N924DN

Part: CYLINDER — BYPASSING (MLG) · airframe 48,122 hrs · 31,871 cycles

ON CLIMBOUT GOT LEFT GEAR UNSAFE LIGHT W/ ASSOCIATED AUTO SPOILER FAIL MESSAGE ON OAP. EXECUTED QRH 4.16 PROCEDURE & LOWERED GEAR AT 230 IAS. GEAR INDICATIONS NORMAL, HOWEVER AUTO SPOILER FAIL ANNUNCIATOR REMAINED THRU LANDING. ANNUNCIATOR WENT AWAY ONCE WE SWAPPED POWER ON SHUTDOWN. CONTINUED FROM ABOVE, AND WAS ABLE TO ARM THE SPOILER HANDLE. JACKED A/C. FOUND LT RETRACT CYLINDER BYPASSING. REPLACED RETRACT CYLINDER PER MD90 AMM 32-33-01 OPS AND LEAK CHK GOOD. (LP# 4989006)

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 47,004 hrs · 31,146 cycles

WIRE BROKEN ON THE LEFT SIDE ABOVE CATWALK, AFT EMERGENCY LIGHT. REMOVED THE DAMAGED PORTION OF THE WIRE AND INSTALLED A NEW CONNECTOR IAW AMM 20-50. OPS CHECKED GOOD.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 47,004 hrs · 31,146 cycles

CRACKED SKIN ON THE LEFT SIDE OF VERTICAL FIN, 3 INCHES IN LENGTH. REMOVED DAMAGE IAW SRM 55-30-05. FABRICATED A FILLER AND INSTALLED A DOUBLER IAW SRM 55-30-05.

Part: ANGLE — CRACKED (BS 1475) · airframe 47,004 hrs · 31,146 cycles

ANGLE CRACKED AT BS 1475. REMOVED AND REPLACED THE ANGLE AT LONGERON 2L IAW DRAWING 9964460.

Part: ANGLE — CRACKED (BS 1472) · airframe 47,004 hrs · 31,146 cycles

ANGLE CRACKED AT BS 1472, LONGERON 2R. REMOVED AND REPLACED THE ANGLE IAW DRAWING 9964460.

Part: INTERCOSTAL — CRACKED (TAILCONE) · airframe 47,004 hrs · 31,146 cycles

TAILCONE INTERCOSTAL CRACKED BELOW RUDDER ACTUATOR ROD END AT BS 1567. FABRICATED A NEW INTERCOSTAL AND INSTALLED.

Part: SKATE ANGLE — CRACKED (RAM AIR INLET) · airframe 47,004 hrs · 31,146 cycles

RAM AIR INLET INTERNAL SKATE ANGLE HAD AN EIGHT INCH CRACK AT AFT END. REPLACED THE SKATE ANGLE.

Part: ANGLE — CRACKED (RAM AIR INLET) · airframe 47,004 hrs · 31,146 cycles

RAM AIR INLET RIGHT INTERNAL SKATE ANGLE HAD A 01 INCH CRACK AT AFT END. REMOVED AND REPLACED THE ANGLE IAW DWG 5912188.

Part: FRAME — CRACKED (RT MLG WW) · airframe 46,465 hrs · 30,826 cycles

RIGHT MAIN LANDING GEAR FORWARD FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM 51-30-02 AND 51-30-05. OPERATION CHECKS GOOD.

Part: LANYARD — BROKEN (L1 DOOR SLIDE) · airframe 44,321 hrs · 29,567 cycles

BROKEN LANYARD ON L1 DOOR SLIDE. REPLACED THE LANYARD IAW MM.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 44,321 hrs · 29,567 cycles

CRACKED INTERCOSTAL ON AFT FRAME BETWEEN BEAMS 4 AND 5. REPLACED IAW SRM 51-30-02.

Part: FRAME — CORRODED (BS 1344) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON FRAME BS 1344 BETWEEN LONGERONS 29R AND 29L. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-0-02 AND 51-10-03.

Part: FRAME — CORRODED (BS 1326) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON FRAME BS 1326 BETWEEN LONGERONS 29L TO 29R. REPAIRED IAW SRM 53-10-02.

Part: WEB — CRACKED (BS 1520) · airframe 44,321 hrs · 29,567 cycles

CRACK ON WEB, BS 1520. REPAIRED IAW SRM 51-11-03.

