N901DE, cancelled Nov 29, 2022
Service difficulty reports · 237
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 = 'N901DE' AND deregistration_id = 'N901DE-2022-11-29' 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 = 'N901DE' AND deregistration_id = 'N901DE-2022-11-29' 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 DALA2020042702299Battery Pack · dischargedON SERVICE CHECK, MAINTENANCE FOUND ROW 31 TO AFT CABIN EMERGENCY ESCAPE LIGHTS OUT. THE BATTERY PACK AT THAT LOCATION WAS REPLACED. OPERATIONAL CHECK WAS GOOD IAW MD88 AMM 33-50. (LP #7180338)SDR DALA2020031301825Battery · dischargedCABIN CEILING EMERGENCY LIGHTS FROM SEATS 10 TO 14 AND 34 TO 36 ARE INOP. R&R BATTERIES ON EMERGENCY LIGHT BATTERY CHARGERS AT SEAT 10AND 34. OPS CKS GOOD. (LP7406853)SDR DALA2020022101315Control Module · malfunctionedPASSING 8000' ELECTRICAL BURNING SMELL COMING FROM MODE CONTROL PANEL AREA. RTB ATL. PULLED J7 AND L5. NO EVIDENCE OF BURNING SMELL IN CABIN. FOUND LIGHTS ON MODE CONTROL PANEL CYCLING FROM ON TO DIM OR OFF AND ODOR FROM PANEL. 693037. REPLACED DFGCP PER MD 88SDR DALA2020011600326Switch · malfunctionedTAILCONE UNSAFE DISPLAYED ON OAP BEFORE PUSHBACK. CYCLED INTER HANDLE SW LITE EXT OK FOR SVC. (LP6956218)SDR DALA2019091205279Battery · dischargedFWD FLIGHT DECK / GALLEY OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES FWD DROP DOWN CEILING FOR FWD FLIGHT DECK GALLEY OVERHEAD EMRG LIGHT IAW AMM 33-50. OPS CHECK GOOD. (LP6188026)SDR DALA2019081104694Engine · failedLEFT ENG FAILURE 2-4 SEC AFTER LIFT OFF ENGINE INDICATIONS SHOWED 0 PER N2 AND 0 PER NE EGT APROX 628 SHUT DOWN ENGINE IAW CHECKLIST. REPLACE NR 1 ENGINE ON SPC 88-7110-9-010.SDR DALA2019032501888Wire Harness · brokenEMERGENCY LIGHTS AT 35ED NOT WORKING. FOND HARNESS BROKEN. REPLACED OPS NML. REF AMM 3352. (LP5845514)SDR DALA2019020700827Battery Pack · inoperativeOVERHEAD EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROWS 14-22. REPL BATTERY PACK REF MD88 AMM 33-53. OPS CHECK GOOD. (LP4702230)SDR DALA2018100805912Fitting · crackedLATE FINDING (IN REF 5700-2246): RT CRACK ON OUTBD FITTING TO ATTACH SLAT TRACK NR 10 AT SLAT PANEL NR 3 RT WING. SLAT PANEL ASSY 3 RT PART NUMBER OFF : 5922533-504 SERIAL NUMBER OFF: DL27 WAS REMOVED PER WORK CARD 2700-4224-RH-03 AND SERVICEABLE SLAT PANEL ASSDR DALA2018100505896Spring · brokenAWR, HIDDEN CRACK: IN REF AMDS 5350-01077-0101 STEP 2. BROKEN SPRING OF TAILCONE EMERGENCY RELEASE MECHANISM AT AFT PASSENGER DOOR UPPER DOOR JAMB. SPRING OF TAILCONE EMERGENCY RELEASE MECHANISM AT AFT PASSENGER DOOR UPPER DOOR JAMB WAS REPLACED PER MD-88 AMM SDR DALA2018092805786Frame · crackedCRACKED FRAME ON STA 1510 CANT REF LONG 10R AT AFT ACC COMPARTMENT. FRAME OF STA1510 AT AFT ACC COMPARTMENT BTW POSITION 9 HRS TO 3 HRS WAS REPLACE PER DC-9/MD 80 SRM 51-30-1, SRM 51-30-2 AND SRM 51-30-5 