N305AS

Part: LAMP — INOPERATIVE (MAIN CABIN) · airframe 70,258 hrs · 28,258 cycles

EMERGENCY LIGHT AT ROW 21 ABC INOP. GROUNDED - YES. RELAMPED EMERGENCY LIGHT ROW 21 ABC REF. AMM 33-51-03-960-801 OPS TEST GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,680 hrs · 28,005 cycles

EMERGENCY LIGHTS IN LH OVERWING AREA ARE INOP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK OPS CHECKED GOOD IAW B737-900 AMM 33-51-06-960-805.

Part: SKIN — CORRODED · corrosion level 2 · airframe 69,680 hrs · 28,005 cycles

SKIN AT STA 364 TO STA 370 STR 26L HAS AREAS OF CORROSION. GROUNDED - YES. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS B737-900 SRM 53-00-01-1A-5. REPAIRED SKIN IAW ASA EA 900-53EA-25528. FOR WORK ACCOMPLISHED SEE ASA T101 W/O 1944292/ N/R-00024 AAR W/O 1021191-1000-0081. THIS IS A STAGE 2 CAT B REPAIR WITH THE INSPECTION THRESHOLD OF 50,000 TOTAL FLIGHT CYCLES, AND REPEAT INTERVALS TO BE DETERMINED W-=16 O.090 R000 L3.4 D.090.

Part: ANGLE — CORRODED · airframe 69,680 hrs · 28,005 cycles

UPON REMOVING DAMAGE FROM FUSELAGE FOUND STR 28 SPLICE TO BE CORRODED. GROUNDED - YES. REMOVED AND REPLACED ANGLE IAW 737-900 SRM 51-40-02-0G-0W=2 O=.045 R=0.00 L=8 D=.045.

Part: SKIN — CRACKED · airframe 69,680 hrs · 28,005 cycles

LH WING L/E SKIN 116A4410 HAS 17 EA HI-LOKS PULLING THROUGH THE SKIN AT THE OB CORNER OF THESKIN DIRECTLY IB OF #1 PYLON ON THE UPPER SURFACE. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS REPAIRED IAW B737-900 SRM 57-41-01-2R-3.

Part: BATTERY PACK — DISCHARGED (MAIN CABIN) · airframe 69,551 hrs · 27,950 cycles

ROW 16DEF EMERGENCY EXIT LIGHTS ABOVE WINDOW INOP. GROUNDED - YES. REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK REF B737-900 AMM 33-57-06. OP CHK GOOD.

Part: BATTERY PACK — DISCHARGED (MAIN CABIN) · airframe 69,551 hrs · 27,950 cycles

ROW 17DEF EXIT LIGHTS ABOVE WINDOW INOP. GROUNDED - YES. REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK REF AMM 33-57-06. 4 EA CBS PULLED/RESET. OP CHK GOOD.

Part: TIRE — FAILED (NOSE GEAR) · airframe 69,506 hrs · 27,934 cycles

LEFT NOSE WHEEL TIRE FAILURE DURING TAKEOFF. GROUNDED - YES. AIR TURNBACK - PERFORMED TIRE TREAD LOSS OR TIRE BURST CONDITIONAL INSPECTION PER B737-900AMM 05-51-54 FOUND MORE THAN 50% OF TREAD MISSING AND LOW TIRE PRESSURE ON LEFT NOSE TIRE. ALSO FOUND DENTS AFT OF NOSE LANDING GEAR DOORS, DENTS ON FUSELAGE APPROX 10" FWD OF E/E DOOR AND APPROX 24" AFT OF E/E BAY DOOR, AND DENT ON E&E BAY DOOR. REMOVED AND REPLACED BOTH NOSE TIRES PER AMM 32-45-21.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,923 hrs · 27,660 cycles

EXT EMER OFFWING GROUND ILLUMINATION LIGHT INOP. GROUNDED - YES. REMOVE & REPLACE POWER SUPPLY AT ROW 20 LOWER UNIT. REF B737-900 AMM 33-51-06--960-806.

Part: BATTERY PACK — INOPERATIVE (MAIN PASSENGER C) · airframe 67,790 hrs · 27,127 cycles

WHILE PERFORMING ASA T.C. #78233001, FOUND EMERGENCY LT BAT PACK M1670 INOP. GROUNDED - YES. REMOVE AND REPLACED M1670 B737-900 IAW AMM 33-51-06-960-806.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 66,609 hrs · 26,631 cycles

F/A REPORTS L-1 DOOR DIFFICULT TO ARM/ DISARM. GROUNDED - YES. FOUND GIRT BAR FITTINGS ON FLOOR VERY DIRTY, LATCH HARD TO OPERATE CLEANED FLOOR FITTINGS, LATCHES, OPS NORMAL L1 NOW ARM/DISARM NORMAL OK FOR CONT SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 66,479 hrs · 26,584 cycles

L1 DOOR DIFFICULT TO PULL CLOSED AND LATCH THE HANDLE. GROUNDED - YES. PERFORMED OPERATIONAL CK & VISUAL CK OF L1 DOOR PER B737-900 AMM 52-11-00 NO DEFECTS NOTED. DOOR OPERATES NORMAL

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,374 hrs · 26,076 cycles

LOWER RIGHT EXIT SIGN AT OVERWING EXIT 16A MISSING LENS COVER. GROUNDED - YES. REPLACED MISSING LENS COVER. NO FURTHER DEFECTS NOTED. REF B737-900 AMM 33-54-01-960-801.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 65,127 hrs · 25,974 cycles

MULTIPLE EMERGENCY LIGHTS INOP. GROUNDED - YES. REMOVED AND INSTALLED SERVICEABLE EMERGENCY BATTERY PACK M1676 IAW B737-900 AMM 33-51-06-960-805, RELAMPED R/H AFT OVERWING EMERGENCY EXIT LIGHT IAW B737-900 AMM 33-51-04-960-801 AND REPLACED POWER SUPPLY FUSE IN ROW 15L POWER SUPPLY IAW B737-900 AMM 33-51-06-960-804, ALL EMERGENCY LIGHTS OPS CHECK GOOD IAW B737-900 AMM 33-51-04-960-801.

Part: PLATE — CORRODED (BS 727-807) · airframe 65,127 hrs · 25,974 cycles

AFT PIT L/H TRANSITION PANEL HAS CORROSION STA 727 TO 807. GROUNDED - YES. REPAIRED AFT PIT LH TRANSITION PANEL AT STA 727 TO 807 IAW B737-900 SRM 53-00-53-2R-JW= 3 O= .040 R= 0 L= 20 D= .040.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,127 hrs · 25,974 cycles

SHEAR TIE ON TOP OF WING BOX AT FS 540 CRACKED LBL54. GROUNDED - YES. REMOVED AND REPLACED SHEAR TIE FITTING IAW B737-900 SRM 51-40-02-0G-0.

Part: SHEAR WEB — CORRODED (BS 986-1016) · airframe 65,127 hrs · 25,974 cycles

AFT WET R/H SHEAR WEB AFT OF R2 DOOR IS CORRODED ON BOTTOM SIDE. GROUNDED - YES. LOCATED & DRILLED NEW R/H SHEAR WEB AFT OF R2 DOOR IAW B737-900 SRM 51-40-05-0G-0 TO BE INSTALLED ON MIG-5 OK275138 W/O 1019457 2000 0145W-2 O- .040 R-0 L- 4 D-.040.

Part: SHEAR WEB — CORRODED (BS 986-1016) · airframe 65,127 hrs · 25,974 cycles

AFT WET L/H SHEAR WEB AFT OF L2 DOOR IS CORRODED ON BOTTOM SIDEW- 1O- .040 R- 0 L- 3 D- .040. GROUNDED - YES. LOCATED & DRILLED NEW L/H SHEAR WEB AFT OF L2 DOOR IAW B737-900 SRM 51-40-05-0G-0 TP BE INSTALLED ON MIG-5 OK275138 W/O 1019457 2000 0145W- 1 O- .040 R- 0 L- 3 D- .040.

Part: TRUNNION — CORRODED (LT MLG) · airframe 65,127 hrs · 25,974 cycles

L/H MAIN LANDING GEAR FWD TRUNNION FITTING HAS CORRSION ON INBD LOWER LUG ON INBD SIDE. GROUNDED - YES. REWORKED TRUNNION FITTING LUG THIS CARD FOR CORROSION REPORTING PURPOSES ONLY FOR ALL WORK ACCOMPLISHED SEE ASA T/C N8757001 S/N 8169746 W/O 1019456 7000/0019W-3 O- 1.180 R-1.018 L-3 D-.162.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 RBL32) · airframe 65,127 hrs · 25,974 cycles

FWD WET AREA INTERCOSTAL AT RBL 32 STA 312 TO 328 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT RBL 32 STA 312 TO 328 IAW BOEING 737-900 SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 LBL45) · airframe 65,127 hrs · 25,974 cycles

FWD WET AREA INTERCOSTAL LBL 45 STA 312 TO 328 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT LBL45 STA 312 TO 328 IAW BOEING 737-900 SRM 51-40-02-0G-0.

