N970EV

Part: DOUBLER — CORRODED (SERVICE DOOR) · airframe 24,380 hrs · 22,329 cycles

FOUND LOWER SERVICE DOOR DOUBLER AT FS 349, RBL 42 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23/51-21-00/53-00-00 TR 53-27. COMPLIED WITH REO 601R-53-21-2344.

Part: BULKHEAD WEB — CRACKED (FUSELAGE) · airframe 24,380 hrs · 22,329 cycles

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

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,370 hrs · 22,317 cycles

FS 280 RBL 9 OTBD FLOORBEAM ANGLE CRACKED. REMOVED CRACKED OTBD FLOORBEAM AT FS 280 RBL 9 AND REPLACED WITH NEW PARTS IAW SRM 51-42-21, PN 601R31113-58.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 24,372 hrs · 22,319 cycles

LBL 27, OTBD FLOOR SUPPORT CORRODED AROUND NUTPLATE HOLES FS 574 - 621. CORROSION FOUND TO BE OUT OF LIMITS. FLOOR SUPPORT REPLACED IAW SRM 53-090-00.

Part: BRACKET — CRACKED (BS 319.7) · airframe 24,372 hrs · 22,319 cycles

SERVICE DOOR SILL PLATE BRACKET CORRODED AT FS 319.70. REMOVED CORRODED BRACKET AT FS 319.70 AND SERVICE DOOR SILL PLATE IAW SRM 51-42-21, 51-41-02. INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-40-11, LOCATING & 51-42-21.

Part: SEAT TRACK — CORRODED (BS 364-694) · airframe 24,380 hrs · 22,329 cycles

SEAT TRACK CORRODED AT FS 364 TO 394. FURTHER INVESTIGATION FOUND CORROSION TO BE BEYOND ALLOWABLE LIMITS OF SRM 53-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,380 hrs · 22,329 cycles

WHILE ACCESSING FOR FOUND FLOOR SUPPORT AT SERVICE DOOR CORRODED. COMPLIED WITH REO 601R-53-21-2346.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 24,380 hrs · 22,329 cycles

SEAT TRACK CORRODED AT FS 364 TO 394. FURTHER INVESTIGATION FOUND CORROSION TO BE BEYOND ALLOWABLE LIMITS OF SRM 53-21-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 24,370 hrs · 22,317 cycles

FS 280, LBL 9, INBD FLOORBEAM ANGLE CRACKED. REMOVED CRACKED INBD FLOORBEAM AT FS 280, LBL 9 AND REPLACED WITH NEW PARTS IAW SRM 51-42-21, PN 601R31113-57.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 24,370 hrs · 22,317 cycles

REAR PRESSURE BULKHEAD FWD FACE RT SIDE OTBD ISOLATOR 2ND UP FROM BOTTOM IS CRACKED. R & R CRACKED ISOLATOR IAW SRM 51-42-06. SDR CLOSED.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 24,370 hrs · 22,317 cycles

FLOOR SUPPORT AT FS 484 RBL 36 CRACKED. REMOVED DAMAGED FLOOR SUPPORT AT RBL 36 IAW SRM 51-42-06 AND SRM 51-42-21. FABRICATED ANGLE IAW NDTM 51-20-06. REPAIRED THE INTERCOSTAL, AT 484 BETWEEN BL 27.00 AND 36.00 IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 24,380 hrs · 22,329 cycles

FLOOR SUPPORT AT FS 319.70, RBL 42 IS CORRODED. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-11. INSTALLED FLOOR SUPPORT IAW SRM 51-42-21 AND 51-42-06 AT FS 319 RBL 42.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 24,380 hrs · 22,329 cycles

INTERCOSTAL AND FLOOR SUPPORT CORRODED AT FS 349.00, RBL 42. REMOVED CORRODED FLOOR SUPPORT BRACKET AT FS 349.00 & RBL 42 IAW SRM 51-42-21. LOCATED & DRILLED NEW SERVICEABLE BRACKET IAW SRM 51-40-11. REPAIRED IAW REO 601R-53-21-2346.

