N953FD

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

ENGINE 2 PYLON HOLE #14HAS REJECTABLE INDICATION DUE TO CORROSION IN SKIN AND A CRACK INDICATION AT 2 O'CLOCK IN THE DRAG FITTING. ACCOMPLISHED EA F-5730-T0370299 PT1 WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITTING, CRACKS/CORROSION REWORK, MAJOR REPAIR

Part: FRAME — CRACKED (BS 1640 S14R) · airframe 34,871 hrs · 24,523 cycles

BODY STATION 1640 S-14R HAS A REJECTABLE CRACK INDICATION IN TOP I/B HOLE FWD LAYER FUSELAGE-MAINFRAME-INSPECTION OF BODY STATION 1640 FUSELAGE FRAME WEB AT STRINGER S-14R-BOEING ALERT SERVICE BULLETIN 757-53A0112-UPPER INBOARD HOLE-DAMAGE REPAIR. ACCOMPLISHED STEPS 1-16 PER E.A. F-5310-T0370386 P1, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

ENGINE #1 PYLON HOLE #4 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #4, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

LH WING #1 ENGINE DRAG FITTING HOLE #1 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED E.A. F-5730-T0370424 PT1 WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #1, MAJOR REPAIR.

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

LH WING #1 ENGINE DRAG FITTING HOLE #14 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED E.A. F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #14, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

LH WING #1 ENGINE DRAG FITTING HOLE #6 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED EA F-5730-T0370424 PT1 WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #6, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

LH WING #1 ENGINE DRAG FITTING HOLE #16 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #16, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

LH WING #1 ENGINE DRAG FITTING HOLE #7 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE COROSION INDICATIONS REPAIR ON HOLE #7, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

ENGINE #1 PYLON HOLE #9 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS- LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #9, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

ENGINE #1 PYLON HOLE #13 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #13, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

ENGINE #1 PYLON HOLE #17 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #17, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

LH WING #1 ENGINE DRAG FITTING HOLE #12 HAS REJECTABLE INDICATIONS DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT.1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #12, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

LH WING #1 ENGINE DRAG FITTING HOLE #11 HAS REJECTABLE INDICATIONS DUE TO CORROSION ACCOMPLISHED E.A. F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #11, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

ENGINE #1 PYLON HOLE #3 HAS A REJECTABLE INDICATION DUE TO CORROSION. ACCOMPLISHED EA F-5730-T0370424 PT1, WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, REJECTABLE CORROSION INDICATIONS REPAIR ON HOLE #3, MAJOR REPAIR

Part: DRAG FITTING — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 34,871 hrs · 24,523 cycles

ENGINE 2 PYLON HOLE #8 HAS REJECTABLE INDICATION DUE TO CORROSION IN SKIN AND DRAG FITTING. ACCOMPLISHED EA F-5730-T0370299 PT1 WINGS - PLATES AND SKINS - RH WING, UPPER SKIN AT DRAG FITTING, CRACKS / CORROSION REWORK. MAJOR REPAIR

Part: NONE — NONE (N/A) · airframe 34,595 hrs · 24,310 cycles

MDIS 953 52-10 7823 06APR22 BWI OPEN U AFTER RAMP LOADED AIRCRAFT, FOUND L1 DOOR GUST LOCK BROKEN. REMOVED BROKEN GUST LOCK FRAGMENTS TO ALLOW DOOR TO BE OPENED AND CLOSED WITH NO HOLD OPEN LOCKING ACTION. FACT 08APR22 14:51 DTW INSTALLED NEW COLLAR ON L1 DOOR PER MM 52-11-08-8-0.. OPS CHECKS GOOD... PER GMM P/N 10-N0244-7 INSTALLED NO S/N... TRACK LEVEL #0

Part: HOSE — FAILED (N/A) · airframe 34,479 hrs · 24,215 cycles

PDIS 953 29-02 7695 26JAN22 BHM FACT U UPON LOWERING LANDING GEAR FOR LANDING, LEFT HYDRAULIC QUANTITY WENT TO .14 AND THE PRESSURE TO 0 PSI. PART 26JAN22 04:44 MC1 U IDENTIFIED PARTS MLG DOWNLOCK ACTUATOR MPN: 271N6119-1 CPN: 2912370 QTY: 1 FACT 26JAN22 07:09 BHM U REPLACED MAIN GEAR UNLOCK ACT. LARGER OF THE TWO HYD. LINES WITH A TEMP FLEX LINE. MM REF. 20-10-10-8 FACT 26JAN22 07:09 BHM REPLACED MAIN GEAR UNLOCK ACT. LARGER OF THE TWO HYD. LINES WITH A TEMP FLEX LINE. MM REF. 20-10-10-8.

