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 VJ9800282Structure · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT FRAME AND SKIN CORRODED BEYOND LIMIT AT FS 889-897, L30-29R. CLEANED CORROSION IAW DC9 SRM 53-04, FABRICATED INTERNAL DOUBLER FROM 2024-T3.032, 5.4 X 5.5 X.032, IAW DC9 SRM. DRILLED AND DEBURRED IAW DC9 SRM 51-10-4. TREATJul 23, 1998 · N902VJ · Doug DC932 · Fuselage Main, StructureSDR VJ9800251Skin · corrodedAFT CARGO COMPT FLOOR SUPPORT FRAME AND SKIN HAVE CORROSION FS 889-897 L30-L29R. CLEANED CORROSION FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 53-04 CONDITION 3, 20 PERCENT TO 50 PERCENT. FABBED INTERNAL DOUBLER IAW DC-9 SRM 2024-T3.032 5.40X5.50X.032. DRILLED AJul 23, 1998 · N902VJ · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800241Duct · looseTAIL COMPARTMENT HI TEMP LIGHT ILLUMINATED IN FLIGHT CLIMB 18,000. FOLLOWED EMERGENCY PROCEDURES AND ISOLATED THE RIGHT SYSTEM. THE LIGHT EXTINGUISH. AIRCRAFT AIR RETURNED. FOUND LOOSE DUCT ON RT PACK SUPPLY, RE-SECURED DUCT IAW MM 21-00 AND 36-00. OPS CHJul 23, 1998 · N935VV · Doug DC932 · Air Distribution SystemSDR TWAA9812119Skin · crackedDURING OP 16 MAINT CHECK, ON RT WING UPPER SURFACE WING SKIN FOUND CRACK AT O/B AFT CORNER OF FUEL TANK ACCESS PLATE NR 1410A. STOP DRILLED CRACK, INSTALLED DOUBLER PER DRW 5951593RE. ACCOMP NDT CRACK CONTAINMENT CHECK PER 51-00-03.Jul 23, 1998 · N995Z · Doug DC932 · Wing, Plate/SkinSDR TWAA9812118Floor · crackedDURING OP 16 MAINT CHECK, FOUND RT CENTER CABIN FLOOR PANEL AT FS 465 TO 579 WITH 5 CRACKS AT U-CHANNELS ON BOTTOM SIDE, NR 39 PANEL. NEW PANEL FABRICATED PER SSRM 53-00-104.Jul 23, 1998 · N995Z · Doug DC932 · Fuselage Floor PanelSDR TWAA9812117Longeron · crackedDURING OP 16 MAINT CHECK LONGERON 23L HAD 1.5 IN CRACK IN O/B FLANGE RUNNING DOWN INTO RADIUS AT FS 200. CONFIRMED BY EDDY CURRENT. REMOVED CRACKED LONG, INSTALLED NEW LONG FROM FACTORY SPLICE TO FACTORY SPLICE, INSTALLED FASTENERS PER SRM 51-30-0 AND 51-30-Jul 23, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9801331Skin · crackedINSPECTION FOUND CRACKS ON AFT PRESSURE BULKHEAD SKIN SPLICE AT BS 996, LONGERONS 7-10L. AN EXTERNAL DOUBLER, INTERNAL FINGER DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW EA 5361-01001.Jul 23, 1998 · N14534 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801330Beltframe · corrodedINSPECTION FOUND E/E BELTFRAME CORRODED AT BS 180 BETWEEN LONGERON 24 AND 25L. THE CORRODED SECTION WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 4.Jul 23, 1998 · N14534 · Doug DC932 · Fuselage Main, FrameSDR CALA9801329Angle · crackedINSPECTION FOUND A 1.5 CRACK IN AFT PRESSURE BULKHEAD ATTACH T-ANGLE AT STA 996, LONGERON 15L. THE T-ANGLE WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 37A.Jul 23, 1998 · N14534 · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800376Longeron · corrodedLONGERON 30 SPLICE CORRODED STA 935-965. REMOVED 2 SPLICE CORRODED. REMOVED 32 .125 FORMED SECTION LONGERON CORRODED, FABRICATED