Part: RISER — CORRODED (AIRSTAR STEP) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON RISER OF STEP NR 13 AT VENTRAL STAIRWAY. REPLACED IAW SRM 51-30-02.

Part: RISER — CORRODED (AFT STAIRWAY) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON INBOARD PLATES, RISERS AND STEP SETTLEMENTS OF AFT STAIRWAY. FOUND TO BE OUT OF LIMITS. REPLACED STEP RISER IAW ERA 465163-14, REV F, AND SRM 51-30-02.

Part: BELLCRANK — CRACKED (PAX DOOR) · airframe 44,321 hrs · 29,567 cycles

CRACKED ON INNER SUPPORT LOWER BELLCRANK AT AFT ENTRANCE STAIRWELL DOOR. REPLACED IAW SRM 51-30-01.

Part: FLOOR SUPPORT — CORRODED (BS 693-750) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON FLOOR SUPPORT, BS 693 - 750. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-05.

Part: SPACER — CORRODED (DOOR FRAME) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON PREVIOUS REPAIR SPACER ON MID CARGO COMPARTMENT DOOR FRAME BEAM BETWEEN BS 700-746. REPLACED THE SPACER IAW SRM 53-60-02 AND 51-0-05.

Part: LONGERON — CRACKED (BS 984) · airframe 44,321 hrs · 29,567 cycles

CRACK ON LONGERON 6L, BS 984. REPAIRED THE LONGERON IAW SRM 53-10-01.

Part: SKIN — CRACKED (BS 1531) · airframe 44,321 hrs · 29,567 cycles

FUSELAGE SKIN CRACKED BS 1531 BETWEEN LONGERONS 22 TO 25L. AREA WAS REPAIRED IAW SRM 53-00-01.

Part: FLOOR SUPPORT — CORRODED (BS 688) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON FLOOR SUPPORT, BS 688, LONGERONS 29 TO 30R. REPLACED THE FLOOR SUPPORT IAW SRM 51-30-05, AND DWG 3957317.

Part: STRUCTURE — CRACKED (BS 693) · airframe 44,321 hrs · 29,567 cycles

CRACK AT BS 693 AND BEAM NR 1. REPAIRED IAW SRM 52-30-02.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 44,321 hrs · 29,567 cycles

HORIZONTAL STABILIZER LEADING EDGE DELAMINATED ON LEADING EDGE GEARED TAB, XE 95, RIGHT ELEVATOR. REPAIRED THE ELEVATOR IAW SRM 55-21-01.

Part: PAN — CRACKED (AFT CARGO DOOR) · airframe 44,321 hrs · 29,567 cycles

AFT CARGO BAY DOOR HAS A CRACKED INNER PAN AT BEAM NR 5 AFT SECTION. REPAIRED THE PAN IAW SRM 52-30-02.

Part: SEAT TRACK — WORN (BS 237-279) · airframe 44,321 hrs · 29,567 cycles

WEAR ON SEAT TRACK, RBL 22 FROM BS 237 - 279. REPAIRED THE SEAT TRACK IAW SRM 51-10-05, AND 53-40-01.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON ACCESS PANELS 620AT, 620CT, AND 620DT. OUT OF LIMITS. REPLACED THE ACCESS PANELS IAW SRM 57-00-04.

Part: MEMBRANE — CRACKED (BS 512) · airframe 44,321 hrs · 29,567 cycles

CRACKED MEMBRANE BS 215, RBL 22. REPAIRED IAW SRM 53-00-01, AND 51-30-02.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON ACCESS PANELS 520DT, 520EB, AND 520DB. OUT OF LIMITS. REPLACED THE ACCESS PANELS IAW SRM 57-00-04.

Part: SKIN — CRACKED (BS 1522) · airframe 44,321 hrs · 29,567 cycles

CRACKED FUSELAGE SKIN, BS 1522 BETWEEN LONGERONS 1 TO 2R. REPAIRED THE SKIN IAW SRM 53-00-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON FLOOR SUPPORT, RIGHT HAND/ LEFT HAND STA 1364-1407, X=-46, X=46. FOUND TO BE OUT OF LIMITS. INSTALLED NEW SUPPORTS IAW SRM 51-30-05.

