Douglas DC-9-33F

Service difficulty reports · 1,681

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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 = 'DC933F'
  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.

SDR ABXA040161Attach Fitting · brokenATTACH FITTING AND ANGLE AFT SIDE OF FRAME 1087 AT 12:30 POSITION, BROKEN. REPLACED IAW DC-9 SRM 51-30-1, 51-30-5 AND 51-30-2.Apr 16, 2004 · N932AX · Doug DC933F · Fuselage Main, Attach FittingsSDR ABXA040160Seat Track · corrodedSEAT TRACK UPPER INBOARD FLANGE CORRODED AROUND FASTENER HOLES AT FS 908 - 945, RBL 44 AND FLANGE CRACKED AT FS 945. REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1 AND 53-05.Apr 16, 2004 · N932AX · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA040159Shear Tie · crackedSHEAR TIE CRACKED FS 965 AT LONGERON 16 LEFT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.Apr 15, 2004 · N932AX · Doug DC933F · Fuselage Main, StructureSDR ABXA040158Attach Angle · crackedLEFT VERTICAL STABILIZER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DC-9 SRM.Apr 15, 2004 · N932AX · Doug DC933F · Vertical Stabilizer Miscellaneous StructureSDR ABXA040157Clip · crackedWING LEADING EDGE SPLICE ANGLE AND DOUBLER CRACKED JUST OUTBOARD OF NR 6 SLAT TRACK. REPLACED ANGLE / DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-5.Apr 14, 2004 · N932AX · Doug DC933F · Leading Edge DevicesSDR ABXA040112Switch · malfunctionedAFTER GEAR HANDLE SELECTED DOWN, NOSE GEAR LIGHT DID NOT ILLUMINATE. RECYCLED GEAR WITH SAME RESULT. CHECKED GEAR DOWN VISUAL (PEEP HOLE) AND NOSE LIGHT ILLUMINATED AT 500 FT AGL ON FINAL. FOUND WIRING HARNESS KINKED BEHIND DOWNLOCK SWITCH CANNON PLUG. RE-Mar 23, 2004 · N934AX · Doug DC933F · Landing Gear Position and WarningSDR ABXA040049Web · crackedCUSP WEB AT FS 887, LEFT BUTT LINE 46 WAS CRACKED. REPAIRED AREA IAW DC-9 SRM 53-01.Jan 16, 2004 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA040048Frame · crackedFRAME 1076 CRACKED AT LONGERON 3 LT. REPAIRED IAW DC-9 SRM 53-03.Jan 15, 2004 · N931AX · Doug DC933F · Fuselage Main, FrameSDR ABXA040047Rib · crackedLEADING EDGE ASSEMBLY RIB WAS CRACKED. REPAIRED IAW DC-9 SRM K05159.Jan 15, 2004 · N931AX · Doug DC933F · Nacelle/Pylon, Frame/Spar/RibSDR ABXA040028Frame · crackedCRACKED FRAME AT LONGERON 2 LT, STA. 1076. REPLACED SECTION OF FRAME BETWEEN LONGERON 3 LT AND 3 RT IAW DC-9 SRM 51-30-5.Dec 30, 2003 · N930AX · Doug DC933F · Fuselage Main, FrameSDR ABXA040027Frame · crackedCRACKED FRAME AT LONGERON 2 RT, STA. 1076. REPLACED SECTION OF FRAME BETWEEN 3 LT AND 3 RT IAW SRM 51-30-5.Dec 30, 2003 · N930AX · Doug DC933F · Fuselage Main, FrameSDR ABXA040026Web · crackedCUSP WEB CRACKED AT FS 310 ABOVE LONGERON 20 LT. REPAIRED AREA IAW SRM 53-01.Dec 30, 2003 · N930AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA040025Skin · corrodedSKIN AT FS 610 BETWEEN LONGERON 28 LT AND LONGERON 28 RT WAS SEVERLY CORRODED, EXFOLIATED AND BULGED. CUT OUT CORROSION AREA OF SKIN, INSTALLED REPAIR DOUBLER / FILLER IAW SRM 53-01.Dec 29, 2003 · N930AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA040024Jackscrew · corrodedJACKSCREW