N841AS

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 36,253 hrs · 32,989 cycles

NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. ACFT RETURNED TO DEPARTURE. GEAR EXTENDED MANUALLY.

Part: ROD — BROKEN (PAX DOOR FLAP) · airframe 36,209 hrs · 32,948 cycles

PAX DOOR WILL NOT OPEN. FOUND PRESSURE RELIEF VENT FLAP ROD BROKEN. REPLACED PAX DOOR VENT FLAP ROD IAW AMM 52-11-15. OPS CHECK GOOD. ACFT OK FOR SERVICE.

Part: SUPPORT BRACKET — CRACKED (CARGO DOOR) · airframe 34,413 hrs · 31,187 cycles

FWD SUPPORT BRACKET IN AFT CARGO DOOR IS CRACKED. R & R FWD SUPPORT BRACKET IAW SRM 51-42-06.

Part: SKIN — DAMAGED (BS 310) · airframe 33,219 hrs · 29,949 cycles

FUSELAGE SKIN DAMAGED AT FS 310 NEAR STR 16L AT SKIN EDGE. REPAIRED IAW GREO 601R-53-21-160, REO 601R-53-21-2447.

Part: FLOOR SUPPORT — CORRODED · airframe 32,433 hrs · 29,130 cycles

RT FLOOR SUPPORT FWD OF SERVICE DOOR CUTOUT IS CORRODED FROM FS 310 TO FS 319. R & R FLOOR SUPPORT ANGLE IAW SRM 51-42-06. LOCATED, DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-11.

Part: RIB — CRACKED (RT WING) · airframe 32,421 hrs · 29,120 cycles

RT WING L/E RIB AT WS 167.46 IS CRACKED AT EDGE OF PICCOLO TUBE CUTOUT. REMOVED CRACKED RIB AT WS 167.46 IAW SRM 51-42-06. INSTALLED NEW RIB, PN 601R12047-4 IAW SRM 51-42-06.

Part: ANGLE — CRACKED (BS 280) · airframe 32,421 hrs · 29,120 cycles

WHILE REPLACING FWD J ANGLE ON FS 280, FOUND INBD CLIPS AT LBL 9 & RBL 9 TO BE CRACKED. REMOVED CLIPS IAW SRM 51-42-21. FABRICATED & INSTALLED INBD CLIPS AT LBL 9 & RBL 9 IAW REO 601R-53-11-926.

Part: POST — CRACKED (BS 409) · airframe 32,433 hrs · 29,130 cycles

FOUND FS 409.00+128 VERTICAL POST BL 0.0 LT & RT SIDE HAVE INDICATIONS NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT AFT FLANGE RADIUS FAILED NDT INSPECTION. REMOVED FS 409+128 BL 0 VERT POST ASSY IAW SRM 51-42-06 & 51-42-21. DRILL/LOCATED NEW SERVICEABLE FS 409+128 BL 0 VERT POST ASSY IAW SRM 51-42-06. INSTALLED NEW POST ASSY IAW REO 601R-53-41-887 AFTER ASSEMBLIED IAW SRM 51-42-06.

Part: BEAM — CORRODED (BS 349) · airframe 32,428 hrs · 29,125 cycles

CORROSION FOUND ON END OF TRANSVERSE BEAM AT FS 349 RT SIDE. REPAIRED IAW REO 601R-53-21-2401.

Part: FITTING — CRACKED (WINDOW) · airframe 32,428 hrs · 29,125 cycles

CO-PILOT SIDE POST LOWER AFT FITTING IS CRACKED (FITTING IS FOR WINDOWS). R & R LOWER AFT FITTING ON THE CO-PILOT'S SIDE POST WITH A NEW SERVICEABLE FITTING IAW SRM 51-42-21.

Part: ANGLE — CORRODED (BS 280) · airframe 32,421 hrs · 29,120 cycles

CORROSION ON FS 280.00 J-ANGLE. R & R WITH NEW SERVICEABLE J-ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 32,428 hrs · 29,125 cycles

CORROSION FOUND ON LOWER SERVICE DOOR SILL ANGLE BETWEEN FS 319 AND FS 349. REMOVED CORRODED SILL FOR REPLACEMENT IAW SRM 51-42-06, 51-42-13 AND 51-42-21. INSTALLED NEW SILL ANGLE IAW SRM 51-42-06, SRM 51-42-13 & SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE SILL ANGLE IAW SRM 51-40-11 AND REMOVED CAP FROM OLD SILL. INSTALLED CAP ON NEW SILL IAW SRM 51-42-13.

