N944AS

Part: FRAME — CRACKED (BS 1418 S2R) · airframe 54,831 hrs · 29,386 cycles

AFT ACCESSORY COMPT FRAME STA 1418 CRACKED AT LONGERON 2R. REMOVED DAMAGED SECTION OF FRAME LOCATED DRILLED AND INSTALLED A REPLACEMENT FRAME SECTION IAW MD 80 SRM 51-30-2 PG 1 AND 51-30-5 PG 1 AND ASA EA 5310 02749.

Part: LONGERON — CRACKED (BS 1407-1421 S2R) · airframe 54,831 hrs · 29,386 cycles

AFT ACCESSORY COMPT LONGERON 2R CRACKED JUST AFT OF 1418 FRAME. REMOVED DAMAGED SECTION OF LONGERON LOCATED DRILLED AND INSTALLED A REPLACEMENT SECTION AND REPAIR SPLICE IAW MD80 SRM 53-02 PG 50 AND 52.

Part: SKIN — DENTED (BS 311-323) · airframe 51,032 hrs · 27,560 cycles

FUSELAGE SKIN DENTED. REMOVED EXISTING INTERNAL REPAIR DOUBLER. MOVED DAMAGED SECTION OF FUSELAGE. INSTALLED EXTERNAL REPAIR DOUBLER TWO INTERNAL FINGER DOUBLERS AND TWO FILLERS PER SRM 53-04.

Part: SKIN — CHAFED (TE FLAP) · airframe 51,032 hrs · 27,560 cycles

LEFT WING OUTBOARD FLAP INBOARD VANE CHAFED ON EXISTING LEADING EDGE REPAIR DOUBLER AT INBOARD END. REMOVED EXISTING DOUBLER. INSTALLED REPAIR DOUBLER PER SRM 51-70-2.

Part: SKIN — DENTED (BS 275-281) · airframe 51,032 hrs · 27,560 cycles

FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION. INSTALLED EXTERNAL REPAIR DOUBLER TWO INTERNAL DOUBLERS AND TWO FILLERS PER SRM 53 04.

Part: SKIN — DENTED (BS 1271-1286) · airframe 51,032 hrs · 27,560 cycles

FUSELAGE SKIN DENTED. REMOVED DAMAGED SECTION AND EXISTING DOUBLER. INSTALLED EXTERNAL REPAIR DOUBLER AND TWO INTERNAL FINGER DOUBLERS PER SRM 53-04.

Part: WIRE — SHORTED (CABIN) · airframe 50,881 hrs · 27,486 cycles

DURING TAXI AFTER LANDING CABIN FILLED WITH SMOKE. EMERGENCY EVACUATION WAS EXECUTED VIA EMERGENCY SLIDES. SOURCE OF SMOKE WAS ARCING FROM HEATER WIRE DAMAGED BY TA BRACKET WHICH BECAUSE OF VIBRATION EVENTUALLY CUT THROUGH THE WIRE INSULATION. DAMAGED WIRE WAS REPLACED AND EVENT IS CONSIDERED A ONE TIME OCCURRENCE. CAMPAIGN WAS INITIATED TO INSPECT HEATER BLANKET WIRING ON ALL MD 80 AIRCRAFT.

Part: DOOR — DENTED (FUSELAGE) · airframe 48,761 hrs · 26,454 cycles

PRE-FLIGHT INSPECTION, FORWARD PAX (L-1) DOOR DENTED AT LOWER EDGE. INSTALLED EXTERNAL REPAIR DOUBLER. (K)

Part: FLOOR PANEL — CORRODED (FS 160-180)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL. (M)

Part: DOOR — DENTED (FS 1204)

OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR DENTED. RE-COLD FORMED SKIN AND INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — PUNCTURED (HORIZONTAL STAB)

OKC - DURING HV CHECK, FOUND VERTICAL STABILIZER HAS PUNCTURE ON RIGHT SIDE AT RADIUS FOR HORIZONTAL STABILIZER. REPLACED DAMAGED SKIN SECTION. (M)

Part: VANE — CHAFED (TE FLAP)

OKC - DURING HV CHECK, FOUND LEFT NR 3 OUTBOARD FLAP VANE L/E REPAIR DOUBLER IS CHAFED. REPLACED DOUBLER. (M)

Part: SKIN — DENTED (FS 399)

OKC - DURING HV CHECK, FOUND FORWARD CARGO BAY DOOR DENTED. RE-COLD FORMED SKIN AND INSTALLED REPAIR DOUBLER. (M)

Part: INTERCOSTAL — CRACKED (FS 185)

OKC - DURING HV CHECK, FOUND MAIN PASSENGER L1 DOOR INTERCOSTAL CRACKED IN RADIUS. REPLACED INTERCOSTAL. (M)

Part: PAN — CRACKED (FS 425)

OKC - DURING HV CHECK, FOUND FORWARD CARGO BAY DOOR PAN CRACKED IN AFT SIDE. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER. (M)