THREADS HAD AREAS WHICH WERE PITTED. REMOVED AND REPLACED HORIZONTAL JACKSCREW IAW DC-9 MM 27-40-01.Dec 26, 2003 · N930AX · Doug DC933F · Stabilizer Control SystemSDR EIA2003169Smoke Goggles · tornSECONDARY OBSERVERS SMOKE GOGGLES FOUND ON INSPECTION TO BE TORN AND UNUSABLE. DMI NR 673 ISSUED IAW MEL 25-10-2 WITH PLACARD INSTALLED. CAT D DUE 4/08/04 2359Z. DMI CLEARED 12/9/03 AND PLACARD REMOVED ON SUBSEQUENT STOP IN SEA.Dec 8, 2003 · N944F · Doug DC933F · Emergency EquipmentSDR EIA2003110Light · weakPORTABLE EMERGENCY EXIT LIGHT JUST INSIDE OF L-1 DOOR INOPERATIVE. REMOVED AND REPLACED PORTABLE EXIT LIGHT IAW DC9 MM 20-50-0 OPS CHECKED GOOD.Aug 26, 2003 · N944F · Doug DC933F · Emergency LightingSDR ABXA030316Seat Track · corrodedSEAT TRACK RIGHT BUTT LINE 34 LOWER INBOARD LEG WAS CORRODED. REPLACED SECTION OF TRACK STA 917 - 931 LEFT BUTT LINE 34 IAW DC-9 SRM 51-30-1.Jul 17, 2003 · N935AX · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA030315Pan · corrodedAREA BETWEEN AFT LOWER CARGO JAMB PAN AND FUSELAGE SKIN EXFOLIATED. LEVEL I BETWEEN FS 904 AND 917. SPLICED IN NEW SECTION OF PAN IAW DC-9 SRM 53-05.Jul 16, 2003 · N935AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA030314Skin · corrodedLEVEL II CORROSION, BULGING SKIN, CUPPED AND BROKEN FASTENERS FLAP LOWER SURFACE AT NR 3 EXPANSION JOINT. REPLACED LOWER SKIN ON RIGHT LOWER NR 3 FLAP SEGMENT IAW DC-9 SRM 51-30-2.Jul 16, 2003 · N935AX · Doug DC933F · Trailing Edge FlapsSDR ABXA030313Attach Fitting · crackedFLOORBEAM TO KEEL ATTACH FITTING CRACKED AFT SIDE AT FS 718. REPLACED FITTING IAW REA D953-47908.Jul 15, 2003 · N935AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA030233Intercostal · crackedFORWARD LOWER CARGO DOOR LOWER AFT STOP FITTING INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2.Jun 10, 2003 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA030232Angle · crackedTWO ANGLES CRACKED (UPPER AND LOWER) IN LEFT PYLON, UNDER PANEL 8111. REPLACED ANGLES IAW SRM 51-30-2 AND 51-30-1.Jun 3, 2003 · N933AX · Doug DC933F · Nacelle/Pylon Miscellaneous StructureSDR ABXA030142Wire · burnedRIGHT AUXILIARY HYDRAULIC PUMP POWER WIRES BURNED THROUGH. REMOVED AND REPLACED THE RIGHT AUXILIARY PUMP. OPS CHECKED GOOD IAW DC-9 AMM 29-10-06-2-0001.May 10, 2003 · N933AX · Doug DC933F · Hydraulic Power System WiringSDR ABXA030162Skin · delaminatedLARGE AREA OF DELAMINATION ON UPPER AND LOWER SURFACE OF THE RIGHT WING INBOARD SPOILER PANEL. REPLACED SPOILER IAW DC-9 MM 27-61-01-4-0001.Apr 21, 2003 · N934AX · Doug DC933F · SpoilersSDR ABXA030121Lock · brokenDURING PRE "D" CHECK, MAINTENANCE FOUND THAT THE FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND THE UPPER LOCK BAR BROKEN. REMOVED AND REPLACED THE UPPER LOCK BAR AND ADJUSTED IAW DC-9 MM 56-10-03-5. OPS CHECKED GOOD.Apr 3, 2003 · N933AX · Doug DC933F · Flight Compartment WindowsSDR EIA2003051Frame · corrodedFORWARD CARGO PIT FRAME AT STA 351, SIDE AT BEND RADIUS. CORRODED BETWEEN LONGERON 30-29 R. INSTALLED REPAIR ON STA 351 FRAME SRM 51-30-02,1 AND 53-03 FIG 2A. HEAT TEATED AND FABRICATED DOUBLERS IAW SRM 53-03 PG 4E AND 4J.Mar 7, 2003 · N944F · Doug