cycles

DURING CLIMB OUT, AFTER FLAPS WERE RETRACTED TO ZERO FOR A FEW SECONDS, RECEIVED A FLAP FAIL CAUTION MESSAGE. RETURNED TO DEPARTURE, LANDED FLAPS 0, BRAKE TEMPS NORMAL, WT 46800.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 22,355 hrs · 21,336 cycles

DURING CLIMBOUT AT APPROX 15,000FT RECEIVED A NLG UP WARNING WHILE RUNNING THE QRH WARNING CLEARED. WHILE LANDING APPROX 1000 FT GOT A NLG DOWN DISAGREE. CONFIRMED WARNING MESSAGE WITH GEAR INDICATION AMBER FOR DOWN AND RED FOR UP. COMPLETED AIRCRAFT JACKING. LOWERING CHECKLIST.

Part: WIRE HARNESS — DAMAGED (NR 2) · airframe 22,354 hrs · 21,335 cycles

ON 1ST APPROACH NLG IND YELLOW AFTER GO AROUND AND GEAR RECYCLED INDICATIONS WERE NORMAL. FOUND NR 2 WOW HARNESS DAMAGED REMOVED AND REPLACED NR 2 WOW HARNESS IAW AWAC SUP 12-029A, OPS CHECKS GOOD AT THIS TIME.

Part: SUPPORT ANGLE — CRACKED (ASSIST MOTOR) · airframe 21,502 hrs · 20,523 cycles

PAX DOOR ASSIST MOTOR FWD SUPPORT ANGLE IN DOOR CRACKED. R & R PAX DOOR ASSIST MOTOR FWD SUPPORT ANGLE IAW SRM 51-40-11 & 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,502 hrs · 20,523 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. R & R NEW DRAG ANGLE ON PAX DOOR IAW REO 601R-52-11-513, REV A.

Part: STRIKER — GOUGED (FS 310) · airframe 21,502 hrs · 20,523 cycles

PAX DOOR CUT OUT FWD SEAL STRIKER GOUGED AT FS 310.00. REPAIRED PAX DOOR CUT OUT FWD SEAL STRIKER IAW REO 601R-53-22-033, TYPE I REPAIR.

Part: CARGO TRACK — CORRODED (FS 559) · corrosion level 2 · airframe 21,502 hrs · 20,523 cycles

CARGO TRACKS ON LBL 9 & RBL 9 AT FS 559+112 HAVE CORROSION. R & R CORRODED SEAT TRACKS AT FS 559+112 AT LBL9 & RBL9 IAW AMM 53-01-11.

Part: BRACKET — CRACKED (FS 180) · airframe 21,502 hrs · 20,523 cycles

SYS 3 BRAKE ACCUMULATOR FWD OTBD BRACKET CRACKED. R & R BRACKET WITH NEW SERVICEABLE BRACKET SRM 51-42-06 AND 51-41-11.

Part: SHUTOFF VALVE — FAILED (ANTI ICE SYSTEM) · airframe 20,403 hrs · 19,399 cycles

RT WING ANTI-ICE CAUTION MESSAGE ON T/O ROLL. ABORTED T/O AT OR BELOW 80 KIAS, MESSAGE CONTINUES W/ANTI-ICE ON. R & R RT MODULATING/SHUTOFF VALVE IAW AMM 30-12-04 OP AND LEAK CHECKED GOOD AT THIS TIME.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 19,184 hrs · 18,142 cycles

SERVICE DOOR CANNOT BE OPENED FROM THE OUTSIDE. HANDLE DOES NOT EXTEND. CLEANED AND LUBED SERVICE DOOR OUTER HANDLE REF AMM 12-20-52. OPS CHECKED GOOD DOOR HANDLE SHAFT WAS COMPLETELY DRY.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS) · airframe 17,640 hrs · 16,533 cycles

AT FL340 AT 300 KIAS, DURING INITIAL DESCENT, ACFT ABRUPTLY NOSED DOWN. NOTICED GEAR AND FLAP INDICATION ON EDI, FLAPS SHOWED EXTEND TO 5 DEG AND RETURNED TO ZERO DISCONNECTED A/P. FLAP HANDLE NEVER MOVED FORM ZERO POSITION. REPLACED FAULTY LT FLAP POSITION TRANSMITTER IAW AMM 27-55-01. OPS CK GOOD SEE 214758/8 OVERSPEED INSP NOT REQUIRED. FLAPS NEVER MOVED. OK FOR SERVICE.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS) · airframe 17,442 hrs · 16,329 cycles

