N870AS

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 32,779 hrs · 30,273 cycles

EMERGENCY RT COVER AND LIGHT BULB MISSING ON NR 1 GALLEY WALL, ENTRANCE LT SIDE. REPLACED EMERGENCY LIGHT ASSY ON IAW AMM 33-5119, GOOD. OK FOR SERVICE.

Part: SKIN — DAMAGED (RUDDER) · airframe 32,582 hrs · 30,051 cycles

DURING FLIGHT CONTROL TEST AFTER PUSHBACK, THE RT RUDDER PEDDAL WILL NOT REACH FULL DEFLECTION. DAMAGE TO RUDDAR, CAUSING OBSTRUCTION, SHEETMETAL REMOVED IAW REO 601R-55-41-197 PERFORMED OPS TEST OF RUDDAR IAW AMM 27-21-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,619 hrs · 29,050 cycles

FUSELAGE SKIN DAMAGE AROUND LOW PRESSURE GROUND CONNECTION DOOR. THE REPAIR HAS BEEN DETERMINED AND CLASSIFIED TO BE MAJOR REAPAIR. RECEIVED AND COMPLIED IAW EA 25-2015-237.

Part: ANGLE — CRACKED (BS 621) · airframe 31,018 hrs · 28,405 cycles

CARGO DOOR CROSSMEMBER ANGLE CRACKED AT FS 621.00 BULKHEAD. R & R ANGLE AT FS 621.00 CARGO DOOR CROSSMEMBER WITH NEW SERVICEABLE PART IAW SRM 51-42-21.

Part: SKIN — CRACKED (RT WING) · airframe 31,031 hrs · 28,420 cycles

FOUND RT LOWER WING PLANK FUEL ACCESS HOLE 640FB HAS MULTIPLE INDICATIONS NOTED ON AFT OTBD SIDE APPROXIMATELY 1.5" LONG, 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 31,018 hrs · 28,405 cycles

CORROSION ON FLOORBEAM AT FS 589.00 BETWEEN LBL 18 AND LBL 27. FOUND TO BE OUT OF LIMITS IAW TR 53-27, REQUIRES REPLACEMENT. REMOVED CORRODED FLOORBEAM CAP AT FS 589.00 BETWEEN LBL 18 AND LBL 27 IAW SRM 51-42-06, 51-42-21 AND 51-42-15. LOCATED AND INSTALLED NEW SERVICABLE FLOORBEAM CAP IAW SRM 51-42-15, 51-42-06 AND 51-42-21.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 31,031 hrs · 28,420 cycles

FS 621, LT FLOOR SUPPORT ANGLE CRACKED AT LBL 36. REO:601R-53-61-5473, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: DOOR SILL — CORRODED (BS 574-621) · airframe 31,018 hrs · 28,405 cycles

CORROSION ON CARGO DOOR SILL FROM FS 621.00 TO FS 574.00. 2 AREAS 0.003 IN. OUT OF LIMITS AT FS 589.00+13 AND FS 605.00+6.25 ENGINEERING REQUIREDD. DAMAGE WAS BLENDED OUT TO SMOOTH CONTOUR IAW REO 601R-53-61-5472. COMPLIED WITH REO 601R-53-61-5472.

Part: SKIN — CORRODED (WING) · airframe 31,031 hrs · 28,420 cycles

WING PLANK AT 540BB HAS CORROSION AT INBD SIDE IN NON-CRITICAL AREA. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.

Part: FRAME — CORRODED (BS 605) · airframe 31,031 hrs · 28,420 cycles

CORROSION ON FRAME AT FS 605.00, STR 27. REMOVED CORROSION ON FS 605. FRAME BETWEEN STR 25L AND 25R IAW SRM 51-21-06. FS 605.00 FRAME FOPUND TO BE OUT OF LIMITS IAW SRM 53-00-00, TRR 53-29. REMOVED OLD FS 605.00 FRAME SECTOR, PN:601R36026-27 BETWEEN FACTORY SPLICES AT STR 20L AND 20R IAW SRM 51-42-06 AND 51-42-21. REF ITEM 3, LOCATED NR 6 FOR DRILL-UP OF NON-FRAME SECTOR. LOCATED AND DRILLED NEW FS 605.00 FRAME SECTOR, PN:601R36026-27 IAW SRM 51-40-11. INSTALLED FS 605, FRAME IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED NEW FS 605.00 FRAME REINFORCING ANGLE, PN:601R36026-35 IAW SRM 51-40-11. INSTALLED REINFORCING ANGLE ONTO FRAME 605 IAW SRM 51-42-06. COMPLIED WITH STS EA 25-2015-109. EA 25-2015-109 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WC.

Part: SKIN — CORRODED (WING) · airframe 31,031 hrs · 28,420 cycles

WING PLANK AT 640BB HAS CORROSION IN SEVERAL AREAS. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.

