N832AS

Part: SENSOR — FAILED (NLG) · airframe 36,811 hrs · 32,387 cycles

GEAR DISAGREE MESSAGE DURING SELECTION OF GEAR UP. COMPLETED WITH QRH, MANUALLY EXTENDED GEAR. NOSE GEAR DID NOT SHOW UP AND LOCKED DURING THE GEAR DISAGREE. ALL GEAR SHOWED DOWN AND LOCKED AFTER MANUEL EXTENSION TO LANDING. RETURNED TO DEPARTURE, R & R NLG FOR GEAR DISAGREE WARNING DMIL. CLEARED ACFT FOR OK FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 202) · airframe 36,376 hrs · 31,997 cycles

BS 202 BULKHEAD IS CRACKED. CUT OUT AND REMOVED ALL CRACKS FROM 202 BULKHEAD AND REMOVED ALL BURRS IAW STEP 1 AND STEP 2 OF REO 601R-53-11-563, REV C. FABRICATED AND DRILLED TO FULL SIZE ALL REPAIR PARTS IAW REO 601R-53-11-563, REV C FAY SEALED ALL REPAIR PARTS , WET INSTALLED ALL FASTENERS COMMON TO REPAIR AREA IAW REO 601R-53-11-563, REV C. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: HEAT EXCHANGER — DENTED (CABIN AIR) · airframe 36,029 hrs · 31,679 cycles

CLIMBING THROUGHT FL210, ALL AIRFLOW FROM GASPERS STOPPED CABIN STARTED TO SLOWLY CLIMB. WE STARTED A EMERGENCY DESCENT AND RETURN TO DEPARTURE. REPEAT WRITE UP. ACFT RETURNED TO DEPARTURE AFTER T/O. R & R HEAT EXCHANGER IAW AMM 21-51-07, ITEM 45B (21-51-00). OPS CHECK GOOD, NO DEFECTS FOUND AT THIS TIME.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 35,922 hrs · 31,582 cycles

RT LOWER EMERGENCY EXIT LIGHT AT EMERGENCY EXIT IS INOPERATIVE. R & R RT LOWER EMERGENCY EXIT LIGHT AT OVERWING EMERGENCY EXIT IAW AMM 33-51-10-400-801. OPS CHECKED GOOD.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 35,922 hrs · 31,582 cycles

CRACK INDICATION NOTED POSSIBLY CORROSION ON THE LT WING LOWER PLANK ACCESS HOLE LANDING FOR PANEL 550FB, 65 PERCENT FULL SCREEN HEIGHT FAILING NDT. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV J.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,922 hrs · 31,582 cycles

UPPER FUSELAGE ADF ANTENNA CUTOUT HAS FRETTING DAMAGE AROUND CIRCUMFERENCE AND SCREW HOLES APPROX 6" L X .125 W X .005 AT WORST LOCATION. REPAIRED IAW BSC EO CL600-2B19-53-I00360, REV A.

Part: BULKHEAD — CRACKED (BS 621) · airframe 35,922 hrs · 31,582 cycles

FS 621 BULKHEAD, LBL 18 FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT BETWEEN WL 117.5 AND 118.5. REPAIRED IAW SRM 51-42-06, 51-41-04 AND REO 601R-53-61-1285, REV D DATED 10/31/2011.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 35,922 hrs · 31,582 cycles

EMERGENCY LIGHT COVER CRACKED. REMOVED AND INSTALLED NEW EMERGENCY LIGHT COVER IAW MM 41-10, 33-60-13.

Part: SUPPORT ANGLE — CRACKED (BS 621) · airframe 35,922 hrs · 31,582 cycles

FS 621 CARGO DOOR BEAM BOTTOM SUPPORT ANGLE IS CRACKED. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE BRACKET ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 280) · airframe 35,922 hrs · 31,582 cycles

FS 280, LBL 9.0 INBD SUPPORT ANGLE CRACKED. REPAIRED IAW SRM 51-42-21, 51-20-06, REO 601R-53-11-726 AND REO 601R-53-11-926.

Part: BULKHEAD — CRACKED (BS 621) · airframe 35,922 hrs · 31,582 cycles

FS 621 BULKHEAD, LBL 27.50 FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT BETWEEN WL 104 AND 110. REPAIRED IAW REO 601R-53-61-1285, REV D DATED 10/31/2011.

Part: BULKHEAD — CRACKED (BS 621) · airframe 35,922 hrs · 31,582 cycles

FS 621 BULKHEAD FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT BL 0 BETWEEN WL 109 AND 111. REPAIRED IAW SRM 51-41-04 AND REO 601R-53-61-1285, REV D, DATED 10/31/2011.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 35,922 hrs · 31,582 cycles

CARGO COMPARTMENT RT FLOOR SUPPORT HAS MINOR CORROSION AROUND FASTENER HOLES FROM FS 559+80 TO 559+112. COMPLIED WITH REO 601R-53-00-526. REMOVED FLOOR SUPPORT IAW SRM 200 51-41-00-00 AND 51-42-06-00. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPORT IAW SRM 51-40-11, 51-42-06, 51-42-15 AND 51-42-21.

Part: BULKHEAD — CRACKED (BS 621) · airframe 35,922 hrs · 31,582 cycles

FS 621 BULKHEAD LBL 27.50 FAILS NDT WITH INDICATION FULL SCREEN HEIGHT AT UPPER CARGO TRACK WL 131. REPAIRED IAW SRM 51-42-06 AND REO 601R-53-61-1541, REV D DATED 10/31/2011.

Part: BULKHEAD — CHAFED (BS 621) · airframe 35,922 hrs · 31,582 cycles

FS 621 BULKHEAD HAS SIX CHAFED AREAS AT WL 102: LBL 27.5-RBL 36.20. REPAIRED IAW REO 601R-53-61-2155.

Part: BULKHEAD — CRACKED (BS 621) · airframe 35,922 hrs · 31,582 cycles

FS 621 BULKHEAD FAILS NDT RBL 18 WITH INDICATION 50 PERCENT SCREEN HEIGHT WL 123 AND 124. REPAIRED IAW REO 601R-53-61-1285, REV D, DATED 10/31/2011.

