N830AS

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 37,432 hrs · 32,942 cycles

COULD NOT OPEN PAX DOOR FROM THE OUTSIDE, HAD TO GO IN THRU THE SERVICE DOOR AND OPEN THE DOOR FROM THE INSIDE. CLEANED AND LUBED PAX DOOR. PERFORMED OPS CK IAW AMM 52-11-00. NO DEFECTS NOTED.

Part: PUSHROD — OUT OF ADJUST (PAX DOOR) · airframe 37,237 hrs · 32,773 cycles

PAX DOOR WONT OPEN EASILY. FOUND PUSHROD TO LATCH CAM TORQUE TUBE TO BE OUT OF ADJUSTMENT. ADJUSTED PUSHROD IAW AMM 52-11-21. OPS CHECKED GOOD IAW AMM 52-11-00.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 37,226 hrs · 32,763 cycles

PASSENGER DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE AT GATE. CLEANED AND LUBED PAX DOOR IAW AMM 12-20-52. OPS CHECKED GOOD IAW AMM 52-11-00.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,612 hrs · 32,220 cycles

LIGHTED FLOOR LEVEL EXIT SIGN INOPERATIVE AT LEFT EMERGENCY EXIT. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,558 hrs · 32,171 cycles

EXTERIOR EMERGENCY LIGHT NR 4 INOPERATIVE. R & R LIGHT ASSY IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 35,668 hrs · 31,382 cycles

NR 3 EMERGENCY CEILING LIGHT COVER MISSING. INSTALLED COVER IAW AMM 33-51-16. NO FURTHER DEFECT NOTED.

Part: SKIN — CRACKED (LT WING) · airframe 35,588 hrs · 31,307 cycles

LT WING FUEL ACCESS PANEL 540EB HAS AN INDICATION ON THE INBD SIDE APPROX .5 X .25" 50 PERCENT FSH FAILED NDT INSPECITON. COMPLIED WITH ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV K.

Part: SKIN — CRACKED (RT WING) · airframe 35,588 hrs · 31,307 cycles

LOWER WING PLANK RT BOOST PUMP CUT OUT LANDING FOR ACCESS PANEL HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE FAILED NDT INSPECTION. REMOVED CORROSION IAW SRM 51-21-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,588 hrs · 31,307 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .3" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH ECTC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541 REV D, DATED: 10/31/2011.

Part: ANGLE — CRACKED (BS 625) · airframe 35,588 hrs · 31,307 cycles

BS 625 ANGLE CRACKED. REMOVED ANGLE IAW SRM 51-42-21. LOCATED, DRILLED & INSTALLED NEW ANGLE IAW SRM 51-40-11 & 51-42-21.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 35,588 hrs · 31,307 cycles

LT CABIN EMERGENCY LIGHT SECTIONS FAIL INSPECTION. COVERS ARE CRACKED AND CRAZED AND LIGHTS ARE FADED. REMOVED DAMAGED SECTIONS AND INSTALLED SERVICEABLE IAW AMM 33-51-01-400-806.

Part: LIGHT — DAMAGED (CABIN) · airframe 35,588 hrs · 31,307 cycles

EMERGENCY LIGHT SECTIONS NR 1 AND 2 FAIL INSPECTION. LENS ARE CRACKED AND CRAZED AND LIGHT STRIPS ARE FADED AND DIM. REMOVED DAMAGED LIGHTS AND INSTALLED SERVICEABLE LIGHTS IAW AMM 33-51-01-400-806.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 35,588 hrs · 31,307 cycles

INTERCOSTAS BETWEEN STRINGERS 12A & 13A LT AT FS 625 ARE CRACKED. REMOVED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 35,588 hrs · 31,307 cycles

SEAT TRACK BETWEEN BS 409 AND 409+128 HAS CORROSION AROUND FASTENERS. FABRICATED, DRILLED AND LOCATED NEW SEAT TRACK IAW REO 601R-53-00-485. REMOVED SEAT TRACK IAW SRM 51-41-02-00 AND INSTALLED IAW REO 601R-53-00-485.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,588 hrs · 31,307 cycles

FS 280 FLOORBEAM AFT ANGLE IS CORRODED AROUND FASTENER HOLES FROM LBL 9 TO RBL 9. R & R ANGLE IAW REO 601R-53-11-926, REV B. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 35,588 hrs · 31,307 cycles

SEAT TRACK BETWEEN BS 409 AND 409+128 HAS CORROSION AROUND FASTENERS. FABRICATED NEW SEAT TRACK SECTION, LOCATED AND DRILLED PREPPED SURFACE AND TOP COATED IAW REO 601R-53-00-485. REMOVED SEAT TRACK IAW SRM 51-41-02-00 AND INSTALLED IAW REO 601R-53-00-485.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 35,588 hrs · 31,307 cycles

