N829AS

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 36,718 hrs · 32,508 cycles

LT AFT EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: INTERCOSTAL — CORRODED (BS 394-409) · airframe 35,769 hrs · 31,633 cycles

INTERCOSTAL AFT OF MAIN AVI DOOR CUTOUT AT FS 394 - 409, S26L HAS MINOR CORROSION ON FWD END OF ATTACH FLANGE. REPAIRED IAW SRM 51-42-06.

Part: SKIN — CORRODED (WING) · airframe 35,769 hrs · 31,633 cycles

ACCESS HOLE 610AB LOWER WING PLANK ACCESS HOLE HAS INDICATIONS OF CORROSION ON LANDING APPROX 50 PERCENT FULL SCREEN HOLE. ACCESS HOLE FAILED NDT. REPAIRED IAW EC/TC EO 600-57-81 & REO 601R-57-21-030, REV J.

Part: SKIN — CORRODED (WING) · airframe 35,769 hrs · 31,633 cycles

LT SIDE LOWER WING PLANK ACCESS HOLE FOR PANEL 540DB HAS INDICATIONS OF CORROSION ON LANDING APPROX 55 PERCENT, FULL SCREEN HEIGHT. ACCESS HOLE FAILED NDT. REPAIRED IAW EC/TC EO 600-57-81 & REO 601R-57-21-030, REV J.

Part: SKIN — CORRODED (WING) · airframe 35,769 hrs · 31,633 cycles

ACCESS HOLE FOR PANEL 650GB ON LOWER WING PLANK HAS INDICATIONS OF CORROSION ON LANDING APPROX 58 PERCENT FULL SCREEN HEIGHT. ACCESS HOLE 650GB FAILED NDT. REPAIRED IAW EC/TC EO 600-57-81 & REO 601R-57-21-030, REV J.

Part: FLOOR SUPPORT — CORRODED (BS 449.85) · airframe 35,769 hrs · 31,633 cycles

RT FLOOR SUPPORT FS 449.85 HAS CORROSION AROUND 1 FLOORBOARD NUTPLATE HOLE. REPAIRED IAW REO 601R-53-41-1689.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,761 hrs · 31,625 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX .4" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541.

Part: POST — CRACKED (BS 409) · airframe 35,768 hrs · 31,632 cycles

FOUND FS 409+128 VERTICAL POST BL 0.0 RT SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69 APPROX .2" IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED RT POST FORM LT POST AT FS 409.00+182 BL 0.0 IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE RT SIDE FS 409+128, BL 0, VERTICAL POST TO SAME SERVICEABLE LT BL 0.00 VERT POST IAW SRM 51-42-06. REPAIRED IAW REO 601R-53-41-889, REV A.

Part: POST — CRACKED (BS 409) · airframe 35,768 hrs · 31,632 cycles

FOUND FS 409+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69.0 APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED FS 409+128, RBL 18.0 CRACKED POST ASSY DRILLED, LOCATED FASTENER HOLES IAW SRM 51-42-06 AND 51-42-22. INSTALLED NEW INBD SIDE POST FOR FS 409.00+128, RBL 18.0, PN 601R32208-324 ON OTBD POST IAW SRM 51-42-06.

Part: PANEL — CORRODED (LT WING) · airframe 35,761 hrs · 31,625 cycles

LT WING LWR WING PLANK ACCESS HOLE 510AB HAS PITTING/CORROSION AT INBD LOCATION. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.

Part: SKIN — CORRODED (RT WING) · airframe 35,761 hrs · 31,625 cycles

RT WING LOWER WING PLANK ACCESS HOLE 640AB CORRODED AT AFT LOCATION. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.

Part: PANEL — CORRODED (LT WING) · airframe 35,761 hrs · 31,625 cycles

LEFT WING LWR WING PLANK ACCESS HOLE 540BB HAS PITTING/CORROSION AT INBD AND OTBD LOCATIONS. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.

Part: SKIN — CORRODED (RT WING) · airframe 35,761 hrs · 31,625 cycles

RT WING LOWER WING PLANK ACCESS HOLE 640BB HAS CORROSION AT FWD AND AFT LOCATIONS. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.

Part: ANGLE — CRACKED (LT WING TE FLAP) · airframe 35,752 hrs · 31,614 cycles

LT OTBD FLAP MIDDLE HINGE POINT OTBD ATTACH ANGLE FOR 595BB IS CRACKED IN RADIUS 2.5". DRILLED UP NEW SERVICEABLE ATTACH ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE ATTACH ANGLE ON LT OTBD FLAP MIDDLE HINGE IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 35,760 hrs · 31,624 cycles

FS 484, FLOOR SUPPORT ANGLE AT RBL 27 IS CRACKED. REMOVED CLIP PN 601R31171-9 IAW SRM 51-42-21 AT FS 484 RBL 27. LOCATED AND DRILLED NEW SERVICEABLE CLIP PN 601R31171-9 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-21.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 35,760 hrs · 31,624 cycles

SERVICE DOOR FLOOR SILL IS CORRODED. REMOVED CORRODED SILL PLATE FROM SERVICE DOOR SURROUND STRUCTURE IAW SRM 51-42-21. LOCATED AND DRILLED NEW SILL PLATE IAW SRM 51-40-11. INSTALLED SERVICE DOOR SILL PLATE IAW SRM 51-42-10, 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 35,768 hrs · 31,632 cycles

FS 484 FLOOR SUPPORT ANGLE AT RBL 27 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE ANGLE IAW SRM 51-40-11. INSTALLED NEW ANGLE IAW SRM 51-42-21.

