N845AS

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 33,523 hrs · 30,250 cycles

TROUBLESHOT INOPERATIVE INTERIOR AND EXTERIOR EMERGENCY LIGHTING SYS. SWAPPED SPLICES ON THE WARDROBES EMERGENCY EXIT LIGHTS IAW ESPM 20-17-31. PERFORMED OPS TEST OF THE EMERGENCY EXIT LIGHTS IAW AMM 33-51-00-710-801. OPS TEST CHECKED GOOD AT THIS TIME.

Part: SKIN — DENTED (AFT FUSELAGE) · airframe 33,522 hrs · 30,249 cycles

DENT FOUND AFT OF APU EXHAUST BELOW APU SHIELD 21" BELOW. REPAIRED IAW REO 601R-53-61-5242 AND VERIFIED ALL STEPS COMPLIED WITH AND EC/TC REO 601R-53-61-5242.

Part: ANGLE — CORRODED (BS 484) · airframe 33,508 hrs · 30,238 cycles

BS 484 ANGLE CRACKED AT LBL 36. R & R ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,508 hrs · 30,238 cycles

LEFT SEAT TRACK CORRODED BS 559 - 559+80. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-00 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 33,508 hrs · 30,238 cycles

LEFT SEAT TRACK CORRODED BS 409+128 - 559. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 349-364) · airframe 33,508 hrs · 30,238 cycles

RIGHT CENTER AISLE SEAT TRACK, RBL 9 CORRODED BS 349 - 364. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11 000-802 AND AMM 53-01-400-802.

Part: SEAT TRACK — CORRODED (BS 409-499) · airframe 33,508 hrs · 30,238 cycles

LT SIDE SEAT TRACK CORRODED BS 409+112 - 499+85. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: BRACKET — CORRODED (BS 310) · airframe 33,508 hrs · 30,238 cycles

FRAME BRACKET BS 310 CORRODED ALONG AFT EDGE AT BOTTOM FWD CORNER OF SERVICE DOOR CUTOUT, JUST AT FLOOR SILL LEVEL. R & R LOWER FRAME BRACKET IAW SRM 53-21-23-00 AND SRM 53-21-23-00.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 33,522 hrs · 30,249 cycles

BROKEN ISLOATORS ON BULKHEAD BS 621. R & R ISOLATORS IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 33,508 hrs · 30,238 cycles

RT SIDE SEAT TRACK CORRODED BS 544 - 559+112. REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 33,508 hrs · 30,238 cycles

RT WING L/E ATTACH ANGLES AT OTBD SIDE OF INBD L/E AND INBD SIDE OF MID L/E ARE CRACKED. REPAIRED IAW SRM 51-40-11 AND AMM 20-21-00-910-801.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,508 hrs · 30,238 cycles

LT SIDE SEAT TRACK CORRODED BS 409+16 TO +112. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 33,508 hrs · 30,238 cycles

RT SIDE SEAT TRACK CORRODED FROM BS 499 - 544. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 349-364) · airframe 33,508 hrs · 30,238 cycles

CENTER ASILE LT SEAT TRACK A LBL 9 CORRODED, BS 349 - 364. REMOVED AND REPLACED SEAT TRACK IAW AMM 200 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 554-559) · airframe 33,508 hrs · 30,238 cycles

LT SIDE SEAT TRACK CORRODED BS 554 - 559+112. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-020-002 AND AMM 53-01-11-400-802.

Part: ARM — CORRODED (PAX DOORWAY) · airframe 33,522 hrs · 30,249 cycles

FWD, PAX DOOR HAND RAIL HINGE ARM "CUP" AT PAX DOOR SILL CORRODED. RIGHT FS310 CORRODED ALONG AFT EDGE AT BOTTOM FWD CORNER OF SERVICE DOOR CUT-OUT, JUST AT FLOOR SILL LEVEL. REMOVED FWD PAX DOOR HAND RAIL HINGE ARM CUP DRILLED UP ATTACH HOLES & HOLES FOR NUTPLATES REF SRM 57-40-11 & DWG 601R31527. INSTALLED NUT PLATES ON HINGE ARM CUP & INSTALLED ASSY IN ACFT IAW SRM 51-42-06 & DWG 601R31527. R & R RT JOINT ANGLE IAW SRM 53-21-23, 51-42-34.

Part: SEAT TRACK — CORRODED (BS 409-499) · airframe 33,508 hrs · 30,238 cycles

RT SIDE SEAT TRACK CORRODED BS 409+112 - 499+85. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-409-802.

Part: SEAT TRACK — CORRODED (BS 499-554) · airframe 33,508 hrs · 30,238 cycles

LT SIDE SEAT TRACK CORRODED BS 499 - 554. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-020-002 AND AMM TASK 53-01-11-420-001.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 33,522 hrs · 30,249 cycles

FLOOR SUPPORT CORRODED ALONG LBL 9 BETWEEN FS 574 AND 621, OUT OF LIMITS. FLOOR SUPPORT CAP R & R IAW 51-40-11 AND REO 601R-53-61-3780.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,522 hrs · 30,249 cycles

RIGHT CENTER AISLE, SEAT TRACK SECTION AT RBL9, FROM 10" FWD OD FS409.0 AFT TP- FS409+128, CORRODED AROUND SEVERAL TRACK ATTACHING SCREWS AND PITTED ON TOP SURFACE. REMOVED SEAT RAIL, IAW SRM 53-01-11. LOCATED AND DRILLED 54 EA NEW FASTENER HOLES IAW SRM 51-40-11. INSTALLED SEAT TRACK IAW AMM 53-01-1-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 33,508 hrs · 30,238 cycles

RT SIDE SEAT TRACK CORRODED BS 409+16 TO .112. REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 33,508 hrs · 30,238 cycles

RT FLOOR SUPPORT BS 310 CORRODED. REMOVED CORROSION IAW REO 601R-53-00-930 AND DETERMINED OUT OF LIMITS. REMOVED RT FLOOR SUPPORT IAW DWG 601R31148 & SRM 51-42-06. INSTALLED FLOOR SUPPORT IAW DWG 601R31148 & SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 4090) · airframe 33,508 hrs · 30,238 cycles

LEFT CENTER AISLE, SEAT TRACK SECTION A LBL 9, BS 4090 - 4090+128, CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-11 AND INSTALLED IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 33,508 hrs · 30,238 cycles

LT SIDE SEAT TRACK CORRODED BS 364 - 409+16. R & R SEAT TRACK IAW AMM 53-01-000-802 & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 499) · airframe 33,522 hrs · 30,249 cycles

LT SIDE SEAT TRACK CORRODED FROM FS 499-499+85 . COMPLIED WITH EC/TC REO 601R-53-00-55 AND REO 601R-53-00-055, REV A, DATED 11/18/2011.

