N901EV

Part: BRACKET — CRUSHED (NLG) · airframe 35,211 hrs · 32,664 cycles

GEAR DISAGREE WARNING. REPLACED BRACKET ON NOSE GEAR SMASHED BY TOWBAR STRAP. OPS CHECKED GOOD.

Part: BRACKET — BENT (PROXIMITY SENSOR) · airframe 34,430 hrs · 31,893 cycles

GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED THE NLG PROXIMITY SENSOR BRACKET IAW AMM. ALL INDICATIONS NORMAL.

Part: SERVO VALVE — MALFUNCTIONED (NLG STEERING) · airframe 33,868 hrs · 31,256 cycles

NOSE WHEEL STEERING INOPERATIVE CAUTION ENROUTE. REMOVED AND REPLACED ELECTRO HYD SERVO VALVE IAW AMM. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,163 hrs · 29,628 cycles

FORWARD EMERGENCY FLOOR LIGHT AND EXIT SIGN ARE INOPERATIVE. R & R ELECTRICAL CONNECTOR IAW ESPM 20-11-00 20-17-10 ON WIRES LY6022 AND LY32A22. R & R EMERGENCY LIGHTS BATTERY NR 2 PACK IAW AMM 33-51-04-400-801, 33-51-04-000-801, IPC 33-51-04, ITEM 17. OPS TEST CHECKED GOOD.

Part: STRUCTURE — CRACKED (BS 202 BULKHEAD) · airframe 32,163 hrs · 29,628 cycles

CENTER LT LOWER CLIP AT 202 PRESSURE BULKHEAD IS CRACKED. REMOVED LT & RT LOWER CENTER POST CLIPS AT 202 PRESSURE BULKHEAD IAW SRM 51-42-21-00. LOCATED, DRILLED AND INSTALLED NEW LT & RT LOWER CENTER POST CLIPS AT 202 PRESSURE BULKHEAD IAW SRM 51-40-11 AND 51-42-21.

Part: SKIN — DAMAGED (LT WING) · airframe 32,163 hrs · 29,628 cycles

WHILE PERFORMING REO 601R-57-21-130, FOUND 1 EA OVERSIZE HOLE ON LT WING PLANK. RECEIVED AND COMPLIED WITH REO 601R-57-21-2436 AND ECTC 601R-57-21-2436.

Part: SHIM — SHIFTED (RT MLG) · airframe 32,163 hrs · 29,628 cycles

REFER TO EO 600-53-2650003, LT AND RT MLG SIDE BRACE FITTING BRACKET SHIMS ARE MIGRATED. COMPLIED WITH PERMANENT REPAIR IAW EC/TC REO 601R-53-41-101-01.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 32,163 hrs · 29,628 cycles

CORROSION AROUND 2 NUTPLATES ON RT FLOOR SILL. RBL 42.5 AND BETWEEN FS 559+32 TO 559+48. CORROSION AROUND 2 NUTPLATES ON RT FLOOR SILL. RBL 42.5 AND BETWEEN FS 559+32 TO 559+48. COMPLIED WITH EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REV. DATED 5/22/2013. REMOVED 2 EA NUTPLATES FROM DISCREPANT AREA IAW SRM 51-45-00. REPLACED 2 EA NUTPLATES AT RBL 42.5 BETWEEN FS 559+32 TO 559+48 IAW SRM 51-45-00.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 32,163 hrs · 29,628 cycles

CORROSION ON LBL 42.5 FLOOR SILL AT FS 559+32. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV, DATED 5/22/2013 AS WRITTEN.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,163 hrs · 29,628 cycles

NR 2 BATTERY PACK INSIDE CABIN FOR EMERGENCY LIGHTS INOPERATIVE. R & R NR 2 EMERGENCY LIGHTS BATTER PACK IAW AMM 33-51-04-000-801/33-51-04-400-801, IPC 33-51-04, FIG 1, ITEM 17. R & R NR 2 EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-04-000-801/33-51-04-400-801, IPC 33-51-04 ITEM 17. OPS TEST OF EMERGENCY LIGHT CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 32,163 hrs · 29,628 cycles

CORROSION AROUND FLOORBOARD SCREW HOLE ON RBL9 AND AT FS 409+40. REMOVED CORROSION AT FS 409+40, RBL 9 INBD SIDE IAW SRM 51-21-06, AND FOUND TO HAVE COMPLETE MATERIAL LOSS. REPAIR FLOORBEAM SUPPORT STRUCTURE IAW SRM 53-00-43. REPAIRED FLOORBEAM AT 409+40 IAW EO 600-53-0772.

Part: BRACKET — CORRODED (BS 319) · airframe 32,163 hrs · 29,628 cycles

BOTTOM CORNER OF SERVICE DOOR CUTOUT AT FS 319.70, STR 17R AND RBL42 CORRODED. LOWER FRAME BRACKET AT FS 319.70 CORRODED OUT OF LIMITS IAW SRM 53-00-00. R & R BRACKET AT FS 319.70 IAW SRM 51-40-11 AND 51-42-21.

Part: PLACARD — CRACKED (SERVICE DOOR) · airframe 32,163 hrs · 29,628 cycles

SERVICE DOOR INNER OPEN/CLOSE HANDLE PHOTOLUMINESCENT "EXIT" PLASTIC PLACARD CRACKED. REMOVED SERVICE DOOR INNER PHOTOLUMINCENT "EXIT" PLACARD BY REMOVING 2 SCREWS WITH A SCREW DRIVER. INSTALLED A SERVICABLE EXIT PLACARD IAW AMM 20-21-00-910-801.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 32,163 hrs · 29,628 cycles

SEAT RAIL SEGMENT ON RBL 9 AND BETWEEN FS 394 TO FS 409+112 CORRODED OUT OF LIMITS. FABRCIATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAIL AT FS 394 TO FS 409+112, RBL9 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRCIATED SEAT RAIL AT RBL 9 FS 304.00-FS 409+112 IAW AMM 53-01-11-400-802.

Part: HANDLE — LACK OF LUBE (RT OVERWING DOOR) · airframe 32,163 hrs · 29,628 cycles

RT OVERWING EMERGENCY EXIT HANDLE FAILS OPS FORCE CHECK. PERFORMED LUBRICATION OF THE RT OVERWING EMERGENCY EXIT HANDLE IAW AMM 12-20-52-640-802, FUNCTIONAL TEST OF HANDLE GOOD REF AMM 52-21-00-720-801.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 32,163 hrs · 29,628 cycles

DENT ON LT FLAP LOWER SKIN OTBD OF OTBD HINGE. REPAIRED IAW SRM 57-52-00 TO LT FLAP LWR SKIN OTBD OF OTBD HINGE AREA. RECEIVED AND COMPLIED WITH EC/TC EO 600-57-0476.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,163 hrs · 29,628 cycles

FWD FUSELAGE SKIN CRACKED AT LT FWD HYDRAULIC BAY DOOR SURROUND JUST BELOW LT AFT LATCH. REMOVED CRACKED SKIN AT LT FORWARD HYD BAY DOOR SURROUND IAW SRM 51-42-06 & 51-42-13. INSTALLED NEW SKIN AT LT FWD HYDRAULIC BAY IAW SRM 51-42-06 & 51-42-13 & DWG 600-37052. DRILLED NEW SKIN IAW SRM 51-40-11. RECEIVED REO 601R-53-11-2890. COMPLIED WITH REO 601R-53-11-2890. COMPLIED WITH EC/TC REO 601R-53-11-2090.

