Douglas DC-9-31

Service difficulty reports · 7,433

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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 = 'DC931'
  ORDER BY difficulty_date DESC"

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SDR 0103259927Skin · damagedDURING AN H-CHECK AT ATLANTA THE FUSELAGE BELLY SKIN AT STA 332 AND BL 0 WAS DISCOVERED TO HAVE HOLES FOR FASTENERS COMMON TO SKIN AND SHEAR CLIP HAVE BEEN ELONGATED. THE SHEAR CLIP IS REPLACED AND THE SKIN IS REPAIRED BY TRIMMING OUT THE DAMAGE AND REINFORCIJun 5, 2001 · N8920E · Doug DC931 · Fuselage Main, Plate/SkinSDR 0105039927Longeron · crackedDuring an Hck in ATL, the longeron 26r end fitting was found cracked at station 598. Repaired per EA 99-181209.Jun 4, 2001 · N8920E · Doug DC931 · Fuselage Main, StructureSDR 0104489927Fitting · crackedDuring H ck in ATL the longeron 26r end fitting was found cracked at sta 598. Repaired per EA. 99-181209.Jun 4, 2001 · N8920E · Doug DC931 · Fuselage Main, StructureSDR 0103269927Keelbeam · gougedDURING AN H-CHECK AT ATLANTA BASE A DEEP GOUGE WAS FOUND IN THE KEEL FORMER AT STATION 737 (RT) JUST BELOW THE BRAKE CONTROL VALVE. THE GOUGE WAS AT THE TOP OF THE FORMER. THE REPAIR TO FORMER WAS ACCOMPLISHED PER EA 99-181256 LOG PAGE 1617459.Jun 4, 2001 · N8920E · Doug DC931 · Fuselage Main, KeelSDR ABXA010346Angle · crackedFLOOR BEAM SUPPORT ANGLE AT 617 LEFT BUTT LINE 20 CRACKED. REPLACED ANGLE BRACKET IAW DC-9 SRM 51-30-5.Jun 4, 2001 · N924AX · Doug DC931 · Fuselage Structure (General)SDR ABXA010345Longeron · crackedCRACKED LONGERON 17 LEFT AT PYLON BULKHEAD. REPLACED LONGERON 17 LEFT IAW DC-9 SRM.Jun 4, 2001 · N924AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA010344Doubler · crackedRIGHT F.S. 699 MAIN FRAME INBOARD POCKET UPPER FORWARD FLANGE CRACKED IN AREA OF "Z" ANGLE. INSTALLED REPAIR ANGLE DOUBLER IAW DC-9 E.A. 53400120-001-1.Jun 3, 2001 · N924AX · Doug DC931 · Fuselage Structure (General)SDR 0103349971Pan · crackedDuring H-check found crack on RH aft emergency exit door lower pan. Repaired per EA. 99-181208.May 31, 2001 · N9335 · Doug DC931 · Emergency ExitsSDR 0101969998Transformer · overheatedON DESCENT, THE LEAD FLIGHT ATTENDANT REPORTED A SMOKE ODOR IN THE AREA OF THE FORWARD FLIGHT ATTENDANT JUMPSEAT WHICH DISSIPATED IN 1-2 MINUTES. FOUND THE LEFT FORWARD READING LIGHT TRANSFORMER WIRING COVER MELTED AND BURNT. REPLACED TRANSFORMER T1-52, WIRIMay 22, 2001 · N8934E · Doug DC931 · Passenger Compartment LightingSDR USAAD01114Downlock Sensor · corrodedPIT-CRW - FLT 1282 - DURING DESCENT, WHEN THE LANDING GEAR WAS EXTENDED THE RIGHT MAIN LANDING GEAR GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. THE LANDING GEAR WAS VERIFIED DOWN BY THE CONTROL TOWER. THE LANDING GEAR WAS CYCLED AND THE GREEN LIGHT ILLUMMay 21, 2001 · N922VJ · Doug DC931 · Landing Gear Position and WarningSDR ABXA010276Longeron · crackedLONGERON 29 LEFT VERTICAL LEG CRACKED AT SPLICE BETWEEN STATION 408 - 427. REPLACED SECTION OF LONGERON 29 LEFT STATION 408 - 427 IAW DC-9 SRM 53-02, FIG 14 AND DC-9 SRM 51-30-5.May 21, 2001 · N938AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA010274Panel · delaminatedUPPER INBOARD TRAILING EDGE BONDED PANEL WAS DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-2 AND 51-30-1.May 21, 2001 · N938AX · Doug DC931 · Wing, Plate/SkinSDR GTIA010400Door · out of rigACY - FLT 8055 - AIR RETURN, AFTER TAKEOFF DURING GEAR RETRACTION HAD 'EXTREME' VIBRATION, RECYCLED GEAR WITH NO RESOLVE. RERIGGED NLG DOOR RT SIDE AND INSTALLED SHIMS IN INBOARD BRACKET. NLG SWING IAW DC9 MM 32-22-01. OPS CHECK NORMAL. NO DEFECTS FOUND AMay 19, 2001 · N969ML · Doug DC931 · Landing Gear Door Retract SectionSDR ABXA010275Angle · crackedKEEL SUPPORT L-ANGLE CRACKED INSIDE LEFT KEEL, AFT SIDE UNDER RESERVOIR. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-1, AND 51-30-5.May 17, 2001 · N938AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 0101759981Power Supply · inoperativeDURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AT CATWALK AND TAIL CONE RELEASE HANDLE. REPLACED SEALED POWER SUPPLY IAW DC-9 WM 33-51-04. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.May 12, 2001 · N994Z · Doug DC931 · Emergency LightingSDR ABXA010222Socket · contaminatedTHE NOSE LANDING GEAR DOWN AND LOCKED (GREEN) LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE CREW PERFORMED ABNORMAL CHECKLIST AND COMPLETED A GEAR RE-CYCLE. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM THE NOSE LANDING GEAR GREEN LIGHT SOCKET. OPERMay 9, 2001 · N924AX · Doug DC931 · Landing Gear Position and WarningSDR 0103359988Skin · crackedDuring H-check found a 1" crack on the fuselage skin panel. Repaired per EA. 99-181165.May 8, 2001 · N8944E · Doug DC931 · Fuselage Main, Plate/SkinSDR USAAD01097Control Valve · failedDTW-PHL FLT 298 - AFTER TAKEOFF, THERE WAS A STRONG CHEMICAL SMELL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING FLOW CONTROL VALVE AND WATER SEPARATOR. (M)May 7, 2001 · N925VJ · Doug DC931 · Cabin Cooling SystemSDR 0101719959Light · inoperativeDURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHT INOPERATIVE AT MOST AFT POSITION. MAINTENANCE REPLACED AFT CATWALK EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL.Apr 29, 2001 · N919RW · Doug DC931 · Emergency LightingSDR 0101729973Battery Pack · dischargedDURING LNE CHECK, FOUND CATWALK EMERGENCY TRACK LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.Apr 27, 2001 · N9337 · Doug DC931 · Emergency LightingSDR 0101579947Battery Pack · dischargedDURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHT INOPERATIVE IN TAIL COMPARTMENT. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK OK.Apr 24, 2001 · N8938 · Doug DC931 · Emergency LightingSDR GTIA010209Angle · crackedFTW - FOUND R-1 DOOR BETWEEN BEAM NR 2 AND NR 3 SKIN ANGLE HAS CRACK. (M)Apr 18, 2001 · N934ML · Doug DC931 · Service DoorsSDR GTIA010221Drive Link · crackedFOUND RIGHT INBOARD SPOILER DRIVE LINK CRACKED. REMOVED DRIVE LINK IAW DC-9 MM 27-61-2 OK TO INSTALL DRIVE LINK. INSTALLED DRIVE LINK IAW MM DC-9 27-61-2. (M)Apr 10, 2001 · N934ML · Doug DC931 · Drag Control SystemSDR 0101319973Power Supply · inoperativeDURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED AFT COMPARTMENT POWER SUPPLY. OPERATIONAL CHECK OK.Apr 10, 2001 · N9340 · Doug DC931 · Emergency LightingSDR GTIA010101Fitting · leakingFLT 284 - ACY - FOUND NR 1 BRAKE IS LEAKING AT AFT UPPER FITTING. REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY IAW DC-9 MM 32-40-01. OPS AND LEAK CHECK GOOD AT THIS TIME. (M)Apr 9, 2001 · N969ML · Doug DC931 · Landing Gear Brake SystemSDR ZW0A0100112Angle · crackedDURING OP 15 MAINT CHECK FOUND POSSIBLE CRACK IN SUPPORT ANGLE AT STA 1046, LONGERON 3L. ACCOMP NDT USING