Part: LOCK — SHEARED (L1 GIRT BAR) · airframe 34,181 hrs · 24,004 cycles

AT A/C BLOCK-IN, WHEN L1 DOOR WAS OPENED FOUND L1 DOOR, PROXIMITY ACTUATOR FOR S10214, DETATCHED FROM GIRT BAR SLIDER (RIVETS SHEARED). COMPLIED WITH PART 2 OF E.A. F-2560-T0364440. REMOVED AND REPLACED L1 DOOR GIRT BAR SLIDER ASSEMBLY PER 757 AMM 25-66-10-2.

Part: ENGINE — FAILED (NR 2) · airframe 34,127 hrs · 23,964 cycles

CLIMBING THROUGH 1000 AGL, VIOLENT SEIZURES FROM RIGHT ENGINE AND EGT REACHED 916. COMPLIED WITH QRC AND QRH. NO EMERGENCY DECLARED. INSTALLED A SERVICABLE #2 ENGINE IAW W/C 7180260-02-02. PERFORMED IDG DISCONNECT, OPS CHECKED PER W/C 2400400-02-01, AND COMPLETED ENG RUN-UP.

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 33,351 hrs · 23,368 cycles

MAIN DECK BS 1661 BL 0 FLOORBEAM TEE FITTING CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G. EVALUATED DAMAGED AREA ORIG. MAT.=.125", REM. MAT.= .106", MAT. LOSS= .019" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A, FIG 101, DETAIL VI. FABRICATED AND INSTALLED A REPAIR ANGLE AND FILLERS IAW SRM 53-00-51-2R, FIG 201. DETAIL I, REPAIR 11.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 33,351 hrs · 23,368 cycles

CORROSION ON FLOOR BEAM @ MAIN CABIN FWD WET AREA BS 365.25 BETWEEN RBL 24 AND RBL 57. REMOVED CORROSION ON FLOOR BEAM AT MAIN CABIN FWD WET AREA STA 365.25 BETWEEN RBL 24 TO RBL 57 IAW B757 SRM 51-10-02-0G. EVALUATED DAMAGED AREA AT STA 365 , RBL 41 TO RBL 44 , ORIG MAT: .125" , REM MAT: .092", MAT LOOS: .033" FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DETAIL VI. FABRICATED AND INSTALLED REPAIR ANGLE IAW B757 SRM 53-00-51-2R , FIG 201, DETAIL III, REPAIR 11. FLOORBEAM AREAS AT STA 365.25 REBL 24 TO RBL 41 AND RBL 44 TO RBL 57 FOUND WITHIN LIMITS IAW B757 SRM 53-00-51-1A FIG 101, DET VI.

Part: WEB — CORRODED (BS 1681-1720) · airframe 33,351 hrs · 23,368 cycles

MAIN DECK BETWEEN BS 1681 - 1720 BL 0 - RBL 58.22 WEB CORRODED.

Part: DECK PLATE — CORRODED (BS 1681-1720) · corrosion level 2 · airframe 33,351 hrs · 23,368 cycles

MAIN DECK BETWEEN STA 1681 - 1720 BL 0 - LBL 58.22 WEB CORRODED FABRICATED AND INSTALLED 1EA REPAIR DOUBLER ON AFT MAIN DECK PLATE AT STA 1681 LBL 24.75 IAW B757 SRM 53-60-51-2R FIG 201 REPAIR 2 ALTERNATIVE I. REMOVED CORROSION ON DECK PLATE AT STA 1681-1720 , BL0 - LBL58.22 IAW B757 SRM 51-10-02-0G. EVALUATED DAMAGED AREA AT STA 1681 LBL 24.75 ORIG. MAT. = .071", REM. MAT. =.049", MAT. LOSS= .022" FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DETAIL III, ALL OTHER AREA AT STA 1681-1720 BL0 - LBL 58.22 FOUND TO BE WITHIN LIMITS IAW B757 SRM 53-00-51-1A FIG 101 DETAIL III.

