N961FD

Part: GUST LOCK — DAMAGED (L1 DOOR) · airframe 59,366 hrs · 29,406 cycles

MDIS 961 52-10 9274 13OCT23 MEM FACT U L1 DOOR GUST LOCK BROKEN. MEL 13OCT23 06:26 MEM U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 16OCT23 "MEL 52-11-01-A: L1 DOOR - INOP." REMOVED BROKEN GUST LOCK PARTS TO ALLOW L1 DOOR TO BE OPENED / CLOSED AND PLACED ON MEL REF B757 MM 52-11-08-6 INSTRUCTIONS. C/7375730 AMM: 52-11-08-8 INSTALLED L1 DOOR HOLD OPEN LOCK SPLIT COLLAR AND CATCH (KIT PN 654N0244-7, N/S/N) REF B757 AMM 52-11-08-8 CHECKED GOOD OK FOR SERVICE

Part: RELAY — FAILED (TE FLAPS) · airframe 58,855 hrs · 29,047 cycles

ON APPROACH, TE LIGHT WITH TE FLAP DISAGREE MESSAGE, WHEN FLAPS SET TO 25. CONFIRMED FLAP HANDLE IN DETENT. COMPLIED WITH QRH FOR SUBSEQUENT APPROACH & LANDING. TROUBLESHOT IAW AMM 27-51 TREE 805, FSEU NR 1 SHOWED FLAP FAIL 217. DURING TEST OF FSEU 1, HAD FAULT FLAP LD RELF, LOWERED FLAPS TO 30 IAW TECH TIP 18-0042, CHKD INBD FLAP INBD LT & RT XMSN FLUID LEVELS GOOD & LOAD LIMITERS NOT TRIPPED, INBD FLAP OTBD XMSN FLUID LEVELS GOOD. TECH TIP 18-0042 & NO DEFECTS. PERFORMED AMM 27-51 FAULT 810, NO FAULTS. R & R RELAY K10245, FLAP LOAD RELIEF RELAY IAW WDM 27-51-51 PAGE 2 SHEET 1. TESTS PASSED IAW AMM 27-51-28-2 & AMM 27-51-00-5. PERFORMED FESU BITE, NO FAULTS IAW AMM 27-51 FAULT 805 . OK FOR SERVICE.

Part: FSEU — FAILED (TE FLAP SYSTEM) · airframe 58,643 hrs · 28,915 cycles

MOVING FLAP LEVER FROM 20 TO 25 A TRAILING EDGE FLAP DISAGREE EICAS MESSAGE DISPLAYED. QRH COMPLIED WITH AND EMERGENCY DECLARED. EMERGENCY DECLARED. REMOVED AND REPLACED #1 FSEU IAW AMM 27-51-01-2. OPS CHECK GOOD. NO DEFECTS NOTED. A/C OK FOR SERVICE. ORIG SUB DATE: 9/22/2022

Part: GUST LOCK — DAMAGED (L1 DOOR) · airframe 58,399 hrs · 28,754 cycles

MDIS 961 52-10 8137 08JUN22 MEM OPEN U L1 DOOR GUST LOCK BROKEN MEL 08JUN22 05:17 MEM U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 11JUN22 "MEL 52-11-01-A: L1 DOOR INOP." C/7319881 PART 08JUN22 05:25 MC1 U IDENTIFIED PARTS L1 DOOR COLLAR ASSY MPN: 654N0244-7 CPN: 5214377 QTY: 1 FACT 09JUN22 22:39 MEM REMOVED AND REPLACED L1 DOOR HOLD OPEN LOCK. OPS CHECK NORMAL. REF 757 AMM 52-11-08-8.

Part: ROD — SHEARED (NLG) · airframe 58,341 hrs · 28,713 cycles

DURING TAXI-IN, NOTICED RIGHT NOSE GEAR DOOR, OPEN AND SWINGING. UPON BLOCK-IN, FOUND RIGHT NOSE GEAR ACTUATING ROD, REF IPC 32-22-02-01 FIG 1, ITEM 40, BROKEN OFF. REPLACED NOSE LANDING GEAR RH FWD DOOR OPERATING ROD IAW AMM 32-20-02-4 AND EA F-3220-T0368416 PART 1. PART 2 OF EA WILL COMPLETE RIG AND ADJUSTMENT, REF WRI 32-20/8069. NOTE: DEFECTIVE OPERATING ROD P/N - 141N0936-1, S/N-UNK.

Part: NONE — NONE (N/A) · airframe 58,259 hrs · 28,653 cycles

EMERGENCY/ UNARMED LIGHT INOP RELAMPED THE EMERGENCY "UNARMED" ANNUNCIATION LIGHT OPS CK GOOD PER B 757 AMM 33-51-00-5. AC OK FOR SERVICE.