Part: CUSP WEB — CORRODED (BS 1238) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON CUSP WEB, BS 1238 BETWEEN RBL 44 TO 60. CUTOUT CRACKS. REPAIR FABRICATED AND INSTALLED IAW SRM 51-30-01, 51-30-02, AND 51-30-08.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON FLOORBEAM, BS 200, BETWEEN RBL 22 TO 54. REPAIRED IAW SRM 51-10-05, 51-30-02, AND 51-30-05.

Part: VANE — DENTED (LT WING TE FLAP) · airframe 44,321 hrs · 29,567 cycles

LEFT WING INBOARD FLAP GUIDE VANE DENTED. REPAIRED THE GUIDE VANE IAW SRM 57-20-05, FIG 5.

Part: FLOORBEAM — CORRODED (BS 200) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON FLOORBEAM, BS 200 AND RBL 54. REPLACED THE FLOORBEAM IAW SRM 51-30-02, 51-30-05, AND 51-10-03.

Part: ANGLE — CRACKED (L1 DOOR) · airframe 44,321 hrs · 29,567 cycles

L1 DOOR HAS CRACKED ANGLE LOWER SECTION INTERNAL STRUCTURE. REPLACED THE ANGLE IAW SRM 51-30-02 AND 51-30-04.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 44,321 hrs · 29,567 cycles

WEAR ON AFT CARGO DOOR FORWARD & AFT LOWER DOUBLERS. REPLACED THE DOUBLERS IAW SRM 51-30-02.

Part: SKIN — WORN (CARGO DOOR) · airframe 44,321 hrs · 29,567 cycles

FORWARD CARGO DOOR WORN ON THE EXTERNAL SKIN LOWER EDGE. REPAIRED THE SKIN IAW ERA 397553-14, REV O.

Part: DOUBLER — WORN (R1 DOOR) · airframe 44,321 hrs · 29,567 cycles

R1 DOOR WORN ON STRAP OVER WEB LOCATED AFT EDGE BEAM 2. DOUBLER WAS REPLACED IAW SRM 51-30-02, 51-30-05 AND 51-30-04.

Part: PAN — CRACKED (CARGO DOOR) · airframe 44,321 hrs · 29,567 cycles

CRACK ON OUTER PAN BELOW FORWARD NR 3 STOP FITTING AT MID CARGO DOOR. REMOVED THE CRACK IAW SRM 52-30-02. FABRICATED AND INSTALLED A DOUBLER IAW SRM 52-30-02.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON FLOOR SUPPORT FROM BS 160-200, RBL 44. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-05, 51-30-02, AND 51-30-05.

Part: BRACKET — CORRODED (R1 DOOR) · airframe 44,321 hrs · 29,567 cycles

R1 DOOR BRACKET CORRODED ON LOWER SECTION. REPLACED THE BRACKET IAW SRM 51-30-02 AND DWG 5961803, REV BS.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 44,321 hrs · 29,567 cycles

ELONGATED HOLES ON FUEL TANK ACCESS PANEL 520QB. REMOVED, FABRICATED AND INSTALLED BUSHINGS IAW SRM 57-00-04.

Part: ATTACH ANGLE — CRACKED (R1 DOOR) · airframe 44,321 hrs · 29,567 cycles

R1 DOOR HAD A CRACKED ANGLE THAT ATTACHES THE BEAM FITTING WITH THE PAN. REPLACED IAW DWG 9911579, REV L

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 44,321 hrs · 29,567 cycles

VERTICAL STABILIZER LEADING EDGE HAD AN ELONGATED HOLE ON LEFT LOWER EDGE. REPAIRED IAW SRM 55-30-05.

Part: SKIN — CRACKED (WING) · airframe 44,321 hrs · 29,567 cycles

CRACKS ON LEADING EDGE OF EXTERNAL LOWER SKIN AT WING FUELING CONTROL ACCESS CUTOUT NEAR SLAT TRACK. REPAIRED IAW SRM 57-20-01. (LP# 2912523)

Part: FLOOR SUPPORT — CORRODED (BS 210) · airframe 44,321 hrs · 29,567 cycles

CORROSION ON FLOOR SUPPORT BS 210, LBL 22. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 51-30-02, AND 51-10-05.

Part: BEAM — CRACKED (L1 DOOR) · airframe 44,321 hrs · 29,567 cycles

L1 DOOR HAD A CRACKED NR 1 BEAM AT FORWARD AFT SECTION. REPAIRED IAW SRM 52-10-02.