DC933F · Fuselage Main, FrameSDR EIA2003052Skin · crackedLONGERON, 4 LEFT STA. 484 CRACK IN SKIN GOING RIVET TO RIVET 1.5 INCHES. REPAIRED CRACK AT LONGERON 4L SA 484 IN FUSELAGE SKIN IAW SRM 53-04, PG 218M, 218Z, 218AA, AB. ORIGINAL SKIN 2014 T6 .050 SUBSTITUTED 2024-T3 .050 IAW SRM 51-60-0 PG 5.Mar 7, 2003 · N944F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIA2003050Skin · damagedSKIN DENT AND LONGERONS BENT STA NR 275 TO 294 LONGERONS 20 AND 21 RIGHT. CUTOUT DAMAGED SKIN AREA AT BS 275 BETWEEN LONGERONS 20-22 REPAIRED IAW SRM 53-04 PG 42-44, 60BV, 60BU, 60RT, AND 60CK. CUTOUT DAMAGE LONGERON AREA 20R AT BS267-285 AND LONGERON 21 ATMar 5, 2003 · N944F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIA2003048Pushrod TubeINTEERCONNECT TUBE BETWEEN PILOT AND COPILOT HAS SEVERE GOUGHING ON LEFT UPPER SIDE' RH UPPER SIDE SLIGHTLY GOUGED DUE TO BOLT LENGTH OF CENTER PEDESTAL AND PANEL INSTILLATIONREPAIRED AS PER ECRA 944-27-161-2 INTERCONNECT TORQUE TUBE REQUIRED SPLICE. CUT TORQUMar 5, 2003 · N944F · Doug DC933F · Flight Control SystemSDR EIA2003047Skin PanelGOUGH AFT OF MAIN CARGO DOOR CORRECTIVE ACTION: CLASS I REPAIR INSTALLED ON L/H FUSELAGE STA 447.5 to STA 457.5, from LONGERON 16L-17L (DOUBLER) PER DC9 SRM 53-04 Pg 60 & DC9 SRM 51-30-5, Pgs 1-30. REPETITIVE INSPECTION REQUIRED PER DC9 SRM 53-04, FIG 12BFeb 28, 2003 · N944F · Doug DC933F · Fuselage Structure (General)SDR ABXA030041Outflow Valve · lack of lubeAIRCRAFT WOULD NOT AUTO PRESSURIZE ON CLIMBOUT. MANUAL PRESSURIZATION ATTEMPTED, BUT OUTFLOW CONTROL WHEEL WOULD NOT MOVE. INSPECTED AND CLEANED OUTFLOW VALVE AS REQUIRED. NO DEFECTS NOTED. REMOVED CIRCUIT BREAKER COLLARS FROM CABIN PRESS CONTROL. OPS CHEJan 17, 2003 · N934AX · Doug DC933F · Pressure Regulator/Outflow ValveSDR ABXA030032Ground Wire · looseRIGHT OVERHEAD EMERGENCY LIGHT DIM. TIGHTENED GROUND WIRE ON RIGHT OVERHEAD EMERGENCY LIGHT FIXTURE. OPS CHECKED GOOD IAW AMM.Jan 11, 2003 · N932AX · Doug DC933F · Light System WiringSDR ABXA020324Clip · crackedCRACKED SHEAR TIE AT STA. 1076 (AFT SIDE) BETWEEN LONGERONS 15 - 16 LEFT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2.Nov 7, 2002 · N932AX · Doug DC933F · Fuselage Structure (General)SDR ABXA020323Frame · crackedSTA 980 FRAME REPAIR BELOW LONGERON 14 RIGHT WAS CRACKED. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5 AND 51-30-2.Nov 7, 2002 · N932AX · Doug DC933F · Fuselage Main, FrameSDR ABXA020322Support · crackedFLOOR SUPPORT FITTING AT F.S. 980 LONGERON 28 LEFT CRACKED UNDER STRAP. REPLACED SUPPORT FITTING IAW DC-9 SRM 51-30-5.Nov 6, 2002 · N932AX · Doug DC933F · Fuselage Structure (General)SDR ABXA020321Floor Support · corrodedFLOOR SUPPORT AT FS 996 LONGERON 30, HEAVILY EXFOLIATED AND BROKEN OFF. REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-30-5.Nov 6, 2002 · N932AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA020320Skin · crackedCRACK IN BELLY SKIN STA 465 BETWEEN LONGERON 29 LEFT TO 30. REPAIRED CRACK IN BELLY SKIN IAW REA D953-45748MR.Nov 6, 2002 · N932AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA020319Former · crackedCRACK AT OUTBOARD END OF FRAME F.S. 