N14186

Part: WIRE — BROKEN (ZONE 200) · airframe 39,972 hrs · 30,002 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED SERVICE DOOR EMERGENCY LIGHT. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT ASSEMBLY AND LAMP. OPS CHECK FAILED. TROUBLESHOT EMERGENCY LIGHT SYSTEM. REMOVED AND REPLACED NR 2 BATTERY POWER SUPPLY TRAY. OPS CHECK FAIL. FOUND WIRE SPLICE SP 7377 TO GROUND NO CONTINUITY. FOUND WIRE W716-0008-20 TO BE BROKEN BETWEEN PIN D ON P7198 AND SPLICE SP7377. REPAIRED WIRE. OPS CHECK SAT. SERVICE DOOR EXTERNAL EMERGENCY LIGHT COMES ON.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

AFT WET AREA LH OMEGA BEAM FROM FR 49 TO FR 52 HAS CORROSION. REMOVED CORROSION ON LH OMEGA BEAM FROM FR 49 TO FR 52.

Part: SWITCH — OUT OF POSITION · airframe 39,004 hrs · 29,094 cycles

ENG 1 FUEL INDICATION SHOWING 0 POUNDS AT CRUISE ALT. FOUND POWER SELECTION TO BE IN BATTERY POSITION AND REFUELING SWITCH TO BE IN OPEN POSITION ON REFUELING PANEL. RESET SWITCHES TO NORMAL CONFIGURATION. OPS CHECK GOOD. COMPLIED WITH ENGINE RUNS AT ALL POWER SETTINGS, NOT FAULT FOUND

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 37,662 hrs · 27,840 cycles

MCD EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EXTERNAL EMERGENCY LIGHT HOUSING. OPS CHECK SAT.

Part: RETAINING RING — FAULTED (MAIN DOOR) · airframe 37,426 hrs · 27,639 cycles

MAIN CABIN DOOR CAN OPEN ONLY FROM OUTSIDE. TROUBLESHOOT DOOR CHECK SECURITY OF INTERNAL DOOR RED HANDLE FOUND NO DEFECTS RESECURED DOOR HANDLE AND TRIED TO OPEN MCD. THE RETAINING RING WAS HYPER EXTENDED AND OUT OF PLACE. THIS CAUSED THE TORQUE TUBE TO INTERMITTENTLY SLIDE AROUND. REMOVED AND REPLACED THE RETAINING RING. OPS CHECK SAT.

Part: CAM — LACK OF LUBE (MAIN DOOR) · airframe 37,426 hrs · 27,639 cycles

MAIN CABIN DOOR ONLY OPENS FROM THE OUTSIDE. INSPECTED MAIN CABIN DOOR AND LATCHES. LUBRICATED MCD ACTUATING CAM. OPENED AND CLOSED DOOR SEVERAL TIMES. OPS CHECK SAT.

Part: DOOR — BINDING (MAIN) · airframe 37,421 hrs · 27,633 cycles

MCD DIFFICULT TO OPEN AFTER FLIGHT. LUBED AND PERFORMED OPS CHECK OF MAIN CABIN DOOR. OPS CHECK GOOD. ALSO PRESSURIZED AIRCRAFT. OPS CHECK SAT

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,226 hrs · 27,462 cycles

FOUND EMERGENCY LIGH BPS  4 TO BE INOP R&R BPS 4. OPS CHECK SAT.

Part: SKIN — CRACKED (FRMS 77-81 S3-9R) · airframe 37,168 hrs · 27,418 cycles

8 CRACKS SUSPECTED ON RH SKIN FR77-81 AND STR 3R-9R. SKIN REPAIRED WITH A DOUBLER ON RH REAR FUSE 2 AT FR 78 BTW STR 5R-7R AND 6 BUSHINGS ON RH REAR FUSE SKIN AT FR 77 & 79 BTW STR 3R-9R

Part: SKIN — CRACKED (FRMS 77-81 S3-9L) · airframe 37,168 hrs · 27,418 cycles

8 CRACKS SUSPECTED ON LH SKIN FR77-81 AND STR 3L-9L. 9 CRACKS FOUND. SKIN REPAIRED WITH A DOUBLER ON LH REAR FUSE 2 AT FR78 BTW STR 5L-7L AND 7 BUSHINGS ON LH REAR FUSE 2 SKIN AT FR 77,79 & 80 BTW STR 3L-9L

Part: SHEAR TIE — CRACKED (FRM 66 S7-8L) · airframe 37,168 hrs · 27,418 cycles

SHEAR CLIP FOUND CRACKED AT FR 66 BTW STR 7L-8L. SHEAR CLIP REPLACED BY FABRICATION WITH ALTERNATE MATERIAL

Part: FLOOR SUPPORT — CRACKED (FRMS 19-23) · airframe 37,168 hrs · 27,418 cycles

AT CF1 FLOOR STRUCTURE AREA, CORROSION AND (3X) CRACKS FOUND ON LH OMEGA BEAM #1 BTW FR 19-23. OMEGA BEAM REPAIRED WITH 3 DOUBLERS ON INBD VERTICAL FLANGE AT FR 21, 22, AND 23 (CORROSION LEVEL 1)

Part: SKIN SPLICE — CORRODED (FRMS 23-24) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

RH SKIN SPLICE BTW FR 23-24 AND STR 19-20 FOUND CORRODED. CIRCUMFERENTIAL STRAP SPLICED ON CENTER FUSE 1 & 2 BTW FR 23-24 AND BTW STR 20L-19R

Part: SKIN — CORRODED (FRM 67 S21L-R) · airframe 37,168 hrs · 27,418 cycles

CORROSION FOUND ON INNER SKIN UNDER FR 67 BTW STR 21L-21R. SKIN REPAIRED WITH A DOUBLER AT FR 67 BTW STR 20L-20R. CORROSION LEVEL 1.

