N914EV

Part: APU — OVERTEMP (ZONE 100) · airframe 39,855 hrs · 39,477 cycles

D: APU OVERTEMP WARNING IN FLIGHT. RAN QRH AND MESSAGE CLEARED.C: MEL 49-10-1ACAT C DUE 5/27/24APU OVERTEMP WARNING IN FLIGHT. RAN QRH AND MESSAGE CLEARED.MAY 17, 2024 STATION: FAR--DEFERRED APU PER CRJ 200 MEL 49-10-1A. MX ACTION COMPLIED WITH AND PLACARD INSTALLED. NO 10 DAY MX LOG BOOK HISTORY NOTED

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 38,964 hrs · 38,580 cycles

L 10TH DUCT WARNING MESSAGE ON CLIMB AT 15000FT. DID THE QRH PROCEDURE, DIRECTED TO GET LEFT ENGINE TO IDLE. DECLARED EMERGENCY AND DID A SINGLE ENGINE LANDING WITH RIGHT ENGINE. (FLIGHT 5541 FILED OPEN)FOUND LEAK COMING FROM LH 10TH STAGE PRSOV FLANGE CRACK FACING LOOPS A50WK AND A51WK. REPLACED LEFT PRESSURE REGULATING SHUT-OFF VALVE ASSY IN REF TO CRJ200 AMM 21-51-43. COMPLIED WITH OPERATIONAL CHECK OF LEFT PRSOV IN REF TO AMM TASK 21-51-43-710-801). ALL INDICATIONS NORMAL. OPS CHECK AND LEAK CHECK GOOD.

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 38,962 hrs · 38,578 cycles

REPEAT L 10TH DUCT WARNING MESSAGE ON CLIMB OUT. PLEASE REVIEW HISTORY AND T/S NEXT OVERNIGHTMCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGHT 5452 FILED CLOSED)OCT 24, 2023 STATION: RDD--REMOVED AND REPLACED HEATING ELEMENT SENSOR AT A17WK PER CRJ-200 AMM 36-21-00 AND OPS CHECK GOOD AND INSPECTED LEFT 10TH STAGE BLEED LOOPS AND FOUND LOOPS TO BE TOUGHING/RUBBING EACH OTHER AT SEVERAL PLACE, REPOSITION LOOPS AS NEEDED AND PERFORMED OPERATIONAL TEST OF BLEED-AIR TEST PER CRJ-200 AMM 36-21-10-710-801 AND OPS CHECK GOOD. PERFORMED GVI INSPECTION OF 10TH STAGE BLEED-AIR DUCTING PER CRJ-200 AMM 36-11-31-210-801 AND NO LEAKS NOTED. PERFORMED ENGINE RUN CHECK PER CRJ-200 AMM 71-00-00 AND OPS CHECK GOOD. A/C OK TO CONTINUE SERVICE

Part: LANDING GEAR — WARNING MESSAGE · airframe 38,275 hrs · 37,868 cycles

GEAR DISAGREE WARNING MESSAGE WHILE SELECTING GEAR DOWN. NOSE GEAR SHOWED DOWN POSITION WHILE MAIN GEAR REMAINED IN UP POSITION. MESSAGE CLEARED DURING GO AROUND. ALL THREE SHOWED DOWN. COMPLIED WITH QRH. (FLT 5135, FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: LANDING GEAR — WARNING MESSAGE · airframe 38,283 hrs · 37,874 cycles

GEAR DISAGREE WARNING MESSAGE WHILE SELECTING GEAR DOWN. NOSE GEAR SHOWED DOWN POSITION WHILE MAIN GEAR REMAINED IN UP POSITION. MESSAGE CLEARED DURING GO AROUND. ALL THREE SHOWED DOWN. COMPLIED WITH QRH. (FLT 5135, FILED CLOSED)UPON ARRIVAL TO A/C FOUND PSEU FLAGGED SOV NEAR, AND DI20 ON. PER FDR DOWNLOAD DATA AND THE FLEET COORDINATOR, THE REASON THE SOV NEAR IS PROBABLY BECAUSE IT IS PART OF THE SPIN DOWN AND THE PARKING BRAKE SOV IS CLOSED WITH THE PARKING BRAKE SET. FLEET COORDINATOR SUGGESTS MLG SELECTOR VALVE TO BE FAULTY. REF CP-1141413 FOR THE MLG SELECTOR VALVE REMOVAL AND REPLACEMENT. PERFORMED AN OPERATIONAL CHECK OF THE LANDING GEAR EXTENTION AND RETRACTION IN REFERENCE TO CRJ200 AMM 32-30-00. OPS CHECK GOOD. VERIFIED EXT AND RETRACTION TIMES WITHIN LIMITS IN REFERENCE TO CRJ200 AMM 32-00-00. OPS CHECK GOOD.

Part: NONE — CORRODED · airframe 37,923 hrs · 37,520 cycles

*LH CABIN PRESSURE FLOOR SILL CORROSION AROUND SCREW HOLES (2EA) BETWEEN FS529.00 & FS540.25 (C-CHECK RO 2/18/2023) REMOVED CORROSION ON THE LEFT-HAND CABIN PRESSURE FLOOR SILL PANEL AROUND 2 EA. SCREW HOLES BETWEEN FS529.00 AND FS540.25, AND EVALUATED AS WITHIN LIMITS. REF. REO 601R-53-41-666 REV. -C DATE: 2012-11-06 DISPOSITION 1.2 (A). NO LEAKS DETECTED. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: NONE — CORRODED · airframe 37,923 hrs · 37,520 cycles

DURING CORRODED FASTENERS REMOVAL FOUND CORROSION ON RBL 9.0 SEAT RAIL SECTION FS 409.0 TO FS 409+16. (C-CHECK RO 2/18/2023) SEAT RAIL AT RBL 9.0 FROM FS409.0 TO FS409+128 WAS REMOVED,FABRICATED AND INSTALLED NEW REF REO 601R-53-00-485 REV. D 2018-01-29 AND SRM 51-41-02-00. ALL STEPS OF REO COMPLIED WITH.

Part: NONE — CORRODED · airframe 37,923 hrs · 37,520 cycles

CORROSION ON FRAME FS 589.00, BETWEEN STGR 19R - 20R. MARKED. (C-CHECK RO 2/18/2023) REMOVED CORROSION ON FRAME FS589.00, BETWEEN STGR 19R-20R REF. CRJ-200 SRM, 51-21-06. PARTS FABBED AND INSTALLED REPAIR PARTS FRAME SECTION -1 AND FRAME SPLICE -2 ON FRAME FS589.00 BETWEEN STGR 19R-20R REF. CRJ-200 REO 601R-53-61-7955 REV --, DATED: 2023-01-31 COMPLIED 51-900-1003-SKY

Part: NONE — DAMAGED · airframe 37,923 hrs · 37,520 cycles

EXISTING PASSENGER DOOR SEAL STRIKER DAMAGE JUST ABOVE FORWARD UPPER PIN STOP FITTING ON FORWARD SIDE OF DOOR CUTOUT (C-CHECK RO 2/18/2023) REMOVED AND REPLACED PASSENGER DOOR SEAL STRIKER JUST ABOVE FORWARD UPPER PIN STOP FITTING ON FORWARD SIDE OF DOOR CUTOUT IAW REO 601R-53-22-033 REV -D DATE 2014/02/17 REPAIR TYPE 1 STEPS. 1-6 (SEE CONTINUATION SHEET FOR FURTHER DETAILS).COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 37,923 hrs · 37,520 cycles

FS 280. BOTH AT LBL 9.0 AND RBL 9.0 (2 EA) INBOARD CLIPS HAS SUSPECT CRACKS AT UPPER RADIUS. (C-CHECK RO 2/18/2023) REMOVED AND INSTALLED 1 EA NEW INBOARD ATTACH CLIP AT LBL 9.0 AT FS 280.0 P/N 601R31113-57 AND 1 EA ATTACH CLIP AT RBL 9.0 P/N 601R31113-58 REF BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10 AND BOMBARDIER REO 601R-53-11-136 REV A DATED 2007/11/01SKYCARD 51-900-1003-SKY COMPLIED WITH

Part: NONE — CRACKED · airframe 37,923 hrs · 37,520 cycles

PRESSURE FLOOR SUPPORT BEAM AT FS 460.0 RBL 9.0 CASTING HAS CRACK AT UPPER RADIUS. (C-CHECK RO 2/18/2023) REMOVED CRACKED FITTING AT FS460.00, RBL 9.0, AND INSTALLED NEW FITTING, PN: 600-31068-19. REF. DWG 601R31146 REV. J, DWG 601R31118 REV. L, CRJ200 SRM 51-42-06, AND CRJ SRM 51-42-21. NO LEAKS DETECTED. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY.

Part: NONE — DENTED · airframe 37,923 hrs · 37,520 cycles

GROUND AIR CONDITIONING DOOR SURROUND (LANDING PLATE) IS PUSHED IN (DENTED) AND DAMAGED. (C-CHECK RO 2/18/2023) REMOVED AND REPLACED FWD ANGLE AT GROUND AIR CONDITIONING DOOR SURROUND REF. CRJ-200 SRM, 51-42-06 AND DWG 601R35226 REV-P. COMPLIED WITH TASK CARD 51-900-1003-SKY, NO LEAK NOTED.

