N315AS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,305 hrs · 27,758 cycles

AFT EMERGENCY EXIT LIGHT COVER MISSING. GROUNDED - YES. AFT EMERGENCY EXIT LIGHT COVER ON LAV D REPLACED REF AMM 33-51-14. OP TESTS PASS.

Part: BATTERY PACK — INOPERATIVE (MAIN CABIN) · airframe 68,303 hrs · 27,757 cycles

DURING COMPLETION OF TC 78233001 LH & RH OVER-WING EMERGENCY EXIT LIGHTS FAILED TO REMAIN ON FOR 15 MINUTES MINIMUM. GROUNDED - YES. REPLACED EMERGENCY LIGHTS RH POWER SUPPLY AND BATTERY PACK, AND LH BATTERY PACK M1695, M1694 REF AMM 33-51-06 AND WDM 33-51-13-3, OPS NORMAL.

Part: TIRE — DEFLATED (NLG) · airframe 68,161 hrs · 27,688 cycles

NOSE WHEEL SHIMMY BETWEEN 60 AND 120 KNOTS ON T/O AND LANDING. GROUNDED - YES. REF AMM 05-51-54 CONDITIONAL INSPECTION TIRE BURST LH NLG TIRE NOTED FOUND PRESSURE @ 200PSI FORWARD E+E BAY DENTED NEAR HANDLE. LH SIDE OF NLG PSEU CONDUIT BRACKETS WIRING AND TUBE BENT. NLG LIGHT ASSY AND TOW PIN ASSY LOOSE. DRAIN MAST FWD RH GEAR WELL INSPECTED NO ENGINE INGESTION OR FLIGHT CONTROL DAMAGE NOTED. 39042 IAN SHICK 09/01/2023. REPLACED TOW FITTING ASSY BOLTS AND NUTS AND INSTALLED TOW FITTING ASSY ON INNER ANGULAR ASSYREF AMM 32-21-14 IAN SHICK 39042. REMOVED TAXI LIGHT ASSY UNBENT CORNER AS REQUIRED RE-INSTALLED TAXI LIGHT ASSY REF AMM 33-45-01 P GARCIA 20465 09/01/2023. WIRE AT LT SIDE CONDUIT WIRE EXPOSED J ELLIOT 07370. REPLACED AIR/GND SENSOR S1014 REF MM 32-09-02, SENSOR BRACKET + CONDUIT TO CONDUIT BOX. SENSOR GAP + OPS CHK GOOD REF SAME MM. 2 EA MIG51A TAGS INSTALLED/REMOVED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,976 hrs · 26,708 cycles

EMERGENCY LIGHT AISLE LIGHT INOP AT ROW 18 LEFT. GROUNDED - YES. RELAMPED AND TESTED IAW AMM 33-51-03-960-801 - OPS NORMAL.

Part: LENS — INCORRECT (EMERGENCY LIGHT) · airframe 65,979 hrs · 26,709 cycles

EMERGENCY LIGHTS LOCATOR EXIT SIGN AT R1 DOOR HAS INCORRECT LENS COVER. GROUNDED - YES. R & R LENS COVER AT R1 DOOR. EMERGENCY LIGHTS OPS CHECK GOOD. IAW AMM 33-51-01-960-801.

Part: WIRE — BROKEN (UNKNOWN) · airframe 65,333 hrs · 26,401 cycles

INTERIOR L1 ENTRY EMERGENCY EXIT LIGHT LOWER DOES NOT ILLUMINATE. GROUNDED - YES. REPAIRED BROKEN GROUND WIRE ON L1 EMERGENCY LIGHT, OPS CHECKS GOOD. IAW B737-900 AMM 33-51-01-960-801 STEP 2C2, B737-900 WDM 33-51-21, BOEING SWPM 20-30-12 STEP 1B PAGE 67. (REF AAR MIG 5 OK320963).

Part: TRANS PANEL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 65,333 hrs · 26,401 cycles

AFT CARGO LH TRANSITION PANEL CORRODED ON UPPER AND LOWER SURFACES. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TRANSITION PNL TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-1A-2 REPAIRED TRANSITION PANEL IAW B737-900 SRM 53-00-53-2R-5W=1.00 O=.040 R=0.00 L=2.00 D=.040.

Part: INTERCOSTAL — CRACKED · airframe 65,333 hrs · 26,401 cycles

FWD WET AREA INTERCOSTAL STA 312 TO 328 RBL 45 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL STA 312-328 AT RBL 45 IAW B737-900 SRM 51-40-02-0G-0.

Part: WEB — CORRODED (AFT CARGO) · corrosion level 2 · airframe 65,333 hrs · 26,401 cycles

AFT CARGO SCUFF PLATE WEB IS CORRODED. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND WEB TO BE OUT OF LIMITS IAW B737-900 SRM 53-60-15-1A-1 REMOVED AND REPLACED WEB IAW B737-900 SRM 51-40-02-0G-0W=.5 O=.050 R=.037 L=1.2 D=.013.

Part: ANGLE — CORRODED (STA 767) · corrosion level 2 · airframe 65,333 hrs · 26,401 cycles

AFT CARGO ANGLE UNDER FWD SHIELD STA 767 TO 787 RBL 21 IS CORRODED. GROUNDED - YES. REMOVED CORROSION ON ANGLE AND DETERMINED OUT OF LIMITS IAW B737-900 SRM 53-60-15-1A-1 INSTALLED NEW ANGLE IAW B737-900 SRM 51-40-02-0G0W=.4 O=.050 R=.038 L=1.2 D=.012.

Part: SPLICE — CORRODED (STA 887) · corrosion level 2 · airframe 65,333 hrs · 26,401 cycles

AFT CARGO FLOOR BOARD SPLICE AT STA 887 IS CORRODED. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND SPLICE TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A-2 REMOVED AND REPLACED SPLICE IAW B737-900 SRM 51-40-02-0G-0W=.5 O=.062 R=.039 L=1 D=.023.

Part: INTERCOSTAL — CRACKED · airframe 65,333 hrs · 26,401 cycles

FWD WET AREA INTERCOSTAL STA 270 TO 294 BL 0 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL STA 270-294 AT BL0 IAW B737-900 SRM 51-40-02-0G-0.

Part: TRANS PANEL — CORRODED (AFT CARGO STA 72) · corrosion level 2 · airframe 65,333 hrs · 26,401 cycles

AFT CARGO RH TRANSISTION PANEL CORRODED UPPER AND LOWER SURFACES. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW B737-900 RM 53-00-53-1A-2 FIG 103 REPAIRED TRANSITION PANEL IAW B737-900 SRM 53-00-53-2R-5W=.5 O=.040 R=0.00 L=1.8 D=.040.

Part: INTERCOSTAL — CORRODED · airframe 65,333 hrs · 26,401 cycles

AFT CARGO BAFFLE AT STA 747 TO 767 RBL 21 IS CORRODED. GROUNDED - YES. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS IAW B737-900 SRM 53-00-53-1A-2. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW B737-900 SRM 51-40-02-0G-0W .5 O .032 R .020 L 1.00 D .012.

Part: SPLICE — CORRODED (727D) · corrosion level 2 · airframe 65,333 hrs · 26,401 cycles

AFT CARGO FLOOR BOARD SPLICE AT STA 727D IS CORRODED. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND SPLICE TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A-2 ORDERED AND RECEIVED NEW SPLICE AND PLACED ON PARTS RACK TO BE INSTALLE DON AAR WO 1020620-1000-0171 SN 8589459W=.5 O=.070 R=.058 L=1.25 D=.012.

Part: RIB — CRACKED · airframe 65,333 hrs · 26,401 cycles

LH HORIZONTAL LE: 3RD RIB FROM INBD END CRACKED. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED RIB IAW B737-900 SRM 55-10-09-2R-4.

Part: TRANS PANEL — CORRODED (500D TO 500K+12) · corrosion level 2 · airframe 65,333 hrs · 26,401 cycles

FWD CARGO RH TRANSITION HAS CORROSION FROM STA 500D TO STA 500K+12 ON UPPER & LOWER SURFACES. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS CUT OUT DAMAGE AND REPAIRED TRANSITION IAW B737-900 SRM 53-00-53-2R-5W=2 O=.040 R=.020 L=6 D=.020.