Part: SHEAR TIE — CRACKED (FRMS 61 S6-7R) · airframe 37,168 hrs · 27,418 cycles

SHEAR CLIP FOUND CRACKED AT FR61 BTW STR 6R-7R. SHEAR CLIP REPLACED BY FABRICATION WITH ALTERNATE MATERIAL

Part: SHEAR TIE — CRACKED (FRM 58 S15-16L) · airframe 37,168 hrs · 27,418 cycles

SHEAR CLIP FOUND CRACKED AT FR 58 BTW STR 15L-16L. SHEAR CLIP REPLACED BY FABRICATION WITH ALTERNATE MATERIAL

Part: FLOOR SUPPORT — CRACKED (FRMS 24-28) · airframe 37,168 hrs · 27,418 cycles

LH OMEGA BEAM 2 CRACK SUSPECTED (X3). 3 CRACKS CONFIRMED ON CENTER FUSE 2 LH OMEGA BEAM #2 AT FR 24-28 AND 27. 3 CUTOUTS DONE. LH OMEGA BEAM #2, 3 CRACKS REPAIRED

Part: SHEAR TIE — CORRODED (FRM 66 S15-17L) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

CORROSION FOUND ON CARGO FR 66 LATERAL SHAPE BTW STR 15L-17L. CORROSION ON SHEAR CLIP OUT OF LIMITS AT FR 68 STR 15L-17L. AT FR 68 BTW STR 17L-15L, SHEAR CLIP REMOVED AND REPAIRED

Part: FLOOR SUPPORT — CRACKED (FRMS 46-50) · airframe 37,168 hrs · 27,418 cycles

AT CF3 FLOOR STRUCTURE AREA, CRACK FOUND ON RH OMEGA BEAM INBD ANGLE BTW FR 46-50. RH OMEGA BEAM INBD ANGLE BTW FR 46-50 REMOVED FOR REPLACEMENT. NEW ANGLE ON RH OMEGA BEAM INBD DRILLED AND READY TO INSTALL. ON RH OMEGA BEAM, INBD ANGLE BTW FR 46-50 REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 46-50) · airframe 37,168 hrs · 27,418 cycles

AT CF3 FLOOR STRUCTURE AREA, CRACK FOUND ON RH OMEGA BEAM OUTBD ANGLE BTW R 46-50. RH OMEGA BEAM OUTBD ANGLE BTW FR 46-50 REMOVED FOR REPLACEMENT. POST AT FR 50 REMOVED FOR ACCESS. RH OMEGA BEAM OUTBD ANGLE DRILLED AND READY TO INSTALL. POST RH AT FR50 REINSTALLED. R OUTBD ANGLE BTW FR 46-50 UNDER OMEGA BEAM REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 35-41) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

AT CF3 FLOOR STRUCTURE AREA, CORROSION FOUND ON RH SILL #3 BTW FR 35-41. RH SILL #3 BTW FR 35-41 REMOVED. AFTER INVESTIGATION, RH SILL #3 BTW FR 35-41 FOUND OUT OF LIMITS. AT CF3 FLOOR STRUCTURE RH SILL #3 BTW FR 35-45 REPLACED

Part: SEAT TRACK — CORRODED (FRMS 41-18) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

AT CF3, CORROSION FOUND ON RH SIDE PASSENGER SEAT TRACK SUPPORT BTW FR 41-48. AT CF3 ON RH SIDE PASSENGER SEAT TRACK SUPPORT BTW FR 41-48, SUPPORT BLENDED OUT OF LIMIT. AT CF3 ON RH SIDE PASSENGER SEAT TRACK SUPPORT BTW FR 41-48, REPAIR DOUBLER FABRICATED. AT CF3 ON RH SIDE PASSENGER SEAT TRACK SUPPORT BTW FR 41-48, REPIAR DOUBLER INSTALLED

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 37,168 hrs · 27,418 cycles

LH MLG WHEEL WELL BAY AREA REAR BULKHEAD CRACK. AT LH MLG WHEEL WELL BAY AREA, REAR CRACKED BULKHEAD REMOVED FOR REPLACEMENT. AT LH MLG WHEEL WELL BAY AREA, NEW REAR BULKHEAD DRILLED AND FITTED. AT LH MLG WHEEL WELL BAY AREA, NEW REAR BULKHEAD INSTALLED.

