N680BR

Part: FLOORBEAM — CORRODED (BS 589) · airframe 20,177 hrs · 18,663 cycles

FLOORBEAM CAP FS 589 BL 0 HAS MINOR CORROSION. REMOVED CAP IAW SRM 51-42-06. LOCATED AND DRILLED UP NEW CAP PN IAW SRM 51-40-11.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 20,177 hrs · 18,663 cycles

FS 621.00 PRESSURE BULKHEAD FWD FACE HAS THREE BROKEN ISOLATORS. REMOVED DAMAGE ISOLATORS AND INSTALLED IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 20,177 hrs · 18,663 cycles

CABIN COMPARTMENT FLOORBEAM BS 484 CRACKED AT RBL 36 AND LBL 36. REPAIRED IAW REO 601R-53-41-059 AND NDTM PT1 51-20-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,177 hrs · 18,663 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED APPROX 1.5 INCHES LONG. R & R THE PAX DOOR AFT DRAG ANGLE IAW SRM 51-42-06 & SRM 51-42-13.

Part: BULKHEAD — CRACKED · airframe 19,529 hrs · 17,958 cycles

AFT PRESSURE BULKHEAD CRACKED AT RBL 27.50. CUT AWAY DAMAGE IAW REO 601R-53-61-1285. COMPLIED WITH NDT EDDY CURRENT INSPECTION OF CUT LINE IAW NDTM 51-20-06, PART 1 AND REO 601R-53-61-1285, REV D. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND FILLERS. INSTALLED ALL PARTS IAW SRM 51-42-06, 51-42-21, 51-23-00, 51-42-21.

Part: BULKHEAD — CRACKED · airframe 19,529 hrs · 17,958 cycles

AFT PRESSURE BULKHEAD CRACKED AT RBL 36.20. CUT AWAY DAMAGE IAW REO 601R-53-61-1285. COMPLIED WITH NDT EDDY CURRENT INSPECTION OF CUT LINE IAW NDTM 51-20-06, PART 1 AND IAW REO 601R-53-61-1285, REV D. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED ALL PARTS IAW REO 601R-53-61-1285, REV D, REO 601R-53-61-4515, SRM 51-42-06,51-42-21,51-23-00 AND SRM 51-42-21.

Part: SWITCH — UNSERVICEABLE (FIRE BOTTLE) · airframe 19,487 hrs · 17,909 cycles

LEFT ENGINE BOTTLE NOT ARMING DURING FIRST FLIGHT OF DAY FIRE WARNING TEST PUSH TO DISCHARGE LIGHT DOESN'T LIGHT UP. CLEANED PBA FOR PUSH LIGHT LT AND RT PUSH TO DISCHARGE SWITCH, INSTALLED A NEW SWITCH ASSY IAW ESPM 20-24-00. OPS CHECK GOOD. (SDR CLOSED)

Part: RELAY — FAILED · airframe 19,469 hrs · 17,889 cycles

OVERBOARD COOL CAUTION MESSAGE. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. OVERBOARD EXHAUST SHUTOFF VALVE (AVIONICS COOLING) INOPERATIVE OPEN. R & R WOW RELAY (K8HK) AND DOOR LOCKED RELAY (K9HK) IAW ESPM 20-22-00. SYS CHECKED GOOD IAW AMM 21-24-34.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 18,033 hrs · 16,281 cycles

FLAPS FAILED ON APPROACH AT 11. EMERGENCY DECLARED AS A PRECAUTION. COMPLIED WITH EC/TC AD 2009-06-12 , ACFT OK FOR SERVICE MCOL 767097 CLEARED .