Part: SPLICE — CORRODED (AFT CARGO 727I) · corrosion level 2 · airframe 65,333 hrs · 26,401 cycles

AFT CARGO FLOOR BOARD SPLICE AT STA 727I IS CORRODED. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND SPLICE OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A-2 ORDERED AND RECEIVED NEW SPLICE AND PLACED ON PARTS RACK TO BE INSTALLED ON AAR WO 1020620-1000-0171 SN 8589459W=.75 O=.070 R=.060 L=2.5 D=.010.

Part: THRESHOLD WEB — CORRODED (FWD CARGO 470) · corrosion level 2 · airframe 65,333 hrs · 26,401 cycles

FWD CARGO LOWER DOOR THRESHOLD WEB HAS CORROSION AT STA 470. GROUNDED - YES. FOUND TO BE EXFOLIATED MORE THAN 50% THROUGH REMOVED AND REPLACED WEB IAW B737-900 SRM 51-40-02-0G-0W=6 O=.045 R=0 L=10 D=.045.

Part: BATTERY PACK — FAILED (PASSENGER CABIN) · airframe 64,590 hrs · 26,060 cycles

CABIN EMERGENCY LIGHTS ON OVERHEAD BINS AT L/H SEAT ROWS 11, 26, AND 29 DO NOT ILLUMINATE. GROUNDED - YES. REMOVED, REPLACED, AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT LIGHTS BATTERY PACK ASSOCIATED WITH M1898 PER B737-900 AMM 33-51-06-960-805.

Part: DOUBLER — CORRODED · corrosion level 2 · airframe 64,590 hrs · 26,060 cycles

CORROSION NOTED ON EXTERNAL FWD ATG4 ANTENNA DOUBLER SKIN APPROXIMATELY BL 0., STA 500B - 500C. GROUNDED - YES. REPAIRED DOUBLER PER ASA EA 900-53EA-24372 REV 00 DATED 05/07/2022.

Part: SKIN — CORRODED · corrosion level 2 · airframe 64,590 hrs · 26,060 cycles

CORROSION NOTED ON EXTERNAL SKIN APPROXIMATELY BL 0, STA 500B - 500C. GROUNDED - YES. REPAIRED PER ASA EA 900-53EA-24372 REV 00 DATED 05/07/2022.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 63,717 hrs · 25,676 cycles

R1 DOOR DIFFICULT TO OPEN, GET STUCK AT MIDWAY POINT WHEN OPENING AND CLOSING INTERMITTENTLY. GROUNDED - YES. OPERATED R-1 DOOR SEVERAL TIMES NO DEFECTS NOTED. OK FOR CONT SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 63,275 hrs · 25,483 cycles

WHILE PERFORMING T.C. # 78233008, FOUND RH AFT OVERWING EXTERIOR EMERGENCY LIGHT INOP. GROUNDED - YES. RELAMPED OVERWING EMER LT IAW AMM 33-51-04-960-801. NO HELP. REMOVED AND REPLACED POWER SUPPLY M1671 IAW AMM 33-51-06-960-806. NO HELP. VERIFIED 6V PRESENT AT ASSEMBLY. BENT LOWER CONTACT UP TOWARDS BOTTOM OF BULB, AND RELAMPED AGAIN. NOW CHECKS GOOD. ALL EMERGENCY LIGHTS FOR ASSY M1671 CHECK GOOD AT THIS TIME.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 61,825 hrs · 24,834 cycles

EMERGENCY EXIT LIGHT LENS COVER L-2 DOOR FELL OFF. GROUNDED - YES. REMOVED & REPLACED L-2 DOOR EMERGENCY EXIT LIGHT ASSY. REF B737-900 AMM 33-51-01-960-802.

Part: LAMP — INOPERATIVE (R2 DOOR SLIDE) · airframe 61,201 hrs · 24,557 cycles

EXTERNAL EMERGENCY LIGHT INOPERABLE AFT OF R2 DOOR. GROUNDED - YES. RELAMPED R2 DOOR EMERGENCY EXIT SLIDE LIGHT, OPS CHECK GOOD, IAW B737-900 AMM 33-51-04-960-801.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 61,201 hrs · 24,557 cycles

RT HORIZ STAB LOWER SKIN IS CRACKED AT STA 129 (MARKED). GROUNDED - YES. CUT OUT CRACK DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER, IAW B737-900 SRM 55-10-01-2R-11 REPAIR 11. ELEVATOR POWER - OFF FLIGHT TEST IS NOT REQUIRED - REPAIR WIDTH LESS THEN 66" IAW B737-900 SRM 55-10-01-2R-11 REPAIR 11 PARA 20.

Part: SNUBBER — ICED (R1 DOOR) · airframe 59,649 hrs · 23,857 cycles

CATERING CREW REPORTS R1 DOOR DIFFICULT TO OPEN. GROUNDED - YES. CLEANED DOOR SEAL & SNUBBER FOUND CONDENSATION & ICE CLEANED MOISTURE & LUBED DOOR - DOOR OPERATES OKAY REF B737-900 AMM 52-41-00.

Part: LENS — DETACHED (CABIN) · airframe 59,150 hrs · 23,609 cycles

R1 EMERGENCY DOOR LIGHT COVER HAS FALLEN OFF. GROUNDED - YES. REPLACED L1186 R1 LIGHT ASSY REF AMM 33-51-01. OPS NML.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,166 hrs · 22,696 cycles

EMERGENCY EVACUATION AISLE LIGHTS AT 28 DEF AND 30 DEF INOP DURING LIGHT TEST. GROUNDED - YES. REPLACED EMERGENCY LIGHT BATTERY PACK M1899. OPERATIONAL TEST PASSES REF AMM 33-51-06-960-806.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,321 hrs · 22,319 cycles

MULTIPLE EMERGENCY LIGHTS INOP THROUGHOUT CABIN. GROUNDED - YES. REMOVED AND REPLACED BATTERY AT SEAT/ROW 7, 16, 23 LT SIDE. AND REPLACED 2 CHARGERS AT SEAT/ROW 7, 16 ABC. ALSO CORRECTED PROVISIONED WIRES AT STATION 642 EXIT LIGHT L1359 FOUND CONNECTED, CAP & STOWED WIRE W1342-0081-16 IAW AMM 33-51-06-960-805 & 33-51-06-960-806 & WDM 33-51-21 OP-CHECK GOOD IAW AMM 33-51-00-720-801.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,321 hrs · 22,319 cycles

MAIN CABIN FLOORBEAM AT STA 360 LBL 8 FASTENER HOLE HAS EVIDENCE OF CORROSION. GROUNDED - YES. REPAIRED FLOORBEAM AT STA 360 LBL 8 IAW SRM 53-10-51-28-13 AND EA 900-53EA-20766 REV 00 DATED 09/25/2018. ORIGINAL THICKNESS IS .200, REMAINING IS .167 , .033 WAS REMOVED. FLOORBEAM FOUND OUT OF LIMITS.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 56,321 hrs · 22,319 cycles

CRACK INDICATION MARKED IN FWD SIDE OF PSI DECK WEB, BS663 I/B LBL 40 - 41, 5" BELOW UPPER CHORD. 1.100" LONG. GROUNDED - YES. CUT AND REMOVED THE DAMAGED LEFT WING REAR SPAR VERTICAL PRESSURE DECK WEB AT BS663, LBL32-LBL48 AND ACCOMPLISHED REPAIR IAW SRM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE 2. THIS REPAIR IS A CATEGORY "B" REPAIR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,321 hrs · 22,319 cycles

LT SIDE FWD ENTRY DOOR FLOOR STRUCTURE INTERCOSTAL CRACK BETWEEN STA 312 AND STA 320. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL REF BAC DWG 141A5400 REV-.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 56,321 hrs · 22,319 cycles

BAFFLE CRACKED AT STA 500K LT SIDE STRINGER 25L. GROUNDED - YES. REMOVED DAMAGED BAFFLE AT STA 500K LT SIDE STRINGER 25L IAW SRM 51-40-02. LOCATED, DRILLED AND INSTALLED NEW BAFFLE PART 143A7503-11 IAW DWG 143A7505 AND SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,321 hrs · 22,319 cycles

