N999FD

Part: NONE — DIRTY (ZONE 800) · airframe 69,790 hrs · 27,595 cycles

PDIS 999 25-60 8906 16DEC21 FSD FACT U BOTH ENTRY DOORS UNABLE TO ARM SLIDE MEL 16DEC21 18:49 FSD U RELEASED FOR SERVICE PER MEL : 52-11-01-B CATEGORY : B EXPIRATION : 19DEC21 "MEL 52-11-01-B: L1 AND R1 _ SLIDE(S)) INOP. NO JUMPSEATERS/ACM'S ARE TO OCCUPY COURIER AREA IN FLIGHT." AT DEPARTURE TIME. NO TIME TO T/S. SUSPECT FROZEN PRECIP IS THE CAUSE C/7298064 SHGN 17DEC21 23:48 CID U DSCRP IS PUT IN WORK FACT 18DEC21 01:25 CID U INSPECTED, CLEANED, AND LUBED L1 AND R1 GIRT BAR SLIDERS AND GIRT BAR FLOOR FITTINGS PER AMM 25-66-10-2. L1 AND R1 DOORS OPEN, CLOSE, AND ARM NORMALLY PER AMM 52-11-00-2. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (SLAT SYSTEM) · airframe 69,563 hrs · 27,436 cycles

LE SLAT ASY AND LE SLAT DISAGREE. COMPLETED QRH, ISSUE WOULD NOT CLEAR. RETURNED TO MCO. EMERGENCY DECLARED. PERFORMED BITE TEST FSEU IAW B757 FRMFIMFX1 27-51-FAULT TREE 803 AND T/S IAW FRMFIMFX1 27-51- 805 NO FAULTS, PERFORMED TECH TIP #18-0044 L/E SLAT DISAGREE TROUBLESHOOTING GUIDE NO FAULTS AT THIS TIME, A/C OK FOR SERVICE

Part: SPRING — BINDING (R1 GIRT BAR) · airframe 69,379 hrs · 27,294 cycles

AT BLOCK IN, R1 DOOR WAS DIFFICULT TO OPEN AND SLIDE COVER BECAME DISENGAGED. REINSTALLED COVER AND PERFORMED OPS CK OF R1 DOOR. FOUND WHILE DISARMING DOOR SLIDE, THE AFT LEAF SPRING ON GIRT BAR CAUSES CONTACT ISSUES ON GIRT BAR SLIDER. DOOR CLOSES OK AND ARMS OK, BUT IS DIFFICULT TO DISARM AND THEREFORE OPEN. REMOVED AND REPLACED R1 GIRT BAR IAW AMM 25-66-10-2. OPS CHECK GOOD.

Part: FRAME — CRACKED (BS 1640 S14R) · airframe 69,369 hrs · 27,286 cycles

DURING ROTO PROBE OF RH BS 1640 AT S-14, CRACKS WERE FOUND IN BOTH BOTTOM HOLES AND BOTH HOLES HAVE INDICATIONS AT 3 O'CLOCK AND 9 O'CLOCK. IT APPEARS THE FRAME IS CRACKED ALL THE WAY ACROSS. COMPLIED WITH E.A. # T F-5310-T0361972 P1 EA TITLE FUSELLAGE-MAIN FRAME STA 1640 FRAME SPLICE REPAIR TO REPAIR CRACK AT ST-14 RIGHT, RELEASE DATE JUN 17, 2021, MAJOR REPAIR.

Part: VALVE — MALFUNCTIONED (TE FLAP SYSTEM) · airframe 68,839 hrs · 26,887 cycles

TRAILING EDGE FLA DISAGREE EICAS MESSAGE WHEN SELECTING FLAPS 1, RAN QRH USED ALTN FLAPS 20 FOR LANDING. AFW U HAD CONFERENCE WITH INBOUND CAPTAIN, STATED WHEN MOVED TO FLAPS 1 HAD NO ACTION, HAD NO ROLL SITUATION ALSO. WENT TO ALTN FLAPS AND LANDING UNEVENTFUL. REMOVED AND REPLACED THE BYPASSED VALVE, IAW 757 AMM 27-81-09-4. RAN THE FLAPS THROUGH HYD AND ELECT ALT (AND WITH LEFT ENG RUNNING), IAW 757 JRH CHPT 5. OPS CHECK GOOD, NO DEFECT NOTED. A/C OK FOR SERVICE. REASON CODE: SCHEDULED REMOVAL/INSTALLATION OFF MPN: 340545 POS: 1 ON MPN: 340545 SRL: 3395 TAG NBR: C96915.

Part: ACTUATOR — FAILED · airframe 68,672 hrs · 26,783 cycles

L/E SLAT DISAGREE , 3000FT @210 KTS, RAN QRH LANDED W/ALT FLAPS 20 T/S IAW FIM 27-51 F/T 805 AND FIM 27-81 F/T 803. BITE CHECK ON FSEU 1 HAS NO EXISTING FAULTS BUT SHOWS FAULT 310 SLAT DISAGREE INTERMITTENT ON LAST LEG. FSEU 2 HAS NO EXISTING FAULTS BUT SHOWS FAULT 226 SLAT PDU XMT ON LAST LEG. INSPECTED SLATS AND CYCLED SEVERAL TIMES IAW FIM. SLAT DISAGREE MESSAGE DID NOT RETURN. CHECKED SLAT PDU POSITION TRANSMITTER FOR PROPER ADJUSTMENT THROUGH ALL SLAT POSITIONS IAW B757 AMM 27-58-01-5, ALL POSITIONS WITH LIMITS, CHECKED CONNECT, WIRING AND PHYSICAL CONDITION OF TRANSMITTER, NO DEFECTS NOTED. INSPECTED PDU I/B AND O/B OVERLOAD INDICATORS, BOTH CHECK GOOD, INSPECTED COMPLETE LEFT AND RIGHT WING SLAT'S ROTARY ACTUATORS OVERLOAD INDICATORS, FOUND #5 SLAT O/B ACTUATOR WAS TRIPPED AND INDICATOR BROKEN, T/S REF FIM 27-81 FAULT TREE 803. INSTALLED #5 LE O/B SLAT ROTARY ACTUATOR REF. 757AMM 27-81-18-4. OPERATIONAL CHECKS GOOD. REMOVED HAMILTON SUNDSTRAND P/N- 755299D S/N- A0929.

