N884AS

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 32,129 hrs · 29,459 cycles

NR 4 EXIT, EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: GENERATOR — SHUTDOWN · airframe 31,098 hrs · 28,455 cycles

ADG DEPLOYED IN FLIGHT DUE TO INADVERTENTLY SHUTTING DOWN OF GEN 1 AND GEN 2 EMERGENCY DECLARED. ACFT RETURNED TO DEPARTURE AFTER T/O. RETRACTED ADG IAW AMM 24-23-01 AND PERFORM IDLE ENGINE RUNS IAW AMM 71-00-00 WITH IDG'S AND APU GENERATOR ONLINE. NO ABNORMALITY FOUND. REFER TO AFDL A598998 FOR LIQUID PENETRANT INSPECTION OF ADG. PREFORMED VISUAL INSPECTION OF THE IAW AMM 05-51-19. NO DAMAGE FOUND.

Part: SPAR — DAMAGED (HORIZONTAL STAB) · airframe 30,764 hrs · 28,181 cycles

AFT SPAR ON RT HORIZONTAL STAB TIP FOUND TO BE DAMAGED DUE TO LIGHTNING STRIKE. CUT AWAY BURNED SECTION OF AFT SPAR AND CLEANED UP ALL SHARP EDGES ON MISDRILLED HOLE ON AFT SPAR TO THE RT OF BURN, WORK DONE REF EA EJ-CRJ255-00032. COMPLIED WITH EDDY CURRENT INSPECTION OF CUTLINE AND MISDRILLED HOLE ON AFT SPAR OF RT HORIZONTAL STABILIZER IAW NDTM 51-20-06 AND EA EJ-CRJ255-00032. NO DEFECTS NOTED AT THIS TIME. STARTED FABRICATING NEW REPAIR PARTS, FABRICATED CUTOUT FILLER FROM 7075 T-6 .040" BATCH 1902286, FABRICATED OTHER FILLER FROM 2024 T-3 .032" BATCH 1517651, FABRICATED REPAIR STRAP FROM 2024 T-3 .050" BATCH 1894010 AND PICKED UP ALL EXISTING FASTENER HOLES IN REPAIR STRAP. WORK DONE REF EA EJ-CRJ255-00032. CUT AWAY ADDITIONAL SECTION OF DAMAGED AREA ON AFT SPAR TO ACCOMMODATE NUTPLATE INSTALLATION IAW EA EJ CRJ255-00032. CUT OUT MEASURES .090". DRILLED AND COUNTERSINKED REMAINING HOLES IN NEW SPLICE AND NEWLY FABRICATED CUTOUT FILLER, 7075 T6 .040" BATCH 1902286, AND PRIMED ALL REPAIR PARTS IAW EA EJ-CRJ255-00032. INSTALLED ALL REPAIR PARTS ON RT HORIZONTAL STAB TIP IAW EA EJ-CRJ255-00032. THIS IS CLASSIFIED AS A MAJOR REPAIR.

Part: ANGLE — CORRODED (BS 280) · airframe 30,363 hrs · 27,768 cycles

FS 280 J-ANGLE CORRODED. REMOVED CORRODED J-ANGLE AT FS 280 PT 600-34017-351 IAW SRM 51-42-06. LOCATED, DRILLED & INSTALLED NEW FS 280, J-ANGLE PT 600-34017-351S IAW SRM 51-42-06 & 51-40-11.

Part: FRAME — CRACKED (605) · airframe 30,363 hrs · 27,768 cycles

FS 605, FRAME AND PREVIOUS USED DOUBLER STRAP CRACKED AT UPPER HOLE LOCATION WHERE STANDOFF SB INSTALLED AFTER INSTALLATION AT RT STR 26 AND RT STR 27. LOCATED AND DRILLED NEW SERVICEABLE FS 605, FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FS 605 FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-06 & 51-42-21 AND TR 51-32.

Part: FLOORBEAM — CORRODED (BS 561) · airframe 30,363 hrs · 27,768 cycles

CORROSION FOUND AT NUTPLATE LOCATION AT LT FS 561.00, STR 17, BUTT LINE 36 TO 47. COMPLIED WITH EC/TC REO:601R-53-41-666 AND REO:601R-53-41-666, REV C.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 30,362 hrs · 27,767 cycles

INTERCOSTAL FS 621-625, STR 14L, ADJACENT TO SKIN, OTBD FLANGE IS CRACKED. REMOVED CRACKED INTERCOSTAL, PN:601R2350121-5 FROM INTERCOSTAL. IN STEP 3 IAW SRM 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL, PN:601R350121-5 IAW SRM 51-40-11. INSTALLED IT ON INTERCOSTAL NOTED IN STEP 3 IAW SRM 51-42-21.

Part: ANGLE — CRACKED (BS 622-625) · airframe 30,363 hrs · 27,768 cycles

OBLIQUE ANGLE CRACKED AT FS 622- FS 625, STR 14L ABOUT LBL 40. REMOVED OBLIQUE ANGLE IAW SRM 51-42-20. LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL ANGLE AT FS 622-FS 625, STR 14L, LBL 40 IAW SRM 51-42-20, SRM 51-40-11 AND SRM 51-42-06.

Part: SKIN — CRACKED (RT WING) · airframe 30,363 hrs · 27,768 cycles

RIGHT WING PLANK ACCESS HOLE CUTOUT FOR PANEL 650CB HAS INDICATIONS AROUND CIRCUMFERENCE OF LANDING 55 PERCENT FSH, AREA MARKED ON ACFT, FAILED NDT. REMOVED RT WING FUEL ACCESS FUEL PANEL 650CB IAW AMM TASK 28-11-01-000-802. INSTALLED RT FUEL PANEL 650CB IAW AMM TASK 28-11-01-400-802. C/W EC/TC EO 600-57-81 C/W IAW REO:601R-57-21-030 REV L.

Part: SKIN — CORRODED (WING) · airframe 30,362 hrs · 27,767 cycles

CORROSION ON LOWER WING PLANK HOLE, 510AB IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO PEEN OF THE REPAIR SURFACE IAW SRM 51-24-11. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.

