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 EIA990088Rib · crackedDURING C-CHECK, NR 2 PYLON RIB AT STATION 1009 CRACKED, NRC NR R047. REPAIRED PER SRM 54-01 FIG 2. (M)Dec 28, 1998 · N933F · Doug DC933F · Nacelle/Pylon StructureSDR EIA990112Rib · crackedDURING C-CHECK, FORWARD CARGO DOOR INTERNAL RIBS CRACKED AT BS 370 AND 389, NRC NR F116. REPLACED FRAMES IAW SRM 51-30-02. (M)Dec 26, 1998 · N933F · Doug DC933F · Cargo/Baggage DoorsSDR EIA990111Fitting · crackedDURING C-CHECK, AFT CARGO LEFT SUPPORT FITTINGS ARE CRACKED AT THE FOLLOWING STATIONS, 813, 832, 895 AND 945. REPLACED SUPPORT FITTINGS IAW SRM 51-30-02. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990110Sill · corrodedDURING C-CHECK, AFT CARGO DOOR LOWER SILL HAS EXFOLIATION CORROSION, NRC K126. REPAIRED IAW SRM 53-05. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990109Sill · corrodedDURING C-CHECK, AFT CARGO DOOR LOWER SILL HAS EXFOLIATION CORROSION, NRC NR K126. REPAIRED IAW SRM 53-05. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990108Skin · dentedDURING C-CHECK, FUSELAGE SKIN DENTED AT BS 484 RIGHT SIDE BETWEEN STRINGER 27R AND 28R, NRC F143. REPAIRED IAW SRM 53-04 FIG 12B. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIA990107Frame · dentedDURING C-CHECK, FUSELAGE FRAME DENTED AT BS 389 RIGHT SIDE, NRC W180. REPAIRED IAW SRM 53-03 FIG 4. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, FrameSDR EIA990106Stringer · crackedDURING C-CHECK, FUSELAGE STRINGER NR 4L CRACKED AT BS 160, NRC W160. REPAIRED IAW SRM 53-02. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIA990105Stansion · crackedDURING C-CHECK, FORWARD CARGO COMPARTMENT, RIGHT SIDE WALL VERTICAL STANSION SUPPORTS FOUND CRACKED AT BS 275, 294, 332 AND 351, NRC H063. REPLACED VERTICAL STANSIONS IAW SRM 51-30-02. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990104Skin · crackedDURING C-CHECK, LEFT PYLON SKIN AND STIFFENER WAS FOUND CRACKED AT STATION 965 ABOVE PANEL NR 8101A, NRC NR P062. REPAIRED IAW SRM 54-04 FIG 17A AND EO 9AV 981123) AND ECRA. (M)Dec 26, 1998 · N933F · Doug DC933F · Nacelle/Pylon, Plate/SkinSDR EIA990103Skin · dentedDURING C-CHECK, FUSELAGE SKIN DENTED AT BS 330-365 AND 446, NRC NR F139. REPAIRED IAW SRM 53-04 FIG 12 AVTEL ENGINEERING DRAWING 98-12-01-024, 98-12-02-002 AND ECRA. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIA990102Stringer · corrodedDURING C-CHECK, FUSELAGE STRINGER 23L FROM BS 160-229 HAS CORROSION, NRC G041. REPLACED STRINGER AT THE ABOVE STATIONS IAW SRM 53-02 FIG 18. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIA990101Stringer · corrodedDURING C-CHECK, FUSELAGE STRINGER 24L FROM BS 160-229 HAS CORROSION NRC NR G041. REPLACED STRINGER AT THE ABOVE STATIONS IAW SRM 53-02 FIG 18. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIA990100Stringer · corrodedDURING C-CHECK, FUSELAGE STRINGER 25L FROM BS 140-229 HAS CORROSION, NRC NR GO41. REPLACED STRINGER AT THE ABOVE STATIONS IAW SRM 53-02 FIG 18. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIA990099Fitting · corrodedDURING C-CHECK, FUSELAGE STRINGER SPLICE FITTINGS CORRODED AT BS 229 AT THE FOLLOWING STRINGERS 19L, 20L, 21L, 22L, 23L, 24L AND 25L, NRC NR H053. REPLACED STRINGER SPLICE FITTINGS AT THE ABOVE NOTED STRINGERS IAW SRM 51-30-02. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990098Skin · wornDURING C-CHECK, FUSELAGE SKIN AT BS 1089 HAS AN ELONGATED FASTENER HOLE FORWARD OF THE VERTICAL STAB ATTACH FITTINGS, NRC NR073. REPAIRED PER SRM 53-31-0 FIG 19 AND ECRA. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIA990097Control Cable · frayedDURING C-CHECK, LEFT AILERON CONTROL CABLE FOUND FRAYED AND ROUTED INCORRECTLY, NRC A-55. REPLACED CABLE AND RIGGED IAW MM 27-10-03. (M)Dec 26, 1998 · N933F · Doug DC933F · Aileron Control SystemSDR EIA990096Frame · crackedDURING C-CHECK, AFT CARGO COMPARTMENT DOOR AFT TORQUE FRAME HAS CORROSION AND A CRACK, NRC NR R089. REPAIRED IAW SRM 53-01 FIG 2. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990095Skin · corrodedDURING C-CHECK, FUSELAGE SKIN AND DOUBLER HAS CORROSION AT BS 350 AT STRINGER 30, NRC NR F106. REPAIRED IAW DRAWING 53-98681-3 AND ECRA AND SRM 53-04. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIA990094Stringer · crackedDURING C-CHECK, STRINGER 14R IS CRACKED JUST AFT OF THE AFT PRESSURE BULKHEAD, NRC NR W191. REPAIRED PER SRM 53-02 FIG 18. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIA990093Longeron · corrodedDURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON 23L HAS CORROSION FROM BS 229-313, NRC NR H052. REPAIRED LONGERON PER SRM 53-11-02 FIG 3B. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIA990092Longeron · corrodedDURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON 22L HAS CORROSION FROM BS 229-313, NRC NR H052. REPAIRED LONGERON PER SRM 53-11-02 FIG 3B. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIA990091Longeron · corrodedDURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON 21L HAS CORROSION FROM BS 229-313, NRC NR H052. REPAIRED LONGERON PER SRM 53-11-02 FIG 3B. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIA990090Stansions · crackedDURING C-CHECK, FORWARD CARGO COMPARTMENT VERTICAL STANSIONS CRACKED AT BS 370 AND 427 ON LEFT SLANTED SIDE WALL ABOVE STRINGER, NRC NR H065. REPLACED VERTICAL STANSIONS PER SRM 53-10-2. (M)Dec 26, 1998 · N933F · Doug DC933F · Fuselage Miscellaneous StructureSDR EIA990087Stringer · corrodedDURING C-CHECK, STRINGER NR 30 WAS FOUND WITH EXFOLIATION CORROSION AT BS 756, NRC NR R137. REPAIRED PER DAC DRAWING 5951685-7 AND ECRA. (M)Dec 15, 1998 · N933F · Doug DC933F · Fuselage Main, Longeron/StringerSDR AU981628Valve · out of rig(AUS) ON DESCENT, LANDING GEAR WAS SELECTED DOWN AND DOOR WARNING LIGHT INDICATED UNSAFE. MANUAL EXTENSION CARRIED OUT PER EMERGENCY PROCEDURES AND AIRCRAFT MADE UNEVENTFUL LANDING. INVESTIGATION FOUND THAT THE MLG CONTROL VALVE WAS NOT RIGGED CORRECTLY.Dec 9, 1998 · Doug DC933F · Landing Gear SelectorSDR EIA980361Strut · flatSEA - DURING POST FLIGHT WALK AROUND INSPECTION, THE RIGHT GEAR STRUT WAS FOUND COMPLETELY DEFLATED. DURING FURTHER INVESTIGATION IT WAS FOUND THAT THE GLAND NUT