N617AS

Part: RIB — CHAFED (TE FLAP) · airframe 43,680 hrs · 19,450 cycles

HARDWARE LOOSE ON UPPER FIXED T/E PANEL BETWEEN INBD AND OTBD FLAPS. REPAIRED RT WING DEFLECTION CONTROL RIB ASSY IAW EA 700-57, EA 09381.

Part: TRANSITION PANEL — CORRODED (BS 677-767) · corrosion level 2 · airframe 43,680 hrs · 19,540 cycles

AFT CARGO BAY RT TRANSITION PANEL CORRODED AT FASTENER LOCATIONS BS 677 TO 767. BLENDED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, REPAIR IAW SRM IAW SRM 53-00-53, REPAIR 5.

Part: TRANSITION PANEL — CORRODED (BS 707-757) · corrosion level 2 · airframe 43,680 hrs · 19,450 cycles

AFT CARGO BAY LEFT TRANSITION PANEL CORRODED AT FASTENER LOCATIONS FS 707 - 757. ACFT GROUNDED. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, REPAIR IAW SRM IAW SRM 53-00-53, REPAIR 5.

Part: TRANSITION PANEL — CORRODED (BS 767) · corrosion level 2 · airframe 43,680 hrs · 19,540 cycles

AFT CARGO BAY LT TRANSITION PANEL CORRODED AT FS 767.0 BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 REPAIR IAW SRM IAW SRM 53-00-53, REPAIR 5.

Part: TRANSITION PANEL — CORRODED (BS 707-757) · corrosion level 2 · airframe 43,680 hrs · 19,540 cycles

AFT CARGO BAY LT TRANSITION PANEL CORRODED AT FASTENER LOCATIONS BS 707 - 757. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, REPAIRED IAW SRM IAW SRM 53-00-53 REPAIR 5.

Part: UNKNOWN — ODOR (CABIN) · airframe 42,705 hrs · 18,988 cycles

AFTER TAKEOFF, F/A REPORTED SMOKE IN CABIN. NO SMOKE OBSERVED ON FLIGHT DECK. ODOR WAS LIKE DIRTY SOCKS. ISOLATED ODOR TO MOTOR. REPLACED RECIRCULATION FAN FILTER. ACCOMPLISHED OIL CONTAMINATION REMOVAL FROM AIR CONDITIONING & PNEUMATIC SYS, TASK 21-00-01-100-801. OPS CHECKED NORMAL. NO DEFECTS NOTED. ODOR WAS ASSOCIATED WITH BORESCOPE PLUG PENETRANT OIL.

Part: FITTING — GOUGED (CARGO BAY) · airframe 41,492 hrs · 22,802 cycles

FWD PIT CAP STRIP CLIP AT BS 500A IS DAMAGED. REMOVED DAMAGED CLIP FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 05 51 40 02 51 30 01 51 20 01 51 70 01 AND BOEING SOPM 20 41 02.

Part: FRAME — WORN (FUSELAGE) · airframe 37,714 hrs · 16,640 cycles

FRAME WORN OUT OF LIMITS BS 654 - BS-674. REMOVED AND REPLACED FRAME IAW BOEING DRAWING 149A7214.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 37,714 hrs · 16,640 cycles

HORIZONTAL STIFFENER CRACKED FORWARD SIDE OF BS 663.75 VAPOR BARRIER ABOVE ACM EXHAUST DUCT. REMOVED AND REPLACED STIFFENER IAW B737 700 SRM 51 40 02.

Part: FRAME — WORN (FUSELAGE) · airframe 37,714 hrs · 16,640 cycles

BELLY OF A/C LEFT SIDE OF KEEL BEAM APPROX STA 650 AT WHEEL WELL CUTOUT LOWER PANEL ATTACH POINT WORN. REMOVED AND REPLACED FRAME IAW B737 700 SRM 53 40 71.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 37,714 hrs · 16,640 cycles

MAIN CABIN FLOOR SUPPORT BRACKET BROKEN AT LBL 1 BS 540. REPAIRED SUPPORT IAW B737 700 SRM 51 70 11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,714 hrs · 16,640 cycles

MAIN CABIN FLOOR INTERCOSTAL CRACKED AT LBL 45 BS 332 - BS 342. REMOVED AND REPLACED INTERCOSTAL IAW B737 700 SRM 51 40 02 AND BOEING DRAWING 141A5400.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,714 hrs · 16,640 cycles

MAIN CABIN FLOOR INTERCOSTAL CRACKED AT LBL 11 BS 344 BS 360. REMOVED AND REPLACED INTERCOSTAL IAW B737 700 SRM 51 40 02 AND BOEING DRAWING 141A5400.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,714 hrs · 16,640 cycles