Part: FRAME — CORRODED (BS 605) · airframe 32,421 hrs · 29,120 cycles

FRAME 605 IS CORRODED AT STRINGER 27. PERFORMED FRAME REPAIR NR 2 FRAME OUTER FLANGE REPAIR TO FS 605 BETWEEN STR 26-27 IAW SRM 53-00-15, REPAIR NR 2. COMPLIED WITH SRM 53-00-15.

Part: ANGLE — CORRODED (PAX DOORWAY) · airframe 32,433 hrs · 29,130 cycles

PAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-21, 51-42-13 & 51-42-06. LOCATED & DRILLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE IAW SRM 51-42-21, 51-42-06 & 51-42-11.

Part: SKIN — CORRODED (BS 559) · airframe 32,428 hrs · 29,125 cycles

EXTERIOR SKIN PANELS BETWEEN FS 559.00+96 AND 559.00+112 CENTERLINE OF BELLY HAS CORROSION AROUND BUTTON HEAD RIVETS. BETWEEN FS 559+96 AND FS 559+112 BETWEEN STR 26L & STR 26R BLENDED AREAS TO SMOOTH CONTOUR. REPAIRED IAW REO 601R-53-51-215 AND SRM 51-42-06.

Part: BRACKET — CRACKED (BULKHEAD) · airframe 32,414 hrs · 29,111 cycles

REAR PRESSURE BULKHEAD AT FS 621.00 HAS 4 ISOLATOR BRACKET ASSY CRACKED AT RBL 45, 1 BRACKET AT RBL 9, 1 BRACKET AT LBL 9, 1 BRACKET AT LBL 27 AND 1 BRACKET AT LBL 36. REMOVED 8 EA DAMAGED ISOLATORS FROM FS 621 PRESSURE BULKHEAD AND INSTALLED NEW ISOLATORS, PN SL2337-3 IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 364-559) · airframe 32,428 hrs · 29,125 cycles

CORROSION ON LT AND RT AISLE SEAT TRACKS FROM FS 364.00 TO FS 559.00+32. REMOVED LT NR 1 SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED & DRILLED NR 1 LT SEAT TRACK FABBED FROM N126-2075 EXTRUSION IAW REO 601R-53-00-485. INSTALLED LT NR 1 FABBED SEAT TRACK PN 126-7075 IAW REO 601R-53-00-485. REMOVED LT NR 2 SEAT RAIL FOR REPLACEMENT IAW AMM 53-01-11-000-802. LOCATED HOLES & INSTALLED A NEW 601R31032-21 NR 2 LT SEAT TRACK IAW AMM 53-01-11-400-802. REMOVED NR 3 LT SEAT RAIL FOR REPLACEMENT IAW AMM 53-01-11-000-802. LOCATED HOLES & INSTALLED A NEW 601R31032-7, NR 3 LT SEAT TRACK IAW AMM 53-01-11-400-802. REMOVED RT NR 1 SEAT RAIL FOR REPLACEMENT IAW AMM 53-01-11-000-802. FABBED NEW SEAT RAIL FROM EXTRUSION N126-7075. LOCATED & DRILLED & COUNTERSUNK IAW REO 601R-53-00-485. RT 2 & 3 SEAT TRACKS REQUIRE REPLACEMENT. R & R NR 2 & NR 3 SEAT TRACKS IAW SRM 51-41-02 & REO 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485.

Part: RIB — CRACKED (RT WING) · airframe 32,421 hrs · 29,120 cycles

RT BATT RIB ASSY CRACKED AT WS 53.60 APPROX 1" LONG. REPAIRED IAW REO 601R-57-51-046.

Part: ANGLE — CRACKED (BS 621-625) · airframe 32,414 hrs · 29,111 cycles

RT FS 621-625 INTERCOSTAL ANGLE CRACKED AT S14R. LOCATED FASTENER HOLES IN NEW ANGLE IAW SRM 51-40-11 AND INSTALLED NEW ANGLE IAW SRM 51-42-21.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 31,467 hrs · 28,117 cycles

FWD WARDROBE FLOOR FLOOD EMERGENCY LIGHT HAS SEVERAL BULBS INOPERATIVE. RELAMPED FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE. OPS CHECKED GOOD.

Part: LATCH — BINDING (PAX DOOR) · airframe 29,047 hrs · 25,441 cycles

UNABLE TO UNLATCH PAX DOOR FROM OUTSIDE. PERFORMED OPS CHECK OF PAX DOOR HANDLE IAW AMM 52-11-02.

