N923EV

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 32,664 hrs · 32,673 cycles

FS280 LBL9 I/B ANGLE CRACKED IN RADIUS, TOP OF ANGLE. (C-CHECK) RO: 10/22/19. FABRICATED NEW ANGLE AND REPLACED IAW REO.

Part: FRAME — CORRODED (BS 513) · airframe 32,664 hrs · 32,673 cycles

* L/H FS 513.00 FRAME HAS SMALL SPOT OF CORROSION APPROX. 1" ABOVE PRESSURE FLOOR SILL AT AFT INB CORNER OF FRAME. (C-CHECK) RO: 10/22/19. PERFORMED BLEND OUT OF CORROSION AT L/H FS 513.00 FRAME 1.0" ABOVE PRESSURE FLOOR SILL I/B CORNER. IAW SRM. FOUND TO BE WITHIN LIMITS. RESTORED FINISH IAW SRM.

Part: PANEL — DAMAGED (STRINGER 20R) · airframe 32,126 hrs · 32,039 cycles

2 ADDITIONAL FASTENER HOLES ELONGATED (APPROX. .225") FOR RH KIDNEY PANEL (132AL). LOCATED ON FWD EDGE OF CUTOUT JUST BELOW STR20R. (C-CHECK) RO: 06/14/2019 REPAIRED 2 ADDITIONAL FASTENER HOLES IAW REO.

Part: FRAME — CORRODED (BS 605) · airframe 32,126 hrs · 32,039 cycles

F.S. 605.00 IS CORRODED ON FORWARD FLANGE BETWEEN STRINGER 26R AND 25L. (C-CHECK) RO: 06/14/2019 REMOVED AND REPLACED FS605 FRAME SECTOR IAW SRM.

Part: ATTACH FITTING — CORRODED (BS 621) · airframe 32,126 hrs · 32,039 cycles

FLOOR BEAM ATTACH FITTING ON FORWARD FACE OF F.S.621.00, LBL 9.00 IS CORRODED. (C-CHECK) RO: 06/14/2019 REMOVED AND INSTALLED NEW SERVICABLE FLOOR BEAM ATTACH FITTING ON FORWARD FACE OF F.S. 621.00 LBL 9.00 IAW SRM.

Part: STRINGER — CRACKED · airframe 32,126 hrs · 32,039 cycles

STRINGER 3L IS CRACKED AT AFT END OF PAX DOOR UPPER SILL. (C-CHECK) RO: 06/14/2019 REPAIRED STRINGER 3L IAW REO AND SRM.

Part: SKIN — CRACKED (LT WING) · airframe 32,126 hrs · 32,039 cycles

L/H LOWER WING PLANK HAS ONE INDICATION NOTED ON EDGE OF CUT OUT AT TOP CORNER FOR ACCESS PANEL 550EB ON I/B SIDE OF HOLE .100" LONG BY 80%FSH. (C-CHECK) RO: 06/14/2019 REPAIRED LH LOWER WING PLANK HOLE FOR ACCESS PANEL 550EB IAW REO.

Part: POST — CRACKED (BS 409) · airframe 32,126 hrs · 32,039 cycles

FS409+128 VERTICAL POST @ BL0 RH SIDE HAS AN INDICATION .1" LONG BY 55% FSH IN THE UPPER AFT RADIUS AT WL69. (C-CHECK) RO: 06/14/2019 . REMOVED AND REPLACED 409 +128 BL0 POST IAW REO AND SRM.

Part: HINGE FITTING — CHAFED (TE FLAP) · airframe 32,126 hrs · 32,039 cycles

HINGE BOX UNDER PANEL 695AB IS CHAFED FROM TO LONG OF A SCREW INSTALLED AT THE FORWARD INBOARD LOWER FAIRING MOUNT. CHAFE IS APPROXIMATELY .005" DEEP WITH HIGH METAL. (C-CHECK) RO: 06/14/2019 REPAIRED FLAP HINGE BOX IAW REO.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,126 hrs · 32,039 cycles

FS621 RPB WEB HAS 3EA AREAS OF CRACK INDICATIONS NOTED IN THE HEEL LINE AREA OF VERTICAL POSTS, 1 AT RBL27 WL102 TO WL113 70%FSH, 1 AT BL0 WL126 TO WL134 50%FSH, AND 1 AT BL0 WL108 TO WL113 60%FHS. (C-CHECK) RO: 06/14/2019 REPAIRED THE 3 CRACK INDICATIONS ON FS621 AT RBL27 WL102 TO WL113, BL0 WL126 TO WL134, AND AT BL0 WL108 TO WL113 IAW REO.

Part: FRAME — CORRODED (BS 349) · airframe 32,126 hrs · 32,039 cycles

FS 349 FRAME SECTOR IS CORRODED FROM STGR 25L TO STGR 25R. (C-CHECK) RO: 06/14/2019 REMOVED AND REPLACED FS349 LOWER FRAME SECTOR IAW SRM.

