N833AS

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 36,935 hrs · 32,361 cycles

RT SIDE FWD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: SMOKE WARNING — ILLUMINATED (CARGO BAY) · airframe 36,650 hrs · 32,104 cycles

SMOKE INDICATION , CARGO SMOKE WARNING, BLEW CARGO BOTTLE, AND DIVERTED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,305 hrs · 31,785 cycles

THE EXTERIOR EMERGENCY FLOODLIGHT AFT OF THE RT WING EMERGENCY EXIT IS INOPERATIVE. R & R THE FLOODLIGHT IAW AMM 33-51-21-400-801. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: SKIN — CRACKED (WING) · airframe 36,305 hrs · 31,785 cycles

SKIN FAILS NDT INBD SIDE 50 PERCENT SCREEN HEIGHT .200 X .200. REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K.

Part: SKIN — CRACKED (WING) · airframe 36,305 hrs · 31,785 cycles

SKIN FAILS NDT INBD SIDE APPROX 8" LT 60 PERCENT SCREEN HEIGHT (X .250). REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K.

Part: SKIN — CRACKED (WING) · airframe 36,305 hrs · 31,785 cycles

SKIN FAILS NDT WITH INDICATION ON INBD SIDE OF HOLE 2" L X .200 50 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K.

Part: SKIN — CRACKED (WING) · airframe 36,305 hrs · 31,785 cycles

SKIN FAILS NDT AROUND ENTIRE HOLE. REPAIRED IAW REO 601R-57-21-1992, ECTC EO 600-57-81 AND REO 601R-57-21-030, REV K.

Part: SKIN — CRACKED (WING) · airframe 36,305 hrs · 31,785 cycles

SKIN FAILS NDT MULTIPLE INDICATIONS INBD SIDE OF HOLE 50 PERCENT SCREEN HEIGHT. 1" L X .250. REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K.

Part: ANGLE — CRACKED (LT WING) · airframe 36,305 hrs · 31,785 cycles

LT WING HAS A CRACKED ANGLE JUST FWD & INBD OF MLG. REMOVED 601R10213-11, ANGLE TO REPLACE WITH NEW ANGLE IAW SRM . INSTALLED ANGLE, PN 601R10213-11 IAW SRM 51-42-06, COUNTERSUNK & ALODINED SRM 51-21-00 & 51-40-11.

Part: SKIN — CRACKED (WING) · airframe 36,305 hrs · 31,785 cycles

SKIN FAILS NDT INDICATIONS INBD & OTBD SIDE OF HOLE .500 X .250 70 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K.

Part: SKIN — CRACKED (WING) · airframe 36,305 hrs · 31,785 cycles

SKIN FAILS NDT AFT SIDE OF HOLE .200 X .200, 60 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,305 hrs · 31,785 cycles

FOUND CARGO DOOR LOWER AFT CORNER FUSELAGE SKIN HAS INDICATION NOTED APRPOX .1" IN LENGTH 90 PERCENT FSH AT THIS LOCATION. IT ALSO, HAS PROTRUDING DENT .2" L X .2 W. FAILED NDT INSPECTION. REPAIRED IAW EO NR: CL 600-2B19-53-I00396 AND REO 601R-53-61-5011, REV. MAJOR REPAIR.

Part: STRUCTURE — CRACKED (PUMP ATTACH) · airframe 36,305 hrs · 31,785 cycles

RIGHT BOOST PUMP CUTOUT HOLE FAILS NDT WITH INDICATIONS ON AFT SIDE OF HOLE ON LANDING, GREATER THAN 50 PERCENT SCREEN HEIGHT, APROX 1. ALSO, HAS SMALLER INDICATIONS AROUND ENTIRE HOLE LANDING 10-20 PERCENT SCREEN HEIGHT APROX .1. REPAIRED IAW REO 601R-57-21-1989. MAJOR REPAIR -- SDR CLOSED.

Part: POST — CRACKED · airframe 36,295 hrs · 31,775 cycles

FS 409.128, RBL 18 VERTICAL POST HAD INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69, REPAIRED IAW REO 601R-53-41-889.

Part: TRUNNION — CRACKED (RT MLG) · airframe 36,295 hrs · 31,775 cycles

INDICATION NOTED IN RT SIDE TURNNION FITTING FASTENER HOLE, 6TH HOLE AFT 9 INDICATION NOTED IN TRUNNION FITTING. 60 PERCENT FULL SCREEN HEIGHT AT OTBD SIDE OF HOLE APPROX .20 IN LENGTH, HOLE FAILS NDT. REPAIRED IAW REO NR 601R-57-21-1988.

Part: SKIN — CRACKED (RT WING) · airframe 36,305 hrs · 31,785 cycles

SUSPECT CRACK AT RT WING WS 148.019, EXTENDING OUT FROM A FASTENER. SUSPECTED CRACK IS LOCATED AFT OF THE AFT WING SPAR BESIDE THE PIE PANEL AND DIRECTLY BELOW THE FLAP FLEX SHAFT. ITEM REQUIRES FURTHER INVESTIGATION. REPAIRED IAW SRM 51-42-06, SRM 51-42-21, SRM 51-41-00, & SRM 51-41-04. SDR CLOSED.

Part: POST — CRACKED (BS 409) · airframe 36,295 hrs · 31,775 cycles

FS 409+128, RBL 18 VERTICAL POST HAD INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED POST IAW SRM 51-42-06 AND 51-42-22.

Part: POST — CRACKED (BS 409) · airframe 36,295 hrs · 31,775 cycles

LBL 18 FS 409+128 OTBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .250" LONG X 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED OTBD & INBD VERT POST AT FS 409+128 LBL 18 IAW SRM 51-42-06. LOCATED AND DRILLED NEW POSTS AND 601R32208-315 AND 601R322008-155 IAW SRM 51-40-11. INSTALLED INBD & OTBD VERT POSTS AT FS 409+128 LBL 18 IAW SRM 51-42-06 AND 51-42-22.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 36,295 hrs · 31,775 cycles

SEAT TRACK FS 409 AND 409+128 CORRODED IN SEVERAL AREAS. REMOVED CABIN SEAT TRACK IAW AMM 53-01-11-00-802. LOCATED & INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802 AND SRM 51-40-11.

Part: SKIN — CHAFED (LT AILERON) · airframe 36,295 hrs · 31,775 cycles

LEFT AILERON UPPER FIXED L/E IS CHAFED AT THREE LOCATIONS APPROX 6.0 INCHES LONG, .400 INCHES WIDE AND .012 INCHES DEEP. REPAIRED IAW REO 601R-57-60-013.