Part: NONE — DENTED · airframe 37,923 hrs · 37,520 cycles

DENT NEAR FS409+16 STGR 26L (C-CHECK RO 2/18/2023) PERFORMED PERMANENT REPAIR TO DENT AREA OF FUSELAGE STATION FS409.00 AT STGR26L. REF. MHIRJ REO 601R-53-31-1258 REV -- DATED 2023-01-26. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR (**RII**)PRESSURE CHECK GOOD

Part: NONE — DENTED · airframe 37,923 hrs · 37,520 cycles

*MULTIPLE DENTS NOTED ON L/H FLIGHT SPOILER UPPER SURFACE (MARKED) (C-CHECK RO 2/18/2023) REMOVED THE PAINT & EVALUATED THE MULTIPLE DENTS ON THE LH FLIGHT SPOILER REF CRJ-200 SRM 57-73-00 AND COMPLIED WITH ALL THE STEPS OF THE REO 601R-57-73-401 REV-- DATED 2023-01-15.COMPLIED WITH TASKCARD 51-900-1003-SKY

Part: NONE — CHAFED · airframe 37,923 hrs · 37,520 cycles

*CHAFFING NOTED AT R/H AILERON L/E LOWER SKIN (MARKED) (C-CHECK RO 2/18/2023) BLENDED OUT DAMAGE ON SKIN PANEL @ AIL STA.370.664 FOUND TO BE WITHIN LIMITS REF REO 670-57-61-194 REV -C DATED 2019-01-07. REMOVED AND REPLACED SKIN PANEL @ AIL STA.324.459 P/N CC670-13053-2. REF: DRAWING CC670-13000 REV -D, CRJ-200 SRM 51-42-06, AND CRJ-200 SRM 51-42-21SKYCARD 51-900-1003-SKY COMPLIED WITH

Part: NONE — CHAFED · airframe 37,923 hrs · 37,520 cycles

* AFT CARGO DOOR, EXTERIOR SKIN REPAIR DOUBLER ( PREVIOUS REPAIR ) HAS CHAFFED AREAS ( 2 EACH ). (C-CHECK RO 2/18/2023) REMOVED & INSTALLED NEW REPAIR DOUBLER (-1) P/N 2024T-3 0.080 PO: T-58292 REF REO NO. 601R-52-31-310 REV -B DATED 2019-06-13, CRJ200 SRM51-42-21 AND SRM51-42-22SKYCARD 51-900-1003-SKY COMPLIED WITH

Part: NONE — DENTED · airframe 37,923 hrs · 37,520 cycles

THE UPPER SURFACE OF THE LH AILERON HAS MULTIPLE DENTS. PLEASE PLOT, MAP AND EVALUATED THE DAMAGE/AREA. IF THE DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. (C-CHECK RO 2/18/2023) DENTS ON THE UPPER SURFACE OF THE LH AILERON ARE FOUND TO BE ACCEPTABLE PROVIDED ALL STEPS OF REO 601R-57-61-828 REV-- 2023-01-30 ARE COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY AND ALL STEPS OF REO 601R-57-61-828 REV-- 2023-01-30. AIRCRAFT MUST NOT BE OPERATED BEYOND 12 MONTHS FROM THE ISSUE DATE OF THIS REPAIR.

Part: NONE — DENTED · airframe 37,923 hrs · 37,520 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA67724-601R-52-11-2861 N914EV MXCODEID55300-PR - DUE TO DENT IN MCD ABOUT 3/4 WAY UP DENT MEASURES 1 1/4 WIDE BY 1 3/4 LONG AND 1/32 DEPTH, COMPLIED WITH TEMPORARY DISPOSITION PER REO 601R-52-11-2861 STEPS 1 -4. PERMANENT REPAIR WITHIN 4700 FH. DUE BY TAT 39955.6., PART NUMBER: - , SERIAL NUMBER: 7752, POSITION: (C-CHECK RO 2/18/2023) COMPLIED WITH PERMANENT REPAIR OF PAX DOOR OUTER SKIN DENT. REF. REO 601R-52-11-2955, REV -- DATED: 2023-01-14 ALL STEPS COMPLIED WITH. OPS CHECKS GOOD, NO LEAKS DETECTED. NO WEIGHT CHANGE DENT DRESS BACK ONLYSKYCARD 51-900-1003-SKY COMPLIED WITH.

Part: UNKNOWN — ODOR (CABIN) · airframe 36,948 hrs · 36,640 cycles

STRONG SMELL OF FUEL IN CABIN (FLIGHT 5682 - FILED CLOSED) UPON FURTHER INSPECTION, FUEL LEAK FOUND INSIDE THE APU BOX AT THE FUEL SHUTOFF SOLENOID VALVE FITTING GOING INTO FUEL CONTROL. REMOVED AND REPLACED THE PACKING ON THE FUEL SHUTOFF SOLENOID VALVE AT THE FUEL CONTROL FITTING. REF CRJ 200 AMM 49-31-05. PLEASE REFERENCE AML 889110

Part: SUPPORT ANGLE — CRACKED (BS 621) · airframe 33,914 hrs · 33,479 cycles

* SUPPORT ANGLE CRACKED ON FS 621 RIGHT SIDE AT APROX STRG14R MARKED (C-CHECK) RO 12/6/2019 REPLACED ANGLE AT AFT SIDE OF FS621 RHS AT APPROX STGR14R IAW SRM. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 33,914 hrs · 33,479 cycles

* SEAT TRACK FS 559+112 TO JUST AFT OF FS 574.0 RBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 REPLACED CARGO SEAT TRACK BETWEEN FS559+112 AND FS574.00 RBL 9 IAW AMM. SEE CONTINUE CARD FOR DETAILS

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* R/H SILL FROM FS 559.0 TO FS 559+80 HAS CORROSION SEVERAL AREAS (C-CHECK) RO 12/6/2019 COMPLIED WITH ALL THE STEPS IAW REO. REMOVED CORROSION ON R/H FLOOR SILL BETWEEN FS559.0 AND FS559.+80. REPLACED BLIND FASTENERS. SILL ORIGINAL THICKNESS IS 0.063 IAW SRM. REMAINING THICKNESS IS 0.053 MATERIAL LOST IS .010. FOUND WITH IN LIMIT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 33,914 hrs · 33,479 cycles

* L/H PRESSURE FLOOR SILL ANGLE HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 LH PRESSURE FLOOR SILL ANGLE IS BLENDED, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* FLOOR BEAM CAP @ FS 559+16 TO FS 559+80 RBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 FABRICATED AND INSTALLED NEW FLOOR BEAM CAP IAW REO. SEE CONTINUE CARD FOR ALL DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 33,914 hrs · 33,479 cycles

* RH SILL FROM FS 559+80 TO FS 621.0 HAS SEVERAL AREAS OF CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON R/H FLOOR SILL FROM FS559.00+90 TO FS621.00 AND EVALUATED REPAIR. REPAIR WAS FOUND WITHIN LIMITS AND RESTORED TO ORIG. CONDITION. AIW REO. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* L/H SILL FROM FS 559.0 TO FS 559+80 HAS CORROSION SEVERAL AREAS (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON L/H FLOOR SILL FROM FS559.00 TO FS559.00+80 AND EVALUATED REPAIR. REPAIR FOUND TO BE WITHIN LIMITS AND RESTORED SILL TO ORIG. CONFIGURATION. IAW REO. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 RBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON THE AFFECTED SEAT TRACK. IAW SRM. REFER TO CONTINUE CARD FOR ADDITIONAL DETAILS.

Part: SUPPORT ANGLE — CRACKED (BS 621) · airframe 33,914 hrs · 33,479 cycles

* SUPPORT ANGLE CRACKED ON AFT SIDE OF FS 621 LEFT SIDE AT APROX STRG14L MARKED (C-CHECK) RO 12/6/2019 REMOVED AND REPLACED CRACKED SUPPORT ANGLE WITH NEW ANGLE ON AFT SIDE OF FS 621 LEFT SIDE AT APROX STRG14L IAW SRM.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* CROSS BEAM TOP CAP FS 559+80 RBL 27 TO THE SILL HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED CORROSION FROM CROSS BEAM TOP CAP FS 559+80 RBL 27 TO THE SILL. THE AREA IS FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 33,914 hrs · 33,479 cycles

* R/H PRESURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 REMOVED CORROSION AND EVALUATED REPAIRS AT 9 LOCATION ON R/H PRESSURE FLOOR SILL PANEL . REPAIRS FOUND TO BE WITHIN LIMITS. IAW REO. NO FASTENERS REMOVED IN REPAIR SO NO PRESSURE CHECK NEEDS TO BE C/W.COMPLIED WITH SKYWEST TASK CARD "STRUCTURAL MAJOR REPAIR **RII**" SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.BLENDS A LOCATION 1,7,8,10,11,12,15 WERE PERFORMED ON R/H PRESSURE FLOOR ANGLE AND NOT PART OF THIS MAJOR REPAIR. SEE CAMP 19795376 JOB 2775281 OP 199 FOR WORK PERFORM AND EVALUATIONS OF THESE LOCATIONS

Part: FLOORBEAM — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* CROSS BEAM TOP CAP FS 559+112 LBL 27 TO SILL HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION AND EVALUATED REPAIRS. REPAIRS FOUND TO BE WITHIN LIMITS AND RESTORED REPAIR TO ORIG. FINISH. IAW SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 33,914 hrs · 33,479 cycles

* SEAT TRACK FS 559+112 TO JUST AFT OF FS 574.0 LBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED OUT CORROSION IS OUT OF LIMITS, REMOVED, REPLACED AND INSTALLED NEW CARGO TIE-DOWN TRACK P/N 601R38779-5 AT FS559+112 TO FS568 LBL9.IAW AMM.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* CROSS BEAM TOP CAP FS 559+80 RBL 9 TO RBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 CROSS BEAM TOP CAP FS 559+80 RBL 9 TO RBL 27 IS BLENDED, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL FINISH IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 33,914 hrs · 33,479 cycles

* L/H PRESSURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 LH PRESSURE FLOOR SILL PANEL BLENDED FROM FS 409+128 TO FS 559.0, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW REO. COMPLIED WITH SKYWEST TASK CARD. PRESSURE CHECK GOOD

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 33,914 hrs · 33,479 cycles

* R/H PRESSURE FLOOR SILL ANGLE HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 BLENDED DAMAGE ON RH FLOOR SILL AT ALL LOCATIONS FS409.128 - FS559.0. IAW SRM. ALL WITHIN LIMITS IAW REO. RESTORED THE CIC AND TOP COAT FINISH. REFERENCE THE CONTINUE CARD FOR A DETAILED DESCRIPTION OF THE WORK PERFORMED. PRESSURE CHECKS GOOD.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 LBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED AND BLENDED OUT CORROSION IS WITHIN LIMITS ON SEAT TRACK AT FS559+80 TO FS559+96 LBL9. IAW SRM.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 RBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED OUT DAMAGE AND RESTORED FINISH TO SEAT TRACK AFT OF FS559+80 TO FS559+96. IAW SRM.