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 18,033 hrs · 16,281 cycles

FLAPS FAILED AT 0 DURING APPROACH. EMERGENCY DECLARED AS A PRECAUTION. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOOD. ACFT OK FOR CONTINUED SERVICE. (CLOSED)

Part: COMPUTER — FAILED (FUEL SYSTEM) · airframe 16,292 hrs · 14,346 cycles

ABNORMAL INCREASE OF FUEL IN CTR TANK. FUEL IMBALANCE MESSAGE. (ENROUTE, ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED) R & R FUEL COMPUTER AND REFUEL/DEFUEL PANEL IAW AMM 28-41-16, OPS CHECK GOOD AND 28-25-16 OPS CHECK GOOD. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 16,238 hrs · 14,279 cycles

RT FUSELAGE AFT MOST EXTERIOR EMERGENCY LIGHT IS INOP. R & R BULB IAW SRM 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CORRODED (BS 574-605) · airframe 15,701 hrs · 13,680 cycles

CARGO FLOORBEAM CAP FROM FS 574.00 - 605.00 LBL 27.00 IS CORRODED AROUND NUTPLATE HOLES. REMOVED CARGO FLOORBEAM CAP FROM STA 574-605 LBL 27.00 IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED, COUNTERSUNK AND DEBURRED NEW CARGO FLOORBEAM CAP IAW SRM 51-40-11. CARGO BY FLOORBEAM CAP FS 574.00 - 605.00 AT LBL 27.00 REQUIRES INSTALLATION. C/W EC/TC REO 601R-53-61-3556 AND REO 601R-53-61-3556.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 15,701 hrs · 13,680 cycles

CARGO FLOORBEAM FITTING AT FS 605.00 - 621.00 LBL 27.00 IS CORRODED AROUND NUTPLATES. REMOVED CARGO FLOORBEAM FITTING IAW SRM 51-42-06, 51-42-21 AND 51-41-02. NEW FITTIGN NEEDS INSTALLED. LOCATED, DRILLED, DEBURRED NEW FITTING IAW SRM 51-40-11. C/W EC/TC REO 601R-53-61-3556 & REO 610R-53-61-3556 REV- DATED 2/27/10.

Part: ANGLE — CRACKED (FS 589) · airframe 15,701 hrs · 13,680 cycles

UPON INSTALLATION OF CARGO DOOR SILL PLATE, FOUND ANGLE AT FS 589.00 TO BE CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,701 hrs · 13,680 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .2" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. REPAIR IAW EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE & THE REPAIR C/W THE REQUIREMENTS OF EC/TC & REO 601R-53-61-1230.

Part: POST — CRACKED (BS 409) · airframe 15,701 hrs · 13,680 cycles

FS 409+128 RBL 18.0 VENT POST FAILS NDT WITN AN INDICATION IN AFT LT "C" CHANNEL. (GREATER THAN 50 PERCENT SCREEN HEIGHT). REMOVED VERT POST IAW SRM 51-42-06. LOCATED & DRILLED IAW SRM 51-40-11 & ASSEMBLED 2 HALVES IAW SRM 51-42-06. INSTALLED VERTICAL POST IAW REO 601R-53-41-889. C/W EC/TC REO 601R-53-41-889 AND MET ALL REQUIREMENTS OF REO 601R-53-41-889. 5. APPLIED WATER DISPLACING CORROSION-INHIBITING COMPOUND BY BRUSH METHOD IAW SRM 51-21-11 STEP 7A-D.

Part: SEAT TRACK — CORRODED (BS 559-621) · airframe 15,701 hrs · 13,680 cycles

CARGO SEAT TRACK SEGMENTS FROM FS 559+80 TO FS 621 ARE CORRODED, QTY 2 SEGMENTS, RBL 9. REMOVED & REPLACED SEAT TRACK SEGMENTS IAW AMM 53-01-11-000-802 AND SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 559-621) · airframe 15,701 hrs · 13,680 cycles

SEAT TRACK SEGMENTS FROM FS 559+80 TO FS 621 AT LBL 9 (QTY 3) ARE CORRODED. REMOVED AND REPLACED SEAT TRACK SEGMENTS IAW AMM 53-01-11-000-802 AND SRM 51-40-11.

