N320AS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,387 hrs · 26,383 cycles

APU SHUTDOWN AUTOMATICALLY INFLIGHT DUE TO MEL ON #1 IDG THIS PUT US IN A SINGLE AC SOURCE SITUATION RAN QRH AND DIVERTED TO KSMF. GROUNDED - YES. DIVERSION - FOUND CANNON PLUG BACKSHELL ON OIL PRESSURE MODULE LOOSE REMOVED AND INSPECTED PLUG AND PINS REINSTALLED APU OPS CHECK NORMAL. (REF 60588686)

Part: LAMP — INOPERATIVE (L AFT EXTERIOR F) · airframe 64,247 hrs · 25,893 cycles

L2 EXTERIOR EMERGENCY EXIT DOOR LIGHT INOP. GROUNDED - YES. RELAMPED IAW 33-51-04-960-801. OPS TEST GOOD.

Part: POWER SUPPLY — INOPERATIVE (MAIN PASSENGER C) · airframe 62,185 hrs · 24,972 cycles

EMERGENCY LIGHTS COMMON TO POWER SUPPLY M1676 INOP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY (M1676) AND INSTALLATION TEST GOOD IAW B737-900 AMM 33-51-06-960-806.

Part: SKIN — CRACKED · airframe 62,185 hrs · 24,972 cycles

L/H S-STAB LOWER SKIN HAS A CRACK LOCATED BETWEEN STAB STA. 129.50 AND 138.70 APROX. 1.5" LONG. CRACK LOCATION HAS BEEN MARKED AND ENDS OF CRACK HAVE BEEN MARKED. GROUNDED - YES. REPAIRED THE L/H HORIZ STAB LOWER SKIN USING MAT .100 2024-T3 AND .071 2024-T3 PER B737-900 SRM 55-10-01-2R-11.REPAIR IS A CAT "B" AND HAS AN INSPECTION THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES PER B737-900 SRM 55-10-01-2R-11.5.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,340 hrs · 24,158 cycles

A/C LEFT, LAST TWO EMERGENCY EXIT AISLE LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK (M1898) REF B737-900 AMM 33-51-06-960-806. 4 C/B'S OPENED, TAGGED, AND RESET. ALL EMERGENCY LIGHTS OPS TEST PASS.

Part: LIGHT — BROKEN (CABIN) · airframe 60,188 hrs · 24,093 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO L-1 DOOR IS BROKEN. GROUNDED - YES. REMOVED, REPLACED, AND TESTED EXIT LOCATOR SIGN AT L-1 DOOR PER B737-900 MM 33-51-01-960-802 - OPS NORMAL.

Part: FLAP — BROKEN (RH WING OTBD RH) · airframe 59,608 hrs · 23,839 cycles

AFTER INFLIGHT USE OF SPEEDBRAKES, WITH SPEED BRAKES STOWED. AIRCRAFT HAD A STRONG RIGHT ROLL TENDENCY. NO ABNORMAL INDICATIONS. WINGS LEVEL FLIGHT REQUIRED 2.5 UNITS LEFT RUDDER TRIM AND 3 UNITS LEFT AILERON. DURING APPROACH HAD A STRONG RIGHT TENDENCY WITH SELECTION OF FLAPS TO 258 AND 30. GROUNDED - YES. PERFORMED GVI OF FLIGHT CONTROLS, FOUND THE INBOARD ROLLER ON THE R/H TRAILING EDGE FLAP (OUTBOARD) HAS BROKEN OFF AND DEPARTED THE A/C. INSTALLED R/H OUTBOARD AFT FLAP PER B737-900 AMM 27-51-22-400-801. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 58,875 hrs · 23,527 cycles

RT AFT EXIT DOOR (R2) EMERGENCY EXIT LIGHTS OUTSIDE & INSIDE DOOR FAILS BATTERY TEST. GROUNDED-YES. REMOVED & REPLACED AFT OVERHEAD FDR PANEL BATTERY PACK S/N 117142 AND OPERATIONS CHECK GOOD, IAW B737-900 AMM 33-51-06-960-806.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 57,701 hrs · 23,048 cycles

FWD CARGO BAFFLE BETWEEN L/H STA 500D TO 500E, LBL 24 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE IAW B737 900 SRM 51 40 02 0G AND B737 900 SRM 51 40 05 0G 0.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 57,701 hrs · 23,048 cycles

FWD CARGO BAFFLE BETWEEN L/H STA 500H TO 500I, LBL 24 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE IAW B737 900 SRM 51 40 02 0G 0 AND B737 900 SRM 51 40 05 0G 0.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,701 hrs · 23,048 cycles

(ODR) BULLNOSE EMERGENCY LIGHTS AT L/H ROWS 6,8,11 FAILED BATTERY CAPACITY CHECK. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT L/H SEAT ROW 6, OPS CK IS GOOD AT L/H ROWS 6 ,8,11 EMERGENCY LIGHTS IAW B737 NG AMM 33 51 06 960 805.

Part: TRIM PANEL — DAMAGED (COCKPIT) · airframe 56,244 hrs · 22,373 cycles

FO R2 WINDOW WILL NOT OPEN PAST FIRST DETENT. GROUNDED - YES. FOUND R2 WINDOW PANEL PLASTIC TRIM STUCK UNDER FWD ROLLER. REMOVED TRIM, R2 WINDOW OPS CK GOOD. FOUND LOWER TRIM SURROUND BELOW R2 WINDOW DAMAGED. REQUIRES P/N 232A1514-6.

Part: ACTUATOR — FAILED (FUEL SYSTEM) · airframe 56,163 hrs · 22,334 cycles

SUSPECTED FUEL LEAK ON # 2 ENGINE OR RIGHT WING. QUANTITES ON # 2 SIDE DECREASED 10 LBS EVERY 1.5-2 MIN FUEL TOTALIZER WENT DOWN PROJECTED INITIALLY 600 LBS FROM PLANNED 7.4 TO 6.8 LANDING FUEL BURN RATES WERE CLOSE TO IDENTICAL FINAL INDICATED LOSS WAS 500LBS. GROUNDED - YES. EMERGENCY LANDING - PERFORMED FQIS BITE IN REF TO FIM 28-41 NO FAULTS NOTED IN CURRENT STATUS OR FAULT HISTORY TRANSFERRED FUEL IN AND OUT OF TANK 2 NO ABNORMALITIES NOTED DURING FUEL TRANSFER. OPENED # 2 ENG COWL AND CORE COWL PERFORMED VISUAL INSPECTION NO FUEL LEAKS NOTED. WALKAROUND WAS PERFORMED NO FUEL LEAKS FOUND. PERFORMED ACTUATOR TEST REF AMM 71-00-00-700-807-F00 NO LEAKS TEST NORMAL. PERFORMED ENGINE RUN NO LEAKS NOTED SUMPED #1 AND #2 FUEL TANKS PER AMM 12-11-00. PERFORMED CROSSFEED VALVE OPS TEST PER AMM 28-22-00 FOUND FUEL TRANSFERRING 10 POUNDS EVERY 2 MIN. REMOVED AND REPLACED ACTUATOR OF THE ENGINE FUEL CROSSFEED VALVE REF AMM TASK 28-22-21. OPS & LEAK CKS GOOD.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 55,863 hrs · 22,188 cycles

FORWARD CABIN ANNUNCIATION LIGHT COVER FELL OFF. GROUNDED - YES. REMOVED & REPLACED FWD OVERHEAD EXIT SIGN LIGHT ASSY AND INSTALLED REPLACEMENT FWD CABIN LIGHT COVER. OPS NORMAL IAW AMM 33-51-01 AND AMM 23-43-00.