Part: ANGLE — CRACKED (BS 484) · airframe 36,295 hrs · 31,775 cycles

BS 484 ANGLE AT RBL 27 IS CRACKED. R & R CRACKED CLIP WITH NEW IAW SRM 51-42-21 AND 51-40-11.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 36,305 hrs · 31,785 cycles

LT WING INBD GROUND SPOILER LOWER INBD SKIN HAS 2 EA DENTS APPROX .100 L X.100 W X .030 D. REPAIRED IAW REO 601R-57-71-382, REV "A".

Part: HINGE — GOUGED (PAX DOOR) · airframe 36,305 hrs · 31,785 cycles

PAX DOOR HINGE HALF ON FUSELAGE HAS ONE GOUGED LUG. LUG IS NEXT TO LAST LUG ON AFT END APPROX .025" L X .004" DEEP. REPAIRED IAW REO 601R-53-21-814, TYPE 1. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 36,295 hrs · 31,775 cycles

SEAT TRACK FS 349 AND FS 409 CORRODED IN SEVERAL AREAS. REMOVED SEAT TRACK IAW 53-01-11-000-802. DRILLED DEBURRED IAW AMM 53-01-11-400-802. INSTALLED NEW SEAT TRACK IAW 53-01-11-400-802. INSTALLED RT SEAT TRACK IAW AMM 53-01-11-400-802.

Part: ANGLE — CORRODED (BS 280) · airframe 36,295 hrs · 31,775 cycles

FS 280.00 FWD J ANGLE IS CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 36,295 hrs · 31,775 cycles

LT BS 484 ANGLE AT LBL 27 IS CRACKED. R & R CRACKED ANGLE WITH NEW IAW SRM 51-42-21 AND 51-40-11.

Part: FLASHLIGHT — INTERMITTENT (COCKPIT) · airframe 35,945 hrs · 31,453 cycles

PILOT FLASHLIGHT WORKS INTERMITTENTLY. R & R CAPTAIN'S FLASHLIGHT IAW AMM 25-61-04, OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 34,009 hrs · 29,696 cycles

EMERGENCY EXIT DOOR LIGHTED SIGN AT ROW 8D INOPERATIVE. R & R LAMP IAW AMM 33-51-13. OPS CHECKED GOOD.

Part: INVERTER — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 34,009 hrs · 29,696 cycles

EMERGENCY EXIT DOOR LIGHTED SIGN AT ROW 8A HALF LIGHT. R & R NR 2 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 32,172 hrs · 28,108 cycles

EMERGENCY LIGHTS FLICKERING. R & R ACCESS BUSS UNDER VOLTAGE RELAY (K1XD) IAW AMM 24-51-27. OPS CHECKED GOOD. OPS CHECK OF EMERGENCY LIGHT SYS IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: CROSSBEAM — CORRODED (BS 349) · airframe 31,464 hrs · 27,450 cycles

CORROSION FOUND ON FS 349 CROSSBEAM AT SERVICE DOOR. REPAIRED IAW REO 601R-53-61-1541.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 31,464 hrs · 27,450 cycles

LOWER EMERGENCY LIGHT AT LT OVERWING EXIT IS INOPERATIVE. TROUBLESHOOT AND FOUND SPLICES ON WIRES MISSING. INSTALLED 2 NEW QUICK DISCONNECT SPLICES ON THE EMERGENCY LIGHT WIRES IAW ESPM CH 20-11-00 AND 20-16-00. PERFORMED OPS TEST OF LIGHTS IAW AMM 33-51-00-710-801. OPS TESTED GOOD.

Part: PRESSURE BLKHD — CRACKED (FUSELAGE) · airframe 31,464 hrs · 27,450 cycles

REAR PRESSURE BULKHEAD IS CRACKED ABOVE CARGO DOOR, OVER AFT TRACK. PRESSURE BULKHEAD REPAIRED IAW ARM 51-52-06.

Part: PRESSURE PANEL — MISREPAIRED (FLOOR) · airframe 31,464 hrs · 27,450 cycles

PRESSURE FLOOR DOUBLER CORRODED AFT OF FS 439.00 RBL43. APPEARS TO BE 10F6 UNDOCUMENTED DOUBLERS INSTALLED ON PRESSURE FLOOR. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3, MINIMUM MATERIAL REMAINING IS .048". R & R DAMAGED DOUBLER IAW REO 601R-53-41-316.

Part: SIGN — INOPERATIVE (CABIN) · airframe 31,464 hrs · 27,450 cycles

RT SERVICE DOOR EXIT SIGN BETA LIGHTS HAS AN LIGHT INTENSITY LESS THAN 100. REMOVED AND REPLACED IAW AMM 33-51-09-400-802. FUNCTIONAL TESTED GOOD IAW AMM TASK 33-51-09-720-801.

Part: SEAT TRACK — CORRODED (BS 559-572) · airframe 31,464 hrs · 27,450 cycles

SHORT SEAT RAIL BETWEEN FS 559.00+112-572.00 AT RBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-944-001.

Part: SEAT TRACK — CORRODED (BS 559-572) · airframe 31,464 hrs · 27,450 cycles

SHORT SEAT RAIL BETWEEN FS 559.00+112-FS572.00 AT LBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-944-001.

Part: FRAME — CORRODED (BS 333 S26-27R) · airframe 31,464 hrs · 27,450 cycles

CORROSION AT FRAME FS 333 STR 26 & 27R. REMOVED CORROSION, FRAME FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS SRM 53-00-00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,464 hrs · 27,450 cycles

SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT RBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-944-001. (CLOSED)

Part: STRUCTURE — CORRODED (BS 349) · airframe 31,464 hrs · 27,450 cycles

CORROSION FOUND AT FS 349 AT PAX DOOR UNDER TEFLON CAP. BLENDED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00.

Part: FRAME — CORRODED (BS 310 S26R) · airframe 31,464 hrs · 27,450 cycles

CORROSION AT FS 310, STR 26R AT FRAME. R & R FS310 FRAME LOWER SECTION IAW SRM 51-42-06 & 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,464 hrs · 27,450 cycles

INBD AND OTBD CLIPS CRACKED AT FS280 LBL9. REMOVED CRACKED CLIPS INBD AND OTBD AT FS 280, LBL9 IAW SRM 51-42-00. INSTALLED NEW CLIPS AT FS 280, LBL9, INBD AND OTBD IAW SRM 51-42-00, PN 601R3113-57. THIS IS A MINOR REPAIR. CAMLOCK AT FS 280 CROSS BEAM REQUIRES INSTALLATION. INSTALLED CAMLOCK AT FS 280 CROSSBEAM IAW SRM 51-42-00. THIS IS A MINOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,464 hrs · 27,450 cycles

INBD AND OTBD CLIPS CRACKED AT FS 280 RBL 9. REMOVED AND INSTALLED IAW SRM 51-42-00.