Part: CHANNEL — CORRODED (DOOR SILL) · airframe 65,127 hrs · 25,974 cycles

MOP SEAL AT L2 DOOR HAS AREAS OF LIGHT CORROSION FS986.5 AND FS951. GROUNDED - YES. REMOVED AND REPLACED L2 MOP SILL IAW B737-900 SRM 51-40-02-0G-0 DUE TO 100% MAT LOSSW- 3 O- .080 R- 0 L-12 D- .080.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 65,127 hrs · 25,974 cycles

FLOOR BEAM AT FS 986.5 HAS AREAS OF CORROSION FROM LBL45-RBL45. GROUNDED - YES. REPAIRED FLOOR BEAM AT FS 986.5 IAW B737-900 SRM 53-70-51-2R-4 BY REMOVING AND REPLACING CORRODED REPAIR PARTS W- 3 O- .150 R- .110 L- 18 D-.040.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,127 hrs · 25,974 cycles

SHEAR TIE ON TOP OF WING BOX AT FS 540 CRACKED LBL41. GROUNDED - YES. REMOVED AND REPLACED SHEAR TIE FITTING IAW B737-900 SRM 51-40-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,127 hrs · 25,974 cycles

SHEAR TIE ON TOP OF WING BOX AT FS 540 CRACKED RBL8. GROUNDED - YES. REMOVED AND REPLACED SHEAR TIE FITTING IAW B737-900 SRM 51-42-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,127 hrs · 25,974 cycles

SHEAR TIE ON TOP OF WING BOX AT FS 540 CRACKED RBL15. GROUNDED - YES. REMOVED AND REPLACED SHEAR TIE FITTING IAW B737-900 SRM 51-40-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,127 hrs · 25,974 cycles

SHEAR TIE ON TOP OF WING BOX AT FS 540 CRACKED LBL8. GROUNDED - YES. REMOVED AND REPLACED SHEAR TIE FITTING IAW B737-900 SRM 51-40-02-0G-0.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,127 hrs · 25,974 cycles

SHEAR TIE ON TOP OF WING BOX AT FS 540 CRACKED RBL32. GROUNDED - YES. REMOVED AND REPLACED SHEAR TIE FITTING IAW B737-900 SRM 51-40-02-0G-0.

Part: TRANSITION PANEL — CORRODED (BS 500H-500I) · airframe 65,127 hrs · 25,974 cycles

FWD PIT R/H TRANSITION PANEL HAS AREA OF CORROSION STA 500H TO 500I. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS, REPAIRED SIDEPLATE IAW B737-900 SRM 53-00-53-2R-5W=1.50" O=0.040" R=0.033" L=4.00" D=0.007".

Part: TRANSITION PANEL — CORRODED (BS 500E-500D) · airframe 65,127 hrs · 25,974 cycles

FWD PIT L/H TRANSITION PANEL HAS CORROSION BETWEEN STA 500E AND 500D. GROUNDED - YES. CORROSION FOUND TO BE OUT OF LIMITS, REPAIRED TRANSITION PANEL IAW B737-900 SRM 53-00-53-2R-5 W: 3 O: .040 R: .025 L: 10 D: .015.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 65,127 hrs · 25,974 cycles

FWD PIT SHIED PANEL AFT OF DOOR CUTOUT HAS AREA OF LIGHT CORROSION. GROUNDED - YES. BLENDED FWD PIT SHIELD PANEL AFT OF DOOR CUTOUT OUT OF LIMITS IAW B737-900 SRM 53-00-53-1A-2, REMOVED AND REPLACED SHIELD IAW B737-900 SRM 51-40-02-0G-0W 2 O .040 R .032 L 3 D .008.

Part: STRUCTURE — CORRODED (BS 1088-1153) · corrosion level 2 · airframe 65,127 hrs · 25,974 cycles

APU COMPARTMENT LH LOWER INSULATION MOUNTING STRIP HAS NUMEROUS CORROSION SPOTS AND CHAFE MARKS BETWEEN STA 1088 THRU STA 1156. GROUNDED - YES. FOUND TO HAVE 100% MAT LOSS REMOVED AND REPLACED L/H SIDE LOWER CHORD (INSULATION MOUTNING STRIP) IAW B737-900 SRM 51-40-02-0G-0W: 1 O: .063 R: 0 L: 12 D: .063.

Part: PLATE — CORRODED (BS 727-767) · airframe 65,127 hrs · 25,974 cycles

AFT PIT R/H TRANSITION PANEL HAS CORROSION STA 727 TO 767. GROUNDED - YES. REPAIRED R/H TRANSITION PANEL IN AFT PIT IAW BOEING 737-900 SRM 53-00-53-2R-5W= 3 O= .040 R= 0 L= 12 D= .040.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 65,127 hrs · 25,974 cycles

AFT PIT DOOR CUTOUT FWD SHIELD PANEL IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED SHIELD PNL IAW B737-900 SRM 51-40-02-0G-0W 2 O .050 R 0 L 3 D .050.

Part: CARGO TRACK — CRACKED (BS 727I-727G) · airframe 65,127 hrs · 25,974 cycles

AFT PIT R/H CARGO TRACK IS CRACKED AT RADIUS AT STA 727G, 727H, AND 727I. GROUNDED - YES. CUT OUT DAMAGED SECTION OF TRACK AND ACCOMPLISHED PERMANENT REPAIR IAW B737-900 SRM 53-00-53-2R-3.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 64,675 hrs · 25,777 cycles

EMERGENCY AISLE LIGHT ARE INOP AT SEATSROWS 26ABC AND 29ABC. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M1898. VERIFIED EMERGENCY AISLE LIGHTS AT ROW 26ABC AND 29ABC ARE WORKING NORMAL. REF B737-900 AMM 33-51-06/201.

Part: BULB — INOPERATIVE (RT FWD OVERWING) · airframe 64,647 hrs · 25,763 cycles

RIGHT FWD OVERWING EMERGENCY EXIT LIGHT BULB INOPERATIVE. GROUNDED - YES. REPLACED THE BULB IAW AMM 33-51-04, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 63,850 hrs · 25,398 cycles

LH FWD GALLEY EMERGENCY EXIT LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED LH FWD GALLEY EMERGENCY EXIT LIGHT BATTERY PACK PER B737-900 AMM TASK 33-51-06-960-805. PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST PER AMM TASK 33-51-00-710-801. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (NLG LOCK) · airframe 63,502 hrs · 25,205 cycles

DURING THE AFTER TAKEOFF CHECKLIST, SELECTED GEAR OFF. THE NOSE GEAR EXTENDED WITH A RED AND GREEN NOSE GEAR LIGHT ILLUMINATED. RAN QRH, GEAR RETRACTED NORMALLY AND STAYED RETRACTED WITH GEAR HANDLE IN THE UP POSITION. DURING LANDING GEAR EXTENDED NORMALLY. GROUNDED - YES. INSTALLED 3 EA DOWNLOCK PINS REF B737-900 AMM 32-00-01-480-801. PERFORMED A/C NOSE JACK LIFT POINT D REF AMM 07-11-21-580-801. REMOVED NLG LOCK ACTUATOR REF AMM 32-33-21-000-801. PERFORMED PARTIAL REMOVAL OF NLG LOCK MECHANISM UP TO STEP AMM 32-33-51-000-801, 2E(5). INSTALLED SERVICEABLE ACTUATOR REF AMM TASK 32-33-21-400-801. REINSTALLED APPLICABLE PARTS OF NLG LOCK MECHANISM PER APPLICABLE STEPS OF AMM TASK 32-33-51-400-801. EXTENSION AND RETRACTION TESTS GOOD. LEAK CHECK OF ACTUATOR GOOD. LOWERED AIRPLANE NOSE OFF JACK REF AMM TASK 07-11-21-21-580-802.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,565 hrs · 24,779 cycles

BATTERY PACK FAILED TO CHARGE/TURN ON EMERGENCY LIGHTS. GROUNDED - YES. REPLACED BATTERY PACK S/N 208194, REF B737-900 AMM 33-51-06.

Part: LIGHT — DETACHED (CABIN) · airframe 60,585 hrs · 23,830 cycles

FA ADVISES EXIT PLACARD NEAR R2 DOOR FELL OFF. ACFT GROUNDED. INSTALLED A NEW EXIT LIGHT ASSY. OPS NORMAL.

Part: FLOOR SUPPORT — CORRODED (BS 927-947) · corrosion level 2 · airframe 59,588 hrs · 23,374 cycles

AFT WET AREA FLOOR SUPPORT LBL 45 BS 927 TO 947 FOUND CORRODED. ACFT GROUNDED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-05-0G-0, AND DWG 147A5690.

