N977EV

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHT) · airframe 22,078 hrs · 20,434 cycles

EMERGENCY LIGHTS ON IN ARM POSITION WITH EXTERNAL POWER GALLEY SWITCH IN OFF POSITION. PUSHED IN CIRCUIT BREAKER, OPS CHECKED GOOD IAW AMM 33-51-00. AC OK FOR SERVICE.

Part: ANGLE — CRACKED (BS 621-625) · airframe 21,355 hrs · 19,716 cycles

FS 621.00 TO 625.00 ANGLES AT RBL AND LBL 14 ARE CRACKED. REMOVED ANGLES AT FS 621.00 TO 625.00, RBL 14 AND LBL 14 IAW SRM 51-42-21. LOCATED AND DRILLED LT ANGLE, MADE FROM S6144-33 PO 14213/1 AND NEW SERVICEABLE RT ANGLE PN 601-35012-52 IAW CRJ 200 51-40-06 AND 51-40-11. INSTALLED ANGLES AT FS 621.00 AND 625.00 RBL 14 AND LBL 14 IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 484) · airframe 21,355 hrs · 19,716 cycles

FS 484.00 ANGLES CRACKED AT RBL 27 & 36. R & R ANGLE AT FS 484.00 RBL 27 IAW SRM 51-42-21. R & R ANGLE AT FS 484.00, RBL 36 IAW REO 601R-53-41-059. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.00 COMPLETED IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 484) · airframe 21,355 hrs · 19,716 cycles

FS 484.00 ANGLES ARE CRACKED AT LBL 27 & 36. R & R ANGLE AT FS 484.00 RBL 27 IAW SRM 51-42-21. R & R ANGLE AT FS 484.00, LBL 36 IAW REO 601R-53-41-059. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.00 COMPLETED IAW REO 601R-53-41-059.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 21,355 hrs · 19,716 cycles

FWD END OF CABIN SEAT TRACK ARE CORRODED. R & R CORRODED SEAT TRACK WITH NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: TRANSMITTER — FAILED (FLAPS) · airframe 21,050 hrs · 19,393 cycles

GEAR/FLAP INDICATIONS CAME UP ON ED1 IN LEVEL FLIGHT AT FL220 AND 280 KNOTS. MONITORED GAUGES AND FLAPS EXTENDED UNCOMANDED UP TO 4 DEGREES. THIS HAPPENED APPOX 4 TIMES IN FLIGHT. ALONG WITH THE FLAPS DEGRADED STATUS MESSAGE AFTER LANDING PAX IN ROW 8 REPORTED LOUD CONTINIOUS POPPING SOUND WHILE AT CRUIS AT ABOUT SAME TIME AS FIRST INCIDENT OCCURED. EMERGENCY DECLARED AS A PRECAUTION. R & R LT FLAP POSITION TRANSMITTER IAW AMM 27-55-01, REF 27-55-00, ITEM 5A. OPS TEST GOOD NO DEFECTS NOTED. SDR CLOSED.

Part: ISOLATOR — BROKEN (AFT BULKHEAD) · airframe 20,395 hrs · 18,694 cycles

ISOLATOR BROKEN ON THE AFT CARGO BULKHEAD. R & R ISOLATOR ON THE AFT CARGO BULKHEAD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,395 hrs · 18,694 cycles

CRACK FOUND ON PAX DOOR AFT DRAG ANGLE AND HAS PROPOGATED BEYOND LIMITS. CUT OUT DAMAGE PORTION OF DRAG ANGLE IAW REO 601R-52-11-513, REV A. COMPLIED WITH EDDY CURRENT INSPECTION IAW NDTM 51-20-06. NO DEFECTS NOTED, FABRICATED ANGLE SECTION AND SPLICE ANGLES IAW REO 601R-52-11-513 REV. A, INSTALLED REPAIR PARTS IAW REO 601R-52-114-513.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,161 hrs · 18,435 cycles

FOUND CRACK ON PASSENGER DOOR AFT DRAG ANGLE. COMPLIED WITH REO 601R-52-11-1360 REV B.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,161 hrs · 18,435 cycles

FOUND CRACK ON PAX DOOR AFT DRAG ANGLE. REPAIRED IAW REO 601R-52-11-513, REV A. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,987 hrs · 18,251 cycles

AFT CENTER CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-16, OP'S CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,358 hrs · 17,577 cycles

LOWER PAX DOOR EXIT SIGN DOES NOT ILLUMINATE. R & R LOWER PAX DOOR EMERGENCY EXIT SIGN IAW AMM 33-51-10-04. (SDR CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,323 hrs · 17,539 cycles

LEFT EXTERIOR NR 7 EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 7 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. RELAMPED NR 7 EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21.