Part: BULKHEAD — CRACKED (BS 621) · airframe 33,914 hrs · 33,479 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER. MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER. AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7752, POSITION: (C-CHECK) RO 12/6/2019 COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER. SEE CONTINUATION CARD FOR DETAILS / (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,914 hrs · 33,479 cycles

* SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 LBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON THE AFFECTED SEAT TRACK. REF CRJ200 SRM 51-21-06. SEE CONTINUATION CARD FOR ADDITIONAL DETAILS

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,783 hrs · 33,340 cycles

GEAR DISAGREE ON TAKE OFF. C/W QRH PROCEDURE ALL THREE GEAR CAME DOWN AND LOCKED. FLT DIVERTED TO MBS. (FLT#4303) CLOSED DEFERRED MLG RETRACTION SYSTEM PER.

Part: ENGINE — OVERTEMP (RIGHT) · airframe 33,686 hrs · 33,225 cycles

RIGHT ENGINE HIGH TEMP, PEAKED 169; FOLLOWING QRH PROCEDURE ENGINE SHUTDOWN IN FLIGHT. EMERGENCY DECLARED. REMOVED AND REPLACED ENGINE OIL LEVEL SIGNAL CONDITIONER, ENGINE REPLENISHMENT SIGNAL CONDITIONER, RH ENGINE LOW-OIL LEVEL PROBE, RH ENGINE VIOLET HARNESS, RH ENGINE BYPASS CHECK VALVE IAW AMM. INSPECTED RH ENGINE OIL FILTER AND RH ENGINE OIL SERVICING COMPLETED. PERFORMED ENGINE RUN ON THE RH ENG IAW AMM, OPS CHECK GOOD.

Part: SENSOR — OUT OF ADJUST (NLG STEERING) · airframe 33,642 hrs · 33,174 cycles

RECEIVED NWS STEERING INOP CAUTION MESSAGE FOLLOWED BY WOW INPUT CAUTION MESSAGE FOLLOWED BY WOW OUTPUT FAIL. NORMAL LANDING AND STEERING OPERATION. FLT 3959. COMPLIED WITH RE-RIG OF SENSOR-TO-TARGET GAP FOR NLG WOFFW PS13GA AND PS4GA IAW AMM, COMPLETED FULL STRUT SERVICE AND OPS CHECK IAW AMM. NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: SEAL — FAILED (NLG) · airframe 33,642 hrs · 33,175 cycles

AFTER TAKEOFF NOSE GEAR DISAGREE ACCOMPANIED BY NOSE DOOR OPEN AND STEERING INOP. PERFORMED QRH PROCEDURE AND LANDED WITHOUT INCIDENT. FLT 3742. REMOVED AND REPACKED BACKUP NLG SEALS AND INSTALLED NEW GUIDE PINS IAW AMM. PERFORMED MLG EXTENSION AND RETRACTION TEST IAW AMM. OPS CHECK GOOD AT THIS TIME. LEAK CHECKED GOOD.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 31,997 hrs · 31,334 cycles

HYD 3 LO PRESS CAUTION MESSAGE AFTER TAKE OFF. (FLT 3623) FO: 7/16/2018 CLOSED / REMOVED AND REPLACED ACMP 3A IAW AMM. SERVICED HYD SYSTEM 3, OPS CHECK GOOD.

Part: BRACKET — BROKEN (NLG) · airframe 30,402 hrs · 29,602 cycles

RECEIVED A GEAR DISAGREE WARNING MESSAGE. CREW COMPLIED WITH QRH & RETURNED TO FIELD. REPLACED THE NOSE GEAR UPLOCK BRACKET. SYSTEM OPS CHECKED GOOD.

Part: SKIN — CRACKED (LT WING) · airframe 30,176 hrs · 29,343 cycles

LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED ON THE LANDING FOR ACCESS PANEL 540DB ON THE OTBD SIDE, BOTH .200 INCH . REPAIRED IAW REO.

Part: SKIN — CRACKED (RT WING) · airframe 30,176 hrs · 29,343 cycles

LOWER RT WING PLANK HAS ONE INDICATION NOTED ON THE LANDING FOR ACCESS PANEL 650GB ON THE AFT SIDE. REPAIRED IAW REO.

Part: SKIN — CRACKED (LT WING) · airframe 30,176 hrs · 29,343 cycles

LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED ON THE LANDING FOR ACCESS PANEL 550BB ON THE OTBD SIDE AND FWD SIDE. REPAIRED IAW REO.

Part: SKIN — CRACKED (RT WING) · airframe 30,176 hrs · 29,343 cycles

MULTIPLE INDICATIONS NOTED IN LOWER WING PLANK AT RT BOOST PUMP ACCESS PANEL LANDING 610CB AROUND ENTIRE CIRCUMFERENCE HORIZONTAL AND VERTICAL SURFACES. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 409) · airframe 30,176 hrs · 29,343 cycles

FS 409 + 128, RBL 18 VERTICAL POST DENTED OTBD OF STRINGER 24R AND ABOUT 5 INCHES FWD OF RBL 18. REPAIRED IN SKIN IAW SRM.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 30,176 hrs · 29,343 cycles

CARGO DOOR SILL CORRODED IN MULTIPLE LOCATIONS AROUND FASTENER HOLES. REPAIRED IAW REO.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 30,176 hrs · 29,343 cycles

FLOORBEAM ANGLE CRACKED AT BS 621 BETWEEN LBL 27 AND 36. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,176 hrs · 29,343 cycles

BS 280 FLOORBEAM CRACKED AT LBL 9 AND RBL 9. REPAIRED IAW REO.

Part: STRUCTURE — DAMAGED (BS 559) · airframe 30,176 hrs · 29,343 cycles

BS 559 LOWER CAP ANGLES BL 9.00 & 18.00 LT & RT. REPAIRED IAW REO.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHT) · airframe 28,862 hrs · 27,860 cycles

CABIN CEILING, AFT MOST EMERGENCY FLOOD LIGHT INOPERATIVE. TROUBLESHOT THE FLOOD LIGHT, FOUND WIRING INCORRECTLY CONNECTED TO LIGHT ASSY. CORRECTED THE WIRING IAW AMM 33-51-16. OPS CHECK GOOD.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 28,863 hrs · 27,862 cycles

DURING OVERNIGHT MAINTENANCE, MAINTENANCE FOUND CABIN CEILING AFT MOST EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE TROUBLESHOT CABIN AFT MOST EMERGENCY FLOOD LIGHT, FOUND WIRING INCORRECTLY CONNECTED TO LIGHT ASSY. CORRECTLY ATTACHED WIRING TO LIGHT ASSY IAW AMM 33-51-16. OPS CHECKED GOOD. DMIL CLEARED AND PLACARD REMOVED. ACFT OK FOR CONTINUED SERVICE.

Part: SKIN — BURNED (BS 265) · airframe 27,900 hrs · 26,802 cycles

8 RIVETS WITH BURN MARKS ON THEM AT FS 265 AND STR 24L, MARKED L. 5 BURN MARKS CONTAINED TO SURFACE FINISH DAMAGE ONLY. RESTORED SURFACE FINISH TO BURN MARKS IAW SRM 51-25-16. REMOVED 3 DAMAGED RIVETS AT FS 265 AND STR 24L IAW SRM 51-42-06. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HOURS. RE-INSPECT EVERY 1200 FLIGHT HRS. ALL WORK IAW REO 601R-53-00-115 REV E. TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 169) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON SKIN EDGE 4" AFT OF FS 169, JUST UNDER STR 25L, MARKED C. REMOVED DAMAGE ON SKIN EDGE 4" AFT OF FS 169 JUST UNDER 25L IAW SRM 51-12-00. DAMAGE IS OUT OF LIMITS IAW SRM 53-00-31. BLEND 0.65" X 0.15" X 0.015". COMPLIED WITH DISPOSITION IAW EA 25-2016-078. RESTORED SURFACE FINISHES SRM 51-26-16. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 310-333) · airframe 27,900 hrs · 26,802 cycles

