N467AW

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,763 hrs · 38,601 cycles

INFLIGHT RECEIVED DISPLAY COOL CAUTION MESSAGE. MESSAGE BECAME INTERMITTENT. EXTINGUISHED AND REMAINED OUT BELOW FL140. *****AIRCRAFT REMOVED FROM SERVICE******** FOUND DUCT TO DISPAY COOL PLENUM OFF. REATTACEHD DUCT IN REF TO AMM 21-24 OPS CHECK GOOD. ALL FANS CHECK GOOD.

Part: SEAT TRACK — CORRODED (FS 449 TO FS 499) · corrosion level 2 · airframe 39,700 hrs · 38,532 cycles

CORROSION ON CABIN LH SIDE SEAT TRACK PN 20276-288-0-0 AT FS449.85 TO FS499.0. P7 - L= 0.800Ï¿½ X W= 0.400Ï¿½ X D= 0.023Ï¿½, REMAINING THICKNESS 0.077Ï¿½, CENTER OF SEAT TRACK AT FS449.85+2.0Ï¿½. *****AIRCRAFT REMOVED FROM SERVICE******* REPLACED WITH A NEW SEAT TRACK PN 20276-288-0-0 AT FS449.85 TO FS499.0. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ CRJ200 AMM 53-01-11-400-802 REV 66, SRM 51-40-11 REV 39, SRM 51-21-11 REV 39, SRM 51-77-00 REV 39 ALL WORK WITHIN LIMITS PERFORMED UNDER AERSALE WORK ORDER 003883, CARD NO. 20051, TT: 39,700:41 TC: 38,532.

Part: DOUBLER — DENTED (FS589 TO FS605) · airframe 39,700 hrs · 38,532 cycles

DENT ON AFT FUSELAGE SKIN AT FS589-605 AND BETWEEN S22R -25R. ADDITIONAL DAMAGE TO FS574-589 AND S22R TO 25R. FASTENERS INSTALLED FOUND CLOSE TO RADIUS OF STRINGER & WEAR DAMAGE TO STRINGER FLANGE DUE TO DOOR. LATCH WEAR. PERFORMED TEMPORARY REPAIR TO SKIN, FABRICATED DOUBLER & TRIPLER. FABRICATED DOUBLER FILLER. INSTALLED DOUBLER, TRIPLER & DOUBLER FILLER. BLENDED DAMAGE TO STRINGER FLANGE. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WERE PERFORMED IAW REO 601R-53-61-7969 REV --.

Part: NONE — NONE (RH HORIZ STAB) · airframe 39,700 hrs · 38,532 cycles

RH HORIZONTAL STABILIZER SHROUD UPPER FLANGE HAS 1 ELONGATED HOLE BETWEEN FSS 110.63 AND FSS 118.63. ****AIRCRAFT REMOVED FROM SERVICE******* TEMPORARY REPAIR DISPOSITION FOR RH HORIZONTAL STABILIZER SHROUD UPPER FLANGE, 1 ELONGATED HOLE BETWEEN FSS 110.63 AND FSS 118.63. STABILIZER ASSEMBLY PN 601R23025-1. ELONGATED HOLE DIMENSION IS L= 0400Ï¿½ X W= 0.250Ï¿½. THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 5000 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REPAIR. VISUAL INSPECTION REQUIRED AT INTERVALS NOT TO EXCEED 500 FLIGHT HOURS. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-55-12-726 REV (--) DATED 2023/02/24. WORK PERFORMED UNDER AERSALE WORK ORDER 003883, CARD NO. 20150, CARD ID # 1833813. N467AW TT: 39,700:41 TC: 38,532.

Part: ANGLE — CORRODED (FS349) · corrosion level 2 · airframe 39,700 hrs · 38,532 cycles

CORROSION ON CABIN FLOOR SUPPORT STRUCTURE AT FS349 AND RBL27 TO RBL 42. *****AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED CABIN FLOOR SUPPORT ANGLE PN 601R38783-13 AT FS349 AND RBL27 TO RBL 42. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ CRJ200 SRM 51-11-00 REV 39, SRM 51-25-06 REV 39, SRM 51-40-11 REV 39, SRM 51-42-20 REV 39, SRM 51-42-13 REV 39, SRM 51-42-15 REV 39, SRM 51-42-20 REV 39 AND SRM 51-42-06 REV 39. ALL WORK WITHIN LIMITS PERFORMED UNDER AERSALE WORK ORDER 003883, CARD NO. 20134, TT: 39,700:41 TC: 38,532.

Part: UNKNOWN — UNKNOWN · airframe 39,700 hrs · 38,532 cycles

COMPLY WITH EO E17/003/453 AFT FUSELAGE MODIFICATION TO FS621.00 PRESSURE BULKHEAD WEB. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH EO E17/003/453 AFT FUSELAGE MODIFICATION TO FS621.00 PRESSURE BULKHEAD WEB. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW EO E17/003/453, REV C, DATED OCTOBER 22, 2020 AND MHIRJ REO 601R-53-61-1240 REV (D) DATED 2016-10-31. WORK PERFORMED UNDER AERSALE WORK ORDER 003883, CARD NO. 00003, TT: 39,700:41 TC: 38,532.

Part: SKIN — CHAFED (RH FLAP VANE) · airframe 39,700 hrs · 38,532 cycles

RH INBOARD FLAP VANE HAS WEAR MARK AT OUTBOARD END OF LEADING EDGE SKIN PN 601R14303-44. WEAR DIMENSIONS FOR P3 ARE - L = 1.800Ï¿½ X W = 0.650Ï¿½ X D = 0.014Ï¿½, WS 135.513+3.5 TO WS 142.512+0.50. ******AIRCRAFT REMOVED FROM SERVICE******** BLENDED DAMAGE OF RH INBOARD FLAP VANE HAS WEAR MARK AT OUTBOARD END OF LEADING EDGE SKIN PN 601R14303-44. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01957 REV IR DATED 2/15/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003883, CARD NO. 20054, CARD ID # 1822430. N467AW TT: 39,700:41 TC: 38,532.

Part: SKIN — CHAFED (RH FLAP VANE) · airframe 39,700 hrs · 38,532 cycles

RH INBOARD FLAP VANE HAS WEAR MARK AT CENTER OF LEADING EDGE SKIN PN 601R14303-52. WEAR DIMENSIONS FOR P2 ARE - L = 2.300Ï¿½ X W = 0.500Ï¿½ X D = 0.012Ï¿½, WS 97.009+6.5 TO WS 106.352+1.0. *********AIRCRAFT REMOVED FROM SERVICE********** BLENDED DAMAGE OF RH INBOARD FLAP VANE HAS WEAR MARK AT CENTER OF LEADING EDGE SKIN PN 601R14303-52. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01958 REV IR DATED 2/15/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003883, CARD NO. 20054, CARD ID # 1822430. N467AW TT: 39,700:41 TC: 38,532.

Part: SKIN — CHAFED (RH FLAP VANE) · airframe 39,700 hrs · 38,532 cycles

RH INBOARD FLAP VANE HAS WEAR MARK AT INBD END OF LEADING EDGE SKIN PN 601R14303-54. WEAR DIMENSIONS FOR P1 ARE - L = 2.100Ï¿½ X W = 0.700Ï¿½ X D = 0.018Ï¿½, WS 50.448+5.0 TO WS 54.848+1.5. *******AIRCRAFT REMOVED FROM SERVICE********** BLENDED DAMAGE OF RH INBOARD FLAP VANE HAS WEAR MARK AT INBOARD END OF LEADING EDGE SKIN PN 601R14303-54. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ257-01959 REV IR DATED 2/15/2023. WORK PERFORMED UNDER AERSALE WORK ORDER 003883, CARD NO. 20054, CARD ID # 1822430. N467AW TT: 39,700:41 TC: 38,532.