Part: AUTOPILOT SYS — INOPERATIVE · airframe 57,278 hrs · 27,956 cycles

TEST FLIGHT: ON CLIMB OUT WITH CENTER AUTO PILOT ON, STAB TRIM WENT FULL UP. DISENGAGE AUTO PILOT AND WAS ABLE TO CONTROL TRIM. HAPPENED TWICE MORE ON CLIMBOUT. DURING DESCENT ON RT AUTOPILOT STAB TRIM WENT FULL NOSE DOWN TRIM. HAND FLOWN THE REMAINDER OF FLT. DURING CONFIGURATION WITH GEAR DOWN AND FLAPS 20, TRIM AGAIN WENT UNCOMMANDED NOSE UP TRIM. REMOVED AND REPLACED ELEVATOR FEEL AND CENTERING UNIT. REMOVED AND REPLACED RIGHT ELEVATOR FEEL AND CENTERING UNIT NEUTRAL SHIFT TRANSDUCER. REMOVED AND REPLACED LEFT AND RIGHT STAB TRIM/ELEVATOR ASSEMBLY MODULE.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 57,277 hrs · 27,955 cycles

AFT CARGO INTERCOSTAL HAS CORROSION ON LOWER OUTBOARD SIDE AT RBL-5 STA 1417. REMOVED INTERCOSTAL AT AFT CARGO STA 1417 RBL 5 AND EVALUATED AND FOUND OUT OF LIMITS, IAW B757 SRM 51-40-02-0G AND B757 SRM 53-00-04-1A FIG 101 DET V. REPLACED INTERCOSTAL BY FABRICATION, IAW B757 SRM 51-30-01-0G FIG 2 NOTE G, 51-40-02-0G AND BOEING DWG 146N5399 REV B. AT AFT CARGO BETWEEN STA 1400 TO 1420 RBL 5.

Part: FAILSAFE — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 57,277 hrs · 27,955 cycles

MAIN CABIN LT SIDE JUST ABOVE STR 17 STA 1520 ON FRAME CORRODED. COMPLIED WITH FEDEX EA NR F-5310-T0358418 P1. FUSELAGE-MAINFRAME-STA 1520 FAILSAFE CHORD CORROSION ABOVE S-17L.

Part: CUSP WEB — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 57,277 hrs · 27,955 cycles

MAIN CABIN RT CUSP WEB CORRODED BETWEEN STA 600 TO 620. REMOVED CORROSION AT MAIN CABIN RT CUSP WEB BETWEEN STA. 600 TO 620 AND EVALUATED ORIGINAL MAT .036", MAT LOSS .015", MAT REM .021". FOUND OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG 101 DET VIII. FABRICATED AND INSTALLED NEW CUSP WEB, IAW B757 SRM 51-30-01-0G, 51-40-02-0G AND BOEING DWG 143N5520 REV B.

Part: CUSP WEB — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 57,277 hrs · 27,955 cycles

MAIN CABIN RT CUSP WEB CORRODED BETWEEN STA 580 AND STA 600. REMOVED CORROSION AT MAIN CABIN RT CUSP WEB BETWEEN STA 580 TO STA 600 AND AFTER EVALUATION FOUND CUSP WEB OUT OF LIMITS, IAW B757 SRM 51-10-02, 53-30-13-1A FIG 101 DET VIII. FABRICATED AND INSTALLED NEW CUSP WEB, IAW B757 SRM 51-30-01-0G, 51-40-02-OG AND BOEING DWG NR 143N5520 REV B AND REV BM.

Part: SHIM — CRACKED (FLOORBEAM) · airframe 57,277 hrs · 27,955 cycles

MAIN CARGO FLOOR SUPPORT SHIM DAMAGED AT STA 1058 BETWEEN LBL 24 AND LBL 45. REMOVED SHIM (COVER PLATE) AT MAIN CARGO FLOOR SUPPORT STA 1058 BETWEEN LBL 24 AND LBL 45 AND FOUND CRACK AND OUT OF LIMITS, IAW B757 SRM 51-40-02-0G 53-00-51-1A. FABRICATED AND INSTALLED NEW SHIM (COVER PLAYE) ON FLOOR SUPPORT, IAW B757 SRM 51-40-02-0G AND BOEING DWG NR 144N5070 REV B.

Part: CREASE BEAM — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 57,277 hrs · 27,955 cycles

MAIN CABIN RT SIDE STA 450 TO 665 CREASE BEAM CORRODED. REMOVED CORROSION AT MAIN CABIN RT SIDE CREASE BEAM BETWEEN STA 450 TO 665 AND AFTER EVALUATION FOUND CREASE BEAM OUT OF LIMITS, IAW B757 SRM 53-30-13-1A FIG 101 DET VIII, SRM 51-10-02. REMOVED AND REPLACED BY FABRICATION CREASE BEAM, IAW B757 SRM 51-40-05-0G, 51-40-02-0G AND BOEING DWG NR 144N5520 REV C.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 57,277 hrs · 27,955 cycles

MAIN CABIN SEAT TRACK FLANGE HAS CORROSION AT RBL 45 STA 1540. REMOVED CORROSION AT MAIN CABIN SEAT TRACK FLANGE RBL 45 STA 1540 AND AFTER EVALUATION FOUND SEAT TRACK OUT OF LIMITS, IAW B757 SRM 51-10-02-0G AND B757 SRM 53-00-52-1A FIG 101 DET VII. REMOVED AND REPLACED BY FABRICATION SEAT TRACK FROM STA 1320 TO 1540 RBL 45, IAW B757 SRM 51-40-05-0G, 51-40-08-0G, 51-40-02-0G AND BOEING DWG NR 146N5130 REV.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 57,277 hrs · 27,955 cycles