Part: LIGHT — BROKEN (CABIN) · airframe 28,592 hrs · 24,919 cycles

EMERGENCY LIGHT FLOOR LEVEL FLOODLIGHT AT PASSENGER DOOR BROKEN. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT IAW CRJ 200 33-51-19-000-801 & -400-801. EMERGENCY LIGHTS OPS CHECKED OK IAW MM 33-51-00-710-801.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 28,592 hrs · 24,919 cycles

PANEL 232BZ HAS A BROKEN WIRE ON THE EXIT LIGHT PANEL. R & R EXIT LIGHT ON PANEL 232BZ IAW AMM 33-51-10-000-801 AND 33-51-10-400-801. OPS CHECK DUE. PERFORMED OPS CHECK FOR EXIT LIGHT ON PANEL 232BZ IAW AMM 33-51-00-710-805. OPS CHECK GOOD. (CLOSED)

Part: WEB — CRACKED (PAX DOOR)

PAX DOOR AFT WEB IS CRACKED AT FWD EDGE OF STEP 832AT. REPAIRED DAMAGE IAW REO NR: 601R-52-11-1901.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 28,592 hrs · 24,918 cycles

AFT BULKHEAD 621 ISOLATOR IS BROKEN. INSTALLED A NEW SERVICEABLE ISOLATOR ON THE 621 BULKHEAD IAW SRM 51-42-13. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: FLOOR SUPPORT — CORRODED (BS 585-600)

CORROSION ON NUTPLATES OF FLOOR SUPPORT FS 585 - 600 LBL 27.

Part: FLOOR SUPPORT — CORRODED (BS 585-600) · airframe 28,592 hrs · 24,918 cycles

CORROSION ON NUTPLATES OF FLOOR SUPPORT, FS 585.0-600.0 APPROX LBL 27. REMOVED AND REPLACED FLOOR SUPPORT PN 601R35031-3 IAW SRM 51-42-21 AND 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 585-600) · airframe 28,592 hrs · 24,918 cycles

CORROSION ON NUTPLATES OF FLOOR SUPPORT FS 585.00-600.00 (APPROX) LBL 27. REMOVED AND INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3778.

Part: POST — CRACKED (BS 409) · airframe 28,592 hrs · 24,918 cycles

FOUND FS 409.0+128, LBL 18 OTBD VERTICAL POST HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH AT AFT FLANGE RADIUS. FAILED NDT INSPECTION. LOCATED & DRILLED NEW SERVICEABLE VERT POST IAW SRM 51-40-11. INSTALLED POST IAW REO 6 10R-53-41-889 & SRM 51-42-06.

Part: BULKHEAD WEB — CRACKED · airframe 28,592 hrs · 24,918 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .5" IN LENGTH 100 PERCENT FSH FAILED NDT INSP. INSTALLED SHIMS ITEMS 4 & 5 IAW REO 601R-53-61-1541. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 28,592 hrs · 24,918 cycles

FS 484 INTERCOSTAL CLIPS CRACKED AT THE INBD AND OTBD SIDE AT RBL 27 AND RBL 36. REMOVED INBD AND OTBD CLIPS AT FS 484, RBL 27 AND RBL 36 IAW SRM 51-42-21. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL 36.00 IS COMPLETED IAW REO 601R-53-41-059.

Part: SKIN — CRACKED (DOOR) · airframe 28,592 hrs · 24,918 cycles

ASD INNER SKIN CRACKED AT AFT CORNER UNDER STEP. REF TO WVAC JOB 8730025 OP 6000 C/W ECTC REO 601R-52-11-279 IAW REO 601R-52-11-279. MCO CLEARED.

Part: BULKHEAD — CRACKED · airframe 28,592 hrs · 24,918 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .5" LENGTH 100 PERCENT FSH FAILED NDT INSP. REPAIRED PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1541.

Part: POST — CRACKED (BS 409) · airframe 28,592 hrs · 24,918 cycles

FS 409+128 VERTICAL POST IS CRACKED AT LBL 27 BOTTOM RIVET INBD SIDE. VERTICAL POST REMOVED IAW SRM 51-42-06. LOCATED AND DRILLED NEW SERVICEABLE POST IAW SRM 51-40-11. INSTALLED VERTICAL POST IAW REO 601R-53-41-1342.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 28,592 hrs · 24,918 cycles

FS 280.0, ANGLE CRACKED AT RBL 9. INSTALLED NEW ANGLE IAW REO 601R-53-11-926, REV.B.

