Douglas DC-9-32

Service difficulty reports · 12,755

Newest first. General aviation reporting is voluntary.

Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR MWEA00854Web · corrodedLIGHT CORROSION ON RIGHT HAND FLOOR WEB FROM STATION 237 - 256. FABRICATED AND INSTALLED REPAIR SECTION.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00853Support Bracket · crackedFLOORBOARD SUPPORT BRACKET HAS CHAFE MARKS, CORROSION, AND A CRACK AT STATION 465 BETWEEN CENTER INTERCOSTAL AND NR 2 SEAT TRACK. REMOVED AND REPLACED SUPPORT BRACKET.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00852Web · crackedCABIN FLOOR WEB CRACKED AT STATION 380 OUTBOARD OF NR 4 SEAT TRACK. FABRICATED AND INSTALLED REPAIR DOUBLER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00851Angle · crackedZ ANGLE FLOOR SUPPORT CRACKED AND CHAFED IN SEVERAL PLACES AT STATION 313 BETWEEN CENTER INTERCOSTAL AND SEAT TRACK NR 3. REMOVED AND REPLACED Z ANGLE.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00850Web · chafedRIGHT HAND FLOOR WEB HAS LITE CHAFE DAMAGE FROM STATION 294 - 313. FABRICATED AND INSTALLED REPAIR DOUBLER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00849Floorbeam · chafedFLOOR SUPPORT AND BEAM AT STATION 522 HAVE CHAFE DAMAGE BETWEEN NR 2 SEAT TRACK AND CENTER FLOOR SUPPORT. FABRICATED AND INSTALLED WEAR STRIP REPAIR.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA00848Angle · crackedZ-ANGLE FLOOR SUPPORT CRACKED AND IS CHAFED AT STATION 313 INBOARD OF SEAT TRACK NR 2. REMOVED AND REPLACED Z-ANGLE FLOOR SUPPORT.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00847Web · crackedLEFT HAND FLOOR WEB CRACKED AT STATION 598. FABRICATED AND INSTALLED REPAIR DOUBLER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00846Web · crackedLEFT HAND SUBFLOOR WEB CRACKED IN RADIUS AROUND LIGHTNING HOLE AT STATION 832. FABRICATED AND INSTALLED REPAIR DOUBLER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00845Web · misdrilledLEFT HAND SUBFLOOR WEB, 2 MISDRILLED HOLES AT STATION 832 UNDER OUTBOARD PHENOLIC SUPPORT ANGLE. FABRICATED AND INSTALLED REPAIR DOUBLER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00844Floorbeam · chafedCABIN FLOORBEAM STATION 598 JUST OUTBOARD OF CENTER FLOORBEAM CHAFED BEYOND LIMITS. INSTALLED FLOORBEAM REPAIR PER BOEING TELEX-MWX-ORD-00-00451H.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA00843Intercostal · gougedGOUGES ON INTERCOSTAL FROM STATION 365 TO 370 RIGHT OF LONGERON 30. FABRICATED AND INSTALLED INTERCOSTAL WEB REPAIR.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00840Stiffener · crackedAFT PRESSURE BULKHEAD, FORWARD STIFFENER BELOW LONGERON NR 1 HAS A CRACK AT TOP HOLE. FABRICATED AND INSTALLED REPAIR DOUBLERS.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00837Bracket · crackedFOUND BRACKET AT STATION 367, LONGERON 30 TO BE CRACKED. REMOVED AND REPLACED BRACKET.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA00836Frame · gougedLEFT FUSELAGE, GOUGE ON FRAME AT STATION 560 AT LONGERON 11 LEFT. FABRICATED AND INSTALLED FRAME REPAIR.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00835Frame · misdrilledFRAME AT STATION 908 HAS 2 INSTALLED RIVETS WITH NO EDGE DISTANCE AT LONGERON RIGHT 8. FABRICATED AND INSTALLED FRAME REPAIR.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00834Frame · crackedSTATION 484 FRAME CRACKED AROUND 3 FASTENERS LONGERON 6 RIGHT ON FORWARD SIDE. REMOVED AND REPLACED FRAME.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA00833Skin · tool damageDRILL MARKS ON APB SKIN WHERE SKIN ATTACHES TO APB TEE AT STATION 996. REPAIRED DRILL STARTS (3) PER BOEING ENGINEERING TELEX 8/30/00.