MAIN CABAIN STA 1540 LBL 45 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION AT MAIN CABIN STA 1540 LBL 45 SEAT TRACK FLANGE AND AFTER EVALUATION FOUND SEAT TRACK FLANGE OUT OF LIMITS, IAW B757 SRM 51-10-02-0G AND B757 SRM 53-00-52-1A FIG 101 DET VII. REMOVED AND REPLACED BY FABRICATION SEAT TRACK FROM STA 1320 TO 1540 LBL 45, IAW B757 SRM 51-40-05-0G, 51-40-08-0G, 51-40-02-0G AND BOEING DWG NR 146N5130 REV.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 57,150 hrs · 27,860 cycles

PDIS 961 71-00 6706 19SEP20 ONT OPEN U LOGPAGES:3339293 AFTER TAKEOFF, AFTER SELECTING VNAV/CLIMB POWER, RIGHT ENGINE EXPERIENCED STRONG COMPRESSOR STALLS WITH LOUD CHUGS, LOSS OF POWER, AND HIGH EGT (905) COMPRESSOR STALL STOPPED WHEN THRUST LEVER WAS RETARDED. ACCOMPLISHED PHASE ONES FOR ENGINE FIRE/ SEVERE DAMAGE AND SHUT DOWN ENGINE. UPON ENGAGING RIGHT AUTOPILOT, RECEIVED STAB TRIM EICAS AND AUTOPILOT DISCONNECTED. RE-ENGAGED AUTOPILOT, AND AUTOPILOT AND STAB TRIM SEEMED NORMAL. HOWEVER STAB TRIM EICAS REAMINED. DIVERTED TO KONT (NEAREST SUITABLE AIRPORT..) PERFORMED BORESCOPE VISUAL INSPECTION IAW AMM 72-00-00-6-2. FOUND NUMEROUS HP BLADES DAMAGED. R&R ENGINE REF WORKCARD 7180260-02- TEST PER AMM 71-00-00-5 ALL ENGINE TEST PASSED.

Part: HANDLE — LACK OF LUBE (TE FLAPS) · airframe 57,041 hrs · 27,773 cycles

TE FLAP DISAGREE ON BASE TURN TO FINAL, WHEN GOING FROM FLAPS 20 TO 25. NO HISTORY PAST 90 DAYS. AFTER DEBREIFING CREW NO 'TE DISAGREE LIGHT' OR EICAS MESSAGE PRESENT. FSEU 1 SHOWED FLA FAIL. RESET FLAP ALTN SWITCH AND ROTARY SWITCH TO NORMAL AND RAN FLAPS WITH NO FAULTS AT ANY DETENT IAW MM 27-51-00-2. INSPECTED FLAPS AND NO OBVIOUS DEFECTS FOUND IAW MM 27-51-00-2. ALL FLAP TRANSMISSION OILS FOUND TO BE GOOD AND NO OVER LOAD INDICATORS TRIPPED IAW MM 12-13-06-3. FOUND FLAP HANDLE HARD TO PULL UP/DOWN IN AND OUT OF DETENTS. LUBED HANDLE IAW FIM 27-51 FAULT TREE 813 AND OP'S CHECKED GOOD. RAN MCDU TEST 40 AND ALL TEST PASSED IAW MM 22-00-02-2. FLAP LEVER DETENT AND FLAP POSITION ANGLE OP'S CHECKED GOOD IAW MM 27-58-01-5, FIGURE 501 TABLE A. NEVER RECEIVED ANY EICAS MESSAGES OR TE DISAGREE LIGHT WHILE MOVING FLAPS THROUGH RANGE. FLAPS OP'S CHECKED GOOD AND WORK PERFORMED IAW MM 27-51-00-2, FIM 27-51, FAULT TREE 805, AND FIM 27-51, FAULT TREE 808. AIRCRAFT OK FOR SERVICE.

Part: COVER — LOOSE (L1 DOOR SLIDE) · airframe 57,012 hrs · 27,753 cycles

SLIDE COVER ON L1 DOOR IS LOOSE. REPLACED DAMAGE POTED INSERTS ON UPPER HINGE COVER PANEL IAW AMM 25-00-00-8. INSTALLED SERVICEABLE SLIDE COVER IAW AMM 25-66-01-4.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 56,791 hrs · 27,609 cycles

FUMES IN COCKPIT ON TAKEOFF ROLL TILL ABOUT 5K FT. REQUIRED CREW TO DON O2 MASK IMMEDIATELY AFTER TAKEOFF. ODOR OF BURNT RUBBER/ENG SMELL MAINLY ON CAPTAINS SIDE. FO DID NOT DETECT ODOR. ODOR CLEARED BEFORE CREW COULD SECURE ANY EQUIPMENT. NO FURTHER OCCURRANCE REST OF FLIGHT. REF B757MM 21-00-01-3 AND JRH,RAN APU, TESTED /RAN ENGINES AT MAX STATIC EPR.COULD NOT DUPLICATE ANY BAD OR SUSPECT ODOR.RAN PACKS NUMEROUS TIMES FROM HOT TO COLD, NO ISSUES.NO FINGINGS IN ALL OTHER INSPECTIONS. A/C GOOD FOR SERVICE.