Part: FRAME — CRACKED (BS 718) · airframe 35,752 hrs · 31,614 cycles

RT FS 718, FRAME PREVIOUS REPAIR SHOWS VISUAL SIGNS OF A CRACK BETWEEN STRINGERS 10R AND 12R. REMOVED SECTION OF FRAME STATION 718 BETWEEN STR 5R AND 21R IAW SRM 51-42-06 AND 51-41-02. RECEIVED NEW FRAME SECTION PO 600-36030-24, REQ'S LOCATING AND DRILLING. LOCATED & DRILLED NEW FRAME SECTION PN 600-36030-24 IAW SRM 51-40-11. INSTALLED NEW SECTION OF FRAME IAW SRM 51-42-06.

Part: FRAME — CRACKED (BS 718) · airframe 35,752 hrs · 31,614 cycles

LT FS 718 FRAME PREVIOUS REPAIR SHOWS VISUAL SIGNS OF A CRACK BETWEEN STRINGERS 10L AND 12L. REPLACED SECTION OF FRAME BS 718 FROM STR 5L-21L IAW SRM 51-42-06 AND 51-41-02 TO ACCOMODATE SB 601R-53-055.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,831 hrs · 30,780 cycles

ROW 1CD EMERGENCY FLOOR STRIP DAMAGED. R & R ROW 1CD EMERGENCY FLOOR TRACK STRIP IAW CRJ 200 33-51-01, NO FURTHER DEFECTS.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 33,587 hrs · 29,676 cycles

AFT EMERGENCY CEILING LIGHT INOPERATIVE. R & R AFT EMERGENCY CEILING LIGHT BULB. OP'S CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 32,986 hrs · 29,103 cycles

FLAPS FAILED, 22 DEG LT, 20 DEG RT. EMERGENCY DECLARED. TROUBLESHOT FLAP SYSTEM IAW FIM 27-50-00 WITH NO DEFECTS NOTED. PEFORMED OPS TEST OF THE FECU FLAP SYS IAW AMM 27-51-05. OPS CHECKED GOOD.

Part: TORQUE LINK — DISCONNECTED (NLG) · airframe 32,702 hrs · 28,852 cycles

GEAR DISAGREE. NOSE GEAR WOULD NOT COME UP. C/W QRH ALSO WOW INPUT CAUTION MESSAGE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) COMPLIED WITH RIL 2585 AND RO 11/973 TO RETURN THE NOSE GEAR TO SERVICE. (CREW FOUND NLG TORQUE LINKS DISCONNECTED AFTER LANDING) (SDR CLOSED)

Part: DOOR — BINDING (MAIN PAX) · airframe 31,678 hrs · 27,905 cycles

COULD NOT GET MAIN CABIN DOOR TO OPEN UPON ARRIVAL. OPS CHECK OG MAIN CABIN DOOR IAW AMM 52-10-00, OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (CARGO BAY) · airframe 31,000 hrs · 27,313 cycles

CARGO BAY SEAT TRACK CORRODED. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW SRM 51-41-02. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 31,000 hrs · 27,313 cycles

PAX DOOR LOWER FWD INTERCOSTAL ARE CRACKED. REMOVED CRACKED LOWER FWD INTERCOSTAL FROM THE PAX DOOR IAW SRM 51-42-06. DRILLED & INSTALLED NEW SERVICEABLE INTERCOSTAL ON THE PAX DOOR IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: ATTACH FITTING — CORRODED (DOOR FRAME) · airframe 31,000 hrs · 27,313 cycles

PAX DOOR FRAME CLIPS ON BOTTOM END AT FS 320.10, 329.50 AND 338.00 ARE CORRODED. REMOVED 5 CORRODED FRAME CLIPS FROM UPPER (HINGE) SECTION. FIT, DRILLED & INSTALLED 5 NEW FRAME CLIPS ONTO UPPER SECTION OF PAX DOOR IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702. RII FOUND TO BE SATISFACTORY.

Part: CHANNEL — CORRODED (PAX DOOR) · airframe 31,000 hrs · 27,313 cycles

PAX DOOR BOTTOM INSIDE (WITH DOOR IN THE CLOSED POSITION) HAS MINOR CORROSION ON CHANNEL & SEVERAL RIVETS. REMOVED FASTENERS IN AREA & CLEANED AREA OF CHANNEL, FOUND CHANNEL TO BE CORRODED BEYOND REPAIR. REPLACEMENT OF CHANNEL. RII FOUND TO BE SATISFACTORY. (CLOSED)

Part: FRAME — CORRODED (BS 333) · airframe 31,000 hrs · 27,313 cycles

FUSELAGE FRAME AT FS 333.00 HAS SEVERAL AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 25L AND STR 25R.

Part: ISOLATOR — BROKEN (PRESS BULKHEAD) · airframe 31,000 hrs · 27,313 cycles

FS 621.00 PRESSURE BULKHEAD HAS ISOLATOR CRACKED. R & R ISOLATOR IAW SRM 51-42-06. MINOR REPAIR.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 31,000 hrs · 27,313 cycles

FS 484, INTERCOSTAL CLIP IS CRACKED AT LBL 36. REINSTALLED PULLEY MOUNTS IAW CRJ 200 AMM 20-24-00-910-801. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27 AND BL 36 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS. FOUND TO BE SATISFACTORY.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,000 hrs · 27,313 cycles

CARGO FLOOR SUPPORT AT LBL 27 OTBB SIDE HAS MINOR CORROSION AROUND NUTPLATES FROM FS 621 TO FS 559+112. REMOVED LBL 27.0 FLOOR SUPPORT CAP FROM FS 559+112 TO FS 621 IAW SRM 51-42-21. LOCATED AND DRILLED FASTENER HOLES IN SERVICEABLE LBL27 FLOOR SUPPORT CAP IAW SRM 51-40-11. C/W EC/TC REO 601R-53-61-3778 AND REO 601R-53-61-3778. FOUND THE FLOOR SUPPORT FITTING AT FS 621 TO BE CORRODED AND REQUIRES REPLACEMENT. REMOVED THE CORRODED FLOOR SUPPORT FOR REPLACEMENT IAW SRM 51-40-02 AND 51-42-21. INSTALLED SERVICEABLE FLOOR RAIL FITTING AT FS621 LBL27.00 IAW REO 601R-53-61-3778.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,000 hrs · 27,313 cycles

