N882AS

Part: ATTACH FITTING — GOUGED (BS 621) · 31,251 cycles

FLOORBEAM ATTACH FITTING BS 621 BULKHEAD FORWARD SIDE, RBL 27 GOUGED. REMOVED AND REPLACED THE ATTACHMENT FITTING IAW REO.

Part: CARGO TRACK — CORRODED (NOT REPORTED) · 31,251 cycles

AFT CARGO TRACK OTBD FLANGE CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM.

Part: NOT REPORTED — DAMAGED (BS 349) · 31,251 cycles

DAMAGE AT FS 349.0 BETWEEN STR 19R AND 20R. REPAIRED IAW REO AND SRM.

Part: CARGO TRACK — CORRODED (BS 574-589) · 31,251 cycles

AFT CARGO TRACK OTBD FLANGE IS CORRODED BS 574 - 589, LBL 9. REMOVED AND REPLACED THE CARGO TRACK IAW REO AND SRM.

Part: SKIN — CRACKED (BS 235) · 31,251 cycles

FUSELAGE SKIN AT NLG WHEEL WELL CUT OUT IS CRACKED, BS 235, LBL 6 AND RBL 6. REPAIRED IAW REO.

Part: FRAME — CORRODED (BS 605) · 31,251 cycles

AFT CARGO, BS 605 FRAME CORRODED BETWEEN STRINGERS 22 AND 24L. REMOVED AND REPLACED THE FRAME IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · 31,251 cycles

REAR PRESSURE BULKHEAD WEB HAS SIX CRACK INDICATIONS. REPAIRED THE BULKHEAD WEB IAW REO.

Part: SKIN — DAMAGED (RT WINGLET) · 31,251 cycles

LOWER WINGLET SKIN PANEL DAMAGED. REMOVED AND REPLACED RT WINGLET LOWER SKIN IAW SRM.

Part: ATTACH FITTING — CORRODED (BS 621) · 31,251 cycles

FLOORBEAM ATTACH FITTING AT BS 621, LBL 27 IS CORRODED ON THE INBD SIDE AND GOUGED ON TOP SIDE. REMOVED AND REPLACED THE ATTACH FITTING IAW REO.

Part: BULKHEAD WEB — DAMAGED (BS 621) · 31,251 cycles

BS 621 BULKHEAD WEB FAILED NDT INSPECTION AT LINTEL FITTING. REPAIRED THE BULKHEAD WEB IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · 31,251 cycles

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

Part: SEAT TRACK — BUCKLED (BS 589-605) · 31,251 cycles

INBD SEAT TRACK BUCKLED BETWEEN BS 589 AND 605, LBL 27. INSTALLED A NEW SEAT TRACK IAW SRM.

Part: DIMMER — BURNED (CABIN LIGHTS) · airframe 32,886 hrs · 30,478 cycles

PILOT REPORTED BURNING ODOR TOWARD LAV AREA. MX REMOVED AND REPLACED THE POWER UNIT DIMMER ON ROW 11AB, 12AB, AND 14AB IAW AMM 33-21-04. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SWITCH — SHORTED (DOOR ASSIST) · airframe 30,051 hrs · 27,508 cycles

PASSENGER DOOR VERY DIFFICULT TO OPEN. REQUIRED 2 PEOPLE TO OPEN. AFTER PUSHING IT APPROXIMATELY HALF WAY, IT FREE-FELL AS NORMAL. FOUND ASD POWER ASSIST SWITCH SHORTED CAUSING DOOR TO CLOSE BY ITSELF. REPLACED PANEL ASSY IAW AMM 33-22-00.

Part: DOOR — BINDING (MAIN PAX) · airframe 29,616 hrs · 27,066 cycles

UNABLE TO OPEN MAIN CABIN DOOR. FELT LIKE FORWARD ASSIST MECHANISM WAS STILL ENGAGED AND RESISTING OUR EFFORTS TO PUSH DOOR OPEN. DOOR OPENED BY ITSELF A FEW MINUTES LATER. PASSENGER DOOR POWER ASSIT SYSTEM: POWER ASSIST SUB-SYSTEM, MOTOR, CONTROL SWITCH, CABLES, PULLEYS, FITTING.

Part: SKIN — GOUGED (FUSELAGE) · airframe 29,540 hrs · 26,982 cycles

SEVERAL GOUGES FOUND ON FUSELAGE SKIN. BLENDED GOUGES IAW SRM 51-12-00 AND TR-51-31. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-31. REPAIRED IAW EA 25-2014-363. MAJOR REPAIR.

Part: SKIN — GOUGED (RT WING) · airframe 29,508 hrs · 26,951 cycles

RT WING LOWER WING ACCESS HOLE FOR ACCESS PANEL 650HB, JUST INBD OF WS 314.50 HAS SCRATCHES IN 2 PLACES REQUIRING ROTO PEENING. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH GREO 601R-57-21-030 AND EC/TC EO 600-57-81.

Part: BULKHEAD — GOUGED (BS 621) · airframe 29,508 hrs · 26,951 cycles

AFT PRESSURE BULKHEAD GOUGED RBL 27.50. REPAIRED IAW EC/TC REO 601R-53-61-2155.

Part: ATTACH ANGLE — CRACKED (DOOR TRACK) · airframe 29,508 hrs · 26,951 cycles

CARGO DOOR TRACK ATTACH ANGLE IS CRACKED AT BS 621. REMOVED AND REPLACED THE ATTACH ANGLE IAW IAW SRM 51-42-21.

Part: BULKHEAD — GOUGED (BS 621) · airframe 29,508 hrs · 26,951 cycles

AFT PRESSURE BULKHEAD FWD FACE GOUGED LBL 18.00. REPAIRED IAW REO 601R-53-61-2155. MAJOR REPAIR.

