N553UA

Part: HYDRAULIC LINE — LOOSE (RT SPOILER) · airframe 70,891 hrs · 26,162 cycles

FLUID LEAK UNDER RT WING NEAR FLAP TRACK OTBD OF ENG. FOUND NR 9 SPOILER LINE LOOSE. SECURED LINE THEN PRESSURIZED & LEAK STOPPED.

Part: DOOR — OUT OF SEQUENCE (L2) · airframe 69,304 hrs · 25,654 cycles

L2 DOOR DID NOT CLOSE PROPERLY, INSIDE HANDLE NOT IN PROPER POSITION. FOUND DOOR OUT OF SEQUENCE, CYCLED L2 DOOR SEVERAL TIMES IAW MM. NO DEFECTS FOUND. OK FOR SERVICE.

Part: IGNITER — FAULTY (NR 1 ENGINE) · airframe 68,637 hrs · 25,447 cycles

CREW REPORTED, ENG NR 1, NO START USING NR 1 IGNITION SYSTEM. REPLACED IGNITER AND PERFORMED IGNITION CHECK AND STARTED ENGINE, OPS NORMAL.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,207 hrs · 20,840 cycles

FRAME DENTED, BS 1620 RBL 30, STR 25R-26R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME INBOARD FLANGE AND FABRICATED A REPAIR J-ANGLE AND STRINGER CLIPS PER SRM 53-00-07, REPAIR 5, OUTER J-ANGLE REPAIR AND INSTALLED PER SRM 53-00-07, RPR 5, TABLE II.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,468 hrs · 25,395 cycles

EEL AT AFT LAV IS INOP. REPLACED EEL STRIP, OPS NORMAL.

Part: UNKNOWN — LEAKING (NR 2 ENGINE) · airframe 68,363 hrs · 25,360 cycles

RAMP CREW REPORTING SOMETHING LEAKING FROM NR 2 ENGINE. DETERMINE FLUID TYPE AND LEAK SOURCE. SUSPECT OIL , CLEANED AREA, PERFORMED 5 MIN IDLE RUN NO LEAKS NOTED. OIL TANK FULL, OIL CONSUMPTION NORMAL IAW TOMC. TANK AT 19 QTS.

Part: SEALANT — DAMAGED (LT ENGINE) · airframe 68,309 hrs · 25,343 cycles

LEFT ENGINE HAS STRIP OF MATERIAL HANGING. WHEN VIEWED FROM BEHIND, IT IS 10 O'CLOCK. 10 INCH PIECE OF SILASTIC REMOVED AT 10 O'CLOCK POSITION ON NR 1 ENGINE EXIT CASE LINER OUTER SEGMENT. REPLACED APPLIED SEALANT IAW AMM.

Part: CONNECTOR — DAMAGED (HANDSET) · airframe 68,121 hrs · 25,282 cycles

FLIGHT ATTENDANT HANDSETS ARE HOT TO COCKPIT SPEAKERS. AFTER REPLACEMENT OF CONNECTOR D42P INTERPHONE SYSTEM OPS CHECKS NORMAL.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 68,041 hrs · 25,254 cycles

CREW REPORT: ENGINE 2 LEAKING OIL ON WALK AROUND. REMOVED AND REPLACED DEOILER SEAL IAW MM, OPS CHECK GOOD.

Part: FAILSAFE — CORRODED (BS 1480 FRAME) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT BS 1480 FRAME FAILSAFE BETWEEN S25-27R CORRODED. FABRICATED & INSTALLED REPAIR ANGLE IAW ECRA 5360-01233. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN, BS 1640 FLOORBEAM CORRODED RBL 52-59. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM. REMOVED DAMAGE AND NDT ACP VALIDATING DAMAGE REMOVAL. INSTALLED REPAIR IAW EA 121184 AND ECRA 5310-05536. MAJOR REPAIR.

Part: TEE FITTING — CORRODED (BS 1440) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT CARGO BAY, BS 1440 ABOVE STRINGER 27R, CARGO FLOOR SUPPORT TEE UPPER SURFACE CORRODED. BLENDOUT WAS OUT OF LIMITS PER NDT MANUAL PART 4 SRM 51-00-00 FIG 2. REPLACED TEE FROM BS 1380 TO 1440 AT STR 27 PER SRM 51-40-02.

Part: FAILSAFE — CORRODED (BS 660) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

FORWARD CARGO BAY, BS 660, WL 150, MAIN FRAME, AFT SIDE AT LBL 1, LBL 2 AND LBL 8 HAS AREAS OF CORROSION. AREA BLENDED AND FOUND TO BE OUT OF LIMITS BY NDT. REPLACED THE FAILSAFE AT BS 660 LBL 22 TO RBL 22 PER SRM 51-40-02. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 324-345) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN R1 CREASE BEAM CORRODED AT BS 324 TO 345 INNER ANGLE. FOUND TO BE OUT OF LIMITS PER SRM 51-40-15. MANUFACTURED NEW ANGLE PER DWG 141N5160 AND GMM 07-35-05 PG 5 PAR 7E. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT CARGO BAY BS 1400-1420 RBL 3, INTERCOSTAL CORRODED. FOUND OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02, 51-40-05, GPM 5-4-0-11, 5-4-0-045, SRM 51-20-01 AND DWG 146N5425. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN, R4 DOOR SURROUND CREASE BEAM BOTTOM WEB CORRODED ON THE UPPER AFT EDGE. FOUND TO BE OUT OF LIMITS, OVER 50 PERCENT. REMOVED AND REPLACED CREASE BEAM IAW 51-40-02 AND DWG 146N8742. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1161) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT CABIN FLOORBEAM, BS 1161 BL 0 - LBL 6 CORRODED. REMOVED CORROSION, MATERIAL LOSS EXCEEDED SRM 53-00-51 FIG 101 SH 4 DET III LIMITS. REMOVED DAMAGED AREA OF TEE. ACCOMPLISHED HFEC OF CUTOUT & OPEN HOLE, NO DEFECTS NOTED. FABRICATED & INSTALLED EXTRUSION REPAIR FROM LBL 17 TO RBL 26 IAW ECRA5310-05536 REPAIR 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,112 hrs · 24,941 cycles

