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 AT9900093Light · out of positionEMERGENCY FLOOR LIGHTING WILL NOT STAY ON. REPLACED FLOOR COVER AND WIRING SPLICES AT ROW NR 1. OPERATIONAL TEST NORMAL IAW MM 33-50.SDR 9900439983Circuit Breaker · failedLOSS OF LEFT AC BUS AND ALL CAPTAIN'S INSTRUMENTS OCCURRED AFTER TAKEOFF. CREW RESET LEFT AC BUS, CIRCUIT BREAKER AND INSTRUMENTS WERE REGAINED. CREW DECLARED AN EMERGENCY. RETURNED TO DTW AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT AC BSDR TWAA9902204Seat Track · corrodedDURING OP 15 MAINT CHECK, FOUND CHAIR TRACK AT STA 214, RBL 44 WITH CORROSION AND DEEP PITTING. INSTALLED NEW TRACK SECTION FROM STA 200 TO 265, INSTALLED (P/N C03580-4) PER DOUGLAS PRINT 5910820.SDR AT9900230Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT FUSELAGE TOP CONTROL CABLE PULLEY BRACKET CORRODED AT THE ATTACHMENT POINT AT BS 1143. REMOVED AND REPLACED TOP CONTROL CABLE PULLEY BRACKET IAW DC9 SRM 51-10-3, MM 27-20, AND OHM 27-00.SDR AT9900205Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO FLOOR TRACK AT BS 318 TO 370 RIGHT SIDE CORRODED. FABRICATED NEW SEAT TRACK, DRILLED, DEBURRED, ALODINED, PRIMED, AND INSTALLED IAW DC9 SRM 53-10-3, 51-10-4, AND 51-10-3.SDR AT9900204Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO DOOR TRACK AT BS 351 TO 370 LEFT HAND SIDE CORRODED. REMOVED CORROSION, LOCATED AND DRILLED NEW TRACK IAW DC9 SRM 53-10-3, 51-10-3, AND 53-20-0.SDR AT9900203Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO FLOOR TRACK AT BS 427 TO 503 CORRODED. REMOVED CORROSION, FABRICATED, DRILLED, DEBURRED, AND INSTALLED NEW SEAT TRACK IAW DC9 SRM 53-05 FIG 4C, 51-10-3, AND 51-10-4.SDR AT9900202Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO FLOOR TRACK CORRODED AT BS 389 TO 465. FABRICATED, DRILLED, DEBURRED, AND INSTALLED NEW SEAT TRACK IAW DC9 SRM 53-05 FIG 4C, 51-10-3 AND 51-10-4.SDR TWAA9902301Frame · crackedDURING CHECK-C MAINT, FOUND LOWER AFT CORNER OF SERVICE DOOR FRAME, OUTSIDE SKIN, WITH 1 INCH CRACK FROM FASTENER HOLE EDGE OF FRAME TO HOLE AND COMES OUT OF HOLE SRO207, 4 INCH UP FROM LONGERON 18R. STARTS AT EDGE OF FRAME. REPAIRED CRACK PER ARA 15866.SDR TWAA9902209Membrane · crackedDURING OP 15 MAINT CHECK, FOUND CRACK IN MEMBRANE BELOW CABIN FLOOR AT STA 218, RBL 46 IN. REPAIRED WEB MEMBRANE PER SRM 51-01, FIG 2.SDR MWEA99061Spar · damagedFOUND DAMAGED HOLE AT RIGHT WING STATION 109.0 AFT SPAR. MTC INSTALLED TEMPORARY REPAIR STRAP.SDR GTIA9900914Web · corrodedMHV - FS 211 R61 WEB HAS CORROSION AND BULGING AREA UNDER EXISTING REPAIR. REMOVED WEB AND DOUBLER FABRICATED NEW WEB PER DC9 SRM 53-11-1 FIGURE 11 SHEET 1 AND 2 LOCATED AND DRILL HOLE TO EXISTING FASTENER HOLES ALODINED PER DC9 SRM 51-10-3 PAGE 15 (22A) PRIMSDR AT9900228Doubler · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE HORIZONTAL STABILIZER BULLET FAIRING CORRODED ON METAL DOUBLER AT AFT END. REMOVED