N978EV

Part: LIGHT — BROKEN (CABIN) · airframe 23,401 hrs · 21,785 cycles

EMERGENCY EXIT LIGHT ON LOWER WALL NEAR PASSENGER DOOR IS BROKEN & NOT WORKING. R & R EMERGENCY EXIT FLOOR LEVEL FLOOD LIGHT BASE FRAME IAW 33-51-19, OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 21,764 hrs · 20,103 cycles

BACKSIDE OF CEILING CABIN EMERGENCY EXIT SIGN IS MISSING. TROUBLESHOT EMERGENCY LIGHT, INSTALLED LENS. OP CHECKED OK IAW AMM 33-51-01.

Part: ANGLE — CRACKED (BS 589) · airframe 21,481 hrs · 19,830 cycles

WHILE REMOVING CARGO DOOR SILL PLATE FOR REPLACEMENT, FOUND CRACKED ANGLE AT FS 589.0, LBL 37 UNDER SILL PLATE. R & R ANGLE WITH NEW AND SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,481 hrs · 19,830 cycles

LEFT SIDE SEAT TRACK AFT SEGMENT IS CORRODED BEYOND LIMITS. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV A DATED 11/18/2011.

Part: ANGLE — CRACKED (BS 621-625) · airframe 21,481 hrs · 19,830 cycles

LEFT AND RT OBLIQUE ANGLES AT FS 621.0 TO 625.3 WL 90 ARE CRACKED AT RADIUS. REMOVED DAMAGED LT AND RT OBLIQUE ANGLES AND INSTALLED NEW ANGLES, IAW SRM 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 21,481 hrs · 19,830 cycles

INTERCOSTAL BRACKET, IS CRACKED WHERE IT ATTACHES TO FUSELAGE SKIN, LOCATED BETWEEN FS 621.0 AND 625.3 WL 100.0, LT SIDE. CRACK IS APPROX 1.0" LONG AT RADIUS. R & R INTERCOSTAL, WITH SERVICEABLE PART IAW SRM 51-42-06 & 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 21,481 hrs · 19,830 cycles

CARGO FLOOR SUPPORT FS 574.00 TO FS 621.00 LT SIDE IS CORRODED SEVERAL AREAS. REMOVED LT CORRODED CARGO FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE CARGO DOOR FLOOR SUPPORT IAW SRM 51-42-06 & 51-42-21 AND REO 601R-53-61-1574.

Part: ATTACH ANGLE — CRACKED (PAX DOOR HANDLE) · airframe 21,481 hrs · 19,830 cycles

AFT ATTACHMENT ANGLE AT INNER PAX DOOR HANDLE BOX MOUNTING STRUCTURE IS CRACKED AT LOWER FASTENER HOLES. REMOVED AFT ATTACHMENT ANGLE IAW SRM 51-42-06. LOCATED AND DRILLED UP NEW ANGLE, IAW SRM 51-40-11. INSTALLED NEW ANGLE IAW SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 21,481 hrs · 19,830 cycles

FLOORBEAM FS 484, RBL 27 TO RBL 36 CRACKED. COMPLIED WITH REO 601R-53-41-059.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,481 hrs · 19,830 cycles

FOUND REAR PRESSURE BULKHEAD WEB AT LBL 27.50 WL 130 HAS A CRACK INDICATION NOTED APPROX .2 INCHES IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1541.

Part: DRAG BRACE — DAMAGED (NLG) · airframe 21,341 hrs · 19,687 cycles

ON DEPARTURE, RECEIVED A GEAR DISAGREE WARNING MESSGE (ROUGHLY 6000 FT) COMPLIED WITH QRH. GEAR RETURNED TO DOWN AND LOCKED IAW QRH. EMERGENCY DECLARED AND RETURNED TO DEPARTURE. R & R NLG DRAG BRACE IAW AMM 32-21-05 LEAK AND OPS CHECKED GOOD, NO DEFECTS. ACFT OK FOR SERVICE REF AIPC 32-21-05 FIG 1, ITEM 5B.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 20,062 hrs · 18,286 cycles