Part: WEB — CORRODED (BS 1681-1720) · airframe 33,351 hrs · 23,368 cycles

MAIN DECK BETWEEN STA 1681 - 1720 BLO - LBL 58.22 WEB CORRODED

Part: DECK PLATE — CORRODED (BS 1681-1720) · corrosion level 2 · airframe 33,351 hrs · 23,368 cycles

MAIN DECK BETWEEN STA 1681 - 1720 BL 0 - RBL 58.22 WEB CORRODED FABRICATED AND INSTALLED 1EA REPAIR DOUBLER ON AFT MAIN DECK PLATE AT STA 1681, RBL 24.75 IAW B757 SRM 53-60-51-2R FIG 201 DETAIL I REPAIR 2 ALTERNATIVE I. REMOVED CORROSION ON DECK PLATE AT STA 1681-1720, BLO-RBL 58.22 IAW B757 SRM 51-10-02-0G. EVALUATED DAMAGED AREA AT STA 1681 RBL 24.75 ORIG MAT. = .071", REM. MAT. = .048", MAT. LOSS = .023" FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A, FIG 101 DET III. ALL OTHER AREAS AT ST. 1681-1720, BL0-RBL588 FOUND TO BE WITHIN LIMITS IAW B757 SRM 53-00 00-51-1A FIG 101 DETAIL II

Part: CARGO TRACK — GOUGED (BS 570-609) · airframe 32,524 hrs · 22,825 cycles

MAIN CARGO TRACK GOUGED. PERFORMED A REPAIR TO THE CARGO TRACK IAW EA-T F-5321-348453 B P4.

Part: CARGO TRACK — GOUGED (BS 440-680) · airframe 32,524 hrs · 22,825 cycles

MAIN CARGO TRACK BETWEEN BS 440-680 WAS FOUND GOUGED. REPLACED THE CARGO TRACK IAW EA - T F-5321-T0348233 A P4.

Part: CARGO TRACK — GOUGED (BS 440-680) · airframe 32,524 hrs · 22,825 cycles

MAIN CARGO TRACK AT BS 440-680 FOUND GOUGED. REPAIRED IAW EA-T F-5321-T0348233, A P4.

Part: FLOORBEAM — CRACKED (BS 580) · airframe 32,524 hrs · 22,825 cycles

FLOORBEAM AT BS 580, LBL 45.5 WAS CRACKED. COMPLIED WITH EA F-5310-T0348746 P1.

Part: MECHANISM — OBSTRUCTED (GIRT BAR) · airframe 31,881 hrs · 22,359 cycles

RIGHT CREW ENTRANCE DOOR DIFFICULT TO CLOSE AND ARM SLIDE. INSPECTED AREA OF DOOR MECHANISM AND FOUND DEBRIS IN THE TRACK OF THE FWD GIRT BAR LOCKING ATTACHMENT AREA. REMOVED AND CLEANED THE DEBRIS AND LUBRICATED. OPERATIONAL CHECKS NORMAL AND SLIDE ARMING NORMAL THRU SEVERAL CYCLES. REF AMM 52-11-25-5 NR 1 PASSENGER DOOR GIRT BAR MECHANISM - ADJUSTMENT/TEST.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,727 hrs · 22,248 cycles

LT MAIN CABIN STA 377 FLOORBEAM UPPER CHORD HAS AREAS OF CORROSION ON FORWARD FLANGE UPPER AND LOWER SURFACES (EXFOLIATED LOWER AT NUTPLATES). COMPLIED WITH EA NR F-5310-T0341012 P1, FUSELAGE- MAINFRAME CORROSION ON STA 377.7 FLOORBEAM LBL 24.75 - LBL 58.22.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,727 hrs · 22,248 cycles

MAIN DECK LT FLOORBEAMS, LBL 7 SEAT TRACK HAS CORROSION FROM STA 345 TO STA 377. REMOVED CORROSION IAW SRM 53-00-52, 100% MATERIAL LOSS OUT OF ALLOWABLE LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-08-0G, 51-40-02-0G, 53-10-52-01 FIG 1 AND VA DWG 3470 REV G.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,727 hrs · 22,248 cycles

MAIN DECK RT FLOORBEAM, RBL 14 SEAT TRACK STA 345 TO 9 G BULKHEAD HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G, MEASURED 100% MATERIAL LOSS, OUT OF ALLOWABLE LIMITS IAW SRM 53-00-52-1A. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-08-0G, 51-40-02-0G & VA DWG 3470 REV G.