Part: ANGLE — CRACKED (BS 625) · airframe 32,163 hrs · 29,628 cycles

BS 625 ANGLE CRACKE. R & R THE ANGLE IAW SRM 51-42-21-00.

Part: SKIN — CRACKED (LT WING) · airframe 31,720 hrs · 29,227 cycles

CRACK FOUND AT LT LOWER WING PLANK WS 148.019 CRACK LENGTH IS .7170. COMPLIED WITH ECTC REO 601R-57-21-130 AND REO 601R-57-21-131. REMOVED UPPER AND LOWER PIE SKIN PANELS IAW SRM 51-42-06 AND 51-42-15 AND 511-42-21. INSTALLED PIE PANELS IAW SRM 51-41-02 AND 51-42-13 AND 57-42-21 IAW DWG 601E-10220 AND 601R-10219. COMPLIED WITH ECTC REO 601R-57-21-130. COMPLIED WITH ECTC REO 601R-57-21-131. UPON REMOVAL OF LT T/E PANEL FOUND JOINT STRAP AT WS 149.014 CRACKED. R & R JOINT STRAP IAW SRM 51-42-063. INSTALLED NEW WITNESS PIE PANEL IAW AMM 11-20-00-000-801.

Part: SKIN — CRACKED (RT WING) · airframe 31,720 hrs · 29,227 cycles

CRACK FOUND AT RT LOWER WING PLANK, WS 148.019. COMPLIED WITH ECTC REO 601R-57-21-130 01 AND REO 601R-57-21-131. REMOVED UPPER PIE PANEL IAW SRM 51-42-06 & 51-42-13. INSTALLED UPPER PIE PANEL IAW CRJ 200 SRM 51-42-06, 51-42-13. COMPLIED WITH ECTC REO 601R-57-21-130-01 AND REO 601R-57-21-130, REV K , DATED 11/27/2013 AS WRITTEN. COMPLIED WITH ECTC REO 601R-57-21-131 AND REO 601R-57-21-131, REV B , DATED 11/28/2013 AS WRITTEN. UPON REMOVAL OF RT T/E PANEL FOUND JOINT STRAP AT WS 148.019 CRACKED. R & R RT JOINT STRAP AT FS148.019 REF SRM 51-42-06. INSTALLED WRITTEN MARK ON PIE PANEL IAW AMM 11-20-00-000-801.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 30,082 hrs · 27,744 cycles

WARDROBE LOWER EMERGENCY LIGHT COVER MISSING. REPLACED WARDROBE LOWER EMERGENCY LIGHT LENS COVER IAW AMM 33-51-19.

Part: UNKNOWN — ODOR (PAX DOOR) · airframe 28,821 hrs · 26,521 cycles

PAX DOOR WILL NOT OPEN AND ELECTRICAL ODOR. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-08. OPS CHECK IS GOOD. PERFORMED INSPECTION OF DOOR ASSIST MOTOR IAW AMM 52-11-08. NO DEFECTS ARE NOTED AT THIS TIME, DOOR OPERATES CORRECTLY. ACFT IS OK FOR SERVICE.

Part: FUEL SYS — MALFUNCTIONED · airframe 28,522 hrs · 26,242 cycles

400 LB IMBALANCE DURING CLIMBOUT, LT TANK, DURING FLIGHT, LEFT TANK IMBALANCE INCREASED TO AROUND 900 LBS WITH PUMPS WORKING, FOLLOWED QRH, DIVERTED. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. PERFORMED OPS CHECK OF FUEL TRANSFER EJECTOR PUMP IAW AMM 28-13-01. PERFORMED OPS CHECK OF SCAVENGE EJECTOR PUMP IAW AMM 28-13-22, NO DEFECTS NOTED.

Part: CONNECTOR — CORRODED (EMERGENCY LIGHTS) · airframe 27,623 hrs · 25,351 cycles

CONNECTOR FOR LT FWD FUSELAGE EMERGENCY LIGHT IS CORRODED. R & R CONNECTOR IAW ESPM 20-17-10 AND WIRING DIAGRAM MANUAL 33-52-00. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,623 hrs · 25,351 cycles

FS 409+128, VERTICAL BEAM IS CRACKED AT RBL 36 INBD SIDE BOTTOM FASTENER HOLE. C/W REO 601R-53-41-189 AT INBD SIDE OF RBL 36, VERTICAL POST AT FS 409+128. C/W REO 601R-53-41-189 AT INBD SIDE OF RBL 36 VERTICAL POST AT FS 409+128. C/W EC/TC REO 601R-53-41-189 AND GREO 601R-53-41-189, REV B.

Part: BULKHEAD — UNKNOWN (BS 621) · airframe 27,623 hrs · 25,351 cycles

FS 621.00, BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, RBL 27.50. REQUIRES REPAIR. C/W REO 601R-53-61-5250, P1 AT RBL 27.5. ADDED WEIGHT OF REPAIR PARTS & FIELD FASTENERS IS 4.10 LBS. C/W REO 601R-53-61-5250, REV. RECEIVED AND VERIFIED FINAL REO 601R-53-61-5250, REV.

Part: VERTICAL BEAM — CRACKED (BS 409) · airframe 27,623 hrs · 25,351 cycles

FS 409+128, VERTICAL BEAM IS CRACKED AT RBL 27 INBD SIDE BOTTOM FASTENER HOLE. COMPLIED WITH EC/TC REO 601R-53-41-056 IAW REO 601R-53-41-056, REV F.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 27,623 hrs · 25,351 cycles

FS 621.00 BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 36.20. REQUIRES REPAIR. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO LBL 36.2 IAW REO 601R-53-61-5250 & REO 601R-53-61-5250.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 27,623 hrs · 25,351 cycles

FS 621 BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 9.50 REQUIRES REPAIR. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO LBL 9.50 IAW REO 601R-53-61-5250 & REO 601R-53-61-5250.

Part: ACCESS PANEL — CRACKED (WING) · airframe 27,623 hrs · 25,351 cycles

FUEL ACCESS PANEL 650EB HAS 2 INDICATIONS ON THE OTBD FWD & AFT SIDES 50 PERCENT FCH FAILED NDT. PERFORMED ROTOPEEN IAW SRM 51-24-11 IAW REO 601R-57-21-030, REV L.

Part: BULKHEAD — UNKNOWN (BS 621) · airframe 27,623 hrs · 25,351 cycles

FS 621.00 BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 18.00. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS AND FINAL REAMED ALL HOLES FOR REPAIR TO LBL 18 IAW REO:601R-53-61-5250. PERFORMED CUT ON BULKHEAD SPLICE IAW REO:601R-53-61-5250.

Part: SKIN — CRACKED (LT WING) · airframe 27,623 hrs · 25,351 cycles

FOUND LT AFT DRAIN VALVE HOLE INBD SIDE AFT LOWER PLANK BETWEEN STR 7 AND 5 MULTIPLE INDICATIONS APPROX .5" IN LENGTH 70 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EA 25-2014-113. EA 25-2014-113 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WC. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHROIZED RII INSPECTOR IAW GMM 3-3 PROCEDURES PRIOR TO THE ACFT BEING RETURNED TO SERVICE.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 27,623 hrs · 25,351 cycles

LEFT FUEL ACCESS PANEL 540DB HAS ONE INDICATION ON THE INBD SIDE 60 PERCENT FCH FAILED NDT. COMPLIED WITH REO 601R-57-21-030. PERFORMED ROTOPEEN IAW SRM 51-24-11 IAW REO 601R-57-21-030, REV L.

