N979EV

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND WINDSCREEN EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED & REPLACED THE EMERGENCY EXIT SIGN IAW ESPM 20-16-00. OPS TESTED IAW AMM 33-51-00-710-801. CHECKED GOOD.

Part: STRUCTURE — CRACKED (BS 187) · airframe 26,576 hrs · 25,147 cycles

CRACK DISCOVERED AT BS 187 NEAR STRINGER 15L. REMOVED THE DOOR LAND FOR PANEL 211AL, FABRICATED AND INSTALLED A NEW DOOR LAND IAW SRM 51-42-06-00, DRAWING #600-33052, SRM 51-40-06-00, 51-40-11-00, 51-42-13, EC/TC REO 601R-53-11-2981 AND REO 601R-53-11-2981. ALL DEFECTS CORRECTED.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND A CRACKED INTERCOSTAL AFT SIDE OF BS 621 BULKHEAD, STRINGER 13L.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND A CRACKED INTERCOSTAL AT AFT SIDE OF THE BS 621 BULKHEAD, STRINGER 14L. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21, & 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

FS280 ANGLE CRACKED. REMOVED CRACKED CLIP. FABRICATED AND INSTALLED NEW CLIP. ALL WORK PERFORMED IAW REO 601R-53-11-2982 AND EC/TC REO 601R-53-11-2982.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

FS280 ANGLE CRACKED. REMOVED CRACKED CLIP. FABRICATED AND INSTALLED NEW CLIP. ALL WORK PERFORMED IAW REO 601R-53-11-2982 AND EC/TC REO 601R-53-11-2982.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED DAMAGED SECTION OF PAX DOOR AFT DRAG ANGLE, PERFORMED NDT INSP OF REWORKED AREA AND CUT LINES. FABRICATED NEW DRAG ANGLE SECTION. INSTALLED NEW AFT DRAG ANGLE PART INTO PREVIOUSLY REMOVED SECTION. ALL IAW REO 601R-52-11-513 AND ECTC REO 601R-52-11-513

Part: ANGLE — CRACKED (BS 484) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND ANGLES BETWEEN RBL 27 & 45 AT BS 484.00 CRACKED. REMOVED , FABRICATED, AND INSTALLED NEW ANGLES. IAW REO 601R-53-41-2125 AND ECTC REO 601R-53-41-2125.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

ANGLES BETWEEN RBL27 AND RBL45 AT CROSSBEAM 484.00 ARE CRACKED. REMOVED 2EA CRACKED CLIPS RBL27 & RBL45 FS484.00 CROSSBEAM. FABRICATED AND INSTALLED SERVICEABLE 2EA CLIPS RBL27 & RBL45 FS484.00 CROSSBEAM. ALL WORK PERFORMED IAW REO 601R-53-41-2125 AND EC/TC REO 601R-53-41-2125.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 26,576 hrs · 25,147 cycles

LEFT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACL IAW REO 601R-53-00-650, EC/TC REO 601R-53-00-650, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 26,576 hrs · 25,147 cycles

RIGHT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 601R-53-00-650, EC/TC REO 601R-53-00-650, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 26,576 hrs · 25,147 cycles

LEFT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 601R-53-00-650, EC/TC REO 601R-53-00-650 AND AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 26,576 hrs · 25,147 cycles

FLOOR SUPPORT BS 310 & 319 IS CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06 AND 51-40-11.

Part: PLATE — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING RETURN TO SERVICE INSPECTIONS FOUND FLOOR SILL PLATE CORRODED BETWEEN FS310.00-319.00. REMOVED UNSERVICEABLE CAP PLATE IAW SRM 51-42-06. DRILLED AND INSTALLED NEW SERVICEABLE PLATE IAW SRM 51-42-06 & 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 26,756 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS, FOUND THE FLOOR SUPPORT CORRODED BS 574 - 621, LBL 27. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06,51-42-21, & 51-40-11. C/W EC/TC REO 601R-53-61-3778 & GREO 601R-53-61-3778 REV A.

Part: PLATE — CORRODED (BS 295-310) · airframe 26,576 hrs · 25,147 cycles

CAP PLATE ON SUPPORT BOX BETWEEN BS 310 AND 295 HAS CORROSION DAMAGE. REMOVED AND REPLACED THE CAP PLATE IAW SRM 51-42-13 AND 51-40-11-00.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND FLOOR SUPPORT CORRODED AROUND SCREW HOLES BETWEEN BS 574 - 621. REMOVED CORROSION IAW SRM 51-42-06, 51-42-21, & 51-40-11. FOUND DAMAGE TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21, & 51-40-11.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 26,576 hrs · 25,147 cycles

BS 589 FLOORBEAM TOP CAP CORRODED BETWEEN RBL 27 & 46. REMOVED AND REPLACED THE TOP CAP IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 409-558) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND SET TRACK LBL 9 CORRODED BETWEEN BS 49+128 - 558. REPAIRED SEAT TRACK IAW EC/TC REO 601R-53-00-530 & GREO 601R-53-00-485 REV B.

Part: SEAT TRACK — CORRODED (BS 409-558) · airframe 25,576 hrs · 25,147 cycles

DURING C CHECK, FOUND SEAT TRACK RB L9 CORRODED BETWEEN BS 409+128 - 558. REPAIRED THE SEAT TRACK IAW EC/TC REO 601R-53-00-530 & GREO 601R-53-00-485 REV B.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,756 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS FOUND SEAT TRACK CORRODED BS 559+84 - 559+92 LBL 9. FABRICATED A NEW SEAT TRACK IAW REO 601R-53-00-485 REV B AND EC/TC REO 601R-53-00-485. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000/-400-802.

Part: SEAT TRACK — CORRODED (BS 559-589) · airframe 26,756 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS, FOUND SEAT TRACK CORRODED BS 559+112 - 589, RBL9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000/-400-802.

