Mcdonnell Douglas MD 83

Service difficulty reports · 3,415

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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 aircraft_model_key = 'MD83'
  ORDER BY difficulty_date DESC"

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SDR GTIA050178Skin · dentedFOUND DENT AT STRINGER 236 BETWEEN LONGERONS 18L AND 19L. CHEMICALLY REMOVED PAINT. CUT OUT DAMAGED AREA. FABRICATED REPAIR IAW. TREATED AND PRIMED REPAIR PARTS. INSTALLED REPAIR IAW. ITEM TRANSFERRED TO LOG PATE NR 0300548-1. (M)May 4, 2005 · N827NK · Doug MD83 · Fuselage Main, Plate/SkinSDR ASMF200505004Switch · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ELEVATOR POWER ON LIGHT DID NOT TURNED ON DURING FLIGHT CONTROL TESTS. ELEVATOR WAS CHECKED PER FREE MOVEMENT, ACCUMULATOR PRESSURE AND HYDRAULIC QUANTITY WERE CORRECT. LIGHT REPORT WAS DEFERRED IAW MEL May 3, 2005 · N861LF · Doug MD83 · Elevator Control SystemSDR ASMF200504019Wheel · out of balanceAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AIRCRAFT EXPERIENCED STRONG VIBRATION DURING TAKEOFF. NOSE LANDING GEAR WAS CHECKED BEING ALL CORRECT IAW MM 32-21-01. AIRCRAFT NOSE LANDING GEAR WAS JACKED DETECTING UNBALANCED BETWEEN BOTH WHEELS. REPLACEDApr 23, 2005 · N881LF · Doug MD83 · Wheel/Ski/FloatSDR ANCF200400048Csd · failedDURING RT ENG START, RT GEN FREQ 396 CPS & GEN CAME ON LINE AT 50 PERCENT N2. REPORTED TO TECH. DURING TAKEOFF ROLL, RT GEN TRIPPED, RESET UNSUCCESFULL. RT CSD OIL TEMP BEGAN RISING UNTIL OFF SCALE, WITH GEN OFF, FOLLOWED CHKLST, CSD DISCONNECTED. THROUGH Apr 20, 2005 · N632CT · Doug MD83 · Alternator-Generator DriveSDR ANCF200400047Smoke · detectedIN BAQ WHEN EXTERNAL POWER WAS CONNECTED SMOKE CAME INTO COCKPIT FROM OVERHEAD PANEL. AS PER AMM 20-50-01 PAGE 201, GROUND ELECTRICAL 106 LINE WAS ISOLATED ON CONNECTOR P1-568 OF CABIN PRESS SELECTOR ELECTRICAL LINES WERE CHECKED BY CONDITIONS ON OVERHEAD PANApr 16, 2005 · N583AN · Doug MD83 · Electrical Power SystemSDR GTIA050127Stud · strippedNR 2 ENGINE USED 4 QUARTS OF OIL DURING FLT NR 931, AIRCRAFT TAIL SWAP WITH 830. FOUND ENGINE OIL FILTER COVER LEAKING. REPLACED 3 HELI-COILS FOR THE PULLED OUT STUDS ON THE GEARBOX, NO LEAKS NOTED ON ENGINE RUN. (M)Apr 12, 2005 · N822NK · Doug MD83 · Turbine Engine Accessory DriveSDR ASMF200504004Computer · failedDURING TRANSIT CHECK, THE STALL SYSTEM TEST WAS INOPERATIVE. DURING REVISION WAS DETECTED SIF LIGHT AT ANNOUNCED PANEL AND STALL WARNING IN COMPUTER NUMBER 1. THE STALL WARNING COMPUTER NUMBER 1 WAS REPLACED IAW MM 34-19-02, TESTED