Part: POST — CRACKED (BS 409) · airframe 30,362 hrs · 27,766 cycles

FS 409+128, RBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADII AT WL 69 .250", LONG BY 60 FSH. FAILED NDT. REMOVED INBD POST, PN:601R32208-32 AND OTBD POST, PN:601R32208-156 AT FS 409+128, RBL 18 IAW SRM 51-42-06. ASSEMBLED 2 STIFFENER 601R32208-156 AND 60132208-32 AND INSTALLED THE POST TO RBL 18, FS 409+128 IAW SRM 51-42-06 AND 51-42-14. LOCATED AND DRILLED HOLES ON 2 NEW STIFFENER 601R32208-32 AND 601R32208-156, RBL 8 INBD AND OTBD POST IAW SRM 51-40-11. INSTALLED INBD AND OTBD POST ON OP 70, STEP 5 ALSO COMPLIED WITH REO:601R-53-41-889. COMPLIED WITH EC/TC REO:601R-53-41-889 AND MET ALL REQUIREMENTS OF REO:601R-53-41-889, REV A. FABRICATED NEW STIFFENER.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 18.00 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 3.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW STEP 1, 2 & 3 OF REO 601R-53-61-5498, P1 AT FS 621, RBL 18. C/W REO 601R-53-61-5498, P1 AT FS 621, RBL 18. INSTALLED ALL REPAIR PARTS AT FS 621 BULKHEAD RBL 18 IAW REO 601R-53-61-5498 P1.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 27.50 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 2.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF THE REAR PRESSURE BULKHEAD WEB AT RBL 27.50 IAW REO 601R-53-61-5498 P1. C/W REO 601R-53-61-54-98, PT 1 AT FS 621.0, RBL 27/50. INSTALLED ALL REPAIR PARTS AT FS 621 BULKHEAD RBL 27.5 IAW REO 601R-53-61-5498 P1.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 27.50 BETWEEN WL 121.43-WL 137.5 APPROXIMATELY 6.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF THE REAR PRESSURE BULKHEAD WEB AT RBL 27.50 IAW REO 601R-53-61-5498 P1. RECEIVED FINAL REO 601R-53-61-5498 AND VERIFIED THAT ALL STEPS OF REO HAVE BEEN C/W FOR REPAIR TO FS 621 BULKHEAD AT RBL 27.50. REO: 601R-53-61-5498 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18.00 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE AT LBL 18.0, FS 621 BULKHEAD IAW STEP 1, 2 & 3 OF REO 601R-53-61-5498 (01). FABRICATON AND INSTALLATON OF ALL REPAIR PARTS AT FS 621, LBL 18 IAW REO 601R-53-61-5498. RECEIVED FINAL REO 601R-53-61-5498 AND VERIFIED THAT ALL STEPS OF REO HAVE BEEN C/W FOR REPAIR OF FS 621 BULKHEAD AT LBL 18. REO:601R-53-61-5498 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: SKIN — CORRODED (WING) · airframe 30,362 hrs · 27,767 cycles

CORROSION ON LOWER WING PLANK HOLE, 540BB IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO PEENING REWORKED AREA IAW SRM 51-24-11. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 9.5 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.5" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW SEP 1, 2 & 3 OF REO 601R-53-61-5498 P1 AT FS 621, RBL 9.5. C/W REO 601R-53-61-5498 P1 AT FS 621, RBL 9.5. INSTALLED ALL REPAIR PARTS AT FS 621 BULKHEAD, RBL 9.5 IAW REO REO 601R-53-61-5498 P1.

Part: SPLICE PLATE — CORRODED (BS 621 BULKHEAD) · airframe 30,362 hrs · 27,767 cycles

SPLICE PLATE AT FS 621 RH RBL 41 IS CORRODED. BLENDED CORROSION ON SPLICE PLATE AT FS 621, RBL 41 IAW REO 601R-53-61-4690. MAXIMUM MATERIAL REMOVED .009. REPAIRED FLOOR ANGLE AT FS 621.00 IAW REO 601R-53-61-4690.

Part: BULKHEAD WEB — CRACKED · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 36.20 JUST ABOVE WL 73.50 APPROXIMATELY 1.5 IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. C/W REO 601R-53-61-5498 P1. INSTALLED ALL REPAIR PARTS AT FS 621, BULKHEAD LBL 36 IAW REO 601R-53-61-5498. C/W REO 601R-53-61-5498 P1.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50, WL 130 APPROX 2.0" IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. UPON MILLING OF CARGO DOOR TRACK IAW REO 601R-53-61-5498. REMOVED EXCESS MATERIAL CARGO DOOR TRACK REQUIRES REPLACEMENT. REO 601R-53-61-5498, REV P1 DATED 06/06/15. MILLED NEW CARGO DOOR TRACK, PN 601R350665 AND REINSTALLED CARGO DOOR AFT TRACK IAW SRM 51-21-16 AND REO 601R-53-61-5498. REMOVED DAMAGE IAW REO 601R-53-61-5498, REV P1.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 9.0" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED PORTION OF THE REAR PRESSURE BULKHAD WEB AT BL 0 IAW REO 601R-53-61-5498. REO 601R-53-61-5498 P1 AT BL 0 FS 621. C/W REO 601R-53-61-5498 P1.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 9.50 BETWEEN WL 73.50-WL 120.43 APPROX 4.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGE PORTION OF THE REAR PRESSURE BULKHEAD WEB AT LBL 9.50 IAW REO 601R-53-61-5498. C/W REO:601R-53-61-5498(P1) AT FS 521, LBL 9.5. INSTALLED ALL REPAIR PARTS AT FS 621 BULKHEAD LBL 9.5 IAW STEPS 1--22 AND STEPS 24-32 OF REO 601R-53-61-5498.

Part: ATTACH BRACKET — CRACKED (BS 280) · airframe 30,362 hrs · 27,766 cycles

BRACKET ATTACHING FROM STR 3L TO FS 280 IS CRACKED. REMOVED CLEAT IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLEAT IAW SRM 51-40-11 AND 51-42-06 AND TR 51-32.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 24" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW STEPS 1-3 OF REO 601R-53-61-5498, REV P1. C/W REO 601R-53-61-5498 P1. INSTALLED ALL REPAIR PARTS AT FS 621 BULKHEAD, LBL 27.50 IAW REO 601R-53-61-5498 P1.

Part: SKIN — CORRODED (WING) · airframe 30,362 hrs · 27,766 cycles

CORROSION ON LOWER WING PLANK HOLE, 640BB, IN SEVERAL LOCATIONS. COMPLIED WITH REO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV L, ROTO-PEENING OF REWORK AREAS IAW SRM 51-24-11.

Part: SKIN — CORRODED (WING) · airframe 30,362 hrs · 27,766 cycles

CORRROSION ON LOWER WING PLANK HOLE, 610AB IN SEVERAL AREAS. COMPLIED WITH REO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV L-ROTO PEEN OF REWORKED SURFACES IAW SRM 51-24-11. C/W REO 601R-57-21-030. LEAK CHECK GOOD. C/W ECTC EO 600-57-81, C/W IAW REO 601R-57-21-030, REV L.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL 18.00 BETWEEN WL 121.93-WL 137.5 APPROXIMATELY 2.5" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE IAW STEP 1, 2 & 3 OF REO 601R-53-61-5498 P1 AT FS 621, RBL 18. COMPLETED REO 601R-53-61-5498 FABRICATION AND INSTALLATION OF ALL REPAIR PARTS AT FS 621, RBL 18. RECEIVED FINAL REO 601R-53-61-5498 AND VERIFIED THAT ALL STEPS OF REO HAVE BEEN C/W FOR REPAIR TO FS 621, BULKHEAD AT RBL 18.

