N922DL, cancelled Sep 20, 2022
Service difficulty reports · 159
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 = 'N922DL' AND deregistration_id = 'N922DL-2022-09-20' 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 = 'N922DL' AND deregistration_id = 'N922DL-2022-09-20' 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 DALA2019072804443Slide · defectiveDURING SCHEDULED DEPLOYMENT TEST, SLIDE FAILED TO DEPLOY REF CARD 2562-7193 FORECAST NO 88-0525-8-0407. SLIDE FAILED TO DEPLOY DUE TO FIRING LANYARD NOT BEING INSTALLED THROUGH THE TAB AND ON THE RETAINING RING. INSTALL OF NEW SLIDE PERFORMED ON TASK CARD 2561SDR DALA2019042002531Stiffener · crackedNOSE COWL CRACKED. INTERNAL FWD BULKHEAD STIFFENER AT 07:00 UPPER AND LOWER FAST. HOLES (2 AREAS)MARKED. INTERNAL FWD BULKHEAD STIFFENER AT 6:30 LOWER FAST. EXTERNAL STIFFENER AT 6.30 MARKED. REM/REPL #1 ENG NOSE COWL PER MD88 AMM 71-10. COWL, NOSE, LT OFF 88-SDR DALA2019020600811Battery Pack · inoperativeOVERHEAD EMERGENCY LIGHTS OUT 22, 23, 24, 25 ROWS. R/R BATTERY SET AT BATTERY PACK B5-104 IAW MD88 AMM 33-53. OPS CK GOOD. (LP5319148)SDR DALA2019011600274Outlet · damagedPAX 4B NOTICED PED CHARGING STATION DAMAGED/CHARRED. NO SMOKE. REPLACED OUTLET, OPS GOOD. (LP5162466)SDR DALA2019010400035Pin · pulledFOUND 1L DOOR SLIDE PIN PULLED OUT. REPLACED 1L DOOR SLIDE ASSY PER W/C 5200-0652. OK FOR SVC. SLIDE, PASSENGE OFF 09-2561-9-0011 00147. (LP5162443)SDR DALA2018121407183Frame · crackedCRACK- 1310 CANT FRAME CRACKED AT TAIL CONE GUIDE PIN 4 OCLOCK POSITION. REMOVED DAMAGED FRAME PN 5966769U501. (458779) DRILLED NEW FRAME AND BEGAN INSTALLATION PER BOEING DWG 5966769. COMPLETED INSTALLATION OF FRAME PER BOEING DWG 5966769. (LP0863490)SDR DALA2018072304609Bracket · out of adjustEMERGENCY SEAT ISLE LIGHT INOP AT SEAT 31 DE. ADJUSTED BRACKET AND BULB FIXTURE AT ISLE SEAT 31 DE. OPS CK GOOD.SDR DALA2018101005977Skin · corrodedFUSELAGE SKIN, STA 750, L-30 CORROSION REPAIR, PERMANENT REPAIR. C/W ERA 455233-14 REV C, MON CLOSED.SDR DALA2018032801981Window · out of adjustFIRST OFFICER'S EMERGENCY ESCAPE WINDOW WILL NOT OPEN. ADJUSTED THE WINDOW IAW AMM 56-10. OPS CHECKED GOOD.SDR DALA2018032601875Nut · looseAT FL330 MASTER CAUTION LOW OIL PRESS RIGHT ENG. RAN QRH, 0 QUANTITY, THEN SHUT DOWN R ENGINE. R PRESSURE AND QUANTITY BOTH 0. WINDMILL 15 MINUTES. UPON ARRIVAL FOUND LOWER COWL COVERED WITH OIL. FOUND LOOSE STUD/NUT ON OIL FILTER CAP W/O-RING PROTRUDING. WIP SDR DALA2018030201318Wire Harness · inoperativeEMERGENCY LIGHT AT SEAT 20 DE INOPERATIVE. REPLACED THE SEAT WIRE HARNESS IAW AMM 33-52. CHECKED GOOD.SDR DALA2017092507058Panel · corrodedCORROSION ON RT HEATER BLANKET AROUND ACCESS NR 1410C CUT OUT (AD). LEVEL CORROSION 2. RT HEATER BLANKET PANEL WAS REPLACED PER AMM 30-80-02-401 BLOCK 401. OVERWING HEATER BLANKET FUNCTIONAL TEST WAS PERFORMED PER AMM 30-80-02-0501. TEST OK.SDR DALA2017092407057Door Frame · damagedAWR HIDDEN DAMAGE: ELONGATED HOLES ON LOWER DOOR JAMB BEAM STA Y=636 TO Y=693 AT MID CARGO COMPARTMENT. ELONGATED HOLES ON LOWER DOOR JAMB BEAM STA Y=636 TO Y=693 AT MID CARGO COMPARTMENT WERE REPAIRED PER ETI-88-17-235 REV 3 AND ER/A 560942-14 REV ORG.SDR DALA2017092207015Spacer · corrodedCORROSION ON SPACER AT MID CARGO COMPARTMENT DOOR JAMB BEAM REPAIR