Part: LENS — MISSING (EXIT SIGN) · airframe 55,673 hrs · 22,103 cycles

EXIT LIGHT COVER ABOVE R1 DOOR IS MISSING. GROUNDED - YES. REMOVED AND REPLACED EXIT SIGN LENS COVER AND LIGHT ASSEMBLY ABOVE R1 DOOR. OPS CHK GOOD. REF AMM 33-51-01.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 53,759 hrs · 21,202 cycles

LT AFT OVERWING EMERGENCY EXIT LIGHT IS BURNT OUT. GROUNDED - YES. REPLACED BULB AT LT AFT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.

Part: SIGN — BROKEN (CABIN) · airframe 52,669 hrs · 20,679 cycles

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

Part: STRINGER CLIP — CRACKED (BS 500A) · airframe 51,875 hrs · 20,294 cycles

FWD CARGO BAY FRAME, BS 500A HAS A CRACKED STRINGER CLIP 21L. ACFT GROUNDED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, ITEM D PAGE 6.

Part: SUPPORT — CORRODED (BS 990) · corrosion level 2 · airframe 51,875 hrs · 20,294 cycles

AFT WET AREA GALLEY GUTTER BS 990, LBL 36 TO LBL 48 IS CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE GALLEY GUTTER IAW SRM 51-40-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 727A-807) · corrosion level 2 · airframe 51,875 hrs · 20,294 cycles

AFT CARGO BAY, LT TRANSITION PANEL HAS MULTIPLE AREAS OF CORROSION FROM BS 727A TO 807. ACFT GROUNDED. REMOVED CORROSION WAS FOUND TO BE OUT OF LIMITS, REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 51,875 hrs · 20,294 cycles

AFT CARGO PIT FLOOR TRACK SUPPORT IS CRACKED IN RADIUS ABOVE ATTACH POINTS AT RBL 16 STA 727E, 727G, 727I, AND 727J. GROUNDED - YES. CUT OUT AND REPAIRED DAMAGED SECTION OF TRACK IAW SRM 53-00-53-2R-3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 51,875 hrs · 20,294 cycles

AFT CARGO PIT FLOOR SUPPORT TRACK HAS CORR AROUND TIE DOWN POINT AT STA 727A LBL16. GROUNDED - YES. REPAIRED DAMAGED SECTION OF CARGO TRACK IAW SRM 53 00 53 2R 3 W 1IN. O .072 R .054 L 3FT. D .018.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 51,875 hrs · 20,294 cycles

L1 DOOR EMERGENCY LIGHT BATTERY FAILED A CHECK. ACFT GROUNDED. REMOVED AND INSTALLED A SERVICEABLE BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-06-960-805.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 51,875 hrs · 20,294 cycles

LEFT FWD OVERWING EMERGENCY LIGHT BATTERY FAILED A CHECK. ACFT GROUNDED. REMOVED, AND REPLACED THE LT OVERWING EMERGENCY LIGHT BATTERY PACK M1694. EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-51-06-960-805.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 51,875 hrs · 20,294 cycles

R1 DOOR EMERGENCY LIGHT BATTERY FAILED A CHECK. ACFT GROUNDED. REMOVED AND INSTALLED A SERVICEABLE R1 DOOR EMERGENCY EXIT LIGHT BATTERY PACK IAW AMM 33-51-06-960-805.

Part: TRANSMITTER — FAILED (TE FLAP) · airframe 50,869 hrs · 19,840 cycles

LE FLAPS AMBER LIGHT ILLUMINATED FLAPS LESS THAN ONE, FLAPS WOULD NOT EXTEND PER QRH ALTERNATE METHOD. GROUNDED - YES. EMERGENCY DECLARED - CONFIRMED FAULT, FSEU BITE SHOWS "TE FLAP SNSR FAULT MSG 27-52259". T/S PER FIM 27-51 TASK 813 TE FLAP SNSR L, FOUND LT FLAP POSN SNSR OFF BY 3 DEGREES (TOLERANCE 0.4 DEG). ALSO, NOTICED LT FLAP NEEDLE ON FLAP POSN INDICATOR ERRATIC & STICKING. REMOVED & REPLACED LT FLAP POSN XMTR (T427) REF AMM 27-58-01 & ADJUSTED/TESTED REF AMM 27-58-01-820-801. ALSO, REPLACED FLAP POSN INDICATOR AS PRECAUTIONARY REF AMM 27-58-02, OPS CK NML. ACCOMPLISHED ALTERNATE DEACTIVATION PROCEDURES REF ASA MAINTENANCE PROGRAM SEC 5-07-01 TABLE 3 ITEMS 1,3,4. REVERSED ALT DEACT PROCEDURES. REF L/P 11818301 FOR A/C APPROACH SURVEY, LLM STATUS REMAINS CAT3A AUTOLAND & HGS. ACCOMPLISHED GP45 FLAP SNSR LRU REPLACEMENT TEST, GP49 DFCS LAND VERIFY TEST REF AMM 22-11-00 AND HGS SYSTEM TEST REF SMM 34-36-00, OPS CK NML.

Part: BEARING — WORN (L1 DOOR) · airframe 50,583 hrs · 19,711 cycles

FORWARD ENTRY DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. FOUND THE L1 DOOR SKIN CLEARANCE TO BE TIGHT AT AFT UPPER EDGE IAW AMM 52-11-00-820-801, STEP 2.J. REPLACED SEVERELY WORN FUSELAGE TORQUE TUBE BEARINGS AND BEARING PLATES IAW DRAWING 141A8205. REINSTALLED & ADJUSTED THE L1 DOOR IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: NUT — LOOSE (L1 DOOR GUIDE) · airframe 49,228 hrs · 19,105 cycles

FA REPORTS L1 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. INSPECTED AND FOUND UPPER GUIDE ARM NUT LOOSE. ADJUSTED UPPER GUIDE ARM IAW AMM 52-11-00-820-801, STEP H. OPS CHECKED DOOR SEVERAL TIMES. DOOR CLOSES NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,191 hrs · 19,086 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT 17A. ACFT GROUNDED. INSTALLED THE LENS. OPS GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 48,935 hrs · 18,949 cycles

WHILE ACCOMPLISHING T/C # 78233001, LT & RT AFT OVERWING EXIT EMERGENCY LIGHT (EXTERIOR). LIGHT WENT OUT BEFORE TIME LIMIT. ACFT GROUNDED. REPLACED THE POWER SUPPLY BATTERY PACKS M1670 AND M1671 IAW AMM 33-51-06-960-805, OPS CHECKED GOOD.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 47,091 hrs · 18,085 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT L1 AND L2 DOORS HAS SEVERAL LAMPS INOPERATIVE. ACFT GROUNED. REPLACED THE LAMPS AND TESTED IAW AMM 33-51-01-960-801, OPS NORMAL.

Part: FLOOR SUPPORT — CRACKED (BS 747-767) · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, RT FLOOR SUPPORT BS 747-767 IS CRACKED. ACFT GROUNDED. R & R CRACKED FLOOR SUPPORT IAW SRM 51-10-02, PARA 9, SRM 51-40-02, AND BAC DWG 146A7500, REV A.