Part: BULKHEAD — CRACKED (BS 621) · airframe 35,922 hrs · 31,582 cycles

FS 621, BULKHEAD RBL 27.50 FAILS NDT WITH INDICATION 50 PERCENT SCREEN HEIGHT AT WL 109 AND 110. REPAIRED IAW REO 601R-53-61-1285, REV D, DATED 10/31/2011.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 34,900 hrs · 30,658 cycles

RT EXTERIOR AFT EMERGENCY LIGHT INOP. REPLACED LAMP IAW AMM 33-51-21, OPS CHECK GOOD.

Part: FAN — FAILED (DISPLAY) · airframe 33,924 hrs · 29,796 cycles

DISPLAY COOL CAUTION MESSAGE IN FLIGHT. FOLLOWED QRH. WHEN SWITCHING FROM NORMAL TO FLIGHT ALTERNATE SMELLED ELECTRICAL BURNING ODOR FOR 10 SECONDS. RECEIVED ODOR TWICE MORE FOR SHORT DURATION OF TIME (DISPLAY COOLING FANS) R & R DISPLAY FAN IAW AMM 21-24-19, OPS CHECKED GOOD.

Part: DOOR — BINDING (PAX DOOR) · airframe 33,674 hrs · 29,566 cycles

AIRSTAIR DOOR REQUIRES EXCESSIVE FORCE TO OPEN, DOOR STICKS IN CLOSED POSITION. PERFORMED OPS CHECK ON AIRSTAIR DOOR IAW AMM 52-11-00. OPS CHECKED GOOD. SDR CLOSED.

Part: BRACKET — UNSERVICEABLE (NLG WOW HARNESS) · airframe 33,613 hrs · 29,512 cycles

GEAR DISAGREE WARNING MESSAGE CLIMBING THROUGH 14,000 FT. COMPLETED QRH PROCEDURE. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE, LANDED NORMALLY. R & R NLG WOW AND CENTERING SENSOR HARNESS BRACKET IAW AMM 32-61-25. ADJUSTED IAW AMM 32-61-05. PERFORMED GEAR SWING IAW AMM 32-30-00. ALL INDICATIONS NORMAL.

Part: HYDRAULIC LINE — DISCONNECTED (MLG BRAKES) · airframe 33,243 hrs · 29,181 cycles

ON LANDING, LOST BRAKING, ALL TIRES BLOWN EXCEPT LEFT OTBD. R & R ALL MLG TIRES IAW AMM 32-41-01. FOUND HYD QUICK DISCONETION LINE LOOSE. RESECURED LINE IAW AMM 32-43-26.

Part: UNKNOWN — MULTIPLE FAIL (APU) · airframe 32,738 hrs · 28,758 cycles

STARTED APU AT 10K AFTER A COUPLE OF MINUTES, TRANSFERED THE BLEEDS TO APU. RECEIVED AN APU OVERTEMP FOLLOWED BY APU FIRE, FOLLOWED BY APU FIRE FAIL, RAN 1A1 CORD AND BLEW BOTTLE THEN RECEIVED APU FIRE EXTINGUISHING SYS FAULT. EMERGENCY DECLARED. R & R APU ASSY IAW MM 49-10-00.

Part: STEP — CRACKED (PAX DOOR) · airframe 31,794 hrs · 27,866 cycles

PAX DOOR LOWER STEP IS CRACKED. R & R LOWER PAX DOOR STEP IAW AMM 52-11-04. OP'S CHECKED GOOD.

Part: HANDLE — BINDING (PAX DOOR) · airframe 31,408 hrs · 27,503 cycles

F/A REPORTS PAX DOOR IS HARD TO OPEN DUE TO LATCH STICKING. CYCLED PAX DOOR SEVERAL TIMES NO DEFECTS NOTED AT THIS TIME OPS CHECKED GOOD IAW AMM 52-11-01. OK FOR SERVICE.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 31,398 hrs · 27,493 cycles

EMERGENCY EXIT SIGN ON MAIN CABIN DOOR BULKHEAD IS BROKEN. R & R EXIT SIGN IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: DOOR — BINDING · airframe 31,313 hrs · 27,415 cycles

MAIN PAX WOULD NOT UNLATCH/OPEN. PERFORMED OPS TEST OF PASSENGER DOOR. DOOR OPS CHECKED GOOD IAW AMM 52-11-05. NO DISCREPANCIES NOTED. ACFT OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,284 hrs · 27,391 cycles

FS 349, SERVICE DOOR FLOOR SUPPORT CORRODED. COMPLY WITH STEPS 3 AND 4 OF REO 601R-53-21-1321. COMPLIED WITH STEP 3 OF REO 601R-53-21-1321. COMPLY WITH STEP 4 OF REO 601R-53-21-1321. COMPLIED WITH STEP 4 OF REO 601R-53-21-1321. COMPLY WITH EC/TC REO. COMPLIED WITH ASA EC/TC REO 601R-53-21-1321. OUT OF SEQ FASTENERS REMOVED IN DAMAGED AREA. INSTALLED NEW FASTENER AS NEEDED IAW SRM 51-42-06 (FASTENER) AND 51-42-21 (HI LITES). SUBMITTED TO THD FOR DISPOSITION. RECEIVED REO 601R-53-21-1321 AND COMPLIED WITH ALL STEPS. RII FOUND TO BE SATISFACTORY. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (PAX DOORWAY) · airframe 31,260 hrs · 27,368 cycles

PAX DOOR FLOOR SUPPORT ANGLE JUST ABOVE SILL CORRODED. FORMED AND BENT PAX DOOR FLOOR SUPPORT ANGLE IAW SRM 51-24-21 AND DWG 601R31527. HEAT TREATED FORMED REPAIR PART FROM O TO T62 IAW SRM 51-24-06. TRIMMED AND FITTED FABRICATED PART TO ACFT BBD DWG 601R31527.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 31,260 hrs · 27,368 cycles

SERVICE DOOR ENTRANCE FLOOR SUPPORT ANGLE ABOVE SILL AT FS 349 CORRODED. REPAIRED IAW SRM 51-41-02.