Part: SEAT TRACK — CORRODED (BS 559-589) · airframe 26,756 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS FOUND SEAT TRACK CORRODED BS 559+112 - 589, LBL 9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000/-400-802 AFTER FABRICATING NEW ONE IAW REO 601R-53-00-485 REV B AND EC/TC REO 601R-53-00-485

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS FOUND SEAT TRACK CORRODED BEYOND LIMITS AT FS558-559+80 RBL9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000/-400-802 AFTER FABRICATING A NEW TRACK IAW REO 601R-53-00-485 REV B & EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,756 hrs · 25,147 cycles

SEAT TRACK IAW 53-01-11-000/-400-802 AFTER FABRICATING A NEW ONE IAW REO 601R-53-00-485 REV B AND EC/TC 601R-53-00-485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS FOUND SEAT TRACK CORRODED BEYOND LIMITS AT FS558-559+80 LBL9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000/-400-802 AFTER FABRICATING A NEW TRACK IAW REO 601R-53-00-485 REV B & EC/TC REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS FOUND SEAT TRACK CORRODED AT FS394-409+128 RBL9. REMOVED AND REPLACED SHORT SEAT TRACK AT RBL9 IAW AMM 53-01-11-000/-400-802 AFTER FABRICATING A NEW ONE IAW REO 601R-53-00-485 REV B & EC/TC REO 601R-53-00-485.

Part: PLATE — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS FOUND CAP PLATE ON SUPPORT BOX CORRODED BETWEEN FS310.00 & 295.00. REMOVED UNSERVICEABLE CAP PLATE IAW SRM 51-42-13 & 51-23-00. DRILLED AND INSTALLED NEW CAP PLATE IAW SRM 51-40-11-00 & 51-42-13.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,756 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS FOUND SEAT TRACK CORRODED BS 559+80 - 559+96, LBL 27. FABRICATED A NEW SEAT TRACK IAW REO 601R-53-00-485 REV B AND EC/TC REO 601R-53-00-485. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000/-400-802.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK FOUND LT FLOOR SILL CORRODED BETWEEN FS 409+80 & 409+128. REPAIRED BY C/W EC/TC REO601R-53-00-530

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK FOUND SEAT TRACK AT LBL9 CORRODED BETWEEN FS394.00 & 409+128. R & R SEAT TRACK IAW EC/TC REO 601R-53-00-485.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK FOUND CLIP ON SERVICE DOOR SILL ANGLE AND CROSSBEAM 349.00 HAS CORROSION DAMAGE. R & R WITH SERVICEABLE CLIP IAW SRM 51-42-21.

Part: DOOR SILL — CORRODED · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND THE ASD LOWER SILL CORRODED. BLENDED CORRODED AREA FROM .100 TO .83 REMAINING. COMPLIED EA 45-2016-360 AND ECTC EA 45-2016-360.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK FOUND SERVICE DOOR SILL ANGLE CORRODED BETWEEN FS333-349. R & R ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK FOUND SEAT TRACK AT RBL9 CORRODED BETWEEN FS364-409. R & R SEAT TRACK IAW CE/TC REO 601R-53-00-485.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND CORROSION DAMAGE ALONG THE PAX DOOR LOWER SILL ANGLE. REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE PER SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK FOUND SEAT TRACK AT LBL9 CORRODED BETWEEN FS354-409. R & R SEAT TRACK BY C/W EC/TC REO 601R-53-00-485.

Part: FRAME — CORRODED (BS 349) · airframe 26,576 hrs · 25,147 cycles

DURING C CHECK, FOUND FRAME BS 349 CORRODED BETWEEN STRINGERS 26 & 27L. BLENDED CORRODED AREA AND REMAINING THICKNESS FOUND TO BE OUT OF SRM LIMITS. COMPLIED WITH EA 45-2016-183 AND ECTC EA 45-2016-183.

Part: TRUNNION — WORN (LT MLG) · airframe 26,576 hrs · 25,147 cycles

DURING RETURN TO SERVICE CHECKS, LT AFT MLG BUSHING BORE REQUIRES OVERSIZE. (THIS IS A MAJOR REPAIR) LINE BORED HOLE, NDT. INSTALLED NEW OVERSIZED BUSHING AND REAMED IAW GREO 601R-57-21-003 REV B AND EC/TC REO 601R-57-21-003.

Part: TRUNNION — WORN (RT MLG) · airframe 26,576 hrs · 25,147 cycles

DURING RETURN TO SERVICE INSPECTIONS, RT AFT MLG BUSHING BORE REQUIRES OVERSIZE. THIS IS A MAJOR REPAIR, LINE BORED THE BUSHING HOLE. NDT. INSTALLED NEW OVERSIZED BUSHING AND REAMED IAW GREO 601R-57-21-003 REV B AND EC/TC REO 601R-57-21-003.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,182 hrs · 24,716 cycles

RT SIDEWALL EXIT SIGN FWD OF EMERGENCY EXIT INOPERATIVE. R & R INVERTER IAW AMM 33-51-07, OPS CK GOOD.

Part: SEAT TRACK — DAMAGED (BS 250-280) · airframe 25,216 hrs · 23,687 cycles

PUNCTURE DAMAGE TO COCKPIT FLOOR BETWEEN PILOT SEAT TRACK, LBL 12.0-LBL 26.00 AND BETWEEN FS 250-FS 280. PUNCTURE IS LOCATED BETWEEN PILOT SEAT TRACK, LBL 12.0-LBL 26.00 AND BETWEEN FS 250-FS 280. MEASURES APPROXIMATELY 1" X 1" SUBMITTED DAMAGE REPORT TO ENGINEERING IAW SRM 51-13-01. RECEIVED PRELIMINARY EA 20-2015-067. TRIMMED DAMAGED AREA OF FLOOR PANEL MAINTAINING 0.5" TRIM RADIUS IAW PRELIMINARY EA 20-2015-067. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3. RII COMPLIED WITH SATISFACTORY IAW GMM 3-3. FABRICATED REPAIR DOUBLER, DRILLED UP EXISTING HOLES AND NEW HOLES UP TO FINAL SIZE IN DOUBLER, TRIMMED TO SIZE, DEBURRED AND APPLIED A023 FINISH IAW STS EA PRELIMINARY 20-2015-067. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3. RII COMPLIED WITH SATISFACTORY IAW GMM 3-3. INSTALLED REPAIR DOUBLER ON COCKPIT FLOOR BETWEEN PILOT SEAT TRACK LBL 12.0 AND LBL 26.0, BETWEEN FS 250 AND FS 280 AND COMPLIED WITH ALL STEPS IAW STS FINAL EA 20-2015-067 AND CREATED 318 IAW SOP 5702. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 24,876 hrs · 23,364 cycles