Part: FLOOR SUPPORT — CORRODED (BS 916) · corrosion level 2 · airframe 59,588 hrs · 23,374 cycles

CORROSION FOUND ON THE FLOOR SUPPORT AT BS 916 AT LEFT O/B LAV MOUNT. ACFT GROUNDED. FOUND OUT OF LIMITS, REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-70-51-1A-1, AND SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 59,588 hrs · 23,374 cycles

FLOOR SUPPORT BETWEEN BS 312 AND 328, LBL 45 IS CRACKED AROUND FASTENER HOLES. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 57-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 270-294.5) · airframe 59,588 hrs · 23,374 cycles

INTERCOSTAL BETWEEN BS 270 AND 294.5, BL 0 IS CRACKED AROUND FASTENER HOLE. ACFT GROUNDED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 59,588 hrs · 23,374 cycles

INTERCOSTAL BETWEEN BS 328 AND 344, LBL 45 IS CRACKED AROUND FASTENER HOLE. ACFT GROUNDED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 59,588 hrs · 23,374 cycles

INTERCOSTAL BETWEEN BS 312 AND 328, RBL 30 IS CRACKED AROUND FASTENER HOLE. ACFT GROUNDED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 59,588 hrs · 23,374 cycles

FLOORBEAM AT BS 947, FOUND CORRODED AT THE LEFT OTBD LAVATORY MOUNT. ACFT GROUNDED. REPAIRED IAW SRM 53-70-51-2R-5, REPAIR 5.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 59,588 hrs · 23,374 cycles

FLOORBEAM, BS 986 HAD MULTIPLE AREAS OF CORROSION ALONG THE TOP AND BOTTOM SIDE. ACFT GROUNDED. FOUND OUT OF LIMITS, REPAIRED THE FLOORBEAM IAW SRM 53-20-51-2R-4.

Part: WEB — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 59,587 hrs · 23,374 cycles

AFT CARGO DOOR CUTOUT LOWER SILL WEB IS CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02-0G-0.

Part: WEB — CORRODED (BS 440-492) · corrosion level 2 · airframe 59,588 hrs · 23,374 cycles

FWD CARGO DOOR CUTOUT LOWER SILL WEB IS CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE WEB IAW SRM 51-40-02-0G-0.

Part: UNKNOWN — OUT OF ADJUST (L1 DOOR) · airframe 57,842 hrs · 22,584 cycles

L1 DOOR IS DIFFICULT TO CLOSE. GROUNDED - YES. REMOVED R1 DOOR LINER AND SLIDE, REF AMM 52-11-31-000-802 AND 25-66-01-000-801. ADJUSTED GUIDE ARM NUT 3 FLAT TURNS DOWN - NO HELP. TURNED NUT BACK TO NORMAL. ADJUSTED UPPER FWD AND AFT LATCH RECEIVERS, ADJUSTED HORIZONTAL ROD AND GUIDE ARM, ADJUSTED ALL STOP PINS, ADJUSTED CENTERING GUIDE. ALL OTHER RIG ADJUSTMENTS CHECKED GOOD, REF AMM 52-11-00-850-801. ACCOMPLISHED DOOR SYSTEM TEST, TESTED GOOD. REINSTALLED THE L1 DOOR LINING, REF AMM 52-11-31-400-802, AND REINSTALLED THE L1 DOOR ESCAPE SLIDE, REF AMM 25-66-01-400-803.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 57,837 hrs · 22,582 cycles

MAIN CABIN FLOORBEAM UPPER TEE CAP CORRODED BS 947, RBL 50. ACFT GROUNDED. COMPLIED WITH EA 900-53EA-19254.

Part: TORQUE TUBE — WORN (L2 DOOR) · airframe 57,641 hrs · 22,490 cycles

L2 DOOR APPEARS TO BE INOPERATIVE. ACFT GROUNDED. FOUND THE L2 DOOR VERTICAL TORQUE TUBE TO BE LOOSE AT LOWER HINGE. REMOVED L2 DOOR FROM A/C. REMOVED WORN TORQUE TUBE ASSEMBLY & INSTALLED NEW TORQUE TUBE ASSEMBLY. REINSTALLED L2 DOOR ON A/C, ACCOMPLISHED RIG ADJUSTMENT, & DOOR SYSTEM TEST, TESTED GOOD. L-2 DOOR IS NOW FULLY OPERATIONAL. ALSO SEE LOG PG. # 11792915 FOR TORQUE TUBE REMOVE AND REPLACE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 57,255 hrs · 22,315 cycles

DURING DESCENT FROM 250 AT APPROXIMATELY FL 215, HAD CABIN ALTITUDE WARNING. CABIN ALTITUDE WAS APROXIMATELY 11,000 FT. CONDUCTED QRC/QRH PROCEDURES. CABIN STABILIZED DURING DESCENT. PROCEEDED TO NORMAL LANDING. ACFT GROUNDED. PERFORMED CABIN PRESSURE CONTROLLER BITE CHECK NR 2 CONTROLLER SHOWED CODE 030, LOW IN FLOW /HIGH LEAKAGE IAW FIM 21-31-801. INSPECTED AIRFRAME FOR LEAKS, NO ABNORMAL LEAKS FOUND. INSPECTED PNEUMATIC DUCT, PRESSURE BULKHEAD, AND AIR CONDITIONING BAYS, NO DEFECTS FOUND. PERFORMED CABIN PRESSURE LEAK TEST IAW AMM 05-51-01, CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,878 hrs · 22,145 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO LEFT AFT OVERWING EXIT HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS AND TESTED IAW MM 33-51-01-960-801, OPS NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 56,675 hrs · 22,060 cycles

R1 DOOR EMERGENCY EXIT IDENTIFIER DAMAGED, LAMPS INOP. GROUNDED - YES. REPLACED LIGHT ASSEMBLY. OPS CHECK NORMAL, REF AMM 33-51-01-960-802.

Part: LENS — BROKEN (CABIN) · airframe 56,363 hrs · 21,917 cycles

F/A REPORTS R1 EXIT LIGHT LENS IS BROKEN. GROUNDED - YES. INSTALLED NEW R1 DOOR EXIT LIGHT LENS.

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 55,548 hrs · 21,550 cycles

L1 DOOR SLIDE PRESSURE LOW. ACFT GROUNDED. REMOVED AND REPLACED THE L1 DOOR SLIDE IAW AMM 25-66-01-400-804 AND 25--66-01-400-803.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,855 hrs · 21,223 cycles

L-1 DOOR EMERGENCY EXIT IDENTIFIER HAS INOP LAMPS. ACFT GROUNDED. REPLACED THE LAMPS. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,855 hrs · 21,223 cycles

BAGGAGE BIN EMERGENCY LIGHT AT 17 ABC INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,512 hrs · 21,058 cycles

EMERGENCY SPOTLIGHT ON ROW 27L BULLNOSE IS INOPERATIVE, REF T/C 78233008. ACFT GROUNDED. RELAMPED 27L BULLNOSE EMERGENCY LIGHT, OPS NORMAL, REF T/C 78233008.

Part: DOOR — STICKING (L2) · airframe 54,459 hrs · 21,036 cycles

FA REPORTS L2 DOOR STICKING. ACFT GROUNDED. PERFORMED OPERATIONAL CHECK OF HANDLE IAW AMM 52-13-00. NO STICKING AT THIS TIME, DOOR OPERATES NORMALLY.

Part: A/C PACK — FAILED (LEFT) · airframe 54,356 hrs · 20,987 cycles

FL 240 CABIN ALTITUDE LIGHT ILLUMINATED. ACFT GROUNDED. CREW WAS UNABLE TO MAINTAIN ALTITUDE. CABIN PRESSURE WARN HORN SOUNDED. PERFORMED QRH AND DESCENDED DUE TO PACK. PERFORMED CONFIDENCE CHECK OF BOTH PACKS AFTER REVERSAL OF PACK, LEFT PACK FAILED CONFIDENCE. PERFORMED & WRENCHED CHECK VALVE FOR LEFT PACK. NO LEAKS AND DEFECTS NOTED. PERFORMED SINGLE PACK OPS CONFIDENCE CHECK FOR LEFT & RIGHT PACK, BOTH PACKS PERFORMED WITHIN AMM PARAMETERS, IAW AMM 21-00-05-700-801.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 53,514 hrs · 20,632 cycles

RT FWD OVERWING EXIT IDENTIFIER INOPERATIVE LAMPS. ACFT GROUNDED. REPLACED THE LAMP, OPS CHECKED NORMAL.

Part: SKIN — CRACKED (BS 1138) · airframe 53,376 hrs · 20,576 cycles

CRACK INDICATION ON LT LOWER HORIZONTAL STABILIZER SKIN AT BS 147, APPROXIMATELY 2" IN LENGTH, 17" FROM AFT SPAR, MARKED IN BLACK. ACFT GROUNDED. REPAIRED LT LOWER HORIZONTAL STABILIZER SKIN AT BS 147 IAW SRM 55-10-01-2R-11. REMOVED AND REINSTALLED L/E PANEL 331BZ AND TIP CAP ASSY IAW AMM 27-41-21.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 53,376 hrs · 20,576 cycles

CRACK INDICATION ON LT LOWER HORIZONTAL STABILIZER SKIN AT BS 175, APPROXIMATELY 1" IN LENGTH, 10" FROM AFT SPAR, MARKED IN BLACK. ACFT GROUNDED. REPAIRED LT LOWER HORIZONTAL STABILIZER SKIN AT BS 175 IAW SRM 55-10-01-2R-11.

Part: SKIN — CORRODED (BS 807-811) · corrosion level 2 · airframe 53,376 hrs · 20,576 cycles

AFT CARGO DOOR INTERIOR SKIN, EXTERIOR SIDE CORRODED. ACFT GROUNDED. REPAIRED AFT CARGO DOOR INNER SKIN IAW REO-G19843, REV "A" AND EA CMPT- 52EA-17047, REV NEW.

