N847AS

Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,748 hrs · 30,709 cycles

EVIDENCE OF CORROSION ON SEAT TRACKS. REMOVED AND REPLACED THE SEAT TRACKS IAW AMM 53-01-11, AND SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 349-559) · airframe 33,748 hrs · 30,709 cycles

EVIDENCE OF CORROSION ON SEAT TRACK BS 349- 559. REMOVED AND REPLACED THE SEAT TRACKS IAW AMM 53-01-11, AND SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (BS 319.7) · airframe 30,684 hrs · 27,551 cycles

FLOOR SUPPORT AND DOUBLER CORRODED AT FS 319.70, RBL 42. REMOVED RT FLOOR SUPPORT FS 310.00 TO FS 319.70 IAW SRM 51-42-06 FOR REPAIR OR REPLACEMENT. LOCATED & DRILLED NEW SERVICEABLE FLOOR SUPPORT, IAW SRM 51-40-11. INSTALLED IAW SRM 51-42-06, 7 51-42-13. LOCATED & DRILLED NEW FLOOR SUPPORT DOUBLER IAW SRM 51-40-11. INSTALLED NEW FLOOR SUPPORT DOUBLER IAW SRM 51J-42-06.

Part: BULKHEAD — CRACKED (BS 621) · airframe 30,684 hrs · 27,551 cycles

INDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD AT LBL 36, WL 78 APPROX .300 IN LENGTH AT 100/5 FULL SCREEN HEIGHT. REPAIRED FS 631 BULKHEAD AT LBL 36 & WL 78 IAW REO 601R-53-61-4765.

Part: BULKHEAD — CRACKED (BS 621) · airframe 30,684 hrs · 27,551 cycles

INDICATION NOTED AT FS 621 REAR PRESSURE BULKHEAD AT LBL 27.50, WL 141 APRROX .150 IN LENGTH AND 55 PERCENT FULL SCREEN HEIGHT. COMPLIED REO 601R-53-61-1546 AND REO 601R-53-61-1541 REV D DATED 10/31/2011.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,684 hrs · 27,551 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. COMPLIED WITH W/O 276849 AND REO 601R-52-11-513.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 30,684 hrs · 27,551 cycles

CARGO FLOORBEAM HAS CORROSION AROUND FASTENER HOLES AT FS 589, BETWEEN LBL 9 AND LBL 27. REMOVED CAP STRIP BETWEEN LBL 9 AND LBL 27 IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FS 589 FLOORBEAM CAP STRIP PN 601R35031-165 BETWEEN LBL 9 AND LBL 27 IAW SRM CH 51-42-06 AND 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 30,684 hrs · 27,551 cycles

PILOTS WINDSHIELD SIDE POST LOWER AFT OTBD FITTING IS CRACKED. REMOVED CRACKED LOWER AFT OTBD FITTING FROM PILOTS WINDSHIELD SIDE POST IAW SRM CH 51-42-21. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE LOWER AFT OTBD FITTING, PN 601R33235-3S ON PILOTS WINDSHIELD SIDE POST IAW SRM 51-42-21.

Part: BRACKET — CORRODED (BS 319) · airframe 30,684 hrs · 27,551 cycles

SERVICE DOOR CUTOUT TEE BRACKET IS SEVERELY CORRODED AT FS 319.70, WL 70.60. REMOVED FITTING IAW SRM 51-42-21 FOR REPLACEMENT. LOCATED & DRILLED NEW SERVICEABLE SERVICE DOOR FITTING IAW SRM 51-40-11 & INSTALLED NEW SERVICEABLE FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 30,684 hrs · 27,551 cycles

CO-PILOTS WINDSHIELD SIDE POST LOWER AFT, OTBD FITTING IS CRACKED. REMOVED CRACKED LOWER AFT OTBD FITTING FROM CO-PILOTS WINDSHIELD SIDE POST IAW SRM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE LOWER AFT OTBD FITTING, ON CP-PILOTS WINDSHIELD SIDE POST IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 30,684 hrs · 27,551 cycles

FS 484.00, ANGLE AT LBL 27 IS CRACKED. REPAIRED IAW REO 601R-53-41-059.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,684 hrs · 27,551 cycles

FLOORBEAM ANGLE CRACKED AT FS 280, LBL 9 INBD AND OTBD. R & R CRACKED FLOORBEAM ANGLE AT FS 280, LBL 9 INBD AND OTBD IAW SRM 51-42-21. FABRICATED NEW FS 280, LBL 9 INBD AND OTBD ANGLE IAW REO 601R-53-11-926.

Part: FLOOR SUPPORT — CORRODED (BS 559-589) · airframe 30,684 hrs · 27,551 cycles

RT FLOOR SILL HAS CORROSION AROUND FASTENER HOLDS BETWEEN FS 559+80 AND FS 589. BLENDED CORROSION IAW SRM 51-21-00. SRM HAS NO ALLOWABLE LIMITS. AMOUNT OF CORROSION REMOVED 0.011", REO 601R-53-00-505.

Part: FRAME — CORRODED (BS 605) · airframe 30,684 hrs · 27,551 cycles

FS 605, FRAME CORRODED BETWEEN STRINGERS 26L AND 26R. R & R FS 605 FRAME FROM STR 25L TO STR 22R IAW REO 601R-53-61-4763 USING SRM 53-00-15, SHEET 2 REPAIR NR 1 FRAME SPLICE REPAIR.