Part: FRAME — CORRODED (BS 349) · airframe 31,260 hrs · 27,368 cycles

CORROSION FOUND AT FS 349 FRAME ON FRONT AND AFT FACE AT S27L. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 51-21-06.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 31,260 hrs · 27,368 cycles

EMERGENCY EXIT DOOR, LT, IS BINDING WHEN OPENING. CHECK DOOR FOR PROPER OPERATION, ADJUST AS REQ. CHECK DOOR FOR PROPER OPERATION, ADJUST AS REQ. FOUND RESISTANCE IN THE HANDLE MECANISIM WAS EXCESSIVE ADJUSTED OVER-WING EXIT IAW AMM 52-21-00-820-801, & PERFORM FUNCTIONAL TEST OF OVER-WING EXIT IAW AMM 52-21-00-710-801. NO FURTHER DEFECTS NOTED. RE-ADJUSTED LT OVER WING EXIT PROX SENSOR IAW AMM 52-70-10-820-801 & OPS CHECKED IAW TASK 52-70-10-710-801. NO FURTHER DEFECTS NOTED. REMOVED OVERHEAD BIN NR 4 LT & PSU'S FOR SEATS 7-13 A, B IAW AMM 25-28-01-000-801 &, 25-23-01-000-801. OK TO INSTALL BIN & PSUS SM161739 7/21/11 INSTALLED OVERHEAD BIN NR4 LT & PSU'S FOR SEATS 7-13 AB IAW AMM 25-28-01-400-801 & 25-23-01-400-801. RII FOUND TO BE SATIFACTORY. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 568-625) · airframe 31,260 hrs · 27,368 cycles

CORROSION FOUND ON LBL 27 FS 568-621 FLOOR SUPPORT. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-20. ITEM 2. FOUND OUT OF LIMITS. INSTALLED FLOOR SUPPORT NEW IAW REO 601R-53-61-378-78.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 31,260 hrs · 27,368 cycles

FLOOR SUPPORT FITTING AT FS 310 BY SERVICE DOOR CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-20. DRILLED & REAMED NEW FLOOR SUPPORT IAW REO 601R-53-21-1332 & ALODINED HOLES & TOP COATED BARE METAL ON ALL ATTACH PARTS IAW CRM 51-21-11 FOR CODING 51-25-01-31-25-16 PRIMER, TOP COAT. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-21-1332. MINOR REPAIR.

Part: WEB — CRACKED (BS 280) · airframe 31,260 hrs · 27,368 cycles

FS 280 WEB CRACKED AT ALTERNATE EXTENSION PULLY BRACKET. PERFORMED ET INSPECTION OF WEB IAW NDT INSPECTION PROCEDURE ET-2. WEB IS VERIFIED AS CRACKED. WEB REPAIRED IAW REO 601R-53-11-926.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,260 hrs · 27,368 cycles

FLOOR SUPPORT AT FS 349.00 LT SIDE UNDER PANEL 231CLF CORRODED. CLEAN CORROSION IAW 51-21-06 AND VERIFY LIMITS. REMOVED CORROSION FROM FS 349 CROSSBEAM AT LBL 40, WL 73, TOP FLANGE IAW SRM 51-21-06. REPAIR DIMENSIONS: 1"X 1.5" X .003" DEEP ORIGINAL THICKNESS .063", REMAINING THICKNESS .060" WITHIN ALLOWABLE LIMITS OF SRM 53-00-00, FIG 102.

Part: ANGLE — CORRODED (BS 280) · airframe 31,260 hrs · 27,368 cycles

FS 280 FWD J-ANGLE CORRODED IN FLIGHT DECK DOORWAY. REMOVED J-ANGLE IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED FASTENER HOLES IN NEW J-ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 AND 51-42-21. MINOR REPAIR.

Part: WEB — CRACKED (BS 280) · airframe 31,260 hrs · 27,368 cycles

FS 280 WEB CRACKED AT ALTERNATE EXTENSION PULLY BRACKET. PERFORMED ET INSPECTION IAW NDT INSPECTION PROCEDURES ET-2. ANGLE VERIFIED AS CRACKED. CUT OUT DAMAGED AREA, NDT CUTOUT AREA IAW NDTM 51-20-06. NO CRACK NOTED. REPAIRED IAW REO 601R-53-11-926.

Part: STRUCTURE — CRACKED (BS 280) · airframe 31,260 hrs · 27,368 cycles

FS 280, RBL 9 INBD CLIP CRACKED. REMOVED CRACKED CLIP IAW SRM 51-42-20. FABRICATED NEW CLIP IAW REO 601R-53-11-926 NOTE 20. INSTALLED NEW CLIP IAW REO 601R-53-11-926, ECTC REO 601R-53-11-926. PERFORMED NDI IAW REO 601R-53-11-926, NO INDICATIONS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 295) · airframe 31,260 hrs · 27,368 cycles

FS 295 OTBD OF LBL 27 FLOOR SUPPORT BOX CORRODED. REMOVED CORROSION IAW SRM 51-21-06. REMOVED DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-00, FIG 102.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 31,260 hrs · 27,368 cycles

FS 484 OTBD, RBL27 FLOOR SUPPORT ANGLE CRACKED PREVIOUS REPAIRED ANGLE MK7236. R & R FLOOR SUPPORT ANGLE IAW SRM 51-40-11, 51-42-21. THIS IS A MINOR REPAIR.

Part: ANGLE — CRACKED (BS 280) · airframe 31,260 hrs · 27,368 cycles

FS 280 LT ANGLE CRACKED OTBD OF RBL 27. VERIFY POSSIBLE CRACK (NDT) AND LENGTH. PERFORMED RT INSP IAW MAC NDT INSPECTED PROCEDURE ET-2 NO INDICATIONS NOTED AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 31,260 hrs · 27,368 cycles

SERVICE DOOR ENTRANCE FLOOR SUPPORT ANGLE ABOVE SILL AT FS 349, CORRODED. REMOVED ANGLE IAW SRM 51-42-06, 51-42-13, 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: STRUCTURE — CRACKED (BS 280) · airframe 31,260 hrs · 27,368 cycles

FS 280, RBL 9 OTBD CLIP CRACKED. REMOVED DAMAGED CLIP IAW SRM 51-42-20. FABRICATED NEW CLIP IAW REO 601R-53-11-926 NOTE 20 IAW EC/TC 601R-53-11-926. PERFORMED NDT IAW REO 601R-53-11-926 NOTE 20, NO INDICATIONS NOTED. INSTALLED NEW CLIP IAW REO 601R-53-11-926.

