Douglas DC-9-33F
Service difficulty reports · 1,681
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 = 'DC933F' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR EIAA980201Fitting · misdrilledDURING 'C5' CHECK, HORIZONTAL STABILIZER CENTER SECTION UPPER AFT FITTING HAS CORROSION. DURING REPLACEMENT, FITTING WAS MISDRILLED. REPLACED FITTING AND REPAIRED AREA IAW ECRA 944-55-033-02. (X)SDR EIAA980197Fitting · crackedMZJ - DURING 'C5' CHECK, RIGHT HAND BODY TO CENTER TANK ATTACH FITTING CRACKED AT BS 579. REPLACED FITTING PER SRM 51-10-03. (X)SDR EIAA980196Frame · crackedMZJ - DURING 'C5' CHECK, AFT ACCY COMPARTMENT, CANTED FRAME CRACKED AT BS 1104, STR 20L. REPLACED CANTED FRAME FROM STR 11L- STR 22L PER SRM'S 51-10-3 AND 51-30-05. (X)SDR ABXA9800360Line · rupturedRIGHT HYDRAULIC FLUID QUANTITY DROPPED TO 0. REPAIRED HYDRAULIC LINE AT THE AUXILIARY PUMP FILTER, OPS CHECKED GOOD IAW DC9 MM.SDR TWAA9806703Former · bentMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 503 FORMER BENT AT UPPER AREA OF WINDOW BELT. REPAIRED PER SRM 53-03, PAGE 5, FIG 4. (M)SDR TWAA9806708Bulkhead Clip · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AFT PRESSURE BULKHEAD AT RADIAL 16L, OUTBOARD END CLIP WITH .5 INCH CRACK RUNING FROM EDGE OF CLIP TO FIRST FASTENER HOLE. REPLACED CLIP AT RADIAL 16L, AFT PRESSURE BULKHEAD, PER SRM 51-01, PAGE 1 ITEM C, AND TWA STSDR TWAA9806707Angle · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND ATTACH ANGLE ON FWD FACE OF FORMER TO FORMER FOOT CORRODED AT FS 937, LONGERON 27L TO 28L. INSTALLED NEW ANGLE PER SRM 51-01 PAGE 1 ITEM C. (M)SDR TWAA9806702Former · crackedDURING OP 16 MAINTENANCE CHECK, FOUND FS 370 FORMER CRACKED ABOVE LONGERON 9R, APPROX .75 INCH LONG. REPLACED FORMER SECTION PER SRM 51-01, PAGE 1 ITEM C, AND TWA STANDARD PRACTICES. (M)SDR TWAA9806701Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 180 LONGERON 4L WITH CRACK .75 INCH LONG. SPLICED IN SECTION OF LONGERON PER SRM 53-02, FIG 18. (M)SDR TWAA9806802Doubler · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION AT FS 937, AFT FACE OF FORMER DOUBLER, ABOVE L28L TO 29L. REMOVED CORROSION PER SRM 51-10-3. INSTALLED NEW DOUBLER PER SRM 51-01, PAGE 1 ITEM C. (M)SDR TWAA9806504Doubler · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AFT FACE OF FORMER DOUBLER AT FS 937 CORRODED ABOVE L28L TO 29L. REMOVED CORROSION PER SRM 51-10-3. INSTALLED NEW DOUBLER PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)SDR ABXA9800324Trim · out of positionCAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. REPOSITIONED WINDOW TRIM.SDR TWAA9806806Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND UPPER FUSELAGE DENT IN FUSELAGE SKIN 3.5 INCH IN BY 2 INCH IN BY .100 DEEP, AT FS 273, JUST ABOVE STRINGER 17L. VERIFIED NO CRACK WITH NDT TEST. REPAIRED PER SRM 53-04, FIG 38. (M)SDR TWAA9806803Former · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON AFT FACE OF FORMER FS 965, BETWEEN L29L AND 29R. REMOVED CORROSION AND REPAIRED PER SRM 53-04, PAGE 4. (M)SDR TWAA9806706Angle · crackedMCI - DURING OP16 MAINTENANCE CHECK, FOUND LEFT FWD OVERWING EXIT ANGLE CRACKED AS SEEN THROUGH UPPER AFT 1 INCH BY 5 INCH INSPECTION SLOT. MADE AND INSTALLED NEW CLIP WITH HI-LOCK PER SRM 51-30-0. (M)SDR TWAA9806503Former · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON AFT FACE OF FORMER FS 965 BETWEEN LONGERONS 29L AND 29R. REMOVED CORROSION AND REPAIRED PER SRM 53-03, PG 4. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X)SDR ABXA9800326Switch · defectiveGEAR DOOR OPEN LIGHT ILLUMINATED DURING UPLATCH CHECK. RECYCLED GEAR, LIGHT EXTINGUISHED. UPLATCH CHECK OK. REPLACED THE LEFT MAIN LANDING GEAR DOOR POSITION SWITCH.SDR TWAA9806807Skin · crackedMCI - DURING OP16 MAINTENANCE CHECK, FOUND .5 INCH CRACK IN FUSELAGE SKIN RUNNING FROM AFT LOWER CORNER OF A CUTOUT FOR 1.375 INCH IN BY 3 INCH REPAIR, STATION 220 ONE INCH ABOVE S17L. CRACK DOES NOT RUN INTO RIVET HOLE. CUTOUT DAMAGE AND ADDED DOUBLER AND FSDR TWAA9806804Former · damagedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND HOLE AT STATION 313 FORMER L9R. MADE METAL REPAIR ON FORMER PER SRM 53-03, PAGE 5 FIG 4, FORMER STATION 313. (M)SDR TWAA9806710Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT FS 917, ATTACH ANGLE ON FWD FACE OF FORMER TO FLOOR SUPPORT, BETWEEN LONGERON 27L AND 28L, WAS CRACKED AND CORRODED. REPLACED ANGLE PER SRM 51-01, PAGE 1, ITEM C AND TWA STD PRACTICE. (M)SDR TWAA9806709Angle · crackedDURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING CRACK INSIDE REAR FLAP ON SUPPORT ANGLE FOR OUTBOARD HINGE, CRACKED ON BOTH INBOARD AND OUTBOARD SIDES. REMOVED AND REPLACED INBOARD AND OUTBOARD SUPPORT ANGLES FOR OUTBOARD HINGE, PER SRM 51-01, ITEM C, AND TWASDR TWAA9806805Skin · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING SKIN CRACKED 12 INCH INBOARD OF INBOARD SIDE OF INBOARD SPOILER AT REAR SPAR UPPER TE. SKIN WAS CRACKED ONE IN LONG. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-01, FIG 3 SHEET 2. (M)SDR TWAA9806808Skin · damagedMCI - DURING OP16 MAINTENANCE CHECK, FOUND AFT END OF AFT CARGO DOOR CUTOUT SKIN DAMAGED BELOW LONGERON 24R. REPAIRED PER SRM 53-05, FIG 80. (M)SDR EIAA980195Support · crackedMZJ - DURING 'C5' CHECK, AFT PIT, FLOOR SUPPORT FRAME CRACKED AT BS 832 FROM STR 26L - STR 27L. REPAIRED FLOOR SUPPORT PER DPS 10-225. (X)SDR EIAA980188Fitting · crackedMZJ - DURING 'C5' CHECK, ATTACH FITTING IN LOWER WING TO FUSELAGE FILLET AREA AT BS 604 AT LBL 39, HAS 2 INCH CRACK. REPLACED FITTING PER SRM 51-30-5. (X)SDR EIAA980181Support · crackedMZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 427 AT STR 26. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X)SDR EIAA980180Support · crackedMZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 390 AT STR 26. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X)SDR EIAA980193Support · crackedMZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED AT BS 832 FROM STR 27R TO STR 28R. REPAIRED FLOOR SUPPORT PER DPS 10-255. (X)SDR EIAA980192Support · crackedMZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED AT BS 794 FROM STR 29L TO STR 28L. REPAIRED FLOOR SUPPORT PER DPS 10-255. (X)SDR EIAA980191Fitting · crackedMZJ - DURING 'C5' CHECK, FRAME ATTACH FITTING CRACKED AT BS 256 AT STR 24R. REPLACED FRAME ATTACH FITTING PER SRM'S 51-30-02 AND 51-10-03. (X)SDR EIAA980190Stiffener · crackedMJZ - DURING 'C5' CHECK, BS 796 BULKHEAD LOWER STIFFENER IS BENT AT BL ZERO. REPLACED STIFENER PER SRM'S 51-10-03 AND 51-30-05. (X)SDR EIAA980189Frame · crackedMJZ - DURING 'C5' CHECK, FUSELAGE