Part: FLOORBEAM — CRACKED (BS 500J) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOORBEAM ANGLE AT BS 500J AFT SIDE IS CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-02 AND BAC DWG 143A7505, REV B.

Part: FLOORBEAM — CRACKED (BS 500F) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOORBEAM ANGLE BS 500F FWD SIDE IS CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-02 AND DWG 143A7505, REV B.

Part: FLOOR SUPPORT — CRACKED (BS 500E-500F) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOOR SUPPORT BS 500E-500F IS CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-02 AND SRM 51-40-05 AND DWG 143A7505, REV B.

Part: SKIN — DENTED (BS 917) · airframe 45,793 hrs · 17,529 cycles

DEFECT 4871496, 2 EA SKIN DENTS IN SKIN BS917 BETWEEN STR 17R-18R. ACFT GROUNDED. REPAIRED THE SKIN IAW EA 900-53EA-16961, REO G19794, REV B, REPAIR IS A CAT B REPAIR, STAGE 3.

Part: FLOOR SUPPORT — CRACKED (BS 500G-500H) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOOR SUPPORT BS 500G-500H IS CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-02 AND DWG 143A7505, REV B.

Part: FLOORBEAM — CRACKED (BS 500J) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOORBEAM ANGLE AT BS 500J FWD SIDE IS CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-02 AND DWG 143A7505, REV B.

Part: FLOORBEAM — CRACKED (BS 500K) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOORBEAM ANGLE AT BS 500K AFT SIDE IS CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-05 AND DWG 143A7505, REV B.

Part: FLOORBEAM — CRACKED (BS 500K) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LEFT FLOORBEAM ANGLE BS 500K FWD SIDE IS CRACKED. ACFT GROUNDED. R & R THE ANGLE IAW SRM 51-40-02 AND DWG 143A7505, REV B.

Part: FLOOR SUPPORT — CRACKED (BS 500I-500J) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOOR SUPPORT BS 500I - 500J CRACKED. ACFT GROUNDED. REPAIRED IAW EA 90053EA-16966, REO-G19784, REV A .

Part: FLOORBEAM — CRACKED (BS 500H) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOORBEAM AT BS 500H FWD SIDE IS CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-02 AND DWG 143A7505, REV B.

Part: FLOORBEAM — CRACKED (BS 500I) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOORBEAM ANGLE AT BS 500I FWD SIDE IS CRACKED. ACFT GROUNDED. R & R THE ANGLE IAW SRM 51-40-02 AND DWG 143A7505, REV B.

Part: FLOOR SUPPORT — CORRODED (BS 500H-500L) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOOR SUPPORT CHANNEL SECTION APPROXIMATELY BS 500H+10 TO 500L IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL THICKNESS IS 0.040", MINIMUM REMAINING THICKNESS IS 0.035", REPLACEMENT OF ZEE CHANNEL SECTION APPROXIMATELY BS 500H+10 TO 500L ACCOMPLISHED ON CARD G66452, IAW SRM 53-00-53-2R-5.

Part: FLOOR SUPPORT — CORRODED (BS 500C-500H) · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, LT FLOOR SUPPORT ZEE CHANNEL SECTION APPROXIMATELY BS 500C+15 TO 500H+10 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION APPROXIMATELY BS 500C+15 TO 500F+7 AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2, ORIGINAL MATERIALS THICKNESS IS 0.040 IN REMOVED 0.004", REMAINING THICKNESS IS 0.036" ALODINED REWORKED AREAS BS 500C+15 TO 500F+7 IAW SRM 51-20-01, PRIMED REWORKED AREAS BS 500C+15 TO 500F+7 IAW BS SOPM 20-41-02 APPLIED TOPCOAT AND BLENDOUT MARKING TO REWORKED AREAS BS 500C+15 TO 500F+7 IAW AMM 51-21-73 AND 51-05-01. REPLACED LT ZEE CHANNEL SECTION SA 500F+8 TO 500L IAW SRM 53-00-53-2R-5.

Part: CHANNEL — CORRODED (BS 500A-500E) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

FWD CARGO COMPARTMENT, RT FLOOR SUPPORT ZEE CHANNEL SECTION APPROXIMATELY BS 500A TO 500E+10 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02 ORIGINAL MATERIAL 0.040" IAW SRM 53-30-53, MATERIAL LOSS 0.008", REMAINING 0.032" OUT OF LIMITS IAW SRM 53-00-53, T8225U. REMOVED Z ANGLE IAW SRM 51-40-02 AND 53-00-53 MATERIAL ID FOR Z ANGLE BAC 1496-444, PO 860620.4 IAW SRM 53-00-53 LOCATED DRILLED AND DEBURRED IAW SRM 53-00-53 ALODINED PART IAW SRM 51-20-01 PAINTED Z ANGLE IAW SOPM 20-41-02, INSTALLED Z ANGLE IAW SRM 53-00-53.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 45,793 hrs · 17,529 cycles

CRACK INDICATION NOTED ON RT LOWER HORIZONTAL STABILIZER SKIN JUST INBD OF STABILIZER BS 147.9. CRACK IS APPROXIMATELY 0.5" LONG AND APPROXIMATELY 9" FWD OF REAR SPAR. CRACK ENDS ARE MARKED AND AREA CIRCLED IN RED. ACFT GROUNDED. REMOVED DAMAGED AREA, AND ACCOMPLISH REPAIR IAW ASA SRM 55-10-01-2R-11, REMOVED 2 EA EXISTING RPEAIRS IAW SRM 51-40-02. REMOVED AND REINSTALLED L/E HORIZONTAL STABILIZER TO GAIN ACCESS IAW AMM 27-41-21.

Part: FLOOR SUPPORT — CORRODED (BS 727-727F) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, LT FLOOR SUPPORT ZEE CHANNEL SECTION IS CORRODED, APPROXIMATELY BS 727+4 TO BS 727F+10. ACFT GROUNDED. REMOVED CORROSION ON AFT CARGO LT FLOOR SUPPORT ZEE CHANNEL AT BS 727+4 TO BS 727F+10, ORIGINAL MATERIAL IS .040 REMOVED .007 REMAINING MATERIAL .033, FOUND TO BE OUT OF LIMITS AI2W SRM 53-00-53-1A2 RECEIVED NEW MATERIAL PN BAC1496-377-7075 T62, REPLACED ZEE CHANNEL SECTION APPROXIMATELY BS 727+4 TO 727+10 IAW SRM 53-00-53-2R-5 .

Part: FLOORBEAM — CORRODED (BS 727D) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, FLOOR PANEL SUPPORT TEE ASSY AT BS 727D+5 IS CORRODED, EXFOLIATED. ACFT GROUNDED. REMOVED CORROSION ON AFT CARGO TEE ASSY FLOOR SUPPORT IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL .070", MATERIAL LOSS .022" REMAINING MATERIAL .048" OUT OF LIMITS IAW SRM 53-00-53-1A-2 TOOL T8225S REPLACED TEE ASSY PO 863114.5 IAW SRM 51-10-02, PARA 9 INSTALLED ON ACFT ON CARD G664006. .