LT TRANSITION PANEL IS CORRODED STA 767 TO 807. GROUNDED - YES. REMOVED CORROSION STA 767-807 LT TRANSITION PANEL IAW SRM 51-10-02 MATERIAL ORIGINAL THICKNESS=.040, MATERIAL REMAINING AT AREAS OF GREATEST LOSS=.023, MATERIAL LOSS=.017 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 FIG 103, IAW SRM 53-60-53 FIG 2, TABLE 2. REMOVED LT TRANSITION PANEL STA 727K+12-803+3, FABRICATED PANELS AND SPLICES, ASSEMBLED PANELS, SPLICES AND NUTPLATES AND INSTALLED IAW SRM 53-00-53 REPAIR 5 AND SRM 51-40-03 TABLE II. ALODINED AND PRIMED AREAS OF CORROSION REMOVAL AND FABRICATED PARTS IAW SRM 51-20-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,321 hrs · 22,319 cycles

MAIN CABIN STA 947.5 FLOORBEAM IS CORRODED ON THE UPPER SURFACE FROM LBL 5 TO RBL 10. GROUNDED - YES. REMOVED AND REPLACED DAMAGED REPAIR PARTS REF EA 900-53EA-20727 REV "00" DATED 09/16/2018 NO LIMITS ALLOWED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 53,584 hrs · 21,006 cycles

EMERGENCY LIGHT POWER SUPPLY M1675 AND M1695 BATTERY PACKS FAILED A CAPACITY CHECK. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED THE BATTERY PACK IAW AMM 33-51-06-960-805. OPS NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 53,584 hrs · 21,006 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 7 RIGHT. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW AMM 33-51-03-960-801. OPS NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 52,134 hrs · 20,358 cycles

DURING EMERGENCY LIGHT TEST, FOUND L1 DOOR EXTERIOR LIGHT & OVERHEAD SIGN INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 51,647 hrs · 20,129 cycles

EMERGENCY LIGHT EXIT SIGN ABOVE L-1 DOOR HAS SEVERAL LAMPS INOP. GROUNDED - YES. RELAMPED AND TESTED PER AMM 33-51-01-960-801 - OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,520 hrs · 20,064 cycles

EMERGENCY LIGHT EXIT SIGN AT RIGHT AFT OVERWING EXIT HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW AMM 33-51-01-960-801. OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,520 hrs · 20,064 cycles

EMERGENCY LIGHT EXIT SIGN AT LEFT FORWARD OVERWING EXIT HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW AMM 33-51-01-960-801. OPS NORMAL.

Part: GLOWSTRIP — DETACHED (CABIN) · airframe 51,333 hrs · 19,987 cycles

GREEN STRIPE LIFTING IN FIRST CLASS FLOOR. GROUNDED - YES. REPLACED FLOOR GLOW STRIP.

Part: FLOOR SUPPORT — CRACKED (BS 986-1016) · airframe 51,262 hrs · 19,961 cycles

MAIN CABIN FLOOR SUPPORT LBL 32, BS 986-1005 FOUND TO BE CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT AIW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 51,262 hrs · 19,961 cycles

MAIN CABIN FLOOR SUPPORT FOUND TO BE CORRODED AT BS 957, LBL 50. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: WEB — CRACKED (BS 986-1016) · airframe 51,262 hrs · 19,961 cycles

MAIN CABIN WEB CRACKED BS 992 - 1016, RBL 33 - 42. ACFT GROUNDED. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02 AND DWG #147A5700, REV A.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 51,262 hrs · 19,961 cycles

MAIN CABIN AFT FLOORBEAM CORRODED BS 986.5, BL 0 - RBL 50. ACFT GROUNDED. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-70-51-2R-4 AND EA-18415.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 51,262 hrs · 19,961 cycles

MAIN CABIN AFT FLOORBEAM PREVIOUS REPAIR TEE CAP CORRODED BS 986.5, LBL 15 - 50. ACFT GROUNDED. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51, THE FLOORBEAM WAS REPAIRED.

Part: STRUCTURE — CORRODED (BS 947) · corrosion level 2 · airframe 51,262 hrs · 19,961 cycles

FOUND RT LOWER INNER STRUCTURE CORRODED AT BS 947.5. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, AND FOUND BEYOND LIMITS IAW SRM 53-70-15. REMOVED THE STRUCTURE IAW SRM 51-40-02, AND INSTALLED IAW DWG 147A8501, REV B.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 51,262 hrs · 19,961 cycles

FOUND THE FLOORBEAM TEE CAP AT BS 947.5 HAS SEVERAL AREAS OF CORROSION BETWEEN LBL 20 TO RBL 20. ACFT GROUNDED. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SM 53-70-51. REPAIRED THE FLOORBEAM TEE REPLACED IAW EA 900-53EA-18413.

Part: FUSE — FAILED (CABIN) · airframe 50,953 hrs · 19,833 cycles

RT FWD OVERWING EXIT OUTSIDE EMERGENCY LIGHT IS INOP. GROUNDED - YES. RELAMPED NO GOOD. CHECK FUSES AT BATTERY PACK CHANGED FUSES PER AMM 33-51-06-960-804. OPS CK'D GOOD.

Part: ATTACH FITTING — CRACKED (BS 500K) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO BAY LEFT INTERCOSTAL ATTACH FITTING IS CRACKED AT BS 500K. ACFT GROUNDED. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-40-02 AND DWG 143A7505 REV B.

Part: FLOOR SUPPORT — CRACKED (BS 500C-500D) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO BAY, FLOOR SUPPORT AT BS 500C TO 500D RBL 21 CRACKED. ACFT GROUNDED. REMOVED AND REPLACED IAW SRM 51-40-02 AND DWG 143A7505.

Part: INTERCOSTAL — CORRODED (BS 767-787) · airframe 50,486 hrs · 19,613 cycles

VERTICLE WEB OF INTERCOSTAL BETWEEN BS 767 - 787, STRINGER 25 - 26R HAS CORROSION. ACFT GROUNDED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1, LOCATED AND DRILLED IAW DWG 146A8123, AND INSTALLED IAW SRM 51-40-02 AND DWG 146A0081 REV A.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,486 hrs · 19,613 cycles

LT HORIZONTAL STAB LWR SKIN HAS CRACK INDICATION STA 101.9 1/B ROW 9" FROM AFT MARKED. GROUNDED - YES. CUT OUT DAMAGED AREA OF LT HOR STAB LWR SKIN AND FABRICATED REPAIR FILLER AND DOUBLER IAW SRM 55-10-01-2R-11. ALODINED AND PRINED IAW SRM 51-20-01. INSTALLED SKIN REPAIR IAW SRM 55-10-01-2R-11. APPLIED TO COAT IAW SRM 51-20-01. INSPECTION THRESHOLD 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION. INSP METHOD IS DETAILED VISUAL INSP AND EXTERNAL LFEC AND INSP INTERNAL IS 9000 FLIGHT CYCLES IAW SRM 55-10-01-2R-11 TABLE 204.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 50,486 hrs · 19,613 cycles

AFT CARGO DOOR INNER SKIN IS CORRODED AT APPROX BS 812, ABOVE LOWER FRAME AT LINER STUD. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 52-30-01-1A-1. FIG 104 DET. E. REPAIRED IAW EA 900-52EA-17868 REV 01, REO-G20334 REV A.

Part: SHIELD — CORRODED (BS 490-500A) · corrosion level 2 · airframe 50,486 hrs · 19,613 cycles

FWD CARGO FLOOR SUPPORT HAS CORROSION BETWEEN BS 490 AND 500A , STRINGERS 25 AND 26R. ACFT GROUNDED. REMOVED CORROSION ON SHIELD IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-30-15 FIG 103. REMOVED AND REPLACED NEW SHIELD IAW SRM 51-40-02 AND DWG 143A0080 REV.

