N317AS

Part: LIGHT — DETACHED (MAIN CABIN) · airframe 66,252 hrs · 26,888 cycles

EXIT SIGN DETACHED AT ROW 17F. GROUNDED - YES. REMOVED AND REPLACED ROW 17(F) RH EMER EXIT SIGN ASSY OPS CK NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 64,798 hrs · 26,234 cycles

ROW 16 AIRCRAFT RIGHT EXIT LIGHT (ADJACENT TO EXIT WINDOW), COVER MISSING. GROUNDED - YES. REPLACED RH EXIT SIGN AS REQUIRED.

Part: BATTERY PACK — FAULTY (MAIN CABIN) · airframe 64,037 hrs · 25,906 cycles

EMERGENCY EXIT LIGHTS ROWS 27 & 29 INOP. GROUNDED - YES. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK, OPS CK GOOD. IAW B737-900 AMM 33-51-06-960-805.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,037 hrs · 25,906 cycles

RH TRAILING EDGE EMERGENCY SLIDE EMERGENCY LIGHT INOP. GROUNDED - YES. REMOVED, REPLACED AND OPS CHECK IS GOOD OF R/H TRAILING EDGE EMERGENCY SLIDE/EMERGENCY LIGHT BATTERY PACK (M1695) IAW B737-900 AMM 33-51-06-960-805 STEPS 4.E(2), (3), (G), (4) AND F. AND B737-900 WDM 33-51-13 PAGE 3, SHEET 1 AND.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,037 hrs · 25,906 cycles

LH TRAILING EDGE EMERGENCY SLIDE EMERGENCY LIGHT INOP. GROUNDED - YES. REMOVED, REPLACED AND OPS CHECK IS GOOD OF L/H TRAILING EDGE EMERGENCY SLIDE / EMERGENCY LIGHT POWER SUPPLY IAW B737-900 AMM 33-51-960-806 AND WDM 33-51-13 PAGE 3 SHEET 1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,037 hrs · 25,906 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED, OPS CHECK IS GOOD OF L/H L2 DOOR EXTERIOR EMERGENCY LIGHT BATTERY PACK (M1673) IAW B737-900 AMM 33-51-06-960-805 STEPS 4.E.(1), (2), (3)(G), (4), (5), (6). F. (4) AND WDM 33-51-14 PAGE 2 SHEET 1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,037 hrs · 25,906 cycles

RH R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. GROUNDED - YES. REMOVED, REPLACED AND OPS CHECK IS GOOD R/H DOOR EXTERIOR EMERGENCY LIGHT BATTERY PACK (M1673) IAW B737-900 AMM 33-51-06-960-805-STEPS 4.E(2), (3), (G), (4) AND F AND WDM 33-51-14 PAGE 2 SHEET 1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,037 hrs · 25,906 cycles

L/H HORIZ STAB #7 RIB IS CRACKED ON 3RD STIFFNER. GROUNDED - YES. REMOVED, REPLACED AND REINSTALLED RIB IAW B737-900 SRM 55-10-09-2R-4, SRM 51-40-02-0G-0.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,037 hrs · 25,906 cycles

R/H HORIZ STAB #8 RIB IS CRACKED ON 3RD STIFFNER. GROUNDED - YES. REMOVED,REPAIRED AND REINSTALLED RIB IAW B737-900 SRM 55-10-09-2R-4.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,037 hrs · 25,906 cycles

R/H HORIZ STAB #4 RIB IS CRACKED ON 2ND AND 3RD STIFFNERS. GROUNDED - YES. REMOVED, REINSTALLED AND REPIARED RIB IAW B737-900 SRM 55-10-09-2R-4.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,037 hrs · 25,906 cycles

L/H HORIZ STAB #5 RIB IS CRACKED ON 2ND AND 4TH STIFFNERS. GROUNDED - YES. REMOVED, REPAIRED AND REINSTALLED RIB IAW B737-900 SRM 55-10-09-2R-4, SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (STA 947) · corrosion level 2 · airframe 64,037 hrs · 25,906 cycles

STA 947 FLOOR BEAM L/H O/B LAV MOUNT CORRODED. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS CUT OUT DAMAGED SECTION OF FLOOR BEAM AND REPAIRED IAW B737-900 SRM 53-70-51-2R-5W=3 O=.180 R=0 L=6 D=.180.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,037 hrs · 25,906 cycles

L/H HORIZ STAB #4 RIB IS CRACKED ON 3RD STIFFNER. GROUNDED - YES. REMOVED,REPAIRED AND REINSTALLED RIB IAW B737-900 SRM 55-10-09-2R-4.

Part: WEB — CORRODED (AFT CARGO) · airframe 64,037 hrs · 25,906 cycles

AFT CARGO DOOR CUTOUT LOWER SILL WEB HAS SPOTS OF CORROSION. GROUNDED - YES. REMOVED AND REPLACED SILL WEB WITH NEW IAW B737-900 SRM 51-40-02-0G-0W=1 O=.050 R=.041 L=4 D=.009.

Part: CARGO TRACK — CORRODED (BS 787-867) · airframe 64,037 hrs · 25,906 cycles

AFT CARGO TRACK RBL 14 HAS SPOTS OF CORROSION STA 787 TO 867. GROUNDED - YES. CUT OUT DAMAGE SECTION AND REPAIRED TRACK IAW B737-900 SRM 53-00-53-2R-3W=1 O=.071 R=.052 L=10 D=.018.

Part: TRANSITION PANEL — CORRODED (BS 727A-847) · corrosion level 2 · airframe 64,037 hrs · 25,906 cycles

AFT CARGO RT TRANSITION PANEL HAS SPOTS OF CORROSION STA 727A TO 847. GROUNDED - YES. PREFORMED SURFACE BLEND AND REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED NEW TRANSITION PANEL IAW SRM 53-00-53-2R-2, SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 727G-727I) · airframe 64,037 hrs · 25,906 cycles

AFT CARGO TRACK LBL 20 STA 727G TO 727I HAS SPOTS OF CORROSION. GROUNDED - YES. REMOVED AND REPLACED CARGO TRACK FROM STA 727G TO 727I WITH NEW IAW B737-900 SRM 53-00-53-2R-3W=2 O=.070 R=.024 L=2 D=.046.