Part: DOOR — DENTED (FS 1163)

OKC - DURING HV CHECK, FOUND AFT CARGO BAY DOOR DENTED. RE-COLD FORMED SKIN AND INSTALLED REPAIR DOUBLER. (M)

Part: SKIN — DENTED (CARGO DOOR)

OKC - DURING HV CHECK, FOUND MID CARGO BAY DOOR SKIN DENTED. REFORMED SKIN AND INSTALLED REPAIR DOUBLER. (M)

Part: FLOOR PANEL — TORN (FS 160-200)

OKC - DURING HV CHECK FOUND CABIN FLOOR PANEL TORN AT CORNER. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 541-579)

OKC - DURING HV CHECK, FOUND FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — PUNCTURED (FS 674-693)

OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — CORRODED (FS 180-200)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL HAS CORRODED INSERTS. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — PUNCTURED (FS 864-886)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 807-826)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — BENT (FS 315-389)

OKC - DURING HV CHECK FOUND CABIN FLOOR PANEL BENT AT CORNER. INSTALLED REPAIR FILLER AND DOUBLER. (M)

Part: FLOOR PANEL — DELAMINATED (FS 826-864)

OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 946-1003)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 826-864)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — CORRODED (FS 160-200)

OKC - DURING HV CHECK, FOUND FLOOR PANEL HAS MISSING AND CORRODED INSERTS. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 579-617)

OKC - FOUND DURING HV-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — CORRODED (FS 200-237)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL HAS MISSING AND CORRODED INSERTS. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 1193-1250)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — PUNCTURED (CABIN)

OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 380)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 769-807)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 389-465)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 1041-1079)

OKC - FOUND DURING HV-CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — CRACKED (FS 1174-1193)

OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL DELAMINATED AND CRACKED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 697-769)

OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 927-1003)

OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (F 617-693)

OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: FLOOR PANEL — DELAMINATED (FS 200-237)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REBONDED FIBERGLASS. (M)

Part: FLOOR PANEL — DELAMINATED (CABIN)

OKC - DURING HV-CHECK, FOUND CABIN FLOOR PANEL DELAMINATED. REPLACED FLOOR PANEL. (M)

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS)

PREFLIGHT CHECK, FOUND OVERHEAD EMERGENCY LIGHTS DID NOT ILLUMINATE WHEN TURNED ON. RESEATED ASSOCIATED BATTERY PACK POWER SUPPLY. CONNECTION WAS LOOSE. (M)

Part: LIGHT — LOOSE (COCKPIT)

SEA - PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTING DID NOT ILLUMINATE DURING SYSTEM TEST. RESECURED LOOSE CONNECTOR AT L2-550. LIGHTS THEN OPERATED PROPERLY. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - DURING PREFLIGHT CHECK, FOUND COCKPIT EMERGENCY OVERHEAD FLOOR LIGHTS INOPERATIVE UPON TEST. RESEATED BATTERIES IN ASSOCIATED POWER SUPPLIES. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS CABIN. RECONNECTED LOOSE MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

SAN - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS AND AT ROWS 13-15. RECONNECTED LOOSE MODULE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CUSP WEB — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN RIGHT CUSP WEB STATION 256 RBL 44 IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 51-10-4. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOORBOARD STATION 256-294 RBL 44 HAS CORROSION AND BARE METAL NUMEROUS PLACES. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-05. (M)

Part: RUB STRIP — DEBONDED (MLG DOOR)

DURING HV CHECK, FOUND RUB STRIP DISBONDED ON DOOR LANDING FOR PANEL 1365C. REMOVED RUBSTRIP, REAMED DISCREPANT HOLES, FABRICATED AND INSTALLED REPAIR SLEEVE BUSHINGS. INSTALLED RUBSTRIP IAW ASA EA 5720-01248 AND AAR EA 10394. (M)

Part: MEMBRANE — CRACKED (CABIN FLOOR)

DURING HV CHECK, FOUND CABIN FLOOR PANEL FROM STATION 886 TO STATION 946 IS CHAFED AND CRACKED. REMOVED DAMAGED W CHANNEL, ORDERED AND INSTALLED NEW W CHANNEL IAW MD80 SRM 51-30-8. (M)

Part: SKIN — DENTED (FUSELAGE)

DURING HV CHECK, FOUND DENT IN FUSELAGE SKIN STATION 218 AND LONGERON 17L D = 1.5, X= .023, LESS THAN 1 INCH FROM LONGERON 17L. COLD WORKED DENT, COMPLIED WITH HFED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-04. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

DURING HV CHECK, FOUND CABIN FLOORBOARD STATION 200-256 RBL 22-44 FIBERGLASS TORN. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: CUSP WEB — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED AND PUNCTURED STATION 218 LBL 32. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-01. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FUSELAGE SKIN DENTED FROM INSIDE OUT AT STATION 1241 AT LONGERON 30. COLD WORKED DENT, COMPLIED WITH HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD80 SRM 53-04. (M)