GALLEY AND WARDROBE EMERGENCY LIGHT INOPERATIVE. R & R FUSE ON BATTERY CHARGER IAW CMM 33-21-70. ACFT EMERGENCY LIGHTS OPS CHECKS GOOD IAW AMM 33-51-00.

Part: BULKHEAD — CRACKED (BS 621) · airframe 24,874 hrs · 23,363 cycles

DURING INSPECTION FOUND A CRACK INDICATION ON THE AFT PRESSURE BULKHEAD AT LBL 27.50 AND WL 130.0 AT THE TOP OF THE DOOR TRACK.

Part: PLACARD — OUT OF POSITION (CABIN) · airframe 22,802 hrs · 21,329 cycles

PHOTOLUMINESCENT CHEVRON MARKERS ROW 8 THRU 14 INCORRECTLY PLACED. REPLACED CHEVRON MARKERS AT ROW 8 TO 14 IAW AMM 33-51-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 22,037 hrs · 20,517 cycles

NR 1 CABIN CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-16, CHECKED GOOD.

Part: FITTING — MISINSTALLED (CARGO DOOR) · airframe 21,877 hrs · 20,343 cycles

(AFT CARGO DOOR HAS MISDRILLED HOLES ON NEW DOOR HANDLE. LOCATED & DRILLED NEW SERVICEABLE FITTING IAW DWG 601R35027. INSTALLED NEW SERVICEABLE DOOR HANDLE HOUSING FITTING ASSY AT CARGO DOOR IAW SRM 51-42-21. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (BS 400-409) · airframe 21,877 hrs · 20,343 cycles

DURING SEAT REMOVAL PROCESS FOUND SEAT TRACK, RBL 9.0 CORRODED AT FS 400-409+128. REPAIRED IAW SRM 51-41-02, 51-24-36, 51-40-11 & GREO 601R-53-00-485. MAJOR REPAIR.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 21,877 hrs · 20,343 cycles

FOUR RT OTBD LOWER ISOLATORS ON AFT PRESSURE BULKHEAD BROKEN. R & R 4 RT OTBD LOWER ISOLATORS ON AFT PRESSURE BULKHEAD IAW SRM 51-42-06 AND 51-42-13.

Part: DOUBLER — CRACKED (DOOR) · airframe 21,877 hrs · 20,343 cycles

ASD FRAME DOUBLER CRACKED AT AFT PULL IN LEVER. R & R ASD FRAME DOUBLER AT AFT PULL IN LEVER IAW SRM 51-42-06-001-001 & 51-42-13-001-001, 51-42-21-001-001.

Part: STIFFENER — GOUGED (FUSELAGE) · airframe 21,877 hrs · 20,343 cycles

ASD PRESSURE RELIEF DOOR STIFFENER GOUGED. REPAIRED IAW REO 601R-52-11-1040.

Part: GLOWSTRIP — DAMAGED · airframe 21,877 hrs · 20,343 cycles

SPARE CHEVRON MARKER DAMAGED LOCATED IN GALLEY 1. REPLACED SPARE CHEVRON MARKER WITH NEW MARKERS IAW EO 600-33-0015LC.

Part: PANEL — DENTED (RT WING) · airframe 21,886 hrs · 20,351 cycles

RT WING L/E DENTED. REMOVED R/T OTBD L/E ASSY IAW AMM 57-41-01-000-806 AND ACCESS PANEL 630BL IAW TASK 57-41-01-000-808. INSTALLED OTBD L/E ASSY QC 44 (630KL) IAW AMM 57-41-01-400-806. RECEIVED SERVICEABLE LEADING EDGE PN 601R12062-4 LOCATED AND TRANSFERED DRILL THE MOUNTING HOLES AS NEEDED REF: SRM 51-40-06-00 AND SRM 51-40-11-00 AND DWG 601R12062. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 21,886 hrs · 20,351 cycles

CARGO DOOR HANDLE HOUSING ASSY HAS MULTIPLE CRACKS. LOCATED & DRILLED SECOND NEW SERVICEABLE FITTING IAW DWG 601R35027. INSTALLED NEW SERVICEABLE DOOR HANDLE HOUSING FITTING ASSY AT CARGO DOOR IAW SRM 51-42-21. REPAIR CLASSIFIED AS MAJOR.

Part: ATTACH FITTING — CRACKED (BS 625 BULKHEAD) · airframe 21,385 hrs · 19,845 cycles

ATTACH FITTING CRACKED ON AFT PRESSURE BULKHEAD, FS 625, STRINGER 12L. REMOVED, FABRICATED AND REPLACED IAW SRM 51-41-21AND IAW EC/TC 601R-53-61-100 AND IAW REO 601R-53-61-422.

Part: ATTACH FITTING — CRACKED (BS 625 BULKHEAD) · airframe 21,385 hrs · 19,845 cycles

ATTACH FITTING CRACKED ON AFT PRESSURE BULKHEAD, FS 625, STRINGER 12R. R & R IAW SRM 51-41-21AND IAW EC/TC 601R-53-61-100 AND IAW REO 601R-53-61-422.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 21,385 hrs · 19,845 cycles

FOUND INTERGRANULAR CORROSION ON RT SEAT TRACK BETWEEN STATIONS FS 409+128-559. REMOVED SEAT TRACK IAW AMM 53-01-11. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,419 hrs · 18,851 cycles

NR 5 AND NR 6 FUSELAGE EXTERIOR EMERGENCY LIGHTS INOPERATIVE. LAMPED EXTERIOR EMERGENCY LIGHTS IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 19,588 hrs · 17,954 cycles

FLAPS FAILED AT ZERO ENROUTE, ACFT DIVERTED, EMERGENCY DECLARED. COMPLIED WITH FLAP FAIL AD 2009-06-12.