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 28,592 hrs · 24,918 cycles

PAX DOOR "EXIT" PLACARD IS TORN. REMOVED TORN PLACARD IAW MM 11-30-00-000-801. APPLIED NEW EXIT PLACARD IAW MM 11-30-00-400-801. (CLOSED)

Part: PLACARD — MISSING (CABIN) · airframe 28,592 hrs · 24,918 cycles

CREW ESCAPE HATCH MISSING ALL EXTERIOR MARKINGS. APPLIED CREW ESCAPE EXTERIOR OPERATION MARKINGS IAW AMM TASK 11-10-03-400-801.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,525 hrs · 24,836 cycles

LT OVERWING FWD EMERGENCY LIGHT INOP. R & R LAMP IN LT OVERWING FWD E-LIGHT W/A SERVICABLE LAMP IAW AMM 33-51-21. OPS CHECK GOOD. (CLOSED)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,583 hrs · 23,722 cycles

F/A'S FALSHLIGHT INOP. R & R F/A'S FLASHLIGHT. OPS CHECK GOOD. REF AMM 25-60-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,434 hrs · 22,381 cycles

AFT EMERGENCY LIGHTS ARE INOPERATIVE.

Part: SWITCH — BROKEN (EMERGENCY LIGHT) · airframe 26,158 hrs · 22,101 cycles

EMERGENCY LIGHT SWITCH BROKEN. FLT 5142 DEL 51 MINS.

Part: POST — CRACKED (BS 409) · airframe 24,962 hrs · 20,933 cycles

FS 409.0 VERTICAL POST AT RBL 18 HAS AN INDICATION ON INBD AND OTBD AFT FLANGES AT WL 69.0. INDICATIONS APPROX 1/4" IN LENGTH AT 50% FSH. FAILED NDT INSPECTION. REMOVED VERTICAL POST AT FS 409+128, RBL 18 IAW SRM 51-42-06. FABRICATED REPLACEMENT INBD AND OTBD POSTS IAW SRM 51-24-21. REF. DWG 601R32208. LOCATED AND DRILLED NEW FABRICATED VERTICAL POSTS INBD AND OTBD. ALL WORK PERFORMED IAW SRM 51-40-11. INSTALLED POST PER SRM 51-42-06 AND REO NR 601R-53-41-846.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,962 hrs · 20,933 cycles

CARGO SEAT TRACK SEGMENTS CORRODED RBL AND LBL 27 F.S. 559+80.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,962 hrs · 20,933 cycles

LT FS 718.00 FRAME IS CRACKED BETWEEN STRINGER 10 AND 12. REMOVED LT FRAME AT FS 718.00 IAW SRM 51-42-06. UPON REMOVAL OF FRAME, LOWER SPLICE PLATE WAS DAMAGED (BENT), REQUIRES REPLACEMENT. FABRICATED NEW LOWER SPLICE PLATE IAW DRAWING 600-36030 AND SRM 51-24-16. INSTALLED LT 718 FRAME TO ACFT STRUCTURE AND UPPER AND LOWER SPLICE PLATES IAW SRM 51-42-06. ALL GROUND WIRES, ACM STRUCTURE MOUNTING BOLTS, AND WIRE BUNDLES THAT WERE REMOVED FOR 718 FRAME ACCESS REQUIRE REINSTALLATION. INSTALLED ALL GROUND WIRES AND MOUNTING BOLTS AND WIRE BUNDLES IAW SRM 51-41-00 AND 51-41-02 AND AMM 51-80-00-400-804. PAINTED LT FS 718 FRAME IAW SRM 51-25-01.S 718.00 FRAME IS CRACKED BETWEEN STRINGER 10 AND 12.

Part: SEAT TRACK — CORRODED (BS 559-615) · airframe 24,962 hrs · 20,933 cycles

CARGO BAY SEAT TRACK SEGMENTS CORRODED LBL 9 F.S. 559+112 AND LBL 9 F.S. 615.50 TOTAL OF (2).

Part: BULKHEAD WEB — CRACKED (BS 559) · airframe 24,962 hrs · 20,933 cycles

FS 559 WEB AND CAP ANGLE HAS INDICATIONS NOTED, LT CAP ANGLE AT LBL 18.0, APPROX .3" (100% FSH), AND RT WEB AT WL 59.10, APPROX 1.0" (90% FSH) AND RT WEB AT WL 54.10, APPROX .5" (70% FSH). ALL FAILED NDT INSPECTION. REPAIRED PRESSURE BULKHEAD STRUCTURE FS 559.00, BL 23L-23R IAW REO 601R-53-41-260.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 24,962 hrs · 20,933 cycles

CARGO SEAT TRACK SEGMENTS CORRODED RBL AND LBL 9.0, F.S. 559+90.