Part: BULKHEAD — GOUGED (BS 621) · airframe 29,508 hrs · 26,951 cycles

AFT PRESSURE BULKHEAD FWD FACE GOUGED AT LBL 36.2 JUST BELOW CARGO DOOR TRACK CROSS MEMBER. REPAIRED IAW REO 601R-53-61-2155.

Part: FLAP — GOUGED (DOOR VENT) · airframe 29,508 hrs · 26,951 cycles

PAX DOOR ICE BREAKER CABLE GOUGING PRESSURE VENT FLAP DURING OPS. REPAIRED IAW REO 601R-52-11-1040.

Part: ANGLE — CRACKED (BS 625) · airframe 29,508 hrs · 26,951 cycles

ANGLE AT BS 625, S14R IS CRACKED. R & R THE ANGLE IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 625) · airframe 29,540 hrs · 26,982 cycles

ANGLE AT BS 625, S14L IS CRACKED, MORE THAN 1" INCH, AFT EQUIP BAY PRESSURE BULKHEAD. R & R THE ANGLE IAW SRM 51-42-21.

Part: ATTACH BRACKET — CRACKED (BS 280) · airframe 29,508 hrs · 26,951 cycles

FUSELAGE STRINGER TO BULKHEAD ATTCHE BRACKET CRACKED AT BS 280 STRINGER 3. REPAIRED IAW SRM 51-42-06-00, SRM 51-42-06-00 AND 51-21-11-00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 29,508 hrs · 26,951 cycles

SEAT TRACK AT BS 559 CORRODED. DETERMINED BEYOND LIMITS IAW SRM 53-21-49, PAGE BLOCK 101-199, FIGURE 101. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11-000-802 & REO 601R-53-00-485.

Part: MOUNT — CORRODED (GALLEY) · airframe 29,540 hrs · 26,982 cycles

GALLEY FLOOR MOUNT PLATE INBD OF RBL 9.00 BETWEEN FS 295.00 AND FS 333.00 THE TOP PLATE IS CORRODED. BLENDED CORROSION & EVALUATED MOUNT PLATE & CAP PLATE. PARTS ARE OUT OF LIMITS IN REF TO SRM 51-21-06 & TR 53-27. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH SNIEO 601R386691 AND INSTALLED CAPPING STRIP AND PLATE IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 349) · airframe 29,508 hrs · 26,951 cycles

STUB FRAMES AT BS 349 CORRODED. REPAIRED IAW SRM 51-21-06-00.

Part: DOOR SILL — CORRODED (BS 319) · airframe 29,508 hrs · 26,951 cycles

SERVICE DOOR SILL FWD CORNER AT BS 319.70 IS CORRODED. DETERMINED OUT OF LIMITS IAW SRM TR 53-27. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-21, 51-41-02, AND DWG 601R38338. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 29,508 hrs · 26,951 cycles

FLOOR SUPPORT BETWEEN BS 310 - 319.70 IS CORRODED. BLENDED AND FOUND OUT OF LIMITS IAW SRM 51-21-06-00. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06, 51-42-06, 51-42-20, AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 513) · airframe 29,508 hrs · 26,951 cycles

CORROSION ON RT PRESSURE FLOOR SUPPORT BS 513. REPAIRED IAW SRM 51-21-06-00 & 51-42-21-00. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 499-513) · airframe 29,508 hrs · 26,951 cycles

CORROSION ON LT PRESSURE FLOOR SUPPORT BS 499 - 513. REPAIRED IAW SRM 51-21-06-00 & 51-42-21-00. MAJOR REPAIR.

Part: HINGE — GOUGED (PAX DOOR) · airframe 29,508 hrs · 26,951 cycles

PASSENGER DOOR HINGE HALF HAS TWO GOUGED LUGS AT NR 2 AND NR 18. REPAIRED IAW REO 601R-52-11-1347. MAJOR REPAIR.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 29,540 hrs · 26,982 cycles

EMERGINCY LIGHT WIRE CONNECTOR BROKEN OFF FUSELAGE SIDE JUST FWD OF SERVICE DOOR. REPLACED EMERGENCY LIGHT WIRE CONNECTOR IAW ESPM 20-16-00. OPS TESTED THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. OPS TESTED GOOD.

Part: DOOR FRAME — CORRODED (BS 364) · airframe 29,540 hrs · 26,982 cycles

AVIONIC DOOR SURROUNDING FRAME AT BS 364 BETWEEN S24L - 24R CORRODED. BLENDED DAMAGE IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM TR 53-33 53-00-31. REPAIRED IAW GREO 601R-53-21-676, REV B.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 29,508 hrs · 26,951 cycles

REAR PRESSURE BULKHEAD FWD FACE HAS BROKEN ISOLATOR. R & R ISOLATOR IAW SRM 51-42-06.

Part: LIGHT — UNSECURE (CABIN) · airframe 28,899 hrs · 26,378 cycles

PAX DOOR ENTRY FWD BULKHEAD EMERGENCY FLOOD LIGHT COVER & LIGHT BAR ARE UNSECURE. R & R PAX DOOR ENTRY FWD BULKHEAD FLOOR EMERGENCY FLOODLIGHT IAW AMM 33-51-19. OPS CHECK GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 28,603 hrs · 26,073 cycles

FLOOR LIGHT COVER MISSING BY MAIN DOOR, LIGHT LENS/ COVERS, INCLUDING EMERGENCY LIGHT. REPLACED LIGHT COVER IAW AMM 33-51-10 DEFER CLEARED PLACARD REMOVED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 27,904 hrs · 25,375 cycles

NR 1 INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-04, OPS CHECKED GOOD.

