N415AW

Part: UNKNOWN — CORRODED (FS563 TO FS621) · corrosion level 2 · airframe 44,109 hrs · 41,979 cycles

R/H FLOOR SILL FROM FS 563 TO FS621 IS FOUND TO BE OUT OF LIMITS. ******AIRCRAFT REMOVED FROM SERVICE********* REPLACE R/H FLOOR SILL BETWEEN FS 563 AND FS621 REF REO 601R-53-61-5376 REV A DATED 2018-10-25

Part: ANGLE — CORRODED (FS310 TO FS349) · corrosion level 2 · airframe 44,109 hrs · 41,979 cycles

FLOOR ANGLE BETWEEN FS349- FS310 AT PAX DR HAS CORROSION. *******AIRCRAFT REMOVED FROM SERVICE************ REPLACED FLOOR ANGLE BETWEEN FS349- FS310 AT PAX DR REF CRJ-200-SRM 51-42-06 AND CRJ-200-SRM 51-42-21

Part: UNKNOWN — CORRODED (FS409+128 TO FS5) · corrosion level 2 · airframe 44,109 hrs · 41,979 cycles

MULTIPLE SPOTS OF CORROSION NOTED ON R/H PRESSURE FLOOR SILL PANEL BETWEEN FS 409+128 AND FS559 ****AIRCRAFT REMOVED FROM SERVICE***** REPAIRED R/H PRESSURE FLOOR SILL REF REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41-3127 REV A DATED 2023-03-08

Part: FLOOR SUPPORT — CRACKED (FS621) · airframe 44,109 hrs · 41,979 cycles

ANGLE BRACKET SECURING FS 621 BULKHEAD TO L/H FLOOR SILL MISSING RIVETS ****AIRCRAFT REMOVED FROM SERVICE******* REPLACED FLOOR SUPPORT ANGLE REF REO 601R-53-61-117 REV E DATED 2018-01-15

Part: NONE — CORRODED (FS559.00+86 TO F) · corrosion level 2 · airframe 44,109 hrs · 41,979 cycles

R/H FLOOR SILL FROM FS 559+86 TOFS563 IS FOUND TO BE OUT OF LIMITS *********AIRCRAFT REMOVED FROM SERVICE******* REPLACE FLOOR SILL BETWEEN FS559.00 +86 FS 621.00 PER CRJ 200 SRM 51-42-21 AND 51-42-06 AND DWG # 601R31133 REV J.

Part: NONE — CORRODED (FS563.00-FS621.0) · corrosion level 2 · airframe 44,109 hrs · 41,979 cycles

L/H FLOOR SILL FROM FS 563 TO FS 621 IS FOUND TO BE OUT OF LIMITS ****AIRCRAFT REMOVED FROM SERVICE******** INSTALLED A NEW LH FLOOR SILL, FROM FS563.00-FS621.00 WITH NEW FASTENERS. REF DRAWING 601R35011 REV-R,

Part: FLOORBEAM — CORRODED (FS 559+80) · corrosion level 2 · airframe 44,109 hrs · 41,979 cycles

RBL 9 FLOOR BEAM CAP HAS CORROSION AT FS 559+80 ****AIRCRAFT REMOVED FROM SERVICE********** REPLACE RBL 9 FLOOR BEAM CAP SECTION REF REO 601R-53-51-650 REV -- DATED 2023-02-28

Part: ANGLE — GOUGED (FS 409+112) · airframe 44,109 hrs · 41,979 cycles

ACFT EXTERIOR- FS 409+112 BETWEEN STRGRS 27/26L VERICAL PLATE FOR FWD DRAW BEAM CORROSION. ********AIRCRAFT REMOVED FROM SERVICE********* REPAIRED LOWER FRAME ANGLE AND FUSELAGE SKIN AT FS 409+112 BETWEEN STR 26L 27

Part: SKIN — DENTED (RH VERTICAL STAB) · airframe 44,109 hrs · 41,979 cycles

DENT NOTED ON R/H VERTICAL STAB BETWEEN RIB#3-RIB #4 AFT OF MID SPAR AND APPROX 14" T/E ****AIRCRAFT REMOVED FROM SERVICE******** REPAIRED PER CRJ-200 SRM 55-31-31

Part: FLOOR SUPPORT — CORRODED (FS 559 TO 559+80) · corrosion level 2 · airframe 44,109 hrs · 41,979 cycles

L/H FLOOR SILL HAS CORROSION FROM FS 559 TO FS 559+48 ******AIRCRAFT REMOVED FROM SERVICE******** REPLACE L/H FLOOR SILL

Part: FLOORBEAM — CORRODED (FS559+80 - FS621) · corrosion level 2 · airframe 44,109 hrs · 41,979 cycles

OUTBOARD PORTION OF SEAT RAIL SUPPORT BEAM IS CORRODED AT BL 27 BETWEEN FS559+80 - FS621 **********AIRCRAFT REMOVED FROM SERVICE********* REMOVED CORROSION FROM O/B SEAT RAIL SUPPORT BEAM LBL27 BETWEEN FS559.00+80 TO FS621.00 PER CRJ 200 SRM 51-21-06. FOUND REWORKED AREA OUT OF LIMITS DUE

Part: COAMING — DENTED (FS574.00 - FS621) · airframe 44,109 hrs · 41,979 cycles

AFT CARGO DOOR SURROUND COAMING IS DENTED/MISSING MATERIAL IN MULTIPLE LOCATIONS *******AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED AFT CARGO DOOR SURROUND COAMING REF CRJ200 SRM 51-41-02 AND SRM 51-42-10.

Part: NONE — NONE · airframe 42,593 hrs · 40,541 cycles

****SUPPLEMENTAL INFORMATION ***** AFTER DOOR CLOSE AND BEFORE PUSH BACK. LH WING TIP WAS STRUCK BY GROUND SUPPORT TUG WHILE TOWING BAGGAGE CARTS. TOW BAR WAS ATTACHED TO PLANE AND PUSH BACK TUG. AIRCRAFT DID NOT SLIDE AFT IMPACT. ***AIRCRAFT REMOVED FROM SERVICE*** R&R SKIN OB AND RIB IAW SRM 51-42-06, SRM 51-40-11, SRM 51-42-15, SRM 51-23-06 AND SRM 51-25-00. RE-WORKED INBD SKIN IAW REO 601R-57-31-1386

Part: NONE — CORRODED (FS 310) · corrosion level 2 · airframe 42,253 hrs · 40,211 cycles

PAX DOOR FWD ANCHOR FITTING PLATE WAS BADLY CORRODED (EXFOLIATION). THE CENTER SECTION OF THIS PLATE EXPANDED DUE TO THE CORROSION WHICH CAUSED THE FORWARD ANCHOR FITTING TO CRACK. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FWD PAX DOOR ANCHOR FITTING AND PLATE. CLEANED PAX DOOR SILL HINGE AREA AND VERIFIED DRAIN LINES OF OBSTRUCTIONS. REPLACED PAX DOOR SEAL DUE TO TEAR, C/W NDT AND DVI OF PAX DOOR FWD ANCHOR ANCHOR FITTING MOUNT AREA MATING SURFACE AND BOLT HOLES FOR EVIDENCE OF ADDITIONAL DAMAGE OR CRACKS. NONE NOTED.

Part: CONTROL UNIT — FAULTED (TE FLAP SYSTEM) · airframe 42,003 hrs · 39,967 cycles

ON APPROACH RECEIVED FLAP FAIL CAUTION MESSAGE. FLAPS FAILED AT 30 DEGREES. MX WILL ATTEMPT THE RESET AS THE CREW WAS ON A TIGHT TAIL SWAP. ***AIRCRAFT REMOVED FROM SERVICE*** T/S IAW FIM SUPP 98-018I. FAULT LOGS SHOW FECU MOST LIKELY ISSUE. R/R FECU IAW AMM 27-51. OP CHECK GOOD. REMOVED PLACARD AND FROM MEL.

Part: SKIN — CRACKED (EXTERIOR) · airframe 41,455 hrs · 39,401 cycles

FS 235 RIGHT SIDE FUSELAGE EXTERNAL SKIN CRACKED AFT OF NOSE LANDING GEAR CUT-OUT, NEXT TO RIGHT RADIUS. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CRACK ON SKIN AT FS 235 RIGHT SIDE AFT OF NOSE LANDING GEAR CUT OUT, IAW CRJ200 REO 601R-53-11-048.

Part: STRUCTURE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 41,455 hrs · 39,401 cycles

T-CAP EXTRUSION IN CARGO BAY ON LBL 27 AT FS 559+118 TO FS 621 IS CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP EXTRUSION IN CARGO BAY AT LBL 27, FS 559+118 TO FS 621.00.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,445 hrs · 39,401 cycles

SEAT TRACK AT FS 559+32 TO FS 559+80, FBL 9 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT FS 559+32 TO FS 559+80, FBL 9.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 41,455 hrs · 39,401 cycles

SEAT TRACKAT FS 409 +112 ON LBL 9 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT FS 409+112, LBL 9.

Part: CONNECTOR — DISCONNECTED (SHUTOFF VALVE) · airframe 40,920 hrs · 38,840 cycles

WING OVERHEAT WARNING MSG ON CLIMBOUT. CW QRH MSG CLEARED WITH WING A TIICE OFF WITHIN 40 SECONDS. RETURNED TO MKE. LANDING WEIGHT UNDER 44 000 LBS, BTMSMAX 3,3,2,3 MC ACARS REPORTS THIS IS THE RH WING AIRCRAFT REMOVED FROM SERVICE UPON INSPECTION OF RH M/SOV FOUND CONNECTOR 2P3HA DISCONNECTED FROM VALVE. RE-CONNECTED CANNON PLUG OPS TESTED IAW AMM 30-12-00. OPS TEST GOOD NO DEFECTS NOTED AT THIS TIME.

