N792AS

Part: HINGE — LACK OF LUBE (L1 DOOR) · airframe 58,198 hrs · 33,102 cycles

FLIGHT ATTENDANT REPORTED L1 DOOR HARD TO CLOSE. ACFT GROUNDED. LUBED DOOR HINGES AND ROLLERS. PERFORMED FORWARD ENTRY DOOR OPERATIONAL TEST. TESTS NORMAL REF B737-400 AMM 52-11-00-705-060.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 57,175 hrs · 32,446 cycles

AFTER STABILIZER REMOVAL FOUND LT HORIZONTAL STABILIZER FWD UPPER ATTACH LUG, STABILIZER SIDE, CORRODED ON AFT FACE. ACFT GROUNDED. REPAIRED LT HORIZONTAL STABILIZER FWD UPPER ATTACH LUG IAW EA CMPT-55EA-16535 FIRST STAGE APPROVAL HAS BEEN GRANTED IAW ASSOCIATED FAA FORM 8100-9, SECOND STAGE APPROVAL IS REQUIRED ON OR BEFORE FEB 08,2018 REFER TO CMPT-55DTI-16537, W 2.9, O 1.140, R 1.067, L 2.9, D .073.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 57,175 hrs · 32,446 cycles

LEFT HORIZONTAL STABILIZER FWD LOWER ATTACH FITTING, STABILIZER SIDE, CORROSION ON FWD FACE. ACFT GROUNDED. REPAIRED LT HORIZONTAL STABILIZER FWD LOWER ATTACH FITTING IAW EA NR COMPARTMENT, 55EA-16544, FIRST STAGE APPROVAL HAS BEEN GRANTED IAW ASSOCIATED FAA FORM 8100-9. SECOND STAGE APPROVAL IS REQUIRED ON OR BEFORE FEB 08, 2018. REFER TO COMPARTMENT-55DTI-16546.

Part: SHEAR TIE — CRACKED (BS 520) · airframe 57,175 hrs · 32,446 cycles

WHILE ACCESSING AREA FOR GROUND AIR CONDITION SKIN REPAIR, NOTICED SHEAR TIE AT BS 520 BETWEEN STR 26L-27L IS CRACKED. ACFT GROUNDED. REMOVED AND INSTALLED NEW SHEAR TIE ANGLE IAW SRM 51-40-02-0G-0.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 57,175 hrs · 32,446 cycles

LEFT WING INBD MIDFLAP, INBD UPPER SURFACE IS CHAFED ON A PREVIOUS REPAIR. ACFT GROUNDED. REPAIRED LT WING INBD MIDFLAP INBD UPPER SURFACE IAW SRM 57-53-01-2R-3, REPAIR 3.

Part: STRAP — CRACKED (BS 312) · airframe 57,175 hrs · 32,446 cycles

FLOORBEAM SUPPORT STRAP CRACKED AT BS 312, RBL 31.60, E & E BAY. ACFT GROUNDED. R & R THE SUPPORT STRAP IAW SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (BS 516-540) · airframe 57,175 hrs · 32,446 cycles

FUSELAGE GROUND AIR CONDITION DOOR CUTOUT SKIN ON RT SIDE IS CRACKED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT THE GROUND AIR CONDTION DOOR CUTOUT IAW SRM 53-30-01-2R-2, REPAIR 2.

Part: BEAR STRAP — CRACKED (BS 303) · airframe 57,174 hrs · 32,446 cycles

FOUND GOUGE/DENT ON INTERIOR FUSELAGE SKIN NEAR UPPER FUSELAGE ASSIST SPRING HINGE SPIGOT. L1 DOOR MIG 2C 317241 INITIATED. ACFT GROUNDED. RESOLVED ON W/O: 321296 TASKCARD: N/R-00011. REPAIRED FUSELAGE SKIN AND BEAR STRAP AT L1 DOOR UPPER HINGE CUTOUT IAW EA 400-53EA-16506. THIS IS A CATEGORY B REPAIR. FIRST STAGE AND SECOND STAGE HAS BEEN GRANTED. THIRD STAGE APPROVAL IS REQUIRED PRIO TO THE INSPECTION THRESHOLD OF 85,000 TOTAL AIRFRAME FLIGHT CYCLES. REFER TO DTIC EC 400-53DTI-16507. CURRENT FLIGHT CYCLES ON ACFT AT TIME OF REPAIR IS 32,446.

Part: GUIDE ARM — LACK OF LUBE (L1 DOOR) · airframe 56,077 hrs · 31,716 cycles

L1 DOOR WOULD NOT OPEN AFTER MULTIPLE ATTEMPS. HANDLE LOCKED IN INTERMEDIATE POSITION AND COULD NOT BE FULLY ROTATE. ACFT GROUNDED. REMOVED DEBRIS AND LUBRICATED GUIDE ARM ECCENTRIC TRACK. DOOR OPERATES NORMALLY.

Part: STRAP — CRACKED (BS 328) · airframe 55,245 hrs · 31,154 cycles

CRACK ON SECONDARY STRAP BELOW FLOORBEAM BS 328 FIRST STRAP LT OF CENTER ABOVE E & E DOOR. ACFT GROUNDED. REMOVED STABILIZER STRAP ABOVE E & E DOOR IAW SRM 51-40-02. INSTALLED NEW STABILIZER STRAP IAW SRM 51-40-02.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 54,469 hrs · 30,697 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN AT R2 DOOR MISSING LENS. ACFT GROUNDED. REPLACED LENS AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.

Part: ATTACH FITTING — CORRODED (FRAMES 55-57) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

AFTER REMOVAL OF RT HORIZONTAL STABILIZER, FOUND THE FWD UPPER LUG CORRODED. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER FWD UPPER LUG IAW EA COMPT-55EA-13723 REV NEW ISSUED 7NOV14 ASSOCIATED FAA FORM 8100-9 PROVIDES FIRST STAGE APPROVAL FOR STATIC STRENGTH. SECOND STAGE APPROVAL REQUIRED WITHIN 24 MOS. OF 29 OCT 14 REFER TO CMPT 55EA 13723, W 2.0", O 1.135", R 1.084", L 2.0", D .051".

