N319AS

Part: BAFFLE — CRACKED (UNKNOWN) · airframe 67,178 hrs · 27,133 cycles

FWD CARGO RH BAFFLE 500B THROUGH 500C IS CRACKED. GROUNDED - YES. FWD CARGO RH BAFFLE STA 500B TO 500C REMOVED AND REPLACED IAW B737-900 SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 67,178 hrs · 27,133 cycles

AFT WET AREA STA 986 FLOOR BEAM EXISTING REPAIR CAP RBL 20 TO RBL 60 IS CORRODED. GROUNDED - YES. DAMAGE FOUND TO BE 100% THROUGH ON EXISTING REPAIR CAP REMOVED AND REPLACED REPAIR CAP IAW B737-900 SRM 51-40-02-0G-0, 53-70-51-2R-4W=1 O=.150 R=0 L=2 D=.150.

Part: FLOORBEAM — CORRODED (UNKNOWN) · airframe 67,178 hrs · 27,133 cycles

AFT WET AREA STA 986 FLOOR BEAM EXISTING REPAIR CAP LBL 20 TO LBL 60 IS CORRODED. GROUNDED - YES. DAMAGE FOUND TO BE 100% THROUGH ON EXISTING REPAIR T-CAP REMOVED AND REPLACED REPAIR T-CAP IAW B737-900 SRM 51-40-02-0G-0, 53-70-51-2R-4W=2 O=.150 R=0 L=3 D=.150.

Part: CHANNEL — CORRODED (MOP SILL) · airframe 67,178 hrs · 27,133 cycles

R2 DOOR MOPSILL IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-70-15-1A-1 LOCATED AND DRILLED NEW MOP SILL IAW B737-90 0SRM 51-40-05-0G-0W=2 O=.080 R=.063 L=6 D=.017.

Part: INTERCOSTAL — CRACKED (UNKNOWN) · airframe 67,178 hrs · 27,133 cycles

FWD WET AREA INTERCOSTAL STA 312 TO 328 LBL 50 IS CRACKED. GROUNDED - YES. REMOVED CRACKED INSTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW B737-900 SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (UNKNOWN) · airframe 6,717 hrs · 27,133 cycles

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

Part: FLOORBEAM — CORRODED (UNKNOWN) · corrosion level 2 · airframe 67,178 hrs · 27,133 cycles

AFT WET AREA STA 947 FLOOR BEAM HAS SPOT OF CORROSION AT RBL 50 OTBD OF LAVE MOUNT FITTING. GROUNDED - YES. REPAIRED 947 FLOORBOARD IAW EA 900-53EA-26330 W=.5" O=.180" R=0" L=2" D=.180".

Part: PLATE — CORRODED (UNKNOWN) · airframe 67,178 hrs · 27,133 cycles

AFT PIT R/H TRANSITION PANEL HAS CORROSION STA 727C+2 TO STA 767. GROUNDED - YES. REMOVED AND REPLACED DAMAGED SECTION OF TRANSITION PANEL STA 727C+2 TO STA 767 IAW B737-900 SRM 53-00-53-2R-5W 3 O .040 R .033 L 20 D .007.

Part: CARGO TRACK — CRACKED (UNKNOWN) · airframe 67,178 hrs · 27,133 cycles

AFT PIT RH CARGO TRACK IS CRACKED IN RADIUS WHERE ATTACHED TO FRAME AT STA 727H, 727I, 727J, 727H, 727I, 727J, 727K, 727L. GROUNDED - YES. CUT OUT DAMAGED SECTION AND REPAIRED TRACK AIW B737-900 SRM 53-00-53-2R-3.

Part: PLATE — CORRODED (UNKNOWN) · airframe 67,178 hrs · 27,133 cycles

AFT PIT L/H TRANSITION PANEL HAS CORROSION STA 757A+11 TO STA 807. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A-2. REMOVED AND REPLACED DAMAGED SECTION OF TRANSITION PANEL IAW B737-900 SRM 53-00-53-2R-5W 3 O .040 R .028 L 20 D .012.

Part: CHANNEL — CORRODED (UNKNOWN) · corrosion level 2 · airframe 67,178 hrs · 27,133 cycles

CORROSION ON RH TRANSITION FROM STA 500C TO STA 500L. GROUNDED - YES. RH TRANSITION REPAIRED IAW B737-900 SRM 53-00-53-2R-6W=1.00 O=.040 R=.020 L=2.00 D=.020.

Part: CARGO TRACK — CORRODED (UNKNOWN) · corrosion level 2 · airframe 67,178 hrs · 27,133 cycles

AFT PIT RH CARGO TRACK IS CORRODED AROUND NUT PLATE. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A-2, REMOVED AND REPLACED DAMAGED SECTION OF CARGO TRACK IAW B737-900 SRM 51-40-02-0G-0W=1 O=.080 R=.062 L=3 D=.018.

Part: SKIN — CRACKED (UNKNOWN) · airframe 67,178 hrs · 27,133 cycles

R/H HORIZONTAL LOWER SKIN HAS A CRACK AT STA 129, 26 FWD OF T/E. GROUNDED - YES. CUT OUT DAMAGE AND RPEAIRED LOWER SKIN IAW B737-900 SRM 55-10-01-2R-11 REPAIR 11.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,159 hrs · 27,121 cycles

OVERWING EMERGENCY EXIT DOOR INTERIOR LIGHT INOP. ROW 17 SEAT A. GROUNDED - YES. ON DEFERRAL.

Part: LENS — DETACHED (FWD GALLEY) · airframe 65,480 hrs · 26,352 cycles

FA REPORTS THAT ON TAKEOFF "EXIT SIGN COVER" NEAR R-1 DOOR FELL OFF. GROUNDED - YES. R1 LWR EMER EXIT LIGHT ASSY REPLACED OPS CHECK GOOD REF B737-900 AMM 33-51-01

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,477 hrs · 26,351 cycles

FA REPORTS "EXIT" SIGN NEAR R-1 DOOR COVER HAS FALLEN OFF. GROUNDED - YES. RESECURED "EXIT" SIGN COVER NEAR R-1 DOOR AS REQUIRED.

Part: BATTERY PACK — DISCHARGED (MAIN CABIN) · airframe 65,432 hrs · 26,333 cycles

REF ASA TC 78233008- EMERGENCY EXIT DOME LT, FWD ESCAPE SIDE LEFT, OVERDOOR EXIT SIGN + FWD ENTRY LT MODULE DID NOT ILLUMINATE DURING EMERGENCY EXIT LT TEST. GROUNDED - YES. REMOVED AND REPLACED BATTERY PACK ON EMERGENCY LIGHT POWER SUPPLY MOD 1675, REF B737-900 AMM 33-51-06, OPS NORMAL.

Part: LAMP — INOPERATIVE (AFT RH EXT FUSEL) · airframe 64,653 hrs · 25,990 cycles

EMERG. LTE AFT FUSELAGE GROUND FLOOD LIGHT (RH) INOP. GROUNDED - YES. RELAMPED & TESTED AFT FUSELAGE RH GROUND EMERG. LIGHT REF AMM 33-51-04. OPS TEST GOOD.

Part: BATTERY PACK — FAULTY (MAIN CABIN) · airframe 63,223 hrs · 25,335 cycles

REF T/C 78233001 EMERG BATT M1671 & M1695 FAILED CAPACITY FUNCT CHECK GROUNDED - YES. REMOVED AND REPLACED EMERG BATT M1671 & M1695 REF B737-900 AMM 33-51-06. OPS TEST GOOD. 4 MIG 51-A TAGS INSTALLED AND REMOVED.

