N850AS

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 33,965 hrs · 30,654 cycles

EXIT SIGN LENS IN GALLEY BY SERVICE DOOR MISSING. REPLACED THE EXIT SIGN LENS IAW AMM 33-51-13.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,656 hrs · 30,351 cycles

NR 5 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R NR 5 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 32,217 hrs · 28,912 cycles

LENS DETACHED ON EMERGENCY LIGHT JUST AFT OF SERVICE DOOR. REPLACED LENS IAW CMM 33-51-21.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 31,656 hrs · 28,344 cycles

EMERGENCY LIGHT NEAR PAX BOARDING DOOR MISSING COVER. REPLACED MISSING EMERGENCY LIGHT COVER IAW AMM 33-51-19. OPS CHECKED GOOD. NO FURHTER DEFECTS NOTED.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 31,181 hrs · 27,865 cycles

WIRING FOR GALLEY EMERGENCY EXIT LIGHT ON TRIM PANEL HAS BROKEN CONNECTOR (QUICK DISCONNECT) ON ACFT SIDE. REPLACED EMERGENCY EXIT LIGHT TRIM PANEL CONNECTOR IAW ESPM 20-17-10. NO DISCREPENCIES FOUND AT THIS TIME.

Part: DOOR — CORRODED (SERVICE DOOR) · airframe 31,181 hrs · 27,865 cycles

MID CAP DOOR ON SERVICE DOOR CORRODED OUT OF LIMITS. R & R MID CAP ON SERVICE DOOR.

Part: ATTACH ANGLE — CORRODED (BS 349) · airframe 31,181 hrs · 27,865 cycles

ATTACH ANGLE BS 349, RT OTBD CORRODED. R & R ATTACH ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 31,181 hrs · 27,865 cycles

FLOORBEAM FS 349 IS CORRODED. REPAIRED FLOORBEAM IAW REO 601R-53-21-2443. NDT PERFORMED. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 31,181 hrs · 27,865 cycles

RT SEAT TRACK AT FS 409 - 409 + 96 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11. CLEANED AREA IAW SRM 51-26-00.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 31,181 hrs · 27,865 cycles

LEFT SEAT TRACK AT FS 349 - 409 CORRODED. INSTALLED SEAT TRACK IAW AMM 53-01-11, SRM 51-21-11, SRM 51-41-02, SRM 51-40-11, SRM 51-23-00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 31,181 hrs · 27,865 cycles

LEFT SEAT TRACK AT BS 559 - 559 + 80 CORRODED. INSTALLED SEAT TRACK IAW AMM 53-01-11, AMM 51-21-11, SRM 51-40-11, SRM 51-41-02, AMM 53-01-11 AND AMM 51-23-00.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 31,181 hrs · 27,865 cycles

LEFT FLOOR SEAT TRACK AT FS 409 - 409 + 96 CORRODED. BLENDED SEAT TRACK. FOUND OUT OF LIMITS IAW SRM 53-21-49 AND SRM 51-21-06. MATERIAL REMAINING 0.40" MINIMUM MATERIAL 0.50". R & R SEAT TRACK IAW AMM 53-01-11. CLEANED AREA IAW SRM 51-26-00.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 31,181 hrs · 27,865 cycles

RIGHT SIDE SEAT TRACK AT FS 409 + 96 - 559 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11. CLEANED AREA IAW SRM 51-26-00.

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 31,181 hrs · 27,865 cycles

RT SEAT TRACK AT FS 349 -409 CORRODED. INSTALLED SEAT TRACK IAW AMM 53-01-11, SRM 51-41-02, SRM 51-40-11, SRM 51-21-11, SRM 51-23-00.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 31,181 hrs · 27,865 cycles

LEFT SEAT TRACK AT FS 409 + 96 - 559 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11, CLEANED AREA IAW SRM 51-26-00.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 31,181 hrs · 27,865 cycles

SERVICE DOOR LOWER SILL HAS CORROSION ON FWD AND AFT SIDES. REMOVED FWD AND AFT CLEAT, REMOVED MID BRACKET, REMOVED KICK ANGLE AND MID CAP, DRILLED NEW KICKANGLE AND MID CAP, INSTALLED MID CAP TO NEW KICK ANGLE, INSTALLED ASSEMBLY IAW SRM 51-42-21, 51-42-06, AND 51-41-02

Part: ANGLE — CORRODED (DOOR THRESHOLD) · airframe 31,181 hrs · 27,865 cycles

PAX DOOR THRESHOLD ANGLE CORRODED. R & R THRESHOLD ANGLE IAW SRM 51-42-06, 51-42-26, 51-40-11, 51-42-21, 51-25-16.

Part: SEAT TRACK — CRACKED (BS 409) · airframe 31,181 hrs · 27,865 cycles

LT SIDE SEAT TRACK FWD OF FS 409.0+128 CRACKED. CLEANED DAMAGE AREA, NO DEFECTS NOTED IAW SRM 53-21-49. DIMENSION AFTER REMOVAL OF DAMAGE: 19.31MM SIDE SEAT TRACK FOUND WITHIN LIMITS IAW SRM 53-21-49, 101 LOCATION Q ALODINED AREA IAW SRM 51-21-11.

Part: BRACKET — CRACKED (BS 280) · airframe 31,181 hrs · 27,865 cycles

BS 280 BRACKET CRACKED LT SIDE. R & R WITH SERVICEABLE PART IAW SRM 51-42-20, SRM 51-42-06, SRM 51-22-00 AND SRM 51-42-20, AMM 51-25-00, AMM 51-25-56.

Part: BRACKET — CRACKED (BS 280) · airframe 31,181 hrs · 27,865 cycles

FS 280 L BRACKET CRACKED RT SIDE. R & R WITH SERVICEABLE PART IAW SRM 51-42-20, SRM 51-42-06, SRM 51-22-00 AND SRM 51-42-20, AMM 51-25-00, AMM 51-25-56.

