N904DA

Part: HANDLE — LACK OF LUBE (TAILCONE RELEASE) · airframe 60,480 hrs · 32,938 cycles

TAILCONE EMERGENCY RELEASE HANDLE EXCEEDS OPENING FORCE DURING TEST. ADJUSTED AND LUBED THE DOOR IAW MM. OPS CHECKED GOOD.

Part: FIRE LOOP — BROKEN (B) · airframe 60,284 hrs · 32,825 cycles

DURING CLIMBOUT, RT ENGINE FIRE DETECTION FAULT ILLUMINATED. AIR RETURN DUE TO QRH GUIDANCE. C/W ODI EVENT, WORKCARD 2611-2002 R ENG FIRE DETECTION INT CHECK FOUND FLAME DEFLECTION B LOOP BROKEN. REPLACED ALL FIVE LOOPS IAW AMM 26-11. OPS CHECKED NORMAL. HIGH POWER RUN ACCOMPLISHED, NO FAULTS.

Part: LEVER — BINDING (COCKPIT) · airframe 61,043 hrs · 33,281 cycles

AT FLARE FOR LANDING, ELEV CONTROL MAN ILLUMINATED AND YOKE CONTROL OF ELEVATOR FELT FROZEN OR JAMMED. DID NOT FEEL MERELY UN BOOSTED AND HYDRAULIC ELEVATOR CONTROL DID NOT INDICATE OFF. TROUBLESHOT AND FOUND LEFT SIDE LEVER ASSEMBLY BINDING. CAUSING MANUAL REVERSION. REMOVED AND REPLACED LEVER ASSEMBLY AND BEARINGS. OPERATION CHECKS GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 60,248 hrs · 32,801 cycles

THREE CEILING EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 32A, 39C, & 1 IN THE CATWALK. EMERGENCY LIGHT IN TAIL, FOUND FIXTURE ASSY WIRED WRONG, MOVED WIRE TO PROPER STUD. ROW 39C: FOUND DISCONNECTED WIRE - RECONNECTED & OPS GOOD. ROW 32A, FOUND DISCONNECTED WIRE, RECONNECTED & OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 59,552 hrs · 32,415 cycles

CATWALK FIRST SIDEWALL EMERGENCY LIGHT INOPERATIVE. FOUND WIRE DISCONNECTED. INSTALLED NEW PIN AND SOCKET. OPERATION CHECKED GOOD.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 58,736 hrs · 31,988 cycles

EMERGENCY EXIT SIGN COVER LOOSE. SECURED.

Part: LIGHT — MISSING (ROW 26 ABC) · airframe 58,643 hrs · 31,935 cycles

EMERGENCY LIGHT MISSING AT ROW 26 ABC. REPLACED THE EMERGENCY LIGHT IAW MM. OPS CHECKED GOOD.

Part: SUPPORT FRAME — CRACKED (NLG) · airframe 58,194 hrs · 31,694 cycles

FOUND 2 CRACKS IN RIGHT NOSE LANDING GEAR SUPPORT FRAME BETWEEN BS 40 AND 60. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW ERA 553838-14, REV O.

Part: PANEL — CRACKED · airframe 58,194 hrs · 31,694 cycles

EMPENNAGE VENTRAL STAIRWAY AFT CUT OUT HAS 8 INCH CRACK IN LIGHT PANEL. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW WEB SECTION IAW PRI/ERA 553835-14 AND DWG 991192.

Part: VANE — GOUGED (RT WING TE FLAP) · airframe 58,194 hrs · 31,694 cycles

RIGHT WING OUTBOARD FLAP VANE LEADING EDGE GOUGED. REPAIRED IAW ERA 553839-14, REV O. AND SRM 51-10-02.

Part: NOT REPORTED — CRACKED (NOT REPORTED) · airframe 58,194 hrs · 31,694 cycles

CRACK FOUND AT THE AFT EMERGENCY WALK WAY. REPAIRED IAW SRM 51-70-01.

Part: FITTING — CRACKED (EMPENNAGE) · airframe 58,194 hrs · 31,694 cycles

CRACK IN THE RIGHT FITTING AT AUX SPAR TO EMPENNAGE ATTACH POINT. REMOVED AND REPLACED FITTING IAW SRM 51-30-02, 51-30-05, AND 51-10-05.