Part: CIRCUIT BREAKER — TRIPPED (TE FLAPS) · airframe 19,342 hrs · 17,672 cycles

DESCENDING THROUGH 12,000 AT 190 KTS, SELECTED FLAPS TO 8 AND RECEIVED A "FLAPS FAIL" CAUTION MESSAGE. FLAPS FAILED AT 0. EMERGENCY DECLARED. RESET CIRCUIT BREAKERS PANEL 1 F-4 & PANEL 2 F-4. OPERATED FLAPS UP & DOWN SEVERAL TIMES. OPS CHECKED GOOD IAW AMM 27-50-00. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,034 hrs · 17,338 cycles

LEFT NR 3 EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,764 hrs · 17,052 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CEILING EMERGENCY LIGHT IAW AMM 33-51-19.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 18,651 hrs · 16,942 cycles

ON LANDING, GEAR HANDLE DOWN RECEIVED A GEAR DISAGREE WARNING MESSAGE. BOTH MAIN GEAR REMAINED UP. EMERGENCY DECLARED. R & R MLG SELECTOR VALVE , IAW AMM 32-32-10, OPS CHECKED IS GOOD, LEAK CHECKED IS GOOD, ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,330 hrs · 16,593 cycles

FORWARD MOST CABIN CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED GOOD IAW AMM 33-51-00.

Part: FLASHLIGHT — INOPERATIVE · airframe 18,224 hrs · 16,475 cycles

CPT FLASHLIGHT INOPERATIVE. R & R COCKPIT FLASHLIGHT AMM 25-61-00, OPS CHECKED GOOD.

Part: UPLOCK BRACKET — DAMAGED (NLG) · airframe 17,424 hrs · 15,616 cycles

AFTER GEAR RETRACTION IT TOOK AT LEAST 2 MINS FOR NOSE TIRES TO STOP ROTATING WITH VIBRATION. ON LANDING NOSE GEAR DID NOT COME DOWN. GEAR DISAGREE MSG, FOLLOWED QRH AND MANUALLY LOWERED NOSE GEAR. (EMERGENCY DECLARED) R & R NLG UPLOCK LATCH BRACKET IAW CMM 32-20-04. OPS CHECK GOOD AND RETORQUED NOSE TIRES IAW AMM 32-42-01. (CLOSED)

Part: PRIORITY VALVE — FAILED (NLG) · airframe 17,424 hrs · 15,616 cycles

NOSE GEAR DISAGREE WARNING ON LANDING COMPLIED WITH QRH AND MANUALLY EXTENDED THE NOSE GEAR. NOSE GEAR DOWN AND LOCKED FROM MANUAL EXTENSION. (ENROUTE, ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED & VEHICLES STANDING BY. R & R NLG PRIORITY VALVE, OPS CHECK AND LEAK CHECK GOOD IAW AMM 32-33-15.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,065 hrs · 15,190 cycles

LEFT EXTERIOR NR 3 EMERGENCY LIGHT INOP. RELAMPED LT WING NR 3 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED LT WING NR3 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,873 hrs · 14,979 cycles

CARGO SEAT TRACK AT FS 559+96 AT RBL 29 IS CORRODED. RESOLVED ON W/O: 181096 TASKCARD: N/R-00226. CARGO SEAT TRACK AT FS 559+96 AT RBL 09 REMOVED AND REPLACED IAW SRM 51-41-04. THIS REPAIR IS CLASSIFIED ASA MINOR REPAIR IAW ASA SOP 5702.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,873 hrs · 14,979 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL FITTING HAS INDICATION NOTED APPROX .4 INCH IN LENGTH 90 PERCENT FSH. FAILED NDT INSPECTION. RESOLVED ON W/O: 181098 TASKCARD: N/R-00441. REPAIRED PRESSURE BULKHEAD WEB AT FS 621.00 LINTEL LOCATION IAW REO 601R-53-61-1230 REV.D STEPS 1-24. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR COMPLIES WITH THE REQUIREMENTS OF EC/TC AND BOMBARDIER REO 601R-53-61-1230 REV.D. ASA RII COMPLIED WITH: 5300083 RII FOUND TO BE SATISFACTORY: 5300083.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 16,873 hrs · 14,979 cycles

FLOORBEAM ANGLE AT FS 280 RBL 9 IS CRACKED. R & R ANGLE FLOORBEAM IAW SRM 51-40-06 AND 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (CARGO BAY) · airframe 16,873 hrs · 14,979 cycles

CARGO SEAT TRACK AT FS 621 AT LBL 9 IS CORRODED. RESOLVED ON W/O: 181096 TASKCARD: N/R-00227. CARGO SEAT TRACK AT FS 621AT LBL 9 REMOVED AND REPLACED IAW SRM 51-41-04. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: ISOLATOR — CRACKED (FUSELAGE) · airframe 16,873 hrs · 14,979 cycles

FOUND REAR PRESSURE BULKHEAD HAS 2 ISOLATORS CRACKED AT LBL 9.5 AND RBL 9.5 WL 100. RESOLVED ON W/O: 181098 TASKCARD: N/R-00444 ). REMOVED AND REPLACED 2 ISOLATOR SL2337-3 AT LBL 9.5 AND RBL 9.5 WL 100 IAW CRJ 200 SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,873 hrs · 14,979 cycles

CARGO SEAT TRACK AT FS 559+96 AT LBL 9 IS CORRODED. RESOLVED ON W/O: 181096 TASKCARD: N/R-00225. CARGO SEAT TRACK AT FS 559+96 AT LBL 9 REMOVED AND REPLACED IAW SRM 51-41-04. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: BEAM — CRACKED (FUSELAGE) · airframe 16,873 hrs · 14,979 cycles