Part: SILL — CORRODED (FUSELAGE) · airframe 31,181 hrs · 27,865 cycles

RT SILL AFT OF SERVICE DOOR HAS CORROSION. R & R RT SILL AFT OF SERVICE DOOR IAW SRM 51-42-06 AND SRM 51-42-10. FOUND OUT OF LIMITS WITH A .010 MAT LOSS IAW SRM TR 53-27-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 31,181 hrs · 27,865 cycles

DURING EMERGENCY LIGHTS OPS TEST, FOUND OVERHEAD EMERGENCY FLOODLIGHT INOPERATIVE AT BS 544. R & R CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 30,752 hrs · 27,426 cycles

FOUR ISOLATORS BROKEN ON AFT PRESSURE BULKHEAD. R & R DAMAGED ISOLATORS ON THE AFT PRESSURE BULKHEAD IAW SRM 51-42-13.

Part: SOCKET — FAILED (GALLEY LIGHT) · airframe 29,514 hrs · 26,129 cycles

STRONG ODOR OF ELECTRICAL SMOKE IN COCKPIT. F/A, F/O AND CAPTAIN NOTICED. F/A STATES SOME HOT SPOTS ON WALL NEAR OR BEHIND COFFEEMAKER. STRONGEST ODOR IN COCKPIT NEAR F/O'S CEILING CIRCUIT BREAKER PANEL. ENROUTE, ACFT DIVERTED, EMERGENCY DECLARED. INSPECTED ELECTRICAL SYS, RAN ENGINES, AND PACKS. FOUND GALLEY WORK LIGHT BULB SOCKET BAD.

Part: O-RING — DAMAGED (HYD SYSTEM) · airframe 27,815 hrs · 24,278 cycles

DURING FLIGHT RECIEVED HYD NR3 LO PRES CAUTION MESSAGE(ENROUTE, ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED AS A PRECAUTION) FOUND O-RING AT UNION ON NR 3A ACCUSTIC FILTER DAMAGED. REPLACED O-RING IAW AMM 29-12-17. OPS AND LEAK CHECKS GOOD. ACFT OK FOR SERVICE AT THIS TIME. (CLOSED)

Part: DOOR — CRACKED (MAIN PAX) · airframe 27,675 hrs · 24,121 cycles

SUSPECTED CRACK, UPPER AFT CORNER OF PAX DOOR. CUT OUT DOOR EDGE. REMOVED ALL BURRS AND SHARP EDGES AT UPPER AFT CORNER OF PAX DOOR IAW REO 601R-52-11-279. COMPLIED WITH EDDY CURRENT INSP IAW NDTM 51-20-06 OF REWORKED AREA. NO DEFECTS NOTED. TOUCHED-UP THE EDGE OF THE CUTOUT IAW SRM 51-21-16. FABRICATED REPAIR ANGLE, & FILLER. AND INSTALLED IAW SRM 51-21-16.

Part: DOOR — CRACKED (MAIN PAX) · airframe 27,675 hrs · 24,121 cycles

SUSPECTED CRACK, UPPER FWD CORNER OF PAX DOOR. CUT OUT DOOR EDGE. REMOVE ALL BURRS AND SHARP EDGES AT UPPER FWD CORNER OF PAX DOOR IAW REO 601R-52-11-279. COMPLIED WITH EDDY CURRENT INSP IAW NDTM 51-20-06 OF REWORKED AREA. NO DEFECTS NOTED. FABRICATED REPAIR ANGLE, & FILLER IAW REO 601R-52-11-279. INSTALLED IAW SRM 51-23-00.

Part: STRUCTURE — CRACKED (LT WING) · airframe 27,455 hrs · 23,880 cycles

AFTER INITIAL INSP OF WING, IAW AD2002-03-14REP, AND SB A601R-57-031, FOUND SUSPECTED CRACK ON LT WING AT WS148.019. COMPLIED WITH HFEC INSP IAW NDTM 51-20-06 FOUND A .300" CRACK AT LT WING BOTTOM AT WS 149.58 JUST FWD OF REAR SPAR. PERFORMED LPI TO DETERMINE END OF CRACK IAW NDTM 511-20-08. STOP DRILLED END CRACK TO .250 DIA IAW REO 601R-57-21-138. PERFORMED EDDY CURRENT INSP OF STOP DRILL HOLE IAW NDTM 51-20-06. REAMED HOLE UP .3125 IAW REO 601R-57-21-138. FINISHED REWORKED AREA AND FILLED WITH AERODYNAMIC SEALANT REO 601R-57-21-138.

Part: SKIN — CRACKED (LT WING) · airframe 27,455 hrs · 23,880 cycles

CRACK ON LT LOWER SKIN WING PLANK AT WS 148.019.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 27,251 hrs · 23,663 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 INOPERATIVE. REMOVED AND REPLACED THE LIGHT BULB AT ROW 5 IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 26,808 hrs · 23,152 cycles

CABIN PRESSURE FLOOR SUPPORT ANGLE IS CRACKED AT LBL 27.0 AT FS 484.00. DB161718. AWAITING EC/TC. RECEIVED ECTC, COMPLIED WITH ECTC REO 601R-53-41-1363 AND REO601R-53-41-1363.

Part: FRAME — CORRODED (BS 364) · airframe 26,808 hrs · 23,152 cycles

FOUND CORROSION AT FS 364.00 AND BETWEEN STR 26R AND 27R. INSTALLED ORIGINAL TEFLON DOOR GUIDES ON FWD SIDE OF AVIONICS BAY DOOR OPENING PER AMM 20-21-00-910-801.

Part: FRAME — CORRODED (BS 364) · airframe 26,808 hrs · 23,152 cycles

FOUND CORROSION AT FS 364.00 AND BETWEEN STRINGER 26L AND 27L. INSTALLED ORIGINAL TEFLON DOOR GUIDES ON FWD SIDE OF AVIONICS BAY DOOR OPENING PER AMM 20-21-00-910-801.