Part: POST — CRACKED (BS 409) · airframe 30,348 hrs · 27,751 cycles

FS 409+128, LBL 18 VERT POST INBD AND OTBD SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADII AT WL 69 APPROXIMATELY .250" LONG BY 50 PERCENT FSH. BOTH INDICATIONS FAILED NDT. NO OTHER INDICATIONS NOTED. REPAIRED IAW EC/TC, REO:601R-53-41-889.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18.00 BETWEEN WL 73.50, WL 120.43 APPROXIMATELY 12" IN LENGTH, 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE AT LBL 18.0, FS 621 BULKHEAD IAW REO 601R-53-61-5498 P1. INSTALLED ALL REPAIR PARTS AT FS 621, BULKHEAD LBL 18 IAW REO 601R-53-61-5498.

Part: POST — CRACKED (BS 409) · airframe 30,348 hrs · 27,751 cycles

FS 409+128, BL 0 VERT POST LT SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 .250", LONG Y 50 PERCENT FSH, FAILED NDT. REPAIRED IAW ECTC REO 601R-53-41-889.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 30,355 hrs · 27,759 cycles

STR 3L ATTACHING ANGLES ARE CRACKED JUST AFT OF FS 280. REMOVED ANGLE, PN 600-31057-19 FROM STR 3L AT FS 280 IAW SRM 51-42-06. DRILLED, LOCATED AND INSTALLED NEW ANGLE, PN 600-31057-19 ON STR 3L AT FS 280.0 IAW SRM 51-40-11 AND 51-42-06 AND TR 51-32. REMOVED ANGLE, PN 600-31057-20 FROM STR 3L AT FS 280 IAW SRM 51-42-06. DRILLED, LOCATED AND INSTALLED NEW ANGLE, SPLICE, FUSELAGE PN 600-31057-20 IAW SRM 51-40-11 AND 51-42-06 AND TR 51-32.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 30,362 hrs · 27,767 cycles

INTERCOSTAL AT BS 349-364, STRINGER 26L IS CORRODED. BLENDED CORROSION FROM INTERCOSTAL 26L AT FS 349-364 MAXIMUM MATERIAL REMOVED .002 IAW SRM 51-21-06, 53-00-00, FIG 102.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,362 hrs · 27,766 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 BETWEEN WL 73.50-WL 120.43 APPROXIMATELY 2.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. CUT AWAY DAMAGED POSITION OF THE REAR PRESSURE BULKHEAD WEB AT BL 0 IAW REO 601R-53-61-5498. RECEIVED FINAL REO 601R-53-61-5498 AND VERIFIED THAT ALL STEPS OF REO HAVE BEEN C/W FOR REPAIR TO FS 621 BULKHEAD AT BL 0. REO:601R-53-61-5498 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 30,348 hrs · 27,751 cycles

CORROSION AT VARIOUS LOCATIONS ON RT FLOOR SILL FROM FS 559.00+80-FS 621.00. REPAIRED IAW: EC/TC REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REV.

Part: CROSSBEAM — CORRODED (BS 598) · airframe 30,355 hrs · 27,759 cycles

CORROSION ON CROSSBEAM AT FS 589.00 BETWEEN RBL 9 & LBL 9. BLENDED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. .021" MATERIAL REMOVED. REPLACEMENT REQUIRED. REMOVED DAMAGED CAP STRIP IAW SRM 51-42-06-00. FABRICATED, LOCATED AND DRILLED NEW SERVICEABLE CAP STRIP PN 601R35031-50701 IAW EO 601R35031, SNEIO S07. FABRICATED CAP STRIP 601R35031-50701 IAW SNIEO 601R35031 S07. INSTALLED NEW FABBED STRIP IAW SRM 51-42-06 AND 51-42-15.

Part: ISOLATOR — CRACKED (BS 621) · airframe 30,355 hrs · 27,759 cycles

CRACKED ISOLATOR ON FS 621 BULKHEAD. R & R THE ISOLATOR IAW SRM CH 51-42-00.

Part: FRAME — CORRODED (BS 605) · airframe 30,355 hrs · 27,759 cycles

CORROSION ON 605 FRAME FROM STR 27 TO STR 24L. FOUND CORROSION ON FS 605, FRAME TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED FS 605, FRAME IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE FS 605, FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-06 & 51-42-21 AND TR 51-32. REMOVED UPPER REINFORCEMENT DOUBLER STRAP ON FRAME 605 IAW SRM 51-42-06. DRILLED DOUBLER STRAP TO NEW 605 FRAME IAW SRM 51-42-06. INSTALLED RIVETS IN DOUBLER STRAP TO 605 FS FRAME IAW SRM 51-42-06. DURING INSTALLATION OF FS 605 FRAME SECTOR FOUND THE FRAME & REINFORCEMENT ANGLE TO BE CRACKED. LOCATED AND DRILLED NEW SERVICEABLE FS 605 FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-40-11. REMOVED FS 605, FRAME IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE FS 605, FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-06 & 51-42-21 AND TR 51-32.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 30,355 hrs · 27,759 cycles

LOWER WING PLANK CUTOUT FOR RT BOOST PUMP, LANDING FOR PANEL 610CB, HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT. COMPLIED WITH EA 32-2015-234. EA 32-2015-234 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NRI WORK CARD.

Part: FRAME — CORRODED (BS 319) · airframe 30,348 hrs · 27,751 cycles

FS 319, FRAME HAS FILIFORM CORROSION FORMING ON FWD SIDE AT STR 27. REPAIRED IAW SRM 51-42-06, SRM 51-21-06, SRM 53-00-00, SRM 51-21-11, SRM 51-25-16, AND SRM 51-25-01.

Part: STRINGER — CORRODED (BS 333-349) · airframe 30,355 hrs · 27,759 cycles

STRINGER 26R HAS CORROSION FROM BS 333 - 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, 51-42-21, AND SRM TR 53-5.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,355 hrs · 27,759 cycles

FLOORBEAM TO BS 280 ATTACH ANGLE AT LBL 9 AND RBL 9 CRACKED. REMOVED AND REPLACED IAW SRM 51-42-21-00, SRM 51-42-21.