DURING INITIAL DESCENT, ACFT ABRUPTLY NOSED DOWN. NOTICED GEAR AND FLAP INDICATION ON EDI, FLAPS SHOWED EXTEDED TO 5 DEG AND RETURNED TO ZERO, DISCONNECTED A/P. FLAP HANDLE NEVER MOVED FROM ZERO POSITION. REPLACED FAULTY LT FLAP POSITION TRANSMITTER IAW AMM 27-55-01. OPS CK GOOD, SEE 214758/8. OVERSPEED INSP NOT REQUIRED. FLAPS NEVER MOVED. OK FOR SERVICE.

Part: PANEL — CRACKED (THRUST REVERSER) · airframe 17,192 hrs · 16,092 cycles

LEFT THRUST REVERSER 4 O`CLOCK SAM PANEL SUPPORT ON TORQUE BOX CRACKED AT MOUNTING FLANGE. REPAIRED CRACKED FLANGE ON LT T/R AT 4 O`CLOCK POSITION BY REMOVING DAMAGED PORTION, FABRICATING & INSTALLING REPAIR DOUBLER AND FILLER IAW REO 601R-78-30-4013.

Part: BRACKET — CRACKED (RT ENGINE) · airframe 17,192 hrs · 16,092 cycles

RT ENG JETPIPE NUTPLATE BRACKET PN 228-50181-833 UNDER PANEL 446BL IS CRACKED. REMOVED CRACKED BRACKET ASSY PN 228-50181-833. LOCATE AND INSTALLED NEW SERVICEABLE BRACKET ASSY PN 228-550181-833 UNDER PANEL 446BL, R JET PIPE.

Part: BRACKET — CRACKED (BS 193) · airframe 17,192 hrs · 16,902 cycles

MOUNT BRACKET FOR AC GROUND POWER UNDER DOOR 122BR IS CRACKED AT RECEPTACLE MOUNT HOLES. R & R AC GROUND POWER RECEPTACLE MOUNT BRACKET IAW SRM 51-42-06, 51-40-11, 51-42-20.

Part: RIB — CRACKED (RT WING) · airframe 1,719,204 hrs · 16,092 cycles

RT WW BATT RIB CRACKED AT WS 53.60. TRIMMED OUT DAMAGED AREA AND REPAIRED IAW REO 601R-57-51-046, REV B.

Part: SKIN — SCORED (RT WING) · airframe 1,719,204 hrs · 16,092 cycles

SCRIBE MARK ON UNDERSIDE OF RT WING AT WS389 JUST AFT OF THE L/E. DEPTH OF SCRIBE MARK MEASURED 0.002" BLENDED SCRIBE MARK AREA TO REMOVE MARK, NOT EXCEEDING ORIGINAL DEPTH OF 0.002". PERFORMED NDT OF AREA, PERFORMED ROTO PEEN OF AREA THEN REAPPLIED FINISH IAW REO 601R-57-31-1136.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 1,719,204 hrs · 16,092 cycles

FWD PAX DOOR SWIVEL BRACKET IS CRACKED. REMOVED & INSTALL BOLTS INTO SWIVEL BRACKET IAW SRM 51-41-02.

Part: BULKHEAD — CHAFED (BS 280) · airframe 1,719,204 hrs · 16,092 cycles

AFT SIDE OF RT 280.80 BULKHEAD CHAFED FROM GALLEY DOOR REPAIRED IAW REO 601R-53-11-1727, REV C.

Part: SILL — CORRODED (BS 574-621) · corrosion level 2 · airframe 1,719,204 hrs · 16,092 cycles

CARGO DOOR SILL HAS CORROSION PN 601R35011-63, FS 574.00 TO 621.00, LEVEL 2 CORROSION. REMOVED CORRODED SILL AND REPLACED WITH NEW SERVICEABLE IAW REO 601R-53-61-1574 AND SRM 51-00-53-00.