Part: SKIN — CRACKED (RT WING) · airframe 58,194 hrs · 31,694 cycles

RIGHT WING FIXED LEADING EDGE BELOW SLAT TRACK NR 8 SKIN CRACKED. REPAIRED IAW SRM 57-20-01.

Part: ATTACH FITTING — CRACKED · airframe 58,193 hrs · 31,693 cycles

CRACK IN LEFT HAND FITTING AT AUXILIARY SPAR ATTACH TO EMPENNAGE. REMOVED AND REPLACED LEFT HAND AUX SPAR ATTACH FITTING IAW SRM 51-30-05, 51-30-01 AND DWG 9917704, REV Y.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 58,193 hrs · 31,693 cycles

LEFT AILERON LOWER SURFACE HAS SMALL AREA OF DELAMINATION. HOT BONDED PERMANENT REPAIR INTO LEFT AILERON LOWER SURFACE IAW SRM 57-50-02 AND 51-10-04.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,193 hrs · 31,693 cycles

CRACK VERIFICATION. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER ON RIGHT AFT NLG DOOR AFT HINGE CUTOUT IAW SRM 53-30-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,193 hrs · 31,693 cycles

EXTERIOR FUSELAGE, AFT HINGE CUTOUT IS CRACKED AT AFT NLG DOOR. STOPPED DRILLED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-01.

Part: CUSP WEB — CORRODED (BS 955) · airframe 58,193 hrs · 31,693 cycles

FOUND CUSP MEMBRANE CRACKED AT BS 955, LBL 64. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER, FILLER AND RING DOUBLER IAW SRM 53-20-02.

Part: BAYONET — WORN (TAILCONE) · airframe 57,547 hrs · 31,311 cycles

DURING TAIL CONE EMERGENCY RELEASE, FOUND LT SIDE UPPER AND LOWER TAIL CONE BAYONETS WORN. REPLACED IAW CMM.

Part: BULB — WRONG PART (EMERGENCY LIGHTS) · airframe 57,300 hrs · 31,152 cycles

EMERGENCY LIGHT NEAR L1 DOOR IS DIM. FOUND INCORRECT BULB INSTALLED AND EMERGENCY LIGHT ASSEMBLY AND STANDBY LIGHT ASSEMBLY CORRECTED. OPS CHECKED OK.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 56,550 hrs · 30,715 cycles

R1 DOOR SLIDE PRESSURE LOW. R & R DOOR SLIDE IAW AMDS 2561-4641.

Part: TRANSMITTER — LEAKING (NR 1 FUEL FLOW) · airframe 53,056 hrs · 28,562 cycles

ON GROUND, WITH EXTERNAL AIR CONNECTED, STRONG ODOR OF FUEL AND EXHAUST FUMES FROM MID TO AFT OF ACFT. ODOR WAS PRESENT THROUGH MID CLIMB. MAINTENANCE FOUND FUEL FLOW TRANSMITTER LEAKING ON NR 1 ENGINE. R & R UPPER FLANGE O-RING IAW AMM. LEAK CHECK AND PACK BURNOUT OK.

Part: SKIN — CRACKED (BS 1437) · airframe 52,856 hrs · 28,443 cycles

FUSELAGE SKIN CRACKED AT FASTENER, RT SIDE, BS 1437, 12 INCHES ABOVE RT PYLON. REPAIRED IAW PRI 531221-14, REV O.

Part: FASTENER — LOOSE (VERTICAL STAB) · airframe 52,856 hrs · 28,443 cycles

LOOSE FASTENERS AT STA ZFS = 52.267 VERTICAL STABILIZER L/E. FOUND FIVE TOTAL HOLES OUT OF LIMITS AND REQUIRED BUSHING REPAIR IAW SG09550004-7003. INSTALLED DOUBLER IAW DW SR-09550004-7003, REV D.

Part: SKATE ANGLE — CRACKED (BS 1458-1486) · airframe 52,856 hrs · 28,443 cycles

INTERNAL STABILIZER ATTACH ANGLE CRACKED, LT SIDE BS 1458 - 1486. R & R THE SKATE ANGLE IAW DWG 5912188.

