N288FE

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 42,318 hrs · 28,654 cycles

INDIVIDUAL EXPULTED THE EVACUATION SLIDE. R & R L1 DOOR ESCAPE SLIDE IAW MM 25-60-015-2.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 42,275 hrs · 28,622 cycles

FOUND EMERGENCY LIGHTS ARMED AND ACFT POWER OFF. BOTH COCKPIT AND ENTRY EMERGENCY LIGHTS, AND EXTERIOR DOOR SLIDE LIGHT INOPERATIVE. REPLACED BATTERIES IAW MM 33-50-001-0. REPLACED EXTERIOR DOOR SLIDE POWER SUPPLY IAW 33-50-051-2. ALL LIGHTS OPS CHECKED NORMAL. OK FOR SERVICE.

Part: SLIDE — DISLODGED · airframe 42,114 hrs · 28,471 cycles

ESCAPE SLIDE FELL OUT OF CONTAINER. REINSTALLED DOOR MOUNTED ESCAPE SLIDE IAW AMM 25-60-015-2. ACFT OK FOR SERVICE.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 41,905 hrs · 28,268 cycles

FWD ENTRY DOOR UPPER HINGE MISREPAIRED. FABRICATED DOUBLER, TRIPLER, AND STRUCTURAL FILLER, AND INSTALLED IAW EA 7-5330-152453.

Part: WEB — CRACKED (CARGO DOOR) · airframe 41,905 hrs · 28,268 cycles

CARGO DOOR INNER WEB IS CRACKED AT LIGHTING HOLE NEAR LEADING EDGE. CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV103. FABRICATED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3 AND 52-30-1 FIG 7. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND EA 7-5230-152450.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 41,905 hrs · 28,268 cycles

LEFT WING OTBD FLAP INBD FAIRING AREA HAS A GOUGE ON L/E SKIN. CUT OUT DAMAGED AREA IAW SRM 51-10-1 AND 57-10-4 FIG 2. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1 AND EA 7-5750-152449.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 41,905 hrs · 28,268 cycles

RIGHT WING I/B FOREFLAP O/B L/E GOUGED. FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-4 FIG 1 REV 103

Part: SHEAR TIE — CORRODED (BS 950E S28-29R) · corrosion level 2 · airframe 41,905 hrs · 28,268 cycles

CORROSION ON SHEAR TIE AT BS 950E BETWEEN STRINGERS 29R AND 28R. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 51-20-1 FIG 7 AND DWG 65-56129 INSTALLED NEW SHEAR TIE IAW SRM 51-30-2 REV 103.

Part: SHEAR TIE — DAMAGED (BS 950A S28-29R) · airframe 41,905 hrs · 28,268 cycles

IMPROPER SPACING BETWEEN FASTENERS IN SHEAR TIE AT BS 950A, FORWARD AND AFT, BETWEEN STR 29R AND 28R. REMOVED SHEAR TIE IAW SRM 51-30-2 LOCATED,DRILLED AND DEBURRED NEW SHEAR TIE IAW SRM 51-30-5 INSTALLED SHEAR TIE IAW SRM 51-30-2

Part: SKIN — MISREPAIRED (BS 460 S24-26L) · airframe 41,905 hrs · 28,268 cycles

SKIN MISREPAIRED AT BS 460, STR 24 TO 26L. CUT OUT DAMAGED SKIN, DOUBLER, AND TRIPLER. FABRICATED STRUCTURAL FILLER, DOUBLER, TRIPLER, AND FILLERS. INSTALLED REPAIR PARTS IAW SRM 53-30-3, FIG 1B.

Part: SKIN — GOUGED (BS 720C S28L) · airframe 41,905 hrs · 28,268 cycles

SKIN BS 720C, STR 28L IS GOUGED. REPAIRED.

Part: SKIN — GOUGED (BS 720C S28L) · airframe 41,905 hrs · 28,268 cycles

BS 720 BELOW S28L SKIN IS GOUGED ABOVE LT RAM AIR DUCT. CUT OUT GOUGED AREA OF SKIN IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 REV 103.

Part: VERTICAL BEAM — DAMAGED (BS 1183) · airframe 41,905 hrs · 28,268 cycles

1183 BULKHEAD HAS INSUFFICIENT FASTENER SPACING ON VERTICAL BEAM, LBL 17.8. TRIMMED DAMAGED AREA AT STA 1183 BULKHEAD 3EA AND AFT FLANGE VERTICAL BEAM LBL 17.8, FABRICATED DOUBLER REPAIR, FILLERS, TEE SECTION, SPLICE REPAIRS AND INSTALLED DOUBLER REPAIR, FILLERS, T SECTION, AND SPLICE REPAIRS IAW EA 7-5310-152441.

Part: SKIN — DAMAGED (BS 464 S26L) · airframe 41,905 hrs · 28,268 cycles

SKIN, BS 464 ABOVE STR 26L HAS A DRILL START. ACCOMPLISHED REPAIR ON NR N00405.

Part: SWITCH — FAILED (LE FLAPS) · airframe 41,630 hrs · 28,040 cycles

AFTER TAKEOFF LEADING EDGE FLAPS FAILED TO INDICATE RETRACTED. FE PANEL SHOWED NR 2 LED NOT RETRACTED. FOUND SWITCH S203 FROZEN AND VERY HARD TO MOVE. REPLACE SWITCH 203 REF WDM27-81-02 AND MM 27-82-001-4. OPS CHECK NORMAL ACFT OK FOR SERVICE.