Part: SHIELD — CORRODED (BS 767-794) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, FWD DOOR SURROUND SHIELD, BS 767-BS 794 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION FROM AFT CARGO FWD DOOR SURROUND SHIELD AT BS 737-BS 794, ORIGINAL THICKNESS .050 IAW SRM 53-60-15-01-1. REMAINING THICKNESS 0.043 MATERIAL LOSS .007, FOUND BEYOND LIMITS IAW SRM 53-60-15. LOCATED, DRILLED, COUNTERSINKED AND DEBURRED NEW SHIELD IAW SRM 51-40-02. REMOVED AND INSTALLED NEW SHIELD IAW SRM 51-40-02 AND DWG 146A0081.

Part: FLOOR SUPPORT — CORRODED (BS 727F-727I) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, LT FLOOR SUPPORT ZEE CHANNEL SECTION IS CORRODED, APPROXIMATELY BS 727F+10 TO BS 727I+8. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. ORIGINAL MATERIAL THICKNESS IS 0.040, REMAINING THICKNESS IS 0.034", REMOVED 0.006". REPLACED LT ZEE CHANNEL SECTION APPROXIMATELY BS 727F+10 TO 727I+8 IAW SRM 53-00-53-2R-5 AND BAC DWG 146A7500, REV A.

Part: ANGLE — CORRODED (BS 767-787) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, DOOR SURROUND LOWER SILL WEB ANGLE, BS 767-BS 787 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1, ORIGINAL MATERIAL THICKNESS IS 0.050 IN, REMOVED 0.007 IN, REMAINING THICKNESS IS 0.043". REPLACEMENT OF NEST HIGHER ASSY, WEB ASSY 146A8123.20 ACCOMPLISHED ON CARD G6664380.

Part: FRAME — CORRODED (BS 787) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, FUSELAGE FRAME SPLICE IS CORRODED AT BS 787, BETWEEN S25-26R. ACFT GROUNDED. CORROSION ON FRAME SPLICE IS FOUND TO BE OUT OF LIMITS DUE TO LOCATION ON INNER CHORD IAW SRM 53-00-07-1A-1. R & R FRAME SPLICE IAW SRM 51-40-02 AND IAW DWG 146A1262, REV.

Part: FLOORBEAM — CORRODED (BS 772) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, FLOOR PANEL SUPPORT TEE ASSY AT BS 772 IS CORRODED, EXFOLIATED. ACFT GROUNDED. REMOVED CORROSION ON AFT CARGO FLOOR SUPPORT TEE ASSY ON BS 772 IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL .070" MATERIAL LOSS .013", REMAINING MATERIAL .057" OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPLACED TEE ASSY PO 863144.4 IAW SRM 51-10-02 PARA 9 INSTALLED ON ACFT ON CARD G664006.

Part: WEB — CORRODED (BS 767-787) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, DOOR SURROUND LOWER SILL WEB IS CORRODED AT APPROXIMATELY BS 772. ACFT GROUNDED. REMOVED CORROSION ANDD FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1. ORIGINAL MATERIAL THICKNESS IS 0.050", REMOVED 0.006 IN, REMAINING THICKNESS IS 0.044". R & R NEXT HIGHER ASSY WEB ASSY 146A8123-20 IAW SRM 51-40-02 AND BAC DWG 146A0081, REV A. INSTALLED NEW SILL WEB IAW SRM 51-40-02 AND DWG 146A0081. REV A.

Part: CHANNEL — CORRODED (BS 727J-767) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

AFT CARGO COMPARTMENT, RT FLOOR SUPPORT ZEE CHANNEL SECTION IS CORRODED, APPROXIMATELY BS 727J+6 TO BS 767. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. ORIGINAL MATERIAL THICKNESS IS 0.040 IN, REMAINING THICKNESS IS 0.033", REMOVED 0.007". REPLACED DAMAGED SECTION APPROXIMATELY BS 727J+6, BS 767 RTH IAW SRM 53-00-53-2R-5 AND DWG 146A7500, REV A.

Part: FLOORBEAM — CORRODED (BS 727I) · corrosion level 2 · airframe 45,793 hrs · 17,529 cycles

PARTS RACK AFT CARGO COMPARTMENT, FLOOR PANEL SUPPORT TEE ASSY AT BS 727I+5 IS CORRODED, EXFOLIATED. ACFT GROUNDED. REMOVED CORROSION ON AFT CARGO FLOOR SUPPORT TEE ASSY IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL .070", MATERIAL LOSS .020" REMAINING MATERIAL .050" OUT OF LIMITS IAW SRM 53-00-53-1A-2, TOOL T8225S REPLACED TEE ASSY PO 863114.5 IAW SRM 51-10-02, PARA 9 INSTALLED ON ACFT WC G664006.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 43,601 hrs · 16,646 cycles

R1 OUTSIDE DOOR EMERGENCY EXIT LIGHT OUT. ACFT GROUNDED. REPLACED THE LAMP IAW AMM 33-51-04.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 41,720 hrs · 15,916 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,169 hrs · 14,903 cycles

EXTERIOR EMERGENCY EXIT LIGHT RIGHT AFT OVERWING EXIT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP & OPS CHECKED GOOD IAW AMM 33-51-04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,169 hrs · 14,903 cycles

EMERGENCY LIGHTS POWER SUPPLY WILL NOT CHARGE. ACFT GROUNDED. REPLACED POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,169 hrs · 14,903 cycles

POWER SUPPLY WILL NOT CHARGE EMERGENCY LIGHTS. ACFT GROUNDED. REPLACED POWER SUPPLY "EMERGENCY LIGHTS".

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,169 hrs · 14,903 cycles

BATTERY PACK WILL NOT CHARGE. ACFT GROUNDED. REPLACED BATTERY PACK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,169 hrs · 14,903 cycles

EMERGENCY LIGHTS POWER SUPPLY WILL NOT CHARGE. ACFT GROUNDED. REPLACED POWER SUPPLY.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 39,169 hrs · 14,903 cycles

CRACK INDICATION FOUND RT HORIZONTAL STABILIZER LOWER SKIN BETWEEN STA.92.70 & 101.90. MARKED AT .550' LONG. 19' AFT OF L/E. ACFT GROUNDED. REMOVED DAMAGE AND INSTALLED PART 1 DOUBLER AND PART 2 FILLER ON RT HORIZONTAL STABILIZER. LOWER SKIN BETWEEN STATION 92.70 AND 101.90 19" AFT OF L/E IAW SRM 55-10-01-2R-11, REPAIR 11. .

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 39,169 hrs · 14,903 cycles

CRACK INDICATION FOUND RT HORIZONTAL STABILIZER LOWER SKIN FWD OF AFT SPAR FASTENERS BETWEEN STA 92.70 & 101.90. REPAIRED DAMAGED AREA IAW SRM 51-10-01-2R-11, REPAIR 11 ON RT HORIZONTAL STABILIZER LOWER SKIN FWD OF AFT SPAR BETWEEN STA 92.7 AND 101.9. REPAIR REQUIRES REINSPECT AT INSPECTION THRESHOLD OF 56000 FLIGHT CYLES.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 39,169 hrs · 14,903 cycles

CRACK INDICATION FOUND RT HORIZONTAL STABILIZER LOWER SKIN BETWEEN STA.138.70 & 147.90. ACFT GROUNDED. REPAIRED CRACK ON RT HORIZONTAL STABILIZER LOWER SKIN IAW SRM 55-10-01-2R-11, REPAIR 11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 39,169 hrs · 14,903 cycles

CRACK INDICATION FOUND LT HORIZONTAL STABILIZER LOWER SKIN FWD OF AFT SPAR FASTENERS BETWEEN STA.92.70 & 101.90. MARKED 1.100' LONG. ACFT GROUNDED. REMOVED DAMAGE AND LOCATED NEW FASTENER HOLES IAW SRM 55-10-01-2R-11. R & R LOCK FASTENER FROM FWD SPAR AREA IAW SRM 51-40-02. RECEIVED NEW MATERIAL, 2024-T3, CLAD PO 782718.1 PO 0 AND .071. FABRICATED NEW REPAIR DOUBLER AND FILLER IAW SR 55-10-01-2R-11. ALODINED AND PRIMERED DOUBLER AND FILLER IAW SRM 51-20-01. INSTALLED DOUBLER AND FILLER AND APPLIED FILLET SEAL IAW SRM 55-10-01-2R-11 .

