N479FE

Part: MECHANISM — DAMAGED (PAX DOOR) · airframe 45,411 hrs · 29,628 cycles

FWD DOOR ENTRY SEAL DID NOT APPEAR TO SEAL UNTIL PASSING 6000 ALT. FWD ENTRY DOOR WOULD NOT OPEN ON LDL. CREW REPORTED THAT DOOR WAS VERY DIFFICULT TO CLOSE LEAVING LAST STATION AND THAT IT MADE SOME POPPING NOISES WHILE CLIMBING. UPON CREW DEBRIEF DOOR WOULD NOT BUDGE AND NOTICED THAT DOOR IS NOT FAIRED BY AT LEAST 1 INCH AT THE TOP SIDE. PUT HOT AIR TO IT FOR QUITE A WHILE STILL NO HELP. DOOR APPEARS TO HAVE SOMETHING VERY BOUND UP OR A MECHANISIM IS BROKEN. DAYLIGHT CAN BE SEEN AT TOP AND AFT SIDE OF DOOR. HANDLE DOESN'T GIVE AT ALL WITH A MECHANIC INSIDE TURNING HANDLE AND A MECHANIC TURNING THE HANDLE ON THE OUTSIDE.

Part: SEAT TRACK — GOUGED (BS 660-740) · corrosion level 2 · airframe 44,408 hrs · 28,804 cycles

GOUGED LOBE SEAT TRACK MAIN CABIN BS 681 RBL 62 REMOVED DAMAGED SEAT TRACK FROM ST 660 T0 STA 740 RBL 62 AT EXISTING SPLICES IAW SRM 51-30-2. DRILLED AND DEBURED NEW SEAT TRACK SIZE 80" IAW SRM 51-30-5 AND SRM 53-10-20 FIG 7A. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED SEAT TRACK AND SPLICES IAW SRM 51-30-2.

Part: STRINGER — DAMAGED (BS 600 S24L) · airframe 44,408 hrs · 28,804 cycles

UPON REMOVAL OF BS 600 FRAME SUPPORT CLIP, FOUND STR 24 L GOUGED AND PUNCTURED. CUT OUT DAMAGED SECTION OF STRINGER 24L AT BS 600, 17.7500" IN LENGTH IAW SRM, REV 102, 51-10-1 AND 53-10-3 FIG 1. FABRICATED STRINGER FILLER USING BAC1498 -142, 7075-T62, 17.7500" IN LENGTH AND 2 SPLICES USING BAC1498 -132, 7075 - T6, 12.2500" IN LENGTH IAW SRM 53-10-3 FIG 1. INSTALLED STRINGER FILLER AND SPLICES IAW SRM 53-10-3, FIG 1 AND 51-30-2.

Part: FRAME — CRACKED (BS 600) · airframe 44,408 hrs · 28,804 cycles

FWD PIT - UPPER SURFACE OF FRAME IS DENTED AT BS 600, ABOVE STRINGER 24 L. REMOVED CRACKED SECTION OF BS 600 FRAME 1" X 2 1/8" ABOVE STR 24L IAW FED EX B727 SRM REV 102 51-10-1 FABRICATED REPAIR DOUBLER FROM 7075 -0 .050 X6" X 12" IAW B727 SRM 53-10-2 FIG 3, 51-40-3 FIG 1 AND 51-30-5 INSTALLED REPAIR DOUBLER IAW B727 SRM 51-30-2 AND 51-40-3 FIG 1

Part: RIB — CRACKED (NR 3 SLAT) · airframe 44,408 hrs · 28,804 cycles

LEFT WING INBD AND OTBD RIBS ARE CRACKED WHERE NR 3 LE SLAT ACTUATOR MOUNTS TO SLAT. REMOVED ACCESS PANEL FOR ACCESS IAW 727 SRM 51-30-2. REMOVED INBD AND OTBD RIBS IAW SRM 51-10-1. LOCATED AND DRILLED NEW INBD RIB SUPPORT PN NR 65-17294U14 PO NR 20013120 AND NEW OTBD RIB SUPPORT PN NR 651729U13 PO NR 20013164 IAW B727 SRM 51-30-5. TREATED AND PRIMED RIBS IAW B727 SRM 51-10-2. INSTALLED NEW INBD AND OTBD RIBS AT NR 3 SLAT L/E ACTUATOR ATTACH POINT IAW SRM 51-30-2. INSTALLED ACCESS PANEL IAW B727 SRM 51-30-2.

Part: SKIN — DENTED (BS 1042) · airframe 44,408 hrs · 28,804 cycles

DENTS 3EA EXTERIOR FUSELAGE BS 1042 STR 24R - 25R. DENTS FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA DIM: 1" X 1" AND FABRICATED REPAIR DOUBLER FROM 2024T3 .071 PO NR 9009120 DIM: 8.6" X 6.7" IAW SRM 53-30-2, FIG 2 AND 53-30-3 FIG 1. DOUBLER TREATED PRIMED & INSTALLED IAW SRM 51-10-2 & 53-30-3 FIG 1.

Part: SKIN — DENTED (BS 1080) · airframe 44,408 hrs · 28,804 cycles

DENT EXTERIOR FUSELAGE BS 1080 STR. 20L. CUT-OUT DAMAGED AREA DIM: 6.5" X 1.75" AND FABRICATED REPAIR DOUBLER SROM 2024T3 .063 PO NR 9009362 DIM: 13.5" X 6.4" & STRUCTURAL FILLER FROM 2024T3 .050 PO NR 9009327, DIM: 13.5" X 3.5" IAW SRM 53-30-2 FIG 2 & 53-30-3 FIG 14. REPAIR PARTS TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2 & 53-30-3, FIG 14.

Part: SKIN — DENTED (ZONE 100) · airframe 44,408 hrs · 28,804 cycles

DENT EXTERIOR FUSELAGE BS 297 STR 23L - 24L DENT FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA 3.05 INCH BY 1.2 INCH AND FABRICATED AND INSTALLED REPAIR DOUBLER OF 2024T3 .050 PO NR 9009378 DIM: 10.5 INCH BY 8.0 INCH AND STRUCTURE FILLER FROM 2024T3 .040 PO NR 9009253 DIM: 10.5 INCH BY 2.0 INCH IAW B727 SRM 53-30-2 FIG 2 AND 53-30-3 FIG 14 REV 102.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,408 hrs · 28,804 cycles

CORROSION LOWER SURFACE OF UPPER TEE ON FLOORBEAM STA 1110, BETWEEN RBL 45 AND RBL 65. AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 4. CUT-OUT DAMAGED AREA OF UPPER TEE DIM: 6" X 2" AND FABRICATED UPPER TEE FROM BAC1505-100617 7075T6, PO NR 29094137 DIM: 23" ANGLE SUPPORT FROM BAC14902785 PO NR 29118113 DIM: 23" X .8750" X 1.8750, ANGLE SUPPORT FROM 7075T6 .090 PO NR 9008486 DIM: 18.3750" X .9375" X 1.3750". REINFORCE STRAP FROM BAC1512-3353 PO NR 9003263 DIM: 22" LONG REINFORCED STRAP FROM BAC 1512-3396. PO NR 9007927 DIM: 18.3750" LONG AND INSTALLED REPAIR PARTS IAW SRM 53-10-8, FIG 1.

Part: SKIN — DENTED (ZONE 100) · airframe 44,408 hrs · 28,804 cycles

DENTS (2 EA) EXTERIOR FUSELAGE BS 1059 STR 25R.

Part: SEAT TRACK — CORRODED (BS 1130-1180) · corrosion level 2 · airframe 44,408 hrs · 28,804 cycles

CORROSION SEAT TRACK MAIN CABIN BS 1130 - BS 1180 RBL 45. R & R SEAT TRACK SECTION FROM BS1130 - BS 1180 IAW SRM 51-30- 2. FABRICATED SEAT TRACK IAW DWG NO 53FX976, TREATED AND PRIMED PARTS IAW SRM 51-30-2 & DWG 53FX976.

Part: SEAT TRACK — CORRODED (BS 610-620) · airframe 44,408 hrs · 28,804 cycles

CORROSION SEAT TRACK LOBE SIDE WALL MAIN CABIN BS 610 - BS 620 RBL 45. REMOVED CORROSION IB FLANGE IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 3 & 53-10-2. REMOVED SEAT TRACK SECTION SRM 51-30-2. FABRICATED SEAT TRACK SECTION MATERIAL BAC 1520-792-7178-T6511 PO NR 9006020 DIM: 214" STA 480 - STA 690 AND FABRICATED ANGLE FROM PN NR 1503-100-122 7178T6 DIM: 13" X 1" & FABRICATED STRAP FROM 7075T6 .250 PO NR 9008114 DIM: 7.5" X 2" IAW SRM 53-10-5 FIG 1 TREATED AND PRIMED AREA & SEAT TRACK IAW SRM 51-10-2. INSTALLED SEAT TRACK STA 480-STA 690 IAW SRM 53-10-5, FIG 1.

Part: FLOORBEAM — CRACKED (BS 740) · airframe 44,408 hrs · 28,804 cycles

MAIN CABIN OVERWING FLOORBEAM T CHORD CRACKED AT LOWER RADIUS RBL 24 BS 760.9. REMOVED DAMAGED CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD FROM BAC1506-1108 MATERIAL 7075T6 PO NR 20013162 DIM: 110" IAW SRM 51-30-5 & 51-10-1 AND DWG 65-16279 REV F DATED 04/19/72. CHORD TREATED PRIMED & INSTALLED IAW SRM 51-10-2 & 51-30-2 & DWG 65-16279 REV F, DATED 04/19/72.