Part: BEAM — CRACKED (L1 DOOR) · airframe 44,321 hrs · 29,567 cycles

L1 DOOR HAD A CRACKED NR 2 BEAM ON FORWARD SECTION. REPAIRED IAW SRM 52-10-02.

Part: BEAM — CRACKED (R1 DOOR) · airframe 44,321 hrs · 29,567 cycles

R1 DOOR CRACK ON BEAM NR 4, FORWARD EDGE. BEAM WAS REPLACED IAW SRM 51-30-01, 51-30-02 AND 51-30-05. (LP# 2910045)

Part: CONTROL WHEEL — JAMMED (COCKPIT) · airframe 44,321 hrs · 29,567 cycles

AUTO CABIN PRESSURIZATION FAILED AFTER TAKEOFF. CABIN ALT. CONTROL WHEEL APPEARED TO BE JAMMED. FOLLOWED QRH AND WAS ABLE TO UNJAM AND OPERATE MANUALLY. PERFORMED RTS. SYSTEM OPERATES SMOOTH AND NORMALLY.

Part: FITTING — OUT OF ADJUST (CABIN) · airframe 44,321 hrs · 29,567 cycles

FOUND NR 3 AND NR 7 FITTINGS NEED ADJUSTMENT. REPAIRED IAW ERA 555253-14, REV O.

Part: LANYARD — DETACHED (EVAC SLIDE) · airframe 44,084 hrs · 29,435 cycles

R1 DOOR SLIDE PACK GIRT BAR LANYARD DETACHED. ATTACHED IAW MM. OPERATION CHECKS GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 43,539 hrs · 29,123 cycles

OVERWING CEILING EMERGENCY EXIT COVER MISSING. INSTALLED THE COVER.

Part: LIGHT — DAMAGED (CABIN) · airframe 43,428 hrs · 29,056 cycles

EMERGENCY LIGHT DAMAGED. INSTALLED A NEW EMERGENCY LIGHTING STRIP. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,428 hrs · 29,056 cycles

EMERGENCY LIGHTING DAMAGED. INSTALLED A NEW EMERGENCY LIGHT. OK FOR SERVICE.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,159 hrs · 28,886 cycles

RT FWD OVER WING EXIT DOOR PAN CRACKED ON FWD SIDE AT 2ND FROM BOTTOM BEAM SUPPORT BRACKET. ACCOMPLISHED ALL STEPS OF AND REPAIRED IAW ERA 549975-14.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 43,159 hrs · 28,886 cycles

FUSELAGE SKIN SPLICE PLATE CORRODED BETWEEN L29L AND L30, STA 1241. ACCOMPLISHED ALL STEPS OF AND REPAIRED IAW ERA 550060-14.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,159 hrs · 28,886 cycles

CORROSION INSIDE FRAME LOWER J-ANGLE OF FLOOR SUPPORT AFT SIDE OF STA 1307 FROM L29L TO L27R. REPLACED CORRODED FRAME SEGMENT IAW SRM 53-10-02, FIG 2. LP 2658230.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 43,552 hrs · 29,130 cycles

AFT CARGO COMPARTMENT CORRODED INTERCOSTAL STA 1288-1307 ON TOP OF L30. REMOVED AND REPLACED INTERCOSTAL IAW SRM 53-00-01.

Part: SKIN — BUCKLED (BS 1475) · airframe 43,151 hrs · 28,881 cycles

LOWER EMPENNAGE SKIN BUCKLED OUT WITH MISSING RIVETS AT LONGERON 27R BS 1475. REPAIRED IAW SRM 53-10-01 FIG 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,552 hrs · 29,130 cycles

FLOOR SUPPORT CORRODED FORWARD GALLEY AREA, STA 180 TO 200. REPLACED SUPPORTS IAW DWG 9936534.

Part: SKIN — BUCKLED (BS 1475) · airframe 43,151 hrs · 28,881 cycles

LOWER EMPENNAGE SKIN BUCKLED, LONGERON 26R BS 1475. REPAIRED IAW SRM 53-10-01 FIG 7 SHT. 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,552 hrs · 29,130 cycles

FORWARD CABIN FLOOR SUPPORT CORRODED, STA 180 RBL 8-44. REPLACED SUPPORT IAW DWG 9936534.

Part: LANYARD — KINKED (TAILCONE SLIDE) · airframe 43,151 hrs · 28,881 cycles

TAILCONE SLIDE LANYARD KINKED AND FRAYED RIGHT SIDE. REPLACED LANYARD IAW MM.

