N976EV

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 25,760 hrs · 23,694 cycles

PILOT'S WINDSHIELD CRACKED ENROUTE, ACFT DIVERTED. R & R WINDSHIELD IAW AMM 56-11-01. OPS & LEAK CHECKED GOOD.

Part: BULKHEAD — CRACKED (BS 621) · airframe 24,608 hrs · 22,531 cycles

FS 621 BULKHEAD FAILS NDT WITH AN INDICATION AT CARGO TRACK LBL 27.5 WL 130.0 GREATER THAN 50 PERCENT SCREEN HEIGHT. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541, REV D, DATED: 10/31/2011.

Part: BULKHEAD — CRACKED (BS 621) · airframe 24,635 hrs · 22,556 cycles

FS 621, BULKHEAD FAILS NDT WITH AN INDICATION AT CARGO TRACK LBL 27.5 WL 130.0 GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541, REV D.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 24,608 hrs · 22,531 cycles

FS 621 PRESSURE BULKHEAD FWD FACE HAS 8 BROKEN ISOLATORS AS MARKED WITH ORANGE TAPE. REMOVED 8 BROKEN ISOLATORS AND REPLACED WITH SERVICEABLE PARTS IAW SRM 51-42-10.

Part: DOOR — BINDING (SERVICE) · airframe 23,997 hrs · 21,874 cycles

SERVICE DOOR DIFFICULT TO OPEN FROM THE OUTSIDE. CLEANED EXCESSIVE LUBRICATION FROM OUTER HANDLE. COMPLIED WITH OPS TEST OF THE SERVICE DOOR. OPS CHECK GOOD. ACFT OK FOR SERVICE. REF AMM 52-41-00.

Part: HANDLE — UNKNOWN (SERVICE DOOR) · airframe 23,989 hrs · 21,866 cycles

SERVICE DOOR HANDLE DIFFICULT TO OPEN. PERFORMED OPS CHECK AT SERVICE DOOR IAW AMM 52-11-00. OPS CHECKED GOOD, NO DEFECT NOTED.

Part: SENSOR — OUT OF ADJUST (MLG) · airframe 23,228 hrs · 21,054 cycles

RT GEAR DISAGREE MESSAGE AFTER TAKE OFF. RAN QRH PROCEDURE AND LANDED WITHOUT ISSUE WITH 3 GREEN INDICATED. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. ADJUSTED PROXIMITY SENSOR. PS11GA (PS7GA) AND TARGET ON UPLOCK LATCH IAW AMM 32-32-05. OPS CHECKED GOOD.

Part: BPSU — FAILED (TE FLAPS) · airframe 22,965 hrs · 20,780 cycles

AFTER TAKEOFF, FLAPS FAILED AT 8 DEGREES. COMPLIED WITH QRH. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. R & R RT BPSU IAW AMM 27-51-10. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOOD

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 22,964 hrs · 20,779 cycles

FLAPS FAILED AT 0 ON APPROACH, SKEW DETECTION SYS DEACTIVATED. EMERGENCY DECLARED. REMOVED AND REPLACED RT BPSU AND FECU. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,796 hrs · 19,466 cycles

PAX DOOR EMERGENCY INOPERATIVE. RELAMPED PAX DOOR OUTER EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,744 hrs · 18,334 cycles

EXTERIOR RT AFT EMERGENCY LIGHT IS INOP. R & R EXTERIOR RT AFT EMERGENCY LIGHT LAMP IAW MM 33-51-21-000-810 AND 33-51-21-400-801. OPS CHECKED GOOD.

Part: CARGO TRACK — CORRODED (BS 605-621) · airframe 20,733 hrs · 18,319 cycles

CORROSION AROUND FASTENER HOLES IN CARGO BAY ON RBL 27 FROM FS 605 TO FS 621. FINAL DRILLED, SEALED AND INSTALLED NEW SEAT RAIL IAW SRM 51-42-21, 51-45-06, 51-42-22, 51-23-00, 51-41-04 & REO 601R-53-61-4064. LOCATED CARGO TRACK CAD IAW SRM 51-40-11. REO 601R-53-61-4064 REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR IAW GMM 3-3 PROCEDURES PRIOR TO THE ACFT BEING RETURNED TO SERVICE. TOP COATED AND CORROSION PREVENTATIVE APPLIED TO AREA IAW SRM 51-21-11 & 51-25-21.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 20,733 hrs · 18,319 cycles