Part: INTERCOSTAL — CRACKED (BS 927-947) · airframe 54,126 hrs · 30,507 cycles

AFT CARGO BAY INTERCOSTAL BS 927-947, S26L IS CRACKED. ACFT GROUNDED. REMOVED AND INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-0G-0 PARA 4 AND 7D.

Part: INTERCOSTAL — CORRODED (BS 927-947) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

INTERCOSTAL CORRODED ON BOTTOM SIDE OF UPPER LEG AT STR 24L BETWEEN STA 927 AND 947. FOUND DURING INSTALL OF THE LT TRANSITION PANEL. ACFT GROUNDED. REMOVED CORRODED ON INTERCOSTAL IN AFT PIT AT STR 24L STA 927 AND 947, INTERCOSTAL IS OUT OF LIMITS IAW SRM 53-00-04-1A-1. REMOVED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02-0G-0, FIG 8, PARA 4 AND PARA 7 AND SRM 51-40-05-0G-0, W 1.0" O .032, R .013", L 2.0", D .019".

Part: TEE FITTING — CORRODED (BS 986-1000) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

TEE FITTING FOUND CORRODED ON LOWER SIDE. ACFT GROUNDED. DRILLED AND LOCATED NEW TEE FITTING IAW SRM 51-40-05-0G-0.

Part: STRINGER — CORRODED (BS 1088-1156) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

APU BAY RT BULKHEAD AFT CUTOUT TOP LANDING HAS CORRODED AREA. ACFT GROUNDED. R & R APU COMPARTMENT RT BULKHEAD TOP STR IAW SRM 51-40-02-0G-0.

Part: ATTACH FITTING — CORRODED (BS 193) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

RT HORIZONTAL STABILIZER FWD LOWER LUG HAS CORROSION. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER FWD LOWER LUG IAW EA COMPARTMENT 55 EA, 13726 REV NEW ISSUED 07NOV14 ASSOCIATED FAA FORM 8100-9 PROVIDES FIRST STAGE APPROVAL FOR STATIC STRENGTH. SECOND STAGE APPROVAL REQUIRED WITHIN 24 MOS OF 29OCT14 REFER TO COMPARTMENT -55DTI-13727.

Part: STIFFENER — CORRODED (BS 1115) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

APU BAY RT BULKHEAD AFT CUTOUT FWD LANDING HAS A CORRODED SPOT ON THE BACKSIDE. ACFT GROUNDED. AT APU COMPARTMENT RT BULKHEAD AFT CUTOUT, FWD STIFFENER REMOVED CORRODED OUT OF LIMITS, R & R DAMAGED STIFFENER IAW SRM 53-80-13-1A-2, FIG 101, 51 40-02-0G-0, W 2.00, O .063, R .022, L 2.00, D .041.

Part: STRINGER CLIP — CORRODED (BS 727G) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

AFT CARGO COMPARTMENT STRINGER CLIP AT BS 727G, S25R IS CORRODED. ACFT GROUNDED. R & R THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0.

Part: SUPPORT — CORRODED (BS 727-847) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

AFT CARGO BAY TRANSITION STRIP LT SIDE IS CORRODED IN SEVERAL PLACES FOM BS 727-BS 747. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1, FIG 101, DETAIL V, LOCATED AND DRILLED REPAIR TRANSITION PANEL IAW SRM 51-40-05-0G-0 INSTALLED TRANSITION PANEL IAW SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

AFT CARGO COMPARTMENT FWD ATA 947, L24L TRANSITION ANGLE SUPPORT HAS CORRODED IN NUMEROUS AREAS. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1, FIG 101, DETAIL V, LOCATED AND DRILLED REPAIR TRANSITION PANEL IAW 400 SRM 51-40-05-06-0, INSTALLED TRANSITION PANEL IAW SRM 51-40-02-0G-0.

Part: WEB — CRACKED (BS 986) · airframe 54,126 hrs · 30,507 cycles

R2 DOOR WET AREA FLOOR WEB AT BS 986.5 AND RBL 29 IS CRACKED. ACFT GROUNDED. REMOVED AND INSTALLED THE WEB IAW SRM 51-40-02-0G-0.

Part: SHEAR TIE — CORRODED (BS 500A) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

FWD CARGO BAY BS 500A SHEAR TIE ON FWD SIDE BETWEEN S27-28R HAS CORROSION. ACFT GROUNDED. REPAIRED THE SHEAR TIE IAW SRM 53-00-07-2R-10.

Part: CHANNEL — CORRODED (R2 DOOR) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

RIGHT MOP SILL ON R2 DOOR CUTOUT CORRODED ON SEVERAL AREAS. ACFT GROUNDED. REMOVED, DRILLED, LOCATED AND INSTALLED NEW INNER CHANNEL IAW SRM 51-40-05-0G-0 AND 51-40-020-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 328-344) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

FLOOR SUPPORT BETWEEN 328 AND 344 AT LBL 10 HAS CORRODED AROUND FASTENER HOLE. ACFT GROUNDED. REMOVED DAMAGED FLOOR SUPPORT AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

BS 986.5 FLOORBEAM HAS CORROSION IN SEVERAL AREAS. ACFT GROUNDED. REPAIRED FLOORBEAM UPPER TEE IAW EA 400 53EA, 13713 REV NEW.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

L1 DOOR AFT GIRT BAR ATTACH BRACKET IS CORRODED. ACFT GROUNDED. ATTACH BRACKET FOUND TO BE 100 PERCENT MATERIAL LOSS OUT OF LIMITS IAW SRM 53-10-51-1A-1. R & R BRACKET IAW AMM 20-50-11-912-006, PG 6.

Part: CHANNEL — CORRODED (BS 285-350) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

L1 DOOR MOPSILL HAS CORROSION. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. R & R MOPSILL IAW SRM 51-40-02-0G-0, PAGE 5, ITEM B.

Part: FLOORBEAM — CORRODED (BS 294) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

BS 294, FLOORBEAM AT RBL 10 HAS CORROSION AROUND FASTENER HOLE. ACFT GROUNDED. REPAIRED THE FLOORBEAM IAW SRM 53-10-51-2R-5, REPAIR 5.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

AFT CARGO BAY FLOOR PANEL CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1, FABRICATED A NEW FLOOR PANEL IAW SRM 51-40-05-0G-0.