Part: ANGLE — CRACKED (BS 484) · airframe 30,684 hrs · 27,551 cycles

FS 484.00, ANGLE AT RBL 27 IS CRACKED. REPAIRED ANGLE IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 30,684 hrs · 27,551 cycles

LT FLOOR SILL HAS CORROSION AROUND FASTENER HOLES BETWEEN FS 559+96 AND 559+112. BLENDED CORROSION IAW SRM 51-21-06, SRM HAS NO ALLOWABLE LIMITS SUBMITTED FOR REPAIR DISPOSITION, AMOUNT REMOVED 0.011". C/W REO 601R-53-51-214.

Part: ANGLE — CRACKED (BS 484) · airframe 30,684 hrs · 27,551 cycles

FS 484.00 ANGLE AT LBL 9 IS CRACKED. R & R ANGLE IAW SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: DOOR — MISINSTALLED (CABIN) · airframe 30,684 hrs · 27,551 cycles

RT OVERWING EMERGENCY EXIT EXCEEDED FORCE TO OPEN. ON FURTHER INVESTIGATION, FOUND LT AND RT EMERGENCY EXIT DOORS INSTALLED IN WRONG LOCATION. FUNCTION TEST GOOD IAW AMM 52-21-00-720-801.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,290 hrs · 27,124 cycles

CEILING AFT EMERGENCY FLOOD LIGHT INOPERATIVE. LAMPED CEILING EMERGENCYH AFT FLOOD LIGHT IAW AMM 33-51-16.

Part: COALESCER BAG — ODOR · airframe 29,464 hrs · 26,251 cycles

ACFT HAS STRONG FUEL ODOR DURING DESCENT. R & R WATER SEPARATOR COLESCER ON LT AND RT PACKS IAW AMM 21-51-13, OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 202) · airframe 29,229 hrs · 25,992 cycles

BULKHEAD CRACKED AT FS 202 BY PARKING BRAKE CABLE. WORK COMPLETED IAW EC/TC REO 601R-53-11-563 AND STARTED DRILLING OUT FASTENERS FOR REPAIR NR 1 IAW EC/TC REO 601R-53-11-563. COMPLIED WITH NDT HFEC INSP ON 202 BULKHEAD, VERIFIED SEVERAL CRACKS, MARKED THE ENDS OF THE CRACKS IAW NDTM 51-20-06. CUT OUT DAMAGE IAW REO 601R-53-11-563, REV A. PERFORMED EDDY CURRENT INSPECTION IAW NDTM 51-20-06 . NO FURTHER DEFECTS NOTED. INSTALLED ALL REPAIR PARTS IAW REO601R-53-11-563.

Part: LATCH — LACK OF LUBE (PAX DOOR) · airframe 29,096 hrs · 25,838 cycles

ON PASSENGER DOOR, TEE HANDLE INDICATOR SHOWS LOCKED WHEN DOOR IS OPEN AND F/A IS HAVING DIFFICULTY OPENING AND CLOSING THE DOOR. LUBRICATED PASSENGER DOOR LATCH MECHANISM. PERFORMED OPS TEST OF THE PAX DOOR LATCH MECHANISM IAW AMM 52-11-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 28,482 hrs · 25,155 cycles

AFT CENTER CEILING EMERGENCY EXIT SIGN HAS SEVERAL INOPERATIVE BULBS. REPLAMPED AFT CENTER CEILING EMERGENCY EXIT SIGN. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,280 hrs · 24,930 cycles

LT OVER WING AFT EMERGENCY LIGHT INOPERATIVE. RELAMPED LT OVERWING AFT EM LIGHT W/A SERVICEABLE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,071 hrs · 24,698 cycles

WHITE EMERGENCY LIGHT ON LOWER PORTION OF FWD WARDROBE HAS INOP BULBS. RELAMPED THE EMERGENCY FLOOD LIGHT ASSY ON THE FWD WARDROBE AS REQUIRED. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,018 hrs · 23,475 cycles

NR5 EMERGENCY EXTERIOR LIGHT WILL NOT ILLUMINATE WHEN COMMANDED. REMOVED AND RELAMPED NR 5 EXTERNAL EMERGENCY LIGHT ASSY IAW 33-51-21. OPS CHECK GOOD.

Part: FLOOR PANEL — CORRODED (BS 409-559)

LT SIDE PRESSURE FLOOR CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 AND FS 559. REPAIRED IAW REO 601R-53-41-666.

Part: FLOOR PANEL — CORRODED (BS 409-559)

RT SIDE PRESSURE FLOOR CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 TO 559. BLENDED CORROSION IAW REO 601R-53-41-666.

Part: FLOOR PANEL — CORRODED (BS 409-559)

RT PRESSURE FLOOR CORRODED AT SEVERAL LOCATION BETWEEN FS 409 TO 559. REPAIRED IAW REO 601R-53-41-666.