Part: FLOOR PANEL — PEELING (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL SURFACE IS PEELING AT SEVERAL LOCATIONS BETWEEN FS 826-864. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL PUNCTURED AT FS 160-200. REPLACED PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING C-CHECK, FOUND FLOOR PANEL IS DELAMINATED AT SEVERAL LOCATIONS FROM FS 927-1003. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS CRACKED AND DISBONDED ON LOWER SURFACE AT FS 977-1003. REPLACED DAMAGED HAT CHANNEL PER MM 20-20-1. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOOR PANEL IS PUNCTURED ON LOWER SURFACE AT FS 826-864. REPLACED FLOOR PANEL PER SRM. 53-05. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

DURING HV CHECK, FOUND CABIN SEAT TRACK AT STATION 242-256, X=-45 IS GOUGED. REMOVED DAMAGED SECTION AND REPLACED PER SRM 53-05. (M)

Part: FLOORBOARD — CRUSHED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FLOORBOARD AT STATION 886-927, RBL 22-44 HAS CRUSHED EDGES. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: ACCESS PANEL — DAMAGED (WING)

OKC - DURING HV CHECK, FOUND FUEL ACCESS PANEL 1355C HAS ONE ELONGATED HOLE. REMOVED AND REPLACED FUEL ACCESS PANEL PER SRM 51-22-2A. (M)

Part: ACCESS PANEL — CORRODED (WING)

OKC - DURING HV CHECK, FOUND LOEWR SRFC OF FUEL ACCESS PANEL 1454 IS CORRODED. REMOVED AND REPLACED FUEL ACCESS PANEL PER SRM 51-22-2A. (M)

Part: SUPPORT FITTING — DAMAGED (LT TE FLAP)

OKC - DURING HV CHECK, FOUND FORWARD HINGE ARM OF LEFT INBOARD FLAP, OUTBOARD HINGE IS DINGED. REMOVED DAMAGE THEN PEENED, TREATED AND PRIMED AREA PER EA 5740-01389. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

OKC - DRING HV CHECK, FOUND METAL FLOORBOARD CHANNEL SUPPORT AT STATION 1003-1079 IS CRACKED. REMOVED DAMAGE AND INSTALLED RPR SPLICES AND ANGLES PER SRM 53-01. (M)

Part: CUSP WEB — CORRODED (FS)

OKC - DURING HV CHECK, FOUND RIGHT CUSP WEB CORRODED AT STATION 984-1003. REMOVED DAMAGED WEB AND INSTALLED NEW PER SRM 51-30-2. (M)

Part: SPLICE PLATE — CRACKED (LT WING)

OKC - DURING HV CHECK, FOUND LEFT WING LEADING EDGE SPLICE PLATE IS CRACKED AT STATION XRS164. REMOVED DAMAGED SPLICE PLATE AND INSTALLED NEW PER SRM 51-10-4. (M)

Part: SKIN — CORRODED (FUSELAGE)

DURING HV CHECK, FOUND AFT PIT SKIN BETWEEN STATION 1149 AND 1155, LONGERON 29L IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER EA 5330-01774. (M)

Part: RUB STRIP — DEBONDED (WING PANEL)

OKC - DURING HV CHECK, FOUND WING PANEL 1371C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

DURING HV CHECK, FOUND CABIN FLOORBOARD AT STATION 180-200, RBL 8 - RBL 44 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: RUB STRIP — DEBONDED (WING PANEL)

OKC - DURING HV CHECK, FOUND WING PANEL 1355C RUBSTRIP IS DISBONED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)

Part: SKIN — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND AFT PIT SKIN BETWEEN STATION 1149 AND 1155, LONGERON 29L-30 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER EA 5330-01774. (M)

Part: CUSP WEB — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN CUSP WEB AT STATION 256, RBL 44 IS CRACKED AT FASTENER HOLE. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-10-4. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - DURING HC CHECK, FOUND SHEAR TIE AT STATOIN 1193, BETWEEN 29R AND 28L IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 51-10-2. (M)

Part: ACCESS PANEL — CORRODED (FUSELAGE)

OKC - DURNG HV CHECK, FOUND LOWWR RING SRFC OF FUEL ACCESS PANEL 1470C IS CORRODED. REMOVED AND REPLACED FUEL ACCESS PANEL PER 51-22-2A. (M)

Part: SKIN — DENTED (AFT CARGO DOOR)

OKC - DURING HV CHECK, FOUND AFT PIT DOOR SKIN DENTED AT STATIN 1186, APPROX 15 INCHES FROM TOP, D=2 INCHES X=.040. REMOVED DAMAGED AREA OF SKIN AND INSTALLED RPR DOUBLERS PER SRM 53-04. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

OKC - DURING HV CHECK FOUND INTERCOSTAL AT STATOIN 769-788, LONGERON 28R IS CORRODED. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW PER SRM 51-30. (M)