Part: DOOR — BINDING (PAX DOOR) · airframe 24,847 hrs · 20,835 cycles

F/A REPORTS PASSENGER DOOR DIFFICULT TO CLOSE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,637 hrs · 20,640 cycles

CAPT FLASHLIGHT INOP.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 24,480 hrs · 20,486 cycles

CRACK FOUND IN GUSSETT AT FS 461.5 OF LT INBOARD SEAT TRACK SUPPORT BEAM.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 23,415 hrs · 19,537 cycles

CLIMBING THROUGH 9000 OUT OF ATL, SUFFERED RIGHT ENGINE VIOLENT BANG AND COMPLETE LOSS OF N1, ITT SPIKED OVER 960 DEG WITH RED ICON. PERFORMED ENG DAMAGE IN FLIGHT QRH PROCEDURE EXPERIENCED SUBSEQUENT SMALLER BANGS WITH ERRATIC N1 PRIOR TO SHUT DOWN , WITH N1 RETURNING TO NIL EACH TIME.---[AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. DEFECT TRANSFERRED TO W/O 89988 N/R 00001 FROM AFDL 372229. DEFECT TRANSFERRED TO W/O 89988 N/R 00001 FROM AFDL 372229. REMOVED AND REPLACED NR 2 ENGINE IAW CRJ 200 AMM 71-00-00.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 23,288 hrs · 19,424 cycles

NR 1 HYD LOW PRESS MSG, RAN FOR APPROX 30 MINUTES. EN ROUTE TO ATL A/C DIVERTED TO ORD DUE TO MTC. EMERGENCY DECLARED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,825 hrs · 18,243 cycles

RIGHT FWD EMERGENCY LIGHT INOP.

Part: BATTERY — DISCHARGED (DEFIBRILLATOR) · airframe 21,774 hrs · 18,199 cycles

DEFIB BATTERY DEAD. AED, AUTOMATIC EXTERNAL DEFIBRILLATOR, AND/OR ASSOCIATED EQUIPMENT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 21,251 hrs · 17,792 cycles

FLAPS FAIL MSG IN FLIGHT FLAPS AT 0 DEG AT FL 300 ORAL WARNING UNIT SOUNDED OVERSPEED IN COCKPIT AND CHIMES IN CABIN. EMERGENCY DECLARED.

Part: LATCH — UNKNOWN (PAX DOOR) · airframe 20,475 hrs · 17,219 cycles

MAIN DOOR LATCH VERY HARD TO DISENGAGE AND HANDLE VERY HARD TO TURN FROM OUTSIDE THE AIRCRAFT.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 20,458 hrs · 17,201 cycles

PAX DOOR WILL NOT CLOSE PROPERLY, OUTER HANDLE INDICATES OUT WITH NORMAL PROCEDURES. FLT 4634 DEL 39 MINS.

Part: SILL — CORRODED (BS 409-559) · airframe 20,409 hrs · 17,160 cycles

LT FUSELAGE PRESSURE DOOR SILL HAS CORROSION FROM FS409+128 TO 559 MULTIPLE LOCATIONS COMPLIED WITH EC/TC REO 601R-53-41-479, NO FURTHER ACTION REQUIRED REF EC/TC REO 601R-53-41-479 ITEM 7.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,409 hrs · 17,160 cycles

RT FUSELAGE PRESSURE DOOR SILL HAS CORROSION FROM FS409+128 TO 559 MULTIPLE LOCATIONS COMPLIED WITH EC/TC REO 601R-53-41-479, NO FURTHER ACTION REQUIRED REF EC/TC REO 601R-53-41-479 ITEM 7.

Part: DOOR TRACK — CRACKED (CARGO DOOR) · airframe 20,409 hrs · 17,160 cycles

FOUND CARGO DOOR TRACK CROSS BEAM MEMBER AFT SIDE BOTTOM ANGLE CRACKED (MARKED).

Part: FITTING — CORRODED (BS 310) · airframe 20,409 hrs · 17,160 cycles

FOUND STA 310 FLOOR FTG AT RBL 45 BADLY CORRODED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 20,409 hrs · 17,160 cycles

FOUND RT CARGO FLOOR TRACK HAS CORROSION (MARKED).

Part: HEAT SHIELD — CORRODED (APU BAY) · airframe 20,409 hrs · 17,160 cycles

BARE METAL AND CORROSION AFT OF APU HEAT SHEILD. NO CORROSION FOUND PAINTED IAW SRM 51-25-01.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 20,409 hrs · 17,160 cycles

FOUND FLOORBEAM AT FS STA 349 LBL 45 HAS CORROSION.

