Douglas DC-9-15F
Service difficulty reports · 851
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 = 'DC915F' 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 = 'DC915F' 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 K11A2008112191508Structure · corrodedW/W CEILING AT STA 620 RBL 40 HAS SIGNS OF CORROSION.SDR K11A2008112191507Support Fitting · corrodedWHEEL WELL CEILING HAS EVIDENCE OF CORROSION AROUND SIDE BRACE SUPPORT FITTING APPROX STA 623 LBL 56.SDR K11A2008112191502Crossbeam · crackedAFT PIT DOOR 2ND FROM THE BOTTOM STOP FITTING CROSSBEAM CRACKED IN 2 PLACES UNDER RADIUS FILLER ON INNER FASTENER FOR STOP FITTING VERIFIED USING HFEC.SDR K11A 200811219150Crossbeam · crackedAFT PIT DOOR FWD STOP FITTING CROSSBEAM CRACKED UNDER RADIOUS FILLER ON OUT FASTENER FOR STOP FITTING VERIFIED USING HFEC.SDR K11A2008112091510Beam · crackedFORWARD CARGO DOOR UPPER CENTER FORWARD STOP FITTING VERTICAL BEAM WEB CRACKED AT TOOLING HOLE AT UPPER AREA VERIFIED BY HFEC.SDR K11A2008112091509Vertical Beam · crackedFORWARD PIT DOOR UPPER CENTER AFT STOP FITTING VERTICAL BEAM WEB CRACKED AT TOOLING HOLE AT UPPER AREA VERIFIED USING HIGH FREQ EDDY CURRENT.SDR K11A2008112191504Floor Panel · damagedMAIN DECK FLOOR PANEL EDGE LIFTING BETWEEN BS 503 AND 566 AT RBL 21.SDR K11A2008112091505Floor Panel · corrodedCORROSION ON TOP OF MAIN DECK FLOOR PANELS BETWEEN BS 370 AND 446, RBL 52.SDR K11A2008112091504Angle · crackedGALLEY SERVICE DOOR HAS CRACK ANGLE FWD OF HINGE TORQUE TUBE.SDR K11A2008112191503Frame · bentSTA 58 FRAME INNER FLANGE BENT LBL 27 10 INCHES UP FROM NOSE GEAR DOOR OPENING.SDR ABXA070033Fitting · crackedRIGHT KEEL BEAM CLOSE-OUT PANEL STRUCTURE, FORWARD LOWER FITTING, CRACKED ON INTERIOR SECTION. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-3 AND 51-30-1.SDR ABXA070034Attach Angle · crackedWING TO FUSELAGE ATTACH ANGLE CRACKED PAST STOP DRILL, RIGHT SIDE. REPLACED ANGLE IAW DC9 SRM.SDR ABXA070032Longeron · crackedLONGERON 16 RIGHT CRACKED AT FRAME FS 332. REMOVED AND REPLACED LONGERON IAW DC9 SRM 51-30-2.SDR ABXA070029Longeron · crackedFS 446, LONGERON 3 RIGHT, CRACKED. REPAIRED CRACKED LONGERON IAW DC9 SRM 53-02, FIGURE 18.SDR ABXA070030Longeron · crackedFS 525, LONGERON 9 LEFT, CRACKED. REPAIRED LONGERON IAW DC9 SRM 53-02, FIGURE 18.SDR ABXA070031Shear Tie · crackedSHEAR TIE CRACKED AT FS 800 ON AFT SIDE, BETWEEN LONGERON 15 RIGHT AND 16 RIGHT. REMOVED AND REPLACED SHEAR TIE AT STA 800 IAW DC9 SRM 51-30-5.SDR ABXA070028Longeron · crackedFS 313, LONGERON 2 RIGHT, CRACKED. REPAIRED CRACKED LONGERON