Part: STRUCTURE — CORRODED (BS 461-499) · airframe 30,355 hrs · 27,759 cycles

CORROSION FOUND AT NUTPLATE LOCATIONS AT RT FS 499.00 AND LT FS 461.00, STR 17. UPON FURTHER INVESTIGATION, FOUND CORROSION DAMAGE AT RT FS 499, STR 17 IS BEYOND LIMITS OF REO 601R-53-41-666. BLENDED PRESSURE FLOOR SILL AT FS 499, RT BL 45, MATERIAL REMOVED .031. AFTER ULTRASOUND INSPECTION, MATERIAL REMOVED FOUND TO BE MAX .005, WITH IN REO 601R-53-41-666. PERFORMED ULTRASOUND INSPECTION OF FS 499 PRESSURE FLOOR REWORKED AREAS, RT SIDE IAW NDTM PN 4 51-00-001. RECORDED RESULTS ON ACFT STRUCTURE FOR ENGINEERING. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C.

Part: FRAME — CORRODED (BS 310) · airframe 30,348 hrs · 27,751 cycles

FS 310, FRAME HAS FILIFORM CORROSION FORMING ON AFT SIDE BETWEEN STR 27 AND STR 26R. REPAIRED IAW SRM 51-42-06, SRM 51-21-06, SRM 53-00-00, SRM 51-21-11, SRM 51-25-16, AND SRM 51-25-01.

Part: ANCHOR FITTING — CORRODED (CARGO BAY) · airframe 30,348 hrs · 27,751 cycles

AFT CARGO BAY, 3 EA CARGO NET ANCHOR PLATES CORRODED. REPLACED 3 EA CARGO NET ANCHOR PLATES IAW SRM 51-41-02.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 30,348 hrs · 27,751 cycles

GALLEY EMERGENCY LIGHT WIRE IS BROKEN AT SPLICE, MARKED WITH RED TAPE. INSTALLED NEW SPLICE ON GALLEY WATER LINE HEATERS IAW GSPM 20-16-00. CONTINUITY CHECK GOOD. NO DEFECTS NOTED.

Part: SKIN — CORRODED (BS 559) · airframe 30,353 hrs · 27,758 cycles

FUSELAGE SKIN AT BS 559+112 HAS MINOR CORROSION AROUND FASTENER HEADS BETWEEN STRINGERS 25L AND 26R. COMPLIED WITH EA 32-2015-229. REMOVED CORROSION IAW SRM 51-21-06 AND SRM 53-00-00. NO DAMAGE ALLOWED IN BLEND ZONE.

Part: FRAME — CORRODED (BS 349) · airframe 30,353 hrs · 27,758 cycles

FS 349, FRAME HAS FILIFORM CORROSION ON AFT SIDE BETWEEN STR 26L AND 25R. REPAIRED IAW SRM 51-40-11-00, PN 601R32005-71.

Part: FRAME — CORRODED (BS 364) · airframe 30,353 hrs · 27,758 cycles

FS 364, FRAME HAS CORROSION ON FWD SIDE BETWEEN STR 25L AND 25R. COMPLIED WITH EA 32-2015-240, REV.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 30,348 hrs · 27,751 cycles

FS 621 TO 625 INTERCOSTAL ANGLE, LOCATED AT RT BL 45, STRINGER 14R, WL 97.5 IS CRACKED. REPLACED INTERCOSTALS AT FS 621-FS 625 RT BL 45, STR 14R, WL 97.5 WITH NEW SERVICEABLE PN 601-35012-52 IAW SRM 51-42-21.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,755 hrs · 27,136 cycles

NR 3 EMERGENGY LIGHT INOPERATIVE. 01-20-2015 PERFORMED OPS TEST OF EMERGENCY LIGHTS, REPLACED THE LAMP IAW AMM 33-51-00. NO FURTHER DEFECTS NOTED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,347 hrs · 26,736 cycles

EXTERIOR RT FWD EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-21, OPS CK GOOD.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 26,481 hrs · 23,830 cycles

CRACK UNDER TRU DOOR AFT LATCH. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REPAIRED IAW REO 601R-53-11-2516.

Part: FITTING — CRACKED (JACK PAD) · airframe 26,481 hrs · 23,830 cycles

JACK PAD FITTING INBD FASTENER HOLE HAD CRACK INDICATION PRIOR TO FINAL SIZE OF HOLE. REPAIRED IAW REO 601R-57-21-1948, REV P1 DATED 2JUN2013 AND REO 601R-57-21-130, REV J.

Part: SKIN — BURNED (BS 409) · airframe 26,481 hrs · 23,830 cycles

BURN BETWEEN FS409+32 AND FS 409+48 BETWEEN STR 22L AND STR 23L. REPAIRED IAW REO 601R-53-31-788. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702.

Part: SKIN — CRACKED (RT WING) · airframe 26,481 hrs · 23,830 cycles

RT WING PLANK CRACKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. COMPLIED WITH EC/TC REO 601R-57-21-131, REV A, DATED 15MAR2013 AND 601R-57-21-131, RV A DATED: 08-29-2011 AS WRITTEN. COMPLIED WITH ECTC REO 601R-57-21-130-01 AND REO 601R-27-21-130-01, REV J, DATED 03/08/2011 AS WRITTEN.

Part: LIGHT — MISSING (GALLEY) · airframe 26,424 hrs · 23,776 cycles

EMERGENCY LIGHT MISSING FROM GALLEY 1. INSTALLED EMERGENCY LIGHT TRACK SEGMENTS IAW EO 600-33-0015-LC.

Part: ATTACH BRACKET — CRACKED (BS 461) · airframe 26,424 hrs · 23,776 cycles

RIGHT SIDE FS 461 INTERCOSTAL ATTACH BRACKET AT RBL 9.0 CRACKED. REPAIRED IAW SRM 51-42-06-00/51-42-20-00, SRM 51-21-11 AND 51-21-16.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 26,424 hrs · 23,776 cycles

LEFT SIDE FS 484 INTERCOSTAL ANGLE CRACKED AT LBL 27. REPAIRED IAW SRM 51-42-001-00.

Part: ATTACH ANGLE — CRACKED (BS 484) · airframe 26,424 hrs · 23,776 cycles

RT SIDE FS 484 HAS CRACKED ANGLE AT RBL 36.0, REPAIRED IAW REO 601R-53-41-059.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 26,424 hrs · 23,776 cycles

LT SIDE FS 484 INTERCOSTAL HAS CRACKED CLIP AT LBL 36. REPAIRED IAW REO 601R-53-41-059.