Part: SHEAR TIE — CRACKED (FRM 67 S7-8L) · airframe 37,168 hrs · 27,418 cycles

SHEAR CLIP FOUND CRACKED AT FR67 BTW STR 7L-8L. AT FR 67 BTW STR 7L-8L SHEAR CLIP REMOVED FOR REPLACEMENT AND REPLACED WITH A NEW ONE.

Part: FITTING — CRACKED (THRUST REVERSER) · airframe 37,168 hrs · 27,418 cycles

LH T/R FIXED STRUCTURE, O/B SIDE INTERNAL AREA BTW STN: XN 3200.00 / XN 4109.70 FITTING FOUND CRACKED. LH TR FIXED STRUCTURE, O/B SIDE INTERNAL AREA, BTW STN: XN 3200.00 / XN 4109.76 STIFFENER REMOVED. LH TR FIXED STRUCTURE O/B SIDE INTERNAL AREA BTW STN XN 3200.00 / XN 4109.70 STIFFENER REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 19-23) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

AT CF1 FLOOR STRUCTURE AREA, CORROSION FOUND ON LH SILL #1 BTW FR19-23. AT CF1 FLOOR STRUCTURE AREA ON LH SILL #1 BTW FR 19-23 BLENDED OUT OF LIMIT. ON LH SILL #1 BTW FR 19-23, SILL REMOVED FOR REPLACEMENT. LH SILL #1 BTW FR 19-23 AT CF1 FLOOR STRUCTURE AREA REPLACED

Part: CROSSBEAM — CRACKED (NLG WW) · airframe 37,168 hrs · 27,418 cycles

IN NLG LH SUPPORT AFT OF FWD CROSSBEAM FOUND CRACKED. IN NLG LH SUPPORT AFT OF FWD CROSSBEAM REPLACED WITH NEW ONE.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

RH WING ACCESS PANEL 632AB AREA, THE ANCHOR NUT RING ON THE WING STRUCTURE IS CORRODED. DOUBLER REPLACED AT RH WING ACCESS PANEL 632AB

Part: SUPPORT — CRACKED (FRMS 61-62 S4-5R) · airframe 37,168 hrs · 27,418 cycles

CARGO DOOR SUPPORT CASTING FOUND CRACKED BTW FR 61-62 AND STR 4R-5R. AT FR61-62 AND BTW STR 4R-5R, CARGO DOOR SUPPORT CASTING REMOVED. CARGO DOOR SUPPORT CASTING REPLACED, BUSHING INSTALLED ON CASTING. CARGO DOOR SUPPORT CASTING INSTALLED COVER

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 37,168 hrs · 27,418 cycles

CARGO DOOR MECH SUPPORT BTW FR 61-62 AND STR 4R-5R FOUND CRACKED. AT RH SIDE BTW FR 61-63 AND BTW STR 4R*5R CARGO DOOR MECH SUPPORT REPLACED.

Part: SUPPORT — CORRODED (FRMS 68-69) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

RADIO ALT 2, OUTSIDE SUPPORT BTW FRAME 68-69 FOUND CORRODED. RADIO ALT 2, OUTSIDE SUPPORT BTW FR 68-69 CORROSION BLENDED AND FOUND OUT OF LIMIT. RADIO ALT 2, OUTSIDE SUPPORT BTW FR 68-69 REMOVED. RADIO ALT 2 OUTSIDE SUPPORT BTW FR 68-69 REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 20-22) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

AT CF1 FLOOR STRUCTURE AREA, CORROSION FOUND ON SERVICE DOOR CUTOUT LOWER CHANNEL BTW FR 20-22. SERVICE DOOR CUTOUT LOWER CHANNEL BTW FR 20-22 REMOVED FOR REPLACEMENT. SERVICE DOOR CUTOUT LOWER CHANNEL BTW FR 20-22 BLENDED OUT OF LIMIT. SERVICE DOOR CUTOUT LOWER CHANNEL BTW FR 20-22 REPLACED

Part: BEAM — CORRODED (FRMS 65-68) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

CARGO LOWER BEAM FOUND CORRODED BTW FR 65-68. CARGO LOWER BEAM BTW FR 65-68 REPLACED

Part: SUPPORT BRACKET — CRACKED (FRMS 67-68 S4-5R) · airframe 37,168 hrs · 27,418 cycles

3 CARGO DOOR SUPPORT BRACKET FOUND CRACKED BTW FR 67-68 ON STR 4R, 5R AND VERTICAL BRACKET. 3 CARGO DOOR SUPPORT BRACKETS REPALCED

Part: SHEAR TIE — CRACKED (FRM 80 S5-7R) · airframe 37,168 hrs · 27,418 cycles

AT RF2 SHEAR CLIP ON FR 80 BTW STR 7R-5R FOUND CRACKED. AT RF2 SHEAR CLIP ON FR80 BTW STR 7L-5L SKIN EXTERNAL AREA STRIPPED WITH CEE-BEE. SHEAR CLIP ON FR 80 BTW STR 7L-5L REMOVED FOR REPLACEMENT. AT RF2 SHEAR CLIP ON FR 80 BTW STR 7L-5L REPLACED WITH NEW PART.