Part: SEAT TRACK — CORRODED (BS 454-559) · airframe 31,018 hrs · 28,405 cycles

RT SIDE SEAT RAILS FROM FS 454 - FS 559+54 HAS SEVERAL AREAS OF CORROSION AROUND THE LOWER EDGE OF THE COIN HOLES; WORST IS AT FS 474, MARKED WITH ORANGE TAPE. REMOVED RT SIDE SEAT RAIL AT FS 449.85 TO FS 495.98 IAW AMM 53-01-11-000-802. INSTALLED RT SIDE SEAT RAIL AT FS 449.85 TO FS 495.98 IAW AMM 53-01-11-400-802. REMOVED RT SIDE SEAT RAIL AT FS 495.98 TO FS 535.02 IAW AMM 53-01-11-000-802. INSTALLED RT SIDE SEAT RAIL AT FS 495.98 TO FS 535.02 IAW AMM 53-01-11-400-802. REMOVED RT SIDE SEAT RAIL AT FS 535.02 TO FS 559.00 IAW AMM 53-01-11-000-802. INSTALLED RT SIDE SEAT RAIL AT FS 535.02 TO FS 559.00 IAW AMM 53-01-11-400-802. SEAT RAILS AT FS 449.85 TO FS 495.98 AND FS 535.02 TO FS 559.00 REQUIRE FABRICATION. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601-R53-00-055, REV A DATED 11/8/2011 AS WRITTEN.

Part: RETAINER — CORRODED (E/E BAY DOOR) · airframe 31,031 hrs · 28,420 cycles

MAIN AVI BAY DOOR SEAL RETAINER IS CORRODED. REMOVED SEAL RETAINER IAW SRM 51-42-06. REPLACED SEAL RETAINERS IAW SRM 51-42-06. PERFORMED OPS TEST OF THE MAIN AVIONICS COMPARTMENT DOOR SEAL IAW AMM 52-42-07-710-801. OPS TESTED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 31,018 hrs · 28,405 cycles

CORROSION ON UPPER SURFACE OF RT FLOOR SILL STRUCTURE FROM FS 409.00+128 TO FS 559.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C, DATED 11/06/12 AS WRITTEN.

Part: DOOR SILL — CORRODED (BS 319-349) · airframe 31,018 hrs · 28,405 cycles

CORROSION ON SERVICE DOOR SILL AT FS 319.70 AND FS 349.00. BLENDED AREA REMOVING CORROSION IAW REO 601R-53-00-530. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530, REV A.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 31,031 hrs · 28,420 cycles

CORROSION ON FLOOR SILL AFT OF PAX DOOR AT FS 349.00. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530, REV A.

Part: FRAME — CORRODED (BS 364) · airframe 31,018 hrs · 28,405 cycles

CORROSION ON FRAME AT FS 364.00 BETWEEN LBL 24 & RBL 24. COMPLIED WITH EA 32-2015-138.

Part: FLOORBEAM — CORRODED (BS 333) · airframe 31,018 hrs · 28,405 cycles

CORROSION FOUND ON AVIONICS BAY FLOORBOARD SUPPORT ANGLE AT FS 333.00. REMOVED FLOORBOARD SUPPORT ANGLE IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED FS 333.00 AVIONICS BAY FLOORBOARD SUPPORT BRACKET IAW SRM 51-40-11 AND SRM 51-42-06.

Part: FRAME — CORRODED (BS 330) · airframe 31,018 hrs · 28,405 cycles

CORROSION ON FRAME AT FS 330.00 BETWEEN LBL 24 & RBL 24. FOUND CORROSION TO BE LOCATED ON FRAME SECTOR AT FS 333.00 NOT FS 330.00. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-00. REMOVED CORRODED FRAME IAW SRM 51-42-21 AND 51-42-06. LOCATED AND DRILLED NEW FS 333.00 LOWER FRAME SECTOR, PN 601R32004-55 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE LOWER FRAME IAW SRM 51-42-00 AND 51-42-21.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 31,018 hrs · 28,405 cycles

SERVICE DOOR SILL, LOWER, ANGLE HAS CORROSION IN SEVERAL AREAS. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED LOWER SILL IAW SRM 51-42-21 AND 51-42-06. LOCATED AND DRILLED NEW SERVICE DOOR LOWER SILL ANGLE, PN:601R38303-253 IAW SRM 51-40-11. INSTALLED NEW SERVICE DOOR LOWER SILL ANGLE, PN: 601R38303-253 IAW SRM 51-23-00, 51-42-10, 51-42-21 AND 51-42-06.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,018 hrs · 28,405 cycles

FS 280.00 FLOORBEAM ANGLE AT RBL 9 OTBD & RBL 27 INBD ARE CRACKED. FABRICATED NEW FS 280, RBL 9 CLIP FROM S6144-13, PERFORMED ANGLE 2024T42 .050" IAW REO 601R-53-11-926, NOTE 20. REMOVED CRACKED CLIP AT FS 280, RBL 9.0, OTBD IAW SRM CH 51-42-21. COMPLIED WITH EC/TC REO 601R-53-11-926 01. REMOVED UNSERVICEABLE CIP. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLIP PT 601R31113-53 IAW SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: FRAME — CORRODED (BS 319) · airframe 31,018 hrs · 28,405 cycles

CORROSION ON FRAME AT FS 319.70 BETWEEN LBL 24 & RBL 24. FOUND CORROSION ON FS 319.70 FRAME OUT OF LIMITS IAW SRM 53-00-00. REMOVED FS 319.70 LOWER FRAME SECTOR FOR REPLACEMENT IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW FS 319.70 LOWER FRAME SECTOR, PN 601R32003-61 IAW SRM 51-42-06 AND 51-42-21.

