N711ZX

Part: HANDLE — BROKEN (ZONE 800) · airframe 93,614 hrs · 24,677 cycles

L4 DOOR EXTERIOR HANDLE MECHANISM BROKEN. REMOVED HANDLE MECHANISM, ADJUSTED AND RE-INSTALLED 4L DOOR HANDLE MECHANISM IAW AMM 52-11. ALL OPS CHECKED GOOD. (7161130)

Part: CONTROLLER — FAULTED (WINDOW HEAT) · airframe 93,393 hrs · 24,627 cycles

DIV/FUME- TO DTW DUE TO L1 WINDOW HEAT TURNED OFF DUE TO FUMES FROM CONNECTOR WITH ICING FORECAST ENROUTE. REPLACED L1 WINDOW, WINDOW HEAT CONTROLLER AND WINDOW HEAT CONNECTOR.

Part: WINDOW — ARCED (ZONE 200) · airframe 91,864 hrs · 24,269 cycles

SHIP 6814 -DIV/FUME/DE- TO CLT DUE TO BURNING RUBBER SMELL IN FLIGHT DECK. CORRECTIVE ACTION: FOUND CAPT WINDSHIELD HEAT TERMINAL J5 WITH ARCING, R/R #1 CAPT WINDOW AND THE WINDOW HEAT CONTROLLER.

Part: SEAL SEAT — DAMAGED (FUEL CELL) · airframe 91,788 hrs · 24,248 cycles

SHIP 6814 -DIV- UNKOWN SMELL IN COCKPIT AND AFT GALLEY. FOUND CENTER FUEL TANK LEAKING INTO RT PACK BAY. CORRECTIVE ACTION: PERFORMED SEALANT REPAIR ON RT CTR FUEL TANK PER B757 AMM 28-11. C/W SFAR88 AND CDCCL PROCEDURES. NO LEAKS NOTED. A/C OK FOR SVC. RT CTR TANK ACCESS PLATE INSTALLED AND LEAK CHECK PER B757 AMM 28-11. (7224976)

Part: HEATER — ODOR (ZONE 200) · airframe 91,788 hrs · 24,248 cycles

SHIP 6814 AT FL380 SMELLED A SLIGHT BURNING SMELL COMMING ONLY FROM THE CAPTAIN SIDE LOWER VENT WHEN OPENED. FOLLOWED PROCEDURES TO REPORT IT AND QRH. CORRECTIVE ACTION: REMOVED CAPT HEATER IAW B757 AMM 21-45. FOUND DEBRIS LODGED IN HEAT. SWAPP SHOULDER HEATER AND INSPECT DUCTS TO SEE IF MORE DEBRIS IS FOUND. INSTALLED CAPT SHOULDER HEAT B757 AMM 21-45. OPS CHK GOOD,NO SMELL OR ODOR INSPECTED DUCTING NO MORE DEBRIS FOUND. (0959778)

Part: WINDOW — ODOR (ZONE 200) · airframe 90,771 hrs · 23,881 cycles

SHIP 6814 ON CLIMB FROM 17000FT TO CRUISE AT 30000FT THERE WAS A CHEMICAL ODOR IN THE FLIGHT DECK DURING THE TIME WE USED THE ENGINE ANTI-ICE SYSTEM. THE ODOR CONTINUED SO I CYCLED THE ANTI-ICE SYSTEM. THE ODOR BRIEFLY INTENSIFIED THEN COMPLETELY DISSIPATED. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW RT WINDOW #3 AMM 56-11. (6880356)

Part: INDICATOR — FAULTED (ZONE 800) · airframe 90,558 hrs · 23,822 cycles

SHIP 6814 4R KNUCKLE KNOCKER WONT EXTEND IN FLIGHT. CORRECTIVE ACTION: FOUND PLACARD ON TOP OF KNOCKER CATCHING ON PAINT DRIP IN CUTOUT . REMOVED PAINT BUILD UP AND OPS CK PER B757 AMM 52-11, CK GOOD. (0707783)

Part: COVER — LOOSE (ZONE 200) · airframe 89,330 hrs · 23,492 cycles

SHIP 6814 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:608. CORRECTIVE ACTION: SECURED 4R EMERG EXIT SIGN COVER. (0495768)

Part: COVER — MISSING (ZONE 200) · airframe 89,154 hrs · 23,457 cycles

SHIP 6814 SLIDE INDICATOR LIGHT COVER WAS MISSING AFTER TAKE OFF. CORRECTIVE ACTION: REPLACED SLIDE LIGHT INDICATOR LIGHT PER B757 AMM 33-51. OPS TEST GOOD. (0475293)

Part: SKIN — CORRODED (BS 1555-1565) · corrosion level 2 · airframe 88,601 hrs · 23,337 cycles

AIRCRAFT 6814, DURING H CHECK MAINTENANCE VISIT, WHILE ACCOMPLISHING JOB CARD 2020-2443, THE STRINGER S-28L P/N 146N3110 179 BETWEEN STA 1555 AND STA 1565 WAS FOUND WITH TWO (2 EA) CORROSION SPOTS. THE LOCATION OF THE CORROSION SPOTS WAS IN THE DATUM OF AN EXTERNAL SKIN REPAIR PER ER/A 618004-14. CORRECTIVE ACTION: BLEND THE DISCREPANT AREA TO REMOVED CORROSION PER B757-200 SRM 53-00-01. FABRICATED THE FWD AND AFT STRINGER SPLICE FROM 0.071 INCH THICK 7075-T0 BARE SHEET, IDENTICAL TO B757-200 SRM 53-00-03. REPAIR 1 REQUIREMENTS EXCEPT OF RETURN FLANGE LENGTH. FOR STRINGER 28L, FABRICATED FILLER SECTION BETWEEN BS 1550-1570 FROM 0.071 INCH CONSTANT THICKNESS 7075-T0 BARE SHEET. INSTALLED THE REPAIR PARTS AS PER B757-200 SRM 53-00-03 REPAIR 1. (LP 0378439, 0378425)

Part: BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 89,591 hrs · 23,550 cycles

SHIP 6814 FOUND CORROSION AT THE BOTTOM OF LAV D AFT WALL. CORRECTIVE ACTION: REPAIRED LAVATORY D AFT INBOARD FRAME PER DELTA ERA 617652-14 REV. ORIGINAL AND REMOVED FABRICATED AND INSTALLED BRACKET PER DELTA ERA 618330-14 REV ORIGINAL. (0374588)

Part: STRAP — CRACKED (BS 1640) · airframe 88,601 hrs · 23,337 cycles

AIRCRAFT 6814, MAIN CABIN BS 1640 FLOOR BEAM LOWER STABILIZER STRAP IS CRACKED AT RBL 45.5. DOT 050. REPAIRED MAIN CABIN BS 1640 FLOOR BEAM LOWER STABILIZER STRAP CRACK AT RBL 45.5. PER B757 SRM 53-00-51-2R REPAIR 12. (LP 0374646)