Part: FUEL SYS — WARNING MESSAGE (UNKNOWN) · airframe 63,103 hrs · 25,278 cycles

FUEL LEAK #1 ENGINE. DIVERTED TO RNO DUE CONFIRMED FUEL LEAK REQUIRING ENGINE SHUTDOWN PER QRH. EMERGENCY DECLARED FOR PRIORITY HANDLING. GROUNDED - YES. DIVERSION - PERFORMED GVI #1 ENG FOUND COWLING WET WITH FUEL AFTER OPENING, FAN & T/R COWLS INSIDE AREAS WERE DRY NO LEAKS NOTED. APPLIED L/H TANK FUEL PRESSURE & OPENED ENG #1 SPAR VALVE. NO LEAKS NOTED. FUEL PUMPS OFF, SPAR VALVE CLOSED. TRANSFERRED FUEL TO LH WING IAW B737-900 AMM 28-26-00-650-802. EXTENDED FLAPS, NO LEAKS NOTED. RETURNED FUEL TO BALANCE. COMPLETED FQIS BITE CHECK, NO FAULTS FOUND REF B737-900 FIM 28-41 TASK 801. COMPLETED #1 ENG BITE CHECK, NO FAULTS FOUND REF AMM 71-00-00. RAN #1 ENG FOR 5 MINUTES. COMPLETED GVI ON #1 ENG, NO LEAKS NOTED REF AMM 71-00-00. INSPECTED ENG #1 AFTER IN-FLIGHT WINDMILLING REF AMM 71-00-00, NO DAMAGE/DEFECTS NOTED. FUEL STICKED #5 FUEL STICK WITH GOOD READING REF AS B737 ALTERNATE FUELING PROCEDURES. AFTER A DETAILED INSPECTION OF COWLING SUBSTANCE, IT WAS NOT FOUND BE FUEL BUT RESIDUAL OIL MIXED WITH INFLIGHT MOISTURE CAUSING STREAKING. REF TSR 712603, ACCOMPLISHED FUEL QUANTITY INDICATING SYSTEM- SYSTEM TEST #1 TANK EMPTY CAPACITANCE VALUES- TANK UNIT CAP IS 396.4 AND COMPENSATOR IS 57.7. BITE TESTS PASS REF AMM 28-41-00-730-801. #1 TANK AND COMPENSATOR UNIT RESISTANCE AND CAPACITANCE WITHIN LIMITS REF AMM 28-41-21-710-801.

Part: POWER SUPPLY — INTERMITTENT (MAIN PASSENGER C) · airframe 62,896 hrs · 25,181 cycles

SEVERAL EMERGENCY LIGHTS ON THE RIGHT AISLE AND RIGHT AFT DOOR NOT WORKING. SOME ON FOR FEW SECONDS ONLY. GROUNDED - YES. REPLACED M1695,M1971, AND M1672 EMERGENCY LIGHTS POWER SUPPLY REF B737-900 AMM 33-51-06-960-806. OP CHECK GOOD REF AMM 33-51-06-960-806.

Part: BULKHEAD — CRACKED · airframe 62,515 hrs · 25,024 cycles

L/H AC BAY 663 BULKHEAD ATTACH ANGLE CRACKED IN VERTICAL LEG 2ND FASTNER OUT FROM KEEL BEAM. GROUNDED - YES. REPAIRED ATTACH ANGLE AT L/H AC B 663 IAW BOEING 737-900 SRM 57-10-10-2R-5.

Part: SKIN — CRACKED · airframe 62,515 hrs · 25,024 cycles

L/H HORIZONTAL LOWER SKIN IS CRACKED AT STA 101 11 INCHES FWD OF REAR SPAR. GROUNDED - YES. REPAIRED LH HORIZONTAL LWR SKIN IAW B737-900 SRM 55-10-01-2R-11, REPAIR 11. THIS IS A CAT B REPAIR WITH A INSPECTION THRESHOLD OF 56,000 TOTAL FLIGHT CYCLES AND REPEAT INTERVALS OF 9000 CYCLES.

Part: SKIN — CRACKED · airframe 62,515 hrs · 25,024 cycles

L/H HORIZONTAL STAB LOWER SKIN CRACKED AT STA 147 17 INCHES FWD OF REAR SPAR. GROUNDED - YES. REPIARS MADE TO LWR SKIN OF L/H HORIZONTAL STAB 17 INCHS FWD OF REAR SPAR AT STA 147 IAW BOIENG 737-900 SRM 55-10-01-2R-11. THIS IS A CAT B REPAIR WITH A 56,000 TOTAL CYCLE THRESHOLD AND REPEAT INTERVALS OF 9000 CYCLES.

Part: SKIN — CRACKED · airframe 62,515 hrs · 25,024 cycles

RH HORIZ STAB LWR SKIN CRACKED AT STA 129 18 INCHES FWD OF REAR SPAR. GROUNDED - YES. REPAIRED CRACKED IAW B737-900 SRM 55-10-01-2R-11 REPAIR 11.

Part: SKIN — DENTED · airframe 62,133 hrs · 24,856 cycles

ON WALKAROUND, PILOT REPORTED DENT, RH SI DE OF FUSELAGE BELOW R1 DOOR CUTOUT STA 312 BETWN STR 21-22. DIMS MEASURED AT: 0.075" D X 2.0" L X 3.0" W. COMMON TO FRAME AT STA 312. OUT OF SRM LIMITS, REQUIRED REPAIR. GROUNDED - YES. ACCOMPLISHED SRM REPAIR PER B737-900 SRM 53-00-01 REPAIR 36. DOUBLER/TRIPLER WERE INSTALLED AFTER DAMAGE REMOVAL WAS PERFORMED. REPAIR WAS PERFORMED IN CONJUNCTION WITH EA 900-53EA-24115 (REV. 2).

Part: LENS — DETACHED (AFT CABIN) · airframe 61,412 hrs · 24,536 cycles

ILLUMINATED SIGN OUTSIDE OF AFT LEFT LAVATORY IS BECOMING DE-ATTACHED AND WIRES ARE EXPOSED. GROUNDED - YES. SECURED EMERGENCY LIGHT COVER OF AFT LEFT LAVATORY PER B737-900 AMM 33-51-00, OPS CHECK GOOD.

Part: STRINGER — CORRODED (BS 540) · corrosion level 2 · airframe 58,666 hrs · 23,360 cycles

STRINGER 26R CORRODED APPROX STA 540. GROUNDED - YES. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1.

Part: STRINGER — CORRODED (BS 540) · corrosion level 2 · airframe 58,666 hrs · 23,360 cycles

STR 25R CORRODED APPROX STA 540. GROUNDED - YES. REPAIRED STR IAW SRM 53-00-03-2R-1.

Part: STRINGER — CORRODED (BS 540) · corrosion level 2 · airframe 58,666 hrs · 23,360 cycles

STRINGER 27R CORRODED, BS 540. GROUNDED - YES. REPAIRED THE STRINGER IAW SRM 53-00-03-2R.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,225 hrs · 23,148 cycles

SEVERAL CABIN EMERGENCY LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLIES M2335, M1898, M1670, M1899, AND M1671 OPS CHECK GOOD IAW B737-900 AMM 33-51-00-710-801.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,225 hrs · 23,148 cycles

AFT PIT BOTTOM SIDE OF RIGHT TRANSITION PANEL CORRODED @ NUTPLATES BS 747- BS 787 GROUNDED - YES. REMOVED CORROSION ON TRANSITION PANEL ( SHIELD) IAW B737-900 SRM 51-10-02 ORIGINAL THICKNESS IS .050. REMAINING THICKNESS IS .026, LOSS OF .024 OUT OF LIMITS IAW B737-900 SRM 53-60-15-1A-1. REMOVED AND REPLACED SHIELD IAW BAC DWG 146A0081 REV A ID:0028. AND B737-900 SRM 51-40-02

Part: TRANSMITTER — FAILED (RT TE FLAP) · airframe 56,505 hrs · 22,373 cycles

UPON SELECTING FLAPS 1, THE RIGHT FLAP STAYED AT UP WHILE LEFT FLAPS WERE BETWEEN UP AND 1. LE DEVICES REMAINED UP. USED ALTERNATE FLAPS WHICH DROVE C/O LE DEVICES PER QRH. GROUNDED - YES. EMERGENCY LANDING DECLARED. FSEU BITE TEST SHOWS FAULT MSG 27-52260 "TE FLAP SNSR R". ACCOMPLISHED B737-900 FIM 27-51 TASK 820 "RIGHT FLAP POSITION TRANSMITTER DISAGREE PROBLEM" FAULT ISOLATION. REMOVED & REPLACED RT FLAP POSITION TRANSMITTER (T428) IAW AMM 27-58-01. ACCOMPLISHED FLAP POSITION TRANSMITTER ADJUSTMENT & TEST IAW AMM 27-58-01-820-801, OPS CK NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,980 hrs · 20,740 cycles

R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP IAW AMM 33-51-04-960-801, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 52,827 hrs · 20,673 cycles

RIGHT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP AND REPLACED THE M1674 BATTERY PACK, OPS NORMAL IAW AMM 33-51-06-960-806.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 52,827 hrs · 20,673 cycles

AISLE EMERGENCY EXIT LIGHTS, BULL NOSE OF STOW BIN, WERE INOPERATIVE ABOVE SEATS 4 DF, 7 DEF AND 10 DEF. ACFT GROUNDED. REPLACED THE M1674 BATTERY PACK, OPS NORMAL IAW MM 33-51-06-960-806.

