N971EV

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 26,257 hrs · 24,295 cycles

EMERGENCY LIGHT FOUND ENTRY DOOR WIRES HANGING LOOSE. REPAIRED BROKEN SPLICE ON ENTRY EXIT LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD AT THIS TIME.

Part: HOSE — BROKEN (HYD SYSTEM) · airframe 25,235 hrs · 23,210 cycles

HYD 3 LO PRESS MSG IN FLT QTY 5, 0 PSI FOLLOWED QRH MANUAL GEAR EXTENTION NORMAL LANDING. AFTER INSP FOUND A BROKEN PRESS HOSE NR 8. R & R PRESS HOSE IAW AMM 29-12-03 REFER TO NEXT PG FOR LEAK CK ON PUMP 3A AND HYD SERVICE FOR SYS 3.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,077 hrs · 23,053 cycles

RT FUSELAGE EXTERNAL NR 2 EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-21. OP'S CHECKED GOOD.

Part: ATTACH FITTING — CORRODED (BS 625.3) · airframe 24,305 hrs · 22,213 cycles

FS 625.30, APPROX WL 90 HAS CRACKED ATTACH FITTING TO REAR OF PRESSURE BULKHEAD. R & R DAMAGED ATTACH FITTING ON AFT SIDE OF PRESSURE BULKHEAD IAW SRM 51-42-21 AND 51-40-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 24,305 hrs · 22,213 cycles

SHORT SEAT TRACK AT BL 9R HAS CORROSION JUST AFT IF 9G BULKHEAD. REMOVED CORRODED SECTION OF SEAT TRACK IAW SRM 53-61-49-00-01. LOCATED, DRILLED & COUNTERSUNK HOLES AS REQUIRED IAW SRM 51-41-02. INSTALLED NEW SEAT TRACK IAW SRM 53-61-49-00-01.

Part: BULKHEAD — CRACKED · airframe 24,305 hrs · 22,213 cycles

REAR PRESSURE BULKHEAD FORWARD FACE IS CRACKED ABOVE AFT CARGO DOOR TRACK, AREA IS MARKED. CUT OUT DAMAGE AND STARTED FABRICATING DOUBLERS IAW REO 601R-53-61-1541. COMPLIED WITH REO 601R-53-61-1541. FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 24,305 hrs · 22,213 cycles

SHORT SEAT TRACK AT LBL 9 HAS CORROSION JUST AFT OF 9G BULKHEAD. REMOVED CORRODED SECTION OF SEAT TRACK IAW SRM 53-61-49-00-01. LOCATED, DRILLED & COUNTERSUNK HOLES AS REQUIRED IAW SRM 51-41-02. INSTALLED NEW SEAT TRACK IAW SRM 53-61-49-00-01.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 24,305 hrs · 22,213 cycles

SHORT SEAT TRACK AT LBL 27 HAS CORROSION JUST AFT OF 9G BULKHEAD. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED OLD TRACK, LOCATED, DRILLED & COUNTERSUNK HOLES AS REQUIRED FOR NEW TRACK AND INSTALLED NEW TRACK SEGMENT IAW SRM 51-42-02 AND 53-61-49.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 24,305 hrs · 22,213 cycles

SHORT SEAT TRACK AT RBL 27 HAS CORROSION JUST AFT OF 9G BULKHEAD. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. LOCATED, DRILLED & COUNTERSUNK HOLES AS REQUIRED FOR NEW TRACK AND INSTALLED NEW TRACK SEGMENT & REMOVED OLD TRACK IAW SRM 53-61-49 AND 51-41-02.

Part: SILL — CRACKED (BS 605) · airframe 24,305 hrs · 22,213 cycles

AFT CARGO DOOR SILL IS CRACKED AT FS 605. COMPLIED WITH ECTC REO 601R-53-61-433 AND REO 601R-53-61-433, REV B.

Part: SEAT TRACK — CORRODED (BS 589) · airframe 24,305 hrs · 22,213 cycles

SEAT TRACK AT RBL 9, BS 589 HAS CORROSION. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. R & R WITH NEW SEAT TRACK IAW SRM 53-61-49.