Part: SEAT TRACK — CORRODED (BS 499) · airframe 33,508 hrs · 30,238 cycles

RT SIDE SEAT TRACK CORRODED BS 499 - 499+85. REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-01-11-000-802 AND AMM 53-01-11-04.

Part: SKIN — DAMAGED (FAIRING) · airframe 33,522 hrs · 30,249 cycles

STANG FAIRING IS BROKEN 434BT. REMOVED OLD SKIN IAW SRM 51-42-13 & 51-42-06, LOCATED & DRILLED NEW SKIN IAW SRM 51-40-11. INSTALLED SKIN IAW SRM 51-42-06 & 51-42-13. RESTORED FINISH IAW SRM 51-25-06 & 51-25-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,523 hrs · 30,250 cycles

DENT FOUND AFT OF APU EXHAUST BELOW APU SHEILD 21 INCHES BELOW. DENT FOUND AFT OF APU EXHAUST BELOW APU SHIELD 21" BELOW. COMPLIED WITH REO 601R-53-61-5242, REV P1 DATED MAR 27, 2014. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,028 hrs · 29,740 cycles

NR 3 EXTERIOR EMERGENCY LIGHT IS OUT. R & R LAMP IN LT SIDE NR 3 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 349-559) · airframe 29,813 hrs · 26,355 cycles

RT SIDE FLOOR SEAT TRACK HAS NUMEROUS AREAS OF CORROSION FROM FS 349 - FS 559 + 80. REPAIRED.

Part: FRAME — CORRODED (BS 364) · airframe 29,801 hrs · 26,345 cycles

FRAME FS 364 CORRODED LBL 26 AND RBL 26.

Part: SEAT TRACK — CORRODED (BS 349-559) · airframe 29,801 hrs · 26,343 cycles

SEAT TRACK CORRODED FROM FS 349- 559+80. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802, SEAT TRACKS FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. INSTALLED SERVICEABLE SEAT TRACKS IAW AMM 53-01-11-400-801.

Part: FRAME — CORRODED (BS 349) · airframe 29,801 hrs · 26,345 cycles

FRAME FS 349 CORRODED BETWEEN LBL 26 AND RBL 26. DRILLED SERVICEABLE FRAME SECTOR TO FIT AND INSTALLED IAW SRM 51-42-06 & SRM 31-42.

Part: FRAME — CORRODED (BS 310) · airframe 29,801 hrs · 26,343 cycles

FRAME 310 CORRODED BETWEEN LBL 26 AND RBL 26 BOTH SIDES. REMOVED AND REPLACED FRAME.

Part: SUPPORT FITTING — CORRODED (DOOR SILL) · airframe 29,801 hrs · 26,345 cycles

SERVICE DOOR SILL PLATE CORRODED AROUND THRESHOLD SUPPORT FITTINGS. REPAIRED IAW AMM 51-25-56-390-802.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 29,801 hrs · 26,343 cycles

ASD UPPER FWD & AFT CORNERS CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06. DWG 601R3003.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 29,801 hrs · 26,343 cycles

ASD UPPER FWD & AFT OTBD "L" ANGLES ARE CORRODED. REMOVED AND INSTALLED IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 364) · airframe 29,801 hrs · 26,345 cycles

FS 364 FRAME CORRODED BETWEEN LBL 26 AND RBL 26. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PROCEDURES UT-3 MAX .MATERIAL REMAINING IS .079", ORIGINAL IS .080", MATERIAL REMOVED IS .001". WITHIN ALLOWABLE IAW SRM 53-00-00 & SRM 51-21-06, REF SRM 53-21-15-00, FIG 6. TREATED PRIMED & APPLIED TOP COAT IAW SRM 51-21-06.

Part: ATTACH ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 29,801 hrs · 26,343 cycles

INTERCOSTAL ATTACHING ANGLE CRACKED AT FS 621, AT REAR PRESSURE BULKHEAD AS VIEWED FROM INSIDE AFT EQUIP BAY AND AT S13A. REMOVED INTERCOSTAL ATTACH ANGLE IAW SRM CH 51-42-20. INSTALLED NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-42-21 & DWG 601-36000.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,801 hrs · 26,343 cycles

CARGO TRACK AT FS 559 + 96 LBL 9 HAS CORROSION. FOUND CORROSION ON CARGO TRACK TO BE OUT OF LIMITS, REMOVED AND REPLACED CARGO TRACK IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,801 hrs · 26,343 cycles

CARGO TRACK AT 559 + 96 LBL 27 HAS CORROSION. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,801 hrs · 26,343 cycles

CARGO TRACK AT FS 559+112 - LBL 9 HAS CORROSION. FOUND CORROSION TO BE OUT OF LIMITS, REMOVED SEAT TRACK IAW SRM 51-41-02. INSTALLED SEAT TRACK IAW SRM 51-41-02 AND AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 29,801 hrs · 26,343 cycles

CARGO TRACK AT FS 559+112 RBL 9 HAS CORROSION. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CARGO TRACK IAW SRM 51-41-02. INSTALLED NEW CARGO TRACK IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (BS 621) · airframe 29,801 hrs · 26,343 cycles

CARGO TRACK AT FS 621 LBL 9 IS CORRODED. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-61-49, 51-41-02. REMOVED CARGO TRACK IAW SRM 51-41-02. INSTALLED SERVICABLE CARGO TRACK IAW AMM 20-21-910-801.

Part: FLANGE — CRACKED (BS 409 BULKHEAD) · airframe 29,801 hrs · 26,343 cycles

VERTICAL BULKHEAD POST AT FS 409 + 128 BL 0.00 HAS A CRACKED ATTACH FLANGE ON LT AFT SIDE JUST BELOW WL 69.00. REMOVED CRACKED FLANGE IAW SRM 51-42-06. INSTALLED NEW FLANGE IAW SRM 51-42-06 AND REO 601R-53-41-889.

Part: SUPPORT — CORRODED (DOOR SILL) · airframe 29,801 hrs · 26,345 cycles

SERVICE DOOR SILL CORRODED AROUND SUPPORT FITTINGS. REMOVED THRESHOLD SUPPORT FITTING IAW SRM 51-21-06. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06. REMOVED SUPPORT FITTINGS IAW SRM 51-42-02. LOCATED, DRILLED AND DEBURED NEW THRESHOLD SUPPORT FITTINGS. INSTALLED SUPPORT FITTINGS IAW SRM 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 314) · airframe 29,801 hrs · 26,343 cycles

SERVICE DOOR FLOOR SUPPORT ANGLE CORRODED AT 314.00 AND RBL 40. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00. INSTALLED SERVICEABLE ANGLE IAW DWG 601R38303, REV AR AND SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 29,801 hrs · 26,343 cycles

CARGO DOOR INTERCOSTAL CRACKED LOWER AFT CORNER. REMOVED, DRILLED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06, 51-42-21, & 51-40-11.