EMERGENCY LIGHT AT TOP OF AIRSTAIR ON LT SIDE WALL HAS LENS BROKEN. REPLACED LENS TO EMERGENCY FLOOD LIGHT AT PAX DOOR IAW AMM 33-51-19. OPS CHECKED GOOD IAW AMM 33-51-00. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,900 hrs · 18,106 cycles

WHITE EMERGENCY LIGHT ON FWD BULKHEAD HAS INOPERATIVE LAMPS. RELAMPED EMERGENCY LIGHT FLOOD LIGHT ON FWD BULKHEAD AS REQUIRED. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,775 hrs · 16,890 cycles

CRACK IN AFT DRAG ANGLE PAX DOOR. REINSPECTED CRACK IN AFT DRAG ANGLE ON PAX DOOR. NO FURTHER DEFECTS NOTED. OK FOR SERVICE.

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 17,956 hrs · 15,987 cycles

PAX DOOR EXIT PLACARD DETERIORATED. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-00. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-00.

Part: PLACARD — MISSING (CABIN) · airframe 17,585 hrs · 15,574 cycles

EXIT PLACARD ON PAX DOOR FELL OFF. REAPPLIED EXIT STICKER TO ASD EXIT PHOTOLUMINISCENT PLACARD AS NEEDED. ACFT OK FOR SERVICE. (CLOSED)

Part: LIGHT — BURNED OUT (CABIN) · airframe 16,969 hrs · 14,837 cycles

SECOND FROM FRONT, EMERGENCY CEILING FLOOD LIGHT IS OUT. RELAMPED SECOND FROM FRONT EMERGENCY CEILING FLOOD LAMP WITH SERVICEABLE BULB AND OPS CHECK GOOD IAW AMM 33-51-06. ACFT OK FOR SERVICE. (CLOSED)

Part: BRACKET — FAILED (NLG) · airframe 16,736 hrs · 14,568 cycles

PROX SYS FAULT STATUS MSG ILLUMINATED FOLLOWED BY GEAR DISAGREE AND NOSE DOOR WARNING MSG WHEN LANDING GEAR LEVEL WAS SELECTED UP AFTER T/O. NOSE GEAR HAD DOWN INDICATION (EMERGENCY ACTIONS TAKEN IAW QRH) CC: 18A R & R NLG WOFFW SENSOR BRACKET IAW AMM 32-61-05. OPS CHECK IS GOOD. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 621) · airframe 16,674 hrs · 14,495 cycles

CARGO TRACK SECTION LOCATED JUST FWD OF FS 621 AT LBL 9 IS CORRODED. REMOVED CORRODED CARGO TRACK JUST FWD OF FS 621 LBL 9 AND INSTALLED NEW TRACK IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,674 hrs · 14,495 cycles

CARGO TRACK SECTION AT FS 559+112 RBL 9 IS CORRODED. REMOVED CORRODED CARGO TRACK, LOCATED FASTENER HOLES IN NEW TRACK AND INSTALLED NEW TRACK IAW SRM 51-40-11 AND 51-41-02.

Part: ANCHOR FITTING — CORRODED (CARGO BAY) · airframe 16,674 hrs · 14,495 cycles

CARGO BAY FLOOR ANCHOR FITTINGS ARE CORRODED. REMOVED CARGO BAY FLOOR ANCHOR FITTINGS AND INSTALLED NEW FITTINGS IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 16,674 hrs · 14,495 cycles

CARGO TRACK SECTION AT 559+96 LBL 9 IS CORRODED. UPON FURTHER INVESTIGATION FOUND CARGO TRACK AT FS 559+96, LBL 9 IS BEYOND REPAIRABLE LIMITS IAW SRM 53-61-49. CARGO TRACK REQUIRES REPLACEMENT. REMOVED CORRODED CARGO TRACK AT FS 559+96 LBL 9, LOCATED FASTENER HOLES IN NEW TRACK AND INSTALLED NEW TRACK IAW SRM 51-40-11 AND 51-41-02.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 16,674 hrs · 14,495 cycles

