N407NV

Part: SPAR CAP — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 56,460 hrs · 37,161 cycles

LT HORIZONTAL STAB UPPER REAR SPAR CAP/AFT BARREL NUT CORRODED. REPAIRED LT HORIZONTAL STAB UPPER REAR SPAR CAP AFT BARREL NUT HOLE IAW SRM 55-03 PARA 30 AND EA NR 16626 DATED 15 DEC 2016.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,330 hrs · 37,096 cycles

L1, R1, AND FWD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. OPS CHECKED GOOD IAW AMM 33-53-00."

Part: LIGHT — WRONG PART (CABIN) · airframe 55,708 hrs · 36,694 cycles

IN FLIGHT, PAX IN 21A TURNED ON PSU LIGHT, PAX REPORT TO F/A ODOR OF BURNING AND SIGN OF SMOKE VISIBLE. SMOKE STOPPED, F/A CONFIRMED ODOR OF SMOKE. ELECTRICAL ODOR AFTER LIGHT WAS OFF. NO MORE SIGN OF SMOKE OR ODOR, DEFERRED ROW 21A, B IAW MEL 25-10 SIT1 DMI 27523 C/W M-PROCEDURE INOPERATIVE, PLACARD INSTALLED. PERFORMED OF READING LIGHT OPS CHECK, NO SIGN OF SMOKE OR BURNING ODOR. ACFT OK FOR SERVICE IAW AMM 33-21-06. FOUND WRONG PN BULBS INSTALLED FOR READING LIGHTS ON PSU AT 21AC, RELAMPED READING LIGHTS IAW AMM 33-22-00 AND OPS CHECK GOOD. REMOVED PSU, INSPECTED, REINSTALLED, NO DEFECTS NOTED. THIS CLEARS MEL 25-10 SIT1, DMI 27523, INOPERATIVE PLACARDS REMOVED AND C/W REINSPECT IAW GMM 21-2-4-7, NO DEFECTS NOTED.

Part: SUPPORT FRAME — CRACKED (FUSELAGE) · airframe 55,572 hrs · 36,620 cycles

FOUND TWO EACH CRACKS IN SUPPORT FRAME AT STATION 1437 LT, LONGERON L7 - L2.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,482 hrs · 36,568 cycles

SLIDE PACK OUT ON JET BRIDGE. RE-STOWED L1 DOOR SLIDE IAW AMM 25-62-00-2-0.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,647 hrs · 36,159 cycles

LEFT OVERWING EMER LAMP INOPERATIVE. RELAMPED LIGHT IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 54,530 hrs · 36,104 cycles

AFT EMER FLASHLIGHT INOPERATIVE. R & R AFT EMER FLASHLIGHT IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 54,431 hrs · 36,052 cycles

ON CLIMB OUT AT APPROX 28000FT, THE NOSE GEAR LIGHT CAME ON. IT WENT OUT AFTER A LIGHT KNOCK BELOW THE FLIGHT DECK WAS HEARD. THE HYDS WERE NORMAL FOR QTY. QRH 32.9 WAS CONSULTED, BUT NOT PERFORMED DUE TO THE LIGHT GOING OUT. REF WO 268973 NLG UNSAFE LIGHT WAS TROUBLE SHOT, PERFORMED IAW MM 32-60-00 & 32-30-00. ALL ISSUES NOTED & CORRECTED IAW MM 32-60-05 & SWPM 20-31-00. ACFT RETURNED TO SERVICE WITH MX CRTL CONCURRENCE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,390 hrs · 36,032 cycles

L2 DOOR & AFT DOOR EMER EXIT DOOR IDENTIFIER LIGHTED SIGNS INOPERATIVE. R & R BATTERY PACK FOR AFT SECTION OF EMER LIGHT AT ROW 34 DEF IAW AMM 33-53-00. OPERATIONS TESTED GOOD.