Part: STRUCTURE — CORRODED (BS 319) · airframe 29,801 hrs · 26,343 cycles

FS 319 CORRODED BETWEEN LBL 26 AND RBL 26 FRONT SIDE. FOUND CORROSION ON FRAME TO BE OUT OF LIMITS. R & R FRAME IAW SRM 51-42-06-00 AND 51-42-21-00.

Part: FRAME — CORRODED (BS 310) · airframe 29,801 hrs · 26,343 cycles

FRAME 310 CORRODED BETWEEN LBL 26 AND RBL 26 BOTH SIDES. FRAME SECTION CORRODED BEYOND LIMITS IAW SRM 53-00-00. REMOVED FRAME IAW SRM 51-42-21 AND SRM 51-42-21. INSTALLED FRAME SECTION IAW SRM 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 29,801 hrs · 26,343 cycles

FS 349 AND LBL 40, FLOORBEAM CORRODED. REMOVED CORROSION FROM FLOORBEAM AND FOUND OUT OF LIMITS IAW SRM 53-00-00. INSTALLED NEW FLOORBEAM ANGLE IAW SRM 51-42-06.

Part: STRUCTURE — CORRODED (BS 349) · airframe 29,801 hrs · 26,343 cycles

FS 349 CORRODED BETWEEN LBL 26 AND RBL26 BOTH SIDES. CORROSION IS OUT OF LIMITS IAW SRM 53-00-00. R & R FRAME IAW SRM 51-42-06.

Part: ATTACH BRACKET — CRACKED (BULKHEAD) · airframe 29,801 hrs · 26,343 cycles

AFT PRESSURE BULKHEAD LINTEL ATTACH BRACKET CRACKED. R & R BRACKET IAW SRM 51-42-20.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · airframe 29,801 hrs · 26,343 cycles

SERVICE DOOR SILL CORRODED. REMOVED SILL ANGLE AT FS 349 RBL40 IAW SRM 51-42-02. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00. INSTALLED SERVICEABLE ANGLE IAW DWG 601R38303 & SRM 51-42-21.

Part: FRAME — CORRODED (BS 364) · airframe 29,801 hrs · 26,343 cycles

FS 364 FRAME CORRODED BETWEEN LBL 26 AND RBL 26.

Part: FLOORBEAM — CORRODED (BS 340) · airframe 29,801 hrs · 26,343 cycles

SERVICE DOOR AREA AT BS 340 RBL 40 CROSSBEAM CORRODED AT TEE AND ATTACHING ANGLE BRACKET. REPAIRED IAW SRM 51-42-21-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,801 hrs · 26,343 cycles

CABIN FLOORBEAM ANGLE CRACKED AT FS 280 AND LBL 9. R & R FLOORBEAM ANGLE IAW SRM 51-42-20.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,801 hrs · 26,343 cycles

CABIN FLOORBEAM ANGLE CRACKED AT FS 280. R & R FLOORBEAM ANGLE IAW SRM 51-42-20.

Part: HYDRAULIC SYSTEM — FAILED (NR 1) · airframe 29,649 hrs · 26,156 cycles

AFTER TAKE OFF HYD 1 LOW PRESSURE CAUTION MESSAGE, QTY AND PRESSURE ZERO. ENGINE RAN FOR 25 MINUTES EMPTY, COMPLIED WITH QRH DIVERTED AND EMERGENCY DECLARED.

Part: ROD — DAMAGED (PAX DOOR) · airframe 29,599 hrs · 26,095 cycles

PAX DOOR WILL NOT OPEN. R & R SPRING ROD ASSY ON PAX DOOR IAW AMM 52-11-15. OPS CHECKED GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 29,288 hrs · 25,779 cycles

EMERGENCY LIGHT COVER IN GALLEY NEAR SERVICE DOOR IS MISSING THE EXIT COVER. R & R IAW AMM 33-51-05. PERFORMED OP TEST IAW AMM 33-51-00-710-801. NO FAULTS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,278 hrs · 25,769 cycles

CABIN CEILING EMERGENCY LIGHT, 2ND FROM FRONT, INOPERATIVE. RELAMPED IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,142 hrs · 25,623 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CEILING EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,824 hrs · 25,263 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,824 hrs · 25,263 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,307 hrs · 24,699 cycles

CABIN AFT MOST CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED CABIN AFT MOST CEILING EMERGENCY LIGHT AS REQUIRED. OPS CK GOOD IAW AMM 33-51-00.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 28,126 hrs · 24,487 cycles

NR 1 & NR 2 EXTERIOR AND NR 1 INTERIOR CEILING EMERGENCY LIGHTS INOP. R & R NR 1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD. R & R NR1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CK GOOD.

Part: SKIN — CRACKED (LWS 148) · airframe 28,029 hrs · 24,373 cycles

WHILE PERFORMING NDT INSP, IN THE LOCAL AREA, FOUND A VISIUAL INDICATION OF A CRACK JUST OTBD OF THE LT WING JACKING POINT AT WS 148.00 AT THE AFT SPAR AREA. WORK COMPLETED IAW: REO 601R-57-21-1409.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 27,579 hrs · 23,859 cycles

CAPTAINS FLASHLIGHT IN-OP. REPLACED CAPTAINS FLASHLIGHT BATTERIES IAW AMM 25-61-00.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 27,543 hrs · 23,810 cycles

RAMP REPORTS PAX DOOR HANDLE BROKE. INSPECTED AND LUBRICATED OUTER AND INNER HANDLES, AND FOUND SAFETY WIRE ON OUTER DOOR HANDLE LUBRICATION POINT BROKEN AND RESAFETIED, OPS CHECK GOOD IAW AMM 52-11-00 AND 52-11-23. (CLOSED)

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,189 hrs · 23,393 cycles

SERVICE DOOR LWR EMERGENCY EXIT SIGN HAS 2 BURNED OUT BULBS. R & R INOP BULBS FROM SVC DOOR LWR EMERGENCY EXIT SIGN IAW AMM 33-51-14.OPS CHECKED GOOD. R & R INOPERATIVE BULBS FROM SERVICE DOOR LWR EMERGENCY EXIT SIGN IAW AMM 33-51-14. OPS CHECKED GOOD.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 26,362 hrs · 22,423 cycles

PLACARDS ARE MISSING ON EXTERIOR OF COCKPIT EMERGENCY EXIT DOOR. USED SILKSCREEN METHOD TO LABEL PLACARDS THAT ARE MISSING IAW AMM TASK 11-10-03-000-801.