Part: SHEAR TIE — CRACKED (FRM 15 S15-16R) · airframe 37,168 hrs · 27,418 cycles

SHEAR CLIP FOUND CRACKED ON FR 15 BTW STR 15R-16R. CRACKED SHEAR CLIP AT FR 15 BTW STR 15R-16R REMOVED. INSTALLATION OF NEW SHEAR CLIP AT FR15 BTW STR 15R-16R COMPLETE

Part: FLOOR SUPPORT — CORRODED (FRMS 22-23) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

AT CF1 FLOOR STRUCTURE AREA, CORROSION FOUND ON RH SILL BTW FR 22-23. AT CF1 FLOOR STRUCTURE AREA, ON RH SILL BTW FR 22-23 BLENDED OUT OF LIMIT. AT CF1 FLOOR STRUCUTRE AREA ON RH SILL BTW FR 22-23, LAYOUT PERFORMED AND DOUBLER REPAIR PART FABRICATED. AT CF1 FLOOR STRUCTURE AREA ON RH SILL BTW FR 22-23 REMOVED. AT CF1 FLOOR STRUCTURE AREA, RH SILL BTW 22-23 REPLACED WITH NEW PART.

Part: SHEAR TIE — CRACKED (FRM 73 S8-10L) · airframe 37,168 hrs · 27,418 cycles

SHEAR CLIP FOUND CRACKED AT FR 73 BTW STR 8L-10L. AT FR 73 BTW STR 8L-10L SHEAR CLIP REMOVED FOR REPLACEMENT. AT FR 73 BTW STR 8L-10L SHEAR CLIP REPLACED. AT FR73 LH PYLON AFT SIDE ACCESS PANEL REMOVE FOR ACCESS. FR73, LH PYLONG AFT SIDE ACCESS PANEL INSTALLED.

Part: SHEAR TIE — CRACKED (FRM 16 S15-16R) · airframe 37,168 hrs · 27,418 cycles

SHEAR CLIP CRACKED AT FR 16 BTW STR 15R-16R SHEAR CLIP AT FR 16 BTW STR 15R-16R REPLACED

Part: GUSSET — CORRODED (FRMS 59-61) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

RH GUSSET BTW FR 59-61 FOUND CORRODED. RH GUSSET BTW FR 59-61 CORROSION BLENDED AND FOUND OUT OF LIMITS. RH GUSSET BTW FR 59-61 REMOVED. RH GUSSET BTW FR 59-61 INSTALLED

Part: ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 37,168 hrs · 27,418 cycles

WING TO BODY FAIRING, ANGLE #4 ON WING FOUND CRACKED ON WING TO BODY, ANGLE #4 REMOVED FOR REPLACEMENT, ANGLE #4 DRILLED. ON WING TO BODY, ANGLE #4 REPLACED WITH NEW ONE.

Part: SHEAR TIE — CRACKED (FRMS 25-26) · airframe 37,168 hrs · 27,418 cycles

CF2, RH FUSE AT FR 25-26 BTW STR 15R-16R SHEAR CLIP CRACKED. ON CF2, RH FUSE AT FR 26 BTW STR 15R-16R SHEAR CLIP REMOVED AND REPLACED.

Part: GUSSET — CORRODED (FRMS 30-36) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

RH GUSSET 2 BTW FR 30-36 FOUND CORRODED. RH GUSSET #2 BTW FR 30-36 FOUND OF OF LIMITS. RH GUSSET #2 BTW FR 30-36 REMOVED FOR REPLACEMENT. RH GUSSET #2 BTW FR 30-36 REPLACED

Part: CABLE — FRAYED (STICK PUSHER) · airframe 37,168 hrs · 27,418 cycles

STICK PUSHER ACTUATOR CABLE STRAND BROKEN WIRE OUT OF LIMIT. STICK PUSHER ACTUATOR REPLACED

Part: FLOOR SUPPORT — CORRODED (FRMS 19-20) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

AT CF1 FLOOR STRUCTURE AREA, CORROSION FOUND ON R/H SILL BTW FR 19-20. FLOOR STRUCTURE AREA, ON R/H SILL BTW FR19-20 LAYOUR PERFORMED AND DOUBLE REPAIR PART FABRICATED. AT CF1 FLOOR STRUCTURE AREA, ON R/H SILL BTW FR19-20 CUT-OUT PERFORMED AND DOUBLE REPAIR PART FULLY DRILLED, AT CF1 FLOOR STRUCTURE AREA ON R/H SILL BTW FR19-20 REPAIR PERFORMED.