CORROSION AROUND FASTENER HOLES IN CARGO BAY ON FLOORBEAM. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-21-06. FOUND OUT OF LIMITS IAW SRM 53-00-00. REMOVED FLOORBEAM IAW SRM 51-42-06. LOCATED, DRILLED, COUNTERSUNK IAW SRM 51-42-06. INSTALLED NEW FLOORBEAM CAP IAW SRM 51-42-06, SRM 51-45-00 & SRM 51-42-15. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED · airframe 20,733 hrs · 18,319 cycles

CORROSION ON CARGO BAY SEAT RAIL AND 2 ANCHOR PLATES AT LBL 18 AND ATTACHING HARDWARE. REMOVED SEVERELY CORRODED SCREWS & TRACKS, ANCHOR PLATES. INSTALLED NEW PART AND HARDWARE, TRACK, 2 EA ANCHOR PLATES IAW SRM 51-41-02. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,733 hrs · 18,319 cycles

FLIGHT DECK FLOOR SUPPORT ANGLE AT FS 280 IS CORRODED. LOCATED AND DRILLED NEW FLOOR SUPPORT FOR FLIGHT DECK FS 280 ANGLE IAW SRM 51-42-06. INSTALLED ANGLE. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: CARGO TRACK — CORRODED · airframe 20,733 hrs · 18,319 cycles

CORROSION ON 1 CARGO BAY SEAT RAIL AND 3 ANCHOR PLATES AND ATTACHING HARDWARE AT LBL 27. REMOVED SEVERELY CORRODED FASTENERS & 1 EA SEAT TRACK, 3 EA ANCHOR PLATES. INSTALLED ALL NEW PARTS & HARDWARE IAW SRM 51-41-02. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: SEAT TRACK — CORRODED · airframe 20,733 hrs · 18,319 cycles

CORROSION ON 2 CARGO BAY SEAT RAILS AT RBL 18 AND ATTACHING HARDWARE. REMOVED CORRODED SCREWS & TRACK SEGMENT. INSTALL NEW TRACK WITH NEW HARDWARE IAW SRM 51-41-02. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 20,733 hrs · 18,319 cycles

CORROSION IN CARGO BAY ON RT FLOOR SUPPORT FROM FS 559+80 - 621. REPAIRED IAW REO 601R-53-61-4074, REV.

Part: SEAT TRACK — CORRODED · airframe 20,733 hrs · 18,319 cycles

CORROSION ON 1 CARGO BAY SEAT RAIL AT RBL 27 AND ATTACHMENT HARDWARE. REMOVED CORRODED SCREWS & CORRODED SEAT RAIL, INSTALLED NEW SEAT RAIL & NEW HARDWARE IAW SRM 51-41-02. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: ANGLE — CRACKED (CARGO DOORWAY) · airframe 20,733 hrs · 18,319 cycles

CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX .3" IN LENGTH. REMOVED CRACKED ANGLE AND REPLACED WITH NEW. INSTALLED NEW ANGLE IAW SRM 51-42-21. MINOR REPAIR.

Part: ANGLE — CRACKED (BS 484) · airframe 20,733 hrs · 18,319 cycles

FS 484, ANGLE AT OBS OF LBL 27 IS CRACKED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLIP (PN 601R31171-17) AT FS 484 OTBD SIDE OF LBL 27 WITH 8 EA NEW HI-LITES IAW SRM CH 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: POST — CRACKED (BS 409) · airframe 20,733 hrs · 18,319 cycles

FS 409+128 VERTICAL POST, RBL 18 FAILS NDT WITH AN INDICATION IN OTBD AFT CHANNEL ON UPPER END. GREATER THEN 50 PERCENT SCREEN HEIGHT APPROX 1" LONG. REMOVED POST IAW SRM 51-42-06 AND INSTALLED SERVICEABLE POST IAW SRM 51-42-06 AND 51-42-22 AND REO 601R-53-41-889.

Part: POST — CRACKED (BS 409) · airframe 20,733 hrs · 18,319 cycles

FS 409+128 VERT POST BL 0 FAILS NDT WITH AN INDICATION IN LT AFT CHANNEL ON UPPER END. GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .1 LONG. REMOVED POST, LOCATED AND DRILLED NEW POST IAW SRM 51-42-06. INSTALLED POST IAW SRM 51-42-06 AND REO 601R-53-41889.