Part: BAFFLE — CRACKED (BS 500H-500I) · airframe 52,006 hrs · 20,281 cycles

BAFFLE BETWEEN 500H AND 500I IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE BAFFLE IAW SRM 51-40-02-0G-0, FIG 8, AND PARA 7D.

Part: BAFFLE — CRACKED (BS 500I-500J) · airframe 52,006 hrs · 20,281 cycles

BAFFLE BETWEEN BS 500I AND 500J IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0.

Part: BAFFLE — CRACKED (BS 500G-500H) · airframe 52,006 hrs · 20,281 cycles

BAFFLE BETWEEN BS 500G AND 500H IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED BAFFLE IAW SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 52,006 hrs · 20,281 cycles

PRESSURE BULKHEAD BS 663 LOWER ANGLE IS CRACKED AT INBD SIDE OF DRAIN. ACFT GROUNDED. REPAIRED THE BULKHEAD ANGLE IAW EA 900-57EA-19857, AND SB737-57-1330-NG 2.

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 52,006 hrs · 20,281 cycles

LH WING REAR SPAR VERTICAL PRESSURE DECK BS663 LOWER ANGLE IS CRACKED AT I/B SIDE OF DRAIN SLOT. REF T/C WORK ORDER 339628 SB737-57-1330-NG-1. GROUNDED - YES. REPAIRED L/H WING REAR SPAR VERTICAL PRESSURE DECK IAW ASA EA 900 57EA 19856 AND SB737 57 1330 NG 1.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

MOP SEAL AT R1 DOOR HAS MULTIPLE AREAS OF CORR. GROUNDED - YES. REMOVED AND REPLACED R1 DOOR MOPSILL IAW SRM 51 40 02 0G 0 W 2 O .085 R .059 L 3 D .026.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

FLOOR SUPPORT, RBL 52 BETWEEN BS 947 AND 967 CORRODED. ACFT GROUNDED. BLENDED AND FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-70-51-1A-1, FIG 103, 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

FLOORBEAM AT FS 986.5 CORRODED ON LT AND RT UPPER CAP REPAIRS. GROUNDED - YES. REPAIRED FLOORBEAM 986.5 IAW SRM 53 70 51 2R 4 W .800 O .125 R .000 L .900 D .125..

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

FWD CARGO PIT BETWEEN STA 500 AND 500A BL 0, ANTENNA DOUBLER HAS AN AREA OF CORR. GROUNDED - YES. REMOVED AND REPLACED ANTENNA DOUBLER CHANNEL IAW SRM 51 40 02 0G 0 W 2 O .063 R 0 L 3 D .063.

Part: FRAME — CORRODED (BS 500D) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500D, LBL 30, FRAME HAS AREA OF CORROSION. ACFT GROUNDED. REPAIRED THE FRAME IAW EA 53EA 19890.

Part: SUPPORT ANGLE — CRACKED (BS 500K) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500K, LBL 20 FWD SIDE OF FRAME INTERCOSTAL SUPPORT ANGLE IS CRACKED. ACCFT GROUNDED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, FIG I, AND SRM 51-40-02-0G-0, PARA 4, AND 7D.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

FWD CARGO PIT BETWEEN STA 500G TO 500H, RT TRANSITION HAS AREAS OF CORR OVER PREVIOUS BLENDOUT. GROUNDED - YES. REMOVED AND REPLACED TRANSITION PANEL IAW SRM 51 40 02 0G 0 W 1 O .040 R .032 L 1.75 D .008.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

FWD CARGO PIT STA 500D LBL30, SUPPORT ANGLE HAS CORR. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO PIT STA 500D LBL30 SUPPORT ANGLE IAW SRM 51 40 02 0G 0 FIG 8 AND PARA 4 W 1 O .050 R .007 L 5 D .043.

Part: SUPPORT ANGLE — CRACKED (BS 500K) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500K, LBL 20 AFT SIDE OF FRAME INTERCOSTAL SUPPORT ANGLE WAS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 53-40-02-0G-0, FIG 8, AND SRM 51-40-02-0G-0, PARA H, AND 7D.

Part: ATTACH ANGLE — CRACKED (BS 500J) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500J, RBL 20, AFT SIDE OF FRAME INTERCOSTAL ATTACH ANGLE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02-0G-0, FIG 8, AND SRM 51-40-02-0G-0, PARA 4, AND 7D.

Part: ATTACH ANGLE — CRACKED (BS 500J) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500J, RBL 20, FWD SIDE OF FRAME, INTERCOSTAL ATTACH ANGLE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02-0G-0, FIG 8, AND SRM 51-40-02-0G-0, PARA 4, AND 7D.

Part: ANGLE — CRACKED (BS 500I) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500L, LBL 20, FWD SIDE OF FRAME INTERCOSTAL ANGLE IS CRACKED. ACFT GROUNDED. REMOVED & REPLACED THE INTERCOSTAL ANGLE IAW SRM 51-40-02-0G-0, FIG 8, AND SRM 51-40-02-0G-0, PARA 4 AND 7D.

Part: SIDEWALL SUPPORT — CORRODED (BS 500D) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500D, LBL 30, GILLINER SUPPORT ANGLE HAS CORROSION. ACFT GROUNDED. REMOVED AND REPLACED SIDEWALL SUPPORT ANGLE IAW SRM 51-40-02-0G-0, FIG 8, AND PARA 4.

Part: ANGLE — CRACKED (BS 500H) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500H FWD SIDE OF THE FRAME INTERCOSTAL ANGLE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, FIG 8, AND SRM 51-40-02-0G-0, PARA 4, AND 7D.

Part: ANGLE — CRACKED (BS 500) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500H, LBL20, FWD SIDE OF FRAME, INTERCOSTAL SUPPORT ANGLE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE INTERCOSTAL ANGLE IAW SRM 51-40-02-0G-0, FIG 8, AND SRM 51-40-02-0G-0, PARA 4 AND 7D.

Part: SUPPORT ANGLE — CRACKED (BS 500J) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500J, LBL 20, FWD SIDE OF FRAME, INTERCOSTAL ANGLE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE INTERCOSTAL ANGLE IAW SRM 51-40-02-0G-0, PARA 4, AND SRM 51-40-02-0G-0, FIG 8.

Part: ATTACH ANGLE — CRACKED (BS 500I) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY BS 500I, RBL 20, FWD SIDE OF FRAME, INTERCOSTAL ATTACH ANGLE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0, FIG 8, AND SRM 57-40-02-0G-0, PARA 4, AND 7D.

Part: SUPPORT ANGLE — CORRODED (BS 500I) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500I, LBL 25 WALL PANEL SUPPORT ANGLE HAS CORROSION. ACFT GROUNDED. REPAIRED THE SUPPORT IAW SRM 51-70-11-2R.

Part: ANGLE — CRACKED (BS 500G) · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, BS 500G, LBL 20, FWD SIDE OF FRAME INTERCOSTAL SUPPORT ANGLE IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, FIG 8 AND SRM 51-40-02-0G-0, PARA 4, AND PARA 7D.

