N753RA

Part: AHRS — FAILED (NR 2) · airframe 39,035 hrs · 26,097 cycles

AIRCRAFT RETURNED OF FLIGHT, 30 DEGREES OF COURSE VARIATION AND CAPTAIN HSI WITH 15 DEGREE OF DIFFERENCE IN RESPECT TO THE COMPASS. DURING CHECK, SWITCH WAS DETECTED IN NORMAL POSITION, HSI CAPTAIN OPERATING NORMALLY, CAPTAIN COURSE WITH 10 DEGREE OF DIFFERENCE IN RESPECT TO THE COMPASS, HSI FIRS OFFICES FELT 5 DEGREE, FIRST OFFICER COURSE WITH 10 DEGREE DIFFERENCE WITH RESPECT TO THE COMPASS AND AN AHRS NR 2 MODE BASIC LIGHT TURNED ON. AHRS NR 1 WAS RESEATED AND RESTORED AND AHRS NR 2 WAS DEFERRED IAW MM 34-38. DURING OVERNIGHT SERVICE AHRS NR 2 WAS REPLACED IAW MM 32-2-10, TESTS WERE CORRECT.

Part: VALVE — FAILED (NLG STEERING) · airframe 38,825 hrs · 25,949 cycles

AFTER LANDING, DURING TAXI, AIRCRAFT WAS NOT TURNED TO RT SIDE, BEING NECESSARY TO USE A TRUCK TO SEND THE AIRCRAFT TO PLATFORM. DURING MAINTENANCE REVISION, THE STEERING CABLE WAS DETECTED WITH DAMAGE. THE CABLE 268 WAS BROKEN. DURING OVERNIGHT SERVICE, CABLE 268 WAS REPLACED AND ADJUSTED IAW MM 32-51-03, TEST CORRECT. DURING OVERNIGHT SERVICE, STEERING CABLE 123D, BOTH NOSE LANDING WEAR WHEELS AND STEERING VALVE WERE REPLACED IAW MM 32-51-00, 32-40-02 AND 32-52-01, RESPECTIVELY, TEST WAS PERFORMED IAW MM 32-52-00, ALL CORRECT.

Part: COOLING TURBINE — FAILED (CABIN COOLING) · airframe 33,743 hrs · 25,201 cycles

DURING TRANSIT CHECK SMOKE IN CABIN WAS REPORTED WHEN GROUND PNEUMATIC UNIT WAS CONNECTED AND LT AIR CONDITIONING SYSTEM WAS ACTIVATED. THE SYSTEM WAS CHECKED AND NO SMOKE EVIDENCE WAS DETECTED. BOTH AIR COOLING TURBINES WERE CHECKED AND LT AIR CONDITIONING SYSTEM WAS DEFERRED IAW MEL 21-1. DURING OVERNIGHT SERVICE AT GDL, LT TURBINE COOLING WAS REPLACED IAW MM 21-51-1, TEST CORRECT.

Part: IGNITER BOX — FAILED (RT ENGINE)

AIRCRAFT RETURNED TO PLATFORM, THE RT ENGINE DID NOT START WHEN THE FUEL CONTROL WAS PUT ON, SHUTTING DOWN THE IGNITION AND THE START VALVE. THE IGNITION BOX WAS REPLACED AND SYSTEM TESTED IAW MM, ALL CORRECT.

Part: LANDING GEAR — OBSTRUCTED (MAIN)

FLT 920 - MEX-MTY - AIRCRAFT RETURNED DUE TO NOSE LANDNG GEAR RETRACTION WAS CLOGGED. ANTI-RETRACTION SECURE WAS USED AND NOSE LANDNG GEAR RED LIGHT TURN ON. AIRCRAFT DID NOT PRESSURIZE AND WINDSHEAR AND STALL INDICATION FAILURE LIGHTS TURN ON. AIRCRAFT WAS SENG TO THE HANGAR TO ATTEND THE FAILURE. NOSE GEAR STRUT SERVICE WAS PERFORMED IAW MM 32-21-02. LANDING GEAR CONTROL LEVER AND ANTI-RETRACTION LATCH WERE INSPECTED FOR OBSTRUCTION AND CONDITION IAW MM 32-31-01, ALL CORRECT. NOSE LANDING GEAR WAS TESTED IAW MM 32-30-00. (M)