Part: FRAME — CORRODED (BS 364) · airframe 32,126 hrs · 32,039 cycles

FS 364 FRAME SECTOR IS CORRODED FROM STGR 25L TO STGR 25R. (C-CHECK) RO: 06/14/2019 REMOVED AND REPLACED FS 364 LOWER FRAME SECTOR IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 32,126 hrs · 32,039 cycles

INTERCOSTAL CORRODED AT STGR 27L BETWEEN FS 349 AND FS 364. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: SUPPORT ANGLE — CORRODED (SERVICE DOOR) · airframe 32,126 hrs · 32,039 cycles

SERVICE DOOR LOWER SEAL SUPPORT ANGLE IS CORRODED. (C-CHECK) RO: 06/14/2019 REPAIRED SERVICE DOOR IAW REO.

Part: SHUTOFF VALVE — FAILED (AC BAY) · airframe 31,051 hrs · 30,803 cycles

WHILE CLIMBING THE RIGHT PACK (ONLY OPERATIONAL PACK) SHUT OFF AND AIRCRAFT BECAME UNPRESSURIZED. EMERGENCY DESCENT WAS COMPLIED WITH. RETURNED TO FIELD. NO PACK HI TEMP OR HI PRESS CAUTION MESSAGES OBSERVED. (FLT 4832) FO: 09/18/2018. CLOSED REMOVED AND REPLACED THE RT PACK PRSOV IAW AMM. OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (BS 621) · airframe 28,679 hrs · 28,184 cycles

FOUND REAR PRESSURE BULKHEAD WEB FWD FACE HAS TWO INDICATIONS NOTED AT LBL 36.2, WL 76 APPROX 1 INCH IN LENGTH, LBL 27.5, WL76 APPROXIMATELY 4 INCHES IN LENGTH BOTH FAILED ULTRASOUND INSPECTION. REPAIRED THE PRESSURE BULKHEAD IAW REO.

Part: BULKHEAD WEB — CRACKED (BS 280) · airframe 28,679 hrs · 28,184 cycles

BS 280 LOWER BULKHEAD WEB IS CRACKED JUST OUTBOARD OF LBL 9. REPAIRED THE BULKHEAD WEB IAW REO.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,728 hrs · 25,021 cycles

FWD OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY EXIT BULB IAW AMM 33-51-21. OPS CK GOOD.

Part: DOOR — UNKNOWN · airframe 25,337 hrs · 24,618 cycles

SERVICE DOOR IS DIFFICULT TO OPEN FROM THE OUTSIDE. PERFORMED OPS CHECK OF SERVICE DOOR IAW AMM 52-41-00, NO FURTHER DEFECTS NOTED.

Part: SKIN — CORRODED (NOT REPORTED) · airframe 25,156 hrs · 24,435 cycles

650EB FUEL TANK LAND HAS CORROSION. COMPLIED WITH ECTC EO 600-57-81.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 25,156 hrs · 24,435 cycles

CRACK FOUND ON LT WINDSHIELD SIDE POST SUPPORT. REMOVED ALL FASTENERS COMMON TO ANGLE 601R34032-21 IAW SRM 51-42-06 AND REMOVED ANGLE 601R 34032-21. PERMANENTLY INSTALLED ALL FASTENERS IN NEW SERVICEABLE ANGLE IAW SRM 51-42-06, DWG 601R34032, DWG 601R34032. LOCATED FASTENER HOLES IN NEW SERVICEABLE ANGLE IAW SRM 51-40-11, DWG 601R34032, REV V AND DWG 601R 33010.

Part: SKIN — CORRODED (NOT REPORTED) · airframe 25,156 hrs · 24,435 cycles

640BB FUEL TANK LAND HAS CORROSION. COMPLIED WITH ECTC REO 600-57-81.

Part: SKIN — CORRODED (NOT REPORTED) · airframe 25,156 hrs · 24,435 cycles

640DB FUEL TANK LAND HAS CORROSION. REPAIRED IAW ECTC EO 600-57-81.

Part: SKIN — CORRODED (NOT REPORTED) · airframe 25,156 hrs · 24,435 cycles

650 BB FUEL ACCESS PANEL LAND HAS CORROSION. REPAIRED IAW ECTC EO 600-57-81.

Part: BRACKET — CORRODED (BS 349) · airframe 25,156 hrs · 24,435 cycles

CORROSION ON BRACKET AT BS 349 AND STR 17R. REMOVED THE BRACKET IAW SRM 51-42-21. INSTALLED A NEW BRACKET IAW SRM 51-42-21-00 .