AND DWG. 9911893 REV. "E". (LP0760687)SDR DALA2018082765255Battery Pack · inoperativeROWS 10 - 15, THE EMERGENCY LIGHTS WERE DIM DURING A TEST. REPLACED THE EMERGENCY LIGHT BATTERY AT ROW 12. OPS CHECKED GOOD.SDR DALA2018071804541Lens · damagedTHE EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. MAINTENANCE REPLACED THE EMERGENCY EXIT COVER DIFFUSER LENS. OPERATIONAL CHECK IS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DALA2018070304334Engine · malfunctionedDUE TO I/B W/U OF RT ENG OIL STAINER CLOG MSG. REPLACING ENG ON SPC NUM 2 88-7110-9-0010 REF LOG 3714976. PER MCC NOTIFICATION, AN EMERGENCY WAS DECLARED.SDR DALA2018040802263Wire Harness · defectiveEMERGENCY LIGHTS AT SEAT 17 AND 26DE INOP SEAT MOUNTED. REPLACED SEAT HARNESS AT SEATS 17DE AND 26DE PER AMM 33-52. OPS CKS GOOD.SDR DALA2018020400636Brake · malfunctionedRIGHT MAIN TIRE BRAKE SMOKING ON TAXI INBOUND. R&R NR 4 MAIN WHL ASSY & NR 4 BRAKE ASSY PER AMM 32-41 & AMM 32-44. LK CK OK.SDR DALA2018011100193Unknown · malfunctionedWHILE TAXIING IN AND MAKING LEFT TURN ON TAXIWAY Z THE RIGHT BRAKE SEEMED TO LOCK UP AND PULL AIRCRAFT TOWARDS EDGE OF TAXIWAY AIRPLANE DEPARTED TAXIWAY AND HIT 2-3 TAXI LIGHTS. INSPECTED A/C PER AMM 05-51-03 NO DAMAGE FOUND. JACKED RT GEAR AND CYCLED BRAKES SSDR DALA2017082106309Actuator · malfunctionedWITH SLATS EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT, SUBSTANTIALLY. TRIM REQUIRED IS 3 DEGREES LT OF THE TRIM REQUIRED WITH A CLEAN WING. DURING CRUISE THE REQUIRED TRIM IS LESS THAN 1 UNIT RIGHT BOTH RUDDER/AILERON WITH BALANCED POWER & FUEL. FLAP BUSS TSDR DALA2017052404152Wedge · damagedDENTED RT TE FLAP 20 INCHES FROM THE OTBD END APROX 9 BY 18 INCHES, APROXIMATELY .40 DEEP AND A BENT T/E WEDGE, FWD END LOWER SURFACE. REMOVED THE OTBD TRAILING EDGE WEDGE. INSTALLED A NEW OTBD FLAP OTBD TRAILING EDGE WEDGE IAW AMM 57-50.SDR DALA2017040602774Wire Harness · out of positionDURING VIS INSPECTION OF THE OVERHEAD WIRE BUNDLE, FOUND THE WIRE BUNDLE CHAFING AGAINST RELAY. ROUTED THE WIRE BUNDLE FOR CLEARANCE AND FOUND NO DAMAGED WIRES. ACFT OKAY FOR SERVICE.SDR DALA2017032902528Brake · draggingNR 4 BRAKE DRAGGING. REPLACED THE NR 4 BRAKE ASSY IAW AMM 32-42.SDR DALA2017022201455Wire · broken1R GIRT BAR WIRE BROKEN. PER AMM 52-12 REPLACED GRT BAR LANYARD. OK FOR SVC.SDR DALA2016121509882Battery Pack · inoperativeCEILING EMERGENCY LIGHTS INOPERATIVE AT ROW 26-28. REPLACED THE BATTERY PACKS IAW AMM 33-53. OPS CHECKED GOOD.SDR DALA2016111408754Light · inoperativeLT AFT OUTSIDE EMERGENCY LIGHT OUT. RELAMPED IAW AMM 33-50. OPS CHK GOOD.SDR DALA2016091206570Skin · damagedAWR HIDDEN DAMAGE: PERFORMED RT WING HINGE COVER AILERON TAB MOD, ELONGATED FASTENER HOLE WAS FOUND ON RT AILERON T/E LOWER SKIN STA XAT=1.978. AILERON WAS REPAIR IAW ER/A NM 550281-14, REV ORIGINAL AND ETI -88-16-296, REV 3.SDR