Part: FUEL CONTROL — MALFUNCTIONED (APU) · airframe 40,533 hrs · 38,457 cycles

SUPPLEMENTAL INFORMATION, ATTEMPTED TO START APU BELOW 10000 FT FIRST ATTEMPT FAILED. UPON SECOND TRY STARTED NORMAL , HOWEVER VERY STRONG FUEL SMELL IN A/C AIRCRAFT. REMOVED FROM SERVICE, INVESTAGTED APU BAY FOIR FUEL. NONE FOUND. STARTED APU SEVERAL TIMES OPS CHECK GOOD IAW AMM 49-10-01. OPERATED BOTH PACKS NO ODOR EVIDENT. SUSPECT RESIDUAL FUEL FROM 1ST START ATTEMPT CAUSED MOMENTARY ODOR. OK FOR SERVICE. R/R APU FUEL CONTROL UNIT IAW AMM 49-31-00-06, OPS CHECK & LEAK CHECK GOOD FOUND APU HANGING 25% DURING START UP NO SMELL NOTED IN CABIN.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 40,312 hrs · 38,249 cycles

ON CLIMB OUT OF DAY AT 7000 FEET THE CREW RECEIVED A RIGHT WINDSHIELD HEAT CAUTION MESSAGE. CREW COMPLIED WITH THE QRH AND THE MESSAGE PERSISTS. DUE TO ICING EN-ROUTE AND AT THE DESTINATION IT WAS DECIDED TO RETURN BACK TO DAY

Part: STRINGER — BENT (FUSELAGE) · airframe 39,589 hrs · 37,547 cycles

STRINGER P/N 600-21302-63 REQUIRES FABRICATION DUE TO PART AVAILABILITY.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,589 hrs · 37,547 cycles

REF LP 326168 / 1 - FUSELAGE AFT OF F.S.755.00 ON BOTTOM SIDE OF FUSELAGE DAMAGED. APPROXIMATELY 28 INCHES BY 9 INCHES OF DENTED / WRINKLED SKIN. TWO STRINGERS DAMAGED ON INSIDE OF FUSELAGE APPROXIMATELY 1 INCH FROM F.S.755.00.

Part: APU — ODOR (CABIN) · airframe 39,516 hrs · 37,468 cycles

DURING ARRIVAL CREW ATTEMPTED APU START WITH NO LIGHT OFF. AFTER TWO MINUTES SUCCESSFULLY STARTED APU THEN RECEIVED ODOR OF FUEL IN CABIN, SHUT DOWN APU.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 39,414 hrs · 37,360 cycles

AFTER T/O AIRCRAFT WOULD NOT PRESSURIZE. NO ASSOCIATED MESSAGES. SWAPPED APC (PRESSURE CONTROLLERS) AND TRIED MANUAL PRESSURIZATION AIRCRAFT WOULD STILL NOT PRESSURIZE. RETURNED TO CAE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,264 hrs · 37,204 cycles

LOWER FLANGE ANGLE AT FS 333 IS CORRODED. REPLACED.

Part: PLUG — DAMAGED (PANEL) · airframe 39,264 hrs · 37,204 cycles

PANEL 131AL HAS A PREVIOUS FREEZE PLUG DAMAGED AT THE 12 O'CLOCK POSITION. REPLACED.

Part: INTERCOSTAL — CRACKED (NOT REPORTED) · airframe 39,264 hrs · 37,204 cycles

UPON C/W ITEM 6 OF EO# E13/024/449 FOUND INERCOSTAL 601R35210-17 TO HAVE A CRACK IN THE FWD CORNER INSTALLED PERMANENT REPAIR ON FOWARD CORNER OF INTERCOSTAL IAW AWAC SUPP# 13-085B

Part: SKIN — CRACKED (TRU DOOR LANDING) · airframe 39,264 hrs · 37,204 cycles

LH TRU DOOR LAND SKIN HAS CRACK AT UPP AFT LATCH CUT OUT REPAIR LH TRU DOOR LAND SKIN AT UPPER AFT LATCH CUT OUT IAW AWAC SUPP# 19-016A

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

*SUPPLEMENTAL INFORMATION* (DIFFICULTY DATE YEAR ENTERED IN ERROR, CHANGED FROM 2018 TO 2019) PAX DOOR ASSIST MOTOR OB MOUNT IS CRACKED AT LOWER RADIUS REMOVE AND REPLACED STIFFENER UAW SRM 51-52-06 AND 51-42-13.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

AEB STRINGER 15L INTERCOSTAL CRACKED REMOVED AND REPLACED AEB STRINGER 15L INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

FUSELAGE SKIN CRACKED IN THE AFT LT CORNER OF THE NLG SPADE DOOR CUT OUT. REPAIRED AFT LT CORNER OF NLG SPADE CUT OUT IAW REO 601R-53-11-048 REV D.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 39,264 hrs · 37,204 cycles

LT WING I/B LEADING EDGE O/B ATTACH ANGLE AT TRANSITION PNL IS CRACKED. REPLACED ANGLE IAW SRM 51-41-02.

Part: ATTACH ANGLE — CRACKED (CARGO DOOR) · airframe 39,264 hrs · 37,204 cycles

*SUPPLEMENTAL INFORMATION* (DIFFICULTY DATE YEAR ENTERED IN ERROR, CHANGED FROM 2018 TO 2019) CARGO DOOR MEMBER AFT LOWER ATTACH ANGLE CRACKED. REPLACE MEMBER ANGLE IAW CRJ 200 SRM 51-42-21.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 39,264 hrs · 37,204 cycles

CARGO DOOR BEAM MEMBER FWD LOWER CLIP CRACKED. REPLACED CLIP IAW SRM 51-42-21.

Part: BEAM — CUT (CARGO DOOR) · airframe 39,264 hrs · 37,204 cycles

CARGO DOOR BEAM MEMBER 601R35050-64 HAS A CUT ON FWD SIDE MADE BY CABLE ASSIST. REPLACED BEAM IAW SRM 51-42-06, 51-42-21.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

CRACKED STRINGER AT FS379.00, STR 3L. REPAIRED STR 3L AT FS 379.00 IAW SRM 53-00-03, 51-20-06, 51-21-11.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,264 hrs · 37,204 cycles

SERVICE DOOR THRESHOLD CORRODED. REPLACED THRESHOLD IAW SRM 51-42-06, 51-23-00.

Part: VANE — CHAFED (TE FLAP) · airframe 39,264 hrs · 37,204 cycles

LEFT WING I/B FLAP VANE HAS 3 WORN SPOTS. (CHAFING) REPAIRED FLAP VANE IAW SRM 51-42-13 AND REO601R-57-52-004 REV-D.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 39,264 hrs · 37,204 cycles

PAX DOOR UPPER EDGE MEMBER AFT EDGE IS CRACKED. REPAIRED PAX DOOR EDGE MEMBER IAW REO 601R-52-11-279 REV-NC.

Part: RIB — CRACKED (LT AILERON) · airframe 39,264 hrs · 37,204 cycles

LEFT AILERON RIB AT STA. 340.481 IS CRACKED. REMOVED AND REPLACED LEFT AILERON RIB AT STA 340.481 IAW CRJ 200 SRM 51-42-06 AND 51-42-13.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

FS 280 STRINGER 3L IB AND OB CLIPS ARE CRACKED. REMOVED AND REPLACED 2 EACHS CLIPS AT FS 280 IB AND OB OF STRINGER 3L IAW SRM 51-42-21 AND 51-42-06.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

FS 280 STRINGER 3L I/B AND OB CLIPS ARE CRACKED. REMOVED AND REPLACED 2 EACH CLIPS AT FS 280 IB AND OB OF STRINGER 3L IAW SRM 51-42-21 AND 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

AEB RT OBLIQUE ANGLE AT STRINGER 14R IS CRACKED. REMOVED AND REPLACED AEB RT OBLIQUE ANGLE AT STRINGER 14R IAW SRM 51-42-21.

Part: STIFFENER — CRACKED (EXHAUST) · airframe 39,264 hrs · 37,204 cycles

EXHAUST FAIRING 446AL FWD STIFFENER RING CRACKED. REPAIRED STIFFENER RING IAW CMM 79-11-00-300-810-A01, REPAIR SRS042.

Part: ATTACH ANGLE — CRACKED (EXTERNAL POWER) · airframe 39,264 hrs · 37,204 cycles

EXTERNAL POWER SERVICE PANEL LOWER ATTACH ANGLE IS CRACKED. REPLACED LOWER ATTACH ANGLE IAW SUPP. 15-039.

Part: RETAINER — CRACKED (PYLON) · airframe 39,264 hrs · 37,204 cycles

PNL 422BT SEAL RETAINER IS CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.

Part: STIFFENER — CRACKED (EXHAUST NOZZLE) · airframe 39,264 hrs · 37,204 cycles

PNL 436AL HAS A CRACKED FWD STIFFENER RING. REPAIRED STIFFENER RING IAW CMM 78-11-00-300-810-A01, REPAIR SRS042.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

LEFT WINDSHIELD POST LOWER FITTING IS CRACKED. REPLACED FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

RIGHT WINDSHIELD POST LOWER FITTING IS CRACKED. REPLACED FITTING IAW SRM 51-42-21.