Part: BRACKET — CRACKED (BS 449.85) · airframe 26,362 hrs · 22,423 cycles

BRACKET CRACKED AT FS 449.85 BELOW RT WING EMERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 162DL ATTACHES TO RJ161728. REMOVED CRACKED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,362 hrs · 22,423 cycles

CRACK INDICATION FOUND AT AFT PRESSURE BULKHEAD LOCATED AT THE TOP OF THE LINTEL ATTACH POINT. AREA IS MARKED. REPAIRED IAW EC/TC REO 601R53-61-1230.

Part: BRACKET — CRACKED (CARGO DOOR FRAME) · airframe 26,362 hrs · 22,423 cycles

CARGO DOOR SUPPORT BEAM HAS CRACKED BRACKET WHERE IT MAKE TO 621.00 BULKHEAD. (LT 04/18/10) (RESOLVED ON W/O: 155601 TASKCARD: N/R-00390 ) JOB 8732425 /OPERATION 207/ REMOVED CRACKED BRACKET FOR CARGO DOOR SUPPORT BEAM AT FS 621.00 BULKHEAD IAW SRM 51-42-21. NEW CARGO DOOR SUPPORT BEAM BRACKET NEEDS TO BE INSTALLED. INSTALLED NEW CARGO DOOR SUPPORT BEAM BRACKET IAW SRM 51-42-21. (CLOSED)

Part: FRAME — CORRODED (BS 333) · airframe 26,362 hrs · 22,423 cycles

FRAME SECTION AT FS 333 FOUND CORRODED AT APPROX RBL 9 AT GROUND STUD ATTATCH POINTS, ONE GROUND STUD CORRODED OUT OF FRAME. (RESOLVED ON W/O: 155601 TASKCARD: N/R-00318 ) JOB 8732425/ OPERATION 135/ REMOVED UNSERVICABLE FRAME FROM FS 333 AND INSTALLED SERVICEABLE FRAME AT FS 333 ALL WORK DONE IAW SRM 51-42-06 AND SRM 51-42-21. (CLOSED)

Part: BRACKET — CRACKED (BS 469.63) · airframe 26,362 hrs · 22,423 cycles

BRACKET CRACKED AT FS469.63 BELOW LT WING ENERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 161DL ATTACHES TO RT 161728. (RESOLVED ON W/O: 155601 TASKCARD: N/R-00370 ) JOB 8732425 /OPERATION / REMOVED CRACKED ANGLE AT FS 469.93 JUST BELOW LT WING EMERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 161DL ATTACHES TO IAW SRM 51-42-06. NEW ANGLE AT FS 469.93 NEEDS TO BE INSTALLED. RECEIVED NEW SERVICEABLE ANGLE PN 601R31037-61 AND INSTALLED IAW SRM 51-42-06 REAPPLIED SELF CONTOURING SEALING PAD TO NEW ANGLE IAW AMM 51-23-00 PG 1. (CLOSED)

Part: SKIN — CORRODED (BS 333) · airframe 26,362 hrs · 22,423 cycles

CORROSION FOUND ON SKIN SPLICE AT FS 333 BETWEEN STR 27 AND 26. REPAIRED IAW REO 601R-53-21-1125.

Part: STRINGER — CORRODED (BS 333 S26R) · airframe 26,362 hrs · 22,423 cycles

CORROSION FOUND ON STR 26R 3" AFT OF FS 333. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. STARTED SPLICE REPAIR FOR STRG 26R IAW SRM 53-00-03. PERFORMED ET INSPECTION OF CUT LINES IAW SRM 53-00-03 PARA.4.(5) IAW NDTM PART 1, 51-20-06. NO INDICATIONS NOTED. CONT WITH STEP 9 OF SRM 53-00-03, PGE 204. COMPLIED WITH STEP 9 OF SRM 53-00-03 INSTALLED ALL FASTENERS EXCEPT FOR FASTENERS THAT ATTACH SPLICES. CONT. WITH STEP 10 OF SRM 53-00-03, PAGE 204. ATTACHED AFT SPLICE ON STAGE 26R ALL WORK DONE IAW SRM 53-00-03. INSTALLED FWD SPLICE ONSTR 26R AND APPLIED PROTECTIVE COATING IAW SRM 53-00-03 AND SRM 51-25-01.

Part: BRACKET — CRACKED (BS 469.63) · airframe 26,362 hrs · 22,423 cycles

BRACKET CRACKED AT FS 469.63 BELOW RT WING EMERGENCY EXIT THAT THE FUSELAGE OVERWING PANEL 162EL ATTACHES TO RT 161728. REMOVED CRACKED ANGLE IAW SRM 51-42-06. INSTALLED NEW ANGLE ALL WORK DONE IAW SRM 51-42-06 AND SRM 51-42-21.

Part: BRACKET — CRACKED (BS 449.85) · airframe 26,362 hrs · 22,423 cycles

BRACKET CRACKED AT FS 449.85 BELOW LT WING EMERGENCY EXIT THAT THE FUSELAGE OVER WING PANEL 161DL ATTACHES TO RT 161728. (RESOLVED ON W/O: 155601 TASKCARD: N/R-00369 ) JOB 8732425 /OPERATION 186/ BRACKET CRACKED AT FS 449.85 BELOW LT WING EMERGENCY EXIT THAT THE FUSELAGE OVER WING PANEL 161DL ATTACHES TO RT 161728. REMOVED CRACKED ANGLE AT FS 449.85 JUST BELOW LT WING EMERGENCY EXIT THAT THE FUSELAGE OVER WING PANEL 161DL ATTACHES TO IAW SRM 51-42-06. NEW ANGLE AT FS 449.85 NEEDS TO BE INSTALLED. INSTALLED NEW ANGLE AT FS 449.85 BELOW LT WING EMERGENCY EXIT IAW SRM 51-42-06, SRM 51-42-20. (CLOSED)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,362 hrs · 22,423 cycles

CRACK INDICATION FOUND ON AFT PRESSURE BULKHEAD LOCATED AT THE TOP OF THE AFT CARGO DOOR TRACK. AREA IS MARKED. PERFORMED CUT OUT ON AFT PRESSURE BULKHEAD AND FABRICATED FILLER AND DOUBLES IAW REO 601R-53-61-1541. NDT REQUIRED OF CUT LINE. PERFORMED ET INSP OF CUT LINE ON AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1541 IAW NDTM PART1, 51-20-06. NO INDICATIONS NOTED AT THIS TIME. DRILLED HOLES FOR FIELD FASTENERS AND BROUGHT ALL HOLES TO FINAL SIZE EXCEPT ON CARGO DOOR TRACK. APPLIED FINISH CODE TO REPAIR PARTS BY APPLYING ALODINE AND PRIMER WORK DONE IAW REO601R-53-61-1541. INSTALLED ALL REPAIR PARTS EXCEPT ITEMS THE REQUIRE DOOR TRACK IAW REO 601R-53-61-1541.