HFEC PER 51-00-03, PART 6 AND FOUND 1 .25 IN LONG CRACK. INSTALLED DOUBLER PER SRM 53-05, PAGE 506, FIG 23B, AND SRM 51-30-5.Apr 6, 2001 · N992Z · Doug DC931 · Fuselage Miscellaneous StructureSDR ZW0A0100111Floorbeam · corrodedDURING OP 15 MAINT CHECK AT STA 965, RBL 5 INCHES AND RBL 14 INCHES, BOTTOM OF CABIN FLOORBEAM HAD A BULGE. REMOVED CORRODED SECTIONS OF FLOORBEAM. INSTALLED REPAIR DOUBLERS AND ANGLES PER SRM 53-05, FIG 79, AND ARA 17099.Apr 5, 2001 · N992Z · Doug DC931 · Fuselage Main, Floor BeamSDR USAAD01085Battery · dischargedPIT - THE COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Apr 3, 2001 · N934VJ · Doug DC931 · Emergency LightingSDR GTIA010089Cover · damagedREPLACED COVER FOR TRACK LIGHTING AT ROW 14. CUT AND INSTALL ADDITIONAL LIGHT LENS AND BULBS. REPLACED FLOOR TRACK LIGHTING COVER AT ROW 14. CUT AND INSTALLED LIGHT LENS AND BULB HOLES IN THE NEW FLOOR TRACK LIGHTING COVER TO MATCH THE OLD FLOOR TRACK LIGHTApr 3, 2001 · N969ML · Doug DC931 · Emergency LightingSDR GTIA010090Cover · missingDTW - FOUND TRACK COVER MISSING AT SEAT ROW 9A. CUT TRACK AND REPLACED AT SEAT ROW 9A IAW DC-9 MM 33-50-00. (M)Apr 3, 2001 · N969ML · Doug DC931 · Emergency LightingSDR GTIA010223Flap · chafedFTW - LEFT FLAP INBOARD TRAILING EDGE CHAFING. REMOVED LEFT FLAP INBOARD TRAILING EDGE. (M)Apr 2, 2001 · N934ML · Doug DC931 · Trailing Edge FlapsSDR 0103279933Skin · crackedDURING AN L-CHECK. THE LOWER AFT CORNER OF THE SERVICE DOOR SKIN WAS FOUND WITH CRACKS. THE SUBJECT SKIN PANEL WAS TRIMMED AND RESTORED USING A SPLICE AFT OF THE DOOR CUT OUT USING EA 99-169344 LOG PAGE 1577098. THE EXISTING SKIN ASSEMBLY 5911407-33 IS MANUFMar 30, 2001 · N1334U · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0106210Skin · crackedDURING OP 15 MAINT CHECK FOUND POSSIBLE CRACK IN SKIN AT STA 1104, LONGERON 5L TO 4L. COMPLIED WITH ARA 17573 REFERRING TO LISTED SRM 53-04, FIG 27 AND SRM 51-01 PARAGRAPH 3B1.Mar 30, 2001 · N992Z · Doug DC931 · Fuselage Main, Plate/SkinSDR 0103289945Skin · wrinkledDURING AN H-CHECK AT ATLANTA, WAVINESS AND SKIN MISMATCH WERE FOUND IN THE AREA OF THE ALTERNATE STATIC PORT. IN ORDER TO CORRECT THE DISCREPANCY, THE FUSELAGE SKIN WAS TRIMMED OUT. HOWEVER, THE FLUSH SKIN REPAIR PER THE DC-9 SRM, CHAPTER 53-04, FIGURE 12C CMar 29, 2001 · N8925E · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0105909Skin · crackedDURING OP 15 MAINT CHECK FOUND FUSELAGE SKIN CRACKED AT STA 1079, CANTED BULKHEAD, LONGERON 3L AND 5L. INSTALLED REPAIR DOUBLER PER SRM 53-04, FIG 27, PAGE 143 AND SRM 51-01, PAGE 2 PARAGRAPH 3.Mar 29, 2001 · N992Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0105908Skin · corrodedDURING OP 15 MAINT CHECK FOUND CORROSION ON SKIN AT STA 351 ON RT SIDE AT LONGERON 29R. INTERIM REPAIR WAS INSTALLED. REPAIRED PER SRM 53-04, FIG 38, SHEET 24, AND ARA 17539.Mar 28, 2001 · N992Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0105604Skin · crackedDURING OP 15 MAINT CHECK FOUND CRACK IN SKIN AT STA 1087, LONGERON 4R. ACCOMP HIGH FREQ EDDY CURRENT AND CONFIRMED .75 INCH CRACK PER 51-00-03 PART 6. REPAIRED PER SRM 53-04, FIG 27.Mar 27, 2001 · N992Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0105202Cargo Track · corrodedDURING OP 15 MAINT CHECK IN THE FWD CARGO COMPT, THE RT FWD CARGO TRACK WAS BADLY CORRODED, STA 218 TO 370. MADE NEW TRACK FROM STOCK. DRILLED HOLES FROM OLD TRACK AND COUNTERSUNK