Part: RELAY — DAMAGED (STALL WARNING)

AIRCRAFT RETURN TO PLATFORM AS DUE TO RIGHT STALL LIGHT ON. DURING CHECK WAS DETECTED THAT THE RELAY R2-58 DAMAGED. IT WAS CHANGED AND TESTS WERE PERFORMED IAW MM.

Part: RELAY — FAILED (FLIGHT DIRECTOR)

FLT 579 - MEX-CUN - AIRCRAFT RETURN TO PLATFORM DUE TO SIF LIGHT TURN ON AND BOTH FLIGHT DIRECTORS DISAPPEAR ON TAKEOFF MODE. DURING CHECK IT WAS DETECTED THAT THE RELAY R2-6 MAINTAINS IN FLIGHT MODE ALL THE TIME. RELAY WAS REPLACED AND TESTS WERE PERFORMED IAW MM 34-19-00. (M)

Part: ACTUATOR — FAILED (NLG)

AIRCRAFT RETURN AS A CONSEQUENCE OF NOSE LANDING GEAR DOOR NOT RETRACTING AND A PRESSURIZATION FAILURE. AIRCRAFT WAS SENT TO THE HANGAR. REPLACED THE NOSE GEAR ACTUATOR ASSEMBLY, NOSE GEAR BUNGEE CYLINDER, NOSE GEAR CONTROL VALVE, AND O-RINGS IAW MM. TESTS OK IAW MM. IN RELATION TO THE PRESSURIZATION REPORT, THE RIGHT FAN AND TWO CIRCUIT BREAKERS WERE CHANGED IAW MM.

Part: FILTER — DIRTY (OIL SYSTEM)

FLT 501 - MEX-OAX - AIRCRAFT SUSPENDS TAKEOFF AS A CONSEQUENCE OF STRAINER CLOGGING OIL FILTER LIGHT COMES ON. STRAINER FILTER AND SWITCH OIL FILTER WAS REPLACED IAW MM 79-20-06 AND 79-34-01, TESTS OK. (M)

Part: HYDRAULIC LINE — BROKEN (HYD SYSTEM)

FLT 402 - PVR-MEX - DURING TRANSIT CHECK DETECTED A LEAK IN THE RIGHT HYDRAULIC SYSTEM. A BROKEN LINE AT ACCESSORY COMPARTMENT AFFECTING THE VENTRAL STAIRWAYS, THE RIGHT ENGINE REVERSE AND THE DIRECTION RUDDER. A FLEXIBLE TUBE WAS INSTALLED. DURING OVERNIGHT SERVICE WAS INSTALLED A STEEL TUBE AND THE SYSTEM WAS CHECKED IAW MM 29-01-03. (M)

Part: SWITCH — FAILED (HYD SYSTEM)

FLT 434 - LAP-PHX - DURING TRANSIT CHECK AN HYDRAULIC LEAK WAS DETECTED IN THE LOWER PART OF THE REAR ACCESSORIES COMPARTMENT. THE RIGHT SYSTEM WAS EMPTY. THE RIGHT SYSTM WAS RECHARGED WITH 6 QUARTS TO FIND SUCH LEAK. LEAK WAS DETECTED WAS IN A PIPE LINE OF THE RUDDER SHUTOFF VALVE. THE PIPE LINE WAS REPLACED. AT ENGINE STARTING CAPTAIN REPORTED RT HYD PRESS LOW LIGHT WAS TURNED ON, AIRCRAFT WAS DISPATCHED BY MEL 29-5 CAT 'C'. AT MTY, THE HYDRAULIC PRESSURE SWITCH WAS REPLACED. (M)

Part: APU — LEAKING (APU BAY)