FRAME LOWER CHORD CRACKED AT BS 275 FROM STR 29L - STR 29R. REPAIRED FRAME PER SRM 53-03, FIG 5. (X)SDR EIAA980187Frame · crackedMZJ - DURING 'C5' CHECK, AFT PIT, FLOOR SUPPORT FRAME AT BS 965 LONGERON 30 CRACKED AND CORRODED. REPAIRED FRAME PER SRM 53-03 PAGES 4A-4J. (X)SDR EIAA980186Intercostal · crackedMZJ - DURING 'C5' CHECK, AFT PIT, LONGERON INTERCOSTAL CRACKED AND CORRODED AT BS 937 AT LONGERON 29R. REPLACED INTERCOSTAL ON LONGERON 29R PER SRM 51-30-02. (X)SDR EIAA980185Support · crackedMZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 256 AT STR 29R. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X)SDR EIAA980183Support · crackedMZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 351 FROM STR 25R - STR 26R, AND STR 28R - STR 29R. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X)SDR EIAA980182Support · crackedMZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 313 AT STR 25L AND STR 26L. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X)SDR EIAA980179Support · crackedMZJ - DURING 'C5' CHECK, AFT PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 851 AT STR 24L TO STR 25LR. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X)SDR EIAA980178Support · crackedMZJ - DURING 'C5' CHECK, AFT PIT, FLOOR SUPPORT FRAME ATTACH FITTING CRACKED IN UPPER CHORD RADIUS AT BS 794 AT STR 28R. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X)SDR EIAA980177Support · crackedMZJ - DURING 'C5' CHECK, AFT PIT FLOOR SUPPORT FRAME CRACKED AT BS 965 AT STR 30. REPAIRED FLOOR SUPPORT FRAME PER SRM 53-03 FIG 2A. (X)SDR EIAA980176Fitting · crackedDURING 'C5' CHECK, FRAME ATTACH FITTING CRACKED AT BS 256 AT STR 24R. REPLACED FRAME ATTACH FITTING PER SRM 51-10-03. (X)SDR EIAA980175Stringer · crackedDURING 'C5' CHECK, LONGERON 16L CRACKED AT BS 963. REPAIRED LONGERON AT BS 963 PER SRM 53-02 FIG 18. (X)SDR EIAA980194Longeron · crackedMZJ - DURING 'C5' CHECK, LONGERON 16L CRACKED AT BS 963. REPAIRED LONGERON PER SRM 53-02 FIG 18. (X)SDR ABXA9800253Window · lack of lubeCAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT ) WOULD NOT OPEN. RELEASED UPPER LOCK BAR, CLEANED AND LUBRICATED LINKAGE. OPS CHECKED GOOD.SDR ABXA9800030Blkhd Stiffener · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT STA 996 AND LONGERON 14R LOWER FLANGE CRACKED. REPAIRED STIFFENER IAW DC9 S/B 53-166, SERVICE REWORK DWG J060110 VIEW V-V AND DACO DWG PL 9915558.SDR ABXA9800029Blkhd Stiffener · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT 996 AND LONGERON 14L LOWER FLANGE CRACKED. REPAIRED STIFFENER IAW DC9 S/B 53-166, SERVICE REWORK DWG J060110 VIEW V-V AND DACO DWG PL 9915558.SDR ABXA9800028Cusp Web · crackedDURING C-CHECK, FOUND RIGHT CUSP WEB AT FS 955 CRACKED APPROX 4 LONG. REPAIRED CUSP WEB IAW ABX REA D953-22256.SDR ABXA9800033Trap Panel · corrodedDURING C-CHECK, FOUND LEFT TRAPEZODIAL PANEL UPPER HORIZONTAL FLANGE EXFOLIATED AND CRACKED. REPLACED TRAPEZODIAL PANEL IAW DC9 S/B 53-182 AND DC9 SRM 51-30-1.SDR ABXA9800032Fitting · corrodedDURING C-CHECK, FOUND THE LEFT PORK-CHOP FITTING CORRODED. REPLACED FITTING IAW DC9 S/B 53-182 AND DC9 SRM 51-30-1.SDR ABXA9800031Floorbeam · corrodedDURING C-CHECK, FOUND FLOORBEAM LOWER FLANGE CORRODED AT STA 937, BL 0.0. REPAIRED FLOORBEAM IAW ABX REA D53-22192MR.
Back to Douglas DC-9-33F