Part: ACCESS DOOR — MISSING (AIRSTART) · airframe 68,657 hrs · 26,773 cycles

DURING AIRCRAFT ARRIVAL MAINTENANCE FOUND L/H LOWER FUSALAGE AIRSTART ACCESS DOOR DETACHED AND MISSING FROM AIRCRAFT FUSELAGE, UPON ACCESS DOOR LEAVING FUSELAGE IN FLIGHT, SMALLER HOLE WAS MADE AT CENTER OF FUSEALAGE CENTERLING. INSTALLED LH GROUND AIR SUPPLY ACCESS DOOR PER REF 52_49_04_4_0. AC OK FOR SERVICE.

Part: ACTUATOR — INOPERATIVE (TRUCK POSITION) · airframe 68,285 hrs · 26,524 cycles

GEAR DISAGREE AFTER TAKEOFF. RAISED GEAR PER QRH. REMOVED & REPLACED RT MAIN GEAR TRUCK POSITIONER ACTUATOR IAW AMM 32-32-15-4. OPS AND LEAK CHECKED GOOD.

Part: STOWAGE BOX — FAILED (COCKPIT) · airframe 68,168 hrs · 26,437 cycles

F/O?S O2 MASK STOWAGE BOX WILL NOT TEST. REPLACED FO'S O2 MASK/STOWAGE BOX PER AMM 35-11-51-4-98. TAG# 7G3378 FOR P/N MXP891-3, S/N SE47881. SYSTEM WILL NOT TAKE TAG #. OFF P/N MXP891-3, S/N SE37958.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 68,102 hrs · 26,388 cycles

AFT CARGO BAY AT FS1540 & STR 25L TIE CLIP DAMAGED DOT 109 052 EVALUATED AND FOUND AFT CARGO COMPT, TIE CLIP AT STA 1540 STR 25L CRACKED. REMOVED FABRICATED AND INSTALLED NEW TIE CLIP AS PER SRM REFS. 53-00-53-1A FIG 101 DET. V , 51-40-02-OG AND DWG 140N2001 REV BN.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,853 hrs · 26,216 cycles

PDIS 999 27-80 6604 16JAN19 PVD FACT U LOGPAGES:2804127 "LE SLAT DISAGREE" MESSAGE WHEN FLAP 1* SELECTED APPROXIMATE AIR SPEED 220 KTS. LANDED WITH FLAPS 20* USING ALTN TE FLAPS FACT 16JAN19 18:27 PVD U T/S "LE SLAT DISAGREE" MSG PRE FIM 27-81-00-815 FAULT TREE 803 FIG 104 AND FIM 27-51-00-815 FAULT TREE 805 OPS CHECKED THE LE SLAT AND FLPS SEVERAL TIMES WITH NORMAL HYD SYSTEM AND ALT SYSTEM NO FAULTS OR MSG RECIVED ON THE EICAS AND FSEU 1, 2, & 3. ALSO CHECKED THE FAULT HISTORY ON FSEU 1, 2, & 3 NO HISTORY OR CODE FOR "LE SLAT DISAGREE". OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: INDICATOR — BROKEN (L1 DOOR) · airframe 67,682 hrs · 26,104 cycles

MDIS 999 52-10 6451 14NOV18 MEM OPEN U CREW BREIFING WITH CAPTAIN: L1 PASSENGER DOOR ARM/DISARM CONDITION INDICATOR BROKEN OFF. L1 DOOR STILL ARMS AND DISARMS OPS CHECK GOOD. PLACED PLACARD IN COCKPIT PITOT COVERS HOLDER BEHIND CAPTAIN FOR FUTURE REPAIR. REF B757 AMM 20-30-01-2, AMM 25-66-00, RESECURED LI DOOR ARM/DISARM CONDITION INDICATOR PLACARD TRACK TO DOOR PANEL AND REINSTALLED PLACARD, DOOR OPERATION AND SLIDE ARM/DISARM OPS CHK OK.

Part: SPACER — OUT OF POSITION (ACCESS DOOR) · airframe 67,428 hrs · 25,942 cycles

EICAS MSG "FWD ACCESS DOOR" ILLUMINATED AFTER TAKE OFF. CHECKED RIGGING OF FWD DOOR WARNING IN ACCORDANCE WITH MM 52-71-00-5. FOUND SPACER FOR COVER TO CONTACT STRIKER. INSTALLED COVER SPACER SO IT WILL NOT HIT STRIKER. OPERATED DOOR SEVERAL TIMES DOOR WARNING WAS ON WITH DOOR OPEN AND OFF WITH DOOR CLOSED.

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 66,517 hrs · 25,307 cycles

EMERGENCY LIGHTS WILL NOT TEST FROM SWITCH ABOVE THE L1 DOOR. FOUND A WIRE LOOSE FROM THE CONNECTION AT THE TEST SWITCH . SECURED THE CONNECTION AND PERFORMED AN OPS TEST IAW AMM 33-51-00-5, LIGHTS OPS TESTED GOOD.

Part: SKIN — DENTED (BS 1590) · airframe 66,454 hrs · 25,267 cycles

FUSELAGE SKIN HAS A LONG DENT AT BS 1590, STRINGER 15L. REPAIRED THE SKIN IAW EA F-5330-TO333465, P1.

Part: STRINGER — DENTED (BS 1590) · airframe 66,454 hrs · 25,267 cycles

BS 1590 LEFT FUSELAGE ON DVI OF DENT CUTOUT, FOUND STRINGER 15L DENTED. CUT OUT THE DAMAGED STRINGER IAW EA F-5310-T0333465 P1. FABRICATED A NEW STRINGER, FILLER, SHIMS IAW EA F-5310-T0333465 P1 AND INSTALLED IAW EA, SRM 51-40-02-0G, AND SRM 51-20-05-0G.

Part: SKIN — DENTED (BS 500) · airframe 66,454 hrs · 25,267 cycles

LOWER EXTERIOR FUSELAGE SKIN HAD A PROTUDING DENT AT BS 500, BETWEEN STRINGERS 26 AND 27L. REPAIRED THE SKIN IAW EA F-5330-T, T0333454 P1.

Part: SKIN — DENTED (BS 525) · airframe 66,454 hrs · 25,267 cycles

LOWER EXTERIOR FUSELAGE SKIN HAD A PROTUDING DENT AT BS 525, BETWEEN STRINGERS 26 AND 27L. REPAIRED THE SKIN IAW EA F-5330-T0333446 P1.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 66,433 hrs · 25,251 cycles

L1 DOOR SLIDE ARM LIGHT NOT ILLUMINATED WHEN L1 DOOR IS ARMED.

