N859AS

Part: WARNING MESSAGE — ACTIVATED (THRUST REVERSER) · airframe 33,902 hrs · 30,812 cycles

RT REVERSER UNLOCKED MSG IN FLT RAN THE QRH, NOTHING CHANGED. REV ON THE UNLOCKED, RT REVERSER UNLOCKED EICAS, AND UNLOCK EMERGENCY STOW. ENROUTE ACFT DIVERTED DUE TO MAINTENANCE EMERGENCY ACTIONS. CYCLED RT THRUST REVERSER IAW 78-30-00, OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,208 hrs · 30,078 cycles

EXTERIOR EMERGENCY LIGHT FWD OF THE ASD IS INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 32,637 hrs · 29,479 cycles

BS 621 BULKHEAD, ISOLATORS ARE CRACKED. R & R THE ISOLATORS IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 621) · airframe 32,637 hrs · 29,479 cycles

BS 621, CARGO DOOR SUPPORT BEAM, AFT LOWER ANGLE IS CRACKED. R & R IAW SRM 51-42-21.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 32,355 hrs · 29,205 cycles

LEFT EXTERIOR EMERGENCY LIGHT AFT OF EMERGENCY EXIT INOPERATIVE. TROUBLESHOT EMERGENCY EXIT LIGHT AND FOUND NR 4 BATTERY NOT TAKING A CHARGE. REPLACED NR 4 BATTERY IAW AMM 33-51-04. OPS CHECK GOOD IAW AMM 33-51-00. NO FURTHER DEFECTS. REF IPC 33-51-04, ITEM 17.

Part: SKIN — DAMAGED (BS 409) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE AT BS 409+16 AND +32 BETWEEN S24-25L. REPAIRED IAW REO 601R-53-00-567, REPAIR E. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 409) · airframe 31,507 hrs · 28,367 cycles

LIGHTING STRIKE BETWEEN BS 409- 409.00+16 S25L. REPAIRED IAW REO 601R-53-00-567, REPAIR O. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 718) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE AT BS 718 BETWEEN S25-26L. REPAIRED IAW REO 601R-53-00-567, REPAIR M. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 654-672) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE AT BS 654.5 AND 672.2 S26L. REPAIRED IAW REO 601R-53-00-567, REPAIR J. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 235-250) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE BETWEEN BS 235-250, S26L. REPAIRED IAW REO 601R-53-00-567, REPAIR NR 1. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 349) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE AT BS 349 S25L. REPAIRED IAW REO 601R-53-00-567, REPAIR D. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 265-280) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE BETWEEN BS 265 AND 280, BETWEEN S25-26L. COMPLIED WITH REO 601R-53-00-267. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 409) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE DAMAGE BETWEEN BS 409+32 TO +48, S25L. REPAIRED IAW REO 601R-53-00-567, REPAIR NR 2. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 169) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE AT BS 169.5 TO LT CENTERLINE. COMPLIED WITH REO 601R-53-00-567. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 589) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE AFT OF BS 589 S25L. REPAIRED IAW REO 601R-53-00-567, REPAIR I. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 250-265) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING DAMAGE AT LOCATION BETWEEN BS 250 AND 265, S26L. COMPLIED WITH REO 601R-53-00-267. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 755) · airframe 31,507 hrs · 28,367 cycles

LIGHTNING STRIKE AT BS 755, BETWEEN S26-27L. REPAIRED IAW REO 601R-53-00-567, REPAIR N. MAJOR REPAIR.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 31,507 hrs · 28,367 cycles

EMERGENCY LIGHT ON INBD AFT OF F/A STATION INOPERATIVE. REPLACED WIRE SPLICES FOR EMERGENCY LIGHT IAW ESPM 20-17-31. FOUND EMERGENCY LIGHTS AT SERVICE DOOR CONNECTOR NOT CONNECTED. CONNECTED IAW AMM 33-51-04 ESPM 20-17-31. OPS TEST ALL EMERGENCY LIGHTS GOOD IAW AMM 33-51-00-710-801.

Part: LIGHT — CRACKED (PAX DOOR) · airframe 31,507 hrs · 28,366 cycles

ASD INNER HANDLE BETA LIGHT CRACKED. R & R BETA LIGHT FOR THE PASENGER DOOR IAW AMM 33-51-09-000-801 AND 33-51-09-400-801.

Part: COVER — DEBONDED (RUDDER) · airframe 31,507 hrs · 28,366 cycles

BOTTOM EDGE OF RUDDER LIGHTNING HOLE TAPE MISSING AND LARGE HOLE COVER DISBONDING FROM RUDDER STRUCTURE. COMPLIED WITH EC/TC, REO 601R-55-41-018 01. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,507 hrs · 28,366 cycles

CORROSION ON END OF FLOORBEAM BS 349 RT SIDE. MAJOR REPAIR.

