Douglas DC-9-41
Service difficulty reports · 2,671
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 = 'DC941' 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 = 'DC941' 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 ABXA9701056Fitting · chafedDURING D-INSPECTION, FOUND THE RIGHT WING NR 5 SLAT OUTBOARD FITTING CHAFED BEYOND LIMITS. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.SDR ABXA9701055Fitting · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING NR 1 SLAT CENTER ATTACH FITTING CORRODED. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.SDR ABXA9701054Fitting · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING NR 2 SLAT CENTER ATTACH FITTING CORRODED. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.SDR ABXA9700959Frame · crackedDURING C-CHECK, FOUND FRAME AT F/STA 1132 LONGERON 2R CRACKED. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 32.SDR ABXA9700958Intercostal · crackedDURING C-CHECK, FOUND INTERCOSTAL AND INTERCOSTAL CLIP CRACKED UNDER WALKWAY PLATFORM AT STA 1231. REPLACED INTERCOSTAL AND CLIP IAW DC9 SRM 51-30-2.SDR ABXA9700957Rib · crackedDURING C-CHECK, FOUND THE RT HORIZONTAL STAB INBOARD LEADING EDGE SECTION, INBOARD RIB CRACKED AT LOCK BOLT. REPAIRED RIB IAW DC9 SRM DRAWING NR K05159.SDR ABXA9700956Rib · crackedDURING C-CHECK, FOUND THE RT HORIZONTAL STAB OUTBOARD LEADING EDGE SECTION, 5TH RIB INBOARD FROM OUTBOARD TIP CRACKED. REPAIRED RIB IAW DC9 SRM DRAWING NR K05159.SDR ABXA9700955Rib · crackedDURING C-CHECK, FOUND THE RT HORIZONTAL STAB OUTBOARD LEADING EDGE SECTION MOST INBOARD RIB INBOARD FROM OUTBOARD TIP CRACKED. REPAIRED RIB IAW DC9 SRM DRAWING NR K05159.SDR ABXA9700954Longeron · crackedDURING C-CHECK, FOUND LONGERON 17R CRACKED AT F/STA 256. REPLACED CRACKED SECTION OF LONGERON FROM F/STA 230 TO 265 IAW DC9 SRM 53-02.SDR ABXA9700953Bellcrank · corrodedDURING C-CHECK, FOUND THE LONGITUDINAL TRIM CABLE BELLCRANK ARM (P/N 5914177-503) CORRODED. REMOVED AND REPLACED ARM IAW DC9 MM 20-10-0 AND 20-16-0.SDR ABXA9700952Flange · crackedDURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR LOWER TRAILING EDGE FLANGE BENT AND CRACKED. REPAIRED FLANGE IAW DC9 SRM 52-05.SDR 9708469763Release Mech · out of adjustDURING TAILCONE FUNCTIONAL CHECK, FOUND THE TAIL CONE DID NOT DROP AND EXCESSIVE FORCE WAS REQUIRED TO REMOVE HANDLE FROM CLIPS. ALSO, FOUND THE UPPER TWO GUIDE PIN BEARING PLATES ON THE TAIL CONE WORN AND NIINE GUIDE PINS WORN. CLEANED SEAL, REPLACED BEARINSDR ABXA9700951Tr Door · crackedDURING C-CHECK, FOUND THE UPPER THRUST REVERSER DOOR INBOARD EXTERIOR FLANGE CRACKED. REPLACED FLANGE IAW DC9 SRM 51-10-4, 51-30-2 AND 51-30-8.SDR ABXA9700950Tr Door · crackedDURING C-CHECK, FOUND THE UPPER THRUST REVERSER DOOR OUTBOARD EXTERIOR FLANGE CRACKED. REPLACED FLANGE IAW DC9 SRM 51-10-4, 51-30-2 AND 51-30-8.SDR ABXA9700949Tr Door · crackedDURING C-CHECK, FOUND THE LOWER THRUST REVERSER DOOR OUTBOARD EXTERIOR FLANGE CRACKED. REPLACED FLANGE IAW DC9 SRM 51-10-4, 51-30-2 AND 51-30-8.SDR ABXA9700948Bracket · chafedDURING C-CHECK, FOUND THE RIGHT WING INBOARD SPOILER PULLEY BRACKET CHAFED BEYOND LIMITS. REPLACED PULLEY BRACKET IAW DC9 SRM 51-30-1.SDR ABXA9700947Angle · brokenDURING C-CHECK, FOUND THE NR 2 PYLON INTERIOR CANTED WEB LOWER ANGLE BROKEN OFF AT FORWARD CORNER IN ACCESS AREA 8206A. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-8.SDR ABXA9700946Fitting · crackedDURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR HORIZONTAL BEAM NR 5 FORWARD END FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXA9700945Fitting · crackedDURING C-CHECK, FOUND THE FLOOR SUPPORT FITTING AT F/STA 718 AND RBL 44 CRACKED AT LOWER END. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXA9700944Cusp Web · corrodedDURING C-CHECK, FOUND THE CUSP WEB BETWEEN F/STA 237 TO 256 LT SIDE CORRODED. REPLACED CORRODED SECTION OF CUSP WEB IAW ABX REA D953-19274-MR.SDR ABXA9700943Doubler · corrodedDURING C-CHECK, FOUND THE RT KIDNEY PANEL NR 5114A AFT ATTACH FLANGE DOUBLER CORRODED. TRIMMED OUT CORRODED SECTION OF DOUBLER AND REPAIRED IAW ABX REA D953-19275.SDR ABXA9700942Frame · corrodedDURING C-CHECK, FOUND THE FRAME AT F/STA 1072 CORRODED BETWEEN LONGERONS 17R AND 18R. REMOVED CORROSION AND REPAIRED IAW ABX REA D953-19271-MR AND REA D953-19275.SDR TWAA9753001Pump · failedSTL - FLT 563 - DURING CRUISE LOST RIGHT HYDRAULIC PRESSURE DUE TO WORN RIGHT ENGINE DRIVEN HYDRAULIC PUMP, MFG P/N 314195, MANUFACTURED BY VICKERS INC. OPERATIONAL CHECK NORMAL. (M)SDR ABXA9700937De-Ice Duct · blownLOOP 'B' FAILED, SELECTED 'A', TESTED, GOT FIRE INDICATION. SHUT DOWN THE RIGHT ENGINE, FIRE LIGHT WENT OUT WITH THROTTLE IN IDLE. REPLACED BLOWN DE-ICE DUCT IAW DC-9 MM.SDR ABXA9701067Panel · delaminatedDURING D-INSPECTION, FOUND THE RIGHT WING LOWER BONDED TRAILING EDGE PANEL INBOARD OF MLG ATTACH FITTING DELAMINATED. REPLACED BONDED PANEL IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.SDR ABXA9701068Arm · crackedDURING D-INSPECTION, FOUND THE FIRST OFFICERS RIGHT RUDDER PEDAL ARM CRACKED AT OUTBOARD ATTACH HOLD. REPLACED RIGHT RUDDER PEDAL ARM IAW DC9 MAINTENANCE MANUAL CHAPTER 20-16-0.SDR ABXA9700905Seat Track · dirtyFIRST OFFICERS SEAT WON'T LOCK IN THE FULL FORWARD POSITION. CLEANED DEBRIS OUT OF THE FORWARD INBOARD SEAT TRACK. THE FIRST OFFICERS SEAT OPS CHECK GOOD.SDR TWAA9753004Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A .25 INCH CRACK IN LONGERON 4L, AT BELTRING STATION. INSTALLED REPAIR PER SRM 53-02, FIGURE 2. (M)SDR 9708239752Batteries · dischargedDURING LINE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LEFT SIDE WILL NOT ILLUMINATE. REPLACED BATTERIES, OPERATIONAL CHECK OK.SDR ABXA9701069Jamb · corrodedDURING D-INSPECTION, FOUND THE WEB AROUND THE AFT BAG BIN DOOR JAMB CORRODED. REMOVED AND REPLACED WEB IAW DC-9 SRM CHAPTER 51-30-2.SDR 9707429753Clips · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE INTERNAL TAIL CONE RELEASE HANDLE FROM RETAINING CLIPS. ADJUSTED CLIPS, OPERATIONAL CHECK OK.SDR ABXA9701072Bracket · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING TIP REAR SPAR ATTACH BRACKET CORRODED. REMOVED AND REPLACED WING TIP ATTACH BRACKET IAW DC-9 SRM 51-30-1.SDR ABXA9701071Bracket · corrodedDURING D-INSPECTION, FOUND THE LEFT WING TIP REAR SPAR ATTACH BRACKET CORRODED. REPLACED BRACKET IAW DC-9 SRM CHAPTER 51-30-5.SDR ABXA9701070Panel · delaminatedDURING D-INSPECTION, FOUND THE RIGHT WING UPPER TRAILING EDGE BONDED PANEL INBOARD OF THE MLG ATTACH FITTING DELAMINATED. REMOVED AND REPLACED PANEL ASSY IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9701051Panel · corrodedDURING D-INSPECTION, FOUND THE LEFT WING UPPER TRAILING EDGE PANEL BETWEEN STATIONS XRS 69 AND XRS 111 CORRODED AND DELAMINATED. REMOVED