Part: LONGERON — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND UNDERSIDE OF LONGERON 30 AT STATION 1200 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER PER SRM 53-2. (M)

Part: RUB STRIP — DEBONDED (WING PANEL)

OKC - DURING HV CHECK, FOUND WING PANEL 1367C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FLOORBOARD AT STATION 160-200, LBL 44-54 IS PUNCTURED. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: RUB STRIP — DEBONDED (WING PANEL)

OKC - DURING HV CHECK, FOUND WING PANEL 1303 RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUB STRIP PER EA 5720-01248. (M)

Part: RUB STRIP — DEBONDED (WING PANEL)

OKC - DURING HV CHECK, FOUND WING PANEL 1361C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FLOORBOARD AT STATION 864-886, LBL 22-44 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: RUB STRIP — DEBONDED (WING PANEL)

OKC - DURING HV CHECK, FOUND WING PANEL 1363C RUBSTRIP DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND METAL FLOORBOARD AT STATION 1003-1079 IS CRACKED. REMOVED DAMAGE AND INSTALLED PRP DOUBLER PER SRM 51-10-3. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOORBOARD AT STATION 160-280, LBL 8 - RBL 8 IS DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: RUB STRIP — DEBONDED (WING PANEL)

OKC - DURING HV CHECK, FOUND WING PANEL 1357C RUBSTRIP IS DISBONDED. REAMED HOLES, INSTALLED RPR BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)

Part: ACCESS PANEL — CORRODED (WING)

OKC - DURNG HV CHECK, FOUND FRETTING CORROSION ON FUEL ACCESS PANEL 1456C. REMOVED AND REPLACD FUEL ACCESS PANEL PER 51-22-2A. (M)

Part: RUB STRIP — DEBONDED (WING PANEL)

OKC - DURING HV CHECK, FOUND WING PANEL 1379 RUBSTRIP IS DISBONDED. REAMED HOLES. INSTALLED PRP BUSHING AND RE-INSTALLED RUBSTRIP PER EA 5720-01248. (M)

Part: ANGLE — CRACKED (FUSELAGE)

OKC - DURING HV CHECK, FOUND RIGHT MLG DOOR CUT OUT AFT OUTBOARD ANGLE CRACKED. REPLACED ANGLE PER SRM 53-05. (M0

Part: FRAME — DAMAGED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FRAME FASTENER HOLE IS WORN OUT OF ROUND AT FS 1322. REMOVED DAMAGE. INSTALLED REPAIR ANGLE, FILLER, AND SHIM PER SRM 53-05. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 160-200 RBL 44 TO RBL 54 HAS MISSING MATERIAL. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FITTING — CRACKED (DOOR FRAME)

OKC - FOUND DURING HV CHECK, AFT CARGO DOOR FRAME TEE- FITTING ON UPPER INNER STRUCTURE IS CRACKED. REPLACED TEE PER SRM 51-30-5. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE STATION 178 BETWEEN 28R AND 29R DENTED D=1.25 BY = .023. COMPLIED WITH HFEC INSPECTION, NO DEFECT NOTED. NO FURTHER ACTION REQUIRED IAW ASA EA 5530-01775. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 200-256 RBL 15 TO RBL 22 FIBERGLASS TORN OFF. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 200-256 RBL 44 TO RBL 22 FIBERGLASS TORN OFF. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

OKC - DURNG C-CHECK, FOUND CABIN FLOORBOARD STATION 168-160 LBL 8 TO RBL 17 FIBERGLASS TORN. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOOR PANEL — TORN (FUSELAGE)

OKC - DURING HV CHECK, FOUND PASSENGER CABIN FLOOR PANEL TORN AT FS 927-1003. REPLACED PANEL PER SRM 53-05. (M0

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

OKC - DURING C-CHECK, FOUND CABIN FLOORBOARD STATION 200-156 LBL 22 TO RBL 14 DELAMINATING. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL PUNCTURED AT FS 160-200. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: PANEL — CORRODED (WING)

OKC - DURING HV CHECK, FOUND FUEL PANEL IS CORRODED. REPLACED PANEL PER SRM 51-22-2A. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND DENT LEFT SIDE FUSELAGE SKIN AT FS 313 AND LONGERON 22L D= 3 INCHES BY =.100 DENT IS LESS THAN 1 INCH FROM LONGERON 22L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD80 SRM 53-04 AND 51-30-5. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

OKC - FOUND DURING C-CHECK, CABIN FLOORBOARD STATION 160-180 RBL 08 TO RBL 44 FIBERGLASS TEARING OFF. FABRICATED REPLACEMENT FLOORBOARD IAW MD80 SRM 53-05. (M)

Part: ANGLE — CRACKED (LT WING)

OKC - FOUND DURING HV CHECK, FOUND LEFT WING LEADING EDGE ATTACH ANGLE IS CRACKED AT STATION XRS 164. REPLACED ANGLE PER SRM 51-10-2. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

