Douglas DC-9-32

Service difficulty reports · 12,755

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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 = 'DC932'
  ORDER BY difficulty_date DESC"

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SDR CALA9801111Angle · corrodedINSPECTION FOUND L-ANGLE ON BULKHEAD FRAME CORRODED AT STA 996, STRINGER 19L. THE ANGLE WAS REMOVED IAW SRM 51-30-02, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-02, 51-10-4, 51-10-3 AND 51-30-02.Jun 16, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801110Cusp · corrodedINSPECTION FOUND CUSP CORRODED AT LT SIDE OF STA 980 TO 996. THE CORRODED SECTION OF CUSP WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE25.Jun 16, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CA980706027Outflow Valve · failed(CAN) ON CLIMB-OUT, AT 26,000 FEET, FLOW LIGHT ILLUMINATED, CABIN DIFFERENTIAL AT MAXIMUM 8 POUNDS PER SQUARE INCH. LEVELED OFF AT 280 WITH CABIN ALTITUDE AT 4,000 ABOUT 1,400 BELOW SCHEDULE, NO STANDBY LIGHT ON. SELECTED MANUAL TO REGAIN SCHEDULE, WHEN AUTOJun 16, 1998 · Doug DC932 · Pressure Regulator/Outflow ValveSDR ABXA9800537Window · lack of lubeCAPTAIN'S SLIDING WINDOW JAMMED WHEN OPENING. CLEANED AND LUBRICATED WINDOW IAW DC9 MM.Jun 16, 1998 · N988AX · Doug DC932 · Flight Compartment WindowsSDR MWEA98739Slide · detachedTHE GALLEY DOOR EMERGENCY SLIDE FELL OFF MOUNTING BRACKETS. MTC RESECURED GALLEY ESCAPE SLIDE.Jun 15, 1998 · N401ME · Doug DC932 · Emergency EquipmentSDR MWEA98738Slide · detachedTHE GALLEY DOOR EMERGENCY SLIDE FELL OFF. MTC RESECURED GALLEY EMERGENCY SLIDE.Jun 15, 1998 · N401ME · Doug DC932 · Emergency EquipmentSDR MWEA98723Pan · damagedTHE FORWARD CARGO DOOR HANDLE RECESS PAN WAS FOUND DAMAGED. REMOVED AND REPLACED PAN USING APPROVED DATA.Jun 15, 1998 · N215ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98722Sill · corrodedTHE FORWARD CARGO DOOR SILL PAN AN SUPPORT STRUCTURE WAS FOUND CORRODED. REMOVED DAMAGED PARTS FABRICATED AND INSTALLED REPAIR SECTIONS USING APPROVED DATA.Jun 15, 1998 · N215ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98721Frame · misrepairedFUSELAGE FRAME AT STA 503 BETWEEN LONG 28R AND 28L HAS PREVIOUS REPAIR THAT DOES NOT MEET SRM REQUIREMENTS. INSTALLED PROPER SPLICE REPAIR IAW SRM.Jun 15, 1998 · N215ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98720Skin · corrodedSKIN BULGED AND IRREGULAR FASTENERS INSTALLED AT STA 436 TO 475 BETWEEN LONGERON 18L AND 26L SKIN SPLICE. REPAIR WAS INSTALLED AND ATTACHING STRUCTURE WAS REPLACED.Jun 15, 1998 · N215ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98719Frame · corrodedFRAME AT STATION 427 LONGERON 30 WAS FOUND CORRODED. REPAIRED FRAME USING APPROVED DATA.Jun 15, 1998 · N215ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98718Frame · corrodedTHE FRAME AT STATION 370 LONGERON 30 WAS FOUND CORRODED. FRAME WAS REPAIRED USING APPROVED DATA.Jun 15, 1998 · N215ME · Doug DC932 · Fuselage Main, FrameSDR MWEA98717Skin · misrepairedPREVIOUS REPAIR AT STA 275 LONG 18R DOES NOT CONFORM TO SRM REQUIREMENT. DOUBLER REPAIR INSTALLED.Jun 15, 1998 · N215ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98716Web · corrodedCUSP WEBS BETWEEN STA 237 TO 275 ON RIGHT SIDE ARE CORRODED. INSTALLED FABRICATED CUSP WEBS L18R.Jun 15, 1998 · N215ME · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801109Panel · crackedINSPECTION FOUND VERTICAL STABILIZER PHENOLIC PANEL CRACKED AT STA 96. THE PANEL WAS REMOVED IAW SRM 51-30-2, A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 55-01, PAGE 1 AND 51-30-2.Jun 15, 1998 · N12538 · Doug DC932 · Vertical StabilizerSDR CALA9801108Strap · corrodedINSPECTION FOUND RT AFT CEILING PANEL ATTACHING STRAPS CORRODED. NEW STRAPS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801091Frame · crackedINSPECTION FOUND FRAME STA 1074 CRACKED AT FASTENERS AT LONGERON 3R, 4R, 5R, AND 4L. THE CRACKED SECTION OF FRAME WAS REMOVED AND A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 30.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Main, FrameSDR CALA9801090Floorboard · splittingINSPECTION FOUND NR 48 FLOORBOARD SKIN SPLITTING AT FS 465 TO 579. SKIN AND FOUR HAT SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 53-21-0 AND 51-70-2.