FLOORBEAM AT FS 349.00 HAS CORROSION FROM RBL 27 TO RBL 36. REMOVED FLOORBEAM IAW SRM 51-21-06. REPAIRED FLOORBEAM THREATED FOR CORROSION PREVENTION IAW SRM 51-21-11, SRM 51-25-06 AND SRM 51-25-16. AND REINSTALLED IAW SRM 51-42-13, 51-42-15 AND 51-45-00.

Part: FRAME — CORRODED (BS 333) · airframe 31,000 hrs · 27,313 cycles

FUSELAGE FRAME AT FS 333.00 HAS SEVERAL AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 25L AND STR 25R. FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-00. REMOVED, LOCATED, DRILLED, AND INSTALLED FRAME IAW SRM 51-40-11, 51-42-06 & 51-42-21.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,000 hrs · 27,313 cycles

FS 280 TRANSVERSE BEAM UPPER AFT "J" CHANNEL IS CORRODED FROM LBL 18 TO RBL 36 AT SEVERAL LOCATIONS. FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-00 AND REMOVED CORROSION IAW SRM 51-21-06.

Part: FRAME — CORRODED (BS 319.7) · airframe 31,000 hrs · 27,313 cycles

FUSELAGE FRAME AT FS 319.70 HAS SEVERAL AREAS OF CORROSION BETWEEN STR 25L AND STR 25R. FOUND CORROSION DAMAGE ON FRAME SECTOR AT FS 319.70 BETWEEN STRINGERS 25L AND 25R TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-00. NEW SERVICEABLE FS 319.70 FRAME SECTOR REQUIRES INSTALL. REMOVED FRAME SECTOR AT FS 319.70 IAW SRM 51-42-056 AND SRM 51-42-21. OK TO INSTALL. INSTALLED NEW SERVICEABLE FRAME SECTOR IAW SRM 51-42-06 AND SRM 51-42-21. FOUND TO BE SATISFACTORY.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 31,000 hrs · 27,313 cycles

FS 280 TRANSVERSE BEAM FWD "J" CHANNEL CORRODED FROM LBL 9 TO RBL 9. INSTALLED NEW CHANNEL IAW SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,000 hrs · 27,313 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED & INSTALLED NEW DRAG ANGLE PN 600-31907-17 IAW SRM 51-42-06/-13.

Part: LIGHT — UNSERVICEABLE (CABIN) · airframe 31,000 hrs · 27,313 cycles

PAX DOOR INTERIOR HANDLE "PULL TO EXIT" SIGN WORN. INSTALLED NEW SERVICEABLE PAX DOOR "PULL TO EXIT" BETA LIGHT IAW AMM 33-51-09-400-801. FUNC TEST GOOD IAW AMM 33-51-09-720-801.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,000 hrs · 27,313 cycles

FS 280.0 FLOORBEAM CLIPS CRACKED AT RBL 9 AND LBL 9. REMOVED AND REPLACED FLOORBEAM FWD CLIPS IAW SRM 51-42-21, REO 60R-53-11-2088 & REO 601R-53-11-926.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,000 hrs · 27,313 cycles

RT NR1 POSITION LIGHT INOPERATIVE. INSTALLED NEW LIGHT.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 31,000 hrs · 27,313 cycles

SEAT TRACK CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEBLE SEAT TRACKS IAW AMM 53-01-11-400-802.

Part: UNKNOWN — ODOR (CABIN) · airframe 30,329 hrs · 26,699 cycles

RECEIVED RT PACK HIGH TEMP CAUTION. MESSAGE DURING CLIMB WITH PACK IN MANUAL MODE. FLIGHT ATTENDANT REPORTED A BURNING SMELL/FOG IN THE CABIN. QRH ACTIONS RETURNED TEMP TO NORMAL RANGE, ALL ASSOCIATED CONDITIONS RETURNED TO NORMAL. PERFORMED OPS CHECK OF RT PACK IAW CRJ 200 AMM 21-51-00. COULD NOT DUPLICATE. OPS CHECK OK AT THIS TIME. A/C OK FOR SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (MLG) · airframe 28,770 hrs · 25,283 cycles

ON DEPARTURE,WHEN SELECTING GEAR UP, RECEIVED "GEAR DISAGREE" WARNING MSG. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. CVR CB OPENED ON RETURN TO GATE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED). UPON INSPECTION FAULT CODE S-18 FAR (RT GEAR UPLOCK). ADJUSTED R/T MLG UPLOCK PROX SWITCH IAW AMM 32-32-05. OP CHECK GOOD IAW AMM 32-30-00.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 28,480 hrs · 24,968 cycles

REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548. JC7020037 1/16/10, ITEM: 1. REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548. JC7020037 1/16/10.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 28,480 hrs · 24,968 cycles

LEFT FS 202.75 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548. REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548.

Part: FLAP SYSTEM — FAILED (TE FLAP) · airframe 28,260 hrs · 24,719 cycles

FLAPS FAIL AT 30 DEG ON APPROACH (EMERGENCY DECLARED).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,961 hrs · 24,418 cycles

LOWER EMERGENCY LIGHT IN PAX ENTRY AREA INOP.