CORRODED DOUBLER, FABRICATED DOUBLER, HEAT TREATED, ALODINE, PRIMED, AND INSTALLED IAW DC9 SRM 55-01 FIG 1, 51-10-2A, 51-10-3,SDR TWAA9902207Support · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORT, 0 IN BL, FROM STA 170 TO 215. REPLACED SUPPORT PER SPM 6-70-01.SDR TWAA9902206Support · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 197, LBL 45 TO 50. REPLACED SUPPORT PER SPM 6-70-01.SDR TWAA9902205Support · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, LBL 44. REMOVED CORROSION PER SPM 6-80-01. REPLACED SUPPORT PER SPM 6-70-01.SDR MWEA99060Pan · crackedFOUND AFT CARGO DOOR LOWER FORWARD DOOR PAN CRACKED. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.SDR GTIA9900913Seat Track · corrodedMHV - AT STATION 980 LBL ONE FASTENER HOLE WAS FOUND TO BE OUT OF LIMITS AFTER CORROSION WAS REMOVED FROM SEAT TRACK REF W/O W195. CUT OUT DAMAGED AREA PER DC9 SRM 53-05 FIG 20A FABRICATED. EXTRUSION FILLER STEEL RUB STRIP TREATED PRIMED AREA PER DC9 SRM 51-SDR AT9900229Bulkhead Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT AFT BULKHEAD AFT SIDE ON THE LEFT HAND PULLEY BRACKET CORRODED ON THE LEGS. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER SECTOR BRACKET AND PRESSURE SEAL. RIGGED AND LEAK CHECKED GOOD IAW DC9 SRM SDR AT9900227Frame · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO FLOOR SUPPORT MEMBER AT BS 351 L-25-26R CRACKED. REMOVED FLOOR SUPPORT, WELDED REPAIR SUPPORT USING 4951 FILLER ROD, AND INSTALLED MEMBER IAW DC9 SRM 51-10-4, 51-30-2, 53-03-0, AND EA 12-5321-29-SDR AT9900226Frame · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT CRACK IN RADIUS AT BS 313 L-26-27R. REMOVED FLOOR SUPPORT, WELD REPAIRED SUPPORT USING 4951 FILLER ROD, TREAT, PRIMED AND INSTALLED IAW DC9 SRM 51-30-2, 53-03-0, 53-01 FSDR AT9900225Frame · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO FLOOR SUPPORT MEMBER UPPER SURFACE CRACKED IN RADIUS AT BS 256 LONGERON 24R. REMOVED FLOOR SUPPORT, WELDED REPAIR SUPPORT USING 4951 FILLER ROD, AND REINSTALLED MEMBER IAW DC9 SRM 51-30-2, 51-10-SDR AT9900224Frame · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO FLOOR SUPPORT COMPARTMENT UPPER SURFACE CRACKED IN THE RADIUS AT BS 237 LONGERON 27. REMOVED FLOOR SUPPORT, WELDED REPAIR SUPPORT USING 4951 FILLER ROD, TREAT, PRIMED AND INSTALLED IAW DC9 SRM 51SDR AT9900223Web · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CARGO COMPARTMENT FLOORING TIE IN MEMBER AT CUSP WEB HAS A CRACK COMING OUT OF FASTENER HOLE TERMINATING AT EDGE OF AFT LOBE AT BS 218 RIGHT SIDE. REMOVED FLOORBOARD AND WEB ASSEMBLY TO GAIN ACCESS TO SDR AT9900222Skin · chafedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE VERTICAL STABILIZER LEFT HAND UPPER PANEL 3703A SKIN CHAFED. BLENDED OUT CHAFE ON LEFT HAND VERTICAL STABILIZER SKIN, TREATED, PRIMED IAW DC9 SRM 55-01-0, 55-32-0, 55-01-0, 51-10-3, AND RES NR 99573.SDR AT9900218Skin · dentedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE RIGHT HAND FUSELAGE SKIN WITH NUMEROUS DENTS, DINGS AND GOUGES AT BS 229 TO 392 L18-26R. REMOVED OLD FUSELAGE SKIN, PLACED NEW SKIN, DRILLED, COUNTERSUNK, FABRICATED DOUBLER REPAIR, TREATED, PRIMED SKIN AND DOSDR AT9900132Intercostal · misdrilledSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO COMPARTMENT AT STA 370 TO STA 375 L-29R INTERCOASTAL UPPER FLANGE AND WEB HAS MISDRILLED FASTENER HOLES. FABRICATED NEW INTERCOASTAL, FIT, DRILLED, TREATED AND PRIMED. LOCATED NEW WEB, DRILLED, DSDR 9900499608Connector · corrodedDURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED CORRODED CONNECTOR NEAR POWER SUPPLY. OPERATIONAL CHECK NORMAL.SDR 9900349608Skin · crackedDURING PERIODIC CHECK, FOUND PYLON AREA SKIN CRACKED AT FS 1038, LONGERON 15R. REPAIRED PER EA 99-163248.SDR TWAA9902208Former · crackedDURING OP 15 MAINT CHECK, FOUND CRACK IN AFT FUSELAGE INTERIOR FORMER RING FOOT AT STA 1087, LONGERON 1L. REMOVED AND REPLACED FORMER FOOT CLIP AT STA 1087, LONGERON 1L PER SPM 6-70-01.SDR GTIA9900905Web · crackedFS 211 R61 WEB AT 1.5 INCH LIGHTNING HOLE FORWARD OF OVAL DUCT IS CRACKED AT RIVET SIDEWALL AREA AFT OF FORWARD GALLEY DOOR. REPAIR OF WEB WILL BE ACCOMPLISHED ON A066C03W258 INSTALLATION OF 2 ANGLE AND OVAL DOCT TO BE INSTALLED ON A066S03 W255. (M)SDR AT9900078Wire · shortedEMERGENCY PATH LIGHTING NOT WORKING FROM BUSINESS CLASS FORWARD TO AND INCLUDING THE L-1 DOOR. REPAIRED SHORTED WIRE ON FORWARD SIDE OF FLOOR TRACK LIGHTING, OPS CHECKED GOOD IAW MM 33-53.SDR TWAA9902110Fitting · corrodedDURING OP 15 MAINT CHECK, FOUND IN CABIN A VERTICAL ATTACH FITTING AT STA 680, RBL 44, BELOW FLOOR, CORRODED AT LOWER END. REMOVED AND REPLACED PER SPM 6-70-01.SDR GTIA9900912Seat Track · corrodedMHV - FORWARD PASSENGER COMPARTMENT SEAT TRACK FS 200-240 HAS CORROSION AFT CORROSION WAS REMOVED FOUND AREA TO BE OUT OF LIMITS REF W/C 147. REMOVED AND REPLACED SEAT TRACK AS REQUIRED PER SRM 51-30-01 AND MANUFACTURED NEW TRACK IAW DC9 SRM 51-10-02 ALODINEDSDR GTIA9900897Bulkhead Frame · crackedMHV - LEFT PYLON BULKHEAD FORWARD FACE BULKHEAD FRAME HAS A 3.5 INCH CRACK BETWEEN STRINGERS 15 AND 16. REMOVED ANGLE AND REPLACED WITH NEW ANGLE 9912243-9 PO NR 8125801 PER DC9 SRM 51-30-2 FOR RIVETS 51-30-5 FOR HI-LOCKS. (M)SDR TWAA9902002Support · corrodedDURING OP 15 MAINT CHECK, FOUND FLOOR SUPPORT AT STA 197, OBL TO LBL 44, CORRODED. REPLACED FLOOR SUPPORT PER SPM 6-70-01, PAGE 2.SDR GTIA9900904Angle · corrodedMHV - AFT CABIN ANGLE FS 995 LBL 0-60 HAS CORROSION BEYOND LIMITS CORROSION. REMOVED TO .035 ONLY ALLOWED .025 OER SRM 53-01 PAGE 6. REMOVED CORRODED ANGLE. REPLACED WITH NEW EXTRUSION 7075-T6511 MATERIAL DRILLED AND LOCATED NEW PART ALODINE AND PRIMED INSTSDR GTIA9900903Skin · lightning strikeMHV - RIGHT ELEVATOR TRAILING EDGE OUTBOARD SIDE HAS EVIDENCE OF LIGHTNING STRIKE. MATERIAL ID 10 DOUBLER 2024T3.020 MATERIAL