Part: FRAME — CORRODED (BS 333) · airframe 20,409 hrs · 17,160 cycles

CORROSION FOUND AT FUSELAGE FRAME STA 333 IN BELLY OF AIRCRAFT. STARTED BLENDING CORROSION FOUND AT FUSELAGE FRAME STA 333 IN BELLY OF AIRCRAFT IAW CRJ 200 SRM 51-21-06. COMPLIED WITH UT THICKNESS CHECK OF BLENDED AREAS IAW CRJ NDTM 51-20-04 FOUND MINIMUM THICKNESS TO BE .038. BEGAN REMOVAL OF 333 FRAME ALL WORK DONE IAW CRJ 200 SRM 51-42-06. FINISHED REMOVING 333 FRAME. DRILLED NEW 333 FRAME ALL WORK DONE IAW CRJ 200 CRM 51-42-06. REAMED ENLONGATED HOLE TO MAX DIA. (.164) TO A ROUND CONDTION AND INSALLED RIVETS IAW CRJ 200 SRM 51-42-06. STARTED INSTALLING FRAME AT FS 333 IAW CRJ 200 SRM 51-42-06. FINISTHED INSTALLING STA. 333 FRAME, INSTALLED BONDING POINTS, AND INSTALLED FLOORBOARD SUPPORT ANGLE,

Part: SEAT TRACK — CORRODED (BS 559) · airframe 20,409 hrs · 17,160 cycles

RT FLOOR SEAT TRACK HAS CORROSION IN AREA BY LAV FUS STA 559+48 TO 559+80 APROX.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 20,409 hrs · 17,160 cycles

FOUND FLOOR SUPPORT ANGLE CORRODED, STA 310-349 AT LOWER SERVICE DOOR SILL (MARKED). REMOVED AND REPLACED FLOOR SUPPORT ANGLE FROM AIRCRAFT.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 20,409 hrs · 17,160 cycles

FS 484 LT SIDE INTERCOSTAL INBD ATTACH CLIP CRACKED AT LBL 27.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 20,409 hrs · 17,160 cycles

FOUND FS 484 LT SIDE INTERCOSTAL CRACKED OTBD SIDE AT LBL 36.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 20,409 hrs · 17,160 cycles

FOUND FS 484 RT SIDE INTERCOSTAL INBD ATTACH CLIP CRACKED AT RBL 27.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 20,409 hrs · 17,160 cycles

FOUND STA 349 TRANSVERSE BEAM CORRODED RT SIDE AT RBL 45 (MARKED). REMOVED CORROSION AND FOUND WITHIN LIMITS IAW CRJ SRM 53-21-15 AND REPLACED AFT ANGLE IAW CRJ SRM 51-42-13.

Part: PLACARD — MISSING (EMERGENCY HATCH) · airframe 20,409 hrs · 17,160 cycles

EMERGENCY CREW HATCH MISSING ALL OUTER PLACARDS.

Part: ATTACH FITTING — CRACKED (BULKHEAD) · airframe 20,409 hrs · 17,160 cycles

RIGHT FS 625 CLIP SUSPECTED CRACKED ON AFT SIDE OF AFT PRESSURE BULKHEAD 3:00. REMOVED, FABRICATED, AND INSTALLED RT FS 625 CLIP ON AFT SIDE OF AFT PRESSURE BULKHEAD 3:00 IAW CRJ 200 SRM 51-24-16, 51-25-01, AND 51-42-06 .050" 2024 T3 PO 10079142.

Part: PANEL — CRACKED (RT WING) · airframe 20,409 hrs · 17,160 cycles

RIGHT WING PLANK CRACKED AT WS 148.19 APPROX (REF AD2002-03-14REP). REPAIRED IAW ALL SRMS.

Part: SIGN — UNSECURE (CABIN) · airframe 20,033 hrs · 16,881 cycles

EXIT SIGN ABOVE SERVICE DOOR UNSECURE AND INOPERATIVE.

Part: SIGN — DAMAGED (CABIN) · airframe 19,033 hrs · 16,081 cycles

EMERGENCY SIGN NEAR FLOOR AT FORWARD DOOR BULKHEAD IS DAMAGED.

Part: ANCHOR FITTING — CRACKED (AIR STAIR DOOR) · airframe 18,830 hrs · 15,924 cycles

ASD AFT ANCHOR FITTING CRACKED.