Part: SKIN — DENTED (BS 402-418) · airframe 53,376 hrs · 20,576 cycles

SKIN DENTED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN REF SRM 53-00-01-2R1 REPAIR 1.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 50,288 hrs · 19,330 cycles

ROW 17 ACFT LT EMERGENCY EXIT LIGHT ON CEILING NO ILLUMINATING. ACFT GROUNDED. RELAMPED ROW 17 LT EMERGENCY EXIT LIGHT, OPS CK GOOD.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,241 hrs · 18,892 cycles

CRACK FOUND ON HORIZONTAL LT STABILIZER LOWER SKIN AT STABILIZER 184.70,9" FROM FWD SPAR BS 184.70. ACFT GROUNDED. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED, COUTERSINKED AND INSTALLED REPAIR IAW SRM 55-10-01-2K-11, REPAIR 11. ALODINED IAW SRM 51-20-01. PRIMED IAW AMM 51-21- PAINTED IAW AMM 51-21-73.

Part: SCREW — LOOSE (L2 WINDOW TRACK) · airframe 47,886 hrs · 18,346 cycles

CAPTAINS SIDE WINDOW, JAMMED AND WILL NOT OPEN. ACFT GROUNDED. FOUND LOOSE SCREW IN TRACK. TIGHTEN SCREW, OPS CK GOOD.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 47,147 hrs · 18,068 cycles

MAIN CABIN BS 727B, LBL 24.75 SEAT TRACK FLANGES HAVE CRACK INDICATIONS. ACFT GROUNDED. REMOVED, DAMAGE, FABRICATED AND INSTALLED REPAIR IAW REO- G17479, REV A AND EA SB737-53-1296-NG-12.

Part: SKIN — CORRODED (BS 951) · airframe 47,147 hrs · 18,068 cycles

LAV WASTE VACUUM OUTLET CUTOUT IS CORRODED. ACFT GROUNDED. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS IS .071, REMOVED .002 WITH .069 REMAINING IS FOUND TO BE WITHIN LIMTIS IAW SRM 53-00-01-1A-1 ALLOWABLE DAMAGES 1 CHAPT 4-B-2-B, FIGURE 103, DETAIL C. APPLIED ALODINE AND PRIME IAW SRM 51-20-01. PRINTED AREA IAW AMM 51-21-99-300-801. REMOVED DOT.

Part: SKIN — CORRODED (BS 1005-1016) · airframe 47,147 hrs · 18,068 cycles

UPPER FUSELAGE SKIN HAS CORROSION BS 1005 - BS 1016, STRINGER 3L TO 3R. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A-1 TREATED AND PRIME IAW SRM 51-20-01.

Part: INTERCOSTAL — CORRODED (580) · airframe 47,147 hrs · 18,068 cycles

RT FWD OVERWING EMERGENCY EXIT CUTOUT LOWER SILL INTERCOSTAL UPPER SURFACE CORRODED BS 580, LBL 72, WL 221. ACFT GROUNDED. REMOVED CORROSION ORIG .080, REMAINING .078, LOSS .002, FOUND TO BE WITHIN LIMITS IAW SRM 53-40-15-1A-1, FIG 102.

Part: INTERCOSTAL — CORRODED (BS 591) · airframe 47,147 hrs · 18,068 cycles

LEFT FWD OVERWING EMERGENCY EXIT CUTOUT LOWER SILL INTERCOSTAL UPPER SURFACE CORRODED BS 591, LBL 72, WL 221. ACFT GROUNDED. REMOVED CORROSION ORIG .080 REMAINING .076, LOSS .004 IAW SRM 53-40-15-1A-1, FIG 102, DETAIL B-B TOOL T8225M FOUND TO BE WITHIN LIMITS ALODINED AND PRIMED IAW SRM 51-20-01 PAINTED AND MARKED BLENDOUT IAW AMM 51-05-01-701. REMOVED DOT.

Part: INTERCOSTAL — CORRODED (EMERGENCY EXIT) · airframe 47,147 hrs · 18,068 cycles

RIGHT FWD OVERWING EMERGENCY EXIT CUTOUT LOWER SILL INTERCOSTAL UPPER SURFACE CORRODED BS 564, LBL 69.5, WL 221. ACFT GROUNDED. REMOVED FWD OVERWING EMERGENCY EXIT CUTOUT LOWER SIL INTERCOSTAL IAW SRM 51-40-02, INTALLED NEW ONE INTERCOSTAL IAW SRM 51-40-02 RECONNECTED WIRES SP 708 AND SP710 IAW SWRM 20-30-12 AND WDM 21-42-11. REMOVED DOT W914.

Part: INTERCOSTAL — CORRODED (BS 630) · airframe 47,147 hrs · 18,068 cycles

LEFT AFT OVERWING EMERGENCY EXIT CUTOUT LOWER SILL INTERCOSTAL UPPER SURFACE CORRODED BS 630, LBL 72, WL 221. ACFT GROUNDED. REMOVED CORROSION, ORIG .080 REMAINING .079, LOSS .001, FOUND TO BE WITHIN LIMITS IAW SRM 53-40-15-1A-1, FIG 102 DETAIL B-B. TOOL T8225M. ALDOINED AND PRIMED IAW SRM 51-20-01.

Part: INTERCOSTAL — CORRODED (BS 618) · airframe 47,147 hrs · 18,068 cycles

LEFT AFT OVERWING EMERGENCY EXIT CUTOUT LOWER SILL INTERCOSTAL UPPER SURFACE CORRODED BS 618.5, LBL 72, WL 221. ACFT GROUNDED. REMOVED CORROSION ORIG .080 REMAINING .078, LOSS .002 FOUND TO BE WITHIN LIMITS IAW SRM 53-40-15-1A-1, FIG 103 DETAIL B-B TOOL NR T8225M. ALODINED AND PRIMED IAW SRM 51-20-01.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 47,147 hrs · 18,068 cycles

MAIN CABIN SEAT TRACK LUG IS WORN AT STA 520, LBL 24.75. ACFT GROUNDED. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-00-52-1A-1, FIG 103, DETAIL A, ORIG .53 REMAINING .514 LOSS .016 TOOL T8225Y. ALODINED AND PRIMED IAW SRM 51-20-01.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 47,147 hrs · 18,068 cycles

MAIN CABIN BS 727B, RBL 45.50 SEAT TRACK FLANGES HAVE CRACK INDICATIONS. ACFT GROUNDED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW REO G17479 REV A AND EA SB737-53-1296-NG-112.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 47,147 hrs · 18,068 cycles

MAIN CABIN BS 727B, LBL 45.5, SEAT TRACK FLANGES HAVE CRACK INDICATIONS. ACFT GROUNDED. CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO G17479, REV A AND EA SB737-53-1296-NG-112.

Part: CHANNEL — CORRODED (BS 727L-767) · corrosion level 2 · airframe 47,147 hrs · 18,068 cycles

AFT PIT RT TRANSITION FROM STA 727L TO 767 HAS CORROSION AROUND FASTENER HOLES. DOT APPLIED BS 727L -BS 767, WL 154-WL 155, STR 24R-STR 25R. ACFT GROUNDED. R & R RT TRANSITION FROM STA 727L TO 767 IN AFT PIT IAW SRM 53-00-53-2R-5, DOT REMOVED.

Part: CHANNEL — CORRODED (BS 727D-727I) · corrosion level 2 · airframe 47,147 hrs · 18,068 cycles

AFT CARGO BAY LEFT TRANSITION FROM BS 727D - 727I HAS CORROSION AROUND FASTENER HOLES. ACFT GROUNDED. R & R LT TRANSITION IAW SRM 53-00-53-2R-5.

Part: SKIN — CORRODED (BS 1016-1083) · airframe 47,147 hrs · 18,068 cycles

UPPER EMPENAGE SKIN HAS CORROSION BS 1016-BS 1083, STR 3L - 3R. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A-1 TREATED AND PRIMED IAW SRM 51-20-01, TOOL T8225N.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 47,147 hrs · 18,068 cycles

MAIN CABIN SEAT TRACK IS WORN AT BS 520, RBL 45.50. ACFT GROUNDED. BLENDED AREA AND FOUND OUT OF LIMITS IAW SRM 53-00-52. CUTOUT DAMAGE, LOCATED DRILLED AND INSTALLED REPAIR PACK IAW REO-G17476 REV A AND EA 900-53EA 12799.

Part: SKIN — DENTED (BS 832-855) · airframe 47,147 hrs · 18,068 cycles

FUSELAGE SKIN AROUND AFT CARGO DOOR CUTOUT, AFT SIDE IS DENTED. ACFT GROUNDED. REMOVED DAMAGE, ACCOMPLISHED HFEC, EDDY CURRENT INSPECTIONS OF ALL OPEN HOLES, COUNTERSINKS AND PRIOR AND NEW TRIMMED SKIN, ACCOMPLISHED INSURANCE CUT OF PRIOR AND NEW TRIMMED SKIN, FABRICATED, LOCATED, AND DRILLED AND INSTALLED INNER DOUBLER, DOUBLER, OUT DOUBLER AND FILTERS IAW REO-G17485 REV A AND SRM 53-00-01-2R-25, REPAIR 25. ALODINED AND PRIMED IAW SRM 51-20-01 PAINTED IAW AMM 51-21-99 AND EA 900-53EA-12839, REV NEW.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 47,147 hrs · 18,068 cycles

MAIN CABIN SEAT TRACK IS WORN BS 520, RBL 24.75. ACFT GROUNDED. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-00-52-1A-1, FIG 103, DETAIL A. ALODINED AND PRIMED IAW SRM 51-20-01.