Part: FLOORBEAM — CORRODED (BS 409) · airframe 24,372 hrs · 22,319 cycles

RT FLOORBEAM CAP HAS AREAS OF CORROSION FORM FS 409 TO 409+64 RBL 9. FOUND RT FLOORBEAM CAP TO BE OUT OF LIMITS IAW REO 601R-53-00-005. R & R RBL 9.0 FLOORBEAM CAP FROM FS 409 - 409+128 IAW SRM 51-42-06 AND CH 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,372 hrs · 22,319 cycles

RT FLOOR SEAT TRACK CORRODED AT FS 409. CORROSION OUT OF LIMITS IAW SRM 53-31-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. FIT, DRILLED UP & COUNTERSUNK NEW SEAT TRACK SECTION IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,372 hrs · 22,319 cycles

LT FLOOR SEAT TRACK CORRODED AT FS 409. CORROSION OUT OF LIMITS IAW SRM 53-31-49. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. FIT, DRILLED UP & COUNTERSUNK NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: CHANNEL — CRACKED (BS 409) · airframe 24,370 hrs · 22,317 cycles

FS 409+128 WL 69.0 RBL 18 INBD CHANNEL INDICATION NOTED IN JOGGLED RADIUS APPROX .10" LT VERTICALLY 60 PERCENT FULL SCREEN HEIGHT. FAILED NDT. REMOVED INBD CHANNEL IAW SRM 51-42-22 & 51-42-06. LOCATE ALL HOLES ON CHANNEL IAW SRM 51-40-11. INSTALLED INBD & OTBD POST TOGETHER FOR RBL 18 FS 409+128 POST IAW SRM 51-42-06. INSTALLED CHANNEL IAW REO 601R-53-41-889.

Part: ANGLE — CRACKED (PAX DOOR HANDLE) · airframe 24,370 hrs · 22,317 cycles

PAX DOOR OUTER HANDLE AFT SUPPORT ANGLE IS CRACKED. ANGLE LOCATED ON INSIDE OF DOOR. R & R OUTER HANDLE AFT SUPPORT ANGLE IAW SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 24,370 hrs · 22,317 cycles

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

Part: FLOORBEAM — CORRODED (BS 409) · airframe 24,370 hrs · 22,317 cycles

LEFT FLOORBEAM CAP HAS AREAS OF CORROSION FROM FS 409.00 TO FS 409+96 LBL 9. REMOVED LIGHT SURFACE CORROSION .003" MAX MATERIAL REMOVED. FOUND TO BE WITHIN LIMITS IAW REO 601R-53-00-005. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW SOP 5702.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 24,370 hrs · 22,317 cycles

OBLIQUE ANGLES AT STRINGER 14L AND 14R CRACKED AT RADIUS AT 621.00 BULKHEAD WEB AFT FACE 621-625. REPLACED CRACKED OBLIQUE ANGLES AT STGR 14L AND STGR 14R AT RADIUS AT 621.00 BULKHEAD WEB AFT FACE 621-625 IAW SRM 51-42-21 PN 601-35012-52/601-35012-51. SDR CLOSED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,175 hrs · 22,100 cycles

LEFT NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LT NR 2 EXTERIOR EMERGENCY LIGHT ASSY IAW AMM 33-51-21.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 23,766 hrs · 21,665 cycles

PAX DOOR OUTER EMERGENCY LIGHT INOPERATIVE. REMOVED THE INOP BULB AND INSTALLED A NEW BULB IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: STEERING SYS — OUT OF ADJUST (NLG) · airframe 21,103 hrs · 18,693 cycles

AFTER T/O, MLG DISAGREE MESSAGE ILLUMINATED WITH LT & RT MLG SHOWING UP & WHITE, NLG INDICATING RED HASH MARKED BOX. ACFT RETURNED TO DEPARTURE. EMERGENCY DECLARED. C/W FUNCTIONAL TEST OF NOSE WHEEL STEERING SYS IAW AMM 32-51-00. REMOVED NLG SHOCK STRUT ASSY, INSTALLED NLG SHOCK STRUT ASSY. INSTALLED NLG LT TRUNNION PIN, & INSTALLED NLG RT TRUNNION PIN IAW AMM 32-21-01. INSTALLED NLG SWIVEL ASSY TO GREASE INSERT & ELECTRO HYD MODULE, RECONNECTED NLG BOTTOM DRAG BRACE TO NLG SHOCK STRUT, RECONNECTED NLG EXTENSION/RETRACTION ACTUATOR ON NLG SHOCK STRUT. ATTACHED DISCONNECTED NLG CONTROL ROD TO NLG SHOCK STRUT. CONNECTED NLG ELECTRICAL CONNECTOR P62, P4GC, P63 & ALL RELECTED ELECTRICAL CONNECTORS ALL IAW AMM 32-21-01 . LUBRICATE NLG IAW AMM 12-20-32-640-801. PRESSURIZED SHOCK STRUT WITH NITROGEN IAW AMM 12-12-32. BLEED HYD SYS NR 3 IAW AMM 29-10-00. C/W FUNCTIONAL TEST OF THE EXTENSION & RETRACTION SYS REQUIRE IAW AMM 32-30-00. C/W FUNCTIONAL TEST OF NOSEWHEEL STEERING SYS REQUIRE IAW AMM 32-51-00 / RII C/W IAW GMM 3-3 FOR INSTALLATION RIGGING. OPS CHECKS NLG SHOCK STRUT ASSY.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 21,088 hrs · 18,673 cycles

