Douglas DC-9-32F
Service difficulty reports · 517
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 = 'DC932F' 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 = 'DC932F' 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 2022F00149Turbine Blades · damagedDURING THE CLIMB BETWEEN 12000 AND 15000 FT, A LOUD BANG WAS HEARD, OBSERVING PARAMETERS OF THE LEFT ENGINE OUT OF RANGE IN RELATION TO THE POSITION OF THE THROTTLE LEVER OF THE SAME ENGINE, PROCEEDING TO SHUTDOWN THE LEFT ENGINE PER QRH.SDR 2022F00144Warning Message · illuminatedINDICATION LOWER CARGO FIRE FOR ONE MINUTE.SDR Y2PA201809250032Skin Panel · corrodedDURING C-CHECK AT KSFB, CORROSION WAS DISCOVERED ON SKIN AT STA 1114, LONGERON 18R. MAINTENANCE AT KSFB. REMOVED AND REPLACED LOWER SKIN FROM STA 1087-1121, LONGERON 18R-23R. REMOVED AND REINSTALLED MIDDLE SKIN FROM LONGERON 15R-18R. REMOVED AND REINSTALLED UPSDR Y2PA2018092530030Pitot Tube · obstructedCREW REPORTED 60 KNOT AIRSPEED DISCREPANCY DURING CLIMB. RAN COM 5.31.5 WITH NO SUCCESS. RETURNED TO KLRD AND DECLARED EMERGENCY. NO FURTHER INCIDENT. MAINTENANCE AT KLRD DISCONNECTED CAPT/FO’S PITOT LINES FROM PITOT TUBES. DURING INSPECTION PITOT OF TUBES FOUSDR Y2PA201804170013Control Panel · inoperativeENCOUNTERED AN ELECTRICAL PROBLEM DURING CLIMB. RETURNED TO DEPARTURE. NO FURTHER ISSUES OCCURRED AND LANDED SAFELY. EMERGENCY DECLARED WITH ATC. LEFT GENERATOR OFF LIGHT ILLUMINATED DURING CLIMB. RAN COM PROCEDURE, NO HELP. APU DID NOT COME ONLINE. MAINSDR Y2PA2017112300031Sensor · failedCREW REPORTED DURING GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. PERFORMED COM PROCEDURE, DECLARED EMERGENCY, REMAINED AIRBORNE TO BURN OFF FUEL TO MEET LANDING WEIGHT REQUIREMENTS. LANDING GEAR EXTENDED NORMALLY. COMPLETED UNEVENTFUL LANDISDR Y2PA2016092900024Warning System · malfunctionedIMMEDIATELY AFTER TAKEOFF, COULD SMELL AN ELECTRICAL BURNING ODOR FOLLOWED BY A MASTER CAUTION LIGHT. SEVERAL ANNUNCIATORS CAME ON AND OFF, FOLLOWED BY THE GPWS FAIL, STALL INDICATION FAIL AND FLAP/RUDDER/STOP INOPERATIVE REMAINING ON. IMMEDIATELY STARTED A SDR Y2PA2016022800004Landing Gear · malfunctionedDURING APPROACH, GEAR HANDLE PLACED IN DOWN POSITION. NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE GREEN. CYCLED GEAR, NOSE GEAR LIGHT STILL DID NOT ILLUMINATE GREEN. DECLARED EMERGENCY AND RAN COM EMERGENCY GEAR EXTENSION PROCEDURE. NOSE GEAR LIGHT STILL DIDSDR Y2PA2016011200001Skin · corrodedMAINTENANCE DISCOVERED A MISSING RIVET FROM THE BELLY SKIN AT FS 585. UPON FURTHER INSPECTION, IT WAS DETERMINED THAT THERE WAS INTERNAL AND EXTERNAL CORROSION AND A TEMPORARY REPAIR WAS INSTALLED AND THE AIRCRAFT WAS FERRIED FOR