Part: CARGO TRACK — CORRODED (BS 621) · airframe 24,305 hrs · 22,213 cycles

CARGO TRACK AT LBL 9 JUST FWD OF FS 621 HAS CORROSION. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. INSTALLED NEW CARGO TRACK IAW SRM 51-41-02 AND 53-61-49.

Part: ATTACH BRACKET — CRACKED (BS 574) · airframe 24,305 hrs · 22,213 cycles

CARGO COMPARTMENT DOOR FWD TRACK, LOWER SUPPORT FRAME, ATTACH BRACKET IS CRACKED AT FS 574. REMOVED CRACKED ATTACH BRACKET IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED NEW BRACKET IAW SRM 51-42-06 & 51-40-11.

Part: SEAT TRACK — CORRODED (BS 544-559) · airframe 24,305 hrs · 22,213 cycles

RT SIDE SEAT TRACK CORRODED AT FS 544 - 559+96. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. DRILLED NEW SEAT TRACK AND COUNTER SUNK IAW SRM 51-40-11-00. INSTALLED NEW SEAT TRACK IAW SRM 51-40-11-00, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 589) · airframe 24,305 hrs · 22,213 cycles

SEAT TRACK AT LBL 9, BS 589 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. R & R WITH NEW SEAT TRACK IAW SRM 53-61-49.

Part: BRACKET — CRACKED (BS 621) · airframe 24,305 hrs · 22,213 cycles

CARGO COMPARTMENT LINTEL AFT FITTING LOWER AFT BRACKET CRACKED AT BS 621. REMOVED CRACKED LINTEL AFT FITTING LWR AFT BRACKET & INSTALLED NEW BRACKET IAW SRM 52-42-21.

Part: SKIN — CRACKED (LT WING) · airframe 24,305 hrs · 22,213 cycles

LT WING LOWER WING PLANK CRACKED AT WS 149.58. COMPLIED WITH REO 601R-57-21-130. CRACK INDICATION ON SHIM. R & R SHIM AT WS 148.019 AT LOWER T/E PANEL, SRM 51-42-06. FOUND TO BE SATISFACTORY. MAJOR REPAIR

Part: STRUT — WEAK (PAX DOOR) · airframe 24,305 hrs · 22,213 cycles

PAX DOOR FAILED FUNCTIONAL CK, DOOR WILL NOT FALL FAST ENOUGH. PAX DOOR COUNTER BALANCE ON AFT SIDE APPEARS TO BE LEAKING AND FEELS WEAK R & R PAX DOOR COUNTERBALANCE GAS-SPRING IAW AMM 52-11-17-400-802 AFT. FOUND TO BE SATISFACTORY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 24,160 hrs · 22,063 cycles

RT SIDE EXTERIOR EMERGENCY LIGHT LENS POPPED OUT. RESECURED RT 3 EMERGENCY LIGHT LENS ASSY. IAW AMM 33-51-21, OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: SIGN — UNSECURE (CABIN) · airframe 24,037 hrs · 21,930 cycles

EXIT LIGHT NEAR SERVICE DOOR UNSECURE. R & R EXIT LIGHTED SIGN BESIDES SERVICE DOOR ON GALLEY WALL. OPS CHECKED GOOD IAW AMM 33-51-13.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 23,688 hrs · 21,543 cycles

DURING FLIGHT, LOST ALL HYD SYS 2 PRESSURE AND QTY WENT DOWN TO 5 PERCENT. DIVERTED, AFTER RUNNING QRH. EMERGENCY DECLARED. FOUND O-RING LEAKING FROM NR 2 HYD RESERVOIR. R & R NR 2 HYD RESERVOIR O-RING IAW AMM 29-11-30. R & R EDP IAW AMM 29-11-01. OPS AND LEAK CHECKED GOOD AND R & R NR 2 HYD MANIFOLD FILTERS IAW AMM 29-11-01. BLED SYSTEMS.

Part: ENGINE — OIL CONSUMPTION (RIGHT) · airframe 23,628 hrs · 21,472 cycles

LOW OIL PRESSURE WARNING ENROUTE, DIVERTED. EMERGENCY DECLARED. SERVICED RT ENGINE OIL SYS IAW AMM 12-13-79. ADDED 5.5 QTS. PERFORMED OIL CONSUMPTION CHECK ON RT ENG IAW AMM 71-00-00-710-810. RAN ENGINE 18 MINS- 0 QTS CONSUMPTION. CHECKED GOOD. ACFT OK FOR SERVICE.