Part: DOOR SILL — CORRODED (BS 574-621) · airframe 25,156 hrs · 24,435 cycles

CARGO DOOR SILL CORRODED AROUND SCREW HOLES AT BS 574 - 621, LBL 70. BLENDED THE DOOR SILL IAW SRM 51-21-06. AREA EXCEEDS ALLOWABLE LIMITS OF EC/TC REO 601R-53-00-526. REPAIRED IAW REO 601R-53-61-5506.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 25,156 hrs · 24,435 cycles

SEAT TRACK CORRODED AT BS 364 - 394, RBL 9. FABRICATED A NEW SEAT TRACK IAW GREO 601R-53-00-485, REV A. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 25,156 hrs · 24,435 cycles

SEAT TRACK CORRODED AT BS 364- 394 LBL 9. R & R THE SEAT TRACK IAW AMM 53-01-11-04 AND 53-01-11-944-001, 53-01-11-000-802, 53-01-11-400-802.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 25,156 hrs · 24,435 cycles

CORROSION FOUND ON FLOORBEAM AT FS 409, RBL 9. BLENDED THE FLOORBEAM IAW SRM 51-21-06. AND FOUND WITHIN LIMITS IAW REO 601R-53-00-005, FIG 1.

Part: SEAT TRACK — CORRODED (BS 394-439) · airframe 25,156 hrs · 24,435 cycles

SEAT TRACK CORRODED BS 394 - 439, RBL 9. FABRICATED A NEW SEAT TRACK IAW GREO 601R-53-00-485, REV A. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 394-439) · airframe 25,156 hrs · 24,435 cycles

SEAT TRACK CORRODED BS 394 - 439, LBL 9. CORROSION FOUND TO BE BEYOND LIMITS IAW SRM 53-21-44. REMOVED DAMAGED SEAT TRACK IAW AMM 53-01-11-020-001. FABRICATED A NEW SEAT TRACK IAW GREO 601RE-53-00-485 REV A, COMPLIED WITH REO 601R-53-00-485 REV A. INSTALLED THE NEW SEAT TRACK IAW AMM 53-01-11-400-802 AND REO 601RE-53-00-601.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 25,156 hrs · 24,435 cycles

CORROSION FOUND ON FLOORBEAM BS 409, RBL 9. BLENDED THE FLOORBEAM IAW SRM 51-21-06.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 25,156 hrs · 24,435 cycles

CORROSION FOUND ON FLOORBEAM AT FS 409, RBL 9. BLENDED THE FLOORBEAM IAW SRM 51-21-06. FOUND OUT OF LIMITS IAW REO 601R-53-00-005.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 25,156 hrs · 24,435 cycles

CORROSION FOUND ON FLOORBEAM AT BS 409, RBL 9. BLENDED THE FLOORBEAM IAW SRM 51-21-06. BLENDED AREAS ARE WITHIN LIMITS IAW REO 601-53-00-005.

Part: FRAME — CORRODED (BS 349) · airframe 25,156 hrs · 24,435 cycles

CORROSION FOUND ON FRAME BS 349 STR 26R-25L. REMOVED CORROSION IAW SRM 53-00-00.

Part: FLOOR PANEL — CRACKED · airframe 25,156 hrs · 24,435 cycles

LEFT SIDE FWD EQUIPMENT COMPARTMENT, TRU, FLOOR PAN CRACKED BETWEEN OUTER SKIN EDGE AND BREAK PRESSURE GOUGES BRACKET. REPAIRED ELECTRICAL BAY FLOOR AT FS 193.00 IAW GREO 601R-53-11-111.

Part: LATCH — FAILED (EMERGENCY EXIT) · airframe 25,156 hrs · 24,435 cycles

RT OVERWING EMERGENCY EXIT DOOR IS DIFFICULT TO OPEN. REMOVED RT OVERWING EXIT DOOR LATCH MECHANISM TO FOM IAW AMM 52-21-02-000-801. ADJUSTED RT OVERWING EMERGENCY EXIT DOOR LATCH MECH REF CMM 52-21-02. REINSTALLED LATCH MECH REF AMM TASK 52-21-02-400-801 OPS TEST GOOD, FUNCTION TEST GOOD.

Part: SIGN — MISSING (CABIN) · airframe 22,054 hrs · 21,266 cycles

EXIT SIGN PANEL MISSING IN THE EXIT ROW. SECURED EXIT SIGN BACK INTO PLACE IAW AMM 25-60-01. OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,264 hrs · 20,452 cycles

FWD BULKHEAD LOWER EMERGENCY FLOOD LIGHT HAS INOPERATIVE LAMPS. REPLACED LAMPS FWD BULKHEAD LOWER EMERGENCY FLOOD LIGHT IAW AMM 33-51-19, OP'S CHECK GOOD.

Part: POST — CRACKED (BS 409) · airframe 20,784 hrs · 19,943 cycles

FOUND FS 409.00+128 VERT POST AT RBL 18 INBD AND OTBD SIDES HAVE INDICATIONS NOTED AT AFT FLANGE RADIUS WL 69 APPROX .2" IN LENGTH X 50 PERCENT FSH BOTH FAILED NDT. R & R DAMAGED INBD AND OTBD RBL 18 FS 409+128 POST IAW REO 601R-53-41-889.

Part: BULKHEAD — CRACKED (BS 621) · airframe 20,784 hrs · 19,943 cycles

FOUND FS 621.00 RPB WEB HAS AN INDICATION NOTED AT LBL 27.5 WL 130 (CARGO DOOR TRACK) APPROX 1" LONG X 100 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 AND REO 601R-53-61-1541, REV D DATED 10/31/2011.