Part: FLOORBEAM — CORRODED (BS 880) · airframe 44,408 hrs · 28,804 cycles

FLOORBEAM ABOVE RT MLG WHEEL WELL FWD SURFACE HAS CORROSION AT BS 880, RBL 44. REMOVED CORROSION ON FLOORBEAM BY MECHANICAL MEANS IAW SRM 51-10-6. AREA UT INSPECTED IAW NDTM 51-00-00 FIG 2 PART 4 WITH ORIGINAL MATERIAL OF .100", .002" REMOVED, REMAINING AREA: .098" IS WITHIN LIMITS IAW SRM 53-10-1, FIG 8. TREATED AND PRIMED IAW SRM 51-10-2.

Part: FLOORBEAM — CORRODED (BS 880) · corrosion level 2 · airframe 44,408 hrs · 28,804 cycles

FLOORBEAM ABOVE RT MLG WHEEL WELL FWD SURFACE HAS CORROSION AT BS 880 RBL 44. REMOVED CORROSION ON FLOORBEAM BY MECHANICAL MEANS IAW SRM 51-10-6. AREA UT INSPECTED IAW NDTM 51-00-00 FIG 2, PART 4 WITH ORIGINAL MATERIAL OF .100", .002" REMOVED, REMAINING AREA: .098" IS WITHIN LIMITS IAW SRM 53-10-1, FIG 8. TREATED AND PRIMED IAW SRM 51-10-2.

Part: SEAT TRACK — DAMAGED (BS 720E) · airframe 44,408 hrs · 28,804 cycles

MISSING SCREW WITH HOLE ELONGATED AND EVIDENCE OF MISSING MATERIAL SEAT TRACK SPLICE MAIN CABIN BS 720E 10", BL 0. REMOVED DAMAGED AREA OF SEAT TRACK AT BL 0 FROM STA 720-740 IAW SRM 51-30-2. FABRICATED SEAT TRACK SECTION IAW SRM 53-10-5 FIG 1 AND P - F SRM 53-10-2 FIG 7A. TREATED AND PRIMED NEW SEAT TRACK IAW B727 SRM 51-10-2. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2, REV 102.

Part: SEAT TRACK — CORRODED (BS 480-690) · airframe 44,408 hrs · 28,804 cycles

CORROSION ALONG WHOLE SEAT TRACK SECTION BS 480 - BS 690 LBL 45. REMOVED SEAT TRACK STA 480 - STA 690 LBL 45 IAW SRM 51-30-2. FABRICATED SEAT TRACK PN BAC 1520-792-7178T 65, PO 9006020, DIM: 204" X 8" STA 480 - 690 AND FABRICATE ANGLE PN 1503-100-122-7178T6, DIM: 13" X 1" AT STRAP FROM 7075T6 .250 PO 9008114 DIM" 7.5" X 2" IAW SRM 53-10-5 FIG 1. LOCATED AND DRILLED SEAT TRACK AND PARTS IAW SRM 51-30-5. TREATED AND PRIMED AREA & PARTS IAW SRM 51-10-2. INSTALLED SEAT TRACK SECTION BS 480 - 690 LBL 45 IAW SRM 53-105.

Part: SEAT TRACK — CORRODED (BS 480-690) · airframe 44,408 hrs · 28,804 cycles

CORROSION ALONG WHOLE SEAT TRACK SECTION MAIN CABIN BS 480- BS 690, LBL 24. EVALUATED AREA FOUND CORROSION AT SEAT TRACK SECTION BS 480 TO BS 700 OUT OF LIMITS IAW SRM 727-200 NOTED 5.4 AND SRM 53-10-5 FIG 1. R & R SEAT TRACK AT LBL 24 FROM BS 480 TO BS 690 AND BS 690 TO BS 720A, 9". INSTALLED SEAT TRACK SPLICES AT LBL 24 BS 690 AND BS 720A 9" IAW SRM 53-10-5, FIG 1.

Part: SEAT TRACK — CORRODED (BS 1130) · airframe 44,408 hrs · 28,804 cycles

CORROSION - RBL 45 SEAT TRACK AT STA 1130, LOWER SURFACE. REMOVED SEAT TRACK IAW SRM 53-10-5, FIG 1. FABRICATED NEW SEAT TRACK SECTIONS FROM BAC 15207927178T6511 IAW SRM 53-10-5, FIG 1 SECTION (1) 99" SECTION AND (2) 74.7500". FABRICATED ANGLE SPLICES 4 EA FROM BAC 1503-1001227178T6511 DIM: 13.1250" X 2 AND 14.1250" X 2. SPLICES DIM: 13" X 2 AND FABRICATED STRAP FROM 7075T6 .250 DIM: 7.1250" EACH ALL IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED NEW PARTS IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 370-390) · airframe 44,408 hrs · 28,804 cycles

CORROSION SEAT TRACK MAIN CABIN BS 370 -BS 390 LBL 45. CLEANED AREA IAW BSOPM 20-30-03 AND EVALUATED AREA NO CORROSION NOTED IAW SRM 51-10-1 AT BS 360- BS 399. EVALUATED AREA FROM BS 400 - BS 480 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 3 AND SRM -200 NOTE 5.4. REMOVED DAMAGED SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792-7178T6511 DIM: 87.7500" IAW SRM 53-10-5 FIG 1 AND FABRICATED ANGLE SPLICES FROM BAC1503-1001227178T6 DIM: 13.5" X 2" EACH. FABRICATED STRAP SPLICE FROM 7075T6 .250 DIM: 7" X 2" IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED NEW PARTS IAW SRM 53-10-5 FIG 1, REV 102.

Part: SEAT TRACK — CORRODED (BS 510-690) · airframe 44,408 hrs · 28,804 cycles

CORROSION ALONG SEAT TRACK MAIN CABIN BS 510 - BS 690 RBL 24. REMOVED CORROSION AT IB FLANGE IAW SRM 51-10-6 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 3 & 53-10-2. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED SEAT TRACK FROM BAC 1520-7927178-T6511 PO 9006020 DIM: 204" X 17" IAW SRM 53-10-5 AND FABRICATED ANGLES FROM PN 1503-1001227178T6 PO 2944688 DIM: 13" 2EA. AND (1) STRAP FROM 7075 T6 .250 PO 9008117 DIM: 7.5" X 2" IAW SRM 53-10-5, FIG 1 TREATED AND PRIMED AREA AND PARTS IAW 51-10-2. INSTALLED SEAT TRACK SECTION AT BS 480-BS 690 IAW SRM 53-10-5, FIG 1.

Part: FLOORBEAM — CORRODED (BS 1130) · airframe 44,408 hrs · 28,804 cycles

CORROSION WITH CRACKING/ LIFTED METAL -STA 1130 FLOORBEAM UPPER CHORD FWD FLANGE, LBL 25 - LBL 45. CUT-OUT DAMAGED AREA FROM 1130 FLOORBEAM UPPER CHORD FWD FLANGE IAW SRM 53-10-8 DETAIL III DIM 12.5 INCH LONG. PERFORMED HFEC ON CUT-OUT IAW NDTM 51-00-00 FIG 23 PART 6, NO CRACKS INDICATED. FABRICATED REPAIR ANGLE PARTS MADE FROM 7075 O .050 PO NR 20006220 APPROX DIM: 12 INCH BY 2 INCH, FABRICATED STRAP FROM 7075 O .063 PO NR 9009327 APPROX DIM: 3 INCH BY 14 INCH IAW SRM 53-10-8 FIG 10 AND 53-10-2 FIG 7. HEAT TREATED MATERIAL TO T6 CONDITION IAW ER NR 2-37153-801 REV A. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 10 DETAIL III REV 102.

Part: FRAME — CORRODED (BS 1030 S27L/R) · airframe 44,408 hrs · 28,804 cycles

AFT PIT HAS SURFACE CORROSION ON FRAME BS 1030 AT STR 27L AND STR 27R. REMOVED CORROSION AT BS 1030 STRINGER 27L IAW SRM 51-10-6. AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. FORMED REPAIR DOUBLER IAW SRM 53-10-2, FIG 5 AND 51-40-3 FIG 1. LOCATED, DRILLED AND DE BURRED HOLES ON DOUBLER IAW SRM 51-30-5 AND 51-40-3 FIG 1. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-2, REV 102.

Part: FRAME — CORRODED (BS 950D S28L) · airframe 44,408 hrs · 28,804 cycles

AFT PIT HAS SURFACE CORROSION ON FRAME BS 950D OTBD OF STR 28L. REMOVED CORROSION ON FRAME AT BS 950D AND STR 28L IAW SRM, REV 102, 51-10-6. C/W U.T. THICKNESS ON AREA IAW NDTM, PT 4, 51-00-00 FIG 3, ORIGINAL MATERIAL .063", MATERIAL REMOVED .033", MATERIAL REMAINING .030", OUT OF LIMITS IAW SRM 53-10-1. FORMED DOUBLER 7.5" X 12.5" USING 7075 - 0, .071" IAW SRM 53-10-2 AND 51-40-3. HEAT TREATED TO T-6 CONDITION IAW FAS ENG REPORT NR 2-37153-101 REV A INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.