SKIN DENTED & GOUGED BS 750 BETWEEN STR 16L & 17L. EVALUATED GOUGE & DENT FOUND EXCEEDING SRM LIMITS. CUT OUT DAMAGE, ACPD HFEC OF CUTOUT & FASTENER HOLES, NO DEFECT NOTED. FABRICATED & INSTALLED REPAIR DOUBLER PER ECRA5330-04355 REV A.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT BILGE BODY FRAME MID CHORD IS CORRODED AT BS 1520 STR 29L-29R, WL 144. MAJOR REPAIR ACCOMPLISHED: MAINT TEXT: REMOVED CORRODED MATERIAL LOSS EXCEED SRM 53-00-07 LIMITS. ACPD HFEC BLENDED AREA & OPEN HOLE PER NDT 51-00-19 & 51-00-1 6, NO DEFECT NOTED. FAB & INSTALLED REPAIR ANGLE PER ECRA 5360-01232.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

CABIN FLOORBEAM TEE CORRODED BS 324 RBL 39-61. REMOVED CORROSION, MATERIAL LOSS EXCEEDED SRM LIMITS. FABRICATED & INSTALLED TEE SPLICE REPAIR FROM BL 0 TO RBL 65 IAW SRM 53-10-08 REPAIR 1. FORMED ANGLE REPAIR FROM RBL 39 TO RBL 61 WITH STRAP SPLICE AT RBL 39.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,112 hrs · 24,941 cycles

FUSE SKIN AT BS 1500-1520 LBL 3 THE .025" HOLES COMMON TO INTERCOSTAL HAVE KNIFE EDGE COND. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE, ACPD HFEC, NO DEFECT NOTED. FABRICATED & INSTALLED REPAIR DOUBLER & FILLER PER SRM 53-00-01 REPAIR 3 PG 201. THIS IS A CAT B REPAIR WITH RE-INSPECT WITHIN 37,500 FLIGHT CYCLE.

Part: CREASE BEAM — CORRODED (BS 345-365.25) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN R1 CREASE BEAM CORRODED AT BS 345-365.25. FOUND CORROSION OUT OF LIMITS. REMOVED AND INSTALLED NEW ANGLE CREASE BEAM IAW SRM. MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,112 hrs · 24,941 cycles

MAJOR REPAIR. EXT FUSE SKIN TOOLING DAMAGE STA 1620 BETWEEN STR 28L & 29L. MAJOR REPAIR ACCOMPLISHED: MAINT TEXT: DAMAGE FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE, ACPD HFEC. NO DEFECT NOTED. FAB & INSTALLED DOUBLER & FILLER PER ECRA5360-01226. THIS REPAIR RECEIVED SECOND STAGE FAA APPROVAL. FULL COMPLIANCE HAS NOT BEEN EVALUATED. A NEW 8100-9 REQUIRE PRIOR TO 34,400 PTC.

Part: FLOOR SUPPORT — CORRODED (BS 686) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

FORWARD CARGO BAY, BS 686 RBL 11 HAS AREA OF CORROSION ON FLOOR SUPPORT. FLOOR SUPPORT CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53. REMOVED AND REPLACED FLOOR SUPPORT IAW DWG 143N5320 AND SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN, BS 1681 FLOORBEAM CORRODED UNDER FASTENER HOLE INBD OF R4 CREASE BEAM. REMOVED CORROSION AND FOUND OUT OF LIMITS. CUT OUT DAMAGE AND NDT PERFORMED AND CONFIRMED NO DAMAGE REMAINS. FABRICATED AND INSTALLED REPAIR ANGLES. MAJOR REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT CARGO COMP AT BS 1420 RBL 21- LBL 5 FRAME IS CORRODED ON INNER CHORD AND WEB IN SEVERAL PLACES REF CORR TASK CARD C53-156-02 AND C53-155-02. MAJOR REPAIR ACCOMPLISHED: DUE TO CORROSION OUT OF LIMITS, REMOVED AND REPLACED FRAME AT STA 1420 STR 24L TO 24R IAW BACO DWG 146N1012, SRM 51-40-02,

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 1,122,176 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE BS 1460 RBL 23 INTERCOSTAL BELOW Z-ANGLE IS CRACKED AND HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REPLACED THE INTERCOSTAL Z-ANGLE AT STA 1460 RBL 23 PER SRM 51-40-02 & FABRICATED NEW INTERCOSTAL PER BAC DWG 146N8522.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,112 hrs · 24,941 cycles

EXTERNAL PROTRUSION AT BS 1600 PLUS 17, 1.25 INCHES BELOW STR 27R. MAJOR REPAIR ACCOMPLISHED: EXTERNAL FUSELAGE DENTED AT STA 1600 PLUS 17 1.25 INCHES BELOW STR 27 MEASURED DEPTH Y= .035, AY=32.5. DENT FOUND TO BE WITHIN LIMITS PER SRM 53-00-01 FIG 101 SHEET 4 DETAIL III. ACCOMPLISHED HFEC NO CRACKS NOTED.

Part: FAILSAFE — CORRODED (BS 1440 FRAME) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT CARGO BAY, BS 1440 FRAME AT BL 0 FAILSAFE FOUND CORRODED. BLENDED CORROSION, MATERIAL LOSS EXCEEDED SRM LIMITS. NDT BLENDED AREA & OPEN HOLES, NO DEFECTS NOTED. FABRICATED & INSTALLED REPAIR ANGLE IAW ECRA5360-01228.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,112 hrs · 24,941 cycles

SKIN DENTED AT BS 1536, 1.5" ABOVE S15L. MEASURED DENT, FOUND OUT SRM 53-00-01 LIMITS. CUT OUT DAMAGE, HFEC PER 51-00-19, NO DEFECT NOTED. FABRICATED & INSTALLED REPAIR DOUBLER & FILLER PER SRM 53-00-01 REPAIR 3 PG 201. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN, BS 365.25 FLOORBEAM CORRODED BL 0-RBL 24. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED DAMAGE AND NDT ACCOMPLISHED TO VALIDATE ALL DAMAGE REMOVED. INSTALLED REPAIR ANGLE IAW ECRA 5310-05538. MAJOR REPAIR.

Part: DOOR — OUT OF POSITION (L2) · airframe 67,112 hrs · 24,941 cycles

L2 DOOR ARM DISARM LEVER BINDING WHEN OPERATED. FOUND ARM DISARM INDICATOR SLIDING DOOR OUT OF TRACK CAUSING BINDING. RE-INSTALLED SLIDING DOOR BACK ON TRACK AND OPS CHECKED GOOD PER AMM 52-11-02 AND AMM 52-11-25.