Part: FITTING — CRACKED (BS 1120) · airframe 54,126 hrs · 30,507 cycles

THRUST BEAM FITTING CRACKED. ACFT GROUNDED. REMOVED AND INSTALLED NEW LT THRUST BEAM FITTING IAW T/C EC SB737-55-1091-400-2.

Part: FLOOR SUPPORT — CORRODED (BS 967) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

FLOOR SUPPORT AT BS 967CORRODED. ACFT GROUNDED. REMOVED AND INSTALLED NEW FLOOR SUPPORT BETWEEN BS 947-967 IAW SRM 51-40-02-0G-0.

Part: ATTACH BRACKET — CORRODED (GIRT BAR) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

L1 DOOR FWD GIRT BAR ATTACH BRACKET IS CORRODED. ACFT GROUNDED. BRACKET FOUND TO BE 100 PERCENT MATERIAL LOSS OUT OF LIMITS IAW SRM 53-10-51-1A-1. R & R THE ATTACH BRACKET IAW AMM 20-50-11-912-006.

Part: SHEAR TIE — CORRODED (BS 500D) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

FWD CARGO BAY AT BS 500D, FWD SIDE OF SHEAR TIE BETWEEN S27L AND S27R CORRODED. ACFT GROUNDED. REPAIRED IAW SRM 53-00-07-2R-17, REPAIR 17.

Part: SHEAR TIE — CORRODED (BS 500A) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

FWD CARGO BAY AT BS 500A BETWEEN S27L AND S27R FWD SIDE OF SHEAR TIE CORRODED. ACFT GROUNDED. REPAIRED SHEAR TIE IAW SRM 53-00-07-2R-17, REPAIR 17.

Part: SHEAR TIE — CORRODED (BS 500E) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

FWD CARGO BAY RT SIDE AT BS 500E ON THE SHEAR TIE AT STRINGER 26R FWD SIDE AREA OF CORRODED. ACFT GROUNDED. REPAIRED THE SHEAR TIE IAW SRM 53-00-07-2R-3. REPAIR 3.

Part: SHEAR TIE — CORRODED (BS 500B) · corrosion level 2 · airframe 54,126 hrs · 30,507 cycles

FWD CARGO BAY RT AT BS 500B AND S26R ON SHEAR TIE FWD SIDE AREA OF CORROSION. ACFT GROUNDED. REPAIRED THE SHEAR TIE IAW SRM 53-00-07-2R, REPAIR 7.

Part: SKIN — CHAFED (LT FLAP) · airframe 54,126 hrs · 30,507 cycles

LEFT INBD MIDFLAP UPPER INBD SKIN CHAFED. ACFT GROUNDED. REPAIRED LT INBD MIDFLAP UPPER INBD SKIN IAW SRM 57-53-01-2R-3, REPAIR 3.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 54,126 hrs · 30,507 cycles

NR 5 SLAT INBD DELAMINATED LOWER SURFACE. ACFT GROUNDED. REPAIRED THE SLAT IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — CHAFED (RT WING) · airframe 54,126 hrs · 30,507 cycles

RIGHT WING INBD EXHAUST GATE UPPER OTBD CORNER IS CHAFED. ACFT GROUNDED. R & R UPPER SKIN IAW SRM 51-40-02-0G-0.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 54,123 hrs · 30,506 cycles

RAMP REPORTED A DENT ON AFT CARGO ALUMINUM FLOOR PANEL BS 802. ACFT GROUNDED. FOUND CRACK AT BASE OF DENT. STOP DRILLED CRACK IAW EA 400-53EA-13447. CLEANED AREA APPLIED TWO LAYERS OF SPEED TAPE. INSTALLED REPAIR DOUBLER IAW EA 400-53EA-13447. REFER SRM 51-70-13-OG-0, FIG 1. MATERIAL USED 2024T3, ALUM .080". REMOVED MANY BLIND FASTENER FROM REPAIR DOUBLER LOCATION. REPAIR DOUBLER REPAIR COMPLETE ACCOMPLISH REPETITIVE INSP OF BLIND FASTENERS FOR SECURITY EVERY 500 FLIGHT HOURS. REPLACE BLIND FASTENERS AS REQUIRED. REMOVED TEMP REPAIR AND ACCOMPLISH PERMANENT REPAIR OF THE SUBJECTED CARGO COMPARTMENT PANEL OR REPLACE PANEL AT HMV.

Part: LINER — OUT OF POSITION (L2 DOOR) · airframe 51,082 hrs · 28,631 cycles

L2 DOOR HITS UPPER CORNER OF BULB SEAL WHEN OPENED. ACFT GROUNDED. REPOSITIONED DOOR LINER BULB SEAL IAW AMM 52-13-21-401-006.

Part: SUPPORT — CORRODED (BS 727D-767) · corrosion level 2 · airframe 51,080 hrs · 28,630 cycles

AFT CARGO RT TRANSITION PANEL CORRODED AROUND NUTPLATES BWTWEEN BS 727D TO 767. R & R CORRODED SECTION.

Part: WEB — CORRODED (BS 793-830) · corrosion level 2 · airframe 51,080 hrs · 28,630 cycles

AFT LOWER CARGO COMPT DOOR THRESHOLD WEB CORRODED UPPER SURFACE BS 793 - 830, R & R WEB.

Part: BEARING — FAILED (LT MLG) · airframe 49,931 hrs · 27,978 cycles

GEAR RETRACTED NORMALLY ON DEPARTURE LT MAIN THEN EXTENDED ON CLIMBOUT. RAN LANDING GEAR DISAGREE CHECKLIST ALL GEAR REMAINED RETRACTED WITH GEAR HANDLE IN UP POSITION. ACFT GROUNDED. REMOVED AND INSTALLED A NEW ACTUATOR PIN AND BEARINGS TO LT MLG UPLOCK LINK ASSY. REQUIRES GEAR SWING REF AMM 32-32-31-404-056 9C (1) (I-K) AND COTTER PINS INSTALLED. NEW LT MLG UPLOCK SENSOR WAS INSTALLED, ACCOMPLISHED TEST OF THE LANDING GEAR POSITION INDICATING AND WARNING SYS AND OPS TEST OF LT MLG IAW AMM 32-61-00-725-001 & OPS CK GOOD.