GEAR DISAGREE MSG AFTER TAKE OFF, NOSE GEAR WOULD NOT RETRACT. (ACFT RETURNED TO DEPARTURE AFTER T/O. R & R SELECTOR VALVE IAW AMM 32-22-20-04. OPS CHECK BAD, NO HELP. R & R NLG UPLOCK ASSY AND ADJUSTED NLG UPLOCK PIN BRACKET IAW AMM 32-33-05. OPS CHECK AND LEAK CHECK GOOD.

Part: TERMINAL — DAMAGED (CIRCUIT BREAKER) · airframe 20,730 hrs · 18,247 cycles

DURING TAXI NOTICED STRONG ELECTRICAL BURNING ODOR ON FLT DECK. CHANGING PACKS AND BLEED SOURCE HAD NO EFFECT. STRONGEST SMELL IN NR 2 CBP AREA AND RT GALLEY AREA BY SERVICE DOOR. (GATE RETURN) ( HYD AC MOTOR PUMPS (ACMP) (SYS 1 AND 2) ACMP 1B ) ( HYD AC MOTOR PUMPS (ACMP) (SYS 1 AND 2) ACMP 1B ) (ITEM RESOLVE UNDER MDDR: 558994-2) R & R BURNED C/B A1 HYD NR1 IAW ESPM, REPLACED TERMINAL TO C/B A6 HYD PUMP NR1 IAW ESPM, PERFORMED FUNCTION TEST OF HYD SYS NR1 AND NR2 IAW AMM 29-10-00-720-801.

Part: FLOORBEAM — CRACKED (BS 574) · airframe 20,688 hrs · 18,198 cycles

FOUND CRACK ON FLOORBEAM UPPER FLANGE LAST OTBD FASTENER HOLE AT FS 574.00 LBL 45. REPAIRED IAW REO 601R-53-61-3846.

Part: ANGLE — CRACKED (BS 605) · airframe 20,688 hrs · 18,198 cycles

LT ANGLE UNDER CARGO DOOR SILL AT FS 605.00, LBL 43, HAS CRACK IN RADIUS. REMOVED LT ANGLE AT FS 605.00 IAW SRM 51-42. LT ANGLE REQUIRES LOCATING, DRILLING OF HOLES AND INSTALL. ANGLE BRACKET, PN 601R35011-13 AT FS 605.0 LBL 43 LOCATED, DRILLED AND INSTALLED IAW SRM 51-40-01. (CLOSED)

Part: WEB — CRACKED (PAX DOOR) · airframe 20,688 hrs · 18,198 cycles

PAX DOOR FWD WEB HAS CRACK APPROX .4" FROM EDGE TO CTR OF RADIUS ON VERTICAL SURFACE, UNDER FIRST FIXED STEP APPROX 2.1" FROM INNER DOOR SKIN SURFACE. COMPLIED WITH STEPS 1 AND 2 OF REO 601R-52-11-1873. CUT OUT DAMAGED AREAS PAX DOOR FWD SIDE PANEL BOTTOM STEP. COMPLIED WITH REO 601R-52-11-1873 STEP 3. PERFORMED EDDY CURRENT OF PAX DOOR FWD SIDE PANEL CUTOUT AND PARTS IAW NDTM 51-20-06. NO INDICATIONS NOTED. PAINTED IAW SRM 57-25-00. INSTALLED NEW PLACARD IAW AMM 11-30-00-400-801.

Part: FLOORBEAM — CORRODED (BS 574-621) · airframe 20,688 hrs · 18,198 cycles

CARGO BAY FLOORBEAM CAP AT LBL 27 OTBD FROM FS 574 TO FS 621 HAS CORROSION AROUND NUTPLATES.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,688 hrs · 18,198 cycles

FS 280, AFT FLOOR SUPPORT ANGLE IS CRACKED OTBD OF RBL 9 AND LBL 9 & CORRODED ON TOP SIDE ALONG BULKHEAD AT RBL 9 AND LBL 9. FS 280 BULKHEAD WEB IS CRACKED BELOW FLOOR OTBD OF RBL 9 AND LBL 9. FS 280 FLOOR SUPPORT CLIPS ARE CRACKED INBD AND OTBD AT LBL 9 AND RBL 9. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926.