Part: STRUCTURE — CRACKED (BS 280) · airframe 31,260 hrs · 27,368 cycles

FS 280, LBL 9 INBD CLIP CRACKED. REMOVED DAMAGED CLIP, LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-11, 51-42-20. PERFORMED NDI IAW REO 601R-53-11-926, NO INDICATIONS NOTED. INSTALLED NEW CLIP IAW REO 601R-53-11-926.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 31,260 hrs · 27,368 cycles

FS 349 AT SERVICE DOOR FLOOR SUPPORT CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REPAIRED IAW REO 601R-53-21-1321.

Part: SKIN — CHAFED (CENTER WING) · airframe 31,260 hrs · 27,368 cycles

CENTER LEFT WING BOX LOWER SKIN CHAFED AND PITTED WITH POSSIBLE CORROSION .2500" WIDE, 18" LONG, .006 DEEP, UNDER PANEL 193AB. BLENDED CHAFING AND PITTING NO CORROSION FOUND 1.5 WIDE 30IN LONG. .006 DEEP IAW SRM 57-00-31. PERFORMED UT THICKNESS OF BLEND AREA IAW NDT INSPECTION PROCEDURES, UT-3 MINIMUM MATERIAL REMAINING ON LOWER WING SKIN IS .109". ORIGINAL THICKNESS IS .110, WITHIN ALLOWABLE LIMITS IAW SRM 57-21-31. ROTO PEENED REPAIRED AREA IAW SRM 51-24-11. PERFORMED LPI, TYPE 1 METHOD C ON BLEND AREA IAW MAC NDT INSPECTION PROCEDURES PT-1, NO INDICATIONS NOTED. TREATED BARE METAL, PRIMED AND PAINTED IAW SRM 51-21-16 AND 51-12-00.

Part: FRAME — CORRODED (BS 333 S25-27R) · airframe 31,260 hrs · 27,368 cycles

FS 333.00 FRAME CORRODED FROM STR 25-27R. REMOVED AND INSTALLED NEW FRAME SECTION IAW SRM 51-42-06 AND 51-42-20. MINOR REPAIR.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 31,260 hrs · 27,368 cycles

5 CARGO BAY TIE DOWN POINTS ARE CORRODED, 3 AT LBL 27.00 2 AT LBL 9.0. REMOVED CORRODED FTGS (5 PLACES ) AND REPLACED WITH NEW FTGS IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (BS 574) · airframe 31,260 hrs · 27,368 cycles

CARGO TRACK AT APPROX FS 574 CORRODED. R & R CARGO TRACK IAW AMM 20-21-00-02 AND 53-01-11-04.

Part: FRAME — CORRODED (BS 319.7 S25-27L) · airframe 31,260 hrs · 27,368 cycles

FS 319.70 FRAME CORRODED FROM STR 25-27L. R & R FRAME IAW SRM 51-42-06. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 621) · airframe 31,260 hrs · 27,368 cycles

SEAT TRACK AT FS 621, LBL 9.0 CORRODED. FOUND OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED WITH SEAT TRACK IAW AMM 53-01-11-000-802.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,260 hrs · 27,368 cycles

PAX DOOR FLOOR SUPPORT ANGLE JUST ABOVE SILL CORRODED. REMOVED PAX DOOR FLOOR SUPPORT ANGLE. CORROSION OUT OF LIMITS IAW SRM 53-21-23 AND 53-00-00 SH88030. COMPLIED WITH STEP 5 OF EC/TC EO 600-53-0700 IAW NDTM PART 1, 51-20-06 NO INDICATIONS NOTED. INSTALLED ANGLE IAW SRM 51-42-21 AND 51-42-06.

Part: SKIN — CRACKED (PAX DOOR) · airframe 31,260 hrs · 27,368 cycles

ASD BOTTOM SECTION CENTER SKIN CRACKED AT AFT, AFT SECTION OF DOOR. REPAIRED IAW REO 601R-52-11-279.

Part: SEAT TRACK — DAMAGED · airframe 31,260 hrs · 27,368 cycles

CO-PILOT SEAT RAILS LOCKING HOLES ELONGATED. MEASURE ELONGATED COPILOT SEAT RAILS. HOLES INBD AND OTBD. DETERMINED HOLES TO BE OUT OF LIMITS IAW SRM 53-11-49, TRACKS REQUIRE REPLACEMENT. REMOVED SEAT TRACKS ON COPILOT SEAT. LOCATED AND PULLED NEW SEAT TRACKS IAW SRM 51-40-11. THIS IS A MAJOR REPAIR. CONTINUE FAB OF NEW PILOTS SEAT TRACK. LOCATED, CUT TO FIT, TREATED AND PRIMED, INSTALLED NEW CO PILOTS SEAT TRACK IAW SRM 51-40-11 AND MM 53-01-05. RII FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 31,260 hrs · 27,368 cycles

CABIN FLOOR SEAT TRACK HAS CORROSION DAMAGE FS 364-394 LBL 9.0. FOUND OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED WITH NEW SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 31,260 hrs · 27,368 cycles

PILOT'S SEAT RAILS LOCKING HOLES ELONGATED. MEASURE ELONGATED PILOT SEAT RAILS LOCKING HOLES INBD AND OTBD. DETERMINED HOLES TO BE OUT OF LIMITS IAW SRM 53-11-49, TRACKS REQUIRE REPLACEMENT. REMOVED SEAT TRACKS ON PILOTS SEAT IAW AMM 25-11-01. DRILLED DEBURED TREATED AND PRIMED NEW PILOTS SEAT TRACKS IAW SRM 51-40-11. THIS IS A MAJOR REPAIR. INSTALL PILOTS SEAT TRACKS. INSTALLED PILOTS SEAT TRACKS IAW MM 53-01-05. RII FOUND TO BE SATISFACTORY.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,734 hrs · 26,917 cycles

FWD EMERGENCY CEILING LIGHT IS INOP. R & R FWD EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OP'S CHECKED GOOD. R & R FWD EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OP'S CHECKED GOOD.