Part: FRAME — CORRODED (BS 349 S27R/L) · airframe 26,808 hrs · 23,152 cycles

CORROSION ON LEFT AND RIGHT RADIUS ON STR 27 FWD OF FRAME 349. INSTALLED NEW STR 27 SECTION AND DOUBLERS IAW SRM 53-00-03, MINOR REPAIR. REPAIRED IAW SRM 53-00-03.

Part: SKIN — DAMAGED · airframe 26,808 hrs · 23,152 cycles

DURING REMOVAL OF STRINGER AT STA346, STR 27 FOUND EXISTING HOLE TO BE .250 IN DIAMETER. SUBMIT TO THD AND REPAIR. RECEIVED REO 601R-53-21-12-48 TO FREEPLUG SKIN AT STA 346, STR 27. NEED TO COMLY WITH STEP 1 OF REO 601R-53-21-1248. REAMED EXISTING .250 ROLE IN SKIN AND COUNTER SUNK TO .035 AT STA 346, STR 27 IAW REO 601R-53-21-1248, STEP 1. (REAMED HOLE TO .3795) NEED TO COMPLY WITH REO 601R-53-21-1248, STEP 2, NDT FOR DEFECTS IN REAMED HOLE. COMPLIED WITH STEP 2 OF REO 601R- 53-21-1248. IAW NDTM PART1, 51-20-06. NO INDICTATIONS NOTED AT THIS TIME. COMPLY WITH STEP 3-9 OF REO 601R-53-21-1248. COMPLIED WITH STEPS 3-9 OF REO 601R-53-21-1248. RECEIVED AND COMPLIED WITH EC/TC REO 601R-53-21-1248. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.

Part: RIB — CORRODED (RT WING) · airframe 26,808 hrs · 23,152 cycles

RIGHT WING OUTBOARD LEADING EDGE INBOARD RIB AT WS 252.87 HAS CORROSION. AFTER BLENDING CORROSION ON RIB AT WS 252.87 FOUND TO BE OUT OF LIMITS PER SRM 57-41-12. RIB TRIMED TO FIT & LOCATED FASTNER HOLES IN NEW LEADING EDGE IAW SRM 51-40-11. INSTALLED NUT PLATES IN INBD FLANGE LEADING EDGES SRM 51-42-06. TOUCHED UP BARE METAL IAW SRM 51-21-00 & SRM 51-25-06.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 26,808 hrs · 23,152 cycles

CARGO TRACK, RBL 9.0 AT FS 559+112 IS CORRODED. REPAIRED IAW REO601R-53-51-141.

Part: FRAME — CORRODED (BS 319.70) · airframe 26,808 hrs · 23,152 cycles

FRAME FS 319.70 BETWEEN S25L AND S25R FWD & AFT SIDE HAS CORROSION. REMOVED AND INSTALLED NEW FRAME IAW SRM 51-42-06.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 26,808 hrs · 23,152 cycles

LT INBD FLAP LOWER SURFACE OTBD END DENTED. EVALUATED DENT ON LT OTBD FLAP LOWER SKIN BETWEEN WS 144 AND 147,3" FWD OF T/E. DENT MEASURES 2.8"X2.0X.0725", EXCEEDING ALLOWABLE DAMAGE LIMIT OF SRM 57-52-00, FIG 101, SH 2. PERFORM REPAIR IAW SRM 57-52-00. REPAIRED LT INBD FLAP LOWER SURFACE OUTBD AFT END DAMAGED SKIN IAW SRM 57-52-00 FLUSH REPAIR NR 2 AND FIG 202. GF88021 THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY. (CLOSED)

Part: FLOORBEAM — CORRODED (BS 585.605) · airframe 26,808 hrs · 23,152 cycles

CARGO FLOORBEAM FS 585.605 LBL 9.0 IS CORRODED. COMPLIED WITH STEPS 4-10 OF REO 601R-53-61-3988. COMPLIED WITH EC/TC REO601R-53-61-3988. THIS IS A MINOR REPAIR.

Part: FRAME — CORRODED (BS 310 S25L/R) · airframe 26,808 hrs · 23,152 cycles

FRAME FS 310.00 BETWEEN S25L AND S25R FWD & AFT SIDE HAS CORROSION. REMOVED IAW SRM 51-42-06 AND INSTALLED NEW FRAME SECTION IAW SRM 51-40-11, 51-42-06, 51-42-21, & AMM 51-23-00-910-801.

Part: SILL — CORRODED (BS 513) · airframe 26,808 hrs · 23,152 cycles

LT PRESSURE FLOOR CORRODED AT FS 513, LBL 43 (3 LOCATIONS). REMOVED CORROSION IAW SRM 53-41-45. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT UT-3. MIN. MATERIAL REMAINING IS .078" ORIGINAL MATERIAL IS .080". 002" REMOVED. COMPLIED WITH STEPS 2.2C OF REO 601R-53-41-666. NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH STEPS 2.2 A, B, D, E AND F OF REO 601R-53-41-666.

Part: WEB — CORRODED (BS 473.15) · airframe 26,808 hrs · 23,152 cycles

LT PRESSURE FLOOR CORRODED AT FS 473.15 LBL 43 (2 LOCATIONS). REMOVED CORROSION IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 26,808 hrs · 23,152 cycles

CARGO RT FLOOR SUPPORT HAS CORROSION AROUND NUTPLATES FROM FS 605-TO FS 621. REO 601R-53-61-3990 AND STEP 1 HAS BEEN COMPLIED WITH. COMPLIED WITH STEP (2) OF REO 601R-53-61-3990 PER NDTM 51-26-06. NO INDICATIONS NOTED. COMPLIED WITH 3 THRU 5 OF REO 601R-53-61-3990. COMPLIED WITH STEP 6 OF REO 601R-53-61-3990. THIS IS CLASIFIED AS A MAJOR REPAIR.

Part: WEB — CORRODED (BS 461.5) · airframe 26,808 hrs · 23,152 cycles

RT PRESSURE FLOOR CORRODED AT 461.50. BLENDED/REMOVED CORROSION IAW SRM 53-41-45. OUT OF LIMITS. REPAIRED IAW GREO 601R-53-41-666.