Part: OIL SYSTEM — WARNING MESSAGE (RIGHT ENGINE) · airframe 23,628 hrs · 21,472 cycles

AFTER TAKE OFF RECEIVED RT ENGINE OIL PRESSURE MASTER WARNING MESSAGE. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. EMERGENCY DECLARED. ACFT OK FOR SERVICE.

Part: TRIM SYSTEM — MALFUNCTIONED · airframe 22,758 hrs · 20,506 cycles

STAB TRIM & MACH TRIM WOULD NOT ENGAGE. EMERGENCY DECLARED. COMPLIED WITH FIM 27-00. RESET CIRCUIT BREAKER CBP2-F5 AND CBP4-A1. OPS CHECKED GOOD IAW 27-40-00. OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,497 hrs · 20,212 cycles

F/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-02. CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,622 hrs · 18,092 cycles

AFT EMERGENCY CEILING LIGHT IS INOP. REMOVED AND REPLACED AFT EMERGENCY CEILING LIGHT BULB IAW CRJ 200 AMM 33-51-16. OP'S CHECKED GOOD, ITEM: 1. REMOVED AND REPLACED AFT EMERGENCY CEILING LIGHT BULB IAW CRJ 200 AMM 33-51-16. OP'S CHECKED GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,490 hrs · 17,940 cycles

NR 1 AND 2 LT SEAT TRACKS ARE CORRODED. REMOVED CORRODED SEAT TRACKS AND INSTALLED DUPLICATED TRACKS IAW AMM 53-01-11, SRM 51-25-06, 51-25-16, 51-21-11, 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,490 hrs · 17,940 cycles

NR 1 AND 2 RT SEAT TRACKS ARE CORRODED. REMOVED SEAT TRACK, LOCATED DRILLED AND COUNTERSUNK NEW SEAT TRACK, TORQUED SCREWS IAW AMM 53-01-11.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 20,490 hrs · 17,940 cycles

FS 280 LT INBD CLIP AT LBL9 IS CRACKED. REMOVED CRACKED CLIP, DUPLICATED SERVICEABLE CLIP, TREATED, PRIMED AND INSTALLED SERVICEABLE CLIP IAW SRM 53-21-43; 51-24-21; 51-42-21; 51-25-06; 51-25-10; 51-21-11.

Part: FLOOR SUPPORT — CORRODED · airframe 20,490 hrs · 17,940 cycles

FLOOR SUPPORT CORRODED AT AFT OTBD END OF FLOORBOARD 232CRF. REMOVED CORROSION AT FLOOR SUPPORT AT AFT OTBD END OF FLOORBOARD IAW SRM 51-21-06, 17550 10-17-10.

Part: ATTACH FITTING — CORRODED (BS 320) · airframe 20,490 hrs · 17,940 cycles

PAX DOOR LOWER AFT FRAME CLIP AT FS 320 CORRODED. FABRICATED AND INSTALLED SERVICEABLE FRAME CLIP AT FS 320 IAW SRM 51-24-21, 51-42-06 AND 51-42-21.

Part: ATTACH FITTING — CORRODED (BS 320) · airframe 20,490 hrs · 17,940 cycles

PAX DOOR LOWER FWD FRAME CLIP AT FS 320 CORRODED. FABRICATED AND INSTALLED SERVICEABLE FRAME CLIP AT FS 320 IAW SRM 51-24-21, 51-42-06 AND 51-42-21.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 20,490 hrs · 17,940 cycles

FS 280 RT INBD CLIP AT RBL 9 IS CRACKED. REMOVED CRACKED CLIP, DUPLICATED SERVICEABLE CLIP, TREATED, PRIMED AND INSTALLED SERVICEABLE CLIP IAW SRM 51-25-06; 53-21-43; 51-24-21; 51-42-21; 51-25-16; 51-21-11, 16948 10-17-10.

