N938DN, cancelled Aug 25, 2020
Service difficulty reports · 40
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N938DN' AND deregistration_id = 'N938DN-2020-08-25' 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 n_number = 'N938DN' AND deregistration_id = 'N938DN-2020-08-25' 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 DALA2018081505096Structure · damagedNR 1 ENGINE UPPER PYLON APRON CENTER SECTION MISSING AND AFT SECTION DAMAGED. R & R THE PYLON APRON CENTER AND AFT SECTIONS .SDR DALA2018080644880Battery Pack · inoperativeOVERWING EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE, LOWER INTERIOR EXIT SIGNS. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-55-03. OK FOR SERVICE.SDR DALA2018073104782Frame · crackedTAIL INTERIOR CANTED FRAME CBS 1520 AFT WEB NEAR 2 CLOCK POSITION IS CRACKED AT INR T-CHORD. REPAIRED STA 1520 CANTED BULKHEAD FRAME PRI 569819-14AD REV 0 AND ERA 569819-14AD REV ORIGINAL SECTION I.SDR DALA2018072704718Not Reported · corrodedSUB FLOOR UNDER FLOOR BOARDS 221GF AND 221HF IS IN CORRODED AT FASTENER HOLES BETWEEN STA 168 AND STA 200. REPAIRED W/ REF TO PRI 570298-14, REV 0; PRI 570298-14, REV 1 AND ERA 570298-14, REV ORIG.SDR DALA2018072704717Frame · not reportedERA 569819-14 SECTION I ISSUED FOR REPAIR TO STA 1520 NEAR L7R. REPAIRED STA 1520 CANTED BULKHEAD FRAME REF PRI 569819-14AD REV ORIGINAL.SDR DALA2018072504674Frame · crackedTAIL INTERIOR CANTED FRAME CBS 1520 AFT WEB NEAR 10 CLOCK POSITION IS CRACKED AT INNER T-CHORD. REPAIRED WEB REF SRM 53-10-03 FIG 9C.SDR DALA2018072404640Skin · crackedLEFT SIDE FUSELAGE APPROXIMATE LOCATION FRAME 1496 BETWEEN STRINGER 3 AND 4. TWO CRACK INDICATION WITH BAY MARKED. REPAIRED PER PRI 570252-14 REV 0,1,2 AND ERA 570252-14 REV ORIGINAL.SDR DALA2018020200716Terminal · looseEMERGENCY EXIT LIGHT AT ROW 27 INOPERATIVE ON BOTH SIDES. SECURED TERMINAL LUG AT S3-554, STA 1126R. OPERATION CHECKS GOOD.SDR DALA2018010800158Lens · unknownEMERGENCY EXIT COVER DIFFUSER LENS DAMAGED ON OR MISSING. REPLACED LENS OPERATION CHECKS GOOD.SDR DALA2018010200024Light · damagedEMERGENCY FLOOR LIGHTING DAMAGED. SECURED LIGHT STRIP. OPERATION CHECKS GOOD.SDR DALA2017101807625Battery Pack · abnormalLEFT AFT OVERWING EXIT SIGN AND RIGHT AFT OVERWING EXIT SIGN INOPERATIVE. REPLACED THE BATTERY PACKS.SDR DALA2017101507528Skin · dentedTAIL CONE SKIN DENTED. COMPLIED WITH PRI 540706-14, REV B, REVISION 0, 1, & 2 IAW ERA 540706-14, REV B.SDR DALA2017092207046Lens · missingEMERGENCY EXIT LENS COVER MISSING AT DOOR 1R. INSTALLED NEW EMER EXIT LENS COVER.SDR DALA2017080305943Slide · unsecureL1 DOOR SLIDE UNSECURED. REMOVED AND REPLACED IAW MM.SDR DALA2017033002575Cover · unsecureEXIT SIGN COVER OVER CABIN MAIN ENTRANCE DOOR KEEPS FALLING DOWN. SECURED THE COVER. (LP# 9461452)SDR DALA2017032102277Cover · looseEMERGENCY EXIT SIGN COVER LOOSE. RE INSTALLED COVER.SDR DALA2017021301205Light · inoperativeEMERGENCY FLOOR LIGHTING INOPERATIVE. RESECURED 17A - 20A FLOOR LIGHTING. OKAY FOR SERVICE.SDR DALA2016081206004Skin · crackedAIRCRAFT SKIN HAS CRACK AT BS 1437. REPAIRED IAW PRI/ERA 549478-14.SDR DALA2016081106030Skin · crackedFUSELAGE SKIN CRACKED AT NOSE WHEEL WELL AFT DOOR HINGE CUTOUT. REPAIRED IAW SRM 53-30-01.SDR DALA2016081006068Attach Angle · brokenVERTICAL STABILIZER LEADING EDGE LOWER RIGHT INNER ATTACH ANGLE BROKEN. REPLACED THE ATTACH ANGLE IAW DWG 5912188.SDR DALA2016081006034Attach Angle · brokenVERTICAL STABILIZER LOWER LEFT INNER ATTACH ANGLE IS BROKEN. REPLACED IAW DWG 5912188.SDR DALA2016080905950Threshold · corrodedL1 DOOR THRESHOLD STRIP CORRODED. REPLACED IAW SRM 51-30-00.SDR DALA2016080905903Longeron · crackedLONGERON 2R CRACKED AT BS 1475. REPAIRED