Part: SKATE ANGLE — CRACKED (BS 1458-1486) · airframe 52,856 hrs · 28,443 cycles

INTERNAL STABILIZER ATTACH ANGLE RT SIDE, BS 1458-1486 CRACKED. R & R SKATE ANGLE IAW DWG 5912188.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 52,203 hrs · 27,990 cycles

ALL AFT AIRSTAIRS LIGHTS INOPERATIVE. FOUND WIRES DISCONNECTED, CONNECTED THE WIRES AND OPERATES NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,260 hrs · 26,810 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS FOR TAIL SECTION CATWALK INOPERATIVE. MAINTENANCE R & R BATTERY PACK, B5-212. OPERATION CHECKS GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 50,260 hrs · 26,810 cycles

DURING SERVICE CHECK, TWO EMERGENCY LIGHTS INOPERATIVE AROUND ROW 35 AND 38. MAINTENANCE FOUND CONNECTOR WIRES J2-38B AND J2-48A LOOSE. RESEATED. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,870 hrs · 26,558 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY LIGHT ROW 36L, INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,870 hrs · 26,558 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY CEILING LIGHT ROW 38R INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 49,817 hrs · 26,528 cycles

DURING SERVICE CHECK, OVERWING EMERGENCY EXIT SIGN INOPERATIVE. FOUND WIRES DISCONNECTED IN CEILING PANEL. RECONNECTED WIRES. OPERATION CHECKS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 48,514 hrs · 25,781 cycles

L1 DOOR EMERGENCY EXIT SIGN OVER DOOR INOPERATIVE. REPLACED LAMP. OPERATION CHECKED GOOD. OK FOR SERVICE.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 48,175 hrs · 25,611 cycles

L1 DOOR SLIDE, CANNOT SEE HORIZONTAL LINE ON THE GIRT BOTTOM EDGE IAW MM 25-61-01-420-801, PG 3. R & R L1 DOOR SLIDE IAW AMM.

Part: RIB — CRACKED (RT WING) · airframe 48,174 hrs · 25,610 cycles

RT WING FIXED L/E RIB AT OTBD EDGE OF SLAT IS CRACKED AT LOWER END. REJECTED, EDGE DISTANCE WAS NOT MAINTAINED ON REPAIR. REPAIRED CRACK AND MISDRILLED HOLES IAW ERA 509152-14, REV. O.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 48,175 hrs · 25,611 cycles

MAIN CABIN CUSP WEB AT STRINGER 18 IS CRACKED AT THE LIGHTNING HOLE LOCATED AT STA 1355R. REPAIRED MAIN CABIN CUSP WEB IAW SRM 51-10-03, 53-20-02 AND 53-10-03.

Part: BULKHEAD WEB — CRACKED (BS 1520 S4L) · airframe 48,174 hrs · 25,610 cycles

AFT AIRSTAIR AREA AT BS 1520 STRINGER 4L BULKHEAD WEB IS CRACKED. REPAIRED BULKHEAD IAW ER/A 510925-14 REV O.

Part: STRINGER — CRACKED (BS 1520) · airframe 48,174 hrs · 25,610 cycles

AFT AIRSTAIR AREA SKIN AT BS 1520 CANTED BULKHEAD STRINGER 4R IS CRACKED. REPAIRED STRINGER IAW ER/A 510924-14 REV O.

Part: ANGLE — CORRODED (BS 1364) · airframe 48,174 hrs · 25,610 cycles

AFT LAVATORY BS 1364, LBL 20 ANGLE CORRODED. REMOVED CORROSION. 100 PERCENT MATERIAL LOSS. OUT OF LIMITS. REPAIRED IAW ER/A 510933-14, REV O.

Part: SUPPORT BRACKET — DAMAGED (LT MLG WW) · airframe 48,175 hrs · 25,611 cycles

LEFT WHEEL WELL PANEL SUPPORT BRACKET DAMAGED. R & R SUPPORT BRACKET IAW ER/A 510934-14, REV O.

Part: STRUCTURE — CORRODED (BS 1344) · airframe 48,174 hrs · 25,610 cycles

DURING HMV, FOUND AFT CARGO BS 1344, BETWEEN STR 25 AND 26L EVIDENCE OF CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED FILLER, TREATED, PRIMED AND INSTALLED IAW SRM 51-10-03, 51-20-00 AND ERA 510932-14, REV O.

Part: SEAT TRACK — CORRODED (BS 1364) · airframe 48,174 hrs · 25,610 cycles

AFT LAVATORY, BS 1364 LBL 22 SEAT TRACK UPPER END CORRODED. REMOVED CORROSION. OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, FIG 6.