Part: WEB — CORRODED (BS 461.5) · airframe 26,808 hrs · 23,152 cycles

LT PRESSURE FLOOR CORRODED AT FS 461.50 LBL 43. REMOVED CORROSION IAW SRM 53-41-45.

Part: SILL — CORRODED (BS 499) · airframe 26,808 hrs · 23,152 cycles

LT PRESSURE FLOOR CORRODED AT FS 499, LBL 43 (2 LOCATIONS). REMOVED CORROSION IAW SRM. COMPLIED WITH STEPS 1.2C AND 2.2C OF GREO 601R-53-41-666. NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH STEPS 1.2 AND 2.2 A, B, D, E AND F OF REO 601R-53-41-666.

Part: FRAME — CORRODED (BS 349) · airframe 26,808 hrs · 23,152 cycles

FOUND CORROSION AT FS 349, BETWEEN STR 25L AND 25R. DRILLED OF NEW FRAME SECTION AND PREP FOR INSTALLED IAW SRM 51-42-06.

Part: WEB — CORRODED (BS 424) · airframe 26,808 hrs · 23,152 cycles

LT PRESSURE FLOOR CORRODED AT FS 424.00. REMOVED CORROSION IAW SRM 53-41-45.

Part: WEB — CORRODED (BS 522.4) · airframe 26,808 hrs · 23,152 cycles

LT PRESSURE FLOOR CORRODED AT FS 522.40, LBL 43. REMOVED CORROSION IAW SRM. PERFORMED UT THICKNESS INSP OF BLEND AREA IAW NDT INSP PROCEDURE UT-3 MIN. MATERIAL REMAINING ON FLOOR ANGLE AT FS522.40 IS .079" ORIGINAL MATERIAL IS .080". 001" REMOVED. NO DAMAGE ALLOWED WITHIN 2D OF A FASTENER IAW SRM 53-41-45 THD ASSISTANCE REQUIRED. REPAIRED IAW GREO 601R-53-41-666.

Part: WEB — CORRODED (BS 439) · airframe 26,808 hrs · 23,152 cycles

LT PRESSURE FLOOR CORRODED AT FS 439, LBL 43 (4 LOCATIONS). REMOVED CORROSION IAW SRM 53-41-45.

Part: WEB — CORRODED (BS 540) · airframe 26,808 hrs · 23,152 cycles

LEFT PRESSURE FLOOR CORRODED AT FS 540.25, LBL 43. REMOVED CORROSION IAW SRM. PERFORMED UT THICKNESS INSPECTION OF AREA IAW MAC NDT INSPECTION PROCEDURE YT-3 MIN. MATERIAL REMAINING ".079" ORIGINAL MATERIAL IS .080". 001" REMOVED. REPAIRED IAW GREO 601R-53-41-666.

Part: WEB — CORRODED (BS 484) · airframe 26,808 hrs · 23,152 cycles

LT PRESSURE FLOOR CORRODED AT FS 484 LBL 43 (2 LOCATIONS). REMOVED CORROSION IAW SRM.

Part: WEB — CORRODED (BS 449.85) · airframe 26,808 hrs · 23,152 cycles

LT PRESSURE FLOOR CORRODED AT FS 449.85 LBL 43 (3 LOCATIONS). REMOVED CORROSION IAW SRM.

Part: FRAME — CORRODED (BS 349) · airframe 26,808 hrs · 23,152 cycles

CORROSION ON LT AND RT RADIUS ON STR 27, 3-3.5 INCHES FWD OF FRAME 349. REMOVED CORROSION IAW SRM 51-21-06. BLENDED AREAS EXCEED LIMITS IAW SRM 53-00-00, FIG 101, SHEET 3 AND SRM 51-31-59, FIG 3, CUT AND REMOVED STRINGER SECTION IAW SRM 53-00-03, FIG 202. DRILLED NEW STRINGER IAW SRM 53-00-03. PERFORMED EDDY CURRENT INSP IAW SRM 53-00-03 AND NDTM PT 1, 51-20-06. NO DAMAGE NOTED AT THIS TIME.

Part: ISOLATOR — BROKEN (PRESS BULKHEAD) · airframe 26,808 hrs · 23,152 cycles

CARGO AFT PRESSURE BULKHEAD HAS 6 BROKEN ISOLATORS. REPLACED BROKEN ISOLATORS IAW SRM 51-42-13. MINOR REPAIR.

Part: POST — CRACKED (BS 409) · airframe 26,808 hrs · 23,152 cycles

FS409+128, BULKHEAD, LBL18.00 VERTICAL POST CRACKED THRU LOWER OTBD ATTACH FASTENER PROPAGATING INTO RADIUS. REPAIRED IAW REO 601R-53-41-056.

Part: FRAME — CORRODED (BS 349) · airframe 26,808 hrs · 23,152 cycles

FOUND CORROSION AT FS349 BETWEEN STR 25L AND 25R. BLENDED IAW SRM 51-12-00.

Part: ISOLATOR — BROKEN (PRESS BULKHEAD) · airframe 26,808 hrs · 23,152 cycles

CARGO AFT PRESSURE BULKHEAD HAS 6 BROKEN ISOLATORS MARKED. R & R BROKEN ISOLATORS IAW SRM 51-42-13. THIS IS A MINOR REPAIR. (CLOSED)

Part: FRAME — CORRODED (BS 333) · airframe 26,808 hrs · 23,152 cycles

FOUND CORROSION AT FS333 BETWEEN STR 25L AND 25R. REMOVED CORROSION IAW SRM 51-21-06 AND 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 589-605) · airframe 26,808 hrs · 23,152 cycles

CARGO FLOORBEAM, LBL 9.0 IS CORRODED THROUGH BETWEEN FS 589.00-605.00. REPAIRED IAW REO 601R-53-61-3988.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 26,808 hrs · 23,152 cycles

INTERCOSTALS BETWEEN FS349 AND FS364 AT APPROX RBL3 AND LBL3 HAVE CORROSSION. BLENDED CORROSION AS REQUIRED REF SRM 51-21-06 AND SRM 51-12-00. THIS IS A MAJOR REPAIR.