MAIN CABIN FLOOR INTERCOSTAL CRACKED AT LBL 45 BS 310 - BS 322. REMOVED AND REPLACED INTERCOSTAL IAW B737 700 SRM 51 40 02 AND BOEING DRAWING 141A5400.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,714 hrs · 16,640 cycles

MAIN CABIN FLOOR INTERCOSTAL CRACKED AT BS 310 - BS 322. REMOVED AND REPLACED INTERCOSTAL IAW B737 700 SRM 51 40 02 AND BOEING DRAWING 141A5400.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,714 hrs · 16,640 cycles

MAIN CABIN INTERCOSTAL CRACKED AT BL 0 BS 344 BS 360. REMOVED AND REPLACED INTERCOSTAL IAW B737 700 SRM 51 40 02 AND BOEING DRAWING 141A5400.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,714 hrs · 16,640 cycles

MAIN CABIN FLOOR STRUCTURE CORRODED AFT SECTION BETWEEN BS 1006 AND BS 1016. REMOVED AND REPLACED SUPPORT IAW BOEING DRAWING 147A5710.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,714 hrs · 16,640 cycles

MAIN CABIN FLOORBEAM CORRODED BS 986.5 LBL 30. REPAIRED FLOORBEAM IAW B737 700 SRM 53 00 51 REPAIR 1 FIG 203.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,714 hrs · 16,640 cycles

MAIN CABIN FLOOR SUPPORT CORRODED BS 992.8 RBL 40. REMOVED AND REPLACED SUPPORT.

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 37,692 hrs · 16,633 cycles

HIGH PRESSURE DOOR (92 UPPER STOP PAD WORN INTO CHORD). REPAIRED DAMAGE.

Part: STOP FITTING — DAMAGED (FUSELAGE) · airframe 37,683 hrs · 16,628 cycles

HIGH PRESSURE DOOR 192DR UPPER STOP PAD WORN INTO CHORD REMOVED LOWER SEAL. REMOVED DAMAGED STOP PAD. MEASURED CHORD DAMAGE. CHORD IS .125 INCH THICK CHORD WEAR IS .25" DIA. X .021" DEEP. CHORD DAMAGE IS OUT OF LIMITS OF SRM 53 30 71 AD1 FIG 105C. REPAIRED WORN CHORD AS PER EA 700 53EA 04417 RE-INSTALLED SEA AS PER SRM 51 40 02.

Part: TAB — BENT (LIGHT HOUSING) · airframe 33,447 hrs · 14,720 cycles

ROW 6 RT PROX LIGHT INOP. FOUND BENT GROUND TAB SHORTING TO CENTER TAB CAUSING FUSE F4 AT M1647 TO BLOW, LIGHT ASSY AT ROW 6 RT I L1065. REMOVED AND REPLACED LIGHT ASSY HOUSING, REPLACED FUSE, OPS CHECKS GOOD.

Part: PAN — CRACKED (FUSELAGE) · airframe 33,447 hrs · 14,720 cycles

R2 DOOR LOWER LINER SUPPORT PAN AFT SUPPORT CRACKED, OUT OF LIMITS. REMOVED AND REPLACED WITH NEW.

Part: SKIN — DENTED · airframe 33,447 hrs · 14,720 cycles

DENT IN RVSM AREA LT SIDE BS 3951, 5 INCHES ABOVE STR 17L. INSTALLED REPAIR DOUBLER IAW ASA EA.

Part: PLATE — GOUGED (TE FLAP) · airframe 33,447 hrs · 14,720 cycles

RIGHT I/B MAIN FLAP I/B AFT FLAP PROGRAMMING TRACK CLOSE OUT PLATE IS GOUGED BEYOND SRM LIMITS. REMOVED AND REPLACED WITH NEW.

Part: SKIN — CHAFED (LE SLAT) · airframe 33,447 hrs · 14,720 cycles

NR 8 SLAT T/E WEDGE LOWER SURFACE HAS AREAS OF CHAFES AT T/E OUT OF LIMITS PER SRM.

Part: SKIN — CHAFED (LE SLAT) · airframe 33,447 hrs · 14,720 cycles

NR 6 SLAT T/E WEDGE LOWER SURFACE HAS AREAS OF CHAFES OUT OF LIMITS PER SRM. REPAIRED PER EA.

Part: SKIN — CHAFED (LE SLAT) · airframe 33,447 hrs · 14,720 cycles

NR 7 SLAT T/E WEDGE LOWER SURFACE HAS AREAS OF CHAFES AT T/E OUT OF LIMITS PER SRM. REPAIRED PER EA ALODINE, PRIME, PAINT.

