N848AS

Part: LIGHT — UNSERVICEABLE (GALLEY) · airframe 35,754 hrs · 32,467 cycles

LOWER EMERGENCY LIGHT IN GALLEY UNSERVICEABLE. R & R GALLEY EMERGENCY LIGHT IAW AMM 33-51-10.

Part: BATTERY — DISCONNECTED (EMERGENCY LIGHTS) · airframe 35,110 hrs · 31,804 cycles

NR 3 AND 4 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. FOUND NR 2 EMERGENCY BATTERY PACK NOT INSTALLED IN CHARGER UNIT. INSTALLED BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 35,037 hrs · 31,724 cycles

EMERGENCY EXIT INOPERATIVE ON SIDE PANEL OF GALLEY NR 1. REPLACED BROKEN CONNECTOR J122LY BY REMOVING IT AND INSTALLING A NEW ONE IAW ESPM 20-17-31. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801, OPS TEST GOOD.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 35,037 hrs · 31,724 cycles

SEAT TRACK CORRODED OUT OF LIMITS IAW SRM 53-31-49 AND SRM 53-21-49. FABRICATED & INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485.

Part: ATTACH BRACKET — CRACKED · airframe 35,037 hrs · 31,724 cycles

CARGO DOOR LINTEL AFT BRACKET ATTACHED TO PRESSURE BULKHEAD CRACKED, REMOVED THE BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-11, SRM 51-42-21.

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 35,033 hrs · 31,718 cycles

5 BROKEN ISOLATORS FOUND ON THE AFT PRESSURE BULKHEAD FWD FACE. REPLACED 5 BROKEN ISOLATORS ON AFT PRESSURE BULKHEAD FWD FACE IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 35,033 hrs · 31,718 cycles

SEAT TRAC AT RBL9 BS 559-559+80 CORRODED. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-802, AND SRM 51-40-11.

Part: FRAME — CORRODED (BS 409) · airframe 35,033 hrs · 31,718 cycles

CORROSION AROUND 2 NUTPLATES UNDER FLOORBOARD 251ALF ON RBL9 AND AT FS 409+16 AND FS 409+32. REMOVED CORROSION IAW SRM 51-21-06. REMOVED .023 MATERIAL THICKINESS .063" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. C/W REO 601R-53-21-064.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 34,295 hrs · 30,972 cycles

EMERGENCY EXIT SIGN COVER MISSING BETWEEN GALLEY SERVICE DOOR AND SNACK BINS. REINSTALLED EMERGENCY LIGHT COVER IAW AMM 33-51-13.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 31,233 hrs · 27,815 cycles

AFT CEILING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AFT CEILING EMERGENCY LIGHT, FOUND WIRES TO BE DISCONNECTED. CONNECTED WIRES AND REINSTALLED LIGHT. OPS CHECKED GOOD, WORK DONE IAW MM 33-51-16-000-801 AND 33-51-16-400-801.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,229 hrs · 27,810 cycles

RT PRESSURE FLOOR SUPPORT IS CORRODED INBD OF EMERGENCY EXIT. REPAIRED IAW REO 601R-53-41-666, REV C.

Part: BEAM — CORRODED (BS 349) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON PAX DOOR AFT FRAME LOWER TRANSVERSE BEAM AT FS 349.00. REPAIRED IAW REO 601R-53-21-2392. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,233 hrs · 27,815 cycles

FS 280 FLOORBEAM CRACKED AND CORRODED. REMOVED DAMAGED AND REPAIRED IAW SRM CH 51-42-06, 51-42-10 & 51-42-21, & REO 601R-53-11-926.

Part: FLOOR SUPPORT — CORRODED (BS 310-364) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON RT FLOOR SUPPORT FWD OF SERVICE DOOR FROM FS 319.70 TO FS 310.00 AND AFT OF DOOR FROM FS 349.00 TO 364.00. REPAIRED IAW SRM 51-42-06, SRM 53-00-00 AND IAW REO 601R-53-21-2385.

Part: SILL — CORRODED (PAX DOOR) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON PAX DOOR LOWER SILL. REMOVED SILL ANGLE (LOWER) IAW SRM 51-42-21 & 51-42-06. LOWER SILL ANGLE FOUND TO HAVE CORROSION EXCEEDING LIMITS IAW SRM 53-00-00-01, T/R-53-27 . LOCATED & DRILLED NEW LOWER SILL ANGLE, IAW SRM 51-40-11-00. INSTALLED NEW SERVICEABLE PAX DOOR LOWER SILL ANGLE IAW SRM CH 51-42-06 & CH 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON FS 280.00 FLOOR SUPPORT. REMOVED DAMAGED FWD FLOOR SUPPORT IAW SRM CH 51-42-06 & 51-42-21. LOCATED & DRILLED NEW SERVICEABLE FLOOR SUPPORT, IAW SRM 51-40-11. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06.

Part: BEAM — CORRODED (BS 349) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON THE END OF THE TRANSVERSE BEAM FS 349.00, RBL 36 AT SERVICE DOOR AFT FRAME. COMPLIED WITH STEP 1 OF REO 601R-53-21-2391, REV P1 CUT AWAY DAMAGE.