Part: LIGHT — FAILED (CABIN) · airframe 41,290 hrs · 27,764 cycles

DURING MAINT PRE-DEPARTURE CHECKS OF EMERGENCY EXIT LIGHTING, NOTED THAT EXIT LIGHT OVER L1 DOOR IS DIM AND FLICKERING. REMOVED COVER AND SWITCHED LIGHT "ON" IT IS BRIGHT & STEADY. REMOVED LIGHT AND AGAIN, BRIGHT AND STEADY ON BATTERY PACK. WHEN INSTALLED IN THE ACFT THE LIGHTS REVERT TO DIM AND FLICKERING. RESET LIGHT BY SWITCHING FROM "ARM" TO "ON" AND BACK TO "ARM" AGAIN NO HELP. R & R EXIT LIGHT IAW MM 33-50-001-2. OP CHECK NORMAL. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. AWAITING TDR RESULTS.

Part: GYRO — FAILED (NR 1) · airframe 41,264 hrs · 27,739 cycles

DURING FLT, HSI SHOWS HDG FLAG RAN QRH HSI WORKS WHEN SWITCHED TO BOTH ON 2. DIVERTED TO ALTERNATE STA R & R NR 1 DG IAW M/M 34-21-071-4-0. OPS CHECK NORMAL, OK FOR SVC. ACFT IS NOT CAT II IAW GMM 6-5-400, CAT II CHECK.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,557 hrs · 27,130 cycles

MAIN CARGO DECK FLOORBEAM UPPER "T " BS 1130 HAS CORROSION BETWEEN LBL25 AND LBL46. CUTOUT CORRODED SECTION IAW SRM 53-10-8 FIG 10 (SHEET 9). HFEC INSPECTED IAW NTM 51-00-19 PT.6, NO CRACK INDICATION NOTED. FABRICATED FILLER FROM 7075-T6 .156. FABRICATED DOUBLER ON MAE TRAVELER NR T9/784510 TREATED AND PRIMED IAW SRM 51-20-2. INSTALLED BOUBLER AND FILLER IAW SRM 51-30-2. CLASSIFIED MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,557 hrs · 27,130 cycles

MAIN CARGO DECK FLOORBEAM AT STA 720A HAS CORROSION AND SCRIBE MARKS ON UPPER " T " SECTION BETWEEN LBL25 AND RBL25. REMOVED DAMAGED AND CORRODED SECTION IAW SRM 53-10-8 FIG 3, FABRICATED REPAIR PARTS ON TRAVELERS T9/783984,T9/783989,T9/784001,T9/783983,AND T9/783990. LOCATED AND DRILLED PARTS IAW SRM 51-20-1. TREATED AND PRIMED REPAIR PARTS 5 (EA) IAW SRM 51-10-2. INSTALLED REPAIR PARTS 5 (EA) IAW SRM 53-10-8, FIG 3.

Part: FRAME — CRACKED (ZONE 200) · airframe 40,557 hrs · 27,130 cycles

FUSELAGE FRAME STA 890 OUTER CHORD CRACKED AT STRINGER 14R. REMOVED DAMAGE IAW SRM 51-30-2. FABRICATED NEW ANGLE AND NEW DOUBLER IAW SRM 53- 10-2 AND TRAVELERS NR T9/783599 ANDT9/783600, LOCATED AND DRILLED ANGLE AND ANGLE DOUBLER IAW SRM 51-30-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,557 hrs · 27,130 cycles

SEAT TRACK LBL 25 CORRODED ON NUMEROUS LOCATIONS FROM STA 500-690. REMOVED SEAT TRACK IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM 60-6549/24 BATCH NR 1514987 LOCATED AND DRILLED IAW SRM 51-30-2. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2 AND 53-10-5.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,557 hrs · 27,130 cycles

MAIN CARGO DECK FLOORBEAM UPPER TEE BS 1130 HAS CORROSION BETWEEN LBL 0 AND LBL 13. REMOVED CORROSION ON FLOORBEAM UPPER TEE BS 1130 BETWEEN LBL 0 AND LBL 13 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-8 FABBED 3 (EA) FILLERS AND NEW ANGLE P/N BAC 1505/100393 IAW SRM 53-10-8. NDT CHECKED NO CRACKS FOUND IAW NTM 51-00-19 PG-6. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2, AND INSTALLED IAW SRM 53-10-8 AND SRM 51-30-2. CLASSIFIED AS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1030) · airframe 40,557 hrs · 27,130 cycles

MAIN CARGO DECK FLOORBEAM UPPER 'T' BS 1030 HAS CORROSION BETWEEN LBL 0 AND LBL 25 FABRICATED ANGLES REPAIRS FOR FLOORBEAM UPPER 'T' ON MAE TRAVELER T9/783860 IAW WITH SRM 53-10-8, FABRICATED 2 FILLERS BATCH NR 000104977, TREATED AND PRIMED ANGLES REPAIRS, FILLERS IAW SRM 51-10-2 AND INSTALLED IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,557 hrs · 27,130 cycles