Part: CHANNEL — CORRODED (BS 500K) · airframe 47,147 hrs · 18,068 cycles

FWD CARGO BAY HAS CORROSION ON RT TRANSITION PANEL AT BS 500K+14. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS, REMOVED DAMAGE IAW SRM 51-10-02. FABRICATED NEW CHANNEL & SPLICE PLATE IAW SRM 51-20-01. INSTALLED ZEE CHANNEL & SPLICE PLATE IAW SRM 53-00-53-2R-5 & SRM 51-40-02.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 47,147 hrs · 18,068 cycles

MAIN CABIN SEAT TRACK IS WORN BS 520, LBL 45.50. ACFT GROUNDED. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-00-52-1A-1, FIG 103, DETAIL A. ALODINED AND PRIMED IAW SRM 51-20-01.

Part: STRIKER — WORN (DOOR) · airframe 45,223 hrs · 17,349 cycles

HIGH PRESSURE DOOR 192. FWD RT OTBD LATCH STRIKE PLATE WORN THRU, ACFT GROUNDED. BLENDED OUT DAMAGE ON TOP SURFACE OF LOWER CHORD. MATERIAL REMOVED .025, AREA .060 LENGTH, .050 WIDTH, BLENDED OUT DAMAGE FROM EDGE OF LOWER CHORD, MATERIAL REMOVED .030, AREA .060, REF SRM 51-40-71-1A-1. CONTINUED TO BLEND DAMAGE UPPER SURFACE INBD LOWER FLANGE OF LONGITUDINAL CHORD AT STA 549 AREA. AREA OF BLEND 3.7 LONG BY .7 WIDE. MATERIAL THICKNESS REMAINING IN BLEND AREA .083, REF SRM 53-40-71-1A-1, 31628, EA 900-53EA-11392, COMPLETED.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 44,657 hrs · 17,135 cycles

L1 DOOR WILL NOT CLOSE. ACFT GROUNDED. ADJUSTED L1 DOOR GUIDE ARM IAW STEP H(1) MM 52-11-00-820-801. OPS CK GOOD. CLEARANCE CHECK GOOD IAW TABLE 501 AND FIG 503 MM 52-11-00-820-801. NO DAMAGE NOTED TO DOOR SKIN OR CUTOUT.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 44,004 hrs · 16,902 cycles

LIGHTED EXIT SIGN COVER LOOSE. ACFT GROUNDED. SECURED EXIT SIGN FWD RT OVERWING EXIT COVER.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,565 hrs · 15,648 cycles

RIGHT OVERWING FWD EMERGENCY LIGHT INOPERATIVE. (EXTERIOR) . RELAMPED, CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,824 hrs · 15,393 cycles

EMERGENCY LIGHT BATTERY M1694 UNDER SEAT ROW 15ABC INOPERATIVE. ACFT GROUNDED. R & R EMERGENCY BATTERY UNDER SEAT ROW 15 ABC IAW MM 31-51-06-960-806. EMERGENCY LIGHT OPS CHECK GOOD IAW MM 33 51 00 720 801.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,824 hrs · 15,393 cycles

EMERGENCY LIGHT BATTERY PACK M2335 UNDER SEAT ROW 6ABC INOPERATIVE. ACFT GROUNDED. R & R EMERGENCY BATTERY PACK POWER SUPPLY AT SEAT ROW 6ABC (M2335) AND OPS CHECKED GOOD IAW AMM 33-51-06-960-806.

Part: BUSHING — MIGRATED (HORIZ STAB) · airframe 35,488 hrs · 13,833 cycles

LEFT HORIZONTAL STABILIZER AFT LOWER ATTACH LUG AFT BUSHING MIGRATING. ACCOMPLISHED REPAIR TO LT HORIZONTAL STABILIZER AND CENTER SECTION REAR SPAR CLEVIS LUGS IAW TIMCO REO G 13457 REV A DATED 17 JAN 11.

Part: BUSHING — CORRODED (HORIZ STAB) · airframe 35,488 hrs · 13,833 cycles

LT HORIZONTAL STABILIZER CENTER SECTION MIDDLE STABILIZER ATTACH POINT CLEVIS FORWARD AND AFT BUSHINGS CORRODED. REMOVED AND REPLACED BUSHINGS IAW TIMCO REO G 13457 REV A.

Part: BUSHING — CORRODED (HORIZ STAB) · airframe 35,488 hrs · 13,833 cycles

HORIZONTAL STABILIZER CENTER SECTION AFT ATTACH FITTING FOR OUTBOARD STABILIZER UPPER AFT BUSHING PITTED/CORRODED IN BORE AND FORWARD FLANGE. REMOVED AND REPLACED BUSHINGS IAW TIMCO REO G 13457.

Part: BUSHING — LOOSE (HORIZ STAB) · airframe 35,488 hrs · 13,833 cycles

LT HORIZONTAL STABILIZER AFT LOWER ATTACH LUG FORWARD AND AFT BUSHINGS HAVE BROKEN SEALANT. REMOVED AND REPLACED BUSHINGS IAW TIMCO REO G 13457.

Part: BUSHING — CORRODED (HORIZ STAB) · airframe 35,488 hrs · 13,833 cycles

CENTER HORIZONTAL STABILIZER AFT ATTACH FITTING FOR LT HORIZONTAL STABILIZER UPPER LUG FORWARD BUSHING FLANGE PITTED/CORRODED. REMOVED AND REPLACED BUSHING IAW TIMCO REO G 13457.

Part: RIB — CRACKED (HORIZ STAB) · airframe 35,488 hrs · 13,833 cycles

LEFT HORIZONTAL STABILIZER INTERNAL RIB CRACKED AT STAB STA 101.90 REPAIRED IAW B737 900 SRM 55 10 09 REPAIR 4.

Part: MECHANISM — LACK OF LUBE (L1 DOOR) · airframe 32,160 hrs · 12,530 cycles

FWD ENTRY DOOR STIFF AND DIFFICULT TO OPEN AN CLOSE. UPON OPENING THIS LEG DOOR MADE A CRACKING / POPPING SOUND PERFORMED FIM TASK 52 10 00 810 807. LUBRICATED FWD ENTRY DOOR MECHANISM. FWD ENTRY DOOR OPERATES NORMALLY. OK FOR SERVICE.

Part: SUPPORT FITTING — WORN (FLAP TRACK) · airframe 30,031 hrs · 11,700 cycles

RT OTBD FLAP, OTBD FLAP TRACK SUPPORT FITTING WORN FROM SEAL. REPAIRED FITTING.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,031 hrs · 11,700 cycles

(2) AFT EMERGENCY AISLE LIGHTS GO OUT 2 MIN INTO CYCLE LT SIDE. REMOVED AND REPLACED BATTERY PACK M1898. OPS CHECK GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 30,031 hrs · 11,700 cycles

(2) AFT RT EMERGENCY AISLE LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK M1899. OPS CHECK GOOD.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

FWD CARGO FLOOR PANEL CORRODED. REPLACED FLOOR PANEL.

Part: WEB — CRACKED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

CRACK FOUND IN WEB BAFFLE STA 500B 500C RBL 21 WL 160. REPLACED WITH NEW BAFFLE DWG 143A7505.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT IN FWD CARGO BS 470 500D ON GETTING OK TO CLOSE. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,031 hrs · 11,700 cycles

EMERGENCY EXIT LIGHT BATTERY M1672 ABOVE AFT GALLEY CENTER CEILING PANEL RIGHT SIDE WILL NOT CHARGE. REMOVED AND REPLACED BATTERY PACK M1677.

Part: RETAINER — CRACKED (BS 663) · airframe 30,031 hrs · 11,700 cycles

VAPOR BARRIER SEAL RETAINER CRACKED. REPLACED DOUBLER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

ELONGATED HOLE BS 500L LBL21 TOP OF FRAME. REPAIRED FRAME.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

CRACKED INTERCOSTAL BS 927 TO 947 BL0. REPLACED INTERCOSTAL.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,031 hrs · 11,700 cycles

LT HORIZONTAL STABILIZER LOWER SURFACE IS CRACKED. REPAIRED IAW EA 900 55EA 01352

Part: FLOOR PANEL — GOUGED (CARGO BAY) · airframe 30,031 hrs · 11,700 cycles

ACB NR 5 FLOOR PANEL HEAVILY GOUGED. REPLACED FLOOR PANEL.

Part: FLOOR PANEL — GOUGED (CARGO BAY) · airframe 30,031 hrs · 11,700 cycles

FCB FLOOR PANEL NR 3 IS HEAVILY GOUGED. REMOVED AND REPLACED FLOOR PANEL NR 3 IN FCB.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED. REMOVED AND REPLACED.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

AFT RT MOPSILL CORRODED REMOVED AND REPLACED AFT SERVICE DOOR MOPSILL.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 30,031 hrs · 11,700 cycles

AFT CARGO BAY FLOOR PANEL NR 3 CORRODED. REPLACED FLOOR PANEL.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO BAY BILGE BS 500E RBL6 STR ON STR CLIP REPLACED STRINGER CLIP.