Part: FRAME — CORRODED (BS 950B S28L) · corrosion level 2 · airframe 44,408 hrs · 28,804 cycles

AFT PIT HAS SURFACE CORROSION ON FRAME AT BS 950B OTBD OF STR 28L. REMOVED CORROSION AT BS 950B STR 28L IAW SRM 51-10-6. AREA FOUND TO BE OUT OF LIMITS IAW SRM REV 102. FORMED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1 & 53-10-2. LOCATED, DRILLED & DEBURRED DOUBLER IAW IAW SRM 51-30-5. INSTALLED DOUBLER IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 360-480) · airframe 44,408 hrs · 28,804 cycles

CORROSION SEAT TRACK SECTION MAIN CABIN BS 360-480 BL 0. CLEANED AREA IAW BSOPM 20-30-03, EVALUATED AREA NO CORROSION NOTED IAW SRM 51-10-1 AT BS 360-440, REMOVED DAMAGED SECTION BS 430-600 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178-T6511 DIM: 170" IAW SRM 53-10-5 FIG 1. FABRICATED ANGLE SPLICES FROM BAC1503-1001227178-T6511 DIM: 13.7500" 2 EA AND FABRICATED STRAP SPLICES FROM 7075T6 .250 DIM: 8.5" X 2" IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2 AND INSTALLED SEAT TRACK SECTION AT BL 0 BETWEEN BS 430-600. INSTALLED SEAT TRACK EXTRUSION REPAIR AT BL 0 BS 430 IAW SRM 53-10-5 FIG 1.

Part: SILL — GOUGED (BS 560 S4L) · airframe 44,408 hrs · 28,804 cycles

UPPER SILL WEB GOUGED AT BS 560, STR 4L. REMOVED INNER SKIN AT UPPER SILL IAW SRM 51-30-2. FABRICATED INNER SKIN USING 2024-T3, .090", PO NR 9009093 APROX DIM 88" X 33.75" IAW SRM 53-10-2, FIG 3A AND DWG NR 53FX1551. INSTALLED INNER SKIN AT BS 526 TO BS 616 BETWEEN STR 4L AND 2L IAW SRM 51-30-2, REV 102.

Part: SEAT TRACK — CORRODED (BS 360-480) · airframe 44,408 hrs · 28,804 cycles

CORROSION SEAT TRACK SECTION MAIN CABIN BS 360 -BS 480 LBL 24. CLEANED AREA FROM BS 360- BS 480 LBL 24 IAW BSOPM 20-30-03. EVALUATED AREA FOUND CORROSION AT BS 380- BS 480 IAW SRM 51-10-1 OUT OF LIMITS IAW SRM 53-10-1 AND SRM 727-200 9G NOT 5.4. REMOVED DAMAGED SECTION FROM BS 370 - BS 480 LBL 24 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION ANGLE SPLICES AND STRAP SPLICE IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED SEAT TRACK SECTION AND SPLICES IAW SRM 51-10-2. INSTALLED SEAT TRACK AND SPLICES IAW SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1030) · airframe 44,408 hrs · 28,804 cycles

CORROSION - STA 1030 FLOORBEAM UPPER CHORD, UPPER AND LOWER SURFACE, APPROX RBL 9. CUT-OUT DAMAGED AREA 1.8 INCH STA 1030 RBL 8 IAW SRM 53-10-8 FIG 8. FABRICATED REPAIR ANGLES FROM BAC 1490-2888 7075T6 PO NR 29103176 DIM: 13 INCH 1 AND 9 INCH 1 AND FILLER FROM 7075T6 .125 PO NR 2911789 DIM: 1.8 INCH IAW SRM 53-10-8 FIG 8 DETAIL I AND 53-10-2 FIG 7. TREATED AND PRIMED REPAIR PARTS AND WORK AREA IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 8.

Part: WEB — CRACKED (CARGO DOOR FRAME) · airframe 44,408 hrs · 28,804 cycles

NR 1 CARGO DOORWAY FRAME, BS 560, STR 19R, WEB CRACKED NEXT TO DOOR STOP FITTING. REMOVED WEB FROM C-1 DOOR CUT OUT FRAME AT BS 560 IAW SRM, REV 102, 51-30-2. FABRICATED NEW WEB USING 7075 -T6, .071" X 80" X 18" IAW SRM 53-10-2 FIG 3 AND DWG NR 65-56100, REV F INSTALLED NEW WEB IAW SRM 51-30-2.

Part: DOOR FRAME — CRACKED (BS 620 S25R) · airframe 44,408 hrs · 28,804 cycles

NR 1 CARGO DOORWAY FRAME, BS 620, STR 25R, WEB CRACKED, ORIGINATING FROM SEAL RETAINER FASTENER HOLE. REMOVED WEB AT BS 620 FRAME FROM STRINGER 16R TO 28R IAW SRM, REV 102, 51-30-2. FABRICATED NEW WEB USING 7075-T6, .071" X 24" X 139.5" IAW MFG DWG NR 65-56101 REV F. INSTALLED WEB IAW SRM, REV 102, 51-30-2.

Part: SUPPORT — CRACKED (TRUNNION) · airframe 44,408 hrs · 28,804 cycles

CRACK RT FWD STIFFNER NLG TRUNNION SUPPORT. REPLACEMENT OF STIFFENER ACCOMPLISHED ON SNRM NR N00463, WORK ORDER NR 00047694.

Part: SUPPORT — CRACKED (TRUNNION) · airframe 44,408 hrs · 28,804 cycles

CRACK RT AFT STIFFNER NOSE TRUNNION SUPPORT. NO WORK ACCOMPLISHED ON THIS WORK CARD. REPLACEMENT OF STIFFENER ACCOMPLISHED ON SNRM NR N00463, WORK ORDER NR 00047694, SDR TRACKING NR 10-0807.

Part: FLOORBEAM — CORRODED (BS 890) · airframe 44,408 hrs · 28,804 cycles

FLOORBEAM ABOVE RT MLG WHEEL WELL CORRODED ON FWD SURFACE BS 890, RBL 22 TO RBL 28. CUT-OUT DAMAGED AREA AT BS 890 RBL 22 TO 28 DIM: 4.125" X 2.750" AND 2" X 2.9" IAW SRM 51-40-4, FIG 1. HFEC INSPECTED CUT-OUT IAW NDTM 51-00-00 FIG 23, PT 6 NO DEFECTS NOTED. FABRICATED ANGLES FROM 7075O .125 DIM: 16" X 6.150" (2 EA ) AND 17.750" X 6.3" (2 EA). SHIM REPAIR FROM 7075T6 .050 DIM: 16.5" X 5.5" (2 EA) 7075T6 .100 DIM: 4.125" X 2.750" AND 2.9" X 2" IAW SRM 53-10-2 FIG 7 AND 51-40-4 FIG 1. HEAT TREATMENT INSP 7075O TO T6 IAW ER 2-37153-801 REV A. LOCATED AND DRILLED PART REPAIR IAW SRM 51-40-4, FIG 1. TREATED AND PRIMED NEW PARTS. INSTALLED REPAIR INSTALLATION AT BS 890 RBL 18 TO 35 IAW SRM 51-30-2.

Part: SKIN — CHAFED (BS 720E S19R) · airframe 44,408 hrs · 28,804 cycles

FUSELAGE SKIN CHAFED AT LAP SEAM, STR 19R, STA 720E. CUT-OUT DAMAGED AREA DIM: 5.5" X 2.7500" IAW SRM 53-30-3 FIG 6. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23, PART 6, NO DEFECTS NOTED. FABRICATED DOUBLER FROM 2024T3 .071 DIM: 13" X 9" AND 2 EA TAPER FILLERS FROM 2024T3 .071 DIM: 1" X 6" EA. PO NR 9009120 AND 2 EA FILLERS FROM 2024T3 .063 DIM: 7.5" X 12.5" AND 2.5" X 5.5" PO NR 9009208 IAW SRM 53-30-3 FIG 6. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 6.

Part: FRAME — DAMAGED (BS 460 S8R) · airframe 44,408 hrs · 28,804 cycles

WIRE BUNDLE STAND OFF BROKEN AND FRAME DAMAGED, STA 460, STR 8R. REMOVED DAMAGED STAND OFF IAW SRM 51-30-2. DRILLED OUT DAMAGE AT FRAME UP TO .125 DIA IAW SRM 53-10-1, FIG 1 AND INSTALLED .1250" SOLID FASTENER AT FRAME IAW SRM 51-30-2. INSTALLED NEW STAND OFF IAW SRM 51-30-2.

Part: SKIN — GOUGED (BS 720E S19L) · airframe 44,408 hrs · 28,804 cycles

FUSELAGE SKIN GOUGED AT LAP SEAM, STR 19L, STA 720E. REMOVED FASTENERS AS REQUIRED AND CUT-OUT DAMAGED AREA ON UPPER AND LOWER LAP SEAM DIM: 3" X 4.3750" 2 EA IAW SRM 53-30-3 FIG 6. HEFC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PART 6, NO DEFECTS NOTED. FABRICATED DOUBLER FROM 2024T3 .071 DIM: 9" X 13" PO NR 9009120 AND TAPER SHIMS 2 EA FROM 2024T3 .071 DIM: 6" X 1" PO NR 9009120 AND 2 EA FILLERS FROM 2024T3 .063 DIM: 4 .2500" X 2.8750" AND 11.5" X 6.7500" PO NR 9009353 IAW SRM 53-30-3, FIG 6. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3, FIG 6.

