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 EIAA97221Floor Beam · corrodedMZJ - DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE LOWER T-CHORD OF THE FLOOR BEAM AT BS 642. REPAIRED BY FABRICATING AND INSTALLING A REPAIR T-CHORD, RESTORED AREA FINISH IAW EVERGREEN INTERNATIONAL AIRLINES ECRA 915-53-017-2. (X)SDR GAIA9751Latch Mechanism · out of adjustKHA - FLT 423 - ELP TO YPI - AFTER TAKEOFF, THE 'GEAR DOOR OPEN' LIGHT ILLUMINATED WHEN THE GEAR UPLATCH CHECK WAS PERFORMED. THE CREW PUT THE GEAR HANDLE UP AND PERFORMED ANOTHER UPLATCH CHECK AND THE LIGHT STAYED OUT. AN UNEVENTFUL LANDING WAS MADE AT YIP.SDR GAIA9736AFrame · crackedDURING B-CHECK INSPECTION FOR AD 73-09-02, A CRACK WAS DISCOVERED ON THE RIGHT FUSELAGE FRAME AT STA 544 JUST BELOW THE FLOOR LINE. THE AIRCRAFT WAS FERRIED TO DFW FOR REPAIR. THE FRAME WAS REPAIRED PER DC-9 SB 53-117. THE AIRCRAFT WAS RETURNED TO SERVICE. SDR GAIA9736Frame · crackedDURING 'B' CHECK INSPECTION FOR AD 73-09-02 A CRACK WAS DISCOVERED ON THE RIGHT FUSELAGE FRAME AT STATION 544 JUST BELOW THE FLOOR LINE. THE AIRCRAFT WAS FERRIED TO DFW FOR REPAIR. (M)SDR GAIA9734Switch · out of adjustKHA - FLT 564 - FNT-YIP - ON APPROACH TO YIP, AFTER EXTENDING THE LANDING GEAR THE FLIGHT CREW NOTICED THAT THE LANDING GEAR DOOR WARNING LIGHT STAYED ON LONGER THAN NORMAL. THE LANDING GEAR WAS RECYCLED ONCE TO EXTINGUISH THE LIGHT. A UNEVENTFUL LANDING WASSDR GAIA9733Connector · wornKHA - FLT 562, SUS TO DFW - ON APPROACH TO DFW AFTER EXTENDING THE LANDING GEAR, THE LEFT MAIN GEAR RED LIGHT DID NOT GO OUT, ALL DOWN AND LOCKED GREEN LIGHTS CAME ON. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED BARE WIRES AND WATER INSIDE THE LEFT MSDR 97ZZZX2604Hinge · crackedDURING C7 INSPECTION, THE LARGE CARGO DOOR HINGE WAS FOUND WITH A CRACKED HINGE LOBE AT BS 382. EDDIE CURRENT INSPECTION REVEALED CRACKS HAD DEVELOPED ADJACENT TO THE ORIGINAL DISCREPANCY. THE ACFT REMOVED FROM SERVICE FOR REPAIR.SDR EIAA970091Pt2 Probe · pluggedABQ - WHEN TAKEOFF POWER WAS SET, LEFT ENGINE THROTTLE WAS ONE AND ONE-HALF KNOBS BEHIND RIGHT ENGINE THROTTLE. ENGINE REDINGS WERE: LEFT ENGINE EPR 1.97, N1 84 PERCENT, EGT 440, N2 89 PERCENT, F/F 5300 POUNDS. RIGHT ENGINE EPR 1.99, N1 92.5 PERCENT, EGT 51SDR 97ZZZX2603Hinge · crackedDURING C7 INSPECTION, THE LARGE CARGO DOOR HINGE WAS FOUND WITH A CRACKED HINGE LOBE AT STA 358. THE HINGE LOBE WAS TRIMMED OFF AND RECURRENT INSPECTIONS WERE ESTABLISHED FOR THIS AREA. AT THE SUBSEQUENT A-CHECK, ADDITIONAL CRACKS WERE FOUND IN THE HINGE