Part: SKIN — CRACKED (BS 235 S26R) · airframe 29,457 hrs · 25,773 cycles

CRACK IN SKIN AT AFT RT SIDE OF NLG DOOR CUT OUT AT FS 235 AT STR 26R.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,288 hrs · 25,625 cycles

LT FWD OVERWING EMERGENCY LIGHT INOP. R & R EMERGENCY LIGHT BULB IAW AMM 33-51-21.

Part: ACTUATOR — FAILED (MLG) · airframe 28,648 hrs · 25,059 cycles

GEAR DISSAGREE CAUTION MSG FOR RT MAIN GEAR AFTER GEAR WAS SELECTED DOWN. AFTER APPROX 1 MINUTE, FELT GEAR DROP IN PLACE THEN GOT 3 GREEN INDICATION. R & R RT MLG SIDE STAY ACTUATOR IAW AMM 32-32-01. OPS AND LEAK CK GOOD. (CLOSED)

Part: PRIORITY VALVE — FAILED (MLG) · airframe 28,000 hrs · 24,488 cycles

NOSE GEAR DISAGREE ON TAKEOFF, HYD 3 PUMP MAKES NOISE TEMP AT 102 (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED. R & R NLG PRIORITY VALVE. SWUNG GEAR SEVERAL TIMES WITH NO FURTHER DEFECTS NOTED OPS AND LEAK CHECK GOOD REF 32-33-15.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,045 hrs · 24,525 cycles

STRONG ELECTRICAL ODOR IN COCKPIT. INSPECTED ACFT COULD NOT FIND EVIDENCE OF CHAFING OR ELECTRICAL PROBLEMS. REF AMM 05-50-00.

Part: CONNECTING ROD — MISRIGGED (PAX DOOR) · airframe 27,892 hrs · 24,386 cycles

ASD OUTTER HANDLE HARD TO OPEN. UPON INSP FOUND ASD PRESSURE VALVE DOOR NOT CLOSED. ADJUSTED PRESSURE VALVE DOOR RODS PER CRJ 200 AMM 52-11-15. ALSO ADJUSTED OUTTER HANDLE MECHANICAL RODS PER CRJ 200 AMM 52-11-03. OPS CHECK GOOD.

Part: DOOR — STIFF (MAIN PAX) · airframe 27,834 hrs · 24,316 cycles

F/A REPORTS PASSENGER DOOR DIFFICULT TO OPEN.

Part: DOOR — STUCK (MAIN PAX) · airframe 27,782 hrs · 24,254 cycles

PASSENGER DOOR IS DIFFICULT TO OPEN. FLT 5454.

Part: DOOR — BINDING (PAX DOOR) · airframe 27,699 hrs · 24,166 cycles

F/A REPORTS THE MAIN PAX DOOR IS DIFFICULT TO OPEN.

Part: DOOR — STIFF (MAIN PAX) · airframe 27,526 hrs · 23,974 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN

Part: DOOR — STIFF (MAIN PAX) · airframe 27,526 hrs · 23,974 cycles

FA REPORTS PASSENGER DOOR IS DIFFICULT TO OPEN

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

FIVE (5EA) RIVNUTS ON FLOORBEAM FS 559+4 AND FS 559+64 NEED REPLACED IAW SRM 51-42-34 RBL 9. UPON INVESTIGATION, FOUND FASTENERS TO BE BLIND NUTS NOT RIVNUTS. REPLACE 6 EACH BLIND NUTS. DRILLED 6 EACH AND REMOVED PER SRM 51-42-34. INSTALLED 6 NEW BLIND NUTS IAW SRM 51-42-34 BETWEEN FS 559+50 TO 559+64.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

CABIN SEAT TRACK CORRODED. REMOVED CORROSION FROM LBL 9 SEAT RAIL BETWEEN FS 409 + 126 AND 559 + 4 IAW SRM 51-21-06, AREA IS OUT OF LIMITS IAW SRM 53-21-49 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

SEAT RAIL AT RBL 9 BETWEEN FS 559 + 4 AND FS 559 + 64 CORROSION IS OUT OF LIMITS IAW CRJ 200 SRM 53-21-49 FIG 101. REF MWC 1-188. LOCATED HOLES IN NEW SEAT RAIL IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK. AFTER REMOVING OLD SEAT TRACK IAW AMM 53-01-11-400-801.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

SEAT RAIL AT RBL 9 BETWEEN FS 364 AND FS 399.5 CORROSION IS BEYOND LIMITS IAW CRJ 200 SRM 53-21-49 FIG 101. REF MWC 1-188.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

SEAT RAIL AT RBL 9 BETWEEN FS 399.5 AND FS 409 + 126 CORROSION IS BEYOND LIMITS IAW SRM 53-21-49 FIG 101. REF MWC 1-188. REMOVED SEAT RAIL IAW SRM 51-41-02. DRILLED IAW SRM 51-40-11, INSTALLED SEAT TRACK PER AMM 53-01-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

SEAT RAIL AT LBL 9 BETWEEN FS 399.5 AND FS 409 + 126 CORROSION IS BEYOND LIMITS IAW CRJ 200 SRM 53-21-49 FIG 101. REF MWC 1-188.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

SEAT RAIL AT RBL 9 BETWEEN FS 409 + 126 AND FS 559 + 4 CORROSION IS BEYOND LIMITS IAW CRJ 200 SRM 53-21-49 FIG 101. REF MWC 1-188. REMOVED SEAT RAIL IAW SRM 51-41-02. LOCATED AND COUNTERSUNK NEW RAIL IAW SRM 51-40-11, 51-41-02. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

SEAT RAIL AT LBL 9 BETWEEN FS 364 AND FS 399.5 CORROSION IS BEYOND LIMITS IAW CRJ 200 SRM 53-21-49 FIG 101. REF MWC 1-188.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

SEAT RAIL AT LBL 9 BETWEEN FS 409 + 126 AND FS 559 + 4 CORROSION IS BEYOND LIMITS IAW SRM 53-21-49 FIG 101. REF MWC 1-188. REMOVED SEAT RAIL IAW SRM 51-41-02. INSTALLED NEW RAIL IAW AMM 53-01-11-400-802. LOCATED AND COUNTERSUNK FASTENER HOLES IN NEW RAIL IAW SRM 51-41-02, 51-40-11.