Part: FLOORBEAM — CORRODED (BS 1364) · airframe 48,174 hrs · 25,610 cycles

AFT CABIN BS 1364, LBL 20 FLOORBEAM CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW ERA 510933-14, REV.

Part: FRAME — CORRODED (VERTICAL STAB) · airframe 48,174 hrs · 25,610 cycles

VERTICAL STABILIZER UPPER FORWARD END, LT SIDE FRAME FOR SKIN PANEL, CORRODED. WORK ACCOMPLISHED ON ER/A 510927-14, REV O.

Part: SKIN — CORRODED (VERTICAL STAB) · airframe 48,174 hrs · 25,610 cycles

VERTICAL TIP FORWARD END, RT SIDE FRAME FOR SKIN PANEL CORRODED. WORK ACCOMPLISHED ON ER/A 510927-14, REV O.

Part: WEB — CORRODED (BS 160) · airframe 48,174 hrs · 25,610 cycles

FORWARD GALLEY RT SIDE BS 160 SUPPORT WEB CORRODED. REMOVED CORROSION, OUT OF LIMITS IAW 53-00-01. OK FOR SERVICE IAW ERA 510923-14, REV O.

Part: SEAT TRACK — DAMAGED (BS 1174-1212) · airframe 48,174 hrs · 25,610 cycles

AFT CARGO COMPARTMENT BS 1174 TO 1212 LT SEAT TRACK SUPPORT HAS SEVERAL MISDRILLED HOLES. FABRICATED ALL SPLICES IAW SRM 53-40-01, PG 41.

Part: CARGO TRACK — DAMAGED (BS 1212-1250) · airframe 48,174 hrs · 25,610 cycles

AFT CARGO COMPARTMENT BS 1212-1250 LT CARGO TRACK HAS SEVERAL PREVIOUS MISDRILLED HOLES. INSTALLED CARGO TRACK LT, STA 1174-1250 IAW SRM 53-40-01, PG 40.

Part: CARGO TRACK — CORRODED (BS 1174-1212) · airframe 48,174 hrs · 25,610 cycles

AFT CARGO COMPARTMENT BS 1174 TO 1212 LT CARGO TRACK SUPPORT HAS LIGHT CORROSION AT SCREW HOLES. FABRICATED NEW CARGO TRACK SECTION IAW 53-40-01, FIG 7 FOUND ADDITIONAL DAMAGE. FOUND TO BE OUT OF LIMITS OF SRM 53-40-01.

Part: CARGO TRACK — CORRODED (BS 1079-1136) · airframe 48,174 hrs · 25,610 cycles

AFT CARGO COMPARTMENT BS 1079 TO 1136, LT CARGO TRACK SUPPORT HAS CORROSION AROUND HOLES INSTALLED LT CARGO TRACK IAW SRM 53-40-01 PG 40. OUT OF LIMITS IAW SRM 53-00-01, PG 9.

Part: SKIN — CORRODED (BS 788-845) · airframe 48,174 hrs · 25,610 cycles

RT SIDE LOWER EXTERNAL FUSELAGE SKIN CORRODED BS 788+10" - 845 AT FORWARD FILLET FAIRINGS. BLENDED AFFECTED AND FOUND SECOND AREA GOUGED BLENDED AREA OUT OF LIMITS IAW SRM 53-30-01. FABRICATED AND INSTALLED REPAIR SRM 53-30-01 PAGES 69-81.

Part: ATTACH ANGLE — CORRODED (BS 388) · airframe 48,174 hrs · 25,610 cycles

FORWARD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL WEB ATTACH ANGLE CORRODED FROM BS 388. REMOVED CORROSION. OUT OF LIMITS. R & R DAMAGED SECTION OF ATTACH ANGLE IAW SRM 53-60-02, FIG 11.