DALA2016091206524Door · corrodedAWR HIDDEN DISCREPANCE, CM: CORROSION ON LOWER OTBD FACE AT RT MLG FIXED DOOR IN REF CARD 00693. MLG FIXED DOOR RT WAS REPLACED IAW AMM 32-12-01-201.SDR DALA2016090906486Tab · nickedRE-WRITE: LATE FINDING: NICK ON LT ELEVATOR CONTROL TAB T/E. ELEVATOR CONTROL TAB OFF SN 53378 WAS REPLACED BY ELEVATOR CONTROL TAB ON SN 53380 IAW IPC 55-20-03 AND WAS INSTALLED IAW CARD 2730-4334; JOB 001-0232.SDR DALA2016090806462Support Fitting · corrodedCORROSION ON RT MLG SUPPORT FITTING BUSHING BORE. REPAIRED IAW ER/A 549274-14AD REV ORIG.SDR DALA2016090706437Spring · brokenAWR RII: BROKEN EMERGENCY EXIT PRESSURE BULKHEAD DOOR ARM SPRING. SPRING PN 4951062-1 WAS REPLACED IAW AMM 53-53-02 AND WAS VERIFIED WITH IPC 52-10-02.SDR DALA2016090606420Spring Assy · corrodedRUSTED PISTON END AT RUDDER TRIM TAB ACTUATOR ON AFT ACCESSORY COMPARTMENT. RUDDER TRIM LOAD-FEEL SPRING ASSY WAS REMOVED AND INSTALLED IAW AMM 27-207. AREA AT SHAFT OF RUDDER TRIM LOAD-FEEL SPRING ASSY WAS REWORKED MEASUREMENT ORIGINAL 0.686" AND MINIMUM RESDR DALA2016090606428Hinge Bracket · damagedAWR: HIDDEN DISCREPANCY, ELONGATED HOLES ON NR 4 FORWARD FIXED FLAP HINGE BRACKET STA XW=333.147 RT WING. FORWARD FIXED FLAP HINGE BRACKET STA XW= 333.147 RT WING WAS REPLACED IAW AMM 57-40-01-201, STEP 3H, 1 TO 9B.SDR DALA2016090606426Doubler · wornINITIAL, WEAR ON EXTERNAL PREVIOUS REPAIR DOUBLER ON FORWARD LOWER CORNER AT FORWARD CARGO COMPARTMENT DOOR. DAMAGE DOUBLER ON FORWARD LOWER CORNER WAS REPLACED IAW ER/A 486624-14MA, REV ORIGINAL.SDR DALA2016090406410Door Frame · corrodedINITIAL, CORROSION ON UPPER DOOR JAMB, STA Y=1160 BETWEEN LONG PROJECTION 18 RT TO 19 RT AT AFT CARGO COMPARTMENT, C3. DUE TO EXCESSIVE DAMAGE BEAM ON C3 WAS REPLACED IAW SRM 51-10-3/51-10-4, 51-30-5 AND DWG N-5936072 REV U.SDR DALA2016090206357Door · crackedINITIAL: CRACKED LT WING OTBD FLAP INBD BUTE DOOR MID SECTION INNER AREA. LEFT WING OTBD FLAP INBD BUTE DOOR WAS REPAIRED IAW ER/A466345-14MA, REV B.SDR DALA2016090206354Beam · crackedCRACKED AFT EDGE BEAM NR 1 AT MAIN ENTRANCE DOOR, L1. THIS CARD WAS ATTENDED WITH ERA 549270-14, REV ORIGINAL.SDR DALA2016090106329Bulkhead · unknownRIGHT APB LOWER CHORD CUT LINE DOES NOT MEET REQUIREMENTS OF SRM, STA Y=1338, AREA WAS REPAIRED IAW ER/A 549254-14, REV ORIGINAL.SDR DALA2016090106328Stringer · crackedCRACK ON STRINGER 11, LT WING, OTBD SIDE STA XRS=168 APPROXIMATELY STR 11, LT WING WAS REPAIRED IAW DWG NR SR-09570100, REV B AND ER/A 549281-14AD, REV ORIGINAL REPETITIVE INSPECTION WILL BE MONITORED WITH LOG PAGE 2660039 IAW ERA 549281-14AD, REV ORIGINAL, SESDR DALA2016090106323Doubler · corrodedCORROSION ON INTERNAL DOUBLER AROUND AFT LAVATORY SERVICE PANE. CORROSION ON INTERNAL DOUBLER WAS REPAIRED IAW ER/A 549257-14, REV ORIGINAL REPETITIVE INSPECTION WILL BE PERFORMED WITH LOG 2657213, ER/A 549257-14, REV ORIGINAL, SECTION II.SDR DALA2016083106307Release Mech · wornWORN TAILCONE RELEASE CAM AT AFT ACCESSORY COMPARTMENT. WORN ON TAILCONE RELEASE MECHANISM CAM BASE WAS MEASURED AND WAS FOUND OUT OF LIMITS, MAX PERMISSIBLE 0.025" X 0.280" MAX MEASURED 0.062" X 0.