Part: BULKHEAD — CRACKED (BS 621) · airframe 20,784 hrs · 19,943 cycles

FOUND FS 621.00 RPB WEB HAS AN INDICATION NOTED AT LBL 46 WL 108 (CARGO DOOR LINTEL FITTING) APPROX .5" LONG X 100 PERCENT FSH. FAILED NDT INSPECTION. UPON REPAIR OF FS 621 LINTEL FOUND PN 600-35013-39 TO HAVE A DRILL START. REMOVED PART IAW SMM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ANGLE PN 600-35013-39 IAW SRM 51-42-00 AND 51-42-21.

Part: ANGLE — CRACKED (BS 473) · airframe 20,784 hrs · 19,943 cycles

AT FS 473.15, RBL 27.00, INTERCOSTAL INBD AFT NESTING ANGLE IS CRACKED. REQUIRES REPLACEMENT. R & R ANGLE IAW SRM 51-42-10, 51-40-11 AND 51-42-21.

Part: SEAT TRACK — CORRODED (BS 364-399.5) · airframe 20,781 hrs · 19,940 cycles

SEAT TRACK CORRODED BETWEEN FS 364 AND 399.50, RBL 9. R & R SEAT TRACK IAW AMM 53-01-11-400-802.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 20,784 hrs · 19,943 cycles

CARGO COMPARTMENT FLOOR TRACKS AND TIE DOWNS ARE CORRODED AND REQUIRE REPLACEMENT. R & R CARGO FLOOR TRACKS IAW SRM 51-41-04.

Part: SEAT TRACK — CORRODED (BS 399.5-409) · airframe 20,781 hrs · 19,940 cycles

SEAT TRACK CORRODED BETWEEN FS 399.5 AND 409+126, RBL 9.0. R & R TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 20,784 hrs · 19,943 cycles

RT FLOOR SEAT TRACK CORRODED BETWEEN FS 409+126 AND FS 559+4, RBL 9. REMOVED CORRODED RT FLOOR SEAT TRACK BETWEEN FS 409+126 AND FS 559+4 RBL 9 IAW SRM 51-41-02. LOCATED AND DRILLED HOLES FOR NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11 P/N 601R31032-75. INSTALLED NEW SERVICEABLE SEAT TRACK BETWEEN FS 409+126 AND FS 559+4 RBL 9, PN 601R31032-7S IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 20,784 hrs · 19,943 cycles

CARGO COMPARTMENT FLOOR SILL AT LBL 45 HAS CORROSION FROM FS 574.00 TO 621.00. R & R CARGO DOOR SILL WITH NEW SERVICEABLE SILL PLATE IAW REPAIR REO 601R-53-61-1574, REV A.

Part: ANGLE — CRACKED (BS 621-625) · airframe 20,781 hrs · 19,940 cycles

LT FS 621-625 INTERCOSTAL ANGLE CRACKED AT STR 14L. REMOVED INTERCOSTAL ANGLE IAW SRM 51-42-06. INSTALLED SERVICEABLE INTERCOSTAL ANGLES AT STRINGER 14L FROM FS 621-625 IAW REO 601R-53-61-422 AND SRM 51-42-21.

Part: ANGLE — CRACKED (BS 621-625) · airframe 20,781 hrs · 19,940 cycles

RT FS 621-625 INTERCOSTAL ANGLE CRACKED AT STR 14R. REMOVED INTERCOSTAL ANGLE AT FS 621-625 IAW SRM 51-42-06. INSTALLED SERVICEABLE INTERCOSTAL ANGLES AT STRINGER 14R FROM FS 621-625 IAW REO 601R-53-61-422 AND SRM 51-42-21.

Part: LIGHT — CRACKED (CABIN) · airframe 20,781 hrs · 19,940 cycles

RT OVERWING EMERGENCY EXIT BETA LIGHT CRACKED ON PULL HANDLE. REMOVED CRACKED BETA LIGHT FROM RT OVERWING EMERGENCY EXIT PULL HANDLE & INSTALLED NEW SERVICEABLE BETA LIGHT PN BA670-47804-1 IAW AMM 20-21-00-910-801.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 20,566 hrs · 19,712 cycles

FOUND EMERGENCY LIGHTS INOPERATIVE, BLOWN FUSE ON BATTERY CHARGER ASSY. REPLACED BATTERY CHARGER ASSY NR 4 IAW AMM 33-15-05. ALSO REPLACED AFT LIGHT ASSY IAW AMM 33-51-21. EMERGENCY LIGHT OPS TESTED GOOD IAW AMM 33-51-00.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,441 hrs · 19,577 cycles

RT FUSELAGE AFT MOST EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER IAW AMM 33-51-05 AND AIPC REF 33-51-04-01 FIG 1, ITEM 18 OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT RETURN TO SERVICE.