NEW LONGERON FROM EXTRUSION S1242886, IAW SRM 53-02 FIG 15, DRILLED, TRIMMED AND DEBURRED LONGERON AND SPLICE REPAIRS IAW DC-9 SRJul 22, 1998 · N912VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800248Splice · corrodedAFT PIT FRAME SLICE STA 937 28L IS CORRODED. REMOVED CORROSION MATERIAL LOSS WAS 90 PERCENT AND BEYOND LIMITS. REMOVED FLOOR SUPPORT AND SPLICE CAP. CUT FRAME, FABBED REPAIR OUT OF 7075-0 .050 AND 2 EA SPLICES OUT OF 7075-0.071 AND 0.050. FABBED REPAIR DOUJul 22, 1998 · N902VJ · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9812206Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965, AFT SIDE OF BULKHEAD. REPLACED CRACKED LONGERON SECTION AND SPLICED PER SRM 53-02, FIG 18.Jul 22, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9812203Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 16L CRACKED AT STA 965, AFT SIDE OF BULKHEAD. REPLACED CRACKED LONGERON SECTION AND SPLICED PER SRM 53-02, FIG 18.Jul 22, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9812116Bulkhead Chord · corrodedDURING OP 16 MAINT CHECK, FOUND AT FS 604, THE AFT BULKHEAD OF THE FWD CARGO COMPT, THE BOTTOM CHORD AT STA 30 HAD AREA OF CORROSION. REMOVED CORROSION PER SRM 51-10-03. REPAIRED PER SRM 53-03, FIG 10 ITEM 503.Jul 22, 1998 · N995Z · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9812115Tie · corrodedDURING OP 16 MAINT CHECK, FOUND STRINGER END TIE CORRODED AT STA 994, STR 27R AND 28R. REMOVED AND REPLACED 2 (P/N 4912515-1), INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-05.Jul 22, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98813Slide · fell offTHE GALLEY SLIDE FELL OFF. MAINTENANCE RESECURED THE GALLEY SLIDE.Jul 22, 1998 · N204ME · Doug DC932 · Emergency EquipmentSDR VJ9800372Skin · corrodedCORROSION ON INNER SKIN UNDER LONGERON 28R STA 935. REMOVED LONG 28R AND INNER SKIN FOUND TO BE OUT OF LIMITS. FABBED NEW INNER SKIN 2024 T-3 .025 EXTERNAL SKIN CORROSION OUT OF LIMITS. FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106.Jul 21, 1998 · N912VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800371Skin · corrodedCORROSION ON INNER SKIN STA 935 UNDER LONGERON 29R. REMOVED LONGERON 29R AND INNER SKIN FOUND CORROSION OUT OF LIMITS. FABBED NEW INNER SKIN FROM 2024 - T3 .025 EXTERNAL SKIN CORROSION OUT OF LIMITS, FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106 AND INSTALLEDJul 21, 1998 · N912VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800253Skin · corrodedCORROSION ON INNER SKIN STA 935 UNDER LONGERON 29R. REMOVED LONG 29R AND INNER SKIN FOUND CORROSION OUT OF LIMITS. FABBED NEW INNER SKIN 2024-T3.025 EXTERNAL SKIN CORROSION OUT OF LIMITS FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106 AND INSTALLED LONG 29R.Jul 21, 1998 · N912VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800252Skin · corrodedCORROSION ON INNER SKIN UNDER LONG 28R STA 935. REMOVED LONG 28R AND INNER SKIN FOUND CORROSION OUT OF LIMITS, FABBED NEW INNER SKIN 2024-T3.025. EXTERNAL