Part: SEAT TRACK — CORRODED (BS 500H-500L) · airframe 39,169 hrs · 14,903 cycles

CABIN SEAT TRACK UPPER SURFACE, SCALLOPED AREA HAS CORROSION & BARE METAL. BS 500H - BS 500L, LBL 45. ACFT GROUNDED. FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1, FIG 103, DETAIL A ALODINED IAW AMM 51-21-41 PRIMED IAW AMM 51-21-99.

Part: SEAT TRACK — WORN (BS 500E-500G) · airframe 39,169 hrs · 14,903 cycles

CABIN SEAT TRACK UPPER SURFACE WORN AND CORRODED IN SCALLOPED AREA. BS 500E- 500G, LBL 45, ACFT GROUNDED. FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1, FIG 103, DETAIL A. ALODINED IAW AMM 51-21-91 PRIMED IAW AMM 51-21-99.

Part: TRANSITION PANEL — CORRODED (BS 727-727D) · corrosion level 2 · airframe 39,169 hrs · 14,903 cycles

AFT CARGO FLOOR TO SIDEWALL TRANSITION PANEL, UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. BS 727-BS 727D, STR 25L-STR 26L. ACFT GROUNDED. REMOVED CORROSION FROM TRANSITION PANEL BETWEEL STA 727 & STA 727D, STR 25L & 26L FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A2, FABRICATED NEW TRANSITION AND SPLICE PANEL IAW SRM 53-00-53-2R-5, TREATED WITH ALODINE AND PRIMER IAW SRM 51-20-01, INSTALLED NEW TRANSTION PANEL IAW SRM 53-00-53-2R-5.

Part: TRANSITION PANEL — CORRODED (BS 727H-727L) · corrosion level 2 · airframe 39,169 hrs · 14,903 cycles

AFT PIT FLOOR TO SIDEWALL TRANSITION PANEL, UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. BS 727H - 727L, STR 25 - 26L. ACFT GROUNDED. REMOVED CORROSION FROM TRANSITION PANEL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A. REMOVED, FABRICATED AND INSTALLED NEW TRANSITION AND SPLICE PANEL IAW SRM 53-00-53-R2-5.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,169 hrs · 14,903 cycles

FWD SEAT TRACK, BS 727B AT LBL 45.50 CRACKED. ACFT GROUNDED. REPAIRED SEAT TRACK IAW REO-G17396.

Part: TRANSITION PANEL — CORRODED (BS 727D-727H) · corrosion level 2 · airframe 39,169 hrs · 14,903 cycles

AFT PIT FLOOR TO SIDEWALL TRANSITION PANEL, UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. BS 727D-727H, STR 25-26L. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FABRICATED NEW TRANSITION PANEL AND SPLICE AND INSTALLED IAW SRM 53-00-53-2R5.

Part: SEAT TRACK — CORRODED (BS 480-500) · airframe 39,169 hrs · 14,903 cycles

CABIN SEAT TRACK UPPER SURFACE CORRODED. BS 480 - 500, LBL 45. ACFT GROUNDED. FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1, FIG 103, DETAIL A. ALODINED IAW AMM 51-21-41, PRIMED IAW AMM 51-21-99.

Part: SEAT TRACK — CORRODED (BS 500A-500B) · airframe 39,169 hrs · 14,903 cycles

CABIN SEAT TRACK UPPER SURFACE HAS CORROSION. BS 500A-500B, LBL 45. ACFT GROUNDED. FOUND WITHIN LIMITS IAW SRM 53-00-52-1A-1, FIG 103 DETAIL A ALODINED IAW AMM 51-21-41 PRIMED IAW AMM 51-21-99.

Part: TRANSITION PANEL — CORRODED (BS 767-847) · corrosion level 2 · airframe 39,169 hrs · 14,903 cycles

AFT CARGO FLOOR TO SIDEWALL TRANSITION PANEL, UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. BS 767-BS 847, STR 25L-STR 26L. ACFT GROUNDED. REMOVED CORROSION FROM TRANSITION PANEL BETWEEN STA 767-STA 847, STR 25L, STR 26L, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A2. FABRICATED NEW TRANSITION PANEL AND SPLICE IAW SRM 53-00-53-2R-5. TREATED WITH ALODINE AND PRIMER IAW SRM 51-20-01. INSTALLED NEW TRANSITION PANEL IAW B SRM 53-00-53-2R-5.

Part: SEAT TRACK — CORRODED (BS 480-500) · airframe 39,169 hrs · 14,903 cycles

CABIN SEAT TRACK UPPER SURFACE HAS CORROSION IN SCALLOPED AREA. BS 480-500+10, RBL 25. ACFT GROUNDED. R & R SEAT TRACK AND CHANNEL IAW REO-G17394.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,169 hrs · 14,903 cycles

LAVATORY WASTE TANK VACUUM OUTLET SKIN CUT OUT IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. FOUND IN LIMITS IAW SRM 53-00-01. ALODINE AND PRIMER APPLIED IAW SRM 51-20-01. TOP COAT APPLIED IAW AMM 51-21-00.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 39,169 hrs · 14,903 cycles

MAIN CABIN SEAT TRACK, BS 520, RBL 24.25 IS WORN ON CROWN. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G17394, REV A, & EA 900-5E3A-1264, REV NEW.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 39,169 hrs · 14,903 cycles

MAIN CABIN SEAT TRACK, BS 520, LBL 45.75 IS WORN ON THE CROWN. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G17394, REV A.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 39,169 hrs · 14,903 cycles

MAIN CABIN SEAT TRACK, BS 520, LBL 45.75 IS WORN ON CROWN. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G17394, REV A, AND EA 900-53EA-12654, REV NEW.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 39,169 hrs · 14,903 cycles

MAIN CABIN SEAT TRACK, BS 520, LBL 24.25 IS WORN ON CROWN. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G17394, REV A.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 39,169 hrs · 14,903 cycles

CABIN FLOOR SUPPORT UPPER FLANGE CRACKED, BS 328-344, LBL 46. ACFT GROUNDED. R & R FLOOR SUPPORT IAW DWG 141A5400.