Part: BOLT — DAMAGED (LT ELEVATOR) · airframe 54,390 hrs · 36,032 cycles

DURING TAKEOFF ROLL CTR GRAVITY 10.47, FLAP 4 AT APPROX 120 KTS, THE NOSE STARTED TO COME UP. PILOT PUSHED YOKE FWD TO FULL FWD & NOSE STILL CAME UP, TAKEOFF ABORTED. REMOVED LT ELEVATOR ACTUATOR FOM. INSTALLED LT ELEVATOR ACTUATOR IAW AMM 27-30-08. SEE LOG PAGE 596314 FOR OPERATIONS & LEAK CHECK. WHILE REMOVING LT ELEVATOR HINGE BOLT TO FOM BOLT WAS DAMAGED. REINSTALLED BOLT IAW ERO 5520-002 REVA REINSPECT DUE AT NEXT A CHECK.

Part: ACTUATOR — DEFECTIVE (LT ELEVATOR) · airframe 54,390 hrs · 36,032 cycles

DURING TAKEOFF ROLL CG 10.47, FLAP 4 AT APPROX 120 KTS, THE NOSE STARTED TO COME UP. PILOT PUSHED YOKE FWD TO FULL FWD & NOSE STILL CAME UP, TAKEOFF ABORTED. ADDITIONAL CORRECTIVE ACTION INFO FOR CONTROL NR WX0A2015081972822. FOUND MISSING COTTER PIN FROM LT ELEVATOR BOOST CYLINDER TO CONTROL TAB. REMOVED LT ELEVATOR ACTUATOR & INSTALLED LT ELEVATOR ACTUATOR IAW AMM 27-30-08.

Part: BEAM — CORRODED (FUSELAGE) · airframe 53,899 hrs · 35,816 cycles

AFT CARGO DOOR CUT OUT LOWER JAMB BEAM CORRODED IN NUMEROUS AREAS BETWEEN STATION 1155 & 1212. ACCOMPLISHED BLEND OUT, LOCATED, DRILLED & INSTALLED A TITANIUM REPAIR DOUBLER IAW SRM 53-05 FIG 123 OPTION 1. WORK ACCOMPLISHED ON WO 251582 M301 ITEM 297 & WO 1011806-8300-0037.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,899 hrs · 35,816 cycles

LOWER EXTERNAL FUSELAGE SKIN CORRODED AT STATION 807, LONGERON 29R. ACCOMPLISHED BLEND OUT REPAIR, LOCATED DRILLED & INSTALLED EXTERNAL DOUBLER BETWEEN LONGERON 28R & LONGERON 30, STATION 807 IAW EA 05-2015-024. WORK ACCOMPLISHED ON WO 251582 M301 ITEM 161, WO 1011806-1000-0022, TOTAL TIME 53898.7 TOTAL CYCLES 35816.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,899 hrs · 35,816 cycles

NOSE LANDING GEAR BAY RT AFT DOORS, THE FUSELAGE SKIN IS CRACKED AT AFT HINGE AREA AT STATION 94.55 & R 28 POSITION. REPAIRED IAW SRM 53-O5 FIG-158. DOUBLER LENGTH 19"", WIDTH 5.5 & DEPTH .071. WORK ACCOMPLISHED ON WO 1011806-1200-0081 M301 ITEM 430.

Part: PAN — CRACKED (FUSELAGE) · airframe 53,899 hrs · 35,816 cycles

LOG PAGE 251582 ITEM 199 LEFT WINDOW RING PAN CRACKED AT FS 855. REPAIRED RING PAN IAW SRM 53-05 FIG 122.

Part: DIAPHRAGM — CORRODED (FUSELAGE) · airframe 53,899 hrs · 35,816 cycles

LOG PAGE 251582 ITEM 312 CABIN FLOOR DIAPHRAGM, WEB, PUNCTURED WITH CORROSION. REPAIRED DIAPHRAGM, WEB, IAW SRM 51-70-4 FIG 2.