2 BURN MARKS ON RIVETS ON STR 23L BETWEEN FS 310 - 333. REMOVED 2 FASTENERS. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENERS, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HOURS. RE-INSPECT EVERY 1200 FLIGHT HRS. ALL WORK IAW REO 601R-53-00-115, REV E. TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 250-265) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON RIVET ON STR 24L BETWEEN FS 250/265, MARKED K. REMOVED DAMAGED RIVET ON STR 24L BETWEEN FS 250/265 IAW SRM 51-42-06. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115 REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HOURS. RE-INSPECT EVERY 1200 FLIGHT HOURS. ALL WORK IAW REO 601R-53-00-115, REV E. TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 235) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON RIVET ON FS 235 BETWEEN STR 25L/26L, MARKED I. REMOVED DAMAGED RIVET ON FS 235 BETWEEN STR 25L/26L IAW SRM 51-42-06. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115 REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HOURS. RE-INSPECT EVERY 1200 FLIGHT HOURS. ALL WORK IAW REO 601R-53-00-115 REV E, TEMP REPAIR TYPE, NR 3 AND SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 265-280) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON RIVET ON STR 23L BTWN F.S. 265 - 280. REMOVED DAMAGED RIVET ON STR 23L BETWEEN FS 265/280 IAW SRM 51-42-06, DAMAGE CONTAINED TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE,PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E, REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HRS. RE-INSPECT EVERY 1200 FLIGHT HRS. ALL WORK IAW REO 601R-53-00-115, REV E. TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 202) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON RIVET ON FS 202.75, 1" ABOVE STR 26L, MARKED E. REMOVED DAMAGED RIVET ON FS 202.75, 1" ABOVE STR 26L IAW SRM 51-42-06. FOUND DAMAGE TO BE CONTAINED TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HOURS. RE-INSPECT EVERY 1200 FLIGHT HOURS. ALL WORK IAW REO 601R-53-00-115, REV E TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 202) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON RIVET 4" AFT OF FS 202.75 AND 1" ABOVE STR 26L, MARKED F. REMOVED DAMAGED RIVET 4" AFT OF FS 202.75 AND 1" ABOVE STR 26L IAW SRM 51-42-06. FOUND DAMAGE TO BE CONTAINED TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HOURS. RE-INSPECT EVERY 1200 FLIGHT HOURS. ALL WORK IAW REO 601R-53-00-115 REV E, TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 280) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON RIVET ON STR 22L AND FS 280, MARKED P. REMOVED DAMAGED RIVET ON STR 22L AND FS 280 IAW SRM 51-42-06. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HRS. RE-INSPECT EVERY 1200 FLIGHT HRS. ALL WORK IAW REO 601R-53-00-115, REV E. TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 220-235) · airframe 27,900 hrs · 26,802 cycles

2 BURN MARKS BETWEEN FS 220/235 AND STR 25L/26L, MARKED H. REMOVED DAMAGE FROM DAMAGED LOCATION 1 IAW SRM 51-12-00, DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-31. REMOVED DAMAGED RIVET FROM DAMAGE LOCATION 2 IAW SRM 51-42-06, FOUND DAMAGE TO BE CONTAINED TO RIVET ONLY. MATERIAL REMOVED WAS .600" L X .600" W X .009" D. MEASURED REMAINING MATERIAL THICKNESS AT DAMAGED LOCATION H IAW SRM 51-12-00 AND SRM 53-11-31. MB7011995 03/13/2016 AT 17:00. MEASURED REMAINING MATERIAL AT LOCATION H= 0.054". RECEIVED STS EA 25-2016-078 AND COMPLIED WITH DISPOSITION IAW EA 25-2016-078. RESTORED SURFACE FINISHES. DAMAGE LOCATION H BLEND OUT. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY FOR DAMAGE LOCATION, H DAMAGE RIVET. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HOURS. RE-INSPECT EVERY 1200 FLIGHT HOURS. ALL WORK IAW REO 601R-53-00-115 REV.E. TEMP REPAIR TYPE NR 3 AND SOP 5719, H DAMAGE RIVET. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 250-265) · airframe 27,900 hrs · 26,802 cycles

3 RIVETS WITH BURN MARKS ON STR 23L BETWEEN FS 250 - 265. REMOVED 3 DAMAGE RIVETS ON STR 23L BETWEEN FS 250/265 IAW SRM 51-42-06, DAMAGE CONTAINED TO RIVET ONLY. INSTALLED 3 TEMP FASTENERS, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3, TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HRS. RE-INSPECT EVERY 1200 FLT HOURS. ALL WORK IAW REO 601R-53-00-115, REV E TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 280-295) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON RIVET ON STR 23L, BETWEEN FS 280 - 295. REMOVED DAMAGE RIVET ON STR 23L BETWEEN FS 280/295 IAW SRM 51-42-06, DAMAGE CONTAINED TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE,PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3, TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HRS. RE-INSPECT EVERY 1200 FLIGHT HRS. ALL WORK IAW REO 601R-53-00-115, REV E. TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDER A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 202-220) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON SKIN BETWEEN FS 202.75/220 AND STR 25L/26L, MARKED G. REMOVED DAMAGE BETWEEN FS 202.75/220 & STR 25L/26L IAW SRM 51-12-00. DAMAGE IS OUT OF LIMITS IAW SRM 53-00-31. BLEND 0.5" X 0.5" X 0.006. COMPLIED WITH EDDY CURRENT IAW NDTM 51-20-06. NO DEFECTS NOTED AT THIS TIME. MEASURED REMAINING MATERIAL AT LOCATION G= 0.057". COMPLIED WITH DISPOSITION IAW EA 25-2016-078. RESTORED SURFACE FINISHES SRM 51-26-16. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 295-310) · airframe 27,900 hrs · 26,802 cycles

BURNS ON STR 23L BETWEEN FS 295 - 310. REMOVED DAMAGE FROM BURNS ON STR 23L BETWEEN FS 295/310 IAW SRM 51-12-00. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-31. MATERIAL REMOVED WAS .600"L X .600"W X .009" DEEP. NR 2: .600"L X .600"W X .009" DEEP, NR 3: .600"L X .600"W X .009" DEEP. MEASURED REMAINING MATERIAL THICKNESS AT DAMAGE LOCATION R(1), R(2), R(3) IAW SRM 51-12-00 AND SRM 53-21-31. MEASURED REMAINING MATERIAL AT LOCATION R(1) = 0.054", R(2) = 0.054", R(3) = 0.054". COMPLIED WITH DISPOSITION IAW EA 25-2016-078. INSTALLED 01 FASTENER. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 250) · airframe 27,900 hrs · 26,802 cycles

2 RIVETS WITH BURN MARKS ON FS 250 AND STR 24L, MARKED J. REMOVED DAMAGED RIVETS ON F 250 AND STR 24L IAW SRM 51-42-06. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HRS. RE-INSPECT EVERY 1200 FLIGHT HOURS. ALL WORK IAW REO 601R-53-00-115, REV E. TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDER A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 409) · airframe 27,900 hrs · 26,802 cycles

BURN MARK ON RIVET ON STR 23L AND BS 409. REMOVED FASTENER. FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER, ALODINE, PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115, REV E. REPAIR TYPE 3 TEMPORARY. VALID TILL NEXT C-CHECK IN 4153 FLIGHT HRS. RE-INSPECT EVERY 1200 FLIGHT HRS. ALL WORK IAW REO 601R-53-00-115, REV E. TEMP REPAIR TYPE NR 3 AND SOP 5719. THIS IS CONSIDER A MAJOR REPAIR IAW GMM 5-3.

Part: SKIN — BURNED (BS 364) · airframe 27,900 hrs · 26,802 cycles

DEFECT DESCRIPTION: BURN MARK ON RIVET ON BS 364 BTWN STR 21-22. REMOVED FASTENER.FOUND DAMAGE CONTAIN TO RIVET ONLY. INSTALLED TEMP FASTENER ,ALODINE,PRIMED AND PAINTED. ALL WORK IAW REO 601R-53-00-115 REV.E.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 27,061 hrs · 25,912 cycles

CABIN SEAT RAIL, RBL9 CORRODED AT FS 364.00. BLENDED CORRODED AREA AND FOUND TO BE OUT OF LIMITATIONS IAW SRM 53-21-49-01. REMOVED CABIN SEAT RAIL RBL9 AT FS 364.00 IAW AMM 53-01-11-000-802. INSTALLED 1 EA SERVICEABLE SEAT RAIL, RBL9 AT FS 364.00 IAW AMM 53-01-11-400-802.

Part: STRUCTURE — CRACKED (BS 621-625) · airframe 27,061 hrs · 25,912 cycles

UPON REMOVAL OF BRACKET BETWEEN FS 621 - 625 LT SIDE, FOUND Z-MEMBER CRACKED. REMOVED Z-MEMBER IAW SRM 51-42-21, LOCATED AND DRILLED FASTENER LOCATIONS IN NEW Z-MEMBER IAW SRM 51-40-11. INSTALLED NEW SERVICABLE Z-MEMBER IAW SRM 51-42-06-00. REMOVED U BRACKET IAW SRM 51-42-06 AND SRM 51-42-21. INSTALLED NEW SERVICABLE 4-CHANNEL BRACKET IAW SRM 51-42-21-00 AND 51-42-06-00.

Part: RIB — CRACKED (RT WING) · airframe 27,061 hrs · 25,912 cycles

RT BATTERY RIB CRACKED AT WS 56.30 INSIDE RT WHEEL WELL. COMPLIED WITH EC/TC REO 601R-57-51-046, REPAIR NR 3.

Part: RIB — CRACKED (LT WING) · airframe 27,061 hrs · 25,912 cycles

LT BATTERY RIB CRACKED AT WS 56.30 INSIDE LT WHEEL WELL. COMPLIED WITH ECTC REO 601R-57-51-046, REPAIR NR 2.

Part: ANGLE — CRACKED (BS 280) · airframe 27,061 hrs · 25,912 cycles

CRACKED CLIP AT RBL9, FS 280 INBD SIDE. R & R DAMAGED CLIP ON FS 280 AT RB 69 IN REF TO SRM 51-42-21-00.

