N343NW

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 200) · airframe 95,206 hrs · 43,160 cycles

UPON ARRIVAL AFT LEFT LAV OXYGEN MASK DEPLOYED FROM CEILING. RESTOWED OXYGEN MASKS IN THE AFT LEFT LAV PER 320 AMM 35-21. VERFIED DOOR SECURED. A/C OK FOR SVC. (LP: 7595500)

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE) · airframe 95,206 hrs · 43,160 cycles

O2 MASK IN AFT LAV IS DROPPED. REPACKED LAV O2 MASKS PER A320 AMM 35-21. OK FOR CONT SVC. (LP: 7858597)

Part: LATCH — UNSECURE (OXYGEN BOX) · airframe 94,507 hrs · 42,784 cycles

SHIP 3243 DISC: O2 MASK DEPLOYED IMMEDIATELY AFTER ROTATION. I WAS ABLE TO RESTOW MASK, HOWEVER THE FITTINGS WHICH LATCH THE ACCESS PANEL ARE NOT FULLY SECURE. MASK WAS NOT ACTIVATED AND NO O2 WAS RELEASED. C/A: RESTOWED O2 MASKS AS PER A320 AMM 35-21. PANEL IS SECURED. OK FOR SVC. (LP: 1025554)

Part: OXYGEN BOX — OPEN (ZONE 900) · airframe 94,291 hrs · 42,671 cycles

SHIP 3243 DISC: AFT GALLEY O2 MASK COMPARTMENT OPENED & DEPLOYED. C/A: RESECURED O2 MASKS IN COMPARTMENT PER A320 AMM 35-21 - ALL CHECKS NORMAL. (LP: 7386038)

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 200) · airframe 93,507 hrs · 42,268 cycles

SHIP 3243 DISC: ON TAXI OUT FA'S CALLED AND ADVISED MULTIPLE OXY MASKS DROPPED FROM OVERHEAD. C/A: ONLY AFT GALLEY MASKS DROPPED. RESECURED REF A320 AMM 3521. MASKS SECURED GENERATORS NOT ACTIVATED. (LP: 6352682)

Part: APU — AERATED (APU) · airframe 92,966 hrs · 41,988 cycles

SHIP 3243 DISC: AFTER STARTING ENG #1 ON APU BLEED HAD A ACRID SMOKE AROMA. START CONDUCTED WITH SLIGHT TAILWIND. AROMA SEEMED TO CLEAR BUT REAR OF A/C REPORTED HEADACHE AND NAUSEA. C/A: TROUBLESHOOT PER A320 TSM 05-50-810-831-A. CORRECTIVE ACTION TYPE 10. RAN APU AND ENGINES TO BLEED SHIFT WITH NO ABNORMAL ODORS PRESENT. PACKS RAN FROM APU AND ENGINE BLEED. ALL OPS NORMAL. (LP: 6562238)

Part: ADIRU — FAULTED (NR 3) · airframe 92,877 hrs · 41,945 cycles

SHIP 3243 - DIV - TO GRR DUE TO CAT 3 DUAL MESSAGE IN THE STATUS PAGE INOP SYS LIST ON APPROACH. WEATHER IN DTW WAS BELOW MINIMUMS. CORRECTIVE ACTION: COULD NOT DUPLICATE FAULT. RTS. LATER R/R ADIRU #3. OK FOR SERVICE. (LP: 6570978)

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 200) · airframe 92,856 hrs · 41,930 cycles

SHIP 3243 DISC: PASSENGER OXYGEN STORAGE - GALLEY MODULES, OXYGEN MASKS DEPLOYED IN AFT GALLEY. C/A: FWD TO MEL 35-21-01D,PLACS INSTALLED,MCC NOTIFIED,C/W M PROC. REMOVED AND REPLACED 2L GALLEY EMERGENCY OXYGEN MODULE IAW A320 AMM REF 35-21-41. PLACARD REMOVED. MC NOTIFIED. (LP: 6570942)

Part: LATCH — BROKEN (OXYGEN PANEL) · airframe 92,805 hrs · 41,904 cycles

SHIP 3243 DISC: OXYGEN PANEL LATCH BROKEN / LOCATIONS:103 / MYCABIN TEXT: FRC352301103 OXYGEN MASK PANEL ABOVE 2L DOOR OPENED ON TAKEOFF. OXYGEN MASKS. C/A: FOUND NO BROKEN PARTS. PERFORMED PACKING OF THE OXYGEN MASK ASSEMBLIES & CHECKED PANEL DOOR CLOSE OK IAW A320 AMM 35-21-43- 550-801-A. OK FOR SERVICE. (LP: 0655706)

Part: DOOR — OPEN (ZONE 200) · airframe 92,754 hrs · 41,879 cycles

SHIP 3243 DISC: ON LANDING O2 MASK DOOR IN AFT GALLEY (AIRCRAFT LEFT OPENED). C/A: STOWED OXYGEN RAFT DOOR PER A320 AMM 35-21. OPS CHECKS NORMAL. A/C OK TO CONTINUE. (LP: 6497688)

Part: OXYGEN MASK — UNWANTED DEPLOY (ZONE 200) · airframe 92,108 hrs · 41,528 cycles

SHIP 3243 DISC: OXYGEN MASK PANEL FELL OPEN AND MASKS DEPLOYED ON TAKEOFF IF THE AFT GALLEY. C/A: *** CONTRACT MAINTENANCE EVENT - OCM: 285388 *** REPACKED AFT GALLEY O2 MASKS PER A320 AMM 35-21. OK FOR SVC. (LP: 0486733)

Part: WARNING MESSAGE — FALSE INDICATION (BRAKES) · airframe 91,915 hrs · 41,435 cycles

SHIP 3243 - ATO - AT 60 KTS DUE TO BRAKES HOT ECAM WARNING. CORRECTIVE ACTION: BSCU SHOWS NO FAULTS. SPUN BOTH LEFT AND RIGHT MLG WHEELS, NO DRAGGING OR BINDING NOTED. OK TO CONTINUE. (LP: 6062826)

Part: ENGINE — STALLED (LEFT) · airframe 91,148 hrs · 41,014 cycles

SHIP 3243 -ATB- DUE TO LEFT ENGINE STALL AFTER TAKEOFF WITH HIGH EGT. CORRECTIVE ACTION: REPLACING ENGINE DUE TO LPT BLADE DAMAGE/METAL IN THE TAILPIPE.

Part: LIGHT — DAMAGED (SEAT 21D) · airframe 91,032 hrs · 40,948 cycles

SHIP 3243 DISC: LOC 21D EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. C/A: R/R 21D EMERGENCY LIGHT HOUSING PER A320 AMM 33-51. OPS CHECK GOOD. OK FOR SVC. (LP: 5349190)

Part: INDICATOR — INOPERATIVE (DOOR SLIDE) · airframe 90,771 hrs · 40,819 cycles

SHIP 3243 DISC: SLIDE INDICATOR LIGHT INOP OR DAMAGED. C/A: REPLACED LEAKS. MEL AND PLACARD REMOVED. (LP: 0210147)

Part: DOOR FRAME — CRACKED (CABIN) · airframe 90,583 hrs · 40,705 cycles

SHIP 3243 DISC: CRACK INDICATION FOUND OPEN HOLE ON DOOR STOP 7 FR66LH HOLE 2, CRACK L ENGTH 0.100 INCH, CRACK DIRECTION 12 0'CLOCK. (VIEW AFT FACE TO FWD FAC E). AA 5311-01216, AD RELATED, ACTIONS REQUIRED PRIOR TO FURTHER FLIGH T. HOLE DIAMETER IS SMALLER THAN THE STARTING DIAMETER (0.251 INCH. C/A: PERFORMED PERMANENT REPAIR ON DOOR STOP FITTING 7 HOLE 2 AT FRAME 66 LH AS PER A320 SRM 53-41-12-300-011. JOB COMPLETE. (LP: 0165923)

Part: DAMPER — MALFUNCTIONED (DOOR) · airframe 90,586 hrs · 40,706 cycles

SHIP 3243 DISC: DONT WORK CORRECTLY DOOR DAMPER 831 (DAMPER FUNCTION ONLY). C/A: REPLACED DOOR DAMPER 831 AS PER A320 FAM AMM-52-11-14-000-001-A AND AMM-52-11-14-400-001-A. NOT FOUND LEAK. RII INSPECTION COMPLETE. (LP: 0165849)

Part: DAMPER — MALFUNCTIONED (DOOR) · airframe 90,586 hrs · 40,706 cycles

SHIP 3243 DISC: DONT WORK CORRECTLY DOOR DAMPER 841 (DAMPER FUNCTION ONLY) C/A: REPLACED DOOR DAMPER 841 AS PER A320 FAM AMM-52-11-14-000-001-A AND AMM-52-11-14-400-001-A. NOT FOUND LEAK. RII INSPECTIONCOMPLETE. (LP: 016841)

Part: DAMPER — MALFUNCTIONED (DOOR) · airframe 90,586 hrs · 40,706 cycles

SHIP 3243 DISC: DONT WORK CORRECTLY DOOR DAMPER 841 (DAMPER FUNCTIONS ONLY). C/A: REPLACED DOOR DAMPER 841 ASPER A320 FAM AMM 52-11-14. NO FOUND LEAK JOB WAS ACCOMPLIED ON LOG #0165841 PLACARD REMOVED. (LP: 5017323)

Part: DAMPER — MALFUNCTIONED (DOOR) · airframe 90,586 hrs · 40,706 cycles

SHIP 3243 DISC: DONT WORK CORRECTLY DOOR DAMPER 831 (DAMPER FUNCTIONS ONLY) . C/A: : REPLACED DOOR DAMPER 831 AS PER A320FAM AMM 52-11-14 NO FOUND LEAK JOB WAS ACCOMPLISHED ON LOG # 0165849. (LP: 5017322)