Part: STRINGER — CORRODED (BS 654.5-672.2) · airframe 31,229 hrs · 27,810 cycles

AFT EQUIPMENT COMPARTMENT STRINGER 19R IS CORRODED BETWEEN FS 654.5 AND 672.2. STRINGER DAMAGED BEYOND REPAIR, REMOVED STRINGER IAW SRM 51-42-06. LOCATED, DRILLED & INSTALLED NEW STRINGER IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 310) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON FRAME AT FS 310.00 BETWEEN S26L AND 26R. REPAIRED IAW SRM 51-42-06 AND 51-42-21.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 31,229 hrs · 27,810 cycles

CARGO DOOR SILL IS CORRODED AROUND ALL NUTPLATES. REMOVED CARGO DOOR SILL IAW SRM 51-42-06, 51-42-21 & 51-42-10. INSTALLED NEW SERVICEABLE SILL IAW REO 601R-53-61-1574, REV A.

Part: FRAME — CORRODED (BS 349) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON FRAME AT FS 349 BETWEEN STR 26L AND 26R. REMOVED LOWER FRAME SECTION FS 349 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE LWR FRAME SECTION AT FS 349 AND INSTALLED FRAME IAW SRM 51-40-21, 51-42-06, 51-42-21.

Part: SILL — CORRODED (PAX DOOR) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON PAX DOOR LOWER SILL FWD AND AFT CUPS. REPAIRED IAW SRM CH 51-42-06 & 51-42-11.

Part: FLOORBEAM — CORRODED (BS 310) · airframe 31,233 hrs · 27,815 cycles

THE FLOORBEAM STRUCTURE MOUNT IS CORRODED AT FS 310. REMOVED FLOORBEAM SUPPORT MOUNT IAW SRM 51-42-21. LOCATED & INSTALLED FLOORBEAM JOINT ANGLE IAW SRM 51-40-11 & 51-42-21, PN 601R38335-1.

Part: SILL — CORRODED (BS 319.7-349) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON SERVICE DOOR SILL FROM FS 319.70 TO FS 349.00. REMOVED SILL IAW SRM 51-42-06 AND SRM 51-42-21 AND SRM 51-42-10. DRILLED, LOCATED AND INSTALLED NEW SERVICEABLE SILL IAW SRM 51-42-06, 51-42-21 AND 51-42-10.

Part: FITTING — CORRODED (SERVICE DOOR) · airframe 31,233 hrs · 27,815 cycles

SERVICE DOOR FITTING IS GOUGED AND CORRODED. REMOVED SERVICE DOOR FITTING BETWEEN FS 319 AND 349 IAW SRM 51-41-02. LOCATED AND DRILLED NEW SERVICE DOOR FITTING, IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE SERVICE DOOR FITTING IAW AMM 20-21-00-910-801.

Part: FRAME — CORRODED (BS 314.7) · airframe 31,233 hrs · 27,815 cycles

CORROSION ON FRAME AT FS 314.7 BETWEEN STR 26L AND STR 26R. REMOVED LOWER SECTION OF FRAME AT FS 319.00, STR 24L-24R IAW SRM 51-42-06 & 51-42-21. LOCATED & DRILLED HOLES COMMONT TO SKIN AND SPLICE & NEW SERVICEABLE FRAME SECTOR PN 601R32003-61 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FRAME AT FS 319.7 IAW SRM 51-42-06, 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 31,229 hrs · 27,810 cycles

FS 409+128 VERTICAL POST LBL 18 INBOARD AFT UPPER RADIUS FAILED NDT WITH INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX .2 LONG. REMOVED INBD & OTBD VERTICAL POST AT LBL 18 FS 409+128 IAW SRM 51-42-22. LOCATED AND DRILLED NEW VERTICAL POST AT LBL 18, FS 409+128 IAW SRM 51-40-11. INSTALLED INBD AND OTBD VERTICAL POST AT FS 409+128 LBL 18 IAW REO 601R-53-41-889.

Part: SUPPORT BRACKET — CRACKED (WINDSHIELD) · airframe 31,228 hrs · 27,809 cycles

RIGHT WINDSHIELD LOWER SIDE POST SUPPORT BRACKET IS CRACKED, APPROX .500" LONG. INSTALLED NEW SUPPORT BRACKET IAW SRM 51-42-21.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 31,228 hrs · 27,809 cycles

BROKEN QUICK DISCONNECT FOR EMERGENCY LIGHTS IN WARDROBE. INSTALLED QUICK DISC SPLICES FOR WARDROBE EMERGENCY LIGHT IAW ESPM 20-17-10 ON ACFT SIDE. OPS CHECKED, EMERGENCY LIGHTS REO 33-51-00-710-801.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,225 hrs · 27,807 cycles

FS 621, BULKHEAD FWD FACE FAILS NDT WITH AN INDICATION ON LBL 36.20, WL 80 GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-53-61-4747.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,225 hrs · 27,807 cycles

FS 621 BULKHEAD FWD FACE FAILS NDT WITH AN INDICATION ON RBL 27.50, WL 83-93 GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-53-61-1285.

Part: ANGLE — CRACKED (BS 280) · airframe 31,228 hrs · 27,809 cycles

INBD AND OTBD ANGLES AT FS 280.00 LBL 9 CRACKED. ANGLES REPLACED IN CONJUNCTION WITH REO 601R-53-11-926.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 31,228 hrs · 27,809 cycles

FLOORBEAM AT FS 484.00, RBL 27 AND RBL 36 CRACKED. FABRICATED AND INSTALLED FLOORBEAM ANGLE IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 280) · airframe 31,228 hrs · 27,809 cycles

INBD AND OTBD ANGLES AT FS 280.00, RBL 9 CRACKED. ANGLES REPLACED IN CONJUNCTION WITH REO 601R-53-11-926.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 31,229 hrs · 27,810 cycles

FLOORBEAM ANGLES AT FS 484.00, LBL 27 AND LBL 36 ARE CRACKED. FABRICATED AND INSTALLED NEW ANGLES IAW REO 601R-53-41-059.