WAS COMPLETELY DISENGAGED FROM THE OUTER CYLINDER. (M)Dec 3, 1998 · N945F · Doug DC933F · Main Landing Gear Strut/Axle/TruckSDR EIA980350Retract Mech · dirtySEA - DURING APPROACH SET FLAPS INDICATED AS FOLLOWS 5 DEGREES, 9 DEGREES, 15, L 18 - R 16) 25 = 27.5, 40-45. CHECKED ADJUSTMENT OF CONTROL VALVE PUSHROD ARM PER MM 27-52-1, INSPECTED AND CLEANED DEBRIS (EXCESSIVE AND DIRTY LUBE) FROM FOLLOW-UP CABLES. (M)Nov 20, 1998 · N945F · Doug DC933F · Trailing Edge Flap Control SystemSDR EIA980349Valve · failedSEA - DURING APPROACH SET FLAPS TO 15 DEGREES (L FLAP 20R, R FLAP 15) FLAPS THEN BLEW BACK TO 10 DEGREE WHILE 15 SELECTED, SELECTED 25 GOT 30, SELECTED 40 GOT 45 INITIAL LANDED WITH 38 DEGREES. REPLACED FLAP CONTROL VALVE PER MM 27-51-1 SYSTEM CHECKED GOOD. Nov 19, 1998 · N945F · Doug DC933F · Trailing Edge Flap Control SystemSDR AU981546Switch · out of adjust(AUS) LEFT MAIN LANDING GEAR DOOR MICROSWITCH OUT OF ADJUSTMENT.Nov 17, 1998 · Doug DC933F · Landing Gear Position and WarningSDR EIAA980337Skin · crackedMZJ - DURING C4 CHECK, LEFT FORWARD DOOR SKIN AT FED LOWER CORNER IS CRACKED AT TWO PLACES. REPAIRED PER SRM 52-05 FIG 32. (M)Oct 31, 1998 · N945F · Doug DC933F · Passenger/Crew DoorsSDR EIAA980332Skin · corrodedMZJ - DURING C4 CHECK, UPPER FUSELAGE AFT ADF ANTENNA DOUBLER HAS CORROSION. REPAIRED PER SRM 53-04 AND ECRA 945-54-027-2. (M)Oct 31, 1998 · N945F · Doug DC933F · Fuselage Main, Plate/SkinSDR EIAA980330Skin · corrodedMZJ - DURING C4 CHECK, FS 1121 LONGERON 16L-18L, SKIN AND FRAME HAS CORROSION. REPAIRED DAMAGED SKIN AND STRAP PER ECRA 945-53-026-2. (M)Oct 31, 1998 · N945F · Doug DC933F · Fuselage Main, Plate/SkinSDR 99ZZZM133Frame · corrodedMZJ - DURING C4 CHECK, FS 1121 LONGERON 16L-18L, SKIN AND FRAME HAS CORROSION. REPAIRED DAMAGED SKIN AND STRAP PER ECRA 945-53-026-2. (M)Oct 31, 1998 · N945F · Doug DC933F · Fuselage Main, FrameSDR 99ZZZM132Longeron · corrodedMZJ - DURING C4 CHECK, FS 1121 LONGERON 16L-18L, SKIN AND FRAME HAS CORROSION. REPAIRED DAMAGED SKIN AND STRAP PER ECRA 945-53-026-2. (M)Oct 31, 1998 · N945F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIAA980336Longeron · crackedMZJ - DURING C4 CHECK, MAIN CABIN FS 980, LONGERON 17R HAS CRACK. REPAIRED PER SRM 53-02. (M)Oct 27, 1998 · N945F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIAA980334Floorbeam · corrodedMZJ - DURING C4 CHECK, AFT CARGO FLOORBEAM UPPER FLANGE AT FS 980 LBL 48 HAS CORROSION AT A PREVIOUS REPAIR. REPAIRED PER SRM 53-05 AND ECRA 945-53-004-2. (M)Oct 25, 1998 · N945F · Doug DC933F · Fuselage Main, Floor BeamSDR EIAA980331Longeron · corrodedMZJ - DURING C4 CHECK, FS 1089 LONGERON 14R, LONGERON HAS HEAVY CORROSION. REPAIRED DAMAGED LONGERON PER ECRA 945-53-026-2. (M)Oct 22, 1998 · N945F · Doug DC933F · Fuselage Main, Longeron/StringerSDR EIAA980333Spar · corrodedMZJ - DURING C4 CHECK, RIGHT PYLON FORWARD SPAR UPPER BEAVER TAIL HAS CORROSION. REPAIRED PER SRM 54-04 AND ECRA 945-54-025-2. (M)Oct 21, 1998 · N945F · Doug DC933F · Nacelle/Pylon StructureSDR EIAA980325Window · failedSEA - AFTER APPROXIMATELY 20 MINUTES OF FLIGHT, THE