Part: BRACKET — CRACKED (BS 621) · airframe 26,362 hrs · 22,423 cycles

CABIN AFT PRESSURE BULKHEAD FRAME 621 NUT PLATE ISOLATOR BRACKET CRACKED AT 2ND ROW FROM BOTTOM RBL 9.50.

Part: ISOLATION MOUNT — CRACKED (BS 621) · airframe 26,362 hrs · 22,423 cycles

AFT PRESSURE BULKHEAD FS 621, NUT PLATE ISOLATOR BRACKET CRACKED AT 2ND ROW FROM BOTTOM LBL 27.50. R & R ISOLATOR IAW SRM 51-42-13.

Part: BRACKET — CRACKED (BS 621) · airframe 26,362 hrs · 22,423 cycles

AFT PRESSURE BULKHEAD FS 621, ISOLATOR NUT PLATE BRACKET CRACKED AT 1ST ROW FROM BOTTOM LBL 27.50. R & R ONE ISOLATOR WITH CR3213-5-2 RIVETS AT FS 621 ROW 1 ON LBL 27.50 IAW SRM 51-42-13.

Part: BRACKET — CRACKED (BS 621) · airframe 26,362 hrs · 22,423 cycles

CABIN AFT PRESSURE BULKHEAD FS 621, NUT PLATE ISOLATOR BRACKET CRACKED AT 2ND ROW FROM BOTTOM LBL 9.50. R & R 2 ISOLATOR IAW SRM 51-42-13.

Part: SPRING — FAILED (PAX DOOR GATE) · airframe 26,182 hrs · 22,216 cycles

PASSENGER BOARDING DOOR WILL NOT OPEN NORMALY WITH OUT EXTERIOR ASSISTANCE. R & R PASSINGER DOOR PRESSURE VENT-FLAP DOOR SPRING IAW AMM 5 2-11-15 OPS CHECK GOOD.

Part: PLACARD — MISSING (PAX DOOR) · airframe 26,097 hrs · 22,111 cycles

F/A REPORTS OPEN AND EXIT PLACARDS MISSING FROM PAX DOOR. INSTALLED PLACARDS AMM 11-30-00.

Part: HANDLE — LACK OF LUBE (MAIN PAX DOOR) · airframe 26,097 hrs · 22,111 cycles

F/A REPORTS PAX DOOR DIFFICULT TO OPEN. LUBRICATED HANDLE, INSPECTED DOOR MECHINISM, AND OPERATIONAL TEST GOOD. AMM 52-11-01.

Part: HANDLE — BINDING (PAX DOOR) · airframe 26,029 hrs · 22,042 cycles

F/A REPORTS ENTRY DOOR HARD TO CLOSE/OPEN HANDLE MESSED UP. PERFORMED OPERATIONAL TEST OF PASSENGER DOOR IAW AMM 52-11-00. NO DEFECTS NOTED.

Part: ROLLER CAM — LACK OF LUBE (MAIN PAX DOOR) · airframe 25,988 hrs · 21,989 cycles

MAIN PAX DOOR STICKING AND HARD TO OPEN. LUBED PAX DOOR HANDLE ROLLER GUIDE IAW AMM 12-20-52. OP CK GOOD. ACFT OK FOR SERVICE.

Part: DOOR — STUCK (MAIN PAX) · airframe 25,856 hrs · 21,842 cycles

PAX DOOR WOULDNT OPEN FROM THE INSIDE.

Part: PIN — STUCK (PAX DOOR) · airframe 25,830 hrs · 21,812 cycles

FA REPORTS WHEN THEY TRY TO OPEN THE PAX DOOR PINS WILL NOT DISENGAGE NEEDS TO MOVE HANDLE DOWN AND UP A FEW TIMES TO OPEN.

Part: DOOR — STUCK (MAIN PAX) · airframe 25,562 hrs · 21,512 cycles

F/A UNABLE TO OPEN PAX DOOR WITHOUT ASSISTANCE FROM OUTSIDE.

Part: FLOOR SKIN — CRACKED (BS 460) · airframe 25,539 hrs · 21,486 cycles

HFEC INDICATION NOTED AT 60% FSH APPROX 1" LONG IN THE PRESSURE FLOOR AT RBL 4.50 APPROX 1.25" FWD OF THE F.S. 460 INTERCOSTAL. INDICATION APPEARS TO RUN PARALLEL WITH INTERCOSTALS. FAILS NDT INSP AT THIS TIME. COMPLIED WITH EC/TC REO 601R-53-41-884A BY PERFORMING TEMPORARY REPAIRS TO THE PRESSURE FLOOR WEB AT FS 460.00 IAW REO 601R-53-41-884, REV D. ALL REQUIREMENTS OF THE REO WAS MIT.

Part: ANGLE — CRACKED (BS 559) · airframe 25,539 hrs · 21,486 cycles

WHILE PERFORMING HFEC INSP OF F.S. 559.0 WEB AND CAP ANGLE, THREE INDICATIONS WERE NOTED AS LISTED 1) 2", 100% FSH IND NOTED AT RBL 18.0 WL 59.10 IN CHEM MILLED RADIUS, 2) .1", 75% FSH IND NOTED AT RBL 9.0 WL 58.70 APPROX Ï¿½" O/B OF CHEM MILLED RADIUS, AND .2", 70% FSH IND NOTED IN CAP ANGLE RADIUS BELOW LBL 18.0 VERT POST. FAILS NDT INSP AT THIS TIME. C/W CC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.

Part: DOOR — STIFF (MAIN PAX) · airframe 25,457 hrs · 21,400 cycles

F/A REPORTS PAX DOOR VERY DIFFICULT TO OPEN. " MUST JIGGLE.'

Part: LOCK — INOPERATIVE (PAX DOOR) · airframe 25,402 hrs · 21,341 cycles

MAIN ENTRANCE DOOR NOT RELEASE LOCKS WHEN OPENED

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,904 hrs · 20,846 cycles

RT FWD EXTERIOR EMERGENCY LIGHT BURNED OUT.

Part: DOOR — BINDING (PAX DOOR) · airframe 24,607 hrs · 20,563 cycles

F/A REPORTS PAX DOOR IS HARD TO OPEN.

Part: DOOR — BINDING (PAX DOOR) · airframe 24,607 hrs · 20,563 cycles

PAX DOOR DIFFICULT TO OPEN FROM INSIDE.