Part: CHARGER — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 20,439 hrs · 19,574 cycles

RT FUSELAGE AFT MOST EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER IAW AMM 33-51-05 AND AIPC REF 33-51-04-01 FIG 1, ITEM 18. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT RETURN TO SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,434 hrs · 19,571 cycles

CABIN CEILING EMERGENCY LIGHT 3RD FROM FRONT INOPERTAIVE. REPLACED THE LAMP IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 20,198 hrs · 19,343 cycles

F/O'S FLASHLIGHT INOPERATIVE. REPLACED BATTERIES IAW AMM 25-61-02.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 19,424 hrs · 18,506 cycles

EXTERIOR EMERGENCY LIGHT FWD OF THE SERVICE DOOR IS OUT. RELAMPED NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,983 hrs · 18,006 cycles

FWD CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED THE INOP BULB AND INSTALLED A NEW BULB IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,941 hrs · 17,960 cycles

NR 7 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 18,877 hrs · 17,884 cycles

EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED WHEN EITHER FIGHT DECK OR F/A SWITCH IS SELECTED ON. LIGHTS ILLUMINATE FOR LESS THAN 5 SECONDS THEN EXTINGUISH. CHARGED UP EMERGENCY LIGHT SYS IAW AMM 33-51-00. PERFORMED OPS CHECK. OPS CHECKED GOOD.

Part: FLASHLIGHT — UNSERVICEABLE (COCKPIT) · airframe 18,719 hrs · 17,709 cycles

CAPTAIN`S FLASHLIGHT IS VERY WEAK AND DIM. R & R CAPTAIN'S FLASHLIGHT. OPS CHECKED GOOD IAW AMM 25-60-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,105 hrs · 17,030 cycles

LEFT CENTER FUSELAGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND INSTALLED A NEW BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,515 hrs · 16,366 cycles

EXTERNAL EMERGENCY LIGHTS 8 AND 9 INOP. R & R NR 4 EMERGENCY BATTERY PACK IAW AMM 33-51-04, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,434 hrs · 15,142 cycles

EXTERIOR EMERGENCY LIGHT NR3 INOP. R & R EXTERIOR EMERGENCY LIGHT NR3 IAW AMM 33-51-21. OP'S CHECK GOOD. (CLOSED)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,428 hrs · 15,134 cycles

FWD LT FLOOR LEVEL EXIT SIGN INOP. R & R LT FWD FLOOR LEVEL EXIT SIGN ASSY IAW AMM 33-51-10. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 589-610) · airframe 16,016 hrs · 14,662 cycles

SEAT RAIL BEAM CAP AT FS 610-589, LBL 27 HAS CORROSION AT 4 EA LOCATIONS. REMOVED SEAT RAIL CAP AT FS 569-610 IAW SRM 51-42-06, 51-42-21. LOCATED, DRILLED NEW SEAT RAIL CAP IAW SRM 51-42-06, 51-42-21. NEW SEAT RAIL CAP REQUIRES INSTALLATION. INSTALLED NEW SEAT RAIL CAP AT FS 569-610, LBL 27 IAW REO 601R-53-61-3778, SRM 51-42-21. (CLOSED)

Part: BEAM — CRACKED (BS 280) · airframe 16,016 hrs · 14,662 cycles

LONG CRACK FOUND FS 280 TRANSVERSE BEAM, RBL 11 BOTTOM OF BEAM NEXT TO RADIUS MARKED WITH RED TAPE. REMOVED FASTENERS AND OTBD CLIP ON TRANSVERSE BEAM FS 250, RBL 9 IAW SRM 51-42-21, 51-42-06. COMPLIED WITH STEP 1 OF REO 601R-53-11-171. COMPLIED WITH REO 601R-53-11-171 STEP 2. PERFORMED EDDY CURRENT IAW NDTM 51-20-06. NO INDICATIONS NOTED. PERFORMED LPI OF 2 FABRICATED ANGLES IAW NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. C/W STEPS 11, 12 AND 13 OF REO 601R-53-11-171, STEP 5, C/W ECTC REO 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171.

Part: BEAM — CRACKED · airframe 16,016 hrs · 14,662 cycles

TRANSVERSE BEAM IS CRACKED OTBD OF ALTERNATE EXTENSION CABLE PULLEY ON RT SIDE APPROX 1" LONG. REPAIRED FS 280 TRANSVERSE BEAM IAW EC/TC REO 601R-53-11-138.

Part: FRAME — CORRODED (BS 333 S25L/R) · airframe 16,016 hrs · 14,662 cycles

FRAME SECTION AT FS 333.00 FROM STRINGER 25L TO 25R IS CORRODED. REMOVED FASTENERS FROM FRAME SECTION AT FS 333, FROM STR 23L TO 23R IAW SRM 51-42-06 AND 51-42-21. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-15 AND 53-00-00. REMOVED FRAME SECTION FROM ACFT IAW SRM 51-42-06 AND 51-42-21. RECEIVED NEW SERVICEABLE FRAME SECTION. INSTALLED NEW SERVICEABLE FRAME SECTION AT FS 333 BETWEEN STR 23L AND 23 RT IAW SRM 51-42-06 AND 51-42-21. APPLIED FILLET SEAL TO NEW SERVICEABLE FRAME SECTION TO FUSELAGE MATING AREA IAW SRM 51-23-00.