Part: CONTROL ROD — BENT (R1 DOOR) · airframe 30,607 hrs · 21,508 cycles

R1 DOOR SHOWS ARMED WHEN UNARMED. FOUND CONTROL ROD FOR THE SLIDE ARMING RETRACTABLE DOOR MECHANISM, BENT. REMOVED AND REPLACED THE CONTROL ROD. ADJUSTED THE CONTROL ROD AND PERFORMED A TEST OF THE SLIDE ARMING SYSTEM. COULD FIND NO OTHER DEFECTS. OK TO CONTINUE IAW AMM 52-11-20-5.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,550 hrs · 21,452 cycles

DURING PRE FLIGHT CHECK, FOUND RT EMERGENCY EXIT LIGHT AND SLIDE LIGHT INOPERATIVE. WILL NOT TEST. REMOVED AND REPLACED NR 2 EMERGENCY POWER SUPPLY BATTERY PACK. EMERGENCY LIGHTS TEST GOOD IAW AMM 33-51-07-2. ACFT OK FOR SERVICE.

Part: LIGHT — INTERMITTENT (EVAC SLIDE) · airframe 30,548 hrs · 21,450 cycles

JUMPSEATER REPORTED L1 SLIDE LIGHT FLICKERING DURING APPROACH AND LANDING. REMOVED AND REPLACED L-1 SLIDE LIGHT ASSY IAW WD 25-66-01. OPS CHECKS NORMAL IAW AMM 33-51-06-2-1.

Part: DOOR — OUT OF SEQUENCE (L1) · airframe 30,143 hrs · 21,149 cycles

LEFT FWD ENTRY DOOR SLIDE WOULD NOT ARM AFTER CLOSING. NO LIGHT ILLUMINATED WHEN POSITIONING HANDLE TO ARM. FOUND L1 DOOR OUT OF SEQUENCE, HAD TO REMOVE GIRT BAR AND SEQUENCE DOOR PROPERLY, AFTER DOOR WAS IN PROPER SEQUENCE REINSTALLED GIRT BAR AND PERFORMED OPERATIONAL CHECK, ALL WORK ACCOMPLISHED IAW AMM 25-66-10-2,52-11-00-5 AND 25-66-01-4, ACFT OK FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 294 hrs · 20,670 cycles

AT FL 370 THERE WAS A LOUD BANG FOLLOWED BY THE L1 WINDSHIELD SHATTERED. NO LOSS OF PRESSURIZATION. DUE TO L1 WINDOW SHATTERED, R&R WINDOW TEMP CONTROLLER PRECAUTIONARY REF MM 30-41-01-4. GROUND OPS CK GOOD AT THIS TIME. A/C OK FOR SERVICE. REMOVED AND REPLACED L1 WINDOW AS REQ REF MM 56-11-01-4. ALL CKS GOOD AT THIS TIME. A/C OK FOR SERVICE.

Part: ENGINE — FAILED (RIGHT) · airframe 28,324 hrs · 19,888 cycles

AT FL 390, ACFT SHUDDERED WITH A ASSOCIATED POP. EGT WENT INTO RED, FOR RT ENGINE. IMMEDIATELY BROUGHT RT THROTTLE TO IDLE. EGT WAS IN THE RED APPROX 15 SECONDS AFTER THROTTLE WAS AT IDLE, MOTOR RAN NORMALLY AT IDLE. CAPTAIN STATED THAT HE OBSERVED THE RT ENGINE EGT IN EXCESS OF 935 & THAT IT WAS APPROX AT THAT TEMPERTURE FOR 10 TO 15 SECONDS. REMOVED RIGHT ENGINE PER W/C 71T0002-RR AND INSTALLED SERVICEABLE ENGINE PER W/C 71T0902-RR. ALL REQ'D ENGINE RUNS COMPLETE. ACFT OK FOR SERVICE.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 27,977 hrs · 19,625 cycles