Part: DOOR — OUT OF RIG (L2) · airframe 49,709 hrs · 27,861 cycles

F/A REPORTS L2 DOOR WILL NOT OPEN. R & R CAM CRANK FWD ROLLER BEARING, AND ON FURTHER INVESTIGATION FOUND AFT BEARING SERVICEABLE. REASSEMBLED CAMPLATE IAW MM 52-13-11-404-014, STEP 3D(10)(B)(1)(2). R & R ROD END BEARING ON GUIDE ARM ASSY. REQUIRED ADJUSTMENT. REMOVED UPPER AND LOWER HINGE COVERS, REMOVED DOOR GUIDES, REMOVED GUIDE ARM BOLT PRESSURE PLATE. BEGAN INITIAL DOOR RIIG IAW MM 52-13-00-705-001. ADJUSTED GUIDE ARM IAW AMM 52-13-00-705-001 3F(2)(A)(B)(C). ADJUSTED STOP PINS IAW AMM 52-13-00-705-0013F(9)(A)(B)(C)(D)(E)(F). ADJUSTED GUIDE, IAW AMM 52-13-00-705-001 3F(10). COMPLETED DOOR RIG IAW AMM 52-13-00-705-001. REINSTALLED L2 DOOR LINER & SLIDE ASSY REF AMM 52-13-21-404-006 & AMM 25-61-35/ 201. ACCOMPLISHED L2 DOOR TEST, TESTED GOOD REF AMM 52-13-00-705-003 & 52-13-00-705-034, ACCOMPLISHED EA 400-52EA-09812, ACCOMPLISHED PRESSURIZATION CK DOOR, CK GOOD REF AMM 05-51-91.

Part: FLIGHT DIR — FAILED (RIGHT MLG WELL) · airframe 48,741 hrs · 27,219 cycles

ON CLIMB, COULD NOT GET LNOV OR VNAV TO ENGAGE AND HAS NO FLT DIRECTOR VERTICAL LINE AND THROTTLES WERE NOT SETTING TO CLIMB MODE. FLT DIRECTOR WOULD WORK IN LEVEL CHANGE AND HEADING. SELECT. AUTOTHROTTLE STAYED IN THR HOLD. FMS STAYED IN T/O MODE. DURING DESCENT CABIN CLIMBED TO 10,000 PERFORMED AN EMERGENCY DESCENT & DECLARED AN EMERGENCY. REPLACED M990 CARD, SENSORS S105/S106 AND GRD SPOILER INTERLOCK CABLE. ATC OPS TESTED, GPWS OPS TESTED & PRESSURE CONTROL SYS OPS TESTED NORMAL. COMPLETED OPS TEST OF A/T SYS, A/T LRU INTERFACE TEST IAW MM 22-00-01 OPS NML, COMPLETED LAND VERIFY TEST IAW MM 22-00-01 OPS NORMAL. ACFT REMAINS CAT 3/HGS. SCREW PLACARD SHOWS SAME.

Part: PLATE — LACK OF LUBE (L1 DOOR) · airframe 46,223 hrs · 25,772 cycles

THE L1 ENTRANCE DOOR IS HARD TO OPEN. FOUND UPPER CAM PLATE WITH NO GREASE. LUBED CAM PLATE REF AMM 12 25 21 643 007. PERFORMED FWD ENTRY DOOR TEST WITHIN LIMITS REF AMM 52 11 00 755 051. OK FOR SERVICE.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,175 hrs · 25,081 cycles

FOUND CORROSION ON AFT SIDE OF BS 1016 LOWER CHORD COMMON TO LT DRAIN HOLE. REPAIRED LOWER CHORD PER ASA EA 400 53EA 05662 AND BFG ER 11 02904.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,175 hrs · 25,081 cycles

FWD SIDE OF AFT PRESSURE BULKHEAD RBL 2 JUST AFT OF BS 1016 CHORD HAS CORROSION ON SKIN UPPER SURFACE. REPAIRED PER ASA EA 400 53EA 05662 AND ER 11 02904.

Part: SKIN — CRACKED (LT WING) · airframe 45,175 hrs · 25,081 cycles

LEFT WING LEADING EDGE CRACKED 2 PLACES AT NR 3 SLAT. REPAIRED BOTH CRACKS IAW ASA EA 400 57EA 05632.

Part: SUPPORT — CRACKED (E&E BAY) · airframe 45,175 hrs · 25,081 cycles

E-BAY RIGHT IRU SHELF DRIP PAN FORWARD SUPPORT IS CRACKED. REMOVED AND REPLACED FORWARD SUPPORT IAW B737 400 SRM 51 40 02.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 45,175 hrs · 25,081 cycles

SEAT TRACK CRACKED AT OUTBOARD UPPER FLANGE FASTENER HOLE. REMOVED AND REPLACED SEAT TRACK SECTION IAW B737 400 SRM 53 00 52.

Part: FILTER — DIRTY (AC BAY) · airframe 41,636 hrs · 23,033 cycles

AT FL 180 WHEN APU GENERATOR PUT ONLINE ON LEFT SIDE VISIBLE SMOKE AND BURNING SMELL IN COCKPIT. APU BLEED WAS CLOSED. SMELL RETURNED AT 7000FT ON DESCENT. REMOVED AND REPLACED HEP A FILTERS LT AND RT ACM'S INSPECTED BEHIND P4 AND P5 PNL'S AND UNDER APU LWR SHROUD. PERFORMED OPERATIONAL CHECKS AND LEAK'S. NO ODOR DETECTED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,633 hrs · 23,031 cycles

STRINGER 20L CORRODED FWD OF 1016. REMOVED AND REPLACED SECTION OF STR 20L STA 994 TO AFT END.