Part: DOOR FRAME — DAMAGED · airframe 90,583 hrs · 40,705 cycles

AHIP 3243 DISC: CRACK INDICATION WAS FOUND IN LOWER INBOARD HOLE, DOOR STOP FITTING #1 , FR66 RH SIDE. CRACK DEPTH: 0.110 INCHES APPROX. HOLE DIAMETER IS SMALLER THAN STARTING DIAMETER 6.38 MM (0.251 INCH), AA 5311- 01216 , AD RELATED, ACTION REQUIRED PRIOR TO FURTHER FLIGHT. C/A: PERFORMED PERMANENT REPAIR LOCATED FRAME 66 RH AT LEVEL OF DOOR STOP 1 IN LOWER INBOARD HOLE, DOOR STOP FITTING #1, FR66 RH SIDE AS PER A320 SRM 53-41-12-300-010 ITEM 2 RE-CHECK IS REQUIRED DUE TO REPAIR IS CATEGORY B. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 33,000 FC (FH NOT RELEVANT) AND SUBSEQUENT INSPECTION AT INTERVALS 10,700 FC (FH NOT RELEVANT) AS PER A320 SRI 53-41-12-205-009, STEP 2, TABLE 001. RII INSPECTION COMPLETE. (LP: 0160853)

Part: STOP FITTING — DAMAGED (DOOR FRAME) · airframe 90,583 hrs · 40,705 cycles

DISC: AD. RELATED (AA5311-01216) R2 DOOR STOP #7 AT FR66 1 EA. HOLE EXCEEDING LIMIT. HOLE #3. REF BY PEMCO/ AIRBORNE NR 14845.0059. C/A: FR 66 R/H DOOR STOP FITTING NO.7 4EA FASTENERS HOLES COLD WORKED AND OVERSIZED TO 0.281" IAW A320 SRM 53-41-12-300-008, 53-41-12 -300-009, NTM 51-10-01, 51-10-08. REPAIR CAT B, REQ INSPECTION WITH A THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT OF 56600 FC (FH NOT RELEVANT0 WITH SUBSEQUENT INSPECTION INTERVAL OF 186002 FC (FC NOT RELEVANT) PER SRM 53-41-12-205-008 JOB COMPLETED. (LP: 0160666)

Part: STOP FITTING — DAMAGED (DOOR FRAME) · airframe 90,583 hrs · 40,705 cycles

DONT WORK CORRECTLY PASSENGER CREW DOOR 842 DAMPER (REFERENCE RII AMD S CARD 5210-7089-RA) AT AFT GALLEY AREA. C/A: REMOVED DAMPER UNSERVICEABLE CONDITION PN: FE174-004, SN: 102 ON PASSENGER CREW DOOR 842 AS PER A320 FAM AMM 52-13-14-000-001-A STEP 1 THRU 4.A EXCEPT STEP 3.A ITEM (4) AND STEP 3.D. REPLACED DAMPER DOOR PASSENGER CREW 842 AS PER A320 FAM AMM 52- 13-14-000-001-A AND AMM 52-13-14-400-001-A. RII INSPECTION COMPLETE 831911 (AE201QC) JOB COMPLETE)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,315 hrs · 40,551 cycles

SHIP 3243 DISC: R DOOR SLIDE ARMING HANDLE CAN BE PUSHED IN THE ARM DIRECTION WITH THE SAFETY PIN INSTALLED. C/A: REMOVED DOOR PNL'S FOR ACCESS (WIP) 174073. REMOVED SLIDE ARMING HANDLE (WIP) 174073. INSTALLED SERVICEABLE ARMING HANDLE IAW A- 320 AMM 52-11-22. OPS CHECK GOOD. INSTALLED DOOR PANELS PER A- 320 AMM 25-23-46. (801266) RII INSPECTION COMPLETE. (LP: 0069215)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,336 hrs · 40,565 cycles

.SHIP 3243 DISC:FLIGHT CREW REPORTED DOOR 1R SLIDE ARMING HANDLE CAN PUSHED IN THE ARM DIRECTION WITH THE SAFETY PIN INSTALLED. C/A: FOUND ARMING HANDLE CASTING WORN/GROOVED WHERE PIN IS SUPPOSED TO STOP ARM. AOG WORKING. 153923. INSTALLED SERVICEABLE ARMING HANDLE ASSY PER A320 AMM 52-11-22. NEED TO INSTALL STOP/FLAG WIP 145518 QC1971. SERVICED DOOR ASSIST BOTTLE IAW A320 AMM 52-10 LEAK CHECK GOOD (WIP) 174073. QC1971. (CONT ON LOG 4600965). INSTALLED ARMING HANDLE PIN STOP BRACKET IAW A-320 AMM 52-11-22. INSTALLED DOOR PANELS PER A-320 AMM 25-23-46. OK FOR SVC. ( 801266) RII STEPS COMPLETE. (LP: 4600960)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,313 hrs · 40,550 cycles

SHIP 3243 DISC: DUE TO INOPERATIVE BIN ON ROW 16ABC, LH OW ESCAPE LIFE LINES ARE CONSIDERED INOP. C/A: DEFERRED AND PLACARDED PER A320 MEL 25-60-14B. (LP: 4600941)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,243 hrs · 40,520 cycles

SHIP 3243 DISC: EVACUATION SLIDE BOTTLE VIEW PORT LENS DAMAGED / MISSING. C/A: COVERED VIEW PORT WITH CLEAR TAPE FWD TO NEF 25-61-01, OK TO CONTINUE, JOB COMPLETE. (LP: 0051396)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,984 hrs · 40,389 cycles

SHIP 3243 DOOR 1L HARD TO CLOSE. CORRECTIVE ACTION: CLEANED DEBRIS OFF DOOR SILL AND CLEANED GIRT BAR. OPS CHECK GOOD. (4383380)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,441 hrs · 39,537 cycles

SHIP 3243 RT FWD " EMERG. EXIT HATCH HANDLE LIGHT " INOP. CORRECTIVE ACTION: REPLACED LIGHT ASSEMBLY. OK FOR SERVICE. (9969172)

Part: NONE — NONE · airframe 88,138 hrs · 39,407 cycles

SHIP 3243 - DIV - TO PHX DUE TO FUMES IN THE CABIN/STRONG BURNING PLASTIC SMELL. FOUND THE LH RECIRCULATION FAN C/B POPPED. CORRECTIVE ACTION: REPLACED THE LH AIR RECIRCULATION SYSTEM FAN. OK FOR SERVICE. (8427236)

Part: DOOR — UNSECURE (EMERGENCY EXIT) · airframe 87,554 hrs · 39,135 cycles

RIGHT AFT OVERWING EXIT SHOWS OPEN ON ECAM. SECURED AFT RT EMER EXIT HANDLE COVER IAW AMM 25-23. DOOR INDICATION NOW, OPS CHECKED NORMAL IAW AMM 52-71.

Part: NONE — NONE (NONE) · airframe 87,554 hrs · 39,135 cycles

SHIP 3243 ERA 604305-14AD REPAIR TO FR 68, STR22L-STR23L IS DTE LIMITED TO 6 MONTHS. CORRECTIVE ACTION: COMPLIED WITH EXTENSION. (2543017)

Part: NONE — NONE (NONE) · airframe 87,554 hrs · 39,135 cycles

WHILE ACCOMPLISHING LT FR. 68 INSPECTION FOUND REPAIRS THAT COULD INHIBIT HFEC IN THAT AREA "WC 5311-01244-01B, SB A320-53- 1491 RO, EASA PAD 21-090" CONTACTING ENGINEERING TO SEE IF ALTERNATE INSPECTION INSTRUCTIONS ARE REQUIRED. CORRECTIVE ACTION: SUBMITTED SDR AS REQUIRED. (2543770)

Part: NOT REPORTED — DAMAGED (NOT REPORTED) · airframe 87,554 hrs · 39,135 cycles

MULTIPLE DAMAGE. REPAIRED IAW PRI 604305-14AD REV. O, 1, 2, 3, 4, 5 AND ER/A 604305 REV. ORIGINAL.

Part: BEARING SUPPORT — CORRODED (LT MLG TRUNNION) · airframe 87,554 hrs · 39,135 cycles

SHIP 3243 L/H NOSE GEAR TRUNION BEARING SUPPORT STRUCTURE HAS PITTING/CORROSION AROUND BEARING MOUNTING HOLES. CORRECTIVE ACTION: COMPLIED WITH PRI 604284-14 REV 0, REV 1, REV 2 AND ER/A 604284-14 REV ORIGINAL. (2540172)

Part: SUPPORT — CORRODED (SWIVEL BEARING) · airframe 87,554 hrs · 39,135 cycles

RIGHT NOSE GEAR HAD PITTING & CORROSION AROUND SWIVEL BEARING SUPPORT BOLT HOLES. COMPLIED WITH ERA 604287-14 REV. 0.

Part: ANCHOR FITTING — CORRODED (RT MLG) · airframe 87,554 hrs · 39,135 cycles

RIGHT MLG ANCHOR FITTING HAS PITTING AFTER BEARING REMOVAL. REPAIRED PER A320 SRM 57-26-13.