Part: FRAME — CORRODED (BS 310) · airframe 31,018 hrs · 28,405 cycles

CORROSION ON FRAME AT FS 310.00 BETWEEN LBL 24 & RBL 24. FOUND CORROSION ON FRAME TO BE OUT OF LIMITS IAW SRM 53-00-00. COMPLIED WITH REO 601R-53-21-2612 P1.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,018 hrs · 28,405 cycles

FS 280.00 FLOORBEAM ANGLE AT LBL 9 INBD & OTBD ARE CRACKED. FABRICATED NEW FS 280, LBL 9 INBD AND OTBD CLIPS FROM S6144-13, PREFORMED ANGLE 2024T42 .050" IAW REO 601R-53-11-926, NOTE 20. REMOVED CRACKED LBL 9 INBD AND OTBD CLIPS AT FS 280 IAW SRM CH 51-42-21. COMPLIED WITH ECTC REO 601R-53-11-926 01.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 31,018 hrs · 28,405 cycles

CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AROUND 3 FASTENER HOLES BETWEEN FS 310.00 AND FS 349.00 LBL 27. COMPLIED WITH EC/TC REO 601R-53-00-005.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,067 hrs · 26,456 cycles

EMERGENCY LIGHT LAMP INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD, IAW AMM 33-51-00.

Part: PRIORITY VALVE — FAILED (MLG) · airframe 28,439 hrs · 25,811 cycles

GEAR UP DISAGREE WARNING AFTER DEPARTURE. LT AND RT GEAR WERE IN DISAGREEMENT (RED). COMPLIED WITH QRH. MANUAL GEAR HANDLE WAS PULLED IAW QRH. EMERGENCY DECLARED. RETURNED TO DEPARTURE AND LANDED AT 46500 LBS. R & R MLG PRIORITY VALVE IAW AMM 32-32-15. OPS CHECKED GOOD, NO FAULTS AT THIS TIME. OPS CHECKED GOOD IAW AMM 32-30-00-730-801. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,026 hrs · 25,400 cycles

CENTER CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OP'S CHECKED GOOD IAW AMM 33-51-16.

Part: SKIN — CRACKED (RT WING) · airframe 27,330 hrs · 24,661 cycles

RIGHT LOWER WING SKIN IS CRACKED .25" LONG AT WS 148.09 - REINFORCING ANGLE IN T/E ABOVE SKIN IS CRACKED .75" LONG. C/W ECTC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV J, DATED 03/08/2011 AS WRITTEN. C/W ECTC REO 601R-57-21-131 AND REO 601R-57-21-131, REV A DATED 08/29/2011 AS WRITTEN. REPAIRED IAW REO 601R-57-21-639.

Part: ANGLE — CRACKED (BS 621) · airframe 27,330 hrs · 24,661 cycles

FS 621, BULKHEAD AFT SIDE FS 621-625 ANGLES CRACKED. REMOVED CRACKED LT & RT FS 621-625 ANGLES AND INSTALLED SERVICEABLE ANGLES IAW SRM 51-40-11 AND SRM 51-42-06.

Part: ATTACH BRACKET — CRACKED (BS 280) · airframe 27,330 hrs · 24,661 cycles

PAX DOOR UPPER SILL ATTACHMENT BRACKET CRACKED AT FS 280. REMOVED CRACKED BRACKET AT FS 280, STR 3 IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLE ANGLE, PN 600-31057-19 IAW SRM 51-40-11. UPON FURTHER INVESTIGATION ANGLE, PN 600-31057-20, FS 280, STR 3 WAS FOUND TO BE CRACKED. REMOVED ANGLE, PN 600-31057-20, FS 280, STR 3 IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLE ANGLE, PN 600-31057-20 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE ANGLE, PN 600-31057-19 AT FS 280 STR 3L ON INBD SIDE OF STR IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE ANGLE, PN 600-31057-20 AT FS 280 STR 3L ON OTBD SIDE OF STR IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (BS 621) · airframe 27,330 hrs · 24,661 cycles

FS 621, BULKHEAD FAILS NDT WITH AN INDICATION FSH AT LBL 27.50, WL 130). REPAIRED IAW REO 601R-53-61-1541, REV D.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 27,329 hrs · 24,660 cycles

LEFT CABIN FLOOR SUPPORT IS CORRODED AT FOUR NUTPLATE LOCATIONS. DAMAGE IS APPROX BETWEEN FS 409+128 AND FS 559. REPAIRED IAW TASK 51-26-0-110-801, SRM 51-21-11, 51-27-19, 51-21-06, 51-26-00 AND REO 601R-53-41-666.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 27,330 hrs · 24,661 cycles

PRESSURE BULKHEAD FWD FACE HAS FIVE CRACKED ISOLATORS. R & R ISOLATORS ON FS 621 BULKHEAD IAW SRM 51-42-06.

Part: CARGO TRACK — CORRODED · airframe 27,330 hrs · 24,661 cycles

CARGO TRACKS CORRODED AROUND FASTENER HOLES AT LBL 27 AND LBL 9. R & R CARGO TRACKS IAW AMM 20-21-00-910-801.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,329 hrs · 24,660 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED IAW SRM 51-42-06 AND 51-42-10 AND REO 601R-52-11-513, REV A.