Part: TRANSITION PANEL — CORRODED (BS 727A-847) · corrosion level 2 · airframe 64,037 hrs · 25,906 cycles

AFT CARGO L/H TRANSITION HAS SPOTS OF CORROSION STA 727A TO 847. GROUNDED - YES. REMOVED AND REPLACED L/H TRANSISTION FROM 727A TO 847 WITH NEW IAW B737-900 SRM 53-60-53-01-2W=2 O=.040 R=.001 L=1 D=.040.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 64,037 hrs · 25,906 cycles

L/H HORIZONTAL LOWER SKIN IS CRACKED AT HSS 138 APROX 18 INCHES AFT OF FRONT SPAR. GROUNDED - YES. REPAIRED L/H HORIZ STAB LOWER SKIN @ STA 138 IAW B737-900 SRM 55-10-01-2R-11. THIS IS A CAT B REPAIR.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 64,037 hrs · 25,906 cycles

R/H HORIZONTAL LOWER SKIN IS CRACKED AT HSS 129 APROX 12 INCHES FWD OF REAR SPAR. GROUNDED - YES. REPAIRED R/H HORIZ STAB LOWER SKIN @ STA 129 IAW SRM 55-10-01-2R-11. THIS IS A CAT B REPAIR.

Part: BATTERY PACK — INOPERATIVE (MAIN PASSENGER C) · airframe 63,427 hrs · 25,627 cycles

WHILE ACCOMPLISHING ASA T/C EMERGENCY LIGHTS OP CK. FOUND INTERIOR R1 MAIN EXIT LIGHT, EXTERIOR R1 LIGHT INOP AND EMERGENCY LIGHT ON FIRST CLASS OVERHEAD BIN INOP. GROUNDED - YES. REMOVED AND REPLACED M1674 BATTERY PACK. R1 INTERIOR AND EXTERIOR EGRESS LIGHT OPS NORMAL REF B737-900 AMM 33-51-06-960-805. CHARGED SYSTEM AND FIRST CLASS OVERHEAD BIN EMERGENCY LIGHT CHECKS GOOD REF AMM 33-51-60-610-802.

Part: LAMP — INOPERATIVE (EXTERIOR FUSELAG) · airframe 63,222 hrs · 25,534 cycles

EXTERIOR EMERGENCY LIGHT AT R2 DOOR IS DIM. GROUNDED - YES. REPLACED EXTERIOR EMERGENCY LIGHT AT R2 DOOR LIGHT BULB. IAW 737-900 AMM 33-51-04-960-801.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 58,936 hrs · 23,590 cycles

RT HORIZONTAL LOWER SKIN HAS A CRACK AT STA 175 9.5 INCHES FWD OF REAR SPAR DOT A154-001. GROUNDED-YES. REPAIRED RT HORIZ LOWER SKIN CRACKED AT STA 175, IAW 737-900 SRM 55-10-01-2R-11 REPAIR 11. THIS IS A CAT B REPAIR REQUIRES INSPECTION AT THRESHOLD OF 56,000 FLT CYCLES INTERVAL OF 9,000 FLT CYCLES.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 58,936 hrs · 23,590 cycles

LT HORIZONTAL LOWER SKIN HAS A CRACK AT STA 125 AT REAR SPAR, DOT A-154-002. GROUNDED-YES. REPAIRED LOWER STAB SKIN, IAW 737-900 SRM 55-10-01-2R-11. THIS IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL FLT CYCLES & INSPECTION INTERVAL OF 9,000 FLR CYCLES TOTAL A/C FLT CYCLES AT TIME OF REPAIR 23,590.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,713 hrs · 22,076 cycles

MULTIPLE EMERGENCY EXIT LIGHTS NEAR L1 DOOR INOP (COMMON TO POWER SUPPLY M1675). GROUNDED - YES. T/S, FOUND BAD EMERGENCY LIGHT PWR SUPPLY, REMOVED AND REPLACED M1675 IAW B737-900 AMM 33-51-06-960-806 AND B737-900 WDM 33-51-12. OPS TESTED GOOD IAW B737-900 AMM 33-51-06-960-806.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,713 hrs · 22,076 cycles

MAIN CABIN FLOOR STRUCTURE, FORWARD WET AREA (SEC 41) INTERCOSTAL P/N:141A5410-22 LOCATED AT STA 344-STA 360, LBL 11.10, WL 208.1 CRACKED AT FASTENER HOLE LOCATION. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL PART 141A5410-148 AT STA 344-STA 360 LBL 11.10 WL 208.1 IAW SRM 51-40-02-09-0 AND DRAWING 141A5400 REV A SHEET 46.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,713 hrs · 22,076 cycles

MAIN CABIN FLOOR STRUCTURE, FORWARD WET AREA (SEC 41) INTERCOSTAL P/N:141A5410-3 LOCATED AT STA 277-STA 294.525, BL 0, WL 208.1 CRACKED AT FASTENER HOLE LOCATION. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL PART 141A5410-139 AT STA 277-STA 294.525 BL O WL 208.1 IAW SRM 51-40-02-09-0 AND DRAWING 141A5400 REV- SHT 20.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,713 hrs · 22,076 cycles

MAIN CABIN FLOOR STRUCTURE, FORWARD WET AREA (SEC 41) INTERCOSTAL P/N:141A5410-12 LOCATED AT STA 312-STA 328, RBL 31.60, WL 208.1 CRACKED AT FASTENER HOLE LOCATION. GROUNDED - YES. REMOVED INTERCOSTAL IAW SRM 51-40-02-0G-01, LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0, INSTALLED NEW INTERCOSTAL IAW DWG 141A5400 REV- SHT 39 AND SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 55,713 hrs · 22,076 cycles

CRACK FOUND INBOARD OF RT STABILIZER STA 129.50 MEASURING 1.25" IN LENGTH LOCATED IN THE MIDDLE OF THE BAY. GROUNDED - YES. REMOVED DAMAGE (CUT-OUT) CRACK ON RT STAB STA 129-50, APPROX 16" FWD OF REAR SPAR, ALSO INCLUDED EXISTING REPAIR AT STAB STA 138.8 REPAIRED IAW SRM 55-10-01-2R-11. REPAIR IS CATEGORY "B" REPAIR.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,713 hrs · 22,076 cycles