Part: STRUCTURE — CORRODED (BS 294.5) · airframe 44,408 hrs · 28,804 cycles

E/E COMPARTMENT, RT MID CHORD CORRODED AT STA 294.5. REMOVED CORROSION FROM RT MID CHORD AT STA 294.5 IAW SRM, REV 102, 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 1. R & R MID CHORD PN 65-19862-20 AND 2 VERTICAL STIFFENERS, PN 65-19863-10 AND 65-19863-12, IAW DWG NR 65-18415. INSTALLED RT MID CHORD AND 2 VERTICAL STIFFENERS IAW DWG NR 65-18415 AND SRM 51-30-2.

Part: SKIN — DENTED (BS 400 S17-19L) · airframe 44,408 hrs · 28,804 cycles

DENT BS 400 STR 17L - 19L EXTERIOR FUSELAGE. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA DIM: 2.6250" X 2.8750" IAW SRM 53-30-3 FIG 3. HFEC INSP CUT-OUT AREA IAW NDTM 51-00-00, FIG 23, PART 6, NO DEFECTS NOTED. FABRICATED FILLER FROM 2024T3 .050 SIZE: 1.7500" X 2.5" AND DOUBLER FROM 2024T3 .063 SIZE: 11" X 8.5" PO NR 9009353 AND PO NR 9009378 IAW SRM 53-30-3 FIG 3. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 3.

Part: SKIN — CRACKED (RT WING) · airframe 44,408 hrs · 28,804 cycles

RT INBD FOREFLAP CARRIAGE ATTACH FITTING AREA AT STA 224, SKIN CRACKED FWD OF ATTACH FITTING. CUT OUT DAMAGED AREA, DIMENSIONS .750" X .218" IAW SRM, REV 102, 57-50-4, FIG. 1. FABRICATED FILLER USING 2024 T-3, PO NR 9002222, DIMENSIONS .050" X .750" X .218" AND DOUBLER USING 2024 T-3, PO NR. 9009353, DIMENSIONS .063" X 5" X 4.375" IAW SRM 57-50-4 FIG 1 AND 57-50-2 FIG 3. TREATED AND PRIMED DOUBLER, FILLER, AND REPAIR AREA IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2 AND 57-50-4 FIG 1.

Part: FRAME — DAMAGED (BS 500 S8R) · airframe 44,408 hrs · 28,804 cycles

FRAME DAMAGED BY TOO LONG HARDWARE INSTALLED IN WIRE BUNDLE STAND OFF CLAMP, STA 500, STR 8R. REMOVED STAND OFF IAW SRM 51-30-2. DRILLED OUT DAMAGED AREA .125 DIA IAW SRM 53-10-1, FIG 1 INSTALLED .1250" SOLID FASTENER IAW SRM 53-10-1 FIG 1 & 51-30-2. INSTALLED NEW STAND OFF IAW SRM 51-30-2.

Part: FRAME — MISMANUFACTURED (BS 344 S4L) · airframe 44,408 hrs · 28,804 cycles

FASTENERS WITH NO SPACING IN FRAME, STA 344, STR 4L. CUT-OUT DAMAGED AREA, FABRICATED REPAIR ANGLES FROM 7075-0 .050 PO NR 9009327 DIM: 7.4" X 3.3" & 7.4" X 3" HEAT TREATED TO 7075T6 IAW ENGINEERING REPORT NR 2-37153-801, REV A. TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED IAW SRM 53-10-4 FIG 1, 53-10-2 FIG 3, REV 102.

Part: RIB — CRACKED (NR 7 SLAT) · airframe 44,408 hrs · 28,804 cycles

NR 7 SLAT HAS 1 RIB CRACKED ON OTBD SIDE OF ACTUATOR FWD MOUNT.

Part: RIB — CRACKED (NR 5 SLAT) · airframe 44,408 hrs · 28,804 cycles

NR 5 SLAT RIB OTBD OF ACTUATOR FWD MOUNT, PREVIOUS REPAIR DOUBLER IS MISSSING 1 FASTENER AND DOUBLER IS INSTALLED ON TOP OF BUTTON HEAD RIVET. ACCOMPLISHED NR 5 SLAT RIBS REPLACEMENT ON NR N00260 SO 00047694, SDR 10-0780

Part: ANGLE — CRACKED (NR 2 SLAT) · airframe 44,408 hrs · 28,804 cycles

NR 2 SLAT LOWER T/E CHORD ANGLE IS CRACKED BELOW T-DUCT. R & R NR 2 SLAT ASSY ON NR NR N00252, WORK ORDER NR 00047694. NO MX PERFORMED ON THIS SNRM.

Part: RIB — CRACKED (NR 6 SLAT) · airframe 44,408 hrs · 28,804 cycles

NR 6 SLAT HAS 2 CRACKED RIBS AT ACTUATOR FWD MOUNT. NBD SIDE IS CRACKED AT AFT NUTPLATE AND OTBD SIDE CRACKED IN BOTTOM RADIUS. REMOVED ACCESS PANELS AND CRACKED RIBS AT NR 6 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIBS IAW SRM 51-30-5. INSTALLED NEW RIBS PN 65-17294U14, PO NR 20013120 AND 65-17294U13, PO NR 20013164 AND ACCESS PANELS IAW SRM 51-30-2, REV 102.

Part: BEAM — MISMANUFACTURED (BS 1183 BULKHEAD) · airframe 44,408 hrs · 28,804 cycles

FWD BS 1183 BULKHEAD LBL 18 VERTICAL BEAM HAS FASTENER WITH NO SPACING. CUT-OUT DAMAGED AREA AT VERTICAL BEAM, FABRICATED REPAIR PARTS & INSTALLED. REPAIR PARTS AT BS 1183 LBL 18 VERTICAL BEAM IAW EA 7-5310-135529.

Part: RIB — CRACKED (NR 4 SLAT) · airframe 44,408 hrs · 28,804 cycles

LT WING NR 4 L/E SLAT INBD RIB IS CRACKED WHERE ACTUATOR MOUNTS TO RIB. REMOVED CRACKED RIB IN NO. 4 L/E SLAT WHERE ACTUATOR MOUNTS IAW FED EX B727 SRM, REV102, 51-30-2 AND COVE PANEL FOR ACCESS IAW B727 SRM 51-30-2. LOCATED AND DRILLED TWO RIBS IAW B727 SRM 51-30-5. INSTALLED RIBS AND COVE PANELS IAW B727 SRM 51-30-2.

Part: RIB — CRACKED (NR 5 SLAT) · airframe 44,408 hrs · 28,804 cycles

NR 5 SLAT HAS ONE RIB CRACKED INBD SIDE OF ACTUATOR FWD MOUNT. REMOVED WEB PNL FOR ACCESS AND REINSTALLED IAW B727 SRM 51-30-2. REMOVED 2 EA. RIBS FOR CRACKS AND FABRICATED 1 RIB FROM 2024-0 .040 PO 24146179 DIMS: 16 3/4" X 6" IAW SRM 57-20-2 FIG 2 & 51-30-2. HEAT TREATED RIB TO T4 CONDITION IAW ENGINEERING REPORT 2-37153-801 REV A. LOCATED AND DRILLED 1 EA. FABRICATED RIB AND 1 EA. PROCURED RIB PO 2001349 IAW SRM 51-30-5. TREATED AND PRIMED RIBS IAW SRM 51-10-2 & INSTALLED RIBS IAW SRM 51-30-2 REV 102.

Part: ANGLE — CRACKED (NR 7 SLAT) · airframe 44,408 hrs · 28,804 cycles

NR 7 SLAT LOWER AFT CHORD ANGLE IS CRACKED BELOW T-DUCT.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 44,083 hrs · 28,574 cycles

HIT BIRD ON FINAL 36L IN MEM, SHATTERED CAPTAINS WINDSHIELD. INSTALLED L1 WINDOW AS PER MM 56-11-011-4 UP TO STEP 6B5. INSTALLED PER MM 56-11-011-4 STEP 6 THRU 7G AND I. REINSTALLED CAPTS WINDOW WIPER PER MM 30-42-042-2 AND GLARESHIELD PER MM 25-10-062-4.

Part: CONTROL VALVE — LEAKING (CABIN AIR) · airframe 43,981 hrs · 28,474 cycles

UNABLE TO CONTROL PRESSURIZATION WITH ANY MODE (AUTO, STANDBY, OR MANUAL). DESCENDED TO 11,000. PERFOMED OPS CHECK OF CABIN PRESS CONTROL SYSTEM PER MM 21-31-000-1 ALL MODES OP CHECK NORMAL. VERIFIED CABIN OUTFLOW VALVE IS CLOSED WHEN COMMANDED CLOSED. WITH APU ATTEMPTED TO PRESSURIZE A/C TO PERFORM DECAY CHECK APU WOULD ONLY BRING A/C TO 3.1DP., WHILE USING EXTERNAL AIR SOURCE THE HUFFER OVERHEATED. ALSO WHILE A/C WAS PRESSURIZED. FOUND AIR STILL COMING FROM THE AVI EXHAUST EVEN THOUGH THE VALVE WAS WRENCHED CLOSED. REPLACED EQUIP COOLING FLOW CONTROL VALVE REF M.M 21-58-021-4. PERFORMED DECAY CK REF MM 05-51-101-2, GROUND OPS CK GOOD AT THIS TIME. ACFT OK FOR SERVICE.