Part: CARGO TRACK — GOUGED (BS 500) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO BAY LT SIDE FLOOR CARGO TRACK GOUGED AT BS 500 ABOVE STRINGER 27L. ACFT GROUNDED. DAMAGE WAS BEYOND LIMITS IAW SRM 53-00-53-1A-2 FIG 103. CUT OUT THE DAMAGED SECTION OF CARGO TRACK BS 460+10 - 500+12, LBL 17 IAW SRM 53-00-53-2R-3, A NEW CARGO TRACK SECTION WAS FABRICATED, LOCATED AND DRILLED IAW SRM 53-00-53-2R-3. ALODINED AND PRIMED IAW SRM 51-20-01 AND INSTALLED IAW SRM 53-00-53-2R-3.

Part: CHANNEL — CRACKED (BS 500E) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO THE LEFT TRANSITION PANEL CRACKED AROUND FATENER AT 500E ABOVE STRINGER 26L. ACFT GROUNDED. REMOVED AND REPLACED IAW SRM 53-00-53, SRM 53-00-53, SRM 53-00-53, ALODINED PART IAW SRM 51-20-01, PRIMED IAW SOPM 20-41-02, AND SRM 53-00-53.

Part: FLOOR SUPPORT — CORRODED (BS 500K-500L) · corrosion level 2 · airframe 50,486 hrs · 19,613 cycles

FWD CARGO FLOOR SUPPORT HAS CORROSION BETWEEN BS 500K AND 500L RBL 14. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 103. REMOVED DAMAGED SECTION OF THE FLOOR SUPPORT.

Part: SUPPORT BRACKET — CRACKED (BS 500F) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO BAY SUPPORT BRACKET CRACKED AT BS 500F, STRINGER 25R. ACFT GROUNDED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (BS 500K) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO BAY LT SIDE TRANSITION SUPPORT ATTACH ANGLE CRACKED AT 500K STRINGER 26L. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505 REV B.

Part: CARGO TRACK — CORRODED (BS 500L) · corrosion level 2 · airframe 50,486 hrs · 19,613 cycles

FWD CARGO BAY , CARGO TRACK HAS CORROSION AT BS 500L STRINGER 27L. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53. REMOVED AND REPLACED THE CARGO TRACK IAW DWG 143A7501, AND SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (BS 500G) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO BAY, SUPPORT BRACKET CRACKED AT BS 500G, STRINGER 25R. ACFT GROUNDED. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-02, DWG 143A1232 REV A, DWG 3143A1232 REV A, AND SRM 51-40-02.

Part: SHIELD — CORRODED (BS 767-787) · airframe 50,486 hrs · 19,613 cycles

AFT CARGO FLOOR SUPPORT HAS CORROSION BETWEEN BS 767 AND 787, STRINGER 25 AND 26R. ACFT GROUNDED. BLEND OUT AREA FOUND OUT OF LIMITS. IAW SRM 53-60-15-1A-1, LOCATED DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW DWG 14A0081-REV A.

Part: STRAP — CORRODED (BS 780-840) · airframe 50,486 hrs · 19,613 cycles

AFT CARGO FLOOR SUPPORT HAS CORROSION BS 793, RBL 20. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. REMOVED STRAP IAW SRM 51-40-02. LOCATED AND DRILLED A NEW STRAP IAW SRM 51-40-05 AND DWG 146A8120 REV E, INSTALLED NEW STRAP IAW SRM 51-40-02 AND DWG 146A8120 REV E. AND 146A0081 REV B.

Part: FLOOR SUPPORT — CORRODED (BS 767-787) · airframe 50,486 hrs · 19,613 cycles

AFT CARGO FLOOR SUPORT HAS CORROSION BETWEEN BS 767 - 787, STRINGER 25 AND 26R. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-40-02 AND DWG 146A0081 REV A.

Part: ANGLE — CORRODED (BS 784) · corrosion level 2 · airframe 50,486 hrs · 19,613 cycles

AFT CARGO BAY ANGLE HAS CORROSION AT BS 784 STRINGER 25R. ACFT GROUNDED. REMOVED AND REPLACED IAW SRM 51-40-02, SRM 51-40-02 AND DWG 146A8320 REV A.

Part: FRAME SPLICE — GOUGED (BS 727L) · airframe 50,486 hrs · 19,613 cycles

AFT CARGO FRAME SPLICE GOUGED BS 727L STRINGER 25R. ACFT GROUNDED. REMOVED AND REPLACED THE FRAME SPLICE IAW SRM 51-40-02, DWG 146A1300 REV G, AND 146A125 REV-.

Part: FRAME — GOUGED (BS 727I) · airframe 50,486 hrs · 19,613 cycles

AFT CARGO BAY RIGHT FRAME GOUGED AT BS 727I BETWEEN STRINGERS 24-25R. ACFT GROUNDED. REPAIRED THE FRAME IAW HAECO REO-G20331 REV B AND ASA EA 900-53EA-17866.

Part: ANGLE — CORRODED (BS 784) · corrosion level 2 · airframe 50,486 hrs · 19,613 cycles

AFT CARGO BAY ANGLE HAS CORROSION AT BS 784 STRINGER 25R. ACFT GROUNDED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-40-02 AND DWG 146A8320 REV A.

Part: CHANNEL — CORRODED (BS 500A-500F) · corrosion level 2 · airframe 50,486 hrs · 19,613 cycles

FWD CARGO FLOOR TRANSITION PANEL HAS CORROSION AT NUMEROUS SPOTS BETWEEN BS 500A AND 500F, STRINGERS 25 AND 26R. ACFT GROUNDED. CORROSION REMOVED AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION PANEL SECTION AND SPLICED IN NEW SECTION IAW SRM 53-00-53-2R-5 AND DWG 14A7500 REV A.

Part: CARGO TRACK — CORRODED (BS 500K-500L) · corrosion level 2 · airframe 50,486 hrs · 19,613 cycles

FWD CARGO TRACK HAS CORROSION BETWEEN BS 500K AND 500L RBL 14. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A FIG 103. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 143A7500 & SRM 53-00-53-2R-3.

Part: WEB — CORRODED (BS 793-847) · corrosion level 2 · airframe 50,486 hrs · 19,613 cycles

AFT CARGO BAY FLOOR SUPPORT WEB WAS CORRODED BETWEEN BS 793 AND 847, RBL 21 AND 29. ACFT GROUNDED. BLENDED OUT AREA AND FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103, DETAIL G. REMOVED OLD WEB IAW SRM 51-40-02. LOCATED DRILLED AND INSTALLED A NEW WEB IAW DWG 146A8340 REV P.

Part: FLOOR PANEL — GOUGED (FWD CARGO) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO FLOOR PANEL 120DF IS GOUGED. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW DRAWING 453A1610-81 REV A. APPLIED ALODINE & PRIMER IAW SOPM 20-41-01 & DRAWING 453A1610 REV T.

Part: FLOOR PANEL — GOUGED (BS 727A-727E) · airframe 50,486 hrs · 19,613 cycles

AFT CARGO FLOOR PANEL 140AF IS GOUGED. ACFT GROUNDED. FABROCATED A NEW FLOOR PANEL IAW DRAWING 453A2610-37 REV D. APPLIED ALODINE & PRIMER IAW SOPM 20-41-01 DRAWIND 453A2610 REV K.

Part: FLOOR PANEL — GOUGED (BS 760-887) · airframe 50,486 hrs · 19,613 cycles

AFT CARGO FLOOR PANEL 140CF IS GOUGED. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW PL453A2610 SHT 10 REV K & DRAWING 453A2610 SHT 11 REV C. APPLIED ALODINE & PRIMED IAW 453A2610 SHT 10 REV K & SOPM 20-41-01.

Part: FLOOR PANEL — GOUGED (BS 727J-767) · airframe 50,486 hrs · 19,613 cycles

AFT CARGO FLOOR PANEL 140BF IS GOUGED. ACFT GROUNDED. ALODINED, FABRICATED, AND PRIMED THE FLOOR PANEL IAW DWG 453A2610 REV F, SOPM 20-41-01 AND 20-41-02.

Part: FLOOR PANEL — GOUGED (BS 500-500D) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO FLOOR PANEL 120CF IS GOUGED. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW DRAWING 453A1610-80 REV A, SOPM 20-41-01 AND DRAWING 453A1610 REV T.

