Douglas DC-9-32
Service difficulty reports · 12,755
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 = 'DC932' 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 = 'DC932' 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 AT9900170Panel · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND FLOOR PANEL AT BS 897-965 LEFT SIDE CORRODED AROUND FASTENER HOLES. REMOVED AND REPLACED FASTENERS, CLEANED CORROSION, FABRICATED REPAIR FLOOR PANEL, ALODINE, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, AND 51-10-4.SDR AT9900131Slide · looseGALLEY DOOR SLIDE CAME OUT OF BIN. RESECURED GALLEY DOOR EVACUATION SLIDE IAW MM 25-62-0.SDR 9900639985Skin · crackedDURING PERIODIC CHECK, FOUND VERTICAL STABILIZER LEADING EDGE STRUCTURE FORMER CRACKED AT FS 36, 43, 50 AND 148. FABRICATED AND INSTALLED DOUBLERS PER EA 99-162413.SDR CALA9900162Vane · corrodedINSPECTION FOUND LT WING FLAP O/B FIXED VANE I/B END LOWER SURFACE CORRODED WITH RIVETS PULLING THROUGH. THE LT O/B FLAP VANE WAS REMOVED AND REPLACED IAW MM 27-51-3.SDR AT9900221Skin · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FUSELAGE SKIN BULGE AT BS 275 L-18L. STRIPPED AREA, REMOVED FASTENERS, FOUND CORROSION. REMOVED SECTION OF SKIN ABOVE AND BELOW LONGERON 18. FABRICATED FINGER DOUBLER, FILLERS, AND EXTERNAL DOUBLERS, ALODINESDR AT9900150Light · inopFOUND THE FLOOR PATH LIGHTING ASSEMBLY MISSING AT ROW 24DEF. INSTALLED SERVICEABLE LIGHT ASSEMBLY IAW MM 33-53-01, OPS CHECKED GOOD. LENS (P/N 07912), SOCKET (P/N 08169-1).SDR AT9900188Frame · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AT CABIN FRAME BS 929 LBL 2-3L AND LBL 3R. CUT OUT CORRODED SECTIONS, INSTALLED TWO DOUBLERS, FILLERS, AND ANGLES IAW DC9 SRM 51-10-3, 51-30-2, AND 53-03 FIG 4.SDR ABXA9900154Floorbeam · corrodedDURING C-CHECK, FOUND FLOORBEAM CORRODED, UPPER 'T' CAP AT STATION 699. REPAIRED IAW ABX REA D953-26839MR.SDR ABXA9900153Frame · crackedDURING C-CHECK, FOUND RIGHT FUSELAGE FRAME STATION 658 CRACKED. REPAIRED IAW DC9 SRM 53-03.SDR ABXA9900152Longeron · crackedDURING C-CHECK, FOUND LONGERON 17 LEFT, STATION 980 CRACKED. REPLACED SEGEMENT OF LONGERON IAW DC9 SRM 53-02.SDR ABXA9900151Angle · crackedDURING C-CHECK, FOUND LEFT MAIN LANDING GEAR 'Z' ANGLE CRACKED. REPLACED 'Z' ANGLE IAW DC9 SRM 51-30-1.SDR GTIA9900921Skin · misrepairedSTATION 992 LEFT STRINGER 22-23 THERE IS A CLASS III SKIN REPAIR WITH CHERRY RIVETS INSTALLED ALSO NUMEROUS FASTENERS WITH SHORT CENTER TO CENTER SPACING. REMOVED TEMP REPAIR FABRICATED DOUBLER TRIPLER AND FILLER TRIMMED OUT ADDITIONAL AREA ALODINED AND PRIMESDR CALA9900156Blkhd Bracket · crackedINSPECTION FOUND TWO AFT CARGO FORWARD BULKHEAD SPLICE BRACKETS WITH .5 INCH CRACKS. NEW FITTINGS WERE INSTALLED IAW SRM 51-10-1 AND 51-00-00.SDR CALA9900155Support · corrodedINSPECTION FOUND FORWARD CABIN FLOOR SUPPORT TEE CHANNEL CORRODED AT