Part: ATTACH FITTING — CORRODED (BS 339) · airframe 20,490 hrs · 17,940 cycles

PAX DOOR LOWER AFT FRAME CLIP AT FS 339 CORRODED. FABRICATED AND INSTALLED SERVICEABLE FRAME CLIP AT FS 339 IAW SRM 51-24-21, 51-42-06 AND 51-42-21.

Part: ATTACH FITTING — CORRODED (BS 339) · airframe 20,490 hrs · 17,940 cycles

PAX DOOR LOWER FWD FRAME CLIP AT FS339 CORRODED. FABRICATED AND INSTALLED SERVICEABLE FRAME CLIP AT FS339 IAW SRM 51-24-21, 51-42-06 AND 51-42-21.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 20,490 hrs · 17,940 cycles

RIGHT 484 INTERCOSTAL CLIP IS CRACKED. (OPEN)

Part: FITTING — CRACKED · airframe 20,490 hrs · 17,940 cycles

RIGHT BATHTUB FITTING AT RBL19 IS CRACKED. (OPEN)

Part: PLACARD — TORN (CABIN) · airframe 20,490 hrs · 17,940 cycles

PAX DOOR OPEN/EXIT, AND ASSIST PLACARDS ARE TORN. (OPEN)

Part: BULKHEAD — CRACKED (BS 202) · airframe 20,001 hrs · 17,392 cycles

BS 202 BULKHEAD IS SUSPECT FOR CRACK AT LT PARKING BRAKE CABLE. WORK COMPLETED IAW INSPECT FS 202 BULKHEAD CRACK IAW NDTM 51-20-06. FABRICATED SHIMS ALSO FABRICATED DOUBLER IAW EC/TC REO 601R-53-11-563. REMOVED DAMAGE AS SHOWN IN REO 601R-53-11-653. COMPLIED WITH EDDY CURRENT INSP IAW NDTM 51-20-06, PART 1 NO DEFECTS NOTED AT THIS TIME. PICKED UP EXSITING FASTNERS AND NEW FASTNERS IN -1 DOUBLER, FINAL SIZE ALL HOLES IN -1 DOUBLER, PRIMED -1 DOUBLER ALL WORK IAW EC/TC REO601R-53-11-563, REFER TO EC/TC REO 601R-53-11-1940 05, W/O 166020 FOR WORK ACCOMPLISH FOR STEPS 6 THROUGH 12. RECEIVED FINAL REO 601R-53-11-1940 06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,597 hrs · 16,905 cycles

AFT CEILING EMERGENCY LIGHT OUT. (RESOLVED ON W/O: 155136 TASKCARD: N/R-00049) R & R AFT CEILING EMERGENCY LIGHT IAW AMM 33-51-16-400-801. OPS TEST OF EMERGENCY LIGHTS GOOD IAW AMM 33-51-00-710-801. (CLOSED)

Part: PLACARD — MISSING (PAX DOOR) · airframe 19,584 hrs · 16,892 cycles

EXIT PLACARD MISSING ON PAX AIRSTAIR DOOR. INSTALLED PLACARD IAW AMM 11-30-02.

Part: SWITCH — BROKEN (FLASHLIGHT) · airframe 19,099 hrs · 16,327 cycles

F/A FLASHLIGHT SWITCH IS BROKEN.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 18,630 hrs · 15,785 cycles

FLAPS FAILED AT 20 [EMERGENCY DECLARED].

Part: DOOR — STUCK (PAX DOOR) · airframe 17,965 hrs · 15,137 cycles

PAX DOOR WILL NOT OPEN OR CLOSE. FLT 5606 DEL 20 MINS. PASSENGER DOOR POWER ASSIST SYSTEM.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 17,197 hrs · 14,425 cycles

STEERING INOP IN FLIGHT, RESET PER QRH AND REOCCURRED MULTIPLE TIMES, REPEAT WRITE UP EMERGENCY DECLARED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 16,593 hrs · 13,869 cycles

FLOORBEAM AT LBL 9 FS 589 TO FS 621 HAS CORROSION ON OUTBOARD FLANGE FLOORBOARD ATTACH HOLES. REMOVED FLOORBEAM CAP AT LBL 9, FS 589 TO FS 621 IAW SRM 51-42-06 AND 51-42-21. DRILLED NEW SERVICEABLE FLOORBEAM CAP IAW SRM 51-40-11. OK TO INSTALL. INSTALLED NEW SERVICABLE BEAM CAP IAW SRM 51-42-06 AND 51-42-21 AND 51-42-28. REINSTALLED SERVICEABLE LOWER WEB. INSTALLED ALTERNATE FASTENERS IN FLOORBEAM CAP IAW REO 601R-53-61-2849. EC/TC REO 601R-53-61-2849 INCORPORATED.