- 328 IAW CMM 53-50-07. THEREFORE CAM WAS REPLACED IAW AMM 5SDR DALA2016083106311Doubler · corrodedCORROSION ON INTERNAL DOUBLER AROUND AFT LAVATORY SERVICE PANEL. FRAME CLIP STA Y=1309 & Y=1322 FROM LONGERON 18LT TO 26LT; LONGERON 20 LT & 21 LT FROM STA Y=1322 TO Y=1338; INTERCOSTALS, 2 EA, BETWEEN LONG 21 LT AND 22 LT FROM STA Y=1322 TO Y=1338; AND LONGESDR DALA2016083106310Doubler · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER AND LOWER DOOR JAMB AT FWD CARGO COMPARTMENT DOOR JAMB. LOWER DOOR JAMB WAS REPAIRED IAW SRM 53-05, FIG 44A.SDR DALA2016083106304Fitting · corrodedCORRODED R1 GIRT BAR FITTINGS ABOVE FLOOR PANEL 160G. R1 GIRT BAR FITTINGS ABOVE FLOOR PANEL 160G WERE REPLACED IAW DWG 3936193, REV ORIGINAL.SDR DALA2016083106303Skin · corrodedCORROSION ON INTERNAL HOLES LOWER ACCESS DOOR CUTOUT STA XRS=189 TO 214 BETWEEN STR 12 AND STR 15 AT LT WING. CORROSION ON HOLES WERE REPAIRED IAW ER/A 549272-14AD, REV ORIGINAL. THIS DOCUMENT IS READY TO ENTRY AND MONITOR WILL BE WORK IAW ER /A 549272-14AD,SDR DALA2016083106302Skin · corrodedCORROSION ON INTERNAL HOLES LOWER ACCESS DOOR CUTOUT STA XRS=-189 TO 214 BETWEEN STR 12 AND STR 15 AT RT WING. CORROSION ON HOLES WAS REPAIRED IAW ER/A 549272-14AD, REV ORIGINAL. THIS DOCUMENT IS READY TO ENTRY AND MONITOR WILL BE WORKED IAW ER/ A 549272-14 SDR DALA2016083106300Skin · damagedINITIAL: LIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA Y:731-750, FORWARD AND AFT CORNERS. LIGHTNING STRIKE ON LT WINDOW BELT WAS REPAIRED IAW ER/A 549248-14AD REV ORIGINAL.SDR DALA2016083106297Frame · crackedCRACKED FRAME ON STA Y=1485 CANT BELOW OF STAIR VENTRAL ACTUATOR AT AFT ACCESSORY COMPARTMENT. FRAME ON STA Y=1485 CANT BELOW OF STAIR VENTRAL ACTUATOR AT AFT ACCESSORY WAS REPAIRED IAW SRM 53-03D, FIG 43.SDR DALA2016083106294Finger Doubler · bentBENT EDGE ON FINGER DOUBLER AT FUSELAGE SKIN REPAIR BETWEEN STA Y=237 TO STA 256 AND LONGERONS 17LT TO 18LT, REF LOG NR 1542341. SECTION STRIP DOUBLER WAS REPAIRED IAW SRM 53-04-3, FIG 12.SDR DALA2016083006288Skin · bulgedBULGING FUSELAGE SKIN BS 608 - 617, LONGERONS 29 - 30R. DOUBLERS WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-30-3, 51-10-3 PARR. 14, 21, 51-20-0 AND DWG 5911412 REV. DU.SDR DALA2016083006287Skin · delaminatedDELAMINATED RT ELEVATOR GEARED TAB UPPER SKIN AT HORIZONTAL STABILIZER. THE GEARED TAB WAS REPLACED IAW SRM SRM 55-04 P.4.SDR DALA2016083006283Skin · bulgedBULGING FUSELAGE SKIN BTW BS 636 - 655, LONGERONS 29 - 30R. DOUBLER WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.
Back to N901DE, cancelled Nov 29, 2022