Part: CUSP WEB — CORRODED (BS 465) · airframe 48,174 hrs · 25,610 cycles

DURING HMV, RT CABIN CUSP WEB AT STA 465+4 HAS CORROSION ON THE TOP AND BOTTOM SIDE AS MARKED. CPCP 53-211-01. CHECKED LIMITS OF ORIGINAL .020 REMT .014 LOSS OF MATERIAL, .006 FOUND DAMAGED AREA OUT OF LIMITS IAW SRM 53-00-01, FIG 3, VOL I. FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 53-20-02, FIG 10, VOL I.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,749 hrs · 24,805 cycles

NR 114 STA 1475 STR 1 AND BETWEEN STR 2LT .250 SKIN CRACKED LOOKING UP FROM WALKWAY MARKED. REPAIRED PER ERA503973-14 REV ORIG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,749 hrs · 24,805 cycles

N/R 94 SKIN CRACKED LEFT SIDE STA 1475 FROM RIVET JUST OTBD OF SKATE ANGLE. REPAIRED PER ERA 503973-14 REV ORIG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,749 hrs · 24,805 cycles

N/R113 STA 1475 STR 1 AND BETWEEN STR 2 RT 1.5 IN SKIN CRACKED LOOKING UP FROM WALKWAY MARKED. REPAIRED PER ERA503973-14 REV ORIG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,749 hrs · 24,805 cycles

SKIN CRACKED RT SIDE STA 1475 FROM RIVET OUTBOARD OF SKATE ANGLE, N/R 90. REPAIRED PER ERA503973-14 REV ORIG.

Part: SKIN — WORN (VERTICAL STAB) · airframe 46,749 hrs · 24,805 cycles

WHILE PERFORMING VERTICAL STABILIZER LEADING EDGE SKIN INSPECTION EA_JIC 02-470871-12AD REV C ME01,9 LEADING EDGE HOLES WERE FOUND WORN AND WRITTEN ON NR CARD 99, PER STEP 3 OF SAME EA JIC, ME05 WAS ISSUED. THE LEADING EDGE WAS REMOVED ON NR 107 AND REPAIRS WERE ACCOMPLISHED PER SERVICE GENERAL REPAIR DRAWING SG09550004 WITH NO DEVIATIONS ON NR 108. THE LEADING EDGE WAS REINSTALLED ON NR 107 WHERE IT WAS PREVIOUSLY REMOVED.

Part: SKIN — DAMAGED (CARGO DOOR)

MID CARGO AFT DOOR FRAME SKIN DAMAGE. TRIMMED DAMAGED AREA NO EVIDENCE OF CRACKS. ACCOMPLISHED HFEC OF DAMAGE CUTOUT PER NPTSPM 06-10-01.001 NO CRACKS NOTED. REPAIRED DAMAGE PER ERA 503192-14, REV ORIG. OK FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 49,973 hrs · 26,624 cycles

FUSELAGE, MID CARGO DOOR CUTOUT, BS 750, DTA SKIN TRIM OUTER AFT EDGE.

Part: CABLE — FRAYED (TAILCONE) · airframe 46,065 hrs · 24,431 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND THE CABLE FOR THE TAIL CONE NITROGEN BOTTLE FRAYED. MAINTENANCE INSTALLED, RIGGED AND SAFETIED NEW CABLE PER JIC/OPN 69100.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 46,065 hrs · 24,431 cycles

DURING CHECK, MAINTENANCE FOUND 3 INCH CABLE FOR LOCKING HTE INSIDE HANDLE FRAYED. INSTALLED NEW CABLE, REF OPN 69100 CARD 1. TAILCONE EMERGENCY RELEASE MECHANISM. OPERATION CHECKS GOOD. RII C/W ON OPN 69100 QC 1978.

Part: TIRE — DAMAGED (NLG) · airframe 45,915 hrs · 24,352 cycles

UPON LANDING, WITH FULL RIGHT REVERSER AND MAX BRAKES, BRAKING ACTION WAS REPORTED NIL. AIRCRAFT SLID OFF RUNWAY. MAINTENANCE PERFORMED SIDE LOAD CHECKS. NO DEFECTS NOTED BESIDES NOSE TIRES. REMOVED AND REPLACED NOSE LANDING GEAR TIRES. AIRCRAFT OKAY FOR SERVICE.