Part: FRAME — CRACKED (CARGO DOOR) · airframe 31,507 hrs · 28,366 cycles

FRAME CRACKED INSIDE CARGO DOOR AFT LOWER CORNER. REMOVED VERTICAL AFT MEMBER, PN 601R35027-31 IAW SRM 51-42-13 AND 51-42-20. LOCATED AND DRILLED HOLES IN VERTICAL AFT MEMBER, PN 601R35027-31 IAW SRM 51-42-13 AND 51-42-20. INSTALLED NEW VERTICAL MEMBER FRAME INSIDE AFT CARGO DOOR AT LOWER CORNER IAW SRM 51-42-06, 51-42-13, 51-42-21 AND DWG 601R35027.

Part: HOUSING — GOUGED (DOOR HANDLE) · airframe 31,507 hrs · 28,366 cycles

CARGO DOOR HANDLE HOUSING GOUGED. COMPLIED WITH STEP 1 OF REO 601R-52-31-086. MAJOR REPAIR.

Part: HINGE — GOUGED (PAX DOOR) · airframe 31,507 hrs · 28,366 cycles

ASD HINGE GOUGED LOBES. COMPLIED WITH REO 601R-53-21-2518 AND EC/TC REO 601R-53-21-2518. MAJOR REPAIR.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 31,507 hrs · 28,366 cycles

ASD AFT DRAG ANGLE CRACKED. REMOVED AFT TOP ANGLE, PN 600-31907-159 IAW SRM 51-42-13. INSTALLED DRAG ANGLE IAW SRM 51-42-13-00 AND DWG 600-31907.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 31,507 hrs · 28,366 cycles

TWO ISOLATORS ARE CRACKED ON REAR PRESSURE BULKHEAD. REMOVED ISOLATORS IAW SRM 51-42-06 AND REPLACED IAW SRM 51-42-13.

Part: HINGE — GOUGED (PAX DOOR) · airframe 31,507 hrs · 28,366 cycles

PASSENGER DOOR HINGE DOOR SIDE IS GOUGED. COMPLIED WITH REO 601R-52-11-1347 AND EC/TC REO 601R-52-11-1347.

Part: LIGHT — DAMAGED (CABIN) · airframe 31,507 hrs · 28,366 cycles

EMERGENCY LIGHT HAS MOST OF TRACK STAINED, TOO SHORT AT EXITS. REPLACED IAW MM 41-10, 33-60-13.

Part: ANGLE — CRACKED (BS 280) · airframe 31,507 hrs · 28,366 cycles

ANGLE CRACKED AT FS 280 AND LBL 9. R & R ANGLE IAW SRM 51-42-06 AND 51-42-21-00.

Part: STRUCTURE — CRACKED (INLET DUCT) · airframe 31,507 hrs · 28,366 cycles

APU LOWER INLET DUCT CRACKED. REMOVED APU LOWER INLET DUCT IAW AMM 49-14-01-000-801 AND REPLACED IAW AMM 49-14-01-400-801.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 31,505 hrs · 28,365 cycles

LEFT OVERWING EMERGENCY EXIT COVER CRACKED AT LOWER END IN TWO PLACES. REPLACED OVERWING EMERGENCY EXIT COVER IAW AMM 25-26-04-400-801.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 31,505 hrs · 28,365 cycles

RT OVERWING EMERGENCY EXIT COVER CRACKED AT LT LOWER END. REPLACED OVERWING EMERGENCY EXIT COVER IAW AMM 25-26-04-400-801M.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,507 hrs · 28,366 cycles

SKIN DAMAGED COMPLIED WITH EC/TC REO 601R-53-00-567 PERMANENT REPAIR. MAJOR REPAIR.

Part: SEALANT — MISSING (WNG-BDY FAIRING) · airframe 31,181 hrs · 28,020 cycles

AT FL280 AND 280 IAS, ACFT STARTED TO FLUTTER LIKE DRIVING ON A DIRT ROAD. NO ACFT CONTROL LOST AT ANYTIME. SLOWED ACFT AND IT STOPPED MOMENTARILY THEN STARTED AGAIN. SLOWED TO ABOUT 240 ICAS, DIVERTED, EMERGENCY DECLARED. INSPECTED ACFT AND FOUND THAT THE RT SIDE WING TO FUSELAGE FAIRING WAS UNSEALED IN SEVERAL PLACES. APPLIED SEALANT TO FAIRING IAW SRM 51-14-06.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,980 hrs · 26,782 cycles

LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LT AFT OVERWING EMERGENCY LIGHT IAW AMM 33-51-21. OPS TESTED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,798 hrs · 25,553 cycles

F/O FLASHLIGHT INOPERATIVE. R & R THE F/O'S FLASHLIGHT ASSY AND OPS CHECKED GOOD IAW AMM 25-61-00. DMIL 3184028 CLEARED PLACARD REMOVED.

