N909NN

Part: SIGN — BROKEN (ZONE 200) · airframe 38,561 hrs · 16,741 cycles

AIRCRAFT WAS NOT GROUNDED: AFT GALLEY EXIT SIGN BROKEN OVER AFT LEFT DOOR. REMOVED AND REPLACED AFT GALLEY EXIT SIGN OVER AFT LEFT DOOR. PER AMM 33-53-01.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 38,258 hrs · 16,591 cycles

AIRCRAFT WAS NOT GROUNDED: AFT DOOR AIRCRAFT RIGHT GIRT FLAP NOT PROPERLY PLACED INSIDE SLIDE COMPARTMENT HARD TO ARM DISARM DOOR. ADJUSTED GIRT BAR RETAINER CLIPS ON 2R PASSENGER DOOR. PER AMM 25-66-01.

Part: BAFFLE — DAMAGED (ZONE 100) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: HOLES IN FORWARD CARGO COMPARTMENT BAFFLE ASSEMBLY LOCATED FROM STA 500F TO STA 500G, LBL 26. REPLACED BAFFLE ASSEMBLY PER AARD 51-00-05-1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500H, RBL 26. REPLACED CLIP PER AARD 51-00-05-1.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500H, S26R. REPLACED BAFFLE CLIP PER AARD 51-00-05-01.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CIP AT STA 500G, RBL 26. REPLACED BAFFLE CLIP PER AARD 51-00-05-01.

Part: ATTACH BRACKET — CORRODED (ZONE 800) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON APU DOOR RIB 3 INSULATION BLANKET ATTACH BRACKET AT STA 1112, WL 148.5. REPLACED BRACKET PER SRM 51-40-02.

Part: ANGLE — CRACKED (ZONE 100) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500F, S26R. REPLACED CLIP PER AARD 51-00-05-1.

Part: ATTACH BRACKET — CORRODED (ZONE 800) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON APU DOOR RIB 5 INSULATION BLANKET ATTACH BRACKET AT STA 1112, WL 148.5. REPLACED BRACKET PER SRM 51-40-02.

Part: ATTACH BRACKET — CORRODED (ZONE 800) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON APU DOOR RIB 4 INSULATION BLANKET ATTACH BRACKET AT STA 1112, WL 148.5. REPLACED BRACKET PER SRM 51-40-02.

Part: ANGLE — CRACKED (ZONE 100) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500G, S26R. REPLACED CLIP PERAARD 51-00-05-1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500G, LBL 26. REPLACED CLIP PER AARD 53-00-01-6.

Part: ANGLE — CRACKED (ZONE 100) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500H, LBL 26. REPLACED CLIP PER AARD 53-00-01-6.

Part: SKIN — WORN (ZONE 100) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: WEAR MARK ON FUSELAGE SKIN INTERNAL SURFACE AT STA 277 PLUS 6 INCHES, FROM S2L TO S3L. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-00-01-2R PROCEDURE 20.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 323, RBL 30. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOORBOARD SUPPORT AT STA 540, RBL 1. REPLACED SUPPORT PER AARD 51-00-05 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOORBOARD SUPPORT AT STA 540, LBL 1. REPLACED FLOORBOARD SUPPORT PER AARD 51-00-05.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL FROM STA 727G TO STA 727H, RBL 26. REPLACED TRANSITION PANEL PER AARD 51-00-05-1 AND SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL AT STA 727C, RBL 26. REPLACED TRANSITION PANEL PER AARD 51-00-05-1 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL LOCATED AT FROM STA 957 TO STA 959, LBL 49. REPLACED INTERCOSTAL PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT STA 986.5, LBL 43. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 4 AND EA 359257.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL FROM STA 727J TO STA 747, RBL 26. REPLACED TRANSITION PANEL PER SRM 51-40-02.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHIELD FROM STA 767 TO STA 787, RBL 26. REPLACED SHIELD PER AARD 51-00-05-1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT STA 986.5, RBL 43. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 4.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR LOWER CUT OUT WEB AT STA 847, RBL 23. REPLACED WEB PER AARD 51-00-05.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO TRANSITION PANEL LOCATED FROM STA 400 TO STA 500I, LBL 26. REPLACED TRANSITION PANEL PER AARD 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,619 hrs · 15,358 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT TRANSITION PANEL LOCATED FROM STA 400 TO STA 500I, RBL 26. REPLACED TRANSITION PANEL PER AARD 51-00-05-01.