Part: SKIN — CRACKED (LT WING) · airframe 27,329 hrs · 24,660 cycles

LEFT LOWER WING SKIN CRACKED .25" LONG AT WS 148.019. C/W EC/TC REO 601R-57-21-130 AND GENERIC REO 601R-57-21-130, REV J. C/W EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131, REV A. REPAIRED IAW REO 601R-57-51-639, SRM 51-42-06, 51-42-21 & REO 601R-57-21-639 AND SNIEO 601R10336 S01P1.

Part: CONTROL LEVER — FAILED (TE FLAPS) · airframe 26,148 hrs · 23,437 cycles

ON SELECTING FLAPS FROM 8 TO 20 DEGREES, FLAPS FAIL CAUTION MESSAGE DISPLAYED. VERIFIED FLAPS STUCK AT 8 DEGREES ON EICAS FLIGHT CONTROL PAGE. COMPLIED WITH QRH. EMERGENCY DECLARED. COMPLIED WITH AD 2009-06-12 TROUBLESHOOTING FOR FLAP FAILURES. R & R FLAP CONTROL LEVER IAW AMM27-51-01. PART ROBBED FROM OTHER ACFT. OPS CHECK GOOD, NO FAULTS AT THIS TIME. SDR CLOSED.

Part: MOTOR — MALFUNCTIONED (DOOR ASSIST) · airframe 26,100 hrs · 23,385 cycles

PASSENGER DOOR DOES NOT OPEN FULLY. R & R PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. PERFORMED OPS CHECKS OF THE PWR DOOR ASSIST IAW AMM 52-11-08-720-802. NO DEFECTS NOTED DEFER CLEARED PLACARD REMOVED. SDR CLOSED.

Part: DETECTION SYS — MALFUNCTIONED (LT NACELLE) · airframe 25,337 hrs · 22,564 cycles

DURING FIRE WARNING TEST, DID NOT GET LEFT ENGINE FIRE LOOP-B WARNING MESSAGE AND LEFT FIRE PUSH SWITCH DOES NOT ILLUMINATE. INSPECTED LT ENGINE FIRE LOOPS, NO PROBLEMS NOTED. FOUND LT FIRE PUSH SWITCH LIGHT LOOSE IN ITS SOCKET. RESECURED THE FIRE PUSH SWITCH LIGHT IAW ESPM 20-24-00 ENGINE FIRE LOOPS OPS CHECK IAW AMM 26-11-00 GOOD AT THIS TIME.

Part: PIN — MISSING (DOOR HANDLE) · airframe 25,294 hrs · 22,518 cycles

SERVICE DOOR RELEASE HANDLE NOT FUNTIONAL. PIN MISSING. REPLACE MISSING PIN ON SERVICE DOOR RELEASE HANDLE. OPS CHECKED GOOD IAW AMM 52-41-02. (SDR CLOSED)

Part: ISOLATOR — BROKEN (BS 621 BULKHEAD) · airframe 23,396 hrs · 20,422 cycles

APPROX RBL 36, WL 92 ON AFT BULKHEAD, ISOLATER BROKEN RT SIDE. R & R RT OTBD ISOLATOR AT WATER LINE 92 ON FS 621 BULKHEAD IAW SRM 51-42-13. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 23,394 hrs · 20,419 cycles

FWD LEFT EMERGENCY LIGHTS ARE INOP ON TEST. FOUND CONNECTORS J11LY AND P10LY SWAPPED WITH CONNECTORS J20LY AND P21LY. INSTALLED TO ORIGINAL CONFIG AND RESEATED CONNECTORS IAW ESPM 20-17-10. PERFORMED OPS CHECK IAW AMM 33-51-00-710-801. SYS CHECKS GOOD. OK FOR SERVICE. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 23,394 hrs · 20,419 cycles

FS 280, FWD FLOOR SUPPORT ANGLE IS CORRODED. R & R FWD FLOOR SUPPORT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-06. REPAIR CLASSIFIED AS A MINOR.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 23,394 hrs · 20,419 cycles

FLOOR SUPPORT CORRODED FS 349 AT SERVICE DOOR SURROUND LOWER AFT FRAME BRACKET. REMOVED CORROSION, FOUND WITHIN LIMITS IAW SRM 53-21-15 AND SRM 53-00-00.

Part: POST — CRACKED (BS 409) · airframe 23,394 hrs · 20,419 cycles

INDICATION NOTED AT FS 409+128 BL 0.00 WK 69.0 RADIUS OF RT CHANNEL APPROX .10" LENGTH, 55 PERCENT. REMOVED POST ASSY IAW SRM 51-42-06, 51-42-21. INSTALLED NEW SERVICEABLE POST ASSY IAW REO 601R-53-41-889.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,394 hrs · 20,419 cycles

FS 280 AFT FLOOR ANGLE IS CRACKED OTBD OF RBL9 AND OTBD LBL9, REPAIRED IAW REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 23,394 hrs · 20,419 cycles

FLOORBEAM TEE AT FS 589 BETWEEN LBL 9 AND RBL 9 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND WITHIN LIMITS IAW SRM 53-00-00. ALODINED, PRIMED AND PAINTED IAW SRM 51-22-00.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,394 hrs · 20,419 cycles

RBL 9.0 SEAT TRACK FS 409.00 TO FS 409.0+128 HAS SEVERAL AREAS OF CORROSION. REMOVED SEAT TRACK, FABRICATED, AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-11, 51-25-00, 51-25-00 AND AMM 53-01-11-400-802. REPAIR CLASSIFIED AS A MINOR.