Part: ACTUATOR — FAILED · airframe 55,827 hrs · 26,953 cycles

PDIS 961 27-80 5336 05DEC18 LEVEL 10000 FT, 220 KIAS AND SLOWING, RECEIVED EICAS " LE SLAT DISAGREE" AND DISCRETE "LEADING EDGE" WHILE EXTENDING FLAPS 1. EMERGENCY DECLARED. COMPLETED INSTALLATION OF BAD ROTARY ACTUATORS IAW MM 27-81-18-4/6. ALL INSPECTION PLATES REINSTALLED AS WELL AS LEAK AND OPS CKS. ALL TESTS NORMAL. REF. WRI 27-80-5339, 27-80-5340, 27-80-5341 AND 27-80-5343 FOR WORK PERFORMED. PARTS INFO REQ. FOR SDR. DR PARTS INFO FOR LEFT SLAT INBOARD ACTUATOR. MPN: 755299D POS: 2I OFF SRL: A1789 ON SRL A1746 MPN: 755299A

Part: ACTUATOR — FAILED (SLAT SYSTEM) · airframe 55,827 hrs · 26,953 cycles

PDIS 961 27-80 5336 05DEC18 LEVEL 10000 FT, 220 KIAS AND SLOWING, RECEIVED EICAS " LE SLAT DISAGREE" AND DISCRETE "LEADING EDGE" WHILE EXTENDING FLAPS 1. EMERGENCY DECLARED. COMPLETED INSTALLATION OF BAD ROTARY ACTUATORS IAW MM 27-81-18-4/6. ALL INSPECTION PLATES REINSTALLED AS WELL AS LEAK AND OPS CKS. ALL TESTS NORMAL. REF. WRI 27-80-5339, 27-80-5340, 27-80-5341 AND 27-80-5343 FOR WORK PERFORMED. PARTS INFO REQ. FOR SDR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,815 hrs · 26,942 cycles

MAIN CABIN STA 1505 STR 1 CRACKED. REMOVED DAMAGED SECTION DIM 12" STA 1500 IAW SRM 53-00-03-2R REPAIR 2 FIG 201 DET 1. REMOVED FWD SECTION ON STR 1 FROM STA 1492 TO EXISTING SPLICED STA 1460 IAW SRM 51-40-02-0G. FABRICATED NEW REPAIR STRINGER SECTION AND SPLICE IAW SRM 51-30-01-0G AND SRM 53-00-03-2R FIG 201, REPAIR 2. FABRICATED SHIMS IAW SRM 51-30-01-0G FIG 101, INSTALLED REPAIR SECTION AND SPLICE IAW SRM 53-00-03-2R REPAIR 22R FIG 201.

Part: BOTTLE — DISCHARGED (PAX DOOR) · airframe 55,058 hrs · 26,419 cycles

NR 1 PASSENGER DOOR ASSIST BOTTLE DISCHARGED, REQUIRES SERVICING. REMOVED AND REPLACED CYLINDER EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4.

Part: FSEU — MALFUNCTIONED (TE FLAPS) · airframe 54,876 hrs · 26,316 cycles

TRAILING EDGE FLAP DISAGREE LIGHT. LOCKED AT 20 DEGREES. COMPLIED WITH QRH. PERFORMED FSEU BITE PROCEDURE IAW FIM 27-51-00, FIG 104, FOUND NO CURENT FAULTS FOR NR 1 FSEU FOUND FLA FAILDED ON SEVERAL TRIES COULD NOT GET A GOOD BITE ON NR 2 FSEU. REMOVED AND REPLACED THE 2 FSEU IAW AMM 27-51-01-2. OPS CHECKED GOOD. PERFORMED FIM 27-51 FIG 810 WITH NO DEFECTS NOTED. LOAD RELIEF WORKS NORMAL AND NO BITE ON ADC 1 OR 2. OPERATED FLAPS THROUGH AMNY CYCLES WITH NO DEFECTS NOTED. ACFT OK FOR CONTINUED SERVICE.

Part: SEAT TRACK — DAMAGED (BS 580-600) · airframe 54,764 hrs · 26,246 cycles

LOCK ON CENTERLINE BETWEEN STRINGERS 3L-R FOUND DAMAGED AT SEAT TRACK. REMOVED LOCK AND PLACED IN COURRIER COMPT. LOCK ID D611 MEL 29JUN17 18:59 SEAT TRACK LOBE DAMAGED. WILL REQUIRE SHEET METAL FOR REPAIR. FOUND TRACK TO BE DAMAGED, APPROX 72 HOUR FOR REPAIR. TECH TOOK PICTURES OF DAMAGED AREA TO TRY TO FACILITATE REPAIR. IT APPEARS THAT THE SEAT TRACK GOES UNDERNEATH THE SOLID BULKHEAD. DAMAGE IS LOCATED ON BL 0 AT BS 620. SEAT TRACK IS ONE PIECE FROM BS 440 TO 879. REPAIRED TRACK WITH EA F-2550-T0334526 REV A.

Part: FUEL SYS — LEAKING (LT WING) · airframe 54,452 hrs · 26,064 cycles

LEFT WING INBOARD DRY BAY CENTER FORWARD DRAIN HAS A RUNNING FUEL LEAK.