Part: DOOR — BINDING (CABIN) · airframe 27,356 hrs · 23,801 cycles

PAX DOOR HARD TO OPEN.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

FS 460 PRESSURE FLOOR HAS MULTIPLE CRACK INDICATIONS NOTED FWD AND AFT SIDE FS 460 RBL 9 AND LBL 9. TEMP REPAIR COMPLIED WITH IAW REO 601R-53-41-884A. THIS SDR WILL REMAIN OPEN PENDING MTC DETERMINATION OF AN APPROPRIATE CORR ACTION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

RIGHT AFT SEAT TRACK AT FS 559.00 - 559.00+80 RBL 9 CORRODED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

RT AFT FUSELAGE, FS 559.00+80 FLOOR SUPPORT PLATE CORRODED BETWEEN RBL 9 AND RBL 27.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

FS 460 PRESSURE FLOOR HAS MULTIPLE INDICATIONS NOTED BETWEEN FWD AND AFT SIDE OF FS 460 BL 0.0 AND RBL 9.0 AND BETWEEN FWD SIDE OF FS 460 BL 0.0 AND LBL 9.0. MULTIPLE INDICATIONS IN ALL THREE AREAS APPROX 3.0 INCH IN LENGTH 90 PERCENT, 50 PERCENT AND 30 PERCENT. ALL AREAS FAILED NDT INSP. COMPLIED WITH EC/TC REO 601R-53-41-884A BY PERFORMING TEMPORARY REPAIRS TO THE PRESSURE FLOOR WEB AT FS 460.0 PER REO 601R-53-41-884 REV.A.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

REAR PRESSURE BULKHEAD HAS AN INDICATION NOTED AT RBL 9.5, WL 84 APPROX .2 INCH IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM 51-41-02

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2 INCH IN LENGTH 90 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED PRESSURE BULKHEAD IAW REO 601R-53-61-1230.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

PRESSURE BULKHEAD INTERCOSTAL FS 621-625 STRINGER 14L IS CRACKED APPROX 1 INCH L.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

LT 621 TO 625 OBLIQUE ANGLE IS CRACKED APPROX .5 INCH L AT STR 14L.

Part: SKIN — DAMAGED (LT WING) · airframe 27,013 hrs · 23,451 cycles

LT WING LOWER PLANK ACCESS HOLE 540CB HAS MULTIPLE HFEC INDICATIONS 0.1 INCH IN LENGTH, 50 PERCENT 80 PERCENT FSH ON THE FWD CRITICAL AREA OF THE LANDING. INDICATIONS ARE MARKED ON THE ACFT. FAILS NDT AT THIS TIME. C/W EC/TC EO 600-57-81 & C/W IAW REO 601R-57-21-030 REV G.

Part: SKIN — DAMAGED (RT WING) · airframe 27,013 hrs · 23,451 cycles

RT WING LOWER PLANK ACCESS HOLE 640FB HAS MULTIPLE HFEC INDICATIONS NOTED ON THE AFT PORTION OF THE LANDING. INDICATIONS ARE APPROX 0.1 INCH IN LENGTH WITH 50 PERCENT 80 PERCENT FSH SIGNALS. AREAS ARE MARKED ON THE AIRCRAFT. FAILS NDT AT THIS TIME. INDICATIONS ARE IN THE CRITICAL AREA OF THE LANDING. C/W EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G.

Part: SKIN — DAMAGED (LT WING) · airframe 27,013 hrs · 23,451 cycles

LT WING LOWER PLANK ACCESS HOLE 540DB HAS MULTIPLE HFEC INDICATIONS 0.1 INCH IN LENGTH, 50 PERCENT 80 PERCENT FSH ON BOTH FWD AND AFT CRITICAL AREAS OF THE LANDING. INDICATIONS ARE MARKED ON THE AIRCRAFT. FAILS NDT AT THIS TIME. C/W EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

RIGHT FS 484 FLOOR SUPPORT INTERCOSTAL PREVIOUS REPAIR ANGLE AT RBL 27 CRACKED .2 INCH LONG.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

FS 460 PRESSURE FLOOR HAS MULTIPLE INDICATIONS NOTED BETWEEN FWD AND AFT SIDE OF FS 460 BL 0.0 AND RBL 9.0 AND BETWEEN FWD SIDE OF FS 460 BL 0.0 AND LBL 9.0. MULTIPLE INDICATIONS IN ALL THREE AREAS APPROX 3.0 INCHES IN LENGTH 90 PERCENT, 50 PERCENT AND 30 PERCENT. ALL AREAS FAILED NDT INSP. REMOVED TORN SEAL FROM PANEL 413AL. INSTALLED NEW SEAL IAW AMM 54-63-01-000-801 AND 54-63-01-400-801.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 27,013 hrs · 23,451 cycles

VERTICAL STAB DRAG ANGLE DIAPHRAGM CRACKED 1.1 INCH LONG ON RT AFT SIDE UNDER RUDDER.

Part: SKIN — DAMAGED (RT WING) · airframe 27,013 hrs · 23,451 cycles

RT WING LOWER PLANK ACCESS HOLE 640CB HAS MULTIPLE HFEC INDICATIONS NOTED ON THE O/B NON-CRITICAL AREA OF THE LANDING. INDICATIONS ARE APPROX 0.1 INCH LONG WITH 50 PERCENT 80 PERCENT FSH SIGNALS. AREAS ARE MARKED ON THE AIRCRAFT. FAILS NDT AT THIS TIME. C/W EC/TC EO 600-57-81 & C/W IAW REO 601R-57-21-030 REV G.