Part: FAILSAFE — CORRODED (BS 1500) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT BILGE, BS 1500 FRAME FAILSAFE CORRODED. REMOVED CORROSION FROM FAILSAFE BETWEEN STR 29L & 29R. MATERIAL LOSS EXCEEDED SRM 53-00-07 LIMITS. ACCOMPLISHED HFEC OF BLENDED AREA & OPEN HOLES, NO DEFECT NOTED. FABRICATED & INSTALLED REPAIR ANGLE PER ECRA 5360-01231.

Part: FRAME — CORRODED (BS 1480) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT CARGO BAY BS 1480 FRAME S25-27R FOUND CORRODED. BLENDED CORROSION, MATERIAL LOSS FOUND EXCEEDING SRM LIMITS. ACCOMPLISHED HFEC OF BLENDED AREA & OPEN HOLES, NO DEFECTS NOTED. FABRICATED & INSTALLED REPAIR ANGLE IAW ECRA5360-01233. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

CREASE BEAM INTERCOSTAL CORRODED AT L4 DOOR, FWD & AFT OF DOOR DRAINS. REMOVED CORROSION, MATERIAL LOSS FOUND TO EXCEED SRM 53-60-13. FABRICATED AND INSTALLED CREASE BEAM INTERCOSTAL PER DRAWING 146N5230 & SRM 51-40-02. MAJOR REPAIR.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN, BS 1640 TO 1680 RBL 52 INBOARD OF R4 DOOR C CHANNEL UNDER DRAIN PAN CORRODED. REMOVED CHANNEL AND FOUND OUT OF LIMITS. INSTALLED NEW CHANNELS IAW SRM AND DRAWING 146N5230. MAJOR REPAIR.

Part: LEAD — BROKEN (CABIN) · airframe 67,112 hrs · 24,941 cycles

CABIN SEAT ROW 12 LEFT POWER LEAD IN WIRE BROKEN FOR EMERGENCY ESCAPE LIGHTING. REPLACED EMERGENCY ESCAPE POWER LEADER FOR EEL SYSTEM AND OPS CHECKED EMERGENCY LIGHTS IAW AMM. OPS CHECK GOOD M10813 STA 930 WL 217 LBL 70 WDM 33-51- 21 PG 1.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

AFT CARGO BAY AT BS 1410 LBL 20 SUPPORT ANGLE IS CORRODED ON LOWER SIDE. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM. REPLACED SPLICE ANGLE WITH NEW IAW DWG 146N5390 AND SRM 51-40-02. MAJOR REPAIR.

Part: WIRE — MISREPAIRED (EMERGENCY LIGHTS) · airframe 67,112 hrs · 24,941 cycles

AFT EMERGENCY LIGHT TEST SWITCH WIRE W3534003722 AT BS 1656 WL 286. TERMINAL END HAS IMPROPER CRIMP FROM PREVIOUS REPAIR. REPLACED TERMINAL END OF AFT EMERGENCY LIGHT TEST SWITCH IAW SWPM 20-30-11, WDM 33-51-15, WIRE W3534003722. TESTED GOOD IAW AMM 33-55-01.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN, BS 365 FLOOR CHANNEL CORRODED FWD END RBL 26. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS. REPAIRED AND INSTALLED DOUBLER AT BS 365.25 RBL 26 IAW AMM 53-20-98. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

R1 DOOR CREASE BEAM WEB CORRODED. REMOVED, FABRICATED & INSTALLED NEW WEB CREASE BEAM WEB IAW DWG 141N8422 AND SRM 51-40-02 AND SRM 51-40-05. MAJOR REPAIR.

Part: SKIN — WORN (E&E DOOR) · airframe 67,112 hrs · 24,941 cycles

E&E DOOR EXTERNAL HANDLE CUTOUT HAS WEAR GROOVE ON EDGE. E&E COMPARTMENT DOOR OUTER SKIN GOUGE REPAIRED IAW EA 121167 REV IR AND ECRA 5240-01669.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

CABIN FLOOR SHEAR WEB AT BS 1681 RBL 50 REQUIRES REMOVAL DUE TO FLOORBEAM ACCESS. MAJOR REPAIR ACCOMPLISHED: REMOVED SHEAR WEB DOUBLER REPAIR AT BS 1681 TO EVALUATE CORROSION ON SHEAR WEB. REMOVED CORROSION. FABRICATED & INSTALLED REPAIR DOUBLER PER ECRA 5330-04259 & SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN, BS 365.25 FLOOR CHANNEL CORRODED AT FWD END RBL 45. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS DUE TO 90% MATERIAL LOSS. FABRICATED AND INSTALLED REPAIR DOUBLER, PRIMED, PAINTED, AND CIC AREA IAW AMM 53-20- 98 AND 51-10-02 AT BS 365.25 RBL 45. MAJOR REPAIR.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,112 hrs · 24,941 cycles

PASSENGER CABIN, R4 DOOR SURROUND FWD FRAME BOTTOM ANGLE CORRODED ABOVE WEB. REMOVED & REPLACED BOTTOM ANGLE DUE TO MATERIAL LOSS GREATER THAN 50%. NEW ANGLE INSTALLED IAW SRM 51-40-02 AND DWG 146N8722. MAJOR REPAIR.

Part: FRAME — CORRODED (BS1460 LBL 15- R) · airframe 67,112 hrs · 24,941 cycles

AFT PIT BS 1460 LBL 15 TO RBL 5 WL 138 FRAME HAVE CORROSION ON BOTH FWD AND AFT SIDE. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE EXCEEDING SRM 53-00-07 LIMITS. FABRICATED & INSTALLED NEW FRAME PER SRM AND BOEING DWG 146N1014.

Part: BATTERY — FAULTY (MAIN) · airframe 66,524 hrs · 24,735 cycles

STATUS MESSAGE MAIN BATTERY CHARGER DISPLAYED IN FLT. REPLACED "MAIN BATTERY" PER AMM.

Part: BATTERY — DISCHARGED (MASTER) · airframe 66,272 hrs · 24,649 cycles

MAIN BATTERY CHARGES STATUS MESSAGE. REMOVED AND REPLACED MAIN BATTERY AND REMOVED AND REPLACED MAIN BATTERY CHARGER.

