N820AS

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,260 hrs · 35,302 cycles

LIGHTED FLOOR-LEVEL EXIT SIGN INOPERATIVE AT LT EMERGENCY EXIT. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 39,163 hrs · 35,213 cycles

LIGHTED FLOOR-LEVEL EXIT SIGN AT LEFT EMERGENCY EXIT INOPERATIVE. R & R WIRE SPLICE CONNECTORS IAW SPM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 39,116 hrs · 35,168 cycles

F/A COULD NOT OPEN PASSENGER DOOR FROM THE IN SIDE GROUND CREW HAD TO OPEN DOOR. LUBE THE HARDWARE AND PERFOMED. OPS CHECK IAW AMM 52-11-03, CHECK GOOD ACOK TO SERVICE.

Part: DOOR — OUT OF LIMITS · airframe 38,537 hrs · 34,638 cycles

LEFT TRU DOOR DOES NOT FIT PROPERLY, PARTICULARLY IN RVSM AREA. TRIMMED TO FIT LT TRU DOOR IAW AMM 52-44-11. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: DOOR — OUT OF LIMITS · airframe 38,539 hrs · 34,639 cycles

RIGHT TRU DOOR DOES NOT FIT PROPERLY, PARTICULARLY IN RVSM AREA. TRIMMED TO FIT RIGHT TRU DOOR IAW AMM 52-44-11. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,087 hrs · 34,251 cycles

EXIT SIGN INOPERATIVE. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 37,950 hrs · 34,136 cycles

GALLEY LIGHTED FLOOR LEVEL EXIT SIGN DAMAGED. R & R SIGN IAW AMM 33-51-10. SYS OPS CHECKED GOOD. NO FURTHER ACTION.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,950 hrs · 34,136 cycles

LEFT EMERGENCY EXIT LIGHTED FLOOR LEVEL EXIT SIGN INOPERATIVE. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,829 hrs · 34,028 cycles

FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. R & R LIGHT ASSY IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,829 hrs · 34,028 cycles

FLOOR LEVEL EXIT SIGN INOPERATIVE AT LT OVERWING. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD.

Part: O-RING — FAILED (ENGINE OIL) · airframe 37,425 hrs · 33,676 cycles

AFTER TAKEOFF, RECEIVED RT OIL PRESSURE WARNING MESSAGE ACCOMPANIED WITH FLUCTUATIONS OF 25-36 PSI C/W QRH RETURNED TO DEPARTURE. ACFT RETURNED TO DEPARTURE AFTER TAKE OFF, EMERGENCY DECLARED. R & R RT ENGINE OIL PRESSURE SWITCH O-RING IAW AMM-79-31-03, LEAK CHECK GOOD.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 35,326 hrs · 31,721 cycles

PASSENGER DOOR LOWER SILL FROM FS 295 - 364 AT STRINGER LOCATION 18L IS CORRODED AT MULTIPLE LOCATIONS TO INCLUDE HANDRAIL STOW CUPS. REPAIRED FLOOR SILL FS 215 -364 IAW EO CL600-2B19-53-I00135.

Part: BULKHEAD — CRACKED (FUELAGE) · airframe 35,326 hrs · 31,721 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT BL 0.0 WL 142 APPROX 1.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-4823 AND REO 601R-53-61-1285, REV D, DATED 10/31/2011.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,326 hrs · 31,721 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX .2" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541 REF D.

Part: ANGLE — CRACKED (BULKHEAD) · airframe 35,326 hrs · 31,721 cycles

AFT SIDE OF REAR PRESSURE BULKHEAD HAS RT FS 621 - 625 OBLIQUE ANGLE CRACKED AT THE RADIUS APPROX .40" LONG. R & R RT FS 625 OBLIQUE ANGLE & SEALED IAW SRM REF 51-42-06, PN 601-35012-52.

Part: FRAME — CORRODED (BS 319 S26L) · airframe 35,326 hrs · 31,721 cycles

MAIN AVIONIC COMPARTMENT FUSELAGE FRAME 319 IS CORRODED AT STR 26L. REMOVED FRAME SECTOR IAW SRM 51-42-06. LOCATED & DRILLED NEW FRAME SECTOR IAW 51-40-11. INSTALLED NEW FRAME SEGMENT IAW SRM 51-42-06 & 51-42-21.

Part: FRAME — CORRODED (BS 333 S26R) · airframe 35,326 hrs · 31,721 cycles

MAIN AVIONIC COMPARTMENT FUSELAGE FRAME BS 333 IS CORRODED AT STR 26R. REMOVED CORRODED FRAME SEGMENT & SERVICEABLE REINFORCING ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW FRAME SECTOR AND REINSTALLED SERVICEABLE REINFORCING ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: FRAME — CORRODED (BS 310) · airframe 35,326 hrs · 31,721 cycles

MAIN AVIONIC COMPARTMENT FUSELAGE FRAME BS 310 CORRODED AT STR 26R. REMOVED FRAME SECTOR IAW SRM 51-42-06 & 51-42-21. TRIMMED FRAME SECTOR TO FIT AND LOCATED DRILL DEBURR IAW SRM 51-40-11 & 51-42-06 & 51-21-11. INSTALLED FRAME SEGMENT IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 35,326 hrs · 31,721 cycles

MAIN AVIONIC COMPARTMENT DOOR CUTOUT INTERCOSTAL BETWEEN FS 349 AND 364 BETWEEN STR 26-27R IS CORRODED. REMOVED CORRODED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL AND INSTALLED IAW SRM 51-42-06 AND 51-42-21.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,326 hrs · 31,721 cycles

PILOTS SIDE WINDOW POST AFT LOWER ATTACHMENT ANGLE IS CRACKED. R & R PILOT SIDE WINDOW POST AFT LOWER ATTACHMENT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: DOOR FRAME — CORRODED (BS 349 S26-27L) · airframe 35,326 hrs · 31,721 cycles

MAIN AVIONICS COMPARTMENT DOOR CUTOUT FRAME AT FS 349 BETWEEN STRINGERS 26L AND 27L ARE CORRODED. REMOVED CORRODED FS 349 LWR FRAME SEGMENT IAW SRM 51-42-06 & 51-42-21. DRILLED & LOCATED NEW FRAME. INSTALLED NEW FS 349 LWR FRAME SEGMENT IAW SRM 51-42-06 & 51-42-21.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 35,326 hrs · 31,721 cycles