Part: FRAME — CORRODED (BS 349 S27) · airframe 16,016 hrs · 14,662 cycles

FRAME SECTION AT FS 349.00 IS CORRODED AT STRINGER 27. REMOVED CORROSION FROM FRAME FS 349.00 STRINGER 27 IAW SRM 51-21-06. AREA OF CORROSION REMOVED WITHIN LIMITS IAW SRM 53-00-00, FIG 102 (SHEET 2). MATERIAL REMOVED .002, REMAINING MATERIAL .061. PAINTED REPAIR IAW SRM 51-25-16.

Part: BRACKET — CRACKED (BULKHEAD) · airframe 16,016 hrs · 14,662 cycles

FOUND REAR PRESSURE BULKHEAD HAS 2 ISOLATOR BRACKETS CRACKED LBL 9.0 AND RBL 9.0 WL 100. REMOVED 2 EA MOUNTING BRACKETS AND 2 EA CRACKED ISOLATORS. INSTALLED 2 EA NEW ISOLATORS ON SAME SERVICEABLE MOUNTING BRACKETS AND INSTALLED 2 EA SAME SERVICEBLE MOUNTING BRACKETS IAW SRM 51-42-06.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 16,016 hrs · 14,662 cycles

FOUND CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED .3" IN LENGTH. REMOVED CARGO DOOR SUPPORT BEAM CRACKED AFT LOWER ANGLE. LOCATED FASTENER HOLES IN NEW ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-40-11 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,016 hrs · 14,662 cycles

BOTH RT 280 CLIP AT RBL 9 CRACKED ON UPPER CORNER. REMOVED BOTH 280 CLIPS RBL 9 IAW SRM 51-42-06, 51-42-21. LOCATED AND DRILLED NEW 280 CLIPS IAW SRM 51-42-06, 51-42-21. INSTALLED BOTH 280 CLIPS RBL 9 IAW SRM 51-42-06, 51-42-21.

Part: SUPPORT FITTING — CRACKED (RT ACM) · airframe 16,016 hrs · 14,662 cycles

RT ACM SUPPORT CLIP CRACKED. REMOVED CRACKED CLIP AND INSTALLED SERVICEABLE CLIP IAW 51-42-06.

Part: BULKHEAD — CRACKED (BS 559) · airframe 16,016 hrs · 14,662 cycles

FS 559.00 SEMI-PRESSURE BULKHEAD WEB FAILED NDT INSP IN 3 LOCATIONS: 1 IN WEB AT WL 59.0 INBD OF POST AT RBL 18, 1 IN WEB AT WL 58.7-59.1 OTBD OF POST AT RBL 9.0, 1 IN WEB AT WL 51.7 OTBD OF POST AT LBL 9.0. CRACK INDICATIONS ARE APPROX .05"-.30" LONG AND OVER 50 PERCENT FSH. REPAIRED FS 559 BULKHEAD CAP ANGLES AND WEBS FROM LBL 27 TO RBL 27 IAW REO 601R-53-41-260 REV E, STEPS 1 THRU 14. C/W EC/TC REO 601R-53-41-260 AND REO 601R-53-41-260 REV E, DATED AS WRITTEN.

Part: PLACARD — WORN (ESCAPE HATCH) · airframe 16,016 hrs · 14,662 cycles

ALL 4 CREW ESCAPE HATCH EXTERNAL PLACARDS ARE WORN. REMOVED WORN PLACARDS IAW CRJ 200 MM 11-10-03-000-801. APPLIED NEW SILKSCREEN ON HATCH IAW CRJ 200 MM 11-10-03-400-801.

Part: PLACARD — WORN (CABIN) · airframe 16,016 hrs · 14,662 cycles

LT AND RT OVERWING EMERGENCY EXIT EXTERNAL FLAPPER PLACARDS ARE WORN. APPLIED NEW SILKSCREEN TO LT AND RT OVERWING EMERGENCY EXITS IAW MM 11-10-03-400-801

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 16,016 hrs · 14,662 cycles

SERVICE DOOR INNER HANDLE "EXIT" BETA SIGN IS CRACKED. R & R SERVICE DOOR INNER HANDLE "EXIT" BETA SIGN IAW AMM 33-51-09-000-802 AND 33-51-09-400-802. FUNCTIONAL TEST GOOD.