Part: ANGLE — CRACKED (BS 484) · airframe 23,394 hrs · 20,419 cycles

FS 484 ANGLE AT LBL 27.0 IS CRACKED. R & R ANGLE IAW REO 601R-53-41-059.

Part: PLACARD — DETERIORATED (ESCAPE HATCH) · airframe 23,394 hrs · 20,419 cycles

CREW ESCAPE HATCH SILKSCREENS ARE FADED. REAPPLIED CREW ESCAPE HATCH SILKSCREENS IAW AMM 11-10-03-400-801. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 574) · airframe 23,394 hrs · 20,419 cycles

CARGO SEAT TRACKS FWD OF FS 574, LBL AND RBL 9 ARE CORRODED. INSTALLED NEW SEAT TRACKS IAW AMM 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 280) · airframe 23,394 hrs · 20,419 cycles

FS 280.00 AFT "J" ANGLE IS CRACKED LBL9 JUST OTBD OF MLG ALTERNATE EXTENSION BRACKET. C/W EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,394 hrs · 20,419 cycles

CARGO TRACKS AT FS 559+80 LBL AND RBL 9 AND 27 ARE CORRODED. INSTALLED NEW CARGO TRACK IAW AMM 53-01-11-400-802 AND SRM 51-40-00.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 23,394 hrs · 20,419 cycles

FS 621 PRESSURE BULKHEAD HAS 6 CRACKED ISOLATORS 2 AT RBL 36, 1 AT RBL 27, 2 AT LBL 18 AND 1 AT LBL 27. R & R ISOLATORS PN SL2337-3 IAW SRM 51-42-06. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)

Part: ANGLE — CRACKED (BS 484) · airframe 23,394 hrs · 20,419 cycles

FS 484.00 ANGLE AT RBL 27.0 IS CRACKED. R & R ANGLE IAW REO 601R-53-41-059.

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 23,394 hrs · 20,419 cycles

RT NR1 FLOOR SEAT TRACK FS 364-FS 399.5 IS CORRODED RBL 9.00. REMOVED AND REPLACED WITH NEW SEAT IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 23,394 hrs · 20,419 cycles

RT NR 2 SEAT TRACK FS 399.5 TO FS 409+128 IS CORRODED RBL 9.00. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802. REPAIR CLASSIFIED AS A MINOR.

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 23,394 hrs · 20,419 cycles

FS 280, LBL9.0 OTBD CLIP IS CRACKED AND RBL9.0 INBD AND OTBD CLIPS ARE CRACKED. C/W EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,394 hrs · 20,419 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. COMPLIED WITH STEP 5 OF ASA EC/TC REO 601R-52-11-513 IAW NDTM PT1 51-20-06. NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH EC/TC REO 601R-52-11-513.

Part: SEAT TRACK — CORRODED (BS 399-409) · airframe 23,394 hrs · 20,419 cycles

LEFT NR 2 FLOOR SEAT TRACK FS 399.5 TO FS 409+128 LBL 9 IS CORRODED. R & R WITH NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-06, 51-40-00 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,394 hrs · 20,419 cycles

RT NR 4 CABIN FLOOR SEAT TRACK FS 559.00 +80, RBL 9 IS CORRODED. R & R SEAT TRACK IAW SRM 51-40-06, 51-40-00 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 23,394 hrs · 20,419 cycles

LT/ RT NR 3 FLOOR SEAL TRACKS FS 409+128 TO FS 559.00 LBR 9 AND RBL 9 ARE CORRODED. R & R LT AND RT NR 3 FLOOR SEAT TRACKS AT FS 409+128 - 559.00, LBL 9 IAW AMM 53-01-11-400-802 & SRM 51-40-00. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATIONTHIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,394 hrs · 20,419 cycles

F/A FLASHLIGHT INOP. R & R FLASHLIGHT IAW AMMA25-61-04. OPS OK. DEFER CLEARED. PLACARD REMOVED. (CLOSED)

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,394 hrs · 20,419 cycles

F/A FLASHLIGHT INOP. R & R FLASHLIGHT IAW AMMA25-61-04. OPS OK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,922 hrs · 19,881 cycles

LT FUSEALAGE POSITION NR 2 EMRGENCY LIGHT INOP. RELAMPED LT FUSELAGE POS NR 2 EMERGENCY LIGHT IAW 33-41-21.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,796 hrs · 19,740 cycles

LEFT NR 2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LT NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD. RELAMPED LT NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 22,644 hrs · 19,570 cycles

LT SIDE NR2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LT SIDE NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,549 hrs · 19,460 cycles

FWD CABIN EMERGENCY CEILING LIGHT IS INOP. R & R FWD EMERGENCY CEILING LIGHT IAW AMM 33-51-16. OPS CHECK GOOD. R & R FWD EMERGENCY CEILING LIGHT IAW AMM 33-51-16. OPS CHECK GOOD. (CLOSED)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,549 hrs · 19,460 cycles

LEFT EXTERNAL EMERGENCY LIGHT OVER LT WING IS INOP. R & R LT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. ITEM: 1 R & R LT EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,362 hrs · 19,246 cycles

THE SERVICE DOOR EXTERIOR LIGHT IS INOP. REPLACED THE SERVICE DOOR EXTERIOR EMERGENCY LIGHT. DONE IAW THE AMM CHAPTER 33-51-21. (CLOSED)

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,757 hrs · 18,544 cycles

CAPT FLASHLIGHT INOP. R & R BATTERIES, OPS CK GOOD, AMM 25-60-01.