LOBESDR 97ZZZX2092Line Assy · chafedRUDDER TRAVEL UNRESTRICTED LIGHT CAME ON IN CRUISE FLIGHT. FOUND VERTICAL STABILIZER PITOT STATIC LINE CHAFED THROUGH AND LEAKING AT BULKHEAD. WHEN REMOVING SAME LINE FROM ANOTHER AIRCRAFT IN HEAVY CHECK, FOUND LINE CHAFED IN THE SAME PLACE. (N NR 196US). SSDR 97ZZZX2122Control Cable · corrodedDURING ROUTINE SERVICE CHECK, FOUND LEFT FLAP BUS CABLE BROKEN.SDR 97ZZZX2121Gasket · damagedDURING CRUISE, AFT LAVATORY WATER HEATER GASKET FAILED ALLOWING WATER TO LEAK INTO THE LAVATORY WASHSTAND AREA. WATER RAN THROUGH THE LAVATORY FLOOR SEAMS AND DOWN ONTO THE RIGHT ENGINE THRUST REVERSER CONTROL VALVE DRUM AND FROZE. WHEN THE AIRCRAFT ATTEMPTESDR 97ZZZX2091Line Assy · chafedRUDDER TRAVEL UNRESTRICTED LIGHT CAME ON IN CRUISE FLIGHT. FOUND VERTICAL STABILIZER PITOT STATIC LINE CHAFED THROUGH AND LEAKING AT BULKHEAD. WHEN REMOVING SAME LINE FROM ANOTHER AIRCRAFT IN HEAVY CHECK, FOUND LINE CHAFED IN THE SAME PLACE. (N NR 196US). SSDR GAIA9648Door Switch · failedKHA - FLT 490 - CVG-ROC - WHILE IN CRUISE THE 'GEAR DOOR OPEN' LIGHT ILLUMINATED CREW PROCEEDED TO ROC AND USED ALTERNATE GEAR EXTENSION PROCEDURES. DUE TO THE USEOF ALTERNATE GEAR EXTENSION PROCEDURES THE MAIN GEAR DOORS DRAGGED ON THE GRUOND CAUSING MINOR DSDR Y2PA96104Retract Mech · froze upYIP - LANDING GEAR HANDLE FROZEN IN THE 'UP' POSITION. AFTER MISSED APPROACH, GEAR HANDLE OPERATED NORMALLY. INSPECTED AND FOUND ICE AND STANDING WATER IN BOTH MAIN GEAR WHEEL WELLS AND GEAR CONTROL VALVE AREA. REMOVED WATER AND ICE FROM BOTH WHEEL WELL ARESDR Y2PA96102Window · failedIND - FLT 23340 - DURING CRUISE, FL 350, THE OUTER PANE OF THE FLIGHT DECK FIRST OFFICER'S MAIN WINDOW CRACKED. THE COMPANY OPERATION MANUAL PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED AT ITS ARRIVAL LOCATION (IND) WITHOUT INCIDENT. A MECHANIC WAS SENT FSDR EIAA96103Skin · corrodedDURING C-CHECK INSPECTION, DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE SKIN AT BS 642, LONGERON 30, BL 0.0. AFFECTED AREA WAS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FINGER DOUBLERS AND EXTERNAL REPAIR DOUBLERS WET WITH SEALANT AND TOP COATSDR 97ZZZM180Skin · corrodedDURNG C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, BL 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 IN WIDTH. AFFECTED AREA WAS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FISDR 97ZZZM179Skin · corrodedDURING C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, BL 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 INCH IN WIDTH. AFFECTED