Part: ANGLE — CRACKED (BS 484) · airframe 20,733 hrs · 18,319 cycles

FS 484, ANGLE AT OBS OF RBL 27 IS CRACKED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLIP (PN 601R31171-9) AT FS 484 OTBD SIDE OF RBL 27 WITH 8 EA NEW HI-LITES IAW SRM CH 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 20,733 hrs · 18,319 cycles

FS 621.0 BULKHEAD CARGO PANEL NUTPLATE ISOLATORS MISSING OR BROKEN 3 EA, 1 AT LBL 9, 2ND FROM FLOOR, 1 AT RBL 9 2ND FROM FLOOR, AND 1 AT LBL 27, 4TH UP FROM FLOOR. R & R ISOLATORS AND REINSTALLED ISOLATOR BRACKETS IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 20,733 hrs · 18,319 cycles

CORROSION ON FLOOR SUPPORT AROUND NUTPLATES LBL 27, FS 574.00-621.00. REMOVED FLOOR SUPPORT AND MATCHED DRILL NEW FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3778.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 20,733 hrs · 18,319 cycles

RIGHT FS 349 FLOORBEAM CORRODED ON OTBD END AT SERVICE DOOR ENTRANCE. REPAIRED IAW REO 601R-53-21-1286.

Part: WEB — CRACKED (BS 280) · airframe 20,733 hrs · 18,319 cycles

FS 280.0 WEB IS CRACKED OTBD OF LBL 9, RBL 9. REPAIRED IAW REO 601R-53-11-926, REV B.

Part: INTERCOSTAL — CRACKED (BS 621-625.3) · airframe 20,733 hrs · 18,319 cycles

RIGHT FS 621.00-625.30 INTERCOSTAL AT S14R IS CRACKED NEAR RADIUS APPROX .7" LONG. R & R CRACKED INTERCOSTAL IAW SRM 51-42-21. CLASSIFIED AS A MINOR REPAIR.

Part: CONTROL UNIT — FAILED (SPROILERONS) · airframe 19,537 hrs · 16,890 cycles

"SPOILERONS" MESSAGE IN FLIGHT(EMERGENCY DECLARED). R & R NR 2 SECU IAW AMM 27-61-05. OPS CHECK GOOD, NO DEFECT NOTED AT THIS TIME. (CLOSED)

Part: ECU — FAILED (NLG) · airframe 18,232 hrs · 15,399 cycles

IAW FIM 32-50-00 R & R NWS ECU IAW AMM 32-51-10. OPS CHECK GOOD. (CLOSED)

Part: STEERING SYS — INOPERATIVE (NLG) · airframe 18,232 hrs · 15,399 cycles

AFTER T/O RECEIVED "STEERING INOP" CAUTION MESSAGE. RETURNED TO DEPARTURE. STEERING RESET ON GROUND. (EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,084 hrs · 15,237 cycles

NR 4 CEILING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,084 hrs · 15,237 cycles

RT EXTERIOR NR 2 EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,084 hrs · 15,237 cycles

LT EXTERIOR NR 4 EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,239 hrs · 14,341 cycles

FWD OVERWING EMERGENCY LIGHT INOP.

Part: WIRE — BROKEN (CABIN) · airframe 17,098 hrs · 14,191 cycles

WARDROBE LOWER EMERGENCY LIGHT WIRE HAS END BROKEN OFF.

Part: POST — DAMAGED (FUSELAGE) · airframe 17,098 hrs · 14,190 cycles

LT FS 409.0+128 O/B VERTICAL POST LBL 18.0 HAS AN INDICATION NOTED APPROX .2 INCHES IN LENGTH 50 PERCENT FSH AT WL 69.0. FAILED NDT INSPECTION. REMOVED LBL 18 POST IAW CRJ SRM 51-42-06. FABRICATED OUTBOARD REPLACEMENT POST USING 7075-0 .063" PO 104141/3 IAW SRM 51-24-21. REF DWG 601R32208. PAINTED POST IAW SRM 51-25-01. LOCATED FASTENER HOLES IN NEW O/B SECTION OF POST IAW SRM 51-40-11. ASSEMBLED O/B SECTION TO I/B SECTION OF POST IAW SRM 51-42-06. SEALED AND INSTALLED POST TO THE BULKHEAD IAW SRM 51-42-06 AND 51-42-22. ALSO INSTALLED THE POST IAW REO 601R-53-41-889. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,098 hrs · 14,190 cycles

JOB 8760125 OPERATION 198 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL FITTING HAS AN INDICATION NOTED APPROX .2" IN LENGTH 70% 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: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,098 hrs · 14,190 cycles

FLOOR SEAT TRACK RBL 9, FS 399.5 HAS CORROSION AROUND SCREW HOLES. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-11 AND AMM 53-01-11-420-001B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,098 hrs · 14,190 cycles