Part: ANGLE — CRACKED (BS 280) · airframe 27,061 hrs · 25,912 cycles

CRACKED CLIP AT LBL9, FS 280.00 INBD SIDE. R & R DAMAGED CLIP ON FS 280 AT LBL9 IN REF TO SRM 51-42-21-00.

Part: FRAME — CORRODED (BS 349) · airframe 27,061 hrs · 25,912 cycles

FS 349, FRAME CORRODED BETWEEN RBL 42 AND RBL 27. REMOVED RT SIDE WINDSCREEN SUPPORT ANGLE IAW SRM 51-42-06, FOUND TO BE CORRODED OUT OF LIMITS. DRILLED UP NEW SERVICEABLE RT SIDE WINDSCREEN SUPPORT ANGLE IAW SRM 51-40-11-00. REMOVED CORROSION DAMAGE IAW SRM 51-21-06. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00. FORMED REPAIR ITEMS -1, -2, & -3 IAW REO 601R-53-21-2657 & SRM 51-24-16. INSTALLED NEW RT SIDE WINDSCREEN SUPPORT ANGLE IAW SRM 51-42-21 51-42-13. COMPLIED WITH EC/TC REO 601R-53-21-2657. FABRICATED LOCATED DRILLED & INSTALLED ALL REPAIR PARTS IAW REO 601R-53-21-2657 SRM 51-42-21 51-42-13.

Part: HINGE — GOUGED (PAX DOOR) · airframe 27,061 hrs · 25,912 cycles

ROLL PIN IN PAX DOOR HINGE PIN HAS MIGRATED AND GOUGED. THE PIANO HINGE ON THE FUSELAGE SIDE. COMPLIED WITH EC/TC, REO 601R-53-21-814.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 27,061 hrs · 25,912 cycles

RIGHT FLOOR SUPPORT CORRODED AT RBL 42, BS 319.70. BLENDED AREA IS OUT OF LIMITS IAW REO 601R-53-0053. REPAIRED THE FLOOR SUPPORT BETWEEN BS 280 - 409+128 IAW REO 601R-53-00-530, REV A.

Part: SKIN — CHAFED (LT AILERON) · airframe 27,061 hrs · 25,912 cycles

LT AILERON CHAFED ALL ALONG L/E TOP SIDE. COMPLIED WITH REO 601R-57-60-013. BLENDED AREAS ARE WITHIN LIMITS IAW REO 601R-57-60-013.

Part: BRACKET — CRACKED (BS 625-627) · airframe 27,061 hrs · 25,912 cycles

BRACKET CRACKED AT BETWEEN BS 627 - 625 ON LT SIDE MAC32QC 9/2/15 (KF). REMOVED THE BRACKET IAW SRM 51-42-21. LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-11. INSTALLED NEW BRACKET IAW SRM 51-42-21.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 26,857 hrs · 25,702 cycles

LIGHTED FLOOR-LEVEL EXIT SIGN BY SERVICE DOOR DAMAGED. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,612 hrs · 24,425 cycles

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

Part: BULKHEAD — CRACKED (AFT) · airframe 25,070 hrs · 23,861 cycles

AFT PRESSURE BULKHEAD CRACKED AT LBL 27.5 WL 130 AT END OF DOOR TRACK, CRACK APPEARS TO EXTEND UNDER TRACK. EXPOSED CRACK IS .9.

Part: CHARGER — INOPERATIVE · airframe 23,688 hrs · 22,509 cycles

CEILING EMERGENCY FLOODLIGHT NR 2 AT BS 409+ 86 AND NR 4 AT BS 559+71 INOPERATIVE. TROUBLESHOT SYS, AND FOUND NR 4 BATTERY CHARGER FAULTY. REPLACED AND PERFORMED TEST OF NR 4 BATTERY CHARGER ASSY IAW AMM 33-51-04-740-801 AND SUBTASK 33-51-04-740-004. OPS TESTED GOOD.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 23,678 hrs · 22,500 cycles

FWD WALL ATTACHMENT BRACKET CRACKED. REPLACED BRACKET IAW VCMM 53-10-02.

Part: SUPPORT ANGLE — CORRODED (DOOR SILL) · airframe 23,678 hrs · 22,500 cycles

ASD LOWER SILL SUPPORT ANGLE CORROSION AROUND PROXIMITY SWITCH AND GROUNDING STUD. INSTALLED LOWER ASD SILL IAW SRM 51-42-21-00 AND SRM 51-42-13-00.

Part: SKIN — DAMAGED (LT WING) · airframe 23,688 hrs · 22,509 cycles

FOUND ONE HOLE ON LT WING OVERSIZED. COMPLIED WITH REO 601R-57-21-2035, REV P1. MAJOR REPAIR

Part: SKIN — DAMAGED (RT WING) · airframe 23,688 hrs · 22,509 cycles

FOUND ONE HOLE ON RT WING OVERSIZED. COMPLIED WITH REO 601R-57-21-2034, REV P1. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 23,688 hrs · 22,509 cycles

SEAT TRACK RBL 9, SEGMENT FS 409+128 TO 559+4 CORRODED AT SEVERAL AREAS. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485. R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,678 hrs · 22,500 cycles

SEAT TRACK LBL 9, FS 559+4 TO 559+85 CORRODED AT SEVERAL AREAS. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802.

Part: INTERCOSTAL — CRACKED (BS 654-672) · airframe 23,683 hrs · 22,506 cycles

INTERCOSTAL BETWEEN FS 654.0 AND 672 S4L CRACKED. REMOVED INTERCOSTAL IAW SRM 51-42-20. INSTALLED INTERCOSTAL IAW SRM 51-42-06 AND DWG PL 601RJ5210.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,688 hrs · 22,509 cycles

SEAT TRACK RBL 9 FS 559+4 TO 559+85 CORRODED. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 23,684 hrs · 22,507 cycles

SEAT TRACK LBL 9 FS 399 - 409+128 CORRODED. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 364-398) · airframe 23,684 hrs · 22,507 cycles

SEAT TRACK RBL 9 FS 364 TO 398 CORRODED. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,683 hrs · 22,506 cycles

SEAT TRACK UNDER LAVATORY AT RBL 27 AND FS 559+80 AND FORWARD IS CORRODED. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: ISOLATOR — BROKEN (AFT PRSRE BLKHD) · airframe 23,677 hrs · 22,499 cycles

REAR PRESSURE BULKHEAD FWD FACE HAS BROKEN NUTPLATE ISOLATOR AT RBL 9.0. R & R ISOLATOR ON AFT PRESSURE BULKHEAD AT RBL 9 IAW SRM 51-42-13-00.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 23,683 hrs · 22,506 cycles

RIGHT SIDE SEAT TRACK SEGMENT CORRODED BETWEEN FS 409+112 AND 449.85. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 20-21-00 & 53-01-11-000-802, AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,683 hrs · 22,506 cycles

SHORT 8 INCH SEAT TRACK CORRODED BETWEEN FS 559+80 AND 559+96 AT RBL 9. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485.

Part: ISOLATOR — BROKEN (AFT PRESSURE BHD) · airframe 23,677 hrs · 22,499 cycles

REAR PRESSURE BULKHEAD FWD FACE HAS (2 EA) BROKEN NUTPLATE ISOLATORS AT LBL 18.0. R & R ISOLATORS ON AFT PRESSURE BULKHEAD FWD FACE AT LBL 18 IAW SRM 51-42-13-00.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 23,688 hrs · 22,509 cycles

SEAT TRACK LBL 9, FS 409+129 TO 559+4 CORRODED. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: ISOLATOR — BROKEN (AFT PRSRE BLKHD) · airframe 23,677 hrs · 22,499 cycles

REAR PRESSURE BULKHEAD FWD FACE HAS BROKEN NUTPLATE ISOLATOR AT LBL 36.20. R & R ISOLATOR ON AFT PRESSURE BULKHEAD AT LBL 36.20 IAW SRM 51-42-13-00.

Part: ISOLATOR — BROKEN (AFT PRSRE BLKHD) · airframe 23,677 hrs · 22,499 cycles

REAR PRESSURE BULKHEAD FWD FACE HAS BROKEN NUTPLATE ISOLATOR AT RBL 36.20. R & R ISOLATOR ON AFT PRESSURE BULKHEAD AT RBL 36.20 IAW SRM 51-42-13-00.

Part: ANGLE — CRACKED (BS 625) · airframe 23,677 hrs · 22,499 cycles

CRACKED ANGLE FS 625 RT SIDE, REMOVED CRACKED ANGLE AT FS 625 RT SIDE IAW SRM 51-42-20-001-001-A01. INSTALLED NEW ANGLE AT FS 625 RT SIDE ALL WORK DONE IAW SRM 51-42-20.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 23,677 hrs · 22,499 cycles

AFT CARGO DOOR LOWER SILL CORRODED REPAIRED IAW REO 601R-53-00-526.