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA001038Frame · misdrilledSTATION 929 FRAME RIGHT HAND SIDE IN BETWEEN LONGERON 4 AND 5 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001037Frame · misdrilledSTATION 929 FRAME LEFT HAND SIDE IN BETWEEN LONGERON 4 AND 5 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BEOING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001035Frame · misdrilledSTATION 929 FRAME LEFT HAND SIDE IN BETWEEN LONGERON 5 AND 6 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001034Frame · misdrilledSTATION 832 FRAME LEFT HAND SIDE IN BETWEEN LONGERON 5 AND 6 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001033Frame · misdrilledSTATION 813 FRAME RIGHT HAND SIDE IN BETWEEN LONGERON 5 AND 6 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001032Frame · misdrilledSTATION 870 FRAME RIGHT HAND SIDE IN BETWEEN LONGERON 5 AND 6 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001031Frame · misdrilledSTATION 870 FRAME LEFT HAND SIDE IN BETWEEN LONGERON 5 AND 6 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001030Frame · misdrilledSTATION 851 FRAME RIGHT HAND SIDE IN BETWEEN LONGERON 4 AND 5 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001029Frame · misdrilledSTATION 851 FRAME RIGHT HAND SIDE IN BETWEEN LONGERON 5 AND 6 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001028Frame · misdrilledSTATION 832 FRAME RIGHT HAND SIDE IN BETWEEN LONGERON 4 AND 5 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001026Frame · misdrilledSTATION 794 FRAME LEFT HAND SIDE IN BETWEEN LONGERON 4 AND 5 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001025Frame · misdrilledSTATION 794 FRAME LEFT HAND SIDE IN BETWEEN LONGERON 5 AND 6 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001024Frame · misdrilledSTATION 775 FRAME RIGHT HAND SIDE IN BETWEEN LONGERON 5 AND 6 HAS A GROUP OF PLUG RIVETS WITH IMPROPER SPACING. FABRICATED AND INSTALLED FRAME REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, FrameSDR MWEA001023Skin · damagedELONGATED HOLES IN SKIN AT STATION 1019 AT LONGERON 15 RIGHT. INSTALLED SKIN REPAIR PER BOEING ENGINEERING APPROVED REPAIR SCHEME 00-10-03-011.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA001022Skin · tool damageFUSELAGE SKIN AT LONGERON 6 RIGHT FORWARD OF APB HAS THREE DRILL MARKS. FABRICATED AND INSTALLED SKIN REPAIR DOUBLER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA001021Skin · dentedFUSELAGE SKIN DENT AT STATION 955 AT LONGERON 26 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA001020Skin · crackedFUSELAGE SKIN CRACKED IN AFT ACC COMPARTMENT RIGHT HAND SIDE AT STATION 1038 LONGERON RIGHT 18. FABRICATED AND INSTALLED REPAIR DOUBLER.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA001018Skin · damagedSTATION 83 RIGHT HAND LOWER SIDE OF CENTER COCKPIT WINDOW HAS 2 OVERSIZED HOLES THAT ARE PRESENT THROUGH SKIN. INSTALLED BUSHING REPAIR PER BOEING ENGINEERING TELEX.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA001017Skin · dentedFUSELAGE SKIN DENTED IN 3 AREAS BELOW GALLEY SERVICE DOOR AREA AT STATION 114 AND LONGERON 19 RIGHT, STATION 156 AND LONGERON 19 RIGHT, STATION 170 AND LONGERON 19R. FABRICATED AND INSTALLED REPAIR DOUBLERS.Oct 20, 2000 · N302ME · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000495Skin · corrodedDURING A SCHEDULED INSPECTION, FOUND CORROSION BEYOND LIMITS AT BS 541-560 L30. SKIN REPAIR WAS INSTALLED IAW DC9 SRM 51-30-02, 51-30-05, 51-10-03, AND 53-04 FIG 12B.Oct 19, 2000 · N807AT · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0017403Floor Panel · corrodedDURING OP 15 MAINT CHECK IN THE FWD CABIN, THE FLOOR MEMBRANE HAD CORRODED AND WORN AT STA 160 TO 200, LBL 44 INCHES. REMOVED MEMBRANE AND FABRICATED NEW PART PER DRAWING AA9910078 AND SRM 51-30-3. INSTALLED PER SRM 51-30-0 AND 51-10-4 OF SRM.Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Floor PanelSDR TWAA0016412Web · corrodedDURING OP 15 MAINT CHECK THE FWD CABIN FLOOR MEMBRANE WAS CORRODED AND WORN AT STA 200 TO STA 160, LBL 44 TO LBL 56. REMOVED MEMBRANE AND FABRICATED NEW PART PER DRAWING 9910078 AND SRM 51-30-3. INSTALLED PER SRM 51-30-0 AND 51-10-4.Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Floor PanelSDR TWAA0016411Web · crackedDURING OP 15 MAINT CHECK THE FWD CABIN FLOOR MEMBRANE WAS CORRODED THROUGH AND CRACKED AT STA 160, LBL 2. REMOVED AND REPLACED PART PER DRAWING 9910078. INSTALLED PART PER SRM 51-30-0.Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016410Floor Support · corrodedDURING OP 15 MAINT CHECK IN THE FWD CABIN CORROSION WAS FOUND ON THE FLOOR SUPPORT AT STA 218, LBL 0 TO LBL 44. REMOVED FLOOR SUPPORT. FABRICATED NEW PART PER DRAWING 9910078. INSTALLED PER SRM 51-30-0 AND SRM 51-10-4.Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016409Floor Support · corrodedDURING OP 15 MAINT CHECK IN THE FWD CABIN, THE FLOOR SUPPORT WAS CORRODED AT STA 200 TO 237, LBL 14. REMOVED AND REPLACED FLOOR SUPPORT PER DRAWING 9910078. INSTALLED PER SRM 51-30-0.Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016408Floor Support · corrodedDURING OP 15 MAINT CHECK IN THE FWD CABIN THE FLOOR SUPPORT AT STA 160 TO 200, AT LBL 56, HAD CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER DRAWING 9910078. INSTALLED NEW PART PER SRM 51-30-0.Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016407Floor Support · corrodedDURING OP 15 MAINT CHECK IN THE FWD CABIN THE FLOOR SUPPORT AT STA 160 TO 200, LBL 44, WAS CORRODED. REMOVED FLOOR SUPPORT. FABRICATED NEW PART PER DRAWING 9910078 AND SRM 51-10-3. INSTALLED PER SRM 51-30-0 AND 51-10-2.Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA0016406Frame · corrodedDURING OP 15 MAINT CHECK, THE FRAME AT THE LAST LT WINDOW, AFT SIDE OF WINDOW CUT AT STA 918 TO 935 HAD CORROSION ON THE FLOOR WEB TO FUSELAGE SKIN. CUT OUT CORROSION PART OF FLOOR WEB PER SRM 51-70-4 FIG 2. REPAIRED WEB AREA PER SRM 57-70-04 FIG 2.Oct 19, 2000 · N996Z · Doug DC932 · Fuselage Main, FrameSDR TWAA0017402Skin · corrodedDURING OP 15 MAINT CHECK ON THE AFT FUSELAGE, LONGERON 20L TO 21L, STA 965, THE TOP AFT CORNER OF THE PRESSURE OUTFLOW CONTROL VALVE CUTOUT HAD CORROSION, 4 INCH BY 5. REPLACED THE LT FUSELAGE SKIN FROM STA 784 TO 996, LONGERON 18 TO 26L, PER DRAWING 5911423.Oct 18, 2000 · N996Z · Doug DC932 · Fuselage Main, Plate/SkinSDR 0003999940Attach Angle · crackedDURING L-CHECK, FOUND CRACK IN RIGHT HAND PYLON UPPER ATTACH ANGLE AT BS 996. REPAIRED PER EA 99-17403 AND SRM 54-04 FIGURE 10. REF LOG PAGE 1510889.Oct 18, 2000 · N3322L · Doug DC932 · Nacelle/Pylon, Main FrameSDR ABXA000474Vane · delaminatedLEFT FLAP INBOARD FIXED VANE WAS DELAMINATED 280 SQ IN ON UPPER SURFACE AND 145 SQIN ON LOWER SURFACE. REPLACED FIXED VANE IAW DC9 MM.Oct 18, 2000 · N901AX · Doug DC932 · Trailing Edge FlapsSDR TWAA0016405Membrane · crackedDURING OP 15 MAINT CHECK, THE MEMBRANE WAS CRACKED AT STA 892, RT SIDE. INSTALLED NEW MEMBRANE PER SRM 51-01 AND SRM 51-30-02.Oct 18, 2000 · N996Z · Doug DC932 · Fuselage Miscellaneous Structure
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