RIGHT AFT (R3) WINDOW BEGAN MAKING A SHRILL NOISE AND WAS NOTED TO BE DELAMINATED. WITH FROZEN MOISTURE BETWEEN PLIES. (M)Oct 16, 1998 · N945F · Doug DC933F · Passenger Compartment WindowsSDR EIAA980317Retract Mech · malfunctionedSEA - NO GROUND SHIFT ON TAKEOFF. (M)Oct 8, 1998 · N944F · Doug DC933F · Landing Gear Retraction/Extension SystemSDR EIAA980316Retract Mech · malfunctionedSEA - NO GROUND SHIFT ON TAKEOFF. (M)Oct 8, 1998 · N944F · Doug DC933F · Landing Gear Retraction/Extension SystemSDR EIAA980335Floorbeam · corrodedMZJ - DURING C4 CHECK, FS 996 FLOORBEAM WEB HAS EXFOLIATION CORROSION. REPAIRED PER SRM 53-05 FIG 72. (M)Oct 3, 1998 · N945F · Doug DC933F · Fuselage Main, Floor BeamSDR EIAA980329Skin · crackedMZJ - DURING C4 CHECK, FORWARD CARGO DOOR OUTER SKIN CRACK FROM FASTENER HOLE WAS FOUND. REPAIRED PER SRM 52-01 FIG 2, AND 52-32-0. (M)Oct 1, 1998 · N945F · Doug DC933F · Cargo/Baggage DoorsSDR EIA980265Boost Pump · failedSEA - AIR TURNBACK FROM SEA DUE TO CENTER TANK BOOST PUMP CB AFT CENTER BOOST PUMP, CB POPPED AFTER TAKEOFF, RESET AND CB POPPED WITHIN 2 MINUTES. REMOVED AND REPLACED AFT CENTER BOOST PUMP. OPS AND LEAK CHECK GOOD PER MM 28-20-7. ALSO, CHECKED WIRING HARNESep 22, 1998 · N944F · Doug DC933F · Fuel Boost PumpSDR EIAA980264Pump · failedSEA - AIR TURN BACK DUE TO CENTER TANK BOOST PUMP FAILURE. AFT CENTER BOOST PUMPS. QA AND QB POPPED AFTER TAKEOFF, RESET AND POPPED AFTER THREE MINUTES. REMOVED AND REPLACED AFT CENTER BOOST PUMP. OPS AND LEAK CHECK GOOD PER MM 28-20-1. (M)Sep 18, 1998 · N944F · Doug DC933F · Fuel Boost PumpSDR EIAA980239Indicator · failedOAK - UPON ARRIVAL AT BILLINGS, LEFT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR UNSAFE RED LIGHT DID NOT ILLUMINATE UPON THROTTLE BACK AT TOP OF DESCENT. PERFORMED LOW APPROACH AT BILLINGS FOR MX AND TOWER VERIFICATION OF GEAR EXTENSION. GEAR APPEARED DAug 28, 1998 · N933F · Doug DC933F · Landing Gear Position and WarningSDR EIAA980238Switch · failedOAK - UPON APPROACH INTO OAK, LEFT GEAR UNSAFE LIGHT DID NOT ILLUMINATE WHEN THROTTLES WERE RETARDED. UPON GEAR EXTENSION, LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE. PERFORMED LOW PASS FOR MAINTENANCE AND CONFIRMED GEAR WAS DOWN. NO HORN NOTED AT FL 40 AND HAug 27, 1998 · N933F · Doug DC933F · Landing Gear Position and WarningSDR 98ZZZM821Connectors · faultyOAK - UPON APPROACH INTO OAK, LEFT GEAR UNSAFE LIGHT DID NOT ILLUMINATE WHEN THROTTLES WERE RETARDED. UPON GEAR EXTENSION, LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE. PERFORMED LOW PASS FOR MAINTENANCE AND CONFIRMED GEAR WAS DOWN. NO HORN NOTED AT FL 40 AND HAug 27, 1998 · N933F · Doug DC933F · Landing Gear Position and WarningSDR EIAA980237Seal · failedSEA - DURING CLIMB, PASSING 4 PSI DIFFERENTIAL, A LOAD PULSATING HUM, VIBRATION AND AIR NOISE WAS HEARD FROM MAIN CABIN. PRESSURIZATION BECAME UNCONTROLLABLE. RETURNED TO SEA. REPLACED FORWARD UPPER CARGO DOOR PRESSURE SEAL PER MM 52-32-01. PRESSURIZATION Aug 24, 1998 · N944F · Doug DC933F · Cargo/Baggage Doors
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