Douglas DC-9-33F

Service difficulty reports · 1,681

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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"

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SDR 200200269Skin · crackedREPAIRED WINDOW BELT LOCATION STA 756-775 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/SkinSDR 200200268Skin · crackedREPAIRED WINDOW BELT LOCATION STA 522-541 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/SkinSDR 200200267Skin · crackedREPAIRED WINDOW BELT LOCATION STA 351-370 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/SkinSDR ABXA020029Angle · crackedRIGHT ENGINE PYLON LOWER ATTACH ANGLE BULGED AND CRACKED AT STATION 996. REPAIRED IAW SRM 54-04.May 29, 2002 · N931AX · Doug DC933F · Nacelle/Pylon Miscellaneous StructureSDR ABXA020028Fitting · crackedFS 965 RIGHT BUTT LINE 48, FITTING WAS CRACKED AT FORWARD SIDE OF FLOOR BEAM. FABRICATED AND INSTALLED FITTING IAW DC-9 SRM.May 23, 2002 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA020027Floorbeam · corrodedCORROSION ON AFT FACE OF TRANSVERSE FLOOR BEAM AT WEB STATION 996, BL 0, LBL 36.May 20, 2002 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA010910Fitting · rustedSTEEL BEAM ABOVE THE RIGHT CLEARVIEW WAS RUSTED ON THE AFT END, BOTH INSIDE AND OUTSIDE OF BEAM. REPLACED BEAM IAW DC-9 SRM 51-30-1 AND 51-30-5.May 19, 2002 · N930AX · Doug DC933F · Fuselage Structure (General)SDR ABXA020026Fitting · crackedFS 775 RIGHT, CABIN FLOOR SUPPORT LOWER FITTING WAS CRACKED. REPLACED THE SUPPORT FITTING IAW DC-9 SRM 51-10-4 AND 51-30-5.May 16, 2002 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA020025Fitting · crackedFS 775 LEFT, CABIN FLOOR SUPPORT STRUT LOWER FITTING WAS CRACKED. REPLACED THE LOWER FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.May 16, 2002 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA020024Fitting · crackedFS 832 RIGHT, CABIN FLOOR SUPPORT STRUT LOWER FITTING WAS CRACKED. REPLACED THE SUPPORT FITTING IAW DC-9 SRM 51-10-4 AND 51-30-5.May 16, 2002 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA020023Fitting · crackedFS 945 LEFT, CABIN FLOOR STRUT LINE FITTING WAS CRACKED. REPLACED THE STRUT LINE FITTING IAW DC-9 SRM 51-30-5.May 16, 2002 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA020022Floorbeam · corrodedFS 937, RBL 22, HAD LEVEL I CORROSION ON THE CABIN FLOORBEAM HORIZONTAL FLANGE. REPAIRED THE FLOORBEAM IAW DC-9 SRM 53-05.May 16, 2002 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA020021Fitting · crackedFITTING CRACKED IN LEFT KEEL AREA, FS 676 AT LONGERON 29 LEFT. REPLACED FITTING IAW DC-9 SRM 51-30-5.May 15, 2002 · N931AX · Doug DC933F · Fuselage Main, KeelSDR ABXA020020Cap · crackedFS 604, LONGERON 29 LEFT END CAP WAS CRACKED. REPLACED END CAP AT FS 604 IAW DC-9 SRM 51-30-5.May 15, 2002 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA020019Fitting · crackedLEFT AND RIGHT ATTACH ANGLES FOR LONGERON 30, AFT OF FS 604 (PRESSURE DOME) WERE CRACKED. REPLACED ATTACH ANGLES IAW DC-9 SRM 51-30-5.May 15, 2002 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA020018Fitting · corrodedCABIN FLOOR SUPPORT STRUT LOWER FITTING CRACKED AT FS 237, LONGERON 23 RIGHT. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2.May 15, 2002 · N931AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA020017Fitting · corrodedLEVEL I CORROSION ON FRAME FOOT AND ATTACH BOLTS AT FS 256, LONERON 18 RIGHT. REPLACED THE FRAME FOOT IAW DC-9 SRM 51-30-5 AND 51-30-1.May 15, 2002 · N931AX · Doug DC933F · Fuselage Main, FrameSDR ABXA020016Fitting · corrodedLEVEL I CORROSION ON FRAME FOOT AND ATTACH BOLTS AT FS 332, LONGERON 18 RIGHT. REPLACED THE FRAME FOOT FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.May 15, 2002 · N931AX · Doug DC933F · Fuselage Main, FrameSDR ABXA020015Seat Track · corrodedLEVEL I CORROSION AND EXFOLIATION ON SUBFLOOR AT SCREWS FOR PILOTS INBOARD AFT SEAT TRACK. DETERMINED CORROSION TO BE OUT OF LIMITS, REPLACED THE CAPTAIN'S SEAT TRACK IAW DC-9 SRM 51-10-4 AND 51-30-1.May 14, 2002 · N931AX · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA020011Skin · corrodedBULGE IN FUSELAGE SKIN AND FASTENER HEADS DISHED AT FS 446, L30 AND L29L. CLEANED CORROSION ON INNER SKIN PER DC9 SRM 51-10-3. REPLACED DOUBLERS DUE TO CORROSION PER DC9 SRM 51-30-2.May 14, 2002 · N931AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA020013Door Frame · corrodedCORROSION ON AFT LOWER CARGO DOOR JAMB AT WEB STATION 897-937. BLENDED CORROSION AND REPLACED A SECTION OF JAMB WEB IAW DC9 SRM.May 14, 2002 · N931AX · Doug DC933F · Fuselage Main, StructureSDR ABXA020012Doubler · corrodedBULGE IN FUSELAGE SKIN AND FASTNER HEADS DISHED AT FS 439 L30L AND 29L.REPLACED DOUBLER P/N-5911412-47 PER DC9 SRM 51-30-2.May 14, 2002 · N931AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA020014Fitting · crackedLEFT FORWARD DOOR, FORWARD HINGE FITTING WAS CRACKED IN 3 PLACES.REPLACED DOOR FITTING P/N-4916564-1 IAW DC9 SRM 51-30-1.May 14, 2002 · N931AX · Doug DC933F · Fuselage, Door HingeSDR ABXA020010Web · corrodedE/E BAY STA 218, RBL 30- LBL 30, SUBFLOOR HAD MINOR CORROSION. REPAIRED AREA AT STATION 218 RBL 30, LBL 30 SUBFLOOR IAW DC9 SRM.May 13, 2002 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA010909Panel · delaminatedLEFT WING LOWER INBOARD BONDED PANEL HAD A LARGE AREA OF DELAMINATION AROUND FASTENERS. REPLACED BONDED PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2.May 10, 2002 · N930AX · Doug DC933F · Wing, Plate/SkinSDR ABXA010908Tee Chord · crackedAFT PRESSURE BULKHEAD NR 2 TEE HAD 2 VERTICAL CRACKS APPROXIMATELY 1 INCH IN LENGTH AT LONGERON 14 RIGHT AND LONGERON 16 RIGHT. REPLACED THE NR 2 TEE IAW EA 53120033-006 AND REA D953-44179.May 9, 2002 · N930AX · Doug DC933F · Fuselage Main, BulkheadSDR ABXA010873Retract Cylinder · defectiveSHORTLY AFTER