CORRECT. LATER, AIRCRAFT RETApr 8, 2005 · N861LF · Doug MD83 · Stall Warning SystemSDR ASMF200503024Apu · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF AFTER PUSH BACK, THE RIGHT ENGINE HAD A HOT STARTING PROMOTED BY LOW PRESS FORM THE APU. ENGINES WERE STARTED WITH A GPU AND APU WAS DEFERRED IAW MEL 49-1-2. DURING OVERNIGHT SERVICE, APU WAS TESTED IN BOTH MODMar 31, 2005 · N945AS · Doug MD83 · APU Bleed Air SystemSDR ASMF200503023Pitot Line · misusedAIRCRAFT REJECTED TAKEOFF AND RETURNED TO PLATFORM AS A CONSEQUENCE OF AT 80 KTS, THE AUXILIARY AIR SPEED INDICATOR SHOWS O KTS. DURING CHECK, MAINTENANCE PERSONNEL DETECTED THAT THE PITOT PNEUMATIC LINE WAS WRONGLY CONNECTED AND LOOSED. ADDITIONALLY THE STAMar 31, 2005 · N881LF · Doug MD83 · Pitot/Static SystemSDR ANCF200400043Engine · bird ingestionDURING ROTATION THE RT ENGINE WAS IMPACTED WITH A BIRD. ALL ENGINE PARAMETERS WENT DOWN TO IDLE AND RETURNED SLOWLY TO NORMAL PARAMETERS IAW AMM 05-51-08 PAGE 601 BIRD STRIKE CONDITION. CHECK WAS ACCOMPLISHED AND NOT FOUND DAMAGE IN THE ENGINE AREAS.Mar 19, 2005 · N593AN · Doug MD83 · Engine (Turbine/Turboprop)SDR ASMF200503016Csd · overheatedAIRCRAFT RETURNED, TEMPERATURE IN RT CSD INCREASED HIGHLY AFTER TAKE OFF AND BATTERIES CIRCUIT BREAKER POPPED OUT. RT CSD WAS SERVICED IAW MM 24-10-1, TESTED CORRECT. DURING OVERNIGHT SERVICE CSD FILTERS AND OIL WERE REPLACED IAW MM 24-10-01 AND CSD WAS SERVIMar 19, 2005 · N861LF · Doug MD83 · Alternator-Generator DriveSDR ANCF200400041Overheat Sensor · dirtyAFTER TAKEOFF, TAIL COMP TEMP LIGHT CAME ON. ABNORMAL CHECK LIST WAS PERFORMED AFTER LT ENGINE WAS REDUCED, 1.5 MIN LATER THE LIGHT WENT OFF, LT PACK WAS SWITCHED TO OFF AND LT ENG POWER RESTRICTED. IAW AMM 36-20-02 PAGE 201, TAIL COMPARTMENT OVERHEAT SENSORMar 15, 2005 · N583AN · Doug MD83 · Overheat DetectionSDR FRISBY05004Housing · crackedDURING T/O, EXPERIENCED TOTAL LOSS OF PRESSURE IN LT HYD SYS & A LOSS (5 PSI REMAINING) OF RT HYD SYSTEM. FLT CREW REPORTED NO HYD PRESSURE WHEN SELECTING GEAR UP. SELECTED GEAR HANDLE DOWN & STARTED WITH EMERGENCY CHECK LISTS. RETURNED TO ARLANDA (STOCKHOLMar 13, 2005 · Doug MD83 · Hydraulic System, AuxiliarySDR ASMF200503011Skin · dentedDURING TRANSIT CHECK SCRATCH AND DENT WERE FOUND IN THE BOTTOM OF THE MAIN DOOR BETWEEN STA Y-231, LONGERON 17 AND 18. THE SCRATCH AND DENT WERE REWORKED AND ULTRASONIC INSPECTION WAS PERFORMED IAW SRM 53-04, FIG 38, TABLE A, CONDITION 1, ALL CORRECT.Mar 13, 2005 · N861LF · Doug MD83 · Fuselage Main, Plate/SkinSDR ASMF200503009Nose Cowl · damagedDURING TRANSIT