Part: BULKHEAD — UNKNOWN (BS 621) · airframe 27,623 hrs · 25,351 cycles

FS 621.00, BULKHEAD EXCEEDS LIMITATIONS OF REO 601R-53-61-1285, LBL 27.50 REQUIRES REPAIR. REMOVED ANGLE 601R36008-39, FS 621, BULKHEAD AFT SIDE LBL 27.50 IAW SRM 51-42-06 AND 51-42-21. INSTALLED ANGLE 601R36008-39 AFT SIDE OF FS 621, BULKHEAD LBL 27.50 IAW SRM 51-42-00 AND 51-42-21. PERFORMED CUTOUT OF BULKHEAD WEB IAW REO 601R-53-61-5250.

Part: ACCESS PANEL — CRACKED (WING) · airframe 27,623 hrs · 25,351 cycles

FUEL ACCESS PANEL 550DB HAS 1 INDICATIION ON THE FWD, INBD SIDE 50 PERCENT FCH FAILED NDT. PERFORMED ROTOPEEN IAW SRM 51-24-11 REO 601R-57-21-030, REV L.

Part: BULKHEAD WEB — CORRODED · airframe 27,623 hrs · 25,351 cycles

FOUND REAR PRESSURE BULKHEAD WEB, RBL 9.50, WL 103 HAS INDICATION NOTED APPROX 1.0" IN LENGTH, 50 PERCENT FSH, FAILED NDT INSPECTION. LOCATED AND DRILLED IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO RBL 9.5 IAW REO 601R-53-61-5250. PERFORMED CUTOUT OF BULKHEAD WEB IAW REO:601R-53-61-5250.

Part: BULKHEAD WEB — CRACKED · airframe 27,623 hrs · 25,351 cycles

FOUND REAR PRESSURE BULKHEAD WEB RBL 18.00, WL 107 HAS INDICATION NOTED APPROX 1.0" IN LENGTH, 50 PERCENT FSH, FAILED NDT INSPECTION. PERFORMED CUTOUT OF BULKHEAD WEB IAW REO: 601R-53-61-5250. COMPLIED WITH REO:601R-53-61-5250 IAW NDTM PT 1 51-20-06. C/W REO 601R-53-61-5250 AT RBL 18.

Part: BULKHEAD WEB — CRACKED · airframe 27,623 hrs · 25,350 cycles

FOUND REAR PRESSURE BULKHEAD WEB, RBL 36.20, WL 82-WL 85 HAS INDICATIONS NOTED APPROX 3.0" IN LENGTH, 70 PERCENT FSH, FAILED NDT INSPECTION. LOCATED AND DRILLED REPAIR IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS & FINAL REAMED ALL HOLES FOR REPAIR TO RBL 36.2 IAW REO 601R-53-61-5250. PERFORMED CUTOUT OF BULKHEAD WEB IAW STEP 1 OF REO:601R-5361-5250. COMPLIED WITH REO:601R53-61-5250 IAW NDTM PT 1, 51-20-06.

Part: BULKHEAD WEB — CRACKED · airframe 27,623 hrs · 25,351 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 112-WL 107.5 APPROX 4.5" IN LENGTH, 50 PERCENT FSH, FAILED NDT INSPECTION. REMOVED STIFFENER ANGLE FROM FS 621.00, BULKHEAD AT WL 120.43 IAW SRM 51-42-06. INSTALLED STIFFENER ANGLE IAW CJR 20, SRM 51-42-00 AND 51-42-22 AND 51-42-21. LOCATED AND DRILLED REPAIR ITEMS IAW REO 601R-53-61-5250. FABRICATED REMAINING PARTS AND FINAL REAMED ALL HOLES FOR REPAIR TO BL 0. IAW REO:601R-53-61-5250. PERFORMED CUTOUT OF BULKHEAD WEB IAW REO 601R-53-61-5250.

Part: BULKHEAD WEB — CRACKED · airframe 27,623 hrs · 25,351 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROXIMATELY .5" IN LENGTH, 100 PERCENT FSH, FAILED NDT INSPECTION. REMOVED CARGO COMPARTMENT DOOR FOR ACCESS IAW AMM 52-31-00-000-801. REMOVED AFT CARGO BALANCE SPRING BOX IAW AMM 52-31-08-000-801. REMOVED AFT CARGO DOOR TRACK AT FS 621.00 FOR ACCESS IAW SRM 51-42-06. REMOVED CARGO DOOR BALANCE SPRING MOUNT BRACKET IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 27,623 hrs · 25,350 cycles

CORROSION ON FLOORBEAM CAP AT FS 589.00, RBL 27. REMOVED DAMAGED CAP IAW SRM 51-42-06. INSTALLED CAP IAW SRM 51-40-11, 51-42-06 AND 51-42-15.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 27,623 hrs · 25,350 cycles

FS 621 PRESSURE BULKHEAD ISOLATOR LOCATED SECOND UP FROM BOTTOM AT RBL 9 IS CRACKED. REMOVED CRACKED ISOLATOR IAW SRM 51-42-13. INSTALLED NEW ISOLATOR IAW SRM 51-42-13.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 27,623 hrs · 25,350 cycles

STRINGER 3L FWD UPPER AND LOWER ATTACH ANGLES CRACKED JUST AFT OF FS 280 BULKHEAD. REMOVED 2 ATTACH ANGLES AT FS 280 STGR 3L IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW ATTACH ANGLES AT FS 280, STGR 3L IAW SRM 51-42-06 AND 51-42-02.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,623 hrs · 25,350 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED NEAR DOOR ASSIST PULLEY. REPAIRED IAW REO 601R-52-11-513 & EC/TC 601R-52-11-513 WITH PN 601R31772-5, MATERIAL.

Part: SKIN — CRACKED (WING) · airframe 27,623 hrs · 25,350 cycles

LOWER WING PLANK AT RT BOOST PUMP LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS. NOTED ON HORIZONTAL AND VERTICAL SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMERENCE. FAILED NDT INSP. COMPLIED WITH EA 26-2014-038. PERFORMED ROTO PEEN IAW SRM 51-24-11 & SURFACE FINISH OF 125RT IAW EA 26-2014-038.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 26,964 hrs · 24,694 cycles

DURING APPROACH, CAPTAIN`S SIDE WINDSCREEN BEGAN BURNING. SELECTED LT WINDSHIELD HEAT OFF BURNING STOPPED. R & R WINDSHIELD IAW AMM 56-11-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,706 hrs · 24,435 cycles

NR 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,591 hrs · 24,345 cycles

CABIN AFT MOST CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 25,939 hrs · 23,769 cycles

EMERGENCY EXIT LIGHT COVER AT MAIN CABIN DOOR BROKEN. RESECURED EMERGENCY LIGHT COVER AT CABIN DOOR IAW AMM 33-51-10. NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 24,577 hrs · 22,408 cycles

LOST ABOUT 5 PERCENT POWER IN LT ENGINE EVERY FEW SECONDS ON CLIMBOUT. ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED AS A PRECAUTION. PERFORMED ACCELERATION CHECK ON LT ENGINE, OPS CHECKED GOOD IAW AMM 71-00-00-710-802. ACFT OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 23,896 hrs · 21,691 cycles

SEVERAL AREAS OF CORROSION ALONG RT CARGO FLOOR SUPPORT FROM FS 559+80 TO 559+112 AROUND FASTENER HOLES. FOUND DAMAGE DEPTH TO BE APPROX 0.30 WHICH EXCEEDS 10 PERCENT OF LOCAL THICKNESS OF 0.063. REMOVED FLOOR SUPPORT IAW SRM 51-42-06. FABRICATED A NEW FLOOR SUPPORT IAW SNIEO 601R31133-S01 STEP 2. INSTALLED NEW FLOOR SUPPORT IAW SNIEO 601R31133-501.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,887 hrs · 21,680 cycles

FOUND THE RT FLOOR SILL TO HAVE ONE AREA OF CORROSION AT 559+30 TO 559+84 .4" X 1" X .015" DEEP. FOUND DAMAGE BEYOND REPAIRABLE LIMITS. REPAIRED IAW REO 601R-53-51-194.