LAVATORY AREA FLOORBEAM AT STA 328 HAS CORROSION AT APPROX RBL 36 ON THE UPPER CHORD FWD EDGE (MARKED) REMOVED CORROSION 0.080 ORIGINAL 0.025 MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. CUT OUT DAMAGE AND FABRICATED REPAIR ON TRAVELER T9/783258 IAW SRM 53-10-8. INSTALLED REPAIR IAW SRM 53-10-8 AND 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,557 hrs · 27,130 cycles

SEAT TRACK LBL 45 CORRODED ON NUMEROUS LOCATIONS FROM STA 500 - 690. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION FROM STA 500 - 690 LBL 45 IAW SRM 51305, FABRICATED FROM PN 60-6549/24 BATCH NR 1514987.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 40,557 hrs · 27,130 cycles

AFT CARGO LT SIDE OF 1183 BULKHEAD FWD FACE DOME NUT AT LBL 27 HAS CORROSION ON IT AND ON SKIN 6 O'CLOCK POS UNDER AIR DUCT (INNER MOST). REMOVED CORROSION IAW SRM 51-10-6 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 1 SH2 NOTE C. FABRICATED REPAIR DOUBLER IAW SB 727-53-0171 FIG 3. INSTALLED DOUBLER IAW DAW SB 727-53-0171 FIG 3 AND SRM 51-30-2.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,557 hrs · 27,130 cycles

SEAT TRACK LBL 0 CORRODED ON NUMEROUS LOCATIONS FROM STA 500 - 575. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 BS 500 TO 580, REINSTALLED 4 STRAPS IAW SRM 51-30-2, FABRICATED SEAT TRACK SECTION ON MAE TRAV NR T9/ 82953, BATCH NR 0001541987, LOCATED AND DRILLED SEAT TRACK SECTION IAW SRM 51-30-2.

Part: SKIN — CANNING (ZONE 100) · airframe 40,557 hrs · 27,130 cycles

AFT CARGO BILGE SKIN OIL CANNING BETWEEN STA 1100 AND 1130, HAS WORKING RIVETS AT STR 27L, STR 28L, AND STR 29L. CUT-OUT DAMAGED AREA IAW SRM 53-30-3 FIG 3, FABBED FILLERS IAW SRM 53-30-3. FABBED DOUBLER IAW SRM 53-30-3 LOCATED AND DRILLED IAW SRM 51-30-5 AND SRM. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2 AND 53-30-3. REMOVED AND REPLACED WORKING FASTENERS IAW SRM 51-30-2. CLASSIFIED AS A MAJOR REPAIR.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 40,557 hrs · 27,130 cycles

NOSE LANDING GEAR BULKHEAD STA NR 351.20 HAS 3 CRACKS MIGRATING FROM 1 FASTENER HOLE ATTACHING THE NOSE GEAR LOCK ACTUATOR FITTING TO BULKHEAD. IN CORRECT TAIL NUMBER ENTERED IN BLOCK 1C, PLEASE SEE SDR 09-0763 FOR AIRCRAFT N482FE.

Part: HEATER — INOPERATIVE (WINDOW) · airframe 40,301 hrs · 26,952 cycles

L1 WINDOW HEAT FAILED EN ROUTE. TURNED OFF AND BACK ON SEVERAL TIMES BUT WINDOW HEAT CONTINUED TO FAIL. CHECKED/RESET BOTH L1 AC AND DC CONTROL PER MOCC. NO HELP. WINDOW VERY COLD. RELEASED FOR SERVICE PER MEL/CDL: 30-15-A CATEGORY: C EXPIRATION: 07NOV08 "MEL 30-15-A: L1 WINDOW HEAT, INOP. ACFT RESTRICTED FROM OPERATING INTO ICING CONDITIONS. DO NOT EXCEED 250 KIAS BELOW 10,000 MSL."

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 40,301 hrs · 26,952 cycles

L1 WINDOW HEAT FAILED EN ROUTE. TURNED OFF AND BACK ON SEVERAL TIMES BUT WINDOW HEAT CONTINUED TO FAIL. CHECKED/RESET BOTH L1 AC AND DC CONTROL PER MOCC. NO HELP. WINDOW VERY COLD. ACN RELEASED FOR SERVICE PER MEL/CDL: 30-15-A CATEGORY: C. REPLACED BROKEN C/B C665. AFTER LAST ENTRY, FOUND CONTROL UNIT SERIAL NUMBERS FOR POS L1 AND L2 DID NOT MATCH MAXI. CONFIRMED BAD CONTROL UNIT TO HAVE MSN 7002. REMOVED AND REPLACED L1 CONTROL UNIT AND INSTALLED CONTROL UNIT WITH MSN 8892 IN L2 POSITION TO MATCH MAXI REF MM 30-41-033-4, WDM 30-41-11 AND SMP CH 20. OP CKS ARE GOOD AT THIS TIME.

Part: SWITCH — MISINSTALLED (AIRSTAIR DOOR) · airframe 38,242 hrs · 25,304 cycles

AFT AIRSTAIR AMBER LT ILLUMINATED PRIOR TO BLOCKOUT- ADJUSTED BY MAINTENANCE WHEN AFT AIRSTAIR AMBER LT ILLUMINATED IN FLIGHT- RAN QRH RED TABS. ENT BY: 353958 MEL 08DEC05 10:15 IND ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CAT: C EXP: 16DEC05 C/0257532. FOUND S395 SW INSTALLED INCORRECTLY. INSTALLED CORRECTLY. ALSO FOUND WRONG SW ACT INSTALLED. INSTALLED PROPER ASSY.