Part: NONE — NONE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST RH SEAT ROW # 22 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (8741215)

Part: MASK — INOPERATIVE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST LH SEAT ROW # 1 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741208)

Part: NONE — NONE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST RH SEAT ROW # 25 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741218)

Part: MASK — INOPERATIVE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST RH SEAT ROW # 16 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741211)

Part: NONE — NONE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST LH SEAT ROW # 29 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741219)

Part: NONE — NONE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST RH SEAT ROW # 23 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (8741217)

Part: MASK — INOPERATIVE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST LH SEAT ROW # 18 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741212)

Part: NONE — NONE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST LH SEAT ROW # 19 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741214)

Part: MASK — INOPERATIVE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST LH SEAT ROW # 15 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741210)

Part: NONE — NONE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST RH SEAT ROW # 18 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741213)

Part: NONE — NONE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST LH SEAT ROW # 23 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741216)

Part: MASK — INOPERATIVE · airframe 85,773 hrs · 38,172 cycles

SHIP 3243 DURING TEST LH SEAT ROW # 12 PSU/O2 PANEL DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8741209)

Part: NONE — NONE · airframe 85,041 hrs · 37,794 cycles

SHIP 3243 EMERGENCY LIGHT LENS MISSING AT SEAT ROW 20DEF. CORRECTIVE ACTION: R&R EMERGENCY LIGHT ASSY AT SEAT ROW 20DEF REF A320 AMM 33-51. OK FOR SERVICE. (8234931)

Part: NONE — NONE (NONE) · airframe 87,554 hrs · 39,135 cycles

SHIP 3243 ERA 588847-14AD REVISED TO REV A TO INCORPORATE STAGE II AND III DTA. FOLLOW ON ACTION IS REQUIRED (CRACK). COMPLIED WITH ERA. (1859112)

Part: NONE — NONE (NONE) · airframe 87,554 hrs · 39,135 cycles

SHIP 3243 ERA 588847-14AD REVISED TO REV A TO INCORPORATE STAGE II AND III DTA. FOLLOW ON ACTION IS REQUIRED (CRACK). CORRECTIVE ACTION: COMPLIED WITH ERA. (1859132)

Part: NONE — NONE (NONE) · airframe 87,554 hrs · 39,135 cycles

SHIP 3243 ERA 588847-14AD REVISED TO REV A TO INCORPORATE STAGE II AND III DTA. FOLLOW ON ACTION IS REQUIRED (CRACK). CORRECTIVE ACTION: COMPLIED WITH ERA. (1859115)

Part: LIGHT — DETACHED (SEAT 16D) · airframe 83,453 hrs · 36,879 cycles

SHIP 3243 EMERGENCY LIGHT HANGING AT SEAT 16D, BROKEN OFF. CORRECTIVE ACTION: SECURED LIGHT ASSY PER A320 AMM 33-52. OK FOR SERVICE. (7821526)

Part: PIN — STUCK (R2 DOOR ARMING) · airframe 83,428 hrs · 36,869 cycles

SHIP 3243 DOOR 2R ARMING PIN STUCK. CORRECTIVE ACTION: REPLACED ARMING PIN AT 2R DOOR OPS CHECK GOOD OK FOR SERVICE. WORK PERFORMED PER A320 AMM 52-12. (7771596)

Part: LIGHT — BROKEN (SEAT 16FED) · airframe 83,346 hrs · 36,827 cycles

SHIP 3243 ON SVC CHECK FOUND SEAT 16 F,E,D EMERGENCY PATH LIGHT BROKEN. CORRECTIVE ACTION: RE-SECURED EMERGENCY PATH LIGHT AT SEAT 16. OPS CK GOOD. (7771558)

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 83,207 hrs · 36,735 cycles

SHIP 3243 - ENTRY DOOR ARMING LEVER HARD TO OPERATE LOCATIONS 602. CORRECTIVE ACTION: CLEANED 1R DOOR GRIT BAR ATTACHMENTS PER A320 AMM 52-12. OPS CHECK GOOD. (1796440)

Part: PSU — NO TEST (SEAT 22DEF) · airframe 83,168 hrs · 36,719 cycles

SHIP 3243 DURING TEST FOUND PSU OXY PANEL 22DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7332105)

Part: PANEL — NO TEST (PSU SEAT 33 DEF) · airframe 83,168 hrs · 36,719 cycles

SHIP 3243 DURING TEST FOUND PSU OXY PANEL 33DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7332107)

Part: PANEL — NO TEST (SEAT 27 ABC) · airframe 83,168 hrs · 36,719 cycles

SHIP 3243 DURING TEST FOUND PSU OXY PANEL 27ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7332106)

Part: FRAME — CRACKED (FRM 16) · airframe 82,279 hrs · 36,330 cycles

CRACK INDICATION FOUND IN HOLE 3 AT LEVEL OF DOOR STOP FITTING 1 AND FRAME 16 LT SIDE. CORRECTIVE ACTION: REPAIRED PER ERA 588771-14 AD REV 0, 1, 2 AND ER/A 588771-14AD REV ORIGINAL.

Part: STIFFENER — CRACKED (FRAME 36) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 (Y- 765) AT FR 36. CORRECTIVE ACTION: REPAIRED PER ERA 588773-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FRM 68) · airframe 82,279 hrs · 36,330 cycles

CRACK INDICATION ON FRAME 68 RT DOOR STOP 1 LOWER INBOARD HOLE. CORRECTIVE ACTION: REPAIRED PER ER/A 588847-14AD REV ORIGINAL.

Part: STIFFENER — CRACKED (FRAME 36) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 (Y254 ) AT FR 36. CORRECTIVE ACTION: REPAIRED PER ER/A 588773-14AD REV ORIGINAL.

Part: STIFFENER — CRACKED (WING) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 (Y254 ) AT FR 36. CORRECTIVE ACTION: REPAIRED PER ER/A 588773-14 AD REV. ORIGINAL.

Part: FRAME — CRACKED (FRAME 36 RT) · airframe 82,279 hrs · 36,330 cycles

CRACK INDICATION ON FRAME 36R -Y1292 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 588917-14AD REV ORIGINAL.

Part: STIFFENER — CRACKED (FRAME 36) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 (Y- 765) AT FR 36. CORRECTIVE ACTION: REPAIRED PER ER/A 588773-14AD REV ORIGINAL.

Part: STIFFENER — CRACKED (FRM 36) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 (Y765 ) AT FR 36. CORRECTIVE ACTION: REPAIRED PER ERA 588773-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FRM 16) · airframe 82,279 hrs · 36,330 cycles

CRACK INDICATION ON FRAME 16 LT SIDE IN HOLE 3 AT LEVEL OF DOOR STOP FITTING. CORRECTIVE ACTION: PERFORMED REPAIR PER ERA 588771-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FRAME 36 LT) · airframe 82,279 hrs · 36,330 cycles

CRACK INDICATION ON FRAME 36L Y1292 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 588917-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FRAME 36 RT) · airframe 82,279 hrs · 36,330 cycles

CRACK INDICATION ON FRAME 36R -Y1292 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 588917-14 AD REV ORIGINAL.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND IN HOLE 1 AT LEVEL OF DOOR STOP FITTING 7 AND FRAME 16 RT SIDE. CORRECTIVE ACTION: REPLACED INTERCOSTAL FITTING, PER ERA 588845-14AD REV ORIGINAL.

Part: SKIN — DAMAGED (EXTERIOR) · airframe 82,279 hrs · 36,330 cycles

HOLE EXTERNAL SKIN BEYOND ALLOWABLE LIMITS, AS PER AMDS 5312 -01183-0402 LOCATED FR 35 BETWEEN STRG 29L TO STR 30L AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 589271-14 AD REV ORIGINAL.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND IN HOLE 3 AT LEVEL OF DOOR STOP FITTING 1 AND FRAME 16 RT SIDE. CORRECTIVE ACTION: REPLACED INTERCOSTAL FITTING, PER ERA 588845-14AD REV ORIGINAL.

Part: STOP FITTING — CRACKED (PAX DOOR FRAME) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND IN HOLE 3 AT LEVEL OF DOOR STOP FITTING 7 AND FRAME 16 RT SIDE. CORRECTIVE ACTION: REPLACED INSTERCOSTAL FITTING, PER ERA 588845-14AD REV ORIGINAL.

Part: NOT REPORTED — CRACKED (NOT REPORTED) · airframe 83,580 hrs · 36,954 cycles

SHIP 3243 CRACKS FOUND PER ER/A 588847-14AD. CORRECTIVE ACTION: REPAIRED PER ER/A 588847-14AD. (1698347)

Part: DOOR FRAME — CRACKED (FRM 16) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND IN HOLE 3 AT LEVEL OF DOOR STOP FITTING 7 AND FRAME 16 LT SIDE. CORRECTIVE ACTION: PERMANENT REPAIR PER ER/A 588759-14AD.

Part: FITTING — CRACKED (DOOR FRAME 6) · airframe 82,279 hrs · 36,330 cycles

CRACK ON FITTING DOOR LOCATED APPROXIMATELY 3 INCHES FROM CARGO DOOR FRAME 6 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED DOOR FITTING, AS PER A320 SRM 51-72-11. OK FOR SERVICE.

Part: DAMPER — NO TEST (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

PASSENGER CREW DOOR 832 DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER. OK FOR SERVICE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 82,279 hrs · 36,330 cycles

WINGS/CENTER WING/FRONT SPAR FLOOR BEAM AND VERTICAL STIFFENER AT FR 36 CRACKS. CORRECTIVE ACTION: MONITOR CRACKS PER ER/A 588773-14.

Part: DOOR FRAME — CRACKED (FRM 16) · airframe 82,279 hrs · 36,330 cycles

CRACK FOUND IN HOLE 1 AT LEVEL OF DOOR STOP FITTING 7 AND FRAME 16 LT SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 588759-14AD REV 0 AND ER/A 588759-14AD REV ORIGINAL.

Part: SKIN — DENTED (INTAKE) · airframe 82,279 hrs · 36,330 cycles

DENT SKIN AIR INTAKE LIP ON ENGINE 1. CORRECTIVE ACTION: EVALUATED DENT AND FOUND WITHIN LIMITS, AS PER A320 SRM 64-10-00 PAGE 107, FIGURE 102 AND ITEM 5, PAGE 118 AND MONITOR CONDITION DENT ZONE CL2 AT 750 FLIGHT HOURS/750 FLIGHT CYCLES/4 CALENDAR MONTHS.

Part: DOOR FRAME — DAMAGED (FRAME 16) · airframe 82,279 hrs · 36,330 cycles

DOOR FRAME EXCEEDS MAXIMUM HOLE DIAMETER AT DOOR STOP FITTING NR 1 FR 16 RT. CORRECTIVE ACTION: COMPLIED WITH ER/A 588845-14 AD REV ORIGINAL. OK FOR SERVICE.