FLT 419 - MEX-VSA - CREW REPORTED THE PRESENCE OF SMOKE IN THE PASSENGER CABIN AND SMOKE DETECTORS ACTIVATED IN THE LAVATORIES. LEFT A/C PACKAGE AND COOLING TURBINE CHIP DETECTOR WAS CHECKED, OK, IT WAS FOUND OIL WASTES FROM THE PNEUMATIC APU. (M)

Part: A/C PACK — CONTAMINATED (CABIN COOLING)

FLT 419 - MEX-VSA - 5 MINUTES BEFORE PUSH BACK, CAPTAIN REPORTED THE PRESENCE OF SMOKE INSIDE THE CABIN, BOTH SMOKE DETECTORS IN THE REAR LAVATORIES WERE ACTIVATED. FOUND OIL LEAKED INTO THE COOLING TURBINE OF THE LEFT A/C PACK. AIRCRAFT WAS DISPATCHED IAW MEL 21-1. AT RON MEX 03/04 IT WAS REPLACED THE ASSY COOLING TURBINE AND WATER SEPARATOR IAW MM 21-01 AND 21-20-2, TESTS OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SJC - FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE, RELAMPED. NO LAMP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK OK. (M)

Part: O-RING — CUT (FCU)

AIRCRAFT GROUND INTERRUPTED AND SHUTDOWN NR 1 ENGINE WITH A LEAK REPORTED BY ANOTHER AIRCRAFT. FOUND FUEL LEAK BETWEEN FUEL CONTROL AND ENGINE FUEL PUMP. PLAN TO REPLACE FUEL CONTROL AND ENGINE FUEL PUMP OR SEALS AS REQUIRED. FOUND CUT O-RINGS ON FUEL CONTROL. REPLACED CUT O-RINGS. LEAK CHECK OK DURING ENGINE RUN. (M)

Part: LIGHT — INOPERATIVE (CABIN)

CCI - ROW 14 SEAT EMERGENCY LIGHT INOPERATIVE. RECONNECTED WIRE AND SECURED. OPS CHECK GOOD. (M)

Part: HYDRAULIC LINE — DAMAGED (RT HYD SYS)

RIGHT HAND HYDRAULIC SYSTEM LOST QTY AND PRESSURE ON APPROACH TO LAX. PERFORMED EMERGENCY PROCEDURE AND LANDED NORMALLY. REPLACED HYDRAULIC HOSE.

Part: BATTERY PACK — DISCHARGED (CABIN)

SNA - LAST 4 ROWS OF EMERGENCY LIGHTS ILLUMINATED IN LAST 15 MINUTES OF FLIGHT. TURNING COCKPIT SWITCH OFF AND BACK TO ARM HAD NO EFFECT. REPLACED BATTERIES FOR SEAT EMERGENCY LIGHTING CHECK OK. (M)

Part: WIRE — DISCONNECTED (CABIN)

SJC-CCI - NR 24 EMERGENCY LIGHT INOPERATIVE. RECONNECTED WIRE. OPS CHECK NORMAL. (M)

Part: UNKNOWN — ODOR (CABIN)

RNO - AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED ODOR IN CABIN, DESCRIBED AS BURNING MATCHES. ODOR DISSIPATED SHORTLY THEREAFTER. CONTINUED FLIGHT. NO FURTHER OCCURRENCE. INSPECTED BOTH ENGINES AND APU FOR OIL LEAKS AND HYDRAULIC LEAKS, NONE NOTED. RAN ENGINES AND APU AND BOTH PACKS FOR SEVERAL MINUTES. NO ODOR IN CABIN. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

RNO-CCI - 2 UPPER EMERGENCY PAMPS WHICH SHINE DOWN ON TAIL SLIDE INOPERATIVE. REMOVED AND REPLACED CHARGER. OPS CHECK GOOD. (M)

Part: SKIN — MISREPAIRED (FUSELAGE)