Part: SKIN — CRACKED (LT WING) · airframe 26,481 hrs · 23,829 cycles

LT WING PLANK CRACKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REPAIRED IAW EC/TC REO 601R-57-21-131, REV A: DATED 15 MAR 13 AND REO 601R-57-21-131, REV A DATED 05-29-2011 AND ECTC REO 601R-57-21-130 AND GENERIC REO 601R-57-21-130, REV J DATED 03/08/2011.

Part: TRACK — CRACKED (CARGO DOOR) · airframe 26,424 hrs · 23,776 cycles

CARGO DOOR FWD LOWER TRACK CHANNEL CRACKED. REPAIRED IAW SRM 51-42-06-00.

Part: LIGHT — BROKEN (CABIN) · airframe 25,631 hrs · 22,953 cycles

EMERGENCY LIGHT LOCATED JUST BELOW THE OPEN ARROW ON F/A MODULE LAMP BASE IS BROKEN. R & R EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: DOOR — OBSTRUCTED (MAIN PAX) · airframe 25,159 hrs · 22,455 cycles

PAX DOOR IS HARD TO OPEN. OPS CHECKED GOOD, REMOVED DEBRIS FROM TRACK. SDR CLOSED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,926 hrs · 22,220 cycles

EXTERIOR EMERGENCY LIGHT FWD OF LT OVERWING DOOR IS OUT. RELAMPED EXT EMERGENCY LIGHT NR 5 IAW AMM 33-51-21, OP'S CHECKED GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 24,862 hrs · 22,148 cycles

NR 7 AND NR 8 EMERGENCY LIGHTS AND THE SECOND FROM FWD AND MOST AFT CENTER CEILING EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: LATCH — OUT OF ADJUST (PAX DOOR) · airframe 24,806 hrs · 22,083 cycles

MAIN PAX DOOR WILL NOT OPEN WITHOUT EXCESSIVE FORCE. ADJUSTED AFT MID LATCH PIN ON MAIN CABIN DOOR OPS CK GOOD REF-MM 52-11-23. (SDR CLOSED)

Part: LIGHT — DAMAGED (CABIN) · airframe 24,617 hrs · 21,853 cycles

LEFT AND RIGHT FWD EMERGENCY LIGHTING DAMAGED. R & R LEFT AND RIGHT FWD EMERGENCY LIGHTING IAW AMM 33-51-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,367 hrs · 21,559 cycles

RT SIDE MIDDLE OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED RT SIDE MIDDLE OVERWING EMERGENY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 22,678 hrs · 19,683 cycles

WHILE PERFORMING LC2 CHECK, FOUND EMERGENCY EXIT LIGHTS AT THE SERVICE DOOR AND PAX DOOR INOP. AFTER TROUBLESHOOTING, FOUND POWER INPUT WIRES SWAPPED BETWEEN 2 EMERGENCY LIGHTS AT SERVICE DOOR DS17LY AND DS11LY RECONNECTED INPUT WIRES TO CORRECT LOCATION INPUT WDM 33-51-00 AND ALSO REPAIRED A BROKEN WIRE BEHIND F/A STA THAT GOES TO LOWER EMERGENCY. LIGHT ON WINDSCREEN AT PAX DOOR DS 18LY IAW ESPM 20-16-00 THEN TESTED EMERENCY LIGHTS IAW AMM 33-51-00-710-801. NO DEFECTS FOUND.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 22,671 hrs · 19,671 cycles

CORROSION ON FLOORBEAM AT FS 349 ON RT SIDE. REPAIRED IAW REO 601R-53-21-1268.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 22,671 hrs · 19,671 cycles

CORROSION ON FLOORBEAM AT FS 349.00 ON RT SIDE. INSTALLED REPAIR PARTS IAW REO 601R-53-21-1268.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 22,671 hrs · 19,671 cycles

CARGO FLOOR SUPPORT LBL 27 BETWEEN FS 574.00 AND 621.00 IS CORRODED AROUND THE NUT PLATES. REPLACED FLOOR SUPPORT CAP IAW SRM 51-42-21.

Part: BEAM — CORRODED (BS 333) · airframe 22,671 hrs · 19,671 cycles

WHILE INSPECTING AVIONICS COMPARTMENT DOOR CUTOUT SURROUNDING STRUCTURE, FOUND CORROSION ON BEAM AT FS 333 BETWEEN S26 - 27R. INSTALLED BEAM IAW SRM 51-42-06.

Part: DOOR FRAME — CORRODED · airframe 22,671 hrs · 19,671 cycles

CORROSION AT BOTTOM CORNER OF SERVICE DOOR FRAME CUT OUT. FABRICATED OF REPAIR PARTS AND INSTALLED IAW REO 601R-53-21-1267 IAW STEP 4-11.

Part: SUPPORT — CORRODED (BS 349) · airframe 22,671 hrs · 19,671 cycles

SUPPORT ANGLE ATTACHED TO AFT SIDE OF RT TRANSVERSE BEAM AT FS 349. HAS CORROSION ACROSS TOP. REMOVED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 22,671 hrs · 19,671 cycles

CORROSION ON FLOOR SUPPORT, SHORT BEAM, AT FS 349.00 ON RT SIDE. REMOVED CORROSION IAW SRM 51-21-06. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00. REPAIRED IAW REO 601R-53-21-1268.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 22,671 hrs · 19,671 cycles

CARGO FLOOR SUPPORT CRACKED AT FS 621.00 AND LT FLOOR SILL. CARGO FLOOR SUPPORT ANGLE AT LT F/S 621.00 NEEDS TO BE REMOVED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06 AND 51-42-21. DRILLED NEW SERVICABLE FLOOR SUPPORT ANGLE SRM 51-40-11. INSTALLED FLOOR SUPPORT ANGLE IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 22,671 hrs · 19,671 cycles

CARGO FLOORBEAM LBL 27.0 BETWEEN FS 574.00 AND 621.00 IS CORRODED AROUND NUT PLATES. REMOVED CORROSION IAW SRM 51-21-06. BEYOND REPAIRABLE LIMITS IAW SRM 53-00-00. REMOVED AND REPAIRED LBL27 FLOORBEAM CAP IAW SRM 51-42-06 AND SRM 51-40-11.

Part: SILL — CORRODED (BS 574-621) · airframe 22,671 hrs · 19,671 cycles

CARGO FLOOR SILL AT CARGO DOOR IS CORRODED AROUND NUTPLATES ON UPPER AND LOWER SURFACE BETWEEN FS 574.00 - 621.00. REMOVED CORROSION ON SILL IAW SRM 51-21-06, FOUND TO BE OUT OF LIMITS. CARGO DOOR SILL IS OUT OF LIMITS BEING R & R.