Part: FLOOR PANEL — CORRODED (COCKPIT) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

COCKPIT FLOOR PANEL AT VIEWER IS CORRODED. REPLACED FLOOR PANEL.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO BAY FLOOR PANEL. REPLACED FLOOR PANEL.

Part: FRAME — DAMAGED (BS 500K) · airframe 30,031 hrs · 11,700 cycles

FRAME BS 500K LT HAS OVERSIZED HOLE AT CARGO FLOOR TO SIDEWALL. REPAIRED FRAME.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

BS 500B RT FUSE FRAME HAS OVERSIZED HOLE AT FLOOR TO SIDEWALL SUPPORT. REPAIRED FRAME.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION IN FWD CARGO BAY NR 1 FLOOR PANEL BEYOND LIMITS. REMOVED CORROSION OUT OF LIMITS FABRICATED CARGO BAY NR 1 FLOOR PANEL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

BS 500F FRAME RT HAS AN OVERSIZED HOLE AT CARGO FLOOR TO SIDEWALL. REPAIRED FRAME.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

BS 500D FRAME RT HAS OVERSIZED HOLE AT CARGO FLOOR TO SIDEWALL. REPAIRED FRAME.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

BS 500C RT FUSE FRAME HAS OVERSIZED HOLE AT FLOOR TO SIDEWALL SUPPORT. REPAIRED FRAME.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

G4B WALL SUPPORT BS 992 RBL 33-44. REPLACED SUPPORT. REPLACED WALL SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

G4B WALL SUPPORT BS992 1015 LBL 31 WL 208 IS CORRODED.

Part: SCUFF PLATE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

ACB DOOR WAY FWD SCUFF TIE DOWN PLATE CORROSION OUT OF LIMITS. REMOVED AND INSTALLED FABRICATED FWD SCUFF TIE DOWN PLATE IAW SRM 51 40 05.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

G4B WALL SUPPORT BS 992, LBL, 33-44, WL 208 IS CORRODED. REPLACED WALL SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

G4B FLOOR SUPPORT BS 992-1025 RBL 31 WL 208 IS CORRODED. REPLACED FLOOR SUPPORT.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

AFT CARGO BAY FLOOR PANEL SPLICE CORRODED. REPLACED EXTRUSION PER DEG 146A941 ALODINE PRIME INSTALLED NUTPLATES.

Part: FLOOR PANEL — GOUGED (CARGO BAY) · airframe 30,031 hrs · 11,700 cycles

AFT CARGO BAY FLOOR PANEL GOUGED. REMOVED AND REPLACED FLOOR PANEL.

Part: SKIN — DENTED (HORIZ STAB) · airframe 30,031 hrs · 11,700 cycles

LT HORIZONTAL STAB L/E IS DENTED. DENT OUT OF LIMITS TRIMMED OUT DAMAGE FABRICATED AND INSTALLED DOUBLER.

Part: SKIN — DENTED (HORIZ STAB) · airframe 30,031 hrs · 11,700 cycles

LT HORIZONTAL STAB L/E IS DENTED STAB STA 104. FOUND TO BE OUT OF LIMITS CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR PARTS DOUBLER.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 30,031 hrs · 11,700 cycles

FWD CARGO BAFFLE BS 500G-500H LBL 25 WL 156 CRACKED. REMOVED AND REPLACED BAFFLE.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 30,031 hrs · 11,700 cycles

AFT CARGO BAY FLOOR PANEL NR1 PUNCTURED. FABRICATED NEW FLOOR FLOOR PANEL PER SRM 53-60-53.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION ON STR CLIP, REMOVED AND REPLACED STRINGER CLIP.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 30,031 hrs · 11,700 cycles

FWD CARGO BAY BAFFLE IS CRACKED. REPLACED BAFFLE.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 30,031 hrs · 11,700 cycles

FWD CARGO BAFFLE BS 500H-500I LBL 25 WL 156 CRACKED. REMOVED AND REPLACED BAFFLE.

Part: SPLICE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

AFT CARGO BAY FLOOR PANEL SPLICE CORRODED. REPLACED EXTRUSION BAC1505-100581 PER B DWG ALODINE AND PAINT INSTLLED NUTPLATES.

Part: TEE FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

FLOOR STRAP CORRODED AFT CARGO BAY. OUT OF LIMITS, REMOVED AND INSTALLED NEW FLOOR STRAP PER SRM 51-40-05.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

FLOOR PANEL SUPPORT CRACKED. REMOVED AND REPLACED.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

FWD CARGO BAY BILGE, BS 500H STR CLIP CORRODED BEYOND LIMITS. REMOVED AND REPLACED STRINGER CLIP.

Part: FLOORBEAM — CORRODED (BS 500R) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

FWD CARGO BAY FLOOR TRACK BEAM IS CORRODED BEYOND LIMITS. REMOVED FABRICATED AND INSTALLED PER SRM 53-00-53.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

FWD CARGO BAY INTERCOSTAL CORRODED BEYOND LIMITS. REPLACED INTERCOSTAL.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

RBL 51 SHEAR TIE, BS 986.5 IS MISDRILLED FABRICATED NEW SHEAR TIE AND REPLACED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

FLOOR PANEL SUPPORT CRACKED. REMOVED AND REPLACED WITH NEW.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

RBL 51 SHEAR TIE MISDRILLED BS 986.5 FABRICATED NEW SHEAR TIE AND REPLACED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

CRACKED BRACKET ON RT SIDE OF PACKS EXHAUST. REPLACED BRACKET.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

INTERCOSTAL CRACKED FWD CARGO BAY. REMOVED AND REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

INTERCOSTAL CRACKED BS 500I-500J, FWD CARGO BAY LBL 25. REMOVED AND REPLACED INTERCOSTAL.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

ATTACH BRACKET CRACKED, RT SIDE OF PACK EXHAUST. REPLACED BRACKET.

Part: STRINGER CLIP — CORRODED · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO BAY BILGE BS 500J RBL 6 STRONGER CLIP CORRODED STRINGER. REMOVED AND REPLACED STRINGER CLIP IN FWD CARGO BAY BILGE BS 500 RBL 6 AT STRINGER.

Part: STRINGER CLIP — CORRODED · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO BAY BILGE BS 500H RBL 15 STRINGER CLIP CORRODED AT STRINGER. REMOVED AND REPLACED STRINGER CLIP.

Part: SUPPORT — CHAFED · airframe 30,031 hrs · 11,700 cycles

FOUND FAIRING FORMER SUPPORT AT 649, RBL 43, WL 148 TO HAVE CHAFE DAMAGE EXCEEDING 10 PERCENT OF PART THICKNESS. REMOVED AND REPLACED FAIRING SUPPORT.

Part: SUPPORT — CORRODED (BS 867-885) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT RBL 21 BS 885-867 AFT CARGO BAY. REPAIRED FLOOR AND SIDEWALL SUPPORT.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

FOUND CORROSION ON BS 947.5 FLOORBEAM AFT FLANGE RBL 57 WL 208. REPAIRED PER ER-09-2614-EA-900-53EA-01395.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT RBL 21 BS 885 TO 867 AFT CARGO BAY. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT ZEE AFT CARGO BAY BS 867 885 RBL 21.

Part: SUPPORT — CRACKED (RT WING) · airframe 30,031 hrs · 11,700 cycles

RW UPPER TE PANEL SUPPORT CRACKED. REPLACED WEB ASSY.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FLOORBEAM BS 947 LBL 4 TO RBL 4 CORROSION AND PITTING IN UPPER FLANGE AROUND NUT PLATE HOLES. REPAIRED PER ER 09-2614-EA-900-53EA-01395.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FOUND ON FLOORBEAM STA 947 RBL 53 AND WL 208 FLOOR PANEL HOLE. REPAIRED PER ER 09-2614-EA-900-53EA-01395.

Part: FLOOR SUPPORT — CRACKED (BS 270-277) · airframe 30,031 hrs · 11,700 cycles

FLOOR SUPPORT STRAP CRACKED BS 270-277 LBL 26 WL 208. REPLACED FLOOR SUPPORT.

Part: STRINGER CLIP — CORRODED · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO BAY BILGE BS 500H LBL6 STR CLIP CORRODED AT STRINGER. REMOVED AND REPLACED STRINGER CLIP BS 550H LBL6.

Part: INTERCOSTAL — CORRODED (BS 947-967) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION ON INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 30,031 hrs · 11,700 cycles

INTERCOSTAL CRACKED. REPLACED WITH NEW INTERCOSTAL.

Part: SUPPORT — CORRODED (BS 500L) · airframe 30,031 hrs · 11,700 cycles

FWD CARGO BAY LWR BULKHEAD RAIL ASSY HAS CORROSION. REPLACED SUPPORT.

Part: SHEAR TIE — CRACKED (BS 538) · airframe 30,031 hrs · 11,700 cycles

PANEL SUPPORT UPPER SKIN CRACKED. REMOVED AND REPLACED UPPER SKIN.