Part: PDU — FAILED (THRUST REVERSER) · airframe 29,339 hrs · 25,780 cycles

LEFT THRUST REVERSER UNLOCKED MESSAGE DURING CLIMB, EMERGENCY DECLARED. PERFORMED CHECKLIST AND COMPLIED WITH QRH PROCEDURE. AIR RETURN TO DEPARTURE. R & R LT ENGINE PDU IAW AMM 78-32-03 AND 78-32-03, ITEM 5A. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 29,170 hrs · 25,596 cycles

F/O FLASHLIGHT INOPERATIVE. R & R F/O FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 27,676 hrs · 23,946 cycles

CA'S FLASHLIGHT INOP. REPLACED BATTERIES, CAPT FLASHLIGHT IAW AMM 25-60-00. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,309 hrs · 23,528 cycles

CORROSION AROUND SEVERAL SCREW HOLES UNDER FLOORBOARD 251ALF AND ON FLOORBEAMS. BLENDED AREA AT RBL9 BETWEEN FS 409.00+48 AND FS 409.00+64 HAS A REMAINING THICKNESS OF .025 WITH MATERIAL THICKNESS IS .050 AND IS OUT OF ALLOWABLE LIMITS. IAW SRM 53-00-00, FIG 101 AND FIG 102 AND ALSO IAW REO 601R-53-00-005.

Part: ATTACH FITTING — CRACKED (BS 621) · airframe 27,309 hrs · 23,528 cycles

CLIP CRACKED REAR BULKHEAD AFT FACE AT FS 621 ON 3RD INTERCOSTAL FROM BOTTOM ON LT SIDE. CLIP CRACKED ON REAR BULKHEAD AFT FACE WAS FOUND TO BE AT FS 625 LT SIDE. R & R IAW SRM 51-40-11 AND 51-42-20 APPLIED SEALANT AND FINISH COAT IAW 51-25-00 AND 51-23-00. THIS IS A MINOR REPAIR.

Part: ATTACH FITTING — CRACKED (BS 621) · airframe 27,309 hrs · 23,528 cycles

CLIP CRACKED REAR BULKHEAD AFT FACE AT FS 621 ON 3RD INTERCOSTAL FROM BOTTOM ON RT SIDE. CLIP CRACKED REAR BULKHEAD AFT FACE AT FS 621 ON 3RD INTERCOSTAL FROM BOTTOM ON RT SIDE RT.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,309 hrs · 23,528 cycles

RT SIDE SEAT RAIL HAS MINOR CORROSION AT SEAT LOCATION 12CD. REMOVED MINOR CORROSION ON RT SIDE SEAT RAIL. REMOVED .008" MATERIAL AT LOCATION 12CD. IAW SRM 51-21-06. CONTACT MFG FOR DAMAGE LIMITATIONS AND REPAIR PROCEDURE. REPLACE SEAT IAW STEP 3. REMOVED RT SIDE SEAT RAIL AT LOCATION 12CD. IAW AMM 53-01-11-000-802. RECEIVED SERVICEABLE SEAT TRACK SECTION. PN 601R38312-137 FOR REPLACEMENT OF SECTION BETWEEN FS 559 TO 559+80 ON RT SIDE SEAT RAIL. MFG THD NO LONGER REQUIRED. PICKED UP FASTENER HOLES AND COUNTERSINKS. IAW SRM 51-40-11 AND 51-41-02. INSTALL SERVICEABLE SEAT TRACK SECTION. INSTALLED SERVICEABLE RT SIDE SEAT RAIL AT SEAT LOCATION 12CD IAW AMM 53-01-11-400-802. THIS IS A MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 27,309 hrs · 23,528 cycles

9L SEAT TRACK SEGMENT FROM FS 364 TO 394 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM INNER LOWER SURFACE OF SEAT TRACK AT STA 364 ON LT PASSENGER SEAT TRACK. BLEND DIMENSION 1" LENGTH X .5" WIDTH X .055" DEPTH. OUT OF LIMITS IAW SRM 53-21-49. R & R SEAT TRACK SEGMENT. REMOVED 9L SEAT TRACK SEGMENT FROM FS 364 TO FS 394 IAW AMM TASK 53-01-11-000-802, DB80016 3. FABRICATE AND/OR REPLACE SEAT TRACK. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-420-001.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 27,309 hrs · 23,528 cycles

9R SEAT TRACK SEGMENT FROM FS 409 TO 559 + 32 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM SEAT TRACK. BLEND DIMENSIONS .5" WIDE X .5" LONG X .022" DEEP. OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK SEGMENT IAW AMM 5.-01-11-000-802. FABRICATED SEAT TRACK SEGMENT IAW REO 601R-53-00-396 STEPS 1, 2. COUNTERSINK FASTENER HOLES IN NEW SEAT TRACK SECTION AND COMPLY WITH STEPS 3 AND 4 OF REO 601R-53-00-396. COUNTERSUNK FASTENERS HOLES IN NEW SEAT TRACK SECTION AND COMPLIED WITH STEPS 3 AND 4 OF REO 601R-53-00-396. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 27,309 hrs · 23,528 cycles