Part: ISOLATOR — BROKEN (BS 621) · airframe 15,701 hrs · 13,680 cycles

FS 621 ISOLATOR AT RBL9 IS BROKEN. REMOVED AND INSTALLED NEW ISOLATOR ON FS 621 RBL 9 IAW SRM 51-42-13.

Part: SILL — CORRODED (BS 574-621) · airframe 15,701 hrs · 13,680 cycles

FLOOR SUPPORT SILL ON RT SIDE APPROX RBL 49 FROM FS 574 TO 621 HAS CORROSION AROUND NUTPLATE LOCATION. REMOVED NUTPLATES (10) FROM FLOOR SUPPORT IAW CRJ SRM 51-42-10 FIGURE 4. BLENDED AREA REMOVING CORROSION IAW CRJ SRM 51-21-06 STEP 6A. PRIMED AND PAINTED IAW CRJ SRM 51-21-06 STEP 6 A(1)(D).

Part: ISOLATOR — CRACKED (PRESS BLKHEAD) · airframe 15,701 hrs · 13,680 cycles

FOUND REAR PRESSURE BULKHEAD ISOLATOR IS CRACKED LBL9.0, APPROX WL 90. REMOVED AND REPLACED CRACKED ISOLATOR IAW SRM 51-42-10 FIG 4 AND 51-42-13 STEP 8.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 15,701 hrs · 13,680 cycles

RT FS621 FLOOR SUPPORT ANGLE PREVIOUS REPAIR IS CRACKED. REPAIR OF THE DAMAGED PORTIONS OF ANGLE 601R35031-239 IS COMPLETED IAW REO 601R-53-61-117 & MEETS WITH ALL ITS REQUIREMENTS.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 15,701 hrs · 13,680 cycles

LT FS621 FLOOR SUPPORT ANGLE PREVIOUS REPAIR IS CRACKED. REPAIR OF THE DAMAGED PORTIONS OF ANGLE 601R35031-239 IS COMPLETED IAW REO 601R-53-61-117 & MEETS ALL ITS REQUIREMENTS.

Part: POST — CRACKED (BS 409) · airframe 15,701 hrs · 13,680 cycles

FS 409+128 BL 0.00 VERT POST FAILS NDT WITH AN INDICATION IN AFT RT "C" CHANNEL. (GREATER THAN 50 PERCENT SCREEN HEIGHT). REMOVED POST IAW SRM 51-42-06. POST LOCATED & DRILLED INBD & OTBD POST HOLES IAW SRM 51-40-11. INSTALLED INBD & OTBD POST HOLES TOGETHER, IAW SRM 51-42-06. INSTALLED POST BL0, IAW REO 601R-53-41-889. INSTALLED NEW SERVICEABLE INBD & OTBD POST ANGLES AT BL0, IAW SRM 51-42-06/REO 601R-53-41-889. C/W EC/TC REO 601R-53-41-889 & MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: CARGO TRACK — CORRODED (CABIN) · airframe 15,701 hrs · 13,680 cycles

CARGO SEAT TRACK SEGMENT AT RBL 27 FOR LAV ATTACHMENT IS CORRODED. REMOVED & REPLACED SEAT TRACK SEGMENT FOR LAV ATTACHMENT IAW AMM 53-01-11-000-802 AND SRM 51-40-11.