Part: SEAT TRACK — CORRODED (BS 364-398) · airframe 23,684 hrs · 22,507 cycles

SEAT TRACK LBL 9 FS 364-398 CORRODED. NEW SEAT TRACK FABRICATED IAW GREO 601R-53-00-485. R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,688 hrs · 22,509 cycles

SEAT TRACK LBL 9 FS 559+86 TO 559+94 CORRODED. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485. R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 559.72) · airframe 23,683 hrs · 22,506 cycles

LEFT SIDE SEAT TRACK SEGMENT CORRODED AT FS 559.72. R & R SEAT TRACK WITH NEW SEAT TRACK IAW AMM 20-21-00 & 53-01-11-000-802 & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 23,684 hrs · 22,507 cycles

SEAT TRACK RBL 9 FS 399 - 409+128 CORRODED. SEAT TRACK FABRICATED IAW GREO 601R-53-00-485, R & R SEAT TRACK IAW AMM 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,678 hrs · 22,500 cycles

SEAT TRACK, LBL 9 SEGMENT FS 559+110 TO 559+122 CORRODED. REMOVE CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 20-21-00, AMM 53-01-11-000-802 & 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 23,677 hrs · 22,499 cycles

SHORT 10 INCH SEAT TRACK CORRODED BETWEEN FS 559 + 112 AND FS 574 AT RBL 9. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485, REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: BRACKET — CRACKED (FLAP CABLE) · airframe 23,683 hrs · 22,506 cycles

CABLE ROLLER BRACKET CRACKED AT FS 484.00 AND LBL 36L. R & R CABLE ROLLER BRACKET AT FS 484.00 AND LBL 36L IAW REO 601R-53-41-059, REV."B" AND REO 601R-53-41-1744. MAJOR REPAIR.

Part: SHIELD — DAMAGED (WIRE HARNESS) · airframe 23,677 hrs · 22,499 cycles

RT IDG HARNESS T2 & T3 CLOTH SHIELDING HAS HOLES. REPAIRED DAMAGED CLOTH SHIELDING IAW REO 601R-24-21-004, NO DAMAGE FOUND TO WIRE CORE. COMPLIED WITH ECTC REO 601R 24-21-004 AND GREO 601R-24-21-004, REV A. MAJOR REPAIR.

Part: SUPPORT ANGLE — CORRODED (DOOR SILL) · airframe 23,677 hrs · 22,499 cycles

ASD LOWER SILL SUPPORT ANGLE CORROSION AROUND PROX SWITCH AND GROUNDING STUD. REMOVED LOWER SILL ANGLE IAW SRM 51-42-06, 51-42-13 AND 51-42-21. DRILLED AND INSTALLED LOWER SILL ANGLE IAW SRM 51-40-11-00.

Part: SHIELD — DAMAGED (LT IDG HARNESS) · airframe 23,677 hrs · 22,499 cycles

LT ENINE IDG HARNESS CLOTH SHIELDING HAS HOLES. REPAIRED DAMAGED CLOTH SHIELDING ON LT ENG IDG WIRES IAW REO 601R-24-21-004, NO DAMAGE FOUND TO WIRE CORE. COMPLIED WITH ECTC REO 601R-24-21-004 AND MFG REV A. MAJOR REPAIR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,804 hrs · 20,551 cycles

EXTERNAL EMERGENCY LIGHT 7 AFT OF THE LT OVERWING EXIT INOPERATIVE. RELAMPED EXTERIOR EMERGENCY LIGHT 7 AFT OF THE LT OVERWING EXIT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,957 hrs · 19,675 cycles

EMERGENCY EXIT LIGHT INOPERATIVE IAW AMM 33-51-21. R & R EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 20,957 hrs · 19,675 cycles

EMERGENCY LIGHTS (FWD) ARE INOPERATIVE. R & R BATTERY CHARGER ASSY NR 1 IAW AMM 33-51-05. R & R FUSES AT BATTERY PACK NR 2 IAW VCMM 33-22-11.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 20,286 hrs · 18,930 cycles

HYD SYS 1 HAS LOW PRESSURE IN FLIGHT. EMERGENCY DECLARED. R & R ENGINE DRIVEN PUMP ON SYS 1A IAW AMM 29-11-01. OPS AND LEAK CHECKED GOOD.

Part: LINE — LEAKING (HYDRAULIC SYSTEM) · airframe 20,183 hrs · 18,813 cycles

DURING FLIGHT, HYD NR 1 LOW PRESSURE CAUTION MESSAGE. ACFT DIVERTED AND AN EMERGENCY WAS DECLARED. REPLACED HYD LINE SYS NR 1 BETWEEN ACMP AND EDP RETURN LINE FIREWALL IAW AMM 29-11-00.

Part: OIL SYSTEM — FLUCTUATES (RT ENGINE) · airframe 19,939 hrs · 18,524 cycles

RIGHT ENGINE OIL PRESSURE EICAS WARNING INDICATION APPEARED IN FLIGHT ON AND OFF. OIL PRESSURE FLUCTUATED BETWEEN 25-38PSI AT 90 N1. LANDED AT IDLE. EMERGENCY DECLARED. COMPLIED WITH SPECIAL INSPECTION IAW ENG MANUAL 72-00-00, PARA 3J, ADDED 6 QTS OF OIL, INSPECTED MAGNECTIC CHIP DETECTOR AND OIL FILTER, NO FURTHER DEFECTS NOTED. RT ENGINE PLACED ON DAILY INSPECTION OF CHIP DETECTOR INDICATOR FLAG FOR 50 FLT HOURS IAW PARA 3J ITEM F. ACFT PLACED ON 5 DAY OIL WATCH IAW MAINTENANCE CONTROL. PERFORMED ENGINE RUN, OPS AND LEAK CHECKED GOOD.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 19,879 hrs · 18,452 cycles

F/A REPORTS EMERGENCY LIGHT COVER LOOSE AT SEAT 1+2 A+B. R & R EMERGENCY FLOOR LIGHT IAW STG M41-10.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,735 hrs · 18,284 cycles

EXIT EMERGENCY LIGHTS INOPERATIVE. R & R BULB ASSY IAW AMM 33-51-21.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 19,702 hrs · 18,255 cycles

ON DESCENT NOTICED CABIN ALT CLIMBING AT 2500 FPM CYCLED PRESSURE CONTROLLERS DID NOT REGAIN CONTROL, ATTEMPTED MANUAL MODE AGAIN NO CONTROL. LANDED WITH EMERGENCY DEPRESS ON IAW QRH. REPOSITIONED DUCT INSULATION FROM LT OUTFLOW VALVE. PERFORMED OPS CHECK OF PRESSURIZATION IAW AMM 21-31-10. DEFER CLEARED. PLACARD REMOVED.

Part: FLOOR SUPPORT — CRACKED (BS 461) · airframe 19,666 hrs · 18,217 cycles

DURING INSPECTION OF THE PRESSURE FLOOR, FOUND FLOOR SUPPORT BRACKET TO BE SUSPECTED TO BE CRACKED AT FS 461, RBL 9. PERFORMED EDDY CURRENT INSPECTION OF FLOOR SUPPORT BRACKET IAW MAC NDT PROCEDURE ET-2. BRACKET CONFIRMED CRACKED, EXCEEDS 50 PERCENT FSH FROM .040. REMOVED FLOOR SUPPORT BRACKET IAW SRM 51-42-06 AND 51-42-21. DRILLED AND INSTALLED NEW FLOOR SUPPORT BRACKET IAW SRM 51-42-21.

Part: ATTACH FITTING — CRACKED (INTERCOSTAL) · airframe 19,666 hrs · 18,217 cycles

CLIP CRACKED ON AFT SIDE FS 621 ON INTERCOSTAL INBD OF LBL 36.20 APPROX STR 15 (MARKED) REMOVED CRACKED CLIP AND REPLACED WITH NEW CLIP PN: 601-35012-51, REF SRM 51-42-21.

Part: LIGHT — DAMAGED (CABIN) · airframe 19,603 hrs · 18,138 cycles

FWD WARDROBE EMERGENCY FLOOR FLOOD LIGHT FIXTURE DAMAGED. R & R FWD WARDROBE EMERGENCY FLOOR FLOOD LIGHT ASSY IAW AMM 33-51-19, OP'S CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,603 hrs · 18,138 cycles

NR 3 CABIN CEILING EMERGENCY LIGHT INOP. RELAMPED NR3 CABIN EMER LIGHT IAW AMM 33-51-16, OP'S CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,306 hrs · 17,798 cycles

AFT MOST CABIN CEILING EMERGENCY LIGHT INOP. RELAMPED AFT MOST CABIN CEILING EMERGENCY LIGHT AS REQUIRED. OPS CK GOOD IAW AMM 33-51-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,886 hrs · 17,344 cycles

F/A FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHLIGHT IAW AMM 25-61-00.

Part: BULKHEAD — CRACKED (BS 559) · airframe 18,537 hrs · 16,968 cycles

FS 559 BULKHEAD FAILS NDT WITH AN INDICATION IN WEB AT RBL 18 AND AN INDICATION IN CLIP ANGLE UNDER RBL 9 POST. BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. INSTALLED LT CAP ANGLE AND SPLICE IAW REO 601R-53-41-260. INSTALLED REPAIR PARTS ON LT 559 IAW REO 601R-53-41-260 REV E, REO 601R-53-41-609. PAINTED LT 559 REPAIR IAW SRM 51-25-16. CUT RT LOWER CAP ANGLE AND RT WEB AT FS 559. REMOVED BURRS AND SHARP EDGES ON CUT LINES IAW REO 601R-53-41-260, REV E STEPS 1 AND 2. C/W REO 601R-53-41-260, REV D PERFORMED EDDY CURRENT OF RT FS 559 WEB AND CAP ANGLE CUTLINES IAW NDTM 51-20-06. NO INDICATIONS NOTED.

Part: BULKHEAD — CRACKED (BS 559) · airframe 18,537 hrs · 16,968 cycles

FS 559 BULKHEAD FAILS NDT WITH AN INDICATION IN WEB AT RBL 18 AND AN INDICATION IN CAP ANGLE UNDER RBL 9 POST, BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. C/W EC/TC REO 601R-53-41-260 AND REO 601R-53-41-260, REV E. C/W EC/TC REO 601R-53-41-609 02 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-609, REV B.