Part: SKIN — DENTED (BS 640 S25-26L) · airframe 88,601 hrs · 23,337 cycles

AIRCRAFT 6814, LOCATED DENT APROX STA 640, BTWN STR 25-26L. CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN DENT AT STA 640 BETWEEN STRINGER 25-26L PER DELTA ERA 618020-14 REV. ORIGINAL. (LP 0369744)

Part: SKIN — DENTED (BS 640 S25-26L) · airframe 88,601 hrs · 23,337 cycles

SHIP 6814 FUSELAGE SECTION 43, EXTERNAL SKIN AT BS 640, STR 25L-26L DENTED. DTA MONITOR INSP REF ERA 618020-14. CORRECTIVE ACTION: REF ERA 618020-14. (0366488)

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 88,601 hrs · 23,337 cycles

SHIP 6814 FLOOR BEAM AT FRAME 1640 CORRODED. CORRECTIVE ACTION: REPAIRED MAIN CABIN FLOR BEAM STA 1640 IAW B757 SRM 53-00-51-2R PROCEDURE 9. (0360014)

Part: ANGLE — CORRODED (BS 1470 RBL 8) · corrosion level 2 · airframe 88,601 hrs · 23,337 cycles

SHIP 6814 AFT CARGO COMPARTMENT FLOOR SUPPORT Z ANGLE HAS CORROSION AT BS 1470 RBL 7.5. DOT 054. CORRECTIVE ACTION: EVALUATED AFT CARGO COMPT FLOOR SUPPORT Z ANGLE AT STA 1470 RBL 7.5, FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-53, REMOVED AND REPLACED ANGLE IAW B 757 SRM 51-40-02. (0351924)

Part: FRAME — CORRODED (BS 1440 S26) · corrosion level 2 · airframe 88,601 hrs · 23,337 cycles

SHIP 6814 AFT CARGO FRAME STA.1440 STR 26 FOUND CORROSION AT CONNER EDGE OF THE WEB AFTER TRANSITION PNL REMOVED. CORRECTIVE ACTION: EVALUATED FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-60-04, REMOVED AND REPLACED WEB IAW B 757 -200 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (BS 1238 RBL 17) · corrosion level 2 · airframe 88,601 hrs · 23,337 cycles

SHIP 6814 AFT CARGO COMPARTMENT BILGE AREA HAS CORROSION ON INTERCOSTAL LOWER ANGLE BS 1238 AND BS 1238 RBL 17. DOT 019. CORRECTIVE ACTION: REMOVED CORROSION AT AFT CARGO COMPT BILGE AREA INTERCOSTAL ANGLE AT STA 1238, RBL 17, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED INTERCOSTAL IAW DWG # 146N5516 REV A AND IAW B 757 SRM 51-40-02. (0351723)

Part: TRANSITION PANEL — CORRODED (BS 1410-1530) · corrosion level 2 · airframe 88,601 hrs · 23,337 cycles

SHIP 6814 AFT CARGO COMPARTMENT LH FLOOR TRANSITION PANEL HAS AREAS OF CORROSION ON UPPER AND LOWER SURFACES BETWEEN BS 1410 AND BS 1530. LBL 24. DOT 032. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CARGO TRANSITION PANEL AT STA 1410-1530 IAW B 757 SRM 51-40-02. (0351933)

Part: TEE FITTING — UNKNOWN (DOOR) · airframe 88,601 hrs · 23,337 cycles

SHIP 6814 AMDS 5310-01371-0201 STEP 4. REQUIRES AN SDR TO BE SUBMITTED PER TOPP 20-50-20 VIA LOG FUINCTIONS UPON COMPLETION OF TEE CLIP REPAIR. CORRECTIVE ACTION: DOORS L4 AND R4 HAVE TEE CLIPS REPLACED SDR REQUIRED PER AMDS 5310-01371-02010. (0326183)

Part: DRAG FITTING — DAMAGED (NOT REPORTED) · airframe 88,601 hrs · 23,337 cycles

SHIP 6814 FASTENER #11 FOUND OVERSIZE WHILE WORKING WC 5720-01100-02B RH DRAG FITTING INSP. CORRECTIVE ACTION: BHEC INSPECTED #11 HOLE PER MTC REQUEST REF B757 NDTM 51-00- 16PART 6. NO ITEMS NOTED. CW PRI 616845-14 REV 0. C/W PRI 616845-14 REV 1. CW PRI 616845-14 REV 2. ALL PRI REVS 616845-14 REV 0,1,2 MATCH FINAL ERA 616845-14AD REV ORIG. C/W ERA616845-14 AD REV ORIG. (0289057)

Part: NONE — NONE (NONE) · airframe 88,601 hrs · 23,337 cycles

SHIP 6814 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 616845-14AD. CORRECTIVE ACTION: REF ERA 616845-14. (0283506)

Part: HANDLE — UNSECURE (L2 DOOR) · airframe 88,333 hrs · 23,273 cycles

SHIP 6814 L2 DOOR WILL NOT CLOSE, OUTER HANDLE IS NOT FLUSH. CORRECTIVE ACTION:

Part: BOTTLE — LOW PRESSURE (R4 DOOR SLIDE) · airframe 87,644 hrs · 23,110 cycles

DURING SERVICE CHECK MAINTENANCE FOUND RT NR 4 DOOR SLIDE PRESS GAUGE ON RED. CORRECTIVE ACTION: REPLACED R4 SLIDE PACK ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 44D) · airframe 86,387 hrs · 22,849 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 44D INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,920 hrs · 22,750 cycles

SHIP 6814 NO EMERG LIGHT SEAT 33D. CORRECTIVE ACTION: INSTALLED NEW EMERGENCY LIGHT ASSEMBLY AT SEAT 33D IN REFERENCE TO B/E AEROSPACE / PINNACLE CMM 25-22-58. ALL OPS GOOD. (7070845)

Part: DOOR — OBSTRUCTED (R1) · airframe 83,773 hrs · 22,321 cycles

(AIRCRAFT 6814, L/P 6060498) 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED FOD FROM 1R DOOR.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 83,808 hrs · 22,327 cycles

SHIP 6814 DOOR 1R HARD TO ARM. CORRECTIVE ACTION: R/R NEW DOOR SLIDE PER WORK CARD AND PERFORMED DVI, NO DAMAGE.

