N992DL, cancelled Dec 30, 2022
Service difficulty reports · 202
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 = 'N992DL' AND deregistration_id = 'N992DL-2022-12-30' 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 = 'N992DL' AND deregistration_id = 'N992DL-2022-12-30' 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 DALA2019040802290Frame · crackedAFT TAIL CONE CTR FRAME CRACKED AT GUIDE PIN 4:00. REMOVED R/H LWR CANTED FRAME. DRILLED NEW CANTED FRAME. INSTALLED R/H LWR TAIL CONE CANTED FRAME PER DWG 9911843.SDR DALA2018091005506Battery · dischargedTAIL COMPARTMENT WALKWAY CENTER EMERGENCY LIGHT OUT. REFERENCED WDM 33-51-13. FOUND NO POWER AT LAMP. REPLACED BATTERIES IN POWER SUPPLY B5-28 (LOCATED IN AFT RIGHT LAVATORY CEILING). OPS CHECK OK. PN'S OFF AND ON TWO 41B004AD07G3 BATTERIES.SDR DALA2018082705251Slat · damagedNR 1 LEFT SLAT WAS DAMAGED. REPLACED THE SLAT IAW W/C 2700-4224-LH-01.SDR DALA2018082805309Structure · damagedDURING A WALK AROUND, FOUND THE GAUGE ON THE LT WING L/E UNDER SLAT NR 1, XFS 136. COMPLIED WITH A DETAILED VISUAL INSPECTION OF THE DAMAGED AREA. FABRICATED A REPAIR DOUBLER IAW SRM 57-06B, FIG 13. COMPLETED INSTALLATION OF REPAIR IAW SRM 57-06B, FIG 31SDR DALA2018061604037Control Cable · severedTAKING THE RUNWAY LOST ALL STEERING TO THE RIGHT VIA THE TILLER. FOUND NOSE WHEEL STEERING CONTROL CABLE 123A SEVERED. REMOVED AND REPLACED 123A REF AMM 32-51. PERFORMED STEERING TEST REF AMM 32-52. CKS NML.SDR DALA2018011200223Door Frame · crackedCRACK ON CORNER UP SIDE OF DOOR JAMB FWD WHEEL WELL LT. DOOR JAMB FWD WHEEL WELL LT ( PAN ) WAS REPLACED PER DC9/MD80 SRM 51-30-2 AND 51-30-5.SDR DALA2018011100192Door Frame · crackedCRACK ON CORNER UP SIDE OF DOOR JAMB FWD WHEEL WELL RT. DOOR JAMB FWD WHEEL WELL RT ( PAN ) WAS REPLACED PER SRM 51-30-02 AND 51-30-05.SDR DALA2017112008216Power Supply · inoperativeEMERGENCY LIGHTS FOR SEATS ROWS 31 AFT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERIES IAW AMM 33-53. OPS CHECKED GOOD.SDR DALA2017111508158Wire · shortedEMERGENCY LIGHTS FOR SEATS 31-36 WILL NOT WORK IN TEST MODE. REPLACED AFT EMERGENCY LIGHTS BATTERY AND CHARGER, B5-212, IAW AMM 33-53. REPAIRED A SHORTED WIRE L902T14 IAW WDM 33-51-14. THE SYSTEM CHECKED GOOD IAW AMM 33-53.SDR DALA2017030801876Support Fitting · wornTAIL CONE CAM MECHANISM SUPPORT FITTING WORN, AND FAILED TORQUE CHECK. REMOVED THE TAIL CONE SUPPORT FITTING AND REPLACED THE SHAFT AND SUPPORT FITTING IAW AMM 53-53-02 AND AMDS 5350-010770101.SDR DALA2016091906708Skin · deterioratedFLAME SPRAY DETERIORATED ON RUDDER WITHIN 7" OF FORWARD SPAR ON BOTH SIDES. R & R RUDDER.SDR DALA2016032902418Light · damagedTHE FLIGHT CREW FOUND EMERGENCY LIGHTS