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.
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
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 CALA9801267Intercostal · crackedINSPECTION FOUND TWO CRACKS IN INTERCOSTAL AT STA 996 TO 1019, RBL 20. THE CRACKS WERE STOP DRILLED, AN ANGLE STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-01, 51-30-2, AND 51-30-0.SDR CALA9801266Skin · damagedINSPECTION FOUND LIGHTNING STRIKE DAMAGE TO SKIN BELOW FLOOR LINE AT WING SCAN LIGHT AT STA 522. A DOUBLER AND FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38.SDR VJ9800272Cargo Track · corrodedFORWARD LT CARGO TRACK CORRODED BEYOND LIMIT AT STA 270-390. REMOVED CORROSION IAW DC9 SRM 53-01, FIG 1, AND FABRICATED TIE DOWN TRACK MATERIAL, 102 1/2 BY 1 INCH, IAW DC9 SRM 53-21-0. TREATRED CARGO TIE DOWN TRACK IAW DC9 SRM 51-10-3.SDR VJ9800233Cargo Track · corrodedFWD CARGO LT STA 270-390 HAS SURFACE CORROSION. MECH REMOVED CORROSION 100 PERCENT BEYOND LIMITS IAW DC-9 SRM 53-01 FIG 1. FABBED CARGO TIE DOWN TRACK MATERIAL 2955978-1200 102.5 BY 1 IAW DC9 SRM 51-10-3.SDR VJ9800228Duct · failedNR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF, THROTTLE RETARDED AND LIGHT EXTINGUISHED. CREW ELECTED TO RETURN TO ATL MAINTENANCE BASE. INSPECTED AIRCRAFT AND FOUND BLOWN DUCT. REPLACED NR 2 ENGINE NOSE COWL ANTI-ICE DUCT, RAN ENGINE AND NO LEAKSDR TWAA9812302Former · corrodedDURING OP 16 MAINT CHECK, FOUND FORMER CORRODED AT INBD ANGLE STA 1038, BETWEEN S15R AND S17R. CORROSION GROUND TO A DEPTH OF .090. REMOVED CORROSION PER SRM 51-10-3. REPAIRED FORMER 1038 PER ARA 15366A. INSTALLED FORMER 2014-T6 L ANGLE WITH HI-LOCKS.SDR TWAA9812009Skin · wornDURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN WORN AT LONGERON 26L, STA 815, UNDER FUSELAGE FAIRING. TRIMMED DAMAGED AREA WHICH IS FOR A LAP SEAM. INSTALLED REPAIR PER SRM 53-04 FIG 12B.SDR TWAA9812008Intercostal · crackedDURING OP 16 MAINT CHECK, FOUND INTERCOASTAL CRACKED AT AFT END OF PULLEY CLUSTER AT STA 1010, RBL 20 INCHES. NEW SUPPORT FABRICATED IN SHOP PER DRAWING 9915540, DRILLED NEW PART AND INSTALLED AND SEALED PER SRM 53-03.SDR TWAA9812007Frame · crackedDURING OP 16 MAINT CHECK, FOUND FRAME WITH APPROX 1 IN CRACK AT STA 980, LONGERON 17R. ACCOMPLISHED FRAME REPAIR BY CUTTING DAMAGED SECTION OUT BETWEEN L14R AND L16R, AND FLOOR LINE. INSTALLED NEW SECTIONS OF FRAME AND SPLICED PER SRM 53-03, FIG 32, SHEETS 1SDR TWAA9812006Skin · damagedDURING OP 16 MAINT CHECK, FOUND LT HORIZ STAB, LEADING EDGE OF STAB DAMAGED AND FILLET DETERIORATED APPROX 20 IN FROM O/B END. INSTALLED DOUBLER PER SRM 55-03, FIG 3 PG 5.SDR CALA9801271Frame · corrodedINSPECTION FOUND BELTFRAME CORRODED AT STA 895, LONGERON 18L. THE CORRODED SECTION OF FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9801270Frame · crackedINSPECTION FOUND A 5 INCH CRACK IN BELTFRAME AT STA 446, LONGERON 5L. THE BELTFRAME WAS REPAIRED IAW SRM 53-03, FIGURE 4.SDR CALA9801265Floor Panel · separatedINSPECTION FOUND FLOOR PANEL SKIN SEPARATING AT STA 579 TO 680. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, PAGE 11 AND 53-05, PAGE 122B.SDR CALA9801264Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 980, RBL 21 AND RBL 34. THE CORRODED AREAS WERE CUT OUT, AN ANGLE, FILLER, AND SHIM WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 20A.SDR CALA9801263Stringer · corrodedINSPECTION FOUND STRINGER/FRAME CORRODED AROUND FASTENERS AT KEEL BOX INTERIOR, STA 598, STRINGER 29R. THE KEEL BOX WEB WAS REMOVED. TWO REPAIR ANGLES WERE FABRICATED IAW SRM 53-01, FIGURE 2 AND 51-10-2A. THE ANGLES AND KEEL BOX PANEL WERE INSTALLED IAW SRM SDR ABXA9800742Frame · crackedDURING C-CHECK FOUND CRACKED FRAME FS 965 LONGERON 15L. REPLACED FRAME SECTION FS 965 LONGERON 15L IAW DC9 SRM 53-03.SDR TWAA9811506Bulkhead · crackedDURING OP 16 MAINTENANCE CHECK AT STA 965, THE BULKHEAD WEB HAD 2 EACH CRACKS APPROX 2 INCHES LONG AT WL 200, JUST INBD OF LONGERON 18R. REPLACED FULL BULKHEAD WEB WITH SAME AS ORIGINAL .032 INCH 7075T6 ALUMINUM MATERIAL. ATTACHED WITH MS L0470AD RIVETS AND SDR CALA9801261Angle · corrodedINSPECTION FOUND FLOOR GILL LINING ATTACH ANGLE CORRODED IN AFT CARGO COMPARTMENT AT STA 996, BL 0 TO LBL 6. THE CORRODED SECTION OF ANGLE WAS CUT OUT. TWO L-ANGLES AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30SDR VJ9800226Battery Pack · dischargedFWD OVERWING EMERGENCY LIGHTS OUT. REPLACED FWD OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY IAW 33-50; OPS CHECKED GOOD.SDR VJ9800225Connector · dirtyFIRE LOOP B LIGHT ILLUMINATED ON NR 1 ENGINE WITHOUT ANY OTHER WARNING BEING EVIDENCED. FOLLOWED PROCEDURES AND TESTED OPPOSITE LOOP WHICH TESTED GOOD. AIRCRAFT LANDED WITHOUT INCIDENT AND UPON INSPECTION OF BLEED AIR DUCTS NO LEAKS WERE DETECTED. ALSO, INSSDR TWAA9812003Frame · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 965, FORMER S29L TO S29R. SPLICE REPAIRED FORMER PER SRM 53-03, FIG 2A.SDR TWAA9812002Skin · crackedDURING OP 16 MAINT CHECK, FOUND A CRACK IN FUSELAGE SKIN LEFT SIDE JUST BELOW THE LEFT PYLON STA 965. AREA HAD AN INTERIM REPAIR WITH BLIND FASTENERS. ACCOMP EDDY CURRENT AND NO CRACKS FOUND, REF 51-00-03. INSTALLED DOUBLER PER SRM 53-04, PAGE 93.SDR TWAA9811909Longeron · corrodedDURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 24L WITH INNER GRANULAR CORROSION ON ATTACH FITTING AT FWD SIDE OF FS 996. REMOVED CORROSION PER SRM 51-10-03, STEP 35, PAGE 21. ALODINED AND PRIMED PER TWA STD PROCEDURES. INSTALLED NEW ATTACH FITTING PER SRM SDR TWAA9811504Skin · defectiveDURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE UPPER AND LOWER SKIN THICKNESS MEASURED BY NDT WAS .024 INCH. SKIN THICKNESS IS .063 INCH AT STA 815, L26R. REPAIRED SKIN PER SRM 53-04, FIG 12B, PAGE 45. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)SDR CALA9801257Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN ATTACH ANGLE AT RT DORSAL FIN LOWER FORWARD ACCESS PANEL. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2.SDR CALA9801256Floor Panel · brokenINSPECTION FOUND FLOOR PANEL BROKEN AT STA 522 TO 579. THE FLOOR PANEL WAS REMOVED IAW MM 53-20-0. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-20-0 AND 53-21-0.SDR CALA9801255Floorbeam · crackedINSPECTION FOUND A 4 INCH CRACK IN RADIUS OF FORWARD CARGO FLOORBEAM AT STA 351, BL 0. AN L-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 78.SDR CALA9801254Cusp · corrodedINSPECTION FOUND CUSP CORRODED AT FS 986, RBL 62. THE CORRODED AREA OF CUSP WAS CUT OUT. A REPAIR CUSP AND L-ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-05, 51-20-2, AND 51-10-30.SDR CALA9801253Bracket · crackedINSPECTION FOUND A .25 INCH CRACK AT BOLT HOLE OF LT WING SUPPORT BRACKET, XRS 332. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-1, 51-10-2, 51-10-2A, AND 51-10-3.SDR CALA9801252Floor Panel · corrodedINSPECTION FOUND FORWARD PIT FLOOR PANEL CORRODED AND DELAMINATED AT STA 313 TO 357. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.SDR CALA9801251Clip · crackedINSPECTION FOUND RT WING LEADING EDGE RIB CLIP CRACKED JUST INBOARD OF WS XOS 429. THE CRACK WAS STOP DRILLED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 51-30-5.SDR CALA9801250Frame · damagedINSPECTION FOUND LIGHTNING STRIKE DAMAGE ON WINDOW FRAMES 28 TO 30R. REPAIRED IAW ECRA 5330-02683.SDR MWEA98791Cover · detachedTHE GALLEY SLIDE COVER POPPED OUT. MTC REINSTALLED GALLEY SLIDE COVER.SDR MWEA98790Girt Bar · lack of lubeTHE FLIGHT ATTENDANT REPORTED DIFFICULTY ARMING THE GALLEY SLIDE GIRT BAR. MTC CLEANED AND LUBED GALLEY SLIDE GIRT BAR AND HOLDER.SDR MWEA98789Cover · detachedTHE ENTRY DOOR SLIDE COVER CAME OFF. MTC REINSTALLED ENTRY DOOR SLIDE COVER.SDR MWEA98788Battery Pack · dischargedWHEN APU BUSS TO GROUND BUSS WAS TURNED OFF THE BACK HALF OF FLOOR TRACK LIGHT CAME ON. MTC REMOVED AND REPLACED AFT FLOOR TRACK BATTERY PACK.SDR CALA9801248Web · corrodedINSPECTION FOUND WEB CORRODED AT CUSP LINE FORWARD AND AFT OF FRAME FITTING AT STA 237 ON LT SIDE. THE CORRODED AREA OF WEB WAS CUT OUT, A REPAIR WEB AND L-ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-01, PAGE 9.SDR CALA9801247End Caps · corrodedINSPECTION FOUND LONGERON 20R AND 21R END CAPS CORRODED IN AFT CARGO COMPARTMENT AT STA 996. THE END CAPS WERE REMOVED IAW SRM 51-30-2. NEW END CAPS WERE FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2.SDR CALA9801246Floor Panel · delaminatedINSPECTION FOUND FORWARD PIT FLOOR PANEL DELAMINATED AT STA 218 TO 313. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.SDR CALA9801245Floor Panel · crackedINSPECTION FOUND FORWARD CARGO PIT FLOOR PANEL CRACKED AT ST 427 TO 522. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010.SDR TWAA9811908Bulkhead Clip · crackedDURING OP 16 MAINTENANCE CHECK, FOUND 2 INCH CRACK ON STA 1143 CANTED BULKHEAD WEB CLIP, RT SIDE A RUDDER TRIM CABLE CUT-OUT. REPLACED CRACKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)SDR TWAA9811907Intercostal · crackedDURING OP 16 MAINTENANCE CHECK, FOUND INTERCOSTAL AT STA 513 ABOVE S27R CRACKED. REPAIRED PER SRM 53-01, PG 10. INSTALLED DOUBLER REPAIR. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)SDR TWAA9811903Longeron · crackedDURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29R CRACKED JUST FORWARD ON STATION 587 FRAME. REMOVED AND REPLACED LONGERON END PER DWG INST 592176 PER SRM 51-01 PAG 1 ITEM C. INSTALLED WITH NEW FASTENERS PER DOUGLAS INST DWG 592176 AND SRM 51-60-0. (M)SDR TWAA9811505Longeron · crackedDUIRNG OP 16 MAINTENANCE CHECK, FOUND LONGERON 17R AT STA 980 WITH .50 INCH CRACK AT ATTACH HOLE TO FORMER. REPLACED SECTION OF LONGERON FROM STA 956 TO STA 996. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02, FIGURE 18. CFT TT: 77,783 HOURS. ACFT TC: 84,SDR TWAA9811202Coffeemaker · malfunctionedTHE OTBD COFFEEMAKER PRODUCED A LARGE SPARK AND ELECTRICAL SMELL. CIRCUIT BREAKERS WERE PULLED. REPLACED COFFEEMAKER. CHECK-C 9-16-97 STL. ACFT TT: 78,249 HOURS. ACFT TC: 84,997. (X)SDR MWEA98785Cover · detachedTHE GALLEY DOOR SLIDE FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE COVER.SDR VJ9800246Support · corrodedLEFT LOWER LINER GILLINER SUPPORT IS CORRODED BETWEEN STA 408-427. REMOVED CORROSION, OUT OF LIMITS, DEPTH GAUGE A-2024, IAW DC-9 SRM 51-10-3, 53-01 FIG 1 (.045 MATERIAL LOSS). FABBED NEW SECTION 7075-0-.063 (1A-35078), HEAT TREATED TO T6 IAW DC-9 SRM 53-21SDR VJ9800232Support · corrodedLEFT LOWER GIL LINER SUPPORT IS CORRODED BETWEEN STA 408-427. REMOVED CORROSION, OUT OF LIMITS, DEPTH GAUGE A-2042, IAW DC9 SRM 51-10-3, 53-01 FIG 1 (.045 MATERIAL LOSS). FABBED NEW SECTION 7075-0-.063 (1A-35078-1). HEAT TREATED TO T-6 IAW DC-9 SRM 53-21-0 SDR VJ9800223Clamp · looseNR 1 ENGINE A-LOOP INDICATION INTERMITTENT DURING FLIGHT. REPLACED 13TH STAGE PNEUMATIC CLAMP AND REPOSITIONED. SUBSEQUENTLY, CHECKED SYSTEM, RECONNECTED CONNECTORS P1-824 AND P1-825 TO R5-27 AND R5-29 RESPECTIVELY. SYSTEM CHECKED GOOD IAW MM 26-10.SDR CALA9801239Floor · corrodedINSPECTION FOUND CABIN FLOOR PANEL CORRODED FORWARD OF RT AFT LAV AT STA 945 TO 965, RBL 44. THE FLOOR PANEL WAS REMOVED AND THE CORRODED SECTIONS WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 1, 51-10-3, AND 51-30-2. THE FLOOR PA
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