Part: BEARING — WORN (LT ELEVATOR) · airframe 39,264 hrs · 37,204 cycles

LEFT ELEVATOR NUMBER 1 HINGE BEARING HAS SIDE PLAY. REPLACED BEARING IAW SUPP. 11-068A.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 39,264 hrs · 37,204 cycles

REAR PRESSURE BULKHEAD HAS A 1" VERTICAL CRACK ON THE FWD FACE, 1/2" O/B OF RBL 27.50, 15-1/2" UP FROM THE FLOOR, EXTENDING UPWARD 1" (3-1/4" DOWN FROM THE 2ND LINER SUPPORT TO TOP OF CRACK) REPAIR TO BE ACCOMPLISHED ON W/O 1016441-2000-0035, SN:6856902. THIS CARED GENERATED FOR SDR TRACKING ONLY.

Part: A/C PACK — OVERTEMP (LEFT) · airframe 39,067 hrs · 36,999 cycles

4847 - RECIEVED SMOKE IN CABIN AND COCKPIT, ISOLATED ISSUE TO LH PACK, SMOKE SMELLED LIKE DIRTY SOCKS, R PACK NORMAL VERIFIED LH PACK OVERTEMPS WHEN SELECTED ON. RH PACK OPS TESTS GOOD IAW AMM 21-51-00. INSPECTED BOTH PACKS IN AFT EQUIPMENT BAY, NO DEFECTS. COCKPIT AND CABIN ARE FREE OF SMOKE. REF 313950/4 FOR MEL.

Part: LENS — LOOSE (COCKPIT) · airframe 39,048 hrs · 36,977 cycles

ON CLIMB OUT AIRCRAFT WOULD NOT PRESSURIZE. TRIED OTHER PRESSURE CONTROLLER AND MANUAL MODE, NO CHANGE. MAX DELTA P OBSERVED WAS 0.3 PSI. AIRCRAFT DID AN AIR RETURN TO ORD. FOUND PRESSURE CONTROLLER SWITCH/LIGHT LENS LOOSE IN PANEL. RESECURED. PRESSURE CHECK GOOD IAW AMM 21-31-00 PRESSURIZED TO 4.1 DELTA P NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 38,754 hrs · 36,681 cycles

RECIEVED OVER PRESS CAUTION ON OPERABLE PACK WHEN AFTER TRANSFER ING BLEEDS. CONTINUED WITH APPENDIX B OF MEL AND ADVANCING THRUST LEVERS TO NORMALS LEVELS THERE WAS NO OVER PRESSURIZATION WITH BLEEDS ON APU. COMPLIED WITH A/C INSPECTION IAW 21-51-06. ALL CHECKS WERE GOOD. COMPLIED WITH A/C TEST IAW 21-51-05. ALL CKS WERE GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 38,389 hrs · 36,351 cycles

ON DESCENT AT FLIGHT LEVEL 25,000 RECEIVED FLAP FAIL CAUTION MSG AND CAS MIS COMP STATUS MSG. MSGS CLEARED AT 10,000 FT FOLLOWED QRH FLAPS 0 LANDING. C/W FLAP RESET PROCEDURE IAW SUP 98-18G BOX 12 FLAPS.

Part: STRUT — LOW (NLG) · airframe 37,459 hrs · 35,396 cycles

GEAR DISAGREE AND NOSE DOOR OPEN WARNINGS UPON GEAR RETRACTION. ALSO RECEIVED WOW INPUT CAUTION, AND STEERING INOP CAUTION. C/W QRH ALL MESSAGES CLEARED EXCEPT WOW INPUT CAUTION. WARNINGS POSTED 5 SECONDS AFTER GEAR RETRACTION AT APPROXIMATELY 1000 FEET, AND 165 KNOTS. NOSE GEAR SHOWED RED, AND MAINS SHOWED GREEN ON SYNOPTIC. EMERGENCY DECLARED. LANDING WAS SMOOTH. MANUAL RELEASE SYSTEM WAS NOT USED. HANDLE WAS NOT MOVED WITHIN 30 SECONDS OF INITIAL SELECTION. NO ICING, TURBULENCE, OR EXCESSIVE FLIGHT CONTROL MOVEMENTS WERE NOTED. SUSPECT NOSE STRUT PISTON NOT BOTTOMED OUT. SERVICED NLG OLEO STRUT IAW AMM 12-12-32 AND SUP 09-055.

Part: UNKNOWN — ODOR (CABIN) · airframe 37,210 hrs · 35,131 cycles

DURING FLIGHT STRONG FUEL SMELL BY ROW 9 AT GATE FUEL SMELL IS STILL PRESENT. RAN BOTH ENGINES AND INSPECTED FUEL LINES SHROUD BY ROWS 9,10,11 AND 12. NO FUEL SMELL OR LEAK DETECTED DURING INSPECTION.

Part: HINGE — WORN (PAX DOOR) · airframe 37,013 hrs · 34,937 cycles

PASSENGER DOOR WOULD NOT PROPERLY CLOSE. FOUND DOOR HINGE WORN. R & R THE PAX DOOR HINGE IAW SRM 53-21-23.

Part: BPSU — INOPERATIVE (TE FLAP SYS) · airframe 36,625 hrs · 34,567 cycles

RECEIVED A FLAPS FAIL CAUTION MESSAGE INFLIGHT, FLAPS INDICATED 0, COMPLIED WITH QRH, PERFORMED FLAPS 0 LANDING. PERFORMED FLAP RESET PROCEDURE IAW 98-18G, BOX 12. REPLACED THE RT BPSU IAW AMM 27-51-10, OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,191 hrs · 34,152 cycles

EMERGENCY EXIT SIGN BY SERVICE DOOR WILL NOT ILLUMINATE.

Part: GENERATOR — FAILED (NR 1) · airframe 36,064 hrs · 34,041 cycles

DURING TAKE OFF ROLL AT APROXIMATELY 100 KTS, THE CAPTAIN`S AND FIRST OFFICER`S PFD AND MFD FLICKERED. CONTINUED TAKE OFF. AT ROTATION, THE NR 1 GENERATOR CAUTION MESSAGE ALONG WITH TCAS FAIL STATUS MESSAGE, WS FAIL AND RA FAIL STATUS MESSAGES. LEVELED AT 5000 FT, COMPLIED WITH QRH. GENERATOR CAUTION CLEARED. RETRNED TO DEPARTURE. LANDED NORMAL. ON TOUCHDOWN, RECEIVED GLD UNSAFE CAUTION MESSAGE. MESSAGE CLEARED WITHOUT CREW ACTION. NO DEFECTS NOTED. R & R THE NR 1 GENERATOR IAW AMM 24-11-01-04. PERFORMED OPS CHECK AND LEAK CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,987 hrs · 33,972 cycles

DURING PREFLIGHT INSPECTION, CREW NOTED WHITE FLOOR EXIT SIGN NEAR SERVICE DOOR ON GALLEY BULKHEAD DID NOT ILLUMINATE. INSPECTED CONNECTORS ON SERVICE DOOR FLOOR LEVEL EMERGENCY LIGHTS, NO DEFECTS NOTED. R & R THE SIGN ASSY IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 35,821 hrs · 33,826 cycles

CABIN FLOOR SUPPORT CORRODED IN SEVERAL PLACES AT LBL45 BETWEEN BS 559.00 & 559+64

Part: POST — CRACKED (BS 409) · airframe 35,821 hrs · 33,826 cycles

VERTICAL POST AT BS 409+128 RBL 18 IS SUSPECTED TO BE CRACKED AT THE O/B AFT LOWER CORNER

Part: SEAT TRACK — CORRODED (BS 399-409) · corrosion level 2 · airframe 35,821 hrs · 33,826 cycles

RIGHT AISLE SEAT TRACK HAS CORROSION SPOTS BETWEEN BS 394 THRU 409+128

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 35,821 hrs · 33,826 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED

Part: POST — CRACKED (BS 409) · airframe 35,821 hrs · 33,826 cycles

BS 409+128 VERTICAL POST AT BL 0 JUST BELOW FLOOR LEVEL CRACKED. REPLACED THE POST.

Part: CARGO TRACK — DAMAGED (BS 559) · corrosion level 2 · airframe 35,821 hrs · 33,826 cycles

CARGO TRACK AT STA 559+80 TO +96, RBL 9 IS CORRODED AND GOUGED.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 35,821 hrs · 33,826 cycles

RT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 409+128 TO 559.

Part: FLOOR SUPPORT — CORRODED (BS 569-621) · corrosion level 2 · airframe 35,821 hrs · 33,826 cycles

FLOOR SUPPORT BS 569 TO 621, RBL 9 IS CORRODED.

Part: CARGO TRACK — DAMAGED (BS 612-617) · corrosion level 2 · airframe 35,821 hrs · 33,826 cycles

CARGO TRACK AT BS 615, LBL 9 IS CORRODED AND GOUGED.

Part: BRACKET — CRACKED (WINDOW) · airframe 35,821 hrs · 33,826 cycles

FLIGHT DECK CTR WINDOW POST RT LOWER BRACKET IS CRACKED

Part: ANGLE — CRACKED (BS 621) · airframe 35,821 hrs · 33,826 cycles

INTERCOSTAL ANGLE AT BS 621, LONGERON 13L IS CRACKED.

Part: BRACKET — CRACKED (WINDOW) · airframe 35,821 hrs · 33,826 cycles

FLIGHT DECK CTR WINDOW POST LOWER LT BRACKET IS CRACKED

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 35,821 hrs · 33,826 cycles

INTERCOSTAL ANGLE AT BS 621, LONGERON 14L CRACKED.

Part: CHANNEL — CRACKED (BS 574) · airframe 35,821 hrs · 33,826 cycles

CARGO DOOR FRAME LOWER CHANNEL FOUND CRACKED BS 574. REPLACED THE CHANNEL.

Part: ANGLE — CRACKED (BS 484) · airframe 35,821 hrs · 33,826 cycles

ANGLE IS CRACKED ON THE INBD SIDE AT BS 484. REPLACED THE ANGLE.