Part: FLOOR PANEL — GOUGED (FWD CARGO) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO FLOOR PANEL 120EF IS GOUGED. ACFT GROUNDED. FABRICATED A NEW CARGO FLOOR PANEL IAW DRAWING 453A1610-83 REV B. APPLIED ALODINE & PRIMER IAW OSPM 20-41-01 & DRAWING 453A1610 REV B.

Part: FLOOR PANEL — GOUGED (AFT CARGO BAY) · airframe 50,486 hrs · 19,613 cycles

AFT CARGO FLOOR PANEL 140EF IS GOUGED. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW DRAWING 453A2610-57 REV C. APPLIED ALODINE & PRIME IAW DRAWING 453A2610-57 REV K, AND SOPM 20-41-01.

Part: FLOOR PANEL — GOUGED (FWD CARGO BAY) · airframe 50,486 hrs · 19,613 cycles

FWD CARGO FLOOR PANEL 120BF IS GOUGED. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL 120BF IAW DRAWING 453A1610 REV T.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,108 hrs · 19,456 cycles

FA REPORTED R2 DOOR LOWER WHITE EXIT SIGN COVER MISSING. ACFT GROUNDED. INSTALLED THE COVER.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,881 hrs · 18,949 cycles

AFT RT EXIT LIGHT COVER MISSING. ACFT GROUNDED. INSTALLED NEW EXIT LIGHT COVER.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 48,438 hrs · 18,767 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT R-2 DOOR HAS BROKEN LENS. ACFT GROUNDED. R & R LENS AND TESTED LIGHT ASSY IAW AMM 33-51-00-960-801. OPS NORMAL.

Part: PUMP — LOW PRESSURE (HYD SYSTEM) · airframe 47,839 hrs · 18,509 cycles

ACFT POWER FELL OFFLINE WHEN SELECTING APU GEN. WHEN RESELECTING GROUND POWER,"A" SYSTEM ELEC HYDRAULIC PUMP INDICATES LOW PRESSURE. ACFT GROUNDED.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 46,419 hrs · 17,923 cycles

RIGHT EXTERIOR AFT OVERWING EMERGENCY LIGHT AND RT FUSELAGE EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. R & R BATTERY PACK AT APPROXIMATELY BS 727C RT, OPS CHECK NORMAL, REF AMM 33-51-06.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,662 hrs · 17,222 cycles

EXIT LIGHT COVER IN SEAT 17F ON WALL MISSING. ACFT GROUNDED. REPLACED COVER PLATE.

Part: PIN — OUT OF ADJUST (OVERWING EXIT) · airframe 42,894 hrs · 16,509 cycles

RIGHT SIDE AFT OVERWING EXIT DOOR DOES NOT OPEN FREELY. ACFT GROUNDED. MADE MINOR VERTICAL STOP PIN ADJUSTMENT IAW MM 52-22-00-820-801 F.5. OPERATED DOOR REF MM 52-22-00-710-801, OPS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,894 hrs · 16,509 cycles

EXIT SIGN NEXT TO L2 DOOR IS MISSING COVER. ACFT GROUNDED. REPLACED EXIT SIGN COVER NEXT TO L-2 DOOR.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 42,122 hrs · 16,221 cycles

L2 DOOR EXIT LIGHT COVER MISSING. ACFT GROUNDED. REPLACED THE L2 DOOR EXIT LIGHT COVER. OPS CHECK GOOD.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 40,807 hrs · 15,714 cycles

EMERGENCY EXIT SIGN FROM LT REAR DOOR MISSING. ACFT GROUNDED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY L1190. EMERGENCY LIGHTS OPS CHECKED NORMAL IAW MM 33-51-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 40,347 hrs · 15,527 cycles

EMERGENCY LIGHT EXIT IDENTIFIER SIGN ON NR 4 GALLEY ADJACENT TO R-2 DOOR HAS BROKEN LENS. ACFT GROUNDED. R & R LENS AND TESTED SIGN IAW MM 33-51-01-960-801. OPS NORMAL.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 39,975 hrs · 15,381 cycles

MISSING EXIT SIGN COVER NEAR FLOOR AT SEAT 17A. ACFT GROUNDED. INSTALLED SERVICEABLE EXIT SIGN COVER, REF AMM 33-51-01.

Part: LENS — DISLODGED (PAX CABIN) · airframe 39,484 hrs · 15,215 cycles

EMERGENCY EXIT SIGN LENS FELL OFF 16F. ACFT GROUNDED. SECURED EXIT SIGN LENS REF EA 900-33EA-10710.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 43,718 hrs · 16,833 cycles

NR 3 SLAT LOVER SURFACE AT ACTUATOR ATTACH POINT HAS CRACK EMINATING FROM 1 EA FASTENER. ACFT GROUNDED. REPAIRED NR 3 SLAT LOWER SURFACE AT ACTUATOR ATTACH POINT IAW SRM 57-42-01-2R.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 43,718 hrs · 16,833 cycles

NR 6 SLAT LOWER SURFACE AT ACTUATOR ATTACH POINT HAS A CRACK COMING FROM A FASTENER. ACFT GROUNDED. REPAIRED DAMAGE TO NR 6 SLAT IAW SRM 57-42-01-2R-8, REPAIR 8 NOTIFIED, SEAM C.

Part: PLATE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 37,942 hrs · 14,635 cycles

AFT CARGO BAY RT SIDE PLATE FOUND TO HAVE CORROSION. REMOVED CORROSION ON LOWER SIDEWALL SUPPORT AS REQUIRED IAW ARM 53-00-53 IN 4 AREAS. 4 OF 4 AREAS FOUND TO BE OUT OF LIMITS USING UT GUAGE T8225Y IAW SRM 53-00-53. REMOVED FLOOR PANEL 140BF AS REQD IAW SRM 51-40-02. REMOVED LOWER SIDEWALL SUPPORT IAW SRM 51-40-02 RECEIVED NEW SIDEWALL SUPPORT AND REPAIR SPLICE IAW BAC DWG 1496-377. LOCD, DRILLED, COUNTERSUNK HOLES IAW SRM 51-40-02. ALODINED, PRIMERED, AND PAINTED IAW SRM 51-20-01 AND SRM 51-21-10. INSTALLED NEW LOWER SIDEWALL SUPPORT IAW SRM 51-40-02 CICD AREA IAW SRM 53-00-53. REINSTALLED FLOORBOARD IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 37,942 hrs · 14,635 cycles

CABIN FLOOR SUPPORT CRACKED BS 344-360, LBL 10. R & R INTERCOSTAL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 37,942 hrs · 14,635 cycles

CABIN FLOOR SUPPORT CRACKED, BS 344-360, BL 0. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 37,942 hrs · 14,635 cycles

CABIN FLOOR SUPPORT CRACKED BS 344-360, LBL 10. R & R CABIN FLOOR SUPPOR IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 37,942 hrs · 14,635 cycles

FLOORBEAM CORRODED BS 986, LBL.4 TO RBL 38. FABRICATED REPAIR PARTS IAW SRM 53-00-51, REPAIR 1, ALODINED IAW SRM 51-20-01, PRIMED IAW SOPM 20-41-02, PAINTED IAW SOPM 20-41-02 AND AMM 51-21-00. INSTALLED REPAIR PARTS IAW SRM 53-00-51.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 37,942 hrs · 14,635 cycles

FLOORBEAM BS 986, LBL.20 TO 40 CORRODED. FABRICATED REPAIR PARTS IAW SRM 51-20-01. PRIMED IAW SOPM 20-41-02. PAINTED PREAIR PARTS IAW SOPM 20-41-02, AMM 51-21-00 INSTALLED REPAIR PARTS IAW SRM 53-00-51, REPAIR 1.

Part: SILL — CORRODED (BS 270-630) · airframe 37,942 hrs · 14,635 cycles

R1 DOOR LOWER SILL CORRODED AROUND FASTENER HOLES. ACFT GROUNDED. R & R CHORD IAW SRM 51-40-02 & BAC DWG 141A8310, REV B.