Part: SIDEWALL SUPPORT — CORRODED (BS 500H-500L) · corrosion level 2 · airframe 52,006 hrs · 20,281 cycles

FWD CARGO BAY, RT TRANSITION PANEL, BS 500H TO 500L HAS NUMEROUS AREAS OF CORROSION OVER PREVIOUS BLENDOUTS. ACFT GROUNDED. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-40-02.

Part: SCREW — SHEARED (PAX DOOR) · airframe 51,952 hrs · 20,255 cycles

L1 DOOR GUIDE ARM RADIUS LINK, PIN SCREW FOUND SHEARED AND AFFECTING EGRESS. ACFT GROUNDED. REMOVED AND REPLACED THE PIN AND SCREW IAW AMM 52-11-21-400-802. OPS CHECKED GOOD. DOOR SWINGS FREELY.

Part: BATTERY PACK — DEFECTIVE (SLIDE LIGHT) · airframe 51,681 hrs · 20,137 cycles

ESCAPE SLIDE LIGHT AT THE RT AFT SERVICE DOOR IS INOPERATIVE. ACFT GROUNDED. REPLACED THE BATTERY PACK FUSE IAW AMM 33-51-06-960-804. OPS CHECKED GOOD.

Part: GUIDE ARM — UNSECURE (PAX DOOR) · airframe 50,785 hrs · 19,731 cycles

L1 DOOR DIFFICULT TO OPEN. ACFT GROUNDED. NO HISTORY LAST 90 DAYS. PERFORMED FIM 52-10 ,TASK 807. FOUND GUIDE ARM MISSING HARDWARE ON LOWER RADIUS LINK. REPLACED MISSING HARDWARE IAW AMM 52-11-21-400-802, STEPS 3.(4)(3)(H)1-3. OPS CHECKED GOOD, DOOR OPERATES SMOOTHLY.

Part: SKIN — CRACKED (NR 5 SLAT) · airframe 52,006 hrs · 20,281 cycles

NR 5 SLAT LOWER SKIN CRACKED. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 57-42-01-2R-8, REPAIR 8.

Part: SKIN — CRACKED (NR 6 SLAT) · airframe 52,006 hrs · 20,281 cycles

NR 6 SLAT LOWER SKIN CRACKED. ACFT GROUNDED. REPAIRED THE SLAT SKIN IAW SRM 57-42-011-2R-8, REPAIR 8.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 48,961 hrs · 18,927 cycles

EMERGENCY LIGHT EXIT SIGN TO THE L2 DOOR IS BROKEN. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED THE SIGN IAW AMM 33-51-01-960-802. OPS NORMAL.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 46,622 hrs · 17,907 cycles

RIGHT AFT AISLE EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. ACFT GROUNDED. R & R POWER SUPPLY FOR RT AFT AISLE EMERGENCY EXIT LIGHTS IAW AMM 33-51-06. OPS CHECK GOOD.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 46,473 hrs · 17,846 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO RT AFT OVERWING EXIT HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. RELAMPED AND TESTED IAW AMM 33-51-01-960-801. OPS NORMAL.

Part: SUPPORT FRAME — CHAFED (BS 650-672) · airframe 46,130 hrs · 17,707 cycles

WING TO BODY FAIRING SUPPORT FRAME UNDER PANEL 193AL IS CHAFED. ACFT GROUNDED. REMOVED AND REINSTALLED PANEL 192JL IAW AMM 53-51-21. R & R SUPPORT IAW SRM 51-40-02 AND DWG 149A7216. TOPCOATED IAW AMM 51-21-73.

Part: FLOOR SUPPORT — CORRODED (BS 747-847) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT CARGO FLOOR SUPPORT AT RT BS 747+6 TO 847, RBL 12 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. CHECKED LIMITS IAW SRM 51-10-02 ORIGINAL MATERIAL .070", MATERIAL REMAINING AFTER BLENDOUT .059" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 103 TOOL T8225.5. REMOVED SCUFF PLATE IAW SRM 51-40-02, REMOVED FLOOR SUPPORT IAW SRM 51-40-02, FABRICATION ACCOMPLISHED ON NR 42676 AND CUSTOMER CARD G656676, INSTALLED FLOOR SUPPORT IAW SRM 51-40-02 AND INSTALL SCUFF PLATE IAW SRM 51-40-02 DOT REMOVED.

Part: RETAINER — CRACKED (BS 289 BULKHEAD) · airframe 46,130 hrs · 17,707 cycles

FS 289 BULKHEAD SEAL RETAINER CRACKED AT T/E CAVITY. ACFT GROUNDED. R & R 1152953-2AAR FITTING IAW SRM 51-40-02. DOT REMOVED.

Part: FLOORBEAM — CORRODED (BS 500L) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

FWD CARGO FLOORBEAM ANGLE AT BS 500L LBL 24 TO RBL 24 CORRODED SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION ON FWD PIT FLOOR SUPPORT ANGLE AT BS 500L, LBL24 TO RBL24 IAW SRM 51-10-02. ORIGINAL THICKNESS IS .080 IAW DWG 143A9485, REMAINING THICKNESS IS .060, REMOVED .020. FOUND TO BE OUT OF LIMITS. R & R WITH NEW SUPPORT IAW SRM 51-40-02 & BAC DWG 143A9485, REV B.

Part: CHANNEL — CORRODED (BS 727I-787) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT PIT TRANSITION PANEL AT RT BS 727I+6 TO BS 787 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED CORROSION FROM AFT PIT TRASITION PANEL RT BS 727I+6 TO BS 787 ORIGINAL THICKNESS IS.040 IAW DWG BAC1496-377, REMAINING THICKNESS IS.000 LOST MATERIAL IS .040 THE TRASITION PANEL IS OUT OF LIMITS IAW SRM 53-00-53, FIG 103 MICROMETER T8361T FABRICATED NEW TRANSITION PANEL IAW SRM 53-00-53, APPLY FINISHING IAW SRM 51-20-01. REMOVED DOT AND OR STREAMER H259 INSTALLED NEW TRANSITION PANEL IAW SRM 53-00-53 .

Part: SUPPORT — CORRODED (BS 727-727F) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT PIT TRANSITION PANEL AT LT BS 727+4 TO 727F+6 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED CORROSION LT TRANSITION PANEL BS 727+4 TO BS 727F+6 IAW SRM 51-10-02. ORIGINAL THICKNESS IS .040" IAW BAC 1496-377. REMOVED .040", REMAINING .000. TRANSITION PANEL OUT OF LIMITS IAW SRM 53-00-53-1A, FIG 103, DETAIL D. REMOVED TRANSITION PANEL IAW SRM 51-40-02. FABRICATED NEW TRANSITION PANEL REPAIR SECTION IAW SRM 53-00-53-2R. ALODINE TREATED & PRIMED NEW TRANSITION REPAIR SECTION IAW SRM 51-20-01. INSTALLED NEW TRANSITION PANEL REPAIR SECTION IAW SRM 51-40-02. REMOVED DOT.

Part: TRANSITION PANEL — CORRODED (BS 747-847) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT PIT TRANSITION PANEL AT LT BS 747+6 TO 847 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED SECTION PANEL FROM BS 747+6 TO 847 IAW SRM 51-40-02. MATERIAL ID FOR FAB BAC 1496-377 7075T62 CLAD IAW SRM 53-00-53-2R-5, PO 860620.1 FABED NEW SECTION IAW SRM 53-00-52-21R-5 ALODINED AND PRIMER IAW SRM 51-20-01 INSTALLED IAW SRM 51-40-02 AND 53-00-52-2R-5, DOT H252 REMOVED .

Part: TRANSITION PANEL — CORRODED (BS 500B-500F) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

FWD PIT LT TRANSITION PANEL FROM BS 500B+10 TO 500F+10 CORRODED IN SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION FWD PIT LT TRANSITION PANEL FROM BS 500B+10 TO 500F+10 IAW SRM 51-10-02 ORIGINAL THICKNESS IS.040 IAW SRM 53-30-53 FROM BS 500B-BS 500C+14 FOUND TO BE WITHIN LIMITS, REMOVED .001. REMAINING .039 FROM BS 500C+14 TO BS 500F+10. REMOVED .012, REMAINING .028 FOUND OUT OF LIMITS IAW SRM 53-00-53-A-1A. REMOVED SECTION FROM BS 500C+14 TO BS 500F+10 AND REPLACED WITH NEW IAW SRM 53-00-53-2R-6 ALODINED IAW SRM 51-20-01 PRIMED IAW SOPM 20-41-02. REMOVED DOT AND OR STREAMER .