Part: POST — CRACKED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

FS 409.00 + 128 VERT POST, LBL 18.0, AFT OUTBOARD FLANGE HAS TWO CRACK INDICATIONS NOTED AT WL 69.0. BOTH INDICATIONS FAIL NDT AT 55 PERCENT FSH (MARKED). INDICATION ABOVE WL 69.0 IS APPROX .312 INCH IN LENGTH INDICATION BELOW WL 69.0 IS APPROX .375 INCH IN LENGTH. REMOVED VERT POST IAW SRM 51-42-06. FOUND POST DAMAGED BEYOND LIMITS. FABRICATED REPLACEMENT POSTS IAW SRM 51-24-21 REF DWG 601R32208. DRILLED NEW POST, PAINTED AND ASSEMBLED POST HALF IAW SRM 51-420-11 AND SRM 51-42-06. INSTALLED SPLICE PLATE IAW SRM 51-42-06. INSTALLED POST ASSY IAW EC/TC C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: POST — CRACKED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

FS 409 + 128 BULKHEAD VERTICAL POST IS CRACKED AT RBL 18 O/B LOWER FLANGE NEAR THE LAST RIVET ON THE BOTTOM. FABRICATED REPLACEMENT POST FS 409 + 128 RBL 18.0 OUTBOARD USING 7075-0 .063 PO 104964/1 REF DWG 601R32208. REMOVED CRACKED VERT POST IAW SRM 51-42-06. DRILLED NEW VERT POST AND TRIMMED TO SIZE IAW SRM 51-40-11. ASSEMBLED POST AND INSTALLED ON ACFT IAW REO 601R-53-41-889. SEALED AREA REPAIRED IAW AMM 51-23-00. PAINTED AREA IAW SRM 51-25-16. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: POST — CRACKED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

FS 409.00+128 VERT POST, LBL 18.0, AFT OUTBOARD FLANGE HAS TWO CRACK INDICATIONS NOTED AT WL 69.0. BOTH INDICATIONS FAIL NDT AT 55 PERCENT FSH (MARKED). INDICATION ABOVE WL 69.0 IS APPROX .312 INCH IN LENGTH INDICATION BELOW WL 69.0 IS APPROX .375 INCH IN LENGTH. REPAIRED FS 559 BULKHEAD BETWEEN LBL 27 AND RBL 27 AND CAP ANGLES IAW REO 601R-53-41-260 AND REO 601R-53-41-1001. COMPLIED WITH EC/TC 601R-53-41-1001 AND MET THE REQUIREMENTS OF REO 601R-53-41-1001. COMPLIED WITH EC/TC 601R-53-41-260 IAW REO 601R-53-41-260 REV. RII COMPLIED WITH.

Part: POST — CRACKED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

FS 409.00 + 128 VERT POST, BL 00, RT AFT FLANGE HAS A CRACK INDICATION AT WL 69.0. INDICATION FAILS NDT INSPECTION AT 60 PERCENT FSH AND APPROX .437 INCH IN LENGTH (MARKED). REMOVED VERTICAL POST AT FS 409 + 128 BL 0 IAW SRM 51-42-06. FABRICATED REPLACEMENT POST USING 7075-0 .063 PO 104141 AND REINFORCEMENT ANGLE USING 7075-0 .032 PO 21968/1 IAW SRM 51-24-21. REF DWG 601R32208. LOCATED HOLES IN RT SIDE POST IAW SRM 51-40-11. LOCATED & DRILLED REINFORCEMENT ANGLE IAW SRM 51-40-11. INSTALLED VERTICAL POST ASSY WITH REINFORCEMENT ANGLES. INSTALLATON OF POST IS COMPLETED IAW REO 601R-53-41-1006 AND MEETS ALL ITS REQUIREMENTS.

Part: WEB — DAMAGED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

FOUND LT FS 559 WEB HAS INDICATION NOTED APPROX .2 INCH IN LENGTH 50 PERCENT FSH AT WL 52.10 O/B OF LBL 9.0, & FOUND RT FS 559 WEB HAS 3 INDICATIONS NOTED: (1) APPROX 1.0 INCH IN LENGTH 90 PERCENT FSH AT WL 59.10 I/B OF RBL 18.0, (2) APPROX .2 INCH IN LENGTH 90 PERCENT FSH AT WL 58.70 O/B OF RBL 9.0, (3) APPROX .5 INCH IN LENGTH 80 PERCENT FSH AT WL 54.10 O/B OF RBL 9.0. ALL THESE AREAS FAILED NDT INSPECTION. REPAIRED BULKHEAD IAW REO 601R-53-41-260 AND REO 601R-53-41-1001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

CABIN FLOOR SEAT TRACKS FROM FS 364.00 TO FS 559.00+64 LBL 9 AND RBL 9 HAVE MINOR SURFACE CORROSION.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 27,096 hrs · 23,527 cycles

RBL 36 FLOOR SUPPORT STRUCTURE FROM FS 621 TO FS 559.00+80 AROUND SCREW HOLES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,570 hrs · 23,022 cycles

EXTERNAL EMERGENCY LIGHT INOP ON LT SIDE. REMOVED AND REPLACED LT AFT EXTERNAL EMERGENCY LIGHT FUSELAGE IAW AMM 33-51-21 OPS CK GOOD.

Part: COVER — CRACKED (FUSELAGE) · airframe 26,088 hrs · 22,560 cycles

RT EMERGENCY EXIT COVER CRACKED IN UPPER CORNER AND WINDOW SHADE DAMAGED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 26,088 hrs · 22,560 cycles

LOWER ATTACH ANGLE OF DOOR REINFORCING BEAM MEMBER IS CRACKED AT FS 621.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,891 hrs · 22,391 cycles

F/O FLASHLIGHT NEEDS BATTERIES.

