N169PL

Service difficulty reports not matched to an aircraft · 55

They name N169PL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N169PL' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASMF200710012Brake · failedCAPTAIN REPORTED THAT DURING TAXING AT RUNWAY THRESHOLD, THE TEMPERATURE OF THE MAIN LANDING GEAR BRAKE NR 1 REACHED 450 CELSIUS DEGREES, SO IT WAS NECESSARY TO STOP THE AIRCRAFT. MAINTENANCE PERSONNEL REPLACED THE LT BRAKE ASSY AND THE MAIN LANDING GEAR WHEEOct 30, 2007 · N169PL · Doug MD88 · Landing Gear Brake SystemSDR ASMF200709010Actuator · damagedCAPTAIN REPORTED THAT IT WAS NECESSARY TO ADJUST THE RUDDER TRIM COMPENSATOR 7 UNITS TO THE RIGHT IN FLIGHT. AT PLATFORM, MAINTENANCE PERSONNEL REPLACED THE RUDDER HYDRAULIC POWER PACKAGE AND THE YAW DAMPER ACTUATOR IAW MM 27-20-04 AND 22-13-01 RESPECTIVELY, Sep 28, 2007 · N169PL · Doug MD88 · Rudder Control SystemSDR ASMF200707010Skin · crackedDURING TRANSIT CHECK, THE AIRCRAFT WAS HIT BY A GATEWAY PROMOTING A CRACK OF 3 INCHES LONG IN FUSELAGE SKIN LOCATED AT STA 271, BETWEEN LONGERONS 17 AND 18 LEFT SIDE. THE NON ROUTINE CARD A0116633 WAS ISSUED, TO REPAIR DAMAGE. REPAIR DETAILS WILL BE SENT AS A Jul 14, 2007 · N169PL · Doug MD88 · Fuselage Main, Plate/SkinSDR ASMF200706004Vortex Gen · damagedDURING TRANSIT CHECK, THE AIRCRAFT WAS HIT BY A GROUND HANDLING TRUCK IN THE LOWER SECTION OF RIGHT WING, DAMAGING IN THE VORTILON AND IN THE FORWARD INBOARD FLAP HINGE FAIRING. MAINTENANCE PERSONNEL REPLACED VORTILION IAW MM 57-20-04 AND THE FORWARD INBOARD FJun 17, 2007 · N169PL · Doug MD88 · Wing Miscellaneous StructureSDR ASMF200705004Line · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO SMOKE ODOR IN PASSENGERS CABIN. A HYDRAULIC LEAK WAS DETECTED IN THE APU INLET DUCT. THE HYDRAULIC LEAK WAS REPAIRED AND WATER SEPARATORS WERE REPLACED IAW MM 21-20-02, TESTED CORRECT. DURING BOARDING, THE HYDRAULIC ODOR WAMay 6, 2007 · N169PL · Doug MD88 · Hydraulic System, MainSDR ASMF200705003Line · leakingDURING TRANSIT CHECK, A LOW HYDRAULIC LEVEL WAS DETECTED IN THE LT SYSTEM WITH AN INDICATION OF 6 QUARTERS. DURING MAINTENANCE INSPECTION, THE LEAK WAS CONFIRMED IN THE LT MAIN WHEEL WELL, SO AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, HYDRAULIMay 4, 2007 · N169PL · Doug MD88 · Hydraulic System, MainSDR ASMF200705001Line · looseAIRCRAFT RETURNED TO PLATFORM, THE LT HYDRAULIC HIGH TEMP LIGHT TURNED ON AND DURING TAXI, THE HYDRAULIC QUANTITY VARIATION 17 - 7 QUARTERS. DURING MAINTENANCE CHECK, THE LT HYDRAULIC SYSTEM QUANTITY WAS CHECKED AND DETECTED WITH LOW LEVEL. THE LT HYDRAULIC REMay 1, 2007 · N169PL · Doug MD88 · Hydraulic System, MainSDR ASMF200703005Apu · failedAIRCRAFT RETURNED DUE TO FUEL ODOR IN THE CABIN AT 28,000 FEET. THE UPPER AND LOWER WING PANELS AND APU WERE CHECKED AND NO LEAKS WERE DETECTED. NEVERTHELESS, THE AIR CONDITIONING WATER