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801089Floorboard · crackedINSPECTION FOUND LT FLOORBOARD PANEL BETWEEN STA 680 AND 756 CRACKED AT THE LT FORWARD NR 5 ATTACH HOLE. A NEW FLOOR PANEL WAS FABRICATED. TWO HAT SECTIONS WERE REMOVED, CLEANED, AND REBONDED TO NEW FLOOR PANEL IAW SRM 53-05, PAGE 1.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801088Floorboard · gougedINSPECTION FOUND FLOORBOARD PANEL NR 86 GOUGED AND CORRODED. A PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 53-05 PAGE 1, 51-20-0 AND 51-30-2.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801087Floorboard · crackedINSPECTION FOUND FLOORBOARD PANEL NR 79 CRACKED AT THE RT FORWARD EDGE. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3, 53-01 PAGE 12-18.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801086Floorboard · crackedINSPECTION FOUND HAT SECTION OF 49 FLOORBOARD CRACKED AT BOTH ENDS. THE HAT SECTION WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-21-0 AND 51-70-2.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801085Rib · crackedINSPECTION FOUND FLAP RIB LEADING EDGE OF LT WING AT XRS 270 CRACKED AND CORRODED. THE FLAP RIB WAS REMOVED IAW SRM 51-30-2. A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.Jun 15, 1998 · N12538 · Doug DC932 · Leading Edge DevicesSDR CALA9801084Floorboard · crackedINSPECTION FOUND FLOORBOARD NR 70 CRACKED. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 122B.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801083Skin · crackedINSPECTION FOUND NR 1 ENGINE PYLON TRAILING EDGE CRACKED AND CHAFED. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4.Jun 15, 1998 · N12538 · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR CALA9801082Housing · crackedINSPECTION FOUND THE LT ELEVATOR OUTBOARD TRIM TAB INBOARD TRIM ROD HOUSING SHIELD CRACKED AT THE INBOARD UPPER COUNTERSUNK HOLE. THE CRACK WAS STOP DRILLED IAW SRM 55-01, FIGURE 2. A PATCH DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2, 51-10-Jun 15, 1998 · N12538 · Doug DC932 · Elevator, Tab StructureSDR CALA9801080Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN LT DORSAL FIN PANEL ATTACH ANGLE. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801079Web · crackedINSPECTION FOUND A 2 INCH CRACK IN CABIN WEB AT STA 756, LBL 53. THE WEB WAS REMOVED IAW SRM 51-30-2. TWO REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-10-4, AND 51-30-2.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801078Panel · gougedINSPECTION FOUND A GOUGE IN LOWER RT WING ACCESS PANEL. THE GOUGED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-6, FIGURE 13.Jun 15, 1998 · N12538 · Doug DC932 · Wing, Plate/SkinSDR CALA9801077Clip · brokenINSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD SIDE STA 996 THIRD HORIZONTAL STIFFENER FROM FLOORING HAD CLIP BROKEN OFF. THE FASTENERS WERE REMOVED IAW SRM 51-30-2. A REPAIR CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, AND 51-30-2.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801076Doubler · crackedINSPECTION FOUND TWO .25 INCH CRACKS IN TITANIUM FINGER DOUBLER AT STA 996, LONGERON 20L. THE FINGER DOUBLER WAS REMOVED AND A NEW FINGER DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND ENGINEERING ORDER 98-888.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801075Floorboard · crackedINSPECTION FOUND CRACKS AT FORWARD AND AFT ENDS OF FLOORBOARD NR 45. THE FLOORBOARD WAS REPAIRED IAW SRM 53-01, PAGE 9.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801074Floorboard · crackedINSPECTION FOUND CRACKS AT THREE SCREW HOLES IN RT FLOORBOARD NR 41. A STRAP WAS FABRICATED AND INSTALLED ON FLOOR PANEL IAW SRM 51-10-2 AND 51-30-2.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801073Fitting · corrodedINSPECTION FOUND FITTING UNDER FRAME AT STA 851, LONGERON 27 TO 28R CORRODED. THE FITTING WAS REPAIRED IAW SRM 51-10-4, 51-10-3, AND 51-30-5.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801072Clip · crackedINSPECTION FOUND TIE CLIP CRACKED AT STA 996, RBL 56. A NEW TIE CLIP WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10-3.