OKC - FOUND DURING HV CHECK, PASSENGER SEAT TRACK GOUGED AT FS 807. REMOVED DAMAGED SECTION AND INSTALLED REINFORCEMENT PER SRM 53-05. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

OKC - DURING HV CHECK, FOUND PASSENGER SEAT TRACK GOUGED AT FS 275-300. REMOVED DAMAGED SECTION AND INSTALLED REINFORCEMENT PER SRM 53-05. (M)

Part: INTERCOSTAL — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND DENT ON INTERCOSTAL FLANGE 1 INCH WIDTH BY 3 INCHES DEEP AT CANTED STATION 1497-1510 AT 25L. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW MD80 SRM 51-30-2 AND DRAWING 99177011. (M)

Part: SKIN — DENTED (FUSELAGE)

OKC - DURING C-CHECK, FOUND RIGHT FUSELAGE FROM STATION 193 TO 204 BETWEEN LONGERON 27R AND 28R IS DENTED WITHIN TWO FRAME BAYS D= 6.00 BY =.060. COLD WORKED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER AND SHIMS IAW ASA EA 5330-01775 AND AAR EA 10890. (M)

Part: FRAME — CORRODED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FRAME CORRODED ON UPPER SURFACE AT FS 1338. REPLACED DAMAGED SECTION AND INSTALLED REPAIR ANGLE PER SRM 51-10-4. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DISBONDING AT SUPPORTS AT FS 200-256. BOND-REPAIRED PER MM 25-00-00. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL HAT CHANNELS DISBONDED AT FS 256-294. BOND-REPAIRED PER MM 20-20-01. (M)

Part: FRAME — DAMAGED (FUSELAGE)

OKC - DURING HV CHECK, FOUND FRAME FASTENER HOLE ELONGATED ON UPPER SURFACE AT FS 1322. REPAIRED HOLE WITH FILLER, SHIM, AND ANGLE PER SRM 53-05. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

OKC - FOUND DURING HV CHECK, SHEAR TIE CORRODED AT FS 636. REPLACED SHEAR TIE PER SRM 51-30-5. (M)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

OKC - DURING HV CHECK, FOUND CABIN FLOOR PANEL DELAMINATED AT FS 1309-1361. REPLACED FLOOR PANEL PER SRM 53-05. (M)

Part: FLOOR PANEL — ELONGATED (FUSELAGE)

OKC - FOUND DURING HV CHECK, CABIN FLOOR PANEL HAS ELONGATED HOLES AT FS 200-256. FIBERGLASS REPAIR PER MM 25-00-00. (M)

Part: CAM — BROKEN (TAILCONE)

OKC - FOUND TAILCONE EMERGENCY SLIDE FAILED TO DEPLOY DURING SLIDE DEPLOYMENT TEST PER WORK CARD 28625000. THE FAILURE WAS ATTRIBUTED NOT TO THE SLIDE ASSEMBLY, BUT TO A BROKEN TAILCONE JETTISON AND HOISTING CONTROL CAM. THE CAM WAS REPLACED, BUT THE DEPLOYMENT TEST WAS DEFERRED TO THE NEXT MD-80 AIRCRAFT IN CHECK. (M)

Part: LANYARD — BROKEN (TAIL CONE)

OKC - WHILE ACCOMPLISHING TAIL CONE EMERGENCY RELEASE TASK CARD STEPS THE LANYARD BROKE AT CAM. CABLE WAS REPAIRED AND REINSTALLED IN PREPARATION FOR AN EMERGENCY SLIDE DEPLOYMENT TEST PER TASK CARD 28625000, WHICH ENCOMPASSES, AS PART OF THE SEQUENCE, A TAILCONE RELEASE/DROP. (M)

Part: ROD — DISCONNECTED (WINDOW)

SJC - PREFLIGHT CHECK, FOUND LT CAPTAINS SLIDING CLEARVIEW WINDOW ACTUATING ROD FOUND DISCONNECTED. RECONNECTED ACTUATING ROD. WINDOW THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA PREFLIGHT CHECK, FOUND FORWARD RIGHT SERVICE (R1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (M)

Part: SLIDE — FAILED (PAX DOOR)

OAK - FOUND DURING 15K CHECK, AFT PASSENGER DOOR EMERGENCY SLIDE FAILED LIGHT CHECK. REPLACED EMERGENCY SLIDE PER TASK CARD 24655000. (M)

Part: SKIN — GOUGED (VERTICAL STAB)

OAK - ON 15K CHECK, VERTICAL STABILIZER SKIN GOUGED ON LEFT SIDE AT LOWER FORWARD END OF CUTOUT FOR HORIZONTAL STABILIZER. BLENDED GOUGE AND INSTALLED DOUBLER PER SRM 55-01. (M)

Part: SLIDE — FAILED (PAX DOOR)