Part: WEB — CRACKED (PAX DOOR) · airframe 16,593 hrs · 13,869 cycles

PAX DOOR AFT WEB IS CRACKED IN 2 PLACES IN ZONE 4 APPROX .125 X .500. COMPLIED W/STEPS 1, 4, 5, 6 & 7 OF BOMBARDIER REO 601R-52-11-702. NDT REQ'ED. PERFORMED EDDY CURRENT INSPECTION ON PAX DOOR AFT WEB IN ZONE 4 CUTOUTS. NO REJECTABLE INDICATIONS FOUND AT THIS TIME. REPORT ATTACHED IAW STEP 2 OF BOMBARDIER REO 601R-52-11-702A AND CRJ NDTM 51-20-06. RESTORE FINISH IS REQUIRED. COMPLIED W/STEPS 3, 8 & 10 OF BOMBARDIER REO 601R-52-11-702. PAINT REQ'ED. EDGE SEALED REPAIR AND PAINTED IAW REO 601R-52-11-702 STEPS 11 AND 12. COMPLIED W/STEPS 13 THROUGH 17 OF BOMBARDIER REO 601R-52-11-702. SUPPLEMENTAL-SDR CLOSED 11/13/2008.

Part: SKIN — CRACKED (PAX DOOR) · airframe 16,592 hrs · 13,869 cycles

PAX DOOR FORWARD SIDE SKIN IS CRACKED AT HANDRAIL STOP/SUPPORT BRACKET.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 16,592 hrs · 13,869 cycles

JOB 8752811 OP 357 PAX DOOR OUTER HANDLE IS CRACKED. RESOLVED ON W/O 101539 TASKCARD NR 00442. PAX DOOR OUTER HANDLE BEING REPLACED UNDER 8752815/5771. REF 8752815/5771 FOR MX ACTION.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,593 hrs · 13,869 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS A INDICATION NOTED APPROX .1 INCH IN LENGTH 100 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: FRAME — CRACKED (BS 559) · airframe 16,592 hrs · 13,869 cycles

LT FS 559 CAP ANGLE LBL 18 HAS AN INDICATION NOTED APPROX .5" IN LENGTH 90% FULL SCREEN HEIGHT FAILED NDT INSP.

Part: PLACARD — DEFECTIVE (EMERGENCY EXIT)

BETA LIGHT PLACARDS ON LT/ RT EMER EXIT DOOR INTERIOR HANDLE COVERS FAILED INTENSITY TEST. (K)

Part: SKIN — CORRODED (RT NACELLE) · airframe 16,593 hrs · 13,869 cycles

RT ENG LIPSKIN HAS CORROSION ON L/E IN SEVERAL AREAS. COMPLIED WITH CMM 71-61-01-200-802-A01. PERFORMED ULTRASONIC INSPECTION OF RT NOSE INLET LIPSKIN IAW WVAC. FOUND RT NOSE INLET LIPSKIN TO BE WITHIN LIMITS. REQUIRES BLEND IN PITTING AREAS. BLENDED RT ENG LIPSKIN IAW CMM 71-61-01-200-802-A01. POLISHED LIPSKIN IAW MM 51-27-00-140-801. COMPLIED WITH CMM 71-61-01-200-802-A01. PERFORMED ULTRASONIC THICKNESS MEASUREMENT OF RT ENGINE NOSE INLET LIPSKIN REPAIRED AREAS C, D, & E. ALL ZONES FOUND TO BE WITHIN LIMITS.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 16,592 hrs · 13,869 cycles

JOB 8752811 OPERATION 184 RT UPPER OBLIQUE ANGLE INTERCOSTAL IN AFT EQUIPMENT BAY FROM FS 621 TO FS 625 IS CRACKED IN RADIUS.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

LT UPPER OBLIQUE ANGLE (INTERCOSTAL) IN AFT EQUIPMENT BAY, FS 621 TO FS 625 IS CRACKED IN RADIUS. (K)

Part: DOOR — LACK OF LUBE (SERVICE DOOR) · airframe 16,441 hrs · 13,750 cycles

PAX SERVICE DOOR IS VERY HARD TO OPEN FROM OUTSIDE. LUBE SERVICE DOOR OK FOR SERVICE.