Part: HYDRAULIC LINE — LOOSE (HYDRAULIC SYS) · airframe 53,867 hrs · 35,800 cycles

DURING APPROACH RECEIVED RT HYD PRESS LOW ANNUNCIATOR. RT HYD QTY INDICATES 2 QTS, FOUND FLUID LEAKING FROM TAIL SECTION OF THE ACFT. FOUND HYD LINE RT SIDE TAIL SECTION B NUT LINE TO RUDDER PRESS GAUGE VIBRATED LOOSE. TIGHTENED HYD LINE RT SIDE RUDDER PRESS GAUGE LINE. SERVICED HYD & PERFORMED LEAK CHECK, NO LEAKS NOTED AT THIS TIME IAW AMM 20-30-02-2 & 12-13-01-3-00 04 30 2015. FOUND PLUG ON RUDDER HYD POWER SOV LEAKING. REPLACED O RING. OPERATIONS LEAK CHECKED GOOD IAW AMM 27-20-09.

Part: SKIN — DENTED (RT WING)

THERE IS A SMALL DENT ON THE LE OF THE RT WING INBD OF THE VORTILLON & DENTS PRESENT ON ACFT DAMAGE LOG ID 47, 48, & 49.

Part: COWLING — DAMAGED (RT ENGINE)

RIGHT ENG UPPER COWL DAMAGED FROM APU EXHAUST. R & R RT ENG UPPER COWL IAW AMM 71-10-03.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 53,577 hrs · 35,665 cycles

JUST AFTER TAKEOFF PRESSURIZATION TRANSFER LOCKOUT & STANDBY ON LIGHT ILLUMINATED & CABIN WAS NOT PRESSURIZING. COMPLETED QRH 21.9, COMPLETED FLIGHT ON REMAINING CONTROLLER. R & R NR ! CABIN PRESS CONTROLLER. GND OPERATIONS CHECKED GOOD IAW AMM 21-32-03, 21-32-11 & 34-11-00.

Part: OXYGEN BOTTLE — DEFECTIVE (CABIN) · airframe 52,812 hrs · 35,283 cycles

AFT FLIGHT ATTENDANT O2 BOTTLE VLV DISASSEMBLED. R & R AFT FLIGHT ATTENDANT O2 BOTTLE & RECONNECTED MASK IAW AMM 25-60-00.

Part: SLIDE — DEPLOYED (SERVICE DOOR)

SERVICE DOOR R1 SLIDE DEPLOYED. INSTALLED R1 DOOR SLIDE IAW AMM 25-62-00 JOB CARD R0902502 SB 304-25-26.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R BATTERY PACK AND OPS CHECKED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SKIN — DAMAGED (ENTRY DOOR)

AFT ENTRY DOOR AFT LOWER RIGHT AFT CORNER DAMAGED. TRIMMED OUT DAMAGED AREAS. HFEC INSPECTED AREAS NO CRACKS NOTED IAW NDTSPM 06-10-01.001. FABRICATED, LOCATED, DRILLED AND INSTALLED DOUBLER AND REPAIR PARTS IAW STS EA 10-2012-184.

Part: SKIN — DAMAGED (FUSELAGE)

UPPER FUSELAGE LIGHTING STRIKE STA 1276 BETWEEN LONGERON 2L & 3L. REMOVED DAMAGE AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW MD80 SRM 53-04-2 FIG 2.

Part: LONGERON — CRACKED (FUSELAGE)

RIGHT W/W LONGERON 20 CRACKED IN RADIUS 1 1/2 INCH LENGTH. CUT OUT DAMAGED AREA HFEC INSPECTED NO CRACK NOTED IAW NDTSPM 6-10-01-001. FABRICATED REPAIR PARTS LOCATED, DRILLED, AND INSTALLED IAW MD80 SRM 53-02 FIG 22.

Part: FRAME — CRACKED (RT MLG)

RIGHT MLG O/B FRAME CRACKED AT FWD CORNER. FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR DOUBLER IAW MD-80 SRM 52-05 FIG 59.