Part: LIGHT — INOPERATIVE (EXTERNAL) · airframe 15,870 hrs · 14,506 cycles

AFT MOST LT EXTERNAL EMERGENCY LIGHT INOP. R & R AFTMOST LT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. R & R AFTMOST LT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 15,641 hrs · 14,243 cycles

RT FWD EXTERNAL EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT BULB IAW AMM 33-51-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,780 hrs · 12,157 cycles

SEVERAL EMERGENCY EXIT LIGHTS INOP. FLT 4983 DEL 428 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,419 hrs · 11,784 cycles

RIGHT FWD LIGHT INOP.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 13,262 hrs · 11,633 cycles

ON CLIMBOUT CABIN WAS CLIMBING AT A RATE OF 600- 800 FPM CABIN W/N PRESSURIZE. EICAS ECS SYNOPTIC PAGE INDICATED ALL WAS NORMAL. EMERGENCY DECLARED. A/C RETURNED TO ORF AFTER T/O. FLT 5567 CX.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 12,742 hrs · 11,154 cycles

CARGO DOOR SUPPORT BEAM AFT LWR ANGLE IS VISIBLY CRACKED IN TWO PLACES APPROX LENGTH ARE 1 1/2" 3/4" ANGLE PN IS 601R-35050-109.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,742 hrs · 11,154 cycles

LT 621 FLOOR SUPPORT ANGLE CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,742 hrs · 11,154 cycles

LT FS 484 FLOOR SUPPORT INTERCOSTAL CLIP CRACKED .1" LONG AT LBL 27. REMOVED AND REPLACED LT FS 484, LBL 27 FLOOR SUPPORT INTERCOSTAL CLIP WITH NEW PART IAW CRJ 200 SRM 51-23-00, 51-40-11, 51-42-06, 51-42-21 AND 51-21-16.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,742 hrs · 11,154 cycles

LT FS 484 FLOOR SUPPORT INTERCOSTAL CRACKED .1" LONG AT LBL 36. THE REPAIR ANGLE DESCRIBED IN REO 601R-53-41-059 STEP 5 WAS FABRICATED USING PRE-MANUFACTURED ANGLE P/N 56144A14, THEREFORE THERE IS NO NEED TO HEAT TREAT OF NDT. COMPLETED REPAIR AT LT FS 484 FLOOR SUPPORT BRACKET IAW BOMBARDIER REO 601R-53-41-059. WORK PERFORMED IAW ASA EC/TC 601R-53-41-059.

Part: SUPPORT — CRACKED (APU DOOR FRAME) · airframe 12,742 hrs · 11,154 cycles

APU INLET DOOR FRAME SUPPORT P/N 601R35210-17 CRACKED .2" LONG AT FWD BOTTOM CORNER RADIUS BETWEEN FS 654.5 - FS 672.20 STR 4L IN AFT EQUIP BAY CEILING. REPLACED APU INLET DOOR FRAME SUPPORT IAW CRJ SRM 51-42-06 FOR SOLID RIVETS, CRJ 200 SRM 51-42-13 FOR CHERRYMAX RIVETS, AND CRJ SRM 51-40-11 FOR FASTENER HOLE PREPARATION.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,742 hrs · 11,154 cycles

RT FS 484 FLOOR SUPPORT INTERCOSTAL CRACKED .1" LONG AT RBL 36. COMPLETED REPAIR AT RT FS 484 FLOOR SUPPORT BRACKET AT RBL 36 IAW BOMBARDIER REO 601R-53-41-059. WORK PERFORMED IAW ASA EC/TC 601R-53-41-059.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,742 hrs · 11,154 cycles

RT FS 621-625 INTERCOSTAL ANGLE CRACKED IN AFT EQUIP BAY. REMOVED ANGLE, LOCATED, AND TRANSFERED HOLES ONTO NEW PART. INSTALLED NEW ANGLE ON A/C IAW CRJ 200 SRM 51-42-06 AND 51-40-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,742 hrs · 11,154 cycles

LT FS 621-625 INTERCOSTAL ANGLE CRACKED IN AFT EQUIP BAY. REMOVED ANGLE, TRANSFERED HOLES ONTO NEW ANGLE. INSTALLED ANGLE ON A/C IAW CRJ 200 SRM 51-40-11 AND 51-42-06.

Part: ECU — UNKNOWN (TE FLAP) · airframe 12,709 hrs · 11,122 cycles

AIRCRAFT RETURNED TO ATL AFTER T/O. FLT 5558 DEL 122 MINS. FLAP ELECTRONIC CONTROL UNIT FECU CHANNELS, A/C WITH SKEW DETECTION SYSTEMS FLAP POWER DRIVE UNIT MOTORS. REMOVED AND REPLACED RT MOTOR AND BRAKE ASSY IAW AMM 27-52-05. OPS CHECK GOOD IAW AMM 27-64-00. DEFER CLEARED PLACARD REMOVED.

Part: SETSCREW — OUT OF ADJUST (PAX DOOR) · airframe 12,151 hrs · 10,615 cycles

CREW REPORTS PAX DOOR HARD TO OPEN. ADJUSTED PAX DOOR INNER HANDLE SET SCREW OPS CHECK GOOD AT THIS TIME. PER CRJ200 AMM 52-11-00.