9L SEAT TRACK SEGMENT FROM 394 TO 409 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM INNER SURFACE OF PASSENGER LT SEAT TRACK AT STA 409 + 128. BLEND DIMENSIONS .025" DEPTH X .5" LENGTH X .5" WIDTH. CORROSION REMOVAL OUT OF LIMITS IAW SRM 53-21-49. R & R SEAT TRACK SEGMENT. REMOVED 9L SEAT TRACK SEGMENT IAW AMM TASK 53-01-11-000-802. FABRICATED NEW SEAT TRACK SECTION IAW SRM 51-41-02. COMPLIED WITH STEPS 1 THROUGH 4 OF THE REO 601R-53-00-396, AND INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. MINOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,309 hrs · 23,528 cycles

CORROSION AROUND SEVERAL SCREW HOLES UNDER FLOORBOARD 251ALF AND ON FLOORBEAMS. BLENDED CORROSSION ON FLOORBEAM. PERFORMED UT THICKNESS INSP OF BLEND AREAS IAW MAC NOT INSP PROCEDURE UT-3. FOUND TO BE IN LIMITS IAW REO 601R-53-00-005.

Part: SEAT TRACK — CORRODED · airframe 27,309 hrs · 23,528 cycles

LT SIDE SEAT RAIL HAS MINOR CORROSION AT SEAT POSITION 3A (SIDE RAIL). REMOVED MINOR CORROSION ON LT SIDE SEAT RAIL AT SEAT POSITION 3A IAW SRM 51-21-06. MATERIAL REMOVAL FROM SIDE SEAT RAIL AT SEAT POSTION 3A WAS .006" AND .369". DAMAGE OUT OF LIMITS, BLENDED OF CORROSION. COMPLIED WITH STEP 2 OF REO 601R-53-31-0713 IAW NDTM 51-20-06 NO CRACK NOTED. REMOVED LT FWD DADO DUCT TO FOM IAW AMM 25-26-02-04, COMPLIED WITH STEP 4 OF REO 601R-53-31-07-13. COMPLIED WITH STEP 3 OF REO 601R-53-31-07-13. FOUND TO BE SATISFACTORY.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 27,309 hrs · 23,528 cycles

9R SEAT TRACK SEGMENT FROM FS 364 TO 394 CORRODED BEYOND LIMITS. REPLACE SEAT TRACK SEGMENT. REMOVED SEAT RAIL SEGMENT FROM FS 364 - 394 IAW AMM 53-01-11-04. REPLACE AND /OR FABRICATE AS NEEDED, INSTALLED SERVICEABLE SEAT RACK AT 9R FS 364 TO 394 IAW AMM 53-01-11-400-802, MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 27,309 hrs · 23,528 cycles

9L SEAT TRACK SEGMENT FROM FS 409 TO 559 + 32 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM LT PASSENGER SEAT TRACK. BLEND DIMENSION .5" LONG X .5" WIDE X .025" DEEP OUT OF LIMITS IAW SRM 53-41-29. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. FABRICATED SEAT TRACK SEGMENT IAW REO 601R-53-00-396. STEPS 1, 2, 3. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 27,309 hrs · 23,528 cycles

9L SEAT TRACK SEGMENT FROM FS 559 + 32 TO 559 + 80 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM SEAT TRACK. BLEND DIMENSIONS .5" WIDE X .5" LENGTH X .024" DEEP. OUT OF LIMITS IAW SRM 53-21-49. REMOVED 9L SEAT TRACK SEGMENT IAW AMM TASK 53-01-11-000-802. FABRICATED AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 27,309 hrs · 23,528 cycles

9R SEAT TRACK SEGMENT FROM FS 394 TO 409 CORRODED BEYOND LIMITS. REMOVED CORROSION FROM RT PASSENGER SEAT TRACK. BLEND DIMENSIONS .75 LONG X .75 WIDE X .023" DEEP OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-06. REPLACED CORRODED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: NUT PLATE — BROKEN (BULKHEAD) · airframe 27,309 hrs · 23,528 cycles

AFT CARGO AFT PRESSURE BULKHEAD HAS NUTPLATE BROKEN AT CTR ROW, 2ND ROW UP FROM FLOOR (ISOLATOR). REMOVED BROKEN ISOLATOR MOUNT ON AFT PRESS BULKHEAD & INSTALLED NEW ISOLATOR MOUNT IAW SRM 51-42-13 THIS IS A MINOR REPAIR.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 27,309 hrs · 23,528 cycles

SEAT TRACK IN AFT CARGO ARE CORRODED AS MARKED. REMOVED CORROSION FROM CARGO TIE-DOWN TRACK AT FS 559+112 LBL 9.00. BLENDED DIMENSION .75" LONG X .75" WIDE X .025" DEEP. OUT OF LIMITS IAW SRM 53-61-49, FIG 101. R & R SEGMENT AT FS 559+112. SM 80079 12/07/10 (LT 12/08/10). R & R CARGO TIE-DOWN TRACK AT FS 559 ON LBL 9.00 IAW AMM 53-01-11-000-802 AND 53-01-11-400-802. (CLOSED)

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 27,309 hrs · 23,528 cycles

2 EA CORRODED NUTPLATES ON LBL 27 AT CARGO DOOR, LT. CORRODED NUTPLATES REPLACED ON JOB 8733921, OP 83 DS9463.

Part: FLOOR SUPPORT — CORRODED (BS 579-609) · airframe 27,309 hrs · 23,528 cycles