Part: DOOR FRAME — DAMAGED (FRAME 16) · airframe 82,279 hrs · 36,330 cycles

DOOR FRAME EXCEEDS MAXIMUM HOLE DIAMETER AT DOOR STOP FITTING NR 7 FR 16 RT. CORRECTIVE ACTION: COMPLIED WITH ER/A 588845-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FRM 68) · airframe 82,279 hrs · 36,330 cycles

CRACK ON FRAME 68 LT DOOR STOP 1 LOWER INBOARD HOLE. CORRECTIVE ACTION: PERFORMED REPAIR, PER 53-41-12-205-010. MONITOR INSPECTION AT 3200 FC INTERVALS.

Part: DAMPER — MALFUNCTIONED (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

PASSENGER CREW DOOR 842 DAMPER NOT WORKING CORRECTLY. CORRECTIVE ACTION: REPLACED DAMPER, PER A320 FAM AMM 52-13-14-0401.

Part: SKIN — GOUGED (FUSELAGE) · airframe 82,279 hrs · 36,330 cycles

GOUGE EXTERNAL SKIN LOCATED BETWEEN FR 51 TO FR 52A AND BETWEEN STR 36R TO STR 40R AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED HFEC AND CRACK NOT FOUND/WITHIN LIMITS. PUT ON MONITOR. RECHECK IS REQUIRED AT INTERVALS OF 21,900 FC.

Part: BUSHING — EXCESS PLAY (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

EXCESSIVE PLAY ON BUSHINGS PASSENGER CREW DOOR 831 UPPER CONNECTION LINK AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED BUSHINGS, OK FOR SERVICE.

Part: DUMMY RAIL — CORRODED (FWD GALLEY) · corrosion level 2 · airframe 82,279 hrs · 36,330 cycles

CORROSION RAIL DUMMY Y503.2 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED RAIL DUMMY Y503.2 LOCATED AT FWD GALLEY AREA, AS PER A320 SRM 51-72-11 AND DWG D53110984.

Part: STRINGER — CORRODED (AFT CARGO) · corrosion level 2 · airframe 82,279 hrs · 36,330 cycles

CORROSION ON STRINGER 43L AT FRAME 55 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER SECTION LOCATED FR 54 TO FR 56 STR 43L AFT CARGO COMPARTMENT, AS PER A320 SRM 51-72-11 AND 51-42-11.

Part: DAMPER — MALFUNCTIONED (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

PASSENGER CREW DOOR 831 DAMPER DOES NOT WORK CORRECTLY DURING OPENING AND CLOSING. CORRECTIVE ACTION: REPLACED DAMPER.

Part: HINGE FITTING — DETERIORATED (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

DETERIORATED PASSENGER CREW DOOR 841 UPPER HINGE FITTING AT FR 16 RT AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED UPPER HINGE FITTING AT FR 16 RT OF PASSENGER CREW DOOR 841, AS PER A20 FAM AMM 52-11-31.

Part: FLOORBEAM — CORRODED (FRAME 20) · corrosion level 2 · airframe 82,279 hrs · 36,330 cycles

CORROSION FLOOR BEAM -Y1292 AT LEVEL OF FR 20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292 AT LEVEL OF FR 20 AT FWD GALLEY AREA, AS PER A320 SRM 51-72-11.

Part: STRINGER — CORRODED (WING) · airframe 82,279 hrs · 36,330 cycles

AT M CHECK CORROSION WAS FOUND WING CENTER TOP AFT PANEL Y-1292 STRINGER. CORRECTIVE ACTION: REPAIRED PER ER/A 532405-14 REV A. OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 82,279 hrs · 36,330 cycles

CORROSION ON FLOOR BEAM -Y450 APPROXIMATELY AT LEVEL OF FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y450 APPROXIMATELY AT LEVEL OF FR 68 AT AFT GALLEY AREA, AS PER A320 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 82,279 hrs · 36,330 cycles

CORROSION ON FLOOR BEAM -Y765 AT LEVEL OF FR 68 AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOCATED FR 66+5" TO FR 70 AFT GALLEY AREA, AS PER SRM A320 51-72-11.

Part: HINGE FITTING — DETERIORATED (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

DETERIORATED PASSENGER CREW DOOR 831 UPPER HINGE FITTING AT FR 16, FWD GALLEY AREA. CORRECTIVE ACTION:REPLACED UPPER HINGE FITTING AT FR 16 OF PASSENGER CREW DOOR. OK FOR SERVICE.

Part: DAMPER — MALFUNCTIONED (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

PASSENGER CREW DOOR 841 DAMPER NOT WORKING CORRECTLY DURING OPENING AND CLOSING. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR DAMPER.

Part: BUSHING — EXCESS PLAY (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

EXCESSIVE PLAY ON PASSENGER CREW DOOR 841 ON BONDED BUSHINGS OF UPPER CONNECTION LINK AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED BONDED BUSHINGS OF UPPER CONNECTION LINK OF PASSENGER CREW DOOR 841. OK FOR SERVICE.

Part: BUSHING — EXCESS PLAY (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

EXCESSIVE PLAY IN PASSENGER CREW DOOR 842 ON BUSHINGS OF UPPER CONNECTION LINK. CORRECTIVE ACTION: REPLACED BUSHINGS. OK FOR SERVICE.

Part: ROLLER — DETERIORATED (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

FOUND DETERIORATED PASSENGER CREW DOOR 831 LOWER GUIDE ROLLERS FWD AND AFT POSITIONS. CORRECTIVE ACTION: REPLACED LOWER GUIDE ROLLERS FWD AND AFT POSITIONS AT DOOR 831. OK FOR SERVICE.

Part: TORSION BAR — OUT OF ADJUST (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

OUT OF ADJUSTMENT TORSION BAR BELLCRANK PASSENGER CREW DOOR 832. CORRECTIVE ACTION: PERFORMED ADJUSTMENT OF RIGGING POINT OF TORSION BAR BELLCRANK OF PASSENGER/CREW DOOR 832 AT AFT GALLEY.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 82,279 hrs · 36,330 cycles

PASSENGER CREW DOOR 831 OUT OF ADJUSTMENT. CORRECTIVE ACTION: PERFORMED ADJUSTMENT ON PASSENGER CREW DOOR NUMBER 831. OK FOR SERVICE.

Part: DOOR — OUT OF RIG (MAIN PAX) · airframe 82,279 hrs · 36,330 cycles

PASSENGER CREW DOOR 841 WAS OUT OF RIG. CORRECTIVE ACTION: PERFORMED ADJ OF PASSENGER CREW DOOR 841. OK FOR SERVICE.

Part: ROLLER — DETERIORATED (PAX DOOR) · airframe 82,279 hrs · 36,330 cycles

DETERIORATED ROLLER PASSENGER CREW DOOR 842 FWD AND AFT LOWER POSITIONS. CORRECTIVE ACTION: REPLACED ROLLER PASSENGER CREW DOOR FWD AND AFT LOWER POSITIONS AT AFT GALLEY AREA DOOR 842. OK FOR SERVICE.

Part: ROLLER — DETERIORATED (CREW DOOR) · airframe 82,279 hrs · 36,330 cycles

DETERIORATED ROLLER PASSENGER CREW DOOR 832 FWD AND AFT LOWER POSITION. CORRECTIVE ACTION: REPLACED ROLLERS ON PASSENGER CREW DOOR 832 FWD AND AFT LOWER POSITIONS AT AFT GALLEY AREA. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,594 hrs · 34,950 cycles

ONE OVERWING EXIT HANDLE LIGHT INOP, R/R LIGHT ASSY.

Part: ACCESS PANEL — MISSING (RT WING) · airframe 78,978 hrs · 34,671 cycles

PDA PART DEPARTING AIRCRAFT. LOG 5580746 RIGHT WING ANTI-ICE VALVE ACCESS COVER MISSING, PANEL 622WB, PERFORMED ERA 576058-14MA REV ORIGINAL. ACCOMPLISHED SEC 1, NO LEAK NOTED, NO SECOUNDARY DEFECTS NOTED. INSTALLED PLATE AND SPEED TAPE AS REQUIRED PER ERA.

Part: ATTACH BRACKET — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 78,791 hrs · 34,593 cycles

LEFT WING NR 1 PYLON INBOARD SIDE, FAIRING ATTACH BRACKET HAS CORROSION ON FRONT AND BACK SIDES, LOCATED BELOW REAR SPAR. REPLACED BRACKET IAW DWG D54530251.

Part: BRACKET — CORRODED (WING) · corrosion level 2 · airframe 78,791 hrs · 34,593 cycles

CORROSION ON ADJACENT BRACKET FOUND ON N/R 97. REMOVED AND REPLACED BRACKET IAW DWG D54510054.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 78,791 hrs · 34,593 cycles

LEFT HAND PRESSURE DECK HOLE A CRACKED. INSTALLED REPAIR IAW EM5311-01171-04A AND ERA 594797-14AD REV O.

Part: COMPUTER — FAULTY (ELEVATOR SYS) · airframe 77,300 hrs · 33,859 cycles

EXPERIENCED AN ELAC 1 FAULT WITH AN UNCOMMANDED AIRCRAFT ROLL, DISCONNECTED ELAC 1 PER QRH AND CONTINUED THE FLIGHT. REPLACED ELAC 1.

Part: STRINGER — CORRODED (FRAMES 56-57) · corrosion level 2 · airframe 76,267 hrs · 33,388 cycles

CORROSION FOUND ON STRINGER 43L BETWEEN FRAMES 56 AND 57. REPLACED THE STRINGER IAW SRM 53-00-13, FIG 201.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 73,886 hrs · 32,305 cycles

EPSU UNIT FWD L MESSAGE FOR EMERGENCY LIGHTS SYS CHECK. R & R FWD EPSU UNIT 10WL.