Part: SEAT TRACK — CHAFED (BS 409-500) · airframe 1,719,204 hrs · 16,092 cycles

LT CABIN SIDE SEAT RAIL IS CHAFED ST APPROX FS 409+55. R & R EXISTING DAMAGE AT SEAT RAIL WITH NEW ON LT CABIN AT APPROX FA 409+55 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 1,719,204 hrs · 16,092 cycles

LT CABIN FLOOR FS409+128 TO FS 559 SEAT RAIL IS CORRODED. REOMOVED UNSERVICEABLE SEAT RAIL AND REPLACED NEW SERVICEABLE SEAT RAIL PN N126-2075 ON LT CABIN FLOOR FS 409+128 TO FS559 IAW AMM 53-01-11.

Part: ANGLE — CRACKED (BS 625) · airframe 1,719,204 hrs · 16,092 cycles

RT OBLIQUE ANGLE PN 601-35012-52 FS625 CRACKED. R & R PN 601-35012-52 IAW REO 601R-53-61-985NC.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 17,192 hrs · 16,092 cycles

PARKING BRAKE FEED THROUGH AT FS 202 IS CRACKED. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71, WL 69.795 IAW REO 601R-53-11-1982.

Part: FITTING — CRACKED (BS 461) · airframe 1,719,204 hrs · 16,092 cycles

BOTH TUBE FITTINGS ON RBL9 OTBD SIDE AT FS461 IS CRACKED. R & R FITTING FS461, 9, IAW SRM 51-42-20.

Part: HINGE — CORRODED (BS 559) · corrosion level 2 · airframe 1,719,204 hrs · 16,092 cycles

LAV SERVICE DOOR UPPER HINGE CORRODED AND LOWER HINGE. REMOVED UNSERVICEABLE LOWER HINGES FROM LAV SERVICE DOOR AND INSTALLED SERVICEABLE HINGES IAW SRM 51-42-21A.

Part: SEAT TRACK — CORRODED (BS 333) · corrosion level 2 · airframe 1,719,204 hrs · 16,092 cycles

NR1 SEAT TRACKS ON LBL 9 HAS CORROSION. REMOVED UNSERVICEABLE SEAT TRACK LBL 9 NR 1 AND REPLACED FOR NEW SERVICEABLE SEAT TRACK PN N126-2075 ON LBL9 NR 1 IAW AMM 53-01-05.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 17,192 hrs · 16,092 cycles

FS 484, RBL 36 CLIP CRACKED. MFG AND INSTALLED NEW CLIP AT FS 484, RBL 36 IAW REO 601R-53-41-059 AND SRM 51-24-21.

Part: ANGLE — CRACKED (BS 625) · airframe 1,719,204 hrs · 16,092 cycles

LT OBLIQUE ANGLE FS625 CRACK REMOVED UNSERVICEABLE LT OBLIQUE ANGLE AND INSTALLED SERVICEABLE LT OBLIQUE ANGLE.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 17,192 hrs · 16,092 cycles

CARGO DOOR CAM TRACK SUPPORT CRACKED. R & R SUPPORT CHANNEL ON CARGO DOOR CAM TRACK IAW SRM 51-42-06.

Part: RIB — CRACKED (LT WING) · airframe 1,719,204 hrs · 16,092 cycles

LT WHEEL WELL BATTERY RIB CRACKED AT WS 53.60. TRIMMED OUT DAMAGED AREA AND REPAIRED IAW REO 601R-57-51-046, REV B.

Part: SKIN — DAMAGED (BS574) · airframe 16,569 hrs · 15,410 cycles

EVALUATE MULTIPLE DENTS IN LOWER FUSELAGE BETWEEN FS 574.00 AND FS 589.00 AND STRINGERS 24L AND 26L. COMPLIED WITH PERMANENT REPAIR TO MULTIPLE DENTS IN LOWER FUSELAGE BETWEEN FS 574.00 AND FS 589.00 AND STRINGERS 24L THRU 26L.

Part: COMPUTER — MALFUNCTIONED (STALL) · airframe 15,720 hrs · 14,530 cycles

STALL FAIL CAUTION AFTER TAKEOFF. QRH COMPLETED. STALL FAIL MESSAGE REMAINS. R & R STALL PROTECTION COMPUTER IAW AMM 27-35-01-000-400-801. OPS CK GOOD IAW AMM 27-35-01-710-801.