FS 280 TRANSVERSE BEAM IS CRACKED 1 INCH IN LOWER RADIUS AT OTBD SIDE OF LBL 9. DAMAGE FOUND TO BE WITHIN LIMITS TO REPAIR IAW REO 601R-53-11-171. CUT OUT DAMAGE IAW STEP 1 OF REO 601R-53-11-171.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 16,873 hrs · 14,979 cycles

FOUND FS 559 LT CAP ANGLE HAS INDICATION NOTED APPROX .3 INCH IN LENGTH 60 PERCENT FSH AT LBL 18.0 AND FOUND RT FS 559 BULKHEAD WEB HAS INDICATION NOTED APPROX .2 INCH IN LENGTH 50 PERCENT FSH AT WL 54.10 O/B OF RBL 9.0. BOTH FAILED NDT INSPECTION. REPAIRED FS 559 PRESSURE BULKHEAD WEB AND CAP ANGLES IAW REO 601R-53-41-260 REV E, STEPS 1-14.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 16,873 hrs · 14,979 cycles

CARGO TRACK AT FS 559+80 AT RBL 9 IS CORRODED. CARGO TRACK REMOVED AND REPLACED IAW SRM 51-41-04. FITTINGS FOUND CORRODED AND CRACKED. REPLACE FITTING. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,873 hrs · 14,979 cycles

CARGO SEAT TRACK AT FS 559+80 AT RBL 27 IS CORRODED. CARGO SEAT TRACK AT FS 559+80 AT RBL 27 R & R IAW SRM 51-41-04. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: PLACARD — DETERIORATED (CABIN) · airframe 16,873 hrs · 14,979 cycles

PAX DOOR PLACARDS DETERIORATED: UP ARROW, "OPEN", "EXIT". REMOVED AND REPLACED THE PAX DOOR PLACARDS UP ARROW, OPEN AND THE EXIT PLACARDS IAW MM 11-30-00-400-801.

Part: STRUT — OUT OF ADJUST (PAX DOOR) · airframe 16,873 hrs · 14,979 cycles

PASSENGER DOOR FAILED FUNCTIONAL TEST. ADJUSTED PAX DOOR FWD GAS STRUT LENGTH IAW AMM 52-11-17-820-802. DOOR NOW OPENS WITH LIGHT PUSH. REPERFORMED FUNCTIONAL TEST OF DOOR IAW AMM 52-11-00-720-802, FUNCTIONAL TESTED GOOD.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 16,873 hrs · 14,979 cycles

CARGO TRACK AT FS 559+80 AT LBL 9 IS CORRODED. CARGO TRACK REMOVED AND REPLACED IAW SRM 51-41-04. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SKIN — CORRODED (BS 574) · airframe 16,873 hrs · 14,979 cycles

RT AFT FUSELAGE EXTERNAL SKIN HAS MINOR SURFACE CORROSION AT FS 574 BETWEEN STRINGERS 24R AND 25R. REMOVED MINOR SURFACE CORROSION IAW SRM 51-21-06. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 16,873 hrs · 14,979 cycles

CARGO TRACK AT FS 559+80 AT LBL 27 IS CORRODED. CARGO TRACK REMOVED AND REPLACED IAW SRM 51-41-04. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: STRUCTURE — DENTED (PAX DOOR) · airframe 16,873 hrs · 14,979 cycles

PASSENGER DOOR INNER LOWER CORNERS ARE DENTED FROM HANDRAILS, RESOLVED ON W/O: 181096 TASKCARD: N/R-00077. REMOVED PAX DOOR LOWER CORNERS AND CLEANED, DRESSED BACK TO ORIGINAL CONTOUR IAW ASA SRM SUPPLEMENT 52-10-31 STEPS C1 AND 2. REQUIRES NDT AND PAINT. COMPLIED WITH ASA SRM SUPPLEMENT 52-10-31 STEP C3. PERFORMED LPI ON PAX DOOR LOWER CORNERS IAW CRJ NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. ASA SRM SUPPLEMENT 52-10-31 STEPS C4-6 REQ'ED. COMPLIED WITH STEPS 4 THROUGH 6 OF STEP C OF ASA SUPPLEMENT 52-10-31. COMPLETED ALL STEPS OF ASA SRM SUPPLEMENT 52-10-31. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: DRAG ANGLE — NONE (PAX DOOR) · airframe 16,873 hrs · 14,979 cycles

POSSIBLE CRACK PAX DOOR BOX AREA INBD OF DRAG ANGLE ON PREVIOUS REPAIR. INSPECTED IAW AMM 52-11-00-210-802 AND SRM 51-11-00. FOUND NO VISUAL CRACKS. PERFORMED LPI ON PAX DOOR UPPER REPAIR ANGLE SUSPECTED AREA IAW NDTM 51-20-10-08. NO INDICATIONS NOTED. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,873 hrs · 14,979 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AFT DRAG ANGLE FROM PAX DOOR AND INSTALLED A NEW DRAG ANGLE ON AFT WEB IAW SRM 51-42-05. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,781 hrs · 14,875 cycles

RT EXTERIOR EMERGENCY LIGHT 2ND FROM THE FRONT IS INOP. RELAMPED RT EXTERIOR EMERGENCY LIGHT 2ND FROM THE FRONT AND OPS CHK GOOD IAW AMM 33-51-21. OPS CK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,781 hrs · 14,875 cycles

LT MOST AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LT MOST AFT EXTERIOR EMERGENCY LIGHT AND OPS CK GOOD IAW AMM 33-51-21.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,698 hrs · 14,789 cycles

RT NR2 EXTERNAL EMERGENCY LIGHT INOP. RELAMPED RT NR2 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. RELAMPED RT NR 2 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD.

Part: SIGN — DISLODGED (PAX DOOR) · airframe 15,457 hrs · 13,357 cycles

EXIT SIGN ON PAX DOOR FELL OFF. INSTALLED EXIT SIGN PLACARD ON PAX DOOR IAW AMM 11-20-00.