Part: SWITCH — MALFUNCTIONED (AIRSTAIR DOOR) · airframe 38,224 hrs · 25,291 cycles

AMBER AFT AIRSTAIR LIGHT ILLUMINATED DURING CLIMB THROUGH 27,000 MSL. ACCOMPLISHED QRH. LANDED UNEVENTFULLY. OPENED AFT AIRSTAIRS, CLEANED SWITCHES, AND CHECKED DOOR WARNING SYSTEM PER M/M 52-70-001-5. OPS CHECKS NORMAL. OK FOR SERVICE.

Part: UPLOCK SWITCH — MALFUNCTIONED (AIR STAIR) · airframe 38,109 hrs · 25,209 cycles

AMBER AIRSTAIR LIGHT ON S/O PANEL CAME ON IN FLIGHT. CHECKED A/C ON ARRIVAL, FOUND DOOR UP AND LOCKED. RAN DOOR SEVERAL TIMES. LIGHT STAYED ON ON FIRST TRY. ADJUSTED UPLOCK SWITCH ON LEFT AND RIGHT SIDE UPLOCK SWITCHES, PER AMM 52-62-001-5. OPS CHECK NORMAL. RII:193167

Part: LINE — CRACKED (FUEL HEAT) · airframe 38,086 hrs · 25,189 cycles

AT 800' AGL AND 180 KIAS NR 2 FIRE LIGHT ILLUMINATED PERFORMED PHASE 1 AND CHECKLIST LANDED UNEVENTFULLY.

Part: SKIN — GOUGED (FUSELAGE) · airframe 36,556 hrs · 24,016 cycles

FUSELAGE EXTERNAL SKIN HAS GOUGES AT BS 1149 BETWEEN STRINGER 6 & 7 LT. SKIN AT BS 1149 BETWEEN STR 6 & 7 LT WAS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED SKIN PER FED EX EA 7-5330-55232.

Part: SKIN — GOUGED (FUSELAGE) · airframe 36,556 hrs · 24,016 cycles

FUSELAGE EXTERNAL SKIN IS GOUGED AT BS 1143 JUST 3 INCHES ABOVE STRINGER 12 LT.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION, STA 760 BL 0 WL 148, DELTA BEAM LWR L-ANGLE HAS CORROSION. ACCESSED DELTA BEAM WEB. REMOVED L-ANGLE AND FOUND L-ANGLE OUT OF LIMITS. FABRICATED NEW L-ANGLE, INSTALLED ANGLE AND REINSTALLED ACCESSED DELTA BEAM WEB FASTENERS AND DME NR 2 ANTENNA CLIPS. ALL WORK DONE IAW SRM 51-30-2, 51-10-2, 51-20-1.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON STR 24L BS 306. REMOVED DAMAGE ON STR 24L BS 306. DAMAGE FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-2, 53-10-3.

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 36,556 hrs · 24,016 cycles

VERTICAL STAB LT STRINGER CRACKED, FIN STA 157.2 STR NR 7 FROM TOP, AT BOLT HOLE. REPAIRED CRACKED STRINGER NR 7L FIN STA 157.2 PER SRM 55-30-4 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON FLOORBEAM AT FLOOR PANEL FASTENER HOLES BS 400 LBL 10 - RBL 10. REMOVED CORROSION IN A 1.0 X2.0 X .038 AREA. ORIG THICKNESS IS .125, TOP CHORD IS OUT OF LIMITS PER SRM 53-10-1. CUT-OUT DAMAGED UPPER CHORD PER SRM 53-10-8. FABRICATED CHORD FROM BAC1505-100617 M536763, ANGLE FROM BAC1490-2785, M 526583 AND BAC1490-2831 M537615 AND STRAP FROM BAC1512-3396 M531513 AND BAC1512-3353 PER SRM 53-10-8. LOCATED, DRILLED, ALODINED, PRIMED, PAINTED, AND INSTALLED ALL PARTS PER SRM 53-10-8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON FLOORBEAM BS 360 LBL 17 - RBL 7 WL 208. FOUND CORROSION ON FLOORBEAM BS 360, LBL 17 TO RBL 17 WL 208 TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8 FIG 8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON FLOORBEAM AT FASTENER HOLES BS 344 LBL 59 - RBL 17 WL 208. REMOVED CORROSION AREAS 77 X 2 X .040 INCHES FROM ORIGINAL .100. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPALCED UPPER CHORD OF FLOORBEAM BS 344 LBL 65 TO RBL 65 PER SRM 51-30-02 AND FED-EX SR 27-53-007