Part: INTERCOSTAL — CRACKED (BS 277-294) · airframe 37,942 hrs · 14,635 cycles

CABIN FLOOR SUPPORT CRACKED, BS 277-294, BL0. R & R CABIN FLOOR SUPPORT IAW SRM 51-40-02.

Part: SEAT TRACK — BROKEN (BS 727B-727D) · airframe 37,942 hrs · 14,635 cycles

MAIN CABIN SEAT TRACK HAS BROKEN OFF SCALLOPS BS 727C 6, RBL 45.5, WL 207.5. ACFT GROUNDED. ALL WORK ACCOMPLISHED FOR SEAT TRACK REPAIR IAW ASA EA 900-53EA-09737, REV NEW DATE ISSUED 05 FEB 2013 IAW REO G15891, REV B 02-05-2013. THIS IS A TIME LIMIT REPAIR, SEAT TRACK REPAIR TO BE REPLACED AT 24 MONTHS.

Part: INTERCOSTAL — CRACKED · airframe 37,942 hrs · 14,635 cycles

MAIN CABIN FLOOR SUPPORT CRACKED BS 328 -BS 344, LBL 47. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 297-312) · airframe 37,942 hrs · 14,635 cycles

MAIN CABIN FLOOR INTERCOSTAL CRACKED BS 294 - 312, BL 0. PERFORMED HFEC IN SUSPECT AREA IAW NTM PR6 51-00-00, PROD 23 TOD T8151A VERIFIED CRACK IN UPPER FWD HOLE. REMOVED CRACK/DAMAGE AREA IAW SRM 53-10-51, FIG 202 REPAIR 6, DETAIL B AND 51-10-02, REV HFEC OF CUTOUT IAW HNTM 51-00-00, PT 6 NO CRACK INDICATION NOTED TOOL T8251A ALODINED CUTOUT IAW SRM 51-20-01 PRIMED CUTOUT IAW SOPM 20-41-02 FABRICATED REPAIR PARTS ITEM FILLER ITEM 3 ANGLE AND ITEM 7 FITTING IAW SRM 53-10-51, PAR 4G ALODINED REPAIR PARTS IAW SRM 51-20-01 PRIMED IAW SOPM 20-41-02, INSTALLED REPAIR PARTS IAW SRM 53-10-51, FIG 203, REPAIR 6, DETAIL D AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 37,942 hrs · 14,635 cycles

CABIN FLOOR SUPPORT CRACKED BS 344-360, LBL 10. ACFT GROUNDED. R & R CABIN FLOOR SUPPORT AT BS 344-BS 360, LBL 10 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 37,942 hrs · 14,635 cycles

CABIN FLOOR SUPPORT CRACKED BS 344-360, BL 0. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 37,942 hrs · 14,635 cycles

CABIN FLOOR SUPPORT CRACKED, BS 312-328, LBL 48. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 37,942 hrs · 14,635 cycles

CABIN FLOOR SUPPORT CRACKED BS 312-328, RBL 30. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: BEAM — CORRODED (BS 344) · corrosion level 2 · airframe 37,942 hrs · 14,635 cycles

CORROSION ON TRANSVERSE BEAM 344 LBL 10-BL0. ACFT GROUNDED. REPAIRED BS 344 .LBL 44-RBL 28 IAW SRM 53-10-51, REPAIR 10 AND SRM 53-10-51, REPAIR 9.

Part: SEAL — DIRTY (EMERGENCY DOOR) · airframe 37,942 hrs · 14,635 cycles

RT AFT OVERWING EMERGENCY DOOR WILL NOT OPEN. INSPECTED RT AFT OVERWING EMERGENCY DOOR REF AMM 52-22-00 FOUND PRESSURE SEAL DIRTY CLEAN SEAL REF BAC 20-30-03. OPS CHECK GOOD REF AMM 52-22-00-710-801. TEST OK.

Part: SEAL — DIRTY (EMERGENCY EXIT) · airframe 37,942 hrs · 14,635 cycles

RIGHT AFT OVERWING EMERGENCY DOOR WILL NOT OPEN. INSPECTED RT AFT OVERWING EMERGENCY DOOR, REF AMM 52-22-00 FOUND PRESSURE SEAL DIRTY, CLEAN SEAL REF CMM 30-30-03. OPS CHECKED GOOD REF AMM 52-22-00-710-801.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,756 hrs · 12,401 cycles

POWER RECEPTACLE DOOR SURROUND CRACKED ON FORWARD SIDE. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER IAW TIMCO REO G13635 REV A DATED 05/09/2011 AND ASA EA 900 53EA 05391 REV NEW DATED 09MAY2011.

Part: SHIM — MIGRATED (VERTICAL STAB) · airframe 31,756 hrs · 12,401 cycles

VERTICAL STABILIZER REAR SPAR LEFT MAIN ATTACH FITTING OUTBOARD SIDE AT LOWER BOLT SHIM MIGRATED. REPAIRED VERTICAL STABILIZER REAR SPAR SHIM MIGRATION IAW REO G13677 AND ASA EA 900 55EA 05374.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,427 hrs · 12,270 cycles

FOUND INTERCOSTAL IN AFT CARGO BAY CRACKED. REMOVED CRACKED INTERCOSTAL FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 900 SRM 51 40 02.

Part: PAD — WORN (ECS DOOR) · airframe 29,661 hrs · 11,609 cycles

STRIKE PAD WORN AND MISLOCATED ON OUTER CHORD RT ECS DOOR FIRST LATCH AFT OF HI PRESS CONNECT DOOR. INSTALLED REPAIR STRAP & EXTENDED STRIKER PLATE.

Part: SKIN — BENT (L1 DOOR) · airframe 27,584 hrs · 10,780 cycles

L1 DOOR AFT CORNER BELOW THE UPPER GATE IS BENT FROM CONTACT WITH AIRFRAME. CUT OUT REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 900 SRM 52 00 01 REPAIR 2. ALODINED PRIMED AND PAINTED AND CICED IAW B737 900 SRM 51 20 01.

Part: FRAME — DAMAGED (BS 500G) · airframe 26,489 hrs · 10,360 cycles

ELONGATED HOLE AT BS 500G ON FRAME. REPAIRED ELONGATED HOLE PER EA.

Part: STRUCTURE — CHAFED (NR 5 SLAT) · airframe 26,489 hrs · 10,360 cycles

WING RIGHT NR 5 SLAT LOWER T/E IS CHAFED IN SEVERAL AREAS. REPLACED NR 5 SLAT LOWER T/E.

Part: BOLT — LOOSE (LT WING) · airframe 26,489 hrs · 10,360 cycles

LEFT WING T/E UPPER PANEL ATTACH BOLTS ARE LOOSE CAUSING CHAFING ON PROGRAM TRACK ROLLER FITTING TAB AND PANEL SUPPORT AT RSS 284. REPLACE BEAM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 26,489 hrs · 10,360 cycles

CARGO TIE DOWN TRACK CRACKED AT BS 727I RBL 13.84. REMOVED, FABRICATED & INSTALLED CARGO TIE DOWN TRACK.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

LEFT ECS BAY AFT BULKHEAD HAS 3 CRACKS COMING FROM FASTENER HEADS SUPPORT STRUCTURE FOR THE HEAT EXCHANGER DUCT. REPAIRED CRACKS PER SRM 51 70 04.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON SIDEWALL SUPPORT IN AFT CARGO BAY. REMOVED SIDEWALL SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED PER SRM 51 40 02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,743 hrs · 31,958 cycles

INTERCOSTAL L-ANGLE CRACKED A FWD ENTRY DOOR WAY BS 300 STR 13L.