CHECK, DETECTED DAMAGE IN RIGHT ENGINE NOSE COWLING BY FOREIGN OBJECT DAMAGE WITH LIP DENT DEPTH OF 0.150 PER 1 DIAMETER AT 03:00 POSITION. AIRCRAFT WAS SENT TO THE HANGAR AND NOSE COWLING WAS REPLACED IAW MM 71-10-01 PAGE 201, ALL CORRECT.Mar 12, 2005 · N831LF · Doug MD83 · Engine Cowling SystemSDR ASMF200503006Skin · damagedDURING TRANSIT CHECK WAS DETECTED HIT IN LT AILERON. DURING REVISION WAS DETECTED DAMAGED THE AILERON FITTING PN 44938931-507. THE LT AILERON WAS REPLACED AND TESTED IAW MM 27-10-0 AND MM 27-10-00. TEST FLIGHT WAS PERFORMED IAW GMM CHAPTER 4-10-6, NOTE 2 AND Mar 8, 2005 · N946AS · Doug MD83 · Trailing Flap Position Indicating SystemSDR GTIA050036Proximity Sensor · defectiveUPON RETRACTION OF SLATS AND FLAPS, SLAT DISAGREE LIGHT CAME ON AND REMAINED ON UNTIL SLATS RE-SELECTED. AFTER LANDING LIGHT CAME BACK ON WHEN SLAT/ FLAP SELECTED TO UP/RETRACT, AIR RETURN. INSPECTED PROXIMITY SWITCHES AND FOUND SWITCH ON NR 1 SLAT (C) SENSOMar 1, 2005 · N828NK · Doug MD83 · Leading Edge Slat Position Indicating SystemSDR ANCF200400040Engine · failedDURING MAINTENANCE CHECKS WITH ENGINES RUNNING UP THE LT ENGINE HAD A STRONG STALL. THE LT ENGINE WAS IMMEDIATELY SWITCHED OFF. DURING THE PRELIMINARY BOROSCOPE INSPECTION, FOUND C6, C7, C13, COMBUSTION CHAMBER, T1 AND T2 IN GOOD CONDITIONS. THE DAMAGE WASFeb 26, 2005 · Doug MD83 · Powerplant SystemSDR ASMF200502001Relief Valve · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSH BACK, CAPTAIN REPORTED LOST OF HYDRAULIC PRESSURE AND QUANTITY. DURING CHECK WAS DETECTED A LEAK FROM THE LEFT HYDRAULIC RELIEF VALVE, IT WAS REPLACED IAW MM 29-10-12, TESTED CORRECT.Feb 3, 2005 · N831LF · Doug MD83 · Hydraulic System, MainSDR ASMF200501008Duct · damagedDURING ENGINES STARTING, RT ENGINE DID NOT STARTED BECAUSE N1 WAS OUT OF SERVICE. DURING MAINTENANCE REVISION WAS DETECTED 8TH STAGE DUCT BROKEN. DUCT WAS REPLACED AND TESTS WERE PERFORMED IAW MM 71-00-01, ALL CORRECT.Jan 15, 2005 · N583MD · Doug MD83 · Engine CrankingSDR AALA20050025Connector · inoperativeSFO - FORWARD SEAT MOUNTED EMERGENCY LIGHT AT SEAT 3E INOPERATIVE. REPLACED FORWARD CONNECTOR FOR FORWARD SEAT MOUNTED EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION.Jan 13, 2005 · N951TW · Doug MD83 · Light System WiringSDR AALA20050006Battery · dischargedSFO - DURING OVERNIGHT MAINTENANCE EMERGENCY OVERHEAD AISLE LIGHTS INOPERATIVE AT ROWS 12-16. REPLACED EMERGENCY OVERHEAD AISLE LIGHTS BATTERY AT 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.Jan 7, 2005 · N9412W · Doug MD83 · Emergency LightingSDR