AFT CARGO COMPT LT FLOOR TRANSITION PANEL HAS MISSING CLICK BOND NUTPLATES AND CORROSION BETWEEN STA 727L-747. GROUNDED - YES. REMOVED CORROSION IN AFT CARGO COMPT LT FLOOR TRANSITION PANEL FROM STA 727K- STA 747. ORIGINAL THICKNESS IS .040, REMOVED .010, REMAINING THICKNESS IS .030. OUT OF LIMITS IAW SRM 53-60-53. REPAIRED TRANSITION PANEL FROM STA 727K TO STA 747+8 IAW SRM 53-00-53-2R-6. INSTALLED NUT PLATES IAW BAC DWG 140N4500.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,713 hrs · 22,076 cycles

MAIN CABIN RT FRAME STA 277 THRU 332.1 - FLOOR BOARD SUPPORT STRUCTURE COMMON TO R1 SERVICE DOOR SILL AREA, UPPER SURFACE HAS BARE METAL AREAS AND AREAS OF CORROSION. GROUNDED - YES. BLENDED INNER CHORD AT R-1 DOOR, ORIGINAL MATERIAL .080 MATERIAL REMOVED .012 REMAINING MATERIAL .068 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-01-2 MATERIAL ID AND SRM 53-1-15-1A-2 FOR ALLOWABLE DAMAGE, REMOVE DAMAGED INNER CHORD AND ATTACH ANGLES AND DOOR SILL IAW SRM 51-40-02, INSTALLED NEW INNER CHORD, DOOR SILL AND ATTACH ANGLES IAW DRAWING 141A831 REV B AND SRM 51-40-2-G-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,713 hrs · 22,076 cycles

FWD CARGO COMPT STA 500G-500H AT S26L INTERCOSTAL UNDER FLOOR TRANSITION PANEL CRACKED IN RADIUS AT RIVET. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AND NEW CLIP IAW SRM 51-40-02 AND DWG 143A7505 REV-.

Part: SIGN — INOPERATIVE (CABIN) · airframe 52,875 hrs · 20,778 cycles

AFT RT EXIT SIGN NOT ILLUMINATING. GROUNDED - YES. REPLACED COVER AND REPLACED AFT RT EXIT SIGN REF AMM 33-51-01. OPS CHK GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 52,074 hrs · 20,409 cycles

EMERGENCY EXIT AREA LIGHTS AT ROWS 28DEF AND ROW 30 DEF ARE INOP. RELAMPED-NO HELP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY EXIT AREA LIGHTS POWER SUPPLY FOR ROWS 28DEF AND ROW 30 DEF. REF B737-900 AMM 33-51-06-960-806. OPS CHECK GOOD. SYSTEM RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 51,913 hrs · 20,323 cycles

WHILE ACCOMPLISHING TC 78233008. FOUND THE EMERGENCY EXIT LIGHTS L1063, L1065 AND L1417 INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805 AND WDM 33-51-12. LIGHTS OPS TESTED NORMAL.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 49,937 hrs · 19,433 cycles

RT AFT OVERWING EXIT AND RT FUSELAGE EMERGENCY LIGHTS INOPERATIVE. ACFT GROUNDED. FOUND POWER SUPPLY FAULTING. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED NORMAL.

Part: FLOOR SUPPORT — CORRODED (BS 727D) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

AFT CARGO, FLOOR SUPPORT AT BS 727D+4 IS CORRODED. ACFT GROUNDED. CORROSION REMOVED IAW DWG 146A9401 REV C AND FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2.

Part: SPLICE — CORRODED (BS 727I) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

AFT CARGO BAY, FLOORBEAM SPLICE AT BS 727I+4 IS CORRODED. ACFT GROUNDED. CORROSION REMOVED IAW IAW DRAWING 146A9401, REV C. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED THE SPLICE.

Part: STIFFENER — CORRODED (BS 727 BULKHEAD) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

AFT CARGO BAY, BS 727 BULKHEAD, RT LOWER SUPORT ANGLE, RBL 8 - 14 IS CORRODED ON BOTTOM SIDE. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103. REMOVED AND REPLACED THE STIFFNER IAW DWG144A2600 REV- AND SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,354 hrs · 19,170 cycles

FORWARD CARGO COMPARTMENT LT BILGE FRAME CHAFED WITH TOOLING MARKS BS 500K. GROUNDED - YES. REPAIRED FUSELAGE FRAME, LOWER LOBE AT STA 500K , LBL 18.24 IAW EA 900-53EA-18365 REV 00. THIS IS A CATEGORY "B" REPAIR WITH FIRST AND SECOND STAGE APPROVAL WITH INSPECTION THRESHOLD OF 75,000 TOTAL FLIGHT CYCLES.

Part: CARGO TRACK — CORRODED (BS 727-727B) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

AFT CARGO BAY CARGO TRACK UPPER SURFACE CORRODED BS 727 - 727B, RBL 14. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-00-53-1A-2 FIG103. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED CARGO TRACK IAW SRM 53-00-53 FABRICATE A NEW CARGO TRACK SECTION AND SPLICE IAW SRM 53-50-53-2R-3. INSTALLED THE CARGO TRACK IAW SRM 53-00-53-2R-3, REPAIR 3.

Part: CHANNEL — CORRODED (BS 727-814) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

AFT CARGO BAY CHANNEL CORROSION BS 727 - 814, STRINGER 25 - 26L. ACFT GROUNDED. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED THE CHANNEL IAW DWG 146A7500, SRM 53-00-53-2R-5, AND SRM 51-40-02.

Part: WEB — CORRODED (BS 440-500) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

FORWARD CARGO DOOR SILL WEB CORRODED BS 440 - 500. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-15. REMOVED THE WEB IAW SRM 51-40-02. FABRICATED A NEW WEB IAW DWG 143A8122 REV A. LOCATED, DRILLED, ALODINED, & PRIMED THE WEB IAW DWG 143A8122, REV - . INSTALLED IAW SRM 51-40-02 & DWG 143A8330.