Part: STRUCTURE — CORRODED (BS 364 S25-26R) · airframe 26,808 hrs · 23,152 cycles

FOUND CORROSION AT FS 364.00 AND BETWEEN S26R AND 25R. BLENDED CORROSION AT FS 364 BETWEEN STR 26R & 27R REF SRM 51-21-06. THIS IS A MAJOR REPAIR.

Part: INTERCOSTAL — CRACKED (BULKHEAD) · airframe 26,808 hrs · 23,152 cycles

SUSPECT CRACK ON INTERCOSTAL MEMBERS AT FS 625 LT SIDE OF AFT PRESSURE BULKHEAD BETWEEN WL 90 & 100 ON INTERCOSTAL BRACKETS 601-35012-19 & -23. CRACKS ARE WITHIN ALLOWABLE LIMITS IAW SB 601R-53-048, REV A.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 26,808 hrs · 23,152 cycles

CABIN PRESSURE FLOOR SUPPORT ANGLE IS CRACKED AT LBL 27.0 AT FS 484.00. NEW FLOOR SUPPORT ANGLE FABRICATED & INSTALLED IAW REO 601R-53-21-248.

Part: FRAME — CORRODED (BS 364 S25-26L) · airframe 26,808 hrs · 23,152 cycles

FOUND CORROSION AT FS 364.00 AND BETWEEN S26L AND 25L. BLENDED CORROSION IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-15, FIG 6, ITEM 5.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 26,808 hrs · 23,152 cycles

CARGO SEAT RAIL BEAM RBL 9.0 AT FS 559+112 IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-53-43-01 AND 51-21-06.

Part: HYDRAULIC SYSTEM — LOW (NR 3) · airframe 26,318 hrs · 22,589 cycles

HYD 3 LOW PRESS CAUTION MESSAGE IN FLIGHT. RAN CHECKLIST AND HAD TO MANUALLY EXTEND GEAR. DECLARED EMERGENCY. (EMERGENCY DECLARED -- EMERGENCY EQUIPMENT REQUESTED TO BE STANDING BY) (CLOSED)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,261 hrs · 22,523 cycles

EXTERIOR EMERGENCY LIGHT(MIDDLE) ON LT & RT SIDE INOP. RELAMPED LT & RT MIDDLE EXTERIOR EMERGENCY LIGHTS IAW AMM 33-51-21. OPS CK GOOD. (CLOSED)

Part: SIGN — INOPERATIVE (RT OVERWING) · airframe 24,684 hrs · 20,741 cycles

FOUND RT OVER WING FLOOR EXIT SIGN INOP.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 24,563 hrs · 20,608 cycles

FLAPS FAILED IN FLIGHT AT 0. FLAPS WERE RETRACTED AFTER TAKEOFF -THATS WHEN THEY FAILED AT 0. (EMERGENCY DECLARED) PERFORMED GROUND MX TEST IAW FIM 27-50-00 PARAGRAPH 21. ALL LRU'S PASSED. OPERATED FLAPS UP AND DOWN NO FAULT MESSAGES NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 24,440 hrs · 20,470 cycles

RT OVERWING EMERGENCY EXIT LWR LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,896 hrs · 18,966 cycles

NUMEROUS EMERGENCY LIGHTS OUT.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 22,817 hrs · 18,896 cycles

CABIN SEAT RAIL P/N 601R-38312-298 HAS CORROSION AND DAMAGE. FS 409R - 409+112R.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,817 hrs · 18,896 cycles

FWD PRESSURE BULKHEAD FS 202.75 HAS A CRACK AT PARKING BRAKE CABLE. REPAIRED CRACK NEAR PARKING BRAKE CABLE AT FWD PRESSURE BULKHEAD IAW REO 601R-53-11-563. COMPLIED WITH ECTC EO 600-53-217 C/W.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,817 hrs · 18,896 cycles

LT AND RT FS 625 OBLIQUE ANGLES CRACKED. REMOVED IAW SRM 51-42-21. HOLES WERE DAMAGED, DRILLED PER SRM 51-40-11. INSTALLED IAW REO 601R-53-61-3021 AND SRM 51-42-21. ECTC REQUIRED. COMPLIED WITH ASA ECTC REO 601R-53-61-3021.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,817 hrs · 18,896 cycles

RT FLOOR SILLS AND FRAME FLANGES/ANGLES FS 424 TO FS 484 HAVE CORROSION IN NUMEROUS PLACES. AREAS PREVIOUSLY REPAIRED IAW REO 601R-53-41-302. REMOVED CORROSION IAW SRM 51-12-00. MATERIAL REMOVED IS BEYOND REPAIRABLE LIMITS OF SRM. REMOVED CORROSION IAW REO 601R-53-41-302. STEPS 2-5. C/W REO 601R-53-41-302A STEP 2. LPI BLENDED AREAS PER NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. C/W REO 601R-53-41-302, STEP 3. C/W REO 601R-53-41-302 CORROSION REMOVAL STEPS 4-5. ALL WORK PERFORMED IAW ECTC 601R-53-41-302.

Part: POST — DAMAGED (FUSELAGE) · airframe 22,817 hrs · 18,896 cycles

FS 409.0 + .28 VERTICAL POST RBL 18.0 HAS 2 INDICATIONS NOTED. BOTH ARE APPROX .3" IN LENGTH 70% FSH INBD AND OTBD SIDES WL 69, BOTH AREAS FAILED NDT INSPECTION. FABRICATED REPLACEMENT VERTICAL POSTS IAW SRM 51-24-21 PER SAMPLE AND REF DWG 601R32208. REMOVED, LOCATED, AND DRILLED NEW VERTICAL POST AND INSTALLED NEW VERTICAL POST IAW SRM 51-40-11 AND SRM 51-42-06 AND REO 601R-53-41-864. COMPLIED WITH ASA ECTC REO 601R-53-41-864.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 22,817 hrs · 18,896 cycles

CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX .5" IN LENGTH.