Part: ANGLE — CHAFED (LT WING TE FLAP) · airframe 33,447 hrs · 14,720 cycles

LEFT I/B MAIN FLAP I/B AFT FLAP TRACK CLOSE OUT ANGLE IS CHAFED BEYOND SRM LIMITS. REMOVED AND REPLACED WITH NEW.

Part: ANGLE — CRACKED (LT WING) · airframe 33,447 hrs · 14,720 cycles

LT WING UPPER T/E PANEL CTR SUPPORT RIB OB ATTACH ANGLE TO DEFLECTION RIB IS CRACKED. REMOVED AND REPLACED

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 33,447 hrs · 14,720 cycles

LT WING UPPER T/E PANEL SUPPORT ANGLE CRACKED OUT OF LIMITS. REMOVED AND REPLACED WITH NEW.

Part: SKIN — CHAFED (LE SLOT) · airframe 33,447 hrs · 14,720 cycles

NR 5 SLOT T/E WEDGE LOWER SURFACE HAS AREAS OF CHAFING. REPAIRED PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 33,447 hrs · 14,720 cycles

LT H STAB SURFACE SKIN HAS EVIDENCE OF A CRACK LOCATED 72 DU FM IB END 17IN FROM AFT EDGE OF STAB LE SKIN. STEP DRILLED CRACKED INSTALLED REPAIR DOUBLER.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 33,447 hrs · 14,720 cycles

RT WING RSS 289 RIB VERTICAL SUPPORT ANGLE FOR COVE SEAL IS CRACKED ON FWD SIDE. REMOVED AND REPLACED VERTICAL SUPPORT ANGLE.

Part: BUTTON — FAILED (R1 DOOR) · airframe 30,888 hrs · 13,379 cycles

CATERER UNABLE TO CLOSE R1 DOOR. REMOVED & REPLACED GALLEY SERVICE (R1) DOOR RELEASE BUTTON ASSY IAW MM 52 41 21.

Part: WEB — CORRODED (BS 847-867) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON WEB RBL 20 BS 847 TO 867 REPAIRED WITH REPAIR PART.

Part: FLOOR SUPPORT — CORRODED (BS 727-847) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON FLOOR SUPPORT ZEE CHANNEL AT LBL 22 BS 727+4 847, REPAIRED WITH REPAIR PART.

Part: SHIELD — CORRODED (BS 767-794) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON WEB RBL 20 BS 767 TO 794.3 REPAIRED WITH REPAIR PART.

Part: CARGO TRACK — CORRODED (BS 747) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON CARGO TIE DOWN TRACK BS 747 RBL I5 REPAIRED WITH REPAIR PART.

Part: PLATE — CORRODED (BS 867) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT AFT TIEDOWN SCUFF PLATE BS 867 CORRODED REPAIRED WITH REPAIR PART.

Part: CARGO TRACK — CORRODED (BS 767) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON FLOOR SUPPORT RAIL BS 767+6 LBL 3 REPAIRED WITH MADE REPAIR PARTS.

Part: CARGO TRACK — CORRODED (BS 767-847) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO CORROSION ON CARGO TIEDOWN TRACK RBL 13.84 BS 767 TO 847 TIE DOWN TRACK REPLACED WITH REPAIR PART.

Part: WEB — CORRODED (BS 794-847) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON WEB UPPER FLANGE UNDER ANCHOR NUTS AT RBL 20 BETWEEN BS 847 AND 794. REPLACED WITH MADE REPAIR PART IAW BOEING ENG DWG 146AB123 AND B737 700 SRM 51 30 01 51 40 05 AND 51 40 02.

Part: WEB — CORRODED (BS 794-847) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON WEB RBL 25 794.3 TO 847 REPLACED WITH MADE REPAIR PART IAW BOEING ENG DWG 146A 8120 AND B737 700 SRM 51 40 05 AND 51 40 02.

Part: FLOOR SUPPORT — CORRODED (BS 727-767) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON FLOOR SUPPORT ZEE CHANNEL RBL 22 BS 727+4 TO 767 ZEE CHANNEL REPLACED.

Part: CARGO TRACK — CORRODED (BS 767) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON FLOOR SUPPORT RAIL AT EXISTING REPAIR BS 767 + 8 RBL 8 FLOOR SUPPORT RAIL REPLACED.