Part: CHANNEL — CRACKED (BS 409) · airframe 21,545 hrs · 18,290 cycles

UPON INSPECTION OF THE PRESSURE BULKHEAD WEB AT FS 409+128 FOUND THE INBD U CHANNEL AT LBL-27 TO BE CRACKED AT LOWER AFT RADIUS AT LOWEST FASTNER HOLE. CRACK PROPAGATES PAST THE LOWEST FASTNER HOLE AND STOPS BEFORE THE NEXT FASTNER HOLE UP. (RESOLVED ON W/O: 154633 TASKCARD: N/R-00002 ) WORK COMPLETED IAW: ITEM: 1, REPAIRED CRACKED INBD U CHANNEL AT LBL-27 IAW REO 601R-53-41-056 REV A / ITEM: 2, RESTORED CIC TO REPAIR AREA IAW SRM51-21-11. (CLOSED)

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,315 hrs · 18,021 cycles

F/O'S FLASHLIGHT IS INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 19,892 hrs · 16,500 cycles

SHORTLY AFTER T/O, RECEIVED A GEAR DISAGREE MSG. EMERGENCY DECLARED, A/C RETURNED TO ATL AFTER T/O.

Part: SKIN — CRACKED (PAX DOOR) · airframe 19,677 hrs · 16,306 cycles

PAX DOOR FWD SKIN WEB IS CRACKED IN RADIUS AT STEPS 832CT AND FIXED MID STEP. REPAIRED PAX DOOR FWD SKIN WEB IAW REO 601R-52-11-702 AND REO 601R-52-11-702.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,677 hrs · 16,306 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED.

Part: POST — DAMAGED (FUSELAGE) · airframe 19,677 hrs · 16,306 cycles

FS 409.0+128 LBL 18.00 VERTICAL POST HAS AN INDICATION NOTED AT O/B SIDE WL 69.0 AFT FLANGE APPROX .2 INCH IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. FABRICATED REPLACEMENT POST IAW 51-24-21.INSTALLED POST IAW SRM 51-42-21 AND 51-42-22.

Part: POST — DAMAGED (FUSELAGE) · airframe 19,677 hrs · 16,306 cycles

FS 409.0+128 RBL 18.0 VERTICAL POST HAS AN INDICATION NOTED I/B AND O/B SIDES WL 69.0 AFT FLANGE APPROX .2 INCH IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. FABRICATED REPLACEMENT POST IAW SRM 51-24-21. INSTALLED POST IAW SRM 51-40-11 AND REO 601R-53-41-889.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,677 hrs · 16,306 cycles

LT FWD FLOOR TRACK (SEAT RAIL) HAS CORROSION DAMAGE ON FWD EDGE. REMOVED & REPLACED SEAT TRACK IAW AMM 53-01-11-400-802 & 51-23-00-390-810.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,677 hrs · 16,306 cycles

RT FWD FLOOR SEAT TRACK HAS CORROSION DAMAGE ON FWD END.

Part: WEB — CRACKED (PAX DOOR) · airframe 19,677 hrs · 16,306 cycles

PAX DOOR AFT WEB CRACKED APPROX .090 WIDE, .030H AT NR 2 HOLE AT FWD STRINGER POWER ASSIST MOTOR. REPAIRED PAX DOOR AFT WEB IAW REO 601R-52-11-1662.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 19,677 hrs · 16,306 cycles

REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2 INCHES IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REPAIR PER EC/TC REO 601R-53-61-1230.

Part: SKIN — CORRODED (FUSELAGE) · airframe 19,677 hrs · 16,306 cycles

LOWER AFT FUSELAGE SKIN AT FS 559+115, STR 26L HAS CORROSION BEYOND SRM LIMITS. COMPLIED WITH EC/TC REO 601R-53-51-085 REV.O AND REO 601R-53-51-085.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 19,677 hrs · 16,306 cycles

RT FS 559 BULKHEAD WEB HAS AN INDICATION NOTED APPROX .3 INCH IN LENGTH 90 PERCENT FSH AT WL. REPAIRED FS 559 BULKHEAD WEB IAW REO'S 601R-53-41-260 AND 601R-53-41-919.

Part: FRAME — NONE (FUSELAGE) · airframe 19,677 hrs · 16,306 cycles

RT FS 718 FRAME WEB HAS A CREASE WITH POSSIBLE CRACK JUST BELOW ACM SUPPORT. PERFORMED EDDY CURRENT INSP OF SUSPECTED AREA IAW NDTM PT 1 51-20-06. NO INDICATIONS NOTED AT THIS TIME. EVALUATED DENT PER SRM 53-00-00 FIG. 102, SHEETS 1 AND 2. WITHIN LIMITS SPECIFIED. NO CREASES WERE NOTED IN DENT DAMAGE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,677 hrs · 16,306 cycles

FS 621 TO FS 625 OBLIQUE AT STR 14 LT AND RT SIDES ARE CRACKED. REMOVED AND REPLACED OBLIQUES PER REO 601R-53-61-422 AND SRM 51-42-21.