Part: SKIN — DAMAGED (RT WING) · airframe 27,013 hrs · 23,451 cycles

RT WING LOWER PLANK ACCESS HOLE 640DB HAS MULTIPLE HFEC INDICATIONS NOTED ON BOTH FWD AND AFT LANDINGS IN THE CRITICAL AREAS. INDICATIONS ARE APPROX 0.1 INCH LONG WITH 50 PERCENT 80 PERCENT FSH SIGNALS. AREAS ARE MARKED ON THE AIRCRAFT. FAILS NDT AT THIS TIME. C/W EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G.

Part: POST — DAMAGED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

FS 409.0+128 VERTICAL POST RBL 18.0 HAS INDICATION NOTED OUTBOARD SIDE AT WL 69.0 APPROX .2 INCH IN LENGTH 50 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. REMOVED DAMAGED VERTICAL POST PER SRM 51-42-06 AND 51-42-21. 2. FABRICATED REPLACEMENT POST IAW SRM 51-24-21. REF DWG 601R32208. INSTALLED VERTICAL POST AT IAW SRM 51-42-06, 51-42-22, AND C/W EC/TC REO 601R-53-41-889.

Part: POST — DAMAGED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

FS 409.0+128 VERTICAL POST RBL 18.0 HAS INDICATION NOTED OUTBOARD SIDE AT WL 69.0 APPROX .2 INCH IN LENGTH 50 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. REMOVED DAMAGED VERTICAL POST PER SRM 51-42-06 AND 51-42-21. 2. FABRICATED REPLACEMENT POST IAW SRM 51-24-21. REF DWG 601R32208. INSTALLED VERTICAL POST AT IAW SRM 51-42-06, 51-42-22, AND C/W EC/TC REO 601R-53-41-889.

Part: POST — DAMAGED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

FS 409.0+128 VERTICAL POST LBL 18.0 HAS INDICATIONS NOTED INBOARD AND OUTBOARD SIDES AT WL 69.0 APPROX .2 INCH IN LENGTH 50 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. REMOVED DAMAGED VERTICAL POST PER SRM 51-42-06 AND 51-42-21. FABRICATED REPLACEMENT POST IAW SRM 51-24-21. REF DWG 601R32208. INSTALLED VERTICAL POSTIAW SRM 51-42-06, 51-42-22, AND C/W EC/TC REO 601R-53-41-889.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 27,013 hrs · 23,451 cycles

RT FS 559 BULKHEAD WEB HAS INDICATIONS NOTED APPROX .2 INCH IN LENGTH 70 PERCENT FSH O/B OF RBL 9.0, WL 58.70 AND WL 59.10 I/B OF RBL 18.0 APPROX. .5 INCH IN LENGTH 70 PERCENT FSH, AND LT AND RT CAP ANGLE HAS INDICATIONS NOTED AT BL 18 APPROX .2 INCH IN LENGTH 50 PERCENT FSH. ALL AREAS FAILED NDT INSP. C/W EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV C.

Part: WIRE — BROKEN (CABIN) · airframe 26,868 hrs · 23,310 cycles

BROKEN EMERGENCY LIGHT WIRE AT FS 310 FOR WARDROBE.

Part: DOOR — STIFF (MAIN PAX) · airframe 25,298 hrs · 21,911 cycles

THE F/A REPORT THE MAIN DOOR IS UNUSUALLY DIFFICULT TO OPEN. CYCLE PAX DOOR SEVERAL TIMES. NO DEFECT NOTED AT THIS TIME. IAW AMM 52-11-00. (B)

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 23,881 hrs · 20,744 cycles

IN FLIGHT SHORTLY AFTER TAKEOFF, RECEIVED AT PAX OUTER DOOR CAUTION MSG FOLLOWED BY A PAX DOOR WARNING RED MSG. COMPLIED WITH QRH THIRD WRITE UP ON DOOR. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 4814 DEL 50 MINS.

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 23,881 hrs · 20,744 cycles

PAX DOOR WARNING MESSAGE. A/C RETURNED TO YOW AFTER T/O. EMERGENCY EQUIPMENT ON STANDBY. FLT 4568 CX.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 23,837 hrs · 20,705 cycles

CABIN DOOR WON'T OPEN FROM OUTSIDE.

Part: HYDRAULIC SYSTEM — LEAKING (NR 1) · airframe 23,725 hrs · 20,611 cycles

HYDRAULIC SYSTEM NR 1 LOST HYDRAULIC FLUID WHILE IN FLIGHT. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED.

Part: ANCHOR FITTING — CRACKED (AIRSTAIR DOOR) · airframe 23,470 hrs · 20,404 cycles

FWD ASD ANCHOR FITTING CRACKED. REMOVED AND REPLACED FWD ASD ANCHOR FITTING IAW AMM CH 52-10-00. RII SATIFACTORY FOR ANCHOR FITTING REPLACEMENT IAW SP 607.

Part: ANCHOR FITTING — CORRODED (AIRSTAIR DOOR) · airframe 23,494 hrs · 20,422 cycles

FWD ASD ANCHOR FITTING CORRODED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,106 hrs · 20,123 cycles

WARDROBE EMERGENCY EXIT LIGHT STRIP INOP.

Part: UNKNOWN — UNKNOWN (TE FLAPS) · airframe 23,002 hrs · 20,038 cycles

FLAPS FAIL CAUTION MSG AT CRUISE. FOLLOWED QRH (BTMS DID NOT GO RED). EMERGENCY DECLARED. FLT 4319 CX.

Part: STRAP — OUT OF POSITION (AIRSTAIR DOOR) · airframe 22,989 hrs · 20,026 cycles

UNABLE TO OPEN ASD, LCL FOUND DOOR HANDLE STRAP CLOSED IN DOOR.