DAMAGED. MAINTENANCE RESECURED THE EMERGENCY EXIT LIGHT AT DOOR R1 AND THE FORWARD EMERGENCY EXIT FLOOR LIGHT IN THE G2 GALLEY.SDR DALA2016021201015Fan · failedF/A NOTICED AN ACRID ODOR AT 1300 FT ON ARRIVAL. TURNED OFF ALL CABIN LIGHTS, ODOR DISSAPATED YET NEVER WENT AWAY. W/C 2120-2367, FOUND RECIRCULATION FAN WITH SMOKE ODOR AND EXCESSIVE VIBRATION. R & R RECIRCULATION FAN IAW AMM 21-20, CONTACTED OK FOR SERVICSDR DALA2015122007681Spar Cap · damagedPREVIOUS TOOL DAMAGE ON NEW RT HORIZONTAL STABILIZER REAR SPAR UPPER CAP XHS=115. REAR SPAR UPPER CAP WAS REPAIRED IAW ER/A 541579-14AD, REV ORIGINAL ETI-88-15-435, REV 2.SDR DALA2015122107683Pan · crackedCRACKED OUTER PAN BETWEEN BEAM 1 AND 2 FWD EDGE AT AFT CARGO COMPARTMENT DOOR. OUTER PAN BETWEEN BEAM 1 AND 2 FWD EDGE AT AFT CARGO COMPARTMENT DOOR, C3 WAS REPAIRED IAW ERA 541561-14, REV ORIG PERMANENT REPAIR.SDR DALA2017121208526Spar Cap · damagedMD88 - STABILIZERS / H.S. / RH REAR SPAR UPPER CAP, XHS 115 / TOOLING DAMAGE. DTA MONITOR INSPECTION LOG REFERENCE ER/A 541579-14AD SECTION II REQUIRES DTA APPROVAL WITHIN 24 MONTHS AFTER SECTION I. ER/A 541579-14AD REV A IS CURRENT. DTA RESTRICTION REMOVED, SDR DALA2015121707657Pan · crackedCRACKED INNER PAN BS 370 . INNER PAN WAS REPAIRED IAW ER/A 541559-14, REV ORIG.SDR DALA2015121707656Hinge · damagedELONGATED HOLES ON FWD/AFT HINGE AT MID CARGO COMPARTMENT DOOR. FWD/AFT HINGES AT MID CARGO COMPARTMENT DOOR WERE REPLACED THEREFORE HINGES ARE OUT OF LIMITS IAW MD-88 52-31- 02 AND ER/A 497387-14MA, REV B. ADJUST AND TEST WILL BE ACCOMPLISHED WITH CARD 5200SDR DALA2015121707653Floor Panel · delaminatedDELAMINATED AND DAMAGED FLOOR PANEL BS 1231 - 1338 . THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.SDR DALA2015121707652Support Fitting · corrodedCORROSION ON LT RETRACT ACTUATOR SUPPORT FITTING BORE. REPAIRED IAW DWG SR09570087, REV B.SDR DALA2015121707651Support Fitting · corrodedCORROSION ON RT MLG RETRACT ACTUATOR SUPPORT FITTING BUSHING VERTICAL FACE AND BORE. REPAIRED IAW DWG SR09570087, REV B.SDR DALA2015121407583Access Panel · corrodedCORROSION AT SETTLEMENT AND COUNTER SKIN AREAS OF FUEL ACCESS PANEL 1466C. FUEL ACCESS 1466C WAS REPLACED IAW SRM 51-22-2A AND IPC 57-30-00-05B AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0454.SDR DALA2015121407588Rib · damagedELONGATED HOLE ON RIB AT RT HORIZONTAL STABILIZER OUTER CONSTANT SECTION REAR SPAR BS XH=27.234 ELONGATED HOLE WAS REPAIR IAW ETI-88-15-418 AND ER/A 541547-14, REV ORIGINAL.SDR DALA2015121307579Structure · corrodedCORROSION ON BARREL NUT HOLE NR 13, BS XM=27.234 AT LT HORIZONTAL STABILIZER. BARREL NUT NR 13 AT LT HORIZONTAL STABILIZER WAS REMOVED IAW AMM 20-10-14 CORROSION WAS REMOVED IAW