Part: LEVER — DEFECTIVE (CABIN DOOR) · airframe 24,336 hrs · 20,310 cycles

F/A REPORTS CABIN DOOR HARD TO OPEN (LATCH LEVER).

Part: HANDLE — STIFF (PAX DOOR) · airframe 24,245 hrs · 20,220 cycles

PAX DOOR HANDLE EXTREMELY HARD TO OPEN AND CLOSE. FLT 5033 DEL 134 MINS.

Part: DOOR — BINDING (PAX DOOR) · airframe 24,047 hrs · 20,009 cycles

FA REPORTS PAX DOOR IS VERY HARD TO OPEN.

Part: DOOR — BINDING · airframe 23,982 hrs · 19,950 cycles

F/A REPORTS DOOR DIFFICULT TO OPEN.

Part: DOOR — BINDING (PAX DOOR) · airframe 23,894 hrs · 19,876 cycles

F/A CANNOT GET PAX DOOR TO OPEN. FLT 4980 DEL 90 MINS.

Part: DOOR — BINDING (PAX DOOR) · airframe 23,521 hrs · 19,540 cycles

PAX DOOR STILL DIFFICULT TO OPEN FROM INSIDE.

Part: DOOR — BINDING (PAX DOOR) · airframe 23,521 hrs · 19,540 cycles

PAX DOOR DIFFICULT OPENING FROM INSIDE. FLT 5514 DEL 54 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,521 hrs · 19,540 cycles

RIGHT SIDE, FWD OVERWING EMERGENCY LIGHT INOP.

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 23,234 hrs · 19,282 cycles

PAX DOOR HANDLE INSIDE VERY HARD TO OPEN. RAN OPS TEST ON PAX DOOR IAW AMM 52-11-21-710-801. OPS CK GOOD. NO DEFECTS NOTED. A/C OK FOR SVC AT THIS TIME.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 23,193 hrs · 19,243 cycles

F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE. C/W OPERATIONAL CK OF PASSENGER DOOR IAW CRJ 200 AMM 52-11-00 NO DEFECTS NOTED OK FOR SERVICE.

Part: LATCH — LACK OF LUBE (PAX DOOR) · airframe 22,734 hrs · 18,836 cycles

FORWARD DOOR DIFFICULT TO OPEN FROM INSIDE AND OUTSIDE. LUBED AND CLEANED PASSENGER DOOR LATCH. OPS CHECK GOOD AT THIS TIME REF: 52-00-00 AND 20-00-00. (S)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 2,264,628 hrs · 18,748 cycles

1 EA LT AND RT AFT OVERWING EXITS LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERG LIGHTING BATTERY PACK AND BATTERY CHARGER IAW AMM`S 33-51-04 AND 33-51-05. OPS CHECK GOOD. CLEARED DEFER AND REMOVED PLACARD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 2,264,628 hrs · 18,748 cycles

NR 2 AND 4 CEILING EMERGENCY FLOOD LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY PACK AND BATTERY CHARGER IAW AMM`S 33-51-04 AND 33-51-05. OPS CHECK GOOD. CLEARED DEFER AND REMOVED PLACARD.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 22,605 hrs · 18,714 cycles

PAX DOOR CANNOT BE OPENED FROM INSIDE. FLT 4254. OPS CHECK DOOR SEVERAL TIMES. OPS CHECKED GOOD. LUBED OUTER DOOR STOW HANDLE. OPS GOOD. OK FOR SERVICE IAW 52-11-01. (B)

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 22,374 hrs · 18,514 cycles

AAR - 2081 - CARGO COMPARTMENT FLOOR PANEL 282ERF CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,374 hrs · 18,514 cycles

AAR - CLIP AT FS 484 RBL 27 CRACKED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 22,374 hrs · 18,514 cycles

AAR - CLIP CRACKED AT FS 280 O/B OF RBL 9. REMOVED DAMAGED CLIP AT FS 280.00 O/B OF RBL 9.00. INSTALLATION OF SERVICEABLE ATTACH CLIP. ALL WORK DONE IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 4/17/08.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,374 hrs · 18,514 cycles

AAR - CLIP AT FS 484 LBL 27 CRACKED (MARKED).

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,374 hrs · 18,514 cycles

AAR - BATH TUB FITTING CRACKED AT RBL 9. REMOVE UNSERVICEABLE TUB FITTING IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. TRANSFERRED HOLES TO SERVICEABLE TUB FITTING FROM UNSERVICEABLE FITTING, IAW CRJ 200 SRM 51-40-11, OK TO INSTALL PLJ 14922 04/13/08. INSTALLED SERVICEABLE FITTING IAW CRJ SRMM 51-42-21. OK TO TOPCOAT. APPLIED TOPCOAT IAW CRJ SRM 51-25-11. DR 15098. SUPPLEMENTAL SDR CLOSED 4/22/08.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,374 hrs · 18,514 cycles

AAR - AFT REPAIR ANGLE AT FS 280 LBL 9 CRACKED. REMOVED DINOTROL AND CLEANED SUSPECTED DAMAGE AREA. AFTER FURTHER INVESTIGATION FOUND AFT REPAIR ANGLE AT FS 280.00 LBL 9.00 TO BE A MARK NOT CRACKED. C/W HFEC INSP OF ANGLE. NO DEFECTS NOTED IAW CRJ 200 NDTM 51-20-06. NO FURTHER ACTION REQUIRED. SUPPLEMENTAL SDR CLOSED 4/17/08.

Part: RIB — DEBONDED (STABILIZER) · airframe 22,374 hrs · 18,514 cycles

AAR - 3016 - LEFT HAND STAB TIP I/B AFT SUPPORT RIB CRACKED. RIB FOUND NOT TO BE CRACKED, DISBONDED ONLY. REBONDED DISBONDED AREAS BY USING EP50A IAW CRJ SRM 51-74-14. SUPPLEMENTAL SDR CLOSED 4/22/08.

Part: STEP — CRACKED (PAX DOOR) · airframe 22,374 hrs · 18,514 cycles

AAR - PAX DOOR STEP 832FT CRACKED OR DISBONDED ON FWD END. REMOVED AND REPLACED DAMAGED PAX DOOR STEP 832 FT (P/N 601R31980-59), WITH SERVICEABLE STEP (P/N 601R31980-59) AS PER CRJ 200 AMM 52-11-04. PERFORMED OPERATIONAL TEST OF PAX DOOR STEPS AS PER CRJ 200 AMM 52-11-04 (NO DEFECTS NOTED). SW 14394 04/20/08. SUPPLEMENTAL SDR CLOSED 4/24/08.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,012 hrs · 18,206 cycles

EXIT EMERGENCY LIGHT FACING FWD ON CEILING AT OVERWING HATCHES IS OUT.