GTIA050003Coalescer Bag · dirtyPBI - FLT 330 - GATE RETURN FOR SMOKE HAZE IN THE CABIN. REMOVED AND REPLACED COALESCER BAG. (M)Jan 4, 2005 · N828NK · Doug MD83 · Humidity Control SystemSDR AALA20041254Battery Pack · dischargedPHX - EMERGENCY LIGHTS AT AFT CABIN ROWS 29, 30 AND 31 INOPERATIVE. REPLACED BATTERY PACK B5-107 FOR EMERGENCY LIGHTS AT AFT CABIN ROWS 29, 30 AND 31. SYSTEM GROUND CHECKED NORMAL OPERATION.Dec 27, 2004 · N9414W · Doug MD83 · Emergency LightingSDR AALA20041253Battery Pack · dischargedPHX - EMERGENCY LIGHTS AT ROWS 24, 25 AND 26 INOPERATIVE. REPLACED BATTERY PACK B5-106 FOR EMERGENCY LIGHTS AT ROWS 24, 25 AND 26. SYSTEM GROUND CHECKED NORMAL OPERATION.Dec 27, 2004 · N9414W · Doug MD83 · Emergency LightingSDR AALA20041252Battery Pack · dischargedPHX - SECOND OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR SECOND OVERWING EXIT EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.Dec 27, 2004 · N9414W · Doug MD83 · Emergency LightingSDR AALA20041251Battery Pack · dischargedPHX - COCKPIT ENTRY WAY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR COCKPIT ENTRY WAY EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.Dec 27, 2004 · N9414W · Doug MD83 · Emergency LightingSDR FRISBY05003Housing · crackedAFTER LANDING ON DECEMBER 25, 2004, THE FLIGHT CREW OF AN ALITALIA MD-80 REPORTED THE HYDRAULIC PRESSURE OF BOTH HYDRAULIC SYSTEMS WENT TO ZERO, BUT THE HYDRAULIC PRESSURE RETURNED TO NORMAL VALUE WITH THE AUXILIARY AND TRANSFER PUMP OFF. GROUND MAINTENANCE CDec 25, 2004 · Doug MD83 · Hydraulic System, AuxiliarySDR AALA20041201Wire · brokenATL - EMERGENCY LIGHT AT SEATS 13DEF INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 13DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.Dec 8, 2004 · N951TW · Doug MD83 · Emergency LightingSDR GTIA040857Gasket · damagedFLL - FLT 758 - AFTER TAKEOFF AT 800 FEET, THE TAIL COMPARTMENT OVERTEMP LIGHT CAME ON, FOLLOWED QRH PROCEDURES THE LIGHT WENT OUT WHEN THE LEFT THROTTLE WAS PLACED IN IDLE. THE LIGHT CAME BACK ON WHEN THE THROTTLE WAS RETURNED ABOVE 1.5 EPR, THE LIGHT WENT ODec 6, 2004 · N822NK · Doug MD83 · Cabin Cooling SystemSDR GTIA040864Floor Support · corrodedFTW - FOUND FORWARD CABIN STATION 207, RBL 11 INCH FLOOR SUPPORT CORRODED. REMOVED CORRODED FLOOR SUPPORT AT STATION 207, RBL 11, FABRICATED NEW FLOOR SUPPORT, TREATED, PRIMED, TOPCOATED AND INSTALLED FLOOR SUPPORT. (M)Dec 3, 2004 · N828NK · Doug MD83 · Fuselage Miscellaneous StructureSDR GTIA040865Access Panel · damagedFTW - FOUND LEFT WING INBOARD BUTTE DOOR INBOARD EDGE, BOTTOM