Part: WEDGE — CHAFED (LE SLAT) · airframe 41,633 hrs · 23,031 cycles

NR 1 SLAT T/E WEDGE HAS DEEP CHAFE ON LOWER AFT CENTER AREA. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,633 hrs · 23,031 cycles

FLOORBEAM AT STA 328 RBL 12 HAS CORROSION. REMOVED CORROSION, FABBED REPAIR PARTS AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,633 hrs · 23,031 cycles

AFT PIT SHEAR TIE CORRODED ON AFT SIDE OF FRAME STA 787. REMOVED SHEAR TIE FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 41,633 hrs · 23,031 cycles

FWD PIT BILGE STA 500B ATTACH ANGLE HAS CORROSION BETWEEN STR 28L - 28R. REMOVED CORRODED ANGLE, FABBED REPAIR AND INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,633 hrs · 23,031 cycles

FWD PIT BILGE STA 500A SHEAR TIE IS CORRODED BETWEEN STR 28L - 28R. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND INSTALLED.

Part: SKIN — DENTED (FOREFLAP) · airframe 41,633 hrs · 23,031 cycles

RIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 73 125. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — DENTED (MIDFLAP) · airframe 41,633 hrs · 23,031 cycles

LEFT I/B MID FLAP TRAILING EDGE WEDGE LOWER SKIN HAS A CLUSTER OF DENTS OUT OF LIMITS. REMOVED CORROSION, FABBED REPAIR PARTS AND INSTALLED.

Part: SKIN — DENTED (FOREFLAP) · airframe 41,633 hrs · 23,031 cycles

RIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 121. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — DENTED (FOREFLAP) · airframe 41,633 hrs · 23,031 cycles

RIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 113. REMOVED DAMAGED AREA FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — DENTED (FOREFLAP) · airframe 41,633 hrs · 23,031 cycles

RIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 150. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — DENTED (FOREFLAP) · airframe 41,633 hrs · 23,031 cycles

RIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 124. REMOVED DAMAGED AREA FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — DENTED (SPOILER) · airframe 41,633 hrs · 23,031 cycles

NR 4 SPOILER LOWER SURFACE HAS A CLUSTER OF DENTS 25 INCHES FROM I/B EDGE. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — DENTED (MIDFLAP) · airframe 41,633 hrs · 23,031 cycles

LEFT I/B MID FLAP TRAILING EDGE WEDGE LOWER SKIN HAS A CLUSTER OF DENTS OUT OF LIMITS. PREPPED DAMAGED AREA, FABBED DOUBLER AND BONDED.

Part: WEDGE — DENTED (MIDFLAP) · airframe 41,633 hrs · 23,031 cycles

LEFT I/B MIDFLAP TRAILING EDGE WEDGE HAS A CLUSTER OF DENTS APPROX 31 INCHES 32 INCHES FROM I/B EDGE. PREPPED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — DENTED (TE FLAP) · airframe 41,633 hrs · 23,031 cycles

RIGHT I/B AFT FLAP TRAILING EDGE WEDGE LOWER SURFACE DENTED 5 INCHES FROM WBL 141. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: WEDGE — DENTED (MIDFLAP) · airframe 41,633 hrs · 23,031 cycles

LEFT I/B MIDFLAP TRAILING EDGE WEDGE HAS A CLUSTER OF DENTS APPROX 43 INCHES 49 INCHES FROM I/B EDGE. PREPPED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: WEDGE — DENTED (MIDFLAP) · airframe 41,633 hrs · 23,031 cycles

LEFT I/B MIDFLAP TRAILING EDGE WEDGE HAS A CLUSTER OF DENTS APPROX 5 INCHES 9.75 INCHES FROM I/B EDGE. PREPPED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,633 hrs · 23,031 cycles

FWD PIT SHEAR TIE FRAME ANGLE AT STA 500A BETWEEN STR 27L - 28L. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER AND BONDED.

Part: SKIN — DENTED (FOREFLAP) · airframe 41,633 hrs · 23,031 cycles

RIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 144 154. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 41,633 hrs · 23,031 cycles

NR 1 SLAT O/B TRAILING EDGE IS DELAMINATED AT CORNER. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — CHAFED (LE SLAT) · airframe 41,633 hrs · 23,031 cycles

NR 3 SLAT LOWER T/E CORNER IS CHAFED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.

Part: SKIN — GOUGED (LE SLAT) · airframe 38,544 hrs · 21,191 cycles

NUMBER 2 SLAT LOWER TRAILING EDGE GOUGED. REMOVED DAMAGED SECTION. INSTALLED DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10.

Part: SKIN — DENTED (SPOILER) · airframe 38,544 hrs · 21,191 cycles

RIGHT INBOARD GROUND SPOILER LOWER SURFACE HAS MULTIPLE DENTS WITH DELAMINATION ON INBOARD TRAILING EDGE. REMOVED DAMAGED AREA. INSTALLED DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10.

Part: SKIN — DAMAGED (SPOILER) · airframe 38,544 hrs · 6,035 cycles

RT OUTBOARD GROUND SPOILER HAS PROTRUSION ON UPPER SURFACE AT O/B END ABOVE LOWER BLADE SEAL RETAINER. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND BONDED DOUBLER IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 38,544 hrs · 21,191 cycles

RIGHT INBOARD AFT FLAP UPPER SURFACE DELAMINATED ON OUTBOARD END. REMOVED DAMAGED AREA. BOND REPAIRED WITH REPAIR PARTS PER SRM 51 70 10.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 38,544 hrs · 6,035 cycles

NR 5 SPOILER UPPER SURFACE HAS MULTIPLE DENTS IN CLUSTERS. PREPPED DAMAGED AREA, FABRICATED REPAIR PARTS BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DAMAGED (RT SPOILER) · airframe 38,544 hrs · 21,191 cycles

RT OUTBOARD GROUND SPOILER HAS PROTRUSION ON UPPER SURFACE AT O/B END ABOVE LOWER BLADE SEAL RETAINER. PREPPED DAMAGED AREA, FABBED REPAIR DOUBLER AND BONDED DOUBLER IAW B737 400 SRM 51 70 10 REP 2.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,544 hrs · 21,191 cycles

RIGHT INBOARD AFT FLAP LOWER SURFACE HAS CLUSTER OF DENTS. BOND REPAIRED DAMAGED AREA PER SRM 51 70 06.