REAR PRESSURE BULKHEAD FORWARD FACE HAS BROKEN ISOLATORS. REMOVED BROKEN ISOLATORS IAW SRM 51-42-10 AND REPLACED IAW SRM 51-42-13.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 35,587 hrs · 31,306 cycles

BS 484 FLOOR SUPPORT PREVIOUS REPAIR ANGLE IS CRACKED, AT RBL 36.00. REMOVED & INSTALLED NEW ANGLE IAW 51-42-21 AND REO 601R-53-41-059. FABRICATED ANGLE IAW REO 601R-53-41-059, FROM S6144-14.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 35,587 hrs · 31,306 cycles

BS 280, FLOORBEAM ANGLE HAS THREE CRACKS AT LBL 9 - RBL 9 . REMOVED FLOORBEAM ANGLES IAW SRM 51-42-21. REPLACED DURING INCORPORATION OF REO 601R-53-11-926.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 35,588 hrs · 31,307 cycles

SEAT TRACK LBL 9 CORRODED FROM BS 364-394. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SKIN — CORRODED (RT WING) · airframe 35,587 hrs · 31,306 cycles

RT WING SKIN ACCESS HOLE -640BB HAS AERAS OF CORROSION. COMPLIED WITH ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV K.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 35,587 hrs · 31,306 cycles

BS 280 FLOORBEAM FWD ANGLE CORRODED LBL 9 - RBL 9. REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06 & 51-42-21.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 35,587 hrs · 31,306 cycles

PAX DOOR HANDLE IS DIFFICULT TO OPEN FROM OUTSIDE, INNER DOOR PLUNGER IS TOUGH TO CLOSE, PAX DOOR LATCH CAUTION MESSAGE IN FLIGHT. ADJUSTED THE PULL-IN LEVER TORQUE TUBE PUSH ROD & THE LATCH CAM TORQUE TUBE PUSH ROD IAW AMM 52-11-21-820-802, SUBTASK 52-11-21-830-004, PARA 9, ITEM C7. FUNCTIONAL & OPS CHECKED IAW AMM 52-11-00-720-801 & 52-11-00-710-801 & PAX DOOR SYSTEM CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 349-379) · airframe 35,588 hrs · 31,307 cycles

PASSENGER COMPARTMENT FLOOR SUPPORT CORRODED AT LBL 45 FROM BS 349-379. REMOVED FLOOR SUPPORT IAW SRM 51-42-66. LOCATED & DRILLED NEW FLOOR SUPPORT IAW 51-40-11.

Part: SKIN — CHAFED (LT AILERON) · airframe 35,587 hrs · 31,306 cycles

LEFT AILERON UPPER L/E IS CHAFED IN SEVERAL AREAS, ALL ALONG L/E SURFACE. DEEPEST CHAFE APPROX .005 DEEP. COMPLIED WITH STEPS NR 1 THRU NR 3 OF REO 601R-57-60-013, REV NC AND COMPLIED WITH EC/TC REO 601R-57-60-013 IAW REO 601R-57-60-013.

Part: SKIN — CRACKED (RT WING) · airframe 35,587 hrs · 31,306 cycles

.8 INCH CRACK IN RT WING LOWER WING PLANK. COMPLIED WITH EC/TC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV J. COMPLIED WITH EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131, REV A.

Part: HANDLE — STIFF (PAX DOOR) · airframe 35,528 hrs · 31,254 cycles

PASSENGER DOOR HANDLE IS DIFFICULT TO OPEN FROM OUTSIDE. IT IS ALSO DIFFICULT TO STOW THE HANDLE INSIDE AT TIMES. DID FIT AND CLEARANCE CHECK OF DOOR HANDLE, OPS CHECK GOOD IAW AMM 52-11-03.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 34,868 hrs · 30,630 cycles

PAX DOOR WONT OPEN FROM OUTSIDE. PERFORMED OPS TEST OF PAX DOOR SEVERAL TIMES, AND LUBED PAX DOOR HANDLE INNER MECHANISM. OPS GOOD IAW AMM 52-11-00 ACFT OK FOR SERVICE.

Part: DOOR — BINDING (MAIN PAX) · airframe 34,590 hrs · 30,377 cycles

CREW REPORTS THAT THE PASSENGER DOOR IS DIFFICULT TO OPEN. REMOVED EXCESS AMOUNT OF GREASE FROM PASSENGER DOOR LOCKPINS AND CAMLOCKS IAW AMM 12-20-52. NO FURTHER DEFECTS NOTED.