ALSO THE REPAIR DOES NOT MEET REQUIREMENTS PER SRM (SM) (C2) (IN REF AMDS 5300-2358). SPACER AT MID CARGO COMPARTMENT DOOR JAMB BEAM REPAIR ALSO THE REPAIR DOES NOT MEET REQUIREMENTS PER SRM, WSDR DALA2017092006983Slide · low pressureLOW PRESSURE ON THE R1 SLIDE. THE R1 SLIDE WAS REPLACED IAW AMM 52-62-00.SDR DALA2017091306874Angle · corrodedAWR.HIDDEN DAMAGE:THIS CARD IS ISSUED WITH THE CORRECT TEXT INSTEAD OF NRC 00805. CORROSION ON LH CUSP ANGLE BTW STA Y=218 TO Y=- 227 AND X=54 TO X=60 AT CABIN FLOOR STRUCTURE. PERMANENT REPAIR ON ANGLE CUSP WAS ACCOMPLISHED PER ETI-88-17-228 REV. 2. AND ER/A SDR DALA2017091406878Angle · corrodedCORROSION ON CEILING SUPPORT ANGLE BS 1231, LBL 18 AND 32 IN THE AFT CARGO BAY. THE ANGLE WAS REPLACED IAW DWG 5956707, REV AT, SRM 51-10-3, 51-10-2, 51-10-4, 51-30-2, AND 51-30-5.SDR DALA2017091306851Longeron Splice · crackedCRACKED LONGERON SPLICE 22L BETWEEN BS 1271 TO 1287. THE LONGERON SPLICE WAS REMOVED AND REPLACED IAW SRM 53-02, FIG.18, 51-30-5, 51-10-3, & 51-10-4.SDR DALA2017091206850Bulkhead · corrodedCORROSION ON AFT BULKHEAD AT WALKING BRIDGE. THE BULKHEAD WAS REPLACED IAW SRM 51-30-2 AND DWG 9911993 REV CJ.SDR DALA2017091206831Intercostal · corrodedCORROSION ON INTERCOSTAL AT WALKING BRIDGE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.SDR DALA2017091206830Access Panel · corrodedCORROSION ON THE LT WING HEATER BLANKET FWD FUEL BOOST PUMP SECONDARY ACCESS COVER. FWD FUEL BOOST PUMP SECONDARY ACCESS COVER WAS REPLACED.SDR DALA2017091006775Floor Support · damagedFLOOR SUPPORT CORRODED AND CRACKED, BS 1287 TO 1307, BL 0. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01, FIG 4.SDR DALA2017091006774Seat Track · corrodedCORROSION OUT OF LIMIT ON THE SEAT TRACK RBL 54, BS 790 - 796. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIG 4F, 51-10-03, PAR 21, 14, AND 51-30-01.SDR DALA2017091006771Door Frame · wornWORN LEFT MLG WW DOOR FRAME AFT CHANNEL BS 937 AND LBL 60. MLG WW DOOR FRAME WAS REPLACED IAW SRM 51-30-2, 51-30-5, SRM 51-10-04 , AND 51-10-3 PAR 14, 21.SDR DALA2017090806750Support · corrodedCORROSION ON GIRT BAR SUPPORTS AT FWD GALLEY SERVICE ENTRACE DOOR. SUPPORTS AT FWD GALLEY SERVICE ENTRANCE DOOR WERE REPLACED. (LP# 0202940)SDR DALA2017090806747Channel · crackedCRACKED PREVIOUS REPAIR ON HAT CHANNEL AT FLOOR PANEL 927E. THE FLOOR PANEL WAS REPLACED IAW SRM 53-01, FIG 2.SDR DALA2017090806742Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 1367C. THE ACCESS PANEL WAS REPAIRED IAW SRM 51-22-2A, AND SRM 51-10-3, PAR 21.SDR DALA2017090806737Angle · crackedCRACKED ANGLE AT BS 389 BETWEEN THE LOWER EDGE AND BEAM NR 1 ON THE FWD CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-2.SDR DALA2017090706711Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PLATES NBR 1371C, 1303C, 1335C. PANELS WERE REPLACED. (LP# 0201594)SDR DALA2017090700004Frame · wornWORN FRAME TEE BS 1380, LOWER FACE BETWEEN LONGERON 24L TO 24R AT AFT ACCESORY COMPARTMENT. REPLACED THE FRAME.SDR DALA2017090706710Spacer · corrodedCORROSION ON SPACER AT THE AFT CARGO DOOR FRAME REPAIR, BS 1174 - 1212. REPAIRED IAW SRM 53-05, FIG 123, 51-10-3, PAR 14, 21, 38, SRM 51-30-5, AND 51-10-2.SDR DALA2017090606672Angle · crackedCRACKED ANGLE ON UPPER SURFACE BS 826, RBL 42. THE ANGLE WAS REPAIRED IAW ERA 498192-14MA, REV A.SDR DALA2017090606667Skin · dentedDENTS ON THE UPPER & LOWER SURFACE SKIN OF THE LT ELEVATOR CONTROL TAB, AND THE ELEVATOR ANTI-FLOAT TAB. THE TAB SKIN WAS REPAIRED IAW SRM 55-04, PAR 3.SDR DALA2017090606666Cusp Web · nickedNICKS ON THE RT CUSP WEB BETWEEN BS 870 - 876, RBL 48 TO 52. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A.SDR DALA2017090606662Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PLATES NR 1410C. FOUND OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A,SDR DALA2017090506606Cusp Web · corrodedCORROSION OUT OF LIMITS ON RT CABIN FLOOR MEMBRANE AT STA Y =662 TO Y=667 AND Y=680 TO Y=683 IN REF NRC 00285. CUSP WEB WAS REPAIRED PER SRM 51-70-4.SDR DALA2017090506605Cusp Web · corrodedAFTER TO REMOVE CORROSION ON CUSP WEB BTW STA Y=1174 TO Y=1193, X=-54 TO X=-60, AREA WAS FOUND OUT OF LIMITS. CORROSION ON CUSP WEB BTW STA Y=1174 TO Y=1193, X=-54 TO X=-60 WAS REPAIRED PER SRM 51-70-04 FIG 2 (SHEET 1).SDR DALA2017090406598Angle · crackedCRACKED ANGLE AT BS 1338, LONGERON 7R AT THE AFT PRESURE BULKHEAD, THE ANGLE WAS REPAIRED IAW SRM 53-01, FIG 3.SDR DALA2017090306594Cusp Web · corrodedCORROSION ON THE CUSP WEB BETWEEN BS 399 - 401, RBL 44 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-4.SDR DALA2017090306539Cusp Web · nickedTWO NICKS ON THE RT CABIN FLOOR CUSP WEB BETWEEN RBL 44 AND 54, BS 1054 TO 1063. THE CUSP WEB WAS REPAIRED IAW SRM 53-01, FIG 1.SDR DALA2017090206530Cusp Web · corrodedCORROSION ON LT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BTW LBL 54 AND 60 FROM BS 598 TO 712. THE CUSP WEB WAS REPLACED IAW SRM 53-05 FIG. 131A-24, AND SRM 51-30-01, 51-30-02, 51-30-05.SDR DALA2017090106501Cusp Web · corrodedCORROSION ON RT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BTW X=-44 AND X=-60 FROM STA Y=503 TO Y=598. SECTION CUSP WEB WAS REPLACE ON STA Y= 503 TO Y=598 BTW X=-44 AND X=-60 PER SRM 53-05 FIG 131A-16, 53-05 FIG131A-24 AND SRM 51-30-01,51-30-02, 51-30-05.SDR DALA2017083106480Angle · corrodedCORROSION ON LT LOWER EPC ANGLE BS 160 AND LBL 50. THE ANGLE WAS REPLACED IAW SRM 51-30-2, 51-30-1, AND DWG 9955780, REV LA.SDR DALA2017082900003Pin · corrodedCORROSION AND WORN RT AND LT INBD FLIGHT SPOILER HINGE CENTER PINS. THE PINS WERE REPLACED.SDR DALA2017082900002Angle · crackedCRACKED ANGLE BETWEEN LOWER EDGE AND BEAM NR 1 AT AFT CARGO DOOR. THE ANGLE WAS REPLACED.SDR DALA2017082900001Splice · corrodedCORROSION ON CUSP ANGLE SPLICE BETWEEN BS 503 - 522, RBL 60. THE CUSP SPLICE WAS REPLACED.SDR DALA2017082806403Floor Panel · delaminatedDELAMINATION FLOOR PANEL NR 200E, 617C, 160E AT PASSENGER CABIN. FLOOR PANEL NR 200E, 617C AND 160E WERE REMPLACED AND IDENTIFIED PER AMM 53-20-01-201.SDR DALA2017082806402Skin · damagedDAMAGE METALIZED COAT ON RUDDER SKIN LT AND RT SIDE. RUDDER WAS REPAIRED PER SRM 51-70-1A PAR 23 AND ERA 092613-14MA REV A.SDR DALA2017082706401Skin · dentedDENTS DAMAGE ON UPPER/LOWER SURFACE SKIN AT LT ELEVATOR GEARED TAB, ALSO DEGRADED SEALANT. ELEVATOR GEARED TAB LT WAS REPAIRED PER SRM 55-04 PAR 2 C AND SRM 51-20-0.SDR DALA2017082606400Pan · crackedCRACK ON RING PAN UPPER FWD CORNER STA Y=846 LEFT SIDE. RING PAN UPPER FWD CORNER STA Y=846 LEFT SIDE WAS REPAIRED PER SRM 53-05 FIG 122 AND 51-10-03.
Back to N922DL, cancelled Sep 20, 2022