Part: POST — CRACKED (BULKHEAD) · airframe 23,887 hrs · 21,680 cycles

BULKHEAD VERTICAL POST AT LBL 18 OTBD SIDE IS CRACKED IN RADIUS ON BOTTOM EDGE OF POST. REMOVED AIR FILTER FOR ACCESS IAW AMM 21-24-01-000-801. INSTALLED AIR FILTER IAW AMM 21-24-01-400-801. REMOVED AIR FILTER HSG BY REMOVING BOLTS, 8 EA FROM SUPPORT STRUCTURE TO ACCESS REPAIR. REINSTALLED AIR FILTER HSG BY INSTALLING BOLTS, 8 EA IAW SRM 51-41-04. REMOVED FS 409+128, LBL INBD & OTBD VERTICAL POSTS IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE INBD & OTBD VERTICAL POSTS AT FS 409+128, LBL 18 IAW SRM 51-42-06 AND REO 601R-53-41-889. ECTC REQUIRED. C/W ECTC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A. RII FOUND TO BE SATISFACTORY.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 23,887 hrs · 21,680 cycles

FS 409+128 BULKHEAD VERTICAL POST AT LBL 27 INBD SIDE IS CRACKED IN RADIUS ON BOTTOM EDGE OF POST. COMPLIED WITH STEPS 1 AND 2 OF REO 601R-53-41-056. STEPS 3-17 OF REO 601R-53-41-056, REQUIRE COMPLIANCE. COMPLIED WITH STEP 3 OF REO 601R-53-41-056, REV F. PERFORMED EDDY CURRENT OF FS 409+128 VERTICAL POST LBL 27 INBD SIDE REPAIR IAW NDTM 51-20-06. NO INDICATIONS NOTED AT THIS TIME. REMOVED PANEL 191BB FOR ACCESS IAW AMM TASK 53-85-01-000-803. OK TO CLOSE PANEL 191BB. INSTALLED PANEL 191BB IAW AMM TASK 53-82-01-400-803. COMPLIED WITH STEPS 4-17 OF REO 601R-53-41-056. COMPLIED WITH ECTC REO 601R-53-41-056 IAW REO 601R-53-41-056, REV F. RII FOUND TO BE SATISFACTORY: WVAC 1. (SDR CLOSED)

Part: ANGLE — CORRODED (PAX DOOR) · airframe 23,887 hrs · 21,680 cycles

CORROSION ON PAX DOOR LOWER SEAL ANGLE UPPER HALF AFT EDGE AND LOWER SEAL ANGLE AROUND FASTENER HOLES. PAX DOOR SILL CORROSION BEYOND LIMITS IAW SRM 51-21-06. REMOVED & LOCATED NEW PAX DOOR SILL PLATE IAW SRM 51-40-16.

Part: POST — CORRODED (BS 349 BULKHEAD) · airframe 23,887 hrs · 21,680 cycles

FS 349 BULKHEAD POST HEAVILY CORRODED. REMOVED AND REPLACED POST IAW SRM 51-42-21 & 51-42-06.

Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 23,887 hrs · 21,680 cycles

SERVICE DOOR ANGLE AT FS 319 IS CORRODED. R & R SVC DOOR ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-06 AND 51-41-02 .

Part: FLOOR SUPPORT — CORRODED (BS 310-333) · airframe 23,887 hrs · 21,680 cycles

CORROSION ON FLOOR SUPPORT AT RBL 9 FROM FS 310.00 TO FS 333.00. REMOVED CORROSION ON FLOOR SUPPORT, FOUND TO BE WITHIN LIMITS IAW REO 601R-53-00-005. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06 & REO 601R38778. STEP 2 OF REO 601R-53-00-005.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 23,887 hrs · 21,680 cycles

CORROSION ON SEAT TRACK FROM FS 364 TO 409. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 23,887 hrs · 21,680 cycles

CORROSION ON FLOOR SUPPORT, RBL27 FROM FS 559+112 TO FS 621.0. REMOVED FLOOR SUPPORT IAW SRM 51-41-02. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-11.

Part: FRAME — CORRODED (BS 33) · airframe 23,887 hrs · 21,680 cycles

FRAME AT FS 33.00 HEAVILY CORRODED. REMOVED AND REPLACED FRAME SECTION IAW SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,887 hrs · 21,680 cycles

SEAT TRACK AFT OF FS 559, RBL 9 CORRODED IN AND AROUND SCREW HOLES. R & R DAMAGED FLOOR SEAT TRACK FROM FS 559+4 TO 559+88, RBL 9 IAW MM TASKS 53-01-11-000-802 AND 53-01-11-400-802. (SDR CLOSED)

Part: ANGLE — CORRODED (DOOR SILL) · airframe 23,896 hrs · 21,691 cycles

CORROSION ON SERVICE DOOR LOWER SILL ANGLE FWD EDGE. REMOVED SERVICE DOOR LOWER SILL ANGLE, FOUND TO BE OUT OF LIMITS IAW SRM 51-42-06 & 51-42-21, 53-00-00. S DRILLED, LOCATED AND INSTALLED NEW SILL ANGLE, IAW SRM 51-40-11.

Part: FRAME — CORRODED (BS 364) · airframe 23,896 hrs · 21,691 cycles

FRAME AT FS 364.00 IS HEAVILY CORRODED. REMOVED FS 364.00 FRAME IAW SRM 51-42-06 AND 51-42-21. DRILLED UP NEW FRAME IAW SRM 51-40-11. INSTALLED NEW FRAME IAW SRM 51-42-06 & 51-41-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,887 hrs · 21,680 cycles

SEAT TRACK AT LBL 9 JUST AFT OF 559 CORRODED IN AND AROUND SCREW HOLE. R & R DAMAGED FLOOR SEAT TRACK FROM FS 559+4 TO 559+88, LBL 9, IAW MM TASKS 53-01-11-000-802 AND 53-01-11-400-802. (SDR CLOSED)

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,887 hrs · 21,680 cycles

CORROSION ON CARGO SEAT TRACK AT FS 559+80 AT RBL9. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-61-49-01. REMOVED AND INSTALLED CORRODED SEAT TRACK IAW 52-41-02-00 SRM .