CO-PILOTS SIDE WINDOW POST AFT LOWER ATTCHMENT ANGLE IS CRACKED. R & R CO-PILOTS SIDE WINDOW POST AFT LOWER ATTACHMENT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 35,326 hrs · 31,721 cycles

LT FWD SEAT TRACK IS CORRODED AT FS 364, LBL 9. R & R LT CABIN FLOOR FWD SEAT TRACK WITH A NEW SERVICEABLE RAIL IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 449-544) · airframe 35,326 hrs · 31,721 cycles

RT CABIN FLOOR 3RD SECTION OF SEAT TRACK IS CORRODED AT FS 449.85, 473.15, 513 AND 544 RBL 9. R & R RT CABIN FLOOR 3RD SECTION OF SEAT TRACK WITH A NEW SEAT TRACK IAW AMM 51-01-11-000-802 AND 51-01-11-400-802.

Part: ANGLE — CRACKED (BS 280) · airframe 35,326 hrs · 31,721 cycles

RBL 9 ANGLE ON OTBD SIDE AT FS 280 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-42-21 & 51-40-11.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 35,326 hrs · 31,721 cycles

MAIN AVIONICS COMPARTMENT DOOR CUTOUT INTERCOSTAL BETWEEN FS 349 AND 364 STRINGER 26L - 27L IS CORRODED. REMOVED CORRODED INTERCOSTAL, LOCATED & DRILLED NEW IAW SRM 51-42-06. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 35,326 hrs · 31,721 cycles

RT CABIN FLOOR 2ND SECTION OF SEAT TRACK IS CORRODED AT FS 394, 409+8 AND 409+86 RBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-020-002, FIG 401.B 1-3. LOCATED & DRILLED NEW SEAT TRACK IAW SRM 51-40-11-00. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 35,326 hrs · 31,721 cycles

RT CABIN FLOOR FWD SEAT TRACK CORRODED AT FS 364 RBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-020-002, FIG 1B 1-3. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-420-001 FIG 401B 1-8.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 35,326 hrs · 31,721 cycles

LEFT CABIN FLOOR 2ND SECTION OF SEAT TRACK IS CORRODED AT FS 394, 409+8 AND FS 409+16 LBL 9. REMOVED SEAT TRACK IAW AMM 53-01-11-000-801. LOCATED, DRILLED AND COUNTERSUNK NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 51-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 449-544) · airframe 35,326 hrs · 31,721 cycles

LEFT CABIN FLOOR 3RD SECTION OF SEAT TRACK IS CORRODED AT FS 449.85, 473.15, 513 AND 544 LBL 9. REMOVED SEAT TRACK IAW AMM 53-01-11-000-801. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. FABRICATED SEAT TRACK IAW REO 601R-53-00-485.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 35,326 hrs · 31,721 cycles

CARGO DOOR INNER SKIN CRACKED AT THE UPPER FWD STOP BRACKET. CUT AWAY DAMAGE TO CARGO DOOR INNER SKIN & CHANNEL WITH CAP ANGLE AT WL 97.25. NDT PERFORMED FOR CUT LINES, REFER TO FORM NDT-9. FABRICATED REPAIR PARTS, HEAT TREATED PARTS REQUIRED FROM TO CONDITION. ETCHED, ALODINED, PRIMED AND PAINTED ALL BARE METAL SURFACES. INSTALLED REPAIR IAW BSC EO CL600-2B19-52-I00141A.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 35,326 hrs · 31,721 cycles

CARGO DOOR AFT VERTICAL MEMBER CRACKED INSIDE OF DOOR AT LOWER AFT DOOR STOP FITTING. R & R AFT VERTICAL MEMBER IAW SRM 51-42-06.

Part: LIGHT — FAILED (CABIN) · airframe 35,326 hrs · 31,721 cycles

SERVICE DOOR INNER HANDLE EXIT SIGN LIGHT FAILED FUNCTIONAL TEST. REMOVED LIGHT IAW AMM 33-51-09-000-802. INSTALLED SERVICEABLE LIGHT IAW AMM 33-51-09-400-802.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,326 hrs · 31,721 cycles

CABIN LIGHTING FAILED TESTS. R & R BULBS IAW AMM 33-21-01-000-801. OPS CHECKED GOOD IAW AMM 33-21-07-400-801.

Part: LIGHT — FAILED (CABIN) · airframe 35,326 hrs · 31,721 cycles

FLOOR EMERGENCY LIGHTS FAILED. INSTALLED SERVICEABLE LIGHT IAW AMM 33-51-01-400-801.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 34,958 hrs · 31,397 cycles

ON ARRIVAL TO ACFT FOUND MAIN CABIN DOOR OUTER HANDLE JAMMED CLOSED, MISALIGNED WITH RECESSED RECEPTICAL. HAD TO PRY HANDLE OUT TO OPEN DOOR DOES NOT APPEAR TO CLOSE PROPERLY. CLEANED AND LUBED PAX DOOR HANDLE AND PERFORMED OPS CHECKED IAW AMM 52-11-23.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 34,653 hrs · 31,142 cycles

PAX DOOR STICKS AND IS REPORTED TO BE DIFFICULT TO OPEN AND CLOSE. LUBRICATED PAX DOOR IAW AMM 52-10-00. OPS CHECKED GOOD, REF 12-20-52.