Part: SPLICE — CORRODED (FLOOR PANEL) · corrosion level 2 · airframe 55,743 hrs · 31,958 cycles

CORROSION ON FLOOR PANEL SPLICE. REPLACED WITH NEW FABRICATED FLOOR SPLICE.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

NR 2 FLOOR PANEL IN THE FWD CARGO BAY HAS CORROSION AT LBL 23. REPLACED FLOOR PANEL WITH FABRICATED ONE PER SRM 51-40-05 AND 51-40-08.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

INTERCOSTAL BRACKET 143A7502 5 WAS CRACKED. REMOVED AND REPLACED BRACKET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

INTERCOSTAL BRACKET 143A7502 13 WAS CRACKED. REMOVED AND REPLACED BRACKET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

INTERCOSTAL BRACKET 143A7502 13 WAS CRACKED. REMOVED AND REPLACED BRACKET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

INTERCOSTAL BRACKET 143A7502 13 WAS CRACKED. REMOVED AND REPLACED BRACKET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

INTERCOSTAL BRACKET 143A7502 13 WAS CRACKED. REMOVED AND REPLACED BRACKET.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

INTERCOSTAL BRACKET 143A7502 19 WAS CRACKED. REMOVED AND REPLACED BRACKET.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

FLOOR SUPPORT SPLICE IN AFT CARGO BAY CORRODED. REPLACED PER SRM.

Part: SKIN — GOUGED (SPOILER) · airframe 26,489 hrs · 10,360 cycles

NR 8 SPOILER AFT I/B LOWER SURFACE CORNER GOUGED. REPAIRED NR 8 SPOILER LOWER SURFACE PER SRM 57-70-01 AND 51-70-10.

Part: SUPPORT — CORRODED (BS 767-787) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY BS 767-787 RBL 23. REMOVED SUPPORT FABRICATED NEW SUPPORT AND INSTALLED PER SRM 51-40-02 AND 51-30-01.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON FLOOR TO SIDEWALL SPLICE PLATE AT BS 727I+5 TO 727I+10 RBL 25 WL 156. REMOVED AND REPLACED SPLICE PLATE.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

CORROSION AT BS 877 ON FLOOR TO SIDEWALL RBL 23. REMOVED SECTION OF SIDEWALL SUPPORT FROM 500C+10 TO 500G AND REPAIRED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

SIDEWALL SUPPORT P/N 146A94003U87 IS CRACKED IN SEVERAL PLACES. REMOVED AND REPLACED SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY. REMOVED, FABRICATED AND INSTALLED NEW FTS.

Part: SPLICE — CORRODED (BS 727) · airframe 26,489 hrs · 10,360 cycles

CORROSION ON SPLICE IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED (FABRICATED) FLOOR SUPPORT SPLICE PER SRM 53-00-53, 51-40-02 AND DWG 146A7506.

Part: SPLICE — CORRODED (BS 727I) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

AFT CARGO FLOOR SUPPORT SPLICE CORROSION OUT OF LIMITS BS 727I+4 LBL 3. REMOVED AND REPLACED WITH FABRICATED FLOOR SUPPORT SPLICE PER SRM 51-40-02 AND 51-40-05.

Part: SPLICE — CORRODED (BS 727I) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

AFT CARGO FLOOR SUPPORT SPLICE CORROSION OUT OF LIMITS BS 727I+4 RBL 3. REMOVED AND REPLACED WITH FABRICATED FLOOR SUPPORT SPLICE PER SRM 51-40-02 AND 51-40-05.

Part: SPLICE — CORRODED (BS 727I) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

AFT CARGO FLOOR SUPPORT SPLICE CORROSION OUT OF LIMITS BS 727I+4 LBL 1. REMOVED AND REPLACED WITH FABRICATED FLOOR SUPPORT SPLICE PER SRM 51-40-02 AND 51-40-05.

Part: SPLICE PLATE — CORRODED (BS 772) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON ACB FLOOR SPLICE PLATE. REMOVED AND REPLACED WITH FABRICATED SPLICE PLATE.

Part: SPLICE — CORRODED (BS 727I) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

AFT CARGO FLOOR SUPPORT SPLICE CORROSION OUT OF LIMITS BS 727I+4 LBL 12.5. REMOVED AND REPLACED WITH FABRICATED FLOOR SUPPORT SPLICE PER SRM 51-40-02 AND 51-40-05.

Part: INTERCOSTAL — CORRODED (BS 767-787) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

INTERCOSTAL SUPPORT ANGLE CORROSION OUT OF LIMITS BS 767 TO BS 787 LBL 3. REMOVED, FABRICATED & INSTALLED SERVICEABLE INTERCOSTAL SUPPORT ANGLE PER SRM 51-30-01 AND DWG 146A8125.

Part: SPLICE — CORRODED (BS 727I) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

AFT CARGO FLOOR SUPPORT SPLICE CORROSION OUT OF LIMITS BS 727I+4 RBL 1. REMOVED AND REPLACED WITH FABRICATED FLOOR SUPPORT SPLICE PER SRM 51-40-2 AND 51-40-05.

Part: FLOOR SUPPORT — CRACKED (BS 727I) · airframe 26,489 hrs · 10,360 cycles

AFT CARGO BAY FLOOR SUPPORT CRACKED. REPAIRED PER SRM 53-00-53 REPAIR 3.

Part: SKIN — DENTED (CARGO DOOR) · airframe 26,489 hrs · 10,360 cycles

FWD CARGO DOOR REQUIRES TO BE RE-SKINNED. REMOVED AND REPLACED SKIN.

Part: SLAT — CHAFED (RT WING) · airframe 26,489 hrs · 10,360 cycles

RIGHT WING NR 8 SLAT LWR T/E IS CHAFED. REPAIRED RIGHT WING NR 8 SLAT LWR T/E.

Part: SKIN — DENTED (CARGO DOOR) · airframe 26,489 hrs · 10,360 cycles

AFT CARGO DOOR REQUIRES TO BE RE-SKINNED. REMOVED AND REPLACED SKIN.

Part: FITTING — GOUGED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

FLOOR TRACK FITTING GOUGED. REMOVED AND REPLACED FLOOR TRACK SECTION.

Part: SLAT — CHAFED (LT WING) · airframe 26,489 hrs · 10,360 cycles

LEFT WING NR 3 SLAT CHAFED ALONG LWR T/E. REPAIRED LT WING NR 3 SLAT ALONG LWR T/E.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,489 hrs · 10,360 cycles

EMERGENCY BATTERY PACK M1899 FAILED OPS CHECK. REMOVED AND REPLACED BATTERY PACK.

Part: SHIELD — CORRODED (BS 847-867) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT SHIELD HAS CORROSION. REMOVED SUPPORT FABRICATED NEW SUPPORT AND INSTALLED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,489 hrs · 10,360 cycles

EMERGENCY BATTERY PACK M1694 FAILED OPS CHECK. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,489 hrs · 10,360 cycles

EMERGENCY BATTERY PACK M1671 FAILED OPS CHECK. REMOVED AND REPLACED BATTERY PACK.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON AFT CARGO BAY CARGO TRACK. REPAIRED CARGO TRACK IAW SRM 53-00-53 REPAIR 3.

Part: SUPPORT — CORRODED (BS 500G-500L) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION FOUND ON FLOOR TO SIDEWALL SUPPORT IN THE FWD BAY RBL 23 BS 500G TO 500L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: FRAME — CORRODED (BS 767) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON FRAME IN AFT CARGO BAY BS 767 RBL 25. REMOVED AND REPLACED FRAME SPLICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO COMPARTMENT BS 727+4 TO BS 727D+4 LBL 23. CORROSION OUT OF LIMITS. REMOVED AND INSTALLED FABRICATED FLOOR TO SIDEWALL SUPPORT ACB.

Part: SUPPORT — CORRODED (BS 727D-727I) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO COMPARTMENT BS 727D+3 TO BS 727I+8 LBL 23. REPLACED FLOOR TO SIDEWALL SUPPORT IN THE AFT CARGO BAY.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

CORROSION ON FRAME IN AFT CARGO BAY BS 787 RBL 25.

Part: SUPPORT FITTING — CORRODED (BS 767) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON FRAME TO SIDEWALL SUPPORT FITTING IN AFT CARGO BAY. REPLACED SUPPORT FITTING PER SRM 51-30-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO COMPARTMENT BS 727C+4 TO BS 867 LBL 23. REMOVED AND REPLACED WITH FABRICATED FLOOR PANEL PER SRM 53-30-53 AND 51-30-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY BS 727C+4 TO 867 LBL 23. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY BS 727+4 TO 727D+3 RBL 23 156. CORROSION OUT OF LIMITS. REMOVED AND INSTALLED FABRICATED FLOOR TO SIDEWALL SUPPORT AFT CARGO BAY BS 727+4 TO 727D+3 RBL 23 156.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727+4 727D+18 LBL 23. REMOVED, FABRICATED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT.