Part: HANDLE — STIFF (DOOR) · airframe 21,509 hrs · 17,790 cycles

ASD OUTER HANDLE IS HARD TO OPEN. FLT 4918 DEL 80 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,991 hrs · 17,365 cycles

FWD CEILING EMERGENCY LIGHT INOP.

Part: DOOR — STIFF (CABIN) · airframe 19,946 hrs · 16,550 cycles

CABIN DOOR VERY DIFFICULT TO OPEN FROM THE OUTSIDE.

Part: PLACARD — FADED (CABIN) · airframe 17,949 hrs · 15,042 cycles

LT OVER WING EMERGENCY EXIT EXTERIOR PLACARD FADED.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 17,906 hrs · 15,007 cycles

LEFT WING AFT EMERGENCY LIGHT IS INOP

Part: SILL — CORRODED (PX DOOR) · airframe 17,848 hrs · 14,964 cycles

ASD LOWER SILL UPPER SURFACE FOUND CORRODED.

Part: TRACK — CORRODED (FUSELAGE) · airframe 17,848 hrs · 14,964 cycles

SHORT FLOOR TRACKS AFT OF LAV AT LBL9, LBL27, RBL9 AND RBL27 HAVE CORROSION, RESOLVED ON W/O: 24018 TASKCARD: N/R-00422. REMOVED AND REPLACED CORRODED FLOOR TRACKS IAW AMM CRJ200 53-01-11 CM20420 JOB COMPLETE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 17,848 hrs · 14,964 cycles

FOUND CRACK AT RBL 9 FS 559.00, RESOLVED ON W/O: 24018 TASKCARD: N/R-00406. PERFORMED ET INSPECTION IN SUSPECT CRACK IAW NDT CRJ 200 NDT MANUAL PART 1 CHAPTER 51-20-06. NO DEFECTS NOTED.

Part: DOOR — CORRODED (AVIONICS BAY) · airframe 17,848 hrs · 14,964 cycles

FOUND CORROSION ON BELLY IN AVIONICS BAY ON 2ND, 3RD AND 4TH RIB FWD OF AVIONICS BAY DOOR. REPAIRED CORROISION DAMAGE ON BELLEY IAW SRM 53-21-15 53-00-00 AND 51-21-06. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 17,848 hrs · 14,964 cycles

FOUND RT FLOOR SUPPORT AT FS 349 AND SERVICE DOOR ENTRANCE O/B SUPPORT THAT RUNS LENGTH OF CABIN CORRODED, CORROSION VIEWED FROM BOTTOM. REPAIRED DAMAGE IAW REO 601R-53-21-666. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,848 hrs · 14,964 cycles

FOUND SURFACE CORROSION AT ASD OPENING FUSELAGE AT CENTER DRAIN BETWEEN ASD HINGE AND FLOOR SUPPORT STRINGER. FOUND DAMAGE REMOVAL TO BE WITHIN ALLOWABLE LIMITS PER SRM 53-00-00, CORROSION DOES NOT APPEAR TO EXTEND TO HINGE. RESTORED SURFACE FINISH PER SRM 51-25-00. JF21503. JOB COMPLETE. (SUPPLEMENTAL SDR) (SDR CLOSED 5/15/2006)

Part: FLOOR PANEL — CORRODED (BS 349) · airframe 17,848 hrs · 14,964 cycles

FOUND RT SIDE FLOOR STRUCTURE AT FS 349 AND SERVICE DOOR ENTRANCE CORRODED. REPAIRED CORROSION ON RT SIDE FLOOR STRUCTURE AT FS349 REF REO 601R-53-21-667. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 17,848 hrs · 14,964 cycles

FOUND FLOOR SUPPORT STRINGER AT PAX DOOR OPENING STA 310 TO 349 CORRODED. STRINGER WAS REPLACED ON N/R-00411 W/O 24018 FOR WORK ACCOMPLISHED PLEASE REFER TO THE FORMENTIONED NON ROUTINE CARD. PSP19749 15MAY06(CLOSED)

Part: CLIP — CRACKED (BS 484) · airframe 17,848 hrs · 14,964 cycles

FOUND LT FS 484 CLIP I/B SIDE CRACKED. REPAIRED CRACKED CLIP IAW REO 601R-53-41-059. CLOSED

Part: PRESSURE PANEL — CORRODED (BS 409-473) · airframe 17,848 hrs · 14,964 cycles

FOUND CORROSION ON PRESSURE DECK AT FS409+128 TO FS 473 - BL36 TO 44LT. REPAIRED IAW REO 601R-53-41-420. (CLOSED)

Part: PRESSURE PANEL — CORRODED (BS 409) · airframe 17,848 hrs · 14,964 cycles

FOUND CORROSION ON PRESSURE DECK FS409+128 TO 473 - BL36 TO44 RT. REPAIRED IAW REO 601R-53-41-420. (CLOSED)

Part: PRESSURE PANEL — CORRODED (BS 473-559) · airframe 17,848 hrs · 14,964 cycles

FOUND CORROSION ON PRESSURE DECK AT FS 473 TO 559 - BL36 TO 44LT. REPAIRED IAW REO6+01R-53-41-420. (CLOSED)

Part: PRESSURE PANEL — CORRODED (BS 473-559) · airframe 17,848 hrs · 14,964 cycles

FOUND CORROSION ON PRESSURE DECK AT FS 473 TO 559, BL36-44R. REPAIRED IAW REO 601R-53-41-420. (CLOSED)

Part: BEAM — CRACKED · airframe 17,848 hrs · 14,964 cycles

LT LOWER BOX BEAM WEB CRACKED AT ACCESS PANEL FWD I/B NP, RESOLVED ON W/O: 24018 TASKCARD: N/R-00138. REPAIRED IAW REO 601R-53-61-366.

Part: CLIP — CRACKED (FUSELAGE) · airframe 17,848 hrs · 14,964 cycles

LT OTBD 484 CLIP CRACKED, RESOLVED ON W/O: 24018 TASKCARD: N/R-00210. WORK COMPLETED IN ACCORDANCE WITH:REO 601R-53-41-059 PSP 19749.

Part: BEAM — CRACKED · airframe 17,848 hrs · 14,964 cycles

RT LOWER BOX BEAM WEB CRACKED AT ACCESS PANEL FWD I/B NP, RESOLVED ON W/O: 24018 TASKCARD: N/R-00139. REPAIRED IAW REO 601R 53-61-366.