STA 160, LBL 8. THE FLOOR SUPPORT T CHANNEL WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-60-0.SDR CALA9900154Wire · brokenEMERGENCY LIGHT BATTERY PACKS FAILED TEST AT LT LAV AND FORWARD ENTRY. REPAIRED BROKEN WIRES, SECURED LOOSE GROUND, AND TIGHTENED BATTERY CONTACTS. OPERATION CHECKED NORMAL IAW MM 33-50-00, PAGE 203.SDR CA990308030Transmitter · faulty(CAN) DURING TAKEOFF ROLL,THE NR 1 ENGINE EPR GAUGE JUMPED FROM TAKEOFF SETTING OF 2.07 TO 2.15, FUEL FLOW JUMPED FROM 6,000 POUNDS PER HOUR TO 8,500 POUNDS PER HOUR AND BACK AGAIN. TAKEOFF WAS REJECTED. THE ENGINE PRESSURE RATIO TRANSMITTER WAS REPLACED. THE SDR AT9900167Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND A CORRODED ANGLE BRACKET ON FORWARD LOWER CARGO DOOR. REMOVED L ANGLE BRACKET, FABRICATED NEW ANGLE, REPAIR DOUBLER AND INSTALLED IAW DC9 SRM 53-05 FIG 7 PAGE 8.SDR AT9900189Web · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND ON THE AFT PIT WEB AT BS 965 TO 985 STRINGER 28-29R CORRODED ON BOTH SIDES. FABRICATED NEW INTERCOSTAL WEB, HEAT TREATED, PRIMED, AND INSTALLED REPAIR IAW DC9 SRM 51-10-2A, 51-10-5, 51-30-8, 53-03 FIG 1, 51-30-2, SDR CALA9900151Floorbeam · chafedINSPECTION FOUND A HOLE CHAFED IN LOWER CHORD OF FORWARD CARGO COMPARTMENT FLOORBEAM AT FS 389, RBL 2. A REPAIR WAS INSTALLED IAW SRM 53-05-00, FIGURE 20A, PAGE 31.SDR CALA9900150Skin · debondedINSPECTION FOUND LT WING LOWER SKIN PANEL DEBONDED AROUND SCREW HOLE FORWARD OF OUTER WHEEL WELL AREA. THE SKIN PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2.SDR CALA9900149Panel · debondedINSPECTION FOUND THE LT WING UPPER T/E FIXED PANEL DEBONDED WITH SURFACE CORROSION ON BOTTOM, JUST I/B OF AILERON. THE PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2 AND 51-30-1.SDR CALA9900148Vane · dentedINSPECTION FOUND LT WING FLAP AFT MOVEABLE VANE DENTED AND ONE SPOT WORN THROUGH AT LOWER SURFACE NEAR I/B END. THE FLAP VANE WAS REMOVED AND REPLACED IAW MM 27-51-2.SDR 9900589601Power Supply · inopDURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL.SDR GTIA9900918Frame · crackedMHV - NO REPAIR FOUND IN THE SRM 53-00 FOR CRACK IN FRAME AT STATION 200 R16. CUT OUT DAMAGED AREA REINSTALLED WEB FABRICATED AND INSTALLED DOUBLER AND TRIPLER BOEING ENGINEERING MSQ NR AVQ-MOJ-99-0005RR AND INSTALLED FASTENERS IAW DC9 SRM 51-30-2, 51-30-5, 5SDR CALA9900141Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RT APU DOOR INNER RIB. THE RIB WAS REPAIRED IAW SRM 52-01-00, FIGURE 2 AND 51-10-3.SDR CALA9900140Tab · delaminatedINSPECTION FOUND LT ELEVATOR CONTROL TAB DELAMINATED ON UPPER SURFACE. THE LT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27-30-00 AND 27-30-3.SDR CALA9900139Fitting · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FITTING OF FORWARD ENTRY DOOR AT UPPER AFT STOP PAD AREA. THE FASTENERS AND FITTING WERE REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 52-03-00, PAGE 5. A DOUBLER WAS INSTALLED IAW SRM 52-03-00, PAGE 5, 51-10-3, AND 51-1SDR CALA9900138Support · corrodedINSPECTION FOUND FORWARD CABIN FLOOR SUPPORT T CHANNEL CORRODED BETWEEN STA 160 AND 229, BL 0. THE CHANNEL WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-60-0.SDR AT9900212Bulkhead Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE CANTED BULKHEAD LEFT HAND LOWER ATTACH BRACKETS HAVE CORROSION RUNNING UNDER THEM AT LONGERON 11 ON THE BACK OF FRAME AT BS 1180. REMOVED BRACKETS AND CORROSION, CUT OUT AREA, FABRICATED FRAME REPAIR AND DOUBLSDR AT9900199Frame · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT LEFT HAND FLOOR SUPPORT FRAME CRACKED AT BS 870. REMOVED CRACKED FRAME, REPAIR FRAME IAW DC9 EA NR 12-5321-29-C1362 AND REINSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2.SDR AT9900198Skin · dentedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND A DENT OUT OF LIMITS AT BS 195R. FABRICATED DOUBLER AND FINGER DOUBLER, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-2, AND RES NR 99443.SDR AT9900139Floorbeam · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOORBEAM AT STA 965 HAS CORROSION AND BLUE WATER STAINS ON LOWER LEG AND AROUND NUT PLATES HOLES LEFT HAND LAVATORY. MECHANICALLY REMOVED CORROSION, FABRICATED TWO DOUBLERS AND INSTALLED IAW DC9 SRM 53-05 FIGSDR AT9900114Bulb · failedDURING A B CHECK, FOUND THE TAIL CONE EMERGENCY EXIT INOPERATIVE. RELAMPED TAIL CONE EMERGENCY EXIT LIGHT IAW MM 33-53-0, OPS CHECKED NORMAL.SDR MWEA99067Girt Bar · detachedTHE GIRT BAR FELL OFF. MAINTENANCE RESECURED FORWARD ENTRANCE DOOR GIRT BAR.SDR GTIA9900917Seat Track · crackedMHV - SEAT TRACK RIGHT SIDE OUTBOARD AT STAITON 420 IS CRACKED EXTENDING .250 FROM ONE OF THE TOP SURFACE HOLES. REMOVED AND REPLACED OF SEAT TRACK FROM STATION 350 TO STATION 470 PER SRM 53-05 FIG 4F PAGE 10K. (M)SDR AT9900200Frame · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND LOWER FUSELAGE FRAME FITTING AT BS 692 CRACKED AT THE BOLT HOLE IN UPPER FLANGE IN FORWARD LOWER INBOARD CORNER OF LEFT WHEEL WELL. STOP DRILLED CRACK, VERIFY BY HFEC, FABRICATED REPAIR ANGLE, TREATESDR AT9900192Skin · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK ON SKIN LEFT HAND SIDE JUST BELOW L-14L AT BS 950. NDT MARKED ENDS OF CRACK, REMOVED CRACK, FABRICATED REPAIR DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-30-2, 53-04 FIG 3A, 51-10-3, AND RSDR AT9900169Strap · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND SIDE WALL TRIM STRAP AT BS 427 RIGHT SIDE CORRODED. MECHANICALLY REMOVED CORROSION, FABRICATED STRAP, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-3, AND 53-01 FIG 1.SDR AT9900116Skin · dentedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE LOWER RIGHT FUSELAGE SKIN FROM STA 389 TO STA 598 L-18R TO L-26R WITH DENTS IN DIFFERENT