Part: BRAKE — FIRE (MLG) · airframe 43,874 hrs · 23,388 cycles

AFTER LANDING AND TAXIING TO THE GATE, THE LEFT MAIN GEAR BRAKE WAS REPORTED BY THE RAMP TO BE ON FIRE. SOME PASSENGERS WERE EVACUATED THROUGH THE R1 SERVICE DOOR AND SLIDE. REPLACED THE NR 1 AND NR 2 BRAKE ASSEMBLIES, BOTH THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES, AND PERFORMED ANTI-SKID SYSTEM TEST. OPERATIONAL CHECK OF THE DUAL ANTI-SKID CONTROL MANIFOLDS CHECKED GOOD. ALL OTHER TESTS PASSED. THE R1 DOOR SLIDE WAS REPLACED PER THE AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 42,705 hrs · 22,890 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHT AT SEAT 1C INOPERATIVE. MAINTENANCE RE-TERMINATED THE WIRES AND OPERATION OF LIGHT NOW CHECKS OK. (2010-D1376) (DLM90103210)

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 42,092 hrs · 22,620 cycles

DURING LINE CHECK MX, FOUND EMERGENCY LIGHT INOPERATIVE AND MISSING LENS IN ROW 1. MX REPAIRED CRUSHED WIRING AND REPLACED MISSING LENS MODULE IN ROW 1. OPS CHECK OF LIGHT CHECKS OK.

Part: HYDRAULIC SYSTEM — LOW (RIGHT) · airframe 40,920 hrs · 22,018 cycles

JUST PRIOR TO DECENDING, RT HYD SYS QTY DROPPED TO 6, DID ABNORMAL IN QRH 1213. CONFIGUERED FOR LAND ICW QRH, LANDED W 28 DEGREE FLAPS. UNEVENTFUL SHUTDOWN WITH LT QTY 11 RT 8 DECLARED EMERGENCY LANDING.

Part: LIGHT — INOPERATIVE (ROWS 13C & 14C) · airframe 40,774 hrs · 21,917 cycles

EMERGENCY ESCAPE PATH LIGHTS INOP AT SEAT ROWS 13C AND 14C. REPLACED ENTIRE FLOOR TRACK LIGHTING FROM ROWS 10 THRU 14 ALL LIGHTS NOW TEST OK.

Part: SLIDE — INOPERATIVE (L2 DOOR) · airframe 40,499 hrs · 21,756 cycles

DURING A PLANNED 2L DOOR SLIDE DEPLOYMENT IAW OP 6800 THE SLIDE DID NOT INFLATE. THIS OCCURRED ON 1-20-10. THE SLIDE PACK WAS ATTACHED TO THE FLOOR FITTINGS AND EXITED THE DOOR CAVITY BUT MERELY HANGED OUTSIDE THE ACFT WITHOUT INFLATING. THE OP 6800 DATA RETRIEVAL WAS SUBMITTED INDICATING THIS AND A SERVICEABLE SLIDE WAS INSTALLED ONTO THE 2L DOOR. THE SLIDE WHICH FAILED TO DEPLOY WAS SENT FOR SHOP EVALUATION WITH ALL NECESSARY DOCUMENTATION.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 37,496 hrs · 19,995 cycles

HIT BIRD AT ABOUT 135 KTS. HIGH SPEED ABORT ACCOMPLISHED AND PARKED WITH HOT BRAKES. RT ENGINE FLUCTUATED AND HAD NOTICABLE POWER LOSS WITH THE BIRD STRIKE. BRAKE TEMP REACHED 650. REPLACED NR 2 ENGINE.

Part: BRAKE — LEAKING (LEFT MLG) · airframe 35,869 hrs · 19,033 cycles

A/C ARRIVED AND HAD A HOT BRAKE NR 2, BRAKE WAS LEAKING HYD FLUID AND STARTED BURNING. FIRE WENT OUT ON ITS OWN. REPLACED NR 1 AND NR 2 BRAKE ASSYS PER M/M.

Part: GENERATOR — ODOR · airframe 32,961 hrs · 17,401 cycles

ELECTRICAL SMELL/SMOKE IN THE CABIN ON ROTATION FROM SJC. CREW ELECTED TO RETURN TO SJC. INFLIGHT EMERGENCY WAS DECLARED. ODOR DISSIPATED PRIOR TO LANDING. NO EMERGENCY DOOR SLIDES WERE BLOWN AND NO INJURIES REPORTED. REPLACED CONVERTER ELECTRONICS UNIT AND INTERCONNECTING HARN ASSY 475757.