AREA WS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNSDR GAIA9639Fitting · crackedDURING C-CHECK, INSPECTION REVEALED SEVENTEEN CRACKED STRUT FRAME ATTACH FITTINGS IN THE LOWER FUSELAGE CARGO COMPARTMENTS. CLOSER INSPECTION REVEALED THE CRACKS TO BE STRESS CORROSION CRACKS ALONG GRAIN LINES. EIGHT FRAMES WERE REPLACED IAW DOUGLAS SRM AND SDR GAIA9638Floor Beam · corrodedDURING C-CHECK, INSPECTION REVEALED CORROSION ON FUSELAGE FLOOR BEAM AT STA 642. REPAIRED FLOOR BEAM IAW KITTY HAWK EA D9-53-037. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR GAIA9637Splice · crackedDURING C-CHECK, INSPECTION REVEALED A CRACKED SEAT TRACK SPLICE AT STA 474. REPLACED SPLICE IAW DOUGLAS SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR GAIA9636Longeron · crackedDURING C-CHECK INSPECTION, REVEALED TWO CRACKS ON LONGERON 30 BY THE PRODUCTION SPLICE AT FUSELAGE STATION 360. REPAIRED LONGERON IAW KITTY HAWK EA D9-35-040. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR ABXA9700304Web · cut outDURING C-CHECK, FOUND A CUTOUT ON LEFT CUSP WEB BETWEEN STA 237-256. REPAIRED IAW ABX READ953-17208-MR.SDR ABXA9700309Frame · misdrilledDURING C-CHECK, FOUND FRAME STA 642 HAD A MISDRILLED HOLE. REPAIRED IAW REA D953-17177-MR.SDR ABXA9700308Vane · delaminatedDURING C-CHECK, FOUND RIGHT FLAP INBOARD FIXED VANE DELAMINATED (AD 92-22-08). REPLACED IAW DC-9 M/M 27-51-3.SDR EIAA9680Skin · corrodedMZJ - EXFOLIATION CORROSION WAS FOUND ON THE LOWER FUSELAGE EXTERNAL SKIIN AT BS 642, LONGERON 30, AND BL 0.000. CORRODED AREA MEASURES 5.25 INCH LONG AND 4.90 INCH WIDTH. TWO EXTERNAL FINGER REPAIR DOUBLERS FABRICATED AND INSTALLED ON TRIMMED OUT AREA. AN SDR Y2PA96088Skin · cannedYIP - LEFT TAIL SECTION SKIN 'OIL CANNED'. SKIN IS IN THE AREA ADJACENT TO THE AFT AIR STAIRS. SKIN PANEL IS IN AN 'UNPRESSURIZED AREA'. REPLACED SKIN PANEL. (M)SDR Y2PA96087Frame · crackedYIP - LEFT MAIN FRAME CRACKED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED MAIN FRAME. (M)SDR Y2PA96086Skin · corrodedYIP - SMALL AREA OF CORROSION NOTED ON THE FORWARD FUSELAGE SKIN, BELOW THE FORWARD BAGGAGE COMPARTMENT OPENING. REMOVAL OF INITIAL CORROSION REVEALED MORE EXTENSIVE (LEVEL 2) AREAS OF CORROSION. REMOVED CORROSION, CLEANED AND TREATED AREA. FABRICATED AND ISDR Y2PA960073Skin · damagedDURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND FWD AIRSTAIRS DOOR HAD DAMAGE AT INSIDE EDGE. REPAIRED FWD AIRSTAIR DOOR IAW AIA 8110-3 AND DRAWING AIA/E/2251. HIDDEN DAMAGE REPORT NR AIA 6015. NON-ROUTINE WORK CARD NR 96-0203. REPORT