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801071Floorboard · crackedINSPECTION FOUND RT SIDE FLOORBOARD HAD FOUR CRACKS AT SCREW HOLES OF FS 756 AND THREE CRACKS AT SCREW HOLES OF FS 680. THE HAT SECTIONS WERE REMOVED, A NEW FLOOR PANEL WAS FABRICATED AND HAT SECTIONS WERE BONDED TO NEW PANEL IAW SRM 51-30-2, 51-10-2, 51-10-3Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801070Floorboard · crackedINSPECTION FOUND CABIN FLOORBOARD NR 45B FORWARD LEADING EDGE LIP CRACKED AND TORN. THE TORN AREA WAS ROUTED OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 122, FIGURE 4, 51-10-3 AND 51-10-4.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801069Floor · corrodedINSPECTION FOUND CABIN FLOOR PANEL NR 29 CORRODED ON UPPER AND LOWER SURFACES AT STA 237, BL 0 TO RBL 22. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-05 AND 51-70-2.Jun 15, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR VJ9800192Mechanism · out of adjustCAPTAIN'S WINDOW WOULDN'T OPEN. ADJUSTED UPPER RELEASE MECHANISM, OPS CHECKED NORMAL.Jun 14, 1998 · N948VV · Doug DC932 · Flight Compartment WindowsSDR MWEA98658Longeron · misdrilledFOUND A DOUBLE DRILLED HOLE THROUGH A FLANGE OF LONGERON AT STATION 940 AT LONGERON 8R. MTC FABRICATED AND INSTALLED NEW SECTION OF LONGERON.Jun 14, 1998 · N215ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98657Rib · crackedFOUND 1 INCH CRACK ON LEFT WING NUMBER 2 SLAT DRIVE OUTBOARD RIB AT XRS 214. MTC FABRICATED AND INSTALLED NEW NOSE RIBS.Jun 14, 1998 · N501ME · Doug DC932 · Wing, Rib/BulkheadSDR GTIA9800069Fuse · blownDTW - TAIL CONE CATWALK EMERGENCY TRACK LIGHTING INOPERATIVE. INSTALLED FUSE IN BATTERY PACK, OPERATIONAL CHECK GOOD. (X)Jun 14, 1998 · N12505 · Doug DC932 · Emergency LightingSDR CALA9801061Clip · crackedINSPECTION FOUND A 2 INCH CRACK OUT OF UPPER FASTENER HOLE IN SHEAR CLIP AT FS 980 BELOW LONGERON 14L. THE SHEAR CLIP WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-22, 51-30-2, AND 51-30-5.Jun 14, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801060Bracket · crackedINSPECTION FOUND TWO CRACKS IN RT WING FLAP LEADING EDGE SUPPORT BRACKET AT XRS 332 TO 232. THE SUPPORT BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-20-0, 51-10-2, 51-10-1, AND 51-10-3.Jun 14, 1998 · N12538 · Doug DC932 · Wing Miscellaneous StructureSDR VJ9800191Csd · failedLT GENERATOR PADDED AND APU CARRYING LT BUSS, RT CSD TEMP INDICATION WENT FULL SCALE HIGH WITH MASTER CAUTION LIGHT ILLUMINATED AND RT CSD OIL PRESSURE LIGHT ON. FLIGHT CREW DISCONNECTED RT CSD AND REQUESTED EMERGENCY AUTHORIZATION TO RETURN TO ATL MAINTENANCJun 13, 1998 · N932VV · Doug DC932 · Alternator-Generator DriveSDR CALA9801102Floorboard · delaminatedINSPECTION FOUND NR 40 FLOORBOARD DELAMINATED AT CENTER AISLE STA 389 TO 465. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 122B.Jun 13, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801059Floorboard · dentedINSPECTION FOUND THREE DENTS WITH A CRACK IN FLOORBOARD PANEL NR 83. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW GMM 10-900-01, PAGE 1, SRM 51-70-1, 51-10-3, AND 53-05.Jun 13, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801058Skin · damagedINSPECTION FOUND RT NLG REAR DOOR DAMAGED BY LIGHTNING STRIKE. THE DAMAGED SKIN WAS REMOVED AND REPAIR SKIN WAS INSTALLED IAW SRM 52-81-0 AND 51-30-2.Jun 13, 1998 · N12538 · Doug DC932 · Landing Gear DoorsSDR CALA9801057Jamb · crackedINSPECTION FOUND A 2.25 INCH CRACK IN FORWARD PASSENGER ENTRANCE DOOR JAMB UPPER FORWARD CORNER INSIDE SKIN. A REPAIR WAS INSTALLED IAW ECRA 5330-02619 AND SRM 53-05, FIGURE 25A. A DIP WAS ISSUED FOR PERMANENT REPAIR PRIOR TO 1,000 LANDINGS OR NEXT SCHEDULEDJun 13, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801056Frame · crackedINSPECTION FOUND A 3 INCH CRACK IN CABIN FRAME AT STA 639, LBL 60. THE CRACK WAS STOP DRILLED IAW SRM 53-03, PAGE 40. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-03.Jun 13, 1998 · N12538 · Doug DC932 · Fuselage Main, Frame
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