Part: SHIELD — CORRODED (BS 767-792) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT CARGO RT SHIELD AT BS 767-792 BETWEEN STR 25-26R CORRODED. ACFT GROUNDED. R & R AFT PIT RT SHIELD AT BS 767-792 BETWEEN STR 25-26R IAW SRM 51-40-02 AND BAC DWG 146A0081, REV A ORIGINAL THICKNESS IS .050, REMAINING .040, REMOVED .010. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A, DOT REMOVED.

Part: ANGLE — CORRODED (BS 727D-727I) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT PIT TRANSITION PANEL AT RT BS 727D+6 TO 727I+6 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED CORROSION FROM THE AFT PIT TRANSITION PANEL BS 727D+6 TO 727I+6 ORIGINAL THICKNESS IS 0.040 IAW DWG BAC 1496-377, REMAINING THICKNESS IS 0.070, REMOVED MATERIAL IS 0.020 THE TRANSITION PAIRED OUT OF LIMITS IAW SRM 53-00-53, FIG 103 MICROMETER T8361T. FABRICATED NEW TRANSITION PANEL IAW SRM 53-00-53. APPLY FINISHING IAW SRM 51-20-01. REMOVED DOT H258. INSTALLED NEW TRANSTION PANEL IAW SRM 53-00-53.

Part: TRANSITION PANEL — CORRODED (BS 500J-500L) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

FWD PIT LT TRANSITION PANEL FROM BS 500J+10 TO 500L CORRODED IN SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION FWD PIT LT TRANSITION PANEL FROM BS 500J+10 TO BS 500L IAW SRM 51-10-02. AFTER FURTHER EVALUATION CORROSION FOUND TO BE MORE THAN 50 PERCENT, OUT OF LIMITS. ORIGINAL THICK .040 IAW SRM 53-30-53. R & R TRANSITION PANEL FROM BS 500J+10 TO BS 500L IAW SRM 53-00-53-2R-6 AND DWG 1143A7501 ALODINED IAW SRM 51-20-01 AND PRIMED IAW SOPM 20-41-02 DOT REMOVED .

Part: TRANSITION PANEL — CORRODED (BS 500G-500A) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

FWD PIT RT TRANSITION PANEL FROM BS 500A TO 500G+4 CORRODED SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION ON FWD PIT RT TRANSITION PANEL FROM BS 500A TO 522G+4 IAW SRM 51-10-02, ORIGINAL THICKNESS IS .40 IAW SRM 53-30-53. REMOVED .010 REMAINING THICKNESS IS .030 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. R & R TRANSITION ANGLE FROM BS 500A TO 500G+4 IAW SRM 53-00-53-2R-6 ALODINED IAW SRM 51-20-01 AND PRIMED IAW SOPM 20-41-02. REMOVED DOT AND OR STREAMER .

Part: ANGLE — CORRODED (BS 727H-727J) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT PIT TRANSITION PANEL AT LT BS 727H+8 TO 727J+8 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED SECTION PANEL FROM 727H+8 TO 727J+8 IAW SRM 51-40-02 AMT ID. FOR FABRICATED 1496-377-7075-T62 CLAD IAW SRM 53-00-53-2R-5, PO 860620.2, FABRICATED NEW SECTION IAW SRM 53-00-53-2R-5. ALODINED & PRIMER IAW SRM 51-20-01 INSTALLED IAW SRM 51-40-02 & 53-00-53-2R-5 DOT REMOVED.

Part: ANGLE — CORRODED (BS 727F-727H) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT PIT TRANSITION PANEL AT LT BS 727F+6 TO 727H+8 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED SECTION PANEL FROM BS 727F+6 TO 727H+8 IAW SRM 51-40-02, AMT ID FOR FAB BAC 1496-377-7075-T62 CLAD IAW SRM 53-00-53-2R-5, PO 860620.2 FABRICATED NEW SECTION IAW SRM 53-00-53-2R-5. ALODINED & PRIMED IAW SRM 51-20-01. INSTALLED IAW SRM 51-40-02 & 53-00-53-2R-5, DOT REMOVED.

Part: TRANSITION PANEL — CORRODED (BS 727-747) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT PIT TRANSITION PANEL AT LT BS 727J+8 TO 747+6 CORRODED IN SEVERAL SPOTS. ACFT GROUNDED. REMOVED SECTION PANEL FROM BS 727J+8 TO 747+6 IAW SRM 51-40-02 MATERIAL ID FOR FABRICATED BAC 1496-377, 7075, T62 CLAD IAW SRM 53-00-53-2R-5, PO 860620.2 FABRICATED NEW SECTION IAW SRM 53-00-523-2R-5, ALODINED AND PRIMER IAW SRM 51-20-01, INSTALLED IAW SRM 51-40-02 AND 53-00-523-2R-5, DOT H253 REMOVED.

Part: FLOOR PANEL — GOUGED (AFT CARGO) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

AFT CARGO FLOOR PANEL 140CF CORRODED AND GOUGED ALL ARROUND. ACFT GROUNDED. FABRICATED NEW AFT CARGO FLOOR PANEL 140 OF IAW DWG 453A2610, REV C. ALODINED & PRIMED IAW SRM 51-20-01.

Part: FLOOR PANEL — GOUGED (CARGO BAY) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

PARTS RACK ITEM, AFT PIT FLOOR PANEL 140BF GOUGED AND CORRODED ALL ARROUND. ACFT GROUNDED. FABRCIATED NEW AFT CARGO FLOOR PANEL 140BF IAW DWG 453A2610, REV E. ALODINED AND PRIMED IAW SRM 51-20-01.

Part: FLOOR PANEL — CORRODED (BS 500D-500H) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

PARTS RACK, FWD PIT FLOOR PANEL 120 DF CORRODED ALL AROUND THE EDGES. ACFT GROUNDED. FLOOR PANEL 120DF FOUND TO BE BEYOND LIMITS IAW SRM 53-00-53 MAT ID 2024-T3 .071 PO 860430.3 AND FABRICATED IAW DWG 453A1610, REV A ALODINED IAW SRM 51-20-01 PRIMED IAW AMM 51-21-72, REMOVED DOT.

Part: FLOOR PANEL — CRACKED (BS 727A-727D) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

PARTS RACK AFT PIT FLOOR PANEL 140AF CORRODED AROUND EDGES. ACFT GROUNDED. FABRICATED NEW PANEL IAW DWG 453A2610, REV C ALODINED AND PRIMED IAW SRM 51-20-01. REMOVED DOT H250.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 46,130 hrs · 17,707 cycles

FWD PIT FLOOR PANEL 120EF CORRODED ALL AROUND THE EDGES. ACFT GROUNDED. FABRICATED NEW FWD CARGO FLOOR PANEL 120EF IAW BAC DWG 453A1610, REV B ALODINED AND PRIMED IAW SRM 51-20-01.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 45,805 hrs · 17,579 cycles

EMERGENCY LIGHTS OPS CHECK, FWD ENTRY LIGHTS INOPERATIVE. ACFT GROUNDED. VERIFIED POWER SUPPLY M1675 TEST BUTTON INOPERATIVE. REPLACED M1675 REF AMM 33-51-06. OPS NORMAL.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 42,575 hrs · 16,315 cycles

CRACK FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN AT STABILIZER STA 128.50. CRACK IS APPROXIMATELY 1' IN LENGTH LOCATED 10' FORWARD OF THE REAR SPAR. MARKED ON ACFT. ACFTT GROUNDED. REMOVED DAMAGE MATERIAL ID FOR DOUBLER 2024T3, .100, PO 808272.1 AND FILLER 2024T3, .063, PO 823655.1 FABBED LOCATED DRILLED DEBURRED AND COUNTERSUNK IAW SRM 55-10-01-2R-11 ALODINED AND PRIMED IAW SRM 51-20-01 INSTALLED DOUBLER AND FILLER IAW SRM 55-10-01-2R-11 AND PAINTED IAW AMM 51-21-73-870-801.