Part: FLOORBEAM — CORRODED (BS 993) · corrosion level 2 · airframe 39,169 hrs · 14,903 cycles

CABIN FLOORBEAM ANGLE UPPER SURFACE HAS CORROSION. BS 993, RBL 33-43. ACFT GROUNDED. R & R CABIN FLOORBEAM ANGLE IAW SRM 51-40-02 & BAC DWG 147A5700, SHT 1, REV B.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 39,169 hrs · 14,903 cycles

CABIN FLOOR SUPPORT UPPER FLANGE CRACKED, BS 312 - 328, RBL 31. ACFT GROUNDED. R & R FLOOR SUPPORT IAW DWG 141A5400 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 988-1016) · corrosion level 2 · airframe 39,169 hrs · 14,903 cycles

FLOOR SUPPORT CORRODED BS 988 - 1016, RBL 31. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-70-51-1A-1 FIG 103 AND FOUND OUT OF LIMITS IAW SRM 53-70-51-1A-1 FIG 103 DETAIL C. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 278-295) · airframe 39,169 hrs · 14,903 cycles

CABIN FLOOR SUPPORT UPPER FLANGE CRACKED, BS 278-295, BL 0. ACFT GROUNDED. R & R FLOOR SUPPORT IAW DWG 141A5400.

Part: DOOR — BINDING (R2) · airframe 37,219 hrs · 14,175 cycles

F/A REPORTS R2 DOOR WILL NOT CLOSE PROPERLY. ACFT GROUNDED. FOUND DOOR NOT SEATED BUT LATCHED FULLY. 1 IN EVERY 3 CLOSINGS WILL BINDING ESPECIALLY WHEN CLOSED SLOWLY AND WITH OUT USING UPPER GRAB HANDLE. REPLACED GUIDE ARM & LOWER FUSELAGE RADIUS LINK, STOP PLATE & BEARING AND ADJUSTED DOOR REF AMM 52-41-00-820-801, ACCOMPLISHED DOOR TEST, TESTED GOOD REF AMM 52-41-00-700-801.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 35,553 hrs · 13,555 cycles

TWO CRACKS LT HORIZONTAL LOWER SKIN. REPAIRED CRACK IAW SRM 55-10-01 REPAIR 11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 35,553 hrs · 13,555 cycles

CRACKED LT HORIZONTAL LOWER SKIN. REPAIRED CRACK IAW SRM 55-10-01 REPAIR 11.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,444 hrs · 13,508 cycles

EMERGENCY LIGHT AISLE FLOOD LIGHT AT ROW 19 LT INOPERATIVE. REPLACED LAMP AND TESTED IAW MM 33-51-03-960-801. OPS NORMAL.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 34,889 hrs · 13,308 cycles

L2 EXIT SIGN, FELL OFF. ACFT GROUNDED. REPLACED EXIT SIGN COVER & SECURED AS REQUIRED. ACFT OK FOR SERVICE.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 32,974 hrs · 12,643 cycles

RT HORIZONTAL STAB LOWER SKIN CRACKED. CUT OUT DAMAGED AREA & INSTALLED REPAIR DOUBLER IAW SRM 55-10-01, REPAIR 11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 32,974 hrs · 12,643 cycles

RT HORIZONTAL STAB LOWER SKIN CRACKED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER REF SRM 55-10-01, REPAIR 11.

Part: SLIDING WINDOW — DRAGGING (COCKPIT) · airframe 31,788 hrs · 12,213 cycles

CAPTAIN`S SLIDING WINDOW DRAGGING IN TRACK. SERVICED LOWER TRACK IAW AMM 12-25-81-600-801.

Part: WEB — CORRODED (BS 438-495) · corrosion level 2 · airframe 31,788 hrs · 12,213 cycles

FORWARD CARGO DOOR CUT OUT LOWER WEB FROM STA 438 TO STA 495 STR 25R BL 35R HAS CORRODED AROUND SEVERAL FASTENER HOLES. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS IS .045 REMAINING IS .035 .010 WAS REMOVED. FOUND TO BE OUT OF LIMITS REF SRM 53-30-15. REMOVED AND REPLACED WEB REF SRM 51-40-02 AND DWG 143A8122 REV D.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 31,788 hrs · 12,213 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT FROM BS 757 TO 847 AND RBL 13.5 HAS CORROSION. REPAIRED IAW SRM 53-00-53.

Part: FLOOR SUPPORT — CORRODED (BS 732D) · corrosion level 2 · airframe 31,788 hrs · 12,213 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT AT RBL 8 AND BS 732D HAS CORROSION. FABRICATED NEW REPAIR ANGLE IAW SRM 53-00-53 REPAIR 3. ALODINED PRIMERED AND PAINTED ANGLE IAW SRM 51-20-01 AND AMM 51-21-99. INSTALLED NEW REPAIR ANGLE AS REQUIRED IAW SRM 53-00-53 REPAIR 3 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 31,788 hrs · 12,213 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 772 AND RBL 8 HAS CORROSION. REPAIRED IAW SRM 53-00-53.

Part: CARGO TRACK — CORRODED (BS 732D) · corrosion level 2 · airframe 31,788 hrs · 12,213 cycles

CARGO TRACK FOUND CORRODED. REPAIRED.

Part: FLOOR SUPPORT — CORRODED (BS 732D) · corrosion level 2 · airframe 31,788 hrs · 12,213 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT AT RBL 3 AND BS 732D HAS CORROSION. FABRICATED NEW REPAIR ANGLE IAW SRM 53-00-53 REPAIR 3. APPLIED ALODINE AND PRIME IAW SRM 51-20-01 AND PAINTED ANGLE IAW AMM 51-21-99. INSTALLED NEW REPAIR ANGLE IAW SRM 51-40-02 AND SRM 53-00-53.

Part: WEB — CORRODED (BS 792-849) · corrosion level 2 · airframe 31,788 hrs · 12,213 cycles

AFT CARGO DOOR CUTOUT LOWER WEB S 792 TO 849 S25R, RBL 35 HAS AREAS OF CORROSION. WEB FOUND TO BE OUT OF LIMIT IAW SRM 53-60-15. LOCATED DRILLED DEBURRED NEW WEB IAW SRM 51-40-05. INSTALLED NEW WEB IAW SRM 51-40-02 AND DWG 146A8340.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,788 hrs · 12,213 cycles

E&E COMPARTMENT LOOKING UP CABIN FLOORBEAM INTERCOSTAL CRACKED AT FLOORBOARD ATTACH HOLE BS 350. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 31,788 hrs · 12,213 cycles

CABIN FLOORBEAM INTERCOSTAL CRACKED BS 344 TO BS 360 LBL 12. REMOVED AND REPLACED CABIN FLOORBEAM INTERCOSTAL AT BS 344 TO BS 360 LBL 12 AS REQUIRED IAW B737 900 SRM 51 40 02.

Part: VALVE — FAILED (AC BAY) · airframe 26,954 hrs · 10,469 cycles

(ATB TO ANC) LEFT AC PACK TRIP ANNUNCIATION OCCURRED FOLLOWING TAKEOFF AND COULD NOT BE RESET. AIRCRAFT CABIN PRESSURIZATION DROPPED TO 12K FEET ONE HALF HOUR INTO FLIGHT AT FL350 AND ALTITUDE WARNING HORN SOUNDED. PAX OXYGEN MASK DID NOT AUTO DEPLOY BUT FLIGHT CREW DONNED OXYGEN MASKS. DESCENDED AND RETURNED TO ANC. REPLACED DEFECTIVE TEMPERATURE CONTROL VALVE AND A RUPTURED FLEXIBLE DUCT BETWEEN THE CONDENSER AND THE HPWS MIX MUFF IN RT AIRCON BAY.