Part: COWLING — DENTED (RT ENGINE) · airframe 66,174 hrs · 24,613 cycles

CREW REPORT: DENT ON RT ENGINE COWLING BEHIND OIL SERVICE DOOR SAMC TEXT: LCL MAINT REPORTS: NR 2 ENGINE LEFT FAN COWL HAS A SMOOTH DENT APPROX 9.0\L X 6.0\W X 0.03125\DEEP, LOCATED AFT OF OIL SERVICE ACCESS PANEL, NO DELAMINATION, CRACKS OR CREASE. BEYOND ALLOWABLE DAMAGE LIMITS OF SRM 54-21-01 PAGE 101-102. (INSPECTED INSIDE OF FAN COWL, NO DAMAGE NOTED) OPBLM .18JUN12 ACCOMPLISHED INTERIM SPEED TAPE REPAIR PER EC-RA 5450-01962, CHECK TAPE CONDITION ONCE DAILY, ACCOMPLISH PERMANENT REPAIR WITHIN 150HRS.

Part: STRUCTURE — DENTED (RT COWLING) · airframe 66,174 hrs · 24,613 cycles

CREW REPORT, DENT ON RIGHT ENGINE COWLING BEHIND OIL SERVICE DOOR SAMC TEXT: MAINT REPORTS, NR 2 ENGINE LEFT FAN COWL HAS A SMOOTH DENT APROX 9.0\L X 6.0\W X 0.03125\DEEP, LOCATED AFT OF OIL SERVICE ACCESS PANEL, NO DELAMINATION, CRACKS OR CREASE. BEYOND ALLOWABLE DAMAGE LIMITS OF SRM 54-21-01 PAGE 101-102. (INSPECTED INSIDE OF FAN COWL, NO DAMAGE NOTED) OPBLM TOMC-.18JUN12. ACCOMPLISHED INTERIM SPEED TAPE REPAIR PER EC-RA 5450-01962, CHECK TAPE CONDITION ONCE DAILY, ACCOMPLISH PERMANENT REPAIR WITHIN 150HRS. WORK ACCOMPLISHED BY LCL MAINT. OPBLM TOMC-18JUN12.

Part: PACKING — LEAKING (VALVE) · airframe 66,023 hrs · 24,567 cycles

FLAP SLAT DEPRESS VALVE LEAKING. REPLACED PACKINGS, OPS CHECKED NORMAL. RESERVE SYSTEM HYD, NO LEAKS.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 65,315 hrs · 24,322 cycles

DOOR 4 LEFT EMERGENCY OUTSIDE SLIDE LIGHT INOP. LIGHT SOCKET MOUNTS ARE DAMAGED WILL NEED NUT PLATES SECURED. FOUND HIGH RESISTENCE PIN 9- LIGHT SOCKET SUSPECT BAD CONNECTOR D4504 REF WD 33-51-15 MAY REQUIRE AFT-AFT LAV REMOVAL. CONFIRMED 2K OHMS TO GND PIN 9. FOUND PUSHED BACK PIN ON CONNECTOR D4504, REINSERTED PIN, REPLACED POWER SUPPLY FUSE. RPL'D BROKEN NUT CLIPS ON BRACKET. LIGHT OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,889 hrs · 24,167 cycles

DURING TEST OF EMERGENCY LIGHTS, FLOOR LIGHTS INOPERATIVE. REPLACED POWER SUPPLIES M735 AND M10699. FLOOR EMERGENCY AISLE LIGHTS CHECKED GOOD. RELAMPED EMERGENCY LIGHT AT SEAT 5F, OPS CHECKED OK

Part: WIRE — OUT OF POSITION (CABIN) · airframe 64,887 hrs · 24,166 cycles

THE 4 LT EXTERIOR FUSELAGE EMERGENCY EXIT LIGHT INOP. FOUND SECTION OF EMERGENCY AISLE LIGHTS, AND ONE EMER EXIT LIGHT AND SIGN LIGHT AND DOOR 4L EXT LIGHT IS OUT. ALL RECEIVE POWER FROM M10818 POWER SUPPLY, REF WDM 33-51-15 PG 1. (ON ORDER B29). FOUND OPEN IN WIRE W3534-0109-16 BETWEEN CONNECTOR D6638, PIN 9 AND LIGHT ASSY L56. FOUND WIRE WRAPPED TOO TIGHT AND CONNECTOR NOT CONNECTED ALL THE WAY. REPOSITION WIRE AND RECONNECTED CONNECTOR, RESISTANCE AND OPS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (R4 DOOR) · airframe 64,030 hrs · 23,855 cycles

RIGHT AFT ENTRY DOOR LIGHT INTERMITTENT. ENTRY DOOR 4R EICAS MESSAGE AND OVERHEAD LIGHT ON WITH DOOR CLOSED. VERIFIED DOOR IS CLOSED AND DOOR SLIDE ARMS PROPERLY PER

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,638 hrs · 23,715 cycles

DOOR 1R SLIDE LIGHT DOES NOT ILLUMINATE. RELAMPED AND SLIDE LIGHT WORKED PROPERLY.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 63,597 hrs · 23,700 cycles

EMERGENCY EXIT FLOOR LIGHTING IS INOP FROM SEAT ROW 21 TO SEAT ROW 27. RE-ATTACHED CONNECTOR AND INSTALLED NEW TRACK COVER.

Part: WINDOW — BURNED (COCKPIT) · airframe 63,316 hrs · 23,593 cycles

COCKPIT WINDOW L-1 HAS SMALL BURN MARK ON LOWER EDGE TOWARD THE RIGHT. REPLACED THE L1 WINDOW PER MM.

Part: HINGE — DEFECTIVE (CEILING PANEL) · airframe 63,311 hrs · 23,592 cycles

CEILING PANEL DISLODGED AT ROW 39-40 IN MOD TURB. REPLACED HINGE AND LATCH.

Part: NOSE COWL — DAMAGED (NR 1 ENGINE) · airframe 62,838 hrs · 23,418 cycles

NR 1 ENGINE CONTACTED LOADING BRIDGE ON ARRIVAL TO GATE. REPLACED NOSE COWL.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 62,778 hrs · 23,394 cycles

FO WINDOW LOWER LEFT CORNER APPROX 3-4 INCH RADIUS CLOUDY WHITE COLOR ARCING IN AREA OF DELAMINATION AND DISCOLORATION. OLD WINDOW REMOVED, NEW IS INSTALLED AND FIRST TORQUE ACCOMPLISHED. SLING WAS NOT USED. NEED TO CONTINUE FROM AMM STEP (12) (B) TO COMPLETION. NEED TO ACCOMPLISH STEP 20,21,22 OF MM. COMPLETED WINDSHIELD INSTALLATION.