Part: ANGLE — CRACKED (NLG WW) · airframe 23,888 hrs · 21,682 cycles

VERTICAL ANGLE ON LT SIDE OF NLG WHEEL WELL INTERNAL BOX STRUCTURE BETWEEN FS 202.75 AND 235.00 IS CRACKED AT THE TOP BETWEEN (2) RIVETS. DAMAGE IS APPROX 1 INCH LONG. REMOVED CRACKED ANGLE IAW SRM 51-42-06 & 51-42-21. DRILLED NEW SERVICEABLE ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: ANGLE — CRACKED (BS 621-625) · airframe 23,887 hrs · 21,680 cycles

RT FS 621-625 OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED RT FS 621-625 OBLIQUE ANGLE AND REPLACED WITH NEW PARTS IAW SRM 51-40-11 AND 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,887 hrs · 21,680 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED APPROX 2" LONG, JUST ABOVE PWR ASSIST PULLEY BRACKET. REMOVED PAX DOOR AFT DRAG ANGLE, LOCATED AND DRILLED UP NEW ANGLE PN 601R31772-5S AND INSTALLED IAW SRM 51-42-06 AND SRM 51-40-11. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 23,887 hrs · 21,680 cycles

CLIP CRACKED AT FS 280.00, RBL 9. R & R CLIP AT FS 280.00, RBL 9 IAW SRM 5J1-42-21.

Part: ANGLE — CRACKED (BS 280) · airframe 23,887 hrs · 21,680 cycles

ANGLE CRACKED AT FS 280.00, RBL 9. R & R ANGLE AT FS 280.00, RBL 9 IAW IAW SRM 5J1-42-21. T

Part: WEB — CRACKED (PAX DOOR) · airframe 23,887 hrs · 21,680 cycles

PASSENGER DOOR AFT STAIR WEB CRACKED AT 3RD STEP FROM TOP JUST INBD OF GAS STRUT SUPPORT BRACKET. INSTALLED GAS STRUT SUPPORT BRACKET ASSY ONTO AFT WEB ASSY ONTO PAX DOOR IAW SRM 51-42-06. REMOVED HANDRAIL STOP CUP FROM AFT WEB TO GAIN ACCESS FOR REPAIR. INSTALLED HANDRAIL STOP CUP ONTO AFT WEB ONTO PAX DOOR IAW SRM 51-42-21. REPAIRED CRACKED AFT WEB ASSY AT 3RD STEP JUST INBD OF GAS STRUT SUPPORT BRACKET IAW REO 601R-52-11-702. REQ'S FILLET SEAL & PAINT AROUND REPAIR AREA. SEALED AREA AROUND WEB IAW SRM 51-23-00. PAINTED REPAIRED AREA IAW SRM 200 51-25-01 AS DIRECTED BY 601R-52-11-702, REV C. EC/TC REQ'D FOR REO 601R-52-11-702. C/W EC/TC REO 601R-52-11-702 AND MET ALL THE REQUIREMENTS OF REO 601R-52-11-702, REV C. RII FOUND TO BE SATISFACTORY.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 23,888 hrs · 21,682 cycles

RT AFT PHOTOLUMINESCENT AISLE PATH MARKER IS MISSING THE CHEVRON MARKER. INSTALLED NEW SERVICEABLE CHEVRON MARKER IAW AMM 33-51-01-400-806. (SDR CLOSED)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,421 hrs · 21,157 cycles

F/O FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,156 hrs · 20,851 cycles

NR 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,441 hrs · 20,095 cycles

FWD RT WING EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 22,441 hrs · 20,095 cycles

DURING POST FLIGHT, FOUND COVER TO FWD RT WING EMERGENCY LIGHT MISSING. REPLACED RT SIDE OVER WING FWD EMERGENCY LIGHT LENS COVER IAW AMM 33-51-21.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 22,173 hrs · 19,807 cycles

EXIT SIGN BROKEN. R & R EMERGENCY EXIT SIGN LENS COVER, CHECKS GOODS. AMM 33-51-13. DEFER CLEARED, MX NOTIFIED.

Part: SIGN — CRACKED (CABIN) · airframe 22,173 hrs · 19,807 cycles

F/A TRIPPED INTO GALLEY SERVICE DOOR, KNOCKING OFF EXIT SIGN. SIGN FELL AND CRACKED, WILL NOT STAY IN PLACE. (LIGHT LENS/ COVERS (INCLUDING EMERGENCY LIGHT) (INCLUDING EMERGENCY LIGHT) ) R & R EMER EXIT SIGN LENS COVER, CHECKS GOODS. AMM 33-51-13. DEFER CLEARED, MX NOTIFIED. (CLOSED)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 21,815 hrs · 19,414 cycles

NR1 & NR2 EXTERIOR AND NR1 INTERIOR CEILING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04, OP'S CHECK GOOD. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04, OP'S CHECK GOOD.

Part: FIRE BOTTLE — INOPERATIVE (CARGO BAY) · airframe 21,652 hrs · 19,228 cycles

CARGO BRL LO MSG INFLIGHT. (NOTE THIS IS THE 2ND TIME THIS ACFT HAS HAD THIS DISCREPENCY IN 2 DAYS) QRH COMPLIED WITH, LANDED AT NEAREST SUITABLE AIPORT. (ENROUTE, ACFT DIVERTED, DUE TO MX -- EMERGENCY DECLARED) REMOVED BOTH CARGO BOTTLES AND INSTALLED SERVICABLE BOTTLES IAW AMM 26-25-01. OPS CHECK GOOD.

Part: CONTROL UNIT — FAILED (PFD) · airframe 21,077 hrs · 18,580 cycles

REPEAT WRITE-UP ENROTE FO'S PFD , MFD FLIGHT DIRECTOR, NAV2 AUTOPILOT WERE ALL LOST AND WENT BLANK MULTIPLE TIMES ALSO, CAPTAINS FLIGHT DIRECTOR WAS LOST DC TIE 1 CLOSED AT ONE POINT. NOTICED A DC BUS 2 MSG ALSO, BUT IT EXTINGUISHED ITSELF (ENROUTE, ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED) R & R BROKEN CB AT CB2 E11 IAW ESPM CRJ200 20-23-00. OPS TAST GOOD. ALSO, R & R GEN1 GCU ASSY IAW AMM 24-11-07. OPS CHECKED GOOD IAW AMM 24-11-01.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 20,330 hrs · 17,712 cycles

GALLEY SERVICE DOOR FLOOR EMERGENCY EXIT SIGN LIGHT COVER MISSING. (RESOLVED ON W/O: 168315/ TASKCARD: N/R-00004) REPLACED GALLEY SERVICE DOOR FLOOR EMERGENCY FLOOD LIGHT COVER IAW CMM 33-21-58. REPLACED GALLEY SERVICE DOOR FLOOR EMERGENCY FLOOD LIGHT COVER IAW CMM 33-21-58. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,524 hrs · 16,806 cycles

NR 4 CEILING EMERGENCY FLOOD LIGHT INOP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,524 hrs · 16,806 cycles

LT NR 1 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 19,291 hrs · 16,531 cycles

FLOORBEAM CAP HAS CORROSION AROUND NUTPLATE HOLES FS 589 TO FS 621 LBL 27.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 19,291 hrs · 16,531 cycles

CARGO FLOOR SUPPORT AT LBL 45 HAS CORROSION FS 574 TO FS 621 AND SEVERAL GOUGES AT FS 589 LARGEST .700"L X .300"W X .018" DEEP APPROX.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 19,291 hrs · 16,531 cycles

WIRE PULLED OUT OF EMERGENCY EXIT LIGHT ELECTRICAL CONNECTOR ON WARDROBE.

Part: INTERCOSTAL — CRACKED (BS 640) · airframe 19,291 hrs · 16,531 cycles

INTERCOSTAL AT RBL 18 CRACKED IN RADIUS ON LWR AFT FLANGE AT FS 640 BETWEEN WL 119.12 AND WL 111.09.

