Boeing DC-9-83
Service difficulty reports · 16,530
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 = 'DC983' 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 = 'DC983' 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 AALA20160331010Skin · crackedAIRCRAFT WAS IN BASE MX. FUSELAGE SKIN CRACKED AT STATION 1474 & LONGERON 24R. REPAIRED SKIN IAW SRM 53-01-00-001.SDR WX0A2016040173122Unknown · not reportedON CLIMB OUT WITH DFGS SWITCH ON NR 1 POSITION FLIGHT & DIRECTOR FAILED ON NR 1 SIDE WITH A BLANK FMA DISPLAY AUTOPILOT & AUTO THROTTLE FAIL. RAN QHR 31.3 & 31.8, LOST NR 2 FMA & FLIGHT DIRECTOR WHEN DFGS SWITCHED TO NR 2. FMA & FLIGHT DIRECTOR RETURNED AT 1SDR AALA20160331005Connector · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB RT ENG OIL TEMPERATURE INCREASED TO 200 DEGREES. FOUND LOOSE WIRE & BACK SHELL ON CONNECTOR FOR TEMPERATURE SENSOR. REPLACED OIL TEMPERATURE CONNECTOR SDR AALA20160331001Portable Light · no testAIRCRAFT WAS NOT GNDED. L1 DOOR PORTABLE EMER LIGHT FAILED TO TEST. R & R LIGHT ASSEMBLY IAW AMM 33-53-00. SYS CHECKED NORMAL.SDR WX0A2016040173121Sense Line · rupturedRIGHT ENG EPR READS UP TO 0.3 HIGH ERRATICALLY DURING FLIGHT. WITH HIGHER ALTITUDE CORRESPONDING TO GREATER DEVIATION. QRH 72.10 YIELDS NO HELP. FOUND NR 2 ENG PT2 LINE RUPTURED. R & R PT2 LINE IAW AMM 71-00-00-4-13B 40. LEAKED CHECKED SYS, FOUND SYS SATISDR WX0A2016040173120Connector · defectiveSTALL INDICATOR FAILURE ON OAP. DURING CRUISE RAN QRH 85.4, STALL SYS 2 DID NOT TEST, PULLED FIRST OFFICERS STALL SYS NR 2 CB. FOUND HARD FAULT ON STALL COMP NR 2 RT AOA VANE ON MX TEST. R & R RT AOA VANE TRANSDUCER CONNECTOR, BITE TEST STALL WARNING SYS OKSDR WX0A2016040173119Skin · damagedRIGHT STATIC PORT SKIN PLATE DAMAGED ON AIRFRAME SIDE. REPAIR FOR FUSELAGE SKIN DAMAGE FS 598 - 617, LONGERON 24R - 25R AT STATIC PORT, CUT OUT ACCOMPLISHED IAW WO 919-03-2006 FOR ALL WORK DETAILS PERFORMED.SDR WX0A073118Unknown · not reportedON DESCENT WHILE SELECTING DFGC 2, THE ATTITUDE SELECTOR WENT BLANK, IT ILLUMINATED. WHEN IT WENT BLANK, THE AUTO PILOT & AUTO THROTTLES KICKED OFF & THE FIRST OFFICER LOST THE FLIGHT DIRECTOR, WHEN IT CAME BACK ON WE WERE ABLE TO RESELECT ALL MODES. HOWEVERSDR WX0A2016040173117Computer · malfunctionedON CLIMB OUT, DUAL PLATFORM FAIL WAS INDICATED AFTER LOSING FLIGHT DIRECTOR, AUTO THROTTLE & AUTO PILOT. SYS CAME BACK AFTER 25 MIN RETURN TO FIELD. BOTH 1 & 2 VG'S, NR 1 DFGC R & R & WIRING CHECKS OF VGS SEE LOG PAGE 677417 & WO 293781, 