Part: VALVE — FAILED (MLG) · airframe 34,157 hrs · 30,683 cycles

"GEAR DISAGREE "MASTER WARNING COMPLIED WITH QRH CYCLED GEAR TOOK APPROX 60 SEC FOR GEAR TO COME UP RT MAIN WAS SLOW TO COME DOWN HDY 3 PRESSURE WAS 2700PSI. EMERGENCY DECLARED AS A PRECAUTION. R & R PRIORITY VALVE IAW AMM 32-32-15 IPC REF 32-32-10 ITEM 205 / R/R ACMP PUMP IAW CRJ 200 AMM 29-11-03 IPC REF 29-11-03 ITEM 40A / PERFORMED FUNCTIONAL TEST OF THE LANDING GEAR EXTENSION AND RETRACTION. OPS CHECK GOOD NO FURTHER DEFECT NOTED. SDR CLOSED.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 33,290 hrs · 29,896 cycles

FLAPS FAIL, 20 DEGREES, UPON SELECTING FLAPS 30 DEGREES SPEED 180 KTS. EMERGENCY DECLARED, COMPLIED WITH EC/TC AD 2009-06-12. NO FAULTS. OK FOR SERVICE

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 33,042 hrs · 29,664 cycles

AT FL300 THE CAPTAINS WINDSHIELD BEGAN TO SPARK AND DELAMINATED RESULTING IN A CRACKED WINDSHIELD. FOLLOWED QRH, DIVERTED. R & R LT WINDSHIELD IAW AMM 56-11-01. LEAK AND OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 32,774 hrs · 29,421 cycles

EMERGENCY LIGHTS TURN ON WHEN SWITCH IS TURNED TO ARM. FOUND CIRCUIT BREAKER OPEN, CLOSED CIRCUIT BREAKER, OPS CHECKED GOOD IAW AMM 33-51-00.

Part: COALESCER BAG — CONTAMINATED · airframe 32,478 hrs · 29,146 cycles

ODOR IN CABIN ON GROUND AND IN FLIGHT. ODOR LIKE DIRTY SOCKS. OPS CHECK OF THE PACKS RT AND LT. OPS CHECKED GOOD, NO ODOR WITH REF TO AMM 21-51-00.

Part: FCU — FAILED (TE FLAPS) · airframe 32,371 hrs · 29,043 cycles

FLAPS FAIL MESSAGE IN FLIGHT GOING FROM 0 TO 8 DEGREES. EMERGENCY DECLARED AS A PRECAUTION. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOOD.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 30,956 hrs · 27,774 cycles

PAX DOOR LWR FWD INTERCOSTAL IN DRAIN RAMP AREA IS CRACKED. REMOVED UNSERVICABLE LWR FWD INTERCOSTAL AND INSTALLED SERVICABLE INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21. PAX DOOR LWR INNER STRUCTURE. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.

Part: FLOORBEAM — CRACKED (BS 589) · airframe 30,956 hrs · 27,774 cycles

CARGO BAY FLOORBEAM CAP AT LBL9 OTBD FLANGE AT FS 589 IS CRACKED. REPAIRED FLOORBEAM IAW EC/TC REO 601R-53-61-4009 AND REO 601R-53-61-4009. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 589) · airframe 30,956 hrs · 27,774 cycles

CARGO BAY FLOOR CAP STRIP BETWEEN STR9L AND STR27L AND FS 589 IS CORRODED. REMOVED FLOORBEAM CAP AND REPLACED WITH NEW STRIP IAW SRM 51-42-06. MAJOR REPAIR.

Part: ATTACH ANGLE — CORRODED (PAX DOOR) · airframe 30,956 hrs · 27,774 cycles

PAX DOOR LWR ATTACH ANGLES (5 EA) ARE CORRODED. REMOVED PAX DOOR LWR ATTACH ANGLES. LOCATED AND INSTALLED NEW ATTACH ANGLES IAW SRM 51-42-06.

Part: SKIN — CORRODED (SERVICE DOOR) · airframe 30,956 hrs · 27,774 cycles

CORROSION ON INNER SKIN OF SERVICE DOOR JUST ABOVE HINGE AREA. BLENDED OUT MINOR CORROSION, REMOVING 0.002 OF MAT'L USING DEPTH GAUGE 1916 D/D 1-14-12 (ORIG THK 0.063) REMAINING THICKNESS WAS 0.061 BLENDED IAW SRM 51-21-06. MINOR REPAIR.

Part: PLATE — CORRODED (CARGO DOOR) · airframe 30,956 hrs · 27,774 cycles

CARGO DOOR SEAL PLATE IS CRACKED AT FS 589. R & R CARGO DOOR SEAL PLATE IAW SRM 51-42-06. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 30,956 hrs · 27,774 cycles

SUPPORT BRACKET BETWEEN LT WING INBD AND CTR L/E'S IS CRACKED ON OTBD UPPER CORNER. R & R SUPPORT BRACKET BETWEEN LT WING INBD AND CENTER L/E'S IAW SRM 51-41-02 AND 51-45-00.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 30,956 hrs · 27,774 cycles

FS 484, LBL 36 OTBD CLIP CRACKED. REPAIRED IAW REO 601R-53-41-059. MAJOR REPAIR.

Part: SILL — CORRODED (FUSELAGE) · airframe 30,969 hrs · 27,786 cycles

SERVICE DOOR SILL HAS CORROSION ACROSS SILL FROM FWD TO AFT FRAMES. REMOVED UNSERVICEABLE SERVICE DOOR SILL. INSTALLED SERVICEABLE DOOR SILL IAW SRM 51-42-21. THIS IS A MAJOR REPAIR SILL PLATE FOR THE SERVICE DOOR, FABRICATED AND INSTALLED IAW EO 600-53-0687, DWG 601R33038-253, GMM 5-11 AND THE SRM AND MEETS WITH THEIR REQUIREMENTS RII FOUND TO BE SATISFACTORY 5001437 AAR 1671, DUE 5-4-11, CALIPERS. (SDR CLOSED)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 30,956 hrs · 27,774 cycles

FS 484, LBL 9, OTBD CLIP CRACKED. REPAIR COMPLETED IAW REO 601R-53-41-059. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED · airframe 30,956 hrs · 27,774 cycles

PAX DOOR FLOOR SUPPORT STRUCTURE HAS CORRODED FASTNERS, CORRODED SEAL STRUCTURE, AND MISSING FASTNERS, MARKED. REMOVED UNSERVICABLE PAX DOOR ANGLE WEB AND INSTALLED SERVICABLE PN 601R31527-151 IAW SRM 51-42-06. PAX DOOR CUTOUT SILL AREA. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 30,956 hrs · 27,774 cycles