FLOOR SEAT TRACK RBL 9, FS 364 HAS CORROSION AROUND SCREW HOLES. REMOVED SEAT TRACK & INSTALLED NEW FLOOR SEAT TRACK IAW AMM 53-01-11.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,098 hrs · 14,190 cycles

RT FS 559 BULKHEAD WEB HAS AN INDICATION NOTED AT WL 59.10 I/B OF RBL 18.0 APPROX .3" IN LENGTH 70% FSH. FAILED NDT INSPECTION. COMPLIED WITH REPAIR AT FS 559 BULKHEAD LT AND RT WHEEL WELL IAW REO 601R-53-41-260 REV.C, STEPS 1-14. PAINTED RT BULKHEAD REPAIRED AREA IAW SRM 51-25-01. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 17,098 hrs · 14,190 cycles

JOB 8760121 OPERATION 139 PAX DOOR AFT DRAG ANGLE IS CRACKED 1.25"L JUST ABOVE THE DOOR ASSIST CABLE PULLEY. REPAIRED PAX DOOR CRACKED AFT DRAG ANGLE PRE-EXISTING REPAIR IAW REO 601R-52-11-513 REV.A.

Part: SILL — CORRODED (BS 325-343) · airframe 17,098 hrs · 14,190 cycles

THE ANGLE ABOVE THE PAX DOOR LOWER SILL IS HEAVILY CORRODED BETWEEN FS 325.5 AND FS 343. CLEANED SURFACE MATERIAL FROM ANGLE ABOVE PAX DOOR LOWER SILL BETWEEN FS 325.5 AND 343. FOUND PEELING PAINT AND VERY MINOR SURFACE CORROSION AFTER PAINT REMOVAL IAW 51-26-00-150-803 AMM. CORROSION DEPTH NOT MEASURABLE. OVER 30 PERCENT OF THE LENGTH IS CORROSION DAMAGED. ANGLE IS OUT OF LIMITS. REMOVED DAMAGE IAW SRM 51-42-06, 51-42-13, AND 51-42-21. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06, 51-42-13, AND 51-42-21.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 16,313 hrs · 13,485 cycles

ON T/O NOSE GEAR WOULD NOT RETRACT, MAINS WERE DASHES. ACFT RETURNED TO DEPARTURE AFTER T/O - EMERGENCY DECLARED. FLIGHT 5412 DEL 122 MINS.

Part: STEP — CRACKED (AIRSTAIR DOOR) · airframe 15,694 hrs · 12,900 cycles

ASD UPPER TOP STEP CRACKED ON AFT SIDE. R&R ASD UPPER TOP STEP IAW 52-11-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,969 hrs · 12,257 cycles

RT FWD EXTERIOR EMER LIGHT INOP RELAMPED RT FWD EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. (B)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 1,487,825 hrs · 12,184 cycles

RT EMERGENCY EXTERIOR OVERWING FWD LIGHT INOP RELAMPED RT EMERGENCY EXTERIOR OVERWING FWD LIGHT IAW CRJ MM 33-51-21. OPS CHECK GOOD [SDR CLOSED](B)

Part: SIGN — BROKEN (CABIN) · airframe 13,392 hrs · 10,973 cycles

EXIT SIGN CAGE ASSEMBLY IN CABIN BROKEN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,238 hrs · 10,843 cycles

CABIN EMERGENCY TRACK LIGHTING AT SEAT 10CD HAS A SEGMENT INOP. (ELECTROLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM)

Part: FLAP — MALFUNCTIONED (WING) · airframe 13,150 hrs · 10,778 cycles

FLAP FAILED AT BASE TO FINAL ATL, 8 SELECTED FAILED AT 2. EMERGENCY DECLARED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 13,144 hrs · 10,774 cycles

FLAPS FAILED AT 0 DEGREES. EMERGENCY DECLARED. SKEW DETECTION SYSTEM. 09-06-07 REMOVED SKEW DET. DUMMY UNIT AND INSTALLED NEW SKEW DETECTION UNIT IAW CRJ AMM 27-51-15. PERFORMED OPS TEST OF SKEW DETECTION SYSTEM IAW TASK 27-51-15-710-802. OPS CK GOOD. PEFORMED OPS TEST OF FLAP SYSTEM TASK 27-54-00-710-801. OPS CK GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,691 hrs · 10,417 cycles

FLAPS FAIL AT 8 DEGREES AFTER TAKEOFF. COMPLIED WITH QRH LANDED FLAPS 8 DEGREES. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLTS 4438, 4797 CX. FOUND BROKEN WIRE ICE81C22BLU PIN B AT 1J9CE...REPAIRED WIRING IAW CRJ WMM CHAPTER 20-11-00. INSTALLED SKEW DETECTION UNIT..FLAP SYSTEM OPS CHECKED GOOD IAW CRJ AMM 27-51-00. CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,682 hrs · 10,411 cycles

FLAPS FAIL CAUTION MSG WITH FLAPS AT 20 DEG. TOWER DECLARED EMERGENCY. EMERGENCY EQUIPMENT AS A PRECAUTION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,610 hrs · 10,358 cycles

RIGHT OBLIQUE ANGLE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,610 hrs · 10,358 cycles

LEFT OBLIQUE ANGLE CRACKED.