Part: FILTER — FAULTY (COCKPIT) · airframe 62,569 hrs · 23,322 cycles

FLT DECK NOISE. DUE TO CHRONIC FLT DECK NOISE ISSUES WITH REPORTS OF BLOCKAGE IN THE CABIN OVERHEAD DISTRIBUTION DUCTS AND THE CABIN SIDEWALL OUTLETS NEED TO ACP THE FOLLOWING: CLEAN THE CABIN OVERHEAD DUCTS. CLEAN THE CABIN SIDEWALL OUTLETS, VALIDATE SIDEWALL OUTLETS ARE CLEAN WITH VIDEO PROBE. TAKE NOISE AND AIRFLOW LEVEL CKS REF SVC TIP BEFORE AND AFTER CLEANING (AIRFLOW METER 056-1535, SOUND METER 056-0698). AFTER CLEANING WITH PACKS ON & BOTH RECIRC FANS ON CK FOR PROPER AIRFLOW AT ENTIRE OVERHEAD DUCT RUN & ALL SIDEWALL OUTLETS. CLEANED DIRTY SIDEWALLS ROW 32, 33, 34. PICS ON RVMS SITE. DBS BEFORE 71 AND 73, AFTER CLN AND EE FILTER CHANGE (170-3699) DBS 70 WITH LT AND 71 WITH BOTH FANS ON. EVERYTHING ELSE ON DUCTS CLEAN. DBS VERY LOW IN FLT DECK.

Part: WIRE — BROKEN (FUEL SYSTEM) · airframe 62,167 hrs · 23,170 cycles

FUELER REPORTS THAT AUTO PRERELT DOES NOT WORK. FOUND WIRE OPEN BETWEEN D40324J -PIN 22 OF FUELING PANEL DISCONNECT P28 AND D2440A -PIN D8 OF M121 FUEL QTY PRO UNIT. ISOLATED PROBLEM TO BETWEEN D40328P-PIN 22 AND D42344P-PIN 22. FOUND WIRE W3484-4002Y-18 BROKEN ONE AND A HALF FEET FROM CONN. D40328, REPAIRED SAME WITH ENVIRONMENTAL SPLICE. DISCONNECTED CONNECTORS D42344, D40328 AND D40324 FOR T-S OF DF948. REINSTALLED CONNECTORS.

Part: VALVE — FAULTY (AC PACK) · airframe 61,825 hrs · 23,034 cycles

PACK ISSUE, FLIGHT DIVERTED. LT PACK WENT FULL HOT ON CLIMBOUT. WENT MANCOLD, NO HELP. TEMP WAS UNBEARABLY HOT AIR CHRON. HAS HISTORY NO FAULTS ON PACK OR ZONE CONTROLLERS. NO TIME TO TROUBLESHOOT. PACK WILL RUN HOT INTERMITTENTLY. PROBLEM STARTED AFTER HEAT EXCH AND COND WERE REPLACED & LAX FOUND PACK INLET OBSTRUCTED. SUGGEST INSP HEAT EXCH FOR FOD AND CHECKING LOW LIMIT VALVE FOR PROPER OPERATION. REPLACED ZONE TEMP SELECTOR. OPERATED PACK SYS ALL WORKED NORMAL.

Part: UNKNOWN — MALFUNCTIONED (L2 DOOR) · airframe 61,813 hrs · 23,029 cycles

CREW REPORT: DOOR 2L NOT ARMING PROPERLY. CHECKED DOOR ARMING OPERATION. DOOR ARMS NORMALLY EXCEPT SLIDE INDICATOR DOES NOT POP OUT. SLIDE ARMED LIGHT OPS NORMALLY AND GIRT BAR ENGAGES. DOOR DISARMS NORMALLY. STICKER APPLIED PER MEL 2566F.

Part: PITOT LINE — UNKNOWN (NR 2) · airframe 60,353 hrs · 22,498 cycles

REPLACE AUX 2 PITOT LINE WHERE THE PERMA SWAGE REPAIR WAS PREVIOUSLY INSTALLED. REPLACED AUX 2 PITOT AND ACCOMPLISHED LEAK TEST, NO LEAKS FOUND.

Part: SWITCH — FAULTY (CONTROL PANEL) · airframe 60,345 hrs · 22,493 cycles

MAIN BATT CHARGER MSG SEVERAL REPORTS OF MAIN BATT CHARGER STATUS MSG. REPLACE STANDBY POWER SWITCH ON P5 PANEL. R & R STANDBY POWER CONTROL PANEL IAW MM. OPS CHECK GOOD.

Part: DUCT — DAMAGED (SEAT ROW 13) · airframe 60,345 hrs · 22,492 cycles

LOUD NOISE AND TURBULENT SOUNDING AIR FLOW COMING FROM THE CEILING PANEL AND VIDEO MONITOR AT SEAT ROW 13. FIBERGLASS INSULATION DEBRIS NOTICED IN AREA. REMOVED CEILING PANELS AND FOUND OVERHEAD DUCT AT ROW 10 HAS ABOUT 6 INCH HOLE IN TOP SIDE OF DUCT. HOLE IS APPROX MID OF RIGHT SIDE TOP. REPAIRED DUCT LEAK AND ACCMP'D THE OVERHEAD DUCT COA. NO LEAKS NOTED.

Part: LEVER — BINDING (R4 DOOR) · airframe 60,134 hrs · 22,412 cycles

4R ARM LEVER BINDS. DISCONNECTED LOWER PUSHROD "D", NO HELP. DISCONNECTED PUSHROD "A" TO TRIGGER PIN MECH. NO HELP. DISCONNECTED PUSHROD "C" BINDING STOPPED. ISOLATED BINDING TO TORQUE SHAFT. FOUND ALL PUSH RODS RECONNECTED. CLEANED AND LUBED PUSHRODS AND LINKAGES. GRD CKS NORMAL. DOOR 4R REQUIRES VERIFICATION OF PROPER RIGGING DUE TO DISCONNECT AND RECONNECT OF TORQUE TUBES AND LINKAGES. ACP SAFETY AND SECURITY PER MM, NO DEFECTS FOUND.

Part: ACTUATOR — MALFUNCTIONED (FLAP/SLAT SYSTEM) · airframe 60,122 hrs · 22,409 cycles

FLAP SLAT DISAGREE, FLIGHT DIVERTED. LOCKED OUT BETWEEN 0 AND 1 AFTER TAKE OFF. L/E SLAT DISAGREE DISPLAYED ON EICAS. CREW ACCOMPLISHED IRREGULAR PROCEDURE 14.70.5. FOUND NR 6 ROTARY ACTUATOR INDICATOR POPPED. REPLACED NR 6 L/E SLAT DRIVE ROTARY ACTUATOR, OPS CHECK OK.