Part: NONE — NONE · airframe 38,503 hrs · 37,387 cycles

WHILE CLIMBING OUT OF KHPN AND GOING THROUGH 10,000', THE CABIN ALT CAUTION MESSAGE INDICATED. THE FO LEVELED OFF AND RETURNED TO 10,000' WHICH I COORDINATED WITH DEPARTURE CONTROL. THE CABIN WAS INDICATING AN ALTITUDE OF 9,300 AT THAT TIME. WE RAN THE QRH FOR CABIN ALT AND WERE UNABLE TO ESTABLISH A LOWER CABIN PRESSURE (NEITHER RESETTING THE PRESS CONT NOR MANUAL PRESSURIZATION CONTROL PROCEDURE WORKED). WE CONTACTED DISPATCHED AND RELAYED OUR SITUATION WHILE LOOKING AT POSSIBLE DIVERSION OPTIONS. DISPATCH INITIALLY REQUESTED WE CONTINUE ON OUR ROUTE AT 10,000 AND ASKED FOR A LITTLE TIME TO EVALUATE THE OPTIONS, EVENTUALLY REQUESTING THAT WE DIVERT TO KDAY WHERE THE AIRCRAFT COULD BE REPAIRED AND WE WOULD LIKELY BE ABLE TO SWAP AIRCRAFT TO CONTINUE TO KORD. SHORTLY AFTER COORDINATING WITH DISPATCH, WE RECEIVED A DISPLAY COOL CAUTION MESSAGE. WE RAN THE QRH FOR DISPLAY COOL AND THE MESSAGE CLEARED WHILE USING THE STDBY MODE ON THE DSPLY FAN. WE COMPLETED THE FLIGHT WITHOUT FURTHER INCIDENT AND SWAPPED AIRCRAFT IN DAY TO COMPLETE THE PLANNED FLIGHT TO ORD. ****AIRCRAFT REMOVED FROM SERVICE**** R&R VACUUM REGULATOR IAW AMM 21-31-07 PRESSURIZATION TEST REQUIRED BEFORE RETURN TO SERVICE REF 334612/3 FOR PRESSURIZATION TEST P/N: 131402-2, SN ON 1775D, SN OFF: 1091D ARW

Part: SKIN — DENTED (FS 682) · airframe 38,178 hrs · 37,040 cycles

MULTIPLE DENTS ON AFT FUSELAGE SKIN AT FS682.00 - FS700.00 AND RH STR22 TO STR24. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENTS ON AFT FUSELAGE SKIN AT FS682.00 - FS700.00 AND RH STR22 TO STR24 AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION P1- L = 7.200Ï¿½ X W = 0.550Ï¿½ X D = 0.011Ï¿½, P2- 6.00Ï¿½ X W = 0.500Ï¿½ X D = 0.007Ï¿½, P3- 0.500Ï¿½ X W = 0.450Ï¿½ X D = 0.006Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01692 REV IR DATED 10/05/2021.

Part: SKIN — DENTED (FS 605) · airframe 38,178 hrs · 37,040 cycles

DENT ON AFT FUSELAGE SKIN AT FS605.00 TO FS621.00 AND STR18L TO STR20L. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS605.00 TO FS621.00 AND STR18L TO STR20L AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 5.300Ï¿½ X W = 0.500Ï¿½ X D = 0.016Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01695 REV IR DATED 10/06/2021.

Part: NONE — DENTED (WS 220) · airframe 38,178 hrs · 37,040 cycles

RIGHT HAND OUTBOARD FLAP CENTER HINGE BOX AT WS220.00 HAS A GOUGE DAMAGE. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE ON RIGHT HAND OUTBOARD FLAP CENTER HINGE BOX AT WS220.00. ROTO PEENED REWORKED AREA. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-57-21-3526 REV (-) DATED 2021-10-06.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 35,713 hrs · 34,461 cycles

RT I/B FLAP VANE SKIN OB OF CENTER VANE ACT CHAFED. REMOVED AND REPLACED RT IB FLAP VANE SKIN OUTBOARD INSTALLED NEW FLAP VANE LEADING EDGE IAW SRM 51-42-13.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,713 hrs · 37,461 cycles

FS 409+128 BULKHEAD RBL 18 POST OUTBD SIDE HAS A CRACK INDICATION ON THE LOWER RADIUS. REPLACED.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

CARGO DOOR BEAM MEMBER 601R35050-64 HAS CUT MARKS FWD AND AFT FROM CABLE ASSIST. REPLACED DAMAGED BEAM IAW SRM 51-42-06, 51-40-11.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

ATTACH ANGLE CRACKED ON BOTTOM AFT CARGO DOOR BEAM, FS621.00. REPLACED ANGLE IAW SRM 51-42-06, 51-40-11-00, TR51-42, 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

VERTICAL POST AT FS 409+128, BL0 CRACKED ON BOTH LEFT AND RIGHT AFT ANGLES. REPLACED LEFT AND RIGHT AFT ANGLES IAW SRM 51-42-06, REO601R-53-41-889 REV-D.

Part: POST — CRACKED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

409+128 VERTICAL POST @ LBL18 CRACKED. REPLACED VERTICAL POST @ FS409+128, LBL18 IAW REO 601R-53-41889 REV-D.

Part: PANEL — CRACKED (PYLON) · airframe 35,713 hrs · 34,461 cycles

PANEL 446AL HAS CRACKED STIFFENER RING. REPLACED STIFFENER RING IAW CMM 20-42-06, 20-40-11.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 35,713 hrs · 34,461 cycles

AVIONICS BAY DOOR SEAL RETAINER CORRODED. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

FS 621 BULKHEAD RBL 36 PREVIOUS REPAIR HAS SCREW MARKS. REMOVE AND REPLACED DOUBLED IAW REO# 601R-53-61-1285 REV E.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

FS 621 BULKHEAD RBL 18 PREVIOUS REPAIR HAS SCREW MARKS. REMOVED AND REPLACED DOUBLER IAW REO# 601R-53-61-1285 REV E.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

FS 621 BULKHEAD RBL 27 PREVIOUS REPAIR HAS SCREW MARKS. REMOVED AND REPLACED DOUBLER IAW REO# 601R-53-61-1285 REV E.

Part: LANDING — CRACKED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

LT AFT TRU LAND LATCH IS CRACKED. REPAIRED TRU LAND LATCH AREA IAW SUPPLEMENT 19-016B.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

FS 621 BULKHEAD WL 103.5 AT LBL 18 PREVIOUS REPAIR HAS SCREW MARKS. REMOVED AND REPLACED DOUBLER IAW REO# 601R-53-61-1285 REV E.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

CARGO DOOR FWD TRACK LOWER SUPPORT CHANNEL IS CRACKED. REPLACED SUPPORT CHANNEL IAW SRM 51-42-06, 51-41-02.

Part: RETAINER — CRACKED (PAX DOOR) · airframe 35,713 hrs · 34,461 cycles

PASSENGER DOOR LOWER CENTER SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW REO 601R-52-11-915 AND SRM 51-42-13.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,713 hrs · 34,461 cycles

AFT PRESSURE BULKHEAD FS621.00 ON THE LEFT SIDE STR13L, INTERCOSTAL IS CRACKED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.