Part: FLOOR PANEL — CORRODED (BS 409-559)

RT PRESSURE FLOOR CORRODED AT SEVERAL LOCATION BETWEEN FS 409 AND 559. PERFORMED UT THICKNESS INSPECTION OF BLEND AREAS IAW MAC NDT INSPECTION PROCEDURE UT-3. BLENDS AREAS ARE WITHIN ALLOWABLE LIMITS OF REO 601R-53-41-666 TABLE 2.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,975 hrs · 23,423 cycles

AFT PRESSURE BULKHEAD FWD FACE IS CRACKED ABOVE LINTEL ATTACH POINT. PERFORMED CUT OF ANGLE IAW REO 601R-53-61-1230. COMPLIED WITH STEP 7 OF REO 601R-53-61-1230. NO INDICATIONS NOTED AT THIS TIME. COMPLY WITH STEPS 8-14 OF REO 601R-53-61-1230. FABRICATED PN 601-35012-17 AND 601-35212-97 AND COMPLIED WITH STEPS 8-12 OF REO 601R-53-61-1230. INSTALLED REPAIR ITEM IAW STEP 13 AND 14 IAW REO 601R-53-61-1230 ALSO PERFORMED STEPS 1-4 OF REO 601R-53-61-3955.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 26,975 hrs · 23,423 cycles

SERVICE DOOR SILL ANGLE HAS CORROSION DAMAGE. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23, DRILLED/SEALED PLATE & INSTALLED IAW SRM 51-42-21, SRM 51-42-06 AND SRM 51-42-21. MINOR REPAIR.

Part: BULKHEAD — CORRODED (BS 202) · airframe 26,975 hrs · 23,423 cycles

SMALL AREA OF CORROSION ON THE FWD SIDE OF FS 202.00 BULKHEAD AROUND THE PARKING BRAKE CABLE. REMOVED SURFACE CORROSION IAW SRM 51-26-00,

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,975 hrs · 23,423 cycles

SHORT CARGO TIE DOWN SEAT RAILS AT WL 73.5 LBL 9.00,FS 559.00+80 TO FS 559.00+96 HAS CORROSION. R & R SHORT CARGO TIE DOWN SEAT RAIL ON LBL 9.00 BETWEEN FS 559 + 80 TO FS 559 + 96 IAW AMM 20-21-00-02. THIS IS A MINOR REPAIR.

Part: PRESSURE PANEL — CORRODED (CABIN FLOOR) · airframe 26,975 hrs · 23,423 cycles

LT SIDE PRESSURE FLOOR CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 AND 559. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS OF BLENDED AREA IAW MAC NDT INSP PROCEDURE UT-3. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS OF SRM 53-41-45 FIG 101. DAMAGE IS WITHIN LIMITS OF REO 601R-53-41-666.

Part: ATTACH FITTING — CRACKED (BS 473.15) · airframe 26,975 hrs · 23,423 cycles

LT O/W FUSELAGE PANEL, 161DL, ATTACH STRUCTURE JUST FWD OF CTR WING-TO-FUSELAGE ATTACH FITTING AT FS 473.15 CRACKED APPROX .5"L. R & R FUSELAGE PANEL 161DL ATTACH ANGLE PN 601R31037-61 IAW SRM 51-42-20 AND 51-23-16. MINOR REPAIR.

Part: PRESSURE PANEL — CORRODED (CABIN FLOOR) · airframe 26,975 hrs · 23,423 cycles

RT SIDE PRESSURE FLOOR CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 TO 559. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS OF BLENDED AREAS IAW MAC NDT INSP PROCEDURE UT-3. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS OF SRM 53-41-45 FIGURE 101. DAMAGE IS WITHIN LIMITS OF REO 601R-53-41-666.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 26,975 hrs · 23,423 cycles

SEAT TRACK CORRODED AT LBL9 FROM 409+126 TO 559+4. REMOVED AND INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802, STEP 2B.

Part: CARGO TRACK — CORRODED (BS 559-574) · airframe 26,975 hrs · 23,423 cycles

CORROSION FOUND ON SHORT CARGO TIE DOWN SEAT RAIL AT WL 73.5, RBL 9.00,FS 559.00+112 TO FS 574.00. R & R CARGO TIE DOWN SEAT RAIL ON RBL 9.00 BETWEEN FS 559.00 + FS 574 IAW AMM 20-21-00-02. THIS IS A MINOR REPAIR.

Part: CARGO TRACK — CORRODED (BS 559-574) · airframe 26,975 hrs · 23,423 cycles

CORROSION FOUND ON SHORT CARGO TIE DOWN SEAT RAIL AT WL73.5, LBL9.00, FS 559.00+112 TO FS 574.00. R & R SHORT CARGO TIE DOWN SEAT RAIL SECTION ON LBL 9.00 BETWEEN FS 559 + 112 TO FS 574.00 IAW AMM 20-21-00-02. THIS IS A MINOR REPAIR.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 26,975 hrs · 23,423 cycles

CORROSION FOUND ON SHORT CARGO TIE DOWN SEAT RAIL AT WL73.5, RBL9.00, FS 559.00+80 TO FS559.00+96. R & R SHORT CARGO TIE DOWN SEAT RAIL SECTION ON RBL 9.00 BETWEEN FS 559 + 80 TO FS 559 + 96 IAW AMM 20-21-00-02. THIS IS A MINOR REPAIR. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 26,975 hrs · 23,423 cycles

FLOOR SUPPORT HAS MINOR CORROSION AROUND SCREW HOLES AT LBL 27 FROM FS 589.00 TO 621.00. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-21-06 BEAM IS OUT OF LIMITS IAW 53-00-00. REMOVED FLOOR SUPPORT CAP FROM LBL 27, FS 574.00-FS 620.00. ALL WORK DONE IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW FLOOR SUPPORT CAP IAW REO 601R-53-61-3778. APPLIED FINISH TO AREA AND CIC IAW SRM 51-25-16, 51-21-11 AND REO 601R-53-61-3778, FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 26,975 hrs · 23,423 cycles

SEAT TRACK CORRODED FROM 409+126 TO 559+4 AT RBL9. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-000-802 AND AMM 53-01-11-400-802.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,765 hrs · 23,173 cycles

FIRST OFFICERS FLASHLIGHT INOP. REPLACED FO'S FLASHLIGHT IAW CRJ 200 AMM 25-60-00.