Part: TRANSITION PANEL — CORRODED (BS 500A-500D) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

FORWARD CARGO BAY RT TRANSITIONAL PANEL CORRODED BS 500A - 500D. ACFT GROUNDED. REPLACED THE TRANSITION PANEL IAW SRM 53-00-53-2R-5 ORIG.

Part: DOUBLER — CORRODED (BS 500-500A) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

DOUBLER AT A DISCONTINUED ANTENNA MOUNT IN THE FORWARD CARGO BAY, CORRODED . BS 500 - BS 500A, STRINGER 27L - 27R. ACFT GROUNDED. REMOVED ANTENNA MOUNT AND BLANKING PLATE IAW B737-900 SRM 51-40-02, LOCATED & DRILLED IAW DWG 143A3230 REV -. INSTALLED DOME NUTS, 4 EA. CORNER SUPPORT ANGLES, AND NEW ANTENNA MOUNT IAW DWG 143A3230, REV -, APPLIED FILLET SEAL & FASTENER DOME SEALS IAW AMM 51-31-00-390-801.

Part: CHANNEL — CORRODED (BS 727-727F) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

AFT CARGO BAY CHANNEL CORRODED BS 727 - 727F+10, STRINGER 25 - 26R. ACFT GROUNDED. CORROSION REMOVED IAW SRM 51-40-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED IAW SRM 53-00-53-1A-2 AND 51-40-02.

Part: DOUBLER — CORRODED (BS 500A-500B) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

DOUBLER AT A DISCONTINUED ANTENNA MOUNT IN THE FORWARD CARGO COMPARTMENT, CORRODED . DOT ATTACHED. BS 500A - BS 500B, STR 27L - STR 27R. ACFT GROUNDED. REMOVED CORRODED ANTENNA MOUNT AND BLANKING PLATE IAW SRM 51-40-02, LOCATED & DRILLED THE NEW ANTENNA MOUNT IAW DWG 143A3230 REV -. INSTALLED DOME NUTS, CORNER SUPPORT ANGLES, AND NEW ANTENNA MOUNT IAW DWG 143A3230 REV- , APPLIED FILLET SEAL AND DOME SEAL ON FASTENERS IAW AMM 51-31-00-390-804.

Part: WEB — CORRODED (BS 794-847) · corrosion level 2 · airframe 49,354 hrs · 19,170 cycles

UNDER AFT CARGO DOOR SCUFF PLATES , WEB, CORRODED. DOT ATTACHED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1, REMOVED WEB IAW SRM 51-40-02, LOCATED AND DRILLED THE WEB IAW SRM 51-40-05 AND DWG 146A8340 REV -, INSTALLED THE WEB IAW SRM 51-40-05 AND DWG 146A8340 REV- AND SRM 51-40-02.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,327 hrs · 19,159 cycles

EMERGENCY LIGHT BATTERY PACKS M1673, M1670, AND M1695 FAILED DEEP CYCLE TEST. ACFT GROUNDED. REPLACED M1695 EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY, M1670 BATTERY PACK AND M1695 BATTERY PACK IAW AMM 33-51-06 AND WDM 33-51-13. TESTED - OPS. NORMAL.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 48,864 hrs · 18,956 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ON NR 1 GALLEY ADJACENT TO R1 DOOR IS BROKEN. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED EXIT LOCATOR SIGN IAW AMM 33-51-01-960-802. OPS NORMAL.

Part: BEARING — WORN (R1 DOOR) · airframe 47,926 hrs · 18,520 cycles

R1 DOOR WILL NOT CLOSE AND LATCH PROPERLY. ACFT GROUNDED. VERIFIED R1 DOOR WILL NOT CLOSE USING INSIDE HANDLE. UPPER AFT SECTION OF DOOR LINER MUST BE PUSHED OUT FOR ROLLERS TO ENGAGE. REMOVED R1 DOOR, R & R R1 DOOR UPPER LINK ASSY UPPER HINGE LOWER CAM PLATES AND GUIDE ARM ROD END BEARINGS. REINSTALLED AND ADJUSTED R1 DOOR. OPS CHECK GOOD, REF MIG2C 40-0013277 THROUGH 40-0013280, MIG2C 40-0023277/8/9 AND 40-0013289.

Part: ANGLE — CORRODED · corrosion level 2 · airframe 43,011 hrs · 16,478 cycles

AFT CARGO FLOOR SUPPORT ANGLE CORRODED. ACFT GROUNDED. REMOVED CORRODED AFT CARGO FLOOR SUPPORT ANGLES 2 EA AND REPLACED NEW IAW SRM 51-40-02, DWG 146A0081. CORROSION BEYOND REPAIR LIMITS.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 43,011 hrs · 16,478 cycles

CRACK FOUND ON LWR SKIN OF RT HORIZONTAL STABILIZER. JUST INBD OF STAB, STA 138.7 APPROX 17.5' FWD OF REAR SPAR. CRACK IS APPROX 0.75' LONG. ACFT GROUNDED. REPAIRED IAW SRM 55-10-01-2R-11. INSPECTION THRESHOLD 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 43,011 hrs · 16,478 cycles

CRACK FOUND ON LWR RT HORIZONTAL STABILIZER SKIN. CRACK IS JUST FWD OF REAR SPAR BETWEEN STABILIZER STA 92.7 & 101.9. CRACK IS APPROXIMATELY 1.75' LONG. ACFT GROUNDED. REPAIRED IAW SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 43,011 hrs · 16,478 cycles

RT HORIZONTAL STABILIZER LOWER SURFACE HAS A CRACK AT STABILIZER STA 147.9 8.5" AFT OF FRONT SPAR APPROX .5" IN LENGTH. DOT APPLIED. ACFT GROUNDED. REPAIRED IAW SRM 55-10-01-2R-11, INSPECTION THRESHOLD 56,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION, METHOD: DETAIL VISUAL INSPECTION AND EXTERNAL LOW FREQUNECY EDDY CURRENT INSPECTION INTERVAL: 9,000 FLT CYCLES.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,750 hrs · 14,095 cycles

EMERGENCY BATTERY POWER SUPPLY 1694 WOULD NOT CHARGE. R & R POWER SUPPLY AND TEST GOOD IAW AMM 33-51-06-960-806.