REPAIR. MAINTENANCE INSTALLESDR K11A2013060616001Fuel Cap · missingFUEL REPORTED AS VENTING FROM RT WING, NOTED FUEL IMBALANCE AND RETURNED TO DEPARTURE. UPON INVESTIGATION, FOUND RT OVERWING FUEL CAP MISSING, REPLACED CAP AND FUELED TO VTO, NO LEAKS NOTED.SDR Y2PA20130511039Line · failedCREW REPORTED POST V1 & JUST INTO ROTATION, MASTER CAUTION ILLUMINATED FOR LT OIL PRESSURE LOW. DECISION MADE TO LEAVE MLG DOWN. OIL PRESSURE LOW & QTY DECREASING, NORMAL CHECKLIST COMPLETED & ABNORMAL CHECKLIST LEADING TO A PRECAUTIONARY SHUTDOWN. CREW SDR Y2PA20130507036Skin · crackedDURING C-CHECK INSPECTION AT YIP, MX DISCOVERED THE LT FLAP LOWER SKIN CRACKED. MX AT REPAIRED IAW SRM 57-01, FIGURE 3, SHEET 2 AND EA 96-51-02 R1.SDR Y2PA20130507035Hinge · crackedDURING C-CHECK INSPECTION, MX DISCOVERED THE LT WING CENTER AFT FLAP HINGE CRACKED. MX R & R HINGE IAW AMM 27-51-1 AND OHM 27-50-1.SDR Y2PA20130507034Bracket · corrodedDURING C-CHECK INSPECTION, MX DISCOVERED THE MAIN UPPER CARGO DOOR LOWER SILL BRACKET CORRODED. MX R & R BRACKET IAW SRM 51-30-5.SDR Y2PA20130507033Panel · delaminatedDURING C-CHECK INSPECTION, MX DISCOVERED THE INBD LT T/E WING PANEL DELAMINATED. MX R & R PANEL WITH SERVICEABLE IAW SRM 51-30-2.SDR Y2PA20130507032Panel · delaminatedDURING C-CHECK INSPECTION, MX DISCOVERED THE SECOND FROM OTBD LT T/E WING PANEL DELAMINATED. MX R & R PANEL WITH SERVICEABLE IAW SRM 51-30-2.SDR Y2PA20130507031Tee Fitting · corrodedDURING C-CHECK INSPECTION, MX DISCOVERED A TEE FITTING CORRODED AT BS 160 ON THE RT CUSP LINE. MX R & R TEE FITTING IAW SRM 51-30-2 AND 51-30-5.SDR Y2PA20130507030Cusp Web · crackedDURING C-CHECK INSPECTION, MX DISCOVERED A CRACKED WEB AT STATION 953, LONGERON 18L. MX REPAIRED IAW SRM 53-01, FIGURE 2, SHEET 3 AND EA 96-51-02 R1.SDR Y2PA20130507029Longeron · corrodedDURING C-CHECK INSPECTION, MX DISCOVERED LONGERON END SHOVEL CORRODED IN THE LOWER AFT CARGO BAY AT BS 996 ON LONGERONS 29L. MX R & R SHOVELS IAW SRM 51-30-5.SDR Y2PA20130507028Sleeve · crackedDURING C-CHECK INSPECTION, MX DISCOVERED BOTH LT AND RT HORIZONTAL STABILIZER HINGE BOLT SLEEVES CRACKED. MX R & R SLEEVES IAW AMM 55-10-0.SDR Y2PA20130507027Skin · corrodedDURING C-CHECK INSPECTION, MX DISCOVERED THE LOWER AFT CARGO BAY SKIN CORRODED AT BS 756, LONGERON 27L 29R. MX REPAIRED IAW EA 13-53-321 AND DER DWG 53-13118-1, 8110-3, DATED 3/19/13.SDR Y2PA20130507026Web · corrodedDURING C-CHECK INSPECTION, MX DISCOVERED THE LOWER AFT CARGO BAY CENTERLINE WEB CORRODED AT BS 996. MX REPAIRED IAW SRM 53-01, FIG 2 SHEET 3 AND EA 96-51-02 R3.SDR Y2PA20130507025Window Frame · crackedDURING INSPECTION IAW AD 2002-21-09, 2 EACH .5" CRACKS WERE DISCOVERED IN THE CENTER FRAME OF THE