SKIN CORROSION OUT OF LIMITS, FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106 AND INSTALLED LONG. 28R.Jul 21, 1998 · N912VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800245Pan · corrodedDURING C CHECK, FOUND FWD GALLEY RT OUTBOARD PAN AT FWD INB CORNER OF R-1 DOOR FS 160 LONG 18 R B/L 55R HAS EXFOLIATED CORROSION LEVEL 2. R-1 FWD ENTRY FLOOR PANEL, TRANSITION PLATE AND LOWER SIDE WALL CLOSEOUT PANEL STA 160- 20 RBL 40-TO 55 FOR ACCESS IAW DCJul 21, 1998 · N902VJ · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800243Support · corrodedDURING C CHECK, FOUND AFT CABIN CENTER FLOOR BOARD SUPPORT HAS CORROSION ON TOP AT STA 965. REMOVED CORROSION 100 PERCENT OF THE MATERIAL STA 965 BLO. REMOVED SECTION OUT OF LIMITS. FABBED REPAIR ANGLES 4 EA FROM 7075-T6 .032 2 EA 9.5 X 1X 1, 2 EA. 7.5 X 1 Jul 21, 1998 · N902VJ · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800236Megaphone · malfunctionedEMERGENCY MEGAPHONE DOES NOT WORK. REPLACED FWD MEGAPHONE.Jul 21, 1998 · N918VV · Doug DC932 · Emergency EquipmentSDR VJ9800231Cover · detachedCOVER DISLODGED ON EMERGENCY EVACUATION SLIDE ASSEMBLY OF GALLEY DOOR. REINSTALLED SLIDE COVER AND PERFORMED REQUIRED INSPECTIONS.Jul 21, 1998 · N913VV · Doug DC932 · Life JacketSDR TWAA9812121Skin · corrodedDURING OP 16 MAINT CHECK, FOUND AT BOTTOM OF FUSELAGE SKIN AT FWD END OF RT WHEEL WELL, CORROSION THRU WHERE HINGE PIN SHIELD COVERS. REMOVED CORROSION PER SRM 51-10-03. REPAIRED PER SRM 53-04, FIG 38. REINSTALLED BATH TUB FITTING AND RELATED PARTS PER SRM Jul 21, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9812120Bulkhead · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION AT BOTTOM OF AFT PRESSURE BULKHEAD, 6 IN LBL TO 6 IN RBL. REMOVED CORROSION BY CUTTING OUT CORRODED SECTION PER SRM 53-03, FIG 9 PAGE 12B. INSTALLED DOUBLER PER SRM 53-03, FIG 9.Jul 21, 1998 · N995Z · Doug DC932 · Fuselage Main, BulkheadSDR CALA9801318Seat Track · corrodedINSPECTION FOUND SEAT TRACKS CORRODED AT STA 237 RT O/B AND STA 803-845, LBL 48. THE CORRODED SECTIONS OF SEAT TRACKS WERE CUT OUT. NEW SEAT TRACKS, SPLICES, AND PLATES WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 4F AND 51-30-1.Jul 21, 1998 · N18544 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9812126Skin · dentedDURING OP 16 MAINT CHECK, FOUND DENT ON NR 1 L/E SLAT, LT WING, EXCEEDING ALLOWABLE LIMITS PER SRM 57-03, PG 20A. DENT IS 2.5 BY 17 IN BY .150 DEEP. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR PER SRM 57-09, FIG 10F.Jul 20, 1998 · N998R · Doug DC932 · Leading Edge DevicesSDR TWAA9812124Intercostal · corrodedDURING OP 16 MAINT CHECK, FOUND INTERCOSTAL AT 29R BADLY CORRODED AT STA 965 TO 980. MADE NEW PER SRM 51-01, FABRICATED INTERCOSTAL FROM 7075-0 AND HEAT TREATED PER SRM 53-11-3 PAGE 108. REMOVED CORROSION BY REPLACING INTERCOSTAL PER SRM 51-01, PAGE 1 ITEM CJul 20, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9812123Doubler · misinstalledDURING OP 16 MAINT CHECK, FOUND REPAIR INSTALLED