Part: WEB — CRACKED (PAX DOOR) · airframe 20,688 hrs · 18,198 cycles

PAX DOOR AFT WEB IS CRACKED AT FASTENER HOLE FOR DRAG ANGLE AND STIFFENER. REMOVED CRACKED AFT WEB FROOM PAX DOOR. REMOVED ASSOCIATED STIFFENERS AND ANGLES. FIT, DRILLED AND INSTALLED SAME SERVICEABLE STIFFENERS AND ANGLES ONTO NEW WEB IAW SRM 51-42-06 AND 51-42-10. INSTALLED NEW AFT WEB ONTO PAX IAW SRM 51-42-06 AND 51-42-13.

Part: FLOOR SUPPORT — CORRODED (BS 319) · airframe 20,688 hrs · 18,198 cycles

FS 319, WL 73 AT SERVICE DOOR FLOOR SUPPORT ANGLE CORRODED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06, SRM 51-42-10 AND SRM 51-42-21. INSTALLED A NEW SERVICEABLE CLIP IAW SRM 51-42-21, 51-42-06 & 51-42-13.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 20,688 hrs · 18,198 cycles

FS 484 FLOOR SUPPORT ANGLE OTBD RBL 27 CRACKED. REMOVED IAW SRM 51-42-21. NEW ANGLE 601R31171-9 FITTED AND DRILLED IAW SRM 51-40-11. NEW CLIP 601R31171-9 INSTALLED AND FLOOR SUPPORT ANGLE AT FS 484, RBL 27 REPAIRED IAW REO 601R-53-41-059. REPAIR TO THE INTERCOSTAL AT FS 484 BETWEEN RBL 27.00 AND RBL 36 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,688 hrs · 18,198 cycles

FS 280 OTBD OF LBL 9, WL 73 FLOOR SUPPORT J-ANGLE CRACKED AT ALTERNATE EXTENTION PULLEY BRACKET. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 20,688 hrs · 18,198 cycles

CARGO BAY FLOOR SEAT RAILS AT LBL 27 FS 559.00+80 TO 559.00+96, 559.00+104, 559.00+110, AND 567.00 ARE CORRODED. REMOVED AND INSTALLED SERVICEABLE SEAT RAILS IAW 51-41-02 SRM.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 20,688 hrs · 18,198 cycles

FS 484 FLOOR SUPPORT ANGLE INBD RBL 36 CRACKED. REPAIR TO THE FLOOR SUPPORT AT FS 484 BETWEEN RBL 27.00 AND RBL 36 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS.

Part: SEAT TRACK — CORRODED (BS 559-569) · airframe 20,688 hrs · 18,198 cycles

CARO BAY FLOOR SEAT RAILS AT RBL 9 FS 559.00+91 TO 559.00+96 AND FS 559.00+110 TO 569.00 ARE CORRODED. REMOVED SEAT RAILS IN CARGO COMPARTMENT. REF AMM 53-01-11-000-802 & INSTALLED NEW SERVICEABLE RAILS AT SAME LOCATIONS, REF AMM 53-01-11-400-802.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 20,688 hrs · 18,198 cycles

REAR PRESSURE BULKHEAD HAS 5 BROKEN ISOLATORS. REMOVED 5 BROKEN MOUNT ISOLATORS FROM 621 BULKHEAD BY DRILLING RIVETS FROM ISOLATORS AND MOUNT BRACKETS. INSTALLED FIVE NEW SERVICEABLE ISOLATOR MOUNTS BY INSTALLING ISOLATORS ON BRACKETS WITH RIVETS IAW SRM 51-42-13. (CLOSED)

Part: SEAT TRACK — CORRODED (BS 559) · airframe 20,688 hrs · 18,198 cycles

CARGO BAY FLOOR SEAT RAIL AT RBL 27 FS 559.00+80 TO FS 559.00+96 IS CORRODED. REMOVED SEAT TRACK IN CARGO BAY REF AMM 53-01-11-000-802 & INSTALLED NEW SERVICEABLE TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559-617) · airframe 20,688 hrs · 18,198 cycles