Part: DOOR SEAL — LACK OF LUBE (SERVICE DOOR) · airframe 34,663 hrs · 32,767 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. LUBED SERVICE DOOR SEAL AS REQUIRED. OPS CHECKED GOOD.

Part: PUSHROD — DIRTY (PAX DOOR) · airframe 34,452 hrs · 32,582 cycles

MAIN PAX DOOR DIFFICULT TO OPEN. CLEANED PUSHRODS, PIVOTS, ARMS, SPRING ROD, PRESS VLV DOOR PIVOTS & INSPECTED ICE BREAK CABLE. LUBED ALL AFFECTED MOVING PARTS ASSOCIATED WITH INNER & OUTER DOOR HANDLE IAW 12-20-52 AS APPLICABLE. OPERATIONS CHECKED GOOD IAW AMM 52-11-00.

Part: COMPUTER — MALFUNCTIONED (AHRS)

FLIGHT 3880, 3818 RECEIVED EFIS COMP MON DURING TAKEOFF ROLL AT APPROX 50 KNOTS. DG SPINS ERRATICALLY, BTMS 3-3-2-3. R & R 1 AHRS COMPUTER IAW AMM 34-21-01. OPERATIONS CHECKED GOOD NO OTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,957 hrs · 31,186 cycles

EXIT DOOR LIGHTING, GREEN STRIP BURNT OUT OR INOPERATIVE AT SEAT 7D ABOUT 7 - 8 INCHES. PLACARDED & PLACED ON MEL.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 32,617 hrs · 30,860 cycles

FLIGHT 3817, AT 25,000 FT YAW DAMP 1 STATUS MSG AFTER UNCOMMANDED YAW MOTION. R & R YAW DAMP 1 ACTUATOR IAW AMM 22-22-01. OPERATIONS CHECKED GOOD. SN OFF 3598 & SN ON 661 JC.

Part: SIGN — INOPERATIVE (CABIN) · airframe 32,406 hrs · 30,657 cycles

BOTH ELECTROLUMINESCENT EXIT IDENTIFIER SIGNS ON FWD BULKHEAD ARE NOT ILLUMINATING.

Part: LIGHT — LOOSE (CABIN) · airframe 32,374 hrs · 30,629 cycles

FLIGHT 3755 EMERGENCY LIGHT STRIP LOOSE BETWEEN ROW 11D & 12D. REPLACED FLOOR LIGHT STRIP PROTECTIVE COVER AS REQUIRED.

Part: STRIP — LOOSE (CABIN) · airframe 32,374 hrs · 30,629 cycles

EMERGENCY FLOOR LIGHT STRIP LOOSE BETWEEN ROW 11D & 12D.

Part: WARNING SYSTEM — ACTIVATED (LANDING GEAR) · airframe 32,210 hrs · 30,466 cycles

UPON GEAR RETRACTION, RECEIVED NOSE DOOR OPEN & GEAR DISAGREE RED WARNING. MAIN GEAR INDICATED UP WHILE NOSE GEAR REMAINED DOWN & INDICATED GREEN DOWN MSG. REMAINED UNTIL WE PUT THE GEAR HANDLE DOWN, 5 - 7 MINUTES, IAW QRH, LANDED NORMALLY. NO OBVIOUS DAMAGE TO NOSE GEAR. SEE 257464 4 FOR HYD 3A PUMP MEL.

Part: LANDING GEAR — UNKNOWN · airframe 31,441 hrs · 29,739 cycles

ON TAKEOFF RECEIVED GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH. 5 SECONDS AFTER GEAR SELECTED UP, NOSE DOOR & ANTI-SKID MESSAGES ALSO PRESENT. RT MLG SHOWED RED. MANUAL RELEASE WAS USED. HYD QTY PRESSURE & TEMP ALL NORMAL IN ALL 3 SYSTEMS. ALL PUMPS WERE SELECTED TO AUTO THEN ON FOR THE QRH.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,805 hrs · 25,945 cycles

OBLIQUE ANGLE AT FS 621.00, BULKHEAD CRACKED AT 14L.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,805 hrs · 25,945 cycles

OBLIQUE ANGLE AT FS 621, BULKHEAD IS CRACKED AT STRINGER 14R.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,214 hrs · 29,543 cycles

CORROSION ON FRAME AT FS 605.00 IN CARGO BILGE AREA.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,805 hrs · 25,723 cycles

COMPLIED WITH 4DMI17961, REPAIR LOWER SKIN BETWEEN FS 598-605.

Part: COWLING — CRACKED · airframe 26,805 hrs · 25,945 cycles

RIGHT UPPER CORE COWL INBD FWD LE CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,214 hrs · 29,543 cycles

RIGHT & LEFT SEAT TRACKS HAVE CORROSION ON FWD ENDS.

Part: MOUNT BRACKET — CRACKED (RT MLG WW) · airframe 31,214 hrs · 29,543 cycles

RIGHT MLG WW BRAKE LINE MOUNT BRACKET IS CRACKED.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 31,214 hrs · 29,543 cycles

LEFT MLG WW DRAG ANGLE ADJACENT TO BATTERY RIB IS CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,214 hrs · 29,543 cycles

CARGO SEAT TRACKS ARE CORRODED AT LBL 9 AT FS 564, LBL 9 AT FS 559+75 & RBL 9 AT FS 564.00.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 31,214 hrs · 29,543 cycles

RIGHT MLG WW DRAG ANGLE ADJACENT TO BATTERY RIB IS CRACKED.

Part: SKIN — DENTED (TE FLAP) · airframe 31,215 hrs · 29,543 cycles

LEFT INBD FLAP LOWER SKIN DENTED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 31,214 hrs · 29,543 cycles

FS 280 FLOOR SUPPORT CLIP AT RBL OTBD IS CRACKED.

Part: RIB — CRACKED (RT WING) · airframe 31,214 hrs · 29,543 cycles

RIGHT MLG WW BATTERY RIB IS CRACKED.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,214 hrs · 25,543 cycles

SERVICE DOOR THRESHOLD IS CORRODED.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 31,215 hrs · 29,543 cycles

AC GND POWER RECEPTACLE MOUNT BRACKET CRACKED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,215 hrs · 29,543 cycles

RIGHT FLOOR SILL FWD OF SERVICE DOOR CORRODED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,215 hrs · 29,543 cycles

PASSENGER DOOR LOWER SILL HAS CORROSION NEAR PROX SENSOR ON LOWER FLOOR SUPPORT ANGLE.

Part: ANGLE — CRACKED (RT WING) · airframe 31,215 hrs · 29,543 cycles

RIGHT WING LE TRANSITION DUCT SUPPORT ANGLE CRACKED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 31,215 hrs · 29,543 cycles

HYDRAULICS NR 2 FILTER MANIFOLD BRACKET CRACKED AT LOWER AFT CORNER.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 30,285 hrs · 28,688 cycles

DURING CLIMB AT 14,000 FT, RT PACK FAILED WITH ASSOCIATED RT PACK OFF STATUS MSG. NO OVER TEMP OR OVER PRESS ASSOCIATED WITH PACK OFF MSG. COMPLIED WITH QRH, PACK WN RESET. COORDINATED WITH ATC, DESCENDED TO 10000FT, DECLARED EMER & CONDUCTED UNPRESSURIZED FLIGHT. INSPECTED BOTH PACKS FOR LOOSE DUCTS, NO PHYSICAL DEFECTS NOTED. VERIFIED RT PACK ACM SPINS FREELY & HAS OIL. ALL DUCTING IS ATTACHED, RAN PACK IN AUTO OR MANUAL MODES. OPERATIONS CHECKED GOOD IAW AMM 21-51.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 29,481 hrs · 27,929 cycles

UPON GEAR RETRACTION RECEIVED RED WARNING GEAR DISAGREE MSG, AIRSPEED 195 KNOTS, ON RETRACTION, GEAR SELECTED UP, NO OTHER EIC. AS MSG POSTED, MAINS WEE WHITE, NOSE WAS RED, MANUAL RELEASE SYS OPERATED IAW QRH, HYD QUT NR 3 50 PERCENT TEMP 65 DEG, HYD PUMP 3B ON. IAW 272855 4 FOR LANDING GEAR RETRACTION MEL.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 29,082 hrs · 27,537 cycles

WHILE IN CRUISE AT FL310, RT WINDSHIELD CRACKED. REQUESTED IMMEDIATE DESCENT & ATC GAVE CLEARANCE TO 10,000. RAN QRH, DIVERTED TO RDU & DECLARED AN EMERGENCY. LANDING WAS UNEVENTFUL. R & R FIRST OFFICER`S WINDSHIELD, PERFORMED OPERATIONS & LEAK CHECK GOOD IAW AMM 56-11-01.

Part: RECEPTACLE — FAULTY (EXTERNAL POWER) · airframe 28,636 hrs · 27,117 cycles

4053 RAMP MANAGER REPORTS FLAMES AND SMOKE AT AC RECEPTACLE WHEN AC POWER APPLIED. SUSPECT EXTERNAL POWER PLUG ON JET BRIDGE WET & CAUSED A SHORT. NO DAMAGE TO ACFT NOTED, NO CB POPPED, ALL ELEC SYS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 28,237 hrs · 26,732 cycles

AFTER TAKE OFF, APU SOV OPEN MESSAGE DISPLAYED. COMPLIES WITH QRH AND RETURNED TO DEPARTURE. PERFORMED OPS CHECK OF APU, NO APU SOV MESSAGE PRESENT. OPS CHECKED GOOD IAW AMM 49-10-01.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 26,481 hrs · 25,012 cycles

RIGHT FLAP VANE L/E CHAFED IN THREE LOCATIONS. REPAIRED IAW REO 601R-57-52-004 REV D.