FS 484, RBL 36, OTBD CLIP CRACKED. REPAIR TO THE 484 CLIP IS COMPLETED IAW REO 601R-53-41-059. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 589) · airframe 30,956 hrs · 27,774 cycles

FLOORBEAM STRUCTURE AT FS 589.0 OTBD IS CRACKED AT CARGO DOOR SEAL PLATE. R & R FLOORBEAM AT FS 589 IAW SRM 51-42-06 AND 51-42-21. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED · airframe 30,956 hrs · 27,774 cycles

CARGO BAY FLOORBEAM CAP AT LBL27 IS CORRODED. R & R FLOORBEAM CAP IAW SRM 51-42-06 AND 51-42-21. MAJOR REPAIR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,956 hrs · 27,774 cycles

REPAIR FROM RBL 27 TO LBL27 HAS SEVERAL UNSERVICEABLE FASTENERS. REMOVED UNSERVICABLE ANGLE AND INSTALLED SERVICABLE ANGLE PN 600 34017-3515 IAW SRM 51-42-06. LOCATION: FS280 FWD FLOOR SUPPORT ANGLE. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 30,956 hrs · 27,774 cycles

FS 349.00 OTBD OF LBL 27 HAS CORRODED HARDWARE, FLOOR SUPPORT STRUCTURE. REMOVED UNSERVICABLE HARDWARE AND INSTALLED SERVICABLE HARDWARE IAW SRM 51-42-13.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 30,956 hrs · 27,774 cycles

CARGO BAY COMPARTMENT HAS 1 ISOLATOR ON FS 621 AFT PRESSURE BULKHEAD BROKEN. R & R ISOLATOR IAW SRM 51-42-10.

Part: BULKHEAD — CRACKED (BS 559) · airframe 29,746 hrs · 26,707 cycles

VERIFY CRACK START AND STOP ON FWD SIDE OF 559. BULKHEAD AT RBL 18 POST. PERFORMED EDDY CURRENT INSP ON FWD SIDE OF PRESSURE BULKHEAD AT FS 559.00, RBL 18.0 IAW MAC NDT INSP PROCEDURE ET-2 MARKED ENDS OF CRACK. (CLOSED)

Part: FLOOR SUPPORT — CRACKED (BS 559) · airframe 29,746 hrs · 26,707 cycles

FLOOR SUPPORT HAS CRACK INDICATIONS AT FS 559, LBL 18.00 AND RBL 18.00. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.

Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 28,959 hrs · 25,985 cycles

EMERGENCY EXIT LAMP AT AIRSTAIR MISSING/ BROKEN. REPLACED EMER EXIT LIGHT FIXTURE AT PAX DOOR LOCATION IAW AMM 33-51-10. (CLOSED)

Part: BATTERY PACK — INTERMITTENT (EMERGENCY LIGHTS) · airframe 28,928 hrs · 25,956 cycles

EMERGENCY LIGHT ON CABIN OVERHEAD FWD SIDE COMES ON THEN GOES OUT AFTER ONE SECOND. (RESOLVED ON W/O: 154036 TASKCARD: N/R-00005 ) R & R BATTERY AND BATTERY CHARGER IAW IAW AMM 33-51-05-04 AND 33-51-04-04, OPS CKS GOOD IAW 33-51-04-740-801/ ITEM: 1/ EMERGENCY BATTERY REPLACED IAW AMM 33-51-04-04 / ITEM: 2 / EMERGENCY BATTERY CHARGER REPLACED IAW AMM 33-51-05-04 / ITEM: 3 / EMERGENCY BATTERY AND CHARGER OPS CKS C/W IAW AMM 33-51-04-740-801. (CLOSED)

Part: FLAP SYSTEM — OBSTRUCTED (TE FLAPS) · airframe 28,644 hrs · 25,606 cycles

FLAPS FAILED WHEN SELECTING 0 AFTER TAKE OFF (AT 2 DEG) POST FLIGHT FOUND SNOW BETWEEN WING T/E AND FLAP LEADING EDGE. ENROUTE, ACFT DIVERTED EMERGENCY DECLARED - EMERGENCY VEHICLES ON STANDBY AS A PRECAUTION. C/W AD 2009-06-12, OPS TEST GOOD IAW AMM NR 27-54-00-710-801.

Part: FLASHLIGHT — MALFUNCTIONED (COCKPIT) · airframe 28,482 hrs · 25,440 cycles

CAPTAINS FLASHLIGHT WORKS BETTER IN OFF POSITION THAN ON.

Part: FLASHLIGHT — FAILED (COCKPIT) · airframe 28,482 hrs · 25,440 cycles

R & R CAPT FLASHLIGHT IAW AMM 25-60-00. (CLOSED)

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 28,102 hrs · 25,033 cycles

ON DEPARTURE GOT PAX DOOR LATCH CAUTION MSG AT 6000' FELT & HEARD A RUMBLE AND THEN GOT PASSENGER DOOR WARNING MSG. COMPLIED W/QRH [EMERGENCY VEHICLES WERE ROLLED AS A PRECAUTION -- AIRCRAFT RETURNED TO BTR AFTER T/O]...FLT 5518 DEL 130 MINS

Part: DOOR — STUCK (MAIN PAX) · airframe 27,986 hrs · 24,914 cycles

MAIN ENTRY DOOR DIFFICULT TO OPEN FROM INSIDE

Part: DOOR — BINDING (PAX DOOR) · airframe 27,904 hrs · 24,835 cycles

PASSENGER DOOR DIFFICULT TO OPEN FROM INSIDE OR OUT SIDE. FLT 5364 DEL 27 MINS.

Part: WIRE — PULLED (COCKPIT) · airframe 27,070 hrs · 23,973 cycles

FLOODLIGHT ON COCKPIT PANEL 221FLW HAS BROKEN BASE AND WIRES ARE PULLED OUT OF LIGHT ASSY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,070 hrs · 23,973 cycles

CARGO BAY FLOORBEAM HAS CORROSION BETWEEN FS 559+96 AT RBL 9. REMOVED CORROSION IAW SRM 53-00-00 FIG 102, 51-21-06. BLENDED AREA OF CARGO BAY FLOORBEAM IAW NDTM PART 1 51-20-08. NO RELEVANT INDICATIONS NOTED AT THIS TIME.