Part: LATCH — LACK OF LUBE (PAX DOOR) · airframe 34,052 hrs · 29,877 cycles

PAX DOOR LATCH HARD TO CLOSE OR OPEN. LUBRICATED PASSENGER DOOR HANDLE LATCH. OPS CHECKED OK MM 52-10-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 33,698 hrs · 29,566 cycles

RIGHT SIDE ABOVE WING EMERGENCY LIGHT HSG BROKEN. R & R THE RT SIDE EMERGENCY LIGHT COVER IAW AMM 33-51-21. OPS CHECK GOOD. CDL CLEARED. MCC NOTIFIED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 33,698 hrs · 29,566 cycles

LEFT SIDE AFT ABOVE WING EMERGENCY LIGHT HSG BROKEN. R & R THE LT SIDE EMERGENCY LIGHT COVER IAW AMM 33-51-21. OPS CHECK GOOD. CDL CLEARED. MCC NOTIFIED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 33,698 hrs · 29,566 cycles

R & R THE LT SIDE ABOVE WING EMERGENCY LIGHT HOUSING BROKEN. R & R THE LT SIDE EMERGENCY LIGHT COVER IAW AMM 33-51-21. OPS CHECK GOOD. CDL CLEARED. MCC NOTIFIED.

Part: TIRE — FAILED (NLG) · airframe 32,388 hrs · 28,373 cycles

RIGHT NOSE TIRE BLEW AT V1 (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION). PERFORMED VISUAL INSP OF NLG AND DOORS IAW AMM-32-20-00. NO DEFECTS NOTED AT THIS TIME. R & R RT AND LT NOSEWHEEL AND TIRE ASSY IAW AMM-32-42-01. (SDR CLOSED)

Part: FIXTURE — BURNED (GALLEY LIGHT) · airframe 32,158 hrs · 28,158 cycles

BURNING ODOR IN COCKPIT AND GALLEY AREA. (WORK LIGHTS) R & R BURNED GALLEY LIGHT FIXTURE. OPS CHECKED GOOD IAW AMM 33-26-047.

Part: APU — SMOKE (APU BAY) · airframe 30,985 hrs · 27,121 cycles

AFTER APU SHUTDOWN, THERE WAS A LARGE AMOUNT SMOKE COMING FROM APU EXHAUST AREA AUXILIARY POWER UNIT APU. DOOR POSITION VERIFIED CLOSED. R & R APU ASSEMBLY IAW AMM 49-10-00. OPS AND LEAK CHECKED GOOD.

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 30,902 hrs · 27,037 cycles

WARDROBE AFT EMERGENCY LIGHT HOUSING BROKEN. R & R FLOOR LEVER EMERGENCY FLOOD LIGHT HOUSING ON WARDROBE IAW AMM 33-51-19-000-801 & 33-51-19-400-801. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 30,892 hrs · 27,029 cycles

SERVICE DOOR THRESHOLD ANGLE CORRODED. REMOVED SILL ANGLE IAW SRM 51-42-21. SILL ANGLE AND INSTALLED IAW SRM 51-40-11 AND SRM 51-42-21.

Part: CROSSBEAM — CORRODED (BS 349) · airframe 30,886 hrs · 27,023 cycles

CORROSION ON CROSSBEAM AT 349 AND RBL 41 TO RBL 42. REPAIRED IAW SRM 51-24-06 AND REO 601R-53-21-2224.

Part: BULKHEAD — CRACKED (BS 625) · airframe 30,886 hrs · 27,023 cycles

AFT EQUIPMENT BAY, PRESSURE BULKHEAD RT CLIP CRACKED AT FS 625.

Part: BRACKET — CRACKED (CARGO DOOR) · airframe 30,911 hrs · 27,045 cycles

CARGO DOOR FWD RAIL SUPPORT BOTTOM BRACKET CRACKED. REMOVED CARGO DOOR FWD RAIL SUPPORT BRACKET FOR REPLACEMENT IAW SRM 51-41-02 & SRM 51-42-06. DRILLED NEW SUPPORT BRACKET IAW SRM 51-40-11 & ALODINED HOLES IAW SRM 51-21-11. INSTALLED NEW BRACKET ONTO CARGO DOOR FWD RAIL WET WITH SEALANT IAW SRM 51-42-06, SRM 51-41-02 AND SRM 51-25-16.

Part: STAND OFF — CRACKED (FUSELAGE) · airframe 30,911 hrs · 27,045 cycles

CARGO COMPARTMENT AFT BULKHEAD STAND OFF BRACKET CRACKED RT PRESSURE BULKHEAD 1ST FROM FLOOR. REMOVED AND INSTALLED NEW STAND OFF MOUNT IAW SRM 51-77-00, 51-42-13.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 30,886 hrs · 27,023 cycles

CORROSION ON FLOORBEAM AT FS 349. RBL 41 TO RBL 42. REPAIRED IAW REO 601R-53-21-2224, STEP 1 & 2.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 30,886 hrs · 27,023 cycles

CARGO TRACK CORRORED AT 559.00 + 80 AND LBL 9. REMOVED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED CARGO TRACK IAW AMM 20-21-00-910-801.