Part: PUSHROD — OUT OF ADJUST (DOOR LOCK INDI) · airframe 14,713 hrs · 13,543 cycles

LOWER MOST INDICATOR ON MAIN CABIN DOOR DOES NOT SHOW FULLY CLOSED. ADJUSTED INNER PAX DOOR LOCK INDICATOR PUSH ROD IAW 52-11, ALL INDICATIONS, OK. (K)

Part: PANEL — MALFUNCTIONED (RT ADC) · airframe 14,644 hrs · 13,473 cycles

LOST ADC NR 1 INFORMATION DURING CLIMBOUT, SWITCHED TO ADC NR 2 INDICATIONS NORMAL. C/W QRH, PERFORMED AIR RETURN TO DEPARTURE. LANDED AT 47.200 LBS, 300 FT/MIN. BRAKE TEMPS READ 5-5-5-6. FOUND AIR DATA REF PANEL NR 2 TO HAVE NO OUTPUT TO AIR DATA COMPUTERS. REMOVED AND REPLACED ADRP NR 2 IAW AMM 34-10-00. OPS CHECK OF NR 1 AND NR 2 AIR DATA SYS ARE GOOD. (K)

Part: OVERHEAT LOOP — MALFUNCTIONED · airframe 13,491 hrs · 12,394 cycles

188294/3 - RT 14TH DUCT WARNING MESSAGE ON TAKEOFF. ABORTED AT 80 KNOTS, BRAKE TEMPS 4, 4, 1, 2. REMOVED AND REPLACED PYLON 14TH STAGE BLEED LOOP. OPS CHECK GOOD. (K)

Part: SENSOR — MALFUNCTIONED (OVERHEAT LOOP) · airframe 13,436 hrs · 12,344 cycles

DLY RT 14TH STAGE DUCT OVERHEAT ILLUMINATED AFTER T/O, CW QRH WARNING PERSISTED WITH RT 14TH STAGE TURNED OFF. REMOVED AND REPLACED BLEED AIR SENSING LOOP A40WK IN RT WHEELWELL OPS CHECK GOOD AT THIS TIME IAW AMM 36-21-00. (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 13,199 hrs · 12,111 cycles

LOWER SILL OF PAX DOOR ENTRANCE CORRODED. R&R LOWER SILL OF PAX DOOR ENTRANCE IAW CRJ 200 SRM 51-42-06 AND 51-42-01.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 13,199 hrs · 12,111 cycles

PAX AFT STAIR ANGLE FOUND CRACK LENGTH .650. PAX AFT STAIR ANGLE REPAIRED IAW REO 601R-52-11-513.

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,199 hrs · 12,111 cycles

131262-36 - PAX DOOR AFT SIDE PANEL FOUND CRACK (CRACK LENGTH 0.650) PAX DOOR AFT SIDE PANEL CRACK REPAIRED IAW REO-601R-52-11-702. (K)

Part: PANEL — CRACKED (PAX DOOR) · airframe 13,199 hrs · 12,111 cycles

PAX DOOR FWD SIDE PANEL FOUND CRACK (CRACK LENGTH 0.600) PAX DOOR FWD SIDE PANEL CRACK REPAIRED IAW REO 601R-52-11-702. (K)

Part: BRACKET — CRACKED (FUSELAGE) · airframe 13,199 hrs · 12,111 cycles

CRACK FOUND ON BRACKET FS 280 RBL 9 INBD. CRACK LENGTH .500. BRACKET ON FS 280 RBL 9 INBD REPLACED IAW SRM 51-42-06 AND SRM 51-42-20.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,199 hrs · 12,111 cycles

CRACK FOUND ON TOP ANGLE AFT FACE OF PILOT BULKHEAD FS 280 LBL 9. CRACK LENGTH IS 1.500. CUT OUT PERFORMED AND PART FABRICATED AND INSTALLED ON TOP ANGLE AFT FACE OF PILOT BULKHEAD FS 280 LBL P IAW REO 601R 53-11-138 REV NC.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 13,199 hrs · 12,111 cycles

CRACK FOUND ON Z BRACKET FS 280 LBL 9 INBD AND OTBD. CRACK LENGTH IS .500. Z BRACKET ON FS 280 LBL 9 INBD AND OTBD REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-20.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 13,199 hrs · 12,111 cycles