Part: DOOR — OUT OF POSITION (ZONE 800) · airframe 35,129 hrs · 15,106 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTANDENT REPORTS LEFT AFT LAVATORY DOOR WILL NOT OPEN. REPOSITIONED LEFT AFT LAVATORY DOOR INTO UPPER DOOR FRAME TRACK ASSEMBLY. OPERTIONAL CHECKED LAVATORY DOOR AND CHECKED NORMAL. PER AMM 25-40-15.

Part: GIRT BAR — MISINSTALLED (ZONE 800) · airframe 34,960 hrs · 15,022 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN DOOR 1L SLIDE IS COMING OUT OF BRACKET. INSTALLED GIRT BAR ONTO DOOR FOR SAFE MOVEMENT OF DOOR. PER AMM 25-66-00.

Part: TRACK — LACK OF LUBE (ZONE 800) · airframe 34,950 hrs · 15,018 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY-E DOOR HARD TO OPEN FULLY. CONSTANTLY GETS STUCK HALF WAY OPEN. LUBED DOOR TRACK. OPERTIONAL CHECK NORMAL.

Part: TUBE — MISSING (GIRT BAR) · airframe 34,507 hrs · 14,800 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD ENTRY DOOR GIRT BAR MISSING ONE RED INDICATOR. INSTALLED NEW HEAT SHRINK AT FWD ENTRY DOOR. PER AARD 25-66-00-4.

Part: TUBE — MISSING (GIRT BAR) · airframe 34,207 hrs · 14,656 cycles

AIRCRAFT WAS NOT GROUNDED: RED HEAT SHRINK ON R2 DOOR NEEDS REPLACEMENT. REPLACED RED HEAT SHRINK ON R2 DOOR. PER AARD 25-66-00-4 STEP (6)(G).

Part: THRESHOLD — UNSECURE (AFT LAVATORY) · airframe 33,879 hrs · 14,500 cycles

AIRCRAFT WAS NOT GROUNDED: AFT LAVATORY D DOOR GETS JAMMED. TIGHTENED DOOR THRESHOLD HARDWARE PER AMM 25-40-15.

Part: TUBE — MISSING (GIRT BAR) · airframe 33,849 hrs · 14,489 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR GIRT BAR HAS MISSING RED HEAT SHRINK OF RH SIDE OF DOOR. MAINTENANCE INSTALLED HEAT SHRINK TUBE AT R1 DOOR IAW W/C 2523J012-001.

Part: OVEN — ODOR (ZONE 900 - LAV/G) · airframe 29,607 hrs · 12,427 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY OVEN # 2 HAS BURNING ODOR. REPLACED OVEN PER AMM 25-32-03. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: GIRT BAR — DISLODGED (ZONE 800 - DOORS) · airframe 28,549 hrs · 11,914 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT AFT ENTRANCE DOOR SLIDE COMPARTMENT DISLODGED FROM DOOR. SECURED GIRT BAR AT LEFT ENTRANCE DOOR PER AMM 25-66-00.

Part: SCREW — STRIPPED (ZONE 800 - DOORS) · airframe 27,931 hrs · 11,633 cycles

AIRCRAFT WAS GROUNDED: FOUND R1 DOOR SLIDE SECURING SCREW LOOSE AND STRIPPED. INSTALLED R1 DOOR SLIDE FORWARD MOUNTING SCREW PER AMM 25-66-01-400-803.

Part: MODULE — NONE (ZONE 200 - FUSE) · airframe 27,919 hrs · 11,630 cycles

AIRCRAFT WAS GROUNDED: LEFT SPAR VALVE CLOSED LIGHT ILLUMINATED IN FLIGHT. ENGINE STILL RUNS. LIGHT FINALLY WENT OUT ON ITS OWN. REPLACED P5-2 FUEL SYSTEM MODULE PER AMM 28-22-43. ACCOMPLISHED SATISFACTORY # 1 ENGINE RUNS PER AMM 71-00-00.

Part: ACTUATOR — DEFECTIVE (ZONE 400 - NAC/P) · airframe 27,917 hrs · 11,628 cycles

AIRCRAFT WAS GROUNDED: LEFT SPAR VALVE CLOSED LIGHT ILLUMINATED AT CRUISE. REPLACED LEFT ENGINE FUEL SPAR VALVE ACTUATOR V38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 28-22-11.