Part: SKIN — CHAFED (FOREFLAP) · airframe 38,544 hrs · 21,191 cycles

RIGHT OUTBOARD FOREFLAP PREVIOUS REPAIR CHAFED ON UPPER SURFACE AT INBOARD END. REMOVED DAMAGED AREA. INSTALLED DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10.

Part: SKIN — DENTED (GROUND SPOILER) · airframe 38,544 hrs · 21,191 cycles

RIGHT INBOARD GROUND SPOILER IS DENTED ON LOWER INBOARD SURFACE 6 INCHES FROM INBOARD END. REMOVED DAMAGED AREA. INSTALLED DOUBLER FILLER AND BOND REPAIRED PER SRM 51 70 10.

Part: SKIN — CHAFED (MIDFLAP) · airframe 38,544 hrs · 21,191 cycles

LEFT INBOARD MIDFLAP UPPER SURFACE CHAFED AT INBOARD END 15 INCHES FORWARD OF TRAILING EDGE. REMOVED DAMAGED AREA. INSTALLED DOUBLER FILLER AND BOND REPAIR PER SRM 57 53 01 AND 51 70 10.

Part: SKIN — DENTED (NR 4 SPOILER) · airframe 38,544 hrs · 6,035 cycles

NR 4 SPOILER HAS A DENT ON LOWER SURFACE 2 INCHES O/B OF I/B END 8.5 INCHES FWD OF TRAILING EDGE. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, AND BONDED THE REPAIR IAW SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (FOREFLAP) · airframe 38,544 hrs · 21,191 cycles

LEFT INBOARD FOREFLAP HAS CLUSTER OF DENTS ON LOWER SURFACE OUTBOARD OF INBOARD TRACK. REMOVED DAMAGED AREA. REPAIRED WITH DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10.

Part: SKIN — DENTED (RT WING LE) · airframe 38,544 hrs · 21,191 cycles

RIGHT WING INBOARD LEADING EDGE DENTED. REMOVED DAMAGED AREA. INSTALLED DOUBLER AND FILLER PER SRM 57 41 01.

Part: SKIN — DAMAGED (NR 4 K FLAP) · airframe 38,544 hrs · 21,191 cycles

RIGHT FIXED LEADING EDGE DAMAGED, NO SPECIFICS AT NR 4 K FLAP ACTUATOR LOWER EDGE. REMOVED DAMAGED AREA. INSTALLED DOUBLER AND FILLER PER SRM 57 41 01.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 38,544 hrs · 6,035 cycles

RT OUTBOARD AFT FLAP PREVIOUS REPAIR IS DELAMINATED ON INSIDE UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED REPAIR IAW B737 400 SRM 51 70 10.

Part: SKIN — PUNCTURED (SPOILER) · airframe 34,869 hrs · 19,151 cycles

NR 4 GROUND SPOILER HAS HOLE NEAR THE TRAILING EDGE. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND SKIN IAW SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (FORE FLAP) · airframe 34,869 hrs · 19,151 cycles

LT IB FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE JUST OB OF IB TRACK. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND SKIN IAW SRM 51 70 10 PG 201.

Part: SKIN — DENTED (FORE FLAP) · airframe 34,869 hrs · 19,151 cycles

LT IB FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE OB OF MIDDLE TRACK. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10 PG 201.

Part: SKIN — DENTED (AFT FLAP) · airframe 34,869 hrs · 19,151 cycles

RT OB AFT FLAP HAS 2 EACH DENTS AT OB END OF UPPER SURFACE. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (FLAP) · airframe 34,869 hrs · 19,151 cycles

DENT ON TOP SURFACE OF RT IB AFT FLAP. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND SKIN IAW SRM 51 70 10 PG 201.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,869 hrs · 19,151 cycles

FWD CARGO DOOR LOWER SILL WEB IS CRACKED. REMOVED CRACKED WEB FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 51 40 2 AND 51 20 01.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,869 hrs · 19,151 cycles

TWO DENTS ON FUSELAGE SKIN, DENTS IN ADJACENT BAYS. CUT OUT DAMAGED SECTIONS OF SKIN, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW ASA EA 5330 02231.

Part: SKIN — DENTED (FORE FLAP) · airframe 34,869 hrs · 19,151 cycles

SEVERAL DENTS ON LOWER SURFACE OF RIGHT I/B FORE FLAP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED SKIN FILLER AND DOUBLER IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (E&E BAY DOOR) · airframe 34,869 hrs · 19,151 cycles

E&E COMPARTMENT DOOR DENTED ON RRIGHT EDGE. REMOVED DENTED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-30-01, 51-40-01 AND 51-40-02.

Part: SKIN — DENTED (MID FLAP) · airframe 34,869 hrs · 19,151 cycles

LEFT O/B MID FLAP HAS 3 EACH DENTS ON TOP SURFACE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED SKIN FILLER AND DOUBLER IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,795 hrs · 17,960 cycles

FASTENER HOLE DAMAGED WHILE REWORKING LIGHTNING STRIKE AT STA 312 WL 186 ON FUSELAGE SKIN LEFT SIDE. REF LOG PG 6219267 & EA 5310 02686 CUT OUT DAMAGED AREAS ON SKIN & FRAME AT FASTENER HOLE. INSTALLED REPAIR DOUBLERS.

Part: WASHER — MISSING (L-1 DOOR) · airframe 32,617 hrs · 17,874 cycles

L 1 DOOR HARD TO CLOSE INSTALLED MISSING THRUST WASHER (TORQUE TUBE THRUST WASHER) ON LWR HINGE ASSY AND ADJUSTED DOOR PER AMM.

Part: GUIDE ARM — OUT OF ADJUST (PAX DOOR) · airframe 31,306 hrs · 17,161 cycles

ON DESCENT AFT ENTRY DOOR ILLUM'D LIGHTS EXTINGUISHED PRIOR TO LANDING. PRESSURIZATION NORMAL. DOOR LIGHT ILLUM AT CABIN DIFF PRESS OF 1.6 PSI AND WENT OUT AT .5 PSI. ADJUSTED GUIDE ROD PER AMM 52 13 00.