Part: FLAP — FAILED (WING) · airframe 19,334 hrs · 15,996 cycles

FLAP FAIL AFTER TO WHILE BRINGING FLAPS FROM 8 TO 0. EMERGENCY DECLARED. ACFT RETURNED TO ATL AFTER T/O. FLT 5105X2

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,789 hrs · 15,497 cycles

STEERING MSGS CAUTION MESSAGE UPON GEAR RETRACTION. EMERGENCY VEHICLES REQUESTED TO BE ON STANDBY AS A PRECAUTION.

Part: LATCH — BROKEN (SERVICE DOOR) · airframe 17,620 hrs · 14,470 cycles

EXTERNAL SERVICE DOOR AFT LATCH BROKEN.

Part: DOOR — STUCK (MAIN PAX) · airframe 16,306 hrs · 13,345 cycles

PAX ENTRY DOOR WOULD NOT CLOSE.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 16,253 hrs · 13,302 cycles

FLAPS FAIL MESSAGE, FLAPS FAIL AT 20 DEGREES. EMERGENCY DECLARED.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 16,241 hrs · 13,288 cycles

FLAPS FAIL AT 20' ON FINAL APPROACH INTO ATL- LANDING UNEVENTFUL. SELECTING FLAPS 30' WHEN THE FAILURE OCCURED. EMERGENCY DECLARED. EMERGENCY EQUIP ON STANDBY.

Part: DOOR — BINDING (PAX DOOR) · airframe 16,167 hrs · 13,233 cycles

F/A REPORT PAX BOARDING DOOR DIFFICULT TO OPEN, APPEARS TO BE CAUGHT ON SOMETHING.

Part: STEP — CRACKED (PAX DOOR) · airframe 15,778 hrs · 12,926 cycles

PAX DOOR FOLDING STEP, HALF IS CORRODED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 15,778 hrs · 12,926 cycles

CRACK FOUND ON BRACKET TO INTERCOSTAL 484 RBL 27.

Part: SILL — CORRODED (FUSELAGE) · airframe 15,778 hrs · 12,926 cycles

CORROSION FOUND ON LOWER SILL OF PAX DOOR FS 319 AND FS 335.

Part: PLACARD — MISSING (CABIN) · airframe 15,778 hrs · 12,926 cycles

CREW ESCAPE HATCH PLACARDS MISSING AND FADED. PAINTED CREW ESCAPE HATCH PLACARDS IAW SRM 51 25 00

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,778 hrs · 12,926 cycles

CRACK FOUND ON FLOOR SUPPORT FITTING FS 460 RBL 9 O/B. REMOVED AND REPLACED FLOOR SUPPORT FITTING IAW SRM 51-41-43. SUPPLEMENTAL - SDR CLOSED 07/05/07.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,778 hrs · 12,926 cycles

ANGLE CRACKED ON AFT PRESSURE BULKHEAD AT BAGGAGE DOOR BEAM FS 621.00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 15,778 hrs · 12,926 cycles

CRACK FOUND ON CLIP FS 280 LBL 9 AND RBL 9. NEW CLIP INSTALLED AS PER SRM 51-42-20. SUPPLEMENATAL- SDR CLOSED 07/03/07.

Part: ANGLE — CRACKED (T/E FLAP) · airframe 15,778 hrs · 12,926 cycles

RIGHT SIDE O/B FLAP HINGE ARM W/S 264 I/B SIDE ANGLE CRACKED. ANGLE FABRICATED IAW SRM 51-24-16. ALODINED, PRIMED AND PAINTED IAW SRM. ANGLE ON RIGHT O/B HINGE ARE REMOVED AND REPLACED IAW SRM 51-42-13. SUPPLEMENTAL - SDR CLOSED 07/05/07.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 15,634 hrs · 12,813 cycles

LEFT NR 2 EXTERNAL EMERGENCY LIGHT INOP.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 15,583 hrs · 12,770 cycles

LEFT 640 BONDED DOUBLER IS CRACKED.

Part: DRAIN — LEAKING (LT ENGINE) · airframe 15,491 hrs · 12,699 cycles

STRONG FUEL SMELL IN FLT DECK ON DESCENT AND AT GATE LT ENG WAS LEAKING FUEL FROM DRAIN. FLT 4532 CX.

Part: FLAP — MALFUNCTIONED (WING) · airframe 14,889 hrs · 12,262 cycles

FLAP FAIL AT 8 DEGREES ON APPROACH. EMERGENCY DECLARED. FLT 4093 CX.

Part: A/C PACK — CONTAMINATED · airframe 14,711 hrs · 12,134 cycles

STRONG ACRID ODOR THROUGHOUT AIRCRAFT WHEN PACK TEMP IS INCREASED, SUSPECT PACKS ARE CONTAMINATED. AIRCRAFT RETURNED TO ATL AFTER T/O.

Part: FRAME — CRACKED (BS 640) · airframe 14,422 hrs · 11,923 cycles

RIGHT SIDE 640 FRAME CRACKED.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 14,422 hrs · 11,923 cycles

REFER TO MCO 048003, PAX DOOR OUTER HANDLE CRACKED. PERFORM REINSPECTION EVERY ROUTINE CHECK.