Part: BEAM — CRACKED (FUSELAGE) · airframe 17,848 hrs · 14,964 cycles

FS 280 BEAM CRACKED AT LOWER RADIUS AT LBL 9, RESOLVED ON W/O: 24018 TASKCARD: N/R-00228. REPAIRED FS 280 BEAM CRACK INCORPORATING EC REO 601R-53-11-926.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,848 hrs · 14,964 cycles

ALL SUPPORTS THAT HOLD FLOORBOARD 221ALF JUST FWD OF FS 280 CORRODED, RESOLVED ON W/O: 24018 TASKCARD: N/R-00231. REPAIRED CORROSION JUST FWD OF FS 280.

Part: FRAME — CRACKED (BS 718 S11L) · airframe 17,848 hrs · 14,964 cycles

LT FRAME STA 718 CRACKED AT STR 11, RESOLVED ON W/O: 24018 TASKCARD: N/R-00140. REPAIRED LT FRAME STA 718 CRACK IAW SRM 51-42-16 AND REO 601R-53-61-193-1.

Part: BEAM — CORRODED (FUSELAGE) · airframe 17,848 hrs · 14,964 cycles

FS 280 BEAM CORRODED ON TOP FLANGE AT NUTPLATE HOLES, RESOLVED ON W/O: 24018 TASKCARD: N/R-00229. REPAIRED CORROSION TO 280 BEAM IAW REO 601R-53-11-926.

Part: RIB — CRACKED (RT WING) · airframe 17,848 hrs · 14,964 cycles

RT WING BAT RIB CRACKED. REPAIRED IAW REO 601R-57-51-046 (CLOSED)

Part: RIB — CRACKED (LT WING) · airframe 17,848 hrs · 14,964 cycles

LT WING WHEEL WELL BATT RIB CRACKED.

Part: STEP — CRACKED (PAX DOOR) · airframe 17,848 hrs · 14,964 cycles

ASD FIRST STEP WHEN OPEN CRACKED, RESOLVED ON W/O: 20097 TASKCARD: N/R-00083. REMOVED AND REPLACED ASD FIRST STEP IAW AMM 52-11.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 17,848 hrs · 14,964 cycles

AEB RT STA 640 POSSIBLY CRACKED.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 17,848 hrs · 14,964 cycles

FLIGHT STATION, FWD OF FS 280 FLOOR PANEL, FLOOR SUPPORT CORRORED, RESOLVED ON W/O: 24018 TASKCARD: N/R-00126. REMOVED AND REPLACED FLOOR SUPPORT ANGLE.

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE ATTACH ROD CONNECTED TO THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — DISCONNECTED (CABIN)

FLT 4620 - DURING A GROUND INSPECTION IN ATL, THE MIDDLE TO REAR SECTION OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AN EMERGENCY FLOOR TRACK LIGHT FILAMENT KNOCKED OUT OF THE TRACK CONNECTOR AND RECONNECTED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE HANDRAIL HINGE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP IAW MM. OPERATIONAL CHECKS GOOD. (K)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 14,056 hrs

DURING A C-CHECK, THE FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLES AT FS 621 ON THE LT AND RT SIDES IAW EO 600-53-0105.

Part: CLIP — CRACKED (FUSELAGE) · airframe 14,056 hrs

DURING A C-CHECK, THE CLIPS AT FS 280, LBL 9 IB AND OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS280, LBL 9 IB AND OB.

Part: CLIP — CRACKED (FUSELAGE) · airframe 14,056 hrs

DURING A C-CHECK, THE CLIPS AT FS280, RBL 9 IB AND OB WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIPS AT FS280, RBL 9 IB AND OB.

Part: HANDLE — CRACKED (E/E BAY)

DURING A C-CHECK, THE MAIN AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE MAIN AVIONICS BAY DOOR HANDLE ASSEMBLY.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 14,056 hrs

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY ABOVE THE SERVICE DOOR.

Part: CLIP — CRACKED (FLOOR SUPPORT) · airframe 14,058 hrs

DURING A C-CHECK, THE FLOOR SUPPORT CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CLIPS AT FS 484, LBL 36 AND RBL 36 IAW EO 600-53-0098.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 14,057 hrs

DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT LB0 WAS FOUND TO BE CRACKED UNDER THE FIRE LOOP BRACKET BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO 600-53-0072.

Part: SCAVENGE PUMP — FAILED (LT ENGINE)

FLT 4479 - DURING CRUISE FROM CHS-DFW, AT APPROXIMATELY 36,000 FEET THE LEFT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED WITH THE OIL PRESSURE FLUCTUATING BETWEEN 20-30 PSI. THE CREW COMPLIED WITH THE QRH AND UPON REDUCING THE LEFT ENGINE THE IDLE, THE OIL PRESSURE WENT UP TO 40 PSI. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED INTO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LUBE AND SCAVENGER PUMP ON THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4242 - DURING A GROUND INSPECTION IN BTR, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN BTR, THE BOTTOM STOP FOLD DOWN BRACKET ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PSU — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN DFW, THE FORWARD EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHTS POWER SUPPLY UNIT. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — SHORTED (EMERGENCY LIGHT)

FLT 4232 - DURING A GROUND INSPECTION IN DFW, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND A SCREW SHORTING AGAINST THE BULB ON THE PASSENGER DOOR FLOODLIGHT AND ADJUSTED THE FLOODLIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LT AND RT AFT DOUBLERS AT FS 718 BETWEEN STRINGERS 10 AND 12 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT AFT DOUBLERS AT FS 718 BETWEEN STRINGERS 10 AND 12 IAW ASA EO 600-53-0067A. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FS 718 FORWARD SIDE BETWEEN STRINGERS 10 AND 12 WERE FOUND TO BE CRACKED BYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT FS 718 FORWARD SIDE BETWEEN STRINGERS 10 AND 12 IAW ASA EO 600-53-0067A. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4414 - DURING A GROUND INSPECTION AT MGM, THE AFT EMERGENCY CEILING LIGHT NEXT TO THE LAVATORY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP NEXT OT THE LAVATORY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (T/E FLAP)

DURING FLIGHT FROM YOW TO ATL, FLAPS FAILED AT 8 DEGREES. THE CAPTAIN DECLARED AN EMERGENCY. AIRCRAFT DIVERTED AND LANDED SAFELY IN SYR. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT BRAKE AND POSITION SENSING UNIT. MAINTENANCE ALSO REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT AND THE LEFT FLAP ACTUATOR. (M)

Part: BRAKE — SEIZED (MLG)

FLT 4408 - DURING FLIGHT FROM ATL-SBN, ON TAXI OUT RIGHT BRAKE LOCKED UP AND BLEW TIRE. MAINTENANCE TOWED AIRCRAFT BACK TO GATE. MAINTENANCE REMOVED AND REPLACED RIGHT INBOARD BRAKE AND WHEEL ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)