L1 DOOR SLIDE WILL NOT DISARM. GIRT BAR REMAINS ENGAGED IN FWD FLOOR LOCK. SLIDE STOWED. FOUND GIRT LOOSE FROM DOOR. ATTACHED IAW MM 25-66-10-2. OPS CHECKED NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 27,913 hrs · 19,582 cycles

DURING PREFLIGHT, R-1 DOOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — DIRTY (PAX DOOR SLIDE) · airframe 27,701 hrs · 19,431 cycles

WHEN CLOSING LT ENTRY DOOR AND ARMING FOR FLIGHT, SLIDE "ARMED" LIGHT DID NOT ILLUMINATE. TRIED A SECOND TIME AND IT ILLUMINATED. CLEANED BOTH GIRT BAR PROXIMITY SWITCHES ON L1 DOOR . ARMED L-1 DOOR SLIDE MULTIPLE TIMES WITH NORMAL INDICATION , IAW MM 25-66-00-0.

Part: LAMP — UNSECURE (L1 DOOR SLIDE) · airframe 27,488 hrs · 19,275 cycles

L1 DOOR SLIDE LIGHT DOESNT ILLUMINATE WHEN ARMED INTIL TAPPING LIGHT. SECURED LAMP IAW SMP. OPERATED ARM SYS NUMEROUS TIMES. OPS CHECKED GOOD. AC OK FOR CONTINUED SERVICE.

Part: TRANSDUCER — FAILED (RT ENGINE) · airframe 27,086 hrs · 19,016 cycles

RT ENGINE SHUTDOWN AS A PRECAUTION FOR HIGH ENGINE VIBRATION (4.0) AMBER. RT ANTI-ICE VALVE FAILED TO OPEN IN ICING AND VIBRATION STARTED RT AFTER. SUSPECT COMPRESSOR BLADES WERE ICED. TROUBLE SHOT IAW FIM 71-05, PERFORMED AVM BITE IAW FIM 77-31 HAD A B8 FAULT ON RT ENGINE CLEARED FAULT AND DID NOT RETURN. REPLACED NR 2 ENG AVM ACCELEROMETER IAW AMM 77-31-01-4. NO FURTHER FAULTS ON RT AVM. R & R RT ENG AVM REF AMM 77-31-03-4. RAN ENG AND PERFORMED ENG VIBE SURVEY IAW AMM 71-00-00-5-3 ALL READINGS WITHIN LIMITS N1 WAS 1.5 UNITS AT 1.5 EPR- N2 WAS 1.1 UNITS AT 1.5 EPR- N3 WAS .9 UNITS AT 1.5 EPR AND BB WAS 1.9 UNITS AT 1.5 EPR. SEE WRI 30-20/0535 FOR A/I INFO ALL WORK IAW AMM 71-00-00-5, 77-31-01-4 FIMS 77-31, 71-05 AND AMM 71-00-00-6. ACFT OK FOR SRVICE. RT ENG ANTI-ICE VALVE REPLACED IAW AMM 30-21-03-4.

Part: SKIN — DENTED (ZONE 100) · airframe 26,955 hrs · 18,928 cycles

EXTERIOR SKIN DENTED AT BS 324 STR 24. REPAIR CARRIED OUT AS PER E.A F-5310-155921. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — DAMAGED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

LEFT CREASE BEAM AT BS 1584 HAS DAMAGED. CREASE BEAM REPAIRED IAW EA F-5310-161089, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (BS 560 S25R) · corrosion level 2 · airframe 26,955 hrs · 18,928 cycles

FWD CARGO DOOR ASSY INNER CHORD AT FRAME BS 560 BELOW S25R AROUND FASTENER HOLE WITH CORROSION. REPAIR CARRIED OUT ON FWD CARGO DOOR IAW EA F-5230-161088, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,955 hrs · 18,928 cycles

AFT LOWER CARGO COMPARTMENT DOOR CUTOUT EXT SKIN BETWEEN STA 1380 TO STA 1400 AND STR 26R TO STR 27R WITH CORROSION AROUND FASTENER HOLES. REPAIRED IAW EA F-5310-155912, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: PAN — DAMAGED (ZONE 800) · airframe 26,955 hrs · 18,928 cycles

CABIN, DOOR 1R EXTERIOR HANDLE RECESS HAS SCRATCHES ON LOWER EDGE. R & R IAW SRM 51-40-02, REV 106 AND DWG 141N6100, SHT 14 REV F. REPAIR IS CLASSIFIED AS MAJOR.