CARGO BAY FLOOR SEAT RAILS AT LBL 9 FS 559.00+91 TO 559.00+96, FS 559.00+110 TO 569.00, FS 583, FS 600.00, AND FS 612.00 TO 617.00 ARE CORRODED. R & R SEAT RAIL AT LBL 9 BETWEEN FS 559.00+110 & FS 569 IAW SRM CH 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 20,688 hrs · 18,198 cycles

CARGO BAY FLOORBEAM AT LBL 27 OTBD FROM FS 574.00 TO FS 621.00 HAS CORROSION AROUND NUTPLATES. INSTALLED FLOORBEAM CAP IAW REO 601R-53-61-3778 AND REO 601R-53-91-3778, REV NC DATED 8/21/2010 AS WRITTEN. INTALLED MYLAR, PLASTIC COVER, DINITROL AND PULLEY BRACKET ON FLOORBEAM CAP AT FS 574 TO FS 621, LBL 27 IAW SRM 51-41-02, 251-27-19, 51-21-11. CONTINUED ON MWC CO 7527310 JOB 8752731 OP 286.

Part: POST — CRACKED (BS 409) · airframe 20,688 hrs · 18,198 cycles

FOUND FS 409.0+128, RBL 18.0 OTBD VERTICAL POST HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS, FAILED NDT INSP. REMOVED BOTH POST INBD AND OTBD IAW SRM 51-42-06. DRILLED & LOCATED FASTENER HOLES IAW SRM 51-40-06. INSTALLED SERVICEABLE POST IAW SRM 51-42-06 & REO 601R-53-41-889. C/W EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REVISION A.

Part: POST — CRACKED (BS 409) · airframe 20,688 hrs · 18,198 cycles

FOUND FS 409.0+128, LBL 18.0 OTBD VERTICAL POST HAS INDICATION NOTED APPROX .3" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS, FAILED NDT INSPECTION. REMOVED INBD & OTBD POST. DRILLED UP NEW SERVICEABLE OTBD POST IAW SRM 51-40-06 & RIVETED INBD & NEW SERVICEABLE OTBD POST TOGETHER IAW SRM 51-42-06. INSTALLED POST ASSY IAW SRM 51-42-06, REO 601R-53-41-889. SEALED & PAINTED FASTENERS IAW SRM 51-23-00 & 51-25-16. C/W EC/TC REO 601R-53-41-889 & MET ALL REQUIRMENTS OF REO 601R-53-41-889, REV A.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 20,688 hrs · 18,198 cycles

CABIN FLOORBEAM STRUCTURE HAS CRACKS AT FS 280.0 RBL 9.0 INBD AND OTBD CLIPS. UPON FURTHER INVESTIGATION FOUND ADDITIONAL DAMAGE AT FS 280 BETWEEN RBL 9 AND LBL 9.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 20,688 hrs · 18,198 cycles

POSSIBLE CRACK ON AFT PAX DOOR DRAG ANGLE. REMOVED DAMAGED DRAG ANGLE AND INSTALLED A NEW DRAG ANGLE IAW SRM 51-42-06 AND 51-42-13.

Part: FLOORBEAM — CRACKED (FS 280 LBL9) · airframe 20,688 hrs · 18,198 cycles

CABIN FLOORBEAM STRUCTURE HAS A CRACK AT FS 280.0 LBL 9.0 INBD CLIP. UPON FURTHER INVESTIGATION FOUND ADDITIONAL DAMAGE AT FS 280 BETWEEN RBL 9 AND LBL 9.

Part: PLACARD — WORN (PAX DOOR) · airframe 20,688 hrs · 18,198 cycles

PAX DOOR ARROW DOWN AND EXIT PLACARDS WORN ON 5TH AND 3RD STEPS. R & R PAX DOOR ARROW AND EXIT PLACARDS IAW AMM 11-30-00-000-801 AND 11-30-00-400-801.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,170 hrs · 16,447 cycles

REFER TO DMIL 524331-1. NR3 INTERIOR CEILING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,170 hrs · 16,447 cycles

LT AND RT NR 1 EXTERIOR EMERGENCY LIGHTS INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,170 hrs · 16,447 cycles

NR3 INTERIOR CEILING EMERGENCY LIGHT INOP (CABIN EMERGENCY LIGHTS - CEILING LEVEL EMERGENCY FLOOD LIGHTS)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,839 hrs · 16,088 cycles

RIGHT EMERGENCY DOOR EXIT EXT. FWD EMERGENCY LIGHT IS INOP.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 18,804 hrs · 16,054 cycles

FWD PAX DOOR ANCHOR FITTING CRACKED

Part: KEYPAD — DEFECTIVE (FMS) · airframe 18,062 hrs · 15,325 cycles

FMS KEYPAD NOT WORKING CORRECTLY. WHEN PUSHING A LINE SELECT KEY IT OFTEN SELECTS THE LINE ABOVE OR BELOW THE DESIRED LINE. AUTO/ INHIBIT ON ITS OWN AT RANDOM TIMES.