Part: DOOR — OBSTRUCTED (R1) · airframe 83,630 hrs · 22,295 cycles

SHIP 6814 F/A REPORTS 1R DOOR WONT ARM AT DEPT TIME. CORRECTIVE ACTION: CLEARED DEBRIS FROM SILL AREA. 1R DOOR SLIDE OPS/IND NML. (6060454)

Part: STRAP — OUT OF POSITION (R1 DOOR) · airframe 83,630 hrs · 22,295 cycles

SHIP 6814 DOOR 1R HARD TO ARM. CORRECTIVE ACTION: FOUND HOOK ON DEPLOYMENT STRAP OF SLIDE IPC REF 25-66-01-51, ITEM 420, WRAPPED AROUND FWD GIRT ADJUSTING ROD AND HANGING BELOW THE DOOR. REPACKED DEPLOYMENT STRAP PER AMM 25-66-01. DOOR NOW CLOSES AND ARMS NORMALLY. (1254269)

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 83,596 hrs · 22,289 cycles

SHIP 6814 DOOR 1R WILL NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS @ R1 DOOR GIRT BAR TRACK. OPS NML. (6060432)

Part: D-RING — OUT OF POSITION (R1 DOOR ARMING) · airframe 83,514 hrs · 22,275 cycles

DUE TO REPORTS OF 1R DOOR HARD TO ARM. FOUND D-RING UNDER GIRT BAR. REINSTALLED D-RING PROPERLY. OPS CK DOOR ARMING MULTIPLE TIMES. NO FAULTS NOTED.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR SLIDE) · airframe 83,499 hrs · 22,272 cycles

R1 DOOR WOULD NOT ARM. FOUND OBSTRUCTION UNDER GIRT BAR CLEARED DOOR OPS CHECK NORMAL.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 83,084 hrs · 22,196 cycles

(AIRCRAFT 6814, L/P 6056532) DOOR 1R SLIDE INDICATOR LIGHT INOP. CLEANED DEBRIS ON GIRT BAR CYCLE DOOR MULTIPLE TIMES.

Part: LENS — UNKNOWN (CABIN) · airframe 83,084 hrs · 22,196 cycles

(AIRCRAFT 6814, L/P 1184309) EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:601 / INTERIOR. REPLACED EMERGENCY EXIT COVER DIFFUSER LENS LOCATION:601 IAW AMM 33-51. OPERATES NORMAL. OK FOR SERVICE.

Part: DOOR — OBSTRUCTED (R1) · airframe 81,984 hrs · 21,990 cycles

COULD NOT ARM 1R DOOR. CORRECTIVE ACTION: REMOVED DEBRIS OPS NORMAL. (5639626)

Part: GUIDE ARM — OUT OF ADJUST (R2 DOOR) · airframe 81,253 hrs · 21,847 cycles

SHIP 6814 R-2 DOOR DOESN'T CLOSE. ADJUSTED GUIDE ARM PER B757 AMM 52-11. DOOR OPS NORMAL. (5197680)

Part: SWITCH — FAILED (SLIDE LIGHT) · airframe 81,163 hrs · 21,829 cycles

SHIP 6814 L3 SLIDE LIGHT INOP. CORRECTIVE ACTION: T/S AS PER B757 AMM 25-66-77. REPLACED SWITCH S10223. (5197640)

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 80,115 hrs · 21,622 cycles

SHIP 6814 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND SLIDE LANYARD/STRAP CAUGHT ON GIRT BAR. REMOVED OBSTRUCTION. DOOR NOW OPS NML. PER AMM 52-11. (4476698)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 80,005 hrs · 21,602 cycles

(AIRCRAFT 6814, L/P 4476664) ON SERVICE CHECK FOUND EMERGENCY LIGHTS AT SEATS 27 DEF TO 35 DEF INOP. REPLACED POWER SUPPLY AND BATTERY PACK LOCATED ABOVE 35DEF IN REF TO AMM REF 33-51 OPS CHECK GOOD.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 79,922 hrs · 21,586 cycles

SHIP 6814 1R GIRT BAR WON'T ARM. CORRECTIVE ACTION: ADJUSTED GIRT BAR. OPS OK PER AMM 52-11. (4476642)

Part: UNKNOWN — UNKNOWN (GALLEY CART) · airframe 77,506 hrs · 21,140 cycles

FLT ATTENDANT RECEIVED AN ELECTRICAL SHOCK WHEN REMOVING THE RIGHT SIDE CART FROM ITS STOWED POSITION IN THE MID GALLEY. CHECKED FOR PROPER GROUNDING FROM MID GALLEY TO STRUCTURE. NO FAULTS FOUND IAW WDM 25-31. ALL WIRING ON THE MID GALLEY SECURE AND SHOWING CORRECT VOLTAGE. COULD NOT DUPLICATE.

Part: COLLAR — BROKEN (R1 DOOR) · airframe 76,957 hrs · 21,022 cycles

R1 DOOR HOLD OPEN LOCK COLLAR BROKEN. R & R THE HOLD OPEN COLLAR IAW AMM 52-11.

Part: GIRT BAR — FAILED (L1 DOOR) · airframe 73,276 hrs · 20,318 cycles

L1 DOOR, GIRT BAR FAILED SPRING SLIDER TEST. REMOVED AND REPLACED L-1 DOOR GIRT BAR PER AMM 25-66-10-002-001 AND 25-66-10-402-022 ADJUSTMENT CHECK GOOD PER 52-11-25-825-001 AND CARD 2560-1492-0201.

Part: COUNTERBALANCE — MALFUNCTIONED (L1 DOOR) · airframe 73,276 hrs · 20,318 cycles

L1 DOOR, COUNTER BALANCE IS NOT OPERATING CORRECTLY. REMOVED AND RE-INSTALLED L1 DOOR REMOVED AND REPLACED COUNTER BALANCE. REMOVED AND REPLACED ROTARY SNUBBER AND INSTALLED NEW SPACER PER AMM 52-11-01-004-001, AMM 52-11-10-004-030, AMM 52 -11-10-404-015, AMM52-11-004-001, AMM 52-11-11-404-007, RIG CHECK ACCOMPLISHED ON CARD 2040-0191-1L, RIG CHECK GOOD.

Part: SUPPORT ANGLE — CRACKED (BS 1420) · airframe 73,313 hrs · 20,325 cycles

AFT CARGO DOOR UPPER FRAME SUPPORT ANGLE IS CRACKED 5 BRACKETS BACK FROM THE FRONT. REPAIRED THE SUPPORT ANGLE BS 1420 IAW ER/A 556004-14, REV ORIG.

Part: GIRT BAR — FAILED (R2 DOOR) · airframe 73,276 hrs · 20,318 cycles

R2 DOOR, GIRT BAR FAILED DURING SPRING SLIDER TEST. REPLACED GIRT BAR AT R2 DOOR IN REF AMM 25-66-10-402-022 AND AMM 52-11-25-825-001, TASK CARD 2560-01792-0201.

Part: GIRT BAR — FAILED (L4 DOOR) · airframe 73,276 hrs · 20,318 cycles

L4 DOOR GIRT BAR FAILED DURING SPRING SLIDER TEST. REMOVED AND REPLACED L4 DOOR GIRT BAR PER AMM 25-66-10-402-022, AMM 52-11-25-825-001 AND CARD NR 2560-01492-0201 OPS CHECK GOOD.