Part: FRAME — CRACKED (FRM 68) · airframe 73,347 hrs · 32,086 cycles

CRACK INDICATION FOUND AT RADIUS ON FRAME 68 AT STRINGER 8R. REPAIRED THE FRAME IAW ER/A 553542-14AD REV ORIGINAL.

Part: FRAME — CORRODED (FRM 16) · airframe 73,347 hrs · 32,086 cycles

CORROSION ON FRAME 16, STRINGER 23R. REPAIRED THE FRAME IAW ERA 532404-14AD REV A.

Part: WEB — CORRODED (FRAMES 69-70) · airframe 73,343 hrs · 32,085 cycles

CORROSION ON WEB IN AFT GALLEY AREA, STRINGER 23L BETWEEN FRAME 69 TO FRAME 70. REPLACED THE WEB AND FASTENERS IAW SRM 51-72-11 AND DRAWING D53470100

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 73,339 hrs · 32,084 cycles

EMERGENCY LIGHT LENS DAMAGED, REPLACED THE LENS

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,919 hrs · 31,888 cycles

LEFT SIDE WING BOX FRAME 43 CRACK INDICATION. REPAIRED PER WORKCARD 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.

Part: DOOR FRAME — DAMAGED (FRM 20) · airframe 82,279 hrs · 36,330 cycles

FR 20 LT ELONGATED HOLE AT DOOR STOP 1, REPAIRED PER ER/A 532986-1. CORRECTIVE ACTION: PERFORMED REPETITIVE INSPECTION ON FR 20 LT AT DOOR STOP 1 HOLE NR 16, AS PER ER/A 532986-14. OK TO CONTINUE.

Part: SKIN — CORRODED · airframe 70,184 hrs · 30,590 cycles

AFT ATG4 ANTENNA STEP 2A AN AREA OF POSSIBLE CORROSION, C/W PRI ERA 542338-14AD, REV 0 STEP 2, WORKED THE CORROSION IAW SRM CH 51-73-00.

Part: DOOR FRAME — CORRODED (FRM 66) · airframe 67,855 hrs · 29,466 cycles

DURING INSPECTION, FOUND CORROSION ON DOOR AFT FACE FRAME 66 STRINGERS 22L - 23L. PERFORMED TIME LIMITED REPAIR IAW ERA 532979-14 REV. ORIGINAL AND PRI 532979-14 REV. 0, 1 AND 2.

Part: SKIN — BENT (PAX DOOR) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND BENT PASSENGER CREW DOOR EXTERNAL SKIN, 841 DOOR, UPPER PLATE ON UPPER FUSELAGE. REPLACED UPPER PLATE LOCATED ON UPPER FUSELAGE, AT PASSENGER CREW DOOR EXTERNAL SKIN, 841 DOOR, IAW SRM 51-72-11 AND DWG 52111475.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 41R TO STR 42R, L=0.800", W=0.300", D=0.004". REPLACED CLEAT LOCATED FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 41R TO STR 42R IAW SRM 51-72-11 AND DWG D53231586.

Part: STRINGER — CORRODED (FRAMES 67-68) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 27L BETWEEN FRAMES 67 AND 68 IN BULK CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 27L IAW ERA 533417-14 REV.ORIGINAL SEC.1 AND PRI 533417-14 REV.O.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION SHEAR TIE ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STRINGERS 41R TO 42R. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53231586.

Part: STRINGER — CORRODED (FRAME 31-34) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FWD CARGO COMPARTMENT ON STRINGER 43L BETWEEN FRAME 31 TO FRAME 34 L=1" W=0.5" D=0.003. REPLACED STRINGER ON FWD CARGO COMPARTMENT ON STRINGER 43L BETWEEN FRAME 30+15" TO FR 34+6" IAW SRM 51-72-11 AND DRAWING D53231626.

Part: STRINGER — CORRODED (FRAMES 29-31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 40R ON FWD CARGO COMPARTMENT BETWEEN FRAME 29 TO FRAME 31 L=1" W=0.5" D=0.003. PERFORMED PERMANENT REPAIR ON STRINGER IAW SRM 53-0013 FIG 201(SHEET 2).

Part: STRINGER — CORRODED (FRAMES 31-34) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION STR ON FWD CARGO COMPARTMENT ON STR 41L BETWEEN FRAME 31 TO FRAME 34, L=1", W=0.5", D=0.003" . REPLACED STR LOCATED ON FWD CARGO COMPARTMENT ON STR 41L BETWEEN FRAME 31 TO FR 34 IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STR 43L TO STR 44, L=0.850", W=0.300", D=0.005", SSI532180. REPLACED CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STR 43L TO STR 44 IAW SRM 51-72-11 AND DWG D53231626 AND D53230320.

Part: SKIN — DENTED (FRAME 25) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL SKIN AT FR.25+8.5" AND STR.42L ON LOWER FUSELAGE. PERFORM PERMANENT REPAIR ON EXTERNAL SKIN AT LEVEL FR 25+8.5" ON LOWER FUSELAGE IAW SRM 53-00-11, PARAGRAPH 4W, STEP 7, FIG 239.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STRINGER 39R TO STRINGER 40R L=1.000" W=0.500" D=0.004". REPLACED SHEAR TIE IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STRINGER 39R TO STRINGER 40R IAW SRM 51-72-11 AND DWG D53231626, D53230320.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 34 BETWEEN STRINGER 43R TO STRINGER 44, L=0.850", W=0.500", D=0.003. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 34 BETWEEN STR 43R TO STR 44R IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STRINGER 41 TO STRINGER 42R, L=0.900", W=0.550", D=0.002. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 41R TO STR 42R IAW SRM A320 51-72-11, DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 42L TO STR 43L, L=0.950", W=0.600", D=0.004", SSI 532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 42L TO STR 43L IAW SRM 51-72-11 AND DWG D53231626.

Part: FITTING — WORN (PAX DOOR) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND WEAR ON MAIN DOOR FITTING FORWARD POSITION ON LT MLG. REPLACED FITTING ON MAIN DOOR FORWARD POSITION ON LT MLG IAW SRM 51-72-11 AND DWG D53370600.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 33 BETWEEN STRIN GER 42R TO STRINGER 43R L=0.800 W=0.400 D=0.004 .(SSI 532180). REPLACED CLEAT IN FWD CARGO COMPARTMENT FR 33 BETWEEN STR 42R TO STR 43R IAW SRM 51-72-11. DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 40L TO STR 41L, L=1.000", W=0.300", D=0.003". SSI 532180). REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 40L TO STR 41L IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 33 BETWEEN STR 43R TO STR 44, L=0.950, W=0.300, D=0.002. SSI 532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON EXACT LOCATION, FRAME 33 BETWEEN STR 43 LT SIDE TO STR 43 RT IAW SRM 51-72-11, DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STR 40L TO STR 41L L=1.000", W=0.800", D=0.008", SSI532180. REPLACED CLEAT ON FWD CARGO COMPARTMENT LOCATED FRAME 29 BETWEEN STR 40L, TO STR 41L IAW SRM 51-72-11 AND DWG D53231626 AND D53230320.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 40L TO STR 41L, L=0.600", W=0.400", D=0.002, SSI 532180. REPLACED CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 40L TO STR 41L IAW SRM 51-72-11 AND DWG D53231645.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 41L TO STR 42L, L=1.000", W=0.400", D=0.004, SSI 532180. REPLACED CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 41L TO STR 42L IAW SRM 51-72-11 AND DWG D53231626 AND D53230320.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y254 AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 21, L=1" W=0.200", D=0.003", SSI 531189. REPLACED FLOORBEAM -Y254 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24 IAW ER/A NR 532969-14, PRI 532969-14 AND SRM 51-72-11 DWG D53110900.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT IN FRAME 32 BETWEEN STR 41L TO STR 42L L=0.900", W=0.400", D=0.004", SSI532180. REPLACED CLEAT LOCATED ON FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STR 41L TO STR 42L IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 34 BETWEEN STR 42R TO STR 43R, L=1.000", W=0.450", D=0.003", SSI532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FR 34 BETWEEN STR 42R TO STR 43R IAW SRM 51-72-11.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 40R TO STR 41R, L=1.100", W=0.480", D=0.001". SSI532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 40R TO STR 41R IAW SRM 51-72-11 AND DWG D53231645.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 33 BETWEEN STR 40L TO STR 41L L=0.950", W=0.400", D=0.003". SSI531280. REPLACED CLEAT IN FWD CARGO COMPARMENT ON FRAME 33 BETWEEN STR 40L TO STR 41L IAW SRM 51-42-11 AND DWG D 53231626.

Part: FLOOR SUPPORT — CORRODED (FRAMES 47-64) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE EVALUATED AND FOUND OUT LIMITS ON JOB 250 00-2032-DE, MEAURES OF REWORK ARE L=3.219", W=0.342", D = 0 .075" IN PASSENGER CABIN FROM FRAME 47 TO FRAME 64 - Y 1292. REPLACED SEAT TRACK FROM FRAME 47 TO FRAME 64 -Y1292 AND PERFORMED PERMANENT REPAIR AT LEVEL FR 55 + 9" IAW SRM 53-41-15 PARA 5.B, FIGURE 202, SRM 51-72-11 AND DWG D53476950, D53472000.

Part: SHEAR TIE — CORRODED (FRAME 33) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 33 BETWEEN STR 40R TO STR 41R L=0.900", W=0.450", D=0.002". NOT SSI532180). REPLACED CLEAT LOCATION ON FWD CARGO COMPARTMENT FRAME 33 TO STR 40R TO STR 41R IAW SRM 51-72-11 DG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION CLEAT ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STR 42L TO STR 43L, L=1", W=0.5", D=0.003", SSI 532180. REPLACED CLEAT LOCATED ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STR 42L TO STR 43L SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 42L TO STR 43L, L=0.900", W=0.300", D=0.004". SSI 532180). REPLACED CLEAT LOCATED IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STRINGER 42L TO STRINGER 43L IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 43R TO STR 44, L=1.000", W=0.400", D=0.004". SSI 532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 43R TO STR 43L IAW SRM 51-72-11 AND DWG D53230320.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 42R TO STR 43R, L=1.000", W=0.340", D=0.003". SSI 532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 42R TO STR 43R IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 39L TO STR 40L, L=0.950", W=0.400", D=0.003". SSI 532180. REPLACED CLEAT LOCATED ON FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STR 39L TO STR 40L IAW SRM 51-72-11 AND DWG D53231626.