Part: SWITCH — DIRTY (PAX DOOR) · airframe 27,814 hrs · 25,286 cycles

F/A TRIED OPENING CABIN DOOR AT GATE AND WOULDN'T OPEN. F/O TRIED TO OPEN IT AND IT OPENED WITH DIFFICULTY. AFTER DOOR OPENED, IT STARTED TO RETRACT ON IT'S OWN. PULLED CIRCUIT BREAKERS. CLEANED POWER ASSIST SWICH. OPS CHECKED GOOD IAW AMM 52-60-00.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 26,628 hrs · 24,033 cycles

PASSENGER DOOR WOULD NOT OPEN. ONCE IT OPENED, STARTED TO RETRACT UNCOMMANDED. PERFORMED OP'S TEST OF THE PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. OP'S CHECKED GOOD.

Part: LIGHT — SHORTED (CABIN) · airframe 26,504 hrs · 23,905 cycles

CLIMBING THRU 15K, BOTH THE F/O AND CAPT SMELLED HOT ELECTRICAL/ BURNING PLASTIC ODOR. DIVERTED, ONE OF THE GALLEY OVERHEAD LIGHTS HAD A SHORTED, CAUSING THE ODOR AS NOTED. R & R LIGHT ASSY IAW AMM 33-26-01. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,170 hrs · 23,566 cycles

NR 1 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD IAW AMM 33-51-010.

Part: WIRE — CHAFED (FUEL QTY) · airframe 25,919 hrs · 23,308 cycles

WIRE FOR FUEL QTY PROBE IN PANEL 540BB HAS CHAFE DAMAGE, BECAUSE STANDOFF FOR CLAMP IS NOT LOCATED IN CORRECT POSITION. REPAIRED IAW REO 601R-20-12-111 AND REO 601R-57-21-1862, REV A.

Part: BULKHEAD — DAMAGED (BS 409) · airframe 25,919 hrs · 23,308 cycles

BS 409+128 PRESSURE BULKHEAD AT LBL 18 HAS TWO TOOLING MARKS, WORST IS APPROX 1.5" L X .125 W X .010 D. REPAIRED IAW REO 601R-53-41-1654.

Part: FLOOR SUPPORT — CRACKED (BS 454) · airframe 25,895 hrs · 23,286 cycles

FS 454, FLOOR SUPPORT PREVIOUS REPAIR ANGLE CRACKED, RBL 36. REPAIRED INTERCOSTALS AT FS 484 BETWEEN RBL 27 & RBL 36 IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CRACKED (BS 460) · airframe 25,895 hrs · 23,286 cycles

FS 460 FLOOR SUPPORT FITTING OTBD OF RBL 9 CRACKED. REMOVED DAMAGED FLOOR SUPPORT FITTING AT FS 460 OTBD OF RBL 9 IAW SRM 51-42-21 & 51-42-06. LOCATED FASTENER HOLES ONTO NEW SERVICEABLE FLOOR FITTING IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FLOOR SUPPORT FITTING AT FS 460 OTBD OF RBL 9 IAW SRM 51-42-21 & SRM 51-42-06.

Part: WEB — CHAFED (BS 559) · airframe 25,919 hrs · 23,308 cycles

PRESSURE FLOOR SKIN JUST FWD OF FS 559 INBD OF LBL 9 HAS THREE CHAFES WITHIN A 1 INCH AREA. DEEPEST APPROX .010 DEEP. REPAIRED IAW REO 601R-41-1655R.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 25,895 hrs · 23,286 cycles

FS 484 FLOOR SUPPORT CLIP RBL 27 CRACKED. REMOVED CLIP AT FS 484.00, RBL 27, LOCATED DRILLED UP AND INSTALLED NEW CLIP PN 601R31171-9 IAW SRM 51-40-11 AND SRM 51-42-21.

Part: ANGLE — CRACKED (BS 621-675) · airframe 25,895 hrs · 23,286 cycles

LEFT AFT ECS BAY, BS 621-675 OBLIQUE ANGLE CRACKED. REMOVED CRACKED ANGLE & INSTALLED NEW SERVICEABLE ANGLE PN 601-35012-51 IAW SRM 51-40-11 & 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 25,895 hrs · 23,286 cycles

FOUND FS 409.00+128 VERTICAL POST LBL 18.0 INBD AND OTBD SIDE HAVE INDICATIONS NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT AFT FLANGE RADIUS WL 69.0. FAILED NDT INSPECTION. REMOVED INBD & OTBD POSTS LBL 18 AT FS 409+128 IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLE POSTS, PN 601R-32208-31S & 601R32208-155 IAW SRM 51-40-06 & 51-40-11, RIVETED POSTS TOGETHER IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE INBD & OTBD LBL 18 POSTS PN 601R32208-31S & 601R32208-155 AT FS 409+128 IAW SRM 51-42-06 & SRM 51-42-22.

Part: SEAT TRACK — CORRODED (S 364-409) · airframe 25,919 hrs · 23,308 cycles

LT SEAT TRACK IS CORRODED BEYOND LIMITS AT LBL 9, FS 364 TO FS 409+128. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 25,895 hrs · 23,286 cycles

R5 CABIN SEAT TRACK IS CORRODED BEYOND LIMITS AT RBL 9, FS 364 TO FS 409+128. (EXFOLIATION/FASTENERS PULLING THRU). R & R RT NR 1 FLOOR SEAT TRACK, PN 601R31032-15 IAW AMM 53-01-11-000-802 & 53-01-11-400-802. REMOVED RT NR 2 SEAT TRACK IAW AMM 53-01-11-000-802. LOCATED NEW SEAT TRACK PN 601R31032-21. DRILLED & COUNTERSUNK HOLES IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 25,593 hrs · 22,983 cycles

AFT CARGO BULKHEAD ISOLATORS BROKEN. R & R BROKEN ISOLATORS AFT CARGO BULKHEAD IAW SRM 51-42-13.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,348 hrs · 22,721 cycles

NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. LAMPED LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FAILED · airframe 25,309 hrs · 22,684 cycles