Part: BATTERY — DISCHARGED (CABIN)

IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN POWER SUPPLY BATTERY PACK AN OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE EMERGENCY EXIT LIGHT ASSY AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BALLAST — DEFECTIVE (LAVATORY)

FLIGHT CREW PERSONNEL REPORTED, HOT ELECTRICAL ODOR FROM FRONT LAV. MAINTENANCE DEPARTMENT PERSONNEL FOUND SMELL COMING FROM P4-32 BALLAST. REMOVED AND REPLACED LIGHT BALLAST, OPERATIONAL CHECK OF SYSTEM NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CABIN SEAT TRACK CORRODED AT GALLEY MPUNTING AREA STA 204 RBL 44. REMOVED DAMAGED SECTION TO PREVIOUS SPLICE AT STA 266, FABRICATED, LOCATED DRILLED AND INSTALLED NEW SECTION IAW MD 80 SRM 53-05 FIG 4F.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT CREW REPORTED WISPY SMOKE AND DIESEL SMELL AROUND ROW 6. MAINTENANCE DEPARTMENT PERSONNEL FOLLOWED TABLE 107 IN AMM 21-20-00. UNABLE TO LOCATE SOURCE OF ODOR / SMOKE. OPERATED AIR CONDITIONING PACKS IAW AMM 21-00-00, UNABLE TO DUPLICATE. REMOVED FORWARD PIT PANELS, NO DEFECTS NOTED, IAW AMM 25-52-01. AIRCRAFT RETURNED TO SERVICE.

Part: APU — MALFUNCTIONED (APU BAY)

FLIGHT CREW REPORTED WHILE TAXING TO GATE AFTER LANDING IN SGF AND SWITCHING AIR CONDITIONING PACK TO THE APU THE CABIN FILLED WITH HAZE AND STENCH. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE APU ASSY, IAW ALLEGIANT AIR TASK CARD R0594902. SYSTEM OPS CHECKS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: ENGINE — FAILED (NR 2)

SEIZURE OF THE NR 2 (RIGHT) ENGINE AT 1200FT. PERFORMED EQRH, TRIED TO RELIGHT WITH NO SUCCESS. SECURED THE ENGINE AND LANDED AT FLL. MAINTENANCE DEPARTMENT PERSONNEL PERFORMED ALLEGIANT AIR TASK CARD R0807101, MD80, JT8D ENGINE REMOVAL AND REPLACEMENT. OK FOR CONTINUED SERVICE.

Part: SKIN — DENTED (BS 215)

DURING SCHEDULED INSP, FOUND DENT OF FUSELAGE SKIN AT FS 215, BELOW LONGERON 15R.

Part: SKIN — DENTED (NLG DOOR)

S/O NR 193034 N/R 44359- DURING SCHEDULED INSPECTION, FOUND LT NOSE W/W DOOR HAS A DENT IN INTERNAL SKIN.

Part: SKIN — DENTED (BS 674)

DURING SCHEDULED INSP, FOUND EXISTING DENT RT FUSELAGE SKIN AT FS 674, L-29R - L-30 TO BE WITHIN 1 INCH OF RIVET CENTER LINE.

Part: SKIN — DENTED (BS 632)

DURING SCHEDULED INSP, FOUND EXISTING DENT RT FUSELAGE SKIN AT FS 632, L-28R - L-30 TO BE WITHIN 1 INCH OF RIVET CENTER LINE.

Part: SEAT TRACK — CORRODED (BS 712)

S/O NR 193034N N/R43800 - DURING SCHEDULED INSPECTION, FOUND CORROSION IN MID CARGO COMPARTMENT AT LT FS 712 SUPPORT AT TRACK LOCATION.

Part: TRACK — CORRODED (BS 1007-1212)

DURING SCHEDULED INSPECTION, FOUND LT FWD TRANSITION TRACK HAD CORROSION FROM FS 1007 TO FS 1212 (AROUND NUT PLATE HOLES, AND AT ATTACH POINTS).

Part: SKIN — UNKNOWN (BS 469)

S/O NR 193034, N/R 44304 - DURING SCHEDULED INSPECTION, FOUND LIGHTNING STRIKE AT FS 469 L-26R - L-27R.

Part: SKIN — DENTED (BS 559)

S/O NR 193034, N/R 44334 - DURING SCHEDULED INSPECTION, FOUND DENT ON RT FUSELAGE AT FS 559 L-25R-L-26R FOUND TO BE WITHIN 1 INCH OF RIVET CENTERLINE.

Part: THRESHOLD — CORRODED (ZONE 100)

S/O NR193034 NR 43825 - DURING SCHEDULED INSPECTION, FOUND AFT CARGO COMPARTMENT THRESHOLD HAS AREA OF CORROSION.