Part: STRUCTURE — CORRODED (BS 773-858) · corrosion level 2 · airframe 31,284 hrs · 17,150 cycles

FOUND CORROSION ON PREVIOUS REPAIR FOR DOOR OPENING STRUCTURE AT BSTA 797 STR 25R H. RECEIVED LOCATED AND DRILLED NEW STRAP PER SRM 51 40 05 PG 5 7 AND 51 40 08 PG 1. INSTALLED NEW STRAP PER SRM 51 40 02 PG 1 3.

Part: SKIN — DENTED (RT WING) · airframe 31,284 hrs · 17,150 cycles

RT WING T/E O/B AFT FLAP T/E DENTED A=1.4 Y=.089 A Y=15.73. REMOVED REPAIRED AND REINSTALLED RT WING OB AFT FLAP IAW SRM 51 70 10 57 53 02.

Part: FRAME — PUNCTURED (BS 787) · airframe 31,284 hrs · 17,150 cycles

FOUND FASTENER AT STA 787 ABOVE ATR 25R HAS GOUGED TOP OF FRAME. REMOVED DAMAGED PART OF FRAME AND INSTALLED REPAIR PARTS IAW SRM 51 70 11 FIG 1.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,377 hrs · 15,074 cycles

CORROSION AT R-2 DOOR MOP SILL. REMOVED AND REPLACED MOP SILL. (K)

Part: FRAME — DENTED (AFT CARGO BAY) · airframe 27,377 hrs · 15,074 cycles

FRAME UPPER CHORD DENTED AFT CARGO BAY B-STA 787 BETWEEN STR 24R AND 25R. REPAIRED FRAME. (K)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,377 hrs · 15,074 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT LWR SURFACE. REMOVED AND REPLACED. (K)

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 27,377 hrs · 15,074 cycles

CORROSION ON FWD ENTRY DOOR THRESHOLD ZEE CHANNEL. REMOVED AND REPLACED. (K)

Part: FITTING — CORRODED (CARGO DOOR FRAME) · airframe 27,377 hrs · 15,074 cycles

CORROSION ON LT AFT ENTRY DOOR CUTOUT IB FWD SIDE OF CUTOUT JUST AFT OF UPPER FWD LATCH FITTING. REMOVED AND REPLACED FITTING. (K)

Part: FRAME — DENTED (AFT CARGO BAY) · airframe 27,377 hrs · 15,074 cycles

FRAME UPPER CHORD DENTED AFT CARGO BAY S-STA 787 BETWEEN STR 24R AND 25R. REPAIRED FRAME. (K)

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,377 hrs · 15,074 cycles

CORROSION ON FWD LAV SUPPORT FITTING. REMOVED AND REPLACED FWD LAV SUPPORT FITTING. (K)

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,377 hrs · 15,074 cycles

CORRODION LAV ATTACH FITTING. REMOVED AND REPLACED. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,377 hrs · 15,074 cycles

VERTICAL ANGLE CRACKED AT B-STA 601, RBL 64, WI 204, AND B-STA 601 FRAME. CUT OUT DAMAGED SECTION OF 601 FRAME AND FABRICATED REPAIR ANGLE IAW EA 5330-01934, ER 05-2867. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,377 hrs · 15,074 cycles

FRAME CRACKED AT HAT RACK ATTACH POINT. REPAIRED CRACKED FRAME AT HAT RACK ATTACH POINT. (K)

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2

CORROSION AFT CARGO BAY, TIE DOWN ON FLOOR TRACK. REMOVED DAMAGE AND INSTALLED NEW TRACK IAW SRM. (K)

Part: BEAM — CRACKED (RUDDER) · airframe 27,377 hrs · 15,074 cycles

RT VERTICL T/E BEAM AT RUDDER STA 13.33 CRACKED. REMOVED, FABRICATED AND INSTALLED VERTICAL RT T/E BEAM. (K)

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,377 hrs · 15,074 cycles

FRAME CRACKED AT HAT RACK ATTACH POINT. REPAIRED CRACKED FRAME AT HAT RACK ATTACH POINT. (K)

Part: BEAM — CRACKED (FUSELAGE) · airframe 27,377 hrs · 15,074 cycles

RT VERT T/E BEAM CRACKED AT STA 13.33. REMOVED AND REPLACED. (K)

Part: FRAME — CRACKED (FUSELAGE)

PAE - FOUND FRAME CRACKED AT HAT RACK ATTACH POINT. REPAIRED FRAME AT HAT RACK ATTACH POINT. (M)

Part: FRAME — CRACKED (FUSELAGE)

PAE - FOUND FRAME CRACKED AT HAT RACK ATTACH POINT. REMOVED DAMAGED ARM, FABRICATED REPAIR PARTS AND INSTALLED. (M)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AT FORWARD CARGO BAY, FLOOR TO AFT BULKHEAD SUPPORT ANGLE. REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AT L2 DOOR MOPSILL. REMOVED AND REPLACED. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AT R2 DOOR MOPSILL. REMOVED AND REPLACED. (M)

Part: STIFFENER — CRACKED (FUSELAGE)

PAE - FOUND CENTER FUEL STIFFENER IS CRACKED. INSTALLED NEW STIFFENER. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON SHEAR TIE. BLENDED SHEAR TIE, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED A REPAIR PER SRM. (M)

Part: SILL — CORRODED (FUSELAGE)

PAE - FOUND CORROSION FORWARD ENTRY DOOR MOP SILL AT BS 310-344, LBL 56, WL 208. REMOVED AND REPLACED FORWARD ENTRY DOOR MOP SILL. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LEFT FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED SIDEWALL SUPPORT. (M)

Part: WEB — DAMAGED (FUSELAGE)

PAE - FOUND WEB DAMAGED AT AFT CARGO DOOR CUTOUT. REMOVED, FABRICATED AND INSTALLED WEB. (M)

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

PAE - FOUND CARGO BAY, BS 500F, STRINGER 26R SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT ANGLE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

FOUND STATION 727 BULKHEAD BRACKET IS CRACKED AT BS 727, RBL 5, WL 145. REMOVED AND REPLACED. (M)