Part: TRANSMITTER — FAILED (SLATS) · airframe 60,106 hrs · 22,402 cycles

L/E SLAT DISAGREE MSG, RTFL. REPLACED LT FLAP POS TRANSMITTER PER AMM. TRANSMITTER TESTS OKAY PER AMM. OPERATED FLAPS AND SLATS SEVERAL TIMES, CHECKS OKAY.

Part: ATTACH FITTING — DAMAGED (R2 GIRT BAR) · airframe 59,876 hrs · 22,313 cycles

CANNOT DISARM 2R. REPAIRED AFT GIRT BAR CLIP AT DOOR 2R, OPERATIONAL CHECK OF ARMING HANDLE NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,698 hrs · 22,246 cycles

SEVERAL AISLE EMERGENCY LIGHT INOP NEAR SEAT 22C AND SOME EEL IN THE AREA. FOUND BATTERY PACK WEAK AT 23ABC. BATTERY ASSY REMOVED FROM OVERHEAD UNIT. REPLACED BATTERY ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,335 hrs · 22,106 cycles

EEL STRIP IN FRONT OF AFT LAV DOOR INOPERATIVE. REPLACED EEL STRIP, CHECK OKAY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,335 hrs · 22,106 cycles

EEL STRIP SECTION AT FWD END OF COACH INOPERATIVE. REPLACED BATTERY, CHECKS OKAY.

Part: SLIDE — DEPLOYED (R4 DOOR) · airframe 59,328 hrs · 22,103 cycles

RIGHT AFT NR 4 DOOR SLIDE (GALLEY DOOR) DEPLOYED, REPORTED BY RAMP. REMOVED DEPLOYED SLIDE. SECURED DOOR & COVER. REPLACED RIGHT AFT DOOR NR 4 SLIDE.

Part: LINKAGE — DAMAGED (GIRT BAR) · airframe 58,566 hrs · 21,801 cycles

DOOR 3L WILL NOT ARM. FOUND SHEARED BOLT IN ARMING MECHANISM. WILL NEED BOLT, WASHERS & NUT. REPLACED BOLT, NUT, WASHER AND COTTER PIN FOR SLIDE ARM LINKAGE AT GIRT BAR. DOOR OPS NORMAL.

Part: WIRE HARNESS — CORRODED (NR 1 GENERATOR) · airframe 58,043 hrs · 21,584 cycles

NR 1 GEN TRIPPED OFF LINE, FLIGHT DIVERTED. FOUND IDG WIRE HARNESS CORROSION AT NR 1 IDG. ONE PIN & SOCKET CORRODED AT FIREWALL CONNECTION. REPLACED TERMINAL BLOCK AT IDG. NR 1 IDG OPS CHECKED GOOD. REPLACED GCU. ALL OPS NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,992 hrs · 21,568 cycles

EXTERIOR SLIDE LIGHT AT DOOR 2 LT INOP. RELAMPED LIGHT, OP CHECK GOOD.

Part: RELAY — FAULTED (TAT PROBE) · airframe 57,796 hrs · 21,493 cycles

TAT PROBE EICAS, RTFL. TRIED RELAY K400 IN K410 CURRENT SENSING RELAY POSITION, NO HELP. RE-INSTALLED K400 RELAY IN ORIGINAL POSITION AND PERFORMED RIGHT ANGLE OF ATTACK PROBE HEAT ADJUSTMENT AND TEST, CHECKS GOOD. RE-INSTALLED K410 IN ORIGINAL POSITION, STILL TAT LIGHT ON OVERHEAD PANEL WILL NOT TEST. CHECKED POWER AT CIRCUIT BREAKER R25 FOR TAT PROBE. TAT PROBE DOES NOT HEAT DURING TEST. REPLACED TAT PROBE. ACP'D AFDS TESTS, CHECKS OK. VERIFIED K410 RELAY IS BAD. REPLACED K410. ACP OPS CHECK. CHECKED OKAY.

Part: LAVATORY — OVERFLOW · airframe 57,505 hrs · 21,372 cycles

LAV OVERFLOW, FLIGHT DIVERTED. SERVICED ALL LAVS.

Part: LENS — MISSING (SEAT 1A-B) · airframe 57,010 hrs · 21,166 cycles

EMERGENCY EXIT ILLUM LIGHT OVER SEAT 1A-B MISSING COVER.

Part: TRACK — DIRTY (L2 DOOR) · airframe 56,276 hrs · 20,869 cycles

DOOR 2L WILL NOT ARM. CLEANED AND LUBD SLIDE DOOR TRACKS. OPERATED SEVERAL TIMES. SLIDE ARMS NORMAL

Part: SKIN — DENTED (FUSELAGE) · airframe 56,207 hrs · 20,840 cycles

EXTERNAL FUSELAGE SKIN DENT BEHIND R-4 DOOR, BS 1700, STR 11R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER RPR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,207 hrs · 20,840 cycles

CORROSION ON SKIN AREA BS 1616-1625 STR 29L-29R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN SPLICE PLATE AND FABRICATED A NEW SKIN SPLICE PLATE AND A NEW STRINGER (DUE TO EXCESSIVE MATERIAL LOSS LOCATED BS 1620 BETWEEN S29L-S30).

Part: FRAME — DENTED (FUSELAGE) · airframe 56,207 hrs · 20,840 cycles

FRAME DENTED, BS 1620 RBL 30, STR 25R-26R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME INBOARD FLANGE AND FABRICATED & INSTALLED A REPAIR J-ANGLE (OUTER) AND STRINGER CLIPS.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,207 hrs · 20,840 cycles

AFT OF BULK PIT, STA 1681, LBL 10 SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SHEAR TIE AND FABRICATED & INSTALLED A NEW SHEAR TIE.

Part: STRUCTURE — MISREPAIRED (R2 DOOR) · airframe 56,207 hrs · 20,840 cycles

MED 2R UPPER HINGE ARM CUTOUT REQUIRES REPLACEMENT DOUBLER. MAJOR REPAIR ACCOMPLISHED. REMOVED PREVIOUS INCORRECT REPAIR AND INSTALLED DOUBLER REPAIR.