ER/A 541539-14, REV ORIGINAL. BUSHING WAS FABRICATED AND INSTALLED IAW ER/A REV SDR DALA2015121307578Cusp Web · corrodedCORROSION ON LT CUSP WEB LOWER SURFACE BETWEEN X= 54-X=60 AND BETWEEN BS 627-632, 636-641 AND 648-653. CUSP WEB X 54, 522 TO 788 WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9930538, REV CF.SDR DALA2015121207576Spar Cap · crackedCRACK ON HORIZONTAL STABILIZER RT REAR SPAR CAP AT CRITICAL HOLE CARD. REAR CAP WAS REPLACED IAW DWG 09550030, REV C AND SRM 51-30-1, 51-30-2 AND 51-30-5.SDR DALA2015121207574Access Panel · corrodedCORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1335C. FUEL ACCESS 1335C WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED WITH CARD 2800-0120, JOB 001-0445.SDR DALA2015121207573Tripler · puncturedPUNCTURED PREVIOUS REPAIR TRIPLER ON AFT LAVATORY SERVICE PANEL CUTOUT. REPLACE REPAIR TRIPLER IAW ER/A 529789-14, REV A AND SRM 51-30-2 AND 51-30-5.SDR DALA2015121207572Hinge · crackedCRACK INBD HINGE FITTING AT LT GROUND SPOILER BS XW=47.450, REAR SPAR WING RIB. REAR SPAR WING RIB WAS REPLACED IAW SRM 51-30-2, 51-30-1 AND DWG 5936830-501.SDR DALA2015121207571Structure · damagedTOOL DAMAGE ON BARREL NUT HOLE NR 8 AT RT HORIZONTAL STABILIZER BS XH=27.234. BARREL NUT WAS REMOVED IAW AMM 20-10-14. NEW BUSHING WAS FABRICATED IAW ER/A 541558-14, REV ORIGINAL AND NEW BUSHING WAS INSTALLED IAW 541558-14, REV ORIGINAL AND NEW BARREL NUT WASDR DALA2015121107538Access Panel · corrodedCORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1472C. FUEL PANEL WAS REPLACED.SDR DALA2015121007488Splice · looseLOOSE FASTENERS ON SPLICE OF L/E AT VERTICAL STABILIZER BS ZFS=52.26. ALL HOLES COUNTERSINK WERE MEASURED IAW CARD 5530-01045-05, STEP 2, JOB 055-0001 AND WAS FOUND OUT OF LIMITS, 49 EA. REPAIRED IAW CARD 5530-01045-08, STEP 1, JOB 167-0001 AND SRM 55-03D, SDR DALA2015121007487Doubler · corrodedCORROSION ON PRODUCTION DOUBLER RADIO ALTIMETER ANTENNA SETTLEMENT CUTOUT BS 724 TO 714. PRODUCTION DOUBLER DUE TO EXCECESIVE CORROSION WAS REPLACED IAW DWG 5911412-309, REV DV AND 51-30-5, 51-30-2.SDR DALA2015120907470Slat Track · wornWEAR RT WING SLAT TRACK 13. SLAT TRACK 13 AT RT WING WAS REPLACED IAW AMM 27-80-00.SDR DALA2015120907469Slat Track · wornWEAR ON FLANGES OF LT WING SLAT TRACKS 7, 9 AND 13. LT WING SLAT TRACKS 7, 9 AND 13 WERE REPLACED IAW AMM 27-80-00.SDR DALA2015120907461Access Panel · corrodedCORROSION OUT OF LIMITS ON 2 COUNTERSINK HOLES ON FUEL ACCESS PLATE NR. 1371C. SRM 51-22-2A. FUEL ACCESS PLATE AND BUSHINGS WERE TREATED IAW SRM 51-10-3, NEW BUSHINGS WERE INSTALLED.SDR DALA2015120907460Frame · corrodedCORROSION ON FRAME 1380 BETWEEN BS 24L-24R. FRAME WAS REPLACED IAW SRM 51-30-5, 51-30-2, 51-10-4, 