Part: PROXIMITY SWITCH — INOPERATIVE (L1 DOOR) · airframe 66,433 hrs · 25,251 cycles

L1 DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. REMOVED AND REPLACED THE PROXIMITY SWITCHES FOR THE GIRT BAR ANNUCIATOR LIGHT ON LT PAX DOOR. OPS CHECKED GOOD IAW MM 25-66-11-2.

Part: BULB — INOPERATIVE (ARM INDICATOR) · airframe 66,429 hrs · 25,247 cycles

L1 DOOR SLIDE ARM INDICATION LIGHT INOPERATIVE. REPLACED THE BULBS IAW WDM 25-66-11. LIGHT OPERATES NORMAL WHEN DOOR IS ARMED.

Part: FILTER — DIRTY (RECIRC FAN) · airframe 65,833 hrs · 24,849 cycles

DURING CLIMB AT 15,000 - 21,000 FT, DETECTED FUMES IN COCKPIT. HAD ANTI ICE SWITCHES ON. REMOVED RECIRCULATION AIR FILTER. FOUND FILTER TO BE DIRTY, AND CONTAMINATED. INSTALLED A NEW RECIRCULATION AIR FILTER .

Part: SLIDE — OUT OF POSITION (ZONE 200) · airframe 65,434 hrs · 24,559 cycles

PART OF ESCAPE SLIDE FOR RT DOOR IS HANGING DOWN, SHOWS SIGNS OF GETTING CAUGHT WHEN DOOR IS CLOSED. TROUBLE SHOT & FOUND SAFETY FLAG HANGING DOWN FROM POUCH. INSTALLED FLAG. USING IAW MM-25-66-00-00. ACFT OK FOR SERVICE.

Part: LOCK — FAILED (R1 DOOR) · airframe 65,183 hrs · 24,405 cycles

ON POST FLIGHT, FOUND R1 DOOR SLIDE PRESS GAGE OUT OF GREEN BAND. REMOVED AND REPLACED FWD AND AFT BAR LOCKS R1 ENTRY DOOR IAW MM 25-66-01-4 OPS CHECK GOOD OK FOR SERVICE.

Part: LIGHT — FAILED (ENTRY DOOR) · airframe 650 hrs · 24,315 cycles

LEFT ENTRY DOOR SLIDE LIGHT WILL NOT ILLUMINATE WHEN ARMED. RELEASED FOR SERVICE IAW MEL 25-66-05-A CATEGORY C. L1 ESCAPE SLIDE GIRT BAR, ENGAGEMENT LIGHTS INOPERATIVE. VERIFY & RECORD IN AML & EAML THAT ASSOCIATED SLIDE IS VISUALLY VERIFIED ENGAGED PRIOR TO EACH DEPARTURE. TROUBLE SHOT & FOUND LIGHT ASSEMBLY FOR SLIDE LIGHT INOPERATIVE. R & R L1 DOOR SLIDE ARM LIGHT. OPERATIONS CHECKED NORMAL IAW AMM & WDM REF 33-51-01.

Part: LIGHT — NOT SEATED (L1 DOOR) · airframe 649 hrs · 24,237 cycles

L1 DOOR SLIDE ARM INDICATOR LIGHT NOT ILLUMINATED WHEN DOOR SLIDE IS IN THE ARM POSITION. RESEATED SLIDE LIGHT BULB ASSEMBLY. OPERATIONS CHECKED NORMAL IAW MM 52-11-25-5.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 648 hrs · 24,178 cycles

ON WALK AROUND FOUND LT EXTERIOR EMER LIGHT NOT WORKING, NEAR L1 DOOR. RELEASED FOR SERVICE IAW MEL 33-51-02-02 CATEGORY D. EXTERIOR EMER LIGHTING SYS INOPERATIVE.

Part: SKIN — DAMAGED (TE FLAP) · airframe 648 hrs · 24,150 cycles

LEFT OTBD FLAP UPPER SURFACE HAS HAIL DAMAGE. REPAIRED LT OTBD AFT FLAP IAW EA F-5750-T0318240 PT 1 & SRM 51-70-17.

Part: SKIN — DAMAGED (RT AILERON) · airframe 648 hrs · 24,150 cycles

RIGHT AILERON UPPER SKIN PUNCTURED, 12 INCHES FROM INBD EDGE & AT OTBD END, APPROX 18 INCHES FROM THE EDGE. REPAIRED AILERON IAW EA F-5750-T0318152 PT1 & SRM 51-70-17.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 648 hrs · 24,150 cycles

RIGHT INBD AFT FLAP UPPER SURFACE HAS HAIL DAMAGE. REPAIRED IAW EA F-5750-T0318277 PT

Part: SKIN — DAMAGED (LT AILERON) · airframe 648 hrs · 24,150 cycles

LEFT AILERON UPPER SURFACE HAS HAIL DAMAGE. REPAIRED LT AILERON UPPER SURFACE IAW EA F-5750-T0318151 REV A PT 1 & SRM 51-70-17.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 648 hrs · 24,150 cycles

RIGHT OTBD AFT FLAP UPPER SURFACE CTR AREA EVIDENCE OF DELAMINATION. REPAIRED 8 EACH AREAS OF DELAMINATION IAW SRM 51-20-01, SRM 51-21-10-7 & EA F-5750-T0318133 A PT 1.

Part: FRAME — PUNCTURED (BS 239) · airframe 648 hrs · 24,150 cycles

FRAME UPPER RADIUS PUNCTURED BS 239 BL 0. REPAIRED IAW EA F-5310-T0318094 PT 1.

Part: SKIN — CORRODED (LT WING) · airframe 648 hrs · 24,150 cycles

LEFT WING UPPER SURFACE T/E PANEL HAS SIGNS OF CORROSION WS 70 - 100. REPAIRED IAW EA F-5730-T0318150 PT 1.

Part: SKIN — CORRODED (RT WING) · airframe 648 hrs · 24,150 cycles

RIGHT WING UPPER SURFACE T/E PANEL HAS SIGNS OF CORROSION WS 70 - 100. REPAIRED IAW EA F-5730-T0318162 PT 1.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 63,982 hrs · 23,698 cycles

LOUD POP AT FL400, LT FWD WINDOW PANE SHATTERED & ARCED MOMENTARILY. R & R NR 1 WINDSHIELD IAW AMM 56-11-01-4.

Part: LEVER — BINDING (CREW DOOR) · airframe 63,629 hrs · 23,513 cycles

VERY DIFFICULT TO ARM THE SLIDE ON THE LEFT CREW ENTRY DOOR. REQUIRED SEVERAL ATTEMPTS TO GET IT ARMED. GENERAL VISUAL INSPECTION CARRIED OUT OF THE ARMING SYS. OPS CHECKED IAW MM 25-66-00-5, SYS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,268 hrs · 23,319 cycles

L1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED NORMAL.