Part: FRAME — CORRODED (BS 349 S26-27L) · airframe 31,464 hrs · 27,450 cycles

CORROSION AT FS 349, STR 26L & 27 ON FRAME. REMOVED CORROSION IAW SRM 51-21-06 FRAME FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,464 hrs · 27,450 cycles

SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT RBL 27.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-944-001. (SDR CLOSED)

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,464 hrs · 27,450 cycles

SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT LBL 27.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-400-001. (CLOSED)

Part: ANGLE — CORRODED (BS 349) · airframe 31,464 hrs · 27,450 cycles

CORROSION FOUND ANGLE AT FS 349 AT SERVICE DOOR UNDER TEFLON CAP. REMOVED ANGLE & FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-21-06. INSTALLED SERVICABLE ANGLE IAW SRM 51-42-06.

Part: NUT PLATE — CORRODED (DOOR SILL) · airframe 31,464 hrs · 27,450 cycles

PASSENGER DOOR SILL PLATE ANGLE CORRODED. UPON FURTHER INSPECTION FOUND 5 NUT CLIPS ONLY TO BE CORRODED. R & R IAW MINOR REPAIR.

Part: FRAME — CORRODED (BS 319.7) · airframe 31,464 hrs · 27,450 cycles

FRAME CORRODED AT FS319.70, STR 26R. REMOVED FRAME LOWER SECTION IAW SRM 51-42-06 & 51-42-21. DRILLED NEW SECTION OF FRAME & INSTALLED IAW SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 621) · airframe 31,464 hrs · 27,450 cycles

3 INCH SEAT RAIL FWD OF FS 621.00 AT LBL 9.00 HAS CORROSION ON SURFACE IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-944-001. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,464 hrs · 27,450 cycles

SHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT LBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-400-001. (SDR CLOSED)

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,464 hrs · 27,450 cycles

2 EA ISOLATOR MOUNTS ARE CRACKED ON REAR PRESSURE BULKHEAD FS 621.00. LOCATIONS ARE LBL 9.50 2ND FROM WL 73.0 AND LBL 18.00 AT WL 73.00. REMOVED AND INSTALLED ISOLATOR CROMMETS IAW SRM 51-42-13.

Part: LIGHT — CRACKED (CABIN) · airframe 31,464 hrs · 27,450 cycles

FLOOR MOUNT EMERGENCY EXIT FLOOD LIGHT BASE CRACKED. R & R LIGHT BASE IAW AMM 33-51-19-000-801 STEP 3.A ITEM 2, AND 33-51-19-400-801 STEP 3.A ITEM 3. OPS TESTED IAW AMM 33-51-00-710-801. OPS TESTED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,464 hrs · 27,450 cycles

WARDROBE EMERGENCY EXIT LIGHTED SIGN AT FLOOR LEVEL HAS BROKEN WIRE. REPAIRED 2 BROKEN WIRES IAW ESPM CH 20-11-00 AND 20-16-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 31,464 hrs · 27,450 cycles

EMERGENCY LIGHT INOPERATIVE. R & R BURNED OUT LIGHT BULBS ON EMERGENCY LIGHT PANEL ON FWD SERVICE DOOR SIDE TRIM. OPS CHECKED GOOD.

Part: APU — CONTAMINATED · airframe 30,088 hrs · 26,259 cycles

APU AUTO SHUTDOWN AFTER TAKEOFF. ATTEMPTED TO RESTART APU ON DESCENT AND AFTER START WE SMELLED A STRONG ODOR AND SMELLED LIKE FUEL. (EMERGENCY DECLARED) CLEANED OUT DE-ICING FLUID FROM APU FIRE BOX. PERFORMED OPS CHECK OF THE APU SYS. NO MORE DE-ICING FLUID OR FUEL ODOR. OPS CHECK GOOD OF THE APU SYS IAW AMM49-10-00.

Part: WATER SEPARATOR — FAILED (A/C PACK) · airframe 28,980 hrs · 25,270 cycles

EXCESSIVE FOG COMING OUT OF PACKS AT LOW ALT AND ON GROUND. R&R LEFT WATER SEPERATOR IAW AMM 21-51-13. OPS CHECK GOOD. DEFER CLEARED.

Part: A/C PACK — CONTAMINATED · airframe 28,954 hrs · 25,247 cycles

EXCESSIVE FOG FROM PACKS IN FLIGHT DECK AT LOW ALTITUDES AND ON THE GROUND. UPON INSP FOUND NO DEFECTS NOTED IAW AMM 21-51-01.

Part: A/C PACK — CONTAMINATED (LEFT) · airframe 28,954 hrs · 25,247 cycles

EXCESSIVE FOG FROM PACKS IN FLIGHT DECK, AT LOW ALTITUDE AND ON THE GROUND. REPEAT WRITE UP, OBSCURES COCKPIT VISIBILITY. FOUND EXCESSIVE CONDENSATION IN LT PACK, REMOVED MOISTURE, OPS CHECK GOOD IAW AMM 21-51-01.

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 28,411 hrs · 24,770 cycles

NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. PERFORMED EXTENTION AND RETRACTIONS OF NOSE GEAR AND LANDING GEAR. CYCLED THE GEAR 10 TIMES IAW AMM 32-33-00, AND 32-30-00 OPS CHECK GOOD NO DEFECTS NOTED.

Part: TIRE — FAILED (NLG) · airframe 28,345 hrs · 24,709 cycles

REFER TO LOG PAGE 527189-1, RT NOSE TIRE BLEW ON TAKEOFF. (EMERGENCY DECLARED -- TRUCKS STANDING BY AS A PRECAUTION). R & R NLG WHEEL AND TIRE ASSYS IAW IAW AMM 32-42-01. (CLOSED)

Part: PUMP — DEFECTIVE (HYD SYSTEM) · airframe 28,195 hrs · 24,576 cycles

HYD 2 LOW PRESSURE IN FLIGHT WITH FLUID QUANITY 0 PERCENT (EMERGENCY DECLARED -- EMERGENCY PERSONNEL WERE STANDING BY) R & R EDP ON ENGINE 2 ALSO R & R THE RETURN LINE FROM THE EDP TO THE HARD LINE. OPS CHECK GOOD NO DEFECT NOTED IAW AMM 29-11-01. (CLOSED)

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 27,902 hrs · 24,318 cycles

F/A FLASHLIGHT INOP. R &R F/A'S FLASHLIGHT BATTERIES IAW 25-60-00 OK FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 27,673 hrs · 24,091 cycles

ON APPROACH FLAPS FAIL AT 0 DEGREES WHEN SELECTING FLAPS 8 (EMERGENCY DECLARED) C/W EC TC AP 2009-06-12 ACFT OK FOR SVC. CLOSED.