Part: SKIN — DAMAGED (RT WING) · airframe 27,070 hrs · 23,973 cycles

RT LOWER WING PLANK FUEL ACCESS HOLE 640DB HAS MULTIPLE INDICATIONS NOTED IN AFT LANDING CRITICAL AREA APPROX .5 INCH IN LENGTH 50 PERCENT FSH AND O/B LANDING NON-CRITICAL AREA APPROX .2 INCH IN LENGTH 50 PERCENT FSH FAILED NDT INSP AREAS MARKED ON ACFT. REPAIRED RT WING PLANK AT ACCESS HOLE 640DB IAW REO 601R-57-21-030, STEPS 1-12. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G.

Part: POST — DAMAGED (FUSELAGE) · airframe 27,070 hrs · 23,973 cycles

LEFT LBL 18.0 VERTICAL POST AT FS 409.0+128 O/B SIDE WL 69.0 HAS INDICATION NOTED APPROX .2 INCH IN LENGTH 50 PERCENT FULL SCREEN HEIGHT, FAILED NDT INSPECTION ON AFT FLANGE WL 69.0. REMOVED POST IAW SRM 51-42-06. FABRICATED REPLACEMENT POST IAW SRM 51-24-21.

Part: POST — DAMAGED (FUSELAGE) · airframe 27,070 hrs · 23,973 cycles

RT RBL 18.0 VERTICAL POST AT FS 409.0+128 I/B AND O/B SIDES AT WL 69.0 AFT FLANGES HAVE INDICATIONS NOTED APPROX .2 INCHES IN LENGTH 55 PERCENT FULL SCREEN HEIGHT, FAILED NDT. REMOVED RT RBL 18.0 VERT POST AT FS 409+128 IAW SRM 51-42-06. FABRICATED REPLACEMENT POST IAW SRM 51-24-21. INSTALLED POST IAW SRM 51-42-06 AND EC/TC REO 601R-53-41-889.

Part: POST — DAMAGED (FUSELAGE) · airframe 27,070 hrs · 23,973 cycles

FS 409.0+128 VERTICAL POST BL 0.0 RT SIDE AFT FLANGE AT WL 69.0 HAS INDICATION NOTED APPROX .2 INCH IN LENGTH 70 PERCENT FSH, FAILED NDT INSPECTION. REPAIRED BULKHEAD IAW REO 601R-53-61-1285 AND 601R-53-61-3099.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 27,070 hrs · 23,973 cycles

AN INDICATION WAS NOTED ON THE 621 REAR PRESSURE BULKHEAD FWD FACE AT THE LINTEL ATTACH FITTING UPPER I/B CORNER APPROX .10 IN LENGTH 50 FSH. WHILE PERFORMING REAR PRESSURE BULKHEAD ET INSPECTION, FAILED NDT. REPAIRED PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 27,070 hrs · 23,973 cycles

RIGHT FS 484.00 INTERCOSTAL PREVIOUS REPAIR ANGLE AT RBL 36.0 IS CRACKED. REPAIRED INTERCOSTAL IAW REO 601R-53-41-059

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,070 hrs · 23,973 cycles

CARGO BAY FLOOR SEAT RAIL BETWEEN FS 559.00+80 AND FS 559.00+96 HAS CORROSION AROUND SCREW HOLES AT RBL 27.0. INSTALLED NEW SEAT TRACK IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,070 hrs · 23,973 cycles

CARGO BAY FLOOR SEAT RAILS BETWEEN FS 559.00+80 AND FS 574.00 AT RBL 9 HAVE CORROSION AROUND SCREW HOLES. REMOVED SEAT TRACK IAW SRM 51-41-02. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (CARGO BAY) · airframe 27,070 hrs · 23,973 cycles

CABIN FLOOR SEAT RAILS BETWEEN FS 559.00 AND FS 559.00+80 AT RBL 9 AND LBL 9 HAVE CORROSION. REMOVED CABIN SEAT TRACKS. FABRICATED SEAT TRACK, DRILLED AND COUNTERSUNK HOLES IAW SRM 51-40-11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,070 hrs · 23,973 cycles

CARGO BAY CARGO TRACK BETWEEN FS 559.00+110 AND FS 621.00 AT LBL 9 HAVE CORROSION AROUND SCREW HOLES. REMOVED DAMAGED CARGO TRACK, FABRICATED NEW SECTIONS OF CARGO TRACK. LOCATED, DRILLED, AND COUNTERSUNK 2 OF 5 SECTIONS. ALL WORK PERFORMED IAW SRM 51-40-11.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 27,070 hrs · 23,973 cycles

CARGO FLOOR SEAT RAILS BETWEEN FS 559.00+80 AND FS 559.00+120 AT LBL 27 HAVE CORROSION AROUND SCREW HOLES. REMOVED DAMAGED CARGO TRACK. FABRICATED NEW SECTION OF CARGO TRACK, LOCATED, DRILLED, AND COUNTERSUNK HOLES IAW CRJ 200 SRM 51-40-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,802 hrs · 23,717 cycles

LT FUSELAGE NR 2 EMERGENCY LIGHT INOP.

Part: COVER — MISSING (CABIN) · airframe 26,802 hrs · 23,717 cycles

LOWER EMERGENCY EXIT LIGHT COVER BY ASD, IS MISSING. FLT 5047 DEL 49 MINS.

Part: LIGHT — INOPERATIVE · airframe 26,411 hrs · 23,359 cycles

LT FUSELAGE EMERGENCY LIGHT FWD OF WING INOP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 26,325 hrs · 23,278 cycles

NR 1 EMERGENCY BATTERY PACK FAILED.

Part: DOOR — MALFUNCTIONED (SERVICE DOOR) · airframe 26,174 hrs · 23,140 cycles

SERVICE DOOR WILL NOT STAY OPEN AND LOCKED. COULD NOT DUPLICATE. OK FOR SERVICE. NO FAULT FOUND.