Part: CHANNEL — CORRODED (BS 438-500D) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

FWD CARGO PIT LT ZEE CHANNEL BS 500D TO 438 LBL 21 REPLACED CORRODED SECTION FROM BS 438 TO 500D WITH MADE REPAIR PART IAW B737 700 SRM 53 00 53 REPAIR E FIG 202.

Part: FLOOR PANEL — CORRODED (BS 727D) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT FLOOR PANEL SPLICE TEE BS 727D+6 CORRODED SPLICE TEE REPLACED.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 28,334 hrs · 12,273 cycles

RT HORIZONTAL STAB L E STA 46.00 DENTED REPAIRED CUT OUT FILM AND DOUBLER.

Part: FLOOR PANEL — CORRODED (BS 767) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT FLOOR PANEL SPLICE TEE CORRODED BS 767+6 SPLICE TEE REPLACED.

Part: FLOOR PANEL — CORRODED (BS 887) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT FLOOR PANEL SPLICE TEE CORRODED BS 887 SPLICE TEE REPLACED.

Part: HOUSING — CRACKED (COLLISION LIGHT) · airframe 28,334 hrs · 12,273 cycles

UPPER FUSELAGE ANTI COLLISION LIGHT HOUSING SCREW HOLES CRACKED REPLACED UPPER FUSELAGE ANTI COLLISION LIGHT HOUSING WITH REPLACEMENT PART NR 30 2505 3 PO NR 113319 IAW B737 700 SRM 51 40 02.

Part: FLOOR SUPPORT — BROKEN (BS 540) · airframe 28,334 hrs · 12,273 cycles

FLOORBOARD SUPPORT CHANNEL BROKEN AT BS 540 WL 208 RBL 2. REPAIRED WITH REPAIR PART.

Part: FLOORBEAM — CORRODED (BS 344) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

CABIN FLOORBEAM BS 344 LBL 12 CORRODED REPAIRED WITH REPAIR PART.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 28,334 hrs · 12,273 cycles

FWD CABIN INTERCOSTAL CRACKED BS 312 TO 328 LBL 46. REPAIRED WITH REPAIR PART.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 28,334 hrs · 12,273 cycles

FWD CABIN INTERCOSTAL CRACKED BS 312 TO 328 RBL 31. REPAIRED WITH REPAIR PART.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 28,334 hrs · 12,273 cycles

FWD CABIN INTERCOSTAL CRACKED BS 328 TO 344 LBL 46, REPAIRED WITH REPAIR PART.

Part: INTERCOSTAL — CRACKED (BS 294-277) · airframe 28,334 hrs · 12,273 cycles

FWD CABIN INTERCOSTAL CRACKED BS 294 TO 277 BL 0. REPAIRED WITH REPAIR PART.

Part: CHANNEL — CORRODED (BS 992) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CABIN CORROSION FOUND ON ZEE CHANNEL BS 992 RBL 37, REPAIRED WITH REPAIR PART.

Part: SHEAR WEB — CORRODED (BS 1016) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CABIN CORROSION FOUND ON SHEAR WEB RBL 33 BS 1016+3. REPLACED WITH MADE REPAIR PART IAW BOEING ENG DWG 147A15712 AND B737 700 SRM 51 40 02.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CABIN CORROSION FOUND ON BS 947 FLOORBEAM LBL 53 AROUND CLIP NOT HOLE LOCATION REPAIRED WITH REPAIR PART.

Part: INTERCOSTAL — CORRODED (BS 947-967) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CABIN CORROSION FOUND ON INTERCOSTAL LBL 50 BS 947 TO 967. INTERCOSTAL REPLACED WITH NEW PART.

Part: SHEAR WEB — DENTED (BS 1016) · airframe 28,334 hrs · 12,273 cycles

AFT CABIN DENT FOUND ON SHEAR WEB AT RBL 33.5 BS 1016+5. REPLACED WITH MADE REPAIR PART FOR BOEING ENG DWG 147A5712 AND B737 700 SRM 51 40 02.

Part: FLOOR PANEL — CORRODED (BS 767-887) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT FLOOR PANEL FROM STA 767+6 TO 887 CORRODED ALONG PANEL EDGES AND CRACKED AT STA 792. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 60 53 KG1 AND 51 40 05 AND BOEING ENG DWG 453A2610.

Part: ANGLE — CORRODED (BS 500A-500D) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

FWD CARGO PIT ZEE ANGLE FOUND CORRODED AT BS 500A TO 500D RBL21 FWD CARGO PIT ZEE ANGLE BS 500D RBL21. REPAIRED IAW B737 700 SRM 53 30 53 AND SRM 53 00 53 REPAIR 5.