Part: BEAM — CORRODED (BS 333) · airframe 22,671 hrs · 19,671 cycles

WHILE INSPECTING AVIONICS COMPARTMENT DOOR CUTOUT SURROUNDING STRUCTURE, FOUND CORROSION ON BEAM AT FS333.00 BETWEEN S27 AND 26 RT. REPAIRED IAW SRM 51-42-06.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 22,671 hrs · 19,671 cycles

FASTENERS UNDER SERVICE DOOR THRESHOLD PLATE, MOUNTING BOLTS FOR THE 2 BOTTOM DOOR HOOKS AND 1 FASTENER AT AFT END OF THRESHOLD PLATE HAS CORROSION. ALSO, AREA UNDER CLIP NUT PLATES HAS CORROSION. R & R BOLTS IAW AMM 20-21-00. CLEAN/TREAT CORROSION IAW AMM 51-21-11. BOLTS R & R, CORROSION DAMAGE TREATMENT COMPLIED WITH ON JOB 1 OF NR 142 & 157, STEP 2 THROUGH 11. FOUND CORROSION ON LOWER ANGLE. REMOVED 9 HILOKS FOR ACCESS, REMOVED CORROSION FROM LOWER ANGLE IAW SRM 51-42-20,51-21-06. REQ NDT TO VERIFY MATERIAL LOSS. PERFORMED UT THICKNESS INSP OF BLEND AREA IAW MAC NDT INSP PROCEDURE UT-3 MINIMUM MATERIAL REMAINING IS 054". BLEND AREA REQUIRES EVALUATION FOR ALLOWABLE LIMIT IAW SRM. BLENDED AREA EXCEED LIMITS OF THE SRM 53-00-00 AND 53-21-23. REPLACE LOWER THRESHOLD ANGLE (SERVICE DOOR) WHEN PARTS RECEIVED. REMOVED 2 FITTINGS, 1 BRACKET AND LOWER THRESHOLD ANGLE IAW SRM 51-42-20, 51-42-06, 51-41-00, 51-42-34, BEGAN DRILLING NEW LOWER THRESHOLD ANGLE PN 601R38303-253 IAW SRM 51-40-11. CONTINUE DRILLING UP NEW SERVICE DOOR LOWER THRESHOLD ANGLE. COMPLETED DRILLING UP NEW SERVICE DOOR LOWER THRESHOLD ANGLE SRM 51-40-11.

Part: SEAT TRACK — CORRODED (BS 612-621) · airframe 22,671 hrs · 19,671 cycles

SEAT TRACK CORRODED IN CARGO AT FS612.00 - 621.00 LBL 9.0. FOUND SEAT TRACK CORRODED BEYOND LIMITS IAW SRM 53-61-49. REMOVED CORRODED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 51-21-11, 51-40-11 AND 51-41-04. THIS IS A MINOR REPAIR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 22,671 hrs · 19,671 cycles

CORROSION AT BOTTOM AFT CORNER OF SERVICE DOOR FRAME CUTOUT. REMOVED CORROSION IAW SRM 51-42-13, 51-21-06, BLEND AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 22,671 hrs · 19,671 cycles

2 CLIPS CORRODED ON LOWER PAX DOOR (INBD AND OTBD OF FS 318) BT 161750. R & R BT 161750. REMOVED 2 CLIPS ON LOWER PAX DOOR INBD & OTBD OF FS 318 IAW SRM 51-42-06. INSTALL NEW CLIPS. INSTALLED 2 NEW CLIPS ON LWR PAX DOOR INBD & OTBD OF FS 318 IAW SRM 41-42-06. THIS IS A MINOR REPAIR. (CLOSED)

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 22,671 hrs · 19,671 cycles

2 CLIPS CORRODED ON LOWER PAX DOOR (INBD AND OTBD OF FS 340) BT 161750 R & R. REMOVED 2 EA CLIPS ON LOWER PAX DOOR INBD & OTBD FS 340 IAW SRM 51-42-06. INSTALL NEW CLIPS. INSTALLED NEW CLIPS ON LWR PAX DOOR INBD & OTBD FS 340 IAW SRM 07-42-06. THIS IS A MINOR REPAIR. (CLOSED)

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,747 hrs · 18,607 cycles

CAPTAINS FLASHLIGHT INOP. R & R CAPTAINS FLASHLIGHT BATTERYS IAW AMM 25-61-00. OPS CHK GOOD. OPS CHK GOOD. (CLOSED)

Part: A/C PACK — ODOR · airframe 20,764 hrs · 17,448 cycles

AT LOWER ALTITUDES, PACKS PRODUCE MOLDY ODOR MAKING IT DIFFICULT TO BREATH. THIS OCCURS AT HIGHER POWER SETTINGS. PERFORMED OPEATIONAL CHECK OF LEFT & RIGHT PACKS AT LOW & HIGH TEMPS. ALL CHECKS NORMAL. NO DEFECTS NOTED AT THIS TIME, IAW AMM 21-51-00.

Part: BPSU — FAILED (TE FLAPS) · airframe 20,467 hrs · 17,103 cycles

ON DOWNWIND SELECTED FLAPS 8, FLAPS FAIL CAUTION MSG RAN QRH. (EMERGENCY DECLARED) REFER TO WO NR 147144 N/R-00001 RT BPSU R & R ALL OPS CHECK GOOD MCO CLEARED.

Part: VALVE — FAILED (ANTI ICE SYS) · airframe 20,208 hrs · 16,807 cycles

LT COWL ANTI-ICE CAUTION MSG (EMERGENCY DECLARED -- ENROUTE, ACFT DIVERTED DUE TO MX).

Part: FLAP — FAILED (WING) · airframe 19,246 hrs · 15,794 cycles

FLAP FAIL AT 20 DEGREES ON APPROACH. EMERGENCY DECLARED, ENROUTE, ACFT DIVERTED DUE TO MX.

Part: FRAME — CRACKED (BS 718 S10-11R) · airframe 19,112 hrs · 15,654 cycles

RT FS 718 IS CRACKED BETWEEN STRINGERS 10 AND 11. REPAIRED FRAMES IAW SB 601R-53-055, PART C & C STRUCTURAL REPAIR. THE REPAIR MEETS WITH ALL THE REQUIREMENTS OF SB 610R53-055, REV B.