FLAP FAIL MESSAGE ON FINAL (30 DEG) FOLLOWED QRH, EMERGENCY DECLARED. RESET AND PERFORMED OPS CHECK OF THE FLAPS IAW AMM 27-54-00, OPS CHECKED GOOD AND COMPLIED WITH AD 2009-06-12.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,156 hrs · 22,525 cycles

RT CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT BULB IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,174 hrs · 21,457 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED CRACKED DRAG ANGLE IAW EC/TC REO 601R-52-11-513.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,725 hrs · 19,922 cycles

THE THIRD CEILING EMERGENCY LIGHT IS INOP. REPLACED THE THIRD CEILING EMERGENCY LIGHT. OPS CHECK GOOD. DONE IAW THE AMM CHAPTER 33-51-16.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 22,315 hrs · 19,471 cycles

AFT EMERGENCY CEILING LIGHT IS INOP. R & R AFT EMERGENCY CEILING LIGHT BULB IAW AMM 33-51-16. OP'S CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 319) · airframe 21,614 hrs · 18,693 cycles

CONTINUATION OF MWC 248 LOWER SERVICE DOOR CLIP ON RBL 36 FS 319 ON FLOOR SUPPORT ANGEL FWD AREA IS CORRODED OUT OF LIMITS. PRIOR TO ACFT BEING RETURNED TO SERVICE. PERFORMED AND FOUND SATISFACTORY 12/27/10".

Part: STEP — CRACKED (PAX DOOR) · airframe 21,636 hrs · 18,717 cycles

NUTPLATE ATTACHMENT FLANGE ON PAX DOOR FWD WEB AT BOTTOM STEP 832AT TOP FWD ATTACHMENT SCREW LOCATION CRACKED IN VERTICAL FLANGE. DISCONNECTED PAX DOOR FWD COUNTERBALANCE GAS SPRING CABLE FROM ANCHOR FITTING SWIVEL LEVER IAW AMM 52-11-17-000-802. RECONNECTED PAX DOOR FWD COUNTERBALANCE GAS SPRING CABLE ANCHOR FITTING SWIVEL ELVER IAW AMM 52-11-17-400-802. ADJUSTED AND OPS TESTS GOOD. C/W EC/TC REO 601R-52-11-702 AND MET ALL THE REQUIREMENTS OF REO 601R-52-11-702 REV C. APPLIED PAINT AND CORROSION INHIBITOR TO FWD WEB REPAIR IAW SRM 51-25-01 AND 51-21-11. INSTALLED PAX DOOR FIXED STEP WITH ATTACHING HARDWARE IAW SRM 51-42-21, 51-41-04, ATTACHED LIGHT ASSY TO STEP WITH HARDWARE IAW SRM 51-41-04.

Part: WEB — BROKEN (PAX DOOR) · airframe 21,636 hrs · 18,717 cycles

NUTPLATE ATTACHMENT FLANGE ON PAX DOOR AFT WEB BROKEN OFF AND MISSING AT BOTTOM STEP 832AT TOP AFT ATTACHMENT SCREW LOCATION WITH CRACK EXTENDING INTO VERTICAL FLANGE. REMOVED PAX DOOR STEP 832BT IAW AMM 52-11-04-000-804. OK TO INSTALL STEP 832BT. INSTALLED PAX DOOR STEP 832BT IAW AMM 52-11-04-400-803, OP TEST GOOD. DISCONNECTED PAX DOOR AFT COUNTERBALANCE GAS SPRING CABLE FROM ANCHOR FITTING SWIVEL LEVER IAW AMM 52-11-17-000-802. RECONNECTED PAX DOOR AFT COUNTERBALANCE GAS SPRING CABLE TO ANCHOR FITTING SWIVEL LEVER IAW AMM 52-11-17-400-802, ADJUSTMENT AND OPS TESTS GOOD. C/W EC/TC REO 601R-52-11-702 AND MET ALL THE REQUIREMENTS OF REO 601R-52-11-702, REV C. PAX DOOR AFT WEB REQUIRES RIVETS PAINTED AND AREA DINITROL. PAINTED AFT WEB FASTENERS AND SEALANT IAW SRM 51-25-01. AFT WEB REQUIRES DINITROL. APPLIED DINITROL TO AFT WEB REPAIR IAW SRM 51-21-11. FOUND TO BE SATISFACTORY.

Part: SKIN — CRACKED (LT WING) · airframe 21,614 hrs · 18,693 cycles

LT WING OTBD L/E 530KL, SECOND SHROUDS FROM OTBD END HAS A NUTPLATE RIVET PULLING THROUGH SHROUD AT OTBD END & SKIN IS CRACKING. REMOVED 3 EA NUTPLATES FROM SHROUD IAW SRM 51-45-00 AND 51-42-06. INSTALLED 3 EA NUTPLATES ON SHROUD 2 EACH PN MS21061L08K NUTPLATES & 1 EA MS21047L3 NUTPLATE IAW SRM 51-45-00 & 51-42-06. REMOVED SHROUD. LOCATED AND DRILLED SERVICEABLE SHROUD IAW SRM 51-42-10. INSTALLED SERVICEABLE SHROUD IAW SB 601R-30-031, PAGE 21 OF 85 ITEMS 130-133 AND SRM 51-23-00 AND SRM 51-42-10.

Part: FRAME — CORRODED (BS 349) · airframe 21,614 hrs · 18,693 cycles

FS 349 FRAME IS CORRODED. INSTALLED NEW FRAME SECTION AT FS 349 IAW SRM 51-42-06 AND 51-42-21.