SEPARATORS AND ENGINES WERE CHECKED BY CONDITION AND LEAKS AND NO ODOR NEIMar 12, 2007 · N169PL · Doug MD88 · APU Core EngineSDR ASMF200702008Fuel Control · failedAIRCRAFT RETURNED TO PLATFORM DUE TO RT ENGINE DID NOT ACCELERATE. THE PARAMETERS WERE RT ENGINE N2 54 PERCENT, N1 29 PERCENT AND LT ENGINE N2 56 PERCENT, N1 26 PERCENT, EGT 472 RT AND 462 LT AND FUEL FLOW 87 RT AND 53 LT. AIRCRAFT WAS SENT TO THE HANGAR AND DFeb 27, 2007 · N169PL · Doug MD88 · Fuel Control/Turbine EnginesSDR ASMF200702004Fuel Control · failedAIRCRAFT RETURNED TO PLATFORM, LT ENGINE DID NOT STABILIZE IN IDLE, THE PARAMETERS WERE THE FOLLOWING: EPR´S 1.03, N1 20, EGT´S 486 DEGREE C, N2 44, FF 9700 POUND. LT ENGINE WAS TRIMMED IN IDLE WITH EPR´S 1.03, N1 27, EGT´S 460, N2 55, FF 1160 IAW MM 71-00-00Feb 12, 2007 · N169PL · Doug MD88 · Fuel Control/Turbine EnginesSDR ASMF200701006Inlet · obstructedCAPTAIN REPORTED SMOKE ODOR IN THE CABIN. AIR CONDITIONING SYSTEM WAS SHUTDOWN AND APU DOORS WERE CHECKED, DETECTING A PLASTIC IN THE APU INLET. PLASTIC WAS REMOVED AND WATER SEPARATORS WERE REPLACED IAW MM 21-20-2, TESTED CORRECT. DURING BOARDING, CAPTAIN REPJan 23, 2007 · N169PL · Doug MD88 · APU Core EngineSDR ASMF200610005Water Separator · fullAIRCRAFT RETURNED TO PLATFORM DUE TO EXCESSIVE WATER DRIPPED IN THE PASSENGERS CABIN AT ROW 24 NEAR TO THE AFT GALLEY. THE WATER SEPARATORS WERE DRAINED IAW MM 21-70-00 AND BOTH AIR CONDITIONING SYSTEMS WERE OPERATED IN HEAT MODE, ALL CORRECT. DURING OVERNIGHTOct 5, 2006 · N169PL · Doug MD88 · Humidity Control SystemSDR ASMF200512024Relay · unknownAIRCRAFT RETURNED TO PLATFORM, AC CROSS TIE AND APU GENERATOR WERE OUT OF SERVICE. THE BCU, AC CROSS TIE RELAY AND GCU WERE REPLACED IAW MM 24-20-08, MM 24-20-06, MM 24-20-07 RESPECTIVELY, TESTED CORRECT.Dec 28, 2005 · N169PL · Doug MD88 · Electrical Power SystemSDR ASMF200512016Csd · failedCAPTAIN REPORTED THAT DURING FLIGHT THE LT CSD REACHED 180 GRADES FOR A MINUTE, OVER TEMPERATURE LIGHT TURNED ON AND THE RT ENGINE EGT WAS OUT OF LIMITS AFTER STARTED. THE OPERATIONAL PROCEDURE WAS PERFORMED, THE LT CSD REPORT WAS DEFERRED IAW MEL 24-14-1, THEDec 17, 2005 · N169PL · Doug MD88 · Alternator-Generator DriveSDR ASMF200509002Skin · dentedDURING TRANSIT CHECK AT ONT, IT WAS DETECTED A DENT IN FUSELAGE SKIN OF 2 X 1.875 WITH 0.044 DEPTH, LOCATED AT STA Y=1277 BETWEEN RIGHT LONGERON 22 & 23. DENT WAS EVALUATED AND IT WAS FOUND WITHIN LIMITS IAW SRM 53-04, FIGURE 38, TABLE C, CONDITION 1B. AT MESep 3, 2005 · N169PL · Doug MD88 · Fuselage Main, Plate/SkinSDR ASMF200508012Proximity Switch · failedCAPTAIN REPORTED THAT RT RED MAIN LANDING GEAR LIGHT TURNED ON. THE PROXIMITY SWITCH UNIT WAS TESTED, LIGHT PANEL WAS CHECKED AND SENSORS WERE VERIFIED BUT FAILURE CONTINUED. THE PROXIMITY SWITCH UNIT WAS REPLACED AND FAILURE CODE 310 WAS SHOWN AND RED LIGHTS Aug 21, 2005 · N169PL · Doug MD88 · Landing Gear Position and WarningSDR ASMF200507004Csd · failedDURING CLIMB, LT ENGINE CSD REACHED RED RANGE AND APU WAS OUT OF SERVICE. CHIP DETECTOR WAS VERIFIED AND OIL LEVEL WAS ON YELLOW RANGE. CSD, OIL RADIATOR AND CENTRIFUGAL SWITCH WERE REPLACED IAW MM 24-20-00, 24-10-01 AND 24-10-03. APU WAS TESTED IAW MM 49-6Jul 6, 2005 · N169PL · Doug MD88 · Alternator-Generator DriveSDR ASMF200506028Apu · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF APU DID NOT SUPPORT PNEUMATIC CHARGES FOR ENGINE STARTING. GPU WAS CONNECTED TO ENGINES STARTING AND APU WAS DEFERRED IAW MEL 49-1. DURING OVERNIGHT SERVICE APU WAS TESTED IAW MPCM 49-00-01 SETTING BOTH ENGINJun 28, 2005 · N169PL · Doug MD88 · Airborne Auxiliary Power Unit (APU) SystemSDR ASMF200506024Control Box · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT INBOARD ANTISKID LIGHT TURNED ON. AT PLATFORM, BITE TO ANTISKID CONTROL BOX WAS PERFORMED DETECTING FAILURE IN THE RIGHT INTERIOR DOUBLE SERVO VALVE. VALVE WAS REPLACED IAW MM 32-43-04, TESTED CORRECT.Jun 24, 2005 · N169PL · Doug MD88 · Brake Anti-Skid SectionSDR ASMF200506020Engine · vibrationCAPTAIN REPORTED VIBRATION IN RT ENGINE DURING CRUISE. ACFT SENT TO HANGAR AND WAS CHECKED BY CONDITION AND TESTS PERFORMED IAW MM 72-00-00. ALL CORRECT. RT ENGINE WAS ACCELERATED UNTIL TAKEOFF POWER AND MAXIMUM VIBRATION REGISTERED 0.5, MAXIMUM VIBRATIONJun 18, 2005 · N169PL · Doug MD88 · Engine (Turbine/Turboprop)SDR ASMF200505020Transmitter · looseAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE, DURING PUSH BACK AND RIGHT ENGINE STARTING, IT WAS NO OIL PRESSURE INDICATIONS. THE LP2 RESTRICTOR AND THE RESPECTIVE CONNECTOR WERE CLEANED. THE ENGINES WERE STARTED AND OIL PRESSURE INDICATION WAS CORRECT IAWMay 19, 2005 · N169PL · Doug MD88 · Engine Oil PressureSDR ASMF200505014Bolt · failedAIRCRAFT RETURNED TO PLATFORM, DURING RT ENGINE START, THE LOW PRESSURE LIGHT DID NOT TURN OFF AND THE INDICATION WAS ZERO, N2 REACHED 35 PERCENT AND IT DID NOT INCREASE. THE OIL LEVEL AND RT ENGINE WERE VERIFIED, BEING CORRECT, MAIN OIL FILTER WAS REMOVED ANDMay 9, 2005 · N169PL · Doug MD88 · Turbine Engine Oil SystemSDR ASMF200504015Engine · malfunctionedAIRCRAFT REJECTED TAKEOFF AS A CONSEQUENCE OF DURING TAKEOFF AT 80 KNOTS, OIL PRESSURE REACHED 60 PSI ON RIGHT ENGINE. THE OIL PRESSURE RIGHT ENGINE WAS ADJUSTED IN 43 PSI IAW MM 79-20-03, TESTED CORRECT.Apr 17, 2005 · N169PL · Doug MD88 · Engine Oil PressureSDR ASMF200504001Housing · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AS A CONSEQUENCE OF BOTH CABIN PRESSURE CONTROL VALVES WERE OUT SERVICE AND CABIN ALTITUDE ROSE TO 9500. IT WAS NECESSARY TO CONTROL PRESSURE IN MANUAL DUE TO AN OBSTRUCTION OF WHEEL CONTROL. IN GROUND, BOTH SYSTEM WApr 2, 2005 · N169PL · Doug MD88 · Pressure Regulator/Outflow ValveSDR ASMF200503022Selector · failedAIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF BOTH PRESSURIZATION CONTROLLERS WERE OUT OF SERVICE IN AUTOMATIC MODE AND OUT OF SERVICE IN MANUAL MODE WITH VALVE CLOSED AT 100 AND 200 FT OF CLIMB. AIRCRAFT WAS SENT TO THE HANGAR AND CABIN AIR SELECTOR AND CAMar 30, 2005 · N169PL · Doug MD88 · Air Conditioning SystemSDR ASMF20050301Door · openAIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF PRESSURIZATION LEAK IN RIGHT FORWARD EMERGENCY EXIT. DURING CHECK WAS DETECTED RIGHT FORWARD EMERGENCY DOOR PARTIALLY OPENED. THE RIGHT FORWARD EMERGENCY DOOR WAS INSTALLED CORRECTLY IAW MM 52-21-10, PRESSURIZAMar 1, 2005 · N169PL · Doug MD88 · Emergency ExitsSDR ASMF200502009Transmitter · failedCAPTAIN REPORTED THAT OIL PRESS DURING TAKEOFF & CLIMB RAISING TO 70 PSI, FLASHING INDICATION CRUISE "FT 58 PS’S" REDUCING POWER. CAPTAIN REPORTED STRONG VIBRATION IN THE PAX CABIN. RT ENGINE OIL PRESS ADJUSTED IAW MM, TESTED CORRECT & ENGINE VIBRATION CHECFeb 13, 2005 · N169PL · Doug MD88 · Engine Oil PressureSDR ASMF200409009Engine · damagedDURING BOROSCOPIC INSPECTION TO THE ENGINE NR 2, DAMAGES OUT OF LIMITS WERE DETECTED, NEAR TO THE 14TH STAGE OF BOROSCOPIC POINT, RT SIDE. ENGINE WAS REPLACED IAW MM 71-00-00, TEST WERE CORRECT.Sep 25, 2004 · N169PL · Doug MD88 · Engine (Turbine/Turboprop)SDR ASMF200407031Filter · cloggedAIRCRAFT SUSPENDED TAKEOFF AND RETURNED TO PLATFORM, CAPTAIN REPORTED RT OIL FILTER CLOGGED LIGHT TURNED ON. LIGHT INDICATION WAS CHECKED AND ENGINE WAS TESTED AT 1.7 OF EPR AND LIGHT DID NOT TURN ON. AS A PRECAUTIONARY ACTION, OIL FILTER AND ALARM WERE REPLJul 27, 2004 · N169PL · Doug MD88 · Turbine Engine Oil SystemSDR ASMF200407024Indicator · failedCAPTAIN REPORTED THAT AT THE BEGINNING OF THE TAXI, APPEARED THE AIR SPEED A/S FLAG IN THE LT AIRSPEED INDICATOR. IT WAS PERFORMED A RESET AND THE CADC SWITCH WAS CHANGED OF POSITION, BUT THE TROUBLE CONTINUED. AIR SPEED INDICATOR WAS REPLACED AND SYSTEM TESTJul 22, 2004 · N169PL · Doug MD88 · Airspeed/Mach IndicatorSDR ASMF200404023Wire · groundedCAPTAIN REPORTED THAT DURING TAKE OFF (AIRFOIL ICE PROTECT PRESS ABNORMAL) LIGHT TURNED ON. CABLES WERE CHECKED AND A LINE WAS GROUNDED IN SENSOR S1-46. (AIRFOIL ICE PROTECT PRESS ABNORMAL) LIGHT WIRING WAS REPAIRED IAW WDM 30-11-01, TEST CORRECT.Apr 29, 2004 · N169PL · Doug MD88 · Ice/Rain Protection System WiringSDR MEX2004059Valve · failedFLT 610 - CUN-MEX - FLIGHT RETURNED, 'AIR FOIL ICE PROTECT' OUT OF SERVICE AT 31,000 FEET WITH ICING CONDITIONS. DURING REVISION THE WINGS AND TAIL ANTI-ICE VALVES WERE TESTED AND RELAY R2-189 WAS ADJUSTED. DURING OVERNIGHT SERVICE THE H3766020 AND 2H378C20 Feb 14, 2004 · N169PL · Doug MD88 · Airfoil Anti/De-ice SystemSDR MEX2004051Landing Gear · failedFLT 296 - CUN-GDL - AIRCRAFT RETURNED, NLG DID NOT RETRACT. CAPTAIN REPORTED THE PERFORMED 3 CYCLES BUT FAIL REMAIN. AT PLATFORM, A MAINTENANCE SERVICE WAS