Part: RELAY — WORN (MLG) · airframe 26,053 hrs · 22,344 cycles

AFTER TAKEOFF SELECTED GEAR UP AND RECEIVED GEAR DISAGREE WARNING (EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O) R & R WOW SENSOR NR 1 RELAY, K1GA, IN JB11 IAW ESPM 20-22-00. REFER TO AFDL NR 533372-2 FOR GEAR OPS CKS.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 26,053 hrs · 22,344 cycles

ON TAKEOFF SELECTED GEAR UP, RECEIVED GEAR DISAGREE WARNING. THE PILOT REPORT THAT MANUAL RELEASE HANDLE WILL NOT STOW , LOST NOSE WHEEL STEERING TOWED BACK TO GATE. (EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O) R & R NLG SELECTOR VALVE ASSY IAW AMM 32-33-10, OPS CHECK AND LEAK CHECK IS GOOD, PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW AMM 32-30-00. OPS CHECK IS GOOD. CYCLE GEAR 15 TIMES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,553 hrs · 21,772 cycles

EXTERIOR EMERGENCY LIGHT NR 8 INOP. R & R LAMP IN EXTERIOR EMERGENCY LIGHT NR 8 IAW AMM 33-51-21. OP'S CHECK GOOD.

Part: PSEU — FAILED (MLG) · airframe 25,516 hrs · 21,725 cycles

AFTER TAKEOFF SELECTED, GEAR HANDLE UP, FOLLOWED BY GEAR DISAGREE WARNING MSG. ALL 3 GEAR ICAS SHOW WHITE AND UP WARNING MSG WENT OUT AFTER ABOUT 5-10 SECONDS. COMPLIED WITH QRH, DECLARED EMERGENCY AND RETURNED TO DEPARTURE, LANDED UNDER 47,000 LBS. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED). R & R THE PSEU IAW AMM 32-61-01, OPS CHECK GOOD PERFORMED 5 GEAR SWINGS NO FAULTS FOUND AT THIS TIME. R & R THE PSEU IAW AMM 32-61-01. OPS CHECK GOOD PERFORMED 5 GEAR SWINGS NO FAULTS FOUND AT THIS TIME.

Part: WARNING LIGHT — ILLUMINATED (RT ENG OIL PRESS) · airframe 24,960 hrs · 21,090 cycles

RT ENGINE OIL PRESSURE WARNING IN FLIGHT, SECOND WRITE UP OIL PRESSURE FLUCTUATING BETWEEN 20-37 PSI, WARNING PERSIST AT OR ABOVE CRUISE POWER SETTING. (EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O)

Part: HEATER — MALFUNCTIONED (WINDSHIELD) · airframe 24,775 hrs · 20,868 cycles

FLT 5287, RT WINDSHIELD (NR 3) HEAT CAUTION MSG IN FLT. RAN QRH AND CAUTION MSG STAYED ON. ALSO HAD AN ELECTRICAL BURNING ODOR DID NOT SEE SMOKE AND DID DECLARE AN EMERGENCY. [EMERGENCY DECLARED -- ENROUTE TO ATL A/C DIVERTED TO MGM DUE TO MTC].

Part: FLAP — FAILED (WING) · airframe 24,225 hrs · 20,287 cycles

FLAPS FAIL AT 5 DEGREES. EMERGENCY DECLARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 23,647 hrs · 19,714 cycles

RECEIVED GEAR DISAGREE WARNING AFTER RETRACTING LANDING GEAR ON CLIMBOUT (NOSE GEAR). COMPLIED QRH 47000 LB NORMAL LANDING. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O.

Part: POST — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

OPS 193 CONTINUED FROM JOB NR 8733515 OP NR 173. FS 409.0+128 VERTICAL POST BL 0 HAS INDICATION NOTED APPROX 3 INCH IN LENGTH 90 PERCENT FULL SCREEN HEIGHT RT SIDE WL 69.0 FLANGE, FAILED NDT INSP. INSTALLED NEW SERVICEABLE REINFORCING ANGLE ON POST BL 0 AT WL 69.0 IAW REO 601R-53-41-844 AND SRM 51-42-06 AND 51-42-22. CABIN AIR SUPPLY DUCT REQUIRES RECONNECT AT FS 409+128 TO "Y" DUCT. CONNECTED CABIN AIR SUPPLY DUCT TO "Y" DUCT AT FS 409+128. INSTALLED AND TIGHTENED BAND CLAMP. COMPLIED WITH EC/TC REO 601R-53-41-844 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-844. RII COMPLIED WITH.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

SUSPECT CRACK ON NLG AFT DOOR CUTOUT IN RADIUS ON RT SIDE.