Part: SHEAR TIE — CRACKED (FRM 80 S5-7R) · airframe 37,168 hrs · 27,418 cycles

AT RF2 SHEAR CLIP ON FR 80 BTW STR 7R-5R FOUND CRACKED REPLACED WITH NEW PART

Part: CHANNEL — CRACKED (FRMS 46-50) · airframe 37,168 hrs · 27,418 cycles

AT CF3 FLOOR STRUCTURTE AREA, CRACK FOUNF ON L/H OMEGA BEAM OUTBD ANGLE BTW FR 46-50 ON L/H OMEGA BEAM OUTBD ANGLE REPLACED

Part: SUPPORT — CORRODED (FRMS 30-36) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

R/H SILL 2 BTW FR 30-36 FOUND CORRODED OUT OF LIMITS. INSTILATION OF NEW R/H SILL BTW FR 30-36

Part: FLOOR SUPPORT — CORRODED (FRMS 41-48) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

AT CF3 FLOOR STRUCTURE AREA, PIT CORROSION AROUND NUT PLATE FOUND ON R/H SILL#4 BTW FR 41-48 R/H SILL #4 BTW FR 41-48 REMOVED FOR REPLACEMENT. R/H SILL #4 BTW FR 41-48 REPLACED

Part: SHEAR TIE — CRACKED (FRMS28 S15-16R) · airframe 37,168 hrs · 27,418 cycles

CF2, R/H FUSE AT FR27-28 BTW STR 15R-16R SHEAR CLIP CRACKED CF2, RH FUSE AT FR27-28 BTW STR 15R-16R SHEAR CLIP REMOVED AND REPLACED.

Part: SHEAR TIE — CRACKED (FRM 25 S15-16) · airframe 37,168 hrs · 27,418 cycles

CF2, L/H FUSE AT FR 25 BTW STR 15-16 SHEAR CLIP CRACKED ON CF2, L/H FUSE AT FR 25 BTW 15-16 SILL RIVETS UNDER SHEAR CLIP REMOVED FOR ACCESS. AT L/H FUSE AT FR25 BTW STR 15-16 SHEAR CLIP REMOVED AND REPLACED. ON CF2, L/H FUSE AT FR 25 BTW STR 15-16 SILL RIVETS UNDER SHEAR CLIP REPLACED.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 36,589 hrs · 26,881 cycles

FOUND EMERGENCY BPS 1 INOPERATIVE. REMOVED AND REPLACED BPS #1. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 36,589 hrs · 26,881 cycles

FWD RH EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FWD RH EMERGENCY LIGHT BULB. OPS CHECK NOT SAT. PERFORMED OPS TEST ON #2 BPS. FOUND BPS #2 TO BE INOPERATIVE. REMOVED AND REPLACED BPS2. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.

Part: A/C PACK — ODOR · airframe 35,234 hrs · 25,695 cycles

BAD ODOR COMING FROM PACKS. PERFORMED DECONTAMINATION OF AIR CONDITIONING SYSTEM. NO FURTHER ODORS NOTED.

Part: NONE — INOPERATIVE · airframe 34,798 hrs · 25,275 cycles

PACK 1 BLOWING HOT AIR LOW VOLUME, OVER PRESSURIZED BY 1000FT AVG IN CLIMB UP TO FL320 WHERE IT CONTINUES TO 10KFT. REMOVED AND REPLACED AND OPS CHECKED PNEUMATIC OUTFLOW VALVE AND PNEUEMATIC OUTFLOW VALVE FILTER. OPS CHECK SAT. PROBLEM STILL REMAINS. REMOVED AND REPLACED THE GROUND CONNECTION DOOR RUBBER SEAT RING. CABIN LEAKAGE FUNCTIONAL CHECK SAT.

Part: RIVET — LOOSE (CABIN FLOOR) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

AT CF1 FLOOR STRUCTURE AREA, CORROSION AND TWO LOOSES RIVETS FOUND ON R/H OCTOGONAL DOUBLER AT FR 20 CF1, FLOOR STRUCTURE, OXTOGONAL DOUBLER RH OMEGA BEAM AT FR20 REMOVED/REPLACED

Part: SUPPORT — CORRODED (FRMS 30-36) · corrosion level 2 · airframe 37,168 hrs · 27,418 cycles

L/H SILL 3 BTW FR30-36 FOUND CORRODED. L/H SILL 3 REMOVED FOR REPLACEMENT. L/H SILL 3 REPLACED

Part: NONE — NONE · corrosion level 2 · airframe 33,868 hrs · 24,453 cycles

REAR FUSELAGE - SKIN HAS CORROSION UNDER RAR 2 ANTENNA MOUNT PLATE. REPAIRED WITH CUTOUT OF DAMAGE AT REAR FUSELAGE SKIN UNDER RAR #2 ANTENNA AT FR68-69 AND STR 21L-21R AND INSTALLED REPAIR DOUBLER. CORROSION LEVEL II

Part: NONE — NONE · corrosion level 2 · airframe 33,868 hrs · 24,453 cycles

CARGO DOOR - EXT - LWR INNER DOOR ANGLE HAS CORROSION. REMOVED AND REPLACED LOWER INNER CARGO DOOR ANGLE. CORROSION LEVEL II

Part: NONE — NONE · airframe 33,868 hrs · 24,453 cycles

FUSELAGE EXTERIOR TAIL - CRACK .100" LONG IN FUSELAGE SKIN STARTING AT FASTENER HOLE AT FR 75 STRG 2R. REPAIRED TRIMMED OUT IN FUSELAGE SKIN STARTING AT FASTENER HOLE AT FR 75 STRG 2R WITH REPAIR DOUBLER, REPAIR FILLER, AND FORMED REPAIR ANGLE.