Part: DIVIDER — CHAFED (PYLON) · airframe 35,713 hrs · 34,461 cycles

PYLON PANEL 412DB HAS 2 EACH DIVIDER PANELS KNIFE EDGED. REPLACED DIVIDER PANELS IAW SRM 51-42-06, 51-42-13.

Part: DIVIDER — CHAFED (PYLON) · airframe 35,713 hrs · 34,461 cycles

PYON PANEL 422DB HAS 2 CHAFED DIVIDER PANELS. REPLACED DIVIDERS IAW SRM 51-42-06.

Part: RETAINER — CRACKED (PYLON) · airframe 35,713 hrs · 34,461 cycles

PYLON PANEL 422 DB HAD CRACKED SEAL RETAINER. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,624 hrs · 34,372 cycles

AFTER SELECTING GEAR DOWN ON FINAL APPROACH, RECIEVED GEAR DIS WRNING AFTER 6 SECONDS FROM DOWN SELECTION. RT MAIN GEAR SHOWED RED BOX UP. HYD TEMPS AND PRESSURE NORMAL NO OTHER ASSOCIATED MSGS DISPLAYED CONDUCTED GO AROUND, BROUGHT FLAPS TO 8 DEGREES LEFT GEAR SELECTED.

Part: RVDT — FAILED (NLG STEERING) · airframe 32,847 hrs · 31,667 cycles

DURING CRUISE, RECEIVED A STEERING INOPERATIVE MESSAGE, RAN QRH. LANDING WITH NOSE WHEEL STEERING IN OFF POSITION. AFTER LANDING REARMED NOSE WHEEL STEERING, MESSAGE PERSISTED. REMOVED AND REPLACED LEFT RVDT IAW AMM 32-51. OPS CHECKED GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 32,468 hrs · 31,271 cycles

RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES AFTER LANDING GEAR HANDLE SELECTED UP. MLG SHOWED UP AND LOCKED AND NLG SHOWED DOWN AND GREEN. MANUALLY LOWERED GEAR, LANDING SMOOTH AND UNEVENTFUL. ADJUSTED NOSE LANDING GEAR OLEO CENTERED/EXTENDED PROXIMITY SENSOR (PS12GA) IAW AMM 32-61-05, PERFORMED SEVERAL NOSE GEAR SWINGS, OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 333) · airframe 32,409 hrs · 31,208 cycles

FRAME AT BS 333 ABOVE MAIN ENTRY DOOR IS CRACKED AT EWIS SUPPORT ATTACH POINT.

Part: HEAT SHIELD — CRACKED (APU EXHAUST) · airframe 32,409 hrs · 31,208 cycles

APU EXHAUST HEAT SHIELD PREVIOUS REPAIR WELD CRACKED. REPAIRED APU HEAT SHIELD IAW REO 601R-49-81-003 REV-B.

Part: ATTACH BRACKET — CRACKED (BS 830) · airframe 32,409 hrs · 31,208 cycles

FWD ATTACH BRACKET FOR VERTICAL STAB ACCESS PANEL 326CR IS CRACKED. REPLACED THE ATTACH BRACKET IAW SRM 51-42-20.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 32,409 hrs · 31,208 cycles

PAX DOOR AFT RISER DRAG ANGLE CRACKED.

Part: FITTING — CRACKED (WINDOW POST) · airframe 32,409 hrs · 31,208 cycles

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

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 32,409 hrs · 31,208 cycles

REAR PRESSURE BULKHEAD, STRINGER 14R OBLIQUE ANGLE CRACKED.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 32,409 hrs · 31,208 cycles

REAR PRESSURE BULKHEAD AT STRINGER 14L OBLIQUE ANGLE IS CRACKED.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 32,409 hrs · 31,208 cycles

FLOOR SUPPORT CORRODED AT BS 574 TO 621, LBL 27. REPAIRED THE FLOOR SUPPORT IAW EA 15-2013-442.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 32,409 hrs · 31,208 cycles

ANGLE CRACKED AT BS 280, LBL 9 OTBD. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21, AND 51-40-11.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 32,409 hrs · 31,208 cycles

INBOARD FLOORBEAM ANGLE CRACKED AT BS 280, LBL 9. REPLACED THE ANGLE IAW SRM 51-42-06, AND REO 601R-53-11-926, REV-B.

Part: ANGLE — CRACKED (BS 484) · airframe 32,409 hrs · 31,208 cycles

ANGLE CRACKED AT BS 484, LBL 27. REPLACED THE ANGLE IAW REO 601R-53-41-059, REV-B.

Part: ANGLE — CRACKED (WINDOW FRAME) · airframe 32,409 hrs · 31,208 cycles

RIGHT WINDSHIELD SIDE POST LOWER OTBD ANGLE IS CRACKED. REPLACED THE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (WINDOW POST) · airframe 32,409 hrs · 31,208 cycles

LH WINDSHIELD SIDE POST LOWER OTBD ANGLE IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 32,409 hrs · 31,208 cycles

ANGLE CRACKED AT BS 484, LBL 36 ON INBD SIDE. REPLACED THE ANGLE IAW REO 601R-53-41-059, REV-B.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 31,602 hrs · 30,469 cycles

WHILE PERFORMING TASK MFG10970, SDI INSPECTION OF AFT PRESSURE BULKHEAD FORWARD FACE, FOUND 4 AREAS OF DAMAGE (DIVOTS) AND 1 CRACK. DIVOT #1 FOUND AT FS 621.00 RBL 36.2 WL 103 MEASURING .025 DEEP DIVOT #2 FOUND AT FS 621.00 RBL 27.5 WL 103 MEASURING .025 DEEP DIVOT #3 FOUND AT FS 621.00 RBL 18 WL 103 MEASURING .025 DEEP DIVOT #4 FOUND AT FS 621.00 LBL 18 WL 103 MEASURING .025 DEEP. CRACK FOUND AT FS 621.00 LBL 28 WL 130.5 MEASURING .5" LONG.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 31,199 hrs · 30,083 cycles

FLAPS FAILED AT 0 DEGREES INFLIGHT. COMPLIED WITH QRH, DECLARED EMERGENCY, LANDED AT DCA HAD TIRES INSPECTED AFTER LANDING (NO DEFECTS) BTMS INDICATED 2-3-3-3. PERFORMED FLAP RESET IAW AWAC SUPPLEMENT 98-18G, FLAPS RESET.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 30,922 hrs · 29,824 cycles

FLAPS FAILED AT 20 DEG. PERFORMED FLAP RESET PROCEDURE IAW 98-18G BOX 12. FLAPS RESET.

Part: WARNING LIGHT — ILLUMINATED · airframe 30,709 hrs · 29,634 cycles

ENROUTE, RECEIVED R14TH DUCT WARNING MESSAGE, COMPLIED WITH THE QRH, BOTH COWL & WING ANTI-ICE WERE OFF AT TIME OF OCCURRENCE, SYNOPTIC SHOWS RED DUCT SECTION BETWEEN RT 14TH SOV, RT 14TH MSOV, & RT COWL SOV. REMAINED RED INFLIGHT & ON GROUND.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 30,658 hrs · 29,585 cycles

DURING CLIMB, RECEIVED A RT PACK OFF STATUS MESSAGE. THIRTY SECONDS LATER, RECEIVED A LT PACK HIGH PRESSURE CAUTION AND CAS MISCOMPARE STATUS MESSAGE. ATTEMPTED TO RESET PACKS. COMPLIED WITH QRH. LANDED UNPRESSURIZED.