658 AND LONGERON 27 RIGHT CANTED KEEL AREA. REPAIRED FRAME IAW DC-9 SSRM DWG. #K05159.Nov 5, 2002 · N932AX · Doug DC933F · Fuselage Structure (General)SDR ABXA020318Longeron · crackedLONGERON END CRACKED JUST AFT OF FORWARD "P" DOME ON LONGERON 29 LEFT. REPAIRED AREA IAW DC-9 SRM.Nov 5, 2002 · N932AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR ABXA020317Clip · crackedCLIP CRACKED FRONT SIDE OF FRAME AT F.S. 637 AT LONGERON 29 LEFT. REPLACED CLIP IAW DC-9 SRM 51-30-5.Nov 5, 2002 · N932AX · Doug DC933F · Fuselage Structure (General)SDR ABXA020316Skin · corrodedEXFOLIATION ON LOWER CENTER WING SKIN - XCW 20, AT STRINGER 19 RIGHT. REPAIRED AREA IAW DC-9 SRM 52-03.Nov 5, 2002 · N932AX · Doug DC933F · Wing, Plate/SkinSDR ABXA020315Support · crackedINBOARD SPOILER ACTUATOR OUTBOARD SUPPORT FITTING WAS CRACKED AT UPPER FLANGE. REPLACED SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5.Nov 5, 2002 · N932AX · Doug DC933F · Wing StructureSDR ABXA020314Former · crackedTHIRD LEADING EDGE RIB OUTBOARD OF #11 SLAT TRACK CRACKED AT AFT UPPER END. REPLACED RIB IAW DC-9 SRM 51-30-2, 51-30-5, AND 51-10-3B.Nov 4, 2002 · N932AX · Doug DC933F · Wing StructureSDR ABXA020313Web · corrodedLEVEL I CORROSION ON SUB-FLOOR SEVERAL PLACES, BUTT LINE '0', OUTBOARD TO LONGERON 18 RIGHT, FS 133.4 TO FS 148. REPAIRED AREA IAW DC-9 SRM 53-01.Nov 3, 2002 · N932AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA020276Actuator · failedRUDDER PEDALS WERE STIFF DURING CONTROL CHECK, ON CLIMB OUT OF ICT. CLIMBING TO FL 350, AIRCRAFT STARTED TO YAW AND DUTCH ROLL. DISCONNECTED AUTO PILOT. TURNING OFF YAW DAMPER AND GOING TO MANUAL RUDDER DID NOT STOP YAW/DUTCH ROLL. AIRCRAFT SLOWED AND DESCENDOct 29, 2002 · N934AX · Doug DC933F · Rudder Tab Control SystemSDR ABXA020188Control Cable · brokenON INITIAL CLIMB OUT, EXCESSIVE NOISE AND VIBRATION IN VICINITY OF NOSE GEAR. WHEN GEAR LOWERED, NOISE, VIBRATION STOPPED. FOUND RIGHT FORWARD NOSE GEAR DOOR OPEN, AND DOOR STOP CABLE BROKEN. REPLACED LEFT AND RIGHT NOSE GEAR DOOR STOP CABLES IAW DC-9 MM 32Sep 11, 2002 · N934AX · Doug DC933F · Landing Gear Door Retract SectionSDR EIA2002089Latch · out of adjustFLT 120 - PANC - AFTER TAKEOFF, AFT RIGHT GEAR UNSAFE LIGHT REMAINED ON, UPLATCH CHECK FAILED. PERFORMED ADJUSTMENT/TEST MAIN GEAR DOOR LATCH MECHANISM PER MM 32-31-4, SYSTEM OPS CHECK NORMAL, ALSO GREASED LATCH MECHANISM, CLEANED ELECTRIC PLUGS ON UPLATCH SWAug 2, 2002 · N933F · Doug DC933F · Landing Gear Position and WarningSDR 200200272Skin · crackedREPAIRED WINDOW BELT LOCATION STA 270-256 RT PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 8110-3.Jul 16, 2002 · N941F · Doug DC933F · Fuselage Main, Plate/SkinSDR 200200271Skin · crackedREPAIRED WINDOW BELT LOCATION STA 370-389 RT PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 8110-03.Jul 16, 2002 · N941F · Doug DC933F · Fuselage Main, Plate/SkinSDR 200200270Skin · crackedREPAIRED WINDOW BELT LOCATIONS STA 851-870 LT PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 8110-3.Jul 16, 2002 · N941F · Doug DC933F · Fuselage Main, Plate/Skin
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