Part: SHEAR TIE — CORRODED (BS 319.7 S26-27L) · airframe 21,614 hrs · 18,693 cycles

FRAME FOOT CORRODED AT FS 319.7 BETWEEN STR 27 AND 26L. REMOVED CORROSION IAW SRM 51-21-06. ORIGINAL MAT .050, REM MAT .048. MAT LOSS .002. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 21,614 hrs · 18,693 cycles

FOUND REAR PRESSURE BULKHEAD HAS 2 ISOLATORS CRACKED AT LBL 9.0 AND RBL 9.0 APPROX WL 95. R & R 2EA ISOLATORS IAW SRM 51-42-13. (CLOSED)

Part: POST — CRACKED (BS 409) · airframe 21,614 hrs · 18,693 cycles

FOUND FS 409+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED AT WL 69.0 AFT FLANGE RADIUS APPROX .3" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. INSTALLED VERTICAL POSTS AT FS 409+128 BL 0, IAW SRM 51-42-06 AND 51-42-22.

Part: BULKHEAD — CRACKED · airframe 21,614 hrs · 18,693 cycles

FOUND REAR PRESSURE BULKHEAD WEB LBL 27.50, WL 130 HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 610R-53-61-1541, REV B.

Part: SUPPORT ANGLE — CRACKED (BS 605) · airframe 21,614 hrs · 18,693 cycles

CARGO DOOR SILL SUPPORT ANGLE AT STA 605 LBL 36 FOUND CRACKED WL 73. REPLACED IAW SRM 51-42-21. REPAIR IS CLASSIFIED AS A MINOR.

Part: STRAP — CORRODED (BS 310-349) · airframe 21,614 hrs · 18,693 cycles

PAX DOOR SURROUND LOWER FLOOR STRAP IS CORRODED BETWEEN FS 310 AND FS 349. REMOVED CORROSION FROM THE TOP OF THE PAX DOOR FLOOR SILL PLATE, MAX DEPTH REMOVED IS .005 AND IS WITHIN ALLOWABLE LIMITS OF T/E SRM 53-21-23 & 53-00-00. BLENDED CORROSION IAW SRM 51-21-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 21,614 hrs · 18,693 cycles

FLOOR SUPPORT CLIP AT RFS 484 LBL 27 IS CRACKED. REPLACED WITH NEW IAW SRM 51-42-21. MINOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 621-574) · airframe 21,614 hrs · 18,693 cycles

CARGO BAY FLOOR SUPPORT CAP AT LBL 27 FS 621 TO 574 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3778 AND SRM 51-42-06.

Part: ATTACH FITTING — CORRODED (BS 310) · airframe 21,614 hrs · 18,693 cycles

LOWER SERVICE DOOR CLIP ON RBL 36, FS 310 ON FLOOR SUPPORT ANGLE FWD AREA IS CORRODED OUT OF LIMITS. INSTALLED IAW SRM 51-42-06, 51-42-13 AND 51-42-21.

Part: ANGLE — CORRODED (BS 310-349) · airframe 21,614 hrs · 18,693 cycles

LOWER SERVICE DOOR CUTOUT, RBL 36 FRAME HAS MINOR CORROSION AROUND FLOORBOARD MOUNTING SCREW HOLES FROM FS 310.0 TO 349.0. UPON INVESTIGATION FOUND LOWER SERVICE DOOR CUTOUT ANGLE AT RBL 36 TO BE OUT OF LIMITS IAW SRM 51-21-06. REMOVED LOWER SERVICE DOOR CUTOUT RBL 36 ANGLE FS 310.0 TO 349.0 IAW SRM 51-42-11, 51-42-36, 51-42-21 AND 51-42-06. LOWER SERVICE DOOR ANGLE AT 36 RBL, FS 310 TO FS 349.0 REQS INSTALL. LOWER SERVICE DOOR ANGLE REPLACED 601R38303-253 IAW SRM 51-42-21. REF MX WORK CARD 248, JOB 8750321 FOR FWD CLIP INSTALLATION. RBL 26, STA 310. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: CARGO TRACK — CORRODED · airframe 21,614 hrs · 18,693 cycles

CARGO TRACK IS CORRODED. LOCATED, DRILLED 7 COUNTERSUNK HOLES IN NEW CARGO TRACK IAW SRM 51-41-02. INSTALLED NEW SERVICEABLE CARGO TRACKS IAW AMM 53-01-11-400-802. MINOR REPAIR.

Part: FRAME — CORRODED (BS 349) · airframe 21,614 hrs · 18,693 cycles

FS 349 FRAME CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-15 AND 53-00-00. LOCATED, DRILLED AND DEBURRED & INSTALLED NEW FRAME IAW SRM 51-42-06.

Part: UNKNOWN — CORRODED (BS 333) · airframe 21,614 hrs · 18,693 cycles

FS 333 BOTTOM SECTOR IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-21-15 AND 53-00-00. R & R FRAME IAW SRM 51-42-06 & 51-42-21, PN 601R32004-55.

Part: SKIN — CHAFED (E/E DOOR AREA) · airframe 21,614 hrs · 18,693 cycles

AVIONICS DOOR SURROUND INNER SKIN IS CHAFED AND CORRODED. REPAIRED IAW REO 601R-53-21-676 REV B

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 21,614 hrs · 18,693 cycles

INTERCOSTALS FROM FS 349-364 BETWEEN STRS 26L-26R ARE CORRODED 2 EA. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-00. MINOR REPAIR.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 20,422 hrs · 17,285 cycles

RECEIVED "GEAR DISAGREE" WARNING DURING LANDING CHECK. NOSE WHEEL WOULD NOT EXTEND. FOLLOWED QRH PROCEDURE. CYCLED LANDING GEAR SEVERAL TIMES WITH NO SUCCESS. USED MANUAL RELEASE TO GET NOSE LOCKED DOWN. (EMERGENCY DECLARED) R & R NLG SELECTOR VALVE IAW AMM 32-33-10. OPS AND LEAK CHECK GOOD. ( CLOSED )