Part: STRINGER — CORRODED (FRAMES 29-30) · airframe 72,979 hrs · 31,924 cycles

CORROSION ON STRINGER 42R FWD CARGO BAY BETWEEN FRAMES 29 TO 30. REPLACED THE DOUBLER.

Part: STRINGER — CORRODED (FRAMES 65-66) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON STR 31R BETWEEN FRAME 65 AND FRAME 66 IN BULK CARGO COMPARTMENT NT. SSI 534144. REPLACED STR 31R BETWEEN FR 65 TO FR66 IN BULK CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53480505 AND D53470250.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORRODED CLEAT ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STR 43L TO STR 44, L=1", W=0.5", D=0.003", SS1 532180. REPLACED CLEAT LOCATED ON FWD CARGO COMPARTMENT ON FR29 BETWEEN STR 43L TO STR 43R IAW SRM A320 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 31 BETWEEN STRINGER 39R TO STRINGER 40R, L=1.000", W=0.450", D=0.003". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FR31 BETWEEN STR 39R TO STR 40R IAW SRM A320 51-72-11 AND DWG D53231645 AND D53230811.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH DOOR 833, LT VERTICAL SEGMENT FRAME ON PASSENGER CABIN. SSI 522102. REPLACED LT VERTICAL SEGMENT FRAME ON EMERGENCY EXIT DOOR 833 IAW SRM 51-72-11 AND DWG D522-79010.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STR 42L TO STR 43L, L=0.650", W=0.450", D=0.004", SSI532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STR 42L TO STR 43L AS IAW SRM 51-72-11 AND DWG D53231626.

Part: STRINGER — CORRODED (FRAMES 65) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON STR LOCATED AT LEVEL FRAME 65 AND STR 44 IN BULK CARGO COMPARTMENT. REPAIRED STR LOCATED AT LEVEL FRAME 65 AND STR 44 IN BULK CARGO COMPARTMENT IAW SRM 53-00-13, PARAGRAPH 4.A, FIG 201.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION CLEAT ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STRINGER 41L TO STRINGER 42L L=1", W=0.5", D=0.003". REPLACED CLEAT ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STRINGER 41L TO STRINGER 42L IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION CLEAT ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STRINGER 40R TO STRINGER 41R, L=1", W=0.4", D=0.004". SSI 532180. REPLACED CLEAT LOCATED ON FWD CARGO COMPARMENT ON FRAME 29 BETWEEN STG 40R TO STG 41R IAW SRM 51-72-11 AND DWG D53230320.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH 834 DOOR LT VERTICAL SEGMENT FRAME ON PASSENGER CABIN. SSI 522102. REPLACED VERTICAL SEGMENT FRAME ON EMERGENCY EXIT DOOR 834 IAW SRM 51-72-11 AND DWG D522-79010.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 32 BETWEEN STRINGER 40R TO STRINGER 41R, L=1.000", W=0.500", D=0.003". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FR32 BETWEEN STRINGER 40R TO 41R IAW SRM 51-72-11 AND DWG D53231626.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH 834 DOOR RT VERTICAL SEGMENT FRAME ON PASSENGER CABIN. SSI 522102. REPLACED RT VERTICAL SEGMENT FRAME ON EMERGENCY EXIT DOOR 834 IAW SRM 51-72-11 AND DWG D522-79010.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION CLEAT ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STRINGER 42R TO STIRNGER 43R, L=1", W=0.5", D=0.002". SSI 532180. REPLACED CLEAT ON FWD CARGO COMPARTMENT ON FRAME 29 BETWEEN STR 42R TO STR 43R IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION CLEAT ON FWD CARGO COMPARTMENT ON FR 29 BETWEEN STR 40L TO STR 41L, L=1", W=0.5", D=0.003". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FR29 BETWEEN STR 40L TO STR 41L IAW SRM 51-72-11 AND DWG D53231626.

Part: TEE FITTING — CORRODED (EMERGENCY EXIT) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON EMERGENCY EXIT DOOR 843 RT LOWER T-SECTION IN PASSENGER CABIN, SSI 522102-01-1 AND ATTACH FORM 5100- REPLACED LOWER T-SECTION ON EMERGENCY EXIT DOOR 843RT SIDE. CORROSION MEASURES L=0.800", W=0.410", D=0.003".

Part: SUPPORT FITTING — DAMAGED (FRAME 55) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND ELONGATED HOLE SUPPORT FITTING -Y765, FRAME 55 IN PASSENGER CABIN. REPLACED SUPPORT FITTING -Y765, FRAME 55 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D53472055.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION SPLICE ON FWD CARGO COMPARTMENT ON STRINGER 41L BETWEEN FRAME 30 TO FRAME 31, L=1", W=0.5", D=0.003". REPLACE SPLICE ON FWD CARGO COMPARTMENT, ON STR 41L BETWEEN FRAME 30 TO FRAME 31 IAW SRM 51-72-11 AND DWG D53231544.

Part: FLOOR PANEL — CORRODED (GALLEY) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON INSERT FLOOR PANEL 261NF AT AFT GALLEY AREA, 4 EA. REPLACED FLOOR PANEL 261NF AT AFT GALLEY AREA IAW SRM 53-02-00, PAR 8.H, FIG 209 AND IRM 9701, REV G.

Part: ANGLE — CRACKED (ESCAPE HATCH) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH DOOR 844 RT SEGMENT ANGLE TRANSMITTING PROFILE ON PASSENGER CABIN.

Part: ANGLE — CRACKED (ESCAPE HATCH) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH DOOR 843 LT SEGMENT ANGLE TRANSMITTING P-PROFILE ON PASSENGER CABIN. REPLACED SEGMENT ANGLE TRANSMITTER PROFILE ON EMERGENCY HATCH DOOR 843 LT IAW SRM 51-72-11 AND DWG D52279010.

Part: FITTING — CORRODED (FRAME 66) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 66, AT LEVEL STR 23L AT AFT GALLEY AREA L=0.196", W=0.075", D=0.001". REPLACED CORNER FITTING FRAME 66 AT LEVEL STR 23L AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STRINGER 39L TO STRINGER 40L, L=0.740", W=0.200", D=0.004". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STR 39L TO STR 40L IAW SRM 51-72-11 AND DWG D 53231626.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STRINGER 41L TO STRINGER 42L, L=0.950", W=0.640", D=0.006". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STRINGER 41L TO STRINGER 42L IAW SRM 51-72-11 AND DWG D53231626.

Part: STRUCTURE — CORRODED (FRAMES 66-68) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FR 66 TO FR 68 AT STR 23L AT AFT GALLEY AREA L=0.700", W=0.400", D=0.002". REPLACED LOWER SILL LOCATED BETWEEN FRAME 66 AND FRAME 68 AT STR 23L AT AFT GALLEY AREA IAW SRM 51-72-11, DWG D53480019.

Part: FITTING — CORRODED (FRAME 68) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68 AT LEVEL STR 23L AT AFT GALLEY AREA, L=0.160", W=0.050", D=0.001". REPLACED CORNER FITTING, LOCATED FRAME 68 AT LEVEL STR 23L AT AFT GALLEY AREA IAW SRM 51-72-11, DWG D53480019.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STR 42R TO STR 43R, L=0.500", W=0.450", D=0.006". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STR 42R TO STR 43R IAW SRM 51-72-11 AND DWG D53231626.

Part: ANGLE — CRACKED (ESCAPE HATCH) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH DOOR 834 LT SEGMENT ANGLE TRANSMITTING P-PROFILE ON PASSENGER CABIN. REPLACED SEGMENT ANGLE TRANSMITTING PROFILE ON EMERGENCY EXIT HATCH DOOR 834 RT IAW SRM 51-72-11 AND DWG D52279010.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 40R TO STR 41R, L=0.800", W=0.350", D=0.003". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 40R TO STR 41R IAW SRM 51-72-11 AND DWG D 53231586.

Part: ANGLE — CRACKED (ESCAPE HATCH) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH 834 DOOR LT SEGMENT ANGLE TRANSMITTING P-PROFILE ON PASSENGER CABIN. REPLACED SEGMENT ANGLE TRANSMITTER PROFILE ON EMERGENCY HATCH 834 DOOR LT PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279010.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 42L TO STR 43L, L=0.800", W=0.500", D=0.002". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 30 BETWEEN STR 42L TO STR 43L IAW SRM 51-72-11 AND DWG D53233226 AND D53230320.

Part: STRINGER — CORRODED (FRAMES 27-28) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION STRINGER ON FWD CARGO COMPARTMENT ON STRINGER 43L BETWEEN FRAME 27 TO FRAME 28, L=1", W=0.5", D=0.003". SSI 532180. PERFORMED PERMANENT REPAIR ON FWD CARGO COMPARTMENT ON STR 43L BETWEEN FRAME 27 TO FRAME 28 IAW SRM 53-00-13, PAGE 220 TO PAGE 227/228, FIG 202, SHEET 2.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STRINGER 40L TO STRINGER 41L, L=0.840", W=0.500", D=0.006". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 28 BETWEEN STRINGER 40L TO STRINGER 41L IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT ON FWD CARGO COMPARTMENT ON FRAME 30 AND STRINGER 40L L=0.900", W=0.300", D=0.003". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 30 AND STRINGER 40L IAW SRM 51-72-11 AND DWG D53231626 AND D53230320.