AND REPLACED BONDED PANEL IAW DC9 SRM CHAPTERS 51-30-1.SDR ABXA9700751Blkhd Stiffener · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT LONGERON 14R. REPLACED STIFFENER IAW DC9 SRM 51-30-5.SDR ABXA9700750Blkhd Stiffener · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT LONGERON 15R AND 16R. REPLACED STIFFENER IAW DC9 SRM 51-30-5.SDR ABXA9701050Fitting · corrodedDURING D-INSPECTION, FOUND THE RIGHT MAIN LANDING GEAR ATTACH FITTING CORRODED ON FORWARD AND AFT SIDES OF THE FIXED SIDE BRACE LUG. REPAIRED IAW ABX REA D932-18677-MR.SDR ABXA9701049Fitting · corrodedDURING D-INSPECTION, FOUND THE LEFT MAIN LANDING GEAR ATTACH FITTING CORRODED ON THE FORWARD AND AFT SIDES OF THE FIXED BRACE ATTACH LUG. REPAIRED IAW ABX REA D932-18677-MR.SDR ABXA9701048Fitting · corrodedDURING D-INSPECTION, FOUND LEFT MAIN LANDING GEAR ATTACH FITTING CORRODED IN POCKET AT INBOARD END OF AUX SPAR LOWER FITTING. REPAIRED IAW ABX REA D957-18899-MR.SDR 9707779753Downlock Switch · failedUPON LANDING, GEAR EXTENSION FOR LANDING AT DTW, NOSE WHEEL LIGHT DID NOT SHOW GREEN. RECYCLED GEAR AND GOT ALL NORMAL INDICATION. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE SWUNG GEAR BUT COULD NOT DUPLICATE PROBLEM. REPLACED NOSE GEAR DOWNLOCK SWITCH. SDR ABXA9700546Prox Box · defectiveGEAR DOOR OPEN LIGHT CAME ON DURING CLIMB-OUT. STAYED ON FOR REMAINDER OF FLIGHT. PULLED MLG EMERGENCY EXTEND HANDLE FOR LANDING. AFTER ROLL-OUT, MLG DOOR WAS OPEN. REPRESSURIZED SYSTEM AND DOOR RETRACTED, BUT LIGHT STAYED ON. REPLACED LANDING GEAR PROXISDR ABXA9701077Jamb · corrodedDURING D-INSPECTION, FOUND THE LEFT SIDE OF THE VENTRAL STAIR JAMB HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED AFT JAMB WEB AND CAP IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.SDR ABXA9701076Angle · corrodedDURING D-INSPECTION, FOUND THE LOWER KEEL ATTACH ANGLE CORRODED SEVERAL PLACES FROM FS 642 TO FS 729. REPLACED LOWER KEEL ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-5.SDR ABXA9701075Former · crackedDURING D-INSPECTION, FOUND THE FRAME CLIP AT FS 660 IN THE LEFT LOWER KEEL CRACKED AT CANTED KEEL. REPLACED FRAME AT FS 660 IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9701074Bulkhead Fitting · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR FRAME ATTACH FITTING CRACKED JUST ABOVE STIFFENER AT Z14R BETWEEN LONGERONS 16 AND 17 RIGHT. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9701073Bulkhead Fitting · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR FRAME ATTACH FITTING CRACKED JUST ABOVE STIFFENER Z34 RIGHT AT LONGERON 14 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-2.SDR ABXA9701047Bulkhead Web · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LEFT HAND DOUBLER HAD A BEND RADIUS CRACK. REPAIRED IAW ABX REA D953-18897-MR.SDR GTIA9700270Hydraulic Pump · failedACY - FLT 304 - RUDDER CONTROL MANUAL ANNUNCIATOR LIGHT CAME ON IN FLIGHT. SWITCHED TO MANUAL. PROBLEM CONTRIBUTED TO RIGHT HYD PUMP FAILURE, OPS CHECKED GOOD PER MM 27-20-8 USING AUX HYD PUMP. (M)SDR GTIA9700268Connectors · dirtyBOS - FLT 248 - LEG 3, TAKEOFF PLUS 5 MINUTES RUDDER CONTROL MANUAL LIGHT CAME ON. NO FLUID LOSS OR FLIGHT CONTROL CHANGE. INSPECTED RUDDER POWER PACK UNIT AND CONTROL SYSTEM. REMOVED ELECTRICAL CONNECTORS, CLEANED TERMINALS, THE RE-INSTALLED. OPERATE RUDD
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