Part: DOOR — STUCK (MAIN PAX) · airframe 19,647 hrs · 16,433 cycles

UNABLE TO OPEN PAX DOOR FROM INSIDE. DIFFICULT TO OPEN FROM OUTSIDE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,607 hrs · 15,339 cycles

REFER AFDL 456108-2 STAB TRIM CAUTION, MACH TRIM CAUTION. RAN QRH AND RETURNED. EMERGENCY DECLARED, FLT 4923 DEL 108 MINS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,042 hrs · 14,819 cycles

RBL 9 FS 280 INBOARD CLIP IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 18,042 hrs · 14,819 cycles

LBL 9 OUTBOARD FITTING IS CRACKED AT FS 280. REMOVED AND REPLACED WITH A NEW IAW SRM 51-42-21. REINSTALLED SAME SERVICEABLE ALT RELEASE CABLE BRACKET IAW SRM 51-41-02. OPS CHECK OF MLG ALT RELEASE DUE. PERFORMED THE OPS TEST OF THE LANDING GEAR MANUAL-RELEASE SYSTEM IAW AMM 32-34-00-710-801. NO DEFECTS NOTED AT THIS TIME.

Part: BEAM — CRACKED (FUSELAGE) · airframe 18,042 hrs · 14,819 cycles

VERTICAL BEAM AT FS 409+128, RBL 18.0 CRACKED AT LOWER FASTENER HOLE OTBD SIDE, APPROX .3 INCH IN LENGTH.

Part: POST — UNKNOWN (FUSELAGE) · airframe 18,042 hrs · 14,819 cycles

JOB 8750315 OPERATION 156 RT FS 409+128 VERTICAL POST RBL 18.0 I/B AND O/B POST HAS INDICATIONS NOTED AT WL 69.0 APPROX .3" IN LENGTH 65% FULL SCREEN HEIGHT FAILED NDT INSPECTION.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,042 hrs · 14,819 cycles

FS 559 BULKHEAD WEB AND CAP ANGLE HAVE INDICATIONS NOTED RBL 18, WL 59.10 APPROX .1250 INCH LONG AND LBL IN CAP ANGLE RADIUS APPROX .30 INCH LONG. C/W REO 601R-53-41-260 REV C REPAIR TO PRESSURE BULKHEAD STRUCTURE. C/W EC/TC REO 601R-53-41-260 IAW REO 610R-53-41-260 REV C.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 18,042 hrs · 14,819 cycles

FLOORBEAM FLANGE DAMAGED AT FS 589.00, LBL 9.0 FLANGE IS BENT, AND CRACKED APPROX .75 INCH LONG. REPAIRED FLOORBEAM FLANGE IAW REO 601R-53-00-279 AND REO 601R-53-00-027. LOCATED 12 HOLES AND INSTALLED FASTENERS IAW REO 601R-53-00-027. C/W EC/TC REO 601R-53-00-279 AND MET ALL THE REQUIREMENTS OF REO 601R-53-00-279.

Part: SKIN — CRACKED (PAX DOOR) · airframe 18,042 hrs · 14,819 cycles

PAX DOOR SIDE SKIN IS CRACKED AT HANDRAIL SUPPORT FITTING AFT SIDE NOTE SIDE SKIN HAS A PREVIOUS REPAIR IN ZONE 4. SKIN IS ALSO CRACKED AT ZONE 3. REMOVED PAX DOOR COUNTERBALANCE AND PREVIOUS REPAIR IAW AMM 52-11-17-000-801 AND SRM 51-42-06. PAX DOOR SIDE SKIN REQUIRES REPAIR AND COUNTERBALANCE REQUIRES INSTALL. REPAIRED THE AFT PAX DOOR WEB IAW REO 601R-52-11-702, REV A AND REO 601R-52-11-1622. REINSTALLED AFT COUNTERBALANCE GAS SPRING IAW AMM 52-11-17-400-802. SEALED IAW SRM 51-23-00 AND PAINTED IAW SRM 51-25-01. COMPLETED INSTALLATION OF AFT COUNTERBALANCE IAW AMM 52-11-17-400-802. CHECK GOOD IAW AMM 52-11-17-710-802.

Part: SKIN — CRACKED (PAX DOOR) · airframe 18,042 hrs · 14,819 cycles

PAX DOOR SIDE SKIN IS CRACKED AT HANDRAIL SUPPORT FITTINGS FWD SIDE. REPAIRED PAX DOOR FWD SIDE SKIN AT HARDWARE SUPPORT FITTING IAW REO 601R-52-11-702. COMPLIED WITH EC/TC REO 601R-52-11-702 AND MET ALL REQUIREMENTS OF REO 601R-52-11-702 REV A.

Part: HOUSING — CORRODED (ESCAPE HATCH) · airframe 18,042 hrs · 14,819 cycles

CREW ESCAPE HATCH HAS WATER AND SIGNS OF CORROSION AROUND OUTER HANDLE SPRING AND HSG.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,042 hrs · 14,819 cycles

JOB 8750311 OPERATION 210 PAX DOOR FWD DRAG ANGLE CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,042 hrs · 14,819 cycles

LT FS 621-625 INTERCOSTAL ANGLE CRACKED .3" LONG. REMOVED DAMAGED LT INTERCOSTAL ANGLE AND REPLACED WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-21.

Part: FLAP — FAILED (WING) · airframe 17,958 hrs · 14,737 cycles

FLAPS FAILED AT 20 WHEN SELECTING 8 AFTER TAKEOFF. AIRCRAFT RETURNED TO ATW AFTER T/O, EMERGENCY VEHICLES ROLLED AS A PRECAUTION. FLT 5476 CX

Part: MOTOR — MALFUNCTIONED (DOOR ASSIST) · airframe 1,672,144 hrs · 13,615 cycles

PAX DOOR WOULD NOT OPEN ALL THE WAY. T/S SYSTEM - FOUND DOOR ASSIST MOTOR HOLDING DOOR. CYCLED C/B FOR DOOR ASSIST. DOOR OP CHECKS OK IAW AMM 52-11-00. (B)

Part: SIGN — BROKEN (CABIN) · airframe 16,530 hrs · 13,444 cycles

EXIT SIGN ABOVE SERVICE DOOR IS BROKEN.