SIDE IS DAMAGED. BLENDED OUT DAMAGE MATERIAL LOSS OUT OF LIMITS, FABRICATED NEW DOUBLER, DRILLED AND LOCATED HOLES. OK TO TREAT, PRIME AND INSTALLED DOUBLER. (M)Dec 2, 2004 · N828NK · Doug MD83 · Wing, Plate/SkinSDR GTIA040862Skin · crackedFTW - FOUND FUSELAGE SKIN CUTOUT FOR L1 DOOR HOLD OPEN HOOK CRACKED AND GOUGED OUT. BLENDED GOUGE AND REMOVED CRACKED EDGE AT L1 DOOR CUTOUT, TREATED, PRIMED AND INSTALLED REPAIR DOUBLER. (M)Dec 2, 2004 · N828NK · Doug MD83 · Fuselage Main, Plate/SkinSDR GTIA040863Seat Track · corrodedFTW - FOUND CABIN FLOOR SEAT TRACK CORRODED AT STATION 200-237, RBL 22. REMOVED CORROSION AND SECTION OF TRACK AT STATION 200-237, FABRICATED SECTION OF SEAT TRACK, TREATED, PRIMED AND TOPCOATED, OK TO INSTALL. (M)Dec 2, 2004 · N828NK · Doug MD83 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA040861Slide · failedFTW - FOUND L1 DOOR SLIDE FAILED TO DEPLOY. REPLACED L1 DOOR SLIDE. (M)Dec 1, 2004 · N828NK · Doug MD83 · Escape SlideSDR GTIA040866Wedge · dentedFTW - FOUND RIGHT WING INBOARD FLAP OUTBOARD WEDGE BOTTOM SIDE HAS DENT WITH FILLER COMPOUND. STRIPPED FILLER COMPOUND DENT OUT OF LIMITS, CUT OUT DAMAGE 1.5 INCH BY 2.5 INCH, FABRICATED FILLER AND DOUBLER, DRILLED HOLES. OK TO TREAT AND PRIME AND INSTALLED Dec 1, 2004 · N828NK · Doug MD83 · Trailing Edge FlapsSDR GTIA040875Skin · damagedFTW - FOUND FORWARD CARGO DOOR HAS DENT ON LOWER EDGE OF SKIN APPROX .098 INCH DEEP 1.0 INCH DIAMETER. CUT OUT DAMAGED, DENTED SKIN. FABRICATED REPAIR DOUBLER AND FILLER, TREATED AND PRIMED FABRICATED PARTS AND INSTALLED REPAIR. (M)Nov 30, 2004 · N828NK · Doug MD83 · Cargo/Baggage DoorsSDR ANCF200400036Door · damagedAFTER TAKEOFF AND AFTER LANDING GEAR RETRACTION THE RED GEAR LIGHT REMAIN ON ALONG WITH THE GEAR DOOR OPEN LIGHT. CHECKIST WAS PERFORMED AND THE GEAR WAS CYCLED WITH NO HELP. RETURNED WAS MADE THE GEAR WHEN DONE OK, AND THE GEAR DOOR OPEN LIGHT WHEN OFF NORMNov 27, 2004 · N583AN · Doug MD83 · Landing Gear DoorsSDR ANCF200400035Transducer · malfunctionedTWO REJECTED TAKEOFF WAS PERFORMED DUE WHEEL NOT TURNING COMES ON APPROX 90 KNOTS. REPLACED TRANSDUCER IN MLG RT POSITION NR 3 AND NR 4 IAW AMM:32-43-02 PAG 201 PN OFF:4062575, S/N:OFF:627, S/N ON:5325A POS NR 3.Nov 22, 2004 · N632CT · Doug MD83 · Landing Gear Position and WarningSDR AALA20041157Connector · disconnectedSTL - EMERGENCY PATH LIGHTS AT SEAT 14DEF INOPERATIVE. FOUND CONNECTOR DISCONNECED AT SIDEWALL SEAT 14DEF. RECONNECTED CONNECTOR FOR EMERGENCY PATH LIGHTS AT SEAT 14DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.Nov 22, 2004 · N9413T · Doug MD83 · Light System WiringSDR AALA20041156Battery Pack · inoperativeBNA - EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.Nov 22, 2004 · N9630A · Doug MD83 · Emergency LightingSDR ASAA0480573Lanyard · disconnectedPRE-FLIGHT CHECK - FWD SERVICE (R-1) DOOR EMERGENCY SLIDE LANYARD WAS FOUND DISCONNECTED. RECONNECTED LANYARD. (K)Nov 20, 2004 · N982AS · Doug MD83 · Emergency EquipmentSDR 200411009Cover · crackedAIRCRAFT WITH CAPTAIN REPORT THAT EGT DIFFERENCES BETWEEN ENGINES CONTINUE AT TAKEOFF RUN, LEFT ENGINE HAD EPR 1.87, EGT 510 °C, RIGHT ENGINE HAD EPR 1.78, EGT 580 °C AND THE ACCELERATION WAS STOPPED AT THIS POINT. AIRCRAFT WAS SENT TO THE HANGAR AND CIRCUMFENov 16, 2004 · N881LF · Doug MD83 · Engine (Turbine/Turboprop)SDR AALA20041135Connector · looseDFW - EMERGENCY LIGHT ON FORWARD GALLEY WELL INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT ON FORWARD GALLEY WELL. SYSTEM GROUND CHECKED NORMAL OPERATION.Nov 15, 2004 · N9414W · Doug MD83 · Emergency LightingSDR ASAA0480553Power Supply · dischargedSERVICE CHECK- EMERGENCY OVERHEAD CABIN LIGHTS INOPERATIVE AT OVERWING EXIT ON BOTH SIDES. REPLACED ASSOCIATED BATTERY PACKS (POWER SUPPLYS). LIGHT THEN OPERATED PROPERLY.(K)Nov 4, 2004 · N982AS · Doug MD83 · Emergency LightingSDR ASAA048558Floor Panel · crackedC-CHECK - FLIGHT DECK FLOOR PANEL IS CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW SRM.(K)Nov 2, 2004 · N982AS · Doug MD83 · Fuselage Floor PanelSDR ASAA0480556Pan · gougedC-CHECK - AFT CARGO DOOR LOWER FRAME AND INNER PAN ARE GOUGED ALONG EDGE ADJACENT TO RUB BLOCK. REMOVED DAMAGED AREA. REPAIRED IAW EA.(K)Nov 2, 2004 · N982AS · Doug MD83 · Cargo/Baggage DoorsSDR ASAA0480555Skin · crackedC-CHECK- NLG RT DOOR AFT HINGE COUTOUT IS CRACKED. STOP-DRILLED CRACK. INSTALLED REPAIR DOUBLER IAW SRM.Nov 2, 2004 · N982AS · Doug MD83 · Fuselage Main, Plate/SkinSDR ASMF200410019Strainer · cloggedAIRCRAFT RETURNED TO PLATFORM, RT ENGINE STRAINER CLOGGED LIGHT TURNED ON. ENGINE WAS RESTARTED AND ACCELERATED TURNING OFF THE LIGHT IAW MM 79-35-00. AS A PRECAUTIONARY ACTION, AT GDL THE FILTER WAS REPLACED IAW MM 79-20-06, TESTS WERE CORRECT.Oct 24, 2004 · N881LF · Doug MD83 · Aircraft Fuel Filter/StrainerSDR ASAA0480539Skin · gougedOKC - C-CHECK, FUSELAGE SKIN, STA 237, LONGERON 17L HAS GOUGE WITH DENTS LESS THAN 1 INCH FROM STRUCTURE X=.034, D=1.11. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLERS AND STRAPS IAW SRM 53-04, FIG 12C.Oct 20, 2004 · N982AS · Doug MD83 · Fuselage Main, Plate/Skin
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