WITH BLIND FASTENERS ON FUSELGE SKIN AND NO DOUBLER AT STA 965 AND 970 BETWEEN LONG 16L AND 17L. REPLACED BLIND FASTENERS AND INSTALLED FINGER DOUBLER PER SRM 53-04, PAGE 93.Jul 20, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9812122Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965. REPLACED SECTION OF LONGERON FROM FS 955 TO 996, PER SRM 51-10, PG 1 ITEM C, AND INSTALLED LONGERON SPLICE PER SRM 53-02, FIG 18.Jul 20, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9812005Bulkhead Web · crackedDURING OP 16 MAINT CHECK, FOUND BULKHEAD 965 RBL 58, APPROX 28 IN ABOVE FLOOR LINE WITH CRACK IN WEB. STOP DRILLED AND INSTALLED DOUBLER. INSTALLED NEW WEB PER MO 72J15, PHASE K, PER DRAWING 4709532 REV A, AND 5936993 REV D.Jul 20, 1998 · N995Z · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9812004Bulkhead Doubler · corrodedDURING OP 16 MAINT CHECK, FOUND SPAR WEB DOUBLER ON AFT SIDE OF BULKHEAR WEB, STA 965 RT SIDE, CRACKED. REPAIRED WITH .090 DOUBLER 2024-T3 AND INSTALLED PER MO 72J15, PHASE K AND DAC DRAWING 4709532 AND 5936993.Jul 20, 1998 · N995Z · Doug DC932 · Fuselage Main, BulkheadSDR CALA9801319Fitting · crackedINSPECTION FOUND A .375 INCH CRACK IN AFT CARGO DOOR NR 2 BEAM AFT END FITTING. A NEW FITTING WAS INSTALLED IAW SRM 51-30-1 AND 51-30-5.Jul 20, 1998 · N14534 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9801283Skin · crackedINSPECTION FOUND A 1 INCH CRACK COMING FROM RIVET HOLE IN FORWARD CARGO DOOR AT STA 425. THE CRACK WAS STOP DRILLED, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 52-03, 52-31-0 AND 51-70-2.Jul 20, 1998 · N18544 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9801282Floor Panel · delaminatedINSPECTION FOUND FLOOR PANEL DELAMINATED AT STA 756 TO 680. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-05 AND 51-10-3.Jul 20, 1998 · N18544 · Doug DC932 · Fuselage Floor PanelSDR ABXA9800743Web · crackedDURING C-CHECK, FOUND CUSP WEB CRACKED AT FS 990 LONGERON 18L. REPLACED CUSP WEB IAW REA D 953 24241 MR.Jul 20, 1998 · N983AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800741Angle · crackedDURING C-CHECK, FOUND ANGLE ON FORWARD SIDE OF PRESSURE PANEL CRACKED. REPLACED ANGLE ON FORWARD SIDE OF PRESSURE PANEL IAW DC9 SRM 51-30-2 AND 51-30-5.Jul 20, 1998 · N983AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800740Cusp Web · crackedDURING C-CHECK, FOUND CUSP WEB CRACKED AT LONGERON 18R FS 965. REPLACED CUSP WEB IAW ABX REA D 953 24241 MR.Jul 20, 1998 · N983AX · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800373Intercoastal · corrodedINTERCOASTAL STA 813-832 LONG 27L HAS CORROSION. REMOVED INTERCOASTAL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. FABBED NEW INTERCOASTAL 18.5 BY 5 USING 7075 -0 .040 IAW DC-9 SRM 53-11-3. HEAT TREATED IAW SRM 51-10-2A. TREATED AND PRIMED IAW SRM 51Jul 19, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800370Intercoastal · corrodedINTERCOSTAL STA 851-870 LONG 27L AND BUBBLED ON LONG. REMOVED