Part: STRUCTURE — CRACKED (BS 625 BULKHEAD) · airframe 30,886 hrs · 27,023 cycles

AFT EQUIPMENT BAY, PRESSURE BULKHEAD RT CLIP CRACKED AT FS 625. R & R FWD CARGO DOOR INNER SEAL RETAINER IAW SRM 51-40-11-001-001 AND SRM 51-41-02-001-001.

Part: STAND OFF — CRACKED (FUSELAGE) · airframe 30,911 hrs · 27,045 cycles

CARGO COMPARTMENT AFT BULKHEAD STAND OFF BRACKET CRACKED RT PRESSURE BULKHEAD 1ST FROM FLOOR. REMOVED AND INSTALLED NEW STAND OFF MOUNT IAW SRM 51-77-00, 51-42-13.

Part: THRESHOLD — CORRODED · airframe 30,911 hrs · 27,045 cycles

SERVICE DOOR THRESHOLD CORRODED. REMOVED CORROSION IAW SRM 51-21-06. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REPAIRED IAW SRM 51-42-21 AND 51-42-06.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 30,886 hrs · 27,023 cycles

CARGO TRACK CORRORED AT 559.00 + 80 AND RBL 27. REMOVED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED CARGO TRACK IAW AMM 20-21-00-910-801.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 30,886 hrs · 27,023 cycles

CARGO TRACK CORRORED AT FS 559.00 + 80 AND LBL 27. REMOVED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED CARGO TRACK IAW AMM 20-21-00-910-801.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 30,886 hrs · 27,023 cycles

CARGO TRACK CORRORED AT 559.00 + 80 AND RBL 9. REMOVED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED CARGO TRACK IAW AMM 20-21-00-910-801. REPLACE DAMAGED SEAT TRACK.

Part: CARGO TRACK — CORRODED · airframe 30,886 hrs · 27,023 cycles

CARGO TRACK CORRORED AT 559.00 + 112 AND LBL 9. REMOVED CARGO TRACK IAW AMM 53-01-44-000-802. INSTALLED TRACK RAIL IAW AMM 20-21-00-910-801. REPLACED DAMAGE CARGO TRACK. MATCH DRILLED AND CUT NEW SECTION OF CARGO TRACK IAW SRM 51-40-11 AND 51-24-36.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 30,886 hrs · 27,023 cycles

CARGO TRACK CORRORED AT 559.00 + 112 AND RBL 9. REMOVED CARGO TRACK AT 559.00+112 RBL 9 IAW AMM 53-01-11-000-802. INSTALLED TRACK RAIL IAW AMM 20-21-00-910-801.

Part: DOOR — BINDING (MAIN PAX) · airframe 30,568 hrs · 26,737 cycles

MAIN DOOR WILL NOT OPEN FROM OUTSIDE. CYCLED THE PAX DOOR SEVERAL TIMES. NO DEFECTS NOTED IAW AMM 52-10-01.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,458 hrs · 25,771 cycles

STARTED THE APU ON DESCENT DID NOT START. WAITED 2 MINUTES. RESTARTED THE APU. WE HAD A STRONG FUEL ODOR THROUGHOUT THE PLANE. SHUT DOWN APU. STRONG ODOR REMAINED UNTIL WE OPENED THE DOOR AT THE GATE. CREWS WERE REQUESTED TO MEET ACFT AS A PRECAUTION. PERFORMED OPS CHECK OF APU IAW AMM 49-00-00. NO DEFECT NOTED. ALSO PERFORMED LEAK CHECK OF APU FUEL CONTROL AND LINES. NO LEAKS NOTED. CANNOT DUPLICATE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (PAX DOOR)

PASSENGER DOOR WARNING IN FLIGHT. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED. ADJUSTED FWD AND AFT LATCH PROX SENSORS (PS5M3 AND PS6MB) IAW AMM 52-70-04. OPS CHECKED GOOD.

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 28,167 hrs · 24,607 cycles

HYD SYS 2 FAILURE IN FLIGHT PRESSURE AND QTY INDICATE 0. (EMERGENCY DECLARED -- ENROUTE TO IAD ACFT DIVERTED DUE TO MX) FOUND HYD SYS NR 2 PRESSURE LINE ON BRAKE CONTROL VALVE LEAKING. R & R HYD LINE IAW AMM 20-22-01 LEAK CHECK GOOD. (CLOSED)

Part: PLACARD — UNKNOWN (CABIN) · airframe 26,387 hrs · 22,975 cycles

PAX DOOR PLACARDS (7) TOTAL NEED REPLACED. "OPEN" , "TO OPEN LIFT HANDLE/PUSH DOOR", "EXIT", AND STRIPS ON ENDS OF STEPS.