Part: FIRESHIELD — GOUGED (RT NACELLE) · airframe 26,481 hrs · 25,012 cycles

GOUGE ON FIRESHIELD ON RIGHT LOWER CORE COLW LEADING EDGE. INSTALLED DOUBLER ON TO RIGHT LOWER CORE COWL LEADING EDGE TRIM STRIP.

Part: STRUCTURE — CHAFED (MLG DOOR) · airframe 26,481 hrs · 25,012 cycles

LEFT MLG DOOR HAS CHAFE AREAS NEAR CENTER FWD AREA. REPAIRED LEFT MLG DOOR INNER SKIN IAW SRM 51-42-13 & 51-42-2.

Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 26,481 hrs · 25,012 cycles

LEFT I/B FLAP I/B AFT HINGE BOX MOUNT LUG DAMAGED. BLENDED LEFT I/B FLAP I/B AFT HINGE BOX MOUNT LUG IAW REO 601R-57-21-1863.

Part: BULKHEAD — CHAFED (BS 169) · airframe 26,481 hrs · 25,012 cycles

BULKHEAD AT FS 169.00 HAS CHAFE MARKS FROM RADOME FASTENERS. BLENDED CHAFED AREAS IAW SRM 53-00-00.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 26,481 hrs · 25,012 cycles

CRACK AT FS 605 LEFT O/B UNDER CARGO DOOR SILL PLATE. REMOVED AND REPLACED ATTACH ANGLE AT FS 605 LEFT FWD SIDE UNDER CARGO DOOR SILL PLATE.

Part: RETAINER — CRACKED (LT PYLON) · airframe 26,481 hrs · 25,012 cycles

LEFT LOWER PYLON DIVIDER PANEL SEAL RETAINER CRACKED. REMOVE AND REPLACE SEAL AND SEAL RETAINER PER SRM.

Part: PUSH-PULL ROD — CHAFED (LT MLG DOOR) · airframe 26,481 hrs · 25,012 cycles

LEFT MLG DOOR BELL CRANK PUSH/PULL ROD AND LUG ARE CHAFED. BLENDED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 26,481 hrs · 25,012 cycles

CLIPS AT FS 484 RBL 36 AND RBL 27 AND CRACKED. REMOVED AND REPLACED PER REO 601R-53-41-059.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,481 hrs · 25,012 cycles

ANGLE CRACKED AT FS 280 FLOORBEAM RBL 9. REMOVED AND REPLACED ANGLE.

Part: SKIN — DENTED (RT NACELLE) · airframe 26,481 hrs · 25,012 cycles

RIGHT UPPER CORE COWL SKIN DENT ON O/B SIDE ON POLISHED AREA. REPAIRED DENT PER CMM 71-12-01 REPAIR SRS021.

Part: BLEED VALVE — FAILED · airframe 25,343 hrs · 23,909 cycles

FLIGHT LEVEL 250, RT PACK WENT OFF LINE AND RT 10TH STAGE SHUTOFF VALVE WOULD NOT OPEN. DESCENDED TO 10,000 FT AND TRANSFERRED RT PACK TO APU. EMERGENCY DECLARED.

Part: RETAINER — DAMAGED (PAX DOOR) · airframe 22,090 hrs · 20,537 cycles

PAX DOOR SEAL RETAINER DAMAGED AT FWD LWR CORNER. R & R PAX DOOR FWD LWR SEAL RETAINER IAW SRM 51-42-06 AND 51-42-13.

Part: DOOR FRAME — DAMAGED (BS 310) · airframe 22,090 hrs · 20,537 cycles

PAX DOOR SURROUND STRUCTURE DAMAGED AT FWD LOWER CORNER AFT HINGE ASSY. REPAIRED PAX DOOR CUT OUT SKIN LOWER FWD CORNER IAW SRM 53-21-31. REPAIR NR 1, FIG 202.

Part: PANEL — CHAFED (SERVICE DOOR) · airframe 22,090 hrs · 20,537 cycles

SERVICE DOOR HINGE CLOSE OUT PANEL IS CHAFED ON UPPER SIDE. REPAIRED IAW REO 601R-52-41-169.

Part: SUPPORT — CRACKED (APU ENCLOSURE) · airframe 22,090 hrs · 20,537 cycles

APU ENCLOSURE DOOR HAS 3 EA CRACKS AT LATCH TANG ON BOTTOM SIDE LT SUPPORT BRACE. TOP CENTER SUPPORT BRACE. REAPIRED APU ENCLOSURE DOOR 311B2 IAW REO 601R-49-11-070, REV A.

Part: DOOR — CRACKED (APU ENCLOSURE) · airframe 22,090 hrs · 20,537 cycles

APU ENCLOSURE OIL DOOR HAS CRACK ON INSIDE SUPPORT BRACE. REPAIRED APU ENCLOSURE DOOR 311B2 OIL SENSOR DOOR STRUCTURE IAW REO 601R-49-11-070, REV A.

Part: SKIN — CHAFED (RT AILERON) · airframe 22,090 hrs · 20,537 cycles

RT AILERON IS CHAFED ALONG L/E. REPAIRED RT AILERON L/E IAW REO 601R-57-60-0013.

Part: TRACK — DAMAGED (THRUST REVERSER) · airframe 22,090 hrs · 20,537 cycles

RT THRUST REVERSER INBD LOWER TRACK AND LUG DAMAGED. BLENDED LUG WITHIN LIMITS IAW REO 601R-78-34-2435. R & R WITH INBD TRACK.

Part: FLOORBEAM — CORRODED (BS 589) · corrosion level 2 · airframe 22,090 hrs · 20,537 cycles

CORROSION AROUND NUT PLATE HOLES ON FLOORBEAM SHIM OF FLOOR PANEL NR 281WLF. REMOVED, FABRICATED NEW SKIN.

Part: STRUCTURE — DAMAGED (BS 625) · airframe 22,090 hrs · 20,537 cycles

GROUND AIR SUPPLY CONNECTION SURROUND STRUCTURE IS DAMAGED. REPAIRED GROUND AIR SUPPLY CONNECTION SURROUND STRUCTURE IAW SRM 51-74-16 AND 53-00-03.

Part: PANEL — CHAFED (LT NACELLE) · airframe 22,090 hrs · 20,537 cycles

LT PYLON PANEL 412DB SEPARATES KNIFE EDGE. R & R FWD SEPARATOR, BLENDED AFT SEPERATOR TO WITHIN LIMITS IAW SRM 51-42-06, 51-42-13, 54-10-00 AND 51-12-00.

Part: SKIN — DENTED (NACELLE) · airframe 22,090 hrs · 20,537 cycles

OUTER SKIN DENTED ON 435AT UPPER CORE COWL. REPAIR DENTED DAMAGE ON OUTER SKIN UPPER CORE COWL.

Part: SKIN — CHAFED (LT TAIL PIPE) · airframe 22,090 hrs · 20,537 cycles

INNER SKIN ON LT TAIL PIPE FAIRING CHAFED IN 2 AREAS MARKED. REPAIRED CHAFED AREAS ON LT TAIL PIPE IAW CMM 78-11-00 AND REO 601R-78-10-1173.

Part: FLOOR SUPPORT — CORRODED (BS 565-620) · corrosion level 2 · airframe 22,090 hrs · 20,537 cycles

FLOOR SUPPORT CAP LBL27, FS 565 TO FS 620 HAS CORROSION AROUND NUT PLATE HOLES. R & R WITH SERVICEABLE EXTENSION BRACKET PN 60-14903 ON FLOOR SUPPORT CAP LBL27 AT FS 565 TO FS 620.

Part: SEAT TRACK — CORRODED (CARGO BAY) · airframe 22,090 hrs · 20,537 cycles

ALL CARGO BAY TIE DOWN TRACKS HAVE CORROSION. CLEANED CORROSION (7EA) TIE DOWN TRACKS (4EA) ANCHOR PLATES FOUND TO BE WITHIN LIMITS ALONG WITH REST OF CARGO BAY TIE DOWN TRACKS IAW SRM 53-61-49.

Part: BULKHEAD — GOUGED (BS 621) · airframe 22,090 hrs · 20,537 cycles

FS 621 BULKHEAD IS GOUGED INBD OF LBL9 AT WL80. REPAIRED DAMAGE AT LBL8 IAW REO 601R-53-61-2155. FOUND DAMAGE AT RBL 42.20, WL 76.25. DURING REPAIR AT LBL8. REPAIRED DAMAGE AT RBL 42.20 IAW REO 601R-53-61-2155.

Part: RAIL — CRACKED (CARGO DOOR) · airframe 22,090 hrs · 20,537 cycles

FWD CARGO DOOR SUPPORT RAIL AT FS 584 CRACKED. R & R SUPPORT RAIL BRACKET.

Part: FITTING — CORRODED (BS 310) · airframe 22,090 hrs · 20,537 cycles

PAX DOOR SILL FWD CLEAT HAS CORROSION. REMOVED UNSERVICEABLE FWD CLEAT INSTALLED SERVICEABLE FWD CLEAT.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,090 hrs · 20,537 cycles

PAX DOOR SILL AFT CLEAT HAS CORROSION. REMOVED CLEAT AND BRACKET INSTALLED SERVICEABLE PAX DOOR SILL AFT CLEAT AND BRACKET.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 22,090 hrs · 20,537 cycles

FWD SIDE OF PAX DOOR STEP NR4 SUPPORT IS CRACKED NEXT TO HANDRAIL BRACKET CUT OUT DAMAGED SECTION ON FWD SIDE PANEL PF PAX DOOR THEN FABRICATED NEW SECTION AND INSTALLED IAW B/A REO 601R5211702, REV C.