MWC 131263/139 - CRACK FOUND ON INTERCOSTAL BRACKET FS 484, RBL27 (CRACK LENGTH .500) BRACKET REPLACED IAW SRM 57-42-06. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 13,199 hrs · 12,111 cycles

CRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9 JOB PERFORMED ON PILOT BULKHEAD FS 280, RBL 9 IAW REO 601R-53-11-171, REV "D" SCHEME "B". (K)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,199 hrs · 12,111 cycles

AFT PRESSURE BULKHEAD CRACK AT LINTEL LOCATION REPAIR TO LINTEL LOCATION AT PRESSURE BULKHEAD AFT IAW CRJ 200 REO 601R-53-61-1230 REV D.

Part: CONTROL UNIT — MALFUNCTIONED (BLEED AIR SYS) · airframe 13,115 hrs · 12,021 cycles

RT 14TH DUCT WARNING MSG ON DESCENT INTO PHL, QRH PERFORMED, REQUIRED LANDING WITH RT ENGINE AT IDLE THRUST. R&R BLEED AIR LEAK CALL UNIT IAW AMM 36-21-10. RAN RT ENGINE AT TAKE OFF POWER FOR 30 MINUTES AND 30 MINUTES AT IDLE. OPS CHECK GOOD.

Part: TARGET — LOOSE (RT UPLOCK) · airframe 11,771 hrs · 10,733 cycles

RT MLG DISAGREE ON DEPARTURE. COMPLIED WITH QRH GEAR CAME DOWN ALL THREE SHOWED LOCKED. RT UPLOCK TARGET FOUND LOOSE, RETIGHTENED PER CMM 32-30-16 FUNCTION TEST OF EXTENSION AND RETRACTION TEST GOOD. (A)

Part: CONNECTOR — DAMAGED (WOW) · airframe 10,825 hrs · 9,831 cycles

WOW INPUT CAUTION MESSAGE DISPLAYED ON T/O ROLL AT 100 KNOTS, MESSAGE CLEARED ON GEAR RETRACTION. MESSAGE REAPPEARED ON GEAR EXTENSION DURING LANDING. PROXY FAULTS STATUS DISPLAYED ON GROUND. REPOSITIONED MLG NR 1 WOW HARNESS AS REQUIRED, CLEANED AND RESEATED CONNECTOR PLUG IAW 32-46. PERFORMED GEAR SWINGS. OPS CHECK GOOD. (K)

Part: ANGLE — CRACKED (BS 484) · airframe 8,659 hrs · 7,800 cycles

LT FS 484.0 ANGLE CRACKED APPROX .1 INCH LONG AT PRESSURE FLOOR SUPPORT BEAM LBL 27.0. (K) [SUP 5-1-07] MAINTENANCE REMOVED ANGLE AT FS 484 LT LBL 27 IAW CRJ 200 SRM 51-42-06 AND FABED A NEW ANGLE FROM S6144-14 EXTENSION AND INSTALLED NEW ANGLE IAW BSC SR 601R-53-0029B. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,659 hrs · 7,800 cycles

RT FS 621.00 FLOOR SUPPORT ANGLE CRACKED APPROX .5 INCH LONG. (K) [SUP 5-1-07] MAINTENANCE REMOVED DAMAGED SECTION OF THE RIGHT FLOOR SUPPORT ANGLE AT FS 621 AND INSTALLED REPAIR ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,659 hrs · 7,800 cycles

RT FS 484.0 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT PRESSURE FLOORBEAM RBL 36.0. (K) [SUP 5-1-07] MAINTENANCE CUT AWAY DAMAGED ATTACHMENT FLANGE FABRICATED ANGLE FROM S6144-14 AND INSTALLED ANGLE IAW BOMBARDIER REO 601R-53-41-059A AND BSC SR 601R-53-0030A. (M)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 8,659 hrs · 7,800 cycles

RT FS 484.0 ANGLE CRACKED APPROX .1 INCH LONG AT PRESSURE FLOORBEAM RBL 27.0. (K) [SUP 5-1-07] MAINTENANCE REMOVED CRACKED ANGLE AT FS 484 RBL 27 ON THE PRESSURE FLOORBEAM AND INSTALLED A NEW SERVICEABLE ANGLE P/N 601R31171-9 IAW CRJ 200 SRM 51-42-06 AND 51-42-13. (M)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,659 hrs · 7,800 cycles