Part: POST — CRACKED (BS 409) · airframe 19,260 hrs · 17,478 cycles

FS 409+128 VERTICAL POST RBL 18 FAILED NDT WITH INDICATION FSH IN UPPER INBD AFT RADIUS.

Part: POST — CRACKED (BS 409) · airframe 19,242 hrs · 17,458 cycles

FS 409+128 VERTICAL POST BL 0 FAILS NDT WITH A CRACK INDICATION IN UPPER AFT RT RADIUS. REMOVED AND REPLACED POST IAW SRM 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 19,242 hrs · 17,458 cycles

FS 409+128 VERTICAL POST RBL 18 FAILS NDT WITH A CRACK INDICATION IN UPPER INBD AFT RADIUS. REMOVED VERTICAL POST IAW SRM 51-42-06. LOCATED FASTENER HOLES IN NEW POST IAW SRM 51-40-11. INSTALLED NEW POST IAW SRM 51-42-06.

Part: BULKHEAD WEB — CRACKED (BS 559) · airframe 19,242 hrs · 17,458 cycles

FS 559 BULKHEAD FAILS NDT WITH A CRACK INDICATION ON RBL 18 WEB. REPAIRED IAW REO 601R-53-41-609 02.

Part: BULKHEAD — CRACKED (BS 202) · airframe 18,770 hrs · 16,907 cycles

CRACK ON BS 202 BULKHEAD. FABRICATED REPAIR DOUBLER IAW REO 601R-53-11-563, REPAIR 2 AND INSTALLED REPAIR IAW REO 601R-53-11-2177 P1 AND REO 601R-53-11-563.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,752 hrs · 15,793 cycles

RIGHT EXTERIOR NR 4 EMERGENCY LIGHT INOPERATIVE. RELAMPED RT EXTERIOR NR 4 EMERGENCY LIGHT IAW AMM 33-51-21, OP'S CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,528 hrs · 14,389 cycles

EMERGENCY LIGHT (VERTICAL) AT PAX DOOR AND BOTH EMERGENCY LIGHTS AT SERVICE DOOR ARE INOP. TROUBLESHOT, FOUND EMERGENCY LIGHT WIRING SWAPPED FWD OF SERVICE DOOR OUTBD OF GALLEY. INSTALLED WIRING CORRECTLY IAW WDM 33-51-00 AND COMPLIED WITH OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. NO DEFECTS FOUND.

Part: LAMP — INOPERATIVE (SEAT 4AB) · airframe 16,528 hrs · 14,389 cycles

CABIN CEILING EMERGENCY LIGHT AT SEAT 4AB INOP. R & R CABIN CEILING EMERGENCY FLOOD LIGHT LAMP AT SEAT 4AB IAW AMM TASK 33-51-16-400-801, TESTED EMERGENCY LIGHTS IAW AMM 33-51-00-710-801 NO DEFECTS FOUND.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 16,528 hrs · 14,389 cycles

FS 484.00 RBL 27.00 PRESSURE FLOOR SUPPORT BEAM INTERCOSTAL ATTACH ANGLE CRACKED IN RADIUS. R & R ATTACH ANGLE AT RBL 27 FS 484.00. R & R ATTACHED ANGLE RBL 27 AND FS 484.00 IAW SRM 51-42-21. (CLOSED)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,528 hrs · 14,389 cycles

FS 280 CLIP CRACKED AT RBL 9.0 FLOORBEAM INBD SIDE. R & R CLIP AT RBL9.0 INBD SIDE AT FS280 IAW SRM 51-42-21. (CLOSED)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 16,528 hrs · 14,389 cycles