Part: OIL SYSTEM — LOW PRESSURE (ENGINE) · airframe 43,963 hrs · 28,463 cycles

LOW OIL PRESSURE LIGHT ILLUMINATED, OIL PRESSURE ON S/O'S PANEL INDICATED YELLOW ARC, PREFORMED ENG FAIL/SHUTDOWN CHECKLIST. DURING CHECKLIST OIL QUANITY DROPPED RAPIDLY TO ZERO. OIL PRESSURE IN YELLOW ARE FOR APPROX 130 MIN. DURING DECENT PERFORMED ENG WIND MILLING CHECKLIST. SPOKE WITH THE CAPT ABOUT THE EVENT AND CREW OBSEVATIONS OF THE OIL PRESSURE WITH THE ENGINE RUNNING AND DURING WINDMILLING, WITH THE ENGINE RUNNING, OIL PRESSURE NEVER FELL BELOW YELLOW ARC. DURING WINDMILLING OIL PRESSURE NEVER FELL BELOW 10 PSI. REMOVED AND REPLACED THE ENGINE. OPEN

Part: RELAY — FAILED (FIRE DETECTION) · airframe 43,895 hrs · 28,415 cycles

FL240, GLARESHIELD FIRE LIGHT CAME ON FOR LESS THAN 1 SEC. NO OTHER FIRE INDICATIONS. AT 1135 AND 1140Z FIRE LIGHT AGAIN BLINKED ON AND OFF WITH FIRE BELL FOR LESS THAN 1 SEC AT 1141Z FIRE LIGHT, BELL, AND APU LIGHT ALL CAME ON AND STAYED ON. PULLED APU FIRE HANDLE AND DISCHARGED BOTTLE. COMPLETED QRH PROCEDURES AND DECLARED EMERGENCY. LANDED AT STL AT 1205Z. FIRE TRUCKS CHECKED. AIRCRAFT AFTER ROLLOUT AND TURNOFF WITH NO FIRE INDICATIONS. TAXIED TO PARKING AND SHUTDOWN. REMOVED AND REPLACED APU FIRE TEST AUX RELAY (R151) PER WDM 49-41-01 AND SMP 20-81. RESET APU FIRE HANDLE AND PERFORMED APU FIRE TEST PER JRH CHAP 3-5. ALL TESTS NORMAL. ACN RELEASED FOR SERVICE PER MEL/CDL: 26-11-B "MEL 26-11-B: APU FIRE PROTECTION/DETECTION SYSTEM INOP. DO NOT USE APU." APU DEACTIVATED. APU CONTROL RELAY ON P-9 PANEL OPENED AND COLLARED. APU FIRE BOTTLE READS 0 PSI.

Part: CONTROL VALVE — FAILED (COOLING FLOW) · airframe 43,796 hrs · 28,343 cycles

AIRCRAFT WOULD NOT PRESSURIZE PROPERLY. TWO MIN AFTER LEVEL OFF AT FL320 CABIN PRESSURE CLIMBED THROUGH 10 K MSL. CREW EXECUTED CABIN ALT WARNING/RAPID DEPRESSURIZATION AND EMERGENCY DESCENT CHECKLIST. AIRCRAFT FAILED TO HOLD PRESSURE (CABIN ALT CLIMBING ) ALL PRES MODES. OUTFLOW VALVE INDICATED FULL CLOSED, BUT AIRCRAFT STILL WOULD NOT PRESSURIZE. PERFORMED CONTROLLER SYSTEMS CHECK PER JRH AND OPS. REMOVED AND REPLACED EQUIPMENT COOLING FLOW CONTROL VALVE CHECKS GOOD FOR SECURITY AND OPERATION IAW AMM CH 21-58-021-4.

Part: SKIN — CORRODED (BS 480 S28L) · corrosion level 2 · airframe 42,703 hrs · 27,476 cycles

FWD CARGO BILGE 3" FWD OF STA 480 S-28L AT REPAIR SPLICE OTBD SIDE HAS CORROSION. CUT OUT DAMAGE, FABRICATED REPAIR PARTS STR T7/710940. FABRICATED DOUBLER, FILLER, MAT 2024 T3.100C, AND 7075-T6.071C IAW SRM 53-10-3, 53-30-3. INSTALLED REPAIR STRINGER AND FILLER/DOUBLER IAW SRM 53-10-3FIG 1, 53-30-3 FIG 3A, FS 480, S-28L. REPAIR IS CLASSIFIED AS MINOR REPAIR.

Part: SKIN — DENTED (BS 312-328) · airframe 42,703 hrs · 27,476 cycles

FWD LT LOWER HALF EXTERNAL FUSELAGE BET STA 312-328, STR 22L SKIN HAS DENT. REMOVED PREVIOUS SKIN DOUBLER, FABRICATED SKIN DOUBLER IAW SRM 53-30-3. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR REPAIR.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 42,604 hrs · 27,399 cycles

CABIN ALT WARNING CLIMBING THROUGH FL270, CABIN ALT SHOWED 10,000, CLOSED CARGO HEAT OUTFLOW VALVE, NO CHANGE IN CABIN ALTITUDE. PERFORMED QRH CABIN ALT WARNING CHECKLIST. THEN PERFORMED FAILURE OF PRESSURIZATION OF CONTROL CHECKLIST. SYSTEM WOULD NOT PRESSURIZE IN AUTO OR STBY. IT DID WORK IN MANUAL. OUTFLOW VALVE INDICATED FULL CLOSED IN AUTO AND STBY MODES. REMOVED AND REPLACED PRESSURE CONTROLLER PER M/M 21-31-010-4. OP'S CHECK NORMAL ON GROUND.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 42,610 hrs · 27,404 cycles

CABIN ALT WARNING CLIMBING THROUGH FL270, CABIN ALT SHOWED 10,000, CLOSED CARGO HEAT OUTFLOW VALVE, NO CHANGE IN CABIN ALTITUDE. PERFORMED QRH CABIN ALT WARNING CHECKLIST. THEN PERFORMED FAILURE OF PRESSURIZATION OF CONTROL CHECKLIST. SYSTEM WOULD NOT PRESSURIZE IN AUTO OR STBY. IT DID WORK IN MANUAL. OUTFLOW VALVE INDICATED FULL CLOSED IN AUTO AND STBY MODES. REMOVED AND REPLACED PRESSURE CONTROLLER PER M/M 21-31-010-4. PREMATURE REMOVAL/INSTALLATION, OFF MFG 790960-1, SRL 8711490, ON MFG 790960-1, SRL 79K3611.

Part: ACTUATOR — FAILED (NLG) · airframe 42,481 hrs · 27,303 cycles

UPON LOWERING LANDING GEAR HANDLE, NOSE GEAR DID NOT COME DOWN INITIALLY WITH RED NOSE GEAR LIGHT AND NO NOSE GEAR DOOR LIGHT ON FE'S ANNUNCIATOR PANEL. AFTER APPROX 20 SECONDS, COULD HEAR NOSE GEAR DOORS OPEN AND NOSE GEAR COME DOWN AND LOCKED. LANDING GEAR HANDLE WAS STIFF WHEN LOWERING HANDLE. REMOVED AND REPLACED RETRACT ACTUATOR AND LOCK ACTUATOR.

Part: INDICATOR — INOPERATIVE (EPR) · airframe 41,783 hrs · 26,767 cycles

DURING RUNUP FOR T/O WITH INOP EPR GAUGE NEITHER N1 OR EPR WOULD GET APLC CALCULATED PARAMETERS. REJECTED T/O CALCULATED NR 2 ENG. EPR WAS 2.18 ACHIEVED ONLY 2.03 EPR. CALCULATED N1 WAS 100.6 ONLY ACHIEVED 97.0 N1. ENGINE NOT MAKING ENOUGH POWER.

Part: INDICATOR — INOPERATIVE (NR 2 EPR) · airframe 41,783 hrs · 26,767 cycles

RTO FOR INOP NR 2 EPR GAUGE MAX SPEED WAS 70 KTS. EPR INDICATION WAS GOOD ON HIGH POWER RUNUP.

Part: SHUTOFF VALVE — FAULTY (CABIN PRESSURE) · airframe 41,127 hrs · 26,270 cycles

A/C WOULD NOT MAINTAIN CABIN ALT ON CLIMBOUT. WOULD NOT MAINTAIN PSI IN AUTO-STANDBY OR MANUAL OR ANY BLEED. WHILE TROUBLSHOOTING ITEM FOUND THAT THE RT PACK WAS NOT OPERATING WHEN SELECTED ON, REMOVED AND REPLACED THE RT AIR SHUTOFF VALVE IN REF TO 727-200 AMM 21-55-071-4. PERFORMED OPS CHECK OF THE RT PACK AND PACK OPERATED NORMALLY ALONG WITH THE RT AIR MIX VALVE. PERFORMED A DECAY CHECK PER 727 JRH CHAPT 7 PG 7-51 TO 7-54 DECAY CHECK PASSED, A/C IS OK FOR CONTINUE SERVICE.

Part: SKIN — CORRODED (CENTER WING) · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

COMPLY WITH EA 7-5710-82121, WINGS-STRUCTURE- REPAIR OF CENTER SECTION LOWER SKIN CORROSION. COMPLIED WITH EA 7-5710-82121 WINGS STRUCTURE REPAIR OF CENTER SECTION LOWER SKIN CORROSION THIS IS A MAJOR REPAIR RII:497236.

Part: RIB — CRACKED (LT WING) · airframe 40,759 hrs · 26,000 cycles

NR 2 FLAP TRACK CENTER FAIRING AFT FORMER IS CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-30-2

Part: STIFFENER — CUT (RT WING) · airframe 40,759 hrs · 26,000 cycles

RT WING NR 5 FLAP TRACK FAIRING STIFFNER IS CUT. REMOVED AND REPLACED STIFFNER IAW SRM 51-30-2

Part: FAIRING — CRACKED (RT WING) · airframe 40,759 hrs · 26,000 cycles

NR 8 FLAP TRACK MOVABLE FAIRING HINGE FITTING IS CRACKED. REPLACED FLAP TRACK FAIRING ON WC 76C001-04

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,759 hrs · 26,000 cycles

PREVIOUS REPAIR AT STA 400 BETWEEN 5L AND 6L IS A MAJOR REPAIR IAW SRM 53-30-3 FIG 1.