Part: SUPPORT BEAM — CRACKED (CARGO DOOR) · airframe 19,112 hrs · 15,654 cycles

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

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 19,112 hrs · 15,654 cycles

FS 559.00 BULKHEAD WEB HAS TWO HFEC INDICATIONS NOTED, INDICATION NR 1 IS 75 PERCENT FSH APPROX .25 INCH LONG AT RBL 18.00 AND WL 59.10 INDICATION NR 2 IS 75 PERCENT FSH APPROX .1 INCH LONG AT RBL 9.00 AND WL 54.10, FAILS NDT INSP AT THIS TIME. REPAIRED FS 559 BULKHEAD WEB AND CAP ANGLES FROM LBL 27 TO RBL 27 IAW REO 601R-53-41-260 REV C.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 19,112 hrs · 15,654 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED PAX DOOR ASSIST CABLE PULLEY TO ACCESS FOR AFT ANGLE REPAIR IAW 51-42-22. RE-INSTALLED PAX DOOR ASSIST PULLEY BRACKET IAW SRM 51-42-22.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,112 hrs · 15,654 cycles

CARGO COMPARTMENT FLOOR SEAT RAILS FROM FS 559.0 + 80 TO FS 621.00 HAVE CORROSION AROUND SCREWS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,110 hrs · 15,653 cycles

FWD PRESSURE BULKHEAD CRACKED APPROX 1 INCH LONG AT BRAKE CABLE CUTOUT FS 202.75. REPAIRED CRACKED FWD PRESSURE BULKHEAD FS 202.75 PER ASA EC/TC EO 600-53-217 C/W AND REO 601R-53-11-563.

Part: ISOLATOR — BROKEN (BULKHEAD) · airframe 19,110 hrs · 15,653 cycles

REAR PRESSURE BULKHEAD FWD FACE HAS TWO BROKEN ISOLATORS. REMOVED & REPLACED ISOLATORS ON REAR PRESSURE BULKHEAD IAW CRJ 200 SRM 51-42-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,021 hrs · 15,560 cycles

MOST FWD IN-CEILING EMERGENCY LIGHT INOPERATIVE. FLT 5246 DEL 17 MINS.

Part: STEP — CRACKED (ASD) · airframe 18,725 hrs · 15,289 cycles

ASD BOTTOM STEP CRACKED AND ROD END BENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,233 hrs · 14,842 cycles

EMERGENCY TRACK LIGHTING AT ROWS 6-8 INOP.

Part: DOOR — STUCK (CABIN DOOR) · airframe 18,229 hrs · 14,837 cycles

CABIN DOOR WILL NOT CLOSE.

Part: SHUTOFF VALVE — MALFUNCTIONED (CARGO BAY) · airframe 16,600 hrs · 13,392 cycles

CARGO SOV FAIL STATUS. CARGO CONDITION AIR SOV, DEFERRED CLOSED. REMOVED AND REPLACED CARGO RECIRCULATED AIR SOV IAW AMM 21-55-07 OPS CHECK GOOD AT THIS TIME. DEFER CLEARED, PLACARD REMOVED.

Part: FLAP — MALFUNCTIONED (WING) · airframe 16,362 hrs · 13,199 cycles

FLAPS FAIL - FLAPS 8 TO 0 DEGREES IN 8 DEGREE POSITION. COMPLIED W/ QRH LANDED KATL. A/C RETURNED TO ATL AFTER T/O. FIRE TRUCKS WERE ON STANDBY AS A PRECAUTION. FLT 4688 DEL 41 MINS - NC FLTS 4688, 4288 CX.

Part: A/C PACK — ODOR (LEFT) · airframe 16,063 hrs · 12,947 cycles

LEFT PACK MAKING ABNORMAL NOISE AND ODOR. A/C RETURNED TO ATL AFTER T/O. FLTS 4771, 4910 CX.

Part: UNKNOWN — ODOR (CABIN) · airframe 16,048 hrs · 12,935 cycles

ON SHORT FINAL, FLIGHT CREW SMELLED SOMETHING BURNING. CONTINUED DURING LANDING AND TAXI (AIR CONDITIONING PACK, LT SIDE).

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 15,544 hrs · 12,421 cycles

CAPT'S FLASHLIGHT INOP.

Part: PLACARD — PEELING (AIRSTAIR DOOR) · airframe 15,517 hrs · 12,394 cycles

ASD EXIT PLACARD PEELING LOOSE.

Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 15,227 hrs · 12,094 cycles

LEFT OVERWING EXIT HARD TO OPEN.

Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 15,227 hrs · 12,094 cycles

RT OVERWING EXIT HARD TO OPEN. FLT 4725 CX.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,060 hrs · 11,921 cycles

RANRC 349. RT FS 484 INTERCOSTAL IS CRACKED ON O/B SIDE. [SUP 05-08-07] REPAIRED CRACKED INTERCOSTAL ON O/B SIDE OF RT FS 484 IAW BOMBARDIER REO 601R-53-41-059.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,060 hrs · 11,921 cycles

RANRC 352. FS 280 RT O/B ANGLE CRACKED AT RBL 9. [SUP 05-11-07] REMOVED FS 280 R/H O/B ANGLE AND FABRICATED NEW ANGLE FROM 2024 T-3 .050", PO 8398-1, IAW REO 601R-53-11-137.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 15,060 hrs · 11,921 cycles

FS 280 UPPER AFT FLANGE IS CRACKED ON RT SIDE O/B OF RBL 9. [SUP 05-11-07] REPAIRED FS 280 UPPER AFT FLANGE R/H O/B OF RBL 9 PER: REO 601R-53-11-136. COMPLIED WITH EO 600-53-0091.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 15,060 hrs · 11,921 cycles

FS 280 UPPER AFT FLANGE IS CRACKED ON LEFT SIDE O/B OF LBL 9. [SUP 05-11-07] REPAIRED F.S. 280 UPPER AFT FLANGE LT O/B OF LBL 9 PER: REO 601R-53-11-136.

Part: PLACARD — WORN (COCKPIT) · airframe 15,060 hrs · 11,921 cycles

RANRC 319. ESCAPE CREW HATCH HAS WORN PLACARD (EMERGENCY EXIT). [SUP 05-08-07] REMOVED AND REPLACED ESCAPE CREW EMERGENCY PLACARD WITH NEW SERVICEABLE PLACARD P/N S1859 IAW CRJ 200 AMM 11-20-00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,060 hrs · 11,921 cycles

RANRC 298. RT OBLIQUE ANGLE CRACKED IN AEB. [SUP 05-11-07] REMOVED AND REPLACED RT OBLIQUE ANGLE, P/N 601-35012-52, IAW BOMBARDIER CRJ 200 SRM 51-42-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,752 hrs · 11,636 cycles

LEFT AND RIGHT EMERGENCY LIGHT INOP.

Part: DOOR — STIFF (AIRSTAIR) · airframe 13,894 hrs · 10,874 cycles

CREW REPORTS ASD HARD TO OPERATE.

Part: STEP — CRACKED (ASD) · airframe 13,845 hrs · 10,840 cycles

ASD LOWER BOTTOM STEP CRACKED.