Part: WEB — CRACKED (R1 DOOR) · airframe 73,268 hrs · 20,316 cycles

R1 DOOR, INNER WEB IS CRACKED AT LIGHTNING HOLE BETWEEN UPPER EES ATTACH POINTS. ACCOMPLISHED A PERMANENT REPAIR IAW ER/A 556005-14, REV ORIG.

Part: GIRT BAR — NO TEST (R4 DOOR) · airframe 73,268 hrs · 20,316 cycles

R4 DOOR GIRT BAR FAILED DURING SPRING SLIDE TEST. REPLACED THE GIRT BAR.

Part: GIRT BAR — NO TEST (R1 DOOR) · airframe 73,268 hrs · 20,316 cycles

R1 DOOR GIRT BAR FAILED DURING SPRING SLIDER TEST. REPLACED THE GIRT BAR.

Part: SKIN — DENTED (BS 1675) · airframe 73,268 hrs · 20,316 cycles

FOUND A DENT IN THE FUSELAGE SKIN AT BS 1675, BETWEEN STRINGERS 28 AND 29L. FOUND BEYOND SRM LIMITS IAW SRM 53- 00-01, FIG 101, SHEET 4, DETAIL 3, REF NOTE I ON FIG 101, SHEET 3.

Part: DOOR — MALFUNCTIONED (R4) · airframe 70,988 hrs · 19,859 cycles

R4 DOOR KNOCKER INOPERATIVE. ADJUSTMENT OF THE RETRACTABLE DOOR MECHANISM PERFORMED IAW AMM: 52-11-20. TEST OK.

Part: TORQUE SHAFT — SHEARED (L1 DOOR) · airframe 67,625 hrs · 19,175 cycles

DAMAGE TO L1 DOOR OPENING MECHANISM. FOUND L1 DOOR TORQUE SHEARED AT MID FLANGE. REMOVED L1 DOOR IAW AMM 25-11. INSTALLED L1 DOOR IAW AMM 52-11. CHECKS GOOD.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 66,942 hrs · 19,028 cycles

MAIN CABIN FWD WET AREA, CORROSION ON FLOORBEAM AT BS 365 FRAME IN BL0 TO RBL28. CP53-222-01. REMOVED CORROSION AT MAIN CABIN FWD WET AREA ON FLOORBEAM AT BS 3C5 FROM BL0 TO RBL 28 IAW SRM 51-10-02. EVALUATED AREA WITH DIGITAL CALIPER FOUND TO BE OUT LIMIT IAW SRM 53-00-51. REMOVED T-CHORD AND REPAIR PART IAW SRM 51-40-02 PAR 4T 51-40-02, PAR 7 FABRICATED A NEW T-CHORD REPAIR SECTION FROM BAC1505-100880, PO ST00004765, DIM 87 IAW SRM 53-00-51, REPAIR 8 INSTALLED REPAIR PART IAW SRM 53-00-51, FIG 201. ID TAGGED REPAIR IAW DPS 900-5-1. NR 04 PLEASE CLOSE LOG. CLOSED LOG AND REMOVED MONITOR INSP.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 66,541 hrs · 18,955 cycles

DURING SERVICE CHECK, FOUND 1L DOOR ASSIST BOTTLE PRESSURE IN RED BAND. R & R 1L DOOR ASSIST BOTTLE WITH A SERVICEABLE UNIT IAW AMM 52-11 AS REQUIRED.

Part: SKIN — GOUGED (BS 395) · airframe 64,999 hrs · 18,671 cycles

NR 3 LT FUSELAGE SKIN FOUND GOUGED AT APPROXIMATELY BS 395 BETWEEN STR 17-18LT. BLENDED OUT GOUGE ON LT FUSELAGE, STA 395, STR 17L-18L, ORIG MATERIAL .080, REMAINING MATERIAL .072, MATERIAL LOSS .008 AND IS WITHIN LIMITS SRM 53-00-01, FIG 101 AND DWG 141N3331, REV C. LP1974854.

Part: MOUNT — CORRODED (BS 1717) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

CORROSION FOUND AT AFT GALLEY FLOOR MOUNT FITTING APPROXIMATELY AT BS 1717 AND RBL 40. REFER TO AMDS WC 5100-01627-01. R & R FITTING PN 146N5338-1, PO 711ZX-00301 IAW DWG 146N5300, REV A INSTALLED FITTING IAW DWG 146N5300, REV A. LP1968133.

Part: STRUCTURE — CORRODED (BS 1680-1720) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

MULTIPLES CORROSION AREAS FOUND AT MAIN CABIN AFT FLOOR DECK FROM BS 1720 TO BS 1680 AND BETWEEN BL0 TO LBL 50. REFER TO AMDS W/C 5100-01627-01. FOUND SPOTS OF CORROSION BETWEEN BS 1708 TO 1720, LBL 50 TO RBL 50 OUT OF LIMITS IAW SRM 53-60-51, FIG 101. WORK IN PROGRESS. LP1968307.

Part: DECK PLATE — CORRODED (BS 1701) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

CORROSION FOUND ON AFT DECK PLATE, BS 1701, RBL 24. OUT OF LIMITS IAW 53-60-51, FIG 101.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 64,999 hrs · 18,671 cycles

NR 2 CARGO DOOR EXTERIOR SKIN AT LWR AFT CORNER IS BENT, CRACKED AT PREVIOUS BLEND BS 1460. OPEN.

Part: FLOOR SUPPORT — CORRODED (BS 1640-1660) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

CORROSION AT MAIN CABIN FLOOR SUPPORT BETWEEN BS 1640 TO 1660 LBL 50. FOUND OUT OF LIMITS. R & R FLOOR SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CORRODED (BS 1660-1680) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

CORROSION FOUND AT MAIN CABIN FLOOR SUPPORT BETWEEN BS 1660 - 1680, LBL 50. FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT IAW DWG.

Part: SKIN — DELAMINATED (NR 1 NACELLE) · airframe 64,999 hrs · 18,671 cycles

NR 1 ENGINE, INBD FAN COWL, INNER SIDE HAS AREAS OF DELAMINATION. REMOVED DAMAGE AND APPLIED REPAIR IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 335-375) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

FLOOR SUPPORT HAS CORROSION AT FASTENER LOCATIONS FROM BS 335-375 LBL 58. FOUND TO BE OUT OF LIMITS, IAW SRM. R & R FLOOR SUPPORT. 1

Part: INTERCOSTAL — CRACKED (BS 1320) · airframe 64,999 hrs · 18,671 cycles

AFT CARGO CEILING AREA, INTERCOSTAL IS CRACKED OTBD SIDE AT BS 1320, RBL 47. R & R INTERCOSTAL AT STA 1320 TO 1340, RBL 47 IAW DWG 146N5180, REV B.