RIGHT FS 621 TO FS 625 INTERCOSTAL AT BL 45 STR 14 WL 97.5 IS CRACKED. R & R INTERCOSTAL AT RT FS 621-625 AT BL 45, STR 14, WL 97.5 IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 16,674 hrs · 14,495 cycles

CARGO TRACK SECTION AT FS 559+112 LBL 9 IS CORRODED. REMOVED CORRODED CARGO TRACK, LOCATED FASTENER HOLES IN NEW TRACK AND INSTALLED NEW TRACK IAW SRM 51-40-11 AND 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 16,674 hrs · 14,495 cycles

CARGO BAY FLOORBEAM CAP AT LBL 27 HAS MINOR CORROSION AROUND FASTENER HOLES FOR FLOORBOARD ON OTBD SIDE OF CAP FROM FS 621.0+0 TO FS 574.0. REPAIRED IAW REO 601R-53-61-3400 AND 601R-53-61-3688

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 16,674 hrs · 14,495 cycles

RT FLOOR SUPPORT ANGLE AT FS 621, RBL 27 IS CRACKED. REPAIRED RT FLOOR SUPPORT ANGLE AT FS 621, RBL 27 IAW REO 601R-53-61-117. REPAIR OF THE DAMAGED PORTIONS OF ANGLE 601R35031-239 IS COMPLETED IAW REO 601R-53-61-117 AND MEETS WITH ALL OF ITS REQUIREMENTS.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 16,674 hrs · 14,495 cycles

CARGO TRACK SECTION AT FS 559+96, RBL 9 IS CORRODED. UPON FURTHER INVESTIGATION FOUND CARGO TRACK AT FS 559+96 RBL 9 IS BEYOND REPAIRABLE LIMITS IAW SRM 53-61-49. SEAT TRACK REQUIRES REPLACEMENT. REMOVED CORRODED CARGO TRACK AT FS 559+96 RBL 9, LOCATED FASTENER HOLES IN NEW TRACK AND INSTALLED NEW TRACK IAW SRM 51-40-11 AND 51-41-02.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 16,674 hrs · 14,495 cycles

LEFT FLOOR SUPPORT ANGLE AT FS 621 LBL 27 IS CRACKED. REMOVED FLOOR SUPPORT ANGLE AT FS 621, LBL 27 TO LBL 34 AND DRILLED TO FINAL SIZE NEW SERVICEABLE ANGLE IAW SRM 51-42-06, 51-42-10 AND 41-42-21. INSTALL NEW SUPPORT ANGLE. OK TO INSTALL. INSTALLED NEW SUPPORT ANGLE AT FS 621, LBL 27, TO LBL 34 WITH EXISTING FASTENERS IAW CRJ 200 SRM 51-42-06, 51-42-10 AND 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 16,674 hrs · 14,495 cycles

LEFT FS 621 TO FS 625 INTERCOSTAL AT BL 45, STR 14 WL 97.5 IS CRACKED. R & R LT FS 621-625 INTERCOSTAL BL 45, STR 14, WL 97.5 IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (BS 559) · airframe 16,674 hrs · 14,495 cycles

FOUND FS 559 BULKHEAD WEB HAS A INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH INBD OF RBL 18.0 WL 59.10. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 16,674 hrs · 14,495 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTER ATTACHMENT FITTING HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIR IAW ECTC REO 601R-53-61-1230 HAS BEEN COMPLETE & THE REPAIR COMPLIES WITH THE REQUIREMENTS OF EC/TC REO 601R-53-61-1230, REV D.