Part: NONE — NONE · airframe 33,868 hrs · 24,453 cycles

REMOVE, RE-FABRICATE AND INSTALL DOUBLER AT REAR FUSELAGE SKIN RAR 2 ANTENNA THAT WAS DAMAGED ON INSTALL. REMOVED, FABRICATED AND REINSTALLED REPAIR DOUBLER AT REAR FUSELAGE SKIN RAT 2 ANTENNA

Part: NONE — NONE · corrosion level 2 · airframe 33,868 hrs · 24,453 cycles

MAIN CABIN OMEGA BEAM AT FR 57-61 Y+0 HAS CORROSION. REMOVED AND REPLACED MAIN CABIN OMEGA BEAM AT FR 57-61 Y+0. CORROSION LEVEL II

Part: NONE — NONE · airframe 33,868 hrs · 24,453 cycles

CARGO DOOR INNER SKIN HAS MULTIPLE SCREW DAMAGE. REMOVED AND REPLACE LOWER INNER CARGO DOOR SKIN WEB.

Part: NONE — NONE · airframe 33,789 hrs · 24,378 cycles

MAIN CABIN DOOR IS HARD TO OPEN. CLEANED AND LUBED MCD ROLLERS AND GUIDES. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,515 hrs · 24,140 cycles

LH OVER WING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LH OVER WING EMERGENCY EXIT LIGHT BULB. OPS CHECK SAT

Part: VALVE — MALFUNCTIONED (NR 1 A/C PACK) · airframe 33,468 hrs · 24,100 cycles

PACK 1 VALVE CLOSED MESSAGE 4 TIMES DURING CLIMB. INSPECTED AND FOUND PACK #1 HEAT EXCHANGER HOSE TORN. R&R PACK #1 EAT EXCHANGER HOSE, PACK OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 33,191 hrs · 23,849 cycles

RH FWD OVER WING EMERGENCY LIGHT INOPERATIVE. R&R RH FWD OVER WING EMERGENCY LIGHT. OPS CHECK SAT

Part: CONTROLLER — FAULTED (CABIN TEMP) · airframe 33,190 hrs · 23,847 cycles

SMOKE IN CABIN. PERFORMED GVI OF THE PACK #2 ACM. NO DEFECTS NOTED. DETERMINED THE #2 DIGITAL TEMP CONTROLLER WAS FAULTY. PERFORMED GVI FOR OIL LEAKAGE FROM THE NO 0 CARBON SEAL ON ENGINE #2. NO OIL LEAKS OR DEFECTS NOTED. INSPECTED WATER WASH PORTS ON ENGINE #2. NO OIL OR DEFECTS NOTED. R&R RH DIGITAL TEMP CONTROLLER. OPS CHECK SAT. NO DEFECTS NOTED AT THIS TIME.

Part: SEAT FRAME — CRACKED (SEAT 22A) · airframe 32,956 hrs · 23,630 cycles

SEAT 22A AISLE SIDE FRAME CRACKED. R&R SEAT 22A. OPS CHECK SAT. NO OTHER DEFECTS NOTED.

Part: SEAT FRAME — CRACKED (SEAT 4A) · airframe 32,833 hrs · 23,528 cycles

PAX SEATS 2A, 4A, 5A, 8A, 19A, 23A HAVE CRACKS IN THE RADIUS BELOW ISLE SIDE ARM REST. R&R SEAT. NO OTHER DEFECTS NOTED

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 32,530 hrs · 23,244 cycles

CREW REPORTS CABIN PRESSURE FAIL IN FLIGHT. CABIN ALTITUDE CONTINUED TO CLIMB INTO THE RED TO 10,000 FT IN AUTO BEFORE CREW THEN DESCENDED TO BRING BACK DOWN, NO RAPID LOSS OF PRESSURIZATION. PERFORMED PRESSURIZATION SYSTEM ADJUSTMENTS/TEST. OPERATIONS CHECK SATISFACTORY IN BOTH AUTO AND MANUAL MODES. NO DEFECTS NOTED.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 32,186 hrs · 22,885 cycles

DENT AFT OF MAIN CABIN DOOR 2" FROM DOUBLER. PERFORMED PERMANENT REPAIR OF DENT AFT OF MCD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 32,130 hrs · 22,835 cycles

LH & RH EXTERNAL AFT EMERGENCY LIGHTS INOPERATIVE. R&R BATTERY POWER SUPPLY #4. OPS CHECK SAT.

Part: EXHAUST CONE — MISSING (NR 1 ENGINE) · airframe 30,445 hrs · 21,307 cycles

#1 ENGINE EXHAUST CONE MISSING. R&R #1 ENGINE. OPS AND LEAK CHECK SAT. DOWNLOADED FDR.

Part: HEATER — MALFUNCTIONED (DRAIN NIPPLE) · airframe 29,632 hrs · 20,570 cycles

SMOKE COMING FROM LAV SINK AND BURNING SMELL NOTED. DETERMINED SMOKE/STEAM COMING FROM HEATED DRAIN NIPPLE PULLED AND COLLARED CB E11 LABELED DRAIN HEATERS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,023 hrs · 19,959 cycles

FUSELAGE EXTERNAL SKIN CRACKED AT FR75 APPROXIMATELY 1" BELOW S2L. REPAIRED FUSELAGE EXTERNAL SKIN CRACK AT FR75 STR 2L WITH DOUBLER/FILLER REPAIR.