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION IN FWD CARGO BAY, CORROSION ON INNER SURFACE OF SKIN STA 684 BETWEEN STR 27 LT AND 28 LT. FOUND CORROSION ON SKIN AT BS 684, STR 27L AND 28L TO BE .015 DEEP X 4 X 6 INCHES FROM AN ORIGINAL THICKNESS OF .050 AND IS OUT OF LIMITS IAW SRM 53-30-3. CUT OUT DAMAGE AREA FO SKIN AND FABRICATED DOUBLER AND FILLER FROM 2024T-3 .063 LOT 519699 AND 2024T-3 .050. LOT 532706 AND INSTALLED IAW SRM 53-30-3 FIG 3A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON FLOORBEAM BS 380 LBL 8-55 WL 208. BLENDED CORROSION ON BS 380 FLOORBEAM PER SRM 51-10-1. FOUND LBL 8 OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGED AREA PER SRM 53-10-8. FABRICATED REPAIR PARTS PER SRM 53-10-8. APPLIED ALODINE AND PRIMER TO CUT OUT AND REPAIR PARTS PER FED EX MM 51-20-021-7 & 51-20-151-7. INSTALLED REPAIR PER SRM 53-10-8. INSTALLED STIFFENER AT LBL 14 PER SRM 51-30-2. APPLIED ALODINE & PRIMER. IN LIMITS. BLEND AREA PER FED EX MM 51-20-021-7 & 51-20-151-7.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,556 hrs · 24,016 cycles

RT EXTERIOR FUSELAGE SKIN HAS CREASE AT BS 1143 STR 18R TO 3 INCHES BELOW STR 19R. DAMAGE ON EXTERNAL SKIN BS 1143 STR 18R TO 3" BELOW STR 19R A/Y RATION=76 AREA FOUND TO BE WITHIN LIMITS PER SRM 53-30-1 FIG 1 EXCEPT AT STR 19R. FOUND TO BE OUT OF LIMITS PER SRM 53-30-1 FIG 1. CUT OUT DAMAGE AT BS 1145 STR 19R IN A 1.1 X 1.3 AREA. FABRICATED REPAIR DOUBLER FROM 2024T3 X 0.063 INCH 523505 AND INSTALLED REPAIR AT BS 1143 STR 19R PER SRM 53-30-3 FIG 3.

Part: FRAME — DENTED (FUSELAGE) · airframe 36,556 hrs · 24,016 cycles

FWD CARGO BAY, FRAME DENTED STA 660 STR 24 LT. CUT OUT DENTED MATERIAL FROM FRAME AT BS 660, STR 24L AND PER SRM 51-40-3, 53-10-1, USING 7075-T6, .050 LOT #466242. CUT OUT WAS 1X1

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON FLOOR BEAM AT FLOOR PANEL FASTENER HOLE BS 440, LBL 7.75 - 10.75 (100 PERCENT MATERIAL LOSS). REMOVED DAMAGE AREA OF TOP FLANGE OF FLOORBEAM AT BS 440. FABRICATED, ALODINE, PRIMED, PAINTED AND INSTALLED REPAIR IAW SRM 53-10-8.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON FLOORBEAM AT FASTENER HOLES BS 312 LBL 20 WL 208. REPAIR CORROSION ON FLOORBEAM AT FASTENER HOLES BS 312 LBL 20 WL 208 PER SRM 53-10-8

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

LEFT A/C BAY, DELTA BEAM LWR PLATE HAS CORROSION AT STA 800 LBL 6 WL 140. REMOVED CORROSION ON DELTA BEAM LWR PLATE AT BS 800, LBL 6, WL 140 IN A 2.500X1.00X.029 DEEP. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA 2.00X.500X.090. FABRICATED FILLER AND PLATE FROM 7075-T6 .090 THICK. ALODINED, PRIMERED, INSTALLED AND PAINTED IAW SRM 51-40-2, SRM 53-10-1, SRM 51-30-2, SRM 51-10-3 AND FED EX MM.

Part: FRAME — DENTED (FUSELAGE) · airframe 36,556 hrs · 24,016 cycles

FWD CARGO BAY, FRAME DENTED STA 700 STR 23L. REMOVED DENTED MATERIAL FROM FWD CARGO BAY, FRAME AT BS 700, STR 23L, 24L AND REPAIRED PER SRM 51-40-3 USING 7075-T6 .050 LOT 466242, CUT OUT WAS 1X1 INCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON FLOORBEAM BS 1110, RBL 22, WL 208. CUT OUT CORRODED SECTION OF FLOORBEAM'S TOP CHORD BS 1110 WL 208 RBL 8-23 AND INSTALLED REPAIR ANGLES, TEE CHORD AND STRAPS PER SRM 53-10-8.

Part: FRAME — DENTED (FUSELAGE) · airframe 36,556 hrs · 24,016 cycles

FWD CARGO BAY, FRAME DENTED STA 680 STR 23 LT COMING CUT OUT DENTED MATERIAL 1 X 1 INCH FROM FRAME AT BS 680 STR 23L AND REPAIRED PER SRM 53-10-1, 51-40-3 USING 7075-T6 .050 LOT #466242.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,556 hrs · 24,016 cycles

RT EXTERIOR FUSELAGE SKIN HAS A DENT AT BS 196 BELOW STR 19R 4 INCHES BELOW SKIN LAP. REMOVED DAMAGE AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON FLOORBEAM BS 480 LBL 2-10 WL 208. REMOVED CORROSION BY REMOVING .035 FROM AN AREA OF 2X2 INCHES. AREA IS OUT OF LIMITS. REMOVED DAMAGED AREA OF TOP CHORD. REPAIRED FLOORBEAM IAW SRM 53-10-8, 53-10-1

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,556 hrs · 24,016 cycles

CORROSION ON FLOORBEAM BS 460 LBL 10 WL 208. REMOVED CORROSION ON FLOOR BEAM BY REMOVING .030 FROM AN AREA OF 1X1 INCH. AREA IS OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGE AREA OF TOP FLANGE AND FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8