Part: LATCH — BROKEN (SLIDING WINDOW) · airframe 63,017 hrs · 23,187 cycles

F/O WINDOW LOCK HANDLE EASILY DISPLACED FROM LOCK/STOWED POSITION WITHOUT DEPRESSING UNLOCK BUTTON. TROUBLESHOT F/O SLIDING WINDOW AND FOUND THE BUTTON ON THE LATCH HANDLE IS INTERNALLY BROKEN IAW MM 56-11-02-5. REPLACED F/O SLIDING WINDSHIELD LOCKING HANDLE IAW CMM 56-11-51 PG 704. OP CHECKED NORMAL IAW MM 56-11-02-5

Part: ACTUATOR — DAMAGED (NLG DOOR) · airframe 62,886 hrs · 23,121 cycles

AFTER TAKEOFF WITH GEAR HANDLE UP, RECEIVED A GEAR DISAGREE EICAS MESSAGE AND TOWER REPORTED OUR NLG DID NOT RETRACT. FOLLOWED QRH PROCEDURE AND RTB UNEVENTFUL. R & R NLG DOOR ACTUATOR IAW AMM 32-34-03-4. ACCOMPLISHED FUNCTIONAL TEST AND LEAK CHECK OF NLG DOOR ACTUATOR IAW MM 32-34-03-4. NO DEFECTS WERE FOUND. ACCOMPLISHED GEAR SWING FOR NLG IAW MM 32-34-00-5. NO DEFECTS WERE FOUND.

Part: SKIN — CRACKED (BS 303) · airframe 62,885 hrs · 23,120 cycles

CROWN SKIN, BS 303, S4R, CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EA F-5330-152497.

Part: SKIN — GOUGED (BS 1383) · airframe 62,885 hrs · 23,120 cycles

SKIN GOUGED AT BS 1383, S23-24L. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 51-10-2, SRM 53-00-01 REPAIR 16 FIG 201 AND SRM 51-40-02.

Part: BULKHEAD — GOUGED (APU BAY) · airframe 62,885 hrs · 23,120 cycles

APU COMPARTMENT FWD BULKHEAD PANEL IS GOUGED. DAMAGE IS OUT OF LIMITS IAW SRM 53-80-08, FIG 101, AD1. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 53-80-08, FIG 201, REP2 AND SRM 51-40-02.

Part: GIRT BAR — BROKEN (PAX DOOR) · airframe 62,856 hrs · 23,099 cycles

LEFT FWD ENTRY WILL CLOSE BUT NOT ARM. FOUND FWD DETENT SPRING BENT AND BROKEN. WILL REQUIRE NEW GIRT BAR ASSY. R & R FWD GIRT BAR CAM AND BAR LOCK ASSY. OPS CHECKED NORMAL, REF AMM 25-66-10-2. ACFT OK FOR SERVICE.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 62,533 hrs · 22,893 cycles

LT ENTRY DOOR PULL HANDLE BROKEN. NO RESTRICTION REF: EA F 52-10-166386, L-1 DOOR ASSIST HANDLE BROKEN.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,065 hrs · 22,570 cycles

R1 DOOR SLIDE ILLUMINATION LIGHT INOP. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,065 hrs · 22,570 cycles

R1 DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,880 hrs · 22,460 cycles

L1 SLIDE LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 61,470 hrs · 22,214 cycles

LEFT ENTRY SLIDE DEPLOYED. R & R THE L1 DOOR SLIDE IAW MM 25-66-01-4 AND 25-66-10-2. OPS CHECKED GOOD, OK FOR SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION (MAIN CARGO) · airframe 61,372 hrs · 22,155 cycles

MAIN CARGO FIRE EICAS ALERT ALONG WITH MASTER WARNING ALERTS ILLUMINATED AFTER TAKEOFF CLIMBING THROUGH 2,500 FT. ALERT LASTED APPROX 5 SECONDS. OVERHEAD MAIN CARGO FIRE DETECTION PANEL ILLUMINATED MID, AFT AND CARGO ISLATION LIGHTS. ALL ALERTS EXTINGUISHED AFTER 5 SECONDS. NO DG ABOARD AND APPROX 7000 LBS OF EMPTY CANS ABOARD. VISUALLY INSPECTED MAIN CARGO BAY. NO SMOKE OR FIRE INDICATIONS. PASSENGER OXYGEN SYS AUTO DEPLOYED. CHECKED EICAS FAULTS, NO FAULTS NOTED, PERFORMED FIRE AND CARGO SMOKE TEST OPS CHECKED NORMAL. RESET OXYGEN MASK IN FWD LAV VERIFIED OXYGEN QTY IN BOTH BOTTLES AND ALSO INSPECTED BLOW OUT DISK. OK FOR SERVICE IAW MM 5-11-00-6/26-23-00-5.

Part: BRACKET — UNSECURE (R1 DOOR) · airframe 61,312 hrs · 22,119 cycles

DOOR IR (RT SIDE) KNUCKLE RAPPER DOES NOT STOW WHEN DOOR IS DE-ARMED (INTERMITTENT). SECURED RETRACTABLE DOOR STOP BRACKET REF MM 52-11-20-5. CKS GOOD.

Part: FIRE WARNING — FALSE ACTIVATION (LEFT) · airframe 61,313 hrs · 22,120 cycles

ON A G/A, FIRE WARNING LT, EICAS MAIN CARGO FIRE LIGHT CAME ON FOR LESS THAN 15 SECONDS, LANDED, NO SIGNS OF FIRE. PERFORMED BITE TEST IAW FIM 26-16-30-101, NO FAULTS DETECTED. ACFT OK FOR SERVICE.

Part: PLATE — LOOSE (PAX DOOR) · airframe 61,265 hrs · 22,094 cycles

DOOR ARM/DISARM COVER PLATE LOOSE. REPAIRED AREA USING SRM 51-70-09.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 61,190 hrs · 22,048 cycles

ON PRE-DISPATCH CHECK FOUND L-1 DOOR ESCAPE SLIDE PRESSURE TO BE APPROX 3 NEEDLE WIDTHS BELOW GREEN BAND. REMOVED AND REPLACED L1 ESCAPE SLIDE REF 25-66-01-4. AIRCRAFT OK FOR SERVICE.