Part: LENS — BROKEN (FLASHLIGHT) · airframe 17,729 hrs · 14,996 cycles

F/O EMERGENCY FLASHLIGHT HAS BROKEN LENS.

Part: SKIN — CRACKED (PAX DOOR)

JOB 8752721 OPERATION 299 PAX DOOR AFT SIDE SKIN IS CRACKED BETWEEN STEPS 3 AND 4. REPAIRED PAX DOOR AFT SIDE SKIN IAW BOMBARDIER REO 601R-52-11-702 AND REO 601R-52-11-1541 AND C/W ASA EC/TC NR REO 601R-52-11-702. DEVIATION TO GREO 601R-52-11-702 PER REO 601-52-11-1541 IS COMPLETED AND MEETS WITH THE REQUIREMENTS ASA EC/TC REO 601R-52-11-1541.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 16,634 hrs · 13,977 cycles

JOB 8752721 OPERATION 239. FLOORBEAM OTBD FLANGE AT FS 574 TO FS 621, LBL 27 HAS CORRODED NUTPLATE HOLES. REMOVED FILLER STRIP TO ACCESS BEAM CAP REMOVAL IAW CRJ 200 SRM 51-41-02. REMOVED HARDWARE. 7 BOLTS FROM LT ELEV PULLEY BRACKET JUST FWD OF FS 621 BULKHEAD TO ALLOW MOVEMENT OF PULLEY BRACKET. CABLES WERE NOT DETENSIONED. REMOVED FLOORBEAM CAP AT LBL 27 BETWEEN FS 621 AND 574 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. OK TO INSTALL LBL 27 FS 574-621.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR)

JOB 8752725 OPERATION 78 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 3" IN LENGTH. REMOVED CRACKED ANGLE. INSTALLED NEW ANGLE P/N 601R35050-109 IAW CRJ 700 SRM 51-42-21.

Part: STRIP — BROKEN (FLOORBEAM) · airframe 16,634 hrs · 13,977 cycles

JOB 8752721 OPERATION 251 LBL 27 FLOOR BEAM FILLER STRIP BETWEEN FS 574 TO FS 621 IS BROKEN IN SEVERAL PLACES. REMOVED BROKEN LBL 27 FLOOR BEAM FILLER STRIP BETWEEN FS 576 TO 621 AND INSTALLED NEW SERVICEABLE FILLER STRIP IAW CRJ 200 SRM 51-41-04.

Part: BULKHEAD — DAMAGED (FUSELAGE)

JOB 8752725 OPERATION 63 RH FS 559 BULKHEAD WEB HAS AN INDICATION NOTED AT O/B RBL 9, WL 58.7 3 IN LENGTH 50% FULL SCREEN HEIGHT FAILED NDT INSPECTION . REPAIRED FS 559 FROM LBL 18 TO LBL 9 AND RBL 18 TO RBL 9. ALSO CAP ANGLES ON LH/RH SIDE IAW REO 601R-53-41-260 AND GENERIC REO 601R-53-41-260. C DEVIATION. C/W EC/TC REO 601R-53-41-771 IAW BOMBARDIER REO 601R-53-41-771. C/W REO 601R-53-41-260 ASA EC/TC REO 601R-53-41-260. ASA RII C/W 5300043.

Part: ANGLE — CRACKED (FUSELAGE)

JOB 8752721 OPERATION 103 RT FS 625 OBLIQUE ANGLE CRACKED. DUPLICATE WRITE UP REF MWC 8752721 OP 253 FOR REPLACEMENT.

Part: LENS — CRACKED (CABIN)

JOB 8752721 OPERATION 162 FLOOR EMER FLOODLIGHT LOCATED ON WARDROBE UNIT HAS A CRACKED LENS AND BASE. REMOVED DAMAGED LENS AND BASE IAW CRJ 200 AMM 33-51-19-000-801. INSTALLED SERVICEABLE LENS AND BASE IAW CRJ 200 AMM 33-51-19-400-801. OPS TEST DUE OPS TEST EMERGENCY FLOOD LIGHT ON WARDROBE IAW CRJ 200 AMM 33-51-00-710-801.