Part: BRACKET — DAMAGED (PROXIMITY SENSOR) · airframe 28,242 hrs · 24,973 cycles

NOSE GEAR FAILED TO RETRACT ON CLIMB OUT. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. R & R NOSE GEAR CENTERED PROXIMITY SENSOR BRACKET IAW CMM 32-20-04 PERFORMED OPS CHECK IAW AMM 32-30-00. NO DEFECTS NOTED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (MLG) · airframe 28,101 hrs · 24,824 cycles

GEAR DISAGREE WARNING MESSAGE AFTER T/O RT MAIN GEAR SHOWED A RED BOX COMPLIED WITH QRH AND GEAR CAME DOWN WITH ALTERNATE EXTENSION PROCEDURE. (ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. FOUND RT MAIN UPLOCK PROXIMITY SENSOR GAP OUT OF ADJUSTMENT. ADJUSTED RT MAIN UPLOCK PROXIMITY SENSOR TO SPEC IAW AMM 32-32-05. OPS TESTED GOOD. NO DEFECTS NOTED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 27,557 hrs · 24,233 cycles

LEFT MIDDLE EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. INSPECTED AND FOUND CONNECTOR NOT CONNECTED TO LIGHT ASSY. RECONNECTED CONNECTOR IAW AMM 33-51-21. OP'S CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 27,484 hrs · 24,147 cycles

CORROSION ON RT CENTER AISLE SEAT TRACK FROM FS 349.00 TO FS 409.00. REMOVED DAMAGED FWD SECTION OF SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED A NEW SERVICEABLE FWD SECTION OF SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 27,484 hrs · 24,147 cycles

CORROSION ON LT CENTER AISLE SEAT TRACK FROM FS 349.00 TO FS 409.00. REMOVED DAMAGED SEAT TRACK IAW AMM 53-01-11-000-802 FWD AND AFT SECTIONS. INSTALLED NEW FWD SECTION OF SEAT TRACK IAW AMM 53-01-11-400-802. REPAIR IS CLASSIFIED AS MINOR.

Part: CARGO TRACK — CORRODED (BS 621) · airframe 27,484 hrs · 24,147 cycles

CARGO TRACK CORRODED AT LBL 9 BS 621. R & R CARGO TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 27,484 hrs · 24,147 cycles

FOUND REAR PRESSURE BULKHEAD HAS CRACKED ISOLATOR AT RBL 27.50, WL 137.50 AND ATTACHMENT BRACKET IS BENT. INSTALLED NEW ISOLATOR IAW 51-42-13-00.

Part: FLOOR SUPPORT — CORRODED (BS 574-605) · airframe 27,484 hrs · 24,147 cycles

FLOOR SUPPORT LBL 27 AT FS 574-605 FOUND TO BE CORRODED BEYOND REPAIRABLE LIMITS IAW REO 601R-53-00-005. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-66-3778 AND REO 601R-53-61-3778.

Part: FITTING — CORRODED (FUSELAGE) · airframe 27,484 hrs · 24,147 cycles

ALL FOUR CORNER FITTINGS UNDER CMS ARE CORRODED. REMOVED FITTINGS AND REPLACED WITH NEW PARTS IAW SRM 51-42-06.

Part: ATTACH ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 27,484 hrs · 24,147 cycles

BS 621.00 PRESSURE BULKHEAD ATTACHMENT ANGLE AT STR 11L ON AFT FACE CRACKED. REMOVED CRACKED ATTACH ANGLE, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ATTACH ANGLE IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED · airframe 27,484 hrs · 24,147 cycles

REAR PRESSURE BULKHEAD WEB AT LBL 27.50, WL 130 HAS INDICATION NOTED APPROX .3 INCHES IN LENGTH 90 PERCENT FSH. FAILED NDT INSPECTION.

Part: BULKHEAD — CRACKED · airframe 27,484 hrs · 24,147 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .5" IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW EC/TC REO 601R-53-61-1230 AND GREO 601R-53-61-1230, REV F.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 27,484 hrs · 24,147 cycles

ISOLATOR ON AFT SIDE OF 621.00 PRESSURE BULKHEAD AT STR 13L AND STR 13R CRACKED. INSTALLED NEW ISOLATOR IAW 51-42-13-00.