AREAS. REMOVED AND REPLACED FUSELAGE SKIN IAW DC9 SRM 51-30-2, 51-30-1, AND RES NR 99193.SDR MWEA99062Battery Pack · dischargedFOUND AFT LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED CEILING EMERGENCY BATTERY PACK.SDR GTIA9900923Floor · crackedMHV - FORWARD PASSENGER FLOOR PANEL FOR FS 200-243 LBL 21-42, CORNER CRACKED (TORN). FABRICATED FLOORBOARD IAW DC9 SRM 53-21-0 PAGE 6 INSTALLED STIFFENERS IAW DC9 SRM 51-30-2 PAGE 30. ALODINED AND PRIMED PER IAW DC9 SRM 51-10-3. INSTALLED RIVETS IAW DC9 SRMSDR GTIA9900916Web · crackedMHV - FS 211 R61 WEB AT 1.5 INCH LIGHTNING HOLE IS CRACKED AND HAS CORROSION THATS OUT OF LIMITS PER N/RW25. CUSP HAS BEEN REPLACED PER SRM 53-05-00 FIG 55 FASTENERS INSTALLATION PER SRM 51-30-2 AND SRM 51-30-5. (M)SDR AT9900215Angle · chafedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE L-1 DOOR STRIKING BEHIND MOUNT U-CHANNEL ANGLE ON AFT DOOR JAMB AT UPPER STOP BOLT. BLENDED OUT DAMAGE AREA TO HAVE MINIMUM RADIUS, TREATED TRIMMED AREA, PRIMED AND DRESSED UP IAW DC9 53-01-0, 53-11-0, AND RESDR AT9900168Floor Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND CARGO FLOOR TRACK AT BS 307-503 CORRODED. MECHANICALLY REMOVED CORROSION, REMOVED, REPLACED AND FABRICATED NEW TRACK SECTION, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 53-05 FIG 4C, ANDSDR AT9900096Slide · low pressureAFT TAIL CONE SLIDE PRESSURE IS LOW. REMOVED AND REPLACED TAIL CONE SLIDE IAW MM 25-62-1.SDR TWAA9902304Spar · crackedDURING OP 15 MAINT CHECK, FOUND RT WING WITH APPROXIMATELY .625 INCH CRACK IN REAR SPAR UPPER CAP AT UPPER INBD HOLE AT CENTER HINGE INBD ATTACH BOLT, APPROXIMATELY 10 TO 12 O'CLOCK POSITION. STOP DRILLED CRACK AND INSTALLED DOUBLER AND FILLER PER ARA 16062.SDR TWAA9902303Spar · crackedDURING OP 15 MAINT CHECK, FOUND RT WING WITH .375 INCH LONG CRACK IN REAR SPAR UPPER CAP AT UPPER OTBD HOLE AT CENTER FLAP HINGE OTBD ATTACH BOLT AT APPROX 1130 TO 1230 O'CLOCK POSITION. BLENDED AREA PER SRM 57-01, FIG 1. INSTALLED DOUBLER AND FILLER PER ARASDR GTIA9900915Skin · damagedTEMPORARY REPAIRS ON RIGHT SIDE FUSELAGE AT STATION 293 AND STATION 313. REMOVED TEMPORARY REPAIRS FROM RIGHT SIDE FUSELAGE CUT OUT SECTION OF SKIN AND FABRICATED SKIN SECTION TITANUM DOUBLER AND INSTALLED USING HI-LOCK FASTENER AND SOLID RIVETS IAW ENG DRAWISDR CALA9900121Door · out of adjustTHE LT AFT OVERWING EMERGENCY EXIT DOOR FAILED UNLOCK FORCE TEST. THE LATCH BAR SCREWS WERE ADJUSTED TO OBTAIN THE REQUIRED FORCE TO UNLOCK THE EXIT DOOR IAW MM 52-21-0, PAGE 504.SDR AT9900219Longeron · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT HAND CABIN FLOOR LONGERON 18 CUSP MEMBRANE CRACKED FORWARD OF BS 598 MAIN FRAME RBL 56. FORMED DOUBLER REPAIR, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED DOUBLER REPAIRS IAW DC9 SRM 51-10-2, 53-20
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