Part: FRAME — CORRODED (FUSELAGE) · airframe 22,817 hrs · 18,896 cycles

LT FLOOR SILLS AND FRAME FLANGES AND ANGLES FS 424 TO FS 484 HAVE CORROSION IN NUMEROUS PLACES. AREAS PREVIOUSLY REPAIRED IAW REO 601R-53-41-302. REMOVED CORROSION IAW SRM 51-12-00. MATERIAL REMOVED IS BEYOND REPAIRABLE LIMITS IAW SRM REPAIR & IAW REO. REMOVED CORROSION IAW REO 601R-53-41-302. STEPS 2-5. C/W REO 601R-53-41-302A STEP 2 LPI BLENDED AREAS IAW NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. C/W REO 601R-53-41-302, STEP 3. C/W REO 601R-53-41-302 CORROSION REMOVAL, STEPS 4-5. ALL WORK PERFORMED IAW ECTC 601R-53-41-302.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,817 hrs · 18,896 cycles

2 SECTIONS OF SEAT TRACK BETWEEN FS 364.0 AND 399.5 AT LBL 9 AND RBL 9 ARE CORRODED BEYOND LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 22,817 hrs · 18,896 cycles

LT SIDE SEAT RAIL HAS CORROSION FROM FS 409 BACK. CLEANED LT SIDE PAX SEAT RAILS FROM FS 409 AND AFT IAW AMM 53-01-11-000-802, SUBTASK 53-01-11-020-002 PARA 3A (3) AND UPON FURTHER INVESTIGATION, FOUND NO SIGNS OF CORROSION ON RAILS.

Part: BULKHEAD — CRACKED (BS 559) · airframe 22,817 hrs · 18,896 cycles

LT AND RT FS 559 BULKHEAD WEB AND CAP ANGLE HAVE INDICATIONS AT CAP ANGLES LBL RBL 18 APPROX .3" IN LENGTH 90% FSH AND RT WEB AT WL 58.10 APPROX .2" IN LENGTH 60% FSH, WL 54.10 APPROX .5" IN LENGTH 80% FSH AND WL 59.10 APPROX 1.0" IN LENGTH 100% FSH. ALL THESE AREAS FAILED NDT INSPECTION. REPAIRED LT/RT FS 559 BULKHEAD WEB AND CAP ANGLE THAT FAILED NDT AT LT/RT CAP ANGLE LBL 18 AND RT WEB AT WL 58.10 IAW REO 601R-53-41-260, REV C. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260, REV C.

Part: FRAME — CRACKED (BS 718) · airframe 22,817 hrs · 18,896 cycles

F.S. 718 FRAMES CRACKED AND PREVIOUS REPAIRS. REPAIRED IAW SB 601R-53-055 REV B PART A, B, AND C. INSPECTED AND REPAIRED IAW EC/TC SB 601R-53-055 AND SB 601R-53-05501.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,809 hrs · 18,889 cycles

EMERGENCY LIGHT INOP (LEFT ON). FLT 5105 DEL 87 MINS.

Part: HANDLE — MALFUNCTIONED (PAX DOOR) · airframe 22,803 hrs · 18,883 cycles

PAX DOOR HANDLE WILL NOT STOW. FLIGHT 5030 DEL 19 MINS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,759 hrs · 17,933 cycles

EXTERIOR AFT EMERGENCY LIGHT INOP. REPLACED AFT EMERGENCY LIGHT ON FUSELAGE IAW SRM 33-51-21. OPS CK GOOD. (B)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,762 hrs · 17,087 cycles

LEFT SIDE EXTERIOR 2 EMERGENCY LIGHT INOP.

Part: UNKNOWN — UNKNOWN · airframe 20,291 hrs · 16,658 cycles

THUMPING IN CONTROL WHEEL AND UNDER F/AS FLOOR AFTER GEAR RETRACTION. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 4215 DEL 173 MINS.

Part: STRUCTURE — STUCK (MEDICAL KIT) · airframe 19,232 hrs · 15,827 cycles

FLIGHT EMERGENCY MEDICAL KIT STORAGE COMPARTMENT WILL NOT OPEN. FLT 4392 DEL 34 MINS.

Part: BRACKET — CORRODED (BS 312-340) · airframe 19,175 hrs · 15,781 cycles

CORROSION ON FLOOR SUPPORT BRACKETS AT PAX DOOR ENTRANCE FS 315 FS 340. UNDER FLOOR PANEL 231CLF.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

FRAME CORRODED AT FS 605 BETWEEN STR 26L AND 27.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

FRAME CORRODED AT FS 364.00 BETWEEN STR 26L TO 26R.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

CORROSION ON FRAME AT FS 319 BETWEEN STR 26L TO 25R.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

RIGHT SILL AS MANY SPOTS OF CORROSION BETWEEN FS 409.00 +128 TO FS 559.00 BL 36 TO BL 47.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED AT FS 349.00. SERVICE DOOR LOWER SILL ANGLE REMOVED AND REPLACED AS PER SRM 51-42-21, SEALANT APPLIED AS PER SRM 51-23-00, PAINTED AS PER SRM 51-21-11. SUPPLEMENTAL - SDR CLOSED 06/05/07.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

LEFT SILL AS MANY SPOTS OF CORROSION BETWEEN FS 409.00 AND + 128 TO FS 559.00 BL 26 TO BL 47.

Part: FUEL TANK — CONTAMINATED (LT & RT TANK) · airframe 19,175 hrs · 15,781 cycles

LEFT AND RIGHT FUEL TANK ACCESS PANEL 540AB AND 640AB THERE IS FOD BEHIND THE BAFFLE NEXT TO EJECTOR PUMP.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

CORROSION ON FRAME AT FS 349 BETWEEN STR 26L TO 26R.