Part: HANDLE — INOPERATIVE (SERVICE DOOR) · airframe 16,444 hrs · 13,366 cycles

SERVICE DOOR HANDLE INOP.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 15,862 hrs · 12,857 cycles

ASD HANDLE CRACKED.

Part: DOOR — STUCK (AIRSTAIR DOOR) · airframe 15,782 hrs · 12,790 cycles

FLT 4822, UNABLE TO OPEN ASD.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 14,906 hrs · 11,958 cycles

RIGHT WING EMERGENCY LIGHT INOP.

Part: DOOR — STIFF (MAIN PAX) · airframe 14,791 hrs · 11,836 cycles

F/A REPORTS THAT THE PAX DOOR IS HARD TO CLOSE. MAIN HANDLE WILL NOT STOW ALL THE WAY DOWN.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 14,509 hrs · 11,557 cycles

LEFT FS 640 FUSELAGE SKIN BONDED DOUBLER IS CRACKED JUST AFT OF THE BOX BEAM. [07-23-07] COMPLIED WITH REO 601R-53-61-506 REPAIRED BONDED DOUBLER REFER TO EC/TC EO REO 601R-53-61-506.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,291 hrs · 11,327 cycles

LEFT WINDOW HEAT CAUTION MSG, 1 RESET LIGHT CAME BACK ON AFTER 5 MIN WITH A VERY FAINT ELECTRICAL ODOR IN COCKPIT AND GALLEY WHEN LIGHT CAME BACK ON. A/C RETURNED TO ATL AFTER T/O. FLT 4719 DEL 176 MINS.

Part: UNKNOWN — UNKNOWN (TE FLAPS) · airframe 14,228 hrs · 11,277 cycles

PILOT REPORTED, AFTER TAKEOFF ON FLAP RETRACTION, GOT -FLAPS FAIL- MSG. EICAS SHOWS LEFT AT 18 & RIGHT AT 20. EN ROUTE TO ATL, A/C DIVERTED TO BTR DUE TO MTC. EMERGENCY DECLARED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 14,098 hrs · 11,148 cycles

CLIP CRACKED AT UPPER HI-LITE I/B OF LBL 9 AT FS 280.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 14,098 hrs · 11,148 cycles

FS 280 FWD FLOOR SUPPORT STRUCTURE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,098 hrs · 11,148 cycles

ANGLE CRACKED AT LOWER AFT LOCKPIN FITTING ON PAX DOOR FRAME. (FLAGGED) REPAIRED SEAL STRIKER IAW SRM SUPPLEMENT 53-21-23 REV A. USING 2024 T-3 0.050 PO 8398-1 AND MS204705-5 PO 9506-1 EA934NA PO 9775-1 DT1097 2-20-07 REF TO WORK CARD 289 FOR LPI TEST. RA339. [SUPPLEMENTAL--SDR CLOSED 2/22/07]

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,098 hrs · 11,148 cycles

CRACKED ANGLE O/B OF LBL 27 AT FS 484.00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,098 hrs · 11,148 cycles

OUTBOARD OF RBL 27 ANGLE CRACKED AT FS 484.

Part: WINDOW — CRACKED (CABIN) · airframe 14,098 hrs · 11,148 cycles

PASSENGER WINDOW LEFT SIDE FS 409 CRACKED. (MARKED) REMOVED LT SIDEWALL PANEL 251 ALW IAW CRJ AMM 25-26-01. REMOVED CRACKED SHIELD FROM SIDEWALL PANEL 251 ALW AND REPLACED WITH SERVICEABLE SHIELD P/N 3864045-1. ALL WORK DONE IAW CRJ AMM 25-26-01. OK TO INSTALL SIDEWALL PANEL 251 ALW. INSTALLED SIDEWALL PANEL 251 ALW IAW CRJ AMM 25-26-01. COMPLIED WITH EC/TC REO 601R-26-25-004. DAMAGE WAS TO PASSENGER SIDEWALL PANEL GLARESHIELD. PASSENGER WINDOW FOUND TO BE IN A SERVICEABLE CONDITION. NO FUTHER ACTION REQUIRED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 13,668 hrs · 10,776 cycles

WHILE COMPLYING WITH EO60053-69-0002 FRAME 640 INSPECTIONS, SUSPECT RT DOUBLER TO BE CRACKED AT CENTER SECTION.

Part: LIGHT — BROKEN (CABIN) · airframe 13,230 hrs · 10,407 cycles

EMERGENCY LIGHT JUST INSIDE OF PAX DOOR JUST BELOW ARROW ON FWD WALL BROKEN.

Part: TRIM SYSTEM — INOPERATIVE · airframe 12,970 hrs · 10,182 cycles

STAB TRIM WILL NOT ENGAGE (TOWER ROLLED EMERGENCY VEHICLES AS A PRECAUTION).

Part: PLACARD — PEELING (AIRSTAIR DOOR) · airframe 12,741 hrs · 10,005 cycles

ASD EXIT PLACARD PEELING LOOSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,570 hrs · 9,869 cycles

EMERGENCY EXIT LIGHT AT SERVICE DOOR HAS BULBS INOP.

Part: LINK — CRACKED (STEP) · airframe 12,282 hrs · 9,644 cycles

ASD BOTTOM STEP CRACKED AT ATTACH LINK.