Part: SKIN — CHAFED (LT NACELLE) · airframe 22,090 hrs · 20,537 cycles

LT LOWER CORE COWL CHAFED ON OUTER SKIN NEXT TO DOUBLE LATCH, C/W CMM 71-12-01.

Part: BULKHEAD — CHAFED (BS 280) · airframe 22,090 hrs · 20,537 cycles

AFT 280 BULKHEAD CHAFED FROM FWD GALLEY DOOR. REPAIRED 280, BULKHEAD IAW REO 601R-53-11-1727.

Part: SKIN — CHAFED (LT AILERON) · airframe 22,090 hrs · 20,537 cycles

LT AILERON UPPER L/E IS CHAFED. REMOVED UNSERVICEABLE LT AILERON UPPER L/E. INSTALLED SERVICEABLE LT AILERON UPPER L/E, PN 601R13031-165.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 22,090 hrs · 20,537 cycles

AFT SIDE OF PAX DOOR STEP NR 4 SUPPORT STRUCTURE CRACKED NEXT TO HANDRAIL. CUT OUT DAMAGE SECTION OF AFT SIDE PANEL OF PAX DOOR, THEN FABRICATED NEW SECTION AND INSTALLED IAW REO 601R5211-702, REV C.

Part: FLOOR SUPPORT — CORRODED (BS 589-620) · corrosion level 2 · airframe 22,090 hrs · 20,537 cycles

FLOORBEAM CAP FS 589 TO FS 620.00, LBL 9 HAS CORROSION AT NUT PLATE HOLES. REMOVED CORROSION FROM NUT PLATE HOLES IAW SRM 51-12-00 AND REO 601R-53-00-005, REV B.

Part: STRIP — CHAFED (RT NOSE COWL) · airframe 22,090 hrs · 20,537 cycles

T/E STRIP ON RT UPPER NOSE COWL IS CHAFED. R & R T/E STRIP ON RT UPPER NOSE COWL IAW CMM 71-14-01.

Part: ANGLE — CRACKED (BS 625) · airframe 22,090 hrs · 20,537 cycles

FS 625 LT OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM FS 625 LT AND INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-61-422, REV NC.

Part: FLOORBEAM — CORRODED (BS 589) · corrosion level 2 · airframe 22,090 hrs · 20,537 cycles

FLOORBEAM AT FS 589.00 OTBD NEXT TO FLOOR LEDGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-12-00 AND SRM 51-11-00 ALODINED, PRIMED, TOPCOATED.

Part: ANGLE — CRACKED (BS 625) · airframe 22,090 hrs · 20,537 cycles

FS 625, RT OBLIQUE ANGLE IS CRACKED. REMOVED UNSERVICEABLE OBLIQUE ANGLE FROM FS 625 RT AND INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-61-422, REV NC.

Part: STRUCTURE — CHAFED (NOSE COWL) · airframe 22,090 hrs · 20,537 cycles

T/E OF RT LOWER NOSE COWL IS CHAFED. R & R T/E STRIP ON RT LOWER NOSE COWL IAW CMM 71-14-01.

Part: SELECTOR VALVE — INOPERATIVE (NLG) · airframe 21,869 hrs · 20,320 cycles

ON GEAR EXTENSION RECEIVED "GEAR DISAGREE" MSG FOLLOWED WITH DOWN INDICATION OF THE NLG. FOLLOWED QRH MSG CLEARED AND RECEIVED NORMAL DOWN INDICATION AFTER PULLING THE EMERGENCY EXTEND HANDLE. R & R NLG SELECTOR VALVE IAW AMM 32-33-10.

Part: ADG — UNWANTED DEPLOY · airframe 21,483 hrs · 19,903 cycles

ADG INADVERTANT DEPLOYMENT AT FL310 COMPLIED WITH QRH ALL SYS POWERED NORMALLY PRIOR TO ADG DEPLOYMENT. COMPLIED WITH RETRACTION OF ADG IAW AMM 24-23-01. OPS CK GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 20,953 hrs · 19,357 cycles

INFLIGHT RECEIVED "OTBD GRND SPLR FAULT" AND "FLIGHT SPOILER FAULT" MESSAGES. INFLIGHT AND ON THE GROUND, FLIGHT CONTROL SYNOPTIC PAGE INDICATION FOR BOTH OTBD GRND SPOILERS AND FLIGHT SPOILERS INTEWRMITTENTLY CHANGING COLORS FROM GREEN, WHITE OR YELLOW. DURING FLIGHT NOTICED BUFFETING WHEN MESSAGES WERE DISPLAYED. SELECTED SPOILERS TO MAN DISARM. MESSAGES CLEARED. NO ADDITIONAL BUFFETING NOTED. TROUBLESHOT USING SECU BREAK-OUT BOX, FOUND RT OTBD FLT SPOILER PCU TORQUE MOTOR OUT OF LIMITS. R & R RT OTBD FLT SPOILER PCU REQ AMM 27-62-01 RIG/LK CHECKS GOOD.

Part: SKIN — DAMAGED (BS 755) · airframe 20,120 hrs · 18,474 cycles

ACFT STRUCK BY TUG ON TAIL ON RT SIDE BETWEEN VS 55.625-VS 67.50. REMOVED DAMAGED SKIN IN SECTION STR 13R AND BUTT SPLICE STRAP. REPAIRED IAW 601R-53-71-116.

Part: CONTROL PANEL — FAILED (FUEL CROSSFEED) · airframe 19,665 hrs · 18,005 cycles

AUTO CROSSFLOW INHIBIT MESSAGE ON ED2, NO POWER ON FUEL, DEFUEL PANEL. R & R FUEL/DEFUEL CONTROL PANEL AND HARNESS IAW AMM 28-25-16, PERFORMED OPS TEST IAW AMM 28-25-00. OPS TEST GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (ENGINE OIL SYS) · airframe 18,939 hrs · 17,282 cycles

2 INDICATION OF RT ENGINE LOW OIL PRESSURE WARNING. ENG OIL INDICATION NORMAL. PERFORMED HIGH POWER ENGINE RUN A T/O PWR FOR APPROX 10 MINUTES. OPERATION NORMAL. OIL PRESSURE INDICATION GOOD. INSPECTED LOP SWITCH CONNECTOR AND HARNESS. R & R LOP SWITCH IAW AMM 79-31-03. OPS CHECKS AND LEAK CHECKS GOOD. (ADDED 1 PT OF OIL).

Part: FCU — FAILED (TE FLAPS) · airframe 18,900 hrs · 17,275 cycles

ON APPROACH, FLAPS FAILED WHEN SELECTED TO 30 DEGREES. AIRSPEED WAS 170 KIAS WITH GEAR DOWN. FLAPS FAILED AT 19 DEGREES. FOND NUMEROUS CODES FOR FLAP CONTROL IN FECU, REPLACED FLAP CONTROL LEVER IAW AMM 27-51-01. OPS CK GOOD AT THIS TIME.

Part: CONNECTOR — LOOSE (OIL PRESSURE) · airframe 18,610 hrs · 16,957 cycles

ON CLIMB-OUT, RECEIVED RT ENG OIL PRESS WARNING MSG WITH AURAL WARNING. C/W QRH. REDUCED POWER AND MSG WENT OUT. MSG CAME ON AT 90 PERCENT N1, APPROX 70 PSI. NO OTHER CAS MSGS. FOUND OIL PRESSURE TRANSDUCER CONNECTOR PLUG TO BE VERY LOOSE AT BACKSHELL AND OIL PRESSURE SWITCH BACKSHELL WAS LOOSE FOR RT ENGINE. TIGHTENED IAW POWERPLANT BUILDUP MANUAL 71-00-03. OPS CHECK GOOD. (K)

Part: UNKNOWN — ODOR (CABIN) · airframe 18,233 hrs · 16,587 cycles

BURNING ODOR NOTICED AT MID SECTION OF CABIN, STRONGEST AROUND ROW 8. IT HAS BEEN DETERMINED THAT THIS WAS A RESIDUAL ODOR FROM A PREVIOUS DISCREPANCY CABIN AREA WAS OZONE CLEARED, NO FURTHER SMOKE ODOR EXISTS. (K)

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 18,206 hrs · 16,559 cycles

STRONG BURNING ODOR IN CABIN REQUEST INSPECTION. REMOVED AND REPLACED OVERHEAD BIN LIGHT BALLAST OVER ROW 7CA. OPS CHECK GOOD AT THIS TIME IAW AMM 33-20-00. (K)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 18,208 hrs · 16,560 cycles

STRONG BURING ODOR AT MID CABIN OVERHEAD. FOUND ODOR TO BE VERY STRONG AT CEILING PANEL 7CA. REMOVED CEILING PANE LS AND PAX SERV UNIT PANELS FROM 5AD-8AC FOR T/S. FOUND NO ODOR UNDER PSU`S REMOVED CEILING INSULATION AND VERIVIED THAT NO CHAFED WIRES ON CEILING SIDEWALL AND COAX CABLES THROUGH THAT AREA. ODOR REMOVED AND AROUND EMERGENCY BATTERY PACK NR 3. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND CHARGER IAW AMM 33-51-00. OPS CK GOOD. NO FURTHER ODORS, REINSTALLED PSU AND CEILING PANELS. (K)

Part: IDG — MAKING METAL (LEFT) · airframe 18,022 hrs · 16,381 cycles

CLIMBING THRU FL 200, FELT A THUD AND HAD A NR 1 GEN CAUTION APPEARED, C/W QRH MSG CLEARED. 2 THUD HEARD IDG 1 FAULT CAUTION, RAN QRH DISCONNECTED IDG. FOUND LT IDG OIL SCAVENGE FILTER TO BE CONTAMINATED WITH METAL C/W ACTION FOR MEL 24-11-01-01, REF 192748/4 FOR MEL. 192748/4 - REMOVED AND REPLACED LT IDG. OPS AND LEAK CHECK GOOD. REMOVED MEL. (K)