Part: SKIN — CRACKED (WING) · airframe 19,291 hrs · 16,531 cycles

INDICATIONS NOTED AT LWR WING PLANK ACCESS HOLE, 640DB AT INBD ON PAINTED AREA OF HOLE APPROX 50 PERCENT FULLSCREEN HEIGHT ARE MARKED ON WING. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G.

Part: SUPPORT BEAM — CRACKED (CARGO DOORWAY) · airframe 19,291 hrs · 16,531 cycles

CARGO DOOR SUPPORT BEAM LWR AFT ANGLE IS CRACKED APPROX .5" IN LENGTH. REMOVED CRACKED ANGLE AT CARGO DOOR SUPPORT BEAM LWR AFT, BY REMOVING (7EA) LOCK FASTENERS (4EA) COMMON TO BEAM (3EA) COMMON TO BULKHEAD. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-42-21 FIG 8. INSTALLED IAW SRM 51-42-21, FIG 10 AND FIG 11.

Part: BULKHEAD — CRACKED · airframe 19,291 hrs · 16,531 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.

Part: POST — CRACKED (BS 409) · airframe 19,291 hrs · 16,531 cycles

FOUND FS 409.0+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED AT WL 69 AFT FLANGE RADIUS APPROX .2" IN LENGTH 605 FSH FAILED NDT INSP. REMOVED POST ASSY IAW SRM 51-42-06 AND 51-42-21. POST ASSY INSTALLED AND NEW STIFFNERS IAW REO 601R-53-41-1125 COMPLIED WITH EC/TC REO 601R-53-41-1125 IAW REO 601R-53-41-1125.

Part: POST — CRACKED (BS 409) · airframe 19,291 hrs · 16,531 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18 OTBD SIDE HAS INDICATION NOTED AT WL 69.0 AFT FLANGE RADIUS APPROX .2" IN LENGTH 60 PERCENT FSH FAILED NDT INSP. REMOVED POST IAW SRM 51-42-06. LOCATED AND ASSEMBLED NEW SERVICEABLE OTBD STIFFNEER IAW SRM 51-40-11 & 51-42-06. INSTALLED SERVICEABLE POST IAW REO NR 601R-53-41-889. EDGE SEALED AND PAINTED POST IAW SRM 51-25-16 AND 51-23-20. COMPLIED WITH EC/TC REO 601R-53-41-88A COMPLIED WITH EC/TC RIL NR 1844 IAW RIL NR 1844A.

Part: ANGLE — CRACKED (BS 625) · airframe 19,291 hrs · 16,531 cycles

RT 625 OBLIQUE ANGLE IS CRACKED.

Part: BULKHEAD — CRACKED (BS 559) · airframe 19,291 hrs · 16,531 cycles

FOUND F.S. 559 RT SIDE BULKHEAD WEB HAS 2 INDICATIONS NOTED. C/W EC/TC 601R-53-41-260 IAW REO 601R-53-41-260 REV D.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 19,291 hrs · 16,531 cycles

TRACK SEGMENTS IN THE CARGO BAY ARE CORRODED. REPAIRS MADE IAW SRM 51-41-02, STEP 1(A), SRM 53-61-49, SRM 53-61-49 AND AMM 20-21-00-910-801 STEPS 2A. A-B AND STEP 3A 1-6, IAW AMM 20-21-00-910-801 STEP 2A(1A).

Part: PLATE — CORRODED (DOOR STEP) · airframe 19,291 hrs · 16,531 cycles

SERVICE DOOR STEP PLATE HAS CORROSION UNDER SCREW HOLE APPROX .040" THICK AT EDGE OF 1 HOLE.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,291 hrs · 16,531 cycles

JOB 8761611 OPERATION 178 / PAX DOOR AFT DRAG ANGLE IS CRACKED AT DOOR ASSIST PULLEY BRACKET.

Part: PLACARD — TORN (PAX DOOR) · airframe 19,291 hrs · 16,531 cycles

JOB 8761611, OPERATION 185 / PAX DOOR STEP 832BT EXIT PLACARD IS TORN.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 19,291 hrs · 16,531 cycles

JOB 8761611, OPERATION 142 / STRUCTURE AT CREW ESCAPE HATCH LT HINGE CUTOUT ON FUSELAGE FS 276.0 IS CRACKED AT RADIUS OF CUTOUT.

Part: DOOR — STIFF (ASD) · airframe 18,701 hrs · 15,882 cycles

ASD HARD TO CLOSE / OPEN. FLT 5383 DEL 63 MINS.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 17,970 hrs · 15,176 cycles

FLT 5342 - FLAP FAIL ON APPROACH INTO EVV FLAPS UP POSITION.

Part: FLAP — FAILED (WING) · airframe 15,429 hrs · 12,894 cycles

FLAP FAIL AT 0 DURING APPROACH. EN ROUTE TO PVD A/C DIVERTED TO BOS DUE TO MTC. EMERGENCY DECLARED.

Part: SEAL — CRACKED (PAX DOOR) · airframe 15,367 hrs · 12,854 cycles

SMALL CRACK IN FUSELAGE WHERE BOARDING DOOR SEALS. LOWER RIGHT CORNER OF FUSELAGE. REMOVED AND REPLACED PAX DOOR SEAL REF AMM 52-11-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,367 hrs · 12,854 cycles

LT EMERGENCY LIGHT BURNED OUT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,006 hrs · 12,564 cycles

EMERGENCY EXIT LIGHT ON WARDROBE HAS 1 BULB INOP.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,006 hrs · 12,564 cycles

CABIN EMERGENCY EXITS LIGHTS HAS 1 BULB INOP.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 14,978 hrs · 12,546 cycles

RIGHT WING FLOOR EMERGENCY EXIT LIGHT INOP. REMOVED INOP. RT WING FLOOR EMERGENCY EXIT LIGHT AND INSTALLED SERVICEABLE LIGHT P/N 5020-5 IAW CRJ 200 33-51-10. REQUIRES OPS CHECK. OPS CHECK GOOD IAW CRJ 200 AMM 33-51-01.

Part: FITTING — CORRODED · airframe 14,978 hrs · 12,546 cycles

HORIZ TAB ANTI ROTATION FITTING CORRODED.

Part: HINGE FITTING — CRACKED (ESCAPE HATCH) · airframe 14,978 hrs · 12,546 cycles

RT HINGE CRACKED ON CREW ESCAPE HATCH. REMOVED CRACKED RT. HINGE FITTING ON CREW ESCAPE HATCH AND REPLACED WITH NEW SERVICEABLE HINGE FITTING P/N 600-33217-1001 IAW CRJ AMM 20-21-00. PAINTED RT. HINGE FITTING IAW CRJ SRM 51-25-16. REFER TO W/C 50246/2000/0005 FOR OPS CHECK.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 14,978 hrs · 12,546 cycles

FS 280 FWD FLOOR SUPPORT IS CRACKED I/B OF RBL 9. INSTALLED NEW ANGLE IAW SRM 51-42-06.

Part: WEB — CRACKED (BS 280) · airframe 14,978 hrs · 12,546 cycles

FS 280 WEB UNDER LBL 9 IS CRACKED UNDER THE PARKING BRAKE CABLE FITTING. REPAIRED CRACKED AREA OF FS 280.00 WEB UNDER LBL 9.00 REQUIRES FILLET SEAL/TOPCOAT FILLET SEALED IAW CRJ MM 51-23-00. REAPPLIED TOPCOATED IAW CRJ SRM 51-25-16 ALL WORK ACCOMPLISHED IAW REO 601R-53-11-171 COMPLIED W/ ASA EO600-53-90.