Part: TRANSMITTER — MALFUNCTIONED (SLAT SYS) · airframe 54,449 hrs · 26,062 cycles

AFTER TAKEOFF RECEIVED A LE SLAT DISAGREE EICAS. PERFORMED QRH. COMPLIED WITH LANDING PROCEDURES. REMOVED AND REPLACED LEADING EDGE PDU TRANSMITTER.

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYSTEM) · airframe 54,447 hrs · 26,061 cycles

LE SLAT DISAGREE EICAS MESSAGE AS FLAP EXTENDED TO FLAPS 1, WENT THROUGH QRH PROCEDURE WHICH LEAD TO A LE SLAT ASSYMETRY ISSUE. PERFORMED QRH PROCEDURE FOR LE SLAT ASSYMETRY. NO NOTED ADVERSE ROLL OR YAW. NO AIRCRAFT LIMITS EXCEEDED. NO STATUS MESSAGES NOTED ON SHUT DOWN. CHECKED FSEU AND NO FAULTS WERE FOUND ON 3 FSEU BOXES. RETURNED ALTN FLAP SWITCH TO NORMAL POSITION. CYCLED SLATS /FLAPS THRU SEVERAL CYCLES WITH NO DEFECTS NOTED. OPERATED SLATS/FLAPS IN ALTN AND ALSO NO DEFECTS NOTED. COMPLIED WITH TROUBLESHOOTING IAW FAULT TREE 27-81-803. NO HISTORY NOTED.

Part: CONNECTOR — UNSECURE (RAT) · airframe 54,416 hrs · 26,035 cycles

DURING CRUISE FLIGHT AT FL390, A RAT UNLOCKED EICAS MESSAGE AND RAT UNLOCKED LIGHT IN RAT SWITCH ILLUMINATED. FIVE MINUTES LATER BOTH WARNINGS WERE NO LONGER DISPLAYED. NO RAT UNLOCKED MESSAGE AT BLOCK IN. DEPLOYED RAT IAW AMM 29-21-00-2 AND RECEIVED A RAT UNLOCKED MESSAGE.USING FRM FAULT CODE 29-21-14-00 AND AMM 29-21-17, INSPECTED STOWED LIMIT SWITCH. NO DEFECTS NOTED WITH SWITCH S10258. FOUND ASSOCIATED CONNECTOR UNSECURE. REMOVED, CLEANED, AND SECURED THE CONNECTOR IAW SWPM 20-60-00. STOWED THE RAT IAW AMM 29-21-00-2 AND RAT UNLOCKED INDICATION RETURNED TO NORMAL.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 54,153 hrs · 25,866 cycles

R2 DOOR UPPER HINGE CUTOUT IS CRACKED. LOCATED AND INSTALLED REPAIR DOUBLER PN 143N6158-12 AT R2 DOOR UPPER HINGE CUT OUT IAW SRM 52-10-02-2R. COMPLIED WITH EA F-5210-T0329362 P1. MAJOR REPAIR.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 54,153 hrs · 25,866 cycles

RIGHT WING OB FLAP TOP SECTON INBD SIDE REPAIR DISBONED. REPAIRED IAW SRM 57-53-01-2R FIG 201, SRM 51-70-10 REPAIR 4, AND SRM 51-70-10-2R PARA 20, FIG 208.

Part: DOOR — DELAMINATED (LT MLG) · airframe 531 hrs · 25,125 cycles

LEFT MLG DOOR DELAMINATED. MISSING SECTION CRAZ COMPLY WITH EA F-5280-T0319221 REV NR POS P3. R & R MLG DOOR IAW MM 32-12-01-4 & EA F-5280-T0319221.

Part: BRACKET — LOOSE (L1 DOOR SLIDE) · airframe 531 hrs · 25,102 cycles

L1 DOOR SLIDE COVER LOOSE. TIGHTENED SLIDE COVER ATTACH BRACKETS, AND INSTALLED SLIDE COVER FOR L1 DOOR IAW AMM 52-11-02-4.

Part: BRAKE — LACK OF LUBE (TE FLAP) · airframe 529 hrs · 25,026 cycles

RECEIVED TE FLAP DISAGREE EICAS MSG ON APPROACH WHEN MOVING FLAPS FROM 20' TO 25'. RETRACTED FLAP HANDLE TO 20' IAW GO AROUND PROCEDURES, RAN QRH & LANDED FLAPS 20' TROUBLE SHOT FLAP DISAGREE IAW FIM 27-51 FAULT TREE 808. FOUND LT OTBD FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. RESET INDICATOR, LUBED FLAP TRANSMISSION TORQUE BRAKE IAW AMM 12-21-09. OPERATED FLAPS SEVERAL TIMES, GOT NO DISAGREE. RECHECKED INDICATOR & IT WAS NOT TRIPPED. AC OK FOR SERVICE.