Part: TAIL CONE — DENTED (FUSELAGE) · airframe 26,489 hrs · 10,360 cycles

LEFT SIDE OF TAIL CONE DENTED. REPAIRED DENT ON LT OF TAIL CONE.

Part: INTERCOSTAL — CORRODED (BS 747-767) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON INTERCOSTAL BS 747-767 RBL 21. FABRICATED AND INSTALLED NEW INTERCOSTAL.

Part: SUPPORT — CORRODED (BS 500L) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

FWD CARGO COMPARTMENT AFT LEFT BULKHEAD SUPPORT STRUCTURE HAS CORROSION. REMOVED AND REPLACED BULKHEAD SUPPORT.

Part: SUPPORT — CORRODED (BS 500L) · airframe 26,489 hrs · 10,360 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD SUPPORT STRUCTURE HAS CORROSION AT BS 500L, LBL 24 RBL 24 WL 156.5. REMOVED AND REPLACED WITH NEW BULKHEAD SUPPORT PER SRM 53-00-53 AND 51-40-02.

Part: SUPPORT — CORRODED (BS 727H) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727H-727L LBL 23. REMOVED SIDEWALL SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED.

Part: SUPPORT — CORRODED (BS 727D-727H) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727D+18 727H LBL 23. REMOVED SIDEWALL SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION FOUND ON FLOOR TO SIDEWALL SUPPORT IN THE FWD BAY RBL 23 BS 500G TO 500L. REPLACED FLOOR TO SIDEWALL SUPPORT BS 867 TO BS 901 WL 154 RBL 23.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,489 hrs · 10,360 cycles

SEVERAL AREAS OF CORROSION FOUND ON FLOOR TO SIDEWALL SUPPORT IN THE FWD BAY RBL 23 BS 500D TO 500G. REMOVED AND REPLACED SPLICE ANGLE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 20,936 hrs · 8,205 cycles

CABIN FLOORBOARD SUPPORT ANGLE CRACKED AT STA 540 RBL 1. CUT OUT DAMAGED AREA. FABRICATED REPAIR PART. NDT INSPECTED JOGGLES FOR CRACKS, NO DEFECTS NOTED. LOCATED DRILLED AND INSTALLED REPAIR ANGLE AND REPAIR PART IAW ASA EA5320 01831.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 20,936 hrs · 8,205 cycles

CABIN FLOORBOARD SUPPORT ANGLE CRACKED AT STA 540 LBL 1. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS. INSPECTED JOGGLE AREA FOR CRACKS, NO DEFECTS NOTED. LOCATED DRILLED AND INSTALLED REPAIR ANGLE AND REPAIR PARTS IAW ASA EA5320 01831.

Part: LATCH — BROKEN (SERVICE DOOR) · airframe 19,753 hrs · 7,726 cycles

RELEASE LATCH ON RIGHT FWD SVC DOOR BROKEN. REPLACED R2 DOOR HOLD RELEASE BUTTON.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,197 hrs · 7,037 cycles

DENT ON FUSELAGE SKIN. DENT CUT OUT AND DOUBLER INSTALLED PER ASA EA 5330 02213.

Part: SILL — CORRODED (BS 500L) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

DUST SILL AT BS 500L IS CORRODED. REPAIRED IAW 51-40-02.

Part: SILL — CORRODED (BS 727-767) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT PIT DUST SILL AT RBL 21 IS CORRODED REPAIRED IAW 51 40 02 AND 51 40 05.

Part: SILL — CORRODED (BS 727) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

DUST SILL WEB AT BS 727 CORRODED. REPAIRED IAW SRM 53-00-53 FIG 202.

Part: CARGO TRACK — CORRODED (BS 500L) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

FWD CARGO TIE DOWN FITTING AT BS 500L IS CORRODED. REPAIRED IAW SRM 53-00-53.

Part: FLOOR PANEL — PUNCTURED (BS 727-727D) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT CARGO PIT FLOOR PANEL AT BS 727 IS PUNCTURED REPAIRED IAW 51 40 05.

Part: FLOOR PANEL — CORRODED (BS 887-947) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT PIT FLOOR PANEL AT BS 5887.0 IS CORRODED REPAIRED IAW 51 40 05 AND 51 40 08.

Part: SILL — CORRODED (BS 500L) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

DUST SILL AT BS 500L IS CORRODED. REPAIRED IAW SRM 53900 53 FIG 202.

Part: FLOOR SUPPORT — GOUGED (BS 727F-727G) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT FLOOR SUPPORT BEAM AT LBL 3 IS GOUGED. REPAIRED IAW 53-00-53 REPAIR 2.

Part: FLOOR PANEL — CORRODED (BS 767-887) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT PIT FLOOR PANEL AT BS 767.0 IS CORRODED REPAIRED IAW SDR 51 40 05.

Part: STRAP — CORRODED (BS 767) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

FOUND AFT CARGO PIT FLOOR STRAP AND BS 767 CORRODED. REPLACED IAW SRM 51 40 05.

Part: FLOOR SUPPORT — CORRODED (BS 727-827) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT CARGO FLOOR SUPPORT CHANNEL AT RBL 13.8 IS CORRODED REPAIRED IAW SRM 53 00 53 REPAIR Z.

Part: FLOOR SUPPORT — CORRODED (BS 727-827) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT CARGO FLOOR SUPPORT CHANNEL AT RBL 8.1 CORRODED 53 00 53, REPAIRED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 727-827) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

FOUND AFT CARGO FLOOR SUPPORT CHANNEL AT BL 3.0 CORRODED. REPARIED IAW SDR 53 00 53.

Part: FLOOR SUPPORT — CORRODED (BS 727-827) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT CARGO FLOOR SUPPORT CHANNEL AT LBL 3.0 IS CORRODED REPAIRED IAW 53 00 53.

Part: CARGO TRACK — CORRODED (BS 727-827) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT CARGO CUPPOR CHANNEL CORRODED AT LBL 17.24 AND BS 827 REPAIRED IAW 53 00 53 REPAIR 3.

Part: WEB — CORRODED (BS 495-500L) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

FOUND DUST SILL WEB CORRODED AT BS 500L TO 495. REPAIRED IAW 51 40 62.

Part: FLOOR SUPPORT — CORRODED (BS 727-827) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT CARGO SUPPORT CHANNEL CORRODED AT BS 727H AND LBL 12.3 REPAIRED IAW 53 00 53 REPAIR 2.

Part: ATTACH ANGLE — CORRODED (BS 500L) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

FOUND ATTACH ANGLE AT BS 500L CORRODED IN FWD CARGO PIT. REPLACED IAW SRM 51 40 02.

Part: FLOOR SUPPORT — CORRODED (BS 727-827) · corrosion level 2 · airframe 15,689 hrs · 5,942 cycles

AFT CARGO FLOOR SUPPORT CHANNEL AT LBL8.1 AND BS 727H IS CORRODED. REPAIRED IAW 53 00 53 REPAIR 2.

Part: SCREW — MISSING (MLG)

SEA - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF WITH GEAR HANDLE IN UP POSITION. LEVER WOULD NOT RETURN TO THE DOWN POSITION, WHEN ATTEMPTED TO MOVE BY CREW. 6 GREEN LANDING GEAR INDICATOR LIGHTS AND 3 RED LIGHTS ILLUMINATED THEN ACCOMPANIED THIS. RETURNED TO SEA AND LANDED WITHOUT INCIDENT. INSPECTED LANDING GEAR CONTROL LEVER MODULE. FOUND 3 SCREWS AND WASHERS THAT SECURED TELEFLEX CABLE ASSEMBLY TO REAR OF CONTROL LEVER MODULE MISSING. INSTALLED MISSING HARDWARE, OPS CHECKED SYSTEM, OPS CHECKED GOOD. APPEARS SCREWS WERE NOT INSTALLED ORIGINALLY DURING AIRCRAFT ASSEMBLY. (M)