Part: ATTACH FITTING — BROKEN (BS 472-513) · airframe 42,584 hrs · 16,317 cycles

LT CARGO NET FLOOR ATTACH FITTING IS DAMAGED. LOCATED AT APPROXIMATELY STA 500. ACFT GROUNDED. FABRICATED AND INSTALLED PERMANENT REPAIR IN FWD PIT BETWEEN SAT 505-513 LBL 18.24 IAW REO G18738, REV B, DATED 11 FEB 15 AND EA 900-53EA-14464, REV NEW DATED 11 FEB 2015.

Part: SWITCH — UNKNOWN (EMERGENCY LIGHTS) · airframe 41,086 hrs · 15,714 cycles

FOUND AFT F/A EMERGENCY LIGHT SWITCH ON WITH NO EMERGENCY LIGHT ON. ACFT GROUNDED. VERIFIED NO EMERGENCY LIGHTS ON. CYCLED SWITCH OFF TO ON AND ACCOMPLISHED F/A EMERGENCY LIGHT OPS CHECK WITH SWITCH ON. ACFT EMERGENCY LIGHTS CAME ON ON INSIDE AND OUTSIDE. TURNED SWITCH TO OFF, ALL OPS NORMAL. REF MM 33-41-00-720-801 AND 33-51-06-610-802.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,680 hrs · 15,200 cycles

EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. ACFT GROUNDED. R & R POWER SUPPLY IAW AMM 33-51-06-960-806, OPS CHECKED GOOD IAW AMM 33-51-06-960-806.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 39,680 hrs · 15,200 cycles

EMERGENCY LIGHTS NOT WORKING. ACFT GROUNDED. R & R EMERGENCY BATTERY PACKS IAW AMM 33-51-06, OPS CHECKED GOOD IAW AMM 33-51-06.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 39,680 hrs · 15,200 cycles

CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN AT INBD ROW OF RIVETS 32" AFT OF FWD SPAR. ACFT GROUNDED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 55-10-01, REP 11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 39,680 hrs · 15,200 cycles

CRACK INDICATION FOUND: RT STABILIZER LOWER SKIN AT INBD ROW OF RIVETS 36' AFT OF FWD SPAR. MARKED, LONGITUDINALLY .650' LONG. NR 1 RHSS 101.90. ACFT GROUNDED. CUTOUT DAMAGE, FABBED AND INST REPAIR IAW SRM 55-10-01, REP 11. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 56,000 FLIGHT CYCLES AND REPEAT INSP EVERY 9000 FLIGHT CYCLES IAW SRM 55-10-01, REPAIR 11, TABLE 204. ALODINED AND PRIMED IAW SRM 51-20-01 .

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 39,680 hrs · 15,200 cycles

CRACK INDICATION FOUND ON RIGHT HORIZONTAL STABILIZER LOWER SKIN AT INBD ROW OF RIVETS 25" AFT OF FWD SPAR, . ACFT GROUNDED. CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 55-10-01, REPAIR 11.

Part: SEAT TRACK — CRACKED (BS 727) · airframe 39,680 hrs · 15,200 cycles

MAIN CABIN BS 727B, RBL 45.50 OTBD SEAT TRACK FLANGE AFT HOLE HAS A CRACK INDICATION. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G17288, REV A AND EA SB737-53-1296-NG-106 REV.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,680 hrs · 15,200 cycles

MAIN CABIN BS 727B, LBL 24.75 INBD AND OUTBD SEAT TRACK FLANGE HOLES HAVE CRACK INDICATIONS. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G17288, REV A AND EA SB737-53-1296-NG-106, REV NEW.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,680 hrs · 15,200 cycles

MAIN CABIN, BS 727B, RBL 24.75 INBD AND OTBD SEAT TRACK FLANGE HOLES HAVE CRACK INDICATIONS. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G17288, REV A AND EA SB737-53-1296-NG-106, REV.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 39,680 hrs · 15,200 cycles

MAIN CABIN BS 727B, LBL 45.50 INBD AND OTBD SEAT TRACK FLANGE HOLES HAVE CRACK INDICATIONS. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW REO G17288, REV A AND EA SB737-53-1296-NG-106, REV NEW.

Part: SEAT TRACK — CHAFED (BS 520) · airframe 39,680 hrs · 15,200 cycles

MAIN CABIN SEAT TRACK CHAFED BS 520, LBL 45. ACFT GROUNDED. INSTALLED SEAT TRACK REPAIR IAW REO G17293, REV A AND EA 900-53, EA-12400.

Part: SEAT TRACK — CHAFED (BS 520) · airframe 39,680 hrs · 15,200 cycles

MAIN CABIN SEAT TRACK CHAFED BS 520, LBL 25. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS. REMOVED OLD SECTION OF SEAT TRACK REPLACED WITH NEW AND SPLICE, ALODINED AND PRIMED IAW REO G17293, REV A AND EA 900-53EA-12400, REV.

Part: SEAT TRACK — CHAFED (BS 520) · airframe 39,680 hrs · 15,200 cycles

MAIN CABIN SEAT TRACK CHAFED BS 520, RBL 25. ACFT GROUNDED. INSTALLED REPAIR IAW REO G17293, REV A AND EA 900-53EA-12400.

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 39,680 hrs · 15,200 cycles

MAIN CABIN SEAT TRACK CHAFED BS 520, RBL 45. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS, R & R SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE IAW REO G17293, REV A DATE 3-28-14 AND EA 900-53EA-12400, REV NEW DATE 03-31-2014 .

Part: FLOORBEAM — CORRODED (BS 986.5) · corrosion level 2 · airframe 39,680 hrs · 15,200 cycles

FLOOR STRUCTURE WET AREAS, FLOORBEAM IS CORRODED INBD OF AFT SERVICE DOOR. BS 986.5, LBL 47, WL 200. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51. REPAIRED FLOORBEAM IAW SRM 53-70-51-2R-4.

Part: FLOOR SUPPORT — CORRODED (BS 325) · corrosion level 2 · airframe 39,680 hrs · 15,200 cycles

FLOOR STRUCTURE WET AREAS, R1 DOOR SCUFF PLATE SUPPORT ANGLE IS CORRODED. BS 325, RBL 65, WL 200. ACFT GROUNDED. REMOVED CORROSION ON FLOOR STRUCTURE WET AREAS, R1 DOOR SCUFF PLATE SUPPORT ANGLE, BS325 REB 65, WL200, EDGE DAMAGE MATERIAL REMOVED .196 MAX ALLOAWANCE .100 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15. R & R WITH NEW IAW DWG 141A8310, REV D & SRM 51-40-02 .

Part: FLOORBEAM — CORRODED (BS 986.5) · corrosion level 2 · airframe 39,680 hrs · 15,200 cycles

AFT ENTRY DOOR AREA, FLOORBEAM IS CORRODED, BS 986.5, RBL 48, WL 200. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-70-51. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51. REPAIRED FLOORBEAM IAW SRM 53-70-51-2R-4.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 39,099 hrs · 14,972 cycles

EMERGENCY EXIT SIGN LENS AT L2 DOOR FELL OFF. ACFT GROUNDED. REINSTALLED & SECURED LENS AT L-2 DOOR, CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 38,485 hrs · 14,734 cycles

DURING ACCOMPLISHMENT OF TC 78233008, R1 DOOR FWD ENTRY EMERGENCY LIGHT FAILED TO ILLUMINATE. ACFT GROUNDED. FOUND BROKEN WIRE W0142-0003-20 RETERMINATED WIRE IAW WDM 33-51-12. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,276 hrs · 14,288 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED LAMPS, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,276 hrs · 14,288 cycles

LEFT AFT OVERWING EXIT HANDLE LIGHTS INOPERATIVE. ACFT GROUNDED. REPLACED LAMPS. OP CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 37,276 hrs · 14,288 cycles

EMERGENCY LIGHTS BATTERY PACK M1670 FAILS CAPACITY CHECK. ACFT GROUNDED. REPLACED BATTERY PACK. OPS CHECKED NORMAL IAW MM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 37,276 hrs · 14,288 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1695 FAILS CAPACITY CHECK. ACFT GROUNDED. REPLACED BATTERY PACK. OPS CHECKED NORMAL. IAW MM 33-51-06.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,276 hrs · 14,288 cycles

L1 DOOR OVERHEAD EXIT LIGHT IDENTIFIER HAS BULBS INOPERATIVE. ACFT GROUNDED. REPLACED LAMPS. OPS CHECKED NORMAL.