Part: STEP — CORRODED (PAX DOOR) · airframe 22,833 hrs · 19,903 cycles

LOWER STEP OF PAX DOOR STAIRCASE IS CORRODED.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

RIGHT SILL CORRODED BETWEEN FS 559.00 + 80 TO 559.0 +112.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

CORROSION ON FLOORBEAM BETWEEN FS 559.00 + 80 TO FS 559.00 + 112 RBL 27. [SUP 05-15-07] CORROSION ON FLOOR BEAM BTWN FS 559.00 + 80 TO FS 559.00 +112 RBL 27 REMOVED AS PER 51-21-06. ALODINED, PRIMED AND PAINTED AS PER SRM 51-21-11.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 22,833 hrs · 19,903 cycles

CORROSION FOUND AT SEVERAL PLACES ON PASSENGER DOOR LOWER SILL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

CORROSION ON FLOORBEAM BETWEEN FS 559.00 + 80 TO FS 559.00 + 112 RBL 9. [SUP 05-22-07] CORROSION ON FLOOR BEAM BTWN FS559.00+80 TO FS559.00+112 RBL 9 REMOVED IAW SRM 51-21-06. FOUND BEYOND LIMITS IAW SRM 53-51-43 FIG. 101. REPAIR PREFORMED IAW SRM 53-00-43 REPAIR NR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

CORROSION ON FLOOR SUPPORT STRUCTURE CAP SPLICE AT FS 559.00 + 80 FROM LBL 45 TO RBL 45. CORROSION ON FLOOR SUPPORT STRUCTURE CAP PLICE AT FS 559.00 +80 FROM LBL 45 TO RBL 45. REMOVED AS PER SRM 51-21-06 AND BLENDED AREA. TREATED AS PER SRM (51-21-11)(51-25-06). PAINT APPLED AS PER SRM 51-25-01. MATERIAL THICKNESS .100, MATERIAL REMOVED .005, WITHIN LIMITS AS PER SRM 53-00-00 (FIG 101)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

ANGLE FS 280 LBL 9 TO RBL 9 CORRODED. [SUP 05-15-07] OUT OF LIMITS IAW SRM 53-11-15.ANGLE AT FS 280 LBL 9 TO RBL 9. REMOVED AS PER SRM 51-42-06. INSTALLED ANGLE AT F/S 280 BL9 TO BR9 IAW SRM 51-42-21 ALSO SRM 51-42-13.

Part: PLATE — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

CORROSION ON 3 PLATES BETWEEN FS 574.00 TO 621.00 AND 3 SEALS MISSING. [SUP 05-15-07] CORROSION REMOVED ON 3 PLATES BETWEEN FS 574.00 TO 621.00 IAW SRM 51-21-06. ALODINE APPLIED IAW SRM 51-21-11. FINISH AREA IAW SRM 51-21-16. GASKETS (3) INSTALLED ON 3 PLATES BETWEEN FS 574.00 TO 621.OO IAW SRM 51-41-04. MATERIAL THICKNESS .063, MATERIAL REMOVED .003, WITHIN LIMITS PER SRM 53-00-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

CORROSION ON FLOORBEAM BETWEEN FS 559.00 +112 TO 621 AND LBL 9. [SUP 05-15-07] CORROSION ON FLOOR BEAM BTWN FS 559.00 +112 TO 621 AND LBL 9 REMOVED AS PER SRM 51-21-06. ALODINED AND PRIMED AS PER SRM 51-21-11. PAINTED AS PER SRM 51-21-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

CORROSION ON FLOORBEAM BETWEEN FS 559.00 + TO 621.00 AND LBL 2. [SUP 05-17-07] REMOVED CORROSION AND FOUND OUT OF LIMITS IAW REO 601R-53-00-005. FLOORBEAM FABRICATED AS PER SRM 51-24-36. FABRICATE FLOORBEAM INSTALLED AS PER SRM 51-42-20.

Part: PLATE — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

FLOOR LANDING GEAR PLATE CORROSION BETWEEN FS 559.00 +112 TP 612.00 LBL 45.00 AROUND NUT PLATE HOLES.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

CLIP ON RIGHT AFT FACE BULKHEAD INTERCOSTAL CRACKED FS 621.00. [SUP 05-17-07] REMOVED AND REPLACED IAW REO 601R-53-61-100, AND ASA EO 600-53-174C.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

CORROSION ON FLOOR SUPPORT STRUCTURE CAP SPLICE AT FS 559.00 +112 AND 589.00 FROM LBL 45 TO RBL 45. REMOVED CORROSION AS PER SRM 51-21-06. ALODINED, PRIMED AND PAINTED AS PER SRM 51-21-11. MATERIAL THICKNESS .063", MATERIAL REMOVED .005". WITHIN LIMITS PER SRM 53-00-00 FIG. 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

SEAT RAIL CORRODED AT FS 559.00 + 80 AND RBL 27. [SUP 05-15-07] CORROSION ON SEAT RAIL AT F.S 559.00 +112 RBL 27 REMOVED AS PER SRM 51-21-06. MATERIAL THICKNESS .100, MATERIAL REMOVED .032. OUT OF LIMITS AS PER SRM 53-61-49 FIG 101. NEW SEAT RAIL INSTALLED AT F/S 559.00 +112 RBL 27 AS PER SRM 51-42-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

ANGLE AND CLIP CRACK AT FS 484 LBL 27 AND LBL 36. [SUP 05-15-07] CUTOUT AT CRACKED ANGLE AND CLIP AT FS 484 LBL 27 AND LBL 36 WAS PERFORMED IAW REO 601R-53-41-059. HFEC PERFORMED BY HEATHAIR W/O 36306 IAW REO 601R-53-41-059. NO CRACKS FOUND. AMO 46-90 CRACKED ANGLE AND CLIP AT FS 484 LBL 27 AND 36 WERE REPAIRED IAW REO 601R-53-41-059