FS 280 CLIP CRACKED AT LBL 9.0 FLOORBEAM OTBD SIDE. (RESOLVED ON W/O: 164440 TASKCARD: N/R-00322 ) JOB 8772071/ OPERATION 176/ R & R CLIP ON LBL 9.0 OTBD AT FS 280. R & R CLIP AT FS 280 ON LBL 9.0 OTBD SIDE IAW SRM 51-42-21. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 16,528 hrs · 14,389 cycles

CARGO COMPARTMENT BETWEEN FS 559 + 80 AND FS 574.00, RBL 43.00 FLOOR SUPPORT STRUCTURE UPPER SURFACE AROUND FASTENER HOLES HAS CORROSION. REMOVED CORROSION ON FLOOR SILL IAW SRM CH 51-21-06. PERFORMED UT THICKNESS INSP OF BLEND AREAS IAW MAC NAT INSP PROCEDURE UT-3 MINIMUM THICKNESS REMAINING IS .056". PERFORMED EDDY CURRENT INSP IAW NDTM 51-20-06 AND REO 601R-53-121. NO CRACKS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 16,528 hrs · 14,389 cycles

CARGO COMPARTMENT BETWEEN FS 559 + 80 AND FS 559 + 112 LBL 43.00 FLOOR SUPPORT STRUCTURE UPPER SURFACE AROUND FASTENER HOLES HAS CORROSION. BLENDED CORROSION ON FLOOR SILL IAW SRM 51-21-06. PERFORMED UT THICKNESS INSP OF BLEND AREAS ON LT FLOOR SILL IAW MAC NDT INSP PROCEDURE UT-3 MINIMUM THICKNESS REMAINING OS .061". COMPLIED WITH STEP 3 OF REO 601R-53-51-120 IAW NDTM PART 1, 51-20-06. NO INDICATIONS NOTED. COMPLIED WITH STEPS 4 AND 5 OF REO 601R-53-51-120.

Part: COVER — DAMAGED (GLOWSTRIP) · airframe 16,528 hrs · 14,389 cycles

FLUSH TRACK COVER, FLOOR PHOTOLUMINESCENT FOUND UNSERVICEABLE AT LT AND RT, CTR AND AFT LOCATIONS APPOX 25 FT. R & R LT & RT CTR AND AFT FLUSH TRACK COVERS IAW AMM 33-51-01-000-801 AND 33-51-01-400-801.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 16,528 hrs · 14,389 cycles

CARGO COMPARTMENT BETWEEN FS 605.00 AND FS 621.00, RBL 43.00 FLOOR SUPPORT STRUCTURE AROUND FASTNER HOLES HAS CORROSION. BLENDED CORROSION ON FLOOR SILL BETWEEN FS 605.00 AND FS 621.00 RBL 43.00 IAW SRM CH 51-21-06. PERFORMED LPT THICKNESS MEASUREMENT OF BLENDED AREAS ON FLOOR SILL IAW MAC NDT INSP PROCEDURE UT-3. MINIMUM MATERAL REMAINING IS .046". PERFORMED EDDY CURRENT INSP IAW NDTM 51-20-06 AND REO 601R-53-61-3708. NO CRACKS NOTED.

Part: ANGLE — CHAFED (FIREWALL) · airframe 16,528 hrs · 14,389 cycles

2 EACH ANGLES CHAFED THROUGH AND CRACKED ON RT ENGINE UPPER FIREWALL DOOR 422BT. R & R (2 EA) ANGLES ON RT ENGINE UPPER FIREWALL DOOR PANEL 422BT AND INSTALLED NEW NO STEP DECAL ON PANEL 422BT ALSO IAW SRM 51-42-06 AND AMM 11-20-04.