Part: UNKNOWN — ODOR · airframe 29,876 hrs · 28,845 cycles

INSPECTION FOR ELECTRICAL BURNING ODOR. INSPECTED AVIONICS BAY AND AFT BAY WITH NO ODOR OR EVIDENCE OF ELECTRICAL BURNING. STARTED APU RAN PACKS, NO DEFECTS NOTED. CREW RAN ENGINES WITH NO DEFECTS, SUSPECT JET BRIDGE GPU.

Part: UNKNOWN — MALFUNCTIONED (SERVICE DOOR) · airframe 29,697 hrs · 28,674 cycles

RAMP REPORTS: SERVICE DOOR UNABLE TO BE OPENED FROM OUTSIDE, DOOR OPENS NORMALLY FROM INSIDE ACFT. OUTSIDE HANDLE WILL NOT POP OUT.

Part: MODULATING VALVE — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 28,911 hrs · 27,946 cycles

LEFT WING ANTI-ICE CAUTION MSG. COMPLIED WITH QRH. PERFORMED M ACTION OF MEL 30-12-01-02, DEACTIVATED LT WING ANTI-ICE MODULATION VLV. R & R LT MODULATING VLV. OPERATION & LEAK CHECKED GOOD AT THIS TIME.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 28,929 hrs · 27,972 cycles

CAPTAIN WINDSCREEN CRACKED IN FLIGHT.

Part: DOOR — DIRTY (CABIN) · airframe 28,469 hrs · 27,540 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED & LUBED SERVICE DOOR. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 28,206 hrs · 27,292 cycles

AT 50 FT AGL, GEAR HORN SOUNDED WITH AMBER NOSE GEAR BOX ON EICAS, NO GEAR DISAGREE MSG. ACFT TOUCHED DOWN ON ALL 3 GEARS, INITIATED GO AROUND, WHEN THROTTLES ADVANCED, HORN CEASED & NLG BOX RETURNED TO GREEN, SELECTED GEAR UP FOR GO-AROUND. ALL INDICATIONS NORMAL & ALL NORMAL WHEN GEAR SELECTED DOWN FOR NORMAL LANDING.

Part: SKIN — DENTED (TE FLAP) · airframe 27,823 hrs · 26,927 cycles

RIGHT OTBD FLAP, UPPER SKIN HAS A DENT AT APPROX FLAP STATION 278.00, 2 INCHES AFT OF FRONT SPAR. REPAIRED FLAP UPPER SKIN IAW SRM 57-53-00 REPAIR 2.

Part: SKIN — CHAFED (RT AILERON) · airframe 27,823 hrs · 26,927 cycles

RIGHT AILERON LE UPPER SKIN CHAFED ON BOTH SIDES OF OTBD HINGE.

Part: SKIN — CHAFED (LT AILERON) · airframe 27,823 hrs · 26,927 cycles

LEFT AILERON LE UPPER SKIN CHAFED FROM INBD TO OTBD EDGES.

Part: SHROUD — CRACKED (LT WING)

LEFT WING LE SHROUD ASSEMBLY CRACKED, INBD TO CTR LE OTBD SIDE.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 27,823 hrs · 26,927 cycles

FS 484 INTERCOSTAL ATTACH CLIP CRACKED AT RBL 36.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 27,823 hrs · 26,927 cycles

LEFT LE CTR INBD, LE ATTACH BRACKET CRACKED. REPLACED ANGLE.

Part: VANE — CHAFED (TE FLAP) · airframe 27,823 hrs · 26,927 cycles

LEFT INBD FLAP VANE LE CHAFFED AT WS 105. REPLACED LE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,823 hrs · 26,927 cycles

ANGLE CLIP AT FS 484, OTBD SIDE OF RBL 9 CRACKED. REPLACED CLIP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,823 hrs · 26,927 cycles

ANGLE CLIP CRACKED AT THE OTBD SIDE OF RBL 27 AT FS 484. REPLACED CLIP.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,823 hrs · 26,927 cycles

BATH TUB FITTING CRACKED, TWO EACH AT FS 461, OTBD OF RBL 9. REPLACED FITTING.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,823 hrs · 26,927 cycles

BATH TUB FITTING CRACKED IN 2 SPOTS AT FS 461 OTBD OF RBL 9. REPLACED FITTING.

Part: ATTACH BRACKET — CRACKED (RT COWLING) · airframe 27,823 hrs · 26,927 cycles

RIGHT ENG OUTER NOSE COWL, ATTACH SUPPORT BRACKET CRACKED. R & R RT OUTER NOSE COWL ATTACH BRACKET IAW SRM 51-40-11 & SRM 51-41-02.

Part: MOUNT BRACKET — CRACKED (RT WING) · airframe 27,823 hrs · 26,927 cycles

RIGHT WING LE REFUELING MOUNTING BRACKET CRACKED. REPLACED RT LE REFUEL BRACKET PN 600-62441-13, TAG B59789 IAW SRM 51-42-00 & 51-41-02.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FLOORBEAM 281 IS CRACKED & BUCKLING, JUST OTBD OF RBL 9 IN CABIN. REPAIRED FLOORBEAM STATION 280 RBL 9 IAW EA AWAC-CRJ253-00162 REV IR.

Part: SKIN — CHAFED (TE FLAP VANE)

LEFT INBOARD FLAP VANE LEADING EDGE CHAFED OUT OF LIMITS AT WS 56.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 27,824 hrs · 26,927 cycles

RIGHT INBD FLAP VANE LEADING EDGE CHAFED OUT OF LIMITS AT WS 56.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 27,541 hrs · 26,670 cycles

FLIGHT 9368, FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROW 9 - 12. INSPECTED THE LIGHTS, FOUND CONNECTOR WIRES BROKEN BEYOND REPAIR.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 26,577 hrs · 25,717 cycles

BURNING SMELL COMING FROM FLIGHT DECK. REMOVED EXTERNAL POWER & SMELL WENT AWAY.

Part: APU — MALFUNCTIONED · airframe 26,380 hrs · 25,530 cycles

AT 17,000 FT, RECEIVED APU FAULT CAUTION MSG, APU SHUTDOWN. MC IDG 1 WAS ON MEL AT THE TIME OF ISSUE.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 23,314 hrs · 22,584 cycles

PASSENGER DOOR OUTER HANDLE CRACKED. R & R PAX DOOR OUTER HANDLE.

Part: RETAINER — CRACKED (RT NACELLE) · airframe 23,314 hrs · 22,584 cycles

RT PYLON PANEL 422AT SEAL RETAINER IS CRACKED. R & R SEAL RETAINER.

Part: BRACKET — WORN (RUDDER HINGE) · airframe 23,314 hrs · 22,584 cycles

RUDDER CENTER LOWER HINGE SPERICAL BEARING ATTACH BRACKETS ARE WORN. REMOVED UNSERVICEABLE LWR CENTER HINGE BRACKET AND INSTALLED NEW SERVICEABLE, PN 600-21098-3.

Part: TAILPIPE — CRACKED (RT ENGINE) · airframe 23,314 hrs · 22,584 cycles

RIGHT ENGINE TAIL PIPE FROM FWD STIFFENER IS CRACKED AT INBD 4 O`CLOCK. REPAIRED RT ENGINE TAIL PIPE STIFFENER IAW CMM 78-11-00.