Part: BRACKET — CRACKED (WINDOW) · airframe 27,484 hrs · 24,147 cycles

CO-PILOTS SIDE WINDOW POST LOWER ATTACH BRACKET IS CRACKED. REMOVED AND INSTALLED NEW CO-PILOTS SIDE WINDOW LOWER POST ATTACH BRACKET IAW SRM 51-42-21. MINOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 27,484 hrs · 24,147 cycles

FS 484 FLOORBEAM CRACKED INBD AND OTBD RBL 27 AND 36.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,215 hrs · 23,845 cycles

NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 26,890 hrs · 23,494 cycles

A PIECE OF FLOOR LEVEL TRACK METAL CAME OFF DURING FLIGHT FROM ROW 12 A&B. INSTALLED FLOOR-TRACK EMERGENCY LIGHTING IAW AMM 33-51-01.

Part: LIGHT — MISSING (EMERGENCY EXIT) · airframe 25,510 hrs · 21,926 cycles

EXIT EMERGENCY LIGHT MISSING FROM DMIL 597356-1. REMOVED AND REPLACED FA'S LOWER EMERGENCY EXIT LIGHT OPS CHECKED GOOD IAW AMM 33-51-19.

Part: LIGHT — BROKEN (CABIN) · airframe 25,452 hrs · 21,854 cycles

LOWER EMERGENCY LIGHT ON F/A WARDROBE BASE BROKEN. R & R EMERGENCY EXIT LIGHT OPS CHECKED GOOD IAW AMM 33-51-19.

Part: LIGHT — INOPERATIVE (CABIN)

RT EXTERIOR EMERGENCY LIGHTS NR 4 AND NR 6 INOP. R & R NR 4 AND NR 6 EXTERIOR EMERGENCY LIGHTS IAW AMM 33-51-21. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,237 hrs · 21,610 cycles

ALL EMERGENCY LIGHT INOP AFTER MX ON WARDROBE. WORK COMPLETED IAW ITEM: 1. R & R ALL EMERGENCY BATTERY PACKS IAW M/M 25-24-01. OPS TEST GOOD. COMPLIED WITH FOR THE REPLACEMENT OF ALL EMERGENCY BATTERY PACKS IAW MM 33-51-04 AND IAW GMM 3-3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,031 hrs · 21,375 cycles

OVERHEAD EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED LAMPS IN EMERG EXIT LIGHT IAW CRJ 200 AMM 33-51-14. OPS CHECK GOOD AT THIS TIME.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 24,824 hrs · 21,119 cycles

NR 4 POSITION EXTERIOR EMERGENCY LIGHT INOP. RELAMPED NR4 POSITION EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 24,475 hrs · 20,723 cycles

INBOUND, ON FINAL APPROACH, RECEIVED GEAR DISAGREE WARNING MESSAGE, RAN QRH, PULL MANUAL RELASE HANDLE, DECLAIRED EMERGENCY, LANDED SUSCESSFULLY, TAXIED TO THE GATE. (EMERGENCY DECLARED) ( LANDING GEAR RETRACTION SYS ) R & R MLG SELECTOR VALVE IAW AMM 32-32-10. OPS CHECK GOOD, DEFER CLEARED PLACARD REMOVED.

Part: INTERCOSTAL — CORRODED (BS 364-349) · airframe 23,997 hrs · 20,176 cycles

INTERCOSTAL AT FS 364 TO FS 349 BETWEEN STR 27R AND 26R IS CORRODED AND REQUIRES REPLACEMENT. REMOVED INTERCOSTAL BETWEEN FS 364 AND 349 AND STR 26R AND 27R IAW SRM 51-42-06. NEW INTERCOSTAL REQ'S INSTALL. INSTALLED NEW INTERCOSTAL AT FS 364 TO FS 349 BETWEEN STR 27R AND 26R IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 23,997 hrs · 20,176 cycles

FLOOR SUPPORT CLIPS CRACKED AT FS 280, RBL 9, INBD AND OTBD. REMOVED INBD AND OTBD CLIPS AT FS 280 RBL 9, FABRICATED OTBD CLIP OUT OF S6144-14 .063". LOCATED AND DRILED FASTENER HOLES IN BOTH INBD AND OTBD CLIPS. ALL WORK ACCOMPLISHED IAW SRM 51-40-06 AND IN REF TO REO 601R-53-11-171. REPAIR NEEDS COMPLETED. ANGLES NEED INSTALLED. INSTALLED NEW INBD AND OTBD CLIPS AT FS 280, RBL 9 IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 23,997 hrs · 20,176 cycles

FLOOR SUPPORT CLIPS CRACKED AT FS 280, LBL 9, INBD AND OTBD. REMOVED CLIPS AT FS 280, LBL 9, INBD AND OTBD FOR REPLACEMENT IAW SRM 51-42-21. LOCATE, DRILL AND INSTALL NEW CLIPS. LOCATED AND DRILLED NEW CLIPS FOR FS 280, LBL 9 FLOOR SUPPORT IAW SRM 51-40-11. INSTALL CLIPS. INSTALLED 2EA SERVICEABLE CLIPS IN CONJUNCTION WITH MWC 8742111 OP 154.