Part: HANDLE — CORRODED (ESCAPE HATCH) · airframe 19,175 hrs · 15,781 cycles

CREW ESCAPE HATCH HANDLE CORRODED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

CORROSION ON FRAME AT FS 310 BETWEEN STR 26L TO 26R.

Part: FRAME — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

CORROSION ON FRAME AT FS 319 BETWEEN STR 25L TO 25R.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

CORROSION ON PAX DOORS LOWER SILL BETWEEN FS 310 TO FS 349.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,175 hrs · 15,781 cycles

CORROSION ON LOWER SILL OF THE SERVICE DOOR.

Part: SKIN — CORRODED (BS 559) · airframe 19,174 hrs · 15,781 cycles

EXTERIOR FUSELAGE SKIN AT FS 559.00 + 112, RBL 2.00 IS CORRODED. [SUP 05-31-07] REPAIRED IAW SRM 53-00-31 FIG 103 AND SRM 51-21-06.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 19,174 hrs · 15,781 cycles

CRACK SUSPECT AT FS 484 RBL 27 AND RBL 36 UNDER FLOOR INTERCOSTAL. [SUP 05-31-07] REPAIRED IAW REO 601R-53-41-059.

Part: LIGHT — BROKEN (CABIN) · airframe 19,131 hrs · 15,743 cycles

EMERGENCY FLOOR TRACK LIGHTING BROKEN.

Part: STEP — CRACKED (AIRSTAIR) · airframe 17,860 hrs · 14,768 cycles

A/S/D LOWER STEP CRACKED.

Part: FRAME — CRACKED (BS 640) · airframe 17,860 hrs · 14,768 cycles

RIGHT SIDE FS 640 FRAME DOUBLER SUSPECT CRACKED. FLT 4256 CX. PERFORMED MODIFICATION OF FRAME 640 LEFT AND RIGHT SIDE BETWEEN STR 9 AND STR 12 REF S.B.601R-53-061 APPENDIX B (CLOSED 11/01/06).

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 17,140 hrs · 14,196 cycles

WHEN FLAPS SELECTED TO 8, RECIEVED FLAPS FAIL MSG AND FLAPS STAYED AT ZERO...ENROUTE TO ROA A/C DIVERTED TO GSO DUE TO MTC. A/C DELCARED AN EMERGENCY...FLT 4515 CX

Part: PLACARD — FADED (EXTERIOR) · airframe 16,952 hrs · 14,031 cycles

LEFT OVERWING EMERGENCY EXIT EXTERIOR PLACARD FADED.

Part: DOOR — STIFF (MAIN PAX) · airframe 16,521 hrs · 13,696 cycles

FOUND PAX DOOR HARD TO CLOSE.

Part: LIGHT — BURNED OUT (CABIN)

DURING A HANGAR INSPECTION, THE FORWARD EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CARBON SEAL — LEAKING (LT ENGINE)

DURING CRUISE, AT APPROXIMATELY 27,000 FT, THE CREW RECEIVED A LT ENGINE OIL PRESSURE WARNING MESSAGE. THE OIL PRESSURE AURAL MESSAGES. THE QRH WAS COMPLIED WITH AND THE LT ENGINE WAS KEPT AT IDLE. THE CREW PERFORMED A SAFE SINGLE ENGINE LANDING, WITH EMERGENCY VEHICLES DISPATCHED AS A PRECAUTION. MAINTENANCE REMOVED AND REPLACED THE STARTER CARBON SEAL ASSY IAW AMM. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (FUSELAGE)

DURING A GROUND INSPECTION, THE RT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT EXTERNAL EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: STEP — BROKEN (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BPSU — INOPERATIVE (TE FLAPS)

DURING CLIMB-OUT FROM ATL-ALB, THE CREW ATTEMPTED TO RETURN FLAPS FROM EIGHT DEGREES TO ZERO DEGREES, WHEN AN AMBER FLAPS FAIL CAUTION MESSAGE, WITH THE FLAPS REMAINING AT 8 DEGREES WAS RECEIVED. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT BPSU. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ANCHOR FITTING — CRACKED (DOOR)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT ANCHOR FITTING WAS TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR AFT ANCHOR FITTING. (K)

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION, 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. (K)

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

DURING A C-CHECK, THE PRESSURE FLOOR BETWEEN FS 449.85-473.15, BL45 TO THE FLOOR UNDER THE LT AND RT OVERWING EXITS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR BETWEEN FS 449.85-473.15, BL45 TO THE FLOOR UNDER THE LT AND RT OVERWING EXITS IAW EO. (K)

Part: PRESSURE PANEL — CORRODED (FUSELAGE)

DURING A C-CHECK, THE PRESSURE FLOOR AT FS 424-449.85 LT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR AT FS 424-449.85 LT IAW EO. (K)

Part: FRAME — CORRODED (FUSELAGE)

DURING A C-CHECK, THE MAINFRAME AT FS 473.15 AT THE FLOOR LEVEL UNDER THE LT AND RT OVERWING EXITS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE MAINFRAME AT FS 473.15 AT THE FLOOR LEVEL UNDER THE LT AND RT OVERWING EXITS IAW EO. (K)

Part: BULKHEAD — CORRODED (FUSELAGE)

DURING C-CHECK, THE PILOTS BULKHEAD WEB FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD WEB FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)

Part: PLACARD — WORN (ESCAPE HATCH)

DURING A C-CHECK, THE EXTERIOR EXIT PLACARD ON THE PILOTS ESCAPE HATCH WAS FOUND WORN. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EXIT PLACARD ON THE PILOTS ESCAPE HATCH. (K)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING A C-CHECK, THE FORWARD AND AFT FLOOR SUPPORT ANGLES FS 280 BETWEEN LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD AND AFT FLOOR SUPPORT ANGLES FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FS 484 INTERCOSTAL AT LBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 484 INTERCOSTAL AT LBL 36 IAW EO. (K)