Part: PRESSURE SWITCH — MALFUNCTIONED (RT ENGINE) · airframe 17,991 hrs · 16,353 cycles

RECEIVED RT ENGINE OIL PRESSURE MASTER WARNING ON DESCENT, 3 TIMES COMPLIED WITH QRH OIL PRESSURE INDICATED 63 PSI. REMOVED AND REPLACED RT ENGINE LOW OIL PRESSURE SWITCH IAW AMM 79-31-03. OPS CHECK LEAK CHECK GOOD. RAN ENGINE AT ALL POWER SETTINGS. NO FAULTS NOTED, NO OIL ADDED. (K)

Part: FIRE LOOP — SHORTED (MLG WW) · airframe 17,864 hrs · 16,222 cycles

AFTER DEPARTURE SELECTED GEAR UP, AFTERWARD RECEIVED GEAR BAY OVERHEAT WARNING AURAL ON ED1 MSG, RAN QRH, MSG REMAINED, AND SOUNDED REPEATEDLY, RETURNED TO DEPARTURE. INS AND FOUND LOOP INSULATOR BRACKET MISSING RUBBER, INSULATION MIGRATED INBD, REPLACED FASTENER, MOVED INSULATOR TO PROPER POSITION AND RESECURED IAW AMM 26-10, OPS CHECK OK. (K)

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 1 · airframe 17,321 hrs · 15,695 cycles

LT WING PLANK ACCESS HOLE 510AB CORRODED. LT WING PLANK ACCESS HOLE 510AB. CORROSION REMOVED IAW REO 601R-57-21-030 REV G. EDDY CURRENT PERFORMED IAW REO 601R-57-21-030 REV G. ROTO PEEN PERFORMED AND ALODINE TREATMENT IAW REO 601R-57-21-03, REV G. (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 17,321 hrs · 15,695 cycles

PAX DOOR LOWER SILL LONGERON INNER AND OUTER SURFACE CORRODED. PAX DOOR LOWER SILL LONGERON REPLACED IAW SRM 51-42-06. (K)

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 17,464 hrs · 15,826 cycles

CREW ESCAPE HATCH OUTER HANDLE IS CORRODED. CREW ESCAPE HATCH OUTER HANDLE REPLACED IAW AMM TASK 52-22-03-400-801 AND OPS CHECK FOUND SERVICEABLE IAW CRJ200 52-22-02-710-801. (K)

Part: SILL — CRACKED (BS 589-605) · airframe 17,321 hrs · 15,695 cycles

CARGO DOOR SILL CRACKED AT OTBD FASTENERS FS 589-605. CARGO DOOR SILL. REPAIRED IAW REO 601R-53-61-433. (K)

Part: CROSSBEAM — CRACKED (BS 280) · airframe 17,321 hrs · 15,695 cycles

CROSSBEAM AT FS 280.00, LBL 9.00, WL 72.00 IS CRACKED IN THE LOWER RADIUS, CRACK LENGTH IS .600 INCH LONG. CROSSBEAM REPAIRED IAW REO 601R-53-11-171, SCHEME A. (K)

Part: CROSSBEAM — CRACKED (BS 280) · airframe 17,321 hrs · 15,695 cycles

CROSSBEAM AT FS 280.00, RBL 9.00, WL 72.00 IS CRACKED IN LOWER RADIUS. CRACK LENGTH IS .700 INCH LONG. CROSSBEAM AT FS 280.00, RBL 9.00, WL 72.00 IN LOWER RADIUS REPAIRED IAW REO 601R-53-11-171. REV D REPAIR SCHEME A. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 17,321 hrs · 15,695 cycles

CRACK FOUND ON FWD PRESSURE BULKHEAD FS 202.75 AT BL 23.71 AROUND PARKING BRAKE CABLE. CUTOUT CARRIED/OUT NDT PERFORMED, DOUBLER AND SHIMS FABRICATED AND WET INSTALLED, FITTING REPLACED AND WET INSTALLED. IAW REO 601R-53-11-563. (K)

Part: FITTING — CRACKED (BS 461) · airframe 17,321 hrs · 15,695 cycles

CRACK FOUND ON MACHINED FITTING, FS 461, RBL 9, OTBD MACHINED FLOOR SUPPORT FITTING AT FS 461, RBL 9, WL 72.00. REPLACED IAW SRM 51-42-21 AND DWG 601R31118. (K)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,830 hrs · 15,250 cycles

MWC 17. FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING, INSTALLING REPAIR PARTS IAW REO 601R-53-61-1230 REV D.

Part: COALESCER BAG — ODOR (AIR CON SYS)

NOTICED OILY ODOR COMING FROM AIR CONDITIONING, BOTH PACS IN ENGINE OR APU AS AIR SOURCE, STRONGER WHEN DUCT TEMP IS HOTTER. REMOVED AND REPLACED RT ACM WATER SEPARATOR COALESCER BAG, REACTIVATED LT AND RT PACKS AND OVERBOARD EXHAUST SOV, OPS CHECK GOOD IAW AMM 21-51-00. REMOVED FROM MEL. (K)

Part: APU — ODOR (APU BAY) · airframe 16,388 hrs · 14,824 cycles

RT PAC HAS OIL SMELL WHILE ON APU AIR. OILY SMELL DISSIPATES WHILE ON 10TH STAGE BLEED AIR. REMOVED AND REPLACED APU IAW AMM 49-10-00, OPS CHECK GOOD. (K)

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 12,772 hrs · 11,368 cycles

FLAPS FAIL MASTER CAUTION OCCURRED 15 MINUTS AFTER DEPARTURE. QRH WAS ACCOMPLISHED. FLAPS FAILED AT ZERO DEGREES. EMERGENCY LANDING DECLARED FOR PRECAUTIONARY MEASURES. INTERROGATED FECU, FOUND L-BPSU MISRIGGED, NO EVIDENCE OF TWISTING OR ABNORMAL DEFORMATION DETECTED. NO JAMMED, DISCONNECTED OR DRAGGING COMPONENTS FOUND. REMOVED AND REPLACED L-BPSU IAW SUPP 98-018B. (K)

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,404 hrs · 11,009 cycles

FS 280.0 FLOOR SUPPORT CLIPS PN 601R31113-57 CRACKED APPROX .1 INCH LONG AT IB AND OB SIDE LBL 9.0. (K) [SUP 06-05-07] MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS AT FS 280 LBL 9 IAW CRJ 200 SRM 51-40-11, 51-42-02, 51-42-21. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,404 hrs · 11,009 cycles

FS 280.0 FLOOR SUPPORT ANGLE PN 600-34017-595 CRACKED APPROX .2 INCHES LONG ON AFT SIDE FS 280.0 OB OF LBL 9.0. (K) [SUP 05-17-07] MAINTENANCE REPAIRED DAMAGED SECTION, DRILLED NEW SECTION OF ANGLE AND SPLICES IAW REO 601R-53-11-136 STEPS 1-6 ANGLE P/N 600-34017-595. (M)

Part: SKIN — CORRODED (RT WING) · airframe 12,404 hrs · 11,009 cycles

RT WING PLANK ACCESS HOLE AT 640 AB HAS MINOR PITTING IN CRITICAL AND NON-CRITICAL AREA. (K) [SUP 06-05-07] MAINTENANCE CLEANED EDGE OF FUEL TANK ACCESS DOOR SKIN CUTOUT. BLENDED CORROSION IN DETAIL AREA I AND IV TO DEPTH OF .002 IAW STEPS 1-4 OF BOMBARDIER REO 601R-57-21-030. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,404 hrs · 11,009 cycles

FS 280.0 FLOOR SUPPORT ANGLE PN 600-34017-595 CRACKED APPROX .2 INCHES LONG ON AFT SIDE FS 280.0 OB OF RBL 9.0. (K) [SUP 05-17-07] MAINTENANCE DAMAGED SECTION DRILLED NEW SECTION OF ANGLE AND SPLICES IAW BOMBARDIER REO 601R-53-11-136. (M)

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,404 hrs · 11,009 cycles

FS 280.0 FLOOR SUPPORT CLIPS PN 601R3113-58 CRACKED APPROX .1 INCH LONG AT IB AND OB SIDE RBL 9.0. (K) [SUP 05-17-07] MAINTENANCE REPLACED INBOARD AND OUTBOARD CLIPS AT FS 280 RBL9 IAW CRJ SRM 51-40-11, 52-42-06 AND 51-42-21. (M)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 12,404 hrs · 11,009 cycles

RT WING PLANK ACCESS HOLE AT FUEL PANEL 650CB HAS MINOR CORROSION AROUND APPROX 90 PERCENT OF BONDING AREA. (K) [SUP 06-05-07] MAINTENANCE SANDED CORRODED AREA TO REMOVE DAMAGE MAX BLEND .004 IAW BSC EO NR 601R-57-11217. (M)

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 12,404 hrs · 11,009 cycles

HYDRAULIC LINE SUPPORT BRACKET (ASSY PN 601R75262-153) JUST FWD OF TRANSDUCER IN CEILING OF RT MLG WHEEL WELL CRACKED APROX .1 INCH LONG. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-153 IAW CRJ SRM 51-42-06. (M)

Part: BRACKET — CRACKED (RT MLG WW) · airframe 12,404 hrs · 11,009 cycles

HYDRAULIC TRANSDUCER BRACKET PN 601R75262-157 CRACKED APPROX .1 INCH LONG IN CEILING OF RT MLG WHEEL WELL. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-157 IAW CRJ SRM 51-42-06. (M)