Part: BULKHEAD — CRACKED (RT WING) · airframe 25,844 hrs · 10,027 cycles

RIGHT WING FIXED TRAILING EDGE BULKHEAD AT RSS 289 CRACKED. REMOVED AND REPLACED BULKHEAD ANGLE.

Part: SUPPORT — GOUGED (FUSELAGE) · airframe 20,327 hrs · 7,897 cycles

PNEUMATIC DOOR SUPPORT CHORD DAMAGED REPAIRED CHORD REF ER 08 3633.

Part: FLANGE — WORN (ACCESS PANEL) · airframe 20,327 hrs · 7,897 cycles

ACCESS DOOR HAS WORN THROUGH INBD FLANGE OF LOWER BEAM CHORD. TRIMMED OUT DAMAGE INSTALLED REPAIR IAW ATS ER 08-3633 EA 900-53EA-00276.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 20,327 hrs · 7,897 cycles

LT WING FWD SUPPORT BRACKET FITTING AT RSS 261 AFT FITTING IS CRACKED. REMOVED AND REPLACED LT WING SUPPORT BRACKET AFT FITTING AT RSS 261.

Part: SCUFF PLATE — CRACKED (CARGO DOORWAY) · airframe 20,327 hrs · 7,897 cycles

FWD CARGO BAY DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED. REMOVED AND REPLACED WD CARGO BAY DOOR CUTOUT AFT CORNER SCUFF PLATE.

Part: INTERCOSTAL — BENT (BS 500J-500K) · airframe 20,327 hrs · 7,897 cycles

WHILE WORKING CARD (FUSE 5043 CUST CARD 5140481) FOUND BAFFLE INTERCOSTAL BENT FWD CARGO BAY STA 500S 500K. REMOVED FABRICATED NEW AND INSTALLED INTERCOSTAL.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 20,327 hrs · 7,897 cycles

AFT CARGO BAY FLOOR PANEL BS 767 887 HAS CORROSION. REMOVED AND REPLACED AFT CARGO BAY FLOOR PANEL BS 767 887 IAW SRM 53 60 53.

Part: WEB — BENT (BS 500I-500J) · airframe 20,327 hrs · 7,897 cycles

BAFFLE INTERCOSTAL BENT FWD CARGO BAY STA 500I, 500J LH 26 WL 154. REMOVED

Part: INTERCOSTAL — CRACKED (BS 500K-500L) · airframe 20,327 hrs · 7,897 cycles

BAFFLE INTERCOSTAL CRACKED AT STA 500K 500L LT 26 WL 154. REMOVED FABRICATED NEW AND INSTALLED INTERCOSTAL.

Part: WEB — CORRODED (BS 1016) · airframe 20,327 hrs · 7,897 cycles

CORROSION SHEAR WEB BS 1016 RBL 28 WL 208.1. REPAIRED PER EA 900 53EA 00246, BLENDED AND TREATED.

Part: WEB — CORRODED (BS 986) · airframe 20,327 hrs · 7,897 cycles

CORROSION ON SHEAR WEB BS 986.5 RBL 30 WL 208.1. REPAIRED PER EA 900 53EA 00246 BLENDED AND TREATED.

Part: SUPPORT ANGLE — CORRODED (BS 500L) · airframe 20,327 hrs · 7,897 cycles

CORROSION ON THE LOWER BULKHEAD SUPPORT ANGLE. REPLACED LOWER SUPPORT ANGLE AT BS 500L LBL 25 RBL 25 PER SRM 51-20-05 AND 51-40-01.

Part: SUPPORT ANGLE — CORRODED (BS 727-727I) · airframe 20,327 hrs · 7,897 cycles

CORROSION ON THE LOWER BULKHEAD SUPPORT ANGLE. REMOVED AND REPLACED SECTION BS 727I-772.

Part: SUPPORT ANGLE — CHAFED · airframe 20,327 hrs · 7,897 cycles

FRETTING/CHAFING ON SUPPORT ANGLE FOR FAIRING. REMOVED AND REPLACED INBD SUPPORT ANGLE FOR FAIRING PANEL 193AL PER SRM 51 40 05.

Part: INTERCOSTAL — BENT · airframe 20,327 hrs · 7,897 cycles

BAFFLE INTERCOSTAL BENT FWD CARGO BAY STA 500G-500H. REMOVED FABRICATED NEW AND INSTALLED INTERCOSTAL.

Part: SHIELD — CORRODED (BS 767-787) · airframe 20,327 hrs · 7,897 cycles

CORROSION ON SIDEWALL SUPPORT PLATE SHIELD STA 767 787 RBL 23. REMOVED, FABRICATED NEW SUPPORT AND INSTALLED.

Part: WEB — CRACKED (BS 500H) · airframe 20,327 hrs · 7,897 cycles

WHILE WORKING CUSTOMER CARD 5140480 FOUND BAFFLE INTERCOSTAL CRACKED AT BS 500H AND 500I RBL26 WL154. R&R INTERCOSTAL.

Part: INTERCOSTAL — GOUGED (BS 500I) · airframe 20,327 hrs · 7,897 cycles

SIDEWALL SUPPORT INTERCOSTAL GOUGED AT FASTENER HOLES. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (BS 500K) · airframe 20,327 hrs · 7,897 cycles

SIDEWALL SUPPORT INTERCOSTAL CRACKED AT FASTENER HOLE. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT INTERCOSTAL BETWEEN BS 500J AND 500K IAW SRM 51-40-02 STEP 4B AND C

Part: SKIN — DENTED (CARGO DOOR) · airframe 20,327 hrs · 7,897 cycles

FWD CARGO DOOR OUTER SKIN YELLOW DOT APPLIED AT DENT NOT ON SAD RUN 28 INCHES FROM AFT EDGE 22 INCHES FROM TOP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 20,327 hrs · 7,897 cycles

INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51 40 02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 20,327 hrs · 7,897 cycles

INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51 40 02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,327 hrs · 7,897 cycles

CORROSION ON LT FLOOR TO SIDEWALL SUPPORT FORWARD CARGO BS 500H 500L. REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,327 hrs · 7,897 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,327 hrs · 7,897 cycles

SIDEWALL SUPPORT PLATE IS CORRODED. REPLACED SUPPORT PLATE PER SRM 53 00 53.

Part: BRACKET — CRACKED (RT WING) · airframe 20,327 hrs · 7,897 cycles

RT WING T/E PANEL SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 20,327 hrs · 7,897 cycles

CORROSION ON SHEAR WEB BS 986.5 RBL 30 WL 208. REMOVED CORROSION, PERFORMED NDI TO ENSURE NO CRACKS. ALODINED AND PRIMED. NO ESTABLISHED SRM LIMITS REPAIR WAS DONE PER EA 900 53EA 00246.

Part: ENGINE — OVERSPEED (NR 2) · airframe 17,185 hrs · 6,651 cycles

DURING CLIMB AT APPROX 9000FT NR 2 ENGINE STARTED SURGING. N1 RANGED FROM 60% TO IN EXCESS OF 100%. ENGINE ANTI ICE ON. PULLED NR 2 ENGINE TO IDLE. ENGINE OPERATED NORMAL AT IDLE. ENGINE NR 2 EEC BITE SHOWS FAULT 73 20322. EEC EXC PAGE SHOWS NR 2 ENGINE N1 AT 106.4% (OVERSPEED) FOR .02 SECONDS. REFERENCE LOG 6308286 FOR ENGINE REPLACEMENT.