Part: GENERATOR — LACK OF LUBE (NR 1 ENGINE) · airframe 31,293 hrs · 16,436 cycles

AT CRUISE POWER DISRUPTED W/L AC PWR FAULT AND L GEN OFF MSG GEN WOULD NOT RESET. ACCOMPLISHED QRH PROCEDURE. LEFT BUS RECEIVED PWR FROM APU GEN BUT APU FAULT MSG ILLUMINATED. L ELEC SYS FAIL AND L GEN OIL PRESS MSGS APPEAR WHEN STATUS BUTTON PUSHED. (ATL MTC/0245Z/MB) PRIOR TO DES APU GEN TRIP FOUND LT GEN HAD LOST ALL OIL. REPLACED LT GEN. ALSO FOUND RIGID FLEX LINE TO OIL COOLER LEAKING. REPLACED RIGID FLEX LINE TO OIL COOLER, LEAKED CHECKED LINE AND CHECKED LT GEN FOR PROPER SERVICING, ALL OK L GEN VOLTS AND FREQS CKD OK AND CARRIED LOAD. RAN APU SEVERAL TIMES WITH FULLY LOADED BUSES APU GEN OPS GOOD.

Part: STARTER — UNSERVICEABLE (APU) · airframe 30,675 hrs · 16,095 cycles

ON APU START, APU FAULT DISPLAYED AND SMOKE COMING FROM TAIL COMPT. ON FURTHER INSP, SAW VISIBLE FLAME COMING FROM APU STARTER. FLAME WENT OUT AND NO EXTINGUISHING AGENT WAS NEEDED. REPLACED STARTER, CLUTCH, AND START RELAY.

Part: BRAKE — LEAKING (MLG) · airframe 28,680 hrs · 15,032 cycles

HYDRAULIC QTY LOW LT HAND. FOUND NR 1 BRAKE ASSEMBLY LEAKING FROM THE SIX O`CLOCK POSITION. REMOVE AND REPLACE NR 1 BRAKE ASSY AND SERVICED LT HYDRAULIC SYSTEM AS PER AMM. NO LEAKS FOUND.

Part: COFFEEMAKER — DIRTY (GALLEY) · airframe 28,660 hrs · 15,021 cycles

CLEANED BURNED COFFEE FROM HOT PLATE IN AFT GALLEY DUE TO BURNING SMELL.

Part: ENGINE — FAILED (NR 2) · airframe 27,494 hrs · 14,425 cycles

AS POWER WAS PUSHED UP FOR TAKEOFF RIGHT ENGINE OIL PRESSURE LO LIGHT CAME ON AND OIL PRESSURE INDICATED ZERO. SHUT DOWN ENGINE AFTER APPROX 10 SECONDS. REPLACED ACCESSORY GEARBOX.

Part: STRUT — LOW (NLG) · airframe 25,297 hrs · 13,393 cycles

NOSE GEAR FAILED TO RETRACT ON T/O, 3 VGRN WITH GEAR HANDLE DOWN. SERVICED NOSE GEAR PER M/M 32-21-01-619-801, NOSE GEAR OPERATION CHECKS NORMAL.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 23,886 hrs · 12,671 cycles

NUMBER 2 ENGINE SHUT DOWN ON DESCENT INTO DFW. FOUND NUMEROUS VSV AND ACC FAULTS. REPLACED ENGINE.

Part: DOOR — OPEN (NLG) · airframe 23,758 hrs · 12,602 cycles

AIRCRAFT HAD AN AIR TURNBACK. UPON GEAR RETRACTION, NOSE GEAR MADE A LOUD NOISE AND CONTINUED TO SPIN. NO GEAR OR GEAR DOOR LIGHTS. GEAR ALSO VIBRATED. ONCE AT GATE MAINTENANCE FOUND THE LEFT NOSE GEAR DOOR OPEN. RESECURED NOSE GEAR DOOR.

Part: SCREW — LOOSE (E/E BAY) · airframe 22,154 hrs · 11,795 cycles

AIR TURNBACK, 2L DOOR HAD A LARGE AIRLEAK AUTO CONTROLLER DID NOT HAVE OUTFLOW VALVE FULL CLOSED. GOT CABIN ALT WARN LIGHT CABIN WAS AT 10000 FT/BIT AUTO CONTROLLER 1 FAULTED GROUND SWITCH. PRESSURIZED A/C PER M/M, NO DOOR LEAKS NOTED. FOUND LOOSE SCREW HAD FALLEN INTO RELAY R2-4 SHORTING TERMINALS D1 AND D2. REPLACED RELAY. PERFORMED BIT TEST PER PER M/M. ALL CKS GOOD. PERFORMED TEST OF SYS AND FOUND SYS TESTS NORMAL.