Part: SKIN — MISREPAIRED (BS 1400) · airframe 61,137 hrs · 21,991 cycles

FLUSH REPAIR LOCATED AT BS 1400, BETWEEN S 21L AND S 22L DOES NOT MEET SRM REQUIREMENTS AND WAS REWORKED IAW E.A. F-5330-146509.

Part: CREASE BEAM — DAMAGED (ZONE 200) · airframe 61,137 hrs · 21,991 cycles

STA 1630, CREASE BEAM INNER CHORD HAS A DOUBLE DRILLED HOLE AT NUT PLATE ATTACH HOLE AND .1875 FASTNER HOLE. INCOMING CONDITION. DUE TO DISCREPANCY EFFECTING THE PTF MOD A REPAIR WAS PERFORMED AT STA 1630, RBL 64.40 ON MAE EA 757-5361-16-F3161 AND MAE W/C 118350399E22R03. MAJOR REPAIR

Part: SKIN — MISREPAIRED (BS 236) · airframe 61,137 hrs · 21,991 cycles

FLT CREW COMP LT SIDE AT BS 263 REPAIR SEVERAL RIVITS WITH BAD BUCKTAILS, AS MARKED. REMOVED DOUBLER IAW SRM 51-40-02. COMPLIED WITH EA F-5330-146517. FUSELAGE EXISTION SKIN REPAIR REPLACEMENT AT STA 263 AND WL 220 LT SIDE. MAJOR REPAIR.

Part: STRINGER — GOUGED (BS 1688 S18L) · airframe 61,137 hrs · 21,991 cycles

STRINGER 18L AT 1688 HAS A GOUGE IN THE UPPER SURFACE. REMOVED AND REINSTALLED VENT DUCT IAW SRM 51-40-02. REMOVED DAMAGED STRINGER IAW SRM 51-40-02. FABRICATED NEW STRINGER ON MAE TRAVELER T11/882745. INSTALLED NEW STRINGER IAW SRM 51-40-02. FABRICATED NEW H-CLIP ON MAE TRAVELER T11/883257. INSTALLED NEW H-CLIP IAW SRM 51-40-02. REINSTALLED ALL PARTS REMOVED TO FOM IAW SRM 51-40-02. CLASSIFIED MAJOR REPAIR

Part: SKIN — MISREPAIRED (BS 1690-1710) · airframe 61,137 hrs · 21,991 cycles

REPAIR MISINSTALLED, REPLACEMENT REMOVED AND REPLACED EXISTING REPAIR AT STA 1690-1710 BETWEEN S-17L TO S-19L IAW EA F-5330-146522 . MAJOR REPAIR.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 61,137 hrs · 21,991 cycles

NR 4 L/E SLAT HAS CHAFING ALONG THE TOP OF THE SLAT FROM INBD TO OTBD SIDE. REPAIRED NR 4 SLAT IAW SRM 51-70-10, PN 114N4005-177G, SN A1-0249. REPAIR IS ON THE INBD END AND IS 24" L X 7" W. EA F-5750-146530 GENERATED FOR TRACKING PURPOSES ONLY. CLASSIFIED MAJOR REPAIR.

Part: CHANNEL — CORRODED (NR 6 SLAT) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

NR 6 SLAT INBD INNER L CHANNEL HAS CORROSION REMOVED CORROSION ON NR 6 SLAT INBD " L "CHANNEL IAW SRM 51-10-02 FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG 101 DETAIL II. ORIGINAL MATERIAL .080 AFTER REWORK .060 SLAT. R & R ON N00817, MAJOR REPAIR.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 61,137 hrs · 21,991 cycles

REWORK OF SNRM N00013: REWORK REQUIRED AT STA 740 S-17L TO S-18L. EXTERNAL DOUBLER/TRIPLER REPAIR DUE TO INSTALLATION IN PASSENGER CONFIGURATION REMOVED AND REPLACED EXISTING REPAIR AT STA 740 S-17 TO 18L USING EA-F 5330-1465112 REF SNRM N00013. MAJOR REPAIR. COPY OF 8110-3 ATTACHED.

Part: SKIN — CORRODED (NR 10 SLAT) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

NR 10 SLAT UPPER NOSE SKIN CORRODED AT OSS 736. REMOVED CORROSION ON NR 10 SLAT IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.5 D.028. ORIG MATERIAL .063 AFTER REWORK .035 FOUND OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DETAIL VI. ACCOMPLISHED EA F-5750-146287. MAJOR REPAIR

Part: SKIN — CORRODED (NR 10 SLAT) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

NR 10 SLAT UPPER NOSE SKIN CORRODED AT OSS 809. REMOVED CORROSION ON 10 SLAT IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.5 D=.025 ORIG MATERIAL .063 AFTER REWORK .038. FOUND OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DETAIL VI. ACCOMPLISHED EA F-5740-146287. MAJOR REPAIR

Part: SKIN — DENTED (BS 1640-1660) · airframe 61,137 hrs · 21,991 cycles

EXTERNAL FUSELAGE SKIN STA 1640-1660 S-23R TO S-24R HAS DENT. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 16. CATEGORY "B" MAJOR REPAIR

Part: SKIN — MISREPAIRED (BS 740-760 S6-7L) · airframe 61,137 hrs · 21,991 cycles

REWORK OF SNRM N00031, REPAIR EVALUATED IAW INCORRECT SRM REPAIR REQUIRES REPLACEMENT PREVIOUSLY INSTALLED EXTERNAL SKIN REPAIR BETWEEN STA 740 TO 760 STRINGERS 6L TO 7L. REWORK ACCOMPLISHED ON EA F-5330-146284. MAJOR REPAIR.

Part: SKIN — DENTED (CARGO DOOR) · airframe 61,137 hrs · 21,991 cycles

FWD CARGO DOOR SKIN AFT UPPER CORNER HAS A DENT. EVALUATED DENT A=.5 Y=.030 A/Y RATIO 16.6. FOUND OUT OF LIMIT IAW SRM 52-30-01 FIG 101 DETAIL VI. CUT OUT DAMAGE IAW SRM 52-30-01 FIG 201 REPAIR 4. FABRICATED REPAIR DOUBLER .071 2024 T3 IAW SRM 52-30-01. LOCATED AND DRILLED IAW SRM 52-30-01 FIG 201 REPAIR 4. INSTALLED DOUBLER IAW SRM 52-30-01 FIG 201 REPAIR 4. CATEGORY "B" REPAIR

Part: STRAP — CORRODED (APU BAY) · airframe 61,137 hrs · 21,991 cycles

AFT APU STRAP STA 1825 BETWEEN S-3R TO S-6R HAS CORROSION REMOVED CORROSION AT AFT APU STRAP STA. 1825 BLENDED AREA L=14" W= 1.0" D=.054 ORIG. MATERIAL .100 AND MAT. REMAINING .046 FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG.101 DET. 4 PAGE 104 REMOVED AND REPLACED STRAP FROM STR. 1-L TO 9-R IAW SRM 51- 40-0. MAJOR REPAIR.