53-01 FIG 1.SDR DALA2015120907468Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BS 148 BETWEEN LONGERON 24 LT ON LONG 25 LT. FOUND WITHIN LIMITS IAW SRM 53-04-1, PARR 7E CONDITION 1B.SDR DALA2015120907467Skin · damagedPROTRUSION ON EXTERNAL FUSELAGE, SKIN BS 200-207 BETWEEN LONGERON 30-29 LT ALSO 214 LONGERON 28-29 LT. DENTS ON FUSELAGE SKIN WERE MEASURED PRESENTING THE FOLLOWING CONDITIONS: BS 200-207, LONGERON 29-30 LT X= DEPTH= 0.042 ", D= DIMENTION= 1.500". D/X = 1.56SDR DALA2015120907466Skin · damagedLIGHTNING STRIKE ON AFT EDGE AT WINDOW BELT NR 57 EXTERNAL FUSELAGE SKIN. DAMAGE WAS REMOVED, MEASURED AND TREATED IAW 53-05, FIG 111, SHEET 10 AND 51-10-3 PAR-21. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK IAW TOPP 30-10-70 PAR I PAGE 13.SDR DALA2015120807451Pan · crackedCRACKED REPAIR DOUBLER ON FORWARD UPPER PAN AT FORWARD PASSENGER DOOR LT. FORWARD UPPER PAN AT FWD PASSENGER DOOR L1 WAS REPLACE IAW SRM 51-30-4, 51-30-1, 51-30-2 AND DWG 591421, REV AV.SDR DALA2015120807450Access Panel · corrodedCORROSION AT SETTLEMENT AND COUNTERSKIN AREAS OF FUEL ACCESS PANEL 1409C. FUEL ACCESS 1409C WAS REPLACED IAW SRM 51-22-2A CONDITION II PARAGRAPH, B.SDR DALA2015120707433Hinge · damagedELONGATED HOLE ON FWD/AFT HINGE AT AFT CARGO COMPARTMENT DOOR. DAMAGED HOLE ON FWD HINGE WAS REPAIRED IAW ER/A 497387-14MA, REV B AND AFT HINGE WAS REPLACED FOR A NEW HINGE.SDR DALA2015120707426Skin · wornWORN PREVIOUS REPAIR FILLER ON FUSELAGE SKIN BETWEEN BS 1287-1309 AND LONGERONS 18R-19R. FILLER WAS REPLACED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21 AND 53-04-2, FIG 2.SDR DALA2015120707425Vane · wornWORN PREVIOUS REPAIR DOUBLER ON INBD VANE, OTBD FLAP AT RT WING. REPAIR DOUBLER INBD VANE, OTBD FLAP AT RT WING WAS REPLACED IAW A/C 0992, CARD 2000-8149-05.SDR DALA2015120707424Skin · crackedCRACK ON RT WING SLAT PANEL NR 2 INNER SKIN BS XOS 240, CARD 04, ZONE 12. CRACK ON INNER SKIN WAS ATTENDED IAW SRM 57-01, FIG 3, SHT 2.SDR DALA2015120707423Cargo Track · corrodedCORROSION ON CARGO TRACK, AROUND FASTENERS FROM BS 1003 TO 1155. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2, 51-10-4, 51-10-3 PARS 14 AND 21 AND 38.SDR DALA2015120607421Floor Panel · crackedCRACK ON FLOOR PANEL 1079A. FLOOR PANEL REPAIRED IAW SRM 51-70-1, PAR 10.SDR DALA2015120607420Cusp Web · crackedCUSP WEB CRACKED AT PREVIOUS REPAIR IN AFT CARGO RT SIDE BETWEEN BS 1136-1155. CUSP WEB REPAIR IAW SRM 51-30-2, 53-05, FIG 131A-1, 51-30-5.SDR DALA2015120607422Floor Support · crackedFLOOR SUPPORT CRACKED AT UPPER SUPPORT ANGLE BETWEEN CABIN FLOORBEAMS 1271-1287 LBL 5. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01 51-30-2 AND 51-30-5.
Back to N992DL, cancelled Dec 30, 2022