Part: CARGO TRACK — CORRODED (BS 727I) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO COMPARTMENT CORROSION ON RAIL AT BS 727I+6 LBL 3 WL 156. REPLACED RAIL.

Part: INTERCOSTAL — CORRODED (BS 1006) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

INTERCOSTAL IS CORRODED. REMOVED AND REPLACED INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 30,031 hrs · 11,700 cycles

INTERCOSTAL CRACKED STA 312-328 LBL 48 WL 208. REMOVED AND REPLACED WITH NEW INTERCOSTAL.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 30,031 hrs · 11,700 cycles

INTERCOSTAL CRACKED STA 328 344 LBL 48 WL 208. REMOVED AND REPLACED WITH NEW INTERCOSTAL.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT LBL 21 BS 847 TO 797 AFT CARGO BAY. PART TO BE REPLACED ON DEFECT NR 5185252.

Part: STRIP — CORRODED (BS 727I-767) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO BAY FLOOR TO SIDEWALL CAPSTRIP. REMOVED AND REPLACED CAPSTRAP.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO COMPARTMENT BS 500J-500K+7 RT FLOOR TO SIDEWALL SUPPORT CORRODED AT NUT PLATE. REMOVED AND REPLACED.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

FWD CARGO COMPARTMENT BS 500D+10 500E+12 RBL 25 RT FLOOR TO SIDEWALL SUPPORT CORRODED AT NUT PLATES. REPLACED PER SRM.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO COMPARTMENT BS 500J 500K LT FLOOR TO SIDEWALL SUPPORT CORRODED AT NUT PLATES AND FASTENERS. REPLACED SIDEPLATE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO COMPARTMENT BS 500J 500K LT FLOOR TO SIDEWALL SUPPORT CORRODED AT NUTPLATES AND FASTENERS. REPLACED SIDEPLATE.

Part: STRIP — CORRODED (BS 727I-767) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO BAY FLOOR TO SIDEWALL CAPSTRIP BS 727I-767 LT. REMOVED AND REPLACED CAPSTRAP.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO BAY FLOOR TO SIDEWALL ZEE SUPPORT BS 731-727I LBL 21 WL 156. REMOVED AND REPLACED SUPPORT.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO COMPT, CORROSION ON CARGO TRACK AT BS 727I+6 LBL 17.24 WL 156. REMOVED AND REPLACED CARGO TRACK SPLICE.

Part: FLAP TRACK — GOUGED (TE FLAP) · airframe 30,031 hrs · 11,700 cycles

RIGHT WING INBOARD MAIN FLAP INBOARD AFT FLAP PROGRAMMING TRACK IS WORN AND GOUGED ON THE EDGES OF THE UPPER AND LOWER FLANGES. IN LIMITS

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO BAY FRAME AT BS 500L LBL 25 RBL 25 CORRODED ON UPPER FLANGE. BLENDED CORROSION 10 EA AREAS IN LIMITS.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION ON CARGO TRACK RBL 13, BS 865-807 AFT CARGO BAY. REPLACED CARGO TRACK.

Part: SHIELD — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO COMPT, CORROSION ON SHIELD AT BS 794 767 RBL 22 WL 163. REMOVED AND REPLACED SHIELD.

Part: ROD — DENTED (TE FLAP) · airframe 30,031 hrs · 11,700 cycles

LEFT WING O/B MAIN FLAP O/B END AIRLOAD ROD HAS DENTS WORN INTO IT. BLENDED CONTROL ROD.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO BAY BILGE BS 500C RBL 6 STR CLIP CORRODED STR 28R. REMOVED AND REPLACED STRINGER CLIP.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO COMPARTMENT CORROSION ON RAIL AT BS 727I+6 RBL 3 WL 156. REPLACED RAIL.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO COMPARTMENT CORROSION ON CARGO DOOR CUTOUT LOWER MAIN SILL WEB BS 794-847 RBL 25 WL 163-167. REMOVED AND REPLACED LWR MAIN SILL WEB PER SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 727I-807) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO COMPT, CORROSION ON ZEE SIDE SUPPORT AT BS 727I LBL 22 WL 156. REMOVED AND REPLACED ZEE SIDE SUPPORT BS 807-727I LBL 22 WL 156.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO BAY FLOORBEAM SURFACE BS 500K+1 RBL 13 CORRODED AT NUT CLIP. REMOVED DAMAGED SECTION AND REPLACED WITH REPAIR PARTS.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO COMPT. CORROSION ON ZEE SIDE SUPPORT AT BS 807 TO BS 727I LBL 22 WL 156. REMOVED AND REPLACED ZEE SIDE SUPPORT BS 807 727I LBL 22 WL 156.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO BAY FLOOR TO SIDEWALL Z-SUPPORT BS 731-727I RBL 21 WL 156. REMOVED FABRICATED NEW AND REPLACED AFT CARGO BAY FLOOR TO SIDEWALL ZEE SUPPORT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

BS 986.5 FLOORBEAM CORRODED IN SEVERAL AREAS ON UPPER FLANGES WL 208.1. REPAIRED FLOORBEAM.

Part: INTERCOSTAL — CORRODED (BS 947-967) · airframe 30,031 hrs · 11,700 cycles

CORROSION ON INTERCOSTAL BS 947 TO BS 967 LBL 50 AROUND NUTPLATE HOLES. REMOVED AND REPLACED INTERCOSTAL.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION AFT CARGO COMPARTMENT CORROSION ON ZEE SIDE SUPPORT AT BS 767 TO 727I RBL 22 WL 156. REPAIRED WITH FABRICATED ZEE SUPPORT.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION ON INTERCOSTAL BS 947-967 LBL 50 AROUND NUT PLATE HOLES. REPAIRED INTERCOSTAL.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION ON AFT CARGO BAY CARGO TRACK REPAIR AT BS 772 RBL 13.8 WL 162. TRACK REPLACED.

Part: WEB — CHAFED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

E/E BAY DOOR SURROUND LT SIDE WEB IS CHAFED ABOVE DOOR PIN FITTING BS 364. REMOVED AND REPLACED WEB WITH FABRICATED WEB.

Part: CARGO TRACK — CORRODED (BS 772) · airframe 30,031 hrs · 11,700 cycles

CORROSION ON AFT CARGO BAY CARGO TRACK REPAIR AT BS 772 RBL 13.8 WL 162. ENTIRE TRACK BEING REPLACED.

Part: SKIN — DENTED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

DENT IN MIDDLE EDGE OF AFT CARGO DOOR CUTOUT AFT SIDE BS 845 RBL 53-22 INCHES O/B OF LOWER AFT CORNER. REPAIRED DOOR SKIN.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION ON AFT CARGO COMPARTMENT RAIL BS 727I+6 LBL 8.1 WL 156. REPLACED RAIL.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

CORROSION FOUND ON LANDING GEAR VIEWER SUPPORT WEB STA 260-269 LBL 3-RBL 3 WL 208. REMOVED AND REPLACED.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO COMPT BS 500F+7-500F+14 LT FLOOR TO SIDEWALL SUPPORT. REPLACED FWD CARGO FLOOR TO SIDEWALL SUPPORT.

Part: PLATE — CORRODED (BS 500H-500I) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO COMPARTMENT BS 500H+7 TO 500I+12 FLOOR TO SIDEWALL SUPPORT. SIDEPLATE REPLACED.

Part: PLATE — CORRODED · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO COMPT BS 500G+16 LT FLOOR TO SIDEWALL SUPPORT CORRODED AT LOWER SURFACE. SIDEPLATE TO BE REPLACED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

CORROSION FOUND ON Z-ANGLE CHORD STA 269 LBL 11 RBL 11 WL 208. REMOVED FABRICATED NEW 2" ANGLE AND REPLACED.

Part: PLATE — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,031 hrs · 11,700 cycles

CORROSION FWD CARGO COMPARTMENT 500I+12 LT FLOOR TO SIDEWALL SUPPORT CORRODED AT FASTENERS. SIDEPLATE TO BE REPLACED.

Part: SCUFF PLATE — DENTED (FUSELAGE) · airframe 30,031 hrs · 11,700 cycles

DENT ON AFT CARGO BAY SCUFF PLATE 25 INCHES FWD OF AFT END. DENT REPAIRED.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,823 hrs · 11,617 cycles

DURING T/C 78233001 EMERGENCY LIGHT CHECK FOUND BATTERY PACKS FAILING TEST ON M1695 1671 AND 1673. REPLACED BATTERY PACKS AT M1695 1671 AND 1673 REF MM 33 51 06 960 805. OPS NORMAL.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 28,917 hrs · 11,280 cycles

L 1 DOOR HARD TO CLOSE ADJUSTED L 1 DOOR GUIDE ARM REF M/M 52 11 00 820 801. DOOR OPS CHECK NORMAL.