Part: ANGLE — CORRODED (BS 280) · airframe 15,701 hrs · 13,680 cycles

FWD "J" ANGLE AT FS 280 BETWEEN LBL 9 AND RBL 9 IS CORRODED. REMOVED FWD "J" ANGLE IAW SRM 51-42-06. LOCATED AND INSTALLED FWD "J" ANGLE IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (BS 559) · airframe 15,701 hrs · 13,680 cycles

FOUND FS 559 BULKHEAD WEB RT SIDE HAS INDICATIONS NOTED OTBD OF RBL 9.0 WL 58.70 APPROX .2" IN LENGTH 55 FS AND INBD OF RBL 18.0 WL54.0 APPROX .3" IN LENGTH 60 PERCENT FSH FAILED NDT INSPECTION. REPAIRED FS 559 BULKHEAD AND CAP ANGLES FROM LBL 27 TO RBL 27 IAW REO 601R-53-41-260 REV.D. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV.D

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 15,701 hrs · 13,680 cycles

FS 484 INTERCOSTAL RBL27 AND RBL36 CLIPS ARE CRACKED. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,701 hrs · 13,680 cycles

FLOORBEAM AT FS 280 & LBL9 HAS A 2" CRACK.

Part: PLACARD — WORN (EMERGENCY EXIT) · airframe 15,701 hrs · 13,680 cycles

FLT DECK EMERGENCY EXIT (831) EXTERIOR MARKINGS ARE WORN.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 15,701 hrs · 13,680 cycles

FS 484 INTERCOSTAL, LBL 27 CLIP IS CRACKED. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: PLATE — CORRODED (BS 310) · airframe 15,701 hrs · 13,680 cycles

CORROSION ON FS 310 AT SERVICE DOOR ON SPLICE PLATE. REMOVED SILL PLATE JUST FWD OF SERVICE DOOR CUTOUT IAW SRM 51-42-06, TO ACCESS SPLICE PLATE. LOCATED & DRILLED NEW SPLICE PLATE IAW SRM 51-40-11 & INSTALLED IAW SRM 51-42-21. SILL PLATE REQUIRES INSTALLED. INSTALLED SILL PLATE FWD OF SERVICE DOOR AT WL 73 IAW SRM 51-42-06 & 51-42-21 FS 295.0 - 310.0.

Part: PLACARD — DETERIORATED (ESCAPE HATCH) · airframe 15,701 hrs · 13,680 cycles

CREW ESCAPE HATCH (831) EMERGENCY PLACARD IS DETERIORATED. APPLIED NEW SILKSCREENS ON HATCH (831) IAW MM 11-10-03-400-801.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,701 hrs · 13,680 cycles

JOB 8767911, OPS 183, PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO'S 601R-52-11-513 AND 601R-52-11-751 & ASA ECTC REO 601R-52-11-513.

Part: ANGLE — CRACKED (BS 621-625) · airframe 15,701 hrs · 13,680 cycles

RT 621 TO 625 OBLIQUE ANGLE IS CRACKED. REMOVED FS 625 OBLIQUE ANGLE AND REPLACED W/A SERVICEABLE ONE ON RBL 27 IAW SRM 51-42-06 ST 1, 9 AND 11.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 15,701 hrs · 13,680 cycles

JOB 8767911 OPERATION 46 / LT WINDSCREEN EXIT SIGN ASSY IS BROKEN. REMOVED LT WINDSCREEN EXIT SIGN ASSY IAW AMM 33-51-13-000-801. INSTALLED NEW SERVICEABLE SIGN IAW 33-51-13-400-801. OPS TEST REQUIRED. COMPLIED WITH OPS CHECK ON THE LT WINDSCREEN IAW AMM 33-51-00-710-801. OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (TE FLAP) · airframe 13,661 hrs · 11,604 cycles

THE "FLAPS FAIL" MSG IN CRUISE FLIGHT DESCENDING THROUGH 19,000FT AT 290 KIAS WITH LIGHT TO MODERATE TURBULENCE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 13,644 hrs · 11,587 cycles

EN ROUTE TO ATL RECEIVED "FLAPS FAIL" CAUTION MESSAGE WITH FLAPS INDICATING 0 ON FLT/CTL SYNOPTIC PAGE. EMERGENCY DECLARED.