OAK - DURING 15K CHECK, FOUND FORWARD PASSENGER L1 DOOR EMERGENCY SLIDE FAILED LIGHT CHECK. REPLACED EMERGENCY SLIDE PER TASK CARD 24655000. (M)

Part: CARGO TRACK — CORRODED (FUSELAGE)

OAK - DURING 15K CHECK, FOUND AFT CARGO BAY LEFT TIEDOWN TRACK IS CORRODED AROUND SCREW HOLES FROM FS 1003 TO 1322. REPLACED TIEDOWN TRACK PER SRM 51-10-4. (M)

Part: BEAM — CORRODED (FUSELAGE)

OAK - FOUND DURING C-CHECK, AFT CARGO BAY LOWER DOOR BEAM EDGE CORRODED ON HORIZONTAL LEG. REPLACED LOWER BEAM PER SRM 51-30-2 AND 30-6. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

OAK - DUIRNG C-CHECK, FOUND FLOORBEAM CORRODED ON OUTBOARD OF PANEL F-6, FS 160-196. REPLACED SUPPORT BEAM PER SRM 51-10-4 AND 51-30-2. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OAK - FOUND DURING C-CHECK, FLOOR SUPPORT CORRODED BETWEEN INBOARD AND OUTBOARD SEAT TRACK AT FS 1155 ON RIGHT SIDE. REPLACED SUPPORT PER SRM 51-10-4 AND 51-30-5. (M)

Part: WEB — CORRODED (FUSELAGE)

OAK - DUIRNG C-CHECK, FOUND AFT CARGO BAY FLOOR MEMBRANE CORRODED AT FS 1070. INSTALLED DOUBLER PER SRM 51-10-3 AND 53-01. (M)

Part: WEB — CORRODED (FUSELAGE)

OAK - FOUND DURING C-CHECK, LEFT PASSENGER FLOOR WEB MEMBRANE CORRODED BETWEEN FS 826-845. INSTALLED DOUBLER PER SRM 51-10-3 AND 53-01. (M)

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

LAS - DURING PREFLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)

Part: BALLAST — FAILED (CABIN)

ELECTRICAL SMELL NOTED AT ROW 17. DIVERTED, FOUND ALL FOUR BALLAST SUPPORT GROMMETS FRIED. FERRIED TO SEA. REPLACED DEFECTIVE BALLAST.

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

SEA - LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M)

Part: HARNESS — FAILED (EVAC SLIDE)

OAK - DURING C-CHECK, FORWARD PASSENGER DOOR EMERGENCY SLIDE HARNESS FAILED SYSTEM CHECK. REPLACED EMERGENCY SLIDE. SYSTEM CHECKED OK. (M)

Part: MODULE — DISCONNECTED (CABIN)

SFO - DURING PREFLIGHT CHECK, FIRST FOUR EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED FIRST MODULE. LIGHTS THEN OPERATED PROPERLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

PDX - DURING PREFLIGHT CHECK, FORWARD 1ST CLASS EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DETACHED (L2 DOOR)

SEA - DURING PREFLIGHT CHECK, L2 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. ATTACHED LANYARD. (M)

Part: CONNECTOR — DAMAGED (CABIN)

PDX - DURING PREFLIGHT CHECK, FOUND INOPERATIVE EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN. REPLACED MODULE CONNECTOR AND SECTION OF WIRING. LIGHTS THEN OPERATED PROPERLY. (M)

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA - DURNIG PRE-FLIGHT CHECK, R-1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)

Part: LANYARD — DISCONNECTED (SERVICE DOOR)

LAX - LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M)

Part: LIGHT — INOPERATIVE (FWD PAX ENTRY)

SEA - DURING LINE CHECK, FOUND FORWARD PORTABLE EMERGENCY LIGHT TO BE INOPRERATIVE. REPLACED PORTABLE LIGHT. OP TESTED OK. (M_

Part: LANYARD — DISCONNECTED (ESCAPE SLIDE)

SEA - DURING DISARMING OF R-1 SLIDE (IE UNCLIPPING AND STOWING GIRT BAR), LANYARD BETWEEN GIRT BAR AND SLIDE COVER BECAME DISCONNECTED. REATTACHED LANYARD. (M)

Part: COALESCER BAG — CONTAMINATED (CABIN)

PDX - DURING CRUISE, NOTED STRONG FUEL FUMES, WHICH EVENTUALLY DISSIPATED. REPLACED BOTH AIR CONDITIONING PACK COALESCER BAGS. NO ODOR NOTED. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY CEILING LIGHTS AT ROWS 8, 10 AND 12 WERE FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY AND THE LIGHTS OPERATED NORMALLY. (M)

Part: HARNESS — FAILED (L2 DOOR)

OAK - DURING C-CHECK, L-2 DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REMOVED AND REPLACED L-2 DOOR SLIDE ASSEMBLY WITH SERVICEABLE ASSY. (M)