Part: POST — UNKNOWN (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

JOB 8733515 OPERATION 172 F.S. 409+128 VERTICAL POST LBL 18.0 HAS INDICATION NOTED APPROX .3" IN LENGTH 90% FULL SCREEN HEIGHT OTBD SIDE WL 64 FLANGE FAILED NDT INSP.

Part: POST — UNKNOWN (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

JOB 8733515 OPERATION 173 F.S. 409+128 VERTICAL POST BL 0.0 HAS INDICATION NOTED APPROX .3" IN LENGTH 905 FULL SCREEN HEIGHT RT WL 69.0 FLANGE FAILED NDT INSP.

Part: POST — UNKNOWN (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

JOB 8733515 OPERATION 174 F.S. 409+128 VERTICAL POST HAS INDICATION NOTED APPROX .3" IN LENGTH AT RBL 18.0 WL 69.0 I/B AND O/B FLANGES 90% FULL SCREEN HEIGHT FAILED NDT INSP.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

LT FS 718 FRAME PREVIOUS REPAIR CRACKED 2" LONG BETWEEN STRS 10L AND 11L.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 349.00 INTERCOSTAL TOP CAP BETWEEN LBL 27.00 AND LBL 36.00 HAS SEVERAL NUTPLATE FASTENERS AND ATTACHMENT FASTENERS CORRODED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

REAR PRESSURE BULKHEAD FLOOR SUPPORT ANGLE FS 621 LEFT SIDE IS CRACKED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

FS 559.0 BULKHEAD WEB AND CAP ANGLE HAS INDICATIONS NOTED AT L CAP ANGLE LBL 18 APPROX .4" IN LENGTH 70% FSH AND RT WEB WL 54.10, WL 58.70 WK 54.10 APPROX .3" AND .5" IN LENGTH 100% FSH ALL FAILED NDT INSP. COMPLIED WITH REO 601R-53-41-260, REPAIRE TO PRESSURE BULKHEAD STRUCTURE AT FS 559 BL 23L TO 23R AND MAINTENANCE INSTRUCTION CARD TASK RJ2-53-1. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260, REV C.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 484.00 RBL 27.00 OUTBD ATTACHMENT ANGLE CRACKED.

Part: SILL — CORRODED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN CARGO COMPARTMENT FLOOR STRUCTURE FROM FS 559.00+112 TO FS 621.00 RBL 36.00 SILL PLATE HAS MINOR CORROSION AROUND FASTENER HOLES.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 280.00 LBL 9.00 OUTBD ATTACHMENT ANGLE CRACKED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 484.00 LBL 27.00 OUTBD ATTACHMENT ANGLE CRACKED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 349.00 INTERCOSTAL TOP CAP BETWEEN RBL 27.00 AND RBL 36.00 HAS SEVERAL NUTPLATE FASTENERS AND ATTACHMENT FASTENERS CORRODED.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 9,224 hrs · 7,528 cycles

ON DESCENT INTO INTO ATL THROUGH FL 270 SMELLED BURNING SMELL LIKE ELECTRICAL OR BURNING HAIR. SMELL WAS ISOLATED TO COCKPIT. NONE SMELLED IN PACKS OR BY FA STRONG SMELL LASTED ABOUT 45 SEC. NO INDICATION FROM CBS OR ELEC PAGE.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 484.00 LBL 9.00 OUTBD ATTACHMENT ANGLE CRACKED.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN PASSENGER COMPARTMENT FLOOR STRUCTURE PASSENGER DOOR HANDRAIL CUPS FS 315.00 AND FS 343.00 LBL 36.00 HAS MINOR SURFACE CORROSION.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 280.00 LBL 9.00 INBD ATTACHMENT ANGLE CRACKED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 23,157 hrs · 19,260 cycles

IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 460.00 RBL 9.00 OUTBD INTERCOSTAL ATTACHMENT FITTING CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,124 hrs · 19,226 cycles

EMERGENCY LIGHT ON BY PREVIOUS CREW OR CLEANING CREW. FLIGHT ATTENDANTS REPORTS LIGHT INOP. FLT 5034 DEL 92 MINS.

Part: ANCHOR FITTING — CRACKED (ASD) · airframe 22,808 hrs · 18,918 cycles

ASD FWD ANCHOR FITTING CRACKED. REMOVED & REPLACED TO COMPLY WITH SB 601R-52-116. PERFORMED MX IAW AMM TASKS; 52-11-17-000-803, 52-11-17-400-803, AND S.B. 601R-52-116 WITH REO 601R-52-11-1572. COMPLIED WITH ADJUSTMENT AND OPERATIONAL TEST. CHECKED GOOD.

Part: LINE — FAILED (HYD SYSTEM) · airframe 2,210,539 hrs · 18,299 cycles

HYDRAULIC SYSTEM 3 LOST ALL FLUID WHEN GEAR EXTENDED. EMERGENCY DECLARED, EMERGENCY TRUCKS FOLLOWED A/C TO THE GATE. REMOVED AND REPLACED 3B HYDRAULIC PUMP PRESSURE LINE IAW CRJ 200 AMM 29-12-18. OPS AND LEAK CK GOOD. LINE P/N AE4096G0060-000.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,710 hrs · 17,088 cycles

EMERGENCY LIGHT STRIP DOES NOT ILLUMINATE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 19,638 hrs · 16,262 cycles

CAPT'S FLASHLIGHT DEAD.