Part: FLAP — FAILED (WING) · airframe 15,194 hrs · 13,057 cycles

FLAP FAIL AT 0 DEGREES ON APPROACH FWA, FOLLOWED QRH FOR 0 FLAPS LANDING (EMERGENCY DECLARED).

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,366 hrs · 12,165 cycles

F/A REPORTED CABIN EMERGENCY LIGHT SWITCH WAS LEFT ON, EMERGENCY LIGHTS INOP.

Part: WEB — CRACKED (DOOR) · airframe 13,166 hrs · 10,995 cycles

FOUND CRACK IN INNER SKIN WEB PLATE UNDER OUTER HANDLE DETENT APPROX .25 INCH LONG.

Part: WEB — CRACKED (PAX DOOR) · airframe 13,166 hrs · 10,995 cycles

UPON REMOVAL OF FIXED MID STEP FROM PAX DOOR FOR AFT WEB REPAIR FOUND FWD WEB TO BE CRACKED IN 832CT. FIXED MID STEP INTERSECTION RADIUS. REPAIRED PAX DOOR FWD SKIN WEB AT RADIUS FOR 832CT, FIXED MID STEP INTERSECTION IAW ECTC REO 601R-52-11-702.

Part: SKIN — DAMAGED (LT WING) · airframe 13,166 hrs · 10,995 cycles

LT WING LWR PLANK ACCESS HOLE 540CB HAS EDDY CURRENT INDICATION NOTED 60 PERCENT FULL SCREEN HEIGHT APPROX 0.1 INCH LONG ON LANDING OF I/B SECTION OF RADIUS, NON-CRITICAL AREA APPROX 1 INCH AFT OF CENTER LINE. FAILS NDT INSPECTION. REPAIRED LT WING PLANK ACCESS HOLE 540CB IAW REO 601R-57-21-030.

Part: WEB — CRACKED (PAX DOOR) · airframe 13,166 hrs · 10,995 cycles

UPON REMOVAL OF PAX DOOR STEP 832CT FOR REPLACEMENT OF PAX DOOR OUTER HANDLE, FOUND AFT SKIN WEB CRACKED AT RADIUS FOR STEP 832CT AND FIXED MID STEP INTERSECTION. REPAIRED PAX DOOR AFT SKIN WEB AT RADIUS FOR STEP 832CT AND FIXED MID STEP INTERSECTION IAW ECTC REO 601R-52-11-702.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,166 hrs · 10,995 cycles

FS 280 FLOOR SUPPORT CLIP IS CRACKED O/B OF LBL 9. REMOVED CRACKED CLIP AT FS 280 FLOOR SUPPORT O/B OF LBL 9. INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-06 AND 51-42-21. PREP AND PAINT REQUIRED. PAINTED SUPPORT CLIP IAW SRM 51-25-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,166 hrs · 10,995 cycles

FS 280 FLOOR SUPPORT CHANNEL IS CRACKED O/B OF LBL 9 BESIDE MLG MANUAL RELEASE PULLEY BRACKET. APPROX 1 INCH IN LENGTH. FS 280 FLOOR SUPPORT CHANNEL IS CRACKED O/B OF LBL 9 BESIDE MLG MANUAL RELEASE PULLEY BRACKET. APPROX 1" IN LENGTH. COMPLIED WITH BOMBARDIER REO 601R-53-11-136. REPAIR TO PILOT'S BULKHEAD J-ANGLE AT FS 280 LBL 9, RBL 9. COMPLIED W ITH ASA EO 600-53-91. COMPLIED WITH EC/TC EO 600-53-91. C/W IN ACCORDANCE WITH REO 601R-53-11-16 REV.A.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 13,166 hrs · 10,995 cycles

CARGO DOOR SUPPORT BEAM LWR ANGLE P/N: 601R-35050-109 HAS VISIBLE CRACK EXTENDING APPROX 0.5 INCH FROM FASTENER. REMOVED CARGO DOOR SUPPORT BEAM LWR ANGLE. INSTALLED NEW CARGO DOOR SUPPORT BEAM LOWER ANGLE P/N 601R35050-109 IAW ASA CRJ 200 SRM 51-42-21. LEAK CHECK GOOD AT THIS TIME (DURING PRESSURIZATION) IAW CRJ 200 AMM 21-32-00-863-801.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,166 hrs · 10,995 cycles

LT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621, LBL 40, WL 73. REPAIRED CRACKED LT SIDE FLOOR SUPPORT STRUCTURE AT FS 621, LBL 40, WL 73 IAW REO 601R-53-61-117 REV C. COMPLIED WITH ECTC REO 601R-53-61-117.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,166 hrs · 10,995 cycles

LT/RT FS 625 OBLIQUE ANGLES ARE CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,166 hrs · 10,995 cycles

THE CLIP ON THE INTERCOSTAL AT FS 484 RBL 27 HAS A .250 INCH CRACK IN THE RADIUS AT THE TOP. REMOVED AND REPLACED CLIP ON INTERCOSTAL IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,166 hrs · 10,995 cycles

RT FLOOR SUPPORT IS CRACKED AT FS 621, RBL 40, WL 73. REPAIRED CRACKED RT FLOOR SUPPORT AT FS 621, RBL 40, WL 73 IAW REO 601R-53-61-117 REV C. COMPLIED WITH ECTC REO 601R-53-61-117.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,166 hrs · 10,995 cycles

THE CLIP AT FS 484 LBL 27.00 HAS A .250 INCH CRACK IN THE RADIUS AT THE TOP. REMOVED AND REPLACED CLIP IAW SRM 51-42-21 AND REO 601R-53-41-059, STEP 14. STEPS 1 THRU 13 OF REO 601R-53-059 NOT REQUIRED. COMPLIED WITH EC/TC REO 53-41-059.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,166 hrs · 10,995 cycles

FS 280 FLOOR SUPPORT CHANNEL HAS CRACK IN WEB NEAR LOWER FLANGE O/B OF RBL 9.0. COMPLIED WITH REO 601R-53-11-171, REPAIR TO BULKHEAD AT FS 280 AND RBL 9. COMPLIED WITH EO 600-53-90.