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 25,682 hrs · 22,198 cycles

PAX DOOR OPEN AND EXIT PLACARDS DETERIORATED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,986 hrs · 20,722 cycles

EMERGENCY LIGHTS NOT WORKING PROPERLY.

Part: DOOR FRAME — CRACKED (BS 338) · airframe 22,742 hrs · 19,665 cycles

PAX DOOR AFT FRAME MEMBER AT FS 338.90 IS CRACKED. REF REO 601R-52-11-402 FOR POSSIBLE REPAIR. [07-26-07] REPAIRED IAW ALL SRMS AND EO`S.

Part: STRAP — CRACKED (FUSELAGE) · airframe 22,742 hrs · 19,665 cycles

LEFT SKIN BUTT JOINT STRAP AT FS 640 BETWEEN STR 10 AND STR 11 IS CRACKED; REQUIRES REO 601R 53-61-506. [07-26-07] REPAIRED LT SKIN BUTT JOINT STRAP FS 640 BETWEEN STR 10 AND STR 11 IAW REO 601R 53-61-506.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,742 hrs · 19,665 cycles

SUSPECTED CRACK ON INTERCOSTAL UPPER RADIUS AT FS 484 RBL 27 O/B. LPI WAS PERFORMED ON THE CLIP UPPER RADIUS AT FS 484 RBL 27, O/B IAW NDTM 51-20-08 AND FOUND TO BE CRACKED IN THE UPPER RADIUS, APPROX 1/4". REMOVED DAMAGED CLIP AT FS 484 RBL 27 O/B AND DUPLICATED PART FROM PRE-FORMED STOCK P/N S-6144-3 FROM PO 950007 IAW CRJ 200 SRM 51-40-06, 51-40-11 AND BOMBARDIER DWG NR S6144. OK TO TREAT AND PRIME. ALODINED AND PRIMED IAW CRJ 200 SRM 51-21-11 AND 51-25-06. OK TO INSTALL. INSTALLED DUPLICATED CLIP AT FS 484 RBL 27 O/B IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 07/18/07

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,742 hrs · 19,665 cycles

LEFT FUSELAGE 280 LBL 9 I/B CLIP CRACKED.

Part: STRUCTURE — CRACKED (BS 472) · airframe 22,742 hrs · 19,665 cycles

SUSPECTED CRACK ON THE UPPER I/B RADIUS OF BOTH TAB FITTINGS AT FS 472 RBL 9. PERFORMED LPI ON THE FS 472 RBL 9 UPPER RADIUS OF BOTH I/B AND O/B TAB FITTINGS IAW NDTM 51-20-08. FS 472 RBL 9 UPPER RADIUS OF BOTH I/B AND O/B TAB FITTINGS, APPROX .5 INCH. STARTED REMOVING HI-LOKS IAW CRJ SRM 51-42-21. REMOVED BOTH BATH TUB FITTINGS FROM RBL 9. LOCATED BOTH BATH TUB FITTINGS AT FS 472 RBL 9. OK TO INSTALL I/B FITTING. STARTED INSTALLING I/B FITTING IAW CRJ 200 SRM 51-42-21. STARTED INSTALLING I/B FITTING IAW CRJ 200 SRM 51-42-21. COMPLETED INSTALLATION OF I/B FITTING IAW CRJ 200 SRM 51-42-21. INSTALLED O/B FITTING IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL - SDR CLOSED 07/16/07.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,742 hrs · 19,665 cycles

SUSPECTED CRACK ON INTERCOSTAL UPPER RADIUS AT FS 484 LBL 27 O/B.

Part: ESCAPE HATCH — FAILED (CREW ESCAPE) · airframe 22,742 hrs · 19,665 cycles

CREW ESCAPE HATCH FAILS OPEN AND CLOSE FUNCTIONAL TEST. [07-26-07] REMOVED HATCH, LUBED WITH, D.C. 33. REPLACED AND PERFORMED FUNCTIONAL TEST. NO DECREPANCIES FOUND AT THIS TIME, IAW CRJ 200 AMM .

Part: LIGHT — TORN (CABIN) · airframe 22,417 hrs · 19,397 cycles

EMERGENCY LIGHT BY STAIR DOOR IS TORN.

Part: ANGLE — CRACKED (RT WING) · airframe 21,632 hrs · 18,781 cycles

RT WING MIDDLE LEADING EDGE, I/B ATTACH ANGLE CRACK.

Part: STEP — CRACKED (PAX DOOR) · airframe 20,738 hrs · 18,093 cycles

BOTTM STEP OF PASSENGER DOOR IS CRACKED. FLT 4348 DEL 36 MINS.

Part: STEP — BROKEN (DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR)

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

Part: BRACKET — INOPERATIVE (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT CLOSE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR CABLE SUPPORT BRACKET. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — BROKEN (CABIN)

DURING C-CHECK, EMERGENCY EXIT FLOODLIGHT ASSEMBLY BY THE FLIGHT ATTENDANTS STATION WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT FLOODLIGHT ASSEMBLY BY FLIGHT ATTENDANTS STATION. OPERATIONAL CHECKS GOOD. (K)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 718 LEFT FORWARD BRACKET, UPPER DOUBLER, WAS FOUND TO BE CRACKED IN THE RADIUS BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 178 LEFT FORWARD BRACKET, UPPER DOUBLER. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 280 FLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 280 FLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CO-PILOTS BULKHEAD WEB AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS APPROXIMATELY TWO INCHES OUTBOARD OF RBL 9. MAINTENANCE IS REPAIRING THE CO-PILOTS BULKHEAD WEB AT FS 280 OUTBOARD OF RBL 9 IAW BOMBARDIER REO 601R-53-11-627. (M)

Part: SKIN — CRACKED (RT WING)

DURING A C-CHECK IN MCN, THE LOWER WING PLANK AT WS 148.019 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LOWER WING PLANK AT WS 148.019 RT IAW ASA EO 600-57-0134A. (M)

Part: RIB — CRACKED (LT WING)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M)

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING A C-CHECK IN MCN, THE AVIONICS BAY DOOR EXTERIOR HANDLE WAS FOUND CRACKED AROUND THE INTER BOSS. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE IAW SRM 51-42-06 AND 51-21. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN BTR, THE RIGHT AFT MOST EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT AFT MOST EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. (M)

