N952DN

Part: STARTER — DISINTEGRATED (LT ENGINE) · airframe 43,159 hrs · 34,760 cycles

LEFT ENG DURING START NO N2 ROTATION GROUND CREW REPORTED SPARKS AND FLAMES. COMPLIED WITH MANUAL ABORTED START PROCEDURE PER QRH. FOUND STARTER DISINTEGRATED. NO VISIBLE DAMAGE TO ENGINE CASE OR COWLING. R/R LEFT ENGINE STARTER IAW AMM 80-11-01-401. STARTER SERVED TO FULL. STARTER LEAK CHECK AND ENGINE RUN GOOD. (LP 4680680)

Part: SPAR — NOT REPORTED (HORIZONTAL STAB) · airframe 44,774 hrs · 35,831 cycles

ER/A 570845-14AD ISSUED FOR REPAIR TO LH HORIZONTAL STAB UPPER REAR SPAR BARREL NUT HOLE. FOLLOW ON ACTION IS REQUIRED. C/A ERA REVISED TO REV 'A'. SECTION II INSPECTION REVISED. NEW LOG 1415429 TO TRACK NEW FOLLOW ON ACTION. THIS LOG CAN BE CLOSED ALSO SEE LOG 1415429 (0713242)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,541 hrs · 34,379 cycles

EMERGENCY LIGHT EXIT SIGN AT SEAT 34 INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT SEAT 32C IAW AMM 33-51-03.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 42,224 hrs · 34,198 cycles

AIRBORNE - SMOKE FROM COFFEE POT 102. WHET TO QRH, TURNED OFF GALLEY POWER, SMOKE DISSIPATED. R&R FWD GALLEY F102 COFFEE MAKER. FOUND C/B POPPED ON BACK OF C/M. DID NOT TRY AND RESET OR TEST OLD C/M. FWD GALLEY C/M OPS NORMAL PER AMM 25-33. BREWED 3 FULL POTS. NO DAMAGE TO ELECTRICAL CONNECTOR A/C SIDE. NO SMOKE OR SMELL.

Part: SHUTOFF VALVE — FAILED (ANTI-SKID SYS) · airframe 41,715 hrs · 33,892 cycles

WHILE BOARDING, THE CREW REPORTED AN ANTI-SKID FAULT, FOLLOWED BY AN ELECTRICAL ODOR IN THE COCKPIT. REPLACED THE ANTI-SKID RETURN SHUTOFF VALVE. REPLACED THE APU STARTER AND COALESCER BAGS FOR THE ODOR. TERMINATED A BROKEN WIRE AT TERMINAL C642T20.

Part: SCHRADER VALVE — LOOSE (NLG) · airframe 41,155 hrs · 33,541 cycles

PERFORMED AN AIR TURN BACK TO TPA DUE TO A NOSE LANDING GEAR UNSAFE INDICATION AND NOSE EAR DID NOT RETRACT. AN EMERGENCY WAS DECLARED. TPA MAINTENANCE FOUND THE NLG SCHRADER VALVE LOOSE. THE VALVE WAS SECURED AND THE STRUT WAS SERVICED. A LOG WAS CREATED TO RE-CHECK THE SERVICING.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 40,183 hrs · 32,965 cycles

SERVICE DOOR VERTICAL EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY B5-241 IAW MM. OPERATION CHECKS GOOD.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 40,051 hrs · 32,889 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE FROM SEAT 15 THRU 21. TROUBLESHOT. FOUND ELECTRICAL CONNECTOR FOR BATTERY PACK DISCONNECTED. RESECURED CONNECTOR AND OPERATION CHECKS GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,865 hrs · 32,787 cycles

CABIN LEFT HAND FRAME STA 902 FOUND TO HAVE CRACK. REPLACED ON TASK CARD 5310-01375-06-LT.

Part: ATTACH ANGLE — CRACKED (BS 1520) · airframe 39,862 hrs · 32,785 cycles

AFT LOWER ATTACH ANGLE FOR LOUVER BOX FOUND CRACK AT FRAME, BS 1520, LONGERON 4L. REMOVED AND REPLACED IAW SRM 51-30-05, AND DWG 9911839.