COCKPIT WINDOW SILL. MX R & R THE COCKPIT WINDOW SILL CENTER FRAME WITH NEW IAW SB 53-290 R3, DWG SR09530268, SRM 51-30-2 AND 51-30-5.SDR Y2PA20130507024Spar · crackedDURING C-CHECK X-RAY INSPECTION, MX DISCOVERED THE LT ELEVATOR FRONT SPAR CRACKED OUT OF LIMITS. MX AT YIP R & R THE LT ELEVATOR WITH A SERVICEABLE PART IAW MM 27-30-2.SDR Y2PA20130306010Skin · crackedEMERGENCY PROCEDURE, EMERGENCY DESCENT, UNSCHEDULED LANDING. FUSELAGE SKIN CRACKED AT BS 950 BETWEEN L14-15R, DISCOVERED DURING C-CHECK INSPECTION. MX REPAIRED IAW SRM 54-04, FIG 46.SDR Y2PA20130306009Shear Tie · crackedUNSCHEDULED LANDING, EMERGENCY DESCENT, ETC. SHEAR TIE CRACKED AT BS 945 BETWEEN LONGERONS 14R AND 17R, DISCOVERED DURING C-CHECK INSPECTION. MX REPLACED SHEAR TIE IAW SRM 51-30-5.SDR Y2PA20130306008Fitting · crackedUNSCHEDULED LANDING, EMERGENCY DESCENT. RT PYLON REAR SPAR UPPER CAP FITTING AT STATION Y 1038 FOUND CRACKED DURING C-CHECK INSPECTION. MX REPLACED FITTING IAW SRM 51-30-1, 51-30-3 AND 51-30-5.SDR Y2PA20130306007Fitting · crackedUNSCHEDULED LANDING, EMERGENCY DESCENT, ETC. LT PYLON REAR SPAR UPPER CAP FITTING AT STATION 1038 FOUND CRACKED DURING C-CHECK INSPECTION. MX REPLACED FITTING IAW SRM 51-30-1, 51-30-3 AND 51-30-5.SDR Y2PA20130306006Skin · chafedEVIDENCE OF DAMAGE ON UPPER RT SIDE OF VERTICAL STABILIZER BETWEEN STATION ZV120 NEAR FORWARD END OF UPPER AND LOWER BODY FAIRINGS, DISCOVERED DURING C-CHECK. MX REPAIRED IAW DWG 55301301-1 AND APPROVED 8110-3 DATED 02/19/13.SDR Y2PA20130306005Attach Angle · crackedEMERGENCY PROCEDURE, UNSCHEDULED LANDING, EMERGENCY DESCENT. RT PYLON UPPER PYLON TO FUSELAGE ATTACH ANGLE 12, AFT OF LEADING EDGE HAS 1 CRACK AT CORNER, DISCOVERED DURING C-CHECK INSPECTION. MX REPAIRED IAW SRM 54-04, FIG 10.SDR Y2PA20120910041Turbine Blades · damagedCREW REPORTED AFTER DEPARTURE WHEN TRANSITIONING TO QUIET EPR POWER SETTING A SUDDEN LOUD AND EXTREME VIBRATION OCCURRED. OBSERVED LOSS OF EPR, N1 & N2. LT ENGINE WAS VERIFIED AS FAILING AND SOURCE OF VIBRATION WITH THROTTLE TO IDLE. EMERGENCY DECLARED AND SDR Y2PA2011092000024Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE DURING INSP. MX R & R BATTERY POWER SUPPLY IAW AMM 33-50-0. OPS CHECKS GOOD, NO OTHER DEFECTS NOTED.SDR Y2PA2010111500028Downlock Switch · malfunctionedUPON APPROACH, THE RT MLG DID NOT DISPLAY GREEN INDICATION, ONLY RED. CREW EXECUTED MISSED APPROACH AND REVIEWED COM PROCEDURES. CREW DIVERTED AND DECLARED AN EMERGENCY INBOUND. CREW FOLLOWED COM PROCEDURES FOR MANUAL EXTENSION OF GEAR AND SECONDARY SYS SHOSDR ABXA080151Attach Angle · crackedLEFT VERTICAL STAB ATTACH ANGLE CRACKED, LOCATED AT BASE OF RUDDER. REPAIRED LEFT VERTICAL STAB ATTACH ANGLE