Part: ENGINE — DAMAGED (NR 1) · airframe 28,913 hrs · 11,279 cycles

ON T/O CLIMBING THRU 4000FT IN TURN FLAPS 1 GEAR UP. WE HEARD A LOUD THUMP FOLLOWED BY A YAW TURN TO THE LT F/A REPORTED UNUSUAL NOISE ON THE LT ENG. PILOTS DID NOT SEE ANY UNUSAL ENGINE OR PRESSURE INDICATIONS. RETURNED TO LAS. PAXS IN ROW 25/26 SAW A FIRE BALL AND THEN SMOKE ON NR 1 ENG. DAMAGE FOUND STAGE 3 HPC BLD35. MEASURED TO .055 DIM B. R&R NR 1 ENGINE PER TC 78471000 AND 78471001 WO # 10109.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 26,958 hrs · 10,527 cycles

GOUGE CRACK IN FORWARD CARGO DOOR SKIN. REPAIRED PER SRM 52 00 01.

Part: FLOORBEAM — CORRODED (BS 7271) · airframe 24,232 hrs · 9,444 cycles

AFT CARGO PIT FLOORBEAM TEE CORRODED AT BS 727I+6. REPAIRED FLOORBEAM TEE IAW 51-40-05.

Part: INTERCOSTAL — CORRODED (BS 727) · airframe 24,232 hrs · 9,444 cycles

AFT CARGO PIT LT INTERCOSTAL RACK CORRODED AT BS 727. REPAIRED INTERCOSTAL RACK IAW SRM 53-00-53.

Part: INTERCOSTAL — CORRODED (BS 727) · airframe 24,232 hrs · 9,444 cycles

AFT CARGO PIT LEFT INTERCOSTAL TRACK CORRODED AT BS 727. REPAIRED INTERCOSTAL TRACK IAW SRM 53-00-53 FIG 202.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 24,232 hrs · 9,444 cycles

DENT ON LEFT HORIZ STAB L/E 5FT FROM ROOT. REPAIRED DENT ON L/E IAW SRM 55-10-01.

Part: INTERCOSTAL — CORRODED (BS 727-767) · airframe 24,232 hrs · 9,443 cycles

AFT CARGO PIT LT INTERCOSTAL TRACK (ZEE ANGLE) FOUND CORRODED FROM BS 727 TO 767 + 10 AFT CARGO PIT. LT INTERCOSTAL TRACK (ZEE ANGLE) REPLACED FROM BS 727 TO 767+10 IAW B737 900 SRM 51-40-02 AND 53-00-53 FIG 202.

Part: BULKHEAD — CRACKED (LWS 201) · airframe 24,232 hrs · 9,443 cycles

LEFT WING TRAILING EDGE BULKHEAD AT WBL 201 90 WEB ASSY CRACKED. WEB ASSY REPLACED WITH NEW PART IAW B737 900 SRM 51-40-02.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 24,232 hrs · 9,443 cycles

RAMP REPORTS DENTS ON LT HORIZ STAB 2E 5FT FROM ROOT. REPAIRED IAW B737 900 SRM 55-10-01 REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 727I S26L/R) · airframe 24,232 hrs · 9,443 cycles

AFT CARGO PIT FLOOR SUPPORT TEE BS 727I+6 RBL 17 TO LBL 17 FOUND CORRODED. AFT CARGO PIT SUPPORT TEE AT BS 727I+6 RBL 17 TO LBL 17 WAS REPLACED WITH MADE REPAIR PART IAW B737 900 SRM 51-40-05.

Part: BULKHEAD — CRACKED (RWS 201) · airframe 24,232 hrs · 9,443 cycles

RIGHT WING TRAILING EDGE BULKHEAD AT WBL 201.90 WEB ASSY CRACKED. WEB ASSY REPLACED WITH NEW PART IAW B737 900 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (BS 500J-500K) · airframe 24,232 hrs · 9,443 cycles

FWD PIT RT INTERCOSTAL BS 500J TO BS500K FOUND CRACKED. INTERCOSTAL RT AT FWD PIT REPLACED WITH MADE REPAIR PART IAW B737 900 SRM 51-40-20 AND 53-30-53.

Part: INTERCOSTAL — CRACKED (BS 500I) · airframe 24,232 hrs · 9,443 cycles

FWD CARGO PIT RT BAFFEL AT BS 500I RBL 21 BELOW RT ZEE CHANNEL IS CRACKED. BAFFEL AT RT FWD CARGO PIT AT BS 500G RBL 21 REPLACED WITH MADE REPAIR PART IAW B737 900 SRM 53-30-53 FIG 2 AND 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 727-767) · airframe 24,232 hrs · 9,443 cycles

AFT CARGO PIT RT INTERCOSTAL TRACK ZEE ANGLE FOUND CORRODED FROM BS 727 TO BS 767. AFT CARGO PIT RT INTERCOSTAL TRACK (ZEE ANGLE) BS 727 TO BS 767 REPLACED WITH A MADE REPAIR PART IAW B737 900 SRM 53-00-53 FIG 202.

Part: INTERCOSTAL — CRACKED (BS 500G) · airframe 24,232 hrs · 9,443 cycles

FWD CARGO PIT RT BAFFEL AT BS 500G RBL 21 BELOW RT ZEE CHANNEL IS CRACKED. BAFFEL AT RT FWD CARGO PIT AT BS 500G RBL 21 REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 53-30-53 FIG 2 AND 51-40-02.

Part: SILL — CORRODED (BS 500A-500L) · corrosion level 2 · airframe 24,232 hrs · 9,443 cycles

FWD CARGO PIT RT SIDE STA 500A TO STA 500L DUST SILL HAS CORROSION ON TOP SURFACE FWD CARGO PIT RT SIDE STA 500F + 6 TO 500L. DUST SILL REPLACED IAW B737 900 SRM 53-00-53 FIG 202 REPAIR 5.

Part: INTERCOSTAL — CRACKED (BS 460-480) · airframe 24,232 hrs · 9,443 cycles

FWD PIT RT INTERCOSTAL BS 460 TO BS 480 FOUND CRACKED. CRACK ON INTERCOSTAL AT FWD PIT BS 460, 480 REPAIRED IAW B737 900 SRM 51-70-11 FIG 201.

Part: FLOORBEAM — CORRODED (BS 787 S26L/R) · airframe 24,232 hrs · 9,443 cycles

AFT CARGO BAY TEE FITTING IS CORRODED AT BS 787 RBL 17 LBL 17. AFT CARGO PIT -TEE- AT BS 787 LBL 17 TO RBL 17 WAS REPLACED WITH MADE REPAIR PART IAW B737 900 SRM 51-40-02.

Part: WIRE HARNESS — SHORTED (DOOR LOCK) · airframe 23,303 hrs · 9,016 cycles

DURING CRUISE AT FL 350 VHF COM NR 2 & VHF NAV NR 1 AND ADF NR 2 PANEL DISPLAYS WERE ALL ILLUM'D FULL BRIGHT WITH ALLIED LIGHTS FLASHING. CARGO FIRE DETECTION PANEL LIGHTS ALL ILLUM'D FULL BRIGHT FLIGHT DECK DOOR ANNUNCIATOR LIGHTS ILLUM'D STEADY. SHORTLY AFTER AN ACRID ELECTRICAL SMELL FILLED THE COCKPIT. DURING THE COURSE OF DIVERSION THE ODOR WAS NOTICEABLE IN THE CABIN, BUT TO A LESSER DEGREE. INSP WIRE BUNDLE IN P8 AISLE CNTL STAND, NO DEFECTS NOTED. FOUND COCKPIT DOOR LOCK LIGHT PNL SHORTED. REPLACED PANEL. OP CHECKS GOOD. REF EO5250 01062. REF MM 27-41-00, ALL DISPLAYS TEST NORMAL WITH MASTER DIM & TEST.

Part: SKIN — DENTED (CARGO DOOR) · airframe 18,874 hrs · 7,106 cycles

AFT CARGO DOOR DENTED 24 IN AND 27 IN FROM AFT EDGE AND 15 IN FROM TOP EDGE. REPAIRED IAW SRM 52 00 01 REPAIR Z AND REPAIR 3.

Part: ROLLER — LOOSE (COCKPIT WINDOW)

SEA - DURING LINE MAINTENANCE, THE CAPTAINS SLIDING WINDOW HARD TO CLOSE. TIGHTENED AFT ROLLER. SLIDING WINDOW OPERATES NORMALLY. (M)

Part: STRINGER — DENTED (FUSELAGE)

SEA - DURING C-CHECK, FOUND STRINGER 19L DENTED. REPAIRED STRINGER PER SRM 53-00-03. (M)

Part: GUIDE — DEFECTIVE (ENTRY DOOR)

SEA - DURING LINE MAINTENANCE, FOUND THE L1 DOOR HARD TO CLOSE. REPLACED GUIDE ARM. DOOR THEN FUNCTIONED PROPERLY. (M)

Part: CIRCUIT BREAKER — FAILED (CABIN SIDEWALL)

SEA - DURING PUSHBACK FROM GATE, LEFT SIDE FORE AND AFT EXTERNAL OVERWING EMERGENCY LIGHTS (WITHIN THE SINGLE LIGHT ASSEMBLY) ILLUMINATED, WITH A CORRESPONDING INDICATION ON COCKPIT ANNUNCIATOR PANEL. REPLACED ASSOCIATED POWER SUPPLY CIRCUIT BREAKER. LIGHTS THEN FUNCTIONED PROPERLY. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

SEA - DURING A LINE MAINTENANCE CHECK, THE AFT EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY. EXIT LIGHTS THEN OPERATED NORMALLY. (M)