Part: FLOOR SKIN — CRACKED (BS 460) · airframe 26,387 hrs · 22,975 cycles

FOUND FS 460 PRESSURE FLOOR SKIN HAS MULTIPLE INDICATIONS NOTED BETWEEN BL0.0 AND RBL9.0 1.5" IN LENGTH 60 PERCENT FSH. FAILED NDT INSP AREAS MARKED ON ACFT.

Part: ANGLE — DAMAGED (BS 624) · airframe 26,387 hrs · 22,975 cycles

INDICATION NOTED 75 PERCENT FSH APPROX 0.2" LONG EXTENDING FROM THE UPPER FASTENER OF ANGLE LOCATED AT RBL 27.50, FS 624.00 (APPROX), WL 119 (APPROX) FAILS NDT INSPECTION AT THIS TIME. REMOVED AND REPLACED DAMAGED CLIP AT FS 625.30, RBL 27.5 PER REO NO: 601R-53-61-3420 AND SRM 51-42-06 AND 51-42-21. EC/TC DUE. COMPIED WITH EO EC/TC REO 601R-53-61-3420 AND REO 601R-53-61-3420, REV - -,

Part: POST — CRACKED (BS 409) · airframe 26,387 hrs · 22,975 cycles

FOUND FS 409+128 IB SIDE VERTICAL POST RBL 18.0 HAS AN INDICATION NOTED APPROX .2" IN LENGTH 50% FSH AT WL 49.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED VERT POST ASSY AT FS 409+128 RBL 18 IAW SRM 51-42-06 AND 51-42-21. REQUIRES NEW I/B POST. INSTALLED NEW POST ASSY IAW SRM 51-42-21 AND 51-42-06 . ALL FASTENERS WERE USED IAW REO 601R-53-41-889. PAINTED REPAIRED AREA IAW SRM 51-25-01.

Part: POST — CRACKED (BS 409) · airframe 26,387 hrs · 22,975 cycles

FOUND FS 409+128 OB SIDE VERTICAL POST LBL 18 HAS AN INDICATION NOTED APPROX .2" IN LENGTH 50% FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED VERT POST ASSY AT FS 409+128 LBL 18 IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW O/B AS AN ASSEMBLY IAW SRM 51-42-06, 51-42-21, AND REO 601R-53-41-889.

Part: BULKHEAD WEB — CRACKED (BS 559) · airframe 26,387 hrs · 22,975 cycles

5 INDICATIONS NOTED ON FS 559.0 BULKHEAD WEB AND CAP ANGLE AS LISTED: (1) 100 PERCENT FSH, 1 INCH LONG IN WEB AT RBL 18.0 WL 59.10 (2) 75 PERCENT FSH 0.25 INCH LONG IN WEB APPROX 1 INCH OTBD OF RBL 9.0 WL 59.70 (3) 50 PERCENT FSH, 0.5 INCH LONG IN WEB AT RBL 9.0 WL 54.10 (4) 60 PERCENT FSH, 0.2" LONG IN CAP ANGLE BELOW RBL 18.0 POST (5) 80 PERCENT FSH 0.2 INCH LONG IN CAP ANGLE BELOW LBL 18.0 POST. FAILS NDT INSPECTION AT THIS TIME. OPEN

Part: SUPPORT BEAM — CRACKED (BS 718 S11) · airframe 26,387 hrs · 22,975 cycles

ACM/ ECU SUPPORT BEAM CRACKED AT OTBD END AT FS 718 STR 11.

Part: STRUCTURE — CORRODED (BS 333 S26-27L) · airframe 26,387 hrs · 22,975 cycles

MAIN AVIONICS COMPARTMENT FS 333, STR 26L - STR 27 CTR HAS CORROSION COMMON TO FRAME.

Part: FRAME — CORRODED (BS 349 S27) · airframe 26,387 hrs · 22,975 cycles

MAIN AVIONCIS COMPARTMENT FS 349, STR 27 HAS CORROSION ON FRAME.