Part: ROLL PIN — DAMAGED (DOOR HANDLE) · airframe 25,729 hrs · 22,740 cycles

SERVICE DOOR WILL NOT LATCH IN OPEN POSITION WHEN OPENED FROM INSIDE THE ACFT. ALSO DIFFICULT TO OPEN FROM OUTSIDE. FLT 4167 DEL 155 MINS. REMOVED AND REPLACED DOOR HANDLE ROLL PIN IAW AMM 52-41-01. OPS CHECK GOOD. (S)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,568,428 hrs · 22,702 cycles

FORWARD OVER HEAD EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED FWD OVERHEAD EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD. (B)

Part: LIGHT — MISSING (CABIN) · airframe 24,561 hrs · 21,775 cycles

EMERGENCY FLOOR LIGHTING STRIPS ROW 11 MISSING EGRESS ARROWS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,461 hrs · 21,686 cycles

FOUND FWD CEILING EMERGENCY LIGHT INOP.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 24,433 hrs · 21,660 cycles

FOUND LT SIDE AFT EMERGENCY LIGHT BULB BURNED OUT.

Part: DOOR — BINDS (EMERGENCY EXIT) · airframe 23,921 hrs · 21,209 cycles

EXCESSIVE FORCE REQUIRED TO OPEN EMERGENCY DOOR.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 23,102 hrs · 20,533 cycles

BONDED SKIN DOUBLER CRACKED IN AFT EQUIP BAY, LT SIDE STR 9, FS 640. [07-23-07] REPAIRED IAW EO 601R-53-61-506.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 22,646 hrs · 20,187 cycles

PRESSURE FLOOR SKIN UNDER FLOORBOARD 261 DRF HAS SEVERAL AREAS OF SURFACE CORROSION I/B OF DADO PANEL.

Part: SKIN — CRACKED (RT WING) · airframe 22,646 hrs · 20,187 cycles

RIGHT WING PLANK CRACKED ON WS 148 COMMON TO AFT SPAR FLANGE. PERFORMED REPAIR ON R/H LOWER WING PLANK AFT AT WS 148.019, IAW REO 601R-57-21-130. (EMP 752 - INSP RA333) ALL WORK DONE IAW ASA EO 600-57-13402. (EMP 818 - INSP RA189) FUEL LEAK CHECK REQUIRED. LEAK CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (INSP RA318) (RII - 5000528 - FOR REPAIR.) (RII - 5001437 - FOR FUEL LEAK CHECK)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 22,646 hrs · 20,187 cycles

CRACK THRU 2 FASTENERS ON AFT PRESS BULKHEAD INTERCOSTAL AT FS 623.00 LBL 51.5 STR 13L VERT FANGE OF INTERCOSTAL REQ'S CRACK LENGTH VERIFICATION. SERVICE BULLETIN 601R-53-048, FUSELAGE GENERAL VISUAL INSPECTION OF THE INTERCOSTAL MEMBERS AT FS 621/FS625.3 INCORPATED. CRACK MEASURES LESS THAN 1.50 IN LENGTH. OK FOR CONTINUED SERVICE PER REO 601R-53-61-105 AND SERVICE BULLETIN 601R-53-048. MDA 1064 2-21-07. RA333.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,646 hrs · 20,187 cycles

FS 484 ANGLE CRACKED I/B SIDE OF FLOORBEAM AT LBL 27.0.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,646 hrs · 20,187 cycles

FS 484 ANGLE CRACKED O/B SIDE OF FLOORBEAM AT LBL 27.0 (MARKED).

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 22,646 hrs · 20,187 cycles

FLOOR SUPPORT FITTING AT FS 460.5 O/B OF LBL 9.0 CRACKED MID TOP MARKED. REMOVED CRACKED FITTING IAW CRJ SRM 51-42-21. DRILLED AND LOCATED NEW FITTING P/N 600-31068-19 IAW CRJ SRM 51-40-11. OK TO INSTALL. (INSP RA333) INSTALLED SERVICEABLE FITTING IAW CRJ SRM 51-42-21. (EMP 699) OK TO PAINT. (INSP RA323) TOPCOATED REPAIR AREA IAW CRJ SRM 51-25-16. (EMP699 - INSP RA333). SUPPLEMENTAL - SDR CLOSED 02/15/07.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 22,646 hrs · 20,187 cycles

PRESSURE FLOOR SKIN UNDER FLOORBOARD 261 DLF HAS SEVERAL AREAS OF SURFACE CORROSION I/B OF DADO PANEL.

Part: PLACARD — UNSERVICEABLE (PAX DOOR STEP) · airframe 22,646 hrs · 20,187 cycles

THE -EXIT- PLACARD ON PAX DOOR STEP 832 BT IS UNSERVICEABLE.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 22,260 hrs · 19,901 cycles

NOSE WHEEL STEERING INOP AFTER TAKEOFF & COMPLIED W/QRH. EMERGENCY VEHICLES WERE ON STANDBY AS A PRECAUTION. FLT 4515 DEL 80 MINS.

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 22,010 hrs · 19,717 cycles

NOSE GEAR DISAGREE ON RETRACTION. WEIGHT ON WHEELS MESSAGE WITH NOSE SHIMMY AND NOSE WHEEL STEERING INOP AND NO N/W/S INOP MESSAGE. A/C RETURNED TO SGF AFTER T/O. THE TOWER ROLLED THE TRUCKS AS A PRECAUTION. FLT 4812 DEL 960 MINS.