Part: POST — CRACKED (BS 409) · airframe 23,997 hrs · 20,176 cycles

FOUND FS 409.0+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS A INDICATION NOTED APPROX .2" IN LENGTH 90 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED INBD AND OTBD VERTICAL POSTS AT LBL 18 FS 409+128 IAW SRM 51-42-06. LOCATED AND DRILLED OTBD POST IAW SRM 51-42-06. LOCATED AND DRILLED INBD POST IAW SRM 51-42-06. BOTH POSTS REQUIRE INSTALLATION. INSTALLED FS 409+128 VERTICAL POSTS AT LBL 18 IAW REO 601R-53-41-889 AND SRM 51-42-06. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889 REV A.

Part: FRAME — CORRODED (BS 364) · airframe 23,997 hrs · 20,176 cycles

FS 364.0 HAS CORROSION AT LOWER BELLY SECTION AND REQUIRES REPLACEMENT OF FRAME IN THAT AFFECTED AREA. REMOVED FASTENERS AND CORROSION AROUND EFFECTED AREAS OF FRAME 264.0 AT LOWER BELLY SECTION AND FOUND FRAME TO HAVE AN ORIGINAL THICKNESS OF .080 WITH MATERIAL LOSS AT DEEPEST POINT TO BE .008 MAKING BLEND OUT WITHIN LIMITS IAW SRM 51-42-06, 53-21-15, AND 53-00-00 FIG 102. INSTALLED NEW SERVICEABLE RIVETS IAW SRM 51-42-06 AT FS 364. REQUIRES PAINT. APPLIED PAINT AND CORROSION PREVENTATIVE TO FS 364 FRAME AND BELLY SECTION AND AFFECTED AREAS IAW SRM 51-25-01 AND 51-21-11.

Part: FRAME — CORRODED (BS 349) · airframe 23,997 hrs · 20,176 cycles

FS 349.0 HAS CORROSION AT LOWER BELLY SECTION AND REQUIRES REPLACMENT OF FRAME IN THAT AFFECTED AREA. REMOVED FRAME 349.0 FROM STR 23R TO STR 23L IAW SRM 51-42-06. DRILLED NEW SERVICEABLE FRAME AT FS 349 FRAME STR LBL 23 TO RBL 23 IAW SRM 51-42-06 AND 51-42-21. INSTALLED FRAME AT FS 349 STR LBL 23 TO STR RBL 23 MINUS 4EA LOCK FASTENERS ON OTBD END, 2 AT LBL 23 AND 2 AT RBL 23 IAW SRM 51-42-06 AND 51-42-21. INSTALL 4 EA LOCK FASTENERS. INSTALLED 4 EA LOCK FASTENERS ON OTBD ENDS OF FRAME FS 349 IAW SRM 51-42-21. APPLIED PAINT AND CORROSION PREVENTATIVE TO FS 349 FRAME AND SURROUNDING AREA IAW SRM 51-25-00 AND 51-21-11.

Part: POST — CRACKED (BS 409) · airframe 23,997 hrs · 20,176 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18.0 INBD AND OTBD SIDES HAVE INDICATIONS NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED INBD AND OTBD VERTICAL POSTS AT RBL 18 FS 409+128, LOCATED AND DRILLED OTBD POST IAW SRM 51-42-06. LOCATED AND DRILLED INBD POST IAW SRM 51-42-06. INSTALLED FS 409+128 VRTICAL POSTS AT RBL 18 IAW REO 601R-53-41-889 AND SRM 51-42-06. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889 REV A.

Part: FRAME — CORRODED (BS 333) · airframe 23,997 hrs · 20,176 cycles

FS 333.0 HAS CORROSION AT LOWER BELLY SECTION AND REQUIRES REPLACEMENT OF FRAME IN THAT AFFECTED AREA. REMOVED FRAME AT FS 333, LBL 23 TO RBL 23 IAW SRM 51-42-06. DRILLED TO FINAL SIZE NEW SERVICEABLE FRAME AT FS 333, LBL 23 TO RBL 23 IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE FRAME AT FS 333.0, RBL 23 TO LBL 23 IAW SRM 51-42-06 AND 51-42-21. INSTALLED (6EA) GROUNDING STUDS & WIRES IAW AMM 51-80-00, TEMP REV 51-033, TASK 51-80-00-400-804. C/W ELECTRICAL GROUNDING CHECK OF GROUND STUDS, CHECK GOOD IAW AMM 51-80-00-760-803. APPLIED PAINT AND RIVETS AND FASTENERS IAW SRM 51-25-00.