Part: BULKHEAD — CRACKED (BS 559) · airframe 18,537 hrs · 16,968 cycles

CONTINUATION FS 559 BULKHEAD FAILS NDT WITH AN INDICATION IN WEB AT RBL 18 AND AN INDICATION IN CLIP ANGLE UNDER RBL 9 POST. BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. INSTALLED LT CAP ANGLE AND SPLICE IAW REO 601R-53-41-260. INSTALLED REPAIR PARTS ON LT 559 IAW REO 601R-53-41-260 REV E, REO 601R-53-41-609. LT 559 REPAIR REQUIRES TOPCOAT AND CIC. PAINTED LT 559 REPAIR IAW SRM 51-25-16. CUT RT LOWER CAP ANGLE AND RT WEB AT FS 559. REMOVED BURRS AND SHARP EDGES ON CUT LINES IAW REO 601R-53-41-260, REV E, STEPS 1 AND 2. C/W REO 601R-53-41-260, REV D PERFORMED EDDY CURRENT OF RT FS 559 WEB AND CAP ANGLE CUTLINES IAW NDTM 51-20-06. NO INDICATIONS NOTED.

Part: BULKHEAD — CRACKED (BS 559) · airframe 18,537 hrs · 16,968 cycles

FS 559, BULKHEAD FAILS NDT WITH AN INDICATION IN WEB AT RBL 18 AND AN INDICATION IN CAP ANGLE UNDER RBL 9 POST. BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED & DISCARDED RBL 9 POST, RBL 18 POST AND DOUBLER 601R32026-183 IAW REO 601R-53-41-260, REV D, SHEET 6, STEP C. FABRICATED RT FS 559 PRESSURE BULKHEAD REPAIR PARTS IAW REO 601R-53-41-206, REV E, STEP 5. LT 559 REPAIR REQUIRES CIC. APPLIED CIC IAW SRM 51-21-11. INSTALLED FS 559 RT REPAIR PARTS IAW REO 601R-53-41-609 REV B AND REO 601R-53-41-260, REV E. APPLIED TOPCOAT AND CIC ON RT 559 REPAIR IAW SRM 51-25-16 AND 51-21-11.

Part: BULKHEAD — CRACKED (BS 559) · airframe 18,520 hrs · 16,950 cycles

FS 559 BULKHEAD FAILS NDT WITH AN INDICATION IN WEB AT RBL 18 AND AN INDICATION IN CAP ANGLE UNDER RBL 9 ASST BOTH GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED ANGLE IAW REO 601R-53-41-260, SHEET 8, NOTES 1 AND 2. PERFORMED EDDY CURRENT IAW NDTM 51-20-06. NO INDICATIONS NOTED. FABRICATED REPAIR PARTS IAW REO 601R-53-41-260.

Part: BULKHEAD — CRACKED · airframe 18,520 hrs · 16,950 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATIONS NOTED APPROX .2" IN LENGTH 50 PERCENT FSH FAILED NDT INSPECTION. REPAIR IAW EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR C/W THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230, REV D. ANGLE PART 56144-4 AND INTERCOSTAL PART 601R35212-97. RII FOUND TO BE SATISFACTORY. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,815 hrs · 16,127 cycles

CEILING EMERGENCY LIGHT NR 2 INOP. R & R LIGHT IN CEILING EMERGENCY LIGHT NR2 WITH A SERVICABLE LIGHT. OPS CHECK GOOD IAW AMM 33-51-16. (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,451 hrs · 15,691 cycles

CABIN CEILING EMERGENCY LIGHTS NR2 AND NR4 INOP. RELAMPED CABIN CEILING EMERGENCY LIGHTS NR 2 AND NR 4 IAW CMM 33-22-89. OPS CK GOOD. RELAMPED CABIN CEILING EMERGENCY LIGHTS NR2 AND NR4 IAW CMM 33-22-89. OPS CK GOOD. (CLOSED)

Part: RELAY — FAILED (THRUST REVERSER) · airframe 16,907 hrs · 15,057 cycles

LT REV UNLOCK CAUTION MESSAGE IN FLT. (EMERGENCY DECLARED) (THRUST REVERSER SYS ) R & R LT RELAY 1K7KE IN JB4 IAW AMM 20-42-00. OPS CK GOOD DEFER CLEARED PLACARD REMOVED. (CLOSED)

Part: LAMP — INOPERATIVE (FLASHLIGHT) · airframe 16,774 hrs · 14,894 cycles

CA AND FA FLASHLIGHT BATTERIES INOP. RELAMPED BOTH CA'S AND FA FLASHLIGHT IAW AMM 25-61-00. OPS CK GOOD. (CLOSED)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,480 hrs · 14,557 cycles

NR 5 EXTERIOR EMERGENCY LIGHT IS INOP. RELAMPED NR 5 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD.

Part: DOOR — STIFF (SERVICE) · airframe 16,047 hrs · 14,050 cycles

SERVICE DOOR VERY DIFFICULT TO OPEN FROM THE INSIDE AND OUTSIDE.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 15,997 hrs · 13,995 cycles

LT SIDE INTERCOSTAL FRAME AT FS 625 IS CRACKED.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 15,997 hrs · 13,995 cycles

RT SIDE INTERCOSTAL FRAME AT FS 625 IS CRACKED.

Part: SEAT TRACK — CORRODED (BS 379-409) · airframe 15,997 hrs · 13,995 cycles

SURFACE CORROSION ON RT SIDE TRACK AT FS 379,FS 409,FS 409+16 FS 409+80 AND FS 409+112.

Part: SEAT TRACK — CORRODED (BS 409-513) · airframe 15,997 hrs · 13,995 cycles

SURFACE CORROSION ON RT SIDE SEAT TRACK AT FS 409+128, FS439, FS473.15, FS484 AND FS513. MARKED WITH GREEN TAPE.

Part: FRAME — CORRODED (BS 333) · airframe 15,997 hrs · 13,995 cycles

CORROSION DAMAGE IN INTERNAL MAIN AVIONICS BAY ON FS333.00 FRAME BETWEEN STRINGERS 26LT AND 26RT (MARKED). REMOVED AND REPLACED LWR 333 FRAME SECTION, IAW SR, 51-42-06 AND RESTORED FINISH TO REPAIR A023 IAW SRM 51-42-11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,997 hrs · 13,995 cycles

FS280.00 FLOOR SUPPORT FRAME CLIP CRACKED AT LBL 9.0 (OTBD CLIP).

Part: STRINGER — CORRODED · airframe 15,997 hrs · 13,995 cycles

CORROSION DAMAGE IN INTERNAL MAIN AVIONICS BAY ON STRINGER 27 JUST FWD OF FS349.00 FRAME. PERFORMED SPLICE REPAIR IAW SRM 53-00-03. REFER TO M-234 FOR WORK ACCOMPLISHED AND RII COMPLIANCE.

Part: CARGO TRACK — CORRODED (BS 559-621) · airframe 15,997 hrs · 13,995 cycles

BAGGAGE RAILS BETWEEN FS 559.00+80 AND FS 621.00 HAS SURFACE CORROSION AROUND SCREW HOLES AND ON SCREW HEADS.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 15,997 hrs · 13,995 cycles

RT FS484.00 INTERCOSTAL CLIPS CRACKED AT RBL27.0 AND RBL36.0. REMOVED CRACKED ANGLE AT RHS FS 484 AT RBL 27.0 AND REPLACED WITH NEW ANGLE. REMOVED CRACKED ANGLE AT RHS 484 AT RBL 36.0 AND REPLACE WITH NEW ANGLE, REFERENCE EC/TC REO 601R-53-41-059 FOR WORK ACCOMPLISHED. REMOVED CRACKED ANGLE AT RT FS 484 AT RBL 27.0 AND REPLACED WITH NEW ANGLE. REMOVED CRACKED ANGLE AT RT 484 AT RBL 36.0 AND REPLACED WITH NEW ANGLE, AK REFERENCE EC/TC REO 601R-53-41-059 FOR WORK ACCOMPLISHED.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 15,997 hrs · 13,995 cycles

LHS FS484.00 INTERCOSTAL CLIP CRACKED AT LBL27.0. REMOVED CRACKED ANGLE AT LHS 484.00 AT LBL 27.0 AND REPLACED WITH NEW ANGLE. REFERENCE EC/TC REO 601R-53-41-059 FOR WORK ACCOMPLISHED.

Part: STRINGER — DAMAGED (BS 319-333) · airframe 15,997 hrs · 13,995 cycles

REMOVED DAMAGED STR SECTION AND REPAIRED BY SPLICING NEW STR SECTION BETWEEN FS 319 AND FS 333. RESTORED FINISH TO REPAIR AREA A023 AND APPLIED CIC AS REQUIRED. WORK PERFORMED IAW SRM 53-00-03 AND 51-21-11, 51-42-06. RII C/W IAW SP 607.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,997 hrs · 13,995 cycles

PAX DOOR AFT SIDE PANEL DRAG ANGLE CRACKED AROUND RIVET (MARKED). COMPLIED WITH REO 601R-52-11-513 TO REPAIR ASD AFT DRAG ANGLE. RII C/W SATISFACTORY IAW SP 607 REF SRM 51-24-21.

Part: PLACARD — CRACKED (CABIN) · airframe 15,997 hrs · 13,995 cycles

LEFT WINDSCREEN "EXIT" PLACARD CRACKED.

Part: PLACARD — MISSING (ESCAPE HATCH) · airframe 15,997 hrs · 13,995 cycles

COCKPIT EMERGENCY ESCAPE HATCH PLACARDS WORN/MISSING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,877 hrs · 13,866 cycles

EMERGENCY FLOOR ELECTROLUMINESCENT TRACK LIGHTING SEGMENT NR 1 INOP.