Part: MOUNT — CRACKED (AIRSTAIRS) · airframe 21,059 hrs · 18,975 cycles

ASD AFT ANCHOR MOUNT CRACKED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

DURING A GROUND INSPECTION, THE CENTER SECTION OF THE EMERGENCY FLOOR STRIP LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR STRIP LIGHTS POWER SUPPLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CLAMP — LOOSE (ENGINE)

DURING CLIMB OUT, THE CREW RECEIVED A LT JET OVERHEAT MESSAGE. THE CREW COMPLIED WITH THE QRH WHEN THEY RECEIVED A LT 10TH DUCT WARNING MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DEPARTURE, WHERE IT LANDED SAFELY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE ENGINE SIDE OF THE 14TH STAGE SHUTOFF VALVE PIPE CLAMP LOOSE. MAINTENANCE TIGHTENED THE CLAMP AND RAN THE ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

FLT 4368 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: INVERTER — MALFUNCTIONED (NR 2)

DURING A GROUND INSPECTION, THE EMERGENCY LIGHTS FROM ROWS 2 TO 4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 INVERTER FOR THE EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BATTERY — DISCHARGED (NR 3 BATTERY)

DURING GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BATTERY — DISCHARGED (NR 4 BATTERY)

DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BATTERY — DISCHARGED (NR 1 BATTERY)

DURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BATTERY — DISCHARGED (NR 2 BATTERY)

DURING GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGE THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERTIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN ATL, THE FORWARD SECTION OF EMERGENCY FLOOR LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD SECTION EMERGENCY FLOOR LIGHT STRIP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — BROKEN (CABIN)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOODLIGHT ASSEMBLY AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

FLT 4249 - DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT LIGHT AT ROW 8A WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND LOOSE CONNECTOR TO THE EMERGENCY EXIT LIGHT AT ROW 8A AND RESECURED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PUSH-PULL ROD — BINDING (PAX DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND HARD TO CLOSE WHICH WAS ACCOMPANIED BY AN OUTER HANDLE CAUTION MESSAGE. THE AC WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT FOR MAINTENANCE REPAIRS TO THE PASSENGER DOOR. THE AC WAS FERRIED AND LANDED SAFELY. MAINTENANCE ADJUSTED THE PASSENGER DOOR PUSH-PULL ROD ASSEMBLY IAW MM. OPERATIONAL AND PRESSURIZATION LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: WIRE — BROKEN (DOOR HANDLE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE AND THE GREEN ALIGNMENT MARKS WERE NOT ALIGNED. MAINTENANCE INSPECTED THE AC AND FOUND IT SAFE FOR A FERRY FLIGHT FOR PERFORMANCE OF THE APPROPRIATE C/A. MAINT FOUND THE INNER HANDLE PROXIMITY SWITCH PREVENTING THE HANDLE FROM STOWING PROPERLY AND ADJUSTED THE SWITCH. MAINT ALSO REPAIRED A BROKEN WIRE ON THE OUTER HANDLE STOW SWITCH AND INNER HANDLE SWITCH; ALSO ADJUSTED THE CAM ROLLER TO THE TORQUE TUBE. OPS CHECK GOOD. AC OK FOR SERVICE.

Part: HANDLE — BINDING (PAX DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WAS FOUND DIFFICULT TO OPEN AND THE SLOW HANDLE PUSHING OUT. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE AND INTERNAL MECHANISM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: HANDLE — DAMAGED (PAX DOOR)

FLT 4475 - DURING A GROUND INSPECTION IN MLU, THE FLIGHT ATTENDANT HAD DIFFICULTY CLOSING THE PASSENGER DOOR AND DURING TAKEOFF FROM MLU-ATL A PASSENGER DOOR HANDLE EICAS MESSAGE WAS RECEIVED. THE FLIGHT CONTINUED AND AFTER LANDING SAFELY IN ATL, THE FLIGHT ATTENDANT HEARD A LOUD BANG WHEN THE PASSENGER DOOR WAS UNLOCKED. MAINTENANCE REPAIRED THE PASSENGER DOOR HANDLE, LOCK MECHANISM AND ADJUSTED THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING C-CHECK, THE FLOOR MEMBER WEBBING AT FS 280 BETWEEN LBL9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR MEMBER WEBBING AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)

Part: ANGLE — CORRODED (FUSELAGE)

DURING C-CHECK, THE ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING C-CHECK, THE TRANSVERSE BEAM AT FS 280 BETWEEN LBL9 AND LBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE TRANVERSE BEAM AT FS 280 BETWEEN LBL 9 AND LBL 27 IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, THE RT INBOARD CLIP AT FS 484 BETWEEN RBL 9 TO RBL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINT REMOVED AND REPLACED THE RT IB CLIP AT FS 484 BETWEEN RBL 9 TO RBL 27 IAW SRM. (K)

Part: RIB — CRACKED (LT WING WW)

DURING A C-CHECK, THE LT BATT RIB ASSY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT BATT RIB ASSY AT WS 53.60 IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE ATTACH CLIP AT FS 625 LT ABOVE THE BOX BEAM WAS FOUND TO BE CRACKED BEYOUND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE ATTACH CLIP AT FS 625 LT. (K)

Part: FITTING — CRACKED (PRESSURE FLOOR)

DURING A (C) CHECK, THE FITTING IN THE RT SIDE PRESSURE FLOOR UNDER 262CRF AT APPROX FS 454.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FITTING IN THE RT SIDE PRESSURE FLOOR UNDER 262CRF AT APPROXIMATELY FS 454.00. (K)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FRAME FS 640 BETWEEN STRINGER 9 AND 12 LT WAS FOUND TO BE CRACKED BEYOND LIMITS IN THE RADIUS FORWARD SIDE ABOVE THE BOX BEAM. MAINTENANCE IS REPAIRING THE FRAME FS 640 BETWEEN STRINGER 9 AND 12 LT IAW EO. (K)

Part: LIGHT — DEFECTIVE (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY 'EXIT PULL' LIGHT ON THE PASSENGER DOOR WAS FOUND TO BE UNREADABLE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY 'EXIT PULL' BETA LIGHT ON THE PASSENGER DOOR.