Part: WEB — TORN (PAX DOOR) · airframe 23,314 hrs · 22,584 cycles

PAX DOOR AFT SIDE WEB HAS TEAR FROM ASSIST MOTOR CABLE. REPAIR SIDE PANEL METAL TEAR IAW REO 601R-52-11-2189.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 23,314 hrs · 22,584 cycles

HOLE IN 621.00 BULKHEAD THAT WAS UNDER TEMP REPAIR REF REO 601R-53-61-4974. PERFORMED PERMANENT REPAIR IAW AMM REO 601R-53-61-5045, REV A.

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 23,314 hrs · 22,584 cycles

CARGO DOOR HANDLE ASSY IS CRACKED. R & R WITH NEW HANDLE IAW SRM.

Part: SEAT TRACK — CORRODED (BS 589-621) · corrosion level 2 · airframe 23,314 hrs · 22,584 cycles

CARGO BAY SEAT TRACK LBL 27, FOUND TO BE CORRODED OUT OF LIMITS. R & R SEAT TRACK IAW REO 601R-53-61-3778, REV A.

Part: SILL — CRACKED (BS 589) · airframe 23,314 hrs · 22,584 cycles

CARGO DOOR SILL BS 589 CRACKED UNDER DOOR STOP. R & R SILL ANGLE.

Part: ANGLE — CRACKED (BS 621) · airframe 23,314 hrs · 22,584 cycles

LEFT OBLIQUE ANGLE CRACKED AFT SIDE OF BULKHEAD BS 621. R & R ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 621) · airframe 23,314 hrs · 22,584 cycles

RIGHT OBLIQUE ANGLE AT FS 671, AFT SIDE IS CRACKED. R & R RT OBLIQUE ANGLE IAW SRM 51-42-21.

Part: STRUCTURE — DAMAGED (WING) · airframe 23,314 hrs · 22,584 cycles

WHILE WORKING ON MLG TRUNNION COLD WORKING SB 601R-57-046, REV B, FOUND THREE HOLES ON THE LOWER FLANGE TO BE OVERSIZED. COMPLIED WITH REO 601R-57-21-2010.

Part: DRAG ANGLE — CRACKED (RT MLG) · airframe 23,314 hrs · 22,584 cycles

RIGHT MLG DRAG ANGLE COMMON TO INBD BATTERY RIB IS CRACKED. R & R DRAG ANGLE.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 23,314 hrs · 22,584 cycles

VERTICAL BEAM AT LBL 27, FS 409+128 CRACKED AT BOTTOM. COMPLIED WITH REO 601R-53-41-056, REV E.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 23,314 hrs · 22,584 cycles

VERTICAL BEAM AT LBL27, FS 409+128 CRACKED AT BOTTOM. COMPLIED WITH REO 601R-53-41-056, REV E.

Part: DRAG ANGLE — CRACKED (LT MLG) · airframe 23,314 hrs · 22,584 cycles

LT MLG DRAG ANGLE COMMON TO INBD BATTERY RIB IS CRACKED. R & R DRAG ANGLE.

Part: SKIN — DENTED (BS 202.75) · airframe 23,314 hrs · 22,584 cycles

SKIN HAS A DENT AT FS 202.75 JUST OTBD OF CO-PILOT WINDSHIELD WIPER. REWORKED DENT TO ALLOWABLE LIMITS IAW EA 15-2013-439.

Part: RIB — CRACKED (RT MLG) · airframe 23,314 hrs · 22,584 cycles

RIGHT MLG FWD OTBD BATT RIB IS CRACKED. PERFORM REPAIR IAW REO 601R-57-51-046.

Part: FITTING — CRACKED (BS 283) · airframe 23,314 hrs · 22,584 cycles

AT STRINGER 3L, FS 283 LINTEL FITTING CRACKED. REPLACED FITTING.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 23,314 hrs · 22,584 cycles

FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT AND FABRICATED & INSTALLED SERVICEABLE FLOOR SUPPORT IAW SRM 51-42-21, 51-24-16.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 23,314 hrs · 22,584 cycles

PAX DOOR LOWER EDGE MEMBER CRACKED AT AFT RADIUS. REMOVED EDGE MEMBER CRACK INSTALLED FILLER DOUBLER REPAIR.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 21,399 hrs · 20,746 cycles

FLT 3755: AFTER HOLDING AT LOW ALTITUDES FOR OVER AN HOUR, IN CONSTANT LITE RAIN/SNOW - RECIEVED EFIS COMP MON CAUTION AND IAS YELLOW FLAGS ON BOTH PFD'S AIRSPEED 8-10 KNTS WITHIN 10-15 MINUTES, 20 KNOTS OFF. DETERMINED THAT CAPT'S AIRSPEED WAS MOST ACCURATE. AFTER LANDING/TAXI. IN PROGRESS.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 20,030 hrs · 19,407 cycles

DURING CLIMBOUT, WITH GEAR RETRACTED, REC A GEAR DISAGREE WARNING WITH RED DASHES INDICATED FOR THE NOSE GEAR, MSG CLEARED AFTER RUNNING QRH. C/ FIM 32-60-07, FOUND STORED PSEU CODE S21 NEAR (NOSE GEAR DL1). ADJUSTED GAP AT DOWNLOCK PROXIMITY SENSOR TO 0.064" AND CLEANED CONNECTOR PLUG AT DOWNLOCK PROXIMITY SENSOR, PERFORMED SEVERAL OPS CHECKS OF PROX SYS, ALL CHECKED GOOD.

Part: ACM — ODOR (LEFT) · airframe 18,628 hrs · 17,969 cycles

WHEN PULLING INTO GATE, F/A NOTIFIED CREW OF SMOKE IN CABIN, PERFORMED IAC FOR EVACUATION, DID NOT DISCHARGE LT OR RT ENGINE FIRE BOTTLE OR APU FIRE BOTTLE, LSU SMOKE DETECTOR WENT OFF BOTH PACKS WERE RUNNING ON APU BLEED AIR FOR APPROX 3 MINUTES. RAN BOTH PACKS ON APU AND ENGINE BLEED AIR, RT PACK TEMP CLIMBS RAPIDLY AND PRODUCES STRANGE OIL ODOR AND SMOKE. LT PACK OPERATES NORMALLY PLACED RT PACK ON MEL. CREW RAN ENGINES AND APU AND CW SUP 09-037A LT PACK OPS NORMALLY PLACED RT PACK ON MEL. R & R RT COALESCER BAG AS REQUESTED IAW MX TASK CARD MANUAL 000-21-310-003 WHERE APPLICABLE.

Part: SKIN — CHAFED (LT NACELLE) · airframe 18,477 hrs · 17,813 cycles

LOWER CORE COWL INNER SKIN CHAFED AND GOUGED IN 5 AREAS CUT OUT DAMAGE AND INSTALL REPAIR DOUBLER IAW CMM 71-12-01, AREAS 3, 4, 5 FOUND TO BE LIMITED TO PAINT ONLY.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 18,477 hrs · 17,813 cycles

LT INBD FLAP VANE SKIN HAS CHAFING DAMAGE IN 3 EA FROM STOPS EVALUATED DAMAGE ON LT INBD FLAP VANE IAW SRM 51-12-00 BLENDED IAW SRM 51-12-00 MAT LOSS .019 AT FLAP STATION 60.005.015 AT FLAP STATION 98.505.005 AT FLAP STATION 137.012 WITHIN SERVICEABLE LIMITS IAW REO 601R-57-52-004, REV C.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 18,477 hrs · 17,813 cycles

CARGO DOOR EXTERNAL SKIN IS CHAFED NEXT TO HANDLE. BLENDED DAMAGED AREA IAW REO 601R-53-31-086 .100 MAT THICKNESS .025 MAT LOSS .075 MAT REMAINING MAX IS WITHIN SERVICEABLE LIITS IAW REO 601R-53-31-086.