GENERATSDR Y2PA960072Longeron · corrodedDURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND STATION 229 TO 280 LONGERON 28R CORRODED. REMOVED AND REPLACED LONGERON 28R STATION 229 TO 280 IAW DC9 SRM 51-01 AND 51-30-5. NON-ROUTINE WORK CARD NR 96-0196 AND 96-0249. REPORT GENERATED BY AMESDR Y2PA960071Longeron · crackedDURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND 6 INCH CRACK IN LONGERON 30 STATION 360 TO 366. REMOVED AND REPLACED LONGERON 30 STATION 360 TO 366 IAW DC9 SRM 51-01 AND 51-30-5. NON-ROUTINE WORK CARD NR 96-0196 AND 96-0264. REPORT GENERATED BSDR Y2PA960070Skin · corrodedDURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND CORROSION ON FORWARD BELLY SKIN STATION 237 TO STATION 475. REMOVED AND REPLACED FORWARD BELLY SKIN STATION 237 TO STATION 475 IAW DC9 SRM 51-01 AND 51-30-2. HIDDEN DAMAGE REPORT NR AIA 6015 AND NSDR Y2PA96067Epr Line · puncturedELP - FLT 18920 - LEFT ENGINE 'EPR' LOWER THAN RIGHT ENGINE IN CRUISE. CORRECTIVE ACTION: FOUND SMALL HOLE IN LEFT ENGINE PT7 EPR LINE. REPLACED PT7 LINE. (X)SDR Y2PA96048Door Switch · failedLRD - GEAR DOOR OPEN LIGHT REMAINING ON IN FLIGHT AFTER PERFORMING UPLATCH CHECK. REPLACED RIGHT MAIN GEAR DOOR SWITCH, AND ADJUSTED DOOR STOP BOLT ON GEAR DOOR IAW DC9 MM 32-70-0, 32-31-4. GEAR CYCLED AND CHECKED OK. (M)SDR Y2PA96062Vhf Comm 1 · failedYIP - NR 1 COMM INOP (INTERMITTENTLY) AND NR 2 COMM INOP (INTERMITTENTLY). AIRCRAFT DIVERTED INTO YIP. NO EMERGENCY PROCEDURES NECESSARY. MAINTENANCE WAS NOT ABLE TO DUPLICATE THE PROBLEM ON EITHER COMM. BOTH COMM'S WERE REPLACED AND BOTH SYSTEMS CHECKED SDR Y2PA96060Oil Qty Transm · malfunctionedYIP - UNSCHEDULED LANDING MADE, OIL QTY WENT TO ZERO AND LOW OIL PRESSURE LIGHT FLICKERED. THE OIL PRESSURE REMAINED NORMAL ACCORDING TO THE PRESSURE INDICATOR. REPLACED THE OIL QTY TRANSMITTER AND REPLACED THE OIL PRESSURE SWITCH. ENGINE OPERATED AND CHECKSDR 96ZZZM1268Oil Press Sw · malfunctionedYIP - UNSCHEDULED LANDING MADE, OIL QTY WENT TO ZERO AND LOW OIL PRESSURE LIGHT FLICKERED. THE OIL PRESSURE REMAINED NORMAL ACCORDING TO THE PRESSURE INDICATOR. REPLACED THE OIL QTY TRANSMITTER AND REPLACED THE OIL PRESSURE SWITCH. ENGINE OPERATED AND CHECKSDR 96ZZZM1267Vhf Comm 2 · failedYIP - NR 1 COMM INOP (INTERMITTENTLY) AND NR 2 COMM INOP (INTERMITTENTLY). AIRCRAFT DIVERTED INTO YIP. NO EMERGENCY PROCEDURES NECESSARY. MAINTENANCE WAS NOT ABLE TO DUPLICATE THE PROBLEM ON EITHER COMM. BOTH COMM'S WERE REPLACED AND BOTH SYSTEMS CHECKED GSDR Y2PA96059Door Skin · corrodedDURING C/D BRIDGING CHECK, FOUND