Part: FRAME — CORRODED (BS 319 S25-26L) · airframe 26,387 hrs · 22,975 cycles

CORROSION ON OUTER FRAME FLANGE AT FS 319 AT STR 25L-26L. CUT FLANGE/REMOVED FLANGE ON FS 319 AT STR 25L-26L IAW REO 601R-53-21-1060 & SRM 53-00-15, REPAIR 2. FABRICATED REPAIR PARTS IAW SRM 53-00-15, REPAIR 2. COMPLIED WITH EC/TC REO 601R-53-21-1060 & REO 601R-53-21-1060.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 26,387 hrs · 22,975 cycles

JOB 8723611 OPERATION 223/621 PRESSURE BULKHEAD FWD SIDE HAS TWO CRACKED ISOLATORS, ONE AT LBL 36 BELOW WL 97.50 AND ONE AT RBL 36 ABOVE WL 97.50.

Part: SUPPORT ANGLE — CRACKED (BS 469) · airframe 26,387 hrs · 22,975 cycles

LT WING TO FUSELAGE ACCESS FAIRING SUPPORT ANGLE CRACKED AT FS 469.53.

Part: SUPPORT ANGLE — CRACKED (BS 476) · airframe 26,387 hrs · 22,975 cycles

LT WING TO FUSELAGE ACCESS FAIRING SUPPORT ANGLE CRACKED AT FS 476.57.

Part: FLOOR SKIN — CRACKED (BS 460) · airframe 26,387 hrs · 22,975 cycles

FOUND FS 460 PRESSURE FLOOR SKIN HAS MULTIPLE INDCATIONS NOTED BETWEEN BL 0.0 AND RBL 9.0 1.5" IN LENGTH 60% FSH, FAILED NDT INSPECTION. AREAS MARKED ON AIRCRAFT. C/W EC/TC REO 601R-53-41-884A BY PERFORMING TEMP REPAIRS TO THE PRESSURE FLOOR WEB AT FS 460.00 IAW REO 601R-53-41-884 REV E. ALL REQUIREMENTS OF THE REO WAS MET.

Part: DOOR — NO TEST (MAIN PAX) · airframe 26,387 hrs · 22,975 cycles

PASSENGER DOOR FAILED FUNCTIONAL TEST DOOR FALLS TO FAST.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 26,387 hrs · 22,975 cycles

LEFT 621-625 OBLIQUE INTERCOSTAL IS CRACKED. REMOVED AND REPLACED LT 621-625 OBLIQUE INTERCOSTAL IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 621-625) · airframe 26,387 hrs · 22,975 cycles

RIGHT 621-625 OBLIQUE INTERCOSTAL IS CRACKED. REMOVED AND REPLACED RT 621-625 OBLIQUE INTERCOSTAL IAW SRM 51-42-21.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,385 hrs · 22,973 cycles

FRAME AT FS 319.00 FROM STR 0 TO STR 4R IS CRACKED. REMOVED DAMAGED FROM IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE FRAME IAW SRM 51-42-06 AND 51-42-21 AND DRAWING 601R32003 REV P.

Part: UNKNOWN — FIRE · airframe 26,385 hrs · 22,973 cycles

WITH AC EXTERNAL SELECTED ON BATT BUS, CAPT AND F/O ON BOARD PERFORMING PRE FLT DUTIES, OBSERVED A RUSHING AIR SOUND, COCKPIT AND FED CABIN QUICKLY FILLED WITH SMOKE. EXTERNAL AC WAS DE-SELECTED AND BATT TURNED OFF. WHILE EXITING A/C, FIRE WAS OBSERVED PENETRATING A/C SKIN AFT OF CAPT SIDE WINDOW.

Part: STEP — CRACKED (AIRSTAIR DOOR) · airframe 26,293 hrs · 22,882 cycles

ASD LOWER STEP CRACKED.

Part: FITTING — CRACKED (BULKHEAD) · airframe 26,083 hrs · 22,694 cycles

RELEVANT INDICATIONS OF CRACKS NOTED AROUND THE LINTEL ATTACHMENT FITTING ON THE AFT PRESSUR BULKHEAD. CRACKS MIGRATE APPROXIMATELY 3/16" FROM THE UPPER, LOWER AND THE INBD EDGE OF THE FITTING.

Part: LIGHT — BROKEN (CABIN) · airframe 24,625 hrs · 21,371 cycles

EMERGENCY LIGHT AT PAX DOOR BROKEN.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 24,165 hrs · 20,975 cycles

STAB TRIM / MACH TRIM / AP ND CAUT MSG ON ARRIVAL INTO COLUMBIA. EMERGENCY DECLARED & EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. AUTOPILOT SYSTEM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,633 hrs · 20,531 cycles

F/A FLASHLIGHT IS INOP.