Part: SKIN — MISREPAIRED (BS 324-340) · airframe 61,137 hrs · 21,991 cycles

REMOVED EXISTING REPAIR BS 324-340 STR. 22L TO 23L IAW SRM 51-40-02 AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG.201 REPAIR 15 THIS IS A CLASS "B" REPAIR WITH INSPECTION THRESHOLD OF 29,000 F/C AND REPEAT INSPECTION EVERY 6,000 F/C MAJOR REPAIR.

Part: SKIN — DENTED (BS 377) · airframe 61,137 hrs · 21,991 cycles

FUSELAGE SKIN DENT STA. 377. 3" ABOVE STR. 14-R . EVALUATED 2EA DENTS AT STA 377 S-14R. DENT NR 1 A=1.0 Y=.020 A/Y RATIO 50. DENT NR 2 A=1.25 Y=.025 A/Y RATIO 50. DENTS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO SHEAR TIE IAW SRM 53-00-01 FIG 101 DETAIL III. ACCOMPLISHED EA F-5330-146280. MAJOR REPAIR

Part: CREASE BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

CREASE BEAM WEB AT STA 930 RT SIDE HAS AREA OF CORROSION REMOVED CORROSION ON RT SIDE CREASE BEAM WEB IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13 FIG 101, DETAIL III. ORGINAL MATERIAL .056 AFTER REWORK .047. L=3" X W=3" X D=.009. R & R WEB IAW SRM 53-40-02 AND DRW 144N5140. WEB FABRICATED ON MAE TRAVELER NR T11/872703. CLASSIFED MAJOR REPAIR.

Part: STRAP — CORRODED (ZONE 200) · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN STA 1640, STRAP AT S-12R HAS AREA OF CORROSION ACCOMPLISHED EA F-5310-146269. CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — CORRODED (LT WING SLAT) · airframe 61,137 hrs · 21,991 cycles

LT WING SLAT NR 1, UPPER SKIN T/E HAS SEVERAL CORROSION- SPOTS. REPAIRED NR 1 SLAT IAW SRM 51-70-10.

Part: SKIN — CORRODED (LT WING SLAT) · airframe 61,137 hrs · 21,991 cycles

LT WING SLAT NR 1, UPPER SKIN T/E HAS SEVERAL CORROSION- SPOTS. REPAIRED NR1 SLAT IAW SRM 51-70-10.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 61,137 hrs · 21,991 cycles

REWORK OF SNRM N00016 PREVIOUSLY INSTALLED EXTERNAL DOUBLER REPAIR AT STA 1710- 1718 BETWEEN S-14L TO S-16L REMOVED AND REPLACED REPAIR STA 1710-1718 BETWEEN S-14L TO S-16L IAW SRM 53-00-01 FIG 201 REPAIR 15. CLASSIFIED MAJOR REPAIR

Part: SKIN — CORRODED (NR 1 SLAT) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

LT WING SLAT NR 1, UPPER SKIN T/E HAS SEVERAL CORROSION SPOTS ENTIRE LENGTH. REPAIRED NR 1 SLAT IAW SRM 51-70-10. MAJOR REPAIR .

Part: TEAR STRAP — DAMAGED (ZONE 200) · airframe 61,137 hrs · 21,991 cycles

STA 365, RBL-70 AFT SCUFFPLATE DOME NUT WAS REMOVED AND DAMAGE. THE TEAR STRAP UNDER DOME NUT BY DRILLING APPROX .100 IN TO THE STRAP THE HOLE IS A NR 0.40. COMPLIED WITH EA F-5310-146528 ON MAE N/R 45633750001.

Part: RETAINER — CORRODED (APU DOOR) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

HORZ STAB BOX AREA AT BS 1787 APU DOOR CUT OUT FWD RETAINER WITH CORROSION. REMOVED CORROSIONS AT HORZ STA BOX AREA AT B.S. 1787 APU DOOR CUT OUT FWD RETAINER IAW SRM 51-10-02. BLENDED AREA L=24" W=1.075" D=.060" ORIGINAL MAT .100",REMAINING =.040 FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET II. R & R RETAINER IAW SRM 51-40-02. MAJOR REPAIR.

Part: SUPPORT ANGLE — CORRODED (APU INLET DOOR) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

APU INLET DOOR ATTACH STRUCTURE 1787-1825 S-6R HAS CORROSION. REMOVED CORROSION AT APU INLET DOOR ATTACH STRUCTURE 1787-1825, BLENDED AREA L=2.025" W=1.075" D=.063" ORIG MAT =.063 REMAINING =0, FOUND OUT OF LIMITS IAW NO SRM FOR ALLOWABLE DAMAGE. R & R ANGLE SUPPORT IAW SRM 51-40-02. MAJOR REPAIR.

Part: SUPPORT ANGLE — CORRODED (APU INLET DOOR) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

APU INLET DOOR ATTACH STRUCTURE 1787-1825 S-3R HAS CORROSION. REMOVED CORROSION AT APU INLET DOOR ATTACH STRUCTURE 1787-1825 S-3R,IAW SRM 51-10-02. BLENDED AREA L=3" W=1"D=.063" ORIGINAL MAT .063" REMAINING =0. NO SRM FOR ALLOWABLE DAMAGE. R & R ANGLE SUPPORT IAW SRM 51-40-02 . MAJOR REPAIR

Part: WEB — CORRODED (BS 1102) · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN FLOOR STR. STA .1102 RBL 65 FLOOR WEB HAS AREA OF CORROSION. REMOVED CORROSION MAIN CABIN FLOOR STA 1102 RBL 65 IAW SRM 51-10-02 BLENDED AREA L=2.35" W= 1.10" D= .010 MAT ORIGINAL .063 MAT REMAINING .053 FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13 FIG 101 DET 3 REMOVED AND REPLACED WEB STA 1102 RBL 65 IAW SRM 51- 40-02

Part: SKIN — MISREPAIRED (BS 1360 S21-22L) · airframe 61,137 hrs · 21,991 cycles

FLUSH REPAIR LOCATED AT BS 1360 BETWEEN S 21L AND 22L DOES NOT MEET SRM REQUIRMENTS. REMOVED REPAIR IAW SRM 51-40-02. COMPLIED IAW EA F-5330-146277, MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,137 hrs · 21,991 cycles

CORROSION ON FUSELAGE SKIN UNDER THE ATC ANTENNA.