Part: ANGLE — CRACKED (FUSELAGE)

JOB 8752721 OPERATION 104 LT FS 625 OBLIQUE ANGLE CRACKED. DUPLICATE WRITE YP REF MWC 8752721 OP 253 FOR REPLACEMENT.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 1,621,108 hrs · 13,605 cycles

ELECTROLUMINESCENT "EXIT" SIGN BY SEAT 8A WILL NOT ILLUMINATE. RE-SECURED CONNECTOR, OPS CHECK GOOD PER CRJ200 AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,944 hrs · 12,526 cycles

EMERGENCY FLOOR TRACK LIGHTING FROM 1CD-5CD INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,890 hrs · 12,476 cycles

MIDDLE AFT CEILING EMERGENCY LIGHT INOP.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 14,038 hrs · 11,784 cycles

MAIN GEAR DISAGREE ON APPROACH. EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY.

Part: STRIP — MISSING (CABIN) · airframe 13,992 hrs · 11,739 cycles

AFT EMERGENCY LIGHTING FLOOR STRIP MISSING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,933 hrs · 11,697 cycles

LEFT WING EMERGENCY LIGHT INOP.

Part: ANCHOR FITTING — CRACKED (AIRSTAIR) · airframe 13,891 hrs · 11,660 cycles

ASD FWD ANCHOR FITTING CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,176 hrs · 11,095 cycles

EMERGENCY FLOOR TRACK LIGHTING FROM 8CD TO 12CD INOP.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,856 hrs · 10,861 cycles

AFTER TAKEOFF SWITCHED BLEEDS TO ENGINES AND GOT RT PACK HI PRESS WITH BURNT SMELL IN A/C. FOLLOWED QRH TO RESET BUT DID NOT, ALREADY SINGLE PACK. FINALLY GOT TO RESET AFTER STARTING APU AND SWITCHING BLEEDS. AIRCRAFT RETURNED TO ATL AFTER T/O. FLTS 4856, 4866 CX.

Part: SIGN — DISLODGED (CABIN) · airframe 12,352 hrs · 10,480 cycles

FOUND EXIT SIGN ON AIR STAIR DOOR IS FALLING OFF.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 11,990 hrs · 10,217 cycles

RIGHT INBOARD 484 CLIP CRACKED.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 11,990 hrs · 10,217 cycles

LEFT OUTBOARD 484 CLIP CRACKED.

Part: SKIN — CRACKED (BS 640) · airframe 11,990 hrs · 10,217 cycles

LT INNER SKIN DOUBLER CRACKED AT FS 640 BETWEEN STR 9 AND STR 12 REF BOMBARDIER SB 601R-53-061 (CRACKED AS MARKED). RESOLVED ON W/O: 34785 TASKCARD: N/R-00271. COMPLIED WITH EC/TC REO 601R-53-61-506. THIS REPAIR IS ACCEPTABLE WITH NO FURTHER ACTION REQUIRED. REF REO 601R-53-61-506 REV C AND SDIR 601R-53-61-506RII IS SATISFACTORY.

Part: HANDLE — STICKING (ESCAPE HATCH) · airframe 11,990 hrs · 10,217 cycles

CREW ESCAPE HATCH EXTERIOR HANDLE IS STICKING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 11,990 hrs · 10,217 cycles

FRAME 349 CORRODED ON R/H SIDE. AFT OF SERVICE DOOR. REMOVED 2 SERVICE DOOR SILL PLATE BRACKETS, 2 LOWER SERVICE DOOR LOCK BRACKETS, 1 SERVICE DOOR ANGLE AND STARTED REMOVING FIBERGLAS DOUBLER AND AFT ANGLE ON FRAME 349 R/H SIDE AFT OF SERVICE DOOR TO GAIN ACCESS FOR CORRSION REMOVAL PER SRM 51-42-00 SG7020421. FINISHED REMOVING FIBERGLAS DOUBLER AND AFT ANGLE ON FRAME 349 R/H SIDE AFT OF SERVICE DOOR TO GAIN ACCESS FOR CORRSION REMOVAL PER SRM 51-42-06. REMOVED LIGHT SURFACE CORROSION PER SRM 51-21-06, CORROSION IS WITHIN ALLOWABLE DAMAGE LIMITS PER SRM 53-00-00 SG7020421. ALODINED, PRIMED AND PAINTED BLENDED AREA AND REINSTALLED REMOVED STRUCTURE PER SRM 51-42-00 SG7020421. INSTALLED 2 SERVICE DOOR SILL