Part: FLOOR SUPPORT — CORRODED (BS 767) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

AFT CARGO PIT CORROSION ON FLOOR SUPPORT RAIL BS 767+6 LBL B REPAIRED WITH MADE REPAIR PART.

Part: FLOOR SUPPORT — CORRODED (BS 500-500A) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

CORROSION FOUND ON TOP AND BOTTOM OF FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL AT BS 500 TO BS 500A RBL 21.00. CORROSION BLENDED OUT AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW B737 700 SRM 53 00 53. MADE AND INSTALLED REPAIR PART IAW B737 200 SRM 51 40 05 AND 51 40 02.

Part: DOUBLER — CORRODED (BS 500-500A) · corrosion level 2 · airframe 28,334 hrs · 12,273 cycles

FWD CARGO PIT RADIO ANTENNA DOUBLER FOUND CORRODED AT BS 500 BS 500A BL 0, FWD CARGO RADIO ANTENNA DOUBLER REPLACED WITH REPAIR PART.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 24,454 hrs · 10,406 cycles

UPON GVI PER TC 78011000 FOUND LIGHTNING STRIKE ON FUSELAGE SKIN.

Part: SKIN — BENT (FS 490)

PAE - BELT LOADER CONTACTED AIRCRAFT FUSELAGE SKIN AT FORWARD CARGO DOOR CUTOUT AFT EDGE. CUT OUT DAMAGE AND INSTALLED REPAIR IAW SRM 53-00-01 NR 24. (M)

Part: SUPPORT — CORRODED (BS 767-787) · corrosion level 2

DURING MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 767. REPAIR IAW SRM. (K)

Part: FRAME — BENT (FS 800-787)

PAE - DURING MAINTENANCE CHECK, FOUND FORWARD FRAME CLOSURE WEB BENT, AFT CARGO DOOR CUT OUT. REPAIR IAW SRM 51-40-02. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, FOUND FLOOR TRACK LIGHT INOPERATIVE AT ROW 15C. REPLACED BATTERY PACK, OPS CHECKED GOOD. (M)

Part: STRAP — CORRODED (FLOOR PANEL)

OAK - DURING C-CHECK, FOUND FLOOR PANEL SUPPORT STRAP IS CORRODED AT FS 887. REPLACED STRAP PER MM 51-40-02. (M)

Part: ANGLE — CORRODED (FUSELAGE)

OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR Z-ANGLE. REPLACED WITH NEW 'Z' ANGLE PER SRM. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR TIE DOWN TRACK. SPLICE IN NEW SECTION PER SRM. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OAK - DURING MAINTENANCE C-CHECK, FOUND CORROSION ON FLOOR SUPPORT RAIL. SPLICED FLOOR SUPPORT RAIL PER SRM. (M)

Part: STRUCTURE — GOUGED (FUSELAGE)

SEA - DURING MAINTENANCE CHECK, A GOUGE WAS FOUND IN THE PNEUMATIC ACCESS DOOR SURROUND STRUCTURE. CLEANED UP GOUGE AND INSTALLED REPAIR STRAP PER EA5310-02109. (M)

Part: SKIN — DENTED (CARGO DOOR)

SEA - DURING MAINTENANCE CHECK, FOUND A DENT IN AFT CARGO DOOR. REPAIRED DENT WITH DOUBLER PER EA 5230-01176. (M)

Part: FIRE DETECTOR — MALFUNCTIONED (FWD CARGO BAY)

DURING CLIMB, THE FORWARD CARGO FIRE WARNING LIGHT CAME ON. PILOT FIRED FIRE EXTINGUISHER BOTTLE AND RETURNED TO AIRPORT. INSPECTED FORWARD CARGO COMPARTMENT, THERE WERE NO SIGNS OF A FIRE. DUST FROM A LIVE SHIPMENT OF BIRDS WAS THE LIKELY CAUSE OF THE FIRE WARNING. REPLACED THE FIRE EXTINGUISHER BOTTLE. PERFORMED SYSTEMS TESTS. NO PROBLEMS WERE NOTED.

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE MAINTENANCE, THE EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN ROWS 15 THROUGH 18. RE-CONNECTED THE TRACK LIGHT WIRES AT ROW 18. THE LIGHTS THEN OPERATED NORMALLY. (M)

Part: ROLLER — LACK OF LUBE (PAX DOOR)

PDX - PRIOR TO FLIGHT 313, THE FLIGHT ATTENDANT REPORTED THAT THE L1 DOOR HANDLE WOULD NOT UNLOCK. LUBRICATED DOOR ROLLERS AND THE DOOR OPERATED NORMALLY. (M)