Part: WIRE HARNESS — FAILED (EVAC SLIDE)

OAK - DURING C-CHECK, AFT PAX (TAILCONE) DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REMOVED AND REPLACED THE AFT DOOR EMERGENCY SLIDE HARNESS. (M)

Part: HARNESS — FAILED (L1 DOOR)

OAK - DURING C-CHECK, L1 DOOR EMERGENCY SLIDE HARNESS FAILED THE AMPERAGE CHECK. REMOVED AND REPLACED COMPLETE L1 SLIDE ASSEMBLY WITH SERVICEABLE ASSEMBLY. (M)

Part: LATCH — UNLATCHED (EMERGENCY SLIDE)

BUR - DURING PRE-FLIGHT CHECK, R1 DOOR EMERGENCY SLIDE PACK COVER LATCH WAS FOUND UNLATCHED. RE-LATCHED SLIDE PACK COVER. (M)

Part: FUEL LINE — LEAKING (APU BAY)

PDX - FLT 719, DURING CLIMB, STRONG FUEL ODOR WAS NOTED IN COCKPIT. DISCOVERED FUEL LEAK AT APU ATOMIZER-TO-FUEL LINE ELBOW. TIGHTENED ELBOW FITTINGS. SYSTEM WAS THEN OPS CHECKED, WITH NO ODOR OR LEAKS BEING NOTED. (M)

Part: CHARGER — INOPERATIVE (E/E BAY)

SEA - DURING LINE CHECK, OVERHEAD EMERGENCY LIGHTING AT ROW 6-8 WAS DETERMINED TO BE INOPERATIVE. REPLACED BATTERY CHARGER. LIGHTS THEN OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SJC - DURING LINE CHECK, NUMEROUS EMERGENCY TRACK LIGHTS BETWEEN CABIN ROWS 1-6 AND IN TAIL AREA WERE DETERMINED TO BE INOPERATIVE. REPLACED ASSOCIATED POWER SUPPLIES (BATTERY PACKS). LIGHTS THEN OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,293 hrs · 17,277 cycles

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 6 AND ROWS 13 TO 15 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE RELATED POWER SUPPLY AND OPERATED NORMALLY. (X)

Part: HANDLE — LACK OF LUBE (PAX DOOR)

SEA - PRIOR TO DEPARTURE OF FLT 460, CREW REPORTED THE AFT CABIN ENTRY DOOR HANDLE WAS DIFFICULT TO OPERATE. LUBRICATED THE DOOR HANDLE MECHANISM AND OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEA - PRIOR TO DEPARTURE OF FLIGHT 466, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED LOOSE CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 230, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SAN - PRIOR TO DEPARTURE OF FLT 231, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 92, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (X)

Part: LATCH — INOPERATIVE (R1 DOOR)

SEA - PRIOR TO DEPARTURE OF FLT 566, CREW REPORTED THE R1 DOOR WOULD NOT LATCH IN THE OPEN POSITION. CLEANED SEALANT FROM THE R1 DOOR HOLD OPEN LATCH AND OPERATED NORMALLY. (M)

Part: SPRING — DAMAGED (COCPIT WINDOW)

PDX - DURING MAINTENANCE CHECK, THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW LOWER AFT LOCKING SPRING WAS FOUND DAMAGED. REPLACED THE SPRING AND OPERATED NORMALLY. (M)

Part: WIRE — LOOSE (CATWALK)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPAIRED LOOSE WIRE TO LIGHT ASSEMBLY L2-638 AND REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. REF: OPER CONTROL NR 99ZZZX742. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPAIRED LOOSE WIRE TO LIGHT ASSEMBLY L2-638 AND REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. REF: OPER CONTROL NR ASAA9880260.

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - FLT 535 - CREW REPORTED DIFFICULTY IN CLOSING, THE L1 DOOR AND EXTINGUISHING DOOR LIGHT. ADJUSTED DOOR ROTATING ROD, CRANK AND BAYONET ROD, DOOR OPERATED NORMALLY. (M)

Part: POWER SUPPLY — INOPERATIVE (OVERWING EXIT)

LCQ - DURING 30K CHECK, THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)

Part: SUPPORT — GOUGED (LT WING)

LCQ - DURING 30K CHECK, GOUGES WERE FOUND ON LEFT WING NR 0 L/E SLAT OUTBOARD SUPPORT. REPAIRED IAW ASA EA 5740-01149. (M)

Part: HINGE — GOUGED (ELEVATOR)

LCQ - DURING 30K CHECK GOUGES WERE FOUNDON LEFT ELEVATOR ANTI FLOAT TAB HINGE, 3RD FROM OUTBOARD. REPAIRED IAW ASA EA 5520-01062. (M)

Part: WEB — CORRODED (FUSELAGE)

LCQ - DURING 30K CHECK CORROSION WAS FOUND ON CUSP WEB AT L2 DOOR THRESHOLD. REPAIRED IAW ASA EA 5310-01624. (M)