Part: WARNING LIGHT — ILLUMINATED (BODY OVERHEAT) · airframe 35,647 hrs · 23,290 cycles

LOWER AFT BODY OVERHEAT ILLUMINATED IN FLIGHT AT FL280. ACCOMPLISHED LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED (CHECKLIST) IAW QRH INDICATED SOURCE OF OVERHEAT AS ENGINE NR 3 LOW STAGE BLEED AIR SUPPLY TO THE MAIN WING ANTI-ICE VALVE. LIGHT EXTINGUISHED AND TESTED GOOD. TESTS NORMAL. RAN ENGINES IWA JRH APPROX 1 HR. REMOVED ACCESS PANEL FOR KEELBEAM AREA. INSPECTED FOR LEAKS WITH LASER HEAT DETECTOR IN AFT STAIRWELL,AFT CGO COMPARTMENT, KEELBEAM AREA, FOUND NONE. CHECKED FOR CLEARANCE ON ACCESSIBLE LOOPS. FOUND OK. INSTALLED KEEL BEAM ACCESS PNL. PRIOR HISTORY SHOWS T/S FOR FALSE ALARM. PERFORMED IAW MM 26-14-000-1 HAS BEEN C/W. REPLACED DET CONT. IAW MM. TESTS OK.

Part: OVERHEAT LOOP — OUT OF POSITION (RT MLG WW) · airframe 35,321 hrs · 23,033 cycles

FL 280 LOWER AFT BODY OVERHEAT LIGHT CAME ON. BLEED 3 OPEN, RIGHT PACK OPEN. CARGO HEAT OUTFLOW NORMAL. FOLLOWED QRH PROCEDURE. DESCENDED TO FL 250, RIGHT NR 2 BLEED OPEN, RIGHT PACK ON. CARGO HEAT OUTFLOW NORMAL. INCREASED THRUST ON NR 3 ENGINE TO 85.5 N1. LIGHT STAYED OUT. REMOVED KEEL BEAM ACCESS PANEL IN RT WHEEL WELL. FOUND AFT BODY O/H DETECTOR LOOP IN KEEL BEAM AREA ALMOST TOUCHING PNEUMATIC SUPPLY DUCT. REROUTED LOOP AS REQUIRED. NO OTHER FAULTS FOUND. CLOSED ACCESS PANELS & RESTORED A/C TO NORMAL. PERFORMED TEST IAW MAINTENANCE MANUAL 26-14-00-5, NO FAULTS.

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY) · airframe 35,316 hrs · 23,029 cycles

LOWER AFT BODY OVERHEAT LIGHT STARTED TO FLICKER ON PASSING THROUGH 27K FT. ON CLIMBOUT LIGHT WENT OUT AFTER TURNED OFF RT PACK AND CLOSED BLEED NR 3 COMPLETED QRH PROCEDURES CONTINUED AT FL280. COMPLIED WITH ADJUST AND TEST AND TROUBLE SHOOTING CHART UNABLE TO DUPLICATE. M/M 26-14-000-5 REPLACED OVER HEAT DETECTION CONTROL UNIT M/M 26-14-11.

Part: POSITION SWITCH — FAILED (RT MLG) · airframe 35,002 hrs · 22,779 cycles

ON FINAL AT DSM, EXTENDED LANDING GEAR GOT 3 GREEN LIGHTS, RED DOORS LIGHT ON FORWARD PANEL AND AMBER RT MAIN GEAR DOOR LIGHT ON S/O PANEL. CYCLED GEAR, ALL INDICATIONS NORMAL. ACN RELEASED FOR SERVICE PER MEL/CDL. RT MAIN GEAR DOOR POSITION SWITCH SHOWS NO CONTINUITY WITH DOOR OPEN OR CLOSED. REMOVED AND REPLACED RT MLG DOOR WARNING SWITCH PER 727-200 MM 32-62-011. OPS CHECK NORMAL.

Part: INDICATOR — FALSE ACTIVATION (MLG DOOR) · airframe 35,002 hrs · 22,779 cycles

RED DOOR INDICATOR ON AFTER GEAR RETRACTION DEPARTING DAY. RECYCLED GEAR PER RED TAB PROCEDURE AND LIGHT WENT OUT. CYCLED GEAR DOORS SEVERAL TIMES PER MM 32-62-01. NO DEFECTS NOTED. OK FOR SERVICE.

Part: ACTUATOR — FAILED (SLAT)

02-83 ON T/O FLAP RETRACTED FROM 5 DEG TO 2 DEG, #4 SLAT IND OUT. R&R #4 SLAT ACTUATOR PER MM 27-81-032-4. OK FOR SERVICE.

Part: FITTING — CRACKED (MLG ACTUATOR)

MLG ACTUATOR SUPPORT FITTING COMMON TO 348.2 BULKHEAD CRACKED. REMOVED AND REPLACED FITTING PER MM 32-33-011-4 & SRM 51-30-2.

Part: SHEAR TIE — CORRODED (FUSELAGE)

CORROSION C53-113-01(1) ON FRAME BS 720 LBL 4 TO RBL 4 WL 149 AFT SIDE OF FRAME. REMOVED AND REPLACED SHEAR TIE 51-30-2, 51-31-000-2, 51-20-1, 51-20-021-7, 51-20-031-7.