Part: FITTING — LOOSE (THRUST REVERSER) · airframe 18,477 hrs · 17,813 cycles

RT THRUST REVERSER HAS 2 LOOSE INTERLOCK FITTINGS. REMOVED UNSERVICEABLE FASTENERS AND INSTALLED SERVICEABLE FASTENERS IN RT T/R INTERLOCK FITTINGS (2 EA).

Part: PANEL — CHAFED (RWS 242-213) · airframe 18,477 hrs · 17,813 cycles

PANEL 699AB IS CHAFED. BLENDED DAMAGE ON PANEL 699AB IAW SRM 51-12-00, MAX DAMAGE LOSS .015 MAT REMAINING .046 WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.

Part: PANEL — CHAFED (WS274) · airframe 18,477 hrs · 17,813 cycles

PANEL 699BB CHAFED, BLENDED DAMAGED ON PANEL 699BB IAW 51-12-00, MAX DAMAGE LOSS .010 MAX REMAINING .045 WITHIN LIMITS IAW REO 601R-57-60-020.

Part: STIFFENER — CHAFED (BS 621) · airframe 18,477 hrs · 17,813 cycles

VERTICAL STIFFENER ON AFT SIDE OF BS 621 BULKHEAD AT BL 0 TOWARDS TOP IS CHAFED. BLENDED DAMAGE ON VERTICAL STIFFENER AND FOUND TO BE WITHIN LIMITS. MAX DEPTH O DAMAGE 0.009" MAX LENGTH OF DAMAGE 0.025 IN IAW REO 601R-53-61-1523.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,477 hrs · 17,813 cycles

CLIPS ON FS 280 FLOORBEAM AT LBL9 AND RBL9 ARE CRACKED. REMOVED UNSERVICEABLE CLIPS ON FS 280 FLOORBEAM AT LBL9 AND RBL9. INSTALLED SERVICEABLE CLIPS ON FS280 FLOORBEAM AT LBL9 AND RBL9 IAW SRM 51-42-21, SRM 53-21-43, SRM 51-24-16, SRM 51-40-11.

Part: STOP FITTING — CHAFED (BS 364) · airframe 18,477 hrs · 17,813 cycles

FWD RT STOP FITTING ON THE AVIONIC DOOR IS CHAFED. BLENDED CHAFED AREA AT FWD RT STOP FITTING ON AVIONICS DOOR IAW REO 601R-53-21-2194.

Part: STIFFENER — CHAFED (FS 621) · airframe 18,977 hrs · 18,331 cycles

VERTICAL STIFFENER ON AFT SIDE OF 621 BULKHEAD AT BL0 TOWARDS TOP IS CHAFED. BLENDED DAMAGE ON VERTICAL STIFFENER AFT SIDE OF 621 BULKHEAD AT BL0 DAMAGE FOUND TO BE WITHIN LIMITS: MAX DEPTH OF DAMAGE 0.009 IN/ MAX LENGTH OF DAMAGE 0.025 IN IAW REO 601R-53-61-1523.

Part: SEAT TRACK — CORRODED (BS 574) · airframe 18,477 hrs · 17,813 cycles

LBL9 AND RBL9 CARGO BAY SEAT TRACKS, FS 574 CORRODED. REMOVED UNSERVICEABLE SEAT TRACKS AND REPLACED WITH SERVICEABLE SEAT TRACKS IAW SRM 51-41-02.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 18,477 hrs · 17,813 cycles

FLOORBEAM CRACKED AT FS 484, LBL 27 & 36. REPAIRED FLOORBEAM.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 18,477 hrs · 17,813 cycles

FLOORBEAM CRACKED AT FS RBL 27. REPAIRED FLOORBEAM .

Part: FAIRING — CRACKED (LT WING TE FLAP)

LT OTBD CENTER HINGE ARM FLAP FAIRING GUIDE CRACKED, R & R.

Part: ROLLER — CHAFED (RT WING TE FLAP) · airframe 18,477 hrs · 17,813 cycles

RT WING FLAP ROLLER FITTING IS CHAFED. BLENDED CHAFED AREA AT RT WING FLAP ROLLER FITTING IAW REO 601R-57-51-143. ROTO PEENED AREA IAW REO 601R-57-51-143.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 18,477 hrs · 17,813 cycles

RT INBD FLAP VANE CHAFED ON L/E. BLENDED AREAS ON RT INBD FLAP VANE IAW REO 601-57-52-004 AND SRM 51-12-00. TREATED AREA IAW SRM 51-21-16 AND SRM 51-25-26.

Part: SPAR — CHAFED (LT NACELLE) · airframe 18,477 hrs · 17,813 cycles

LT ENGINE FWD MOUNT SPAR IN PYLON CHAFE FROM ANTI-ICE DUCT. BLENDED CHAFED AREA ON LT ENG FWD MOUNT SPAR IAW REO 601R-54-50-006 & SRM 51-12-00.

Part: ANGLE — CRACKED (BS 621) · airframe 18,477 hrs · 17,813 cycles

LT SIDE OBLIQUE ANGLE ON FS 621 AFT FACE CRACKED. R & R LT OBLIQUE ANGLE IAW SRM 51-40-11 & REO 601R-53-61-422.

Part: ANGLE — CRACKED (BS 621) · airframe 18,477 hrs · 17,813 cycles

RT SIDE OBLIQUE ANGLE ON FS621 AFT SIDE CRACKED. REPLACED RT OBLIQUE ANGLE ON FS 621 IAW SRM 51-42-21.

Part: A/C PACK — ODOR (RIGHT) · airframe 17,690 hrs · 169,980 cycles

RIGHT PACK OVERTEMP AT GATE WITH ACRID ODOR, P/P ON MEL. R & R RT ACM AND RAM AIR CHECK VALVE AND COALESCER SOCK IAW 21-51-10 AND 21-52-07 AS REQUIRED, OPS CK LEAK GOOD. REMOVED PLACARD AND MEL.

Part: DOOR — BINDING (MAIN PAX) · airframe 15,366 hrs · 1,452 cycles

UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE, OPENED FROM OUTSIDE, INNER HANDLE ONLY MOVED 1/2 TRAVEL. CA IN PROGRESS.