PERFORMED TO THE NLG IAW MM 32-21-02 AND A TEST FLIGHT WAS REQUESTED TO VERIFY THE PERFORMANCE OF THE Feb 8, 2004 · N169PL · Doug MD88 · Nose/Tail Landing Gear Strut/AxleSDR MEX2004046Seal · failedFLT 118 - GDL-TIJ - DURING OVERNIGHT SERVICE, NLG SEALS WERE REPLACED IAW MM 32-21-02. GROUND SENSING CONTROL MECHANISM WAS VERIFIED IAW MM 32-23-01, STEERING SYSTEM TEST ACCOMPLISHED IAW MM 32-50-00. LUBRICATION WAS PERFORMED IAW MM 12-21-04 AND NLG EXTENSIOFeb 4, 2004 · N169PL · Doug MD88 · Main Landing Gear Strut/Axle/TruckSDR MEX2004045Seal · failedFLT 118 - GDL-TIJ - AIRCRAFT RETURNED DUE TO NLG DID NOT GO AND AND NLG RED LIGHT CAME ON, THE HORIZONTAL STABILIZER AND PRESSURIZATION WERE OUT OF CONTROL, SEVERAL ALARMS WERE ACTIVATED, TCAS WAS OUT OF SERVICE AND STALL INDICATOR FAILURE AND AUTO BRAKE FAIL Feb 4, 2004 · N169PL · Doug MD88 · Main Landing Gear Strut/Axle/TruckSDR MEX2004013Strut · failedAIRCRAFT RETURNED, DURING LANDING, NLG DID NOT RETRACT. AT PLATFORM WAS DETECTED THE SHOCK STRUT WET WITH HYDRAULIC FLUID AND THE PISTON AND CYLINDER ASSY COMPRESSED. AIRCRAFT WAS SENT TO THE HANGAR WHERE THE NLG STRUT SEALS WERE REPLACED IAW MM AND EXTENSIOJan 8, 2004 · N169PL · Doug MD88 · Main Landing Gear Strut/Axle/TruckSDR MEX2004012Piston · damagedAIRCRAFT RETURN OF FLIGHT, DURING TAKEOFF ROLL, THE NLG HIT A BIG BUMP ON THE RUNWAY AND IT DID NOT RETRACT. DURING REVISION WAS DETECTED THE NLG SHOCK STRUT LOW. AIRCRAFT WAS SENT TO HANGAR, WHERE THE PISTON AXLE ASSEMBLY CYLINDER ASSY AND SHOCK STRUT SEALSJan 8, 2004 · N169PL · Doug MD88 · Main Landing Gear Strut/Axle/TruckSDR MEX2003571Engine · overspeedFLT 460 - GDL-LAX - AIRCRAFT RETURNED, DUE TO DURING TAKEOFF, WITH ATS OUT OF SERVICE, THE RIGHT ENGINE N1 REACHED AN OVERSPEED OF 105.1 PERCENT. CAPTAIN PERFORMED PROCEDURE DURING DESCENT AND THE EPR'S REACHED 2 LASTING 2 MINUTES, AFTER THAT ALL PARAMETERS WDec 29, 2003 · N169PL · Doug MD88 · Engine (Turbine/Turboprop)SDR MEX2003542Ptu · failedAFTER LANDING THE LIGHT OF (L HYD TEMP HI) CAME ON. THE SYSTEM WAS VERIFIED AND THE POWER TRANSFER UNIT WAS FAULTY. THE PTU WAS REPLACED AND THE SYSTEM WAS TESTED IAW MM 29-10-07, ALL CORRECT. (M)Nov 30, 2003 · N169PL · Doug MD88 · Hydraulic System, MainSDR MEX2003500Blade · damagedDURING TRANSIT CHECK, DETECTED DAMAGE ON LEFT ENGINE C1 FAN BLADE AND A .40625 INCH PER .0625 INCH DAMAGE IN THE NOISE SUPPRESSOR. BLADE WAS BLENDED IAW MM 72-00-00. DURING OVERNIGHT SERVICE, BLADE BLENDING WAS INSPECTED IAW MM 78-33-21, FOUND ALL CORRECT ANOct 21, 2003 · N169PL · Doug MD88 · Turbine Engine Compressor SectionSDR MEX2003487Seal · leakingAIRCRAFT RETURNED TO PLATFORM, DURING TAXING, BEFORE TAKEOFF, LT ENGINE OIL QUANTITY DROPPED TO ZERO. LT ENGINE WAS SHUT DOWN WHEN LT OIL PRESS ANNUNCIATOR WAS ILLUMINATED. AIRCRAFT WAS SENT TO THE HANGAR WHERE THE HOUSING OIL FILTER WAS REPAIRED IAW MM 72-0Oct 14, 2003 · N169PL · Doug MD88 · Engine Oil Distribution (Airframe Furnished)SDR MEX2003343Tire · failedAIRCRAFT RETURNED TO PLATFORM, DURING TAXI WHEEL ASSEMBLY NR 4 PRESSURE OUT, THE WHEEL ASSY OF MLG POSITION 4 WAS REPLACED IAW MM 32-40-01, ALL CORRECT.Aug 5, 2003 · N169PL · Doug MD88 · TireSDR MEX2003316Gcu · failedFLT 6581 - MEX-CUN - AIRCRAFT RETURNED TO GATE, AC CROSS TIE NO TEST. DURING REVISION WAS DETECTED ACTR LIGHT AND APU PWR AVAIL LIGHTS ON. THE GCU AND BCU WERE REPLACED IAW MM 24-20-04/08 AND ENGINES AND GENERATION SYSTEM WERE TESTED, ALL CORRECT. (M)Jul 3, 2003 · N169PL · Doug MD88 · AC RegulatorSDR MEX2003224Servo Valve · failedFLT 501 - MEX-OAX - AIRCRAFT ARRIVED WITH CAPTAIN REPORT TIRE NR 4 OF MLG WITH DAMAGE. THE TIRE NR 4 WAS REPLACED BUT ANTI-SKID NO TEST. EXTERIOR DOUBLER SERVO VALVE WAS REPLACED IAW MM 32-43-03, ALL TESTS CORRECT. (M)Jun 12, 2003 · N169PL · Doug MD88 · Brake Anti-Skid SectionSDR MEX2003129Symbol Generator · malfunctionedAIRCRAFT RETURNED TO PLATFORM, AT FIRST OFFICIAL SIDE DURING ENGINES STARTING WERE OF ND AND PFD INDICATIONS OFF. THE SYMBOL GENERATOR DIGITAL COMPUTER WAS RESEATED IAW MM, TESTS CORRECT.Apr 10, 2003 · N169PL · Doug MD88 · AC Indicating SystemSDR MEX2003109Gearbox · inoperativeAIRCRAFT ARRIVED WITH REPORT PRIMARY HORIZONTAL STABILIZER WITHOUT MOVEMENT, IT WAS NECESSARY TO COMPENSATE WITH ELEVATOR DURING FINAL APPROACH. THE GEARBOX ASSEMBLY TRIM AND ALTERNATE ENGINE WERE REPLACED IAW MM AND RELAY LONGITUDINAL TRIM WAS REPLACED IAW MApr 1, 2003 · N169PL · Doug MD88 · Rudder Control SystemSDR MEX2003107Gearbox · stuckDURING FINAL APPROACH LONG TRIM WAS STUCKED, THE NOSE COMPENSATION UP WAS NOT POSSIBLE. THE PRIMARY ACTUATOR ENGINE WAS REPLACE. THE GEAR BOX ASSY TRIM AND ALTRENATE ENGINE WERE REPLACED IAW MM AND RELAY LONGITUDINAL TRIM WAS REPLACED IAW, TESTS CORRECT.Mar 31, 2003 · N169PL · Doug MD88 · Rudder Control SystemSDR MEX2003031Pump · failedAIRCRAFT RETURNED TO PLATFORM, RT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH ZERO PRESSURE INDICATION. RT ENGINE HYDRAULIC PUMP WAS REPLACED IAW MM, ALL CORRECT.Feb 9, 2003 · N169PL · Doug MD88 · Hydraulic Pump (Electric/Engine), MainSDR MEX2002285O-Ring · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED NEAR APU FUEL FEED LINE DRAIN. APU WAS TURNED OFF, HOWEVER THE LEAK CONTINUED, THE FUEL PUMP WAS TURNED OFF AND LEAK DISAPPEARED. LINE WAS CHECKED BUT NO DAMAGE WAS FOUND. THE APU FUEL FEED VALVE WAS DISCONNESep 2, 2002 · N169PL · Doug MD88 · APU Engine Fuel and ControlSDR MEX2002243Strainer · cloggedFLT 416 - AIRCRAFT ABORTED TAKEOFF DUE TO OIL STRAINER CLOGGING TURNED ON. OIL MAIN FILTER WAS REPLACED. RESTRICTORS WERE CLEANED AND THE CLOGGING FILTER ALARM WAS REPLACED IAW MM 79-35. (M)Jul 26, 2002 · N169PL · Doug MD88 · Engine Oil Distribution (Airframe Furnished)
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