Part: PROXIMITY SWITCH — BROKEN (NLG) · airframe 29,026 hrs · 19,962 cycles

LG AIR/GND FAIL MESSAGE IN FLIGHT. GEAR WOULD NOT RETRACT. NO THRUST REVERSERS ON LANDING. R&R NOSE LANDING GEAR WOW PROX SWITCH. OPS CHECK SAT AND FOUND NLG IS OVER SERVICED. PERFORMED NLG SERVICE. OPS AND LEAK CHECK SAT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,023 hrs · 19,959 cycles

DAMAGED SKIN BETWEEN FR 59-60 AND BETWEEN STR 11-12L. REPAIRED DAMAGED SKIN BETWEEN FR 59-60 AND BETWEEN STR 11-12L BY CUT OUT, FILLER, DOUBLER FABRICATION AND INSTALLATION. RESTORED SURFACE PROTECTION.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 29,023 hrs · 19,959 cycles

DURING A "C" CHECK AT MAINTENANCE FACILITY. THE FOLLOWING DISCREPANCY WAS NOTED. AIRCRAFT EXTERNAL SKIN HAS SCRATCH BETWEEN FRAME 27-28; AT STRINGER 21R-21L. BLENDED 2 EACH AREAS AREA A 5.200"L X 0.900"W, AREA B 0.740"L X 0.250"W, ORIGINAL SKIN THICKNESS CHEM MILL: 0.032" SKIN 0.050". NO DAMAGED ALLOWED IN THIS AREA. NO CUTOUT REQUIRED ON B. CUT OUT DAMAGED AREA A. FABRICATED REPAIR PARTS, DOUBLER AND FILLER. APPLIED CHEMICAL CONVERSION TO REPAIR PARTS AND REWORKED AREAS. PRIMERED. APPLIED SEALANT. INSTALLED REPAIR WET.

Part: SKIN — TORN (PAX DOOR)

DURING "C" CHECK A TEAR IN SKIN OF PAX DOOR WAS REPORTED BETWEEN STRINGER 10L-12L, 5" AFT OF FWD EDGE. FABRICATED REPAIR DOUBLER AND FILLER. REMOVED DAMAGE, SEALED, INSTALLED REPAIR PART.

Part: TIRE — FAILED (LT MLG) · airframe 28,246 hrs · 19,169 cycles

LT MLG NR 1 AND 2 TIRES BLEW OUT ON TAKEOFF ROLL. R & R THE WHEEL ASSEMBLIES IAW 32-49-02. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,627 hrs · 18,571 cycles

AISLE EMERGENCY LIGHT INOPERATIVE. R & R THE NR 4 INVERTER, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,620 hrs · 18,566 cycles

AISLE EMERGENCY LIGHT INOPERATIVE. R & R THE NR 4 INVERTER.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,610 hrs · 18,555 cycles

AISLE EMERGENCY LIGHT DID NOT ILLUMINATE. ON BACK SIDE. R & R THE SIGN ASSY OPS CHECKED SAT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,304 hrs · 18,268 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE NR 1 AC/DC EMERGENCY LIGHT INVERTER. OPS CHECKED SATISFACTORY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,656 hrs · 17,690 cycles

OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPS CHECKED GOOD. R & R OVERHEAD EMERGENCY EXIT SIGN OPS CHECK GOOD.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS) · airframe 26,612 hrs · 17,641 cycles

NUMEROUS CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE. SECURED AND CONNECTED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 26,535 hrs · 17,563 cycles

EMERGENCY LIGHT OVER ROW 12 INOPERATIVE. SECURED THE BULB, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 26,533 hrs · 17,561 cycles

EMERGENCY LIGHTS ARE INOPERATIVE, FOUND SWITCH IN ON POSITION. CHARGED BATTERIES. ALL OPS CHECK GOOD.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 25,330 hrs · 16,566 cycles

SERVICE DOOR CENTER SILL HAS CORROSION. R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 25,330 hrs · 16,566 cycles

DURING C-CHECK. TOILET WASTE VALVE SUPPORT CORRODED. R & R TOILET VALVE SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MODULE — INOPERATIVE (COCKPIT) · airframe 19,667 hrs · 12,787 cycles

THE CREW REPORTED UNCOMMANDED THRUST CHANGES IN FLIGHT. HE ACFT LANDED WITHOUT INCIDENT. MX R & R THE THRUST RATING SELECTION MODULES, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CENTER LAVATORY) · airframe 19,434 hrs · 12,638 cycles

LAVATORY OMEGA BEAM AND TOP CAP CORRODED BEYOND LIMITS. CUT-OUT CORRODED PORTION OF OMEGA BEAM AND REMOVED TOP CAP. REPAIRED DAMAGE USING PRINCIPALS OF THE SRM 53-21-10. FABRICATED OMEGA BEAM AND DOUBLERS IAW EC5310-01473

Part: FLOOR SUPPORT — CORRODED (CENTER GALLEY) · airframe 19,434 hrs · 12,638 cycles

GALLEY CENTER SPAR CAP CORRODED BEYOND LIMITS. R & R OMEGA BEAM AND TOP CAP.

