N963DN

Service difficulty reports · 148

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 = 'N963DN' AND registry_match = 'registration'
  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.

SDR DALA2018030201312Skin · crackedCRACK AFT BIFURCATION TRACK FAIRING SKIN INBOARD SIDE AT LT UPPER ENGINE THRUST REVERSER C-DUCT. CRACK WAS STOPPED DRILL PER SRM 54-30-13 PAR (5) VOL IV (ET) HFEC INSPECTION WAS ACCOMPLISHED ON AFT BIFURCATION TRACK FAIRING SKIN INBOARD SIDE AT LT UPPER ENGINEMar 1, 2018 · N963DN · Doug MD9030 · Nacelle/Pylon, Plate/SkinSDR DALA2018030201311Cusp Web · corrodedCORROSION LEVEL 2. (IN REF NRC 00328) CORROSION ON RT CUSP WEB BTW STA Y=731 TO 741, X=-54 TO -60 AT PAX CABIN FLOOR STRUCTURE. CORROSION II IN REF NRC 00966 AREA WAS REPAIRED PER SRM 53-20-02 VOLUME I FIGURE 17.Mar 1, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018030101286Angle · crackedCRACK ON UPPER ANGLES BTW INTERNAL PAN AND BEAM 5 ON STA Y=712 ALSO ON STA Y=730 AT MID CARGO DOOR. ANGLE AND WEB ON BEAM 5 STA Y=712 AND STA Y=730 AT MID CARGO DOOR WERE REPLACED PER SRM VOL II 51-30-02 AND 51-30-05.Feb 28, 2018 · N963DN · Doug MD9030 · Cargo/Baggage DoorsSDR DALA2018030101285Stiffener · crackedCRACK ON STIFFENER OVER FRAME WEB STA CANT 1531 AND 11HRS POSITION AT AFT ACCESSORY COMPARTMENT. DAMAGE OVER FRAME WEB STA CANT 1531 AND 11HRS POSITION WAS REMOVED PER SRM 51-30-05 VOL II. NEW STIFFENER WAS DRILLING AND ADJUSTED PER SRM 51-10-05 VOL II. NEW STFeb 28, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018030101284Rib · crackedCRACK ON RIB STA LES=95.96 INTERNAL STRUCTURE AT LT HORIZONTAL STABILIZER. PERMANENT REPAIR WAS ACCOMPLISHED ON RIB STA LES=95.96 INTERNAL STRUCTURE AT LT HORIZONTAL STABILIZER PER ETI -37-18-359 REV 2. AND ER/A 566298-14 REV ORG.Feb 28, 2018 