Part: UNKNOWN — UNKNOWN (FLAP SYS)

DURING DESCENT, THE CREW RECEIVED A FLAPS FAIL MESSAGE. THE CREW COMPLIED WITHT HE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY. MAINTENANCE COMPLIED WITH EO WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: INTERCOSTAL — CRACKED (FS 280)

DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 280, RBL 9, AT THE FLOOR SUPPORT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL, AT FS 280, RBL 9 FLOOR SUPPORT IAW BOMBARDIER REO 601R-53-11-171. (M)

Part: PLACARD — DETERIORATED (COCKPIT)

DURING A C-CHECK IN MCN, FOUR CREW EMERGENCY EXIT PLACARDS WERE FOUND TO BE DETERIORATED. MAINTENANCE WILL REMOVE AND REPLACE THE FOUR CREW EMERGENCY EXIT PLACARDS. (M)

Part: HINGE — CORRODED (FUSELAGE)

DURING A C-CHECK, THE PASSENGER DOOR TOP STEP UPPER HINGE HALF WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR TOP STEP UPPER HINGE. (K)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR BOTTOM STEP. (M)

Part: HINGE — CORRODED (PAX DOOR STEP)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR TOP STEP UPPER HINGE HALF WAS FOUND TO BE CORRODED. (M)

Part: SEAT TRACK — CORRODED (BS 559)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT FLOOR TRACKS AT FS 559 PLUS 96, RBL 27 AND RBL 9, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT FLOOR SEAT TRACKS AT FS 559 PLUS 96, RLB 27 AND RBL 9, IAW CRJ 200 SRM 51-40-00. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK, THE INTERCOSTAL AT FS 484, RBL 27, WAS FOUND TO BE CRACKED BEYOND LIMITS. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)

Part: LENS — CRACKED (GALLEY)

DURING C-CHECK, THE EMERGENCY EXIT LENS, FORWARD OF THE SERVICE DOOR, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE EMERGENCY EXIT LENS, FORWARD OF THE SERVICE DOOR. (K)

Part: COVER — BROKEN (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN COVER BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN ATL, THE NR 1 BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTS WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION IN ATL, THE FLOOR EMERGENCY LIGHT STRIP FROM ROW 5 FORWARD, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLOOR EMERGENCY LIGHT STRIP, FROM ROW 5 FORWARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PUMP — MALFUNCTIONED (HYD SYSTEM)

DURING DESCENT INTO CRW FROM ATL, AT APPROXIMATELY 20,000 FEET THE CREW RECEIVED A 3A HYD LOW PRESS CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED TO TRI AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE 3A HYDRAULIC PUMP. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT THE STAY ROD LOWER ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVE AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

DURING AN A-CHECK IN MCN, THE BOTTOM STEP AT THE ATTACH LINK ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT OB ANGLES AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT OB ANGLES ON THE LT AND RT SIDES IAW EO 600-53-0105.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FLOOR SUPPORT CLIP AT FS 484, LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT CLIP AT FS 484, LBL 36 IAW EO 600530098.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT AND RT CLIPS BELOW THE BOX BEAM AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT AND RT CLIPS BELOW THE BOX BEAM AS FS621.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE OB CLIP AT FS 280, LBL 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE OB CLIP AT FS 280, LBL 9 IAW SRM 51-42-21.

Part: CLIP — CRACKED (FUSELAGE)

DURING A (C) CHECK, THE OB CLIP AT FS 280, RBL 9 IN THE AVIONICS EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE OB CLIP AT FS 280, RBL9 IN THE AVIONICS EQUIPMENT BAY.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE IB CLIPS AT FS280, LBL9 AND RBL 9 IN THE FORWARD AVIONICS EQUIPMENT BAY WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE IB CLIPS AT FS280, LBL9 AND RBL9 IN THE FORWARD AVIONICS EQUIPMENT BAY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION, THE RT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: ODOR — DETECTED (CABIN)

FLT 4677 - DURING CLIMB-OUT FROM MCN-ATL, THE LAVATORY SMOKE CAUTION LIGHT ILLUMINATED AND AN ELECTRICAL SMOKE SMELL OCCURRED. THE CAUTION LIGHT EXTINGUISHED. THE CREW COMPLIED WITH THE QRH AND PULLED THE APPROPRIATE CIRCUIT BREAKERS AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE RESET THE ASSOCIATED CIRCUIT BREAKERS. THE WIRING AND CONNECTORS IN THE LAVATORY WERE INSPECTED WITH NO ABNORMALITIES DISCOVERED. THE LAVATORY SMOKE DETECTOR ALSO TESTED GOOD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS)

FLT 4484 - WHILE DESCENDING THROUGH FL310, FROM DAL TO ATL, A 'HYD 1 LOW PRESS' MESSAGE WAS RECEIVED BY THE PILOT. THE HYDRAULIC QUANTITY SHOWED ZERO. THE PILOT SLOWED DOWN TO 250 KNOTS PER QRH PROCEDURES AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE NOTED A TOTAL LOSS OF HYDRAULIC QUANTITY. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP DUE TO IT BEING RUN DRY FOR APPROX 37 MINUTES. MAINTENANCE ALSO REPLACED THE NR 1 HYDRAULIC PRESSURE TUBE WHICH WAS DETERMINED TO BE THE SITE OF THE LEAK. LEAK AND OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BPSU — FAILED (T/E FLAP)

FLT 4720 - DURING CLIMB-OUT OF MTY TO ATL, FLAPS RETRACTED ON SCHEDULED. THEN, AT APPROXIMATELY 5000 FEET, THE CAPTAIN RECEIVED A 'FLAPS FAIL' CAUTION MESSAGE. THE FLAPS WERE VERIFIED AT ZERO DEGREES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT MADE AN UNEVENTFUL LANDING IN ATL. MAINTENANCE REMOVED AND REPLACED THE RIGHT BRAKE AND POSITION SENSOR UNIT. (M)