Part: DECK PLATE — CORRODED (BS 1716) · airframe 26,955 hrs · 18,928 cycles

CABIN DECK PLATE AT STA 1716, LBL 45 HAS CORROSION. EPAIRED AS PER E.A. F-5310-155913. REPAIR IS CLASSIFIED AS MINOR.

Part: FRAME — DENTED (ZONE 100) · airframe 26,955 hrs · 18,928 cycles

AFT CARGO FRAME AT BS 1340, STR 26L WITH A DENT ON INNER FLANGE. FRAME REPAIRED IAW EA F-5310-155906, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,955 hrs · 18,928 cycles

AFT CARGO DOOR CUT OUT LOWER SILL CHORD FOUND CORRODED AT RIVETS AREA BS 1400 - 1420. AFTER THRESHOLD SCUFF PLATE REMOVAL. R & R IAW DWG 146N8522, SHT 8, REV- AND EA F-5310-161090, PART 1, REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — CHAFED (BS 1280 S11R) · airframe 26,955 hrs · 18,928 cycles

CABIN, STA 1280, STR 11R HAS CHAFING ON FRAME. REPAIRED IAW SRM 53-00-07 REV. 106, REPAIR 3, FIG. 201. REPAIR IS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

AFTER SEAT TRACK REMOVAL INSIDE MAIN CABIN BETWEEN STA 1076 AND STA 1180 AT LBL24 FASTENER HOLES OBSERVED WITH COUNTERSUNK KNIFE EDGE. R & R WITH SEAT TRACK FABRICATED IAW DWG 144N5021 SHT 1, REV A AND INSTALLED IAW DWG 144N5001 SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (BS 680) · corrosion level 2 · airframe 26,955 hrs · 18,928 cycles

BS 680, CREASE BEAM HAS CORROSION, RBL 64. R & R IAW SRM 51-40-02, REV 106 AND DWG 143N8322 SHT 3, REV-. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

AFTER SEAT TRACK REMOVAL INSIDE MAIN CABIN BETWEEN STA 1076 AND STA 1180 AT RBL45. FASTENER HOLES OBSERVED WITH COUNTERSUNK KNIFE EDGE. R & R WITH SEAT TRACK FABRICATED IAW DWG 144N5021 SHT.1, REV. A AND INSTALLED IAW DWG 144N5001 SHT 3, REV A . REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

AFTER SEAT TRACK REMOVAL, INSIDE MAIN CABIN BETWEEN STA 1076 AND STA 1180 AT LBL 45. FASTENER HOLES OBSERVED WITH COUNTERSUNK KNIFE EDGE. REMOVED AND REPLACED WITH SEAT TRACK FABRICATED IAW DWG 144N5021, SHT 1, REV A AND INSTALLED IAW DWG 144N5001, SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.

Part: ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 26,955 hrs · 18,928 cycles

RT SIDE EMPENNAGE, THE APU INLET CUTOUT AREA - THE LOWER SIDE OF THE CUTOUT, AFTER INLET REMOVAL FOUND TO HAVE COROSION AT BS 1787-1825 AT STRINGER 3. CORRODED ANGLE ON LOWER SIDE OF APU RT INLET CUTOUT AREA AT BS 1787-1825, STR 3R, REMOVED. ANGLE FABRICATED IAW DWG 148N3152, SHT.1 REV.- AND INSTALLED IAW DWG 148N3105, SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 26,955 hrs · 18,928 cycles

RT SIDE EMPENNAGE - APU INLET CUTOUT AREA, THE LOWER SIDE OF THE CUTOUT, AFTER INLET. REMOVAL FOUND TO HAVE CORROSION AT BS 1825 BETWEEN STRINGER 3-6. R & R INNER STRAP AT BS 1825 ON APU RT INLET CUTOUT LOWER SIDE WITH STRAP FABRICATED IAW DWG 148N3138 SHT 1 REV C AND INSTALLED IAW DWG 148N3105 SHT 1, REV C. REPAIR IS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