Part: SUPPORT — CORRODED (BS 1486) · airframe 43,151 hrs · 28,881 cycles

CATWALK, AFT END SUPPORT WEB CORRODED. CANT FRAME BS 1486 LEFT SIDE. OUT OF LIMITS. REPLACED SUPPORT SPLICE IAW DWG 9911843.

Part: SPACER — CORRODED (BS 1212-1266) · airframe 43,151 hrs · 28,881 cycles

AFT CARGO LOWER DOOR FRAME SPACER CORRODED, BS 1212 - 1266. REMOVED AND REPLACED THE SPACER IAW SRM 53-60-02.

Part: SHEAR TIE — CORRODED (BS 1288) · airframe 43,151 hrs · 28,881 cycles

AFT CARGO COMPARTMENT FRAME SHEAR TIE CORRODED, BS 1288 BETWEEN L29 - 30L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-00-01.

Part: SHEAR TIE — CORRODED (BS 1344) · airframe 43,151 hrs · 28,881 cycles

AFT CARGO COMPARTMENT FRAME SHEAR TIE CORRODED, BS 1344, BETWEEN LONGERON L26 - 286R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-01.

Part: CABLE — FRAYED (TAILCONE BOTTLE) · airframe 43,151 hrs · 28,881 cycles

TAILCONE NITROGEN CYLINDER CABLE FRAYED. REMOVED AND REPLACED CABLE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 42,132 hrs · 28,295 cycles

PERFORMED AN AIR TURN BACK DUE TO BOTH AUTO 1 AND AUTO 2, PRESSURE CONTROLLERS FAILED AFTER TAKEOFF. UNABLE TO REGAIN CONTROL OF PRESSURIZATION USING MANUAL MODE. REACTED BACKWARDS TO WHEEL CONTROLS INPUT. BITE CHECK OF BOTH AUTO PRESSURE CONTROLLERS SHOWS NO FAULTS. MANUAL OPERATION IS SMOOTH AND VALVE FOLLOWS POSITION OF CONTROL WHEEL. TROUBLESHOT IAW FIM. NO TROUBLE FOUND. ALSO, PERFORMED OPERATION TEST OF OUTFLOW VALVE IAW AMM. OPERATION CHECKS GOOD. REPLACED AUTO MANUAL CONTROL SWITCH, S1-154 AND CABIN TRANSFER RELAY R2-258 PRECAUTIONARY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,788 hrs · 26,272 cycles

TWO BULBS INOPERATIVE ON CATWALK EMERGENCY EXIT SIGN. REPLACED THE BULBS. OPS CHECKED GOOD.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 37,874 hrs · 25,685 cycles

FOUND WIRE PULLED OUT OF EMERGENCY LIGHT ON LEFT SIDE OF CATWALK. REPINNED. OPS CHECKED GOOD.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 36,674 hrs · 24,949 cycles

LEFT VERTICAL SKIN SPLICE CRACKED AT UPPER LEFT CORRNER OF ACCESS PANEL 370 BL OPENING. FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-30-05, FIG 3. PERMANENT REPAIR.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHTS) · airframe 35,719 hrs · 24,379 cycles

DURING EMERGENCY LIGHT CHECK, EXIT SIGN ABOVE AFT CABIN DOOR AND CEILING INOPERATIVE. REMOVED AND REPAIRED TERMINALS. REMOVED AND REPLACED POWER SUPPLY. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,050 hrs · 23,339 cycles

REMOVED FWD ENTRY DOOR HOLD OPEN PIN SKIN ASSY AND DRILLED UP NEW ASSY IAW SRM 53-30-01. FABRICATED EXTERNAL REPAIR DOUBLER IAW SRM 53-30-01. REPAIRED IAW 53-30-01.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 34,050 hrs · 23,339 cycles

BOTTOM EDGE OF L-1 DOOR DENTED AND OPENING OF GUSSET LOCK CRACKED. REPAIRED LOWER EDGE OF L-1 DOOR IAW SRM 52-01-01, PARAGRAPH 8C 23. REPLACED FWD ENTRY DOOR HOLD OPEN PIN ASSY (GUSSET LOCK) IAW SRM 53-30-01, PAR 9, FIG 8 TO ADDRESS GUSSET LOCK CRACK ON NON ROUTINE 01 THROUGH 09 PERM REPAIR.