Part: ATTACH FITTING — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AT LAVATORY ATTACH FITTING. REMOVED AND REPLACED ATTACH FITTING. (M)

Part: ATTACH FITTING — CORRODED (FUSELAGE)

PAE - FOUND CORROSION AT LAV ATTACH FITTING, BS 947. REMOVED AND REPLACED ATTACH FITTING. (M)

Part: STRINGER CLIP — DAMAGED (FUSELAGE)

PAE - FOUND STRINGER CLIP HAS 1 EXTRA HOLE. REMOVED AND REPLACED STRINGER CLIP. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

PAE - FOUND STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON LOWER SUPPORT FITTING. REMOVED AND REPLACED FITTING. (M)

Part: STRINGER CLIP — DAMAGED (FUSELAGE)

PAE - FOUND STRINGER CLIP HAS FIGURE 8 HOLE. REMOVED AND REPLACED STRINGER CLIP. (M)

Part: ANGLE — CORRODED (FUSELAGE)

PAE - FOUND CORROSION ON GALLEY DOOR THRESHOLD SUPPORT ZEE ANGLE. REMOVED AND REPLACED ZEE ANGLE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

OAK - FOUND AFT CARGO COMPARTMENT, FLOOR SUPPORT ZEE ANGLE CORRODED BEYOND SERVICABLE LIMITS, STATION 727 TO 767 RT. REPLACED ZEE ANGLE SUPPORT AND SUPPORT SPLICES. (M)

Part: BRACKET — CRACKED (RT PYLON)

OAK - FOUND RIGHT ENGINE PYLON ANGLE BRACKET IS CRACKED. REMOVED CRACKED BRACKET AND INSTALLED NEW ANGLE BRACKET ON RIGHT ENGINE PYLON. (M)

Part: FRAME — CORRODED (FUSELAGE)

OAK - FOUND AFT CARGO COMPARTMENT, FRAME AT STATION 767 CORRODED ON FORWARD SIDE FROM STRINGER 25R TO BL 0. REPAIRED FRAME IAW SRM 53-00-07 PAGE 210-212. (M)

Part: WARNING LIGHT — ILLUMINATED (STARTER VALVE)

CLIMBING OUT OF FL 140 NR 3 START VALVE LIGHT ILLUMINATED. PERFORMED QRH STARTER VALVE OPEN LIGHT ILLUMINATED CHECKLIST. TRANSFERRED TO DMI 2699 IAW ENA B727 MEL 80-1-1. CAT "C" PLACARDS INSTALLED.

Part: SKIN — GOUGED (CENTER TANK)

JNU - DURING CHECK, FOUND GAUGE IN CENTER FUEL TANK SKIN ABOVE RIGHT PACK TURBO FAN VALVE. REPAIRED IAW EA. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

SEA - DURING C-CHECK, FOUND STATION 847 TO 867 AND RBL 19 THRESHOLD SUPPORT STRAP AND STRUCTURE CORRODED. REMOVED AND REPLACED IAW SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

SEA - DURING C-CHECK, FOUND Z-ANGLE CORRODED AT BS 767 TO 793 AND RBL 23. REMOVED AND REPLACED IAW SRM. (M)

Part: ANGLE — CRACKED (FUSELAGE)

SEA - DURING C-CHECK, FOUND AFT END OF Z-ANGLE CRACKED AT BS 792 AND RBL 23. REMOVED AND REPLACED IAW SRM. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

SEA - DURING C-CHECK, FOUND INTERCOSTAL AT BS 847-867 AND RBL 25 AND WL 160 CORRODED. REMOVED AND REPLACED IAW SRM. (M)

Part: ANGLE — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT RT Z-ANGLE HAS HEAVY CORROSION FROM STATION 727 TO 767. REMOVED AND REPLACED IAW SRM. (M)

Part: WIRE — DISCONNECTED (CABIN)

YVR - DURING LINE CHECK INSPECTION, FOUND EMERGENCY FLOOR EXIT LIGHTS INOPERATIVE AT AFT OVERWING EXIT ROW 17ABC, WIRE DISCONNECTED. RECONNECTED WIRING ON TRACK LIGHT ASSEMBLY, OPS CHECKED NORMAL. (M)

Part: WIRE — DISCONNECTED (MID CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTING AT ROWS 14-17 WAS FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND THE LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/CONNECTION AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 13-19 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

ANC - PRIOR TO FLIGHT 82, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13-15 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 13 - 17)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 13-17 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 14 - 17)

SEA - PRIOR TO FLIGHT 464, THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 14-17 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: STRAP — BROKEN (BS 727A)

SEA - DURING SCHEDULED C-CHECK, THE AIRCRAFT CARGO COMPARTMENT STATION 727A REINFORCEMENT STRAP UNDER UPPER FLANGE WAS FOUND TO BE BROKEN. REPAIRED PER EA 5310-01800. (M)

Part: ATTACH FITTING — DAMAGED (CARGO DOOR)

SEA - DURING SCHEDULED C-CHECK, THE AFT CARGO DOOR ATTACH LUG FOR THE SNUBBER WAS FOUND TO BE DAMAGED. REPAIRED PER EA 5230-01106. (M)

Part: WIRE — DISCONNECTED (ROW 19)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERABLE AT ROWS 15-19. RECONNECTED WIRING AND LIGHTS AT ROW 19 AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — LOOSE (ROWS 14-18)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 THROUGH 18 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROWS 14-17)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14-17 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACKS — DISCHARGED (CABIN)

PDX - DURING MAINTENANCE CHECK, FOUND THAT THE EMERGENCY EXIT LIGHT SWITCH HAD BEEN LEFT ON AND SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE. REPLACED ALL BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)

Part: BATT CHARGER — FAILED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 2-6 AND LOWER EXIT IDENTIFIER WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 2-6 AND LOWER EXIT IDENTIFIER WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AND LIGHTS OPERATED NORMALLY. (M)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM THE FORWARD CLOSET TO ROW 8. REPLACED BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. (X)

Part: BATTERY — DISCHARGED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM THE FORWARD CLOSET TO ROW 8. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 18. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)