Part: DOOR — STUCK (PAX DOOR) · airframe 27,169 hrs · 23,542 cycles

PAX DOOR COULD NOT BE OPENED FROM INSIDE AIRCRAFT UPON ARRIVAL TO ATL.

Part: DOOR — SLIPPED (PAX DOOR) · airframe 27,166 hrs · 23,539 cycles

PAX DOOR ASST IS SLIPPING AND WON`T OPEN WITHOUT ASSIST. DOOR WOULDN'T OPEN WITHOUT M/X ASST. FLT 5540 DEL 51 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,078 hrs · 23,443 cycles

LEFT OVERWING FLOOR EMERGENCY LIGHT IS INOP.

Part: POST — DAMAGED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

CONTINUED FROM 8724615/125 FS 409+128 VERTICAL POST BL 0.0 RT SIDE HAS INDICATION NOTED AT WL 69.0 APPROX .2 INCHES IN LENGTH 60 PERCENT FSH FAILED NDT INSPECTION.

Part: FITTING — CORRODED (CARGO BAY) · airframe 27,078 hrs · 23,443 cycles

CARGO FLOOR FITTING ON LBL 27 THAT ATTACHES TO THE 621 BULKHEAD HAS SEVERE CORROSION. REMOVED CARGO FLOOR FITTING ON LBL 27 COMMON TO 621 BULKHEAD IAW SRM 51-42-21. REMOVED AND INSTALLED FITTING IAW SRM 51-41-02, 51-42-21. REMOVED 18EA RIVETS FROM FLOORBEAM BOTTOM PLATE TO GAIN ACCESS TO 3EA LOCK FASTENERS IAW SRM 51-42-06. INSTALLED NUTS ON 3EA LOCK FASTENERS IAW SRM 51-42-22. INSTALLED 18EA RIVETS IN FLOORBEAM BOTTOM PLATE IAW SRM 51-42-06.

Part: SEAL PLATE — CORRODED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

FS 309 TO 319 ST 18 OUTBOARD RT SEAL PLATE JUST FWD OF FRAME BRACKET HAS CORROSION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

CONTINUATION FROM CO 7246109, JOB 8724611, OPERATION 255, CARGO FLOOR SUPPORT CAP ANGLE NUT PLATE HOLE CORRODED AT FS 589, LBL 27. C/W EC/TC REO 601R-53-61-3266 AND REO 601R-53-61-3266 REV A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

CARGO FLOOR SUPPORT CAP ANGLE NUT PLATE HOLE CORRODED AT FS 589 LBL 27. OUT OF LIMITS PER SRM 53-61-43 AND SRM 53-00-00. REPAIRED IAW SRM 51-42-36, 51-42-06, 51-42-15, AND REO 601R-53-61-3266A.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

DURING 559 PRESSURE BULKHEAD INSP, 2 INDICATIONS WERE NOTED - 1 AT RBL 9, WL 58.70 APPROX .100 IN LENGTH, THE 2ND NOTED AT RBL 18, WL 59.10 APPROX .100 INCH IN LENGTH. BOTH INDICATIONS 100 PERCENT FULL SCREEN HEIGHT. FAILED NDT INSP. C/W EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV C.

Part: POST — DAMAGED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

FS 409.0+128 VERTICAL POST BL 0.0 RT SIDE HAS INDICATION NOTED AT WL 69.00 APPROX .2 INCH IN LENGTH 60 PERCENT FSH, FAILED NDT INSPECTION. REMOVED VERTICAL POST IAW SRM 51-42-06. FABRICATED REPLACEMENT POST IAW SRM 51-24-21. REF DWG 601R32268. LOCATED & DRILLED NEW RT POST HALF IAW SRM 51-40-11 & SUB ASSEMBLED LT & RT POST HALVES IAW SRM 51-42-06. INSTALLED AT THE 409+128 BULKHEAD. FABRICATED REINFORCEMENT ANGLE FOR UPPER SECTION IAW SRM 51-24-21 REF DWG 601R32208.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .1 INCH IN LENGTH 60 PERCENT FSH FAILED NDT INSPECTION. REMOVED OUTBOARD SEAL PLATE AT FRAME IAW SRM 51-42-06, 51-42-21. REMOVED THE CORRODED BRACKET IAW SRM 51-42-21. LOCATED AND INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-42-21. REINSTALLED O/B RIGHT SILL PLATE IAW SRM 51-42-06 AND 51-42-21.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

FRAME BACK FOR FLOOR AT FS 319.7 STR 18 CORRODED. REMOVED OUTBOARD SEAL PLATE AT FRAME IAW SRM 51-42-06, 51-42-21. REMOVED THE CORRODED RT BRACKET IAW SRM 51-42-21. LOCATED AND INSTALLED NEW SERVICEABLE RT BRACKET IAW SRM 51-42-21. REINSTALLED OUTBOARD RT SILL PLATE IAW SRM 51-42-06 AND 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

FS 484 LBL 36 INTERCOSTAL CRACKED. REMOVED CABLE GUIDE AT LBL 36 IAW SRM 51-42-00. INSTALLED CABLE GUIDE IAW AMM 20-21-00-910-801. REPAIRED INTERCOSTAL IAW REO 601R-53-41-059.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

FS 484 INTERCOSTAL AT LBL 27 CRACKED. REMOVED CRACKED CLIP ON INTERCOSTAL. INSTALLED NEW CLIP IAW SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

FS 460 INTERCOSTAL CRACKED BETWEEN LBL 9 AND LBL 18. REPAIRED INTERCOSTAL IAW REO 601R-41-1013.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 27,078 hrs · 23,443 cycles

FS 460 INTERCOSTAL ATTACHMENT FITTING AT RBL 9 CRACKED IN AFT RADIUS. REMOVED AND REPLACED INTERCOSTAL ATTACHMENT FITTING AT RBL 9 WITH NEW FITTING AND ATTACHED WITH NEW RIVETS AND HI-LITES IAW SRM 51-42-06 AND SRM 51-42-11.