Part: SKIN — CRACKED (BS 640) · airframe 22,246 hrs · 19,403 cycles

RANRC 390. LT BONDED SKIN COMMON TO FS 640.00 FRAME IS CRACKED. COMPLIED WITH LT BONDED SKIN FS 640 REPAIR, IAW EC/TC REO 601R-53-61-506 (JA10220/RA328) 04/12/07.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 22,246 hrs · 19,403 cycles

LT FS 484 INTERCOSTAL HAS CRACK IN CLIP AT LBL 27 IB. REMOVED CRACKED CLIP FROM LT 484 INTERCOSTAL IAW CRJ 200 SRM 51-42-20. DUPLICATE CLIP FROM SALVAGE REWORK ANGLE P/N S6144-3 IAW CRJ 200 SRM 53-41-43.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 22,246 hrs · 19,403 cycles

RIGHT FS 484 INTERCOSTAL HAS CRACK IN CLIP AT RBL 27 IB. REMOVED CRACKED CLIP ON RT FS 484 INTERCOSTALS' AT RBL 27 AND DUPLICATED PER CRJ SRM 53-41-43 FIG. 1 ITEM 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 22,246 hrs · 19,403 cycles

FLOOR SUPPORT STRUCTURE BENEATH SERVICE DOOR THRESHOLD HAS MINOR SURFACE CORROSION. CORROSION FOUND TO BE LIMITED TO SURFACE ONLY AND NO PITTING WAS FOUND. TREATED MINOR CORROSION PER CRJ SRM 51-21-06 AND APPLIED FINISH A023 PER CRJ SRM 51-21-16.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 22,246 hrs · 19,403 cycles

RIGHT WING I/B LEADING EDGE O/B ATTACH ANGLE CRACKED AT RADIUS. REMOVED AND REPLACED RT WING IB LE OB ATTACH ANGLE WITH NEW SERVICEABLE ANGLE P/N 600-12025-8 IAW CRJ MM 20-21-00.

Part: ANGLE — CRACKED (BULKHEAD) · airframe 22,246 hrs · 19,403 cycles

RIGHT OBLIQUE ANGLE AFT OF 621 BULKHEAD IS CRACKED (AS MARKED). REMOVED RT OBLIQUE ANGLE AFT OF621 BULKHEAD. OK TO TREAT AND PRIME RT OBLIQUE ANGLE AND PAINT. OK TO INSTALL.

Part: UNKNOWN — UNKNOWN (NLG STEERING) · airframe 21,860 hrs · 19,120 cycles

NOSEWHEEL STEERING MESSAGE AFTER TAKEOFF. AIRCRAFT RETURNED TO MSN AFTER T/O. EMERGENCY DECLARED.

Part: APU — SHUTDOWN (APU BAY) · airframe 21,720 hrs · 19,025 cycles

APU FAULT WITH AUTO SHUTDOWN. EN ROUTE TO MGM A/C DIVERTED TO BNA. EMERGENCY DECLARED. FLT 4727 CX ON 1-1-07 SEE DEFECT 334575A-2 FOR CX. AUXILIARY POWER UNIT (APU) INTAKE DOOR DEACTIVATED CLOSED.

Part: STEP — BROKEN (AIRSTAIRS) · airframe 20,350 hrs · 17,914 cycles

ASD LWR STEP BROKEN.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 20,178 hrs · 17,763 cycles

ON WALK AROUND FOUND OVERWING EMERGANCY LIGHT'S FWD POSITION INOP. UPON FUTHER T/S FOUND BATTARY FOR FWD POSITION TO BE DEAD.

Part: DOOR — LACK OF LUBE (MAIN PAX)

FLT 4455 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND EXTREMELY DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. (M)

Part: WIRE — BROKEN (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPAIRED BROKEN WIRE ON THE FORWARD OVERHEAD CURVED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. (M)

Part: FRAME — CRACKED (BULKHEAD)

DURING A C-CHECK IN MCN, THE PILOT`S BULKHEAD FS 280 FRAME AT RBL 11 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD FS 280 FRAME AT RBL 11 IAW ASA EO 600-53-0123. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR MIDDLE THRESHOLD ANGLE WAS FOUND TO BE CORRODED BEYOND LIMITS AND THE HOLES IN THE ANGLE WERE ELONGATED. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR MIDDLE THRESHOLD ANGLE. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 484 LEFT INBOARD AND OUTBOARD CLIP ON THE PRESSURE FLOOR WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 484 LT INBOARD AND OUTBOARD CLIP ON THE PRESSURE FLOOR IAW ASA EO 600-53-0098. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

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

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SILL ASSEMBLY, AROUND THE NUT PLATES, FINGER DOUBLERS, ATTACH ANGLES AND TRANSVERSE BEAMS, BETWEEN FS 424 AND FS 559 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SILL ASSEMBLY BETWEEN FS 424 AND FS 559 IAW ASA EO 600-53-0271. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR SILL AT FS 559 PLUS 16 TO FS 621 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SILL AT FS 559 PLUS 16 TO FS 621 IAW ASA EO 600-53-0278. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR SILL WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO DOOR SILL IAW ASA EO 600-53-0117. (M)