Part: ISOLATOR — CRACKED (AFT PRESS BULKHD) · airframe 16,674 hrs · 14,495 cycles

FOUND REAR PRESSURE BULKHEAD Z ISOLATORS ARE CRACKED. R & R 2 RUBBER ISOLATORS ON REAR PRESSURE BULKHEAD IAW SRM 51-42-06.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 16,674 hrs · 14,495 cycles

FOUND CARGO DOOR SUPPORT BEAM LOWER AFT ANGLE IS CRACKED APPROX .3 IN LENGTH. REMOVED DAMAGED CARGO DOOR SUPPORT BEAM LOWER AFT ANGLE & INSTALLED NEW SERVICEABLE LOWER AFT ANGLE IAW SRM CH 51-42-21.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 16,674 hrs · 14,495 cycles

EMERGENCY EXIT LENS CRACKED ON LT WINDSCREEN. REMOVED LT WINDSCREEN EXIT SIGN LENS COVER BY PULLING COVER AWAY FROM LIGHT HSG & INSTALLED NEW SERVICEABLE LENS COVER BY SNAPPING COVER ONTO LIGHT HOUSING UNTIL SECURE.

Part: PLACARD — WORN (ESCAPE HATCH) · airframe 16,674 hrs · 14,495 cycles

CREW ESCAPE HATCH PLACARD "EMERGENCY EXIT "PUSH" RELEASE TURN HANDLE TO "OPEN" PUSH EXIT IN" IS WORN. REMOVED REMAINING SILKSCREEN IAW AMM TASK 11-10-03-000-801 AND APPLIED NEW SILKSCREEN TO CREW ESCAPE HATCH (EMERGENCY EXIT) IAW AMM TASK 11-10-03-400-801.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 15,689 hrs · 13,342 cycles

RT WING EMERG. LIGHT INOP

Part: HANDLE — OUT OF ADJUST (SERVICE DOOR) · airframe 13,033 hrs · 10,770 cycles

SVC - DOOR OUTER HANDLE WILL NOT STOW. REMOVED, CLEANED AND REINSTALLED SERVICE DOOR INNER HANDLE & ACTUATOR IAW CRJ 200 MM 52-41-03. OPS CHECK GOOD, OUTER HANDLE STOWS PROPERLY. (S)

Part: HANDLE — OUT OF POSITION (SERVICE DOOR) · airframe 13,033 hrs · 10,770 cycles

SERVICE DOOR OUTER HANDLE WILL NOT STOW. REPOSITIONED GALLEY SERVICE DOOR HANDLE. OPS CHECK GOOD IAW CRJ200 AMM 52-41-00. (S)

Part: TIRE — FAILED (NLG) · airframe 12,840 hrs · 10,587 cycles

NOSE TIRE BLEW OUT AT ROTATION ON T.O. SPEED KIAS. RETURNED TO ATL EMERGENCY DECLARED. FLT 4901 DEL 278 MINS..NC REMOVED AND REPLACED LT AND RT NOSE TIRES IAW CRJ-200 AMM 32-42-01. [SDR CLOSED] (B)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 1,254,342 hrs · 10,330 cycles

ATTACH CLIP CRACKED AT BS 280 BULKHEAD WEB RBL 9. REMOVED 280 RBL 9 ATTACH CLIP IAW SRM 51-42-21. INSTALLED 280RBL 9 ATTACH CLIP IAW SRM 51-42-21. (B)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 1,254,342 hrs · 10,330 cycles

LT OTBD FLOORBEAM ANGLE CRACKED AT STA 280 BULKHEAD. REMOVED LT OTBD FLOORBEAM ANGLE AT STA 280 ALL WORK DONE IAW SRM 51-42-21. INSTALLED LT OTBD FLOORBEAM ANGLE AT STA 280 ALL WORK DONE IAW SRM 51-42-21.

Part: RIB — CRACKED (LT WING) · airframe 1,254,342 hrs · 10,330 cycles

LT BATTERY RIB CRACKED. REMOVED AND DISGARDED DOUBLER PN 601R10203-31. TRIMMED AWAY DAMAGE AS SHOWN ON REO 601R-57-51-046. CLEANED UP CUT LINE TO SMOOTH FINISH, FABRICATED -5 DOUBLER FROM 7075-0 .063 HEAT TREATED TO T-6 AND -7 FILLER FROM 7075-T-6 .050 LOCATED ALL FASTERNER HOLES AND TRIMMED TO SIZE PER REO 601R-57-51-046. ALODINED, PRIMED AND PAINTED REPAIR PARTS SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 1,254,342 hrs · 10,330 cycles