Part: DOOR FRAME — CRACKED (ESCAPE HATCH) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH DOOR 843 LT VERTICAL SEGMENT FRAME ON PASSENGER CABIN. REPLACED EMERGENCY EXIT HATCH DOOR 843 LT VERTICAL SEGMENT FRAME ON PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279040.

Part: ANGLE — CRACKED (ESCAPE HATCH) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH DOOR 843 RT SEGMENT ANGLE TRAMSMITTING P-PROFILE ON PASSENGER CABIN. REPLACED EMERGENCY EXIT HATCH DOOR 843RT SEGMENT ANGLE TRANSMITTING PROFILE ON PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279040.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 27 BETWEEN STRINGER 41L TO STRINGER 42L L=0.900", W=0.250", D=0.004". REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 27 BETWEEN STRINGER 41L TO STRINGER 42L IAW SRM 51-72-11 AND DWG D53231212.

Part: ANGLE — CRACKED (ESCAPE HATCH) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT HATCH DOOR 833 LH SEGMENT ANGLE TRANSMITTING P-PROFILE ON PASSENGER CABIN. REPLACED SEGMENT ANGLE TRANSMITTING P-PROFILE ON EMERGENCY EXIT HATCH DOOR 833LH IAW SRM 51-72-11 AND DWG D52279010.

Part: FITTING — CORRODED (FRAME 20) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION CORNER FITTING ON PASSENGER CABIN ON FRAME 20 AND STRINGER 23R, L=0.500, W=0.200, D=0.002. REPLACED CORNER FITTING ON PASSENGER CABIN ON FRAME 20 AND STR .23R IAW SRM 51-72-11 AND SRM 51-42-11 AND DWG D53135058.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK LOCATED ON Y-1292 BETWEEN FRAME 41 TO FRAME 47 WITH MEASURES D=0.032", W=0.360", L=4.135" AND FOUND OUT OF LIMITS IAW AMDS 2500-2031 ON PASSENGER CABIN, THIS SEAT TRACK MUST BE REPLACED. REPLACED SEAT TRACK LOCATED ON Y-1292 BETWEEN FRAME 41 TO FRAME 47 IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CRACKED (FRAMES 24-29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON FLOORBEAM -Y254 BETWEEN FRAME 24 TO FRAME 29 IN PASSENGER CABIN. REPLACED FLOORBEAM -Y254 BETWEEN FRAME 24 TO FRAME 35 IAW SRM 51-72-11 AND DWG D53110900.

Part: STRINGER — CORRODED (FRAMES 27-29) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER ON FWD CARGO COMPARTMENT ON STRINGER 44 BETWEEN FRAME 27 TO FRAME 29, L=1", W=0.5", D=0.003". REPLACED STR 44 SECTION ON FWD CARGO COMPARTMENT LOCATED BETWEEN FRAME 27 TO FRAME 29 IAW SRM 51-72-11.

Part: STRUCTURE — CORRODED (FRAMES 16-20) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 20 ON STRINGER 23L, L=0.500", W=0.200", D=0.001". REPLACED LOWER SILL AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 20 ON STRINGER 23L IAW SRM 51-72-11 AND DWG D53110339.

Part: FLOOR SUPPORT — DAMAGED (FRAMES 24-34) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND MISSING MATERIAL FLOORBEAM +Y254 BETWEEN FRAME 24 TO FRAME 34 IN PASSENGER CABIN. REPLACED FLOORBEAM +Y254 BETWEEN FRAME 24 TO FRAME 35 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D53110900.

Part: FITTING — CORRODED (FRAMES 16-20) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION CENTER FITTING ON PASSENGER CABIN FROM FRAME 16 TO FRAME 20 AND STRINGER 23L, L=0.500, W=0.200, D=0.002. REPLACED CENTER FITTING ON PASSENGER CABIN FROM FRAME 16 TO FRAME 20 AND STR 23L IAW SRM 51-72-11 AND SRM 51-42-11 AND DWG D53112225.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK LOCATED ON Y-765 BETWEEN FRAME 41 TO FRAME 47 WITH MEASURES D=0.036", W=0.360", L=3.906", EVALUATED AND FOUND OUT OF LIMITS IAW AMDS 2500-2031. REPLACED SEAT TRACK LOCATED ON Y-765 BETWEEN FRAME 41 TO FRAME 47 IAW SRM 51-72-11 AND DWG D53370500.

Part: STRINGER — CORRODED (FRAMES 67-68) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON STR 28L CONNECTION SECTION BETWEEN FRAME 67 AND FRAME 68 IN BULK CARGO COMPARTMENT. REPLACED CONNECTION SECTION BETWEEN FRAME 67 AND FRAME 68, STR 28L IN BULK CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53480505.

Part: FITTING — CORRODED (FRAME 20) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION CORNER FITTING ON PASSENGER CABIN ON FRAME 20 LT SIDE AND STRINGER 23L, L=0.500, W=0.200, D=0.002. REPLACED CORNER FITTING ON PASSENGER CABIN ON FRAME 20 LT SIDE AND STR 23L IAW SRM 51-72-11 AND DWG D53112225.

Part: STRUCTURE — CORRODED (FRAMES 16-20) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 20 ON STRINGER 23R, L=0.500", W=0.200", D=0.0001". REPLACED LOWER SILL AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 20 ON STR 23R IAW SRM 51-72-11 AND DWG D53110339.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK LOCATED ON Y765 BETWEEN FRAME 41 TO 47 WITH MEASURES D=0.015", W=0.770", L=3.311" EVALUATED AND FOUND OUT OF LIMITS IAW AMDS 2500-2031 ON PASSENGER CABIN. THIS SEAT TRACK MUST BE REPLACED, REPLACED SEAT TRACK LOCATED ON Y765 BETWEEN FRAME 41 TO FRAME 47 IAW SRM 51-72-11, PAG 1-2 AND DWG D53370500.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1162 LOCATED BETWEEN FRAME 67+15" AND FRAME .69 AT AFT GALLEY AREA L=1", W=0.500", D=0.002". REPLACED FLOORBEAM -Y1162 LOCATED BETWEEN FRAME 67+15" AND FRAME 69 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 72,979 hrs · 31,924 cycles

CORROSION ON STRINGER SPLICE 42L IN FWD CARGO BAY BETWEEN FRAMES 30 - 31. REPLACED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y512 LOCATED BETWEEN FRAME 64 AND FRAME 66 AT AFT GALLEY AREA, L=0.500", W=0.400", D=0.003". REPLACED FLOORBEAM -Y512 LOCATED BETWEEN FRAME 64 AND FRAME 66 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472230.

Part: SEAT TRACK — CORRODED (FRAMES 24-35) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y765, FRAME 24 TO 35 WITH MEASURES D=0.040", W= =0.377", L=4.994". EVALUATED AND FOUND OUT OF LIMITS IAW AMDS 2500-20, 30 IN PASSENGER CABIN. THIS SEAT TRACK MUST BE REPLACED. REPLACED SEAT TRACK +Y765 BETWEEN FRAME 24 TO FRAME 35 IAW SRM 51-72-11 AND DWG D53110900.

Part: WEB — CORRODED (FRAME 20) · airframe 72,979 hrs · 31,924 cycles

CORROSION ON WEB AT FRAME 20 AT LEVEL OF STRINGER 23R AT FWD GALLEY AREA. REPLACED WEB IAW SRM.

Part: FLOOR PANEL — CRACKED (GALLEY) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON FLOOR PANEL 262FF AT AFT GALLEY AREA. REPLACED FLOOR PANEL 262FF AT AFT GALLEY AREA MEASURE OF CRACK L=3".

Part: FLOOR PANEL — CRACKED (GALLEY) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CRACK ON FLOOR PANEL 261EF AT AFT GALLEY AREA. REPLACED FLOOR PANEL 261EF AT AFT GALLEY AREA MEASURE OF CRACK L=2.5".

Part: STRINGER — CORRODED (FRAMES 68-69) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 42R BETWEEN FRAME 68 AND FRAME 69 IN BULK CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON STRINGER 42R BETWEEN FRAME 68 AND FRAME 69 IN BULK CARGO COMPARTMENT IAW SRM 53-00-13, TABLE 201, PAR 4A, FIG 201.

Part: SEAT TRACK — CORRODED (FRAME 47-64) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE EVALUATED AND FOUND OUT LIMITS ON JOB 250. REPLACED RAIL SEAT LOC.IN PASSENGER CABIN FROM FRAME 47 TO FRAME 64 -Y765 IAW SRM 51-72-11 AND DWG D53472079, D53476950, D53472000.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE EVALUATED AND FOUND OUT LIMITS ON JOB 250. REPLACED RAIL SEAT LOCATED IN PASSENGER CABIN FROM FRAME 47 TO FRAME 64 +Y1292 IAW SRM 51-72-11 AND DWG D53476950, D53472000.

Part: STRINGER — CORRODED (FRAME 29-31) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION STRINGER ON FWD CARGO COMPARTMENT ON STRINGER 43L BETWEEN FRAME 29 TO FRAME 31, L=1", W=0.5", D=0.003". REWORKED CORROSION ON STRINGER 43L, SECTION FRAME 29 TO FRAME 30+16" FWD CARGO COMPARTMENT IAW 51-74-00.

Part: SEAT TRACK — CORRODED (FRAMES 24-35) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y1292, FRAME 24 TO 35 WITH MEASURES D= 0.043", W=0.390", L=2.714". EVALUATED AND FOUND PUT OF LIMITS IAW AMDS 2500-2030 IN PASSENGER CABIN. THIS SEAT TRACK MUST BE REPLACED. REPLACED SEAT TRACK +Y1292 FRAME 24 TO FRAME 35 IAW SRM 51-72-11 AND DWG D53231346.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND ELONGATED HOLE ACCESS PANEL 640HB IN RT FUEL TANK. REPLACED ACCESS PANEL 640HB DUE TO OUT OF LIMITS HOLE IAW SRM 57-27-11, PARA 4 B, FIG 102.