Part: CABLE — OUT OF RIG (TAIL) · airframe 32,863 hrs · 22,692 cycles

DURING INSPECTION AND RIG CHECK OF CATWALK, MX FOUND LT SIDE LIFT CABLE TENSION LOW. ADJUSTED LIFT CABLE TENSION IAW AMM. OPS CHECKS GOOD.

Part: RETAINER — CRACKED (RT UPPER WINDOW) · airframe 32,863 hrs · 22,692 cycles

DURING PSV IN MSP MX NOTED A 0.5" LONG CRACK COMMON TO THE RT UPPER WINDOW RETAINER. THE CRACK IS TYPICAL TO SRM 56-01, FIG 3 REPAIR, HOWEVER IS NOT LISTED AS EFFECTIVE. THIS ERA 507708-14 APPROVES THE USE OF THE SRM REPAIR.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 31,212 hrs · 21,815 cycles

DOOR 1L DOOR SKIN DAMAGED ON LOWER EDGE NEAR FORWARD END. DAMAGE IS 6 INCHES LONG, 1 INCH HIGH. MAINTENANCE REWORKED EDGE OF DOOR SKIN PER SRM 52-01-01 PAGE 23. ACCOMPLISHED HFEC PER SRM 06-10-01, 001 TO EXTERIOR SKIN. NO CRACKS FOUND.

Part: RELEASE MECH — MISINSTALLED (EVAC SLIDE) · airframe 31,041 hrs · 21,733 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND TAILCONE SLIDE QUICK RELEASE TOGGLES AND MANUAL INFLATION HANDLE AND CABLE IMPROPERLY INSTALLED. MAINTENANCE CORRECTLY REINSTALLED QUICK RELEASE TOGGLES, STOWED AND ROUTED MANUAL INFLATION HANDLE AND CABLE AND CHECKED AFT SLIDE INSTALLATION PER OPERATION 7008. AIRCRAFT OKAY FOR SERVICE. RII COMPLETED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 31,004 hrs · 21,715 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EXIT SIGN BY FLOOR AT ROW 25CD, ONE BULB INOPERATIVE. FORWARD TO MCO/PLACARD PER MEL 33-51-01A. MAINTENANCE REPLACED LIGHT ASSEMBLY PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD. MCO/PLACARD REMOVED. AIRCRAFT OKAY FOR SERVICE.

Part: LANYARD — DISCONNECTED (GIRT BAR) · airframe 30,509 hrs · 21,489 cycles

ITEM REPORTED BY OPERATIONS, R-1 DOOR GIRT BAR LANYARD DISCONNECTED. MAINTENANCE RE-SECURED R-1 DOOR SLIDE LANYARD PER MAINTENANCE MANUAL. AIRCRAFT OKAY FOR SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 CORROSION ON SKIN CLIP STA 1494 R/S. REPLACED SKIN CLIP PER SRM 51-10-03.

Part: VENT — CORRODED (CABIN) · airframe 29,403 hrs · 20,926 cycles

HMV2 CABIN LT SIDE VENT GRILL CORRODED STA 1231-1364. REPAIRED PER SRM 53-00-01.

Part: WEB — CORRODED (CARGO BAY) · airframe 29,403 hrs · 20,926 cycles

HMV2 MID CARGO WEB AT DOORWAY STA 673-750 CORRODED. REPLACED WEB PER SRM 51-30-02 AND DRAWING 9940443.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 MID CARGO L29L CORRODED STA 589. REPLACED SPLICE PER ERA 487473-14 REV 0.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 CUSP WEB CRACKED STA 1134 LBL 54. REPAIRED PER SRM 51-10-03 AND DRAWING SG 09530019.

Part: STRUCTURE — CORRODED (AFT AIRSTAIRS) · airframe 29,403 hrs · 20,926 cycles

HMV2 AFT AIRSTAIR LEFT STEP WALL CORRODED. REPLACED STEP WALL PER SRM 51-10-05.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 RT LWR KEEL BEAM I/B CTR FUEL DRAIN PNEU SUPPORT ROD UPPER ATTACH FITTING CORRODED. REPLACED ATTACH FITTING PER SRM 51-30-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 MID CARGO COMP FLOOR SUPPORT CORRODED FS 655 LBL 14 TO RBL 14. REPLACED FLOOR SUPPORT PER SRM 51-30-05.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 FWD CARGO COMP SKIN STA 237-256 BETWEEN L29L-L30 CORRODED. REPLACED INTERNAL ANGLE AND EXTERNAL DOUBLER PER SRM 51-10-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 MID CARGO FLOOR SUPPORT STA 750 CORRODED. REPLACED FLOOR SUPPORT PER SRM 51-30-05.