LT FS 484.0 INTERCOSTAL CRACKED APPROX .1 INCH LONG AT PRESSURE FLOORBEAM LBL 36.0. (K) [SUP 05-01-07] MAINTENANCE CUT OUT DAMAGED SECTION OF INTERCOSTAL AT FS 484 LBL 36 AT THE PRESSURE FLOOR SUPPORT BEAM FABBED AND INSTALLED NEW ANGLE IAW BOMBARDIER REO 601R-53-41-059 AND BSC SR 601R-53-0030A. (M)

Part: INTERCOSTAL — CRACKED (BS 620-625) · airframe 8,659 hrs · 7,800 cycles

LT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. (K) MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL AT STRINGER 14L BETWEEN FS 621 AND 625.30 IAW CRJ 200 SRM 51-42-06. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 8,659 hrs · 7,800 cycles

RT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .9 INCH LONG. (K) [SUP 05-01-07] MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL FROM 621 TO 625.30 AT STRINGER 14R IAW CRJ 200 SRM 51-42-06. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

AT CRUISE FL230, LEFT ENGINE WAS UNRESPONSIVE TO THRUST LEVER MOVEMENT. PERFORMED ENGINE RUNS WITH SPEED CONTROL ON AND OFF WITH NO CHANGE IN ENGINE PARAMETERS, CLEANED LT T2 SENSOR PER AMM 73-21-11. OPS CHECK GOOD PER AMM 71-00-00. REMOVED FROM MEL. (M)

Part: COALESCER BAG — DIRTY (A/C BAY)

FOUND LEFT PACK EMITS ODOR WHEN SELECTED ON, COMPLIED WITH `CM` ACTION PLACARDED AND PLACED ON MEL. REMOVED AND REPLACED LEFT COALESCER BAG. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

PERMANENT REPAIR IS REQUIRED FOR LIGHTNING STRIKE DAMAGE AT FS 364, STRINGER 8L. REPAIRED LIGHTNING STRIKE DAMAGE TO FUSELAGE IAW BRAS EO 601R-53-6363A. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

PERMANENT REPAIR REQUIRED FOR LIGHTNING STRIKE DAMAGE AT FS 394, STRINGER 8L. REPAIRED LIGHTNING STRIKE DAMAGE IAW BRAS EO 601-R-53-6364A. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

LHS FS 621 FLOOR SUPPORT ANGLE IS CRACKED. INSTALLED REPAIR ANGLE IAW BOMBARDIER, INC REO 601R-53-61-117 REV C. (M)

Part: SKIN — FRETTED (RT WING)

RIGHT LOWER WING PLANK HAS FRETTING DAMAGE AT FUEL TANK ACCESS DOOR CUT OUTS AT WS 116.366 AND WS 136-676. MEASURES .001 TO .002 WIDTH DEEP AROUND ENTIRE CUT OUT. REPAIRED FRETTING DAMAGE BY BLENDING IAW BOMBARDIER INC REO 601R-57-21-030 REV C. (M)

Part: CHANNEL — CRACKED (T/E FLAP)

LEFT OUTBOARD FLAP T/E PUSHED FORWARD, .375 INCH WIDE BY .0625 INCH DEEP. REPAIRED LEFT OUTBOARD FLAP TRAILING EDGE. REMOVED CRACKED CHANNEL P/N 601R14538-3 AND INSTALLED SERVICEABLE CHANNEL P[/N 601R14538-3, IAW CRJ 200 SRM 51-25-01, 51-42-06, 51-42-10 AND BOMBARDIER DRAWING 601R14501. (M)

Part: ODOR — DETECTED (CABIN)

STRANGE ODOR NOTED IN CABIN. REVIEWED HISTORY IN ATA 21-24-33-36-49, NO HISTORY ASSOCIATED WITH CABIN ODOR, INSPECTED CABIN, EXTERIOR, MLG BAGS, CARGO BAY, AFT EQUIPMENT BAY AND AVIONICS BAY. NO DEFECTS NOTED. COULD NOT DUPLICATE WITH PASSENGERS DEBOARDED. (M)