Part: DOOR FRAME — CRACKED (ESCAPE HATCH) · airframe 14,978 hrs · 12,546 cycles

CREW ESCAPE HATCH FRAME AT FS 276.00 HAS CRACK AT LBL 8.5 FROM CREW ESCAPE HATCH HINGE ARM. REPAIRED IAW REO 601R-53-11-1296. COMPLIED WITH ASA EC/TC REO 601R-53-11-1296.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,978 hrs · 12,546 cycles

RIGHT SIDE INBOARD BATHTUB FITTING CRACKED, RESOLVED ON W/O: 75508 TASKCARD: N/R-00108. REMOVED CRACKED RT INBOARD BATHTUB FITTING. LOCATED SERVICEABLE FITTING P/N 600-3106-19 IAW CRJ SRM 51-40-11. OK TO INSTALL. INSTALLED NEW SERVICEABLE FITTING IAW CRJ SRM 51-42-21. OK TO TOPCOAT FASTENERS. AAR 349. APPLIED TOPCOAT TO FASTENERS PER CRJ 200 SRM 51-21-16.

Part: HINGE — CORRODED (AILERONS) · airframe 14,978 hrs · 12,546 cycles

OUTBOARD RT AILERON WING ATTACH HINGE CORRODED, TOP OF WING HINGE. AFTER FURTHER INVESTIGATION, THE DAMAGE ON THE OUTBOARD RT AILERON WING ATTACH HINGE HAS MINOR SURFACE CORROSION. REMOVED SURFACE CORROSION IAW CRJ 200 SRM 51-21-06. APPLIED PROTECTIVE FINISH TO REPAIR AREA IAW CRJ 200 SRM 51-25-16.

Part: STEP — CRACKED (PAX DOOR) · airframe 14,978 hrs · 12,546 cycles

PAX DOOR TOP STEP CRACKED ON THE AFT SIDE. REPAIRED IAW REO 601R-52-11-1401. COMPLIED WITH EO 600-52-43 NO DEFECTS NOTED.

Part: ANGLE — CRACKED (BS 280) · airframe 14,978 hrs · 12,546 cycles

FS 280 LBL 9 I/B AND O/B ANGLES ARE CRACKED. DUPLICATED NEW CLIPS. INSTALLED IAW REO 601R-53-11-171. COMPLIED WITH ASA EO 600-53-0090 RII 5000528.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 14,978 hrs · 12,546 cycles

PAX DOOR FWD SUPPORT CRACKED UNDER STEP 832CT. COMPLIED WITH REO 601R-52-11-702 FOR REPAIR OF PAX DOOR FWD SUPPORT UNDER STEP 832CT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,978 hrs · 12,546 cycles

AAR-2069 - LEFT O/B 484 I/B CLIP CRACKED, RESOLVED ON W/O: 75508 TASKCARD: N/R-00107. REMOVED DAMAGED CLIP AT 484 LEFT O/B - I/B CLIP AND FABRICATED NEW PART FROM 2024T3.063 IAW REO 601R-53-41-059. (13225) 12-4-07. AAR-338. CLIP REQUIRES NOT PERFORMED LPI ON FABRICATED CLIP FOR LT O/B 484 I/B SIDE IAW REO 601R-53-41-059 AND NDTM 51-20-08. NO DEFECTS NOTED (13311) 12-4-07. AAR-338. INSTALLED CLIP IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 280) · airframe 14,978 hrs · 12,546 cycles

FS 280 UPPER AFT ANGLE IS CRACKED O/B OF LBL 9. REPAIRED UPPER AFT ANGLE F.S. 280.00 O/B OF LBL 9.00 IAW REO 601R-53-11-138 REQUIRES FILLET SEAL / TOPCOAT. FILLET SEALED. IAW SRM 51-23-00 AND TOPCOATED. IAW SRM 51-25-16.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 14,978 hrs · 12,546 cycles

PAX DOOR OUTER HANDLE IS CRACKED. REMOVED CRACKED UNSERVICEABLE OUTER HANDLE ASSY IAW AMM 52-11-03. OBTAINED NEW SERVICEABLE OUTER HANDLE ASSY PN 601R31704-7. INSTALLED NEW SERVICEABLE HANDLE ASSY PN 601R31704-7, PERFORMED FUNCTIONAL TEST OF PAX-DOOR OUTER HANDLE AS PER CRJ 200 AMM 52-11-03. NO-DEFECTS. PERFORMED OPERATIONAL TEST OF PAX-DOOR OUTER HANDLE AS PER AMM 52-11-03, NO DEFECTS.

Part: TRACK — CRACKED (THRUST REVERSER) · airframe 14,978 hrs · 12,546 cycles

LT ENG T/R BOTTOM O/B TRACK CRACKED CLOSE TO MOUNTING BOLT. REMOVED UNSERVICEABLE LT ENGINE T/R BOTTOM O/B TRACK IAW SHORTS CMM 78-30-00-040-002-A01. INSTALLED NUTPLATES P/N MS21059L3 AND MS 21061L3 USING MS 20426AD3 RIVETS ON NEW SERVICEABLE TRACK ASSY P/N 228-50809-803 IAW CRJ 200 SRM 51-45-00. OK TO INSTALL. INSTALLED LT ENGINE T/R BOTTOM O/B TRACK IAW SHORTS CMM 78-30-440-010-A01. REFER TO FORM 409D FOR OPERATIONAL CHECK. TRACK INSTALLATION .

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,978 hrs · 12,546 cycles

FS 280 RBL 9 INBOARD AND OUTBOARD ANGLES ARE CRACKED. REMOVED INBOARD/OUTBOARD CLIPS AT FS 280.00 RBL 9.00 DISCARDED DUPLICATED NEW CLIPS. INSTALLED IAW REO 601R-53-11-171 9, REQUIRES FILLET SEAL/TOPCOAT. FILLET SEALED IAW 51-23-00 AND TOPCOATED IAW 51-25-16. FOUND TWO CLIP NUTS MISSING AND INSTALLED TWO SERVICEABLE CLIP NUTS, COMPLIED WITH ASA EO 600-53-90 RII 5000528.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 14,906 hrs · 12,484 cycles

LEFT FWD EXTERIOR EMERGENCY OVERWING EXIT LIGHT INOP.

Part: WARNING LIGHT — ILLUMINATED (ENGINE OIL) · airframe 14,530 hrs · 12,151 cycles

LEFT ENGINE LOW OIL PRESSURE MSG IN FLIGHT AT FL 310, OIL PRESSURE DROPPED TO 0 PSI. C\W QRH, LANDED WITHOUT EVENT. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,648 hrs · 11,453 cycles

LEFT EMERGENCY EXIT LIGHT FWD OF PAX DOOR IS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,456 hrs · 11,306 cycles

LEFT FUSELAGE FWD EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,338 hrs · 11,204 cycles

SECOND FROM AFT CEILING EMERGENCY LIGHT INOP.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,317 hrs · 11,179 cycles

EMERGENCY LIGHTS TURNED ON INTERMITTENTLY DURING FLIGHT.

Part: LIGHT — INOPERATIVE · airframe 13,108 hrs · 10,975 cycles

THE 2ND FROM AFT RIGHT EXTERNAL EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,025 hrs · 10,904 cycles

CEILING EMERGENCY LIGHT 1EA INOP.