Part: INTERCOSTAL — CORRODED (BS 986.5-1006) · corrosion level 2 · airframe 36,750 hrs · 14,095 cycles

MACHINED INTERCOSTAL AT BS 986.5 - 1006, LBL 32.1 CORRODED AND HAS ELONGATED HOLES. REPLACED INTERCOSTAL. WORK ACCOMPLISHED IAW SRM 53-70-51 REPAIR 4.

Part: INTERCOSTAL — CRACKED (BS 986.5-1006) · airframe 36,750 hrs · 14,095 cycles

MACHINED INTERCOSTAL AT BS 986.5 - 1006, RBL 32.10 IS CRACKED AND HAS ELONGATED HOLES. REPLACED MACHINED INTERCOSTAL. WORK ACCOMPLISHED IAW SRM 53-70-51, REPAIR 4.

Part: FLOOR SUPPORT — CORRODED (BS 328-344) · corrosion level 2 · airframe 36,750 hrs · 14,095 cycles

FLOOR SUPPORT CORRODED AT BS 328 TO 344, BL 6. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 36,750 hrs · 14,095 cycles

MAIN CABIN INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL IAW SRM 51-40-02. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-02. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 312-324) · corrosion level 2 · airframe 36,750 hrs · 14,095 cycles

MAIN CABIN FLOOR SUPPORT CORRODED. R & R IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 36,750 hrs · 14,095 cycles

MAIN INTERCOSTAL CRACKED. LT SIDE BS 328, BL 48. REMOVED CRACKED INTERCOSTAL IAW SRM 51-40-02. LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 986.5) · corrosion level 2 · airframe 36,750 hrs · 14,095 cycles

MAIN CABIN BS 986.5 FLOORBEAM CORRODED ON UPPER TEE THE ENTIRE LENGTH. REPAIRED FLOORBEAM LBL 52-RBL 52 IAW SRM 53-70-51, REPAIR 4.

Part: SEAT TRACK — GOUGED (BS 500K-520) · airframe 36,750 hrs · 14,095 cycles

SEAT TRACK AT BS 520, RBL 24.75 IS GOUGED. ACFT GROUNDED. ALL WORK REPAIRED SEAT TRACK ACCOMPLISHED IAW ASA EA NR 900-53EA 10084, REV NEW. IAW REO G16060, REV A DATE 04/04 2013.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 36,750 hrs · 14,095 cycles

SEAT TRACK AT BS 520, LBL 24.75 IS GOUGED. ALL WORK REPAIRED SEAT TRACK ACCOMPLISHED IAW ASA EA NR 900-53EA-10084, REV NEW DATE 04/04 2013 IAW REO G16060, REV A DATE 04/04 2013.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 36,750 hrs · 14,095 cycles

SEAT TRACK AT BS 520, LBL45.50 IS GOUGED. REPAIRED SEAT TRACK, IAW EA NR 900-53EA-10084, REV NEW & REO-G16060, REV A.

Part: SEAT TRACK — GOUGED (BS 500K-520) · airframe 36,750 hrs · 14,095 cycles

SEAT TRACK AT BS 520, RBL 45.50 IS GOUGED. REPAIRED IAW EA NR 900-53EA-10084, REV NEW & IAW REO G16060, REV A.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 34,173 hrs · 13,169 cycles

TWO CRACKS IN LT HORIZONTAL STAB LOWER SURFACE, APPROX STAB STA 130 LOWER IN GAP SKIN CRACK 1.3L AND 1.2L. REPAIRED IAW SRM 51-10-01, REPAIR 11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 34,173 hrs · 13,169 cycles

POSSIBLE CRACK RT HORIZONTAL LOWER SURFACE APPROX STAB STA 130. ACFT GROUNDED. STOP DRILLED 2 CRACKS AND INSTALLED REPAIR DOUBLER IAW SRM 55-10-01, REPAIR 11.

Part: TRACK — LACK OF LUBE (SLIDING WINDOW) · airframe 32,722 hrs · 12,641 cycles

CAPTS SLIDING WINDOW HARD TO MOVE UP AND DOWN WINDOW TRACK. APPEARS TO BE HITTING. LUBED TRACKS AND EXAMINED CAPT SLIDING WINDOW. OPS CHECK NORMAL. PER MM 56 12 11 400.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 30,474 hrs · 11,824 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT SPLICE PLATE BETWEEN FLOORBOARD 140EF AND 140BF IS CORRODED. REMOVED AND REPLACED SPLICE TEE IAW B737 900 SRM 51 40 02 AND 53 00 53.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 30,474 hrs · 11,824 cycles

AFT PIT FLOOR SUPPORT BUTT SPLICES (146A7506 11 13 14) FOUND CORRODED. REMOVED AND REPLACED BUTT SPLICES PER B737 900 SRM 53 00 53.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,474 hrs · 11,824 cycles

SEVERAL FLOOR RAILS AT AFT CARGO FOUND CORRODED AT SEVERAL RAIL SEGMENTS (146A7503 38 41 42 49 50 57). REPAIRED OUT OF LIMIT FLOOR SUPPORTS IAW B737 400 SRM 53 00 53 FIG 201.

Part: BEAM — GOUGED (LT MLG) · airframe 30,474 hrs · 11,824 cycles

LEFT MLG ACTUATOR WALKING BEAM GOUGED ON AFT LOWER SIDE. REPAIRED ACTUATOR WALKING BEAM IAW ASA EA900 32EA 05687 AND REO G13767 REV A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,474 hrs · 11,824 cycles

AFT CARGO FLOOR SUPPORT NUT PLATE MISSING AND HOLE CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED SECTION FABRICATED REPAIR PARTS ALODINED PRIMED AND INSTALLED PER B737 900 SRM 53 00 53.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 30,474 hrs · 11,824 cycles

AFT CARGO FLOOR SUPPORT HAD 2 MISDRILLED HOLES. REPAIRED FLOOR SUPPORT IAW B737 900 SRM 53 00 53 REPAIR 2 FIG 201.