Part: SKIN — GOUGED (FUSELAGE) · airframe 14,963 hrs · 5,720 cycles

FUSELAGE SKIN GOUGED 22 INCHES AFT OF L2 DOOR 18 INCHES UP FROM BOTTOM OF L2 DOOR CUTOUT. TEMP REPAIR INSTALLED PER ASA EA 5330 02215.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

CORROSION AT AFT CARGO PIT FLOOR PANEL AT STA 727. REPAIRED IAW SRM 51-40-05.

Part: RAIL — CORRODED (BS 767) · corrosion level 2

AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724.

Part: RAIL — CORRODED (BS 727D) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT FLOOR RAIL CORRODED. REPAIRED IAW EA5310 02724.

Part: CARGO TRACK — CORRODED (BS 727I) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT FLOOR RAIL SPLICE CORRODED. REPAIRED IAW SRM 51-40-05 AND 51-40-02.

Part: CARGO TRACK — GOUGED (BS 460-500) · airframe 14,726 hrs · 5,624 cycles

FWD CARGO PIT LEFT TIE DOWN TRACK GOUGED. REPAIRED IAW SRM 53-00-53.

Part: CARGO TRACK — CORRODED (BS 727) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT RAIL SPLICE CORRODED. REPAIRED IAW SRM 51-40-02 AND 51-40-03.

Part: RAIL — CORRODED (BS 727) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA 5310 02724.

Part: CARGO TRACK — CORRODED (BS 794-847) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO RT CARGO TIE DOWN TRACK CORRODED. SPLICED IN NEW SECTION.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

FWD CARGO PIT FLOOR PANEL AT STA 727 CORRODED. REPAIRED IAW SRM 51-40-05.

Part: RAIL — CORRODED (BS 767) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724.

Part: RAIL — CORRODED (BS 727D) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724.

Part: SKIN — DENTED (BS 767-847) · airframe 14,726 hrs · 5,624 cycles

DENT ON FUSELAGE SKIN AT BS 767. REPAIRED IAW EA 5330 02213.

Part: CARGO TRACK — CORRODED (BS 727) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT TIE DOWN TRACK SPLICE CORRODED. REPAIRED IAW 51-40-02 AND 51-40-05.

Part: STRAP — CORRODED (BS 787-794) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

AFT CARGO PIT CORROSION ON FLOOR STRAP AT BS 787. REPAIRED IAW SRM 51-40-06.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

CORROSION AT FWD CARGO FLOOR PANEL AT STA 395. REPAIRED IAW 51-40-05.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

CORROSION ON AFT CARGO PIT FLOOR PANEL. REPAIRED IAW SRM 51-40-050.

Part: RAIL — CORRODED (BS 727) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT RAIL SPLICE CORRODED. REPAIRED IAW 51-40-05 AND 51-40-02.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

AFT CARGO PIT PH CARGO TIE DOWN CORRODED. REPAIRED IAW SRM 53-00-53.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

CORROSION ON FWD CARGO FLOOR PANEL AT STA 500A. REPAIRED IAW 51-40-05.

Part: FLOOR SUPPORT — DRILLED (BS 500) · airframe 14,726 hrs · 5,624 cycles

FWD CARGO FLOOR PANEL SUPPORT AT BS 500 HAS DRILLED HOLES. REPAIRED IAW SRM 53-00-53.

Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 14,726 hrs · 5,624 cycles

RIGHT INBOARD TRAILING EDGE FLAP DAMAGE ON LEADING EDGE DUE TO SPOILER LOCKS. REPAIRED IAW EA 5750 02365.

Part: SILL — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

FWD CARGO PIT LT DUST SILL CORRODED REPAIRED IAW SRM 53 00 53

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

CARGO PIT TIE DOWN TRACK CORRODED. REPAIRED IAW SRM 53-00-53.

Part: SILL — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

FWD CARGO PIT LT DUST SILL CORRODED REPAIRED IAW 53 00 53

Part: STRAP — CORRODED (BS 794) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

AFT CARGO STRAP CORRODED AT BS 794.3. REPAIRED IAW SRM 51-40-05.

Part: RAIL — CORRODED (BS 767) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA 5310 02724.

Part: CARGO TRACK — CORRODED (BS 727) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT TIE DOWN SPLICE CORRODED. REPAIRED IAW SRM 51-40-02 AND 51-40-05.

Part: CARGO TRACK — CORRODED (BS 727I) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT RAIL SPLICE IS CORRODED. REPAIRED IAW 51-40-02 AND 51-40-03.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

AFT CARGO PIT DUST SILL CORRODED. REPAIRED IAW SRM 53-00-53.

Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 14,726 hrs · 5,624 cycles

LEFT INBOARD TRAILING EDGE FLAP DAMAGE TO THE FLAPS DUE TO SPOILER LOCKS.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

FWD CARGO PIT FLOOR PANEL CORRODED. REPAIRED IAW 51-40-05.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

FWD CARGO PIT FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-05.

Part: RAIL — CORRODED (BS 767) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

AFT CARGO PIT DUST SILL CORRODED. REPLACED DUST SILL IAW SRM 51-40-05.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

CORROSION AT FWD CARGO FLOOR PANEL AT STA 500D. REPAIRED IAW SRM 51-40-05.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

CORROSION ON AFT CARGO PIT FLOOR PANEL. REPAIRED IAW SRM 51-40-05.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 14,726 hrs · 5,624 cycles

AFT CARGO PIT FLOOR PANEL AT STA 727 CORRODED. REPAIRED IAW 51-40-05.

Part: SHIELD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

CARGO PIT FLOOR SHIELD AT BS 767 CORRODED. REPAIRED IAW 51-40-02.

Part: SUPPORT — CORRODED (BS 500) · corrosion level 2 · airframe 14,726 hrs · 5,624 cycles

FWD CARGO PIT STR LWR SUPPORT CORRODED. REPAIRED IAW SRM 51-40-02.

Part: RAIL — CORRODED (BS 727D) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA 5310 02724.

Part: RAIL — CORRODED (BS 767) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT SUPPORT RAILS CORRODED. REPAIRED IAW EA5310 02724.

Part: RAIL — CORRODED (BS 727D) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT SUPPORT RAIL CORRODED. REPAIRED IAW EA5310 02724.

Part: RAIL — CORRODED (BS 727) · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT RAIL SPLICE IS CORRODED. REPAIRED IAW 51-40-02 AND 51-40-05.

Part: SILL — CORRODED (BS 727-767) · corrosion level 2 · airframe 14,950 hrs · 5,712 cycles

AFT CARGO PIT DUST SILL CORRODED. REPAIRED IAW SRM 53-00-53.

Part: FILTER — DIRTY (A/C PACK) · airframe 11,663 hrs · 4,300 cycles

UPON DESCENT INTO SEA, A VERY STRONG SMELL CAUSED FA TO COUGH AND LEFT AN ODD TASTE IN THEIR MOUTH. ALSO, BOTH F/A`S SAID THEY GOT HEADACHES AND SICK FEELING. INSPECTED ACFT IAW MM. CHECKED APU BLEED AIR VALVE DUCTING NO CONTAMINATION NOTED. INSPECTED AND CLEANED CARGO PITS CHANGED LT RT RECIRC AIR FILTERS. OPS CHECKED, NO DEFECTS NOTED.