293769, 293770 & 29SDR WX0A2016040173116Computer · faultySTALL IND FAILURE ON OAP SEVERAL TIMES IN FLIGHT. STALL SYS 2 WOULDN’T TEST, WENT OUT IN APPROX 1 MINUTE EACH TIME. R & R STALL WARNING COMPUTERS 1 & 2. OPERATIONS HECK GOOD IAW AMM 34-19-02.SDR AALA20160407009Transformer · odorAIRCRAFT WAS GNDED. DURING FLIGHT AN ACRID & ELEC ODOR WAS REPORTED IN THE MID CABIN AREA. FOUND READING LIGHT TRANSFORMER T1-90 HOT & EMITTING ODOR. R & R TRANSFORMER & ACCOMPLISHED OPERATIONAL CHECK IAW AMM 20-50-06. SYS CHECKED NORMAL.SDR WX0A2016032873114Sense Line · rupturedDURING THE CLIMB, NOTICEABLE SPLIT IN THE EPR AS THEY CLIMBED ABOVE FL 250. AT CRUISE AT FL 330 THERE WAS A .25 SPLIT IN THE EPR WITH THE N1 MATCHED. THE EPR WAS LOWER ON THE NR 1 ENG WITH THE N1S MATCHED. WITH THE EPRS MATCHED THERE WAS A 9% DIFFERENCE IN SDR WX0A2016032873113Fuel Control · faultyRIGHT ENG WAS SURGING WHILE CLIMBING TO FL 330. ALL ENG INDICATIONS WERE FLUCTUATING, FF +- 200 N1 UP TO 10 EPR 1.90 2.02. VIDEO WAS EMAILED TO MTC CONTROL SHOWING FLUCTUATIONS. THROTTLES WERE STATIONARY DURING FLUCTUATIONS. LT ENG WAS FLUCTUATING TOO, BUTSDR AALA20160324013Skin · crackedAIRCRAFT WAS GNDED. FUSELAGE SKIN CRACKED AT STATION 1485, ALONG CANT RIVET LINE JUST AFT OF RT T/R ACCUMULATOR ACCESS DOOR. ACCOMPLISHED SKIN REPAIR IAW SRM 53-01-00-001.SDR AALA20160324010Support Fitting · crackedAIRCRAFT WAS IN BASE MX. FWD CARGO COMPARTMENT DOOR STOP PAD SUPPORT FITTING, 3RD FROM TOP ON FWD EDGE, IS CRACKED. R & R FITTING IAW AARD 51-00-05-1 & DWGS CDK2345 & 5910141.SDR AALA20160324002Skin · crackedAIRCRAFT WAS IN BASE MX. FUSELAGE SKIN IS CRACKED AT STATION 1380 & LONGERON 14R. REPAIRED SKIN IAW SRM 53-01-00-001 & AARD 53-30-00-02;.SDR AALA20160330010Shutoff Valve · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING FLIGHT, CABIN CREW REPORTED SEEING SMOKE & VAPOR FROM THE AIR CONDITIONING VENTS & AN ODOR DESCRIBED VARIOUSLY AS BURNED RUBBER, ELEC, FUEL. ACCOMPLISHED CARDSDR AALA20160329007Fitting · leakingAT GATE AFTER PAXS DEPLANED, CREW NOTED A BLUE HAZE IN CABIN, ACCOMPANIED BY AN OIL ODOR. ACCOMPLISHED MCM CARD 21-96-01 & NR 2 ENG IGV CASE LEAKING OIL OUT OF FAN INLET SLEEVE. R & R NR 2 ENGINE IAW MCM 71-91-99. ENGINEERING REPORTED OIL LEAK WAS FROM THE SDR AALA20160324003Shutoff Valve · faultyAIRCRAFT WAS GNDED, AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING FLIGHT, CABIN CREW REPORTED SEEING SMOKE & VAPOR FROM THE AIR CONDITIONING VENTS & ODOR DESCRIBED VARIOUSLY AS BURNED RUBBER, ELEC & FUEL. ACCOMPLISHED CARD 21SDR AALA20160324001Fitting · crackedAIRCRAFT WAS IN BASE MX. RT GND SPOILER ACTUATOR FITTING IS CRACKED AT FWD INBD & OTBD END. R & R ACTUATOR FITTING IAW SRM 51-01-00-001.SDR WX0A2016032873110Engine · overspeedON APPROACH AT 6000 MSL, AUTO-THROTTLE COMMANDED FULL POWER & DISCONNECTED, RESULTING IN BOTH ENGS OVER SPEED. AIRSPEED WAS 170 KTAS EPR 2.10-2.12 N1 APROX 105% & FLASHING LESS THAN ONE SECOND.SDR AALA20160322010Apu · odorAT GATE, PRIOR TO FLIGHT, BOTH PACKS TURNED ON AFTER APU POWERED ON. EGT TOO HOT TURNED OFF RIGHT PACK. FUMES & SMOKE BEGAN FILLING MID TO AFT CABIN, TURNED LT PACK OFF. FOUND APU LEAKING OIL. APU CHANGE PLANNED. ACCOMPLISHED PACK BURNOUT PER WORK CARD 2SDR WX0A2016031873108Proximity Sensor · faultyDURING THE T/O ROLL RECEIVED THE SLAT DISAGREE & THE SLAT AURAL WARNING AROUND 70 KTS. ABORTED T/O. TAXIED BACK TO THE GATE. CAPTAIN WILL PUT THE DISCREPANCY IN THE LOG BOOK. PSEU SN 668 HAD PRIOR FAULT ISSUES WITH SLAT DISAGREE. R & R PSEU IAW AMM 32-60-SDR AALA20160316010Battery Pack · dischargedCEILING EPL LIGHTS INOPERATIVE. REPLACED EMER LIGHT BATTERY PACKS IAW AMM 33-53-00. OPERATIONS CHECKED GOOD. ACFT IN BASE MX.SDR AALA20160321004Fitting · leakingAIRCRAFT WAS NOT GNDED. FUMES FROM PACK SYS REPORTED. FOUND SOURCE TO BE APU INGESTION OF HYD FLUID, DUE TO A LEAKING PRESS BULKHEAD TO PYLON FIRE WALL UNION FITTING. ACCOMPLISHED REPAIR TO RT ENG PRESS LINE IAW AMM 200-12-04. LEAK CHECKED GOOD. .SDR AALA20160315005Battery · dischargedEMER LIGHTS ROWS 27 - 32 FAIL TO TEST. REPLACED B5-107 EMER LIGHT BATTERY POWER SUPPLY IAW AMM 33-53-00. TESTED OK. THE ACFT WAS NOT GNDED.SDR AALA20160315004Battery · dischargedEMER LIGHTS ROWS 12 - 17 FAIL TO TEST. REPLACED B5-102 EMER LIGHT BATTERY POWER SUPPLY IAW AMM 33-53-00, TESTED OK. THE ACFT WAS NOT GNDED.SDR WX0A2016031673106Battery · dischargedAFT FWD FLASHLIGHT NOT BLINKING. INSTALLED NEW FLASHLIGHT BATTERY IAW MM 25-60-00. OPERATIONS CHECKED GOOD.SDR AALA20160330009Floor Support · crackedAIRCRAFT WAS GNDED. CABIN FLOOR PANEL BETWEEN SEATS 20B & 20D REPORTED TO BE SOFT. FOUND FLOOR PANEL SUPPORTS, 2 EACH, CRACKED. R & R SUPPORTS. SEE ALSO AALA 20160317006.SDR AALA20160317006Floor Support · damagedAIRCRAFT WAS GNDED. CABIN FLOOR PANEL, BETWEEN SEATS 20B & 20D, REPORTED TO BE SOFT. MX FOUND FLOOR PANEL SUPPORTS, TWO EACH, CRACKED. R & R SUPPORTS. SEE ALSO AALA 20160330009.SDR AALA20160313002Cabin Pressure · uncontrollableAT 23,000 FEET, CABIN PRESS ALTITUDE WAS CLIMBING