Part: STEP — CRACKED (PAX DOOR)

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

Part: SKIN — CRACKED (LT WING)

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

Part: HANDLE — LACK OF LUBE (PAX DOOR)

FLT 4360 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG UPLOCK) · airframe 17,692 hrs

AFTER TAKEOFF, THE CREW RECEIVED A (GEAR UP DISAGREE) MESSAGE. THE QRH WAS COMPLIED WITH, AND EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE, LANDING SAFELY. MAINTENANCE ADJUSTED THE UPLOCK PROXIMITY TARGET ON THE LEFT MAIN LANDING GEAR (MLG). OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BATTERY — DISCHARGED (POWER SUPPLY)

DURING ROUTINE SERVICE INSPECTION, THE PASSENGER DOOR EMERGENCY FLOODLIGHT AND THE FORWARD OVERWING EMERGENCY EXIT LIGHTS ON THE LT AND RT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY AND POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING AN OVERNIGHT CHECK IN SHV, THE EMERGENCY FLOOR LIGHT SECTION AT ROW 1-C WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AT ROW 1-C. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM)

FLT 4124 - DURING CLIMB-OUT FROM TRI-ATL, THE CREW NOTICED A LARGE FUEL DISPARITY BETWEEN THE PEFORMANCE INITIALIZATION PAGE AND THE TOTAL FUEL ON THE EICAS AND OVER THE FOLLOWING TEN MINUTES THE FUEL QUANTITY DROPPED 2,000 LBS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETUREND TO TRI, LANDIGN SAFELY. MAINTENANCE RESET THE FUEL COMPUTER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

FLT 4829 - DURING AROUND INSPECTION IN DFW, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE ACTUATOR ARM CONNECTION. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (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: BEAM — CRACKED (BULKHEAD)

DUIRNG A C-CHECK IN MCN, THE SECOND FROM AFT CARGO WALL BULKHEAD TRANSFER BEAM UNDER THE SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SECOND FROM AFT CARGO WALL BULKHEAD TRANSFER BEAM UNDER THE SEAL PLATE IAW SRM 51-42-70. (M)

Part: STRINGER — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR STRINGER AT FS 349 AFT OF THE PASSENGER DOOR WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOOR STRINGER AT FS 349 AFT OF THE PASSENGER DOOR IAW ASA EO 600-53-0052. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FIRST SEAT TRACKS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT FIRST SEAT TRACKS IAW ASA EO 600-53-0052. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE ANGLE AT FS 640 AND BL 45 BETWEEN STRINGERS 9 AND 12 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ANGLE AT FS 640 AND BL45 BETWEEN STRINGERS 9 AND 12 IAW ASA EO 600-53-0081B. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT SEAT TRACKS AT FS 349 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT SEAT TRACKS AT FS 349 IAW ASA EO 600-53-0052. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOORBEAMS AT LEFT ADN RIGHT 9 AND 27 BETWEEN FS 280 AND FS 409 PLUS 5 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOORBEAMS AT LEFT AND RIGHT 9 AND 27 BETWEEN FS 280 AND FS 409 PLUS 5 IAW ASA EO 600-53-0052. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTAL BRACKET AT FS 484 AND LBL 27 AND RBL/LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INTERCOSTAL BRACKET AT FS 484 AND LBL 27, RBL/LBL 36 IAW SRM 51-00. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT FS 621 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN DFW, THE EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY FLOOR LIGHT STRIPS IN THE AFT CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY FLOOR LIGHT STRIP CONNECTORS IN THE AFT CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LINE — CHAFED (APU FUEL SYS)

FLT 4463 - DUIRNG FLIGHT FROM MKE-ATL AND ON THE GROND, A FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN AFTER THE ENGINE WAS STARTED WITH THE BLEEDS ON THE AUXILIARY POWER UNIT OR THE ENGINE. MAINTENANCE REMOVED AND EPLACED A CHAFED FUEL LINE ON THE AUXILIARY POWER UNIT. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A HANGAR CHECK IN MCN, FRAME 640 BETWEEN STRINGERS 13 AND 14 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED FRAME 640 BETWEEN STRINGERS 13 AND 14 ON THE RIGHT SIDE IAW ASA EO 600-53-0086. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

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

Part: SUPPORT — CRACKED (LT & RT ENGINE)

DURING A HANGAR CHECK IN MCN, THE LEFT AND RIGHT ENGINE SUPPORT BEAM AT BL 36.20 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT ENGINE SUPPORT BEAM AT BL 36.20 IAW ASA EO 600-53-0073. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A HANGAR CHECK IN MCN, FRAME STATION 718 BETWEEN STRINGERS 10 TO 12 ON THE LEFT AND RIGHT SIDES, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING FRAME STATION 718 BETWEEN STRINGERS 10 TO 12 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-0067A. (M)

Part: DUCT — LEAKING (A/C BAY)

FLT 4541 - DURING DESCENT INTO MCO, A RAPID LOSS OF CABIN PRESSURE WAS EXPERIENCED. AS A PRECAUTIONARY MEASURE THE CREW USED THE OXYGEN MASKS. AN EMERGENCY WAS DECLARED AND THE LANDED SAFELY IN MCO. MAINTENANCE REMOVED AND REPLACED THE LEFT WATER SEPARATOR OUTLET DUCT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING GROUND INSPECTION AT XNA, CREW REPORTED EMERGENCY FLOOR TRACK LIGHTING AT ROW 5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED ROWS 4 AND 5 EMERGENCY FLEX LIGHTING STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ADC — DEFECTIVE (E/E BAY)

FLT 4710 - DURING FLIGHT FROM DFW-SAV, MACH TRIM, F/O''S AIRSPEED, VSI, AND ALTIMETER ALL INOPERATIVE. AN EMERGENCY WAS DECLARED INBOUND TO DFW. AIRCRAFT RETURNED TO AND LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED AIR DATA COMPUTER. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DUCT — DISCONNECTED (WATER SEARATOR)

FLT 4545 - DURING FLIGHT FROM ISP TO ATL, CREW EXPERIENCED A LOSS OF CABIN PRESSURIZATION IN AUTO MODE. CABIN WAS CLIMBING AT 4000 FEET PER MINUTE. CREW MADE AN EMERGENCY DESCENT TO 10,000 FEET. CREW USED THE QRH TO REGAIN PRESSURIZATION IN MANUAL MODE, BUT THAT WAS UNSTABLE. CREW DECLARED AN EMERGENCY AND RETURNED TO ISP. AIRCAFT LANDED SAFELY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND LEFT AIRCRAFT DUCT DISCONNECTED AT THE FORWARD CLAMP OF THE WATER SEPARATOR. MAINTENANCE RECONNECTED DUCT AND CLAMP IAW CRJ MM 21-51-00. OPS CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LAMP — INOPERATIVE (CABIN)

DURING INSPECTION, CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY CEILING LIGHTING SYSTEM LAMP. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

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