OKC - NR 1000-0026 - EXTERNAL REPAIR AT STATION 1030 BETWEEN LONGERON 23L TO 26L IS NOT PER THE SRM. FABRICATED AND INSTALLED ALL REPAIR PARTS IAW MD80 SRM 53-03 FIG 3, 7 AND DWG NR 53-00141-1. LEAK CHECK GOOD IAW MD80 MM 21-00-00. (M)

Part: WIRE — BROKEN (TAIL)

TAIL SECTION AFT EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE. OPS CHECK GOOD PER MM. (M)

Part: BATTERY — INOPERATIVE (TAIL)

TAIL SECTION OVERHEAD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CELL BATTERIES IN POWER SUPPLY. OPS CHECK GOOD PER MM. (M)

Part: AIR DISTR — SMOKE (CABIN)

AT LAX, CABIN FILLED WITH OIL SMOKE AFTER TAKEOFF, TURNED OFF BOTH PACKS AT 5000 FT, OPENED OUTFLOW VALVE. SMOKE SUBSIDED, LANDED AT LAX. REPLACED SET OF COALESCER BAGS, CLEANED WATER SEPARATORS AND PEFORMED BURNOUT OF HIGH PRESSURE PNEUMATIC DUCTING AS OUTLINED IN MM 21-20-02, PAGES 209-216. RAN PACKS, NO SMOKE NOTED. (M)

Part: WIRE — BROKEN (ROW 14)

AT SJC, EMERGENCY LIGHT AT ROW 14 INOPERABLE. REPAIRED WIRING AT TWO PLACES. OPS CHECK GOOD. (M)

Part: BATTERY — DISCHARGED (TAIL)

AT RENO, EMERGENCY EXIT LIGHT INSIDE TAIL SECTION INOPERATIVE. REMOVED AND REPLACED BATTERY. OPS CHECK GOOD. (M)

Part: RELAY — FAILED (E/E BAY)

AT SAN DIEGO, 'DC BUS OFF' ANNUNCIATION ON APPLICATION OF TAKEOFF POWER SETTING. ABORTED TAKEOFF AT LOW SPEED, APPROX 20 KTS. RETURNED TO GATE. REPLACED EMERGENCY POWER DC TRANS RELAY (R2-326). GROUND CHECK NORMAL. (M)

Part: RELAY — FAILED (E/E BAY)

'DC BUS OFF' ANNUNCIATION ON APPLICATION OF TAKEOFF POWER SETTING ABORTED TAKEOFF AT SLOW SPEED (APPROX 20 KNOTS). RETURNED TO GATE. REPLACED EMERGENCY POWER DC TRAN RELAY (R2-326). GROUND CHECK NORMAL. (M)

Part: INDICATOR — FAILED (COCKPIT)

AT SJC, TAKEOFF WAS DISCONTINUED AS NR 2 ENGINE EPR INDICATION NEVER GOT ABOVE 1.3, APPROXIMATELY. REMOVED AND REPLACED NR 2 ENGINE EPR GAUGE AND PERFORMED ENGINE RUN IAW MM 71-00-00. OPS CHECKED GOOD. (M)

Part: LIGHT — INOPERABLE (CABIN)

ROW 9 EMERGENCY FLOOR TRACK LIGHT INOPERABLE. REPAIRED BROKEN WIRES. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERABLE (CABIN)

ROA 20B EMERGENCY RED LIGHT INOP. FOUND LOOSE WIRE AT 20B EMERGENCY LIGHT. OPS CHECKED GOOD. (M)

Part: WIRE — BROKEN (CABIN)

EMERGENCY EXIT LIGHT OUT AT ROW 11 SEAT D. REPAIRED BROKEN WIRES ON LIGHT. OPS CHECK GOOD. (M)

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHT OUT AT SEAT 23D. REPAIRED BROKEN WIRE AT SEAT 23D. OPS CHECK GOOD. (M)

Part: WIRE — FAILED (CABIN)

EMERGENCY LIGHT AT ROW 14 INOP. REPINNED BROKEN WIRE AT CONNECTOR. OPS NOW OK. (M)

Part: WIRE — FAILED (CABIN)