Part: COVER — CRACKED (GALLEY)

DURING A C-CHECK IN MCN, THE FS 280 LT/RT CLIPS INBOARD AND OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 LT/RT CLIPS INBOARD AND OUTBOARD IAW RJ200 SRM 51-42. (M)

Part: COVER — CRACKED (EMERGENCY LIGHT)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT LENS COVER ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LENS COVER ON THE EMERGENCY EXIT LIGHT ABOVE THE SERVICE DOOR. (K)

Part: PSEU — MALFUNCTIONED (MLG)

DURING TAKEOFF FROM CVG-MSG, THE NOSE GEAR FAILED TO RETRACT AND A GEAR DISAGREE WARNING MESSAGE WAS RECEIVED. THE CREW LEVELED THE AIRCRAFT OFF AT 4,000 FEET TO COMPLY WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

FLT 4213 - DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP 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: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED AT BOTH OUTBOARD CORNERS. MAINTENANCE REMOVED AND REPLACED THE TOP STEP ON THE PASSENGER DOOR. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING AN A-CHECK, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4219 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHT FORWARD OF THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP FORWARD OF THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN BTR, THE EMERGENCY FLOOR LIGHTS AT ROWS ONE C/D TO FIVE C/D WERE FOUND TO BE INOPERATIVE. MAINTENANCE SECURED TO LOOSE CONNECTION TO THE EMERGENCY FLOOR LIGHT STRIP FOR ROWS ONE C/D TO FIVE C/D. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR SILL AT FS 349 TO FS 364 ON THE RIGHT SIDE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SILL AT FS 349 TO FS 364 ON THE RIGHT SIDE IAW ASA EO 600-53-0129. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FLOOR SUPPORT ANGLE AT THE SERVICE DOOR ON THE RIGHT SIDE AT APPROXIMATELY FS 319 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FLOOR SUPPORT ANGLE AT THE SERVICE DOOR ON THE RIGHT SIDE AT APPROXIMATELY FS 319. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PILOTS BULKHEAD FLOORBEAM AT FS 280, LBL 9.0 TO RBL 9.0 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD FLOORBEAM AT FS 280, LBL 9.0 TO RBL 9.0 IAW ASA EO 600-53-0130. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE NOSE LANDING GEAR CUTOUT ON THE LEFT AND RIGHT SIDES AT FS 235 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE SKIN AT THE NOSE LANDING GEAR CUTOUT ON THE LEFT AND RIGHT SIDES AT FS 235 IAW ASA EO 600-53-0104. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO AFT WALL FLOOR SUPPORT ANGLES AT FS 621 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0105. (M)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL 0 IAW ASA EO 600-53-0072. (M)

Part: STEP — CRACKED (AIRSTAIR)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ACM — ODOR (RIGHT)

DURING TAKEOFF AND LANDING FROM DFW-RDU, THE RIGHT PACK BECAME UNCONTROLLABLE IN AUTOMATIC OR MANUAL MODES AND SHOWED 17 PSI IN THE RIGHT TENTH STAGE ONLY. A BURNING ODOR ALSO OCCURRED IN THE CABIN. THE AIRCRAFT LANDED SAFELY IN RDU. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR INSPECTION IN XNA, THE RIGHT FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BLOWN RIGHT FORWARD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LINE — FAILED (HYD PRESS SYS)

FLT 4690 - CREW REPORTED THAT HYDRAULIC SYSTEM NR 1 SYNOPTIC PAGE SHOWS ZERO QUANTITY. HYDRAULIC QUANTITY THEN FLUCTUATED BETWEEN 2600-2900 PSI. HYDRAUCLI PUMPS THEN RAN DRY FOR 25 MINUTES WITH NO FLUID. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO ATL. FLIGHT LANDED SAFELY. MAINTENANCE REPLACED NR 1 EDP PRESSURE LINE. MAINTENANCE CHANGED THE ENGINE PUMP AND ELECTRONIC PUMP FOR PREVENTATIVE MEASURES. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EMERG BATTERY — DISCHARGED (CABIN)

DURING DAILY INSPECTION, FOUND EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WINDSHIELD — CRACKED (LT COCKPIT)

DTW/ATL - FLT 4630 - DURING DESCENT AT 12,800 FEET AND 280 KNOTS, THE LEFT WINDSHIELD CRACKED. CREW DECLARED AN EMERGENCY AND LANDED IN ATL WITHOUT FURTHER INCIDENT. ATL MAINTENANCE REMOVED AND REPLACED THE LEFT WINDSHIELD. OPERATIONAL AND PRESSURE CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X)