Part: BEAM — CRACKED · airframe 11,990 hrs · 10,217 cycles

SUSPECT CENTER BOXBEAM CRACKED BELOW UPPER FIRELOOP CLIP. JOB COMPLETE RII COMPLETED IWA E0 600-53-0072BSATIFACTORY REPAIR OF ENGINE BOX BEAM, UPPER AND LOWER ANGLES 8/31/2006// MB14369 EC EO 600-53-72 0001 COMPLIED WITH. PER REO 601R-53-61-345. (SUPPLEMENTAL-SDR CLOSED 9/7/06)

Part: FITTING — CRACKED (FUSELAGE) · airframe 11,990 hrs · 10,217 cycles

FOUND FS 280 RBL9 INBD AND OUTBD CLIPS CRACKED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 11,990 hrs · 10,217 cycles

FOUND FS 280 FWD SUPPORT ANGLE CORRODED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 11,990 hrs · 10,217 cycles

FOUND FS 280 LBL9 INBD AND OUTBD CLIPS CRACKED.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 11,990 hrs · 10,217 cycles

SUSPECT RT 718 DOUBLER TO BE CRACKED (MARKED).

Part: FRAME — CRACKED (BS 640) · airframe 11,990 hrs · 10,217 cycles

POSSIBLE CRACK ON THE LT 640 FRAME BETWEEN 9 AND 12 STR. PERFORMED EDDY CURRENT INSPECTION OF REPAIR DOUBLER AT F.S. 640.00 FRAME, LEFT SIDE, BETWEEN STR. 9 AND STR. 12 I/A/W CRJ 200 NDTM 51-20-06. REPAIR DOUBLER IS CRACKED. REMOVED 640 DOUBLER. STARTED REMOVING RIVETS IN 640 FRAME THROUGH THE SKIN IAW S.B.601R-53-061. REMOVED FASTNER IN FRAME TO GAIN ACCESS,AND CUT FLANGE IAW PLK601R36009. LOCATED EXISTING HOLES IN -37 REINFORCEMENT FLANGE AND -39 DOUBLER IAW S.B. 601R-53-061. LOCATED AND DRILLED ADDED FASTENER HOLES IN -37 REINFORCING FLANGE, ALL WORK PER SB 601R-53-061 AJ 21906. PERFORMED EDDY CURRENT INSPECTION OF CUT LINE AFTER STEP 3 FLANGE CUT PER SB 601R-53-061 IAW CRJ 2OO NDTM PART 1. 51-20-06.

Part: BEAM — CRACKED (FUSELAGE) · airframe 11,990 hrs · 10,217 cycles

FOUND BOX BEAM CRACKED ON THE RT SIDE. FINISHED REMOVEING FASTNERS FROM FRAME AND CUT OUT DAMAGED AREA OF FRAME . ALL WORK DONE IAW WITH PLK601R36009 DK 7022603. REQUEST NDT OF CUT LINE ON RT 640 FRAME. (CLOSED)

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 11,637 hrs · 9,935 cycles

EMERGENCY EXIT LIGHT AT AFT SERVICE DOOR (ON LOWER WARDROBE) WIRES ARE BROKEN.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 11,637 hrs · 9,935 cycles

EMERGENCY EXIT SIGN ON LT WINDSCREEN WIRES ARE BROKEN.

Part: HANDLE — CRACKED (SERVICE DOOR) · airframe 11,637 hrs · 9,935 cycles

AFT SERVICE DOOR EXTERNAL HANDLE CRACKED.

Part: ODOR — DETECTED (CABIN) · airframe 11,600 hrs · 9,902 cycles

STRONG ELECTRICAL SMELL FOR 30 SEC DURING DESCENT.

Part: TIRE — BLOWN (NLG) · airframe 11,547 hrs · 9,858 cycles

RT NOSE TIRE BLEW OUT DURING T/O ROLL. (AN EMERGENCY WAS DECLARED)

Part: LAMP — BURNED OUT (FUSELAGE)

DURING A GROUND INSPECTION, THE RT SIDE, NR 3, EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT SIDE, NR 3, EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT SIDE, NR 3, EXTERNAL EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED OUT (CABIN)

DURING A GROUND INSPECTION, THE CEILING EMERGENCY LIGHT, AT ROW 14 AB, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE CEILING EMERGENCY LIGHT ASSY, AT ROW 14 AB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: PLACARD — WORN (PAX DOOR)

DURING A HANGAR INSPECTION IN MCN, THE PASSENGER DOOR EXIT PLACARD WAS FOUND TO NEEDING REPLACEMENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT PLACARD. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)