Part: INTERCOSTAL — CORRODED (BS 364 S26-27L) · airframe 23,997 hrs · 20,176 cycles

INTERCOSTAL AT FS 364.00 FWD SIDE OF FRAME BETWEEN STR 27 AND STR 26 LT SIDE, HAS CORROSION AND REQUIRES REPLACEMENT. REMOVED INTERCOSTAL AT FS 364 BETWEEN STR 27L AND 26L IAW SRM 51-42-06. INSTALLED NEW INTERCOSTAL AT FS 364 TO FS 349 BETWEEN STRINGERS 27L AND 26L IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 349) · airframe 23,997 hrs · 20,176 cycles

MAIN AVIONICS COMPARTMENT FS 333.0, FS 349.0, FS 364.0 FRAMES HAVE CORROSION. (RESOLVED ON W/O: 155844 TASKCARD: N/R-00404 ) FOR FS 333.0 REFER TO JOB 8742111/343 FOR WORK PERFORMED. FOR FS 349.0 REFER TO JOB 8742111/341 FOR WORK PERFORMED. FOR FS 364.0 REFER TO JOB 8742111/342 FOR WORK PERFORMED. (CLOSED)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,997 hrs · 20,176 cycles

CABIN FLOOR SUPPORT STRUCTURE FS 280.00 LBL 9.0 IS CRACKED. CUT AWAY DAMAGED SECTION OF ANGLE THAT IS CRACKED IAW REO 601R-53-11-138NC. REPAIR NEEDS COMPLETED. REPAIRED CABIN FLOOR SUPPORT STRUCTURE AT FS 280, LBL 9.0 IAW EC/TC REO 601R-53-11-138.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,997 hrs · 20,176 cycles

SEAT RAILS BETWEEN FS 559.00+80 AND RBL 27 ARE CORRODED. R & R SEAT RAILS IAW AMM 53-01-11-000-802 SUBTASK PROC 53-10-11-020-002 B1-3 & 53-01-11-420-001 B1-8.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 23,997 hrs · 20,176 cycles

INTERCOSTAL CLIP CRACKED AT FS 484 AND LBL 27. REMOVED & REPLACED CLIP AT FS 484 LBL27 IAW SRM 51-40-06 & 51-42-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,997 hrs · 20,176 cycles

SKIN AT RT AFT CORNER OF AFT NLG DOOR CUTOUT HAS VISIBLE INDICATION OF BEING CRACKED. PERFORMED EDDY CURRENT OF SKIN AT RT AFT CORNER OF AFT NLG DOOR CUTOUT IAW NDTM 51-20-06. FOUND SKIN RT SIDE AFT CORNER HAS AN INDICATION NOTED APPROX .4" IN LENGTH 90 PERCENT FSH. FAILED NDT. REPAIRED SKIN AT RT AFT CORNER OF NLG DOOR CUTOUT IAW REO 601R-53-11-048. CHECKED NLG REAR DOOR CLEARANCE IAW AMM TASK 32-22-05-220-801. NO DISCREPANCIES NOTED AT THIS TIME. PAINTED REPAIR IAW SRM 51-25-01. C/W EC/TC REO 601R-53-11-0048 IAW REO 601R-53-11-0048 REV C.

Part: SEAT TRACK — CORRODED (BS 559-568) · airframe 23,997 hrs · 20,176 cycles

SEAT RAILS BETWEEN FS 559.00+110 AND FS 568.00 LBL 9 AND RBL 9 ARE CORRODED. R & R SEAT RAILS BETWEEN FS 559.00+110 & FS 568.00 LBL 9 AND RBL 9 IAW AMM 53-01-11-000-802. PROCEDURE SUBTASK 53-01-11-020-002 B1-3 & 53-01-11-420--001 B1-8. AMM 53-01-110-400-802.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,316 hrs · 19,426 cycles

SEVERAL EMERGENCY EXIT LIGHTS DO NOT WORK .

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,150 hrs · 19,234 cycles

EXTERIOR EMERGENCY LIGHTS INOP BY ASD AND SERVICE DOOR.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 23,137 hrs · 19,219 cycles

A/S/D FWD ANCHOR FITTING CRACKED. REMOVED AND REPLACED FWD ASD ANCHOR FITTING IAW AMM 52-11-17. OPS CHECK GOOD. RII C/W SATISFACTORILY IAW SP607 REF AMM 52-11-17.

Part: LIGHT — DETACHED (CABIN) · airframe 21,855 hrs · 17,917 cycles

EMERGENCY LIGHT STRIP AT ROW 11 IS DETACHED FROM FLOOR. FLT 5081 DEL 132 MINS.

Part: DOOR — STUCK (MAIN PAX) · airframe 21,186 hrs · 17,311 cycles

MAIN PASSENGER DOOR IS DIFFICULT TO CLOSE THE MOTOR IS HAVING TROUBLE CLOSING THE DOOR.