Part: SPLICE — CORRODED (CARGO BAY) · airframe 30,474 hrs · 11,824 cycles

AFT CARGO FLOOR BUTT SPLICE CORROSION AROUND NUT PLATES BS 887. REMOVED AND REPLACED SPLICE IAW BOEING DWG 146A9401.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,474 hrs · 11,824 cycles

FWD CARGO BAY FLOOR SUPPORT CORRODED AT NUT PLATE HOLE. REMOVED AND REPLACED WITH NEW IN ACCORDANCE WITH B737 900 SRM 51 40 02.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 30,474 hrs · 11,824 cycles

FWD ENTRY DOOR SKIN EXISTING REPAIR HAD OVERSIZED HOLE. REMOVED EXISTING REPAIR AND FILLER CUTOUT DAMAGED AREA PERFORMED HFEC OF NEW CUTOUT AND EXISTING CUTOUT NO CRACKS FOUND. FABRICATED REPAIR DOUBLER FROM 2024 T3 .071 AND NEW FILLER FROM 2024 T3 .063. APPLIED ALODINE AND PRIMER. REPAIRED REF B737 900 SRM 52 00 01 REPAIR 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,616 hrs · 11,492 cycles

RT FUSELAGE SKIN AT STA 278.5 STR 21 HAS 1EA FASTENER WITH LIGHTNING STRIKE. REPAIRED DAMAGED STRINGER IAW B737 900 SRM 53 00 03 FIG 206. REPAIRED SKIN IAW B737 900 SRM 53 00 01 REPAIR 1.

Part: WINGLET — DAMAGED (LT WING) · airframe 29,616 hrs · 11,492 cycles

TWO EA LIGHTNING STRIKES FOUND ON LT WINGLET. TIP REPAIRED PER ASA EA 900 57EA 4959 AND REPLACED 737 0352 3.

Part: SKIN — BENT (L1 DOOR) · airframe 29,002 hrs · 11,272 cycles

L1 DOOR UPPER AFT DOUBLER RT TOP CORNER BENT OUT. REPAIR PER SRM 737 900 / EA 900 52EA 04526.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,249 hrs · 10,601 cycles

DAMAGE ON PRESSURIZED FUSELAGE SKIN BELLY. DENT WITH GOUGE AND CREASE. CUTOUT DAMAGE O/B FRAME AND SKIN AND INSTALLED REPAIR PARTS.

Part: STRUCTURE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON FWD CARGO BAY NR 4 RT CAPSTRIP HAS CORROSION. REMOVED AND REPLACED CAPSTRIP.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON FWD CARGO BAY NR 3 RT CAPSTRIP HAS CORROSION. REMOVED AND REPLACED CAPSTRIP.

Part: SUPPORT — CRACKED (RT WING) · airframe 25,253 hrs · 9,820 cycles

RT WING I/B FIXED T/E UPPER PANEL SUPPORT AT WBL 189 TO 201 SUPPORT CRACKED. REPLACED T/E UPPER PANEL SUPPORT.

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 25,253 hrs · 9,820 cycles

SPLICE PLATE CRACKED AT BS 727I. REPLACED CRACKED PLATE.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 25,253 hrs · 9,820 cycles

FOUND CRACK IN CARGO TRACK RADIUS. REMOVED AND REPLACED TRACK SECTION.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON BULKHEAD TO FLOOR SUPPORT FWD CARGO BAY. REMOVED AND REPLACED BULKHEAD TO FLOOR SUPPORT.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 25,253 hrs · 9,820 cycles

AFT CARGO BAY CARGO TRACK CRACKED IN TWO PLACES. REMOVED AND REPLACED TRACK SECTION.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON BULKHEAD SUPPORT FWD CARGO BAY. REMOVED AND REPLACED BULKHEAD SUPPORT IN FWD CARGO BAY.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,253 hrs · 9,820 cycles

M1674 BATTERY PACK FAILS DEEP CYCLE. REMOVED AND REPLACED BATTERY PACK AND TESTED.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,253 hrs · 9,820 cycles

M1673 BATTERY PACK FAILS DEEP CYCLE. REMOVED AND REPLACED BATTERY PACK AND TESTED.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,253 hrs · 9,820 cycles

M1676 BATTERY PACK FAILS DEEP CYCLE. REMOVED AND REPLACED BATTERY PACK AND TESTED.

Part: BAFFLE — CRACKED (BS 500J) · airframe 25,253 hrs · 9,820 cycles

FWD CARGO BAY FLOOR TO SIDEWALL BAFFLE CRACKED BEYOND LIMITS. REMOVED CRACKED BAFFLE FABRICATED NEW BAFFLE AND INSTALLED.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,253 hrs · 9,820 cycles

M1695 BATTERY PACK FAILS DEEP CYCLE. REMOVED AND REPLACED BATTERY PACK AND TESTED.

Part: SUPPORT — CORRODED (BS 727E-727I) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT PIT. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT. REPAIRED FLOOR TO SIDEWALL SUPPORT.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 25,253 hrs · 9,820 cycles

RT HORIZONTAL STAB FIXED L/E HAS A DENT OUT OF LIMITS. REPAIRED RT HORIZONTAL STAB FIXED L/E.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

FLOOR TO SIDEWALL SUPPORT ACB CORROSION OUT OF LIMITS. REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (BS 727-727E) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

FLOOR TO SIDEWALL SUPPORT IN ACB CORROSION OUT OF LIMITS. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (BS 500E-500L) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE OUT OF LIMITS. REMOVED AND REPLACED SUPPORT PLATE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

FOUND CORROSION ON FLOOR TO SIDEWALL PLATE FWD PIT. REPLACED FLOOR TO SIDEWALL SUPPORT PLATE FWD CARGO BAY.

Part: SUPPORT — CORRODED (BS 727I-767) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727I. REPAIRED CORRODED AREA.