TAKEOFF, RIGHT HYDRAULIC QUANTITY DROPPED TO 2 GALLONS. THE RIGHT HYDRAULIC PUMPS AND QUANTITY INCREASED TO 10 GALLONS DURING DESCENT. THE PUMPS WERE TURNED BACK ON AND THE QUANTITY ON THE RIGHT SIDE WENT TO ZERO. THE GEAR WAS EXTENDED MANUALLMay 9, 2002 · N931AX · Doug DC933F · Landing Gear Retraction/Extension SystemSDR ABXA010907Skin · crackedCRACK INDICATION IN PAN AND HI-LOK AT THE NR 1 BEAM AFT END AFT LOWER CARGO DOOR. REPLACED THE OUTER SKIN AND PAN IAW DC-9 SRM 51-30-2.May 8, 2002 · N930AX · Doug DC933F · Cargo/Baggage DoorsSDR 200200249Skin · crackedREPAIRED WINDOW BELT LOCATION STA 218-237 LT, PER PART 2 OF ECRA, FAA FORM 8110-3, DC9 SRM 53-04 FIG 34 AND FAA FORM 8110-3.May 7, 2002 · N941F · Doug DC933F · Fuselage Main, Plate/SkinSDR 200200247Pan · crackedREPAIRED CRACKED INNER AND OUTER PANS OF AFT CARGO DOOR AT STOP NR 3 BY STOP-DRILLING CRACKS, PERFORMED HFEC TO VERIFY DAMAGE CONTAINMENT AND INSTALLED DOUBLERS PER DC-9 SRM 52-05 FIG 50 TO INNER PAN AND DC-9 SRM 52-03 FIG 8 SHEET 1 TO OUTER PAN.May 7, 2002 · N941F · Doug DC933F · Cargo/Baggage DoorsSDR 200200246Door Frame · crackedREPAIRED CRACK IN UPPER FWD CORNER OF MAIN CARGO DOOR BY REMOVING TEMPORARY REPAIR, TRIMMING OUT THE CRACK, FABRICATING FILLER AND REINSTALLING EXISTING REPAIR DOUBLER.May 7, 2002 · N941F · Doug DC933F · Fuselage Main, StructureSDR EIA2002045Battery · dischargedEMERGENCY EXIT LIGHT, BATTERIES DO NOT HOLD A CHARGE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY PER MM. SYSTEMS OPS, NORMAL.May 2, 2002 · N933F · Doug DC933F · Emergency LightingSDR EIA2002019Battery · inoperativeDURING CRUISE AT FL 330, AT APPROX 2015Z, THE NR 1 NAV FAILED. SHORTLY AFTER THAT, THE CAPTAINS ADI TUMBLED THEN THE TRANSMITT FUNCTION OF THE RADIOS FAILED. REPLIES WERE MADE BY THE IDENT ON THE TRANSPONDER. ALL LIGHTS IN THE COCKPIT OTHER THAN THE MASTER Feb 10, 2002 · N945F · Doug DC933F · Battery/Charger SystemSDR ABXA010613Web · crackedCUSP WEB CRACKED BETWEEN STATION 870 AND 889 AT LEFT BUTT LINE 54. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.Nov 14, 2001 · N935AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA010612Support · crackedVERTICAL FLOOR SUPPORT FITTING CRACKED F.S. 541 AT LONGERON 24 RIGHT. REPAIRED FITTING IAW DC-9 SSRM DWG K05159, DC-9 SRM 51-30-2 AND 51-30-5.Nov 13, 2001 · N935AX · Doug DC933F · Fuselage Main, StructureSDR ABXA010611Support · crackedVERTICAL SUPPORT FITTING AT STATION 256, LONGERON 24 LEFT CRACKED. REPAIRED FITTING IAW DC-9 SSRM.Nov 13, 2001 · N935AX · Doug DC933F · Fuselage Main, StructureSDR ABXA010610Support · crackedVERTICAL SUPPORT FITTING AT STATION 237, LONGERON 24 RIGHT WAS CRACKED. REPLACED FITTING IAW DC-9 SSRM DWG K05159.Nov 13, 2001 · N935AX · Doug DC933F · Fuselage Main, StructureSDR ABXA010609Support · crackedVERTICAL SUPPORT FITTING AT STATION 256, LONGERON 24 RIGHT WAS CRACKED. REPLACED FITTING IAW DC-9 SSRM DWG K05159.Nov 13, 2001 · N935AX · Doug DC933F · Fuselage Main, StructureSDR ABXA010608Support · crackedVERTICAL SUPPORT FITTING AT STATION 332, LONGERON 24 RIGHT CRACKED. REPAIRED AREA IAW DC-9 SSRM DWG K05159.Nov 13, 2001 · N935AX · Doug DC933F · Fuselage Main, StructureSDR ABXA010607Spar · crackedLEFT UPPER REAR SPAR HAD A HORIZONTAL CRACK IN THE UPPER INBOARD CORNER FROM LEFT BUTT LINE 5 TO BUTT LINE 0. REPAIRED AREA IAW DC-9 SRM 57.Nov 13, 2001 · N935AX · Doug DC933F · Wing SparSDR ABXA010606Track · corrodedFIRST OFFICER'S FORWARD LEFT SEAT TRACK CORRODED AT FORWARD AND AFT MOUNT AREAS. REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1.Nov 13, 2001 · N935AX · Doug DC933F · Fuselage Structure (General)SDR ABXA010605Angle · crackedSMALL ANGLE CRACKED BENEATH KEEL, LOCATED RIGHT OF ANTI-COLLISION LIGHT WIRE FEED THROUGH. INSTALLED NEW ANGLE IAW DC-9 SRM 51-30-1 AND 51-30-5.Nov 13, 2001 · N935AX · Doug DC933F · Fuselage Structure (General)SDR ABXA010604Former · crackedFORWARD LOWER CARGO DOOR FRAME CRACKED INSIDE FORWARD LOWER LIGHTENING HOLE. REPLACED ANGLE IAW DC-9 SRM.Nov 13, 2001 · N935AX · Doug DC933F · DoorsSDR ABXA010603Panel · crackedFORWARD LOWER CARGO DOOR FORWARD EDGE AT 2ND STOP FROM BOTTOM CRACKED AT STOP FITTING. REPAIRED AREA IAW DC-9 SRM 52-05 AND SHP TRAVELER # ST-0148-04.Nov 13, 2001 · N935AX · Doug DC933F · Cargo/Baggage DoorsSDR ABXA010602Pan · crackedFORWARD LOWER CARGO DOOR STOP FITTING CRACKED ON AFT EDGE OF DOOR, 2ND FROM TOP. REPAIRED AREA IAW DC-9 SRM 52-05 AND SHOP TRAVELER # ST-0148-04. NOTE: CRACK WAS IN DOOR INNER PAN, NOT THE FITTING.Nov 13, 2001 · N935AX · Doug DC933F · Cargo/Baggage DoorsSDR ABXA010580Contactor · dirtyCOCKPIT EMERGENCY LIGHTS WOULD NOT COME ON. CLEANED BATTERY PACK AND CONTACTS. SYSTEM OPS CHECKED GOOD IAW DC-9 AMM 33-53-02-4-0001.Nov 13, 2001 · N930AX · Doug DC933F · Emergency LightingSDR ABXA010601Bulkhead · crackedCRACK AT RIVET ON FORWARD FACE OF STATION 37 BULKHEAD, APPROXIMATELY 18 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.Nov 12, 2001 · N935AX · Doug DC933F · Fuselage Main, BulkheadSDR ABXA010600Rib · corrodedEXFOLIATION CORROSION ON LEFT WING REAR SPAR RIB, ABOVE THE CENTER ATTACH POINT OF THE INBOARD BUTE DOOR. REPLACED RIB IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-8.Nov 12, 2001 · N935AX · Doug DC933F · Wing, Rib/BulkheadSDR ABXA010581Battery · defectiveCOCKPIT EMERGENCY LIGHTS WOULD NOT COME ON. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-0-2-4-0001.Nov 11, 2001 · N930AX · Doug DC933F · Emergency LightingSDR ABXA010557Light · malfunctionedCOCKPIT EMERGENCY LIGHTS WOULD NOT TEST. MECHANIC WENT TO GET NEW BATTERIES. UPON MECHANIC'S RETURN, THE CREW INFORMED HIM THAT THE LIGHTS WERE WORKING, BUT ONE BULB WAS OUT. WHEN MECHANIC WIGGLED THE BULB IT CAME ON. REPLACED THE BULB AS A PRECAUTION.Oct 29, 2001 · N930AX · Doug DC933F · Emergency Lighting
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