Part: FITTING — CRACKED (FUSELAGE) · airframe 13,166 hrs · 10,995 cycles

FS 280 FLOOR SUPPORT CLIP AT RBL 9.0 O/B IS CRACKED. REMOVED CRACKED CLIP FLOOR SUPPORT AT RBL 9 O/B. FOR RE-INSTALLATION OF CLIP AT FS 280 FLOOR SUPPORT AT RBL 9 O/B, REF MWC JOB 8773721/254.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,164 hrs · 10,994 cycles

CAPT'S, FO'S AND FA FLASHLIGHT BATTERY ARE WEAK.

Part: VALVE — MALFUNCTIONED (NLG DOOR) · airframe 12,368 hrs · 10,278 cycles

DURING GEAR RETRACTION HEARD A CONSISTANT MECHANICAL BANKING UNDER COCKPIT FOR APP 8 SECONDS. NOISE OCCURED APP 2 TIMES/SECOND. FLT 4743 DEL 45 MINS. EMERGENCY DECLARED. REMOVED AND REPLACED NOSE LANDING GEAR ACTUATOR AND DOOR SELECTOR VALVE IAW AMM 32-22-10 AND AMM 32-22-20. OPS CHECK GOOD. OK FOR SERVICE. (B)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,206,823 hrs · 10,008 cycles

FWD AND AFT CEILING EMERG. LIGHT OUT RELAMPED FWD AFT CEILING EMERGENCY LIGHT IAW 33-51-16. (B)

Part: KNOB — OUT OF POSITION (SERVICE DOOR) · airframe 11,998 hrs · 9,942 cycles

SERVICE DOOR KNOB CAME OFF. SECURED SERVICE DOOR KNOB. OK FOR SERVICE. SDR CLOSED.

Part: DOOR — MALFUNCTIONED (MAIN PAX) · airframe 11,164 hrs · 9,259 cycles

PAX DOOR WILL NOT CLOSE.

Part: LENS — MISSING (MISSING) · airframe 10,709 hrs · 8,876 cycles

EMERGENCY EXIT SIGN AT ROW 8 IN CABIN LENS IS MISSING. FLT 4843 DEL 19 MINS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 10,019 hrs · 8,310 cycles

F/A'S FLASHLIGHT INOP.

Part: OIL SYSTEM — FLUCTUATES (LT ENGINE) · airframe 9,731 hrs · 8,077 cycles

AT FL320, RECEIVED LT ENG WARNING MSG, ENG OIL PRESS FLUX BETWEEN 23 - 34 PSI, FOLLOWED QRH, REDUCED ENG POWER TO GROUND IDLE, RELATED TO DEFECT NR 305469-1. EN ROUTE TO GRB, A/C DIVERTED TO ORD DUE TO MTC, EMERGENCY DECLARED, FLT 4404 (X2) CX AND ON 06/06/07 FLT 4265 CX.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 8,260 hrs · 6,935 cycles

FLOORBEAM ATTACH CLIPS AT 280 FRAME CRACKED, BL 8 AND 10 LEFT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 8,260 hrs · 6,935 cycles

NUTPLATE ISOLATORS ON AFT PRESSURE BULKHEAD CRACKED AT LBL 9.0 AND RBL 9.0.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 8,260 hrs · 6,935 cycles

FOUND FLOORBEAM TO 280 FRAME ATTACH CLIPS CRACKED, BL 8 AND 10 RIGHT.

Part: SKIN — CRACKED (AIRSTAIR DOOR) · airframe 8,260 hrs · 6,935 cycles

ASD INNER SKIN CRACKED AT AFT UPPER CORNER UNDER UPPER STEP.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,260 hrs · 6,935 cycles

FOUND RT SIDE FS 484 INTERCOSTAL CLIP CRACKED AT RBL 27.00.

Part: RIB — CRACKED (LT WING) · airframe 8,260 hrs · 6,935 cycles

FOUND LT BATT RIB CRACKED IN WHEEL WELL.

Part: SKIN — CRACKED (DOOR) · airframe 8,260 hrs · 6,935 cycles

ASD INNER SKIN CRACKED AT UPPER FWD CORNER UNDER UPPER STEP. REMOVED FASTENERS AND REMOVED DAMAGE. PER REO 601R-52-11-279 WHILE REMOVING DAMAGE CUT UNDERLYING STRUCTURE. RECEIVED REO 601R-52-11-1137 OPENED HOLE IN ASD UPPER LEFT CORNER AND INSTALLED BLIND RIVET PER REO601R-52-11-1137 CM20420. FABRICATED 1 REPAIR FROM 2024 T3 .040" AND FABRICATED 2 REPAIR FILLER FROM 2024 T3 .040". LOCATED NEW EXISTING HOLES IN REPAIR PARTS PER REO 01R-52-11-279 CM20420. PERFORMED EDDY CURRENT INSPECTION OF CUT OUT AREA PER REO 601R-52-11-279 IAW CRJ 2OO NDTM PART 1 51-20-06. NO DEFECTS NOTED. INSTALLED REPAIR PARTS PER REO 601R-52-11-279. JOB COMPLETE REB 7019524. 11-6-06 "COMPLIED WITH EC/TC REO 601R-52-11-1137 REV A.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 8,260 hrs · 6,935 cycles

FOUND CORROSION ON CABIN FLOORBEAM FS 349.00 AT LBL 27 TO LBL 44 (MARKED).

Part: RIB — CRACKED (RT WING) · airframe 8,260 hrs · 6,935 cycles

FOUND RT BATT RIB CRACKED IN WHEELWELL. REPAIRED IAW ALL REPAIR MANUALS. (CLOSED)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,260 hrs · 6,935 cycles

LT SIDE FS 484 INTERCOSTAL CRACKED AT LBL 36.00.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 8,260 hrs · 6,935 cycles

FOUND RT SIDE FS 484 INTERCOSTAL CRACKED AT RBL 36.00 (MARKED).