Part: LUG — CORRODED (WS 220) · corrosion level 2 · airframe 13,552 hrs · 12,672 cycles

LT WING FLAP HINGE BOX AT WS 220.00, AFT LUG CORRODED UNDER BUSHING. LT WING FLAP HINGE BOX AT WS 220.00 AFT LUG REPAIRED IAW REO 601R-57-21-1164. (K)

Part: LUG — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 13,552 hrs · 12,672 cycles

LT WING FLAP HINGE BOX AT WS 80.50 AFT LUG CORRODED UNDER BUSHING INBD LT WING FLAP HINGE BOX AT WS 80.50 AFT LUG INBD REPAIRED IAW REO 601R57-21-1164. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 13,552 hrs · 12,672 cycles

AFT PRESSURE BULKHEAD WEB AT THE LINTEL LOCATION IS CRACKED. REO 601R-53-61-1230 REV D CARRIED OUT. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 13,552 hrs · 12,672 cycles

AFT PRESSURE BULKHEAD WEB AT THE LINTEL LOCATION IS CRACKED. REO 601R-53-61-1230 REV D CARRIED OUT. (K)

Part: SILL — CRACKED (BS 589) · airframe 13,552 hrs · 12,672 cycles

FS 589.00, LBL 47.00 CRACK FOUND ON CARGO ENTRANCE SILL. FS 589.00 LBL 47.00 ON CARGO ENTRANCE SILL DAMAGE REPAIRED IAW REO 601R-53-61-433, REV NC. (K)

Part: BRACKET — CRACKED (LT ENG TAILPIPE) · airframe 13,552 hrs · 12,672 cycles

LT ENGINE TAILPIPE FAIRING OTBD ATTACHMENT, NUT PLATE BRACKET ASSY IS CRACKED. REPLACED IAW SRM 51-42-06. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,552 hrs · 12,672 cycles

FS 484.00, LBL 36 INTERCOSTAL FOUND CRACKED. CRACK ON INTERCOSTAL AT FS 484.00, LBL 36, REPAIRED IAW REO 601R-53-41-059, REV A. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,552 hrs · 12,672 cycles

FS 484.00, RBL 27 CLIP OF INTERCOSTAL FOUND CRACKED (CRACK LENGTH .300 INCH). CLIP OF INTERCOSTAL AT FS 484.00, RBL 27 REMOVED AND REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: PRESSURE SWITCH — MALFUNCTIONED (LT ENG OIL SYS) · airframe 13,033 hrs · 12,155 cycles

204552/2 - ON CLIMBOUT, LT ENG OIL PRESS CAS WARNING MULTIPLE TIMES. ACCOMPANIED BY OIL PRESS OF 22-24 PSI UP TO 44 PSI. OIL TEMP WAS 10 DEGREES HIGHER THAN RT. WARNING WENT AWAY WITH POWER REDUCTION. REMOVED AND REPLACED LT LOW OIL PRESSURE SWITCH IAW AMM 79-31-03, OPS CHECK GOOD. (K)

Part: SENSOR — SHORTED (OVERHEAT) · airframe 11,677 hrs · 10,855 cycles

RECEIVED LT STAGE DUCT MSG INFLIGHT. MSG STAYED ON AFTER RETARDING THRUST LEVER TO IDLE. C/W GVI OF LT 10TH STAGE DUCTING WITH ENGINE RUNNING. NO LEAKS DETECTED. LT 10TH STAGE WARN MSG OCCURRED AGAIN WITH ENGINES SHUTDOWN. CONFIRMED BAD INDICATION. REF 193317/1 FOR NEW DISCREPANCY. FOUND 10TH STAGE DUCT SENSING ELEMENT A14WK SHORTED TO GROUND. R&R A14WK IAW AMM 36-21-04. REF L/P 193317/3 FOR LOOB A FAULT.

Part: CABLE — DISLODGED (DOOR ASSIST) · airframe 10,844 hrs · 10,046 cycles

PASSENGER DOOR WILL ONLY PARTIALLY OPEN. FOUND POWER ASSIST MOTOR CABLE WAS OUT OF ROLLER TRACK. REMOVED AND REPLACED PAX DOOR POWER ASSIST MOTOR IAW 52-11-08. C/W ELECTRICAL 52 &51. DOOR ASSIST OPS CHECKS GOOD. (A)

Part: FLAP — MALFUNCTIONED (WING) · airframe 9,705 hrs · 8,949 cycles

FLAPS FAIL CAUTION DISPLAYED ON FINAL APPROACH, COMPLIED WITH QRH BOTH FLAPS DISPLAYED 45 DEGREES. RESET FLAPS, OPS CHECK OK IAW AMM 27-50-AND AWAC SUPLEMENT 98-018B. (K)

Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM)

AFTER TAKEOFF RT TRANSFER SHUT OFF VALVE CAUTION MESSAGE ILLUMINATED AS WELL AS FUEL CHANNEL 1 STATUS MESSAGE. LOST RT ANF AND TOTAL FUEL IND (AMBER DASHES) CENTER TANK INDICATED 0 DURING FLIGHT AUTO CROSSFLOW INHIBIT STATUS MSG ILLUMINATED DURING FINAL APPROACH R X-FLOW SOV CAUTION AND CROSSFLOW/APU PUMP MESSAGE ILLUMINATED AND ALL FUEL QTY READOUTS DASHED AMBER ON GROUND CHECK AUTO CROSSFLOW INHIBIT SWITCH WAS IN NORMAL POSITION AND EMERGENCY WAS DECLARED. REMOVED AND REPLACED FUEL SYSTEM COMPUTER IAW CRJ200 AMM 28-41-16. OPS CHECK GOOD. (M)

Part: WEB — CRACKED (PAX DOOR)

FOUND AFT WEB CRACKED IN RADIUS .300 INCH LONG AT STEP 832CT ON PAX DOOR. 10-04-07 MAINTENANCE REPAIRED WEB IAW BOMBARDIER REO 601R-52-11-702. (M)

Part: WEB — CRACKED (PAX DOOR)

FOUND FORWARD WEB CRACKED IN RADIUS .400 INCH LONG AT STEP 832CT ON PAX DOOR. S/D - MAINTENANCE REPLACED IAW BOMBARDIER REO 601R-52-11-702. (M)

Part: SKIN — DENTED (LT TE FLAP)

LEFT INBOARD FLAP LOWER SKIN DENTED APPROX 2 INCHES DIAMETER BY .083 INCH DEEP, 1.5 INCH FROM TRAILING EDGE OF FLAP, 1 INCH FROM INBOARD EDGE OF FLAP, FLAP P/N 601R14002-1, S/N SB/RJ/937. MAINTENANCE REPAIRED FLAP LOWER SKIN USING EXTERNAL DOUBLER IAW CRJ 200 SRM 57-52-00 REPAIR NR 3. (M)

Part: PANEL — CRACKED

RT LOWER VISOR PANEL 326BR, P/N 600-21134-44, CRACKED APPROX 4.5 INCH LONG AT FORWARD END OF PANEL. MAINTENANCE REPLACED DAMAGED PANEL WITH A SERVICEABLE REPAIRED PANEL P/N 600-31134-44. (M)

Part: SUPPORT BEAM — CRACKED (CARGO DOOR)

CARGO DOOR SUPPORT BEAM LOWER ANGLE, P/N 601R35050-109, CRACKED IN RADIUS APPROX 1.2 INCHES LONG. MAINTENANCE REMOVED AND REPLACED BRACKET (ANGLE) P/N 601R-35050-109 IAW CRJ 200 SRM 51-42-21. (M)

Part: CHANNEL — CRACKED (LT MLG WW)

LT MLG WHEEL WELL BRAKE PRESSURE TRANSDUCER HAT CHANNEL IS CRACKED AT INBOARD LEGS APPROX .20 INCH LONG. MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-159 IAW CRJ SRM 51-42-06. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND LT FS 621 FLOORBEAM ANGLE CRACKED. MAINTENANCE REPAIRED LT FS 621 FLOORBEAM ANGLE BY CUTTING AWAY DAMAGE AREA AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND FS 484 RBL 36 INTERCOSTAL CRACKED IN RADIUS. MAINTENANCE REPAIRED INTERCOSTAL AT FS 484 RBL 36 IAW BOMBARDIER REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0030A. (M)

Part: SKIN — DAMAGED (RT WING)

RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 54.897 9640BB, HOLE NR 1) HAS FRETTING DAMAGE AT INBOARD AND OUTBOARD ENDS OF CUTOUT IN NON-CRITICAL AREA. INBOARD AREA MEASURES APPROX 6 INCH LENGTH BY .30 INCH WIDE BY .005 INCH DEEP. OUTBOARD AREA MEASURE APPROX 5.5 INCH LONG BY .30 INCH WIDE BY .005 INCH DEEP. OUTBOARD AREA MEASURE APPROX 5.5 INCHES LONG BY .30 INCHES WIDE BY .005 INCHES DEEP. MAINTENANCE REPAIRED CORRODED (FRETTING) DAMAGE AREAS IAW REO 601R-57-21-030 REV F. (M)

Part: FLOORBEAM — CRACKED (BS 621)

RT FS 621 FLOOR SUPPORT ANGLE CRACKED. MAINTENANCE REPAIRED AREA IAW REO 601R-53-61-117 REV C. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

FOUND FS 484, LBL 27 INTERCOSTAL CRACKED. MAINTENANCE REPAIRED INTERCOSTAL AT FS 484 LBL 27 IAW REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0029B. (M)

Part: SKIN — CORRODED (LT WING)

LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 54.897 (540BB, HOLE NR 1) HAS FRETTING DAMAGE AT INBOARD AND OUTBOARD ENDS. INBOARD END MEASURES APPROX 9.5 INCH BY .30 INCH BY .004 INCH DEEP. OUTBOARD END MEASURES APPROX 4.5 INCH BY .30 INCH BY .004 INCH DEEP IN NON-CRITICAL AREA. MAINTENANCE REPAIRED FRETTING DAMAGE IAW REO 601R-57-21-030 REV F. (M)

Part: SKIN — CORRODED (LT WING)

LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 12.245 (510AB, HOLE NR 2) HAS FRETTING DAMAGE AROUND ENTIRE CIRCUMFERENCE OF HOLE, IN CRITICAL AREA, APPROX .30 INCH WIDE BY .006 INCH DEEP. MAINTENANCE REPAIRED DAMAGED AREA IAW REO 601R-57-21-030 REV F. (M)

Part: ANGLE — CRACKED (FS 625)

RIGHT OBLIQUE ANGLE IS CRACKED .75 INCH IN RADIUS AT FS 625, WL 100. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE INTERCOSTAL, P/N 601-35012-52 IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (M)

Part: ANGLE — CRACKED (FS 625)

LEFT OBLIQUE ANGLE IS CRACKED .75 INCH IN RADIUS AT FS 625, WL 100. MAINTENANCE REMOVED AND REPLACED INSTALLED SERVICEABLE ANGLE P/N 601-35012-51 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: OIL SYSTEM — OVERSERVICED (APU)

APU AUTO SHUTDOWN AT GATE, STRONG SMELL IN CABIN. FOUND APU OIL OVERSERVICED, SERVICED TO CORRECT LEVEL, COMPLIED WITH OPS CHECK OF BOTH PACKS ON ENGINE AIR PER AMM 21-51-00-710-801. NO FAULTS NOTED. MEL`D APU AS IT STILL AUTO SHUTDOWN. (M)

Part: APU — MALFUNCTIONED (APU BAY)

APU AUTO SHUTDOWN, APU FAULT CAUTION MESSAGE, STRONG FUEL SMELL IN FLIGHT DECK. INSPECTED APU. NO EVIDENCE OF FUEL LEAKS. APU OPS CHECKS NORMAL PER AMM 49-31-00. NO ODOR IN CABIN. (M)

Part: ODOR — DETECTED (COCKPIT)

APU AUTO SHUT DOWN, APU FAULT CAUTION MESSAGE, STRONG FUEL SMELL IN FLIGHT DECK. INSPECTED APU, NO EVIDENCE OF FUEL LEAKS. APU OPS CHECK NORMAL PER AMM 49-31-00. NO ODOR IN CABIN. (M)

Part: SOLENOID VALVE — MALFUNCTIONED (APU)

APU FAULT CAUTION MESSAGE OCCURRED IN FLIGHT DURING STARTUP. COMPLIED WITH QRH. STRONG SMELL OF FUEL FUMES PRESENT IN COCKPIT AND CABIN AFTER, APU SHUTDOWN. REMOVED AND REPLACED ECU AND FUEL SOLENOID VALVE, IAW AMM CHAP 49. NO FUEL LEAKS OR SMELL IN AIRCRAFT. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

GEAR DOWN DISAGREE ON APPROACH. COMPLIED WITH QRH, GEAR DOWN DISAGREE CHECKLIST. PERFORMED LANDING GEAR EXTENSION AND RETRACTION GEAR DISAGREE TEST IAW AMM 32-30-00 BOTH SYSTEMS CHECK GOOD. (M)

Part: FLAP SYSTEM — ICED (WINGS) · airframe 4,655 hrs · 4,095 cycles

FLAP FAIL MESSAGE AFTER TAKEOFF AT 8 DEGREES. INSPECTED AND FOUND ICE ON LT AND RT IB FLAPS. NO DAMAGE NOTED. PERFORMED FLAP CHECKS IAW SRM. OPS CHECK GOOD. (K)

Part: SKIN — CORRODED (RT WING)

RIGHT WING LOWER WING FUEL TANK ACCESS DOOR CUTOUT FOR 650 OUTBOARD HAS PITTING CORROSION LESS THAN .003. MAINTENANCE REMOVED CORROSION, PERFORMED NDT, ROTO-PEENED AND APPLIED SURFACE TREATMENT IAW REO 601R-57-27-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

LEFT WING LOWER WING FUEL TANK ACCESS DOOR CUTOUT FOR 510AB HAS CORROSION LESS THAN .004 INC DEEP IN SEVERAL AREAS. MAINTENANCE REMOVED CORROSION, PERFORMED NDT ROTO-PEENED AND APPLIED SURFACE TREATMENT IAW REO 601R-57-21-030 REV D. (M)

Part: PROXIMITY SENSOR — FAILED (MLG)

ON GEAR RETRACTION, GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH. DOWNLOADED FDR AND FOUND BOTH LT AND RT MLG UPLOCKS INTERMITTENT UPA AND LOCKED. SUSPECT BAD PSEU, REMOVED AND REPLACED PSEU IAW MM. OPS CHECK GOOD. PERFORMED FUNCTION CHECKS OF LANDING GEAR EXTENSION AND RETRACTION IAW MM. CHECK GOOD. (K)

Part: FUEL LINE — CHAFED (APU)

STRONG FUEL SMELL IN CABIN AND COCKPIT WITH APU AIR SUPPLYING PACKS. OK ENGINE AIR. FOUND FUEL LEAK INSIDE APU ENCLOSURE, NO LEAKS WITH APU DEACTIVATED. FOUND APU FUEL LINE CHAFED BY CLAMP. REMOVED AND REPLACED APU FUEL LINE. OPS CHECK GOOD, REF AMM 49-31-00. (M)

Part: ELBOW — LEAKING (HYD SYSTEM)

HYDRAULIC NR 3 LOW PRESSURE CAS MESSAGE INFLGHT NR 3 HYDRAULIC SYSTEM QUANTITY AT ZERO PERCENT COMPLIED WITH QRH, PERFORMED MANUAL GEAR EXTENSION. FOUND FORWARD GROUND PRESSURE LINE FITTING LEAKING. REPLACED ELBOW FITTING. LEAK CHECK GOOD. SERVICED NR 3 SYSTEM. (M)