Part: FRAME — CRACKED (FUSELAGE)

UPPER FLANGE AT BS 640 FRAME IS CRACKED AT FLOOR SUPPORT ATTACH POINT AT RBL 2.5 & LBL 2.5 WL 155. REMOVED AND REPLACED PER SRM 51-40-3.

Part: SPLICE — CORRODED (FUSELAGE)

CORROSION (C53-113-01,1) ON STR 27R AT BS 482. REMOVED AND REPLACED SPLICE PER SRM 51-10-2, 51-20-4, 51-30-2.

Part: FRAME — CRACKED (FUSELAGE)

BS 660 FRAME UPPER FLANGE CRACKED AT FLOOR SUPPORT ATTACH POINTS, RB. 8.5 WL 155. REMOVED AND REPLACED UPPER FLANGE PER SRM 51-40-3.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

ON T/O AT 400 ENG FAIL LIGHT FOLLOWED BY NR 2 FIRE LIGHT & BELL. FOLLOWED RED TABS WHICH IND BLD AIR LEAK. *S/D* REMOVED AND REPLACED 13TH STAGE MANIFOLD ASSY PER WORK CARD 7102-2010 PG 3 TASK 4. LEAK CK NORM. REPLACED MISSING BLOW OUT PNLS ON RIGHT COWLINGS. REMOVED AND REPLACED NR 2 ENG FIREWALL SENSING ELEMENT PER MM 26-11-12. TEST NORM PER MM 26-11-01.

Part: FLOORBEAM — CORRODED (BS 1130)

UPPER LOBE, CORROSION FWD EDGE OF TOP FLANGE ON FLOORBEAM BS 1130, LBL 3 AND FLOORBEAM 1130, LBL 19 TOP FLANGE. REMOVED CORROSION WAS OUT OF LIMITS. INSTALLED FLOORBEAM REPAIR PER EA 7-5310-42947.

Part: FLOORBEAM — DAMAGED (BS 1148 & 1166)

TWO DOUBLE DRILL HOLES BS 1130, LBL 25, 30 AND DOUBLE DRILL HOLES BS 1148 AND 1166. REPAIRED DAMAGE TO FLOORBEAMS DUE TO DOUBLE DRILL HOLES PER EA 7-5310-42962. TREATED AND PRIMED PER 51-20-0.

Part: STRINGER — GOUGED (BS 440)

UPPER LOBE BS 440 STRINGER 8L TOP OF STRINGER GOUGED. BLENDED OUT GOUGE, OUT OF LIMITS. INSTALLED DOUBLER PER SRM 53-10-3 FIG 2.

Part: ANGLE — CORRODED (RT WING)

RT WING LWR SURFACE OF FRONT SPAR CHORD ANGLE HAS EXFOLIATED CORROSION AFT OF NR 5 L/E SLAT T DUCT. REMOVED CORROSION SPAR CHORD METAL. CORROSION BEYOND LIMITS (ORIG THICK 0.316 AFTER BLEND 0.0220). REPAIR STRAP INSTALLED ON UPPER SURFACE OF FRONT SPAR CHORD LWR ANGLE PER AARD 57-30-00-2 PG 2 AND SRM 57-10-4 PG 1-10.

Part: LIBHT — INOPERATIVE (RT MLG DOOR)

98-238 ON INIT T/O, THE RT GEAR DOOR LIGHT REMAIN ILLUM. ACCOMPLISH RED TABS. LIGHT REMAIN ILLUMINATED, SUSP RIGHT GEAR DID NOT RETRACT. WITH GEAR DOWN ANTI-SKID INOP AND SYS 'A' QUANTITY 2.5 GAL. REMOVED ANTI-SKID CONTROL UNIT. REPLACED STRUT DOOR SUPPORT PER 727 MM. REINSTALL ROUT RIGHT ELECT CONDUIT AND SAFTIED. OPS NORM. COMPLIED WITH ENG AUTH 7-3210-40942. OK FOR SERV.

Part: BOLT — FAILED (LT MLG)

AFTER TAKEOFF, LANDING LEVER WOULD NOT MOVE TO THE UP POSITION. FOLLOWED LANDING GEAR LEVER LATCH FAILS TO RELEASE CHECKLIST. MANUALLY RELEASED LANDING GEAR LEVER LATCH AND GEAR RETRACTED NORMALLY. REMOVED AND REPLACED BOLT IN LEFT MAIN LANDING GEAR ACTUATOR LINK FOR GROUND SENSOR. CHECKED CONTROL HANDLE SYSTEM PER ADJUSTMENT AND TEST 727 MAINTENANCE MANUAL 32-31-11. SYSTEM OPERATIONAL CHECK NORMAL.

Part: LOCK SOLENOID — FAILED (LANDING GEAR)

LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. COMPLIED WITH CHECKLIST AND RETURNED TO BASE. FOUND LANDING GEAR LOCK SOLENOID BAD. REPLACED SOLENOID PER BOEING MAINTENANCE MANUAL 32-31-16. GEAR LEVER OPERATIONAL CHECK GOOD.