Part: STEP — CRACKED (AIRSTAIR) · airframe 13,574 hrs · 10,607 cycles

ASD BOTTOM STEP CRACKED AT ATTACH LINK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,049 hrs · 10,188 cycles

EMER EXIT LIGHT AT SERVICE DOOR HAS BULBS INOP.

Part: PLACARD — PEELING (CABIN) · airframe 12,960 hrs · 10,113 cycles

EXIT PLACARD ON THE STAIRS IS COMING OFF.

Part: DOOR — MALFUNCTIONED (MAIN PAX)

DURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT CLOSE AND LOCK. MAINTENANCE CYCLED THE PASSENGER DOOR THROUGH SEVERAL TIMES WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: CLIP — CRACKED (BS 625)

DURING A C-CHECK IN MCN, THE LEFT CLIP, AT FRAME FS 625, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT CLIP, AT FRAME FS 625, IAW CRJ200 SRM 50-42-21. (M)

Part: CLIP — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE RIGHT INBOARD AND OUTBOARD FS 280 CLIPS, AT RBL 9, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD AND OUTBOARD FS 280 CLIPS, AT RBL 9, IAW CRJ SRM 51-42-20. (M)

Part: CLIP — CRACKED (BS 280)

DURING A C-CHECK IN MCN, THE LT INBOARD AND OUTBOARD FS 280 CLIPS, AT LBL 9, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD AND OUTBOARD FS 280 CLIPS, AT LBL 9, IAW CRJ SRM 51-42-21. (M)

Part: INTERCOSTAL — CRACKED (BS 280)

DURING A CHECK IN MCN, THE FS 280 INTERCOSTAL, AT RBL 9, NEAR THE FLOOR SUPPORT ANGLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 280 INTERCOSTAL, AT RBL 9, NEAR THE FLOOR SUPPORT ANGLE IAW ASA EO 600-53-0123. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

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

Part: UPLOCK — INOPERATIVE (NLG) · airframe 10,144 hrs

DURING FINAL APPROACH, UPON SELECTING GEAR DOWN, A GEAR DISAGREE MASTER WARNING WAS RECEIVED. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR (NLG) UPLOCK ASSY. OPERATIONAL CHECKS GOOD. AC OK FOR SERVICE. (K)

Part: STEP — CRACKED (PAX DOOR)

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

Part: MOUNT — CRACKED (PAX DOOR)

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

Part: STEP — CRACKED (PAX DOOR)

DURING HANGAR MAINTENANCE, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. (K)

Part: STEP — BROKEN (PAX DOOR) · airframe 8,976 hrs

DURING AN A-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP.

Part: STEP — CRACKED (PAX DOOR) · airframe 8,891 hrs

DURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: COALESCER BAG — DIRTY (CLIMATE CONTROL)

FOLLOWING CLIMB OUT, UPON LEVELING OFF AT APPROX 31,000 FEET, CREW BEGAN NOTICING A SMELL, JET A FUMES COMING THROUGH THE VENTS IN THE COCKPIT ONLY. AFTER DESCENDING TO 24,000 FEET, CREW ATTEMPTED TO ISOLATE THE SMELL BY SHUTTING DOWN THE LT PACK BUT THE SMELL PERSISTED. THE AC DIVERTED. CREW DID NOT DECLARE AN EMERGENCY BUT ALERTED FIRE AND RESCUE AS A PRECAUTION. AC LANDED SAFELY. MAINT REMOVED AND REPLACED LT AND RT COALESCER BAGS AND RAN BOTH ENGINES AT ALL POWER SETTINGS FOR 1.5 HOURS IN ADDITION TO USING AUX POWER UNIT BLEEDS. NO FUEL SMELLS OCCURRED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT CLIPS AT FS 625 BELOW THE BOX BEAM WERE FOUND TO BE CRAKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT AND RIGHT CLIPS AT FS 625 BELOW THE BOX BEAM. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO BAY FLOOR SILL UNDER THE FORWARD LATCH AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO BAY FLOOR SILL AT FS 562.72-589. (M)

Part: HANDLE — CRACKED (E/E BAY DOOR)

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

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

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

Part: CLIP — CRACKED (INTERCOSTAL)

DURING A C-CHECK IN MCN, THE LEFT INTERCOSTAL CLIP AT FS 484, BL 27 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LEFT INTERCOSTAL CLIP AT FS 484, BL 27 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 FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE TOP STEP ON THE PASSENGER DOOR IAW SRM 51-73-00. (M)

Part: STEP — CRACKED (PAX DOOR)

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

Part: SELECTOR VALVE — INOPERATIVE (MLG)

FLT 4783 - DUIRNG TAKEOFF FROM DFW-AMA, THE LEFT MAIN GEAR FAIL TO RETRAC AND SHOWED INTRANSITION. THE QRH WAS COMPLIED WITH. THE CREW RECYCLED THE GEAR, IT CAME DOWN AND LOCKED. EMERGENCY EQUIPMENT WAS REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE AND PERFORMED GEAR SWINGS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SELECTOR VALVE — INOPERATIVE (MLG DOOR)

DURING CRUISE FROM ATL-MTY, THE NOSE GEAR DOOR OPENED UNCOMMANDED AND THE CREW RECEIVED A GEAR DISAGREE WARNING ACCOMPANIED BY AN AIR DISTURBANCE AND A VIBRATION IN THE AIRCRAFT. THE CREW REDUCED AIR SPEED TO 250 KIAS AND THE WARNINGS WENT AWAY WITH EVERYTHING RETURNING TO NORMAL. THE AIRCRAFT DIVERTED TO DFW AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SELECTOR VALVE AND THE NLG SELECTOR VALVE. OPS CAND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SEAL — LEAKING (WING)

DURING CLIMB-OUT FROM XNA-ATL, WHILE RETRACTING THE FLAPS, THE CREW RECEIVED AN AMBER CAUTION FLAPS FAIL MESSAGE. AN EMERGENCY WAS DECLARED. THE FLAPS FAILED AT ZERO DEGREES AND A ZERO FLAPS LANDING WAS ACCOMPLISHED IN ATL WITHOUT INCIDENT. MAINTENANCE RE-RIGGED THE ENTIRE FLAP SYSTEM, REMOVED MOISTURE FROM THE BRAKE POSITION SENSOR UNIT FLEX SHAFTS AND REPLACED THE TEFLON SEALS ON THE FLEX SHAFTS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — LOOSE (CABIN)

DURING GROUND INSPECTION IN ATL, THE FIRST STRIP OF ORANGE EMERGENCY FLOOR LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REATTACHED A LOOSE CONNECTOR TO THE FLOOR LIGHTING. OPERATIONAL CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — INOPERATIVE (FUSELAGE)

FLT 4589 - DURING GROUND INSPECTION IN ATL, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)