IAW SRM 53-30-01, FIG 14.SDR DALA2016080905902Window Frame · crackedCAPTAIN'S SLIDING WINDOW FRAME CRACKED AT UPPER AFT CORNER. REPAIRED IAW DWG 5911356 AND 5644324 AND PRI/ERA 549506-14.SDR DALA2016071405397Light · shortedFLIGHT CREW REPORTS SPARKS WHILE MOVING CAPTAIN'S LIGHT. CIRCUIT BREAKER TRIPPED AND WAS NOT RESET. INSTALLED NEW LIGHT. OPS CHECKED GOOD.SDR DALA2016052704294Structure · damagedDAMAGE TO L1 DOOR LOWER LT CORNER FLANGE. REPAIRED DAMAGE IAW SRM 52-01-01.SDR DALA2015102806563Frame · damagedUPPER CANTED FRAME AT BS 1567.407 DAMAGED. REMOVED, FABRICATED AND INSTALLED FRAME IAW DWG 9911843.SDR DALA2015092405830Line · leakingDECLARED AN EMERGENCY ON APPROACH DUE TO RT HYD SYS LOW QTY. PERFORMED ALTERNATE GEAR EXTENSION. FOUND PYLON PRESSURE LINE CHAFING AND WORN THROUGH. CUT, REMOVED AND INSTALLED NEW LINE. LEAK CHECKS OK.SDR DALA2015031202113Unknown · hazeF/A REPORTED ODOR AND HAZE IN CABIN JUST PRIOR TO DESCENT. LATER REPORTED HAZE AND MOST OF SMELL HAD CLEARED. TROUBLESHOT. NO TROUBLE FOUND. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS.SDR DALA2014081504544Light · inoperativeEMERGENCY LIGHT INOPERATIVE VENTRAL STAIR AREA. REPAIRED IAW SWPM. OPS CHECKED GOOD.SDR DALA14022839238Skin · damagedFUSELAGE OUTER SKIN DAMAGE AT THE L1 DOOR GUST LOCK PIN CUTOUT. PERFORMED DVI. NO OTHER DAMAGE NOTED. TRIMMED OUT DAMAGED SKIN IAW RI 524991-14. COMPLETED IAW REPAIR INSTRUCTIONS 524991-14.SDR DALA13053549238Battery Pack · disconnectedDURING SERVICE CHECK, EMERGENCY EXIT LIGHTS IN CEILING AT ROWS 24 AND 25 INOPERATIVE. FOUND BATTERY PACK NOT CONNECTED. RECONNECTED AT LOCATION B5-243. OPS CHECKS GOOD.SDR DALA13002939238Structure · crackedAFT ACCESSORY BAY AREA, CRACK AROUND FASTENER AREA BS 1520, LBL 10. ROUTED OUT CRACKED AREA AND FABRICATED REPAIR DOUBLER & SHIMS IAW ER/A 504832-14.SDR DALA13003089238Skin · corrodedDURING HMV, CORROSION WAS FOUND ON THE RT WING CENTER SECTION UPPER WING SKIN AT STA 954 AND BL 0. SUBSEQUENTLY, THE CORROSION WAS R & R IAW ER/A 504829-14. ACCOMPLISHED SECTION 1 OF REPAIR IAW ER/A 504829-14, REV O. REMOVED CORROSION FROM CENTER TANK, RBL SDR DALA12016949238Fitting · crackedFUSELAGE LONGERON FITTING CRACKED. REPAIRED AT BS 1060, L20R IAW ER/A 14-509933 ADDED FOR AC 9238.SDR DALA12016929238Beam · crackedL1 DOOR INTERIOR BEAM CRACKED IN RADIUS AFT SIDE VIEWED THROUGH LIGHTNING HOLE STA 198. STOP DRILLED CRACK .250 DIA, LOCATED AND DRILLED NEW ANGLE AND INSTALLED IAW ERA 504823-14 REV 0, DWG 9955752 AND SRM 51-40-01, 51-40-02 AND 51-40-05. ASSOCIATED ER/A 14-SDR DALA12016919238Beam · crackedFORWARD ENTRY DOOR INTERNAL UPPER BEAM CRACKED IN RADIUS SIDE VIEWED THROUGH LIGHTNING HOLE STA 167. STOP DRILLED CRACK .250 DIAMETER IAW ERA 504823-14 AND SRM 51-00-01. LOCATED AND DRILLED NEW ANGLE IAW ERA 504823-14, REV 0 AND DWG 9955752. INSTALLED REPAISDR DALA12017299238Horn · gougedDURING CHECK, FOUND LT WINGTIP L/E HORN GOUGED, WS 560. FOUND HORN OUT OF LIMITS. REMOVED HORN FROM L/E. WELDED, GROUND WELD FLUSH, HFEC AND MT. NO DAMAGE NOTED. ALODINED, PRIMED AND INSTALLED HORN ON LEFT WINGTIP L/E SRM 51-30-02, 51-10-03 AND ER/A 468102SDR DALA12016969238Tee Fitting · corrodedAFT AIRSTAIR (3RD STAIR FROM THE TOP, ABOVE THE APU ENCLOSURE) AFT RT CORNER HAS EVIDENCE OF CORROSION. R & R LOWER TEE ANGLE IAW SRM 51-10-05, 51-30-02, 51-30-05, 51-10-03 AND AMM 51-10-00-370-802.SDR DALA12014469238Frame · corrodedCORROSION AT AFT CARGO BS 1379 FRAME. AFT SIDE AT L30. REMOVED CORROSION. AREA FOUND OUT OF LIMITS WITH 100 PERCENT MATERIAL LOSS. CUT OUT DAMAGED AREA. FABRICATED TWO REPAIR SPLICES AND NEW FORMER. REPAIR INSTALLED IAW SRM 53-00-01, FIG 1 AND 51-10-03 P
Back to N938DN, cancelled Aug 25, 2020