Part: HOUSING — GOUGED (CRGO DOOR HANDLE) · airframe 36,734 hrs · 14,095 cycles

AFT CARGO DOOR HANDLE HOUSING GOUGED. ACFT GROUNDED. FOUND OUT OF LIMITS REF AMM 52-31-15-801,1,B,(1). REMOVED HANDLE HOUSING, LOCATED AND DRILLED IN NEW HOUSING. INSTALLED HINGE DOOR ASSY TO NEW HOUSING WITH NEW SPRINGS REF EC NG-52EO-06500-2. ACCOMPLISHED HFEC INSPECTION IAW NDT PART 6-51-00-00, FIG 16, NO CRACKS NOTED. INSTALLED NEW HOUSING ASSY REF SRM 51-40-02.

Part: CONNECTOR — FAILED (NR 2 ENGINE) · airframe 40,489 hrs · 16,608 cycles

NR 2 ENGINE FAILED IN CRUISE FL340. AP/AT ON, CROSS-FEED OPEN FOR REMAINING CTR TANK FUEL. COMPLETED QRH PROCEDURE/SHUTDOWN, AND 2 RESTART ATTEMPTS. NO FUEL FLOW OR EGT- SPAR VALVE REMAINED CLOSED WHEN START LEVER WAS RAISED TO IDLE. NO VIBRATIONS NOTED. ACFT GROUNDED. DIV TIME 1 HOUR 15 MINUTES CYCLED NR 2 ENGINE FUEL SPAR VALVE SEVERAL TIMES, NO DISCREPANCIES NOTED. INSPECTED AND REINSTALLED NR 2 ENGINE FUEL SPAR VALVE DISCONNECT PLUG AND JACK, NO DISCREPANCIES NOTED REF AMM 28-22-11. OPENED NR 2 ENG OTBD COWL. NR 2 ENG BITE INOPERATIVE. REPLACED NR 2 EEC. WHILE PERFORMING T/S FOUND NR 2 ENG TAI COWL VALVE AFT COUPLING NOT ATTACHED. REPLACED AFT COUPLING NR 2 TAI DUCT REF AMM 30-21-11. LEAK CHECK NORMAL.

Part: HOUSING — DAMAGED (CARGO DOOR) · airframe 33,425 hrs · 12,901 cycles

BROKEN DOOR BUMPER WITH GOUGE ON FWD CARGO DOOR HANDLE HOUSING. DAMAGE MEASURES GREATER THEN .050 DAMAGE IS BEYOND ALLOWABLE EA LIMITS. ACFT GROUNDED. REMOVED CARGO DOOR HANDLE. R & R HANDLE HOUSING IAW DWG 143A6110. REINSTALLED FWD CARGO DOOR HANDLE REF MM 52-31-14-400-801.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,411 hrs · 12,530 cycles

SUPPORT ANGLE CORRODED. REMOVED AND REPLACED ANGLE.

Part: PLATE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 32,411 hrs · 12,530 cycles

SIDE PLATE HAS CORROSION. REPAIRED SIDE PLATE.

Part: PLATE — CORRODED (FUSELAGE) · airframe 32,411 hrs · 12,530 cycles

SIDEPLATE HAS CORROSION. REPAIRED SIDE PLATE.

Part: INTERCOSTAL — CRACKED (BS 500I-500J) · airframe 32,411 hrs · 12,530 cycles

RIGHT INTERCOSTAL CRACKED, STA 500I, 500J. ACFT GROUNDED. REPAIRED IAW SRM 51-70-11. TYPICAL FORMED SECTION REPAIR.

Part: TRANS PANEL — GOUGED (FUSELAGE) · airframe 32,411 hrs · 12,530 cycles

AFT CARGO COMPARTMENT LEFT TRANSITION PANEL PUNCTURED. REPAIRED IAW B737 900 SRM 53 60 53 REPAIR 5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,411 hrs · 12,530 cycles

INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,411 hrs · 12,530 cycles

INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,411 hrs · 12,530 cycles

INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL.

Part: SKIN — DENTED (BS 440-488) · airframe 32,411 hrs · 12,530 cycles

GOUGE ON FORWARD CARGO EXTERNAL SKIN 13' BELOW TOP AND 22' FROM AFT EDGE. ACFT GROUNDED. ALL WORK ACCOMPLISHED IAW REV B6 14711 EA, NR E00 52EA 07661.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 32,411 hrs · 12,530 cycles

FLOOR PNL SPLICE TEE ASSY CORRODED. REMOVED AND REPLACED TEE ASSY.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 32,411 hrs · 12,530 cycles

AFT CARGO FLOOR PNL SUPPORT CORRODED. REPLACED REPAIR ANGLE.

Part: BUSHING — FROZEN (SLIDING WINDOW) · airframe 31,655 hrs · 12,264 cycles

CAPTAINS SLIDING WINDOW IS DIFFICULT TO OPEN AND CLOSE. WINDOW APPEARS TO BE:" OUT OF ALIGNMENT". FOUND AFT TRACK ROLLER BEARING FROZEN. REPLACED BEARING PER MM 56 12 11 300 802. WINDOW OPS CHECKS OK.

Part: ENGINE — FAILED (NR 1) · airframe 30,188 hrs · 11,712 cycles

DURING DESCENT INTO SEA PILOTS NOTICED BUZZING NOISE AND A LITTLE VIBRATION. ENGINE INSTRUMENTS SHOWED NORMAL. THEN ENG FAIL APPEARED ON NR 1 ENGINE AND WENT OUT A FEW SECONDS LATER. NOISE AND VIBRATION CONTINUED. ENGINE LIMIT SURGE STALL CHECKLIST COMPLETED WHICH LED TO ENGINE FAILURE SHUTDOWN CHECKLIST. REMOVED NR 1 ENGINE REF W/O 126954 T/C 78471000. INSTALLED NR 1 ENGINE PER T/C 78471001.

Part: ROLLER — WORN (ENTRY DOOR) · airframe 28,311 hrs · 11,033 cycles

L1 DOOR DIFFICULT TO CLOSE AND INTERMITANTLY DOES NOT CLOSE FULLY WHEN L1 DOOR HANDLE IS IN CLOSED POSITION. FOUND GUIDE ARM ROLLER WORN ALLOWING AFT END OF DOOR TO BE MIS TIMED WITH THE FWD END. REMOVED/REPLACED AND ADJUSTED GUIDE ARM IAW B737 900 MM 52 11 21 000 802 MM 52 11 21 400 802.

Part: SUPPORT ANGLE — CRACKED (SPOILER) · airframe 26,503 hrs · 10,350 cycles

T/E PANEL I/B OF NR 5 SPOILER SUPPORT ANGLE CRACKED. REMOVED AND REPLACED SUPPORT ANGLE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,503 hrs · 10,350 cycles

CORROSION AROUND NUT PLATE HOLES ON FLOOR TO SIDEWALL SUPPORT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,503 hrs · 10,350 cycles

CRACKED INTERCOSTAL IN FWD CARGO BAY.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 26,503 hrs · 10,350 cycles

RT WING TRAILING EDGE SEAL SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 26,503 hrs · 10,350 cycles

LT HORIZONTAL STAB LOWER EXTERNAL SKIN CRACK AT STAB STA 147.9.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 26,503 hrs · 10,350 cycles

RT WING TRAILING EDGE SEAL SUPPORT ANGLE CRACKED.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 26,503 hrs · 10,350 cycles

RIGHT WING PANEL SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET.