ID FOR TRAILING EDGE 2024T3.040 , ALODINED AND PRIMED PER SRM DC9 51-10-3. INSTALLED FABRICATED PARTS PER SRM 55-20-0 FIG 2. (M)SDR GTIA9900902Floor · crackedMHV - FS 617 RBL 50 RIGHT SIDE FLOOR CHIME PLATE CRACKED ON BOTH SIDES OF LIGHTENING HOLE. REMOVED AND REPLACED FLOOR CHIME PLATE IAW SRM 51-00 AND 51-30-02 JOB COMPLETE. (M)SDR CALA9900106Skin · crackedINSPECTION FOUND TWO 1 CRACKS IN LT FUSELAGE SKIN BY THE AFT STAIR HANDLE IN THE UNPRESSURIZED AREA. THE SKIN WAS REPAIRED IAW SRM 53-01.SDR CALA9900105Wire · looseTHE AFT FLIGHT ATTENDANT STATION EMERGENCY LIGHT SWITCH WAS FOUND INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE ON SWITCH. THE LOOSE WIRE WAS TIGHTENED AND SYSTEM OPERATION CHECKED GOOD IAW MM 33-50-00, PAGES 203-204.SDR CALA9900104Wire · brokenTHE AFT CEILING EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROW 23 TO TAIL SECTION. MAINTENANCE FOUND WIRING TO BATTERY POWER PACKS BROKEN. THE WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0.SDR CALA9900103Wire · brokenTHE CABIN EMERGENCY LIGHTS FROM COCKPIT TO ROW 13 WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0, PAGE 501.SDR CALA9900102Wire · brokenTHE LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION OF THE LIGHTS CHECKED GOOD IAW MM 33-50-0, PAGE 501.SDR AT9900134Support · crackedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND FORWARD CARGO COMPARTMENT STA 351 TO STA 370 L-29L INTERCOASTAL BENT, AND FLOOR SUPPORT WAS FOUND CRACKED. REMOVED AND FABRICATED NEW INTERCOASTAL, RECEIVED NEW SUPPORT, DRILLED, AND INSTALLED BOTH PARTS IAW DC9 SRSDR AT9900077Power Supply · inopFOUND FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY POWER SUPPLY, SYSTEM OPS CHECK GOOD IAW MM 33-50.SDR GTIA9900908Floor · corrodedMHV - FORWARD PASS CABIN FLOOR AT FS 200-243 RBL 21-42 LIGHT CORROSION AFTER CORROSION WAS REMOVED FOUND AREA TO BE OUT OF LIMITS REF CARD W144. REMOVED AREA MATERIAL ID 7075T6.040 PER SRM 53-10-0. FABRICATED REPAIR PARTS PER SRM 53-01 FIG 4 ALODINED AND PRISDR GTIA9900891Angle · corrodedMHV - FORWARD PASS COMPARTMENT FS 160 FLOOR SUPPORT ANGLE CORRODED LBL 15 TO 55. REMOVED SUPPORT ANGLE, FABRICATED NEW SUPPORT FROM 60-2576 7075T6 PO NR 81278 ALODINED AND PRIMED IAW DC9 SRM 50-10-3. INSTALLED SUPPORT IAW DC9 SRM 51-30-0. (M)SDR GTIA9900884Skin · delaminatedLEFT WING UPPER SURFACE OUTBOARD SPOILER IS DELAMINATED AT UPPER INBOARD SECTION APPROX 6 INCH BY 5 INCH OF DELAM ON PART RACK. DELAMINATION AREA IS LARGER THAN ALLOWED LIMITS IN SRM REQUIRES OUTSIDE VENDOR REPAIR REMOVED AND REPLACED. (M)SDR CALA9900097Connector · dirtyTHE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR WAS EXTENDED ON APPROACH TO SDF. QRH PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED AT SDF. THE GEAR DOORS DROPPED OUT ON ROLL OUT RESULTING IN DAMAGE TO THE RT MLG DOOR. MAINTENANCE FOUND C/P TO
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