FLOOR SUPPORT CORRODED AROUND NUT PLATE HOLE ON LBL 27 AT FS 580 (APPROX). BLENDED OUT CORROSION ALL THE WAY THRU MATERIAL AT FUSELAGE STA 579, 585, 591, 597, 603, AND 609 ON OTBD FLANGE OF LBL 27 FLOOR SUPPORT. OUT OF ALLOWABLE LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,309 hrs · 23,528 cycles

FOUND LIGHTED FLOOR LEVEL EMERGENCY SIGN AT SERVICE DOOR AND PAX DOOR INOP. REPLACED PACK NR 1 IAW AMM TASK 33-51-06-400-801 AND RASK 33-51-04-400-801 AND PERFORMED OPS CHECK IAW AMM TASK 33-51-06-740-801. NO DEFECTS NOTED. OPS TEST IS GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,391 hrs · 22,464 cycles

NR 3 CEILING CABIN EMERGENCY FLOOD LIGHT INOP. RELAMPED NR 3 CEILING CABIN EMERGENCY FLOOD LIGHT IAW AMM 33-51-16. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,994 hrs · 22,004 cycles

EXIT LIGHTS NEAR PAX DOOR OUT. RESET EXIT LIGHTS IAW AMM 33-50-01. CKS GOOD.

Part: CHECK VALVE — FAILED (CABIN AIR) · airframe 25,710 hrs · 21,669 cycles

RIGHT AFTER TAKEOFF, F/A CALLED REPORTING SMOKE IN CABIN. SHORTLY AFTER RECEIVED SMOKE TOILET CAUTION - STARTED TO RUN QRH AND CAUTION EXTINGUISHED - SMOKE SLOWLY CLEARED UP - RETURNED TO DEPARTURE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- TOWER DECLARED AN EMERGENCY AS A PRECAUTION). R & R RT ENG BLEED AIR CK VALVE. RAN ENG AND BLEEDS 3 TIMES. NO FURTHER DISCREPANCIES NOTED. IAW AMM 36-11-31.

Part: COVER — MISSING (CABIN) · airframe 24,712 hrs · 20,594 cycles

EXIT LIGHT AT GALLEY SERVICE DOOR MISSING COVER.

Part: DOUBLER — FAILED (FUSELAGE) · airframe 23,710 hrs · 19,657 cycles

JOB 8733915 OPERATION 180 / FRAME DOUBLER P/N 601R5361193-13 AT LT FRAME FS 718.00 FAILED LPI ON S/B 601R-53-055 PART D PROCEDURE K STEP F.

Part: PRESSURE PANEL — CRACKED (BS 460) · airframe 23,710 hrs · 19,657 cycles

FS 460 PRESSURE FLOOR BETWEEN BL 0.0 TO RBL 9.0 HAS INDICATION NOTED 2.8" IN LENGTH FAILED NDT INSP. COMPLIED WITH FS 460 PRESSURE WEB REPAIR IAW REO 601R-53-41-884.

Part: BULKHEAD — CRACKED (BS 621) · airframe 23,710 hrs · 19,657 cycles

2 INDICATIONS NOTED ON FWD SIDE OF FS 621.0 PRESSURE BULKHEAD WEB, ABOVE AND BELOW LINTEL FITTING. INDICATION ABOVE FITTING IS APPROX .2" IN LENGTH AT 80% F.S.H. INDICATION BELOW FITTING IS APPROX .2" IN LENGTH AT 100% F.S.H. FAILED NDT INSPECTION. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR COMPLIES WITH THE REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D. FUSELAGE EXTERIOR REQUIRES PAINT. TOUCHED UP RIVETS IAW SRM 51-25-01.

Part: BULKHEAD — CRACKED (BS 559) · airframe 23,710 hrs · 19,657 cycles

SEMI PRESSURE BULKHEAD WEB FS 559.00 HAS HFEC INDICATION NOTED AT RBL 18 WL 59.10 INDICATION IS APPROX 1.5" LONG AND 100% FULL SCREEN HEIGHT. FAILS NDT INSPECTION. SEMI PRESSURE BULKHEAD WEB FS 559.00 HAS HFEC INDICATION NOTED AT RBL 18 WL 59.10 INDICATION IS APPROX 1.5" LONG AND 100% FULL SCREEN HEIGHT. FAILS NDT INSPECTION. REPAIRED SEMI-PRESSURE BULKHEAD WEB F.S. 559.00 IAW REO 601R-53-41-260. REPAIRED THE SEMI-PRESSURE BULKHEAD WEB AT F.S. 559.00 IAW REO 601R-53-41-260.

Part: POST — DAMAGED (BS 409) · airframe 23,709 hrs · 19,657 cycles

LT AND RT FS 409.0+128 VERTICAL POST AT BL 18.0, WL 69.0 HAS INDICATIONS NOTED LBL 18 O/B SIDE APPROX .2" IN LENGTH AND RH SIDE RBL 18 I/B AND O/B SIDES APPROX .2" IN LENGTH LH AND RH BL 18. FAILED NDT INSPECTION.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 23,411 hrs · 19,368 cycles

FS 202 FWD BULKHEAD CRACKED AT PARKING BRAKE CABLE AREA.