Part: ATTACH FITTING — CRACKED (BS 461) · airframe 16,528 hrs · 14,389 cycles

FS 461.00 RBL 9.00 INTERCOSTAL ATTACH FITTING CRACKED IN AFT UPPER RADIUS. REMOVED INTERCOSTAL BETWEEN RBL9 AND RBL18 AT FS 461.00, REMOVED INTERCOSTAL ATTACHMENT FITTING AT FS 461.00 ON RBL9 FRAME, AND DRILLED NEW FITTING OK TO INSTALL IAW SRM 51-42-21. INSTALLED FASTENERS COMMON TO SIDE OF RBL 9.00 IN INTERCOSTAL ATTACH FITTING IAW SRM 51-42-20 AND DWG 600-31068 INSTALLED 10 FASTENERS COMMON TO PRESSURE FLOOR IAW REO 601R-53-41-1252. INSTALLED INTERCOSTAL BETWEEN RBL 9 AND RBL 18 IAW SRM 51-42-21.

Part: SILL — CORRODED (BS 473) · airframe 16,528 hrs · 14,389 cycles

FS 473.15 RBL 43.00 JUST ABOVE PRESSURE FLOOR SILL STRUCTURE FRAME HAS CORROSION. REWORKED AREA LOCATED ON INNER DOUBLER PN 601R31108-120 AT FS 473.15 IS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00, FIG 101, SHEET 1 AND 3 AREA IS LESS THAN 10 PERCENT OF CROSS SECTIONAL AREA AND IS MORE THAN .1" AWAY FROM ADJACENT RIVET.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 16,528 hrs · 14,389 cycles

CARGO COMPARTMENT BETWEEN FS 574.00 AND FS 621.00, LBL 27.00, FLOORBEAM UPPER CAP INBD & OTBD FASTENER HOLES HAVE CORROSION. STARTED BLENDING CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED UPPER CAP FROM FLOORBEAM AT LBL 27.00, FS 574-621 IAW SRM 51-42-06. DRILLED FASTNER HOLES INTO NEW PART IAW SRM 51-42-21. INSTALLED FLOORBEAM UPPER IAW REO 601R-53-61-3710 & SRM 51-42-21.

Part: SILL — CORRODED (BS 424-513) · airframe 16,528 hrs · 14,389 cycles

FS 424.00 THRU FS 513.00 PRESSURE FLOOR SILL WEB AND FINGER DOUBLERS HAVE CORROSION BETWEEN RBL-36.00 AND RBL 43.00. COMPLIED WITH STEP A A&B IF DISPOSITION 1.2 OF REO 601R-53-41-666 ALL DAMAGED AREAS WITH IN LIMIT IAW REO 601R-53-41-666

Part: WEB — CORRODED (BS 449-559) · airframe 16,528 hrs · 14,389 cycles

FS 449.85 THRU FS 559.00 BETWEEN LBL 36 AND LBL 43.00 PRESSURE FLOOR SILL WEB UPPER SURFACE AND FINGER DOUBLERS HAVE CORROSION. BLEND END OUT CORROSION FROM 21 LOCATIONS 12 OF WHICH FOUND TO BE WITHIN LIMITS. ALL WORK DONE IAW REO 601R-53-41-666 STEPS A&B.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 16,528 hrs · 14,389 cycles

FS 484.00 AT LBL 27 AND LBL 36 INTERCOSTAL ATTACH ANGLES CRACKED THRU UPPER ATTACH FASTENER HOLE. R & R ATTACH ANGLES AT LBL 27 AND LBL 36, FS 484.00. R & R LBL 27 AND LBL 36 INTERCOSTAL ATTACHED ANGLES AT FS 484.00 IAW SRM 51-42-21.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,463 hrs · 14,313 cycles

IN FLT AT 250FL CAPT'S SIDE WINDSCREEN FORMED A CRACK. ALSO, RECEIVED LT WINDSCREEN HEAT CAUTION MSG. R & R CAPTS WINDSHIELD IAW AMM 56-11-01. (CLOSED)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,186 hrs · 13,990 cycles

AFT CEILING EMERGENCY FLOOD LIGHT INOP. (RESOLVED ON W/O: 155465 TASKCARD: N/R-00004 )/ 12 APRIL 2010 -- RELAMPED AFT CEILING EMERGENCY FLOOD LIGHT. OPS CHECK GOOD. RELAMPED AFT CEILING EMERGENCY FLOOD LIGHT. OPS CHECK GOOD. (CLOSED)

Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG) · airframe 16,118 hrs · 13,909 cycles

ON DEPARTURE GEAR UP DISAGREE WARNING. NOSE DOOR OPEN MSG RAN QRH GEAR DOWN & LOCKED RESULTED. GEAR PINNED AT THE GATE ALL 3 IAW MX REQUEST. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED) ADJUSTED NLG CENTERED EXTENDED PROXIMITY SENSOR IAW AMM 32-61-05. RETRACTED AND EXTENDED GEAR 5 TIMES, OPS CHECKS GOOD IAW AMM 32-30-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,941 hrs · 13,691 cycles

LEFT NR 3 EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LT NR 3 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: SWITCH — BROKEN (EMERGENCY LIGHT) · airframe 15,088 hrs · 12,713 cycles

EMERGENCY LIGHT SWITCH BROKEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,717 hrs · 12,341 cycles

2ND FROM FRONT CABIN CEILING EMERGENCY LIGHT INOP.

Part: SWITCH — MISSING (FLASHLIGHT) · airframe 14,176 hrs · 11,816 cycles

F/O FLASHLIGHT MISSING ON/OFF SWITCH.

Part: SIGN — BROKEN (CABIN) · airframe 13,001 hrs · 10,755 cycles

LOWER EMERG EXIT SIGN NEAR FLOOR BROKEN AT PAX BOARDING DOOR. REPLACED LENS AMM 33-51-19.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 12,505 hrs · 10,316 cycles

INTERCOSTAL AT FS 461 RLB 9 CRACKED AT TOP. UPON FURTHER INVESTIGATION FOUND ANGLE CRACKED AT FS 484 RBL 36 INSTEAD OF FS 461 RBL 9. (S)

Part: INTERCOSTAL — CRACKED (BS 484)

FS 484.0 RBL 36.0 INTERCOSTAL CRACKED AT UPPER FASTENER HOLE APPROX .3" LONG. NOT PREVIOUSLY REPAIRED. REPAIRED RBL 36.0 INTERCOSTAL IAW REO 601R-53-41-059, REV. A. (B)

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 12,505 hrs · 10,316 cycles

CARGO DOOR FWD C-CHANNEL CRACKED, APPROX .5" LONG. REMOVED AND REPLACED CARGO DOOR FWD C-CHANNEL IAW CRJ 200 SRM 51-42-06. (S)

Part: ANGLE — CRACKED (BS 621-625) · airframe 12,505 hrs · 10,316 cycles

RT FS 621 - FS 625 UPPER OBLIQUE ANGLE CRACKED .5 INCH IN LENGTH. REMOVED AND REPLACED RT FS 621 - FS 625 OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (S)

Part: SUPPORT BEAM — CRACKED (CARGO DOOR)

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.5" IN LENGTH. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE WITH NEW PART IAW SRM 51-42-21 AND 51-40-11. (B)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 12,505 hrs · 10,316 cycles

FS 280.0 LBL 9.0 I/B CLIP CRACKED. REMOVED OLD CRACKED CLIP AT FS 280.00 LBL 9 I/B. INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-21. (S)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 12,505 hrs · 10,316 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2 INCH IN LENGTH 100% FULL SCREEN HEIGHT. FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD AT LINTEL ATTACHMENT FITTING IAW REO 601R-53-61-1230. REQUIRES PAINT. PAINTED REPAIR AREA IAW SRM 51-25-01. (S)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 12,505 hrs · 10,316 cycles

FS 280 RBL 9.0 O/B CLIP CRACKED. REMOVED OLD CRACKED CLIP AT FS 280.00 RBL 9 O/B. INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-21.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 12,505 hrs · 10,316 cycles

TWO INCH CRACK ON TAIL JUST UNDER AND TO THE RIGHT OF THE NAV LIGHT. REPAIRED 2 INCH SCRATCH INTO THE WIRE MESH ON TAILCONE UNDER THE RT OF NAV LIGHT. NOT A CRACK IAW REO 601R-53-84-001 CRJ SRM 51-74-02. NEED PAINTED. PAINTED REPAIR AREA IAW SRM 51-74-02. (S)

Part: HANDLE — CRACKED (AV DOOR) · airframe 12,066 hrs · 9,957 cycles

AV BAY DOOR HANDLE CRACKED.