Part: WEB — CRACKED (BS 500I) · airframe 25,253 hrs · 9,820 cycles

CRACK ON BAFFLE BS 500I+1 AND DAMAGE ON SAME BAFFLE IN FWD PIT. REMOVED AND REPLACED BAFFLE.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 25,253 hrs · 9,820 cycles

RIGHT WING T/E UPPER PANEL BULKHEAD FLANGE IS CRACKED BETWEEN SPOILER NR 7 AND NR 8. REMOVED AND REPLACED SUPPORT FITTING ON RIGHT WING T/E.

Part: WEB — CORRODED (BS 500H) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON BAFFLE AROUND FASTENER HOLE IN FWD PIT. REMOVED AND REPLACED BAFFLE.

Part: WEB — CORRODED (BS 500K-500L) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON BAFFLE AROUND FASTENER HOLES IN FWD PIT. REMOVED AND REPLACED BAFFLE BS 500K TO 500L LBL 24.

Part: FRAME — CORRODED (BS 500K) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON FRAME AT BS 500K. REPAIRED FRAME.

Part: FRAME — CORRODED (BS 500K) · corrosion level 2 · airframe 25,253 hrs · 9,820 cycles

CORROSION ON FRAME BS 500K OUT OF LIMITS. REMOVED CORROSION AND REPAIRED FRAME.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 25,253 hrs · 9,820 cycles

LT HORIZ STAB LOWER SKIN CRACKED FWD OF REAR SPAR. REPAIRED LT HORIZ STAB LOWER SKIN.

Part: SKIN — CHAFED (LE SLAT) · airframe 25,253 hrs · 9,820 cycles

NR 8 SLAT IS CHAFED ON UPPER T/E LOWER SURFACE O/B END. REPAIRED NR 8 SLAT LOWER SURFACE.

Part: WEDGE — CHAFED (LE SLAT) · airframe 25,253 hrs · 9,820 cycles

NR 8 SLAT I/B END UPPER T/E WEDGE LOWER SURFACE IS CHAFED. REMOVED, REPAIRED AND RE-INSTALLED NR 8 SLAT.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 25,253 hrs · 9,820 cycles

LEFT O/B TRAILING EDGE FLAP HAS DELAMINATED ON THE I/B CORNER 2 X 3 INCHES BOTH UPPER AND LOWER SURFACES. REPAIRED LT OB TE FLAP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,253 hrs · 9,820 cycles

M1672 EMERGENCY EXIT LIGHT BATTERY PACK FAILED DEEP CYCLE CHECK. REMOVED AND REPLACED M1672 BATTERY PACK PWR SUPPLY.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 24,236 hrs · 9,405 cycles

L1 AFT UPPER CORNER SHOWS SIGNS OF SEPARATION ON OUTER SKIN (PREVIOUS REPAIR DOUBLER). REMOVED PREVIOUS REPAIR DOUBLER AND INSTALLED NEW REPAIR DOUBLER.

Part: GUIDE ARM — OUT OF ADJUST (R1 DOOR) · airframe 23,791 hrs · 9,225 cycles

R 1 DOOR HARD TO CLOSE AND HARD TO GET LIGHT OUT. FOUND JAM NUT LOOSE ON GUIDE ARM. READJUSTED GUIDE ARM. DOOR OPS CKS GOOD REF, TASK 52 41 00 820 801 STEP 1. TESTED GALLEY SERVICE DOOR WARNING SYSTEM. OPS CHECKED GOOD.

Part: BUTTON — BROKEN (R1 DOOR) · airframe 22,898 hrs · 8,901 cycles

R1 DOOR GUST LOCK RELEASE BUTTON BROKEN. INSTALLED NEW GUIDE ARM LOCKING BUTTON, MFG P/N 57141. DOOR OPS CHECK NORMAL REF M/M 52 41 21 400 801 ITEM D.

Part: SKIN — CRACKED (L1 DOOR) · airframe 22,517 hrs · 8,773 cycles

L 1 DOOR HAS SKIN CRACK AT TOP GATE/HINGE AREA AT AFT CORNER. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 52 10 02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,726 hrs · 7,702 cycles

CARGO FLOOR TRACK CORRODED ON UPPER AND LOWER SURFACE MOSTLY AROUND NUT PLATE HOLES RBL 13 TO RBL 14 STA 802 TO STA 846. REMOVED DAMAGED CARGO TRACK SECTION STA 767 TO STA 887, LOCATED, FABRICATED A REPLACEMENT TRACK AND SPLICE DRILLED AND INSTALLED IAW B737 900 SRM 53 00 53 REP 4.

Part: FLOORBOARD — CRACKED (CABIN) · airframe 19,726 hrs · 7,702 cycles

CABIN AFT FLOORBOARD AT STA 947 TO STA 986 LBL 17 TO LBL 43 CORNER CRACKED. PREPARED DAMAGED AREA APPLIED POTTING COMPOUND BMS 5 28 TYPE 19 TO DAMAGED CORE: 8 LAYERS (4 EACH SIDE) OF BMS 9 3 1581, REPAIR PLY BONDED IAW B737 900 SRM 53 00 50 PG 201-203.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,726 hrs · 7,702 cycles

CABIN FLOORBEAM CORRODED STA 947.5 AT BL 0 AREA. REMOVED CORROSION, HFEC INSPECTED REWORKED AREA NO CRACKS NOTED. FABRICATED REPAIR STRAP, REPAIR PARTS, LOCATED, DRILLED AND INSTALLED IAW AAR EA 12572 AND ASA EA 5310 02783.

Part: FLOORBOARD — DELAMINATED (BS 907-946) · airframe 19,726 hrs · 7,702 cycles

CABIN AFT FLOORBOARD STA 907 TO STA 946 LBL 17 TO LBL 50 IS DELAMINATED AT INSERTS. PREPARED DAMAGED AREA APPLIED POTTING COMPOUND BMS 5 28 TYPE 19 AND 4 LAYERS OF BMS 9 3 1581, FABRIC REPAIR PLY BONDED IAW B737 900 SRM 53 00 50 REP 1 PGS 201 202.