Part: LIGHT — ACTIVATED (SERVICE DOOR) · airframe 18,549 hrs · 15,452 cycles

SERVICE DOOR EMERGENCY LIGHT EXIT SIGN INOP.

Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 18,497 hrs · 15,411 cycles

SMELL ODOR IN REST OF AIRCRAFT. FOUND TO BE RIGHT PACK NOT WORKING PROPERLY. -OVERTEMP- IN AUTO AND MANUAL MODES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,168 hrs · 15,168 cycles

ALL CARGO FLOOR TRACKS CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,168 hrs · 15,168 cycles

CABIN FWD FLOOR TRACKS LT AND RT HAVE CORROSION.

Part: HANDLE — FROZEN (ESCAPE HATCH) · airframe 18,168 hrs · 15,168 cycles

CREW ESCAPE HATCH HANDLE FROZEN (WILL NOT EXTEND). BLENDED SCRATCHES ON RT TR EXTERIOR SKIN IAW CRJ200 SHORTS CMM 78-30-00 PG 5008. (SUPPLEMENTAL-SDR CLOSED)

Part: PRESSURE PANEL — CORRODED (BS 461-529) · airframe 18,168 hrs · 15,168 cycles

CORROSION AND BARE METAL FOUND ON RT CABIN PRESSURE FLOOR FROM FUS STA 461 TO 529. BLENDED AREAS ON RT CABIN PRESSURE FLOOR FROM STA 461-529 IAW SRM 51-21-06 CB7015474. APPLIED CORROSION INHIBITOR TO RT SIDE CABIN PRESSURE FLOOR AT FUSELAGE STA 461-529 REF CRJ 200 SRM 51-25-56 JOB COMPLETE(SUPPLEMENTAL - SDR CLOSED)

Part: FRAME — CORRODED (BS 349 S27) · airframe 18,168 hrs · 15,168 cycles

CORROSION FOUND ON FUSELAGE FRAME STA 349 AROUND STRINGER 27. REMOVEED CORROSION ON FUSELAGE FRAME STA 349 AROUND STRINGER 27 IAW SRM 51-00-00. (SUPPLEMENTAL - SDR CLOSED)

Part: FRAME — CORRODED (BS 319 S27) · airframe 18,168 hrs · 15,168 cycles

CORROSION FOUND ON FUSELAGE FRAME STA 319 AROUND STRINGER 27. REMOVED CORROSION ON FUSELAGE FRAME STA 319 AROUND STRINGER 27 IW SRM 51-00-00 10-11-06 ( SUPPLEMENTAL - SDR CLOSED 10/13/06 )

Part: FRAME — CRACKED (BS 320) · airframe 18,168 hrs · 15,168 cycles

ASD FWD FRAME MEMBER STA 320 CRACKED LOWER END (LOCKING BAR END)

Part: PRESSURE PANEL — CORRODED (BS 461-513) · airframe 18,168 hrs · 15,168 cycles

CORROSION FOUND ON LEFT CABIN OVER WING PRESSURE FLOOR DOUBLER FROM STA 461 TO 513 VARIOUS LOCATIONS. BLENDED AREAS OF CORROSION ON LEFT CABIN OVER WING PRESSURE FLOOR DOUBLERS FROM STA 461 TO 513 IAW SM 51-21-06 CB7015474 (SUPPLEMENTAL - SDR CLOSED)

Part: BEAM — CORRODED (BS 349) · airframe 18,168 hrs · 15,168 cycles

FOUND BS 349 TRANVERSE BEAM HAS CORROSION AT SERVICE DOOR OPENING. REPAIRED IAW REO 601R-53-21-710 (CLOSED)

Part: SKIN — CORRODED (FUSELAGE) · airframe 18,168 hrs · 15,168 cycles

FOUND EXTENSIVE CORROSION ON BELLY SKINS, RIBS AND STRINGERS FWD OF AVIONICS DOOR.

Part: FRAME — CRACKED (AIRSTAIR DOOR) · airframe 18,168 hrs · 15,168 cycles

ASD AFT FRAME MEMBER STA 338 CRACKED AT LOWER END (LOCKING BAR END).

Part: BEAM — CORRODED (BS 349) · airframe 18,168 hrs · 15,168 cycles

FOUND STA 349 TRANVERSE BEAM HAS CORROSION AT AIR STAIR DOOR OPENING. REMOVED CORRISION ON TRANSVERSE BEAM, WITHIN LIMITS , PRIMED AND PAINTED IAW SRM 51-21-06 CB7015474. (SUPPLEMENTAL - SDR CLOSED)

Part: FRAME — CORRODED (BS 333 S27) · airframe 18,168 hrs · 15,168 cycles

CORROSION FOUND ON FUSELAGE FRAME STA 333 AROUND STRINGER 27. REMOVED CORROSION ON FUSELAGE FRAME STA 333 AROUND STRINGER 27 IAW SRM 51-00-00 (SUPPLEMENTAL-SDR CLOSED).