INTERCOSTAL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1. FABBED NEW INTERCOASTAL 18 1/8 BY 5 USING 7075-0-.050 IAW DC-9 SRM 51-10-2 AND 53-11 FIG 3A. HEAT TREATED IAW SRM 51-10-2A. TREATEDJul 19, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800254Intercostal · corrodedINTERCOSTAL STA 851-870 LONG 27L IS CORRODED AND BUBBLED ON LONGERON. REMOVED INTERCOSTAL AND FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. FABBED NEW INTERCOSTAL 18 1/8X5 USING 7075-0.050 IAW SRM 51-10-2 AND 53-11 FIG 3A. HEAT TREATED IAW DC-9 SRM 51Jul 19, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800242Intercoastal · corrodedDURING C CHECK, FOUND INTERCOSTAL STA 813 - 832 27L HAS CORROSION. REMOVED INTERCOSTAL AND FOUND IT TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. FABBED NEW INTERCOASTAL 18.5 X 5 USING 7075-0-.040 IAW DC-9 SRM 51-10-3. HEAT TREATED IAW DC-9 SRM 51-10-2A. TJul 19, 1998 · N912VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800230Cover · detachedGALLEY DOOR SLIDE COVER DISLODGED. RETURNED TO GATE AND REINSTALLED SLIDE PACK COVER AND PERFORMED REQUIRED INSPECTIONS.Jul 19, 1998 · N933VV · Doug DC932 · Emergency EquipmentSDR VJ9800250Bracket · corrodedCORROSION DUST/PARTICLES EMANATING FROM UNDER I/B WASS OF FWD LAV, AFT OF DOOR CORROSION LEVEL 2. REPLACED CORRODED BRACKET UNDER I/B WALL OF FWD LAV, AFT OF DOOR AND ASSEMBLED COMPONENTS IAW DC-9 MM 25-42-1.Jul 18, 1998 · N902VJ · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800249Frame · corrodedAFT PIT FRAME SPLICE STA 938 28L IS CORRODED. CORROSION FOUND BEYOND SRM LIMITS, FABBED REPAIR REQUIRED. REMOVED FRAME SPLICE, FABBED REPAIR FRAME SPLICE OUT OF 7075-0.063 P NR 1A-34396-1. HEAT TREATED TO T-6. TREATED AND PRIMED REPAIR. INSTALLED REPAIR FJul 18, 1998 · N902VJ · Doug DC932 · Fuselage Main, FrameSDR VJ9800234Bracket · corrodedCORROSION DUST PARTICLES EMANATING FROM UNDER I/B WAS OF FWD LAVATORY AFT DOOR. THE CORROSION WAS FOUND TO BE LEVEL 2. REPLACED CORROSION BRACKET UNDER I/B WALL OF FED AV AFT DOOR AND ASSEMBLED COMPONETS IAW DC-9 MM 25-42-1.Jul 18, 1998 · N902VJ · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800229Power Supply · inoperativeRT EMERGENCY OVERWING LIGHT INOP. REPLACED EMERGENCY POWER SUPPLY.Jul 18, 1998 · N922VV · Doug DC932 · Emergency LightingSDR VJ0900247Bracket · corrodedDURING C CHECK, FOUND DUST/PARTICLES EMANATING FROM UNDER I/B WAS OF FWD LAV AFT OF DOOR CORROSION LEVEL 2. REPLACED CORROSION BRACKET UNDER I/B WALL OF FWD LAV, AFT DOR AND ASSEMBLED COMPONENTS IAW DC-9 MM 25-42-1.Jul 18, 1998 · N902VJ · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801268Support · crackedINSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STA 294, STRINGER 27R. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2 AND THE CRACK WAS STOP DRILLED IAW ECRA 5320-01263. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 532Jul 18, 1998 · N18544 · Doug DC932 · Fuselage Miscellaneous Structure
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