Part: CHANNEL — CRACKED (LT MLG WW) · airframe 12,404 hrs · 11,009 cycles

HYDRAULIC TRANSDUCER HOT CHANNEL PN 601R75262-159 CRACKED APPROX .1 INCH LONG IN CEILING OF LT MLG WHEEL WELL. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET P/N 601R75262-159 IAW CRJ SRM 51-42-06. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,404 hrs · 11,009 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED AT PAX DOOR ASST PULLEY BRACKET. (K) [SUP 06-05-07] CUTOUT DAMAGED SECTION AND REPAIRED IAW BOMBARDIER REO 601R-52-11-513 REV A AND BSC EO 601R-52-11280. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,404 hrs · 11,009 cycles

LT FS 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCHES LONG IN AFT RADIUS. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE ANGLE P/N 601-35012-51 IAW CRJ SRM 51-42-21 AND BSC EO 601R-53-11218. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,404 hrs · 11,009 cycles

RT FS 625.00 OBLIQUE ANGLE IS CRACKED 1.5 INCH LONG IN AFT RADIUS. (K) [SUP 06-05-07] MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE NEW SERVICEABLE ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-21 AND BSC EO 601R-53-11207. (M)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT)

OUTER PASSENGER DOOR HANDLE MESSAGE ON DEPARTURE OUT OF DCA. COMPLIED WITH QRH FLIGHT ATTENDANT SAID THERE WAS UNLOCK INDICATION ON DOOR, DIVERTED TO IAD. TROUBLESHOOT IAW FIM 52-70-00. NO DEFECTS NOTED. OPS CHECK GOOD IAW CRJ AMM 52-11-00, NO DEFECTS NOTED. (M)

Part: CARBON SEAL — DEFECTIVE (ENGINE) · airframe 10,056 hrs · 8,725 cycles

RT OIL PRESSURE DROPPED BELOW 25 PSI ON CLIMB-OUT AND CONTINUED TO CYCLE BETWEEN 25-35 PSI (AIR RETURN). NO INFLIGHT ENGINE SHUTDOWN. FOUND EDP NR 2 AGB CARBON SEAL LEAKING, REMOVED AND REPLACED HYD PUMP NR 2 AGB CARBON SEAL IAW AMM, COMPLIED WITH OIL CONSUMPTION RUNS IAW AMM, LEAK CHECKS GOOD. (K)

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS)

L-PACK HIGH PRESS WHINE, XFERRED TO ENGINE BLEED. WHEN DUCT PRESS 60 PSI OR GREATER. REMOVED AND REPLACED L-PRSOV IAW AMM 2-151-43. FUNCTIONAL TEST OF PRSOV GOOD IAW AMM 21-51-43. (M)

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 7,499 hrs · 6,388 cycles

2 SCRATCHES IN FUSELAGE AT CARGO DOOR CUT-OUT, (APPROX 1 INCH LONG AND .5 INCH LONG.) PERFORMED A MAJOR REPAIR AT FS 549, STR 14-16 IAW EO. (K)

Part: BUSHING — MIGRATED (RT MLG) · airframe 7,499 hrs · 6,388 cycles

RT MLG AFT TRUNNION BUSHING IS MIGRATED 0.15 INCH. REMOVED BUSHING, REAMED BARE AND INSTALLED 1ST OVERSIZE BUSHING IAW MFG REO. (K)

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 7,499 hrs · 6,388 cycles

RT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 50.54 AND WS 66.2 HAS MINOR FRETTING AND FAYING SURFACE LESS THAT .006 INCH DEEP. (K) BLEED MINOR FRETTING ON RT LOWER WING PLANK BETWEEN WS 50-54 AND 66.2 IAW REO. (K)

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 7,499 hrs · 6,388 cycles

LT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 0.00 AND WS 29.42 HAS MINOR FRETTING ON FAYING SURFACE LESS THAN .006 INCH DEEP. C/A PENDING (K)

Part: FLOOR SUPPORT — CRACKED (RT SIDE) · airframe 7,499 hrs · 6,388 cycles

FLOOR SUPPORT ANGLE AT FS 621 RT SIDE IS CRACKED 1 INCH. PERFORMED REPAIR TO RT FS621, FLOOR SUPPORT ANGLE IAW REO. (K)

Part: RIB — CRACKED (RT WING WW)

RIGHT MLG WHEEL WELL AT WS 48.3O FS 523.8 BATTERY RIB IS CRACKED APPROX 1 INCH. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW BOMBARDIER INC REO 601R-57-57-046 REV B. (M)

Part: RIB — CRACKED (LT WING) · airframe 7,496 hrs · 6,388 cycles

LT MLG WHEEL WELL AT WS 48.30 FS 523.8 BATT RIB IS CRACKED APPROX 1 INCH.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 7,499 hrs · 6,388 cycles

FOUND FS 280, FRAME RBL 9, ATTACHMENT ANGLE TO BE CRACKED APPROX 1 INCH LENGTH.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 7,499 hrs · 6,388 cycles

FLOORBEAM ANGLE AT FS 621 LT SIDE IS CRACKED 1 INCH. PERFORMED REPAIR TO RT FS 621 FLOORBEAM ANGLE IAW BOMBARDIER REO 601R-53-117 REV C. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,499 hrs · 6,388 cycles

RT SIDE FS 621-FS 625.3 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .60 INCH. INSTALLED NEW RT INTERCOSTAL AT FS 621-625.3, STR 14R IAW BRAS EO 601R-53-6157. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,499 hrs · 6,388 cycles

LT SIDE FS621-FS625.3 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS, APPROX .70 INCH. INSTALLED NEW LT INTERCOSTAL AT FS 621-625.3, STR 14L IAW BRAS EO 601R-53-6157. (K)

Part: APU — SEIZED (APU BAY) · airframe 7,229 hrs · 6,154 cycles

APU FAILED, REQUESTED INSPECTION. COMPLIED WITH APU INSPECTION FOUND APU TO BE SEIZED. APU INLET EXHAUST NO DEFECTS NOTED. ALSO SUSPECT BAD FCU. COMPLIED WITH ACTION PLACARD PLACED ON MEL. MAINTENANCE VERIFIED APU SEIZED. REMOVED AND REPLACED APU ASSEMBLY. (K)

Part: ACM — ODOR (LEFT)

SMOKE IN CABIN ASSOCIATED WITH APU BLEED AIR HAZE IN COCKPIT AND CABIN. REMOVED AND REPLACED LEFT AIR CYCLE MACHINE, COMPLIED WITH OPS CHECK IAW CRJ AMM 21-51-10, NO SMOKE SMELL NOTED. (M)

Part: BEAM — DAMAGED (RT WING)

RT WING FLAP HINGE BEAM AT WS 178 FORWARD EDGE AND LOWER SURFACE HAS MUSHROOMED METAL AND GOUGES. BLENDED AREAS SMOOTH, PERFORMED EDDY CURRENT INSPECTION OF AREAS, PERFORMED ROTO/FLAP PEEN OF REPAIR AREAS AND RESTORED FINISH TO ORIGINAL CONFIGURATION IAW WVAC EO 601R-57-4318 B. (M)

Part: SKIN — GOUGED (RT WING)

RIGHT WING UNDERSIDE SKIN HAD NUMEROUS SCRATCHES AND GOUGES OUTBOARD OF WS 178 BETWEEN X163-X199. BLENDED AND SMOOTHED OUT DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION OF AREAS, ALODINED PRIMED AND TOP COATED ALL BARE METAL IAW WVAC EO 601R-57-4317. (M)

Part: FITTING — DAMAGED (TE FLAP)

RIGHT WING FLAP HINGE FITTING ASSEMBLY AT WS 178, P/N 601R10088-8 LOWER SURFACE FORWARD EDGE HAS MUSHROOMED METAL AND GOUGES. BLENDED AREAS SMOOTH, PERFORMED EDDY CURRENT INSPECTION OF AREAS, PERFORMED ROTO/FLAP PEEN OF REPAIR AREAS AND RESTORED ORIGINAL FINISH IAW WVAC EO 601R-57-4318 B. (M)

Part: MOTOR — INOPERATIVE (STB TRIM CHANNEL)

STAB TRIM CHANNEL 1 INOPERATIVE REMOVED AND REPLACED MOTOR CONTROL UNIT IAW MM 27-42-05. OPS CHECK GOOD. SHOP REPORT REMARKS, COMPLAINT VERIFIED, REMOVED AND REPLACED DEFECTIVE RESISTOR, INTEGRATED CIRCUIT, DIODE AND CRACKED INDUCTOR. INSPECTED UNIT IAW CMM 27-43-05 REV 01. (M)

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE)

EXPERIENCED RAPID DECOMPRESSION AT FL310, COMMENCED EMERGENCY DESCENT, WERE UNABLE TO REGAIN CONTROL OF PRESSURIZATION IN MANUAL MODE, DROPPED ALL PASSENGER OXYGEN MASKS. DEPLETED OXYGEN SUPPLY, CABIN ALTITUDE RWP. REMOVED AND REPLACED OUTFLOW VALVE. SHOP FINDINGS, FAULT NOT CONFIRMED BUT FAILED VISUAL, REJECTED FOR OVERSPRAY, CONTAMINATED DIAPHRAGM. REPLACED RETAINER, VALVE ASSEMBLY, DIAPHRAGM ASSY, FILTER AND GASKET. (M)

Part: WIRE — LOOSE (CABIN)

CABIN EMERGENCY LIGHTS ARE COMING ON FROM CLIMB-OUT TO CRUISE. INSPECTED AC CONTACTOR BOXES. SECURED LOOSE WIRES ON LINE CONTACTOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ACTT: 10,995:18. ACTC: 12,688. (X)