Part: BLEED AIR SYS — ODOR · airframe 11,331 hrs · 9,335 cycles

OIL/GAS/GREASE ODOR ON DESCENT AND WHEN SWAPPING BLEEDS FROM APU TO ENGINES. OILY AND MOLDY ODOR WHEN TRANSFERRING BLEED TO APU, FLT 4373 DEL 42 MINS.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 10,627 hrs · 8,764 cycles

EMERGENCY LIGHTS FAIL TO ILLUMINATE DURING TEST OR WHEN SWITCHED ON.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,409 hrs · 8,599 cycles

EMERGENCY LIGHTING INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,224 hrs · 8,454 cycles

LEFT OVERWING EMERGENCY LIGHT IS INOP.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 8,818 hrs · 7,390 cycles

ASD HANDLE HAS EVIDENCE OF A CRACK IN FWD RADIUS.

Part: BEAM — CRACKED (FUSELAGE) · airframe 7,832 hrs · 6,634 cycles

FOUND RT LOWER BOX BEAM WEB CRACKED AT FWD IB NUTPLATE.

Part: SKIN — CRACKED (BS 640 S10-11R) · airframe 7,832 hrs · 6,634 cycles

INTERNAL BONDED SKIN DOUBLER IS CRACKED BETWEEN STRINGERS 10 AND 11 ON RT SIDE AT FS 640.00. REFER TO REFERENCE REO 601R-53-61-506

Part: RIB — CRACKED (LT WING) · airframe 7,832 hrs · 6,634 cycles

FOUND LT MLG WHEEL WELL BATTERY RIB IS CRACKED.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 7,832 hrs · 6,634 cycles

FOUND LT FUSELAGE STA 484 OB CLIP IS CRACKED.

Part: ATTACH FITTING — CRACKED (FUSLEAGE) · airframe 7,832 hrs · 6,634 cycles

FOUND LT OUTBOARD RT 280 CLIP LB9 CRACK.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 7,832 hrs · 6,634 cycles

FOUND RT FUSE STA 621 FLOOR ATTACH ANGLE IS CRACKED APROX RBL 27.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 7,832 hrs · 6,634 cycles

RT IB AND OB FUSE 280 CLIPS CRACKED.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 7,832 hrs · 6,634 cycles

FOUND LT FS STA 484 IB CLIP IS CRACKED.

Part: SKIN — CORRODED (LT WING) · airframe 7,832 hrs · 6,634 cycles

FOUND CORROSION ON FUEL TANK ACCESS LANDS OF LT WING ACCESS 510AB AND 540BB.

Part: ATTACH FITTING — CRACKED (BS 625) · airframe 7,832 hrs · 6,634 cycles

BOTH LT AND RT FS 625 CLIPS CRACKED.

Part: DOUBLER — CRACKED (BS 640) · airframe 7,832 hrs · 6,634 cycles

FOUND SUSPECT RT 640 DOUBLER IS CRACKED.

Part: FITTING — CRACKED (DOOR) · airframe 7,832 hrs · 6,634 cycles

FWD AIRSTAIR DOOR ANCHOR FITTING IS CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,811 hrs · 6,608 cycles

EMERGENCY LIGHT ABOVE ROW 2 INOP

Part: BUSS — WARNING MESSAGE (AC SYSS) · airframe 7,785 hrs · 6,568 cycles

AC ESS BUSS CAUTION MSG AND EMERGENCY LIGHTS ILLUMINATED.

Part: BPSU — INOPERATIVE (LEFT)

FLT 4614 - DURING CRUISE FROM AVP-ATL, AT APPROXIMATELY 30,000 FEET, THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE WITH THE FLAPS AT ZERO DEGREES. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY WITH THE EMERGENCY VEHICLES DISPATCHED. THE AIRCRAFT PERFORMED A ZERO FLAP LANDING IN ATL, WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT BPSU. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)