DOOR CORRODED. INSTALLED REPAIR DOUBLER TO FWD AIRSTAIR DOOR PER ENGR DWG AIA/E/2252. REPAIRED AIRSTAIR DOOR PER ENGR DWG AIA/E/2252 COVERED BY AIA 8110-3, N/R CARD 96-0330.SDR Y2PA96058Attach Support · crackedDURING C/D BRIDGING CHECK, FOUND CARGO DOOR FWD ACTUATOR SUPPORT PLATE HAS CRACK UNDER IT ON FUSELAGE SUB STRUCTURE. REPAIRED CARGO DOOR FWD ACTUATOR SUPPORT PLATE IAW EA NR 53-96156 DATED 7-17-96 AND IAW DC-9 SRM, INTERIM REPAIR TILL NEXT C-CHECK OR 2500 HR SDR Y2PA96057Skin · dentedDURING C/D BRIDGING CHECK, FOUND DENT IN FUSELAGE SKIN AT STA 405 STRINGER L-19 LT, 4 BY 3.5 BY .035. REPAIRED DENTS IN FUSELAGE SKIN IAW EA NR 53-96154 DATED 7-11-96, N/R CARD 96-0265.SDR Y2PA96056Door Frame · puncturedDURING C/D BRIDGING CHECK, FOUND PUNCTURE IN LOWER AFT A PIT DOOR FRAME. REPAIRED LOWER AFT DOOR FRAME IAW EA NR 53-96155 FLIGHT VEHICLES, INC N/R CARD 96-0257.SDR Y2PA96055Skin · crackedDURING C/D BRIDGING CHECK, FOUND CRACK IN FUSELAGE SKIN LT SIDE STATION 365 JUST BELOW CARGO DOOR. REMOVED DAMAGED SECTION OF FUSELAGE SKIN AND INSTALLED EXTERNAL REPAIR DOUBLERS AS SHOWN IN FIG 1 OF THIS EA NR 53-96154. N/R CARD 96-0267.SDR Y2PA96054Skin · dentedDURING C/D BRIDGING CHECK, FOUND DENT IN FUSELAGE SKIN AT STATION 392 BETWEEN L20 TO 21 LT 3 BY 3 BY.120. INSTALLED DOUBLER REPAIR IAW DC-9 SRM 53-04 FIG 38. N/R CARD 96-0264.SDR Y2PA96053Burner Can · crackedYIP - FLT 17790 - NR 2 ENGINE TAKES 5 SECONDS LONGER THAN NR 1 ENGINE TO SPOOL UP AND RUNS 50 DEGREES HOTTER THAN NR 1 ENGINE. ALL READINGS WITHIN LIMITS; HOWEVER, ENGINE CONDITION MONITORING SHOW ERRATIC EGT INDICATIONS. PERFORMED BORESCOPE INSPECTION OF NRSDR Y2PA96045Actuator · failedYIP - WITH GEAR RAISED AFTER TAKEOFF RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT CAME ON, GEAR WAS CYCLED AND LIGHTS REMAINED ON. REMOVED AND REPLACED RT MLG ACTUATOR. FOUND LOOSE RIGHT GEAR DOOR SWITCH, TIGHTENED MOUNTING BOLTS. OPS CHECK GOOD. (M)SDR Y2PA96044Retract Mech · out of adjustGEAR DOOR OPEN LIGHT STAYED ON WITH GEAR DOWN AND LOCKED, FOLLOWED EMERGENCY PROCEDURE 2-32-6. AIRCRAFT FERRIED TO DFW FOR MX BOTH MAIN LANDING GEAR DOORS SCUFFED ON LANDING. ADJUSTED LANDING GEAR PUSH/PULL CABLES, CHECKED DOOR LATCH MECHANISM CLEARANCES. PSDR GAIA9620Skin · dentedDURING C-CHECK INSPECTION, REVEALED SEVERAL DENTS ON THE FUSELAGE SKIN FROM STATION 220 TO 313, BETWEEN LONGERON 23 AND 27 RIGHT. REPAIRED FUSELAGE SKIN IAW KITTY HAWK EA D9-53-022. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
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