AFT FLOOR SUPPORT ANGLE CRACKED AT STA 280 BULKHEAD LBL9. JOB COMPLETE, REPAIRED AFT FLOOR SUPPORT ANGLE AT STA 280 BULKHEAD LBL 9 IAW REO 601R-53-11-138.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 1,254,342 hrs · 10,330 cycles

LT SIDE 202 PRESSURE BULKHEAD CRACKED AT BRAKE SYSTEM PUSHROD RESOLUTION DESCRIPTION: (RESOLVED ON W/O: 90658 TASKCARD: N/R-00092) REPAIRED CRACKED PRESSURE BULKHEAD LT SIDE STA 202.75 ON WORK ORDER 90661 TASK CARD E0600-53-0217C/W SDR CLOSED (B)

Part: SUPPORT BEAM — CRACKED · airframe 1,254,342 hrs · 10,330 cycles

UPPER SURFACE OF ENGINE SUPPORT BEAM APPEARS CRACKED AT B.L. 0 AND FS 640. POSSIBLE CRACK NEEDS VERIFIED. PERFORMED EDDY CURRENT INSPECTION OF ENGINE SUPPORT BEAM AT BL 0.00, FS 640.00, ENGINE SUPPORT BEAM VERIFIED CRACKED AT RIGHT HAND FASTENER HOLE FORWARD SIDE IAW NDTM 51-20-06. REPAIRED CRACKED UPPER SURFACE OF ENGINE SUPPORT BEAM IAW REO 601R-53-61-345 AND EO600-53-72-0001 REFER TO ATTACHED M-234 FOR.

Part: WARNING MESSAGE — ILLUMINATED · airframe 12,055 hrs · 9,921 cycles

MACH TRIM CAUTION AFTER FLAPS FAIL ALONG WITH THE LOSS OF COPILOTS PFD, PFD REAPPEARD ON FINAL APPROACH. EMERGENCY DECLARED.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 11,801 hrs · 9,699 cycles

FLAP FAIL AT ZERO ON APPROACH. THE TOWER INITIATED FIRE & RESCUE AS A PRECAUTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,591 hrs · 9,522 cycles

EMERGENCY LIGHT ON AFT CIELING INOP.

Part: STEP — CRACKED (AIRSTAIR) · airframe 11,449 hrs · 9,403 cycles

ASD LOWER BOTTOM STEP CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,167 hrs · 9,172 cycles

LEFT CENTER EMERGENCY LIGHT OVER WING IS INOP.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 11,166 hrs · 9,171 cycles

CREW O2 LOW DUE FUEL SMELL IN COCKPIT CREW USED O2 MASK IN FLT.

Part: PLACARD — TORN (PAX DOOR) · airframe 10,960 hrs · 8,998 cycles

PAX DOOR PLACARDS -EXIT- & -TO OPEN- TORN.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 10,923 hrs · 8,966 cycles

IN FLIGHT, F/A REPORTING A BURNED ODOR SMELL COMING FROM COFFEEMAKER AND ADJACENT WALL IS VERY HOT. PULLED GALLEY COFFEEMAKER C/B AND ODOR AND HEAT WENT AWAY.

Part: LIGHT — UNKNOWN (CABIN) · airframe 10,104 hrs · 8,312 cycles

REMOVED EMERGENCY LIGHT ASSY FROM PAX DOOR ENTRY ASSY BR9279-232 FOR ACFT 832.

Part: UNKNOWN — ODOR (CABIN) · airframe 9,782 hrs · 8,070 cycles

ON CLIMBOUT OF ATL BELOW 10K BOTH F/O AND CAPT PICKED UP A MILD BURNING ODOR, PRIOR TO REACHING 10K ODOR WENT AWAY. UPON LANDING AT FAY BOTH RECEIVED SAME ODOR. F/A REPORTED, ONLY ON TAXI IS A STRONG ODOR OF BURNING.