Part: STEP — DAMAGED (AFT SERVICE DOOR) · airframe 18,604 hrs · 15,761 cycles

ASD BOTTOM STEP SEPARATED AT ATTACHED STAY ROD BRACKET TO STEP COMPOSITE

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION, THE FLIGHT ATTENDANT`S FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT`S FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: PLACARD — MISSING (CABIN)

DURING A C-CHECK IN MCN, THE EMERGENCY ESCAPE PLACARDS ON THE CREW ESCAPE HATCH WERE FOUND TO BE MISSING. MAINTENANCE INSTALLED EMERGENCY ESCAPE PLACARDS ON THE CREW ESCAPE HATCH IAW CRJ AMM 11-20-01. (M)

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING A C-CHECK, THE AVIONICS BAY DOOR HANDLE WAS FOUND TO BE CRACKED. MAINTENANCE WILL REMOVE AND REPLACE THE AVIONICS BAY DOOR HANDLE. (M)

Part: CLIP — CRACKED (BS 280)

DURING A C-CHECK, THE LT OB FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT OB FS 280 CLIP IAW SRM 51-00-00. (M)

Part: BULKHEAD — CRACKED (BS 202)

DURING A C-CHECK IN MCN, THE PRESSURE BULKHEAD AT FS 202.75 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED PRESSURE BULKHEAD AT FS 202.75 IAW BOMBARDIER REO 601R-53-11-583. (M)

Part: FRAME — CRACKED (BS 718)

DURING A C-CHECK IN MCN, THE RIGHT FRAME AT FS 718, STRINGER 11 AND 12, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT SIDE FRAME AT FS 718, STRINGER 11 AND 12, IAW ASA EO 600-53-0066. (M)

Part: CLIP — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE RIGHT INBOARD AND OUTBOARD FS 280 CLIP WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD AND OUTBOARD FS 280 CLIPS IAW CRJ200 SRM 51-42-20. (M)

Part: RIB — CRACKED (LT WING)

DURING A C-CHECK IN MCN, THE LEFT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT BATT RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-0039B. (M)

Part: FRAME — CRACKED (BS 640)

DURING HANGAR MAINTENANCE IN BTR, THE LEFT FS 640, STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT FS 640 FRAME IAW THE CRJ SRM AND DEVIATION BOMBARDIER REO 601R-54-51-011. (M)

Part: LIGHT — MALFUNCTIONED (COCKPIT)

FLT 4537 - DURING CRUISE FROM SHV-ATL, THE CREW NOTICED A STRONG BURNING ODOR FROM THE CAPTAINS MAP LIGHT WHEN IT AS TURNED ON WITH THE LIGHT OPERATING INTERMITTENTLY. THE ODOR DISSIPATED WHEN THE LIGHT WAS TURNED OFF. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS MAP LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BPSU — MALFUNCTIONED (RT WING) · airframe 14,687 hrs

DURING CLIMB-OUT, AT APPROXIMATELY 18,000 FEET, THE CREW RECEIVED A (FLAP FAIL) MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT BRAKE POSITION SENSOR UNIT (BPSU) AND ALSO RIGGED THE LT AND RT FLAP SYSTEM TO ZERO. IN ADDITION, MAINTENANCE RIGGED THE RIGHT BPSU IAW THE MM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: ROLLER — LACK OF LUBE (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS FOUND HARD TO CLOSE. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR UPPER ROLLER LOCKS P/N 6003189534, ADJUSTED THE DOOR HANDLE P/N 601R389643 AND LUBRICATED THE HANDLE ROLLER P/N 601R3189465. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M0

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM UPPER ATTACH ANGLE AT THE FASTENER HOLE WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ENGINE SUPPORT BEAM UPPER ATTACH ANGLE IAW SRM 51-42-20. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 27 AFT CLIP BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 27 AFT CLIP BRACKET IAW ASA EO 600-53-0098. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PASSENGER DORO FORWARD AND AFT HAND RAIL SUPPORT ARM ATTACH ANGLE SILL WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR FORWARD AND AFT HAND RAIL SUPPORT ARM ATTACH ANGLE SILL. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 36 AFT CLIP BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT FS 484 INTERCOSTAL CLIP AT RBL 36 AFT CLIP BRACKET IAW ASA EO 600-53-0098. (M)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE FORWARD INBOARD CORNER LEADING TO THE NUTPLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM AT BL 36.20 ON THE LEFT SIDE IAW ASA EO 600-53-0070. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FRAME FS 718, STRINGERS 10-12 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING FRAME FS 718, STRINGERS 10-12 ON THE RIGHT SIDE IAW ASA EO 600-53-0067A. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT SIDE FS 640 DOUBLER AT STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT SIDE FS 640 DOUBLER AT STRINGER 9 IAW ASA EO 600-53-0075. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SERVICE DOOR INTERCOSTAL ON BOTH SIDES WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR INTERCOSTAL ON BOTH SIDES IAW SRM 51-24-21. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE AFT OUTBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE RACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 IAW SRM 51-40. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE OUTBOARD FLOORBEAM ANGLES AT FS 621, LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE OUTBOARD FLOORBEAM ANGLES AT FS 621, LBL 27 AND RBL 27 IAW ASA EO 600-53-0105. (M)