Part: STIFFENER — CRACKED (BS 1320) · airframe 64,999 hrs · 18,671 cycles

AFT CARGO CEILING AREA, FLOOR SUPPORT VERTICAL STIFFENER IS CRACKED AT FS 1320, RBL 26. R & R FLOOR SUPPORT VERTICAL STIFFENER AT FS 1320, RBL 26 IAW DWG 146N5002, REV C.

Part: INTERCOSTAL — CRACKED (BS 1320) · airframe 64,999 hrs · 18,671 cycles

AFT CARGO CEILING AREA, INTERCOSTAL IS CRACKED FS 1320, RBL 26. R & R INTERCOSTAL IAW DWG 146N5180, REV B.

Part: INTERCOSTAL — CRACKED (BS 1320) · airframe 64,999 hrs · 18,671 cycles

AFT CARGO, CEILING AREA, INTERCOSTAL IS CRACKED AT BS 1320, LBL 47. R & R AFT CARGO CEILNG AREA INTERCOSTAL IAW DWG 146N, 518, REV B.

Part: STIFFENER — CRACKED (BS 1320) · airframe 64,999 hrs · 18,671 cycles

AFT CARGO CEILING AREA, VERTICAL STIFFENER AT STA 1320, RBL 47, CRACKED. R & R STIFFENER IAW DWG 5007, REV A.

Part: STIFFENER — CRACKED (BS 1320) · airframe 64,999 hrs · 18,671 cycles

AFT CARGO CEILING AREA, VERTICAL STIFFENER IS CRACKED FWD SIDE OF FRAME STA 1320, LBL 47. R & R AFT CARGO CEILING AREA VERTICAL STIFFENER IAW DWG 146N5002, REV C.

Part: FLOOR SUPPORT — CORRODED (BS 1640-1681) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

FOUND CORROSION ON FLOOR STRUCTURE SUPPORT INBD OF R4 DOOR OF THE AFT MAIN CABIN FROM FS 1640 TO FS 1681 AND RBL 52. R & R FLOOR SUPPORT BETWEEN FS 1660 TO 1681, RBL 52 IAW DWG 146N5230, REV B, PN 146N5246V6, PO 7112X-00266. INSTALLED SUPPORT IAW DWG 146N5230 REV B. LP1950747.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 64,999 hrs · 18,671 cycles

AFT CARGO FLOOR SUPPORT IS CRACKED, FWD SIDE FS 1320, LBL 26, CEILING AREA. R & R THE FLOOR SUPPORT BETWEEN FS 1320 - 1340 IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 1665) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

MAIN CABIN AT L4 DOOR LOWER FRAME HAS TWO CHANNELS CORRODED BS 1665. R & R THE CHANNELS IAW SRM 51-40-02, PAR 4 & DWG 146N8722, REV B.

Part: FRAME — GOUGED (BS 1280) · airframe 65,436 hrs · 18,747 cycles

MAIN CABIN FRAME , BS 1280, HAS TWO GOUGES AT THE WINDOW BELT, BETWEEN S11-13R. BLENDED OUT AREAS IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-00-07. REPAIR IAW ERA 532895-14AD, REV "0".

Part: SUPPORT CHANNEL — CORRODED (BS 342) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

MAIN CABIN WET AREA, SUPPORT CHANNEL IS CORRODED BS 342, LBL 22. INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-40-02, PAR 4, 51-40-02, PAR 7 AND DWG 141N5170, REV F.

Part: STIFFENER — CORRODED (BS 1661) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

LOWER FRAME AT L4 DOOR CUT OUT, BS 1661 HAS A CORRODED STIFFENER. R & R THE STIFFNER IAW SRM 51-40-02, PAR 7 & DWG 146N8722.

Part: CREASE BEAM — CORRODED (BS 1380-1390) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

FOUND CORROSION ON CREASE BEAM AT RT MAIN CABIN BS 1380 TO 1390. REMOVED CORROSION IAW SRM 51-10-2 AND FOUND OUT OF LIMITS IAW SRM 53-60-13. INSTALLED NEW CREASE BEAM IAW DWG 146N5590, REV B.

Part: STRAP — CRACKED (BS 375) · airframe 64,999 hrs · 18,671 cycles

MAIN CABIN, STABILIZER STRAP UNDER FLOOR IS CRACKED, BS 375, LBL 45. INSTALLED REPAIRS PARTS IAW SRM 53-00-51, FIG 201.

Part: SEAT TRACK — BROKEN (BS 720) · airframe 64,999 hrs · 18,671 cycles

MAIN CABIN SEAT TRACK AT BS 720, RBL 45.5 HAS BROKEN OFF SECTION OF TRACK. REMOVED DAMAGE SECTION OF SEAT TRACK AND REPLACED NEW SECTION AT BS 700-780 IAW DWG 140N5080, REV C.

Part: SEAT TRACK — CORRODED (BS 1640) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

MAIN CABIN SEAT TRACK AT STA 1640, RBL 45, CORRODED. OUT OF LIMITS, INSTALLED SEAT TRACK IAW DRW 146N5130, REV A.

Part: FRAME — DENTED (BS 1420) · airframe 64,999 hrs · 18,671 cycles

AFT CARGO COMPARTMENT FRAME HAS A DENT ON UPPER FLANGE, AT BS 1420, AND ABOVE STR 26L. CUT OUT DAMAGED AREA OF FRAME, DIM 2" X 1", AT FS 1420, STR 26L, FABRICATED REPAIR DOUBLER, DIM 15" X 5" AND INSTALLED REPAIR IAW SRM 53-00-07, FIG 001.

Part: SEAT TRACK — CORRODED (BS 1640) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

MAIN CABIN SEAT TRACK AT BS 1640, RBL 24, CORRODED OUT OF LIMITS. INSTALLED A NEW SEAT TRACK IAW DWG 146N5130, REV A, LP1940852.

Part: SEAT TRACK — CORRODED (BS 1640) · corrosion level 2 · airframe 64,999 hrs · 18,671 cycles

MAIN CABIN AT BS 1640, LBL 24, SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW SRM 53-60-52 DWG 146N5130, REV A.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 64,849 hrs · 18,642 cycles

MAINTENANCE FOUND BROKEN WIRES AT EMERGENCY LIGHT FIXTURE LOCATED AT ROW 19DEF. MAINTENANCE R & R ROW 19DEF EMERGENCY PATH LIGHT ASSY. LP6746398.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,340 hrs · 18,522 cycles

UPON BLOCK IN DOOR 4R WILL NOT DISARM. FAULT COULD NOT BE DUPLICATED. CYCLED ARM/DISARM LEVER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,052 hrs · 18,453 cycles

ROW SEAT 24D EMERGENCY EXIT LIGHT INOPERATIVE, LIGHT FIXTURE BROKEN OFF FROM TRIM. REPLACED THE LAMP AND SECURED LIGHT FIXTURE.

Part: LIGHT — DETACHED (CABIN) · airframe 64,052 hrs · 18,453 cycles

ROW SEAT 25D EMERGENCY LIGHT FIXTURE BROKEN OFF FROM TRIM AND HANGING. SECURED THE LIGHT FIXTURE.