Part: SLIDE — UNSERVICEABLE (OVERWING EXIT) · airframe 56,207 hrs · 20,840 cycles

LT OVERWING SLIDE IS UNRAVELED IN CARRIER. REPLACED LT OVERWING SLIDE.

Part: SLIDE — UNSERVICEABLE (OVERWING EXIT) · airframe 56,207 hrs · 20,840 cycles

RT OVERWING SLIDE IS UNRAVELED. INSTALLED NEW RT OVERWING SLIDE PACK.

Part: DOOR FRAME — DAMAGED (L2 DOOR) · airframe 56,207 hrs · 20,840 cycles

L-2 DOOR REQUIRES FRAME DOUBLER. HFEC INSP OF UPPER HINGE CUTOUT ACCOMPLISHED, NO CRACKS NOTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOOR FRAME DOUBLER AT UPPER HINGE CUTOUT.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,207 hrs · 20,840 cycles

FRAME AT STA 580, STR 24L IS DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,207 hrs · 20,840 cycles

FRAME DENTED STA 600, AT STR 25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER REPAIR.

Part: FUEL FILTER — DIRTY (NR 1 ENGINE) · airframe 55,608 hrs · 20,606 cycles

L ENG FUEL FILTER LIGHT ILLUMINATED. RTFL. REPLACED NR 1 FUEL FILTER. RAN ENGINE, NO LEAKS FOUND AT THIS TIME. OP CHECKS GOOD. NO FAULTS. ACFT OK FOR SERVICE.

Part: SLIDE — UNSERVICEABLE

BOTTLE INADEQUATE. OUTSIDE SERVICE STATION MISTAKE. OVERHAUL AND REPACK SLIDE PER CMM.

Part: GIRT BAR — BROKEN (R3 DOOR) · airframe 54,948 hrs · 20,355 cycles

GIRT BAR DOOR 3R BROKE. INSTALLED NEW GIRT BAR. OPS CHECKED NORMAL.

Part: NOSE COWL — DELAMINATED (NR 2) · airframe 54,945 hrs · 20,353 cycles

WHILE PROCESSING THE AC FOR PAINT, A DELAM INATED AREA WAS FOUND AT THE 10 O'CLOCK POSITION ON THE INBOARD SIDE OF THE NR 2 NOSE COWL. COMPLETELY UN-NOTICABLE VISUALLY FROM THE OUTSIDE. AREA IS 18 INCHES BY 18 INCHES. THERE ARE NO DEPRESSIONS, OR ANY OTHER VISUAL DEFECTS. ASSUME THE HONEYCOMB LAYER HAS DISBONDED FROM THE OUTER SKIN. REPLACED NR 2 ENG NOSE COWL.

Part: GIRT BAR — OUT OF ALIGNMENT (R3 DOOR SLIDE) · airframe 54,893 hrs · 20,333 cycles

DOOR 3R ARMING LIGHT WILL NOT ILLUMINATE. FOUND GIRT BAR OUT OF ALIGNMENT. REALIGNED GIRT BAR. OPS CHECKED GOOD.

Part: WIRE HARNESS — SHORTED (WEATHER RADAR) · airframe 53,968 hrs · 20,012 cycles

CREW REPORT: WX FAIL RADAR SAMC TEXT: ANTENNA MSG ON BOTTOM OF SCREEN. RESET CB TO TRANCVR UNIT, NO HELP. HARNESS SHORTED FROM FWD BULKHEAD TO SCANNER. REPLACED HARNESS.

Part: PDU — MALFUNCTIONED (RUDDER) · airframe 53,085 hrs · 19,671 cycles

A/C REQUIRES 4 UNITS R RUDDER TRIM, A-S 255 IAS FL370 CRUISE 4.0 RWD. REPLACED RUDDER RATIO CHANGER, PREVIOUSLY REPLACED TE FLAP PDU CONTROL VALVE OUTBD CHECK VALVE ADJUSTED RIG OF RUDDER RATIO CHANGER, RUDDER RIG FOUND TO BE OUT OF LIMITS ADJUSTED POGO ROD OF RATIO CHANGER, REPLACED LOWER RUDDER PCU.

Part: PROXIMITY SWITCH — FAULTY (L4 DOOR SLIDE) · airframe 51,749 hrs · 19,199 cycles

DOOR 4L THE SLIDE ARM LIGHT WON'T COME ON.

Part: EEC — MALFUNCTIONED (ENGINE) · airframe 51,547 hrs · 19,129 cycles

A-T DISCONNECTED FL380 IN CRUISE. CURRENT FAULT SHOWS AUTO DISC EEC L- PRIMARY. REPLACED LEFT EEC. NO FURTHER MAINTENANCE ACTION NEEDED.

Part: BOTTLE — LOW PRESSURE (L3 DOOR) · airframe 50,481 hrs · 18,745 cycles

DOOR 3L OPEN ASSIST PRESSURE IS IN RED ZONE. [SUP 06-06-07] REPLACED BOTTLE.

Part: ENGINE — MAKING METAL (NR 2) · airframe 50,477 hrs · 18,743 cycles

DIVERTED DUE TO RIGHT ENGINE OIL FILTER PRESSURE INDICATOR. AMBER ALERT DECLARED. NR 2 ENG MAIN OIL FILTER HAS LARGE QTY OF FERROUS FLAKES. [SUP 06-06-07] ALSO CHECKED NR 123 AND NR 5 BEARING C-D'S AND FOUND EXCESSIVE MATERIAL. FILTER AND C'D'S REINSTALLED. REPLACED ENGINE. ATTRIBUTED THE PROBLEM TO FAILED BEARINGS.

Part: STARTER — FAULTY (ENGINE) · airframe 48,925 hrs · 18,180 cycles

DURING ENGINE START SMOKE AND SPARKS WERE SEEN COMING FROM TAILPIPE OF NR 1 ENGINE. ON ENGINE START NOTIFIED BY GND CREW THAT SMOKE AND SPARKS WERE COMING FROM TAILPIPE OF NR 1 ENGINE. SPARKS CAUSED BY FAULTY STARTER. CHECKED INLET EXHAUST AND CHIP DETECTORS PRECAUTIONARY. ALSO ACCOMPLISHED GENERAL VISUAL OF ENGINE. NO FAULTS FOUND. RE-STARTED ENGINE THREE TIMES AND VERIFIED NORMAL OPERATION WITH NO FURTHER SPARKING. REPLACED STARTER AND START VALVE.