Part: DOOR — STUCK (SERVICE DOOR) · airframe 15,394 hrs · 13,360 cycles

UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 14,972 hrs · 12,946 cycles

FLAPS FAIL CAUTION MSG, EMERGENCY DECLARED. SKEW DETECTION SYSTEM.

Part: STRUCTURE — CRACKED (BS 202) · airframe 14,957 hrs · 12,926 cycles

FS 202 APPEARS TO BE CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,101 hrs · 12,125 cycles

PAX DOOR AND SERVICE DOOR EMERGENCY EXIT LIGHTS INOP.

Part: LIGHT — BROKEN (CABIN) · airframe 14,093 hrs · 12,119 cycles

EMERGENCY LIGHTING FLOOR STRIP IN FRONT OF SEAT 1B BROKEN.

Part: LAMP — INOPERATIVE (EMERGNECY LIGHTS)

RT SIDE FUSELAGE REAR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED REAR EXTERIOR EMERGENCY LIGHT AT RT SIDE OF FUSELAGE IAW CRJ 200 AMM 33-51-21. OPS CHECK GOOD. (A)

Part: UNKNOWN — ODOR (CABIN) · airframe 12,702 hrs · 10,867 cycles

ROTTEN SMELL IN BACK OF CABIN ON TAKEOFF (APU OFF). PASSENGER COMPLAINED BOTH LEGS, TO AND FROM AVL. FLT 4790 DEL 74 MINS.

Part: SUPPORT BEAM — CRACKED (BS 640-625) · airframe 11,835 hrs · 10,115 cycles

UPPER WEB OF ENGINE SUPPORT BEAM BETWEEN FS 640.0 AND FS 625.00 IS CRACK AT RBL 8.0.

Part: SEAL — CRACKED (RT WING SPOILER) · airframe 11,835 hrs · 10,115 cycles

RIGHT WING SPOILER I/B AND CENTER METAL SEALS ON TRAILING EDGE OF WING ARE CRACKED. 10-30-07 REMOVED IAW SRM 51-42-06 AND SRM 51-42-21. REPLACED IAW SRM 51-42-06 AND SRM 51-42-21.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 11,835 hrs · 10,115 cycles

FOUND ONE ANGLE CRACKED IN MEMBER BEAM OF CARGO DOOR AREA ON PRESSURE BLKD FS 621.

Part: SUPPORT BRACKET — CRACKED (RT MLG WW) · airframe 11,835 hrs · 10,115 cycles

RIGHT MLG BAY HYD SUPPORT BRACKET CRACK. RT MLG BAY HYD. SUPPORT BRAQUET REPLACE IAW SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (BS 280) · airframe 11,835 hrs · 10,115 cycles

FOUR FLOOR SUPPORT BRACKETS CRACKED AT FS 280. 10-30-07 REMOVED AND REPLACED IAW SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (AIRSTAIR DOOR) · airframe 11,699 hrs · 9,994 cycles

ASD AFT FRAME DRAG ANGLE IS CRACKED AT THE MOTOR PULLEY BRACKET.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 11,699 hrs · 9,994 cycles

INSIDE ASD ACCESS PANEL 832BR FOUND CRACK IN THE UPPER RADIUS OF THE AFT INTERCOSTAL. (AS VIEWED FACING ACFT WITH DOOR OPEN). ALSO MARKED ON THE OUTSIDE SKIN AS REFERENCE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 11,343 hrs · 9,615 cycles

ON APPROACH AFTER FLAPS STABILIZED AT 30 DEG RECEIVED FLAPS FAIL CAUTION MSG, C/W QRH PROCEDURES, FLAPS REMAINED AT 30 DEG FOR LANDING. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,645 hrs · 8,907 cycles

EXTERNAL EMERGENCY LIGHT INOP NEAR RT WING MOST FORWARD.

Part: BEAM — CRACKED (FUSELAGE) · airframe 9,660 hrs · 8,031 cycles

BOXBEAM CRACKED LOWER LEFT O/B PANEL CUTOUT.

Part: BEAM — CRACKED (FUSELAGE) · airframe 9,660 hrs · 8,031 cycles

BOXBEAM CRACKED LOWER RIGHT O/B PANEL CUTOUT.

Part: FRAME — CRACKED (BS 640) · airframe 9,660 hrs · 8,031 cycles

RT SIDE FRAME 640 BRACKET HAS EVIDENCE OF CRACKED UPPER SECTION. FABRICATED AND INSTALLED NEW FRAME ANGLE AND 640 DOUBLER ON RT. SIDE IAW SB 601R-53-61. JOB COMPLETE (SUPPLEMENTAL - SDR CLOSED)

Part: FRAME — CRACKED (BS 640) · airframe 9,660 hrs · 8,031 cycles

LT SIDE FRAME 640 BRACKET HAS EVIDENCE OF CRACKED UPPER SECTION. FABRICATED AND INSTALLED NEW FRAME ANGLE AND 640 DOUBLER ON RT. SIDE IAW SB 601R-53-61. JOB COMPLETE (SUPPLEMENTAL - SDR CLOSED)

Part: LIGHT — INOPERATIVE (LT WING) · airframe 8,604 hrs · 7,168 cycles

FOUND LT OVERWING EMERGENCY LIGHT INOP.

Part: BULB — BURNED OUT (GALLEY) · airframe 8,604 hrs · 7,168 cycles

GALLEY EMERG EXIT SIGN HAS BULB OUT.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 8,523 hrs · 7,100 cycles

2EA. EMERGENCY LIGHTS INOP ON RT SIDE OF FUSELAGE.

Part: CONTROLLER — SHORTED (COCKPIT)

DURING DESCENT, A CUP OF WATER WAS DROPPED ONTO THE ADG CONTROL PANEL, FOLLOWED BY THE CREW RECEIVING AMBER MASTER CAUTION MESSAGES INCLUDING TCAS FAIL, L AOA HEAT, AND L PITOT HEAT, AND THE ADG AUTOMATICALLY DEPLOYED. THE CREW THEN RECEIVED A MASTER CAUTION AC ESS BUS FAIL MESSAGE. THE ELECTRICAL SYNOPTIC PAGE DETERMINED THE ADG WAS NOT POWERING THE AC ESS BUS BUT THE CREW WAS ABLE TO RESTORE POWER. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED WITH THE AIRCRAFT LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE ADG CONTROLLER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: PLACARD — DAMAGED (CABIN)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR EXIT PLACARD WAS FOUND NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT PLACARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (DOOR)

DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE C/A. (K)

Part: STEP — BROKEN (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN. MAINTENANCE REPAIRED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN AT THE ATTACHMENT ARM. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

DURING A C-CHECK IN TUS, THE FS 484 INTERCOSTAL, LBL 36, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 484 INTERCOSTAL, LBL 36, IAW ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (BS 484)

DURING A C-CHECK IN TUS, THE CLIP ON THE INTERCOSTAL AT STA 484, RBL 27, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP ON THE INTERCOSTAL, AT STATION 484, RBL 27, IAW ASA EC REO 601R-53-41-059. (M)

Part: INTERCOSTAL — CRACKED (BS 484)

DURING A C-CHECK IN TUS, THE FS 484 INTERCOSTAL, AT BL 36, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 484 INTERCOSTAL, AT BL 36, IAW ASA EO 600-53-0098. (M)

Part: FLOOR SUPPORT — CRACKED (BS 621)

DURING A C-CHECK IN TUS, THE LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE, AT FS 621, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT SIDE FLOOR SUPPORT ANGLE, AT FS 621, IAW ASA EO 600-53-0105. (M)

Part: PROXIMITY SENSOR — FAULTY (RT MLG)

FOLLOWING TAKEOFF FROM ATL-CHO, THE CREW BROUGHT THE GEAR HANDLE TO THE UP POSITION AND A FEW SECONDS LATER RECEIVED A GEAR UP DISAGREE WARNING WITH A WHITE INDICATION APPEARING ON THE RIGHT MAIN GEAR. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SELECTOR VALVE — FAULTY (NLG)

FLT 4126 - DURING CLIMB-OUT FROM ATL-MEI, FOLLOWING ROTATION AND GEAR UP THE CREW SIMULTANEOUSLY RECEIVED MASTR CAUTION AND NOSE WHEEL STEERING (NWS) INOP MESSAGES ACCOMPANIED BY A LOUD SNUBBER SOUND FROM THE NOSE COMPARTMENT LASTING APPROXIMATELY TWO MINUTES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING SELECTOR VALVE AND SWUNG THE NOSE GEAR. MAINTENANCE ALSO REMOVED AND REPLACED BOTH NOSE WHEEL AND TIRE ASSEMBLIES. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — BROKEN (CABIN)

DURING HANGAR MAINTENANCE, THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR IN THE FORWARD LOWER SECTION WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE PASSENGER DOOR IN THE FORWARD LOWER SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT THE ATTACHMENT LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4351 - DURING AGROUND INSPECTION IN MGM, THE RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKES GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PDU — FAILED (TE FLAPS)

FLT 4769 - DURNG APPROACH INTO ILM FROM ATL, THE CREW EXPERIENCED A FLAPS FAILURE WHEN SELECTED AT 20 DEGREES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ILM. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT AND RE-RIGGED THE FLAP SYSTEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SENSOR — OUT OF RIG (TE FLAPS)

DURING APPROACH INTO ATL FROM DAL, APPROXIMATELY 5,000 FT AND 250 KIAS, THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW SELECTED AN 8 DEGREE FLAP SETTING WITH NO NOTABLE FLAP CHANGE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE RE-RIGGED BOTH BRAKE POSITION SENSOR UNITS, RESET AND RAN THE FLAPS THROUGH FIFTEEN CYCLES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)