Part: BEARING — BINDING (PAX DOOR)

FLT 4358 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. MAINTENANCE REMOVED AND REPLACED THE AFT ROLLER BEARINGS ON THE PASSENGER DOOR. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION, THE EMERGENCY CEILING LIGHT AT ROW 14 A/B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 14 A/B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: PLATE — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SERVICE DOOR AIRFRAME SILL PLATE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPALCED THE SERVICE DOOR AIRFRAME SILL PLATE. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FORWARD FLOORBEAM ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLOORBEAM ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW SRM 51-00. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCH, THE FLOOR SUPPORT CLIP JUST INBOARD OF THE CARGO THRESHOLD WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CLIP JUST INBOARD OF THE CARGO THRESHOLD IAW SRM 51-00. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CLIPS AT FS 484, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANACE REMOVED AND REPLACED THE CLIPS AT FS 484, LBL 27 AND RBL 27 IAW ASA EO 600-53-0111. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE INTERCOSTALS AT FS 484, LBL 36 AND RBL 38 IAW ASA EO 600-53-0111. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL AT FS 582.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO BAY FLOOR SILL AT FS 582.72-589 IAW ASA EO 600-53-0095. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LT AND RT FLOOR SUPPORT ANGLES ON THE AFT BULKHEAD AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINT REPAIRED THE LT AND RT FLOOR SUPPORT ANGLES ON THE AFT BULKHEAD AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURNG A C-CHECK IN MCN, THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINT R & R THE CLIPS AT FS 280, LBL 9 AND RBL 9 INBOARD AND OUTBOARD IAW SRM 51-42-20. (M)

Part: SIGN — CRACKED (EMERGENCY SIGN)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT SIGN FLOODLIGHT IN THE GALLEY BUT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN FLOODLIGHT ASSEMBLY IN THE GALLEY BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 12,880 hrs

DURING APPROACH, AT APPROXIMATELY 2,800 FEET AND 180 KNOTS THE CREW RECEIVED AN GEAR DOWN DISAGREEMENT ON THE NOSE WHEEL. QRH PROCEDURES WERE COMPLIED WITH AND THE GEAR CAME DOWN NORMALLY. FIRE EQUIPMENT WAS DISPATCHED AS A PRECAUTION AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE JACKED AND SWUNG THE LANDING GEARS TEN TIMES WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY CEILING LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMPS IN THE CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING AN 'A' CHECK IN MCN, FRAME FS 640 BETWEEN STRINGERS 13R AND 14R WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING FRAME FS 640 BETWEEN STRINGERS 13R AND 14R IAW ASA EO 600-53-0088. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING AN 'A' CHECK AT MCN, THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0070. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

DURING AN 'A' CHECK AT MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M)

Part: LIGHT — INOPERATIVE (FUSELAGE)

DURING A GROUND INSPECTION IN DFW, THE LEFT FORWARD UPPER EXTERIOR EMRGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD UPPER EXTERIOR EMERGENCY LIGHT. OPERTIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING INSPECTION, MAINTENANCE FOUND THE AFT CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLAP — MALFUNCTIONED (WING)

ON DECENT, THE CAPTAIN RECEIVED A FLAP FAIL MESSAGE WHEN SELECTING FLAPS TO EIGHT DEGREES. EMERGENCY EQUIPMENT WAS REQUESTED AS A PRECAUTION. A ZERO FLAP LANDING WAS PERFORMED. LANDING WAS UNEVENTFUL. MAINTENANCE CYCLED CIRCUIT BREAKERS 1F4 AND 2F4 AND DETERMINED PROPER OPERATION OF THE FLAP SYSTEM IAW AD. AIRCRAFT OK FOR SERVICE.

Part: FRAME — CRACKED (FUSELAGE)

DURING HANGER MAINTENANCE, A CRACK WAS FOUND TO FUSELAGE FRAME FS718.00 BETWEEN STRINGERS 10 AND 12. MAINTENANCE REPAIRED THE CRACKED FRAME IAW EA/REO.

Part: WINDSHIELD — CRACKED (COCKPIT)

WHILE SITTING AT THE GATE IN ATL, THE CAPTAINS WINDSHIELD SHATTERED FOR UNKNOWN REASONS. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS CRACKED WINDSHIELD. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — BURNED OUT (FUSELAGE)

FLT 4390 - DURING GROUND INSPECTION IN ATL, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ACTUATOR — FAILED (T/E FLAP)

FLT 4466 - ON APPROACH INTO YYZ, AT 7000 FEET, THE FIRST OFFICER, PILOT FLYING, SELECTED THE FLAPS TO 8 DEGREES AND RECEIVED A FLAP FAIL MESSAGE. AN EMERGENCY WAS DECLARED. PROCEDURES WERE FOLLOWED FOR A ZERO FLAP LANDING IAW THE QRH. AIRCRAFT MADE AN UNEVENTFUL LANDING IN YYZ. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

FLT 4545 - DURING FLIGHT FROM ISP TO ATL, CREW RECEIVED A CARGO SMOKE WARNING. CREW BLEW EMERGENCY FIRE BOTTLES AND DIVERTED TO BWI. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTORS AND REPLACED FIRE BOTTLES AND SQUIBBS. OPERATIONAL TESTS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

DURING INSPECTION, RIGHT OVERWING EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING SYSTEM BULB. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BULB — FAILED (ROW 2AB)

DURING INSPECTION, EMERGENCY FLOOR BULB AT 2AB FOUND INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING SYSTEM BULB. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DRIVE UNIT — FAILED (CABIN)

ATL/GPT - FLT 7533 - DURING APPROACH WHEN MOVING FLAPS FROM 30 TO 45 DEGREES, FLAP FAIL MESSAGE ILLUMINATED AND FLAPS LOCKED AT APPROXIMATELY 41 DEGREES. REQUESTED EMERGENCY EQUIPMENT TO BE STANDING BY AS A PRECAUTION. LANDING WAS MADE SAFELY IN GPT WITHOUT FURTHER INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT TO ATL FOR REPAIR. ATL MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X)