Part: UNKNOWN — SMOKE (CABIN) · airframe 18,680 hrs · 12,142 cycles

CREW REPORTED LAVATORY SMOKE INDICATION ON EICAS AND SMOKE IN THE CABIN. CONTRACT MX TROUBLESHOT IAW FIM 21-20-00-801A AND FOUND NO VISUAL INDICATIONS OR ODORS THROUGHOUT THE ENTIRE PROCESS. RAN ENGINES AT HIGH POWER WITH INFLIGHT ENGINE BLEED/APU CONFIGURATIONS, NO FAULTS PRESENT. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,472 hrs · 12,013 cycles

DURING MX INSPECTION THE RT OVERWING INTERIOR EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 5 INVERTER WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 17,984 hrs · 11,690 cycles

AFTER TAKEOFF THE CREW RPEORTED SMOKE IN THE CABIN. THE ACFT RETURNED TO LIT WHERE IT LANDED WITHOUT INCIDENT. UPON INSPECTION THE SOURCE OF THE SMOKE WAS FOUND TO BE THE COFFEEMAKER WHICH WERE DEFERRED UNDER AN NEF AND THE ACFT WAS RETURNED TO SERVICE.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 17,985 hrs · 11,689 cycles

DIVERTED, CREW REPORTED SMOKE IN CABIN, STRONGEST IN GALLEY AREA. CONTRACT MX INSPECTED GALLEY AREA AND FOUND COFFEMAKERS TO BE THE CAUSE OF THE SMOKE. R & R THE INBD COFFEEMAKER ASSY WITH OPS CHECKED SUCCESSFUL.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,678 hrs · 11,487 cycles

SMOKE IN CABIN REPORTED. MX RAN ENGINES AND PACK SYS WITH OPS CHECKS SUCCESSFUL, NO SMOKE NOTED AND SUSPECTED GLYCOL INGESTION DURING DE-ICING. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — FAULTY (BLEED) · airframe 12,239 hrs · 7,578 cycles

THE CREW REPORTED A BLD NR2 LOW TEMP MESSAGE IN ICING CONDITIONS. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX REPLACED THE NR2 BLEED PUSHBUTTON SWITCH. OPS CHECKS WERE GOOD.

Part: ENGINE — FAULTY (NR 1) · airframe 11,304 hrs · 6,686 cycles

CLE FLT 5729 THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.

Part: ACTUATOR — FAULTY (RAM AIR VALVE) · airframe 11,303 hrs · 6,684 cycles

ORD FLT 5789 THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT RAM AIR VALVE LINEAR ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: ACTUATOR — FAULTY (RAM AIR VALVE) · airframe 11,303 hrs · 6,684 cycles

ORD FLT 5789 THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT RAM AIR VALVE LINEAR ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — DEFECTIVE (NLG) · airframe 9,376 hrs · 4,922 cycles

LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS WHEN GEAR IS LOWERED AND GOES AWAY AFTER 3 TO 5 SECONDS. REPLACED NOSE LANDING GEAR UPLOCK PROX SWITCH, PERFORMED GEAR SWINGS, NO MESSAGE PRESENT IAW EMB 145 AMM 31-61-02. TEST FLT SATISFACTORY. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT)

FLT 0110 - ELP - FLIGHT CREW REPORTED LOST E1 OIL QTY DROPPED TO 2 QTS, OIL TEMP WENT INTO THE RED ON CLIMB, E1 SHUTDOWN ON ITS OWN. FLIGHT CREW DECLARED EMERGENCY AND LANDED IN ELP WITHOUT INCIDENT, WHERE MX PERSONNEL IS CURRENTLY CHANGING E1. MX PERSONNEL COMPLETED ENGINE 1 R/R OPERATIONALLY CHECKED SATISFACTORY AIRCRAFT WAS RELEASED TO RETURN TO SERVICE. (A)

Part: SEAL — SWOLLEN (LT WING) · airframe 6,841 hrs · 3,594 cycles

FLT 519 - AUS TO MSY - WHILE FLIGHT CREW WAS PERFORMING A PRE-FLIGHT WALK AROUND ENCOUNTER LT WING FUEL LEAK. MX PERSONNEL REMOVED AND REPLACED FUEL PANEL SEAL AND PERFORMED LEAK CHECK GOOD AND A/C WAS RELEASED TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 4,534 hrs · 2,442 cycles

DURING MAINTENANCE INSPECTION ,THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 4,534 hrs · 2,442 cycles

DURING MAINTENANCE INSPECTION ,THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (COCKPIT) · airframe 3,231 hrs · 1,703 cycles

THE CREW REPORTED THAT THE NR 1 WINDSHIELD HEAT CAUSES SMOKE SMELL. WHEN DESLECTED, SMOKE, SMELL GOES AWAY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE NR 1 WINDSHIELD TERMINAL BLOCK, OPERATIONALLY CHECKED WINDSHIELD HEAT AND WAS UNABLE TO DUPLICATE THE SMELL, AND NO OTHER DEFECTS WERE NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.