Part: SKIN — DENTED (BS 525) · airframe 52,648 hrs · 24,772 cycles

FUSELAGE HAS A DENT AT BS 525 BETWEEN STRINGERS 26 - 27L. REPAIRED IAW EA F-5330-T0313598 REV P1. MAJOR REPAIR.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 52,346 hrs · 24,561 cycles

DURING PREFLIGHT, FOUND L1 DOOR EMER SLIDE LIGHT INOPERATIVE. REMOVED LIGHT ASSEMBLY & CHECKED VOLTAGE TO LIGHT WITH EMER LIGHTS ON, THERE IS NO POWER TO L1 SLIDE LIGHT. DURING TROUBLESHOOTING FOUND PIN 9 OF PLUG D68 PUSHED BACK INTO PLUG BATTERY CHARGER CONNECTOR. REMOVED BATTERY CHARGER & POWER SUPPLY AGAIN & FOUND BENT PIN AT NR 9 POSITION. TRIED TO STRAIGHTEN PIN, BUT IT BROKE OFF. R & R LT EMER BATTERY CHARGER & POWER SUPPLY & RESET PINS IN CONNECTOR D68. IAW AMM 33-51-07-2 & WDM 33-51-12 REASSEMBLED LT EMER SLIDE LIGHT ASSEMBLY & TESTED EMER LIGHTS. ALL LIGHTS OPERATIONS CHECKED NORMAL AT THIS TIME.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 52,346 hrs · 24,561 cycles

DURING PREFLIGHT CHECK, FOUND R1 DOOR EMER SLIDE LIGHT INOPERATIVE. RELAMPED R1 DOOR SLIDE LIGHT, OPERATIONS CHECKED NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,343 hrs · 23,795 cycles

DOOR EMERGENCY EXIT LIGHTS WILL NOT TEST. R & R L1 EMERGENCY EXIT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL.

Part: WEB — DAMAGED (ZONE 200) · airframe 51,232 hrs · 23,707 cycles

MAIN DECK- CARGO DOOR CUTOUT ON FUSELAGE SILL AREA LOWER SILL WEB HAS A PUNCTURE LOCATED JUST AFT OF NR 1 DOOR LATCH FITTING. A REPAIR WAS ACCOMPLISHED ON THE LOWER DOOR SILL WEB BY EA 757-5331-16-F4054. MAJOR REPAIR.

Part: TRACK — FAILED (ZONE 200) · airframe 51,232 hrs · 23,707 cycles

THE CARGO HANDLING SYS, ROLLER RAILS WILL NOT LOCK INTO THE SEAT TRACK CROWNS BETWEEN STA, S660-780 RBL 24.75 AND 45.5. DISCEPANT SEAT TRACKS ARE INCOMING. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD , A REPAIR WAS PERFORMED ON STAM EA 757-5335-16-F4048 AND STAM NR 48525020001 AT STA 640-780, RBL 24.75 AND 45.5. THIS NR IS FOR TRACKING PURPOSES ONLY. "MAJOR REPAIR".

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

LT INBD FLAP, FRONT INBD PANEL HAS CORROSION. REMOVED CORROSION ON LT INBD FLAP INBD PANEL IAW-SRM-51-10-02. CHECK LIMIT ORIG MAT .125 MAT LOSS .030 FOUND OUT OF LIMIT IAW-SRM-57-53-01, FIG 101, DET VIII PG 106, WORK ACCOMPLISHED ON EA F-5750-162474. CAT "A" MAJOR REPAIR.

Part: STRINGER CLIP — CORRODED (BS 1661 S26R) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

FOUND CORROSION AT BS 1661 S26R STINGER CLIP. REPAIRED IAW SRM 53-00-03 REPAIR 2.

Part: SKIN — DENTED (ZONE 200) · airframe 51,232 hrs · 23,707 cycles

DENT IN FUSELAGE AT BS 380 STRINGER 4R A FUSELAGE EXTERNAL SKIN REPAIR WAS ACCOMPLISHED BETWEEN STA 377-418 IAW EA 757-5311-16-F3939 REV- . MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 51,232 hrs · 23,707 cycles

FUSELAGE SKIN MISREPAIRED BS 395 BETWEEN S1 TO 3L. REPAIRED IAW EA 757-5311-16-F3891, REV-.

Part: SKIN — DENTED (ZONE 200) · airframe 51,232 hrs · 23,707 cycles

SKIN DENTED BS 1630 BETWEEN S17 TO 18R. DENT REPAIRED IAW EA 757-5361-16-F3919. MAJOR REPAIR.

Part: STRINGER — CORRODED (ZONE 200) · airframe 51,232 hrs · 23,707 cycles

STRINGER 17R BS 1420-1440 CORRODED REPAIRED EA 757-5361-16-F3901. MAJOR REPAIR.

Part: PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

NR 2 SLAT COVE PANEL JUST BELOW INBD MAIN TRACK FITTING HAS CORROSION. REMOVED CORROSION ON COVE PANEL IAW SRM 51-10-02. REMOVED .019 FROM ORIGINAL THICKNESS OF .050 AND .031 WAS REMAINING. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01, FIG 101, DETAIL III, V, VI. REPLACED COVE PANEL WITH PN FX 114N4076-33. LOCATED AND DRILLED IAW DWG 114N4076 AND SRM 51-40-05. INSTALLED IAW SRM 51-40-02 AND DWG 114N4076. MAJOR REPAIR.

Part: STRUCTURE — MISREPAIRED (AFT CARGO DOOR) · airframe 51,232 hrs · 23,707 cycles

CARGO DOOR LWR FWD CORNER MISREPAIRED. REPAIRED IAW-SRM-52-30-01 FIG.201 REPAIR 4 THIS IS A CAT."B" REPAIR,MAJOR.