AFTER SEAT TRACK REMOVAL INSIDE MAIN CABIN BETWEEN STA 1076 AND STA 1180 AT RBL 24. FASTENER HOLES OBSERVED WITH COUNTERSUNK KNIFE EDGE. R & R SEAT TRACK FABRICATED IAW DWG 144N5021, SHT 1, REV A AND INSTALLED IAW DWG 144N5001, SHT 3, REV A. REPAIR IS CLASSIFIED AS MAJOR.

Part: SILL — CORRODED (ZONE 100) · airframe 26,955 hrs · 18,928 cycles

FWD CARGO COMPT DOOR CUT OUT LOWER SILL LOWER CHORD BETWEEN BS 580 AND BS 600. HAS CORROSION AFTER REMOVAL OF THRESHOLD PANEL. REPAIRED IAW EA F-5310-158077. REPAIR IS CLASSIFIED AS MINOR.

Part: STRAP — CORRODED (BS 1825) · corrosion level 2 · airframe 26,955 hrs · 18,928 cycles

FUSELAGE INTERIOR RT SIDE. AFTER REMOVAL OF THE OUTER SPLICE STRAP FOUND THE INNER SPLICE STRAP AT BS 1825 FROM STR 1 TO STR 6 HAS CORROSION. R & R SPLICE STRAP WITH STRAP FABRICATED IAW DWG 148N3138 SHT 1, REV C AND INSTALLED IAW DWG 148N3105, SHT 1, REV C. REPAIR IS MAJOR.

Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 26,955 hrs · 18,928 cycles

RT SIDE APU INLET DOOR CUTOUT AREA, THE FORWARD SIDE OF THE CUTOUT AT BS 1787 STR 4-7 HAS CORROSION. R & R IAW DWG 148N3105, SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJOR.

Part: ANGLE — CORRODED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

RT SIDE LOWER ATTACH ANGLE FOR THE APU INLET HOUSING IS CORRODED, BS 1787-1825 AT STRINGER 7. CORRODED ATTACH ANGLE R & R WITH ANGLE FABRICATED IAW DWG 148N3152 SHT 1, REV AND INSTALLED IAW DWG 148N3105 SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,955 hrs · 18,928 cycles

AFT LOWER CARGO COMPARTMENT FRAME BS 1340 BETWEEN STR 26L TO STR 27L CORRODED ON INNER FLANGE. FRAME REPAIRED IAW EA F-5310-155906 PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: FRAME — GOUGED (ZONE 100) · airframe 26,955 hrs · 18,928 cycles

AFT LOWER CARGO COMPARTMENT FRAME AT BS 1340 BETWEEN STR 25L TO STR 27L GOUGED. DAMAGED FRAME REPAIRED IAW EA F-5310-155906, PART 1. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

SEAT TRACK AT BS 873, RBL 45 HAS SEAT FITTING DAMAGE TO CROWN. R & R SEAT TRACK FABRICATED IAW DWG 143N5106, SHT 1, REV A AND INSTALLED IAW DWG 143N5080, SHT 5, REV A. REPAIR IS CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

SEAT TRACK AT BS 873 LBL 45 HAS SEAT FITTING DAMAGE TO CROWN. R & R SEAT TRACK, FABRICATED IAW DWG 143N5106 SHT 1, REV A AND INSTALLED IAW DWG 143N5080 SHT 5, REV A. REPAIR IS CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CRACKED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

CREASE BEAM INNER CHORD AT BS 1141 LBL 64, CRACKED. R & R INNER CHORD FABRICATED IAW DWG 144N5200 SHT 3, REV A AND INSTALLED IAW DWG 144N5200, SHT 3, REV A AND SHT 4, REV A. REPAIR IS CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 26,955 hrs · 18,928 cycles

BS 720, RBL 52 FLOORBEAM HAS CORROSION ON UPPER TEE. R & R IAW DWG 143N5504, SHT 2, REV B AND INSTALLED IAW DWG 143N5015, SHT 9 REV B. REPAIR IS CLASSIFIED AS MAJOR.