Part: FLOORBOARD — DELAMINATED (BS 887-907) · airframe 19,726 hrs · 7,702 cycles

AFT CABIN FLOORBOARD STA 887 TO STA 907 RBL 47 TO RBL 67 IS DELAMINATED. PREPARED DAMAGED AREA APPLIED POTTING COMPOUND BMS 5 28 TYPE 19 AND 4 LAYERS BMS 9 3, FABRIC REPAIR PLY BONDED AREA IAW B737 900 SRM 53 00 50 REP 6 PGS 201 203.

Part: FLOORBOARD — DELAMINATED (BS 887-907) · airframe 19,726 hrs · 7,702 cycles

CABIN FLOORBOARD STA 887 TO STA 907 DELAMINATED LBL 47 TO LBL 63. PREPARED DAMAGED AREA APPLIED POTTING COMPOUND BMS 5 28 TYPE 19 AND 4 LAYERS BMS 9 3, FABRIC REPAIR PLY BONDED DAMAGED AREA IAW B737 900 SRM 53 00 50 REP 6 PG 201 203.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,726 hrs · 7,702 cycles

CABIN FLOORBEAM CORRODED IN 2 EACH AREAS STA 986.5. REMOVED UPPER CHORD DAMAGED HORIZONTAL FLANGE, FABRICATED, LOCATED, DRILLED AND INSTALLED REPLACEMENT UPPER T-CHORD AND REPAIR ANGLES AND STRAPS IAW AREA 12566 AND ASA EA 5310 02782.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,726 hrs · 7,702 cycles

MLG W/W KEEL BEAM SUPPORT PANEL MATING SURFACE CORRODED STA 686 RBL 8 TO LBL 8. REMOVED, DAMAGED SUPPORT FITTING, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SUPPORT FITTING IAW B737 900 SRM 51 40 02 PG 6 7 AND SRM 51 40 05 FIG 2 PG 3.

Part: SKIN — GOUGED (FUSELAGE) · airframe 19,726 hrs · 7,702 cycles

AFT LEFT EXTERNAL FUSELAGE DENT WITH A GOUGE AT STA 1030 BELOW STR 12 LT. CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW 737 900 SRM 53 00 01 PGS 201 THRU 207 REPAIR 3.

Part: SKIN — DENTED (BS 810-833) · airframe 19,726 hrs · 7,702 cycles

LEFT AFT FUSELAGE SKIN DENT ON FRAME STA 827 STR 21L WITH DENT AT STA 817. CUT OUT DAMAGED AREA IAW AAR EA 12569, FABRICATED FILLER DOUBLER AND TRIPLER IAW AAR EA 12569, INSTALLED REPAIR PARTS IAW AAR EA 12569 AND ASA EA 5330 02325.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

AFT CARGO CHANNEL SPLICE CORRODED. REPAIRED IAW SRM 51-40-05.

Part: SKIN — PUNCTURED (RUDDER) · airframe 14,338 hrs · 5,407 cycles

RUDDER HAS PUNCTURE ON LOWER LT SIDE. REPARIED IAW SRM 51 70 05.

Part: FLOOR SUPPORT — CORRODED (BS 771-887) · airframe 14,338 hrs · 5,407 cycles

AFT PIT RT FLOOR SUPPORT IS CORRODED REPAIRED IAW EA 5320 01776.

Part: FLOOR SUPPORT — MISDRILLED (BS 500E-500F) · airframe 14,338 hrs · 5,407 cycles

FWD CARGO PIT HOLES DRILLED IN MIDDLE FLOOR SUPPORT BS 500E REPAIRED IAW 53 00 53.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,338 hrs · 5,407 cycles

AFT PIT PH TRANSITION PANEL IS CORRODED AT BS 727I REPAIRED IAW SRM 53 00 53 NR 5.

Part: TRANS PANEL — CORRODED (BS 727) · corrosion level 2 · airframe 14,338 hrs · 5,407 cycles

AFT PIT RT TRANSITION PANEL IS CORRODED BS 727 REPAIRED IAW SRM 53 00 53 REPAIR 5.

Part: FLOOR PANEL — CORRODED (BS 767-887) · corrosion level 2 · airframe 14,338 hrs · 5,407 cycles

AFT CARGO PIT FLOOR PANEL NR 4 CORRODED REPAIRED IAW 51 40 05 FIG 2.

Part: FLOOR PANEL — GOUGED (BS 500-500D) · airframe 14,338 hrs · 5,407 cycles

FWD FIT FLOOR PANEL NR 3 UPPER SURFACE GOUGED REPAIRED IAW SRM 51 04 05 FIG 2.

Part: TRANS PANEL — CORRODED (BS 727) · corrosion level 2 · airframe 14,338 hrs · 5,407 cycles

AFT PIT LT TRANSITION PANEL SIDE PLATE IS CORRODED AT BS 727, REPAIRED IAW SRM 53 00 53.

Part: HMU — DAMAGED (NR 2 ENGINE) · airframe 10,563 hrs · 3,896 cycles

YYC - AFTER START ON NR 2 ENGINE LEVER RAISED TO IDLE MASTER CAUTION ENGINE AND ENGINE CONTROL ON OVERHEAD PANEL ILLUMINATED. GROUND CREW AND OTHER ACFT REPORTED SMOKE AND TORCHING ON NR 2 ENGINE. NR 2 ENGINE LEVER PLACED TO CUT OUT PER TAIL PIPE FIRE CHECK LIST. SMOKE IN CABIN NOTED AND A CABIN EVACUATION WAS INITIATED. WHEN CHECK LIST COMPLETED NO SMOKE IN CABIN OR FROM ENGINE WAS NOTED. FIRE HANDLES PULLED BUT NOT TURNED. WHILE PERFOMING VISUAL INSPECTION NOTED OIL IN THE TAIL PIPE. REPLACED NR 2 ENGINE DUE TO OIL LEAK PER TASK CARD 78471000.

Part: SKIN — GOUGED (CARGO DOOR)

PAE - DURING CHECK, FOUND GOUGES AND DENTS ON AFT CARGO DOOR OUTER SKIN. REPAIRED IAW EA 5230-01265. (M)

Part: ANGLE — CORRODED (BS 500L)

PAE - DURING CHECK, FOUND CORROSION ON FORWARD CARGO BAY AFT BULKHEAD LOWER SUPPORT ANGLE. REPAIRED IAW SRM 51-40-02. (M)