Part: SKIN — DENTED (BS 624) · airframe 72,707 hrs · 20,196 cycles

SKIN DENTED AT BS 624 JUST ABOVE STRINGER 18L. REPLACED THE SECTION OF FUSELAGE SKIN, FROM BS 605 - 661.

Part: SKIN — DAMAGED (BS 1720) · airframe 63,027 hrs · 18,182 cycles

SKIN HAS GOUGE AND PUNCTURE DAMAGE JUST FORWARD OF BS 1720 AND BETWEEN S12-16L. REPAIRED IAW PRI 530287-14, REVISIONS 0- 8 AND FINAL ERA 530287-14.

Part: SPAR — CRACKED (RT WINGLET) · airframe 59,392 hrs · 17,482 cycles

WING RT SIDE WINGLET MOD FORWARD SPAR END FITTING CRACKED. REPAIRED IAW ERA 521730-14, LOG PAGES 1246940, 1252115.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 59,392 hrs · 17,482 cycles

FLOORBEAM BS 1640, UNDER SIDE OF UPPER TEE AT LBL 1, CORROSION AND BARE METAL. REPAIRED UPPER TEE IAW ERA 5721741-14, REV O.

Part: GROUND WIRE — LOOSE (EMERGENCY LIGHT) · airframe 58,686 hrs · 17,341 cycles

RED EMERGENCY LIGHT AT R3 LAVATORY MODULE LOWER RT CORNER INOPERATIVE. TROUBLESHOT IAW WDM 33-51-14. FOUND WIRE W3634-9007-20 NOT CONNECTED TO GROUND. SECURED GROUND WIRE, OPS CHECKED NORMAL.

Part: SEAT TRACK — DAMAGED (STA 1175) · airframe 57,281 hrs · 17,081 cycles

CRACKED SEAT TRACK, ONE LUG SEPARATED BS 1175, RBL 24.75. REMOVED DAMAGE SECTION AND SPLICE REPAIRED IAW SRM 53-00-52, REPAIR 3. MAJOR REPAIR.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 54,683 hrs · 16,560 cycles

EMERGENCY LIGHTS TEST, FOUND PATH LIGHT AT CENTER GALLEY INOPERATIVE. RELAMPED PATH LIGHT AT 2R LAV OPS CHECKED NORMAL. FOUND CONNECTOR D99135P TO BE FAULTY. REPLACED PIN AND CONNECTOR IAW SWPM CH20 EMERGENCY PATH LIGHTS. OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (BS 398-1557) · airframe 53,107 hrs · 16,272 cycles

FUSELAGE SKIN BS 398-1557, STR 8R-4L DAMAGED. REPAIRED IAW ERA 489665-14.

Part: OVEN — FIRE (AFT GALLEY) · airframe 49,731 hrs · 15,620 cycles

SMALL FIRE IN AFT GALLEY NR 2. TWO PIZZA BOXES CAUGHT FIRE. BREAKERS PULLED, FIRE EXTINGUISHED. NO FIRE EXTINGUISHERS WERE REQUIRED.

Part: CABLE — DISCONNECTED (L1 DOOR) · airframe 48,795 hrs · 15,447 cycles

MAINTENANCE DISCOVERED THE EMERGENCY ASSIST BOTTLE AT DOOR L1 WAS NOT PROPERLY CONNECTED. MAINTENANCE RECONNECTED THE BOTTLE TRIGGER CABLE ASSEMBLY AND THE SYSTEM NOW CHECKS TO BE OPERATIONAL.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 45,847 hrs · 14,904 cycles

DURING LAYOVER CHECK FOUND EMERGENCY PATH LIGHT INOPERATIVE AT MID GALLEY FWD PARTITION WALL BEHIND SEAT 4D. MX RECONNECTED THE LIGHT ASSY. OPS CHECKS GOOD.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 44,133 hrs · 14,588 cycles

NR 2 ENGINE HAD BIRD STRIKE FOLLOWED BY VIBS - DIVERTED TO MAD PERFORMED BIRD STRIKE INSPECTION PER 05-51-18 AMM AIRCRAFT FUSELAGE NO DEFECTS NOTED RT ENGINE SHOWS DAMAGE ON FAN BLADES AND ACOUSTIC LINER (DL75E101749).

Part: RESERVOIR — DISCHARGED (R4 DOOR) · airframe 43,413 hrs · 14,451 cycles

THE PRESSURE IN THE EMERGENCY POWER RESERVOIR FOR DOOR 4R WAS FOUND TO BE DEPLETED. THE RESERVOIR WAS REPLACED AND THE SYSTEM WAS RETURNED TO NORMAL OPERATING CONDITION PER MM 52-11-30.

Part: GCU — INOPERATIVE (RT GENERATOR) · airframe 42,273 hrs · 14,227 cycles

AFTER HARD-START PROCEDURES -RT ENG GEN CONTROL WOULD NOT SOME ON - RT ENG GEN OFF EICAS MSG. FWD TO MCO AND PLAC IAW MEL 24-00-01 RT ENG DISCONNECTED AND APU VERIFIED FULL.

Part: SEAL — BROKEN (HYDRAULIC SYS) · airframe 40,030 hrs · 13,806 cycles

LEFT HYD RSVR LIGHT ON. FOUND SEAL ON L HYD PRESS RELIEF SLEEVE BROKEN. REMOVED AND REPLACED PER MM, LEAK CHECK GOOD. LT HYD RSVR LIGHT OFF.

Part: FLOOR PANEL — CORRODED (BS 345) · airframe 39,356 hrs · 13,681 cycles

STA 333 STA 345 RT R-1 FLOOR PANEL CORRODED CP53-221-01-02-05I, C/W AT SAA - SAT ON N/R 126034 JOB 82957480001.

Part: SUPPORT FITTING — CORRODED (FS 580) · airframe 39,356 hrs · 13,681 cycles

SCUFF PLATE SUPPORT FITTING CORRODED ON FWD CARGO DOOR CUTOUT LOWER SILL FS 580 CP53-121-01I, C/W AT SAA - SAT ON N/R 128562 JOB 82960760001.

Part: SEAT TRACK — CORRODED (BS 1635) · airframe 39,356 hrs · 13,681 cycles

MAIN CABIN STA 1635 LBL 24 SEAT TRACK HAS CORROSION IN CENTER AND ON CROWN CP53-251-01-02-05I, C/W AT SAA - SAT ON N/R 126211 JOB 82956970001.

Part: PLATE — CORRODED (BS 1681-1720) · airframe 39,356 hrs · 13,681 cycles

MAIN CABIN STA 1681.8 TO 1720 BL0 THRU 58 RT FLOOR DECK PLATE HAS CORROSION ON UPPER SURFACE CP53-251-01-02-05I, C/W AT SAA - SAT ON N/R 126185 JOB 82957120001.