Part: ATTACH FITTING — CRACKED (BULKHEAD) · airframe 18,168 hrs · 15,168 cycles

CARGO DOOR DOG HOUSE SUPPORT CLIP ON AFT BULKHEAD IS CRACKED (CARGO LINTEL SUPPORT CLIP). ALL WORK DONE IAW CRJ 200 SRM 51-42-20 DK 7022603 (SUPPLEMENTAL-SDR CLOSED)

Part: SKIN — CORRODED (FUSELAGE) · airframe 18,168 hrs · 15,168 cycles

CORROSION FOUND FWD OF AVIONICS DOOR CUTOUT IN BILGE AREA. REPAIRED IAW CRJ 200 SRM 51-00-00. (CLOSED)

Part: WEB — CORRODED (BS 280) · airframe 18,168 hrs · 15,168 cycles

FLOOR WEB IS CORRODED AT FS 280 BETWEEN RBL9 AND LBL9. REPAIRED IAW REO 601R-53-11-926 (SUPPLEMENTAL-SDR CLOSED)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,168 hrs · 15,168 cycles

CO-PILOTS SIDE BULKHEAD WEB CRACKED OTBD OF RBL9. WEB FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED WEB IAW REO 601R-53-11-926 REFER TO N/R-00204 MS 7022223 (SUPPLEMENTAL-SDR CLOSED)

Part: FLOORBEAM — CORRODED (BS 280) · airframe 18,168 hrs · 15,168 cycles

FOUND CORROSION ON FWD AND AFT SUPPORT ANGLES AT FS 280 BETWEEN LBL9 AND RBL9 FLOOR WEB. REPAIRED IAW REO 601R-53-11-926 (SUPPLEMENTAL-SDR CLOSED)

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 18,168 hrs · 15,168 cycles

LT OTBD FS 280 CLIP IS CRACKED. REMOVED AND REPLACED 280 CLIP IAW REO 601R-53-11-925 (SUPPLEMENTAL-SDR CLOSED)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,168 hrs · 15,168 cycles

PILOTS SIDE BULKHEAD WEB CRACKED OTBD OF LBL9. WEB FOUND TO BE OUT OF LIMITS, WEB WAS REMOVED AND REPLACED IAW REO 601R-53-11-926 REFER TO N/R-00204 (SUPPLEMENTAL-SDR CLOSED)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,790 hrs · 14,862 cycles

AFTER GEAR EXTENDED STEER INOP MESSAGE CYCLED SWITCH MESSAGE CLEARED. TOWER DECLARED EMERGENCY.

Part: WARNING MESSAGE — ACTIVATED (TE FLAPS) · airframe 17,057 hrs · 14,284 cycles

AFTER T/O IN LFT, GOT A FLAP FAIL MSG JUST AFTER ROTATING, FLAPS WERE AT 20 DEGREES. NEVER MOVED FLAP HANDLE. DIVERTED TO BTR. EN ROUTE TO ATL A/C DIVERTED TO BTR DUE TO MTC.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHT, NEAR THE TOP OF THE PASSENGER DOOR STEPS, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY LIGHT, NEAR THE TOP O THE PASSENGER DOOR STEPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING A HANGAR INSPECTIO IN MCN, 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. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING INSPECTION, THE GREEN EMERGENCY LIGHTING FORWARD OF ROW 5 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE SECTION OF EMERGENCY FLOOR STRIP LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4637 - DURING A GROUND INSPECTION IN DSM, THE EMERGENCY FLOOR TRACK LIGHTING FROM THE GALLEY TO ROW 6 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR TRACK LIGHTING POWER STRIP FROM THE GALLEY TO ROW 6. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN MDT, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SELECTOR VALVE — MALFUNCTIONED (NLG)

DURING APPROACH INTO ATL FROM EVV AFTER SELECTING GEAR DOWN THE CREW RECEIVED A GEAR DISAGREE WARNING MESSAGE. THE CREW EXECUTED A GO AROUND AND COMPLIED WITH THE QRH. THE CREW SELECTED THE GEAR HANDLE TO THE UP POSITION AND RECEIVED A GEAR DOWN INDICATION OF ALL GREEN AND NORMAL WITH THE ONLY EXCEPTION BEING THE NOSE GEAR DOOR REMAINING OPEN. AN EMERGENCY WAS DECLARED WITH EMERGENCY EQUIPMENT REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR DOOR SELECTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CHANNEL — CRACKED (RT MLG WW)

DURING A C-CHECK, THE MLG WHEEL WELL CHANNEL AT FS 529, RHS UNDER THE UPLOCK BOX WAS FOUND BENT AND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE MLG WHEEL WELL CHANNEL AT FS 529, RHS IAW EO. (K)

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM)

FLT 4414 - DURING CRUISE FROM MEM-DFW, AT APPROXIMATELY 28,000 FEET WITH THE AUTOPILOT ENGAGED, STABILIZER TRIM CHANNELS 1 AND 2 DISENGAGED. THE CREW COMPLIED WITH THE QRH AND ATTEMPTED RE-ENGAGEMENT OF CHANNELS 1 AND 2, WHICH RE-ENGAGED AND DISENGAGED AGAIN. AN EMERGENCY WAS DECLARED. FLAPS WERE SELECTED TO TWENTY DEGREES WITH THE AIRCRAFT LANDING SAFELY IN DFW. THE MAINTENANCE DIAGNOSTIC COMPUTER WAS INTERROGATED AND NO FAULTS WERE FOUND. MAINTENANCE ALSO ENGAGED THE STABILIZER TRIM SEVERAL TIMES AND PERFORMED A HORIZONTAL STABILIZER TRIM CONTROL UNIT SELF-TEST. AGAIN NO FAULTS WERE FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WIRE HARNESS — DAMAGED (NLG)