Part: SMOKE — DETECTED (COCKPIT) · airframe 44,071 hrs · 16,373 cycles

RETURNED TO THE FIELD DUE TO SMOKE IN THE COCKPIT. CAUSE OF INCIDENT WAS A FAILED THRUST DISK & BEARING IN LT ACM. COMPONENT FINDINGS WERE A FAILED THRUST DISK & A FAILED BEARING WHICH ALSO DAMAGED TURBINE & COMPRESSOR SECTIONS. THRUST DISK, BEARING TURBINE ASSY & COMPRESSOR WERE ALL REPLACED & UNIT MADE SERVICEABLE. THIS UNIT INSTALLED ON 06 JUN 2000 & ACCUMULATED A TOTAL OF 15,397 HRS & 5,718 CYCLES PRIOR TO FAILURE. CURRENT MX PROGRAM IS ON CONDITION FOR ACM. A HEALTH CHECK IS PERFORMED ON SYS & TEMP SENSORS CHECKED & CALIBRATED AT 1C. NO CORRECTIVE ACTIONS OR MX PROGRAM CHANGES REQUIRED AT THIS TIME.

Part: WARNING LIGHT — MALFUNCTIONED (L3 DOOR SLIDE) · airframe 43,178 hrs · 16,014 cycles

DOOR 3L SLIDE LIGHT WOULD NOT GO OFF WITH DOOR DISARMED. ALTHOUGH UNABLE TO DUPLICATE INCIDENT, IT IS SPECULATED CONDITION WAS CAUSED BY DIRT OR DEBRIS ON PROXIMITY SENSORS WHICH AFFECTS THE INDUCTANCE NECESSARY FOR SYSTEM OPERATION.

Part: O-RING — LEAKING (EVAC SLIDE)

LOW BOTTLE PRESSURE. RESERVOIR/VALVE ASSEMBLY SHAFT O-RING LEAKING. REPLACED SHAFT O-RING AND BACK-UP O-RING.

Part: SLIDE — LEAKING (CABIN)

ON LOWER TUBE, BOTH SUPPORT LEGS AT THE FRONT END ON UPPER SIDE, OPPOSITE ASPIRATOR, LEAKING. LEAKING ON MITERED CORNER AT BUMPER TUBE ON ASPIRATOR SIDE IN FRONT. SLIDE FAILED AIR RETENTION TEST. LEAKAGE WAS FOUND AT SEAMS. POROSITY WAS FOUND NEAR SEAMS. ABRASION ON ONE SEAM CONTRIBUTED TO LEAKAGE.

Part: CONTROL MODULE — MALFUNCTIONED (SPOILERS) · airframe 40,550 hrs · 15,017 cycles

DURING CLIMB EICAS SPOILER MESSAGE DISPLAYED. FAULTED NR 3 RIGHT SPOILER CONTROL MODULE (SCM) REPLACED NR 7 RIGHT SCM

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,594 hrs · 14,687 cycles

REMOVED SKIN SPLICE DOUBLER AND UPPER LAP TRIPLER AT LEFT SIDE FUSELAGE STA BS 593 IN ANTICIPATION OF SKIN SECTION REPLACEMENT. MAJOR REPAIR ACCOMPLISHED. REINSTALLED SKIN SPLICE DOUBLER AND UPPER LAP TRIPLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,340 hrs · 13,858 cycles

AFT PIT STA 1440 BETWEEN STR 25L AND 26L UPPER FRAME FLANGE DENTED IN TWO AREAS MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,340 hrs · 13,858 cycles

AFT PIT STA 1360 ABOVE STR 26L, TOP OF FRAME FLANGE IS DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR

Part: FRAME — DENTED (FUSELAGE) · airframe 37,340 hrs · 13,858 cycles

AFT PIT STA 1400 BETWEEN STR 25L AND 26L, FRAME UPPER FLANGE DENTED IN TWO AREAS MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR

Part: FRAME — DENTED (FUSELAGE) · airframe 37,340 hrs · 13,858 cycles

AFT PIT STA 1420 BETWEEN STR 25L AND 26L, UPPER FRAME FLANGE DENTED MAJOR REPAIR ACCOMPLISHED. PERFORMED FRAME REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,340 hrs · 13,858 cycles

AFT PIT AT STA 1340 BETWEEN STR 25L AND 26L, TOP OF FRAME IS DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,340 hrs · 13,858 cycles

AFT PIT STA 1480 JUST ABOVE AND BELOW STR 25L FRAME TO FLANGE DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 37,340 hrs · 13,858 cycles

AFT CABIN FUSELAGE FRAME AT BS 1360, HOLE 3.5 INCHES TO THE RIGHT OF STRINGER 1. AFT SIDE OF FRAME HAS TOOLING MARK OR MISDRILLED SURROUNDING AREA OF HOLE. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIR DONE ON AREA.

Part: SKIN — DENTED · airframe 37,340 hrs · 13,858 cycles

LH EXTERNAL FUSELAGE HAS JETWAY DAMAGE (DENTS) AT STA 600 TO 620 BETWEEN STR 16L AND 18L. MAJOR REPAIR ACCOMPLISHED.APPLIED DOUBLER.

Part: CAP — ERODED · airframe 37,340 hrs · 13,858 cycles

CABIN STA 1640, RBL 57" FLOORBEAM TOP CAP HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. PERFORMED SINGLE FLANGE BLENDOUT REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,340 hrs · 13,858 cycles

CABIN FLOOR SUPPORT CORROSION ON UPPER SURFACE, STA 367, RBL 9. MAJOR REPAIR ACCOMPLISHED. REPLACED SUPPORT AT BS 367, STR 9, WL 208.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 37,340 hrs · 13,858 cycles

CABIN PRESSURE DECK FLOOR HAS EXCESS MATERIAL LOSS AT STA 1681, RBL 43 AND RBL 52. MAJOR REPAIR ACCOMPLISHED. DOUBLER APPLIED.

Part: ENGINE — BIRD STRIKE (RIGHT)

RETURNED TO FIELD DUE TO BIRD STRIKE. *S/D* BIRD STRIKE CAUSED RIGHT ENGINE DAMAGE. REPLACED FAN BLADE SET AND NOSE COWL. BORESCOPED 6TH STAGE BLADES, CHECKED OK. ACCOMPLISHED VIBRATION SURVEY, CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN)

CABIN EMERGENCY EGRESS LIGHTING INOP ABOVE SEATS 1AB. RELAMPED, OPERATION CHECKS NORMAL.