Part: CUSP WEB — CORRODED (BS 760-780) · airframe 39,356 hrs · 13,681 cycles

MAIN CABIN INNER CUSP CHORD CORRODED STA 760-780 RBL 64/ C/CW AT SAA - SAT ON N/R 125427 JOB 82959510001.

Part: INTERCOSTAL — CORRODED (BS 333) · airframe 39,356 hrs · 13,681 cycles

STA 333 TOP OF INTERCOSTAL CORRODED RBL 25 - RBL 43, C/W AT SAA -SAT ON N/R 126031 JOB 82957490001.

Part: CUSP WEB — CORRODED (BS 740-760) · airframe 39,356 hrs · 13,681 cycles

MAIN CABIN INNER CUSP CHORD CORRODED STA 760-740 LBL 64, C/ W AT SAA - SAT ON N/R 125430 JOB 82959540001.

Part: SKIN — DENTED (BS 423) · airframe 39,354 hrs · 13,680 cycles

ACCOMPLISHED REPAIR AS REQUIRED PER OMI LOG W/CN U03299225 2 DENTS NOTED AT STA 423 BETWEEN STRINGER S19L AND S20 . 4 FT AFT AND 2 FT BELOW L1 DOOR DENTS MEASURED IAW SRM 53-00-01 PAGE 1014 DETAIL 111 AS DESCRIBED IN CORRECTION ACTION, C/W AT SAA - SAT ON N/R 120424 JOB 82954050001.

Part: STRAP — CORRODED (FS 367) · airframe 39,354 hrs · 13,680 cycles

STA 367 RBL45 HAS CORROSION ON STRAP BETWEEN FLOORBEAM, C/W AT SAA -SAT ON N/R 126040 JOB 82957450001.

Part: INTERCOSTAL — CORRODED (BS 333) · airframe 39,354 hrs · 13,680 cycles

STA 333 TOP OF INTERCOSTAL CORRODED RBL 3 TO RBL 25 CP53-221-01-02-5I, C/W AT SAA -SAT ON N/R 126032 JOB 82957470001.

Part: INTERCOSTAL — CORRODED (BS 1660-1681) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN STA 1660 THRU 1681.8 RBL 10 INTERCOSTAL IS CRACK APPROX 7/8 INCH LONG AND HAS CORROSION AROUND FASTENER HOLE CP53-251-01-02-05I, C/W AT SAA - SAT ON N/R 16192 JOB 82957170001.

Part: SEAT TRACK — CORRODED (BS 880) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN SEAT TRACK STA 880 RBL 25 OTBD LEG ATTACHED TO FLOORBEAM HAS A DEEP GROOVE WORN IT FROM TRAPPED FLOORBOARD SCREW, C/W AT SAA - SAT ON N/R 125429 JOB 82959550001.

Part: SEAT TRACK — CORRODED (BS 1635) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN STA 1635 LBL 45 SEAT TRACK HAS CORROSION IN CENTER OF TRACK CP 53-251-01-02-05I, C/W AT SAA -SAT ON N/R 126207 JOB 82956960001.

Part: FLOORBEAM — CORRODED (BS 377) · airframe 39,354 hrs · 13,680 cycles

STA377 ON FLOORBEAM BL-0 - LBL 60 SEVERAL AREAS OF CORROSION AS MARKED CP53-221-01-02-5I. C/W AT SAA - SAT ON N/R 126038 JOB 82957590001.

Part: SKIN — DENTED (BS 1570) · airframe 39,354 hrs · 13,680 cycles

FUSELAGE EXTERNAL SKIN HAS A DENT AT STA 1570 AND STR 28 LT, C/W AT SAS - SAT ON N/R 134308 JOB 82954990001.

Part: FLOOR SUPPORT — CORRODED (BS 1660-1680) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN AT STA 1660 THRU 1681 LBL 55 FLOOR SUPPORT HAS CORROSION ON UPPER SURFACE CP53-251-01-02-05I. C/W AT SAA - SAT ON N/R 126200M JOB 82957040001.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 39,354 hrs · 13,680 cycles

STA 365 FLOORBEAM BL 0 -RBL 60 CORRODED CP53-221-01-02.5, C/W AT SAA =- SAT ON N/R 126021 JOB 82957530001.

Part: ANGLE — CORRODED (BS 1660) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN STA 1660 FLOORBEAM HAS CORROSION ON UPPER SURFACE AT BL 0 AND LBL 44 CP53-251-01-02-05I, C/W AT SAA -SAT ON N/R 126196 JOB 82957200001.

Part: SEAT TRACK — CORRODED (BS 1630-1635) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN STA 1630 AND 1635 RBL 24 SEAT TRACK HAS GOUGE AND CORROSION IN THE CENTER AND ON CROWN CP53-251-01-02-05I, C/W AT SAA - SAT ON N/R 126216 JOB 82957000001.

Part: FLOOR SUPPORT — CORRODED (BS 1644-1660) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN AT STA 1644 THRU 1660 RBL 57 FLOOR SUPPORT HAS CORROSION ON UPPER SURFACE CP53-251-01-02-05I. C/W AT SAA - SAT ON N/R 126202 JOB 82957060001.

Part: SEAT TRACK — CORRODED (BS 1240) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN SEAT TRACK STA 1200-1280 HAS CORROSION INSIDE TRACK AT STA 1240 RBL 45. C/W AT SAA - SAT ON N/R 134028 JOB 82959450001.

Part: SKIN — DENTED (BS 1872) · airframe 39,354 hrs · 13,680 cycles

EMPENNAGE EXTERNAL DENT FS 1872 S3R- S4R, C/W AT SAA - SAT ON N/R 133993 JOB 82956570001.

Part: CUSP WEB — CORRODED (BS 760-780) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN INNER CUSP CHORD CORRODED STA760-780-RBL64/ C/W AT SAA - SAT ON N/R 125427 JOB 82959510001.

Part: STIFFENER — CORRODED (BS 1700-1720) · airframe 39,354 hrs · 13,680 cycles

MAIN CABIN STA 1700 THRU 1720 BL-0 FLOOR DECK PLATE STIFFENER HAS CORROSION ON UPPER SURFACE, CP53-521-01-02-05I, C/W AT SAA -SAT ON N/R 126204 JOB 82957080001.