MORE THAN 1,500 FEET PER MINUTE. ENG & WING ANTI-ICE WERE ON. CLOSED OUTFLOW VLV, BUT COULDN`T CONTROL CABIN PRESS. EMER DECLARED. EMER DESCENT TO 10,000 FEET. FLIGHT RETURNED WITHOUT FURTHER INCIDENT. PESDR WX0A2016031673107Vertical Gyro · faultyAFTER TAKEOFF, CLIMBING THROUGH 10,000, PLATFORM 2 FAILED, MSG ON FMS SCRATCHPAD. SHORTLY AFTER, PLATFORM 1 FAILED RESULTING IN LOSS OF BOTH FLIGHT DIRECTORS, AUTOPILOT, AUTO THROTTLES & BOTH FMA'S. PERFORMED FAULT REVIEW & SHOWS ATT 1 & 2 SIGNAL FAULTS IAW SDR 2WAA20160314002Line · leakingAT FL 320, CABIN BEGAN TO FILL WITH SMOKE. DECLARED AN EMERGENCY FOLLOWED QRH, DIVERT. PERFORMED EXTENSIVE T/S IAW AMM 49-90-00, FOUND LINE LOOSE AT APU OIL PRESSURE SENSOR. RESECURED OIL LINE IAW AMM 20-12-01, OPS CHECKED NORMAL IAW AMM 21-20-00, NO ODOR NSDR AALA20160314004Slide · unsecureL1 DOOR SLIDE FELL FROM HOUSING. SLIDE DID NOT DEPLOY, BUT SLIDE DEPLOYMENT PIN WAS COMING APART. R & R L1 DOOR SLIDE IAW MM 25-62-00. THE ACFT WAS GNDED.SDR WX0A2016031673105Battery · dischargedTOP FWD EMER FLASHLIGHT DOES NOT BLINK RED. R & R TOP FWD EMER FLASHLIGHT BATTERY. OPERATIONS GOOD IAW AMM 25-60-00.SDR AALA20160311003Battery · dischargedAFT EPL LIGHTS WON`T TEST WHEN USING PACKS AB5-2 & AB5-3. REPLACED BATTERY FOR AFT EPL LIGHTS AB5-3 IAW MM 33-60-00. OPERATIONS CHECKS NORMAL. THE ACFT WAS NOT GNDED.SDR AALA20160311002Battery Pack · dischargedTAIL COMPARTMENT EMER LIGHTS WON`T TEST. REPLACED TAIL COMPARTMENT EMER LIGHTS BATTERY PACK IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL. THE ACFT WAS NOT GNDED.SDR AALA20160311001Battery Pack · dischargedOVERHEAD EMER LIGHTS AT ROWS 23 - 25 WON`T TEST. REPLACED EMER LIGHTS BATTERY PACK FOR ROWS 23 - 25 IAW AMM 33-53-00. OPERATIONS CHECKS NORMAL. THE ACFT WAS NOT GNDED.SDR AALA20160309004Engine · failedRIGHT ENG LOST OIL PRESS & QUANTITY DURING DESCENT. ENG SHUTDOWN. AN EMER WAS DECLARED. ENG WIND MILLED ABOUT 5 MINUTES. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENG TIME WAS ABOUT 10 MINUTES. R & R RT ENG IAW MCM 71-91-99. THE ACFT WAS SDR WX0A2016031173101Connector · looseNO PAXS IN FLIGHT, FERRY FLIGHT. PACKS SHUT DOWN INFLIGHT, LOST PRESSURIZATION, INITIATED RAPID DECENT. HOWEVER AT 14,000 FT CABIN ALT THE PX O2 MASKS DEPLOYED. LT PACK SHOWS 14 PSI AT CRUISE POWER, EVEN WHEN PACK IS OFF. REF WO 290982 ITEMS 1 & 3 FOR TROUSDR AALA20160308003Hose · rupturedAT 34,000 FT, GOT PRESSURIZATION FLOW LIGHT ON. DESCENDED TO 25,000 FT. AT 25,000 FT, THE CABIN DEPRESSURIZED. THE