Part: CLAMP INSULATOR — OUT OF POSITION (NR 1 ENGINE)

NR 1 FIRE DETECTOR CIRCUIT LIGHT ILLUMINATED IN-FLIGHT. THE FIRE WARNING TEST WAS INITIATED AND TESTED SUCCESSFULLY. ENGINE INSTRUMENTS APPEARED NORMAL. FOUND ONE CLAMP INSULATOR OUT OF POSITION. REPOSITIONED INSULATOR AND LOOP. LIGHT EXTINGUISHED WITH COWLING SECURED. FIRE WARNING CKS GOOD.

Part: SKIN — CORRODED (BS 720)

NR0236 AND 011, CORROSION (71C208-02) FWD CARGO BAY SKIN AT BS 720C PLUS 13 JUST I/B OF STR 28L. *S/D* REPAIRED CORROSION DAMAGE IN FWD CARGO BAY SKIN AT BS 720C PLUS 3 IAW FEDEX SRM 53-30-3.

Part: SKIN — CREASED (BS 303)

NR0430 & 009 SHARP CREASE IN SKIN FROM STA 303 - 325 L/H BETWEEN STR 3-4. ****S/D***** REPAIRED CREASE IN SKIN PER FEDEX SRM 53-30-3. DAMAGED AT BS 303 BETWEEN STR 3 & 4L WAS REPAIRED ON NR-0471.

Part: GATE — CORRODED (FWD ENTRY DOOR)

NR0486 & 010 WHILE WORKING NR0400 FOUND FWD ENTRY DOOR UPR GATE TO BE CORRODED SEVERELY. ****S/D**** R/R FWD ENTRY DOOR UPPER GATE. ALL WORK DONE IAW FEDEX SRM 51-30-2.

Part: WEB — CRACKED (BS 294.5-344)

NR0447 AND 008, WHILE ACCESSING WEB FOR REPAIR ON NR0052, FOUND WEB TO BE CRACKED AND CORRODED AT BS 294.5 TO 344 WL 170 RBL 34. *S/D* REMOVED CORROSION ON WEB AND FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED WEB, USING OLD WEB AS A TEMPLATE, ALODINED, PRIMED AND PAINTED, INSTALLED WEB.

Part: SKIN — CRACKED (BS 1220)

NR0444 AND 007, AFT AIRSTAIR CUTOUT L/FWD CORNER CRACKED PAST RIVET BS 1220 STR 26. *S/D* REPAIRED CRACK AT BS 220 STR 26L IAW FEDEX STANDARD REWORK DRAWING SR 27-53-024.

Part: STRINGER CLIP — CRACKED (BS 640)

FWD CARGO BAY STR CLIP HAS TORN EDGE BS 640 STR 27L. FABRICATED STR CLIP AND INSTALLED AT BS 640 STR 27L PER FEDEX SRM 53-10-1.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

NR 0028, 004 LEFT WING O/B FOREFLAP I/B END HAS A LARGE DELAMINATED TEMPORARY REPAIR. *S/D* LEFT WING O/B FOREFLAP I/B END WAS REPAIRED PER FEDEX SRM 51-40-6.

Part: DOORWAY FRAME — GOUGED (BS 848.95)

NR 0419 005. RIGHT AFT EMERGENCY EXIT DOORWAY AFT FRAME IS GOUGED 1.5 INCHES LONG AT BS 848.95 RBL 69.5 WL 234 GOUGE IS IN RADIUS. REWORKED GOUGED AREA OF RT AFT EMERGENCY EXIT DOORWAY FRAME IAW FEDEX EA 7-5310-29767.

Part: BONDING JUMPER — CORROSION (NR 2 LE FLAP)

NR 0261 003. CORROSION AROUND NR 2 K-FLAP OUTBOARD LOWER BONDING JUMPER UPPER ATTACH POINT. REPAIRED NR 2 K-FLAP OUTBOARD LOWER BONDING JUMPER UPPER ATTACH POINT IAW SRM 57-50-03. MOVED ATTACH POINT IAW SRM 27-57-010C.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

DISCREPANCY: (NR 0026)(O01) LEFT WING INBOARD AFT FLAP IS DELAMINATING ALONG 0113 EDGE UPPER AND LOWER SURFACES. CORRECTIVE ACTION: ****S/D****** COMING.

Part: TE WEDGE — DELAMINATED (LT TE MID FLAP)

DISCREPANCY: (NR 0027)(O02) LEFT WING INBOARD MID-FLAP TRAILING EDGE WEDGE IS DELAMINATED 6 INCHES FROM INBOARD END UPPER SURFACE. CORRECTIVE ACTION: ****S/D****** COMING.

Part: SPINDLE/ARM — BROKEN (LT MLG)

WHEN MANUALLY CRANKING THE L/GEAR A SNAP WAS HEARD AND THE MECHANICAL POINTER STOPPED MOVING. THE SNAP WAS HEARD BEFORE REACHING THE MECHANICAL STOP, GEAR DID EXTEND BUT NO FURTHER POINTER MOVEMENT WAS VISIBLE. FOUND MANUAL EXTENSION INDICATOR SPINDLE BROKEN AND FOLLOWER ARM BENT. REPLACED SPINDLE AND ARM AS PER MM 32-34-71. PERFORMED ADJ AND TEST LANDING GEAR MANUAL EXTENSION SYSTEM AS PER MM 32-34-81. ALL CHECKED GOOD, OK FOR SERVICE AND REQUIRED ITEM INSPECTION COMPLIED WITH.