Part: WEB — DAMAGED (CARGO BAY)

LCQ - DURING 30K CHECK, WEB AT MID CARGO COMPARTMENT DOOR JAMB WAS DAMAGED DURING INSTALLATION OF CARGO COMPARTMENT SIDE LINER. REPAIRED IAW ASA EA 5310-01629. (M)

Part: FITTING — CHAFED (LT ELEVATOR)

LCQ - DURING 30K CHECK, WEAR SPOT WAS FOUND ON LEFT ELEVATOR CONTROL TAB HINGE FITTING (4TH FROM INBOARD). REPAIRED IAW ASA EA 5520-01063. (M)

Part: FITTING — CORRODED (SPOILER)

LCQ - DURING 30K CHECK, CORROSION WAS FOUND ON RIGHT WING INBOARD FLIGHT SPOILER HINGE FITTING. REPAIRED IAW ASA EA 2760-01026. (M)

Part: FITTING — GOUGED (TE FLAP)

LCQ - DURING 30K CHECK, GOUGES WERE FOUND ON LEFT T/E FLAP OUTBOARD HINGE FITTING. REPAIRED IAW ASA EA 2750-01066. (M)

Part: BATTERIES — DISCHARGED (COCKPIT)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 8 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)

Part: WIRE — SHORTED (CABIN)

SEA - PRIOR TO DEPARTURE OF FLT 370, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 13 TO 20 WERE INOPERATIVE. REPAIRED SHORTED WIRE AND OPERATED NORMALLY. (M)

Part: WIRE — LOOSE (CABIN)

ONT - PRIOR TO DEPARTUREF OF FLT 539, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 12 AFT WERE INOPERATIVE. REPAIRED LOOSE WIRE AT ROW 12 AND OPERATED NORMALLY. (M)

Part: LIGHT — DEFECTIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LGIHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: INTERIOR MOLDING — LOOSE (L1 DOOR)

ANC - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND TO BE BINDING. RESEATED THE DOOR INTERIOR MOLDING AND OPERATED NORMALLY. (M)

Part: BOTTLE — LOW PRESSURE (R1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, GHE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT LGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 22 TO 33 WERE FOUND DIM. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M)

Part: INFLATION BOTTLE — LOW PRESSURE (L1 DOOR)

SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE. (M)

Part: BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN AND THE EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND DIM. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M)

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

SEA - PRIOR TO DEPARTURE OF FLT NR 524, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO CLOSE. ADJUSTED DOOR MECHANISM PER MM AND OPERATED NORMALLY. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE BATTERY AND OPERATED NORMALLY. (M)

Part: EEL BATT PACK — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 9-11 AND 20-22. REPLACED BATTERY PACK AT ROWS 9-11 AND BATTERIES AT ROWS 20-22. LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 9-11 AND 20-22. REPLACED BATTERY PACK AT ROWS 9-11 AND BATTERIES AT ROWS 20-22. LIGHTS OPERATED NORMALLY.

Part: EEL POWER SUPPLY — DEFECTIVE (CABIN)

PDX - BLOCK TURN BACK OF FLIGHT 564 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 20 WERE FOUND INOPERATIVE DURING TEST. REPLACED THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL GROUND — LOOSE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 13 TO 21 WERE FOUND INOPERATIVE. TIGHTENED LOOSE GROUND STUD AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL BATTERIES — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE TAILCONE EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M)

Part: SEAT TRACK — GOUGED (BS 261)

PAE - DURING 15K CHECK, GOUGE WAS FOUND ON SEAT TRACK AT Y261, X-46, Z-0. REMOVED GOUGED SEAT TRACK. INSTALLED NEW SEAT TRACK IAW DC-9 SRM 53-05. (W)

Part: CARGO TRACK — CORRODED (BS 1153)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y1154, X-14, Z-45. REMOVED CORRODED CARGO TRACK. INSTALLED NEW CARGO TRACK IAW DC-9 SRM 51-01 PG 1, 51-10-03 PG 8 AND 21. (W)

Part: ANGLE — CORRODED (BS 1212)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME TO SKIN ATTACH ANGLE AT Y1212, X-5, Z-50. REMOVED CORRODED ATTACH ANGLE. INSTALLED NEW ATTACH ANGLE IAW DC-9 SRM 51-00, 51-30-02 PG 1 AND 8, 51-30-05 PG 12. (W)

Part: FRAME — CORRODED (BY 1309)

PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AT Y1309, X PLUS 7 TO X-5, Z-48. REMOVED CORRODED SECTION OF FRAME. INSTALLED NEW FRAME IAW DC-9 SRM 53-03 FIG 2A, 51-10-03 PG 1, 3 AND 8. (W)

Part: EEL BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK THE OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS WERE FOUND INOPERATIVE. REPLACED PACK BATTERIES AND LIGHTS OPERATED NORMALLY. (W)