Part: BEAM — CRACKED (FUSELAGE) · airframe 8,260 hrs · 6,935 cycles

FOUND UPPER CENTER BOX BEAM APPEARS CRACKED. REPAIRS MADE IAW BOMBARDIER REO 601R53-61-345. (CLOSED 11/07/06)

Part: ANGLE — CRACKED (AIR STAIR DOOR) · airframe 8,260 hrs · 6,935 cycles

ASD AFT DRAG ANGLE CRACKED AT PULLEY BRACKET. INSTALL REPAIR PER REO 601R-52-11-513 (CLOSED 11/06/06)

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 8,260 hrs · 6,935 cycles

ASD OUTER HANDLE CRACKED. REMOVED AND REPLACED ASD OUTER HANLE IAW CRJ 200 MM CH 52-11-25-000-801 AND SRM 51-42-20 (CLOSED 11/03/06)

Part: ANCHOR FITTING — CRACKED (AIR STAIR DOOR) · airframe 8,260 hrs · 6,935 cycles

ASD AFT ANCHOR FITTING CRACKED. REMOVED AND REPLACED FWD AND AFT ANCHOR FITTING ASSY'S IAW M//M 52-11-17 SEE W/O 41536 TASK CARD EO600-52-66 FOR ANCHOR FITTING MOD AND OPS CKS. (CLOSED 11/06/06)

Part: BEAM — DAMAGED (BS 625-640) · airframe 8,260 hrs · 6,935 cycles

RT BOX BEAM ACCESS PANEL CUTOUT CRACKED AT FWD NUT PLATE, REMOVED ANGLES AND MADE CUT ON RIGHT SIDE BOX BEAM IAW REO 601R-53-61-366. PERFORMED EDDY CURRENT INSPECTION OF CUT LINE & UPPER & LOWER ANGLE AT RT LOWER WEB ACCESS HOLE ON ENGINE SUPPORT BEAM BETWEEN FS 625.30 & FS 640.00. NO DEFECTS NOTED. FABRICATED NEW RT WEB & STARTED PICKING UP HOLES IAW REO 601R-53-61-366. FABRICATED AND DRILLED UP RT INNER DOUBLER AND RT ANGLES AND DOUBLER SPLICE IAW REO 601R-53-61-366. STEPPED UP HOLES ON DOUBLER SPLICE, INNER DOUBLER, AND ANGLES IAW REO 601R-53-61-366. PARTS SENT TO PAINT SHOP. PRIMED & PAINTED DOUBLERS SPLICES AND ANGLES IAW CRJ SRM 51-25-01. STARTED INSTALLING DOUBLER, SPLICE AND ANGLES ON RT LOWER

Part: DOUBLER — CRACKED (BS 640) · airframe 8,260 hrs · 6,935 cycles

LT SIDE 640 DOUBLER CRACKED.

Part: DOUBLER — CRACKED (BS 640) · airframe 8,260 hrs · 6,935 cycles

RIGHT SIDE 640 DOUBLER CRACKED.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 8,260 hrs · 6,935 cycles

ASD OUTER HANDLE CRACKED. REMOVED AND REPLACED ASD OUTER HANLE IAW CRJ 200 MM CH 52-11-25-000-801 AND SRM 51-42-20 REMOVED ASD OUTER HANDLE PER CRJ200 SRM 51-42-16 TRANSFERED PARTS TO NEW HANDLE PER CRJ 200 SRM 51-41-02 REPLACED FLAPPER PER CRJ200 SRM 51-42-03 PRIMED AND PAINTED PER CRJ200 SRM 51-21-16 OK TO INSTALL HANDLE PER CRJ 200 SRM 51-42-16 INSTALLED OUTER DOOR HANDLE ON ASD PER CRJ 200 SRM 51-42-16. OPS CHECK GOOD ON PAX DOOR OUTER HANDLE REF CRJ 200 AMM 52-10-00 (CLOSED 11/10/06)

Part: SKIN — CRACKED (FUSELAGE) · airframe 8,260 hrs · 6,935 cycles

LT BOX BEAM (366) ACCESS PANEL CUTOUT CRACKED AT FWD NUT PLATE, REMOVED ANGLES AND MADE CUT ON LEFT SIDE OF BOX BEAM IAW REO 601R-53-61-366, 10-30-06. PERFORMED EDDY CURRENT INSPECTION OF CUT LINE AND UPPER AND LOWER ANGLE AT LEFT LOWER WEB ACCESS HOLE ON ENGINE SUPPORT BEAM BETWEEN FS 625.30 AND FS 640.00. NO DEFECTS NOTED. FABRICATED NEW LT WEB FROM 2024-T3 .063 AND STARTED PICKING UP HOLES IAW REO 601R-53-61-366. FABRICATED AND DRILLED LT INNER DOUBLER, DOUBLER SPLICE, AND ANGLES IAW REO 601R-53-61-366, 10-31-06. STEPPED UP HOLES ON INNER DOUBLER, DOUBLER SPLICE, AND ANGLE IAW REO 601R-53-61-366 11-01-06, PARTS SENT TO PAINT SHOP. PRIMED AND PAINTED DOUBLERS SPLICES AND ANGLES IAW CRJ SRM 51-25-01. ST

Part: BULB — INOPERATIVE (GALLEY) · airframe 6,954 hrs · 5,937 cycles

GALLEY SERVICE DOOR EMER EXIT LIGHT HAS BULBS INOP.

Part: UNKNOWN — ODOR (FUSELAGE)

DURING CRUISE, A BURNING, ELECTRICAL SMELL WAS NOTICED IN THE COCKPIT AND CABIN. THE APU WAS STARTED, AND SMELL WENT AWAY. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED AIRCRAFT AND PERFORMED POWER RUNS WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: DOOR — BINDING (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR AND NSPECTED THE CABLES WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)