Part: DOOR — OBSTRUCTED (PAX) · airframe 23,334 hrs · 19,296 cycles

PAX DOOR SHOW CAUTION MSG ILLUMINATED ON PUSHBACK. RAMPERS INDICATED A "PIN" WAS OBSTRUCTING ABILITY TO CLOSE HANDLE. GATE RETURN.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 20,813 hrs · 17,120 cycles

PAX DOOR HANDLE BROKEN. COULD NOT OPEN DOOR FROM INSIDE.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 20,484 hrs · 16,865 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOP.

Part: PLACARD — MISSING (AIRSTAIR DOOOR) · airframe 20,375 hrs · 16,774 cycles

EXIT STICKER MISSING ON AIRSTAIR DOOR. FLT 4744 DEL 55 MINS.

Part: WARNING MESSAGE — ACTIVATED (STEERING SYS) · airframe 19,304 hrs · 15,970 cycles

AFTER SELECTING GEAR DOWN FOR APPROACH, STEERING INOP MSG APPEARED. EMERGENCY DECLARED.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,901 hrs · 15,657 cycles

FS 280 BETWEEN LBL 9 AND LBL 27 FLOOR PANEL NUT PLATE SILL CORRODED, JUST O/B OF THE REPAIR CUT LINE. REPAIRED PER REO 601R-53-11-926. ALL WORK DOCUMENTED ON N/R 138. JOB COMPLETE. REB 7019524. 11-29-06. SUPPLEMENTAL - SDR CLOSED 11/30/06.

Part: PLACARD — WORN (ESCAPE HATCH) · airframe 18,901 hrs · 15,657 cycles

EXTERIOR PLACARDS ON CREW ESCAPE HATCH WORN.

Part: SILL — CORRODED (BS 409-461) · airframe 18,901 hrs · 15,657 cycles

SPOTS OF CORROSION AT LT FLOOR SILL DOUBLERS BETWEEN FS 409+128 AND FS 461 AND LBL 36.00 AND 44. COMPLIED WITH EC/TC REO 601R-53-41-462.

Part: SILL — CORRODED (FUSELAGE) · airframe 18,901 hrs · 15,657 cycles

CORROSION ON CARGO DOOR SILL AROUND FLOORBOARD NUT PLATES FROM FS 559.12 TO FS 625.00.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 18,901 hrs · 15,657 cycles

SERVICE DOOR CUTOUT FWD FRAME HAS FITTING SEVERELY CORRODED AT FLOOR LEVEL. REPAIRED CORROSION AND REPLACED FITTING IAW SRM 51-42-06 AND 51-42-21.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 18,901 hrs · 15,657 cycles

CARGO DOOR LENTIL SUPPORT CLIP CRACKED. REMOVED AND REPLACED CARGO DOOR LENTIL SUPPORT CLIP PER CRJ 200 SRM 51-42-13. BM24222 11-24-06. JOB COMPLETE. (CLOSED 11/27/06).

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 18,901 hrs · 15,657 cycles

FLOOR SUPPORT STRINGER CORRODED AT PAX DOOR LOWER SILL. DUPLICATE WRITE UP. REFER TO W/O 42583 N/R-00074 FOR CORRECTIVE ACTION, SM18595 11/24/2006.

Part: BULKHEAD — CORRODED (BS 280) · airframe 18,901 hrs · 15,657 cycles

FUSELAGE STA 280 BULKHEAD, CORROSION ON WEB AND FLOOR SUPPORT ANGLES BETWEEN RBL 9 AND LBL 9. EC/TC REO 601R-53-11-926 COMPLIED WITH.

Part: BULKHEAD — CRACKED (BS 280) · airframe 18,901 hrs · 15,657 cycles

STA 280 BULKHEAD WEB CRACKED AT LBL 9 EMERGENCY GEAR EXTENSION PULLEY BRACKET. REPAIRED DAMMAGE IAW REO 601R-53-11-126, ALL WORK DOCKUMENTED ON N/R-00138 MS7022223 JOB COMPLETE.

Part: FRAME — CRACKED (BS 640) · airframe 18,901 hrs · 15,657 cycles

RIGHT FS 640 FRAME IS CRACKED. REPAIRED DAMAGE TO RT FS 640 FRAME IAW SB 601R-53-061.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 18,901 hrs · 15,657 cycles

INBOARD AND OUTBOARD STA 280 CLIP CRACKED AT RBL 9. DRILLED UP TRIMMED FITTED AND INSTALLED 280 CLIPS REF CRJ 200 SRM 51-42-21. JOB COMPLETE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,901 hrs · 15,657 cycles

FLOOR SUPPORT STRINGER CORRODED AT PAX DOOR LOWER SILL PER MTC. INSTALLED NEW FLOOR SUPPORT STRINGER PER CRJ200 SRM 51-42-21 AND 51-42-06.

Part: INTERCOSTAL — CRACKED (BS 280) · airframe 18,901 hrs · 15,657 cycles

STA 280 AND LBL 9 FLOORBEAM OUTBOARD INTERCOSTAL, REPAIR ANGLE APPEARS CRACKED AT FWD END IN RADIUS.

Part: BULKHEAD — CRACKED (BS 280) · airframe 18,901 hrs · 15,657 cycles

STA 280 BULKHEAD WEB CRACKED JUST OUTBOARD OF RBL 9. REMOVED AND REPLACED 280 WEB SECTION PER REO 601R-53-11-926. JOB COMPLETE.