Part: FRAME — CRACKED (LH MLG WW) · airframe 29,403 hrs · 20,926 cycles

HMV2 LT MLG W/W CUTOUT FWD FRAME I/B CORNER CORRODED AND CRACKED. REPLACED FRAME PER SRM 51-30-05.

Part: DOUBLER — CRACKED (LT MLG DOOR) · airframe 29,403 hrs · 20,926 cycles

HMV2 LT MLG WHEEL WELL DOOR AFT EDGE DOUBLER CRACKED. REPLACED DOUBLER PER SRM 51-10-03.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 FWD CARGO INTERCOSTAL STA 446-427 29R CORRODED. REPLACED INTERCOSTAL PER SRM 51-30-02.

Part: FRAME — CORRODED (RT MLG WW) · airframe 29,403 hrs · 20,926 cycles

HMV2 RT MLG CUTOUT FWD FRAME CORRODED. REPLACED FRAME PER SRM 51-30-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 MID CARGO INTERCOSTAL STA 845 L27L-L28L CORRODED. REPLACED INTERCOSTAL PER SRM 51-30-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 MID CARGO FLOOR SUPPORT CORRODED STA 693. REPLACED FLOOR SUPPORT PER SRM 51-30-5.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 MID CARGO L30 AND L29R STA 580 SPLICES CORRODED. REPLACED SPLICES PER ERA 487473-14 REV 0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 L20R CRACKED AT STA 1051. REPAIR PER SRM 53-10-01 AND BOEING DRAWING SG09530021.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 29,403 hrs · 20,926 cycles

HMV2 AFT PRESSURE BULKHEAD FWD SIDE LOWER LOBE CORRODED. REPLACED DOUBLER PER SRM 51-30-5.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65070038 SKIN PANEL CORROSION BETWEEN STA 1259.5 AND STA 1276, L30 SRM 53-30-01 VOL 3 FIG 3. C/W 65070038.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65070043, SKIN PANEL CORROSION BETWEEN STA 1204.5 AND STA 1212, L30 SRM 53-30-01 VOL 3 FIG 3. C/W 65070043.

Part: STIFFENER — CORRODED (APU DOOR) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65070174, CORROSION ON APU RT ACCESS DOOR STIFFENER. C/W 65070174.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65070083, CORROSION ON 30L BETWWEN STA 1344 AND STA 1364 OF AFT CARGO COMPARTMENT SRM 53-10-03 FIG 2. C/W 65070083.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65070093, CORROSION ON LT NR 2 SEAT TRACK BETWEEN STA 1200 AND STA 1300 SRM 53-40-01 FIG 6. C/W 65070093.

Part: FITTING — CORRODED (FUSELAGE) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65070054, CORROSION ON TRACK FITTING BETWEEN STA 1136 AND STA 1155 SRM 53-40-01 FIG 7. C/W 65070054.

Part: FITTING — CORRODED (CARGO BAY) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65070009, CORROSION ON RT TRACK FITTING BETWEEN STA 579 AND STA 598 OF MID CARGO COMPARTMENT SRM 53-40-01 FIG 7. C/W 65070009.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65070006, CORROSION ON TRACK BETWEEN STA 579 AND STA 693 OF MID CARGO COMPARTMENT SRM 53-40-01 FIG 7. C/W 65070006.

Part: BEAM — CORRODED (CARGO BAY) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65059946, CORROSION ON SPACER OF MID CARGO DOOR BEAM BETWEEN STA 693 AND STA 750 SRM 53-60-02 FIG 9.C/W 65059946.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65059816, CORROSION ON RT TRACK BETWEEN STA 228 AND STA 232 OF FWD CARGO COMPARTMENT SRM 53-40-01 FIG 7. C/W 65059816.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 25,296 hrs · 17,856 cycles

PERFORMED TASK CARD 65069819, CORROSION ON LT TRACK FITTING BETWEEN STA 503 AND STA 522 OF FWD CARGO COMPARTMENT SRM 53-40-01 FIG 7. C/W 65069819.