Part: SKIN — CRACKED (RT WING) · airframe 26,606 hrs · 22,990 cycles

CRACK FOUND ON RT LEADING EDGE OF WINGLET TIP APPROX 7 INCHES FROM BOTTOM OF TIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,046 hrs · 22,468 cycles

EMERGENCY FLOOR LIGHT HAS HALF OF AN ORANGE STRIPE INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,685 hrs · 22,145 cycles

F/A FLASHLIGHT DOES NOT WORK.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 2,453,337 hrs · 21,108 cycles

EMERGENCY EXIT LIGHT BY PAX DOOR ON WARDROBE, HAS CRACK ON LENS COVER. REMOVED AND REPLACED FLOOR-LIGHT EMERGENCY FLOODLIGHT LENS COVER IAW AMM 33-51-19. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,428 hrs · 21,010 cycles

LEFT FWD OVERWING EMERGENCY LIGHT INOP.

Part: DOOR — BINDING (PAX DOOR) · airframe 22,826 hrs · 19,668 cycles

F/A REPORTED MAIN CABIN DOOR HARD TO CLOSE AND OPEN.

Part: DOOR — BINDING (PAX DOOR) · airframe 22,692 hrs · 19,568 cycles

MAIN PASSENGER DIFFICULT TO OPEN AND TO LOCK CLOSE. INITIAL ATTEMPT TO OPEN FROM OUTSIDE WAS TOO HARD TO TURN OUTER HANDLE AND UNLOCK DOOR.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 22,677 hrs · 19,548 cycles

PAX DOOR FS 320.10 FRAME IS CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,677 hrs · 19,548 cycles

LEFT INTERCOSTAL AT FS 625 STRINGER 13L CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,677 hrs · 19,548 cycles

LEFT INTERCOSTAL AT FS 625 STRINGER 14L CRACKED.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 22,677 hrs · 19,548 cycles

LEFT FS 640 BONDED SKIN DOUBLER IS CRACKED AT WL 120, 1 INCH BELOW STRINGER 9L. COMPLIED WITH EC/TC REO 601R-53-61-506 ON LT BONDED SKIN DOUBLER, 1EA 409B ATTACHED TO DOCUMENT STEP SIGN OFFS. SUPPLEMENTAL - SDR CLOSED 08/07/07.

Part: ANGLE — CRACKED (BS 280) · airframe 22,677 hrs · 19,548 cycles

THE 280 AFT ANGLE COMMON TO THE EMERGENCY RELEASE CABLE O/B OF LBL 9 IS CRACKED.

Part: HANDLE — MALFUNCTIONED (EMERGENCY EXIT) · airframe 22,677 hrs · 19,548 cycles

CREW ESCAPE HATCH OUTER HANDLE DOES NOT LATCH PROPERLY. 10-18-07 REPAIRED AFT DRAG ANGLE ON PAX DOOR IAW REO 601R-52-11-513.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,682 hrs · 19,555 cycles

AFT DRAG ANGLE ON PAX DOOR IS CRACKED.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 22,677 hrs · 19,548 cycles

ATTACH ANGLE FOR RB 2 ON AFT SIDE OF MID SPAR IS CRACKED UNDER ACCESS PANEL 325AL ON VERTICAL STABILIZER. [08-07-07] PERFORMED FPI OF ATTACH ANGLE FOR R/B NR 2 ON AFT SIDE. NO DEFECTS NOTED PER CRJ 200 NDTM 51-20-08.

Part: ATTACH FITTING — CRACKED (BS 4848) · airframe 22,677 hrs · 19,548 cycles

FS 484 RIGHT I/B CLIP CRACKED UNDER FLOOR PANEL 262 DRF. PERFORMED FPI ON FS 484.00 R/H I/B CLIP UNDER 263DRF. DEFECTS NOTED PER CRJ 200 NDTM 51-20-28. REMOVED DAMAGED CLIP FROM RT I/B FS 484, FABRICATED NEW SERVICEABLE CLIP USING, .063, 2024-T3, PO# 950028, LOCATED AND DRILLED HOLES, ALODINED, PRIMED, AND PAINTED IAW CRJ SRM 51-25-16. INSTALLED NEW SERVICEABLE CLIP. ALL WORK DONE IAW ASA REO 601R-53-41-059.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,682 hrs · 19,555 cycles

FS 484 RIGHT INTERCOSTAL O/B SIDE UNDER FLOOR PANEL 262DRF CRACKED.

Part: ACCESS PANEL — CRACKED (EXHAUST NOZZLE) · airframe 21,555 hrs · 18,692 cycles

LEFT EXHAUST NOZZLE FAIRING ACCESS PANEL AT 6:00 POS INNER DOUBLER IS CRACKED.

Part: ACCESS PANEL — CRACKED (EXHAUST NOZZLE) · airframe 21,555 hrs · 18,692 cycles

LEFT EXHAUST NOZZEL FAIRING ACCESS PANEL AT 9:00 POS, INNER DOUBLERS IS CRACKED.

Part: TRACK — DAMAGED (CABIN) · airframe 20,581 hrs · 17,939 cycles

EMERG LIGHT TRACK DAMAGED AT ROW 8.

Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 20,321 hrs · 17,713 cycles

APU FIRE FAULT MSG WITH APU FAULT MSG, SHUT APU DOWN MSG CLEARED.

Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 20,178 hrs · 17,593 cycles

REF AFDL 285420 ITEM 1, RECEIVED APU FIRE WARNING SHORTLY AFTER APU START ON DESCENT. FOLLOWED QRH. MESSAGE EXTINGUISHED

Part: WARNING SYSTEM — ACTIVATED (APU) · airframe 20,120 hrs · 17,547 cycles

APU AUTO SHUT DOWN IN FLT WITH TRIPLE CHIME AND FIRE WARNING, APU DOOR REMAINED CLOSED, FIRE WARNING MSG CLEARED AFTER APU SHUTDOWN. FLT 4083 DEL 40 MINS.

Part: STEP — CRACKED (AIR STAIR DOOR) · airframe 20,012 hrs · 17,458 cycles

LWR PAX DOOR STEP IS CRACKED. FLT 4680 DEL 22 MINS.

Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 20,007 hrs · 17,453 cycles

APU FIRE MSG, APU FAULT, APU AUTO SHUTDOWN HAS HISTORY, FLT 4592 DEL 55 MINS.

Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 19,985 hrs · 17,433 cycles

APU FIRE INDICATION GOING INTO BNA, CAPT FOLLOWED QRH SHUT APU DOWN AND MSG CLEARED, BOTTLE WAS NOT USED, FALSE FIRE WARNING, NO EMERGENCY DECLARED, FLT 4346 DEL 45 MINS.

Part: FIRE WARNING — FALSE ACTIVATION (APU SYS) · airframe 19,972 hrs · 17,420 cycles

APU AUTO SHUTDOWN (FALSE FIRE WARNING, NO EMERGENCY DECLARED)

Part: FIRE WARNING — ILLUMINATED (APU) · airframe 19,703 hrs · 17,232 cycles

ON APPROACH TO LEX. APU OVER TEMP FOLLOWED BY APU FIRE WARNING MSG, APU AUTO SHUTDOWN DECLARED AN EMERGENCY... FLT 4161 DEL 36 MINS

Part: BATTERY PACK — DISCHARGED (FUSELAGE)

DURING A GROUND INSPECTION, THE LT AND RT SIDE, MIDDLE SECTION, EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.(K)

Part: SHEAR PIN — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT CLOSE AND LOCK. MAINTENANCE REMOVED AND REPLACED A BROKEN SHEAR PIN IN THE DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SIGN — CRACKED (GALLEY)

DURING C-CHECK, THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR IAW AMM. (K)

Part: SEAT TRACK — CORRODED (BS 559+64)

DURING C-CHECK, THE LT SIDE WALL SEAT RAIL (TRACK) AT FS 559 +64 ABOVE THE BLOWOUT PANEL WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT SIDE WALL SEAT RAIL (TRACK) AT FS 559 +64 IAW SRM. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT IB AND RT OB FS 280 CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT OB AND RT IB FS 280 CLIPS IAW SRM. (K)

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

DURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TO 559 RBL 36 AND 45. MAINTENANCE HAS SUBMITTED A DAMAGE REPORT AND IS AWAITING REO FOR REPAIR. THIS MRR WILL REMAIN OPEN UNTIL THE PROPER DOCUMENTATION IS OBTAINED AND THE REPAIR CAN BE COMPLIED WITH. (K)

Part: FLOOR PANEL — CORRODED (FUSELAGE)

DURING C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559, RBL 36 AND 45. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559, RBL 36 AND 45 IAW EO. (K)

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

DURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMIT ON THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559 RBL 36 AND 45. MAINTENANCE HAS SUBMITTED A DAMAGE REPORT AND IS AWAITING AN REO FOR REPAIR. THIS MRR WILL REMAIN OPEN UNTIL THE PROPER DOCUMENTATION IS OBTAINED AND THE REPAIR CAN BE COMPLIED WITH. (K)

Part: FLOOR PANEL — CORRODED (COCKPIT)

DURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TOO 559 RBL AND 36 AND 45. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TO 559, RBL 36 AND 45 IAW EO. (K)

Part: INTERCOSTAL — CRACKED (BS 280)

DURING C-CHECK, THE INTERCOSTAL AT FS 280, RBL 9 OB OF THE CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTAL AT FS 280, RBL 9 IAW EO. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK, THE AFT FLOOR SUPPORT ANGLES FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CORRODED FLOOR SUPPORT ANGLE IAW EO. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FORWARD FLOOR SUPPORT ANGLE FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND CORRODED BEYOND LIMITS. (K)

Part: LENS — CRACKED (GALLEY)

DURING C-CHECK, THE EMERGENCY EXIT LIGHT LENS COVER ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS COVER ABOVE THE SERVICE DOOR. (K)

Part: PANEL — CRACKED (WING)

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

Part: DOUBLER — CRACKED (FUSELAGE)

DURING C-CHECK, THE RT FS 718 DOUBLER AT STRINGER 10-12 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT FS 718 DOUBLER AT STRINGER 10-12 RT IAW EO. (K)

Part: FRAME — CRACKED (FUSELAGE)

DURING C-CHECK, THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE IAW EO. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A C-CHECK, THE LT AND RT OVERWING EMERGENCY EXIT BETA LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT AND RT OVERWING EMERGENCY EXIT BETA LIGHTS. OPS CHECK GOOD. (K)

Part: HANDLE — DAMAGED (PAX DOOR)

DURING A C-CHECK, THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR HANDLE WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT BETA LIGHT ON THE PASSENGER DOOR. (K)

Part: DOOR — STIFF (PAX)

DURING A C-CHECK, THE PASSENGER DOOR WAS FOUND HARD TO OPEN FROM THE INSIDE AND OUTSIDE. MAINTENANCE RE-RIGGED THE PASSENGER DOOR OUTER HANDLE IAW MM. OPS CHECK GOOD. (K)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAME AND DOUBLER AT FS 718, STRINGER 10-12 LT SIDE IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT OB AND RT IB FS 280 CLIPS WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT OB AND RT IB FS 280 CLIPS IAW SRM. (K)

Part: WARNING SYSTEM — MALFUNCTIONED (APU FIRE)

FLT 4319 - DURING DESCENT INTO BQK FROM ATL, APPROXIMATELY ONE MINUTE AFTER STARTING THE AUXILIARY POWER UNIT AN APU FIRE FAIL AMBER CAUTION MESSAGE WAS RECEIVED. APPROX TWO SECONDS LATER THAT MESSAGE EXTINGUISHED AND THEN AN APU FIRE RED WARNING MESSAGE AND THE FIRE BELL WERE RECEIVED WHICH WENT OUT APPROXIMATELY ONE SECOND LATER, FOLLOWED BY THE APU AUTOMATICALLY SHUTTING DOWN. THE QRH WAS COMPLIED WITH AND THE AIRCRAFT LANDED SAFELY IN BQK. UPON INSPECTION MAINTENANCE FOUND NO INDICATIONS OF AN APU FIRE. MAINTENANCE DEFERRED THE APU UNDER MEL NR 49-10-01B, CAT C, EXPIRING 6/24/05. AIRCRAFT OK FOR SERVICE. (M)

Part: CIRCUIT CARD — MALFUNCTIONED (OVERHEAT LOOP)