Part: DRAIN LINE — CRACKED (NR 1 ENG FUEL) · airframe 40,759 hrs · 26,000 cycles

NR 1 ENGINE FUEL FEED SHROUD DRAIN LINE IS CRACKED STA 870 LT MLG WW. REMOVED AND REPLACED DRAIN LINE IAW MM 20-10-005-4.

Part: LONGERON — CRACKED (NR 2 ENG COWL) · airframe 40,759 hrs · 26,000 cycles

NR 2 LT FWD ENG COWL IS CRACKED IN THE LOWER FRAME ABOVE EACH ALIGNMENT PIN. REMOVED AND REPLACED LONGERON (FRAME.)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,759 hrs · 26,000 cycles

FRAME AT STA 303 NEAR 16L IS CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW SRM 51-30-2.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 40,759 hrs · 26,000 cycles

NR 1 ENGINE UPPER COWL INNER AND OUTER SKIN IS CRACKED. REPLACED UPPER COWL TO BE INST ON WC 74C101-01.

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 40,759 hrs · 26,000 cycles

PREVIOUS REPAIR AT STA 712 TO 724 STR 22L AND 23L IS A MAJOR REPAIR IAW SRM 53-30-3 FIG 1.

Part: CHANNEL — CRACKED (RT WING) · airframe 40,759 hrs · 26,000 cycles

RIGHT WING LOWER T/E PANEL SUPPORT BRACKET CRACKED AT WS 519. REMOVED AND REPLACED CHANNEL IAW SRM 51-30-2.

Part: BULKHEAD — UNKNOWN (CARGO BAY) · airframe 40,759 hrs · 26,000 cycles

PREVIOUS REPAIR AFT PIT AT 1183 BULKHEAD IS A MAJOR REPAIR IAW EO 7-5310-7-2344.

Part: SKIN — UNKNOWN · airframe 40,759 hrs · 26,000 cycles

REPAIR LOCATED ON FUSELAGE AT NR 1 ENGINE, PREVIOUS REPAIR AT FS 1243 BELOW NR 1 PYLON NEEDS ENG EVALUATION TO DETEMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING NEEDED. THIS IS A MODIFICATION INSTALLED IAW DRAWING B27-53-020. THIS IS A MAJOR MODIFICATION IAW GMM 6-2-100.

Part: FLOORBEAM — UNKNOWN (CABIN) · airframe 40,759 hrs · 26,000 cycles

REPAIR ON FLOORBEAM AT STA 1130 BL 0 THRU RBL 18, PREVIOUS REPAIR AT STA 1130 , BL 0 TO RBL 18 NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING NEEDED. THE REPAIR IS WAS INSTALLED IAW SRM 53-10-8 AND IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: SKIN — UNKNOWN · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

REPAIR LOCATED AT APPROX BS 1140 TO 1183 STR 21L TO 23L, PREVIOUS REPAIR AT STA 1140 TO 1183 STR 21L TO 23L NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING EVALUATION REQUIRED. REPAIR HAS BEEN COMPLIED WITH IAW SRM 53-30-3 FIG 3A, THIS IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: FLOORBEAM — CRACKED (MAIN CARGO BAY) · airframe 40,759 hrs · 26,000 cycles

MAIN CARGO DECK FLOORBEAM STA 312 LBL 32 SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-2.

Part: SKIN — UNKNOWN (NR 6 SLAT) · airframe 40,759 hrs · 26,000 cycles

RIGHT NR 6 SLAT L/E HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3 FIG 1.

Part: SKIN — UNKNOWN (NR 2 SLAT) · airframe 40,759 hrs · 26,000 cycles

LEFT SLAT NR 2 HAS PREVIOUS REPAIR ON LWR SURFACE THAT IS A MAJOR REPAIR IAW SRM 57-50-3 FIG 1.

Part: SKIN — UNKNOWN (NR 3 SLAT) · airframe 40,759 hrs · 26,000 cycles

LEFT NR 3 SLAT LOWER SURFACE HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3 FIG 1.

Part: FRAME — UNKNOWN · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

REPAIR LOCATED AT APPROX BS 1010 TO 1016 BETWEEN 23L AND 24L, PREVIOUS REPAIR AT STA 1010 TO 1016 BETWEEN STR 23L AND 24L NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW WITH FAA APPROVED DATA. NO ENGINEERING NEEDED. THIS REPAIR WAS COMPLETED IAW SRM 53-10-4, THIS IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: SKIN — UNKNOWN (NR 3 SLAT) · airframe 40,759 hrs · 26,000 cycles

LEFT NR 3 SLAT L/E LOWER SKIN INBOARD OF INBOARD TRACK HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3.

Part: SKIN — UNKNOWN · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

REPAIR LOCATED ON FUSELAGE AT NR 3 ENG, PREVIOUS REPAIR AT STA 1243 BELOW NR 3 PYLON NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVE DATA.

Part: SKIN — UNKNOWN (NR 8 SLAT) · airframe 40,759 hrs · 26,000 cycles

RIGHT NR 8 SLAT L/E HAS A PREVIOUS REPAIR THAT IS A MAJOR REPAIR IAW SRM 57-50-3.

Part: SKIN — UNKNOWN · airframe 40,759 hrs · 26,000 cycles

REPAIR LOCATED ON FUSELAGE AT NR 3 ENG, PREVIOUS REPAIR AT STA 1243 BELOW NR 3 PYLON NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVE DATA. NO ENGINEERING NEEDED. THIS IS A MODIFICATION COMPLETED BY DRAWING B27-53-020 REV D. THIS IS A MAJOR MODIFICATION IAW GMM 6-2-100.

Part: VERTICAL BEAM — UNKNOWN · airframe 40,759 hrs · 26,000 cycles

REPAIR ON VERTICAL BEAM AT STA 1183, RBL 36.83, WL 230, PREVIOUS REPAIR NEEDS ENG EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IAW FAA APPROVED DATA. NO ENGINEERING ASSISTANCE NEEDED. THIS IS A MODIFICATION COMPLIED WITH PER DRAWING 65C29080. THIS IS A MAJOR REPAIR/ MODIFICATION PER GMM 6-2-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,759 hrs · 26,000 cycles

PREVIOUS REPAIR AT STA 251 TO 267 STR 17L TO 18L IAW SRM 53-30-3 IS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (LWR CARGO BAY) · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

PREVIOUS REPAIR AT STA 1050 FLOORBEAM AT BL 0 IS IAW SRZ 27-53-034E AND IS A MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,759 hrs · 26,000 cycles

PREVIOUS REPAIR AT STA 460 TO 470 STR 10L TO 11L IS IAW SRM 53-30-3 AND IS A MAJOR REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

PREVIOUS REPAIR STA 1114 TO 1138 STR 21R TO 22R HAS BEEN FOUND TO BE IAW EA 7-5330-52176 AND IS A MAJOR REPAIR.

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 40,759 hrs · 26,000 cycles

PREVIOUS REPAIR AT STA 243 TO 280 BTWN STR 21L AND 23L IS IAW SRM 53-30-3 AND IS A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (MAIN CARGO DECK) · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

PREVIOUS REPAIR AT STA 1070 BL 0 TO RBL 65 ON FLOORBEAM IS IAW SRM 53-10-8 AND IS A MAJOR REPAIR.

Part: RIB — CRACKED (LT WING SLAT) · airframe 40,759 hrs · 26,000 cycles

LT WING NR 3 SLAT INTERNAL STRUCTURE AT O/B ACTUATOR MOUNTING SUPPORT RIB CRACKED. REMOVED AND REPLACED SUPPORT RIB IAW SRM 51-40-3 FIG 1.

Part: LONGERON — CRACKED (NR 2 NACELLE) · airframe 40,759 hrs · 26,000 cycles

NR 2 ENG RT AFT COWL AFT LOWER CORNER IS CRACKED. REMOVED AND REPLACED FRAME IAW SRM 51-30-2.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

STRINGER 28R IS CORRODED AT STA 480. REMOVED AND REPLACED STRINGER SPLICE AT STA 480 STRINGER 28R IAW SRM 53-10-3 FIG 1.

Part: SEAT TRACK — UNKNOWN (MAIN CARGO) · airframe 40,759 hrs · 26,000 cycles

SEAT TRACK BL 0 STA 360-480 REQUIRES EXTENSION FOR EO 7-5340-7-5002. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2 MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

PHANTOM SEAT TRACK STA 740-757.5 LBL-45 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

MCD SEAT TRACK HAS CORROSION BS 870 TO 950 RBL 26. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 40,759 hrs · 26,000 cycles

MCD SEAT TRACK STA 1140-1176 BL-0 HAS CORRODED AREAS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.

Part: BUMPER BLOCK — CRACKED (FWD LWR CARGO) · airframe 40,759 hrs · 26,000 cycles

FORWARD LWR CARGO DOOR HANDLE BUMPER STOP BRACKET IS CRACKED. REMOVED AND REPLACED BUMPER IAW SRM 51-30-2.

Part: DEPRESSOR — CRACKED (NR 5 SPOILER) · airframe 40,759 hrs · 26,000 cycles

LEFT WING UPPER T/E ACCESS PANEL SUPPORT PLATE O/B OF NR 5 SPOILER IS CRACKED. REMOVED AND REPLACED PLATE IAW SRM 51-30-2.