CREW DONNED OXYGEN MASKS & PERFORMED EMER DESCENT TO 10,000 FT. AN EMER WAS DECLARED. OXYGEN MASKS DEPLOYED IN THE CABIN WHEN CABIN ALTITUDESDR AALA20160310001Engine · failedTHE INBD CREW REPORTED ODOR & HAZE IN THE CABIN, CAUSING EYES TO WATER & WAS DIFFICULT TO BREATHE. ACCOMPLISHED SIC 21-96-01 & FOUND LT ENG TO BE THE SOURCE OF THE ODOR. R & R THE LT ENG IAW SIC 71-91-99 & BOW. LEAK CHECK & OPERATIONS CHECKED GOOD. ACCOMPLSDR AALA20160306010Heater · malfunctionedPITOT & STALL HEAT OFF LIGHT ILLUMINATED IN CRUISE. ICING CONDITIONS, RETURNED TO LAND DFW Z30 CIRCUIT BREAKER IS POPPED. FLIGHT DECLARED AN EMER & RETURNED WITHOUT FURTHER INCIDENT. R & R RUDDER Q LIMITER PITOT TUBE HEATER, LEAK CHECK GOOD IAW MM 34-11-02. SDR Y2PA20160304009Longeron · crackedDURING C-CHECK, FOUND A CRACK AND CORROSION FOUND ON LONGERON 30 BETWEEN STA 237 AND 232. A REPAIR WAS DONE IAW SRM 51-10-4. PAGES 1-11, 51-30-2 AND 51-30-5 PAGES 1-22, REV 116, 8/15/15.SDR Y2PA20160304008Longeron · corrodedDURING C-CHECK FOUND CORROSION ON LONGERON 30C BETWEEN BS 1231 AND 1250. A REPAIR WAS DONE IAW SRM 53-02, PARA 13, PAGES 57-58E, REV 116.SDR Y2PA20160304007Door Frame · corrodedDURING C-CHECK, FOUND CORROSION AT ELECTRONIC EQUIPMENT BAY DOOR JAMB AND FORWARD AND AFT FS 134 AND 160, STR 27L AND 27R. A REPAIR WAS DONE IAW J2 ENGINEERING, INC. DOCUMENT J2R-0024 REV. IR DATED 22 FEB 2016, FAA APPROVAL IAW 8110-3.SDR Y2PA20160304006Cusp Web · corrodedDURING C-CHECK FOUND THE LOWER CUSP OF THE R1 DOOR HAD MINOR CORROSION NEAR THE FORWARD EDGE AT FLOOR LEVEL THAT WAS BLENDED TO REMOVE CORROSION. A REPAIR WAS DONE IAW J2 ENGINEERING, INC. DOCUMENT J2R-0023,
REV IR DATED 22 FEB 2016, FAA APPROVAL.SDR WX0A2016030873100Indicator · faultyDURING CLIMB OUT THE CREW RECEIVED AN AFT CARGO DOOR ANNUNCIATOR & NOTED THAT THE ACFT WAS NOT PRESSURIZING. LEVELED OFF AT 10000 FT. THE CREW EXECUTED QRH 21.7 CABIN PRESSURE OFF SCHEDULE OR ERRATIC CHECKLIST & IT DID NOT CORRECT THE ISSUE. ADJUSTED UPPER SDR AALA20160302005Trim Motor · malfunctionedEMERGENCY LANDING WAS DECLARED, INBD ACCOUNT STAB TRIM JAMMED AT 6 DEG UP, AFTER SELECTING FLAPS 40 DEG. PERFORMED GO AROUND, ON SECOND ATTEMPT WAS ABLE TO LAND SAFELY BUT STAB TRIM DID JAM AGAIN AT 6 DEG NOSE UP WITH FLAPS AT 40. NO FURTHER INCIDENTS WAS RESDR AALA20160301003Casting · crackedFOUND 3 INCH CRACK IN LT WING INBD GND SPOILER CASTING. R & R LT GND SPOILER CASTING IAW AARD 51-00-05-1. ACFT IN BASE MX.
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