DURING CLIMB-OUT FROM ATL-MKE, THE CREW RECEIVED A GEAR DISAGREE MESSAGE AND COMPLIED WITH THE QRH. THE AIRCRAFT RETURNED WITH EMERGENCY VEHICLES BEING REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DRAG BRACE ELECTRICAL HARNESS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

FLT 4420 - DURING A GROUND INSPECTION IN DFW, THE FIRST FIVE ROWS OF EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE CONNECTION TO THE FIRST FIVE ROWS OF EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SQUAT SWITCH — OUT OF ADJUST (MLG)

DURING CLIMB OUT, UPON GEAR RETRACTION, THE CREW HEARD A STRANGE NOISE FROM THE GEAR WITH ALL INDICATIONS SHOWING NORMAL. WHEN PASSING THROUGH 2,000 FEET THE CREW RECEIVED A GEAR DISAGREE EICAS WARNING MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW ELECTED TO SELECT THE GEAR DOWN AT WHICH TIME ALL INDICATIONS WERE NORMAL AND ALL AURAL MESSAGES DISCONTINUED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, LANDING SAFELY. MAINTENANCE ADJUSTED THE WEIGHT ON WHEELS (WOW) SENSOR UPON DISCOVERING THE GAP WAS OUT OF LIMITS. MAINTENANCE ALSO NOSE JACKED THE AIRCRAFT AND OPERATED THE GEAR FIFTEEN TIMES. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4382 - DURING A GROUND INSPECTION IN MGM, AN EMERGENCY CELING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (AIRSTAIR)

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO COMPARTMENT AFT BULKHEAD LOWER LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: PLATE — CRACKED (FUSELAGE)

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

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

FLT 4708 - DURING APPROACH INTO YUL FROM ATL, THE CREW RECEIVED A FLAPS FAIL MESSAGE. THE CREW COMPLIED WITH QRH PROCEDURES, DECLARED AN EMERGENCY AND REQUESTED EMERGENCY EQUIPMENT. THE AIRCRAFT LANDED SAFELY IN YUL. MAINTENANCE COMPLIED WITH AD 98-20-01, PERFORMED A FLAPS INSPECTION AND RESET THE SYSTEM WITH NO DEFECTS FOUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ACTUATOR — INOPERATIVE (TE FLAP)

FLT 4810 - DURING APPROACH INTO SYR FROM ATL, THE CREW RECEIVED A FLAP FAILURE MESSAGE. WHEN SELECTING THE FLAPS TO EIGHT DEGREES THEY DID NOT MOVE. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT LANDED SAFELY IN SYR. THE LOCAL MECHANIC COMPILED WITH AD 98-20-01 RESETTING THE FLAP SYSTEM AND CYCLING THE FLAPS WITH NO DEFECTS NOTED. THE FLAPS ELECTRONIC CONTROL UNIT CODES SHOWED THE TOP THREE WERE JAMMED. MAINTENANCE REMOVED AND REPLACED THE NR 3 RIGHT OUTBOARD FLAP INBOARD ACTUATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

FLT 4771 - DUIRNG A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 14 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 14. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BEAM — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, LEFT SIDE ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED CRACKED ENGINE SUPPORT BEAM IAW ASA EO 600-53-0073. THIS EO INCLUDES REPAIR SPECIFICATIONS FOR ENGINE SUPPORT BEAM CRACKS AT BL 36.20 FOR CRJ200 AIRCRAFT. THIS EO REFERENCES ASA EO 600-53-0043. REO 601R-53-61-366 REV E, SERVICE BULLETIN A601R-53-059, AND SRM'S 51-00 REV 14 AND 53-00 REV 14. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN MCN, FRAME 718 LEFT WAS FOUND TO BE CRACKED. FRAME 718 RIGHT WAS FOUND ONLY TO HAVE A DOUBLER CRACKED NOT THE ACTUAL FRAME ITSELF. MAINTENANCE REMOVED AND REPLACED THE CRACKED DOUBLER IAW SRM 51-00. MAINTENANCE REPAIRED THE CRACKED LEFT 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 REF. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

DURING FLIGHT FROM ATL, WHILE CLIMBING THROUGH 28,000 FEET AT APPROXIMATELY 290 KNOTS, THE LEFT FRONT WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO TYS AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE PILOTS WINDSHIELD. OPERATIONAL AND PRESSURIZATION CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: COMPUTER — INOPERATIVE (E/E BAY)

FLT 4752 - ON CLIMB-OUT FROM MYR, CAPTAIN RECEIVED BOTH 'STAB TRIM' AND 'MACH TRIM' CAUTION MESSAGES THE CAPTAIN WAS ABLE TO RE-ENGAGE THE STAB AND MACH TRIM ONLY AFTER ENGAGING THE AUTOPILOT. THEN THE 'AP PITCH TRIM INOP' AND 'AP TRIM NOSE DOWN' CAUTION MESSAGES ILLUMINATED. AT THIS POINT AN EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO CHS AND HAD AN OVER GROSS LANDING WITHOUT INCIDENT. MAINTENANCE PERFORMED AN OVER GROSS LANDING INSPECTION. NO DEFECTS WERE NOTED. MAINTENANCE ALSO REORIENTED THE NR 2 ATTITUDE HEADING REFERENCE SYSTEM. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)