Part: LINE — CRACKED (HYD PRESS) · airframe 38,864 hrs · 13,591 cycles

AFTER A COUPLE OF HRS AT CRUISE, LT HYD PUMP EICAS AND LT HYD QTY EICAS. QRH ACCOMPLISHED. FOUND LEFT ENG EDP LEAKING AND ON REMOVAL FOUND DRIVE SHAFT SHEARED FURTHER. LEAK CHECKS REVEALED LT PYLON HYD PRESSURE LINE LEAKING. REPLACED LT EDP AND ALL RELATED HYD FILTERS AND INSTALLED NEW PRESSURE LINE, OPS/LEAK CHK OK.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 38,864 hrs · 13,591 cycles

DURING FLT LEFT HYD QTY AT .24 WITH LEFT QTY AND LEFT ENG DRIVEN PUMP EICAS MSGS. FOUND LT EDP LEAKING ON CASE PUMP BODY. WHEN PUMP REMOVED FO DRIVE SHAFT SHEARED. REPLACED LT EDP IAW AMM 29-11-05-404. REPLACED LT CASE DRAIN AND PRESSURE FILTERS ALL OK EDP OPS NML.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 38,634 hrs · 13,541 cycles

NR 2 ENGINE CHANGE FOR STAGGER.

Part: COVER — LOOSE (CABIN)

LAS - EMERGENCY LIGHTS AT SEAT ROW 13D STICKING UP FROM FLOOR. SECURED PLASTIC COVER OVER EMERGENCY LIGHT AT SEAT ROW 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — LOOSE (CABIN)

DFW EMERGENCY FLOOR LIGHT AT SEAT 12D IS LOOSE. SECURED EMERGENCY FLOOR LIGHTING AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LENS — LOOSE (EMERGENCY LIGHT)

EMERGENCY FLOOR TRACK LIGHT AT SEAT 13DEF LOOSE. SECURED LOOSE FLOOR TRACK PLASTIC COVER AT SEATS 13DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — LOOSE (CABIN)

DFW - EMERGENCY LIGHTS IN BIN AT SEAT ROWS 2EF AND 3EF AND 30DEF INOPERATIVE. RESECURED LIGHT AT BINS AT SEAT ROWS 2EF AND 3EF AND 30DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DFW EMERGENCY PATH LIGHT AT MID LAV AND BETWEEN SEAT ROWS 12 AND 13 INOPERATIVE. REPLACED FEEDER CABLE FROM FORWARD ENTRY TO NUMBER 2 DOOR AND REPLACED LIGHT SEGMENT BETWEEN ROWS 12 AND 13. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN)

STL - EMERGENCY EGRESS LIGHTS AT AFT CABIN FLOOR INOPERATIVE. CLEANED MOISTURE FROM AFT CABIN EGRESS EMERGENCY LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — OUT OF ADJUST (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWELVE GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED TWELVE GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — DEPLOYED · airframe 21,228 hrs · 7,239 cycles

AFTER CHECK-C AND DURING A MINI CABIN EVACUATION THE ESCAPE SLIDE AT THE LEFT SIDE NUMBER 4 CABIN DOOR DEPLOYED AND INFLATED, BUT FELL TO THE GROUND. THE GIRT BAR WAS WITH THE SLIDE.

Part: SLIDE — DISLODGED · airframe 21,228 hrs · 7,239 cycles

AFTER CHECK-C AND DURING A MINI CABIN EVACUATION DEMONSTRATION THE ESCAPE SLIDE AT THE RIGHT SIDE NUMBER 2 DOOR DID NOT INFLATE BUT FELL TO THE FLOOR. THE GIRT BAR WAS WITH THE SLIDE.

Part: SPRING — DEFORMED (GIRT BAR) · airframe 21,228 hrs · 7,239 cycles

THE EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRINGS WERE ADJUSTED ACCOUNT DEFORMED AT THE L1, L2, AND R4 DOORS. THE SPRING WAS REPLACED ACCOUNT BENT AT THE R1 DOOR.

Part: SLIDE · airframe 18,800 hrs · 6,329 cycles

THE RIGHT SIDE FWD CABIN DOOR EVACUATION SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE SLIDE. CHECK-C 11-29-01 MCI. --CLOSED--

Part: LIGHT — MISSING (CABIN) · airframe 14,784 hrs · 4,994 cycles

THE FIRST CLASS EGRESS LIGHTS HAD A SEGMENT MISSING AND WIRES EXPOSED. SPLICED IN ELECTRICAL CONNECTORS P/N 65801-003 AND 91F9705, AND STOWED WIRES. CHECK-C 5-23-00 LAX.

Part: BATTERY — DISCHARGED (FWD CABIN) · airframe 12,456 hrs · 4,280 cycles

THE CABIN EGRESS AND EMERGENCY LIGHTS WERE INOPERATIVE. DRIED OUT THE EGRESS LIGHTS, AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. CHECK-C 5-23-00 LAX.

Part: SKIN — DAMAGED (TE FLAP) · airframe 11,316 hrs · 3,887 cycles

DURING CHECK-C MAINT, THE RT WING AFT FLAP SECTION, 5 FT O/B OF FUSELAGE HAD HOLE IN COMPOSITE LOWER SURFACE 0.90 IN BY 0.5 IN, LOCATED 13 INCHES AFT OF L/E. INSTALLED HOT BOND ON AFT FLAP O/B OF FUSELAGE PER SRM 51-70-10 AND 57-53-01. REPAIR WAS 2 IN BY 3 IN.

Part: SKIN — DENTED (TE FLAP) · airframe 11,316 hrs · 3,887 cycles

DURING CHECK-C MAINT, THE LEFT WING TRAILING EDGE I/B FOREFLAP, MID-SECTION UNDER SURFACE HAD LARGE DENT, APPROX 0.156 IN DEEP BY 1.5 INCHES WIDE AND 5.5 INCHES FROM TRAILING EDGE. REMOVED DAMAGED SKIN AND HONEYCOMB AND INSTALLED METAL HOT BOND PER SRM 51-70-10.

Part: WIRE — CUT (CABIN) · airframe 10,959 hrs · 3,764 cycles

THE FWD CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE JUMPER WIRE DUE TO AN APPARENT CUT IN THE WIRE. CHECK-C 11-20-98 LAX.

Part: WIRE — INOPERATIVE (LAVATORY) · airframe 10,619 hrs · 3,644 cycles

THE EGRESS LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPAIRED THE JUMPER WIRE FOR THE LIGHT STRIP AT THE LAVATORY. CHECK-C 11-20-98 LAX.

Part: SKIN — DENTED (BS 630)

FOUND DENT APPROX 2 IN WIDE BY 3 IN HIGH AND APPROX 0.125 IN DEPTH AT STA 630, LT SIDE ADJACENT TO THE NUMBER 2 CABIN DOOR, 6 IN FROM FLOOR LEVEL BELOW STRINGER 172. INSTALLED EXTERNAL REPAIR TO DAMAGED AREA PER SRM 53-00-01. CHECK-C 11-28-98 LAX.

Part: LAMP — FAILED (ROW 3 AND 4)

THE OVERHEAD EMERGENCY LIGHTS BETWEEN CABIN ROWS 3 AND 4 WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 11-20-98 LAX.

Part: LAMP — FAILED (CABIN)

JFK - FLT 399 - DURING LS CHECK, EMERGENCY LIGHTS FAILED AT R2 AND R4 DOORS. REPLACED LAMPS MFG PN 767. NEW AIRCRAFT.