Part: SKIN — CORRODED (FUSLEAGE) · airframe 61,137 hrs · 21,991 cycles

CORROSION ON FUSELAGE SKIN UNDER THE LT DME ANTENNA.

Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

FLOOR PANEL BETWEEN STA 1681 TO 1720 HAS VARIOUS AREAS OF CORROSION ON SKIN FROM RBL 62 - LBL 62. REMOVED CORROSION AT FLOOR PANEL BETWEEN STA 1681-1720 RBL 62-LBL62 IAW SRM 51-10-02. BLENDED 3EA AREAS OUT OF LIMITS IAW SRM 53-60-51, FIG 201, REPAIR 2. ORIGINAL MATERIAL .071 AFTER REWORK .050. REPAIRED FLOOR PANEL IAW SRM 53-60-51, FIG 201. REPAIR 2 ALTE NR1.

Part: SKIN — DAMAGED (NR 10 SLAT) · airframe 61,137 hrs · 21,991 cycles

RT WING NR10 SLAT, OTBD TO INBD SPOT DELAMINATED FROM INWARD SKIN OUTWARD AND REST OF SKIN HAS NUMEROUS AREAS OF HAIL DAMAGE. REPAIRED NR 10 SLAT DELAMINATION IAW SRM 51-70-10, HAIL DAMAGE REPAIRED IAW SRM 51-70-01. DAMAGE IS LOCATED APPROX 12" FROM O/B EDGE AND 8" FWD OF T/E. FINAL REPAIR DIMENSIONS ARE 3.5"W X 2.5"L PER EA F-5740-146260. CATEGORY "A" MAJOR REPAIR

Part: SKIN — CORRODED (NR 5 SLAT) · airframe 61,137 hrs · 21,991 cycles

NR 5 SLAT LOWER SKIN T/E INTERNAL L-CHANNEL SEVERAL AREAS THE ENTIRE LENGTH HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=1.0",W=2.0',D=.015. ORIGINAL MAT .080 MATERIAL REMAINING .065. FOUND OUT OF LIMITS IAW SRM 57-43-02 FIG 101 DET II. REMOVED AND REPLACED FLEX SKIN, ANGLE, AND SPLICE IAW E A F- 5750-146383 STEP 1 THRU 5. MAJOR REPAIR.

Part: SKIN — CRACKED (NR 10 SLAT) · airframe 61,137 hrs · 21,991 cycles

NR 10 SLAT LOWER INBD SKIN CRACKED AROUND FASTENERS. ACCOMPLISHED EA F-5750-146379. WING -NR10 L/E SLAT NOSE SKIN CRACKS. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1681.8) · airframe 61,137 hrs · 21,991 cycles

AFTER REMOVAL OF FLOOR CLIPS, FOUND CORRISION ON BOTTOM FWD SIDE OF FLOORBEAM STA 1681.8, RBL 5 AND LBL 12, WL 208.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN STA 324, RBL 29 TO RBL 60, WL 208 FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 CHECKED LIMITS OF BLENDED AREA L= 3.0" W=2.0" D=.016 STA 324 RBL 28-31 ,L=3.0" W=2.0" D=.020, STA 324 RBL 41-44 ORIG MAT. .125" REMAINING MAT, .109 AT RBL 28-31 AND .105 AT RBL 41-44 OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DET ,III R & R UPPER CHORD STA 324, RBL 60 -LBL 60 IAW SRM 53-0051, FIG 101, DET III. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

CORROSION ON FLOORBEAM REPAIR STA.1640 RBL19 AND RBL20 WL208 MAIN CABIN. REMOVED AND REPLACED FLOORBEAM BS 1640 LBL 63 TO RBL 63 IAW SRM 51-40-02 MAJOR REPAIR.

Part: FRAME — CRACKED (BS 1520) · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN FRAME AT STA 1520 BETWEEN S-2L TO S-2R HAS MOUNT HOLES OUT OF ROUND. FRAME CRACKED IAW SRM 53-00-07 FIG 101 STEP A ALLOWABLE DAMAGE 2. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 REPAIR NR 3. MAJOR REPAIR.

Part: FRAME — DAMAGED (BS 1600) · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN FRAME AT STA 1600 BETWEEN S-2L TO S-2R HAS ELONGATED MOUNT HOLES. AFTER EVALUATION FOUND RIVETS HOLES CRACKED AT STA 1600 BETWEEN S-2L TO S-2R IAW SRM 53-00-07, FIG 101. ALLOWABLE DAMAGE 2 SF. REPAIRED SECTION FRAME IAW SRM 53-00-07, FIG 201, REPAIR 3 SF. CATEGORY "B" MAJOR REPAIR. SUPPLEMENTAL INSP DUE AT 10,000 FC, AFTER REPAIR INSTALLED, THEN EVERY 12,000 FC USING HFEC METHOD.

Part: SEAT TRACK — CHAFED (BS 680-780) · airframe 61,137 hrs · 21,991 cycles

SEAT TRACK HAS CHAFE MARKS INSIDE CROWN SURFACE FROM BS680 TO 780, LBL45. REMOVED CAHFFED MARKS NSIDE CROWN AT SEAT TRACK BS 680-780 LBL-45 SRM 51-10-02 ORIGINAL MAT.230 AFTER REWORK .200 AMOUNT OF MAT REMOVED FOUND TO BE OUT OF LIMITS SRM 53-00-52 FIG 101 DET I THRU IV. FABRICATED NEW SEAT TRACK FROM BAC1520-792. BATCH 1904663 PER DRAWING 143N5090. TREATED AND PRIMED IAW SRM 51-20-01 PART MARKED PER GMM 7-0-1001 INSTALLED SEAT TRACK IAW SRM 51-40-01 MAJOR REPAIR

Part: CREASE BEAM — CORRODED (BS 755) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