Part: WEB — CRACKED (LT HORZ STAB) · airframe 40,759 hrs · 26,000 cycles

LEFT SIDE OF HORIZONTAL STAB REMOVABLE SPAR WEB IS CRACKED IN 3 SPOTS. REMOVED AND REPLACED WEB IAW SRM 51-30-2.

Part: CYLINDER — DAMAGED (HYD SYSTEM) · airframe 40,547 hrs · 25,837 cycles

WITH FLAPS SET AT 15 DEG, WHEN LANDING GEAR PLACED FROM OFF TO DOWN, A SYS HYD PRESSURE WENT TO ZERO, A HYD QUANTITY WENT TO ZERO. RAN QRH PROCEDURES. LEFT AND RIGHT MAINS WERE GREEN, NOSE GEAR INDICATING UP PRIOR TO RUNNING CHECKLIST. MANUALLY EXTENDED GEAR AND LANDED UNEVENTFULLY. SYS A FLUID SHUTOFF. SWITCHES CLOSED W/ENGINES RUNNING FOR 20 MINUTES. INSPECTED A/C AND FOUND NLG HYD TRANSFER CYCLINDER SEPARATED INTO TWO PIECES, NLG W/W AREA COVERED IN HYD FLUID. R & R NOSE GEAR HYD TRANSFER CYCLINDER. PER 727 MM 32-35-01-4, C/W STEPS 1-4C REQ STEPS 4D, E, AND F.

Part: LIGHT — MALFUNCTIONED (WARNING SYS) · airframe 39,416 hrs · 25,023 cycles

AFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT CLIMBING THROUGH 18,000 AT 310 KTS. LIGHT REMAINED ON 30 MINUTES, EXTINGUISHED ONCE DESCENDED AND SLOWED TO LAND. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 26MAR04, MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP.

Part: WARNING LIGHT — INOPERATIVE (AIRSTAIR DOOR) · airframe 39,381 hrs · 24,990 cycles

AFT AIRSTAIR LIGHT ILLUMINATED ON S/O PANEL. COMPLETED QRH. LIGHT WENT OUT AFTER 15 MIN. MEL 24FEB04 06:03 AC RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 05MAR04 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP.

Part: FLAP — OUT OF RIG (WING) · airframe 39,117 hrs · 24,777 cycles

UPON TAKEOFF WHILE RETRACTING THE FLAPS FROM 5 DEGREES TO 2, BOTH FLAP INDICATIONS STUCK BETWEEN 5 AND 2 AND INTRANSIT LIGHT SHOWED AMBER, THE S/O'S VERIFICATION PANEL SHOWED ALL LED'S DOWN. AFTER APPROX 5 MIN THE LED'S RANDOMLY SEQUENCED TO 2, 3, 6, 7 AND INTRANSIT LIGHT CHANGED TO GREEN, THE FLAP GAUGE NEVER MOVED FROM THE STUCK POSITION BETWEEN 2 DEGREES AND 5. REFERENCED THE QRH. THE FLAP HANDLE WAS DIFFICULT TO MOVE DURING BOTH RETRACTION AND EXTENSION. THE FLAPS EXTENDED NORMALLY TO 5 DEGREES AND THEN ALL THE WAY TO FLAPS 30 ON THE RETURN. RIGGED FLAPS PER MM 27-51-00-2. SPOILER RIG ACCOMPLISHED IAW MM 27-61-005-2. AILERON RIG CHECK ACCOMPLISHED IAW MM 27-10-000-5 AND WO 24672.

Part: POSITION SWITCH — INOPERATIVE (NLG) · airframe 39,037 hrs · 24,718 cycles

NOSE GEAR UNSAFE LIGHT CAME ON AND FLICKERED DURING T/O ROLL WITH A STEADY GREEN. NOSE GEAR DOWN AND LOCKED LIGHT DOORS LIGHT AND S/O NOSE GEAR DOOR LIGHT REMAINED OFF ALL LIGHTS WENT OUT NORMALLY DURING GEAR RETRACTION. OKAY ON LANDING. REMOVED NOSE GEAR POSITION SWITCH C/P FOR TROUBLESHOOTING. REMOVED AND REPLACED NOSE GEAR POSITION SWITCH AS A PRECAUTION IAW 727-200 M/M 32-61-071-4 STEPS 2A-B- AND C(3). AIRCRAFT STILL REQUIRES JACK AND GEAR SWING IAW STEP 2C(4). JACKED ACFT AND C/W 727-200 M/M 32-61-071-4 STEP 2C-(4) AND (5). CYCLED GEAR SEVERAL TIMES ALL INDICATIONS NORMAL. NO DEFECTS NOTED AT THIS TIME.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 38,943 hrs · 24,637 cycles

AFTER LANDING GEAR RETRACTION, RT MLG DOOR LIGHT REMAINED ILLUMINATED (F/O PANEL+S/O PANEL). RECYCLED GEAR PER RED TABS BUT LIGHT REMAINED ILLUMINATED. R/R RT MLG DOOR WARN SWITCH. R/R CONNECTORS D752 & D4660P.

Part: SMOKE DETECTOR — FALSE INDICATION (MAIN CARGO DECK) · airframe 38,755 hrs · 24,489 cycles

MAIN CARGO SMOKE LIGHT NR 4 CAME ON WITH ASSOCIATED ALARM WHILE ON FINAL APPROACH. LIGHT EXTINGUISHED ON ITS OWN AFTER APPROX. I MINUTE. COMPLIED WITH RED TABS AND LANDED UNEVENTFULLY. INTIAL MAIN DECK ( PRE-OFFLOAD ) INSPECTION REVEALED NO SMOKE, FUMES, OR ODOR. DOWN LOADED & CHECKED ALL CONTAINERS NO PROBLEMS FOUND, PERFORMED CARGO SMOKE OPS CHECK PER M/M 26-16-001-5, CHECK GOOD, NOTE: DRY-ICE SHIPPED IN POSITIONS 7 & 8 SUSPECTED CAUSE.

Part: SMOKE DETECTOR — INOPERATIVE (MAIN CARGO) · airframe 38,732 hrs · 24,471 cycles

INFLT RECEIVED MAIN CARGO SMOKE ALARM SEC NR 3 C/W RED TABS AND LIGHT EXT. A/C RECEIVED TO GATE NO FIRE OR SMOKE NOTED AT ARRIVAL. INSPECTED MAIN CARGO DECK SEC NR 3 NO INDICATIONS OF FIRE .CAN AYY 5070 HAD APPX 180 LBS OF DRY ICE MED EQUIP AT SECTION NR 3 RT. PERF M.C. SMOKE DET SYS ADJ/TEST PER M.M. 26-16-001-5 OP'S CK'S NORMAL. R&R NR 3 SMOKE DET AS A PREC. PER M.M. 26-16-001-4, SYS OP'S CK'S OK PER M.M. 26-16-001-5.

Part: SMOKE DETECTOR — MALFUNCTIONED (MAIN CARGO) · airframe 38,731 hrs · 24,470 cycles

INFLIGHT RECEIVED MAIN CARGO SMOKE ALARM IN SECTION NR 3 COMPLIED WITH RED TABS AND LIGHT EXTINGUISHED. A/C RECEIVED INTO GATE NO FIRE OR SMOKE NOTED AT ARRIVAL. INSPECTED MAIN CARGO DECK SECTION NR 3, NO INDICATION OF FIRE ANYWHERE. DEMI CAN AYY 5070 HAD APPX 180 LBS OF DRY ICE FOR MEDICAL EQUIPMENT AT SECTION NR 3 RT. PERFORMED MC SMOKE DETECTION SYS ADJ/TEST PER MM 26-16-001-5, OP'S CHECKS NORMAL. REMOVED AND REPLACED NR 3 SMOKE DETECTOR AS A PRECAUTIONARY PER MM 26-16-001-4, SYS OPS CHECKS NORMAL PER MM 26-16-001-5.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,466 hrs · 24,281 cycles

AFT CARGO BAY BS 950C, STR 26L IS DENTED IN UPPER FLANGE. NO DENTS ALLOWED IN FRAMES. DETERMINED OUT OF LIMITS IAW SRM 53-10-1. REMOVED DENTED MATERIAL AT BS 950C, STR 26L, IAW SRM 51-40-3 FIG 1. SSI INSPECTION PERFORMED IAW BOEING D6-48040-1. FABRICATED, DRILLED, COUNTERSUNK, ALODINED, PRIMED AND INSTALLED REPAIR PART IAW SRM 51-40-3 FIG 1.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,466 hrs · 24,281 cycles

AFT CARGO BAY BS 950F FRAME IS DENTED ABOVE STR 26L. FOUND FRAME OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED SECTION OF FRAME, AND REPAIRED WITH DOUBLER. WORK DONE IAW SRM 51-40-3 FIG 1. REMOVED DAMAGED AREA OF FRAME FED-EX EA 7-5310-68168.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 38,466 hrs · 24,281 cycles

AFT CARGO BAY UPPER FRAME FLANGE PUNCTURED, STA 1130 RBL 21. REPAIRED PUNCTURED FRAME IAW SRM 53-10-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,466 hrs · 24,281 cycles

CORROSION ON FLOORBEAM LOWER CHORD UPPER SURFACE STA 1130, RBL 4, WL 201. REMOVED CORROSION ON FLOORBEAM LOWER CHORD UPPER SURFACE BS 1130, RBL 1-RBL 8, WL 201, IAW SRM. 100 PERCENT MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED LOWER FLANGE OF FLOORBEAM IAW SRM.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,466 hrs · 24,281 cycles

AFT CARGO BAY BS 1130 FRAME IS DENTED AT LBL 27 UPPER FLANGE. DENT IN FRAME BS 1130 AFT CARGO BAY LBL 27 UPPER FLANGE TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER IAW SRM 53-10-1, SRM 51-30-2, SRM 51-40-3 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,466 hrs · 24,281 cycles

CORROSION ON FLOORBEAM LWR CHORD UPPER SURFACE STA 1130 RBL 4 WL 201.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,466 hrs · 24,281 cycles

FRAME CRACKED IN THE FWD CARGO BAY STA 660 RBL 3 WL 148 UNDER FLOOR SUPPORT. FWD CARGO FRAME CRACKED AT BS 660 RBL 3 WL 148 OUT OF LIMITS PER SRM 53-10-4. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,466 hrs · 24,281 cycles

FRAME CRACKED IN THE FWD CARGO BAY. REMOVED DAMAGED FRAME FLANGE. FABRICATED, & INSTALLED REPAIR PARTS IAW SRM 51-40-3 FIG 1.