Part: UNKNOWN — UNKNOWN (TE FLAPS) · airframe 9,629 hrs · 7,954 cycles

FLAP FAIL AT ZERO ON APPROACH. EMERGENCY EQUIPMENT ON STANDBY.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 9,464 hrs · 7,832 cycles

CAPTAIN'S FLASHLIGHT INOP.

Part: RIVET — CORRODED (FUSELAGE) · airframe 7,757 hrs · 6,551 cycles

RANRC 287. MILD CORROSION ON FUSELAGE AROUND SCREW HOLES, THREE (3) RIVETS REQUIRE REPLACEMENT. RESOLVED ON W/O: 27702 TASKCARD: N/R-00205. REMOVED CORROSION. FOUND TO HAVE REMOVED .002 OF MATERIAL. ALODINED PER CRJ SRM 51-21-06. REMOVED AND REPLACED 2EA RIVETS P/N MS 20426AD5-3 PER CRJ SRM 51-42-06.

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,755 hrs · 6,550 cycles

RANRC 206. CRACKS LEFT I/B FS 484.0 LBL 36. RESOLVED ON W/O: 27702 TASKCARD: N/R-00124. REMOVED I/B CLIP AT FS 484.0 AT LBL 27, USED 2024-T42 .063 ANGLE PO R/O 437 TO FABRICATE REPAIR CLIP. FABRICATED CLIP IAW REO 601R-53-41-059. LOCATED AND DRILLED IAW CRJ SRM 51-40-11. ALODINED AND PRIMED IAW CRJ SRM'S 51-21-11 AND 51-25-06. PAINTED IAW CRJ SRM 51-25-00. INSTALLED CLIP, ALL WORK DONE IAW REO 601R-53-41-059.

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,755 hrs · 6,550 cycles

RANRC 199. RIGHT I/B FS 484 CRACKED. RESOLVED ON W/O: 27702 TASKCARD: N/R-00117. REMOVED RIGHT I/B CLIP AT FS 484 RBL 27, USED 2024-T42 .063 ANGLE PO R/O 437 TO FABRICATE REPAIR CLIP IAW REO 601R-53-41-059. LOCATED CLIP IAW CRJ SRM 51-40-11. ALODINED AND PRIMED IAW CRJ SRM'S 51-21-11 AND 51-25-06. APPLIED TOP COAT IAW CRJ SRM 51-25-01. INSTALLED CLIP AT FS 484 RBL 27 IAW REO 601R-53-41-059.

Part: CLIP — CRACKED (FUSELAGE) · airframe 7,755 hrs · 6,550 cycles

RANRC 198. RIGHT I/B AND O/B FS 280 CLIP CRACKED. RESOLVED ON W/O: 27702 TASKCARD: N/R-00116. DRILLED OFF I/B AND O/B CLIPS AND DUPLICATED CLIPS IAW CRJ SRM 51-24-16, USING 2024T .063" PO 8195-1, REQUIRES LPI, PERFORMED FLUORESCENT INSPECTION ON RIGHT I/B AND O/B FS 280 CLIPS, NO DEFECT NOTED PER CRJ NDTM 51-20-05. INSTALLED RIGHT, I/B AND O/B CLIP IAW CRJ SRM 51-42-21, SRM 51-23-00 AND SRM 51-25-16.

Part: SKIN — CORRODED (RT COWLING) · airframe 7,755 hrs · 6,550 cycles

RANRC 168. RIGHT NOSE INLET HAS CORROSION DAMAGE ON COMPOSITE SKIN JUST AFT OF LIPSKIN.

Part: FLEX DRIVE — DIRTY (FLAP DRIVE SYS)

DURING DESCENT, THE CREW RECEIVED A FLAPS FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY VEHICLES WERE DISPATCHED AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY. MAINTENANCE COMPLIED WITH EO AND ALSO REMOVED WATER FROM THE FLEX SHAFT TUBES, CLEANED, AND LUBRICATED ALL OF THE FLEX SHAFTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (CABIN)

DURING A HANGAR INSPECTION, THE RT CENTER EMERGENCY LIGHT ASSY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN RT CENTER EMERGENCY LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)