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL 9 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFT INBOARD BRACKETS AT FS 280, LBL 9 AND RBL IAW SRM 51-40. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM AT BL 0 FIRE LOOP BRACKET IS CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM AT BL 0 IAW ASA EO 600-53-0072. (M)

Part: STEP — CRACKED (PAX DOOR)

DURNG A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP WAS FOUND CRACKED. MAINTENANCE IS REPAIRING THE PASSENGER DOOR TOP STEP IAW SRM 51-73-00. (M)

Part: LAMP — BURNED OUT (FLOOD LT ASSY)

DURING A SCHEDULED INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAIINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

FLT 4736 - UPON TAKEOFF FROM ATL, RETRACTION OF THE FLAPS CAUSED A FLAP FAIL CAUTION MESSAGE TO APPEAR. THE CAPTAIN RAN THE FLAP FAIL CHECKLIST. AN EMERGENCY WAS DECLARED, AND FIRE EQUIPMENT WAS REQUESTED AS A PRECAUTION. AIRCRAFT PERFORMED A ZERO FLAP LANDING IN ICT, WHICH WAS THE ORIGINAL DESTINATION, WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE FLAP SYSTEM. OPERATIONAL CHECK OF THE FLAP SYSTEM GOOD WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. ALL WORKS WAS PERFORMED IAW AD 98-20-01. (M)

Part: TRANSMITTER — INOPERATIVE (RUDDER)

FLT 4737 - CLIMBING THROUGHT 10,000 FEET, STARTED YAWING LEFT AND RIGHT APPROXIMATELY 2-4 DEGREES, BUT LEVELED OFF AT 19,000 FEET. CREW DECLARED AN EMERGENCY AND RETURNED TO ATL. MAINTENANCE REMOVED AND REPLACED THE RUDDER POSITION TRANSMITTER. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: TRANSMITTER — INOPERATIVE (RUDDER)

FLT 4737 - CLIMBING THROUGH 10,000 FEET AIRPLANE STARTED YAWING LEFT AND RIGHT APPROX 2-4 DEGREES, BUT LEVELED OFF AT 19,000 FEET. CREW DECLARED AND EMERGENCY AND RETURNED TO ATL. MAINTENANCE REMOVED AND REPLACED THE RUDDER POSITION TRANSMITTER. OPERATIONAL CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

FLT 4737 - CARGO SMOKE WARNING ISSUED 3 TIMES, THEN AFTER A SHORT INTERVAL, A 4TH CARGO SMOKE WARNING WAS ISSUED. RAN CARGO SMOKE CHECK LIST, FIRED FIRE EXTINGUISHERS, DECLARED AN EMERGENCY, DIVERTED TO MEM. LANDED SAFELY AND EVACUATED AIRCRAFT ON DE-ICE PAD. THERE WAS NO EVIDENCE OF SMOKE OR FIRE - FALSE INDICATION. MAINTENANCE REPLACED CARGO COMPARTMENT FORWARD AND AFT SMOKE DETECTORS, FIRE EXTINGUISHERS AND SQUIBS. ALL SYSTEM OPS CHECKED GOOD, AND AIRCRAFT RELEASED FOR SERVICE. THIS MRR REMAINS OPEN PENDING SHOP REPORT ON SMOKE DETECTORS. (X)

Part: ACTUATOR — FAILED (LT TE FLAP)

TAT - FLT 4700 - PILOT REPORTED FLAPS FAILED ON FINAL APPROACH WHEN SELECTED FROM FLAPS 30 DEGREES TO FLAPS 45 DEGREES. FLAPS FAILED AT 42 DEGREES. LEFT OUTBOARD FLAP WAS FOUND TO BE TWISTED. NR 3 ACTUATOR FAILED TO FULLY EXTEND. LEFT OUTBOARD FLAP AND BOTH ACTUATORS WERE REPLACED. FLAPS WERE RE-RIGGED AND OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (X)