Mcdonnell Douglas MD 83
Service difficulty reports · 3,415
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'MD83' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR WX0A070770Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR WX0A070769Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR YYFAN120MN2311Control Handle · bindingGEAR HANDLE WOULD NOT GO PAST MID POSITION. NO RETRACT.SDR WX0A070771Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR WX0A070762Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR WX0A070804Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION AND CHAFE MARKS FROM STA 770 TO 800. REPLACED SEAT TRACK ASSEMBLY AT THE MAIN CABIN RT I/B STA 741 TO 800 AS PER MD80 SRM 53-05 AND 51-30-1.SDR 2WAA20110125Motor · failedSMOKE IN COCKPIT, DECLARED EMERGENCY, DIVERTED. DISASSEMBLED, CLEANED AND INSPECTED UNIT IAW 27-60-07 REV NR 6, DATED 8/15/06. FOUND MOTOR ASSY DAMAGED, VARIOUS HARDWARE DAMAGED, CAPACITOR LEAKING, RECTIFIER OPEN, BEARINGS WORN, GEAR TRAIN LUBRICATION DRY, DASDR WX0A070757Battery Pack · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR WX0A070759Power Supply · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ASDR WX0A070755Intercostal · corrodedE AND E COMPARTMENT HAS CORRODED INTERCOSTAL AT FS 208, RBL 7, INBOARD SIDE OF DRAIN MAST. REMOVED AND REPLACED INTERCOSTAL IAW MD80 SRM 51-30-1 AND 51-30-2.SDR YYFAN836NK12111Pa System · inoperativeCOCKPIT TO CABIN PA INOP.SDR WX0A070758Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR WX0A070754Skin · damagedL1 DOOR DOES NOT MEET REPAIR REQUIREMENTS PER SRM 52-03 PARA 3. REPAIR L1 DOOR IAW MD80 SRM 52-05 FIG 55, 51-30-05, 51-30-01, 52-12-0, 51-10-3 PARA 14 & 21, AMM 25-22-00 AND 52-11-01 AND 52-11-02.SDR WX0A070753Membrane · crackedFWD CABIN FLOOR WEB DOUBLER CRACKED UNDER GALLEY FLOOR MOUNT STA 218, RBL 11 (1.25 INCH IN LENGTH). REMOVED DAMAGED DOUBLER, FABRICATED, LOCATED, DRILLED AND INSTALLED IAW MD80 SRM 51-10-4 AND SRM 51-30-2.SDR WX0A070752Access Panel · chafedRT WING LEADING EDGE ACCESS PANEL DEEP AREAS OF CHAFING. TRIMMED OUT DAMAGE, HEFC INSPECTED, NO CRACKS NOTED, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW AAR EA 14275.SDR WX0A070751Web · chafedNLG BAY WEB DEEP CHAFE ON RT SIDE OF DOWN LOCK ACTUATOR. REMOVED DAMAGED WEB, LOCATED, DRILLED AND INSTALLED A REPLACEMENT WEB IAW MD80 SRM 51-10-4 AND 51-30-5.SDR WX0A070750Cusp Web · crackedCABIN CUSP WEB CRACKED AT STA 1260 RBL 47 LENGTH OF CRACK 4 INCHES. REMOVED DAMAGED CUSP WEB SECTION STA 1250 TO STA 1307, RBL 46 TO RBL 61. FABRICATED, LOCATED, DRILLED AND INSTALLED CUSP WEB AND RING DOUBLERS IAW BOEING DRAWING SG09530019.SDR WX0A070760Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR WX0A070749Frame · crackedAFT ENTRANCE DOOR CUTOUT FRAME CRACKED .75 INCH ON FWD EDGE 5 INCHES BELOW UPPER DOOR HINGE. STOP DRILLED CRACK, HFEC INSPECTED CRACK CONTAINMENT, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND RADIUS BLOCK IAW MD80 51-01 PG 9, 51-70-05 AND DOUSDR WX0A070756Battery Pack · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR WX0A070748Cusp Web · crackedCABIN CUSP WEB CRACKED AT STA 218 CRACK LENGTH 1.5 INCHES. CUT OUT DAMAGED AREA, HEFC INSPECTED, INOP CRACKS NOTED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW DRAWING SG09530019.SDR WX0A070747Cusp Web · crackedCABIN CUSP WEB CRACKED AT STA 237 RBL 46 CRACK LENGTH 1.75 INCHES. CUT OUT DAMAGED AREA, HEFC INSPECTED, INOP CRACKS NOTED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW DRAWING SG09530019.SDR WX0A070746Floorbeam · damagedCABIN FLOORBEAM UPPER SURFACE DAMAGED AROUND NUT PLATE HOLE STA 1338 RBL 41. CUT OUT DAMAGED SECTION FROM RBL 31 TO RBL 56 FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR ANGLE IAW MD80 SRM 51-70-5 FIG 2.SDR WX0A070745Seat Track · corrodedCABIN FLOOR SEAT TRACK CORRODED STA 267 LBL 22. REMOVED DAMAGED SEAT TRACK STA 200 TO STA 321. LOCATED, DRILLED INSTALLED A REPLACEMENT TRACK AND SPLICE PLATE IAW MD80 SRM 53-05 FIG 4F.SDR WX0A070744Seat Track · corrodedCABIN SEAT TRACK CORRODED AT GALLEY MPUNTING AREA STA 204 RBL 44. REMOVED DAMAGED SECTION TO PREVIOUS SPLICE AT STA 266, FABRICATED, LOCATED DRILLED AND INSTALLED NEW SECTION IAW MD 80 SRM 53-05 FIG 4F.SDR 2ARF201101006Rheostat · damagedCAPTAIN REPORTED THAT DURING TAXING AND WHEN IT WAS TURNED WITH AUTOPILOT SELECTED, THE FLIGHT CONTROLS DID VIBRATION. MX PERSONNEL REPLACED THE DUPLEX AILERON SERVO BRACKET RHEOSTAT IAW MM 22-11-01 AND THE DFGS STATUS/TEST (STP) PANEL WAS CHECKED IAW MM 22-01SDR WX0A070743Web · corrodedWEB UNDER FWD LAV TANK, CORRODED ON UNDER SIDE LBL 44 TO 54 STA 294. ACCOMPLISHED WEB REPAIR IAW DWG SG09530019.SDR WX0A070742Seat Track · corrodedSEAT TRACK CORRODED LBL 54 STA 230. REMOVED SEAT TRACK, FABBED NEW TRACK IAW DC9/MD80 SRM 53-05 AND INSTALLED IAW DC9 SRM 51-30-1 AND 51-30-2.SDR WX0A070741Door Frame · crackedAFT ENTRANCE DOOR FRAME FWD SIDE CUTOUT CRACKED AT UPPER LT CORNER (AS VIEWED FRON AFT FACING FWD) LENGTH .250. STOP DRILLED CRACK, HEFC INSPECTED CRACK CONTAINMENT, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW MD 80 SRM 53-05 FIG 29.SDR WX0A070733Battery Pack · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ASDR WX0A070732Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ASDR 2ARF201101005Plate · brokenCAPTAIN REPORTED THAT DURING CRUISE, ACFT REQUIRED 4 GRADES OF AILERON COMPENSATOR TO MAINTAIN STRAIGHT AND LEVELED FLIGHT. DURING MX REVISION, THE SPIRAL DRIVE PLATE WAS DETECTED BROKEN; SO THE SPIRAL DRIVE PLATE WAS REPLACED IAW MM 27-10-07, TESTED CORRECT.SDR EE4Y1101033Skin Panel · damagedLOWER FUSELAGE AT STA 114.5 BETWEEN LONGERONS 27L AND 28L SKIN WITH LIGHTNING STRIKE. THE SKIN PANEL IS GOING TO BE REPAIRED AS PER SRM REQUIREMENTS.SDR WX0A070732ABattery · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR 2ARF201101004Servo Drive · damagedACFT RETURNED