Part: ANGLE — DAMAGED (T/E FLAP) · airframe 22,833 hrs · 19,903 cycles

ETNRTC 500-13, AT WS 178 OUTB'D FLAP ANGLE ON THE FLAP AFT SIDE ANGLE CRACKED. [SUP 05-15-07] AFTER FURTHER INVESTIGATION HOLE WAS FOUND TO BE DOUBLE HOLED THRERFORE WAS RWORKED TO INSTALL OVERSIZE FASTENER IAW SRM 51 42 20 , 51 42 06.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 22,833 hrs · 19,903 cycles

CORROSION ON FLOOR ANGLE LT AND RT BTWN FS 409.0 + 128 TO FS 559.00. [SUP 05-15-07] ON FLOOR ANGLE L/H AND R/H. CORROSION REMOVED AS PER SRM 51-21-06. CORROSION PREVENTION AS PER SRM 51-21-11 AND PAINT AS PER SRM 51-21-11. MATERIAL THICKNESS .080, MATERIAL REMOVED .002, WITHIN LIMITS PER SRM 53-41-45 FIGURE 101.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,814 hrs · 19,889 cycles

CAPTAIN`S FLASHLIGHT INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,736 hrs · 19,819 cycles

F/A FLASHLIGHT INOP.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 22,652 hrs · 19,762 cycles

GEAR RETRACTION RECEIVED STEERING INOP MSG FOLLOWED BY GEAR DISAGREE WARNING. NOSE GEAR BOX RED. AIRCRAFT RETURNED TO MKE AFTER T/O. EMERGENCY DECLARED BY TOWER. FLTS 4194, 4356 CX.

Part: COWLING — MISSING (NR 1 NACELLE) · airframe 22,586 hrs · 19,710 cycles

TOP COWLING ON LEFT ENGINE NR 1 MISSING ON POSTFLIGHT. COWLING WAS PRESENT ON PREFLIGHT. IT WAS CHANGED IN MCN MTC OVERNIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 22,355 hrs · 19,549 cycles

EXIT FLOOR SIGN OUT.

Part: LAMP — INOPERATIVE (COCKPIT) · airframe 21,393 hrs · 18,836 cycles

CAPTS CHART HOLDER NEEDS RELAMPED.

Part: DOOR — INOPERATIVE (MAIN PAX) · airframe 21,100 hrs · 18,605 cycles

PAX DOOR WOULD NOT OPEN.

Part: DOOR — STICKS (PAX DOOR) · airframe 20,606 hrs · 18,218 cycles

MAIN PASSENGER DOOR STICKS WHEN TRYING TO OPEN IT.

Part: MECHANISM — MALFUNCTIONED (PAX DOOR) · airframe 20,585 hrs · 18,200 cycles

PAX DOOR DIFFICULT TO OPEN.

Part: WIRE — BROKEN (ENG OIL PRES SYS)

DURING CLIMB OUT, CREW OBSERVED THE LT ENGINE OIL PRESSURE GAUGE FLUCTUATING ERRATICALLY WITHOUT STABILIZING. AT APPROXIMATELY 18,000 FEET THE CREW RECEIVED THE FIRST OIL PRESSURE MASTER WARNING THAT IMMEDIATELY EXTINGUISHED, THEN CAME BACK ON. CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT DIVERTED, WHERE IT LANDED SAFELY. MAINT SERVICED THE LT ENGINE WITH 4 QUARTS OF OIL, AND GROUND RAN THE ENGINE FOR 10 MINUTES WITH NO PRESSURE FLUCTUATIONS. A BROKEN WIRE WAS REPAIRED ON THE PRESSURE TRANSDUCER WITH ALL INDICATIONS SHOWING NORMAL. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: SIGN — INOPERATIVE (EMERGENCY EXIT)

DURING A GROUND INSPECTION, THE LOWER EMERGENCY EXIT SIGN, NEAR THE PASSENGER DOOR ENTRANCE, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LOWER EMERGENCY EXIT SIGN ASSEMBLY, NEAR THE PASSENGER DOOR ENTRANCE, IAW AMM 33-50-00. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A GROUND INSPECTION IN CAE, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — LOOSE (CONTROL PANEL)

FLT 4403 - DURING APPROACH INTO HSV FROM ATL, THE CREW RECEIVED A NOSE GEAR DISAGREE MESSAGE. THE AIRCRAFT PERFORMED A GO AROUND TO COMPLY WITH THE QRH. AN EMERGENCY WAS DECLARED AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY IN HSV. MAINTENANCE FOUND A LOOSE GROUND WIRE TO THE 3B TOGGLE SWITCH ON THE ELECTRIC PUMP CONTROL PANEL ASSEMBLY AND RESECURED THE WIRE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: UPLOCK ROLLER — FROZEN (NLG)

DURING A DESCENT INTO BTR FROM CVG, UPON SELECTING GEAR DOWN THE NOSE WHEEL WAS SLOW TO DEPLOY AND RED INDICATIONS WITH A MASTER WARNING AND A GEAR DISAGREE ORAL WARNING WERE RECEIVED. THE AIRCRAFT PERFORMED A GO AROUND TO COMPLY WITH THE QRH. INITIAL ATTEMPTS TO EXTEND THE GEAR MANUALLY WERE UNSUCCESSFUL. UPON REMOVING THE HYDRAULIC PRESSURE FROM SYSTEM NR 3 THE GEAR EXTENDED. DURING ROLLOUT, THE NOSE WHEEL STEERING WAS LOST. THE AIRCRAFT WAS TOWED TO THE GATE SAFELY. UPON INSPECTION MAINTENANCE FOUND THE UPLOCK ROLLER FROZEN AND ADJUSTED THE ROLLER. MAINTENANCE ALSO REMOVED AND REPLACED THE NOSE LANDING GEAR (NLG) SELECTOR VALVE. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FITTING — BINDING (PAX DOOR)