Part: DOOR — STUCK (MAIN PAX) · airframe 12,955 hrs · 10,842 cycles

PAX DOOR WILL NOT CLOSE, FLT 4836 DEL 120 MINS.

Part: WARNING MESSAGE — ILLUMINATED · airframe 12,737 hrs · 10,686 cycles

RECEIVED NWS MSG IN FLIGHT. TOWER DECLARED AN EMERGENCY. FLT 4159 DEL 30 MINS.

Part: UNKNOWN — UNKNOWN (MLG) · airframe 11,674 hrs · 9,873 cycles

ON T/O ROLL OUT AT APPROX 110KNTS, ALL THREE FLT CREW HEARD A METAL TYPE SCRAPPING NOISE FROM UNDER AIRCRAFT AT 150 KNOTS(V1) NOTICED A STAGNATION IN AIRSPEED AND SLIGHT SHIMMING. SUSPECT MAIN GEAR BURST, FLTS 4423,4522 CX.

Part: PLACARD — DAMAGED (AIRSTAIR DOOR) · airframe 11,472 hrs · 9,706 cycles

EXIT PLACARD MARRED ON AIRSTAIR DOOR.

Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 11,309 hrs · 9,580 cycles

AFTER T/O IN JAN RECEIVED "STEERING INOP" CAUTION MSG, COMPLIED W/QRH UNEVENTFUL LANDING AND TOW IN TO GATE.

Part: PANEL — CORRODED (LT WING) · airframe 11,212 hrs · 9,503 cycles

LT WING FUEL PANEL 540EB HAS SURFACE CORROSION WITH PITTING, NEEDS INVESTIGATION.

Part: FRAME — CORRODED (STEP) · airframe 11,212 hrs · 9,503 cycles

FOUND PAX DOOR FRAME UNDER STEP IS CORRODED. SURFACE CORROSION FOUND TO BE WITHIN LIMITS IAW CRJ SRM 51-21-00. REMOVED CORROSION IAW CRJ SRM 51-21-06. OK TO PRIME AND PAINT. TREATED, PRIMED AND APPLIED TOPCOAT IAW CRJ SRM 51-21-11, 51-25-06 AND 51-25-16. (CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 11,212 hrs · 9,503 cycles

FOUND PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED CRACKED SECTION OF PAX DOOR AFT DRAG ANGLE. NDT PERFORMED ON W/C295. FABRICATED REPAIR DETAILS FROM 601R31907-301S IAW REO 601R-52-11-513. OK TO INSTALL. INSTALLED REPAIR DETAILS IAW REO 601R-52-11-513. (CLOSED)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 11,212 hrs · 9,503 cycles

EMERGENCY LIGHT STRIP OVER LAY NR 12 INOP. FOUND EMERGENCY LIGHT STRIP NR 12 OVERLAY TO BE IMPROPERLY CONNECTED. RECONNECTED AND PERFORMED OPS CHECK AND FOUND TO BE IN SERVICEABLE CONDITION IAW CRJ MM 33-53-01.RB732. (CLOSED)

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A GROUND INSPECTION IN MGM, THE EXTERIOR EMERGENCY LIGHT, ABOVE THE RIGHT WING, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EXTERIOR EMERGENCY LIGHT, ABOVE THE RIGHT WING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

FLT 4460 - DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR LOWER STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP. OPERATIONAL CHECKS GOOD. (M)

Part: LANDING GEAR — VIBRATION (NOSE)

FLT 4300 - DURING THE TAKEOFF ROLL FROM ATW-ATL, AT APPROXIMATELY 130 KTS THE AIRCRAFT EXPERIENCED A LOUD SHIMMY FROM THE NOSE WHEEL AREA. THE CREW NOTIFIED THE ATW TOWER AFTER TAKEOFF AND REQUESTED A RUNWAY SWEEP. PIECES OF TIRE WERE FOUND AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT CONTINUED TO ATL AND LANDED SAFELY. MAINTENANCE INSPECTED THE NOSE GEAR, DOOR, FUSELAGE AND AXLES WITH NO DAMAGES NOTED. MAINTENANCE REMOVED AND REPACED BOTH NOSE TIRE WHEEL ASSEMBLIES. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PLATE — CRACKED (FUSELAGE) · airframe 7,367 hrs

DURING A C-CHECK, THE CARGO BAY FLOOR SILL AT FS 562.72-FS 589.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO BAY FLOOR SILL AT FS 562.72- FS 589.00 IAW EO 600-53-0095.

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT LOWER ENGINE SUPPORT BEAMS AT BL 36.20 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT AND RT LOWER ENGINE SUPPORT BEAMS AT BL 36.20 IAW EO 600-53-0070.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 7,367 hrs

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 EO 600-53-0105.

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT AND RT FS 625 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT AND RT FS625 CLIP.

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW EO 600-53-0072.

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,376 hrs

DURING A C-CHECK, THE CLIPS AT FS 484, LBL 36 AND RBL 36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL 36, RBL36 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CLIPS AT FS 484, LBL36 AND RBL 36 IAW EO 600-53-0098.

Part: STRUCTURE — CRACKED (EMERGENCY LIGHT)

DURING C-CHECK, THE EMERGENCY EXIT LIGHT NEAR THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY NEAR THE SERVICE DOOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4512 - DURING A GROUND INSPECTION IN BTR, THE LOWER LEFT EMERGENCY EXIT LIGHT NEAR THE PASSENGER DOOR WAS FOUND WITH SEVERAL LAMPS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE LOWER LEFT EMERGENCY EXIT LIGHT NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: TRIM PANEL — STUCK (STAB)

DURING TAKEOFF, AT APPROXIMATELY 800 FEET THE STAB TRIM AND MACH TRIM DISENGAGED AND THE CREW RE-ENGAGED THEM. WHILE CLIMBING THROUGH 14,00 FEET WITH THE AUTOPILOT ON, STAB TRIM AND MACH TRIM MESSAGES APPEARED AND THEY DISENGAGED AGAIN. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED BY THE TOWER. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED SAFELY WITH THE FLAPS SELECTED AT 45 DEGREES. MAINTENANCE FOUND THE STAB TRIM PANEL CHANNEL 1 BUTTON STUCK PARTIALLY IN AND REMOVED AND REPLACED THE STAB TRIM PANEL. SYSTEM BITE TEST AND OPS CHECK WERE PERFORMED WITH NO DISCREPANCIES NOTED. AIRCRAFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGNECY LIGHT)

FLT 4382 - DURING A GROUND INSPECTION IN MGM, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS BATTERY PACKS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — DETACHED (CABIN FLOOR)

DURING A GROUND INSPECTION IN DFW, AN EMERGENCY FLOOR LIGHTING STRIP WAS FOUND DETACHED. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHTING STRIP. OPERATIONAL CEHCKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (OVERWING EXIT)

FLT 4219 - DURING A GROUND INSPECTION IN DFW, THE FORWARD TWO EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE FORWARD TWO EXTERIOR OVERWING EMERGENCY EXIT LIGHTS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4713 - DURING A GROUND INSPECTION IN DFW, THE AFT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CABLE — BINDING (PAX DOOR)

FLT 4520 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR PRESSURE VALVE CABLE ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OF FOR SERVICE. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

FLT 4694 - DURING A GROUND INSPECTION IN DFW, THE AFT SECTION OF THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE-CONNECTED THE AFT SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (CABIN)

FLT 4414 - DURING A GROUND INSPECTION AT MGM, THE NR 1 EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)