Part: DOUBLER — CRACKED (BS 640) · airframe 14,422 hrs · 11,923 cycles

FOUND RIGHT FS 640 DOUBLER CRACKED.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 13,498 hrs · 11,214 cycles

PAX DOOR OUTER HANDLE CRACKED. C/W TEMP REPAIR PER REO:601R-52-11-1004 VALID FOR 1000 FLT HRS. VISUALLY INSPECT HANDLE FOR ADDITIONAL CRACK(S) AND DAMAGE PROPAGATION AND EVERY SUBSEQUENT ROUTINE CHECK. REMOVED AND REPLACED PAX DOOR OUTER DOOR HANDLE AS PER AMM 52-11-03. DEFER CLEARED. REFER TO AFDL 330652 NR 1 FOR HELICOIL AND INSTALLATION OF STOP NEEDED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,498 hrs · 11,214 cycles

FOUND CABIN EMERG EXIT SIGN AT 8C ARROW LIGHT INOP.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 12,924 hrs · 10,755 cycles

FOUND GALLEY SERVICE DOOR EMERG LIGHT HAS BULBS INOP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING A GROUND INSPECTION IN MGM, THE LEFT SIDE AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE AFT EMERGENCY LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT INBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FS 280 CLIP IAW CRJ200 SRM 51-42-00. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT OUTBOARD FS 280 CLIP WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT OUTBOARD FS 280 CLIP IAW CRJ 200 SRM 51-42-00. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT INBOARD FS 484 CLIP, AT RBL 27, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FS 484 CLIP, AT RBL 27, IAW ASA EO 600-53-0098. (M)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

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

Part: FRAME — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FS 718 FRAMES, BETWEEN STRINGER 10-12 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE LEFT AND RIGHT FS 718 FRAMES, BETWEEN STRINGER 10-12, IAW ASA EO 600-53-0066. (M)

Part: ANGLE — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT FS 640 FRAME ANGLE, INSIDE THE LEFT BOX BEAM ACCESS PANEL, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT FS 640 FRAME ANGLE, INSIDE THE LEFT BOX BEAM ACESS PANEL. (M)

Part: LAMP — BURNED OUT (GALLEY)

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

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DURING A GROUND INSPECTION SHV, THE FIRST OFFICERS FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFICERS FLASHLIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

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. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING HANGAR MAINTENANCE IN BTR, THE SECOND FROM THE FRONT EMERGENCY CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE SECOND FROM THE RONT EMERGENCY CEILING LIGHT. OPERATIONAL CHECKS GOOD. (M)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING AN A-CHECK IN BTR, THE DOUBLER AT FS 640, LBL 45 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE DOUBLER AT FS 640, LBL 45. (M)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

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

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. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

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

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. (M)

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS IN THE AFT EQUIPMENT BAY AT FS 625 BELOW THE ENGINE SUPPORT BEAM WERE OFUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS IN THE AFT EQUIPMENT BAY AT FS 625 BELOW THE ENGINE SUPPORT BEAM. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE SCREW HOLES ON THE CARGO COMPARTMENT FLOOR SILL PLATE AT FS 562.72-589 WERE FOUND TO BE CRACKED AND CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT FLOOR SILL PLATE AT FS 562.72-589. (M)

Part: CLIP — CRACKED (FUSELAGE)

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

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

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

Part: HANDLE — CRACKED (E/E BAY DOOR)

DURING A C-CHECK IN MCN, THE AVIONICS DOOR HANDLE CUP AROUND THE SUPPORT SHAFT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE AVIONICS DOOR HANDLE ASSEMBLY. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4755 - DURING A GROUND INSPECTION IN DFW, AN EMEREGNCY OVERWING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY OVERWING LIGHT LAMP. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE IN MCN, THE PASSENGER DOOR BOTTOM STEP PANEL WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER STEP ASSEMBLY. (M)

Part: DOUBLER — CRACKED (FUSELAGE FRAME)

DURING AN A-CHECK IN BTR, THE DOUBLER ON THE RIGHT FRAME FS 640 AT BL 45 BELOW STRINGER 9 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER ON THE RIGHT FRAME FS 640 AT BL 45 BELOW STRINGER 9 IAW SRM 51-00. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURNG AN A-CHECK IN BTR, THE NR 2 EMERGENCY EXIT CEILING LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY EXIT CEILING LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

DURING HANGAR MAINTENANCE IN BTR, THE EXTERIOR FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR FORWARD EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: MOTOR — BINDING (PAX DOOR)

FLT 4792 - DURING A GROUND INSPECTION IN ORD, THE PASSENGER DOOR WAS BINDING WHEN OPENED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR POWER ASSIST MOTOR, AND CLEANED DEBRIS FROM THE RETRACT MECHANISM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: PUMP — INOPERATIVE (HYD SYSTEM)

FLT 4785 - DURNG CRUISE, THE CREW RECEIVED A RIGHT HYDRAULIC HIGH TEMPERATURE CAUTION MESSAGE. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW SHUT DOWN THE RT ENGINE. AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT REQUESTED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE DRIVEN PUMP, RT HYDRAULIC MANIFOLD FILTER, RETURN FILTER, BOTH CASE DRAIN FILTERS, AND THE HYDRAULIC RESERVOIR FLUID. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — BURNED OUT (FUSELAGE)

FLT 4787 - DURING GROUND INSPECTION IN XNA, THE LEFT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EXTERNAL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — INOPERATIVE (CABIN)

DURING GROUND INSPECTION AT ATL, CRWE REPORTED OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BURNED OUT BULB IN THE CEILING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)