Part: ATTACH ANGLE — CRACKED (BS 1520) · airframe 39,862 hrs · 32,785 cycles

CRACKED ANGLE SUPPORT AT AFT FACE OF FRAME, BS 1520, LONGERON 3L. REMOVED AND REPLACED IAW SRM 51-30-05, AND DWG 9911839.

Part: FRAME — CRACKED (BS 1542) · airframe 39,862 hrs · 32,785 cycles

CRACK ON FRAME ANGLE AT BS 1542 BELOW LOWER BOX. REPAIRED IAW SRM 53-10-03.

Part: DOUBLER — CORRODED (VERTICAL STAB) · airframe 39,862 hrs · 32,785 cycles

VERTICAL STABILIZER INTERNAL DOUBLER HAS FRETTING. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-02 AND DWG 5910242.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 39,862 hrs · 32,785 cycles

VERTICAL STABILIZER LEFT HAND INTERNAL ATTACH CRACKED. REMOVED AND REPLACED VERTICAL STABILIZER LEFT HAND INTERNAL ATTACH ANGLE IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 39,862 hrs · 32,785 cycles

VERTICAL STABILIZER RIGHT HAND INTERNAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.

Part: FRAME — CRACKED (NLG WW) · airframe 39,862 hrs · 32,785 cycles

NOSE LANDING GEAR WHEEL WELL STATION 45R FRAME CRACKED. REMOVED AND REPLACED NOSE LANDING GEAR WHEEL WELL IAW 51-30-02, 51-30-05 AND DWG 9910088.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 39,862 hrs · 32,785 cycles

LONGERON 2L TO FRAME STA 1475 AFT ATTACHMENT CLIP CRACKED. REMOVED AND REPLACED ATTACHMENT CLIP IAW SRM 51-30-05 AND DWG 9964460.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 39,862 hrs · 32,785 cycles

LONGERON 2R TO FRAME STA 1475 AFT ATTACHMENT CLIP CRACKED. REMOVED AND REPLACED ATTACHMENT CLIP AT L2R, STA 1475 IAW SRM 51-30-05 AND DWG 9964460.

Part: HINGE — CRACKED (NLG DOOR) · airframe 39,865 hrs · 32,787 cycles

NOSE LANDING GEAR AT LEFT AFT DOOR AFT HINGE HAS A CRACK IN THE RADIUS. REPAIRED IAW SRM 53-30-01.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 39,862 hrs · 32,785 cycles

LONGERON 2L TO FRAME STA 1475 FORWARD ATTACHMENT CLIP CRACKED. REMOVED AND REPLACED ATTACHMENT CLIP ATL2L STA 1475 IAW SRM 51-30-05 AND DWG 5911432.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 39,862 hrs · 32,785 cycles

LONGERON 2R TO FRAME STA 1475 FORWARD ATTACHMENT CLIP CRACKED. REMOVED AND REPLACED ATTACHMENT CLIP STA 1475 L2R IAW SRM 51-30-05 AND DWG 5911432.

Part: DOUBLER — GOUGED (CARGO DOOR PAN) · airframe 39,862 hrs · 32,785 cycles

MID CARGO DOOR PAN DEEPLY GOUGED. ONLY DOUBLER DAMAGED. REPAIRED IAW SRM 52-30-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,091 hrs · 32,390 cycles

TWO EMERGENCY LIGHTS INOPERATIVE IN THE TAIL COMPARTMENT. REPLACED THE LAMPS. OPERATION CHECKED GOOD.

Part: SIGN — UNSECURE (CABIN) · airframe 38,485 hrs · 32,042 cycles

EMERGENCY EXIT SIGN CENTER AISLE L2 DOOR NEEDS TO BE SECURED. SECURED THE SIGN. OPERATION CHECKED GOOD.

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 35,909 hrs · 30,532 cycles

L1 DOOR SLIDE PINS PULLED. R & R SLIDE ASSEMBLY.

Part: BOTTLE — EMPTY (L1 DOOR SLIDE) · airframe 35,909 hrs · 30,532 cycles

L1 DOOR SLIDE INFLATION PRESSURE AT ZERO. REPLACED L1 DOOR SLIDE JIC 2561-4641.