Part: RIB — CRACKED (RT WING)

DURING A C-CHECK, THE RT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT BATT RIB ASSEMBLY AT WS 53.60 IAW EO. (K)

Part: ANGLE — CRACKED (FUSELAGE)

DURING C-CHECK, THE ANGLE IB OF LBL 9 AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE ANGLE IB OF LBL 9 AT FS 280 IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CLIP AT FS 484, LBL 27 FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 484, LBL 27 FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 484, LBL 27 IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CLIP AT FS 625 LT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CLIP AT FS 625 LT. (K)

Part: THRESHOLD — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CARGO COMPARTMENT THRESHOLD PLATE WAS FOUND TO BE CRACKED AT THE THRESHOLD COVER FORWARD LATCH BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT THRESHOLD PLATE AT FS 562.72 TO FS589.00 IAW EO. (K)

Part: HOUSING — CRACKED (EMERGENCY LIGHT)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT HOUSING BY THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. (K)

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING A C-CHECK, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING C-CHECK, THE DOUBLERS AT FS 718, STRINGER 10-12 LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE DOUBLERS AT FS 718, STRINGER 10-12 LT AND RT SIDES. (K)

Part: STEP — BROKEN (PAX DOOR)

FLT 4336 - DURING A GROUND INSPECTION IN CVG, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN LOOSE FROM THE TIE ROD WHICH WAS ALSO FOUND BENT. MAINTENANCE REATTACHED THE BOTTOM STEP TO THE TIE ROD AND ADJUSTED THE ACTUATING ARM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: UPLOCK — MISALIGNED (NLG)

DURING APPROACH, CREW RECEIVED A GEAR DISAGREE WARNING MESSAGE ON THE NOSE GEAR. THE QRH WAS COMPLIED WITH AND EMERGENCY WAS DECLARED. AC PERFORMED A FLYBY BUT TOWER WAS UNABLE TO COMFIRM IF NOSE GEAR WAS IN THE DOWN POSITION. UPON FURTHER COMPLETION OF THE QRH, THE GREEN DOWN INDICATOR LIGHT CAME ON. THE AC LANDED SAFELY. MAINT ADJUSTED THE NOSE LANDING GEAR (NLG) UPLOCK PIN IAW EO, CYCLED THE GEAR 50 TIMES AND PERFORMED 5 EMERGENCY GEAR RELEASES. ALL OPS CHECKS WERE GOOD. AC OK FOR SERVICE. (K)

Part: STEP — BROKEN (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,648 hrs

DURING CRUISE, THE RT FWD WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED AND THE CREW INITIATED A DESCENT TO 10,000 FT AND REDUCED AIRSPEED TO 250 KNOTS. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT FWD WINDSHIELD. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: CONTROL ROD — BINDING (PAX DOOR)

FLT 4708 - DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR DIFFICULT TO CLISE AND THE DOOR HANDLE DIFFICULT TO STOW. MAINTENANCE ADJUSTED THE PASSENGER DOOR FLAPPER CONTROL ROD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 9768 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 11 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW ELEVEN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — BROKEN (CABIN)

DURING A GROUND INSPECTION IN ATL, AN EMERGENCY FLOOR LIGHT STRIP WAS FOUND BROKEN AT THE FRONT OF THE STRIP. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHT STRIP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR BOTTOM STEP. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTAL AT FS 484, RBL 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTAL AT FS 484, RBL 38 IAW ASA EO 600-53-0098. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: CASE — CRACKED (EMERGENCY LIGHT)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT BASE AND LENS BY THE SERVICE DOOR WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4134 - DURING A GROUND INSPECTION IN SHV, THE EXTERIOR LEFT OVERWING AFT EMEGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR LEFT OVERWING AFT EMEGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DURING GROUND INSPECTION, WHEN SELECTED ON, THE EMERGENCY LIGHTS AT ROW 8 AND THE EXTERNAL OVERWING EXIT LIGHTS WOULD NOT STAY ON. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IN THE NR 3 POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: BEAM — CRACKED (SUPPORT BEAM)

DURING (C) CHECK, INSPECTION WHILE COMPLYING WITH VISUAL INSPECTION OF THE ENGINE SUPPORT BEAMS, THE LEFT SIDE WAS FOUND TO HAVE A CRACK. MAINTENANCE PERFORMED A TEMPORARY REPAIR. THIS REPAIR IS VALID FOR UP TO ONE YEAR FROM DATE OF INCORPORATION.

Part: BATTERY — DISCHARGED (CABIN)

FLT - 4460 - DURING GROUND INSPECTION IN MGM, CREW REPORTED THE EMERGENCY LIGHTING SYSTEM WOULD NOT TEST. THE SYSTEM VOLTS FELL TO 4.5 VOLTS IN 30 SECONDS. CAPTAIN CHARGED THE SYSTEM BATTERIES FROM 0750 TO 0851. MAINTENANCE OBSERVED THE EMERGENCY LIGHTING TEST FOR ONE MINUTE. SYSTEM TEST GOOD. NO FAULTS WERE DISCOVERED. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

FLT 4715 - WHILE EN ROUTE FROM SAV TO DFW, THE CAPTAINS WINDSHIELD SHATTERED. CREW FOLLOWED ABNORMAL PROCEDURES FROM QRH 11-8. CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN JAN. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

FLT 4698 - WHILE EN ROUTE FROM ATLANTA TO NEWBURGHN, NY, A LOUD BANG WAS HEARD ALONG WITH A CONCUSSION THAT REVERBERATED THROUGHOUT THE COCKPIT. A QUICK LOOK AROUND REVEALED THAT THE CAPTAINS WINDSHIELD HAD SHATTERED. AN EMERGENCY WAS DECLARED FOR PRIORITY HANDLING DUE TO THE EXTENT OF DAMAGE. AIRCRAFT LANDED SAFELY IN NEWBURGH. MAINTENANCE REPLACED THE WINDSHIELD. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)