Part: ANGLE — CRACKED (BS 621) · airframe 12,610 hrs · 10,358 cycles

CARGO COMPARTMENT NET SUPPORT HAS CRACKED ANGLE AT FS 621.00. [07-24-07] REMOVED CARGO COMPARTMENT NET SUPPORT ANGLE AT FS 621.00 IAW CRJ 200 SRM 51-42-13. DUPLICATED FROM 2024-T3, .050 IAW CRJ 200 SRM 53-61-23. OK TO ALODINE, PRIME, AND PAINT. ALODINED, PRIMED, AND PAINTED IAW CRJ SRM 51-25-16. OK TO INSTALL. INSTALLED ANGLE IAW CRJ SRM 51-42-21. REQUIRES LEAK CHECK. LEAK CHECK GOOD IAW CRJ AMM 21-30-00. NO DEFECTS NOTED AT THIS TIME.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 12,610 hrs · 10,358 cycles

LEFT FS 484 ATTACH FITTING CRACKED AND BL 27.00 (MARKED). [07-23-07] REMOVED DAMAGED CLIP FROM LT FS 484 BL 27.00. DUPLICATED CLIP USING SERVICEABLE ANGLE IAW CRJ SRM 51-24-16. OK TO ALODINE, PRIME, AND PAINT. OK TO INSTALL. ALODINED, PRIMED, AND PAINTED IAW 51-25-16. INSTALLED IAW CRJ SRM 51-42-20.

Part: STRINGER CLIP — CRACKED (BS 484) · airframe 12,610 hrs · 10,358 cycles

RIGHT FS 484 STRINGER CLIP CRACKED AT BL 27.00 (MARKED).

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 12,610 hrs · 10,358 cycles

PAX DOOR FWD ANCHOR FITTING CRACKED. [07-23-07] REPAIRED IAW; AMM 52-11-17, AND AMM 52-11-17.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 12,610 hrs · 10,358 cycles

PAX DOOR AFT ANCHOR FITTING CRACKED. [07-23-07] REPAIRED IAW; AMM 52-11-17, AMM 25-21-01, AND AMM 25-26-02,

Part: ANGLE — CRACKED (RT WING) · airframe 12,610 hrs · 10,358 cycles

RT WING MIDDLE LEADING EDGE, I/B ATTACH ANGLE IS CRACKED. REMOVED RT WING MIDDLE LEADING EDGE I/B CRACKED ATTACH ANGLE. INSTALLED NEW SERVICEABLE ATTACH ANGLE, P/N 600-12025-8, RT WING MIDDLE LEADING EDGE I/B, IAW SRM 51-40-11. W/C 1102.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,905 hrs · 9,834 cycles

FLOOR EMERGENCY TRACK LIGHTING INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,624 hrs · 9,624 cycles

EMERGENCY CEILING LIGHT 1 EACH INOP.

Part: UPLOCK ROLLER — SEIZED (MLG)

DURING APPROACH, THE CREW ATTEMPTED TO LOWER THE LANDING GEAR WHEN THEY RECEIVED A GEAR DISAGREE WARNING AND A NOSE GEAR UNSAFE INDICATION. THE CREW TERMINATED THE DESCENT AND ENTERED A TRAFFIC PATTERN. THE CREW COMPLIED WITH THE QRH AND CYCLED THE GEAR WITH NO EFFECT. THE MANUAL DEPLOY HANDLE WAS PULLED WITH NO EFFECT. AN EMERGENCY WAS DECLARED AND THE EMERGENCY VEHICLES WERE DISPATCHED. THE NR2 HYDRAULIC SYSTEM WAS SHUTOFF AND THE GEAR MANUALLY CAME DOWN. THE AC LANDED SAFELY. MAINT INSPECTED AC AND FOUND NLG UPLOCK ROLLER TO BE SEIZED UP. MAINT TUBED THE NLG UPLOCK ROLLER, AND PERFORMED GEAR SWING 10 TIMES WITH NO DEFECTS NOTED. AC OK FOR SERVICE. (K)