Part: RIB — CRACKED (HORIZ STAB) · airframe 26,503 hrs · 10,350 cycles

RIGHT HORIZONTAL STAB LEADING EDGE HAS 2 CRACKS IN RIB AT STAB STA 92.7.

Part: RIB — CRACKED (HORIZ STAB) · airframe 26,503 hrs · 10,350 cycles

LEFT HORIZONTAL STAB LEADING EDGE HAS 3 CRACKS IN RIB AT STAB STA 92.7.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 26,503 hrs · 10,350 cycles

LEFT HORIZONTAL STAB LOWER EXTERNAL SKIN POSSIBLE CRACK AT STAB STA 138.7, 10 INCHES AFT OF LEADING EDGE.

Part: BRACKET — CRACKED (NR 2 PYLON) · airframe 20,868 hrs · 8,160 cycles

AT RSS 261 RIGHT JUST AFT OF NR 2 PYLON AFT BRACKET CRACKED AT FIXED TRAILING EDGE. REMOVED CRACKED BRACKET AND REPLACED WITH SERVICEABLE PER SRM 51 40 02 ITEM 9.

Part: BRACKET — CRACKED (NR 1 PYLON) · airframe 20,868 hrs · 8,160 cycles

AT RSS 261 LEFT JUST AFT OF NR 1 PYLON AFT BRACKET CRACKED AT FIXED UPPER TRAILING EDGE. REMOVED CRACKED BRACKET AND REPLACED WITH SERVICEABLE PER SRM 51 40 02 ITEM 9.

Part: BRACKET — CRACKED (NR 1 PYLON) · airframe 20,868 hrs · 8,160 cycles

AT RSS 261 LEFT JUST AFT OF NR 1 PYLON FORWARD BRACKET CRACKED AT FIXED UPPER TRAILING EDGE. REMOVED AND REPLACED CRACKED BRACKET WITH NEW PER SRM 51 40 02 STEP 4B 4C AND SOPM 20 10 1 STEP 2.

Part: BRACKET — CRACKED (NR 2 PYLON) · airframe 20,868 hrs · 8,160 cycles

AT RSS 261 RIGHT JUST AFT OF NR 2 PYLON AFT BRACKET CRACKED AT FIXED TRAILING EDGE. REMOVED CRACKED BRACKET AND REPLACED WITH SERVICEABLE PER SRM 51 40 02 ITEM 9.

Part: SUPPORT — CORRODED (BS 727A-727E) · airframe 20,868 hrs · 8,160 cycles

SEVERAL AREAS OF CORROSION ON LT FLOOR TO SIDEWALL SUPPORT BS 727A TO 727I.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,863 hrs · 8,157 cycles

SEVERAL AREAS OF CORROSION ON LT FLOOR TO SIDEWALL SUPPORT BS 727A TO 727I. REMOVED CORROSION OUT OF LIMITS, REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: SKIN — DENTED (CARGO DOOR) · airframe 20,868 hrs · 8,160 cycles

DENT ON AFT CARGO DOOR EXT SKIN 18 INCHES FWD OF AFT EDGE 14 INCHES DOWN. REMOVED AND REPLACED EXTERIOR SKIN AFT CARGO DOOR PER ER 08 5453.

Part: SKIN — DENTED (CARGO DOOR) · airframe 20,868 hrs · 8,160 cycles

FORWARD CARGO DOOR HAS NUMEROUS DENTS IN THE OUTER SKIN. REPLACED FORWARD CARGO DOOR OUTER SKIN WITH A NEW SOLID SKIN.

Part: SKIN — DAMAGED (LT WING) · airframe 19,335 hrs · 7,539 cycles

BIRD STRIKE TO LT WING JUST INBOARD OF NR 1 ENGINE. REPAIRED PER SRM 57 41 01 REPAIR NR 5.

Part: SKIN — DAMAGED (RT WING) · airframe 19,335 hrs · 7,539 cycles

BIRD STRIKE TO RT WING LEADING EDGE ROOT. REMOVED & REPLACED RT LEADING EDGE SKIN.

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

FWD CARGO FLOOR PANEL NR 2 CORRODED.

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

AFT CARGO PIT FLOOR SUPPORT INTERCOSTAL CORRODED. REPAIRED IAW SRM 51-30-01.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 15,532 hrs · 5,962 cycles

AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02.

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

FWD CARGO DOORWAY LWR WEB FOUND CORRODED. REPAIRED IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 15,532 hrs · 5,962 cycles

AFT CARGO FLOOR ATTACH ANGLE CRACKED. REPAIRED IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02.

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

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

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

FWD CARGO FLOOR PANEL NR 1 CORRODED. REPAIRED IAW SRM 51-40.

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

AFT CARGO CHANNEL CORRODED. REPAIRED IAW SRM 53-00-53.

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

AFT CARGO Z-ANGLE CORRODED. REPAIRED IAW SRM 51-40-05.

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

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

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

AFT CARGO PIT FLOOR SUPPORT -T- CORRODED. REPAIRED IAW SRM 51-40-05.

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

AFT CARGO FLOOR SUPPORT CHANNEL CORRODED. REPAIRED IAW SRM 5310 02720.

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

AFT CARGO PIT FLOOR SUPPORT -T- CORRODED. REPAIRED IAW SRM 51-40-05.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

FWD CARGO PIT FLOOR PANEL NR 3 IS CORRODED. REPAIRED IAW SRM 51-40-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 15,532 hrs · 5,962 cycles

FWD CARGO PIT INTERCOSTAL CRACKED. REPAIRED IAW SRM 53-30-53 FIG 2.

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

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

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

AFT CARGO PIT FLOOR CHANNEL SPLICE CORRODED.

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

AFT CARGO FLOOR SUPPORT INTERCOSTAL CORRODED.

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

AFT CARGO DOORWAY FLOOR STRAP CORRODED. REPAIRED IAW SRM 51-40-05.

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

FWD CARGO PIT CORROSION ON RIGHT SUPPORT-Z. REPAIRED IAW SRM 53-40.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,532 hrs · 59,662 cycles

AFT CARGO FLOOR CHANNEL AT BS 767+5 CORRODED. REPAIRED IAW SRM EA 5310 02720.

Part: PAN — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

AFT LAV SVC PORT LINER PAN CORRODED. REPAIRED IAW SRM 51-40-02.

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

AFT CARGO PIT DOORWAY LOWER WEB CORRODED. REPAIRED IAW SRM EA 5320 01805.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

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

Part: BEAM — CHAFED (FUSELAGE) · airframe 15,532 hrs · 5,962 cycles

AFT CARGO PIT VERTICAL BEAM CHAFED. REPAIRED IAW SRM 51-40-02.

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

AFT CARGO Z-CHANNEL CORRODED. REPAIRED IAW SRM 53-00-53 FIG 201.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

FWD CARGO PIT FLOOR PANEL NR 5 CORRODED. REPAIRED IAW SRM 51-40-05.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

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

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

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

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 15,532 hrs · 5,962 cycles

FWD CARGO PIT CORROSION ON LEFT SUPPORT ZEE. REPAIRED IAW SRM 53-00-53.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02.

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

AFT CARGO Z-CHANNEL CORRODED. REPAIRED IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 15,532 hrs · 5,962 cycles

FWD CARGO PIT FLOOR PANEL NR 4 CORRODED. REPAIRED IAW SRM 51-40-05.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,532 hrs · 5,962 cycles

AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02.

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

AFT CARGO PIT FLOOR SUPPORT CHANNEL CORRODED. REPAIRED IAW SRM EA5270 02720.

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

FWD CARGO PIT CORROSION ON RIGHT CARGO TRACK. REPAIRED IAW SRM 53-00-53.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 15,532 hrs · 45,962 cycles

AFT CARGO FLOOR PANEL CORRODED. REPAIRED IAW SRM 51-40-02.

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

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

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

AFT CARGO FLOOR SUPORT -T- CORRODED. REPAIRED IAW SRM 51-40-05.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 15,532 hrs · 5,962 cycles

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