Part: FLOORBEAM — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1292 LOCATED BETWEEN FRAME 64 AND FRAME 66+5" AT AFT GALLEY AREA L=0.500", W=0.300", D=0.002". REPLACED FLOORBEAM +Y1292 LOCATED BETWEEN 64 AND FRAME 66+5" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472216.

Part: STRUCTURE — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FRAME 66 AND FRAME 68 AT STR 23R AT AFT GALLEY AREA L=0.800", W=0.400", D=0.002. REPLACED LOWER SILL LOCATED BETWEEN FRAME 66 AND FRAME 68 AT STR 23R AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53470150, D53480019.

Part: SEAT TRACK — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292, FRAME 24 TO 35 WITH MEASURES D=0.037" W, W=0.392", L=1.594", EVALUATED AND FOUND OUT OF LIMITS IAW AMDS 2500-2030 IN PASSENGER CABIN. REPLACED SEAT TRACK -Y1292 FRAME 24 TO FRAME 35 IAW SRM 51-72-11 AND DWG D53231346.

Part: FLOORBEAM — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1225 LOCATED BETWEEN FRAME 66+5" AND FR.67+15" AT AFT GALLEY AREA, L=2" W=0.800", D=0.003", SSI 534147. REPLACED FLOORBEAM -Y1225 LOCATED BETWEEN FR 66+5" AND FR 67+15" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000.

Part: FITTING — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 66 AT STR 23R AT AFT GALLEY AREA L=0,175", W=0.066", D=0..001". REPLACED CORNER FITTING LOCATED AT FRAME 66 AND STR 23R AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.

Part: SEAT TRACK — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765, FRAME 24 TO 35 WITH MEASURES D=0.039", W=0.353", L=2.784". EVALUATED AND FOUND OUT OF LIMITS IAW AMDS 2500-20, 30 IN PASSENGER CABIN. REPLACED SEAT TRACK -Y765, FRAME 24-35 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D53231346.

Part: FLOORBEAM — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y512 LOCATED BETWEEN FRAME 64 AND FRAME 70 AT AFT GALLEY AREA L=2", W=1, D=0.004". REPLACED FLOORBEAM Y512 LOCATED BETWEEN FRAME 64 AND FRAME 70 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOORBEAM — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1225 LOCATED BETWEEN FRAME 66+5" AND FRAME 67+15" AT AFT GALLEY AREA L=0.500", W=0.300", D=0.002". EVALUATED FLOORBEAM +Y1225 LOCATED BETWEEN FRAME 66+5" AND FRAME 67+15" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOORBEAM — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1162 LOCATED BETWEEN FR 67+15" AND FRAME 69 AT AFT GALLEY AREA L=0.200", W=0.150", D=0.001". REPLACED FLOORBEAM +Y1162 LOCATED FRAME 67+15" AND FRAME 69 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472000.

Part: FITTING — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68 AT LEVEL STR 23R AT AFT GALLEY A REA L=0.190"; W=0.080"; D=0.001". REPLACED CORNER FITTING LOCATED FRAME 68 AND AT LEVEL STR 23R AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.

Part: FLOORBEAM — CORRODED · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1292 LOCATED BETWEEN FRAME 64 AND FRAME 66+5" AT AFT GALLEY AREA L=0.500", W=0.250", D=0.001". REPLACED FLOORBEAM -Y1292 LOCATED BETWEEN FRAME 64 AND FRAME 66+5" AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472230.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND DAMAGED ACCESS PANEL 640LB. REPLACED THE ACCESS PANEL.

Part: ACCESS PANEL — DAMAGED (WING) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND DAMAGED ACCESS PANEL 640KB . REPLACED THE ACCESS PANEL IAW SRM 57-27-11, PARA 4.B, FIG 102.

Part: FITTING — CORRODED (FRAMES 66-68) · airframe 72,979 hrs · 31,924 cycles

CORROSION ON CENTER FITTING BETWEEN FRAMES 66 - 68, STRINGER 23L IN AFT GALLEY AREA. REPLACED THE FITTING.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-70) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y465 BETWEEN FRAMES 67+10 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWGS: D534 72000 AND D53470100.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 66+5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOORBEAM — CORRODED (FRAME 66) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM LOCATED BETWEEN -Y254 AND -Y160, FRAME 66. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y160 BETWEEN FRAMES 68 - 70 . REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472000 AND D53470100.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y1292 FRAME 16. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12-24 IAW SRM 51-72-11 AND DWG D53110900.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y765 BETWEEN FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472216.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1292 FRAME 20. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12-24 IAW SRM 51-72-11 AND DWG D53112812.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y765 LOCATED BETWEEN FRAMES 66+5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: DUMMY RAIL — CORRODED (FRAMES 12-16) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON DUMMY RAIL Y503.2 AT FWD GALLEY AREA FROM FRAMES 12 TO 16. REPLACED THE DUMMY RAIL IAW SRM 51-72-11 AND DWG D53112825.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-21) · airframe 67,848 hrs · 29,463 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y189, FRAMES 20 TO 21. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,143 hrs · 29,146 cycles

DURING NON-ROUTINE CHECK, FOUND CID'S PANEL WILL NOT TEST EMERGENCY LIGHTS. MAINTENANCE REPLACED BATTERY OF THE EMERGENCY POWER SUPPLY UNIT AND FUNCTIONAL CHECK WAS NORMAL.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 64,940 hrs · 28,135 cycles

EMERGENCY LIGHTS TEST FAILED. REPLACED ESPU.

Part: BATTERY — FAULTY (CABIN) · airframe 60,453 hrs · 25,944 cycles

DURING NON ROUTINE CHECK, FOUND THE EPSU BATTERY AT FWD LEFT OF 10WL FAULT. MAINTENANCE REPLACED BATTERY AND FUNCTIONAL CHECK WAS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 6,251 hrs · 2,743 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 19A INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT 19A AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 55,735 hrs · 23,778 cycles

DURING EMERGENCY LIGHT TEST FOUND PATH LIGHT AT ROW 22 MODULE MISSING, NEW MODULE INSTALLED AND TESTS OK. (2011-00083)

Part: SKIN — DENTED (L2 DOOR) · airframe 67,433 hrs · 29,281 cycles

DENT ON L2 DOOR SKIN. CUTOUT THE DAMAGED AREA IAW SRM 52-10-00, FIG 209, SHEET 3. FABRICATED A REPAIR DOUBLER IAW SRM 52-10-00, FIG 209 SRM 51-44-11 AND SRM 52-10-00 FIG 209. INSTALLED THE REPAIR IAW SRM 52-10-00, FIG 209 AND SRM 51-42-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,868 hrs · 22,950 cycles

DURING TEST FOUND EXIT LIGHT AT SEAT 24C INOP. REPLACED LIGHT ASSEMBLY AND TESTS OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,492 hrs · 17,024 cycles

DURING EMERGENCY LIGHT TEST DISCOVERED EPSU INT LOAD AFT L FAULT INDICATION. REMOVED AND REPLACED BATTERY. OPS CHECKED GOOD.

Part: CABLE — BROKEN (ESCAPE SLIDE) · airframe 37,914 hrs · 15,847 cycles

DURING LIGHT CHECK, FOUND RIGHT OVERWING SLIDE RELEASE CABLE BROKEN BETWEEN COUPLING AND SLIDE INFLATION BOTTLE. REPLACED SLIDE INFLATION BOTTLE ASSEMBLY WITH CABLE PER AMM.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 32,449 hrs · 13,502 cycles

DURING CLIMB RECEIVED CABIN PRRESSURE EXCESS CABIN ALTITUDE MESSAGE AT 10,000 FT. LEVELED OFF AT 11,000 FT AND MESSAGE WENT AWAY. CLIMBED TO 12,800 FT AND MESSAGE RETURNED. LEVELED OFF AT 12,000 FT AND MESSAGE CLEARED FOLLOWED SHORTLY BY THE SAFETY VALVE OPENING, MASKS DEPLOYED. WHILE RETURNING, RECEIVED CAB PR SYS 1 FAULT MESSAGE. TEST OF CABIN PRESSURE CONTROLLER 1 AND 2 CHECKED GOOD. REPLACED OUTFLOW VALVE AND OPERATIONALLY TESTED GOOD. DISCREPANCY RETURNED DURING FERRY FLT. REMOVED DUST CAP FROM THE AMBIENT PRESSURE PORT OF CABIN PRESSURE CONTROLLER 1. SYSTEM TESTED GOOD AND RETURNED AIRCRAFT TO SERVICE.

Part: BRAKE — FAILED (LT MLG)

DURING POST FLIGHT INSPECTION, FOUND SEVERAL CARBON PIECES AROUND THE NR 1 BRAKE AND WHEEL ASSEMBLY. WHEEL REMOVAL REVEALED THAT THE BRAKE CARBON DISCS (ROTORS AND STATORS) WERE OXIDIZED AND REDUCED TO SEGMENTS. MAINTENANCE REPLACED THE NR 1 BRAKE AND WHEEL ASSEMBLY.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

DURING APPROACH, RECEIVED F/CTL FLAPS LOCKED, ALIGNMENT FAULT. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED CHECK AND RIG OF FLAP SYSTEM, OPERATIONAL CHECK OK.

Part: WINDSHIELD — CRACKED (LT COCKPIT)

DURING TAKEOFF ROLL AT 150 KNOTS, THE CAPTAIN'S WINDSHIELD CRACKED VERTICALLY FROM TOP TO BOTTOM THEN CONTINUED CRACKING IN THE UPPER LEFT CORNER. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO DTW AND LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD. OPERATIONAL CHECK OK.

Part: ACTUATOR — LEAKING (NR 3 SPOILER)

HYD-B RSVR LO LVL ANNUNCIATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 SPOILER ACTUATOR LEAKING. REPLACED THE SAME, LEAK OPS CHECK OK.