IAW DC9 SRM 53-05.SDR ABXA080152Pan · crackedMAIN ENTRY DOOR PAN CRACKED FORWARD SIDE (BOTTOM HINGE) SECOND STOP FROM BOTTOM. REMOVED AND REPAIRED DOOR IAW DC9 SRM.SDR ABXA080150Skin · crackedFUSELAGE SKIN CRACKED AT STA 160, LONGERON 20 - 21 LEFT AT AIRSTAIR HINGE FORWARD SIDE. REPAIRED FUSELAGE SKIN CRACK IAW DC9 SRM.SDR ABXA080120Relay · defectivePRIMARY TRIM CIRCUIT BREAKER TRIPPED WHILE SETTING TAKEOFF TRIM. WHILE MECHANIC WAS TROUBLESHOOTING PRIMARY TRIM, HEAVY SMOKE PRODUCED THROUGHOUT FRONT & REAR CABIN. CREW CONDUCTED EMERGENCY SHUT DOWN & EVACUATED AIRCRAFT. FOUND RELAY R20-15 BURNT. REPLACESDR ABXR080108Attach Angle · crackedATTACH ANGLE FOR STA 41 TO STA 69 PRESSURE PANEL INTERCOSTAL CRACKED JUST RIGHT OF PLUG DOOR. REMOVED AND REPLACED ANGLES IAW DC9 SRM 51-30-5.SDR ABXR080107Attach Angle · crackedATTACH ANGLE FOR STA 41 TO STA 69 PRESSURE PANEL INTERCOSTAL CRACKED. SECOND INTERCOSTAL TO THE LEFT OF THE PLUG DOOR. REMOVED AND REPLACED IAW DC9 SRM 51-30-5.SDR ABXR080106Fitting · crackedPYLON UPPER REAR SPAR STRAP CLIP JUST INSIDE PYLON CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW CLIP IAW DC9 SRM 51-30-1 AND 51-30-5.SDR ABXR080105Attach Angle · crackedLEFT WHEEL WELL KEEL WEB UPPER ATTACH ANGLE AT STA 718 CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.SDR ABXR080104Attach Angle · crackedINBOARD BULKHEAD STA 718 ATTACH ANGLE CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXR080103Skin · crackedAFT LOWER CARGO DOOR SKIN CRACKED AT DOOR HANDLE. REPAIRED DOOR IAW DC9 SRM 52-05, FIGURE 30, SHEET 1.SDR ABXR080102Skin · crackedFORWARD LOWER CARGO DOOR SKIN CRACKED AT DOOR HANDLE. REPAIRED AND PAINTED IAW DC9 SRM 25-05 AND 51-10.SDR ABXA070425Battery Pack · defectiveEMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW DC9 AMM CHAPTER 33.SDR ABXA070424Battery · dischargedCABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.SDR Y2PA200700026Csd · failedCREW REPORTED ENGINE VIBRATION THEN FAILURE ON NR 2 ENGINE. IRREGULARITY FILLED OUT BY CREW REPORTED AS FOLLOWS. AFTER DEPARTURE IN CLIMB, VIBRATION FOLLOWED BY NR 2 ENGINE FLAME OUT AT FL190 FOLLOWED BY AIRCRAFT CROSSTIE LOCKOUT. CREW DECLARED AN EMERGENCYSDR ABXA070262Frame · crackedWHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME, REF AD 2002-21-09. REPLACED FRAME IAW DC9 SRM 51-30-02 AND 51-30-05.SDR ABXA070264Angle · crackedWHILE COMPLYING WITH EA 53300036, FOUND CRACKED ANGLE, REF AD 2002-21-09. REPLACED ANGLE IAW DC9 SRM 51-30-05.SDR ABXA070263Bracket · crackedWHILE COMPLYING WITH EA 53300036, FOUND CRACKED BRACKET, REF AD 2002-21-09. REPLACED BRACKET IAW DC9 SRM 51-30-02 AND 51-30-05.
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