Part: SWITCH — FAULTY (L/E FLAP) · airframe 38,064 hrs · 23,979 cycles

DURING FLAP RETRACTION FROM 15 TO 5 L/E FLAP INDICATOR WENT FROM GREEN TO AMBER. S/O LED POSITION INDICATORS SHOWED NR 6 LED RETRACTED. CYCLING FLAPS CHANGED NOTHING. LANDED WITH FLAPS 30 WITH A L/E FLAP AMBER WITH NR 6 INDICATING RETRACTED. REPLACED NR 6 LEADING EDGE FLAP POSITION INDICATING SWITCH IAW M/M 27-82-001-4. OPS CHECKS GOOD.

Part: ENGINE — FAULTY (NR 1)

ON CLIMBOUT NR 1 LOW OIL PRESS LIGHT ILLUM. ENG SHUTDOWN. REMOVED AND REPLACED NR 1 ENG PER W/C 70T0001-01.

Part: PLUG — LOOSE

01-341 AFT T/O WHEN RETRACT GEAR S/O ANNUN PNL LIGHTS OUT. RECONNECTED LOOSE PLUG P4270.

Part: HINGE — GOUGED (CARGO DOOR)

TOP HINGE AT MID POINT HAS A HINGE LOBE W/DEEP GOUGE GROOVE IN IT. REMOVED AND REPLACED HINGES PER DWG B72-53-070 & EA 7-5230-59057 & EO 7-5230-7-5000.

Part: HINGE — CHAFED (CARGO DOOR)

TOP FWD HINGE SEGMENTS ARE RUBBING HARD, DOOR SIDE AND FUSELAGE SIDE.

Part: HINGE — DAMAGED (DOOR)

HINGE HAS SEVERAL LOBES ON DOOR AND ACFT WITH ELONGATED HINGE PIN HOLES. REMOVED AND REPLACED PER EA 7-5230-59057 & EO 7-5230-7-5000.

Part: VALVE — FAILED (A/C BAY)

LEFT PACK INOP. CARGO HEAT OUTFLOW VALVE CLOSED. AC UNABLE TO MAINTAIN PRESS. REMOVED AND REPLACED LEFT PACK VALVE. OPS CHECK NORM OF BOTH LEFT AND RIGHT PACK PRESS AC NORMAL. REMOVED PLACARD TO THE LEFT PACK.

Part: VALVE — FAILED (A/C BAY)

ON CLIMBOUT WITH BOTH PACKS ON CABIN BEGAN TO CLIMB TO 10,000 FT. STARTED A DESCENT, A/C REMAIN UNPRESSURIED UNTIL LAND. *S/D* REMOVED AND REPLACED LT PACK VALVE. OPS CK OF BOTH PACK LT & RT PRESS. AC NORMAL ON GROUND AS PER MM. REMOVED PLACARD.

Part: SWITCH — INOPERATIVE (NLG)

00-45 - UNSAFE GEAR LIGHT ILLUMINATED ON FINAL, ACCOMP BY AURAL WARN HORN. REMOVED AND REPLACED DOWN LOCK SWITCH PER MM 32-61-071-4. OPERATIONAL CK NORM.

Part: CONTROL — LEAKING (RT ELEVATOR)

INFLIGHT LOSS OF A-SYSTEM HYDRAULIC. HYDRAULIC FLUID SHUTOFFS CLOSED FOR 52 MINUTES. *S/D* REPLACED RIGHT ELEVATOR POWER CONTROL PACKAGE PER M/M 27-30-81. REPLACED A-SYSTEM PRESSURE AND CASE DRAIN FILTERS PER M/M 29-11-10, PAGE 102. NO METAL FOUND. OPERATIONAL CHECKS AND LEAK CHECKS GOOD. REMOVED GEAR PINS. DOWNGRADED CAT STATUS TO CHECK CAT II A/C STATUS IS NOT CAT II.

Part: ENGINE — DAMAGE (NR 1)

LOUD BANG HEARD IN CRUISE. NR 1 ENGINE STABILIZED IN CRUISE AT 20 PERCENT N1-0 OIL PRESSURE, BUT QUANTITY OK (71-00-1749). NR 1 ENGINE REPLACED, NOW READY FOR POWER 1 LEAK CHECK RUN. EVIDENCE OF DAMAGE TO TOP OF GEAR BOX, INDICATING SUDDEN STOPPAGE. NR 1 ENGINE REMOVED AND REPLACED PER W.C. NR 70T001, AND W/C NR 72T0301 AND J.R.H. OPS CK NORMAL, OK FOR SERVICE. ENG OFF S/N 689919, JT8D-17 ENG ON S/N 709283, JT8D-17A.

Part: MODULE — LIGHT INOP (LT MLG)

WHEN GEAR LEVER DOWN, LEFT MAIN GREEN DOWN AND LOCK LIGHT DID NOT ILLUMINATE AND OTHER LIGHTS OK. RECYCLED GEAR, THREE GREEN DOWN AND LOCKED LIGHTS OK. FOUND LEFT GEAR LIGHT INOPERATIVE. REPLACED LANDING GEAR MODULE, OPERATIONAL CHECK GOOD.

Part: RIB — CRACKED (WS 760)

STA 760 R/RIB CHORD HFEC CRACK INDICATION FROM FWD HOLES. INSTALLED REPAIR DOUBLER PER BOEING DRAWING 63-68490.

Part: BOLTS — MISINSTALLED (RT RIB)

THREE EACH BOLTS WERE INSTALLED THROUGH HORIZONTAL FRAME BL 70.5, RT RIB CHORD REPAIR FOR EO 7-5710-7-2308 PART 3, BUT NOT PER EO (EO CALLS FOR 3 EACH HI-LOKS INSTEAD). ACQUIRED ESO 11782 DATED 10/24/95 TO ALLOW STO/S BOLTS TO BE INSTALLED, AWAITING EA NR.

Part: FLOORBEAM — CORRODED (BS 400)

FLOORBEAM HEAVY CORROSION ON STA 400 RBL 35 BOTTOM SIDE NR 0360. INSTALLED DOUBLER PER SRM 53-10-8, SEE NR 1032.

Part: FLOORBEAM — CORRODED (BS 480)

HEAVY CORROSION ON FLOORBEAM AT STA 480, JUST I/B OF SEAT T-RACK RBL 25. REMOVED CORRODED AREA AND INSTALLED FILLER AND ANGLES PER SRM 53-10-8 FIG 8.

Part: FLOORBEAM — CRACKED (BS 344)

CRACK IN FLOORBEAM AT STA 344 AT LBL 29.5 FROM CENTER AFT FLANGE. REPAIRED PER SRM 53-10-8.

Part: FRAME — CRACKED (BS 540)

CRACK IN UPPER RADIUS OF FWD CARGO FLOOR FRAME STA 540 RBL 3. STOP DRILLED CRACK, INSTALLED DOUBLER AT FLOOR FRAME STA 540 RBL 3 PER SRM 51-40-3.

Part: BULKHEAD — CRACKED (BS 1183)

AFT CARGO RT 1183 BULKHEAD CRACKED HORIZONTAL ANGLE JUST BELOW FLOOR LINE RBL 50. REMOVED DAMAGED PART, INSTALLED NEW ANGLE PER SRM 51-10-1.

Part: BLKHD ANGLE — CRACKED (BS 1183)

AFT CARGO RT 1183 BULKHEAD CRACKED HORIZONTAL ANGLE JUST BELOW FLOOR LINE RBL 50. REMOVED DAMAGED PART AND INSTALLED NEW ANGLE PER SRM 51-10-1.

Part: SENSOR — FAILED (RT MLG)

DURING T/O WITH WEIGHT OFF LDG GEAR, LDG GEAR LEVER LATCH FAILED TO RELEASE, CB ON P6-3 WERE IN. UPON RETRACTING FLAPS IAW CHECKLIST FROM 5 TO 2 DEGREES, RECEIVED A T/O WARNING HORN. GEAR REMAIN DOWN ON THE GRD, RT MAIN IND LT FLASHES. REMOVED AND REPLACED BOTH AIR AND GROUND SENSING SENSORS (M831, M832), IAW MFG MM 32-0-221. OPS TESTED GOOD AND OK FOR RETURN TO SERVICE. OFF (PN 1899-15), ON (SN 163996), POS AIR REA 02.