Part: GENERATOR — MAKING METAL (NR 1 ENGINE) · airframe 18,978 hrs · 10,166 cycles

LT AC FAULT MSG IN FLT, LT GEN OIL FILTER STATUS MSG. FOUND METAL IN GEN FILTER. REPLACED GEN, OP CHECKS OK.

Part: STARTER — MALFUNCTIONED (APU) · airframe 18,912 hrs · 10,132 cycles

ON APU START ATTEMPT AT THE GATE IN SNA. SMOKE WAS OBSERVED COMING FROM APU COMPARTMENT. MTC OPENED COMPT AND OBSERVED THE STARTER GLOWING RED. FIRE DEPT DISCHARGED HALON INTO COMPT. CTC MTC ADVISED THERE WERE FLAMES INITIALLY WHEN DOOR WAS OPENED. REPLACED APU.

Part: RESERVOIR — LEAKING (RT MLG WW) · airframe 18,315 hrs · 9,820 cycles

LOSS OF RT HYD PRESSURE, WENT TO ZERO AND OVERTEMP. FOUND RT HYD RES. LEAKING INTERNALLY. REPLACED SAME.

Part: INDICATOR — FALSE INDICATION (COCKPIT) · airframe 18,128 hrs · 9,719 cycles

AFTER RAISING GEAR RT MAIN RED LIGHT REMAINED ON. ALL GREENSOUT, GEAR DOOR LIGHT OUT, LOWERED LANDING GEAR PER CKLIST ALL 3 GREEN ON, ALL REDS OUT BUT DOOR LIGHT REMAINED ON FOR APPROX. 2 MIN. LANDING GEAR DOOR LIGHT FLICKERED ON/OFF UNTIL A/C WAS SLOWED FOR APPROACH DOOR LIGHT WENT OUT - JACKED A/C AND SWUNG GEAR - TESTED PROX SWITCHES - NO TROUBLE FOUND - UNABLE TO DUPLICATE

Part: WIRE — DAMAGED (CABIN) · airframe 17,662 hrs · 9,480 cycles

EMERGENCY FLOOR TRACK LIGHTING INOP.FROM 2C TO 12C. FOUND WIRE DAMAGED AT SEAT 2C.REPAIRED SAME.

Part: WIRE — BROKEN (SEAT 13) · airframe 15,435 hrs · 8,299 cycles

FOUND EMERGENCY TRACK LIGHT AT SEAT 13 WITH BROKEN WIRING. SPLICED NEW SOCKET IN LINE, OPERATIONAL CHECKS OK.

Part: VALVE — INOP (LT PACK)

LT PACK FLOW OF ABOUT 20 PERCENT FLOW LIGHT ON FROM T/O TO 10,000. NO CHANGE IN FLOW PERCENT. RATE OF A/C CLIMBING SLOWED TO 1000 PPM, STILL HAD FLOW LITE. REPLACED LT PACK FLOW CONTROL VALVE. A/C PRESSURIZED GOOD.

Part: SCHRADER VALVE — FAILED (NLG)

ON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON WITH HANDLE UP. NLG INDICATOR WAS FLUSH, RECYCLED IN ACCORDANCE WITH POM BUT LIGHT STAYED ON WHEN ANOTHER RETRACTION WAS ATTEMPTED. REPLACED NOSE STRUT SCHRADER VALVE AND O-RING. SERVICED STRUT IN ACCORDANCE WITH MAINT MANUAL. PERFORMED NOSE GEAR RETRACT CHECK, OPERATION NORMAL.

Part: WIRE — BROKEN (CABIN)

ON PREFLIGHT, FLOOR EMERGENCY PATH LIGHTS INOP IN FWD CABIN. FOUND BROKEN WIRE AT SEAT ROW 10. REPAIRED WIRE, OPERATION NORMAL.

Part: HYD TUBE — LEAKING (FS 1322)

IR - L-SYSTEM HYD QTY READS 8 QTS. ON WALK-AROUND, SAW FLUID LEAKING FROM 2 DRAIN HOLES AFT OF MAIN GEAR. FOUND FWD PRESS LINE TO EMPENNAGE RUBBED THROUGH ON OUTFLOW VALVE ACTUATOR AT LT FS 1322. REVERSED BOLTS TO GAIN CLEARANCE AND MADE PERMANENT REPAIR TO LINE WITH RING LOCK.