EMERGENCY LIGHT INOP AT ROW 9 DEF AND 19 DEF. REPAIRED WIRING. OPS CHECK GOOD. (M)

Part: WIRE — DISCONNECTED (CABIN)

EMERGENCY LIGHTS AT SEAT 9DEF WILL NOT ILLUMINATE. RECONNECTED BROKEN WIRE, OPS CHECK OK. (M)

Part: WIRE — DISCONNECTED (CABIN)

EMERGENCY LIGHT ROW 10 INOP. RECONNECTED WIRE UNDER SEAT 10F, OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

BOTH EXTERIOR EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. OPS CHECK GOOD PER MM 33-53-00. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

SEVERAL EMERGENCY LIGHTS ON SEATS INOP. REPAIRED BROKEN WIRES. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

SEAT EMERGENCY LIGHT INOPERABLE AT ROW 18. REPAIRED BROKEN WIRE. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

SEAT EMERGENCY LIGHT INOPERABLE AT ROW 22. REPAIRED BROKEN WIRE. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

SEAT EMERGENCY LIGHT INOPERABLE AT ROW 17. REPAIRED BROKEN WIRE. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHT AT ROW 10 INOPERABLE. FOUND BROKEN WIRES AT ROW 10. RE-SPLICED PER MM. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHT, AT ROW 21, INOPERABLE. FOUND BROKEN WIRES AND SPLICED TOGETHER IAW MM. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — LOOSE (CABIN)

EMERGENCY LAMP AT ROW 20 INOPERABLE. RE-SECURED WIRE CONNECTION AT ROW 20; OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: LIFEVEST — MISSING (CABIN)

LIFEVESTS AT SEAT ROW 15 AND 22 MISSING. REPLACED AS REQUIRED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

EMERGENCY TRACK LIGHTS INOP AT SEATS 7D AND 8D. BROKEN WIRES FOUND. WIRES SPLICED WITH ENVIROMENTAL SPLICES DUE TO LACK OF CONNECTOR/PIN TOOLING. LIGHTS OPS CHECKED NORMAL. (M)

Part: ENGINE — MALFUNCTIONED (RIGHT)

SHORTLY AFTER TAKEOFF, 200 FT APPROX, RIGHT ENGINE BEGAN SURGING. AT 500 FEET, LEFT ENGINE STARTED SURGING. RETURN TO LAND. LANDING WEIGHT 139.9. THROUGH ICE INSPECTION PERFORMED PRIOR TO DEPARTURE DUE TO PREVIOUS ICE REPORTS AT DETROIT. ALL SURFACES WERE ICE FREE. (M)

Part: TRACK — CORRODED (BS 984-1030)

AFT CARGO PIT HAS MULTIPLE SPOTS ON LEVEL 2 CORROSION ON THE RIGHT TIE DOWN TRACK, STATION 984-1030, AND LEFT TIE DOWN TRACK, STATION 1003-1129. REPAIRED TRACK SECTIONS AS REQUIRED IAW SRM 53-0-1 AND 51-10-3. REF AAR NON-ROUTINE AND 1000-0019 AND NR 1000-0020. (M)

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

ON TAKEOFF NORMAL POWER ABOUT 800 AGL LEFT ENGINE COMPRESSOR STALLED, THROTTLE REDUCED TO IDLE. POWER ADVANCED ENGINE RAN OK. RETURNED TO RENO. REMOVED AND REPLACED NR 1 ENGINE IAW CARD 0099 AND MM 71-00-00. ALL PARAMETERS NORMAL, NO LEAKS NOTED. (M)

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHTS OUT AT 6-DEF AND 15-DEF. AT 6-DEF REPINNED CONNECTOR. OPS CHECK NORMAL. AT 15-DEF REPAIRED WIRE BY SPLICE. OPS CHECK NORMAL. (X)

Part: WIRE — FAILED (CABIN)

EMERGENCY EXIT TRACK LIGHT OUT AT SEAT ROW 22. REPAIRED WIRING. OPS GOOD. (X)