Part: FITTING — CRACKED (FUSELAGE) · airframe 19,882 hrs · 16,132 cycles

RIGHT OUTBOARD CLIP FS 280 RBL 9 CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 19,882 hrs · 16,132 cycles

LEFT AND RIGHT SIDE CLIPS ARE CRACKED ON THE AFT SIDE OF THE PRESSURE BULKHEAD FS 625. COMPLIED WITH EC REO 670-55-31-032.

Part: BEAM — CRACKED (FUSELAGE) · airframe 19,882 hrs · 16,132 cycles

CENTER BOX BEAM CRACKED REPAIR PER REO 601R-53-61-345 AND COMPLY WITH EO 600-53-0072 REV B. REPAIRS PERFORMED IAW: REO 601-53-61-345 AND REO 601R-53-61-2563

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 19,872 hrs · 16,122 cycles

ON ROTATION RECEIVED WOW INPUT CAUTION MSG. INTERMITTENT THROUGHOUT FLIGHT, MOST ON. EMERGENCY DECLARED.

Part: ANCHOR FITTING — CRACKED (AIRSTAIR) · airframe 19,506 hrs · 15,821 cycles

AFT A/S/D ANCHOR FITTING ASSY IS CRACKED.

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 18,822 hrs · 15,236 cycles

MAIN DOOR HANDLE WOULD NOT TURN FROM OUTSIDE.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 18,749 hrs · 15,186 cycles

FLAPS FAIL AT 20, TOWER DECLARED EMERGENCY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,451 hrs · 14,948 cycles

RIGHT FWD EXT EMERGENCY LIGHT INOP.

Part: DOOR — STUCK (MAIN PAX) · airframe 17,831 hrs · 14,440 cycles

PAX DOOR WOULD NOT OPEN WITH OUTER HANDLE.

Part: FLAP SYSTEM — FAILED · airframe 17,815 hrs · 14,427 cycles

FLAP FAIL AT 30. EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. FLT 4670 CX.

Part: DOOR — STIFF (MAIN PAX) · airframe 17,653 hrs · 14,313 cycles

FWD PAX DOOR IS VERY DIFFICULT TO UNLATCH AND OPEN FROM THE OUTSIDE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 16,835 hrs · 13,691 cycles

LAV SMOKE DETECTOR HORN DID NOT SOUND WHEN TESTED (LAVATORY SMOKE DETECTION SYSTEM).

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 16,641 hrs · 13,550 cycles

LEFT SIDE FS 640 DOUBLER CRACKED. FLT 4844 CX.

Part: FRAME — CRACKED (FUSELAGE) · airframe 16,641 hrs · 13,550 cycles

LEFT SIDE FS 640 FRAME CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,235 hrs · 12,430 cycles

FOUND CORROSION ON LT SIDE WALL SEAT TRACK, MOST AFT END.

Part: CLIP — CRACKED (BS 484) · airframe 15,235 hrs · 12,430 cycles

RT. OTBD 484 CLIP IS CRACKED, OTBD OF RBL 27. REPAIRED IAW REO601R-53-11--563. (CLOSED)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 15,235 hrs · 12,430 cycles

LT STA 484 INTERCOSTAL CRACKED AT LBL 36. REPAIRED IAW REO601R-53-41-059.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 15,235 hrs · 12,430 cycles

LT STA 484 INTERCOSTAL ATTACH FITTING CRACKED AT LBL27

Part: FRAME — CRACKED (BS 718 S10-11R) · airframe 15,235 hrs · 12,430 cycles

SUSPECT CRACK AT FS 718 FRAME RT SIDE BETWEEN STR10 AND 11. REPAIRED CRACK AT FS 718 FRAME IAW REO 601R-53-61-243 AND EO 600-53-66. (CLOSED)

Part: CLIP — CRACKED (BS 280) · airframe 15,235 hrs · 12,430 cycles

FS280. LT OTBD CLIP IS CRACKED AT LBL9

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 15,235 hrs · 12,430 cycles

SUSPECT CRACK JUST OTBD OF RBL9 AT FLOOR SUPPORT BEAM AT FS280.00

Part: FRAME — CRACKED (BS 672) · airframe 15,235 hrs · 12,430 cycles

POSSIBLE CRACK FROM RIVET, AEB ON ENG AFT MOUNT FWD SPAR AND FRAME, AT FS 672.20 AND STR.10 PERFORMED EDDY CURRENT INSPECTION OF AREA AROUND RIVET AT F.S. 672.20 AND STRINGER 10L, INSIDE AFT EQUIPMENT BAY IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. (CLOSED)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,235 hrs · 12,430 cycles

SUSPECT CRACK AT FWD PRESSURE BULKHEAD BRAKE CABLE CUTOUT. REPAIRED IAW REO-601R-53-11-563 (CLOSED).