IAW DC9 SRM 53-02, FIGURE 18.SDR MJYA0612063Amplifier · failedDURING CLIMBOUT, CAPTAIN'S ADI FROZE IN THE VERTICAL POSITION WITH THE COMPUTER FLAG SHOWING. CAPTAIN'S COMPASS FROZE WITH THE COMPASS FLAG SHOWING.SDR K11A2008112091507Frame · crackedBS 964 FRAME WEB HAS 1.5 CRACK OTBD OF STAIRWELL OPENING ON RT SIDE.SDR K11A2008112091506Door Frame · crackedAFT AIRSTAIRS DOOR CUTOUT FRAME CRACKED AT AFT END RT SIDE, 1 INCH CRACK IN DOOR OPENING FRAME CAP.SDR Y2PA200600015Structure · corrodedCORROSION FOUND AT STATION 897, LONGERON 24L TO BE OUT OF LIMITS. REQUIRES ADDITIONAL REVIEW TO DETERMINE REPAIR.SDR Y2PA200600012Engine · unserviceableAFTER NORMAL TAKEOFF AT APPROX 50 FT IN THE AIR AND PRIOR TO GEAR RETRACTION. A VERY LOUD BANG WAS HEARD WITH AN ACCOMPANYING SHUTTER. CREW CONTINUED TO CLIMB OUT LEAVING GEAR DOWN. AN EMERGENCY WAS DECLARED WITH THE TOWER, SUBSEQUENTLY A NORMAL LANDING WASSDR MJYA0603059Rod End · looseFOUND LEFT MAIN LANDING GEAR ACTUATOR ROD END PULLED LOOSE FROM THE ACTUATOR.SDR MJYA0602057Socket · damagedLEFT LANDING GEAR LIGHT REMAINED ILLUMINATED IN THE BRIGHT MODE AFTER TO WITH THE LANDING GEAR IN THE UP POSITION AFTER THE UP-LATCH CK. GEAR WARNING HORN DID NOT ACTIVATE OR SOUND WITH THROTTLES AT IDLE AND GEAR INDICATING UP.SDR Y2PA060004Csd · unserviceableRIGHT CSD DISCONNECTED IN FLIGHT DUE TO AN OVERHEAT INDICATION (LIGHT AND TEMP INDICATION) AND GENERATOR LOW FREQUENCY. CREW DECLARED EMERGENCY REQUESTING DIVERSION WHEN CSD TEMPERATURE REMAINED AT REDLINE. DURING THE DESCENT THRU FL300 THE CSD COOLED BELOW SDR 0509020Door · delaminatedLT WING, TRAILING EDGE, BUTE DOOR P/N 5919572-1, UPPER SKIN DELAMINATED AT STATION XRS 260 AND SKIN WORN OUT AT STATION XRS 153.SDR 0509019Support Fitting · crackedFWD CARGO COMPARTMENT SUPPORT FITTING CRACKED, LOCATED FROM STA Y305 TO STA Y313 BETWEEN LONGERON 29R AND LONGERON 30.SDR 0509018Support Fitting · crackedAFT CARGO COMPARTMENT SUPPORT FITTING CRACKED, LOCATED AT STA Y661 BETWEEN LONGERON 22R AND LONGERON 24R.SDR 0509017Fitting · crackedRT WING FLAP REAR SPAR WITH FITTING CRACKED, LOCATED AT STA XFLS 300.SDR 0509016Fitting · crackedRT WING FLAP FRONT SPAR WITH FITTING CRACKED, LOCATED AT STA XFLS 288.SDR 0509015Fitting · crackedRT VENTRAL STAIR CUTOUT WITH FITTING CRACKED LOCATED AT STA Y892.SDR 0509014Fitting · crackedLT WING FLAP REAR SPAR WITH FITTING CRACKED LOCATED AT STA XFLS 300.SDR 0509013Support · corrodedCONTROL CABIN WINDSHIELD WITH SUPPORT CORRODED.SDR 0509012Fitting · crackedLT WING FLAP T/E SECTION WITH FITTING CRACKED LOCATED AT