DURING DESCENT, THE CREW RECEIVED AN AUXILIARY POWER UNIT (APU) OVERTEMP MESSAGE. DURING COMPLIANCE WITH THE QRH, AN APU FIRE WARNING WAS RECEIVED AT WHICH TIME THE CREW DISCHARGED THE APU FIRE BOTTLE FOLLOWED BY ALL INDICATIONS GOING AWAY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. UPON LANDING, THE AC WAS INSPECTED BY THE FIRE CREW WITH NO EVIDENCE OF A FIRE, FOUND; THEN PROCEEDED TO THE GATE SAFELY. UPON INSPECTION OF THE AIRCRAFT BY MAINTENANCE, NO EVIDENCE OF A FIRE, FUEL OR OIL LEAKS WERE FOUND. MAINTENANCE REMOVED AND REPLACED THE APU FIRE AND OVERHEAT CONTROL CARD NR 3 AND THE APU FIRE BOTTLE. OPS CHECK GOOD. AC OK FOR SERVICE. (K)

Part: FIRE WARNING — FALSE ACTIVATION (APU BAY)

DURING DESCENT, THE CREW RECEIVED AN AUXILIARY POWER UNIT (APU) OVERTEMP MESSAGE. DURING COMPLIANCE WITH THE QRH, AND APU FIRE WARNING WAS RECEIVED AT WHICH TIME THE CREW DISCHARGED THE APU FIRE BOTTLE FOLLOWED BY ALL INDICATIONS GOING AWAY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. UPON LANDING THE AIRCRAFT WAS INSPECTED BY THE FIRE CREW WITH NO EVIDENCE OF A FIRE FOUND. THEN PROCEEDED TO THE GATE SAFELY. UPON INSPECTION OF AC BY MAINTENANCE, NO EVIDENCE OF A FIRE, FUEL OR OIL LEAKS WERE FOUND. MAINTENANCE REMOVED AND REPLACED THE APU FIRE AND OVERHEAT CONTROL CARD NR3 AND THE APU FIRE BOTTLE. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K)

Part: FIRE WARNING — FALSE ACTIVATION (APU BAY)

DURING DESCENT, THE CREW RECEIVED AN APU FIRE WARNING. THE QRH WAS COMPLIED WITH AND THE MESSAGE EXTINGUISHED PRIOR TO DISCHARGING THE APU FIRE BOTTLE. THE TOWER DECLARED AN EMERGENCY AND THE AIRCARFT LANDED SAFELY. EMERGENCY VEHICLES MET AND FOLLOWED THE AIRCRAFT TO THE GATE AS A PRECAUTION. MAINTENANCE INSPECTED THE AFT EQUIPMENT BAY, AUXILIARY POWER UNIT (APU) ENCLOSURE AND PERFORMED A SYSTEM TEST. NO DEFECTS WERE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: ODOR — DETECTED (COCKPIT)

DURING TAKEOFF AND LANDING, THE CREW NOTICED A HOT BRAKE ODOR. THE AC LANDED SAFELY. MAINTENANCE JACKED THE MAIN LANDING GEARS WITH BRAKES RELEASED. BOTH IB AND OB BRAKES OPERATED FREELY AND ALL GEAR INDICATIONS WERE GOOD. MAINTENANCE ALSO TESTED THE ANTI-SKID SYSTEM. NO DEFECTS WERE NOTED. AIRCRAFT OK FOR SERVICE. (K)

Part: FIRE BOTTLE — BLOWN (APU BAY)

DURING DESCENT, APPROXIMATELY 30 TO 40 SECONDS AFTER THE CREW STARTED THE CREW STARTED THE AUXILIARY POWER UNIT (APU), APU FIRE WARNING AND APU FAULT CAUTION MESSAGES WERE RECEIVED. THE QRH WAS COMPLIED WITH AND THE FIRE WARNING MESSAGE EXTINGUISHED BEFORE THE FO PUSHED THE APU FIRE SWITCH. THE AIRCRAFT LANDED SAFELY. MAINTENANCE CLEARED THE DEFERRAL (DML NR 66488) BY REMOVING AND REPLACING THE APU FIRE BOTTLE AND FIRE BOTTLE CARTRIDGE. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: DOOR — LACK OF LUBE (PAX)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE INSPECTED THE PASSENGER DOOR PANELS, LUBRICATED THE DOOR PIVOT POINTS AND CYCLED THE DOOR SEVERAL TIMES. NO DEFECTS WERE NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: HANDLE — BINDING (PAX DOOR)

FLT 4226 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LEVER — BINDING (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS HARD TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR RELEASE LEVER AND OPEN LOCK MECHANISM. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE FORWARD PASSENGER AND SERVICE DOOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHTS POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR FRAME SILL AT FS 340 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR FRAME SILL AT FS 340 IAW SRM 51-00. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD CLIPS AT FS 484, LBL 27 AND RBL 27 IAW ASA EO 600-53-0098. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR CUT OUT AT FS 235 IN BOTH CORNERS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE NOSE LANDING GEAR CUT OUT AT FS 235 IN BOTH CORNERS IAW ASA EO 600-53-0104. (M)

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE EMERGENCY LIGHT WIRING AT FS 461, RBL 9 WAS FOUND DAMAGED. MAINTENANCE REPAIRED THE EMERGENCY LIGHT WIRING AT FS 461.00, RBL 9. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT THE PILOTS BULKHEAD FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AND OUTBOARD CLIPS AT THE PILOTS BULKHEAD FS 280, LBL 9 AND RBL 9 IAW SRM 51-00. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT SIDE AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT SIDE AFT BULKHEAD FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: PLATE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO THRESHOLD FLOOR LANDING PLATE AT FS 589 AND FS 605 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO THRESHOLD FLOOR LANDING PLATE AT FS 589 AND FS 605 IAW ASA EO 600-53-0117. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE LOWER STEP ON THE PASSENGER DOOR. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FRAME FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FRAME FS 640 BETWEEN STRINGERS 9 AND 12 ON THE RIGHT SIDE IAW ASA EO 600-53-0075. (M)

Part: CLIP — BINDING (PAX DOOR)

FLT 4801 - AT THE GATE AFTER LANDING IN ATL FROM FAY, THE CREW WAS UNABLE TO OPEN THE MAIN PASSENGER DOOR. RAMP PERSONNEL OPENED THE DOOR FROM THE OUTSIDE AND THE PASSENGERS DEPLANED SAFELY. MAINTENANCE ADJUSTED THE OUTER DOOR HANDLE PUSH BUTTON SPRING CLIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LINKAGE — LACK OF LUBE (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS HARD TO CLOSE. MAINTENANCE CLEANED AND LUBRICATED THE INTERNAL LINKAGE ON THE PASSENGER DOOR. NO OTHER RESISTANCE NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — BINDING (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND DIFFICULT TO CLOSE AND SECURE FROM THE INSIDE. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE AND RE-SEATED THE BEARING ON THE LOWER RIGHT ROLLER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING SCHEDULED MAINTENANCE IN MCN, THE ENTRANCE EMEGENCY LIGHT ON THE FORWARD WALL WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACD THE INOPERATIVE EMERGENCY LIGHT LAMP. AIRCRAFT OK FOR SERVICE. (M)