Part: SKIN — DAMAGED (LT WING) · airframe 51,232 hrs · 23,707 cycles

LEFT WING TOP OTBD WINGTIP HAS A LIGHTING STRIKE. FOUND LIGHTENING STRIKE TO BE ON SCREW AND SPLICE STRAP. REMOVED AND REPLACED OUTBOARD RIB LT WING SPLICE STRAP AND SCREW IAW SRM 51-40-02 AND DWG 112N5027. MAJOR REPAIR

Part: STRAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

RT APU INLET DOOR FLANGE TO FUSELAGE HAS CORROSION REMOVED CORROSION FROM FWD STRAP IAW SRM 51-10-02 ORIGINAL MATERIAL . 10 REMAINING .060 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II. R & R FWD STRAP STA 1787 S-3R TO S-6R IAW SRM 51-40-02 AND DWG 148N3105. MAJOR REPAIR.

Part: SUPPORT — CORRODED (BS 1787-1825) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

APU DOOR INLET UPPER SUPPORT BS 1787 - 1825 S3R CORRODED. REMOVED CORROSION AT APU INLET UPPER SUPPORT IAW SRM 51-10-02. BLENDED AREA ORIGINAL MATERIAL .063 MATERIAL REMAINING .023 MATERIAL REMOVED .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-80-15 FIG 101 DETAIL II. REMOVED UPPER SUPPORT AND REPLACED IAW SRM 51-40-02 AND DWG 146N3152. MAJOR REPAIR

Part: SUPPORT — CORRODED (BS 1787-1825) · airframe 51,232 hrs · 23,707 cycles

APU INLET LOWER SUPPORT BS 1787 -1825 S6R CORRODED. REMOVED CORROSION AT APU INLET SUPPORT IAW SRM 51-10-02. BLENDED AREA ORIGINAL MAT .063 MATERIAL REMOVED .040 MATERIAL REMAINING .023 FOUND TO BE OUT OF LIMITS IAW SRM 53-80-15, FIG 101, DETAIL II. R & R LOWER SUPPORT IAW SRM 51-40-02 AND DWG 148N3105. MAJOR REPAIR.

Part: PANEL — CRACKED (NR 2 SLAT) · airframe 51,232 hrs · 23,707 cycles

NR 2 SLAT COVE PANEL CRACKED JUST INBD OF OTBD MAIN SLAT TRACK. REMOVED AND REPLACED NR 2 SLAT COVE PANEL IAW SRM 51-40-02 AND DWG 114N4076. MAJOR REPAIR.

Part: PANEL — CRACKED (NR 2 SLAT) · airframe 51,232 hrs · 23,707 cycles

NR 2 SLAT COVE PANEL CRACKED JUST INBD OF INBD MAIN SLAT TRACK. REMOVED AND REPLACED NR 2 SLAT COVE PANEL IAW SRM 51-40-02 AND DWG 114N4076. MAJOR REPAIR.

Part: PANEL — CORRODED (NR 1 SLAT) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

NR 1 SLAT HAS CORROSION AROUND FASTENERS BEHIND OTBD MAIN SLAT COVE PANEL. CLEANED CORROSION IAW SRM-51-10-02, REMOVED .025 FROM ORIGINAL THICKNESS OF .050 AND .025 REMAINING.FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01 FIG.101 DETAIL IV PG.104. LOCATED AND DRILLED AND INSTALLED NEW COVE SKIN IAW-DWG#114N4076 AND B757- 200-SRM-51-40-02 AND 51-40-05, CAT."A" MAJOR REPAIR.

Part: WEB — CRACKED (BS 660-680) · airframe 51,232 hrs · 23,707 cycles

FOUND WEB, BS 660-680 S17R CRACKED. WEB FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL V, PAGE 103. R & R WEB IAW SRM 51-40-02 AND DWG 143N8322. MAJOR REPAIR.

Part: SKIN — DENTED (BS 660-680) · airframe 51,232 hrs · 23,707 cycles

EXTERNAL FUSELAGE SKIN DENTED BS 660-680 BETWEEN S25 - 26L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REMOVED DAMAGE IAW SRM 53-00-01 FIG 201 REPAIR 7. NO CRACKS FOUND AROUND DAMAGED AREA, FABRICATED REPAIR PARTS IAW SRM 53-00-01 REPAIR 7 FIG 201 P 201 STEPS 4-10, PG 203 TABLE II. INSTALLED ALL REPAIR PARTS IAW SRM 53-00-01 FIG 201 REPAIR 7 AND DWG 143N3691. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1420-1440) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

CREASE BEAM WEB AT BS 1420-1440 CORRODED. REMOVED CORROSION IAW SRM 51-10-02, WEB FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG.101, DET III PG.103, A2. REMOVED AND REPLACED WEB IAW SRM 51-40-02 & DWG 146N5590. MAJOR REPAIR.

Part: FLANGE — CORRODED (BS 1825) · airframe 51,232 hrs · 23,707 cycles

APU INTAKE DUCT CUT-OUT AFT FLANGE HAS CORROSION AT BS 1825. REMOVED CORROSION IAW SRM 51-10-02 ORIGINAL MATERIAL .10 REMAINING .060 OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II. REPAIRED AFT STRAP IAW SRM 53-80-15, FIG 202, REPAIR NR1, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 51,232 hrs · 23,707 cycles

SKIN MISREPAIRED AT BS 667 BETWEEN S27R TO S-28R REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16. MAJOR REPAIR.