STA XFLS 76.SDR 0509011Fitting · corrodedLOWER FUSELAGE - KEEL AREA - LONGERON 30 STA 490.540 LONGERON END ANGLES (RT AND LT) CORRODED.SDR 0509010Fitting · crackedLOWER FUSELAGE - KEEL AREA - LONGERON 29 RT STA 523 OVER LONGERON FITTING CRACKED.SDR 0509009Longeron · corrodedLOWER FUSELAGE - KEEL AREA - LONGERON 29 RT FROM STA 493 TO STA 522 WITH CORROSION.SDR 0509008Support Fitting · corrodedLOWER FUSELAGE - KEEL AREA - STA 576.939 BETWEEN X1.5 AND X8.5 RT SIDE, SUPPORT FITTING CORRODED.SDR ROSA2005040Actuator · failedLOST CABIN PRESSURE AT 19,000 FEET, RETURNED TO AIRPORT. REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR AND CABIN PRESSURE CONTROLLER SIGNAL AMPLIFIER SYSTEM FUNCTION CHECKS SATISFACTORY AT THIS TIME.SDR 91500002Doubler · crackedA 1.375 INCH LONG CRACK IN ACCESS DOOR DOUBLER.SDR 91500001Floorbeam · corrodedMAIN DECK FLOORBEAM CORRODED AT NUT PLATES.SDR 050301Beam · crackedFORWARD CARGO COMPARTMENT, DOOR JAMB, STUB BEAM SHORT FLANGE IS CRACKED.SDR COOSDR05003Door Frame · crackedFWD CARGO COMPARTMENT, DOOR JAMB, STUB BEAM, PN 5921718-1, SHORT FLANGES CRACKED. (K)SDR 0411001Sense Line · looseDURING CLIMB ABOVE 20,000 FT, THE NR 2 ENGINE DID NOT INDICATE CLIMB THRUST (EPR).SDR Y2PA04023Ground Wire · brokenNO GEAR INDICATION ON LT MAIN GEAR, EITHER RED OR GREEN. CREW DECLARED AN EMERGENCY AND DIVERTED. CREW FOLLOWED COM PROCEDURES WITH NO HELP. LT GEAR INDICATION DOES NOT TEST (RED AND GREEN LIGHTS INOPERATIVE). AIRCRAFT LANDED WITHOUT INCIDENT. MECHANIC SESDR EIA2004042Battery · inoperativeEMERGENCY LIGHTS IN COCKPIT EXTREMELY DIM WHEN TURNED ON. REPLACED COCKPIT EMERGENCY LIGHT BATTERY PER DC9 MM 33-53-0, OPS CHECKED GOOD.SDR ROSA060704Battery Pack · inoperativeCABIN EMERGENCY LIGHTS INOP. REMOVED BATTERY PACK 60-0304-31 SN 4094, SENT TO SHOP FOR INSPECTION AND DEEP CYCLE. INSTALLED SAME, SYSTEM FUNCTION CHECKS SATISFACTORY.SDR ROSS0401Switch · intermittentUPON EXTENDING GEAR, NOSE GEAR DOWN LIGHTS DID NOT ILLUMINATE, OTHER SWITCHING STUCK IN AIR MODE. NOTE: NO NOSE UNSAFE LIGHT ILLUMINATED, AFTER LANDING TAPPED ON NOSE GEAR DOWNLOCK SWITCH LIGHTS CAME ON. REMOVED AND REPLACED SWITCH AS PER DC9 MM CH 32-60-00 SDR DM42003F00000Nut · crackedSUBJECT HORIZONTAL STABILIZER ACTUATOR: RECEIVED WITH A CRACKED NUT WITH METAL PARTICLES ON SCREW SECTION AD 200-15-15.SDR 2003F00648Door · delaminatedFOUND DURING 4C CHECK, AFT CARGO COMPARTMENT BARRIER DOOR, DAMAGED INNER AND OUTER SKIN AND HONEYCOMB CORE. DAMAGED PARTS WERE REPLACED BY NEW ONE. (M)
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