Part: LATCH — LACK OF LUBE (CABIN)

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

Part: LATCH — OUT OF ADJUST (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE ADJUSTED THE LATCH MECHANISM DOOR LINKAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PUSHROD — OUT OF ADJUST (PAX DOOR)

FLT 4497 - AFTER LANDING IN DFW, THE MAIN PASSENGER DOOR WOULD NOT OPEN FOR DEPLANING. MAINTENANCE OPENED THE PASSENGER DOOR AND DEPLANING WAS COMPLETED SAFELY. MAINTENANCE ADJUSTED THE PASSENGER DOOR INNER HANDLE PUSH ROD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (FUSELAGE)

DURING AN A-CHECK IN BTR, THE RIGHT EXTERIOR EMERGENCY LIGHT AFT OF THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT LAMP AFT OF THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE CENTER ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REINSTALLED THE ANGLES FROM THE TOP AND BOTTOM OF THE BEAM TO COMPLY WITH HFEC INSPECTION WHICH WAS COMPLETED. NO CRACKS WERE FOUND. MAINTENANCE WILL REPAIR THE CRACKED CENTER ENGINE SUPPORT BEAM IAW REO 601R-53-61-345. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE, THE LEFT AND RIGHT SIDES OF THE FRAME AT FRAME STATION 718 WERE CRACKED BETWEEN STRINGERS 10 AND 12. MAINTENANCE REPAIRED THE CRACKED FRAME IAW ASA EO 600-53-0067. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR FS 718 CRACKS ON CRJ200 AIRCRAFT USING REO 601R-53-61-193, REO 601R-53-61-492, SRM 51-00 REV 14, AND SRM 53-00 REV 14 AS REFERENCES. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, THE ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED ON BOTH THE RIGHT AND LEFT SIDES. MAINTENANCE REPAIRED THE CRACKED ENGINE SUPPORT BEAM IAW REO 601R-53-61-366. (M)

Part: FRAME — CRACKED (FUSELAGE)

WHILE COMPLYING WITH ASA EO 600-53-0069, INSPECTION OF FRAME STATION 640 AT BASE LINE 45, THE FRAME WAS FOUND TO BE CRACKED BETWEEN STRINGERS 13 AND 14. MAINTENANCE WILL REPAIR THE CRACK IN THE FRAME IAW CNDAIR SRM 53-61-15. (M)

Part: SELECTOR VALVE — MALFUNCTIONED (MLG WW)

FLT 4749 - ON FINAL APPROACH INTO DFW, THE NOSE GEAR EXTENDED NORMALLY, BUT THE MLG WOULD NOT. THE CAPTAIN PERFORMED AN EMERGENCY GEAR EXTENSION AND THE GEAR CAME DOWN AT THAT TIME AND ALL GEAR INDICATIONS SHOWED DOWN AND LOCKED. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT HAD AN UNEVENTFUL LANDING IN DFW. MAINTENANCE REMOVED AND REPLACED THE MLG SELECTOR VAVLE. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING GROUND INSPECTION IN ATL, CREW FOUND GREEN FLOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE FORWARD GREEN EMERGENCY TRACK LIGHTING SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

FLT 4768 - DURING GROUND INSPECTION AT MYR, MAINTENANCE DISCOVERED 1 CABIN FLOOR PATH LIGHTING STRIP AT ROW 7 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TWO BROKEN CABLE ASSEMBLIES, ONE AT ROW 7 AND ONE AT ROW 13. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4451 - DURING FLIGHT FROM DFW-AUS, FIRST OFFICERS WINDSHIELD CRACKED. AIRCRAFT RETURNED TO DFW AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4576 - DURING INSPECTION, FOUND FIRST SECTION OF EMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CABLE ASSEMBLY FOR EMERGENCY LIGHTS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (CABIN)

FLT 4505 - DURING INSPECTION, FOUND FRONT HALF OF EMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: TRANSMITTER — INOPERATIVE (LEFT ENGINE)

FLT 4739 - IN CRUISE AT FL 410, CREW RECEIVED LEFT ENGINE OIL PRESSURE MESSAGE AS WELL AS LEFT ENGINE OIL PRESSURE LESS THAN 25 PSI AND 'RED' IN COLOR. CREW PROCEEDED WITH LEFT ENGINE OIL PRESSURE MESSAGE EMERGENCY CHECKLIST. WITH ADVANCEMENT OF LEFT TRUST LEVER, THERE WAS NO CHANGE IN OIL PRESSURE. CREW COMPLETED SINGLE ENGINE PROCEDURES, DECLARED AN EMERGENCY, AND REQUESTED FIRE TRUCKS AND EMERGENCY EQUIPMENT. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REPLACED THE LEFT ENGINE OIL PRESSURE TRANSMITTER. LEAK AND OPERATIONAL CHECK WERE GOOD AFTER GROUND RUNS. AIRCRAFT RETURNED TO SERVICE. (X)

Part: FECU — MALFUNCTIONED (TE FLAPS)

ATL/DTW - FLT 4626 - EXPERIENCED 'FLAP FAIL' MESSAGE ON EICAS DURING VISUAL APPROACH TO DTW. CREW PERFORMED GO-AROUND, DECLARED AN EMERGENCY AND LANDED ZERO FLAPS WITH NO FURTHER PROBLEMS. MTC CNTL INSTRUCTED CREW TO RESET CIRCUIT BREAKERS AND UPON RESET, MESSAGE CLEARED. AIRCRAFT POSITIONED TO MCN FOR A FLAP RIGGING CHECK. MCN MAINTENANCE PERFORMED A DIAGONISTIC CHECK OF THE FECU AND FOUND 5 FAULT CODES AND 3 LRU CODES. MAINT COMPLETED AN OPERATIONAL CHECK OF THE FECU, RIGGING CHECK OF THE BPSU, AND INSPECTED THE FLAPS FOR TWISTING, SKEWING OR ABNORMAL DEFORMATION. C/W AD98-20-1. ALL OPERATIONAL CHECKS WERE COMPLETED SATISFACTORILY, NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X)