Part: FRAME — CRACKED (BS 280) · airframe 16,036 hrs · 13,405 cycles

SUSPECTED CRACK IN AFT LOWER LEG OF FS 280 FRAME AT RBL 12. WORK COMPLETED IN ACCORDANCE WITH: PERFORMED EDDY CURRENT INSPECTION OF SUSPECT AREA IAW CRJ 200 NDTM 61-20-06 PART 1 AND CONFIRMED CRACK MB7011995 06-21-08. PERFORMED EDDY CURRENT INSPECTION OF CUT LINE IAW CRJ 200 NDTM 61-20-06 PART 1 AND NO CRACK NOTED MB7011995 06-21-08. (B)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 16,036 hrs · 13,405 cycles

RBL 9 CLIPS CRACKED INBD AND OUTBD AT FS 280. REMOVED AND REPLACED CLIPS IAW SRM 51-42-21 AND AMM 51-23-00. (B)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 16,036 hrs · 13,405 cycles

LBL 9 CLIPS CRACKED INBD AND OUTBD AT FS 280. REMOVED AND REPLACED CLIPS IAW CRJ 200 SRM 51-42-21 AND AMM 51-23-00. (B)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,630 hrs · 13,041 cycles

LEFT OVERWING EMERGENCY LIGHT IS OUT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,446 hrs · 12,882 cycles

FWD FLOOR EMERGENCY LIGHTS AND LEFT EMERGENCY DOOR EXIT LIGHT INOP.

Part: PLACARD — WORN (CABIN) · airframe 14,766 hrs · 12,318 cycles

THE "EXIT" PLACARD ON ASD WORN.

Part: FLAP SYSTEM — UNKNOWN (TE FLAPS) · airframe 14,766 hrs · 12,318 cycles

FLAP FAIL AT 0. EMERGENCY EQUIPMENT ON STANDBY. FLT 4693 CX.

Part: FLAP SYSTEM — STUCK (TE FLAPS) · airframe 14,749 hrs · 12,302 cycles

FLAP FAIL MSG DURING CRUISE FLT AT 320 SAT 47. FLAPS STUCK AT 0 DEGREES. RAN QRH AND LANDED NO FLAP. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 14,700 hrs · 12,259 cycles

OVERWING EMERGENCY LIGHT ON RIGHT SIDE INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,626 hrs · 12,201 cycles

EMERGENCY EXIT LIGHT RIGHT SIDE AFT OF EMERGENCY EXIT HATCH INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 14,233 hrs · 11,897 cycles

CAPTAIN'S FLASHLIGHT IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,281 hrs · 11,146 cycles

EMERGENCY LIGHT OUT ON THE FLOOR AT SEAT 1 CD.

Part: FRAME — CRACKED (BS 640) · airframe 11,961 hrs · 10,146 cycles

LEFT FS 640.00 FRAME DOUBLER CRACKED.

Part: PLACARD — FADED (PAX DOOR) · airframe 11,084 hrs · 9,454 cycles

EXIT PLACARD ON PAX DOOR FADED.

Part: BULB — INOPERATIVE (CABIN) · airframe 11,031 hrs · 9,407 cycles

RT FUSELAGE MID EMERGENCY LIGHT BULB INOP.

Part: LAMP — BURNED OUT (FUSELAGE)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR EMERGENCY FLOOD LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE PASSENGER DOOR EMERGENCY FLOOD LIGHT. OPERATIONAL CHECKS GOOD. AC FOR SERVICE. (K)

Part: RELAY — SHORTED (EMGR LIGHT SYS)

DURING A GROUND INSPECTION, THE EMERGENCY LIGHT CAME ON WHEN ARMED. THE ACCESS BUS WAS UNABLE TO RECEIVE POWER. MAINTENANCE REMOVED AND REPLACED THE SENSOR RELAY A1XD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)