N929DL

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 73,608 hrs · 55,366 cycles

LT WING:ELONGATED HOLE ON ACCESS PANEL 1363C. REPAIRED IAW SRM 51-22-2A PAR 6 CONDITION II.

Part: ANGLE — CRACKED (SERVICE DOOR) · airframe 73,608 hrs · 55,366 cycles

CRACKED AFT ANGLE OVER BEAM NR 1 ON FWD SERVICE DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-5 AND DWG 9911579 REV L.

Part: ANGLE — CRACKED · airframe 73,608 hrs · 55,366 cycles

CRACKED DOOR PAN ANGLE BTW BEAM 5 AND 6 AT MAIN ENTERANCE DOOR. SPLICE WAS REPLACED PER DC 9/MD80 SRM 51-30-02 AND DWG 5914121 REV. AV. (LP2828943)

Part: SKIN — CRACKED (RT WING SLAT) · airframe 73,608 hrs · 55,366 cycles

RIGHT WING CRACKS AND SHEARED FASTENERS AT SLAT PANEL NR 3 INBD SKIN. REPAIRED IAW SRM 57-01, FIG. 5.

Part: DOOR FRAME — CORRODED (BS 1155-1212) · airframe 73,608 hrs · 55,366 cycles

AFT CARGO DOOR FRAME CORRODED BS 1212 TO 1155. REPAIRED IAW SRM 53-05 FIG. 123 A.

Part: LONGERON — CRACKED (BS 160) · airframe 73,608 hrs · 55,366 cycles

CRACKED LONGERON 3L ON BS 160. REPAIRED IAW SRM 53-02 FIG.18.

Part: FAIRING — CRACKED (LT ELEVATOR TAB) · airframe 73,608 hrs · 55,366 cycles

CRACK ON LT ELEVATOR CONTROL TAB FAIRING. ELEVATOR CONTROL TAB FAIRING WAS REPAIRED IAW SRM 55-01 FIG 2 (SHEET 2).

Part: SKIN — CRACKED (BS 1474) · airframe 73,608 hrs · 55,366 cycles

A CRACK ON THE FUSELAGE SKIN BS 1474 LONGERON 22L. THE SKIN WAS REPAIRED IAW SRM 53-01 FIG. 2 AND SRM 51-30-2.

Part: SPAR CAP — CRACKED (RT WING) · airframe 73,558 hrs · 55,330 cycles

RIGHT WING REAR SPAR CAP XRS=164 CRACKED. REPAIRED IAW ER/A 530469-14AD, REV A.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 73,118 hrs · 55,006 cycles

EMERGENCY LIGHTS AT ROW 25 INOPERATIVE. CONNECTED THE CONNECTOR AND OPS CHECKED GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 72,551 hrs · 54,576 cycles

EMERGENCY LIGHT INOPERATIVE AT SEATS 17D AND 27D. CONNECTED A LOOSE CONNECTION. CHECKED GOOD.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 72,281 hrs · 54,378 cycles

DURING LINE CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOPERATIVE, ROW 15-23. REPAIRED CONNECTOR AT ROW 15. LIGHTS NOW OPERATE NORMAL.

Part: SPRING — BROKEN (TAILCONE RELEASE) · airframe 71,897 hrs · 54,110 cycles

MAINTENANCE FOUND THE TAILCONE DEPLOYMENT MECHANISM SPRING BROKEN. THE SPRING WAS REPLACED IAW DWG 5910828.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 71,228 hrs · 53,634 cycles

MAINTENANCE FOUND SEAT ROW 1 EMERGENCY LIGHT INOPERATIVE. A LOOSE CONNECTOR WAS FOUND AND RECONNECTED. THE LIGHT OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 71,228 hrs · 53,634 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHTING INOPERATIVE FROM SEAT ROWS 15 TO 23. A BROKEN WIRE WAS FOUND AT ROW 15 AND REPAIRED. THE LIGHTS CHECKED GOOD.

Part: INLET — CRACKED (APU) · airframe 71,039 hrs · 53,494 cycles

DURING SEVERE TURBULANCE INSPECTION, FOUND APPROXIMATELY 6" CRACK AT AIR INLET LT SIDE AT BASE OF VERTICAL. WELDED APU AIR INLET IAW ERA 382101-14MA. ACCOMPLISHED FPI OF WELDED AERA IAW PS 900-6-3, NR 2.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 70,472 hrs · 53,083 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 22D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: SPAR CAP — CRACKED (RT WING) · airframe 68,355 hrs · 51,620 cycles

RT WING REAR SPAR LOWER CAP XRS 164, CRACKED 0.250 INCHES AT LOWER-INBD ATTACH BOLT. REPAIR THE SPAR IAW ER/A 530469-14 AD, REV 0.

Part: FRAME — CORRODED (BS 1271) · corrosion level 2 · airframe 68,355 hrs · 51,620 cycles

AFT CARGO BAY FRAME BS 1271 BETWEEN LONGERON 29-30R HAS LIGHT CORROSION ON LOWER SIDE OF FRAME ON BOTH SIDES. CUT DAMAGED AREA IAW SRM 53-03, FIG 2A. FABRICATED REPAIR PARTS IAW SRM 53-03, REV 2A. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-10-3. APPLIED TOP COAT REPAIR PARTS IAW SRM 51-10-3B, INSTALLED FRAME REPAIR IAW SRM 53-03D, FIG 2A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,135 hrs · 51,450 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 21-30 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,829 hrs · 50,474 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,107 hrs · 50,003 cycles

DURING LINE CHECK, NOTED SEVERAL EMERGENCY LIGHTS INOPERATIVE IN FWD CABIN. REPLACED BATTERY PACKS IN FWD DROP DOWN PANEL AT LAV DOOR AND SEAT ROW 12DEF. OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 65,072 hrs · 49,244 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT INOPERATIVE. FOUND A CONNECTOR IN THE WIRE HARNESS LOOSE, CONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BRACKET — LOOSE (TAILCONE RELEASE) · airframe 64,854 hrs · 49,110 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE CABLE SPRING BRACKETS ARE LOOSE. THE BRACKETS HARDWARE WAS REPLACED, RESECURED, AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: FRAME — CRACKED (BS 1474) · airframe 64,859 hrs · 49,112 cycles

CANTED FRAME AT BS 1474, TAIL INTERIOR. CRACKED AT FASTENER 4:00 POSITION. REMOVED CRACKED SECTION. HFEC INSP CUTOUT 2" X 1.5" IAW NDT SPM 06-10-01.001, NO DEFECTS NOTED. INSTALLED DOUBLER IAW SRM 51-70-5. IDENTIFIED REPAIR "P" WITH TAG. JOB COMPLET. REQUIRED INSPECTION COMPLETED. 163440.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 64,854 hrs · 49,110 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 64,307 hrs · 48,740 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 3D IN THE CABIN WAS INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,231 hrs · 47,251 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 24 ABCDE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: MECHANISM — OUT OF LIMITS (TAILCONE RELEASE) · airframe 61,876 hrs · 47,019 cycles

AIRCRAFT FAILED STEP 7 OF THE TAILCONE RELEASE SYSTEM OPERATIONAL CHECK. THE RELEASE MECHANISM CAM EXCEEDED THE ALLOWABLE TORQUE LIMIT. THE SYSTEM WAS CLEANED, LUBRICATED, AND THE SPRING TENSION ADJUSTED PER MANUAL. THE RII STEPS WERE COMPLETED AND SIGNED OFF.

Part: TAIL CONE — OUT OF LIMITS · airframe 61,876 hrs · 47,019 cycles

AIRCRAFT FAILED THE FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, DUE TO THE GAP BETWEEN PIN AND ROD WAS BEYOND ALLOWABLE LIMITS. THE PIN WAS ADJUSTED AND BROUGHT WITHIN LIMITS AND THE RII COMPLETED.

Part: RELEASE CABLE — WORN (TAILCONE) · airframe 61,876 hrs · 47,019 cycles

CHECK FAILED STEP 21 OF THE TAILCONE RELEASE SYSTEM OPERATIONAL CHECK. THE EXTERIOR RELEASE CABLE WAS OUT OF ALLOWABLE LIMITS AT THE CLAMP TO THE INTERNAL RELEASE CABLE. THE CLAMP ON THE CABLE WAS ADJUSTED AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FOLLOW-UP CHECK WAS SUCCESSFUL.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

HIDDEN DAMAGE ELONGATED HOLES ON CUSP ANGLE STRAP BELOW PREVIOUS REPAIR. CUSP ANGLE WAS REPLACED PER ERA 498181-14 REV ORIGINAL.

Part: DOUBLER — DAMAGED (VERTICAL STAB) · airframe 61,250 hrs · 46,565 cycles

DURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR EXTERNAL DOUBLER AND SKIN STA ZFS=50-52. WILL BE A ERA REPAIR CLASSIFIED MAJOR.

Part: DOUBLER — DAMAGED (VERTICAL STAB) · airframe 61,250 hrs · 46,565 cycles

DURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB REMOVABLE LEADING EDGE PREVIOUS EXTERNAL REPAIR DOUBLER STA ZFS=53. REPAIRED WITH AN ERA CLASSIFIED MAJOR.

Part: FINGER DOUBLER — CORRODED (BS 229.25) · airframe 61,250 hrs · 46,565 cycles

DURING HMV CORROSION WAS FOUND ON PRODUCTION FINGER DOUBLERS FROM STA Y=229-250 LONGERON 26RH, ALSO FROM STA Y=229-265 26LT REF SRM 53-04D FIG 12C FOR REPAIR.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 61,250 hrs · 46,565 cycles

DURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR DOUBLER AND REPAIR STRAP STA ZFS=52.

Part: STRAP — DAMAGED (VERTICAL STAB) · airframe 61,250 hrs · 46,565 cycles

DURING HMV ELONGATED HOLES AND CORROSION WERE FOUND ON VERTICAL STAB REMOVABLE LEADING EDGE PREVIOUS REPAIR EXTERNAL SPLICE STRAP STA ZFS=57. WILL BE REPAIED WITH AN ERA CLASSIFIED MAJOR.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 61,250 hrs · 46,565 cycles

DURING HMV ELONGATED REPAIR BUSHINGS WERE FOUND ON VERTICAL STAB REMOVABLE LEADING EDGE REPAIRED SKIN STA ZFS=52-55. WILL BE REPAIRED WITH ERA CLASSIFIED MAJOR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN PREVIOUS REPAIR TRIPLER AT WING FILLET PANELS RUBSTRIP SETTLEMENT AREA STA Y=757-775 BETWEEN LONGERON 26RT-23RT. REF SRM 53-04D FIG 53 FOR REPAIR.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

HIDDEN DAMAGE ELONGATED HOLES ON FRAME CLIP STA 218 BTW LONGERONS 18-19 LT. REPAIRS WERE COMPLETED PER ERA 498181-14 REV ORG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

CORROSION ON FUSELAGE SKIN BELOW RUB STRIP STA 1105. DOUBLER REPAIR WAS INSTALLED IAW DC9/MD80 SRM 53-04 FIG 53.

Part: SKIN — CORRODED (BS 1079-1080) · airframe 61,250 hrs · 46,565 cycles

CORROSION ON FUSELAGE SKIN RUB STRIP AREA STA 1079-1080. REPAIR ACCOMPLISHED IAW SRM 53-04D FIG 53.

Part: RUB STRIP — CORRODED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

CORROSION FUSE SKIN RUB STRIP AREA STA 1102-1106. DOUBLER REPAIR INSTALLED IAW DC9/MD80 SRM 53-04D FIG 53.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

CORROSION ON FINGER DOUBLER AT STA 270-276 BETWEEN LONGERONS 26LT AND 25LT AT FWD CARGO COMPT OVERLAP SKIN.

Part: SKIN — DAMAGED (LT WING) · airframe 61,250 hrs · 46,565 cycles

HIDDEN DAMAGE ELONGATED HOLES ON ACCESS DOOR CUTOUT NR 1355C AND 1357C AT LT WING LOWER SURFACE (LW). REPAIRS WHERE COMPLETED PER ERA 498175-14 AD REV ORIG.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,746 hrs · 10,372 cycles

DENT ON FUSELAGE SKIN PREVIOUS REPAIR DOUBLER STA Y=237 BTW LONG 17LT AND 18LT. REPAIRS WERE COMPLETED PER ERA 498181-14 REV ORIG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

CORROSION ON FUSELAGE SKIN FROM STA Y=239 TO 255 BTW LONG 30 TO 29 LT. REPAIR DOUBLER,STRAPS,FINGER DOUBLER AND NEW SECTION OFF SKIN WERE INSTALLED IAW DC9/MD80 SRM53-40 FIG 12C.

Part: FINGER DOUBLER — DAMAGED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

ELONGATED HOLES ON PREVIOUS REPAIR FINGER DOUBLER STA Y=230-242 BTW LONG 16L-18L. REPAIRS WERE COMPLETED PER ERA498181-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

ELONGATED HOLES ON FUSELAGE SKIN FROM STA Y=229-242 BETWEEN LONGERONS 18 LT. REPAIR WAS COMPLETED PER ERA 498181-14 REV ORIG.

Part: FINGER DOUBLER — DAMAGED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

ELONGATED HOLE ON INTERNAL PRODUCTION FINGER DOUBLE STA Y234LONG 18LT. REPAIRS WERE COMPLETED PER ERA 498181-14 REV ORIG.

Part: MECHANISM — FAILED (TAIL CONE) · airframe 61,250 hrs · 46,565 cycles

DURING TAIL CONE RELEASE, THE CAM TORQUE CHECK TEST FAILED. TAIL CONE RELEASE MECHANISM WAS REPLACED PER MD-88 AMM 53-53-02. 2ND OPERATIONAL CHECK PASSED PER MD88 AMM 53-53-02.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

CRACK WAS FOUND OF 0.650" ON PRODUCTION DOUBLER INTERNAL DOUBLER STA Y=424 FAST HOLE. L26-27 LOWER AFT CORNER OF FWD CARGO DOOR JAMB. REPAIR WASHER WAS FABRICATED AND INSTALLED IAW SR09530117 REV F AND AMR 09553962 REV 2.

Part: SKIN — DAMAGED (RUDDER) · airframe 61,250 hrs · 46,565 cycles

MISSING AND DAMAGED FLAME SPRAY COAT ON RT RUDDER SKIN SURFACE. RIGHT RUDDER SKIN SUFACE WAS REPAIRED IAW DC9/MD80 SRM 51-70-1A PAR 23 AND OPN JIC 1031 CARDS 1770 AND 1778.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,250 hrs · 46,565 cycles

LIGHTNING STRIKE ON THE RT WINDOW BELT FRAME AFT LWR CORNER STA Y=617-636 AT FUSELAGE SKIN FS. LIGHTNING STRIKE WAS BLENDED PER SRM 53-05 FIG 114 AND WAS FOUND OUT OF LIMITS. PERMANENT REPAIR WAS INSTALLED PER SR 09530053 REV C CONFIG 70-03.

Part: WIRE — DAMAGED (CABIN) · airframe 61,180 hrs · 46,514 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHTS AT 31DE THROUGH 35DE INOPERATIVE. MAINTENANCE REPLACED THE WIRING AT 35DE. OPERATIONAL CHECK WAS GOOD.

Part: PANEL — DAMAGED (VERTICAL STAB) · airframe 59,922 hrs · 45,599 cycles

VERTICAL STAB LOWER FIXED LEADING EDGE PANEL, UPPER EDGE ZFS 52 HOLE DAMAGE. REPAIRED IAW ERA 481558-14.

Part: PANEL — DAMAGED (VERTICAL STAB) · airframe 59,909 hrs · 45,589 cycles

VERTICAL STAB LEADING EDGE UPPER REMOVABLE PANEL UPPER AND LOWER EDGE HOLE DAMAGE. REPAIRED IAW ERA 481683-14.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 59,800 hrs · 45,511 cycles

DURING LINE CHECK, MAINTENANCE FOUND FORWARD CABIN EMERGENCY PATHWAY LIGHTS INOPERATIVE DURING TEST. MAINTENANCE FOUND HARNESS PLUG DISCONNECTED AT ROW 2D, RECONNECTED PLUG. OPERATION CHECKS GOOD. AIRCRAFT CLEARED FOR CONTINUED SERVICE.

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 59,324 hrs · 45,254 cycles

NRC 54 CORROSION ON C-2 THRESHOLD. NRC 55 WASHERS MISSING/CRACKED ON C-2 THRESHOLD. REPAIRED PER SRM 53-05 FIG 123.

Part: LANYARD — MISINSTALLED (L1 DOOR SLIDE) · airframe 59,206 hrs · 45,182 cycles

DURING LINE CHECK, MX FOUND L1 DOOR SLIDE LANYARD INSTALLED INCORRECTLY. MX INSTALLED LANYARD IAW MM 25-62-00.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 57,549 hrs · 44,090 cycles

VERT STAB ZFS 44 LT SKIN, LT FWD SPAR CHORD AND WEB CRACK. REPAIRED IAW ERA 481559-14.

Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 57,545 hrs · 44,087 cycles

VERTICAL STAB FRONT SPAR UPPER RT CHORD HAD OVERSIZED HOLES AND WAS REPAIRED IAW ERA 482312-14.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 57,545 hrs · 44,087 cycles

VERTICAL STAB HOLES WORN ON LT SIDE CHORD COMMON TO L/E PANEL STRUCTURE WAS REPAIRED IAW ERA 481678-14.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 57,545 hrs · 44,087 cycles

BHEC INSPECTION OF FASTENER HOLES ON VERTICAL STAB RT SIDE INDICATIONS OF CRACKING IN HOLE NR 7 AT ZFS52. STEPPED UP HOLE BELOW ZFS52 RT SIDE TO .250" COMP-LIED WITH PRI 481680-14 REV 2 4/24/2010 1000 EST.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 57,545 hrs · 44,087 cycles

LT VERT STAB L/E SKIN, WEB AND CHORD CRACKED REPAIRED IAW ERA 481906-14. (DLM88101445)

Part: WATER HEATER — OVERHEATED (LAVATORY) · airframe 56,344 hrs · 43,316 cycles

AFT LT LAV SMOKE DETECTOR CHIRPING AT GATE. FOUND AFT LT LAV WATER HEATER OVERHEATING. FWD ITEM TO NEF 381.043 FOR REPLACEMENT-ALSO DETERMINED EXTERNAL START CART CONTRIBUTING FUMES INTO THE CABIN. REMOVED START CART (14138)-NO FURTHER ISSUES.

Part: O-RING — MISSING (NLG) · airframe 55,693 hrs · 42,890 cycles

NOSE GEAR DOOR RED ILLUMINATED UPON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT. SERVICED NOSE GEAR PER MM. FOUND AIR VLV MISSING O-RING. REPLACED SAME, LEAK CHECKS GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,012 hrs · 41,777 cycles

CRACK AND CORROSION IN BELLY SKIN AT POTABLE WATER DRAIN, FS 593.6, BTW L-29R AND L-30. CUT OUT DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 54,012 hrs · 41,777 cycles

C1 CARGO JAMB WAS FOUND CORRODED BEYOND LIMITS AND REPAIRED PER SRM 53-05D FIG 804.

Part: SENSOR — OUT OF LIMITS (RT MLG) · airframe 46,707 hrs · 36,917 cycles

AFTER TAKEOFF, THE RT MAIN GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE AND LIGHT REMAINED ILLUMINATED. JACKED AIRCRAFT AND SWUNG GEAR. ALL INDICATIONS NORMAL. CHECK RT UP LATCH SENSOR. GAP WAS OUT OF LIMITS. REPLACED RT MLG UP AND LATCH SENSOR IAW AMM 32-60-00. OPS CHECK GOOD

Part: ODOR — DETECTED (CABIN) · airframe 45,934 hrs · 36,369 cycles

ELECTRICAL BURNING POPCORN ODOR ON APPROACH INTO ATL. AFT GALLEY. INSPECTED AIRCRAFT AND RAN PACKS, PERFORMED DUCT BURNOUT.

Part: SLIDE — DISCHARGED (R1 DOOR) · airframe 38,719 hrs · 31,359 cycles

FWD GALLEY DOOR SLIDE PRESSURE LOW . REPLACED SLIDE

Part: ENGINE — ACTIVATED (NR 1) · airframe 38,418 hrs · 31,137 cycles

IN FLIGHT SHUT DOWN, LOSS OFF OIL PRESSURE AND QTY. PRESSURE WENT TO ZERO AT PWR FOR APPROX 30 SEC. WINDMILL AT ZERO PSI FOR 10 MIN. RETURN TO CVG. REPLACED ENGINE.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 37,301 hrs · 30,329 cycles

CORROSION ON C-1 LOWER THRESHOLD FWD OF AFT STOP. REPAIRED PER MD-80 DRD 53-05-D FIG 804.

Part: O-RING — LEAKING (APU CHIP DETECT) · airframe 35,033 hrs · 28,598 cycles

AFT CABIN SMOKE DETECTERS GOING OFF IN FLIGHT. FOUND 1 AFT SMOKE DETECTOR BAD AND APU OIL LEAK.NO ODER NOTICED IN CABIN. PERFORMED OP 5088 T/S FOR SMOKE IN CABIN AND PERFORMED DUCT BURN OUT.REPLACED SMOKE DET.

Part: CONTROL CABLE — SEVERED (RT MLG WW) · airframe 33,833 hrs · 27,725 cycles

ON FINAL APPROACH, GPWS WARNING TOO LOW-FLAPS SOUNDED. FLAPS INDICATED 40 DEGREES, GREEN LAND LIGHT ON, ON TAXI IN, THE SLATS WILL NOT RETRACT AND HANDLE IS DIFFICULT TO MOVE AND DISAGREE LIGHT REMAINS ON. FOUND CABLE 207B BROKEN RT W/W. REPLACED BROKEN ELEVATOR FORCE SERVO TORQUE LIMITER CABLE NR 207B AND REPLACED THE NR 208B CABLE FOR PREVENTITIVE MEASURES.

Part: ENGINE — MAKING METAL (NR 1) · airframe 32,852 hrs · 27,004 cycles

NR 1 ENGINE OIL STRAINER CLOG LIGHT ILLUM AND WOULD NOT EXTINGUISH WHEN THROTTLES RETARDED. OIL TEMP REACHED 144 DEGREES. FOLLOWED POM SHUT DOWN ENGINE. FOUND METAL IN FILTER AND ON CHIP DETECTOR. REPLACED ENGINE.

Part: LINE — LEAKING (NR 4 BRAKE) · airframe 32,835 hrs · 26,991 cycles

AIR ABORT AND RETURN TO ATL DUE AFT FLT ATTS REPORTING STRANGE SMELL IN AFT HALF CABIN. ODOR CONFIRMED BY PAX AS WELL. FOUND HYD LEAKING ON NR 4 BRAKE. REPLACED LEAKING BRAKE LINE. PERFORMED DUCT BURNOUT.

Part: OVEN — FAILED (FWD GALLEY)

DURING TAXI OUT FROM LAX, FLT ATTENDANT REPORTED SPARKS AND SMOKE COMING FROM FWD GALLEY. C/B POPPED. REPLACED GALLEY OVEN.

Part: GCU — INOPERATIVE (RIGHT)

A/C DIVERTED TO MCO. RIGHT GEN FAIL LIGHT IN FLIGHT WITH CROSSTIE LOCKOUT. REPLACED RIGHT GENERATOR CONTROL UNIT.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ON LAYOVER, FOUND AFT EMERGENCY FLOOR TRACK LIGHTING INOP. FOUND POWER SUPPLY AND BATTERY PACK INOP. REPLACED PWR SUPPLY AND BATTERY PACK. EMERGENCY FLOOR LIGHTING OPS TEST NML.

Part: RETRACT MECH — MALFUNCTIONED (NLG DOOR)

ON T/O, THE NOSE GEAR DOOR ON THE COPILOT'S SIDE DID NOT CLOSE. FLIGHT RETURNED TO CAE. ON RETURN TO CAE, THE RT NOSE GEAR DOOR WAS FOUND OPEN. MTC INSPECTED THE DOOR LOCKING MECHANISM AND FOUND OPERATIONALLY OK FOR SERVICE.

Part: LINE — RUPTURED (RT PYLON)

ON CLIMBOUT FROM ATL FOLLOWING SLAT RETRACTION, RT HYDRAULIC QTY AND PRESSURE WENT TO ZERO. RETURNED ATL. FOUND RT ENGINE HYDRAULIC PUMP PRESSURE LINE RUPTURED IN PYLON JUST BEFORE IT ENTERS THE FUSELAGE. REPLACED LINE RETURNED TO SERVICE.

Part: ANGLE — CRACKED (NR 2 PYLON)

FOUND DURING A-1 LETTER CHECK - NR 2 PYLON UPPER SKIN TO FUSELAGE SKIN, ATTACH ANGLE WAS FOUND WITH A .75 INCH CRACK. REPAIRED PER SRM 54-04 A, FIG 4.

Part: CHANNEL — CRACKED (RT WHEELWELL)

RT MLG W/W DOOR JAMB FWD CHANNEL CRACKED AT UPPER RADIUS APPROX 2.25 INCHES. REPAIRED PER SRM 53-05, FIG 78.

Part: ANGLE — CRACKED (NR 2 PYLON)

FOUND DURING LETTER CHECK, NR 2 PYLON UPPER SKIN TO FUSELAGE ATTACH ANGLE WITH A .75 INCH CRACK. REPAIRED PER SRM 54-04 A FIG 4.