Part: SUMP — LEAKING (NR 1 ENG OIL) · airframe 27,583 hrs · 11,474 cycles

AIRCRAFT WAS GROUNDED: SHORTLY AFTER POWER REDUCTION ON DECENT, MUSTY TYPE OF ODOR WAS NOTICED ON FLIGHT DECK AND AFT CABIN. ODOR DISSIPATED SHORTLY BEFORE LANDING. MAINTENANCE ACCOMPLISHED SMOKE ODOR FUMES INITIAL TROUBLESHOOTING JOB CARD 08L00021001. ENGINE #1 OIL SUMP LEAK IDENTIFIED AS ODOR SOURCE, CONTAMINATING LEFT HAND PACK. ENGINE #1 REPLACED PER JOB CARD 08L40072003. ACCOMPLISHED SATISFACTORY ENGINE POWER RUNS. ODOR NOT PRESENT AFTER ENGINE POWER RUNS.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 27,583 hrs · 11,474 cycles

AIRCRAFT WAS GROUNDED: SHORTLY AFTER POWER REDUCTION ON DECENT, MUSTY TYPE OF ODOR WAS NOTICED ON FLIGHT DECK AND AFT CABIN. ODOR DISSIPATED SHORTLY BEFORE LANDING. * (OPEN)

Part: CONTROL PANEL — SMOKE (AIR TRAFFIC) · airframe 25,617 hrs · 10,571 cycles

AIRCRAFT WAS GROUNDED: AT FL340, EXPERIENCED SMOKE IN COCKPIT FROM "FL' BUTTON ON TRANSPONDER AND FOUND "ELECTRICAL PANEL LIGHTS" CIRCUIT BREAKER POPPED; FLIGHT DIVERTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED AIR TRAFFIC CONTROL CONTROL PANEL IAW AMM 34-53-03, OPS CHECK GOOD.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 22,860 hrs · 9,351 cycles

AIRCRAFT WAS NOT GROUNDED: #'1 MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE PER AMM 25-64-00.

Part: BEARING — BINDING (AILERONS) · airframe 22,691 hrs · 9,276 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS AILERONS VERY STIFF IN FLIGHT AND ON GROUND. REMOVED & REPLACED AILERON CENTERING MECHANISM CAM FOLLOWER BEARING IAW JOB CARD 1422. OK FOR SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 22,102 hrs · 8,993 cycles

AIRCRAFT NOT GROUNDED: LAVATORY SMOKE LIGHT ILLUMINATED ON OVERHEAD PANEL. F/A CHECKED ALL LAVS. SMOKE LIGHT ON IN AFT LEFT LAV. NO SMOKE VISABLE. LIGHT EXTINGUISHED. LT AFT LAV SMOKE DETECTOR TESTS GOOD IAW AMM 26-14-00.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 20,647 hrs · 8,346 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS LAVATORY SMOKE ALERTED IN COCKPIT FOR AFT LEFT LAV. F/A CHECKED LAV AFTER PAX EXITED AND FOUND NO EVIDENCE OF SMOKE OR FIRE. ALERT EXTINGUISHED AFTER 3 MINUTES. PERFORMED LEFT LAVS SMOKE DETECTOR TEST IAW AMM 26-14-00-730-801. OPS CHECK NORMAL.

Part: TRANSITION PANEL — CORRODED (BS 500A-500I) · corrosion level 2 · airframe 19,470 hrs · 7,820 cycles

CORROSION FOUND ON THE FORWARD CARGO BAY RT TRANSITION PANEL BETWEEN BS 500A AND 500I. REPLACED THE TRANSITION PANEL.

Part: TRANSITION PANEL — CORRODED (BS 500A-500F) · corrosion level 2 · airframe 19,470 hrs · 7,820 cycles

CORROSION FOUND ON THE FORWARD CARGO BAY LEFT TRANSITION PANEL BETWEEN BS 500A AND 500F. REPAIRED THE TRANSITION PANEL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,470 hrs · 7,820 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR SUPPORT AT BS 950 AND LBL 50. REPLACED FLOOR SUPPORT PER 51-00-05-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,470 hrs · 7,820 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR SUPPORT BETWEEN BS 947 AND BS 967 AT RBL 50. REPLACED FLOOR SUPPORT PER 51-00-05-1.