Part: FRAME — CRACKED (BS 640) · airframe 18,901 hrs · 15,657 cycles

LEFT FS 640 FRAME IS CRACKED. REPAIRED DAMAGE TO LT FS640 FRAME IAW SB601R-53-061

Part: FRAME — CRACKED (BS 640) · airframe 18,901 hrs · 15,657 cycles

LEFT AND RIGHT 640 FRAME CRACKED. WORK ACOMPLISHED IN N/R/ 00099 AND N/R-00100

Part: PLACARD — FADED (EMERGENCY EXIT) · airframe 17,722 hrs · 14,705 cycles

LT OVERWING EMERGENCY EXIT DOOR EXTERIOR PLACARD FADED.

Part: PLACARD — FADED (EMERGENCY EXIT) · airframe 17,722 hrs · 14,705 cycles

LT OVERWING EMERGENCY EXIT DOOR EXTERIOR PLACARD FADED.

Part: BULB — BURNED OUT (CABIN) · airframe 17,593 hrs · 14,597 cycles

FOUND EMERGENCY EXIT SIGN AT ASD HAS BULBS OUT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN VPS, THE EMERGENCY LIGHTS, NEAR THE SERVICE DOOR AND FORWARD PASSENGER DOOR, WERE FOUND IN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHTS INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE, THE PASSENGER DOOR LOWER STEP WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP. (M)

Part: PITOT TUBE — CLOGGED (AIRSPEED)

DURING TAKEOFF FROM ATL-HOU, THE FIRST OFFICERS AIRSPEED INDICATOR FAILED AND DURING CLIMB-OUT THE CREW RECEIVED STALL FAIL AND MACH TRIM MESSAGES FOLLOWED BY A YAW DAMP 1 INOPERATIVE MESSAGE. THE QRH WAS COMPLIED WITH WITHOUT THE MESSAGES CLEARING. AIRCRAFT HANDLING DEGRADED WITH NO FLIGHT CONTROL FAILURES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE FOUND THE RIGHT PITOT TUBE HEAD CLOGGED WITH REMAINS FROM A BIRD STRIKE. NO DAMAGE WAS NOTED TO THE PITOT TUBE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WEB — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE PASSENGER DOOR RUNNER WEB LOWER AFT AREA WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR RUNNER WEB LOWER AFT AREA IAW BOMBARDIER REO 601R-52-11-683. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FS 484 INBOARD CLIPS AT LBL 27 AND RBL 27 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FS 484 INBOARD CLIPS AT LBL 27 AND RBL 27 IAW WITH ASA EO 600-53-0098. (M)

Part: CLIP — CRACKED (FUSELAGE)

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

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 LEFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTNENANCE REPAIRED THE ENGINE SUPPORT BEAM AT BL 36.20 LT IAW ASA EO 600-53-0070. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INBOARD AND OUTBOARD CLIPS AT FS 280 LEFT AND RIGHT WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE INBOARD AND OUTBOARD CLIPS AT FS 280 LEFT AND RIGHT. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW ASA EO 600-53-0072A. (M)

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE FUSELAGE FRAME FS 718, STRINGER 10-11, LHS AND RHS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FUSELAGE FRAME FS 718, STRINGER 10-11, LHS AND RHS IAW ASA EO 600-53-0066. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE ENGINE SUPPORT BEAM AT BL 36.20 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM AT BL 36.20 RT IAW ASA EO 600-53-0073. (M)

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING HANGAR MAINTENANCE IN BTR, THE ENGINE SUPPORT BEAM AT BL 36.20 RT AT THE RIGHT ACCESS PANEL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED THE PERMANENT REPAIR TO THE ENGINE SUPPORT BEAM AT BL 36.20 RT AT THE RIGHT ACCESS IAW ASA EO 600-53-0070 AND ASA EO 600-53-0234. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT)

FLT 4316 - DURING A GROUND INSPECTION IN DFW, THE FIRST SECTION OF EMERGENCY FLOOR LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE FIRST SECTION OF EMERGENCY FLOOR LIGHTS CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

FLT 4589 - DURING A GROUND INSPECTION IN CAE, THE FIRST SECTION OF THE EMERGENCY FLOOR LIGHT STRIP WOULD NOT ILLUMINATE. MAINTENANCE FOUND A LOOSE CONNECTOR ON THE SECOND EMERGENCY FLOOR LIGHT STRIP AND RECONNECTED IT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — FAULTY (CABIN) · airframe 13,669 hrs

DURING HANGAR MAINTENANCE, THE EMERGENCY LIGHTS WERE FOUND FLICKERING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT TRACK BETWEEN ROWS 2 TO 5. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT)

FLT 4686 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT COVER BY THE PASSENGER DOOR WAS FOUND MISSING. MAINTENANCE INSTALLED A NEW COVER AND ALSO REMOVED AND REPLACED THE LAMP ON THE EMERGENCY EXIT LIGHT BY THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: OVERHEAT LOOP — MALFUNCTIONED (LT MLG WHEEL)

DURING DESCENT TO 11,000 MSL, THE CREW RECEIVED AN OVERHEAT MLG FAIL MESSAGE WHICH EXTINGUISHED AFTER APPROX FIVE SECONDS. SUBSEQUENTLY THE CREW RECEIVED A MLG OVERHEAT WARNING MESSAGE WHICH CYCLED ON AND OFF FOR THE REMAINDER OF THE FLIGHT. THE QRH WAS COMPLIED WITH AND PRIORITY HANDLING REQUESTED DUE TO REOCCURRING MESSAGE. AN EMERGENCY WAS DECLARED WITH EMERGENCY VEHICLES ON STANDBY. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT MAIN OVERHEAT WHEEL ASSY LOOP AND HARNESS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: ROD END — LACK OF LUBE (PAX DOOR)