Part: FLAP — FAILED (WING) · airframe 13,269 hrs · 11,247 cycles

FLAP FAIL AT 0 DEGREES AT 200 KIAS. EMERGENCY DECLARED.

Part: FLAP SYSTEM — FAILED (WING) · airframe 13,259 hrs · 11,238 cycles

FLAP FAIL AT 0 DEGREES WHEN LANDING IN GRR, RAN QRH, DECLARED AN EMERGENCY AND A 0 FLAP LANDING UNEVENTFUL. EMERGENCY DECLARED. FLT 5599. FOUND MOISTURE IN TORQUE TUBE. DRIED, LUBED, OP CHECKED IAW AMM 27-54-01.

Part: FLAP — FAILED (WING) · airframe 13,245 hrs · 11,230 cycles

FLAPS FAIL MSG ON EICAS AT 200 KAS FLAPS INDICATING 0. EN ROUTE TO CID A/C DIVERTED TO MLI DUE TO MTC, EMERGENCY DECLARED.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 13,170 hrs · 11,157 cycles

FLT 5575 - FLAPS FAIL MESSAGE ON DESCENT, WHEN SELECTING 8 DEGREES. FAILED AT ZERO. EMERGENCY VEHICLES ROLLED AS A PRECAUTION.

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 1,203,107 hrs · 10,180 cycles

FLAPS FAIL AT ZERO WHEN SELECTING 8 DEGREES. FLT 4349 CX EMERGENCY DECLARED. REMOVED AND REPLACED BPSU LT SIDE IAW CRJ200 AMM 27-50-01. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME. [SDR CLOSED](B)

Part: TRANSDUCER — MALFUNCTIONED (OIL PRESSURE) · airframe 1,197,100 hrs · 10,139 cycles

OIL PRESSURE INDICATING 156 PSI IN ALL PHASES FROM CLIMB TO SHUTDOWN AT GATE. AIRCRAFT RETURNED TO ATL AFTER T/O---EMERGENCY DECLARED. FLT 4531 DEL 156 MINS REMOVED AND REPLACED RT ENG OIL PRESSURE TRANSDUCER IAW AMM 79-31-03, LEAK AND OPS CHECK GOOD. (B)

Part: PLACARD — WORN (PAX DOOR) · airframe 11,491 hrs · 9,724 cycles

AAR - PAX DOOR STEP "EXIT" PLACARD WORN.

Part: FLANGE — CRACKED (BS 280) · airframe 11,473 hrs · 9,709 cycles

FS 280.00 OUTBD OF RBL 9.00, LOWER FLANGE CRACKED. REPAIRED IAW REO 601R-53-11-171.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 11,473 hrs · 9,709 cycles

AAR - 8010 - PAX DOOR OUTER HANDLE IS CRACKED.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 11,473 hrs · 9,709 cycles

484.00 INTERCOSTAL CRACKED AT ATTACH POINT LBL 36, REPAIRED INTERCOSTAL, IAW REO'S 601R-53-41-059 AND 601R-53-41-662.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 11,473 hrs · 9,709 cycles

CABIN SUBFLOOR, 484.00 INTERCOSTAL CRACKED AT ATTACH POINT RBL 36.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 11,475 hrs · 9,713 cycles

AAR - CRACK ON PAX DOOR LOWER FWD CORNER UNDER HINGE STEP.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 11,473 hrs · 9,709 cycles

FS 280.00 LBL 9.00 OUTBD ATTACH ANGLE CRACKED. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH ASA EC/TC REO 601R-53-21-852.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 11,473 hrs · 9,709 cycles

FS 280.00 RBL 9.00 INBD ATTACH ANGLE CRACKED.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 11,473 hrs · 9,709 cycles

FS 280.00 RBL 9.00 OUTBD ATTACH ANGLE CRACKED. REMOVED CRACKED ANGLE. REPAIRED FS 280.00 RBL 9.00 O/B ATTACH ANGLES PER REO 601R-53-11-171. COMPLIED WITH EO 600-53-0090.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 11,473 hrs · 9,709 cycles

FS 280.00 RBL 9.00 INBD ATTACH ANGLE CRACKED.