Part: STRAP — STUCK (PAX DOOR) · airframe 12,151 hrs · 10,615 cycles

PAX DOOR WILL NOT OPEN. HANDLE STRAP STUCK IN LOCKED POSITION. FREED STRAP AND DOOR OPENED NORMALLY. NO DEFECTS NOTED AT THIS TIME.

Part: SMOKE WARNING — ILLUMINATED (CARGO) · airframe 10,567 hrs · 9,247 cycles

SMOKE CARGO EICAS WARNING MSG ON SHORT FINAL. COMPLIED W/QRH AND MSG OUT. BOTTLES NOT BLOWN, EMERGENCY DECLARED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,044 hrs · 8,777 cycles

NR 2 EMERGENCY LIGHT BATTERY CHARGER INOP.

Part: UNKNOWN — WARNING LIGHT (NLG STEERING) · airframe 9,193 hrs · 7,933 cycles

STEERING INOP MSG AFTER TAKEOFF, COMPLIED WITH QRH, LANDED W/ NWS OFF, HIT A LARGE BUMP ON TAKE OFF INTERSECTING RUNWAYS, EMERGENCY DECLARED.

Part: DOOR — MALFUNCTIONED (MAIN PAX) · airframe 9,105 hrs · 7,843 cycles

PAX DOOR HARD TO OPEN. ONCE OPENED, IT CLOSED ITSELF, NO HELP FROM ANYONE. TO OPEN IT AGAIN, PRESSED DOOR ASSIST BUTTON ONCE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,809 hrs · 7,575 cycles

FLIGHT ATTENDANT FLASHLIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,641 hrs · 7,424 cycles

FUSELAGE EMERGENCY LIGHT NOT COMING ON.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 7,765 hrs · 6,672 cycles

PAX DOOR OUTER HANDLE CRACKED, MARKED.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 7,765 hrs · 6,672 cycles

280 CLIP CRACKED RBL 9 O/B.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 7,765 hrs · 6,672 cycles

280 CLIP CRACKED RBL 9 O/B.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 7,765 hrs · 6,672 cycles

LEFT SIDE OUTBOARD CLIP CRACKED AT FS 280 LBL 9.0.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 7,765 hrs · 6,672 cycles

CLIP CRACKED AT LBL 9 FS 280 O/B CLIP.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 7,765 hrs · 6,672 cycles

CLIP CRACKED AT RBL 9 FS 280 I/B CLIP.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 7,765 hrs · 6,672 cycles

CLIP CRACKED AT LBL 9 FS 280 I/B CLIP.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 7,765 hrs · 6,672 cycles

CREW ESCAPE HATCH OUTER HANDLE IS CORRODED.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 7,765 hrs · 6,672 cycles

RIGHT SIDE FLOOR ANGLE CRACKED AT FS 621.00 (MARKED). RESOLVED ON W/O: 35318 TASKCARD: N/R-00141. C/W REPAIR ON RT SIDE FLOOR ANGLE IAW REO 601R-53-61-117.

Part: ANCHOR FITTING — CRACKED (AIRSTAIRS) · airframe 7,306 hrs · 6,298 cycles

ASD FWD ANCHOR FITTING CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,253 hrs · 6,259 cycles

EMERGENCY LIGHTING ORANGE STRIP NOT WORKING. A/C SWAP TO 919, FLT 4299 DEL 133 MINS.

Part: WARNING LIGHT — ILLUMINATED (APU DOOR)

FLT 4541 - DURING CRUISE FROM ATL-SHV, AFTER SHUTTING DOWN THE APU, THE CREW RECEIVED AN `APU DOOR INHIBIT/OPEN` MESSAGE WITH A FUEL SMELL COMING FROM THE PACKS. THE AIRCRAFT LANDED SAFELY IN SHV. MAINTENANCE RESET THE APU DOOR TO THE NORMAL POSITION. THE APU STARTED NORMALLY WITH NO ODOR OF ANY KIND DETECTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — SEPARATED (PAX DOOR)

DURING AN A-CHECK, THE PASSENGER DOOR BOTTOM STEP ATTACH BRACKET TO THE STAY ROD WAS FOUND SEPARATING FROM THE STEP. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN MCN, THE EMERGENCY FLOOR LIGHTS AT ROWS 5 THROUGH 8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT CONNECTOR CABLE AT ROWS 5 THROUGH 8. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — INOPERATIVE (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEOP ON THE PASSENGER DOOR WAS FOUND TO BE BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BPSU — MALFUNCTIONED (T/E FLAP)

DURING APPROACH, THE CREW RECEIVED A FLAPS FAIL AMBER CAUTION MESSAGE. THE FLAPS INDICATED ZERO DEGREES ON THE PRIMARY EICAS AND SYNOPTIC PAGES AND THE FLAPS HAD NOT BEEN CALLED FOR PRIOR TO THE CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND EMERGENCY VEHICLES WERE REQUESTED AS A PRECAUTION. THE AIRCRAFT DIVERTED, PERFORMING A ZERO FLAP LANDING AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT FLAP BRAKE POSITION SENSOR UNIT (BPSU) AND RIGGED THE FLAPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.