Part: SHIELD — CORRODED (BS 492-500A) · corrosion level 2 · airframe 19,470 hrs · 7,820 cycles

FORWARD RIGHT AFT CARGO SHEILD HAS CORROSION BETWEEN BS 492 - 500A. REPLACED THE SHIELD.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 19,470 hrs · 7,820 cycles

CABIN FLOOR SUPPORT CRACKED AT BS 540 AND RBL 2. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 19,470 hrs · 7,820 cycles

CABIN FLOOR SUPPORT CRACKED AT BS 540 AND LBL 2. REPLACED THE FLOOR SUPPORT IAW 51-00-05-1

Part: SLIDING WINDOW — FAULTY (L2) · airframe 18,819 hrs · 7,525 cycles

L2 SLIDING WINDOW DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE L2 WINDOW IAW 56-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 18,619 hrs · 7,439 cycles

BULKHEAD WEB CRACKED BEHIND THE RIGHT HYDRAULIC FILTER . REPAIRED THE BULKHEAD WEB 57-10-10-9

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 16,367 hrs · 6,442 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. SLC-ORD FLIGHT RETURNED TO SLC ACCOUNT LANDING GEAR WOULD NOT RETRACT. OVERWEIGHT LANDING UNEVENTFUL. ACCOMPLISHED GENERAL VISUAL INSPECTION. CLEANED PROXIMITY SWITCHES. CHECKED OPERATION OF LIMIT SWITCHES. VERIFIED OPERATION OF THE LANDING GEAR SELECTOR VALVE. CYCLED LANDING GEAR 4 TIMES. OPERATIONAL CHECK GOOD PER AMM 32-32-00.

Part: LENS — MISSING (CABIN) · airframe 15,757 hrs · 6,186 cycles

THE AIRCRAFT WAS NOT GROUNDED. FORWARD GALLEY, ISLE EXIT LIGHT MISSING. REMOVED AND REPLACED FWD GALLEY ISLE EXIT LIGHT LENS IAW AMM 33-50-00 OPS CHECK NORMAL.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 15,217 hrs · 5,956 cycles

LENS ON OVERHEAD EMERGENCY EXIT AT ROW 23 LEFT AND 25 RIGHT BROKEN. REMOVED AND REPLACED LENS IAW AMM 33-51-00, GOOD FOR SERVICE.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 14,993 hrs · 5,862 cycles

ON OPENING THE L1 DOOR AT GATE, EMERGENCY SLIDE COVER OPENED AND EMERGENCY SLIDE FELL OUT, DID NOT INFLATE. REINSTALLED SLIDE PACK IAW AMM 25-66-01. THE AIRCRAFT WAS GROUNDED.

Part: COVER — MISSING (EXIT SIGN) · airframe 14,557 hrs · 5,672 cycles

EMERGENCY EXIT SIGN COVER AT 1R DOOR MISSING. REPLACED EMERGENCY EXIT COVER PER M/M 33-51-01 OPS CHECK OK. THE AIRCRAFT WAS NOT GROUNDED.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 14,164 hrs · 5,520 cycles

L1 DOOR SLIDE PACK IS LOOSE. INSTALLED THE SLIDE PACK IAW AMM 25-66-01. OPS CHECKED GOOD.

Part: LATCH — DIRTY (ZONE 800) · airframe 13,773 hrs · 5,375 cycles

AIRCRAFT NOT GROUNDED. R1 EMERGENCY DOOR GIRT BAR IS DIFFICULT TO UNLATCH. CLEANED GIRT BAR LATCH. OPERATIONAL CHECK GOOD.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 8,767 hrs · 3,389 cycles

AIR INTERRUPTED, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE THE R2 WINDOW INNER PANE CRACKED. R & R R2 WINDOW & ASSOCIATED WINDOW HEAT CONTROLLER IAW AMM 30-41-11-000-801 & 30-41-11-400-801. SEE ALSO AALA20150708012.

Part: WINDOW — CRACKED (COCKPIT) · airframe 8,765 hrs · 3,388 cycles

AIR INTERRUPTED, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE THE R2 WINDOW INNER PANE CRACKED. R & R R2 WINDOW & ASSOCIATED WINDOW HEAT CONTROLLER IAW AMM 30-41-11-000-801 & 30-41-11-400-801. SEE ALSO AALA20150710003.