Part: PLACARD — DAMAGED (CABIN) · airframe 11,473 hrs · 9,709 cycles

AAR - 2031 - EMERGENCY EXIT INSTRUCTION PLACARD ON CREW ESCAPE HATCH UN READABLE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 11,473 hrs · 9,709 cycles

FWD PRESSURE BULKHEAD CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH. COMPLIED WITH REO 601R-53-11-563 AND EO 600-53-217 C/W TO REPAIR THE FWD PRESSURE BULKHEAD.

Part: STRUCTURE — CRACKED (DOOR) · airframe 10,694 hrs · 9,076 cycles

ASD CRACKED UNDER TOP STEP AFT AREA.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 10,694 hrs · 9,076 cycles

ASD AFT DRAG ANGLE CRACKED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 10,461 hrs · 8,890 cycles

F/A'S FLASHLIGHT IS INOP.

Part: COVER — MISSING (TAILCONE) · airframe 10,127 hrs · 8,636 cycles

RIGHT ENG MISSING INSPECTION COVER ON TOP LEFT SIDE OF TAIL CONE. FLTS 4672, 4713 CX.

Part: OIL SYSTEM — LOW (LT ENGINE) · airframe 9,496 hrs · 8,160 cycles

LEFT ENGINE SHUTDOWN, LOW OIL. EMERGENCY DECLARED. FLTS 4449, 4578 CX.

Part: FLAP SYSTEM — FAILED · airframe 9,014 hrs · 7,786 cycles

FLAPS FAIL MESSAGE IN FLIGHT FAILED AT 8 COMPLIIED WITH QRH LANDED ON 27R WITH 200 FPM MAXIUM AT TOUCHDOWN WITHOUT INCIDENT. EMERGENCY EQUIPMENT ON STANDBY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 8,669 hrs · 7,531 cycles

FLAPS FAIL CAUTION MSG ON APPROACH, WHEN FLAPS SELECTED TO 8 DEGREES. EMERGENCY DECLARED. FLTS 4177, 4353 CX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,008 hrs · 7,045 cycles

RT FUSELAGE EXTERIOR EMERGENCY LIGHT 1 EA INOPERATIVE.

Part: BPSU — INOPERATIVE (TE FLAPS) · airframe 7,545 hrs · 6,651 cycles

FLYING AT 27000, GOT A FLAPS FAIL MSG PROCEEDED WITH QRH PROCEDURES AND RECEIVED FLAPS 0 LANDING (TOWER ROLLED EMERGENCY EQUIPMENT).

Part: EXTINGUISHER — INOPERATIVE (FIRE SYS) · airframe 7,519 hrs · 6,633 cycles

CARGO COMPT. FIRE EXTINGUISHER SYSTEM OPS CHECK FAILED.

Part: CONTROL UNIT — FAILED (STAB TRIM)

STAB TRIM/MACH FAIL. PERFORMED BITE CHECK OF HSTCU. CLEANED YOKE MOUNT DISC SWITCHES AND STAB/TRIM SWITCHES. PERFORMED OPS CHECK. NO DEFECTS NOTED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE AFT EMERGENCY DOOR LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 3,293 hrs · 2,678 cycles

DURING CLIMB OF FLIGHT 7250 CREW REPORTED GROUND AND FLIGHT SPOILER FAULTS. CREW RETURNED TO IAD AND FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE NR 1 SPOILER ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 2,435 hrs · 1,995 cycles

DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL PERFORMED A SATISFACTORY OPERATIONAL CHECK AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT HALF OF THE EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 4 INVERTER. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE MID TO AFT OF CABIN. REMOVED AND REPLACE P/N 2013-1A BATTERY. OPS CHECKED GOOD