DURING A GROUND INSPECTION, UPON CLOSING THE PASSENGER DOOR AN OVERBOARD COOL MESSAGE WAS RECEIVED AND THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT FOR THE PURPOSE OF MAINTENANCE REPAIR TO THE PASSENGER DOOR. THE AIRCRAFT WAS FERRIED AND LANDED SAFELY. MAINTENANCE ADJUSTED THE DOOR FRAME SPIGOT FITTING IAW MM. OPS CHECK GOOD, AIRCRAFT OK FOR SERVICE. (K)

Part: SKIN PANEL — CRACKED (LT WING)

DURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER WING PLANK AT WS 148.019 LT SIDE IAW EO. (K)

Part: RIB — CRACKED (RT WING)

DURING A C-CHECK, THE RT MAIN LANDING GEAR WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT MAIN LANDING GEAR WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 IAW EO. (K)

Part: ANGLE — CRACKED (FUSELAGE)

DURING C-CHECK, THE RT OB FS 484 ANGLE AT BL 27 TO 36 IAW EO. (K)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK, THE PASSENGER DOOR AFT FRAME AT FS 338.90 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR AFT FRAME AT FS 338.90 IAW EO. (K)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING AN A-CHECK, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CEILING EMERGENCY LIGHT LAMP. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT)

FLT 4232 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT COVER AT THE FORWARD BULKHEAD BY THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE FORWARD BULKHEAD BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CABLE — INOPERATIVE (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN MCN, THE AFT EMERGENCY FLOOR LIGHT SECTION WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLOOR LIGHT CABLE ASSEMBLY AND CABLE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PSEU — FAILED (MLG)

DURING CLIMB-OUT, AFTER SELECTING THE LANDING GEAR UP, THE CREW RECEIVED A GEAR DISAGREE WARNING AND ASSOCIATED ENGINE INDICATION AND CREW ALERT SYSTEM MESSAGES. THE NOSE GEAR FAILED TO RETRACT BUT THE GEARS WERE CONFIRMED AS BEING DOWN BY THE TOWER. THE CREW REQUESTED EMERGENCY EQUIPMENT BE ON STANDBY AS A PRECAUTION AND THE AIRCRAFT RETURNED, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. MAINTENANCE ALSO PERFORMED A FLIGHT FUNCTIONAL CHECK OF THE LANDING GEAR SYSTEM, CYCLED THE GEAR SEVERAL TIMES AT SPEEDS OF 160-200 KNOTS AND AT VARIOUS PITCH ATTITUDES WITH OUT ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: ANCHOR — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANANCE REMVOED AND REPLACED THE AFT ANCHOR ON THE PASSENGER DOOR, AND ALSO REMOVED AND REPLACED THE DOOR ANCHOR GUIDE SHAFT WHICH WAS WORN. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SPIDER DUCT BRACKET IN THE AFT EQUIPMENT BAY IAW AMM 21-52-00. (M)

Part: HINGE — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE UPPER STEP HINGE ON THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE UPPER STEP HINGE ON THE PASSENGER DOOR IAW ASA EO 600-53-0052A. (M)

Part: SEAL — CORRODED (SERVICE DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE SERVICE DOOR SEAL PLATE WAS FOUND TO BE CORRODED BEYOND LIMTIS. MAINTENANCE IS REMOVING AND REPLACING THE SERVICE DOOR SEAL PLATE IAW ASA EO 600-53-0052A. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE ATTACH ANGLE UNDER THE RIGHT FORWARD FLOOR PANEL INBOARD OF THE SERVICE DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE ATTACH ANGLE UNDER THE RIGHT FORWARD FLOOR PANEL INBOARD OF THE SERVICE DOOR IAW SRM 51-00. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE SKIN RADIUS ON THE RIGHT SIDE AT FS 235 IAW ASA EO 600-53-0122. (M)

Part: SEAL — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE CARGO COMPARTMENT SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT SEAL PLATE IAW SRM 51-00. AIRCRAFT OK FOR SERVICE. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT FS 484 INTERCOSTALS AT BL 27 TO 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT FS 484 INTERCOSTALS AT BL27 TO 36 IAW ASA EO 600-53-0098. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER LEFT AND RIGHT FLOOR SUPPORT ANGLES IAW ASA EO 600-53-0105. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE LEFT AND RIGHT SIDE BRACKETS AT FS 718 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CRACKED BRACKETS AT FS 718 IAW ASA EO 600-53-0067A. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS AND RIG CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DOOR — LACK OF LUBE (MAIN PAX)

DURING A GROUND INSPECTION IN DFW, THE MAIN PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE MAIN PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LINK — WORN (AILERONS)

FLT 4690 - DURING CLIMB-OUT FROM ATL-YUL, AT APPROXIMATELY 5,000 FEET THE CREW NOTICED A CYCLICAL VIBRATION IN THE AIRFRAME WITH THE AIRCRAFT VIBRATING ABOUT 45 TO 60 SECONDS EACH TIME, FOR ABOUT 1 TO 2 SECONDS, WHICH WAS VERY DEEP IN FREQUENCY. WHILE THE CREW WAS COMPLYING WITH QRH PROCEDURES SHORTLY AFTER DISENGAGING THE AUTOPILOT AT APPROXIMATELY 17,000 FEET, THE AIRCRAFT ROLLED VIOLENTLY TO THE RIGHT AND WITHIN 15 TO 30 SECONDS IT ROLLED AGAIN. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CHA, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT INBOARD AND OUTBOARD POWER CONTROL UNIT OUTPUT LINKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)