TO PLATFORM DUE TO DURING TAXING AND WHEN IT WAS TURNED WITH AUTOPILOT SELECTED, THE FLIGHT CONTROLS VIBRATED. MX PERSONNEL REPLACED THE DUPLEX SERVO AILERON DRIVER IAW MM 22-11-00 AND THE DFGS STATUS/TEST (STP) PANEL WAS CHECKED IAW MM 22-01-05SDR EE4Y1101032Skin · bulgedDURING THE INSPECTION COOPESA FOUND THE LOWER EXTERNAL FUSELAGE FROM STA 1201 TO 1207 AT LONG 30 BULGED SKIN. PERMANENT REPAIR WILL BE PERFORMED AS PER DER APPROVAL.SDR EE4Y1101030Skin · damagedDURING THE INSPECTION COOPESA FOUND THE LOWER FUSELAGE AT STA 169 BETWEEN LONG 28 LT AND LONG 29 LT SKIN WITH LIGHTNING STRIKE. PERMANENT REPAIR WILL BE PERFORMED AS PER DER APPROVAL.SDR EE4Y1101029Skin · damagedDURING THE INSPECTION COOPESA FOUND THE LOWER FUSELAGE AT STA 138.5 BETWEEN LONG 27 LT AND 28 LT SKIN WITH LIGHTNING STRIKE. PERMANENT REPAIR WILL BE PERFORMED AS PER DER APPROVAL.SDR EE4Y1101031Frame · crackedDURING THE INSPECTION COOPESA FOUND THE AFT ACCESSORY COMPARTMENT CANTED STA 1463, -X8.5 OUTBOARD CHORD CRACKED. PERMANENT REPAIR WILL BE PERFORMED AS PER DER APPROVAL.SDR WX0A070730Fire Loop · failedFLIGHT CREW REPORTED LT ENG FIRE DETECTION LOOP A FAILED IN FLIGHT, QRH PERFORMED. MAINTENANCE PERSONNEL VERIFIED GOOD RESISTANCE D-V AT LT FIRE DETECTION UNIT CONNECTOR. 465 OHMS, NO CHAFING AND OBIVIOUS DEFECTS ON ENGINE, SYSTEM OPS CHECKS GOOD IAW AMM 26-1SDR WX0A070740Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR 2ARF201101003Water Separator · leakingACFT PERFORMED AN UNSCHEDULED LANDING, DUE TO LOSS OF CABIN PRESSURE AT 36,000 FT. DURING MX REVISION, THE LT WATER SEPARATOR DUCT WAS DETECTED LEAKING; SO THE AIR CONDITIONING, PNEUMATIC AND ANTI ICE SYS LEAK CHECKS WERE PERFORMED IAW MM 21-00-00, 36-00-00 ANSDR 2011FA0000019Unknown · odorFLIGHT 487, SEATS 36D AND 36E. SEATS ARE LOCATED NEXT TO THE ENGINE. THERE WAS A STRONG SMELL OF FUEL IN THE CABIN RESULTING IN A HEADACHE.SDR WX0A070738Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR 2ARF201101002Controller · inoperativeACFT RETURNED OF FLIGHT DUE TO RT AIR CONDITIONING WAS SHUTDOWN AND THE LT AIR CONDITIONING WAS NOT ENOUGH TO MAINTAIN CABIN PRESSURE. DURING MX REVISION, THE RT CABIN TEMP CONTROLLER WAS DETECTED INOPERATIVE IN AUTOMATIC MODE; SO THE REPORT WAS DEFERRED IAW MSDR WX0A070734Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR WX0A070737Battery · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERSDR WX0A070735ABattery Pack · dischargedDURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ASDR EE4Y1101027Seat Track · corrodedUPPER FUSELAGE PAX CABIN AT STA 218, -X55 SEAT TRACK WITH CORROSION. DAMAGED SEAT TRACK WAS REPAIRED IN ACCORDANCE WITH MD-80 SRM 53-05 FIGURE 4F VIEW E.SDR EE4Y1101026Skin · scratchedLOWER EXTERNAL FUSELAGE SKIN AT STA 1304 BETWEEN LONGERONS 18R AND 19R WITH SCRATCH. DAMAGED SKIN WAS REPAIRED PER BOEING DWG SG09530001 VIEW D1 SHEETS 1 AND 3.
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