Part: TRACK — CORRODED (CARGO BAY)

DURING SCHEDULED INSPECTION, FOUND RT FWD TRANSITION TRACK HAD CORROSION FROM FS 1079 TO FS 1155 (AROUND NUT PLATE HOLES, INSIDE TRACK AND STEP DOWN ANGLE ATTACHED TO AFT END OF TRACK).

Part: SKIN — DENTED (BS 221-226)

S/O 193034 NR 44270 - DURING SCHEDULED INSPECTION, FOUND MULTIPLE DENTS LT UPPER FUSELAGE AT FS 221-226.5, L-4L.

Part: SKIN — DENTED (BS 146)

S/O NR 193034 NR 44297 - DURING SCHEDULED INSPECTION, FOUND EXISTING DENT AT FS 146, L-18L IS WITHIN 1 INCH OF INTERNAL DOUBLER, WITH SHARP CREASE.

Part: SKIN — DENTED (BS 530)

S/O NR 193034 SN 44327 DURING SCHEDULED INSPECTION, FOUND DENT ON RT FUSELAGE AT FS 530, L-24R - L-25R FOUND TO BE WITHIN 1 INCH OF RIVET CENTER LINE.

Part: SKIN — DENTED (BS 120 L23L)

DURING SCHEDULED INSP, FOUND PREVIOUSLY REPORTED AT FS 120, L-23L OUT OF LIMITS IAW SRM 53-04 FIG. 38, SHT. 13, CONDITION 3, D/X = 2.94 AND .720 INCH FROM INTERNAL STRUCTURE.

Part: SKIN — DENTED (BS 503)

S/O NR 193034 SN 44337 DURING SCHEDULED INSPECTION, FOUND EXISTING DENT RT FUSELAGE AT FS 503, L-24R - L-25R FOUND TO BE WITHIN 1 INCH OF RIVET CENTER LINE.

Part: SKIN — DENTED (BS 579)

S/O NR 193034, NR 44335 - DURING SCHEDULED INSPECTION, FOUND DENT ON RT EXTERIOR AT FS 579, L-26R - L-27R FOUND TO BE WITHIN 1 INCH OF RIVET.

Part: SKIN — DENTED (L1 DOOR)

S/O NR 193034 SN 44296 DURING SCHEDULED INSPECTION, FOUND DENT ON L-1 DOOR SKIN AT FS 195, L-9L.

Part: SKIN — DENTED (BS 246)

DURING SCHEDULED INSP, FOUND PREVIOUSLY REPORTED DENT AT FS 246.5, L-22R - L-23R IS CREASED, OUT OF LIMITS IAW SRM 53-04 FIG. 38, SHT. 13, CONDITION 3.

Part: STRUCTURE — DAMAGED (RT ELEVATOR)

S/O NR 193034, NR 44285, DURING SCHEDULED INSPECTION, FOUND TORN METAL WITH POSSIBLE LIGHTNING STRIKE DAMAGE ON RT ELEVATOR LOWER SURFACE TOP CAP AT T/E AND OTBD AFT EDGE WITH RIVETS BROKEN LOOSE ON UPPER SIDE.

Part: SKIN — DENTED (BS 211 L15L)

DURING SCHEDULED INSP, FOUND DENT NEXT TO L-15L AT FS 211.5 OUT OF LIMITS DUE TO BEING CLOSE TO LONGERON.

Part: SKIN — DAMAGED (BS 317)

S/O NR 193034 NR 44260, DURING SCHEDULED INSPECTION, FOUND CREASE AT FS 317, LONGERON 29R.

Part: CUSP WEB — CORRODED (BS 646)

S/O 193034, N/R 44180, DURING SCHEDULED INSPECTION, FOUND LT CABIN CUSP WEB HAS CORROSION AT FS 646.

Part: SKIN — CHAFED (CARGO DOOR)

S/O 193034 NR 43687 - DURING SCHEDULED INSPECTION, FOUND C-1 CARGO DOOR EXTERNAL SKIN LOWER FWD AND AFT AREA HAS WEAR (CHAFE).