Part: FRAME — MISREPAIRED (BS 1280 S9-13L) · airframe 51,232 hrs · 23,707 cycles

FRAME MISREPAIRED AT BS 1280 STR 9-13L. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 PG 202 REPAIR 3.

Part: FRAME — MISREPAIRED (BS 1280 S9-13R) · airframe 51,232 hrs · 23,707 cycles

FRAME MISREPAIRED AT 1280 STR 9-13R. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 PG 202 DETAIL I REPAIR 3.

Part: SEAT TRACK — GOUGED (BS 700-780) · airframe 51,232 hrs · 23,707 cycles

MAIN CABIN AREA BETWEEN BS 700 - 780 LBL 45 SEAT TRACK NICKED, GOUGED, AND SCRATCHED. REPAIR CLASSIFIED AS A MINOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 640-685) · airframe 51,232 hrs · 23,707 cycles

MAIN CABIN AREA BETWEEN BS 640- 685 LBL 25 SEAT TRACK WITH NICKS, GOUGE, AND SCRATCHES. REPAIR CLASSIFIED AS A MINOR.

Part: FRAME — DENTED (BS 377) · airframe 51,232 hrs · 23,707 cycles

CABIN FRAME HAS A DENT BS 377, STR 6R. COMPLIED WITH EA F-5310-162465

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

CABIN FLOORBEAM HAS CORRISION BS 324, RBL 32 TO RBL 64. REMOVED AND REPLACED FLOORBEAM TEE IAW SRM 51-40-02 AND DWG 141N293. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 740) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

MAIN CABIN FLOORBEAM BS 740, LBL 45 - 60 HAS CORROSION ON UPPER ANGLE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REPAIRED FLOORBEAM UPPER ANGLE IAW SRM 53-00-51 FIG 201 REPAIR 3. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1220-1260 S17) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

MAIN CABIN AREA BETWEEN BS 1220- 1260, STR 17L CREASE BEAM CORRODED. R & R IAW SRM 51-40-02 AND DWG 146N5590. MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 1320-1380) · airframe 51,232 hrs · 23,707 cycles

STRINGER 17R , BS 1320-1380 CORRODED.

Part: FLOORBEAM — CORRODED (BS 345) · airframe 51,232 hrs · 23,707 cycles

MAIN CABIN SEC 41, AREA AT BS 345, LBL 4 HAS CORROSION ON FLOORBEAM. FLOORBEAM REPAIRED IAW SRM 53-00-01, FIG 201, PG 201, REPAIR 3 AND DWG 141N5160. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (BS 1540-1640) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

SEAT TRACK BS 1540 - 1640 RBL 45, NICKED, GOUGED, AND CORRODED. REMOVED DAMAGE IAW SRM 51-10-02, SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-00-52. DETAIL VII PG 102, FIG 101 R & R STEAT TRACK IAW SRM 53-00-52 AND DWG 146N5125. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 51,232 hrs · 23,707 cycles

FLOORBEAM UPPER TEE, BS 1640 BL 0 - RBL 65, CORRODED. R & R FLOORBEAM IAW DWG 146N5500 SH 1, REV D AND SRM 51-40-02. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101 AND SRM 53-00-51, FIG 101, SH4. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

CABIN FLOORBEAM HAS CORROSION BS 365, LBL 34- RBL.70. REPAIRED FLOORBEAM UPPER TEE IAW SRM 53-00-51, FIG 201, REPAIR 3. THIS IS A CAT "A" MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1360-1380) · airframe 51,232 hrs · 23,707 cycles

STRINGER 17R CREASE BEAM WEB, BS 1360-1380 CORRODED. REPAIR CONSIDERED MINOR.

Part: WEB — CORRODED (BS 1350-1360) · airframe 51,232 hrs · 23,707 cycles

STRINGER 17R WEB LOWER SIDE, BS 1350-1360 CORRODED. FOUND TO BE IN LIMITS.

Part: CREASE BEAM — CORRODED (BS 730-760) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

MAIN CABIN AREA, STRINGER 17L CREASE BEAM BS 730-760 CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. R & R IAW SRM 51-40-02 AND DWG 143N8322. MAJOR REPAIR.

Part: STRINGER — CORRODED (BS 660-760 S17R) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

STRINGER 17R BS 660-760, CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. INSTALLED STRINGER IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 377.7) · corrosion level 2 · airframe 51,232 hrs · 23,707 cycles

MAIN CABIN SEC 41, AREA AT BS 377.7 FLOORBEAM CORRODED. BLENDED CORROSION IAW SRM 51-10-02. CHECKED LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III, D=.029 W=.6 L=1.3 ORIGINAL MATERIAL THICKNESS, .150 AFTER BLEND .121 FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM REPAIR IAW SRM 51-40-02. INSTALLED FLOORBEAM REPAIR IAW SRM 51-40-02, DWG 141N5112, AND SRM 53-00-51 REPAIR 3, STA 377, RBL 30 -LBL 62. MAJOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 1440) · airframe 51,232 hrs · 23,707 cycles

AT BS 1440 INNER CREASE BEAM CORRODED ON RT SIDE.