FLT 4243 - DURING A GROUND INSPECTION IN DFW, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR WAS VERY DIFFICULT TO OPEN. MAINTENANCE COULD NOT DUPLICATE THE PASSENGER DOOR DISCREPANCY. THE PASSENGER DOOR HANDLES AND ROD ENDS WERE LUBRICATED FOR PREVENTATIVE MAINTENANCE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PASSENGER DOOR)

DURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN ON THE FORWARD CORNER. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING GROUND INSPECTION IN SHV, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (LEFT)

FLT 4162 - DURING TAKEOFF ROLL FROM ATL TO PHL, THE CAPTAIN REPORTED THE LT ENGINE OIL PRESSURE WAS 20 LBS LESS THAN THE RT ENGINE, BUT STILL WITHIN LIMITS. AFTER TAKEOFF THE LT ENGINE OIL PRESSURE CONTINUED TO DECREASE WITH THE LOWEST PRESSURE BEING 49 LBS. THE CREW ALSO REPORTED AN OIL BURNING ODOR WHEN THE PACKS SWITCHES WERE SELECTED FROM APU TO ENGINE. AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE. (M)

Part: ENGINE — ODOR (LEFT)

FLT 4637 - DURING CLIMB-OUT FROM BTR-DFW, THE CREW NOTICED A STRANGE OILY ODOR IN THE AIRCRAFT WHEN SWITCHING THE PACKS FROM THE APU TO THE TENTH STATE BLEEDS. THE ODOR BEGAN TO DISSIPATE WHEN THE BLEEDS WERE SWITCHED BACK TO THE APU. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (CABIN AIR)

FLT 4511 - DURING CRUISE FROM CHS-DFW, THE CREW NOTICED A SLIGHT OILY AND MOLDY ODOR WHEN THE PACKS WERE OPERATED OFF THE TENTH STAGE BLEEDS WITH NO VISIBLE SIGNS OF SMOKE. THE AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE COULD NOT DUPLICATE THE ODOR ON THE GROUND. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: DIODE — INOPERATIVE (THRUST REVERSER)

FLT 4529 - DURING CLIMB-OUT FROM ATL-MGM, THE CREW RECEIVED A LEFT THRUST REVERSER UNLOCK AMBER CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND THE LEFT ENGINE WAS REDUCED TO FLIGHT IDEL FOR A SINGLE ENGINE LANDING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED TERMINAL DIODE MODULE 207-7 AND ZENER DIODE 1CR1KE. OPS CHECK OF THE SYSTEM GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SKIN — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT SIDE FS 718 FRAME SKIN BELOW THE DOUBLER WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT SIDE FS 718 FRAME SKIN BELOW THE DOUBLER IAW ASA EO 600-53-0067A. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

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

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE AFT EQUIPMENT BAY FRAMES FS 718, STRINGERS 10 TO 12 ON THE LEFT AND RIGHT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE AFT EQUIPMENT BAY FRAMES FS 718, STRIGNERS 10 TO 12 ON THE LEFT AND RIGHT SIDES IAW ASA EO 600-53-0067A. (M)

Part: RIB — CRACKED (LT WING)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WLS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT AND RIGHT BATT RIB ASSEMBLY AT WS 53-60 IAW ASA EO 600-57-039A. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4340 - DURING GROUND INSPECTION IN ATL, THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT LAMP. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTON IN DFW, THE EXTERIOR SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR SERVICE DOOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: APU — INOPERATIVE (FUSELAGE)

DURING DESCENT INTO MLB FROM ATL, AS THE AUXILIARY POWER UNIT WAS POWERED UP EXTREME JET FUEL FUMES OCCURRED IN THE CABIN THROUGH THE ENVIROMENTAL CONTROL SYSTEM. THE CREW SHUT DOWN THE AUXILIARY POWER UNIT AND THE AIRCRAFT LANDED SAFELY IN MLB. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

AFTER LANDING IN ATL AND DURING DEPLANING OF PASSENGERS AT THE GATE, THE CAPTAINS LEFT FRONT WINDSHIELD SHATTERED. THE WINDSHIELD HEAT HAD ALREADY BEEN TURNED OFF WHEN IT OCCURRED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS LEFT FRONT WINDSHIELD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 4798 - ON GROUND IN ATL, CREW DISCOVERED GREEN EMERGENCY LIGHT FLOOR STRIP AT ROW 3 WAS INOPERATIVE. MAINTENANCE FOUND STRIP IN POSITION ABOVE THE ONE TO THE AFT. STRIP WAS REMOVED AND PLACED IN ITS CORRECT POSITION. AIRCRAFT OK FOR SERVICE. (M)

Part: THRUST REVERSER — MALFUNCTIONED (ENGINES)

FLT 4613 - DURING FIGHT FROM LGA-RIC, CREW RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE. THE RIGHT THRUST LEVER DID NOT RETARD TO IDLE. THE AIRCRAFT WAS CONTROLLABLE WITH NO BUFFET OR YAW. THE CREW FOLLOWED THE CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY IN RIC. MAINTENANCE CYCLED THE THRUST REVERSER MANUALLY SEVERAL TIMES AND RAN ENGINES AND DEPLOYED PNEUMATICALLY SEVERAL TIMES WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. (M)