HOLES. TREATED AND PRIMED TRACK. ACCOMPLISHED PER SPM 6-70-01.Mar 20, 2001 · N992Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA010222Cowling · crackedFTW - NR 2 ENGINE PYLON FIXED COWL CRACKED 3 PLACES. REMOVED EDGE MEMBER FROM ANGLE IAW DC-9 SRM 34-02. (M)Mar 19, 2001 · N934ML · Doug DC931 · Engine Cowling SystemSDR ABXA010102Cap · crackedNR 6 AFT PRESSURE BULKHEAD TEE CAP APPEARED TO BE CRACKED AT LONGERON 14L. MAINTENANCE INSPECTED AND REPLACED THE TEE SECTION IAW ABX EA 53120037-004 AND EA 53120037-006.Mar 19, 2001 · N948AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA010103Intercostal · crackedINTERCOSTAL WAS CRACKED AT FASTENER HOLE ON AFT SIDE OF FUSELAGE STATION 1143, JUST OUTBOARD OF LEFT RUDDER TORQUE TUBE VERTICAL ATTACH FITTING. MAINTENANCE INSPECTED AND REPAIRED THE INTERCOSTAL IAW DC-9 SUPPLEMENTAL SRM AND SRM 51-30-5.Mar 19, 2001 · N948AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA010104Fitting · crackedRIGHT LOWER VENTRAL DOOR STOP FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE DOOR STOP FITTING IAW DC-9 SRM 51-30-2.Mar 19, 2001 · N948AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA010105Stiffener · crackedAFT PRESSURE BULKHEAD LEFT HOIZONTAL STIFFENER WERE CRACKED ADJACENT TO LONGERON 14 AND 15L. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-9 SRM 51-30-5.Mar 19, 2001 · N948AX · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA010406Skin · crackedPIT - FOUND SKIN CRACKED 1 INCH, STATION 1095 LONGERON 4 RIGHT. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 27. (M)Mar 16, 2001 · N926VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0104913Web · corrodedDURING OP 15 MAINT CHECK FOUND MEMBRANE SKIN UNDER CABIN FLOOR AT STA 200 TO 218, RBL 57, WAS CORRODED. FABRICATED NEW MEMBRANE AND INSTALLED RIVETS AND BOLTS.Mar 15, 2001 · N992Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0104908Longeron · crackedDURING OP 15 MAINT CHECK FOUND LONGERONS 17R, 12R, AND 16R WERE CRACKED AT STA 965. SPLICED IN NEW LONGERON FROM STA 965 TO 996 PER SRM 53-02, FIG 18.Mar 14, 2001 · N992Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0104707Angle · corrodedDURING OP 15 MAINT CHECK THE RIGHT GALLEY SERVICE DOOR FRAME WAS CORRODED INSIDE THE AFT LOWER CORNER, INSIDE FRAME TO FLOOR STRUCTURE. CUT AND REMOVED CORRODED SECTION OF CUSP ANGLE FROM STA 164 TO 229. FABRICATED NEW CUSP ANGLE AND SPLICED PARTS, TREATED Mar 9, 2001 · N992Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0104706Web · crackedDURING OP 15 MAINTENANCE CHECK, FOUND MEMBRANE UNDER FLOOR AT STA 160 TO 200, RBL 21 INCHES, WAS CRACKED AND CORRODED. REMOVED DAMAGED MEMBRANE BETWEEN STA 160 TO 200, RBL 0 INCHES TO 44 IN. MADE NEW MEMBRANE AND INSTALLED.Mar 9, 2001 · N992Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0104705Floor Support · corrodedDURING OP 15 MAINTENANCE CHECK FOUND FLOOR SUPPORT AT STA 200, RBL 20 IN TO 43 IN, WAS CORRODED. FABRICATED NEW FLOOR SUPPORT, TREATED, PAINTED AND INSTALLED FASTENERS.Mar 9, 2001 · N992Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0104704Floor Support · corrodedDURING OP 15 MAINTENANCE CHECK, FLOOR SUPPORT AT STA 160 TO 200, RBL 47 IN, WAS CORRODED. FABRICATED NEW FLOOR SUPPORT, TREATED, PAINTED AND INSTALLED FASTENERS.Mar 9, 2001 · N992Z · Doug DC931 · Fuselage Miscellaneous Structure
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