INBD CREASE BEAM CORRODED AT BS 755, RBL 62. REMOVED CORROSION AT I/B CREASE BEAM IAW SRM 51-10-02 ORIG. MAT. .071 AFTER REWORK .061 FOUND OUT OF LIMITS IAW SRM 53-30-13 FIG. 101 DET. VIII FABRICATED NEW PER SRM 51-30-01 AND DWG 143N5529 WITH MAT. BAC1515-553/24 BATCH 1896249 AND INSTALLED IAW SRM 51-40-02 THIS IS 'A' MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN, STA 365, RBL 2- 60, WL 208, FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .125 MATERIAL REMOVED .017. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL VI. FABRICATED T- CHORD MATERIAL BAC1505-100800 7075-T6 BATCH NR 1964356 IAW SRM 53-00-51, FIG 201, REPAIR 3. FABRICATED 2 & 3 ANGLES ON TRAVLER NR T11/866147, FABRICATED 4 & 5 STRAPS ON TRAVLER, T11/866148. INSTALLED T- CHORD & REPAIR ANGLES & STRAPS AT STA 365, RBL 70- LBL 14, IAW SRM 53-00-51, FIG 201, REPAIR 3, THIS IS A CATEGORY A . MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 395) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN STA 395, RBL 11, WL 208, FLOORBEAM TOP STRAP (PLATE) HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIGNAL MAT THICKNESS .125 AFTER REWORK .108 MAT LOSS .017 AREA OF DAMAGE L(1") X W(1") OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. REMOVED UPPER TEE RBL 09- RBL 70 IAW SRM 51-10-02. FABRICATED REPAIR PARTS FROM BAC 1505-100880 IAW SRM 53-00-51, FIG 201, TABLE I. REPAIR STRAPS FABRICATED ON TRAVELER T11/866150, REPAIR ANGLES FABRICATED ON MAE TRAVELER T11/866149. REPAIR PARTS, ANGLES, AND STRAPS INSTALLED AT STA 395, RBL 09- RBL 70, IAW SRM 51-40-02. CATEGORY A REPAIR. MAJOR REPAIR.

Part: SKIN — UNKNOWN (BS 1352) · airframe 61,137 hrs · 21,991 cycles

PREVIOUS BLEND OUT AT STA 1352, BETWEEN STR 29R TO 30 ON FUSELAGE SKIN.

Part: CREASE BEAM — CORRODED (BS 660-760) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

LT INBD CREASEBEAM HAS CORROSION BS 660 TO 760. REMOVED CORROSION ON CREASE BEAM IAW SRM 51-10-02 ORIG. MAT. 0.080 AFTER REWORK 0.054 FOUND TO OUT OF LIMITS IAW SRM 53-30-15 FIG. 101 DET. IV. REMOVED AND REPALCED CREASE BEAM IAW SRM 51-40-02 THIS IS" A " MAJOR REPAIR WITH NO FOLLOW UP INSPECTIONS.

Part: SKIN — DAMAGED (BS 1377 S25L) · airframe 61,137 hrs · 21,991 cycles

PREVIOUS BLEND OUT AT STA 1377.5 2.3" ABOVE STR 25L ON FUSELAGE SKIN. FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET. II. REPAIRED IAW SRM 53-00-01. REPAIR NR 16, THIS IS CAT "B" REPAIR FROM TIME OF REPAIR 16,000 F/C WITH REPEAT INSPECTIONS AT EVERY 6,000 F/C. THIS IS MAJOR REPAIR.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

STRINGER 22-R INSIDE FWD CARGO COMPARTMENT BS 740-760 HAS CORROSION. REMOVED CORROSION ON S-22R STA 740-760 IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.0 D=.020. ORIGINAL MATERIAL .071 AFTER REWORK .051. NO ALLOWABLE DAMAGE FOR SF STRINGERS. REPAIRED STRINGER IAW SRM 53-00-03, FIG 201, REPAIR 2. CATEGORY "A" MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN, STA 418-440, RBL 45,WL 208, SEAT TRACK IS GOUGED. REMOVED GOUGE ON SEAT TRACK STA 418-440 RBL 45 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL V. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN,STA 377, RBL 11, WL 208, FLOORBEAM TOP STRAP (PLATE) HAS CORROSION. REMOVED CORROSION ON PREVIOUSLY INSTALLED FLOORBEAM REPAIR AT STA 377, RBL 11 IAW SRM 53-0051, REPAIR 3 FOUND TO BE OUT OF LIMITS ARIG MAT 0.125 AFTER REWORK 0.101. REMOVED FLOORBEAM REPAIR AND FAB. NEW REPAIR PARTS IAW SRM 53-00-51 REPAIR 3 AND INSTALLED NEW REPAIR AT STA 377, RBL-4-RBL-16 IAW SRM 53-00-51. REPAIR 3 THIS A MAJOR 'A' REPAIR NO FOLLOW UP INSP REQUIRED.

Part: SEAT TRACK — GOUGED (BS 418-440) · airframe 61,137 hrs · 21,991 cycles

MAIN CABIN, STA 418-440, RBL 25, WL 208, SEAT TRACK IS GOUGED. REMOVED GOUGE FROM SEAT TRACK STA 418-440 RBL 25 AND FOUND TO OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL V. R & R SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

FLOORBEAM, STA 1661, BL 0, WL 208 CORRODED MAIN CABIN. REMOVED CORROSION ON FLOORBEAM, STA 1661, BL 0 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. ORIG MATERIAL .125 MATERIAL LOSS .035. R & R STA 1661 FLOORBEAM IAW SRM 51-40-02. CATEGORY "A" MAJOR REPAIR

Part: CHANNEL — CORRODED (BS 263) · airframe 61,137 hrs · 21,991 cycles

NLG WHEELWELL FWD BOTTOM "L" CHANNEL AT STA 263 JUST BELOW NLG DOOR UNSAFE LIGHT IS CORRODED. COMPLIED WITH EA F-5310-146250. MAJOR REPAIR.

Part: ANGLE — CORRODED (NR 10 SLAT) · airframe 61,137 hrs · 21,991 cycles

NR 10 SLAT COVE ANGLE CORRODED. REMOVED CORROSION ON NR 10 SLAT IAW SRM 51-10-02. ORIG MATERIAL .063 AFTER REWORK .000 MATERIAL LOSS .063 FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101, DETAIL II. L= 131" X W=2" X D=.063. R & R COVE ANGLE IAW SRM 51-40-02. CLASSIFIED MAJOR REPAIR.

Part: SKIN — CORRODED (NR 3 SLAT) · corrosion level 2 · airframe 61,137 hrs · 21,991 cycles

NR 3 SLAT LOWER SURFACE AT SEAM BETWEEN SLAT AND AERODYNAMIC SEAL HAS CORROSION. REMOVED CORROSION ON NR 3 SLAT LOWER SURFACE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG 101, DETAIL II. L-139" X 1" X D=.063 ORIG MATERIAL .063 AFTER REWORK .000. ACCOMPLISHED EA F-5750-146377. CLASSIFED AS MAJOR REPAIR.