Part: LENS — DAMAGED (CABIN) · airframe 15,235 hrs · 12,430 cycles

"EXIT" LENS DAMAGED ABOVE SERVICE DOOR

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A ROUTINE SERVICE CHECK IN CAE, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: TIRE — DAMAGED (RT MLG)

AFTER DEPARTING, THE CREW WAS ADVISED THAT THE MLB TOWER HAD FOUND TIRE DEBRIS ON THE RUNWAY AND SUSPECTED IT WAS FROM THEIR AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT CONTINUED ON, LANDING SAFELY UPON ARRIVAL. MAINTENANCE FOUND DAMAGE TO THE RT IB TIRE WHICH APPEARED TO BE CAUSED FROM A LARGE NAIL. MAINT REMOVED AND REPLACED THE RT IB AND RT OB MAIN TIRE AND WHEEL ASSEMBLIES. NO FURTHER DAMAGE WAS NOTED. AIRCRAFT OK FOR SERVICE. (K)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

DURING AN A-CHECK IN BTR, THE EMERGENCY FLOOR LIGHTS AT ROWS 9 C/D WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE EMERGENCY FLOOR LIGHT CONNECTORS AT ROW 9/CD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A-CHECK IN BTR, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR) · airframe 11,465 hrs

DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 11,320 hrs

DURING A GROUND INSPECTION, THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHTS BATTERY PACK CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

DURING HANGAR MAINTENANCE, THE AFT SECTION OF EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT FOR THE AFT SECTION OF EMERGENCY LIGHTS IN THE CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,216 hrs

DURING A GROUND INSPECTION, THE AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT INTERCOSTALS AT FS 625 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT INTERCOSTALS AT FS 625 IAW SRM 51-42-20.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT IB AND OB CLIPS AT FS280 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACIG THE LT AND RT IB AND OB CLIPS AT FS280.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT FLOOR SUPPORT ANGLES AT FS 621 IAW EO600-53-0105.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK, THE IB INTERCOSTAL AT FS 484, RBL 27 IAW EO 600-53-0098.

Part: LIGHT — CRACKED (CABIN)

DURING C-CHECK, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY ABOUT THE SERVICE DOOR.

Part: STEP — CRACKED (PAX DOOR)

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

Part: LATCH — BINDING (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE MAIN PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE AND THE OUTER HANDLE WOULD NOT ROTATE. MAINTENANCE ADJUSTED THE MAIN PASSENGER DOOR LATCH MECHANISM IAW AMM 52-11-02. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (FUSELAGE)

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

Part: STEP — CRACKED (AIRSTAIR)

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

Part: CONNECTOR — DISCONNECTED (CABIN)

FLT 4228 - DURING A GROUND INSPECTION IN MCI, THE RIGHT SIDE EMERGENCY FLOOR LIGHTS AT ROW TWO WERE FOUND TO BE INOPERATIVE. MAITNENANCE RECONNECTED THE RIGHT SIDE EMERGENCY FLOOR LIGHTS AT ROW TWO. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING AN A-CHECK IN BTR, THE LEFT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EMERGENCY EXIT LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HANDLE — INOPERATIVE (ESCAPE HATCH)

DURING A C-CHECK IN MCN, THE COCKPIT EMERGENCY ESCAPE HATCH OUT HANDLE WOULD NOT DEPLOY. MAINTENANCE REMOVED AND REPLACED THE COCKPIT EMERGENCY ESCAPE HATCH OUTER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

FLT 4397 - WHILE BOARDING THE AIRCRAFT IN YUL-ATL, THE CREW DISCOVERED AN APPROXIMATE 8 INCH CRACK AT THE BOTTOM OF THE CAPTAINS WINDSHIELD. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD. OPS AND HEAT CHECKS GOOD. AIRCAFT OK FOR SERVICE. (M)

Part: WIRE — DAMAGED (CABIN)

FLT 4242 - DURING HANGAR CHECK IN BTR, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE DEFERRED THE LEFT OVERWING EMERGENCY LIGHT IAW MEL NR 33-51-02, PENDING REPLACEMENT OF A BAD DIODE. UPON FURTHER TROUBLESHOOTING, MAINTENANCE FOUND A BAD WIRE AT TERMINAL BOARD 107-2, PIN A AND REPAIRED THE WIRE WHICH CLEARED THE DEFERRAL. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

FLT 4504 - DURING GROUND INSPECTION IN ATL, THE LEFT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4653 - ON GROUND, FORWARD ORANGE SECTION OF FLOOR EMERGENCY LIGHTING DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHTING STRIP. OPERATIONAL CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M)