Part: STRUCTURE — LEAKING (EVERYWHERE) · airframe 34,696 hrs · 29,790 cycles

DIVERTED DUE TO OIL FUME ODOR IN CABIN. RT GENERATOR OFF AND RT AC POWER FAULT WITH CORRESPONDING LOSS OF AC POWER. RT GENERATOR OVERHEAT STATUS MESSAGE ON EOAP. SHORTLY AFTER ENGINE GENERATOR FAILURE, APU WAS STARTED. F/A REPORTED A SMOKE OIL FUME ODOR IN CABIN. MAINTENANCE TROUBLESHOT AND FOUND APU OIL TEMP SENSOR LOOSE AND LEAKING OIL. SECURED THE SENSOR. FOUND RT VSCF GENERATOR LEAKING OIL AND REPLACED IT. R & R CEU AND EPCU DUE TO CONTINUED FAULTS DURING TROUBLESHOOTING. AFTER ENGINE HIGH POWER RUN FOUND OIL LEAKING FROM ENGINE GEARBOX AT VSCF GARLOCK SEAL. REPLACED SEAL. LEAK AND OPS TEST ON GEARBOX AND APU OIL SENSOR CHECKS GOOD.

Part: FRAME — CRACKED (BS 924) · airframe 34,496 hrs · 29,667 cycles

LEFT FUSELAGE OVERWING FRAME AT BS 924 CRACKED AT CUSP WEB. R & R OVERWING FRAME AT BS 924 IAW AMDS 5310-01375-07-LT AND DWG SR90530027, CONFIG -7009.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 33,538 hrs · 29,056 cycles

UPPER AFT SKIN PANEL ON THE RT SIDE OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED. PERFORMED A BONDED REPAIR IAW ERA 531274-14AD.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 33,538 hrs · 29,056 cycles

THE UPPER AFT SKIN PANEL ON THE RT SIDE OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED DURING INSPECTION. REPAIRED IAW ERA 531274-14, REV O.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 32,100 hrs · 28,114 cycles

EMERGENCY EXIT SIGN INOPERATIVE. R & R POWER SUPPLY. OPS CHECKED OK.

Part: LANYARD — UNKNOWN (TAILCONE) · airframe 29,380 hrs · 26,401 cycles

TAILCONE SLIDE RELEASE LANYARD CLEVIS PINS NOT TAKED WITH AND "X" IAW DWG 8370024. R & R TAILCONE SLIDE RELEASE LANYARD IAW AMM.

Part: DOOR FRAME — DAMAGED (CARGO DOORWAY) · airframe 29,380 hrs · 26,401 cycles

BLEND OUTS ON AFT CARGO DOOR FRAME. FABRICATED DOUBLER, STRAP AND BUSHINGS IAW ERA 513348-14. INSTALLED REPAIR PARTS IAW 51-30-05, 51-30-02 AND ERA 513398-14.

Part: FRAME — CRACKED (BS 1542) · airframe 29,380 hrs · 26,401 cycles

BS 1542, CANTED FRAME LOWER END IS CRACKED. REMOVED DAMAGED SECTION BS 1542. FABRICATED NEW FRAME, REPAIR SPLICE DOUBLER AND SHIMS. INSTALLED REPAIR PARTS IAW ERA 513397-14.

Part: LONGERON — CRACKED (BS 1379) · airframe 29,380 hrs · 26,401 cycles

LONGERON 20L, FS 1379, UNDER LT LAV FLOOR, FASTENER IS TOO CLOSE TO RADIUS AND POSSIBLE CRACK. REMOVED, FABRICATED, DRILLED AND INSTALLED SHEAR TIE IAW SRM 51-10-02, 51-30-02, 51-30-05, 51-10-03, ERA 2-37153-801, REV A.

Part: LONGERON — CORRODED (BS 1488 L11) · airframe 29,380 hrs · 26,401 cycles

AFT ACCESSORY BAY, CANTED FRAME 1488, AFT FACE FROM LONGERON R7 TO L11 SEVERAL STIFFENERS HAVE LIGHT SURFACE CORROSION. REMOVED CORROSION. STIFFENERS WITHIN LIMITS. LONGERON FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, PRIMED AND INSTALLED STIFFENER AND LONGERON IAW SRM 51-30-02 AND 51-30-05.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 29,380 hrs · 26,401 cycles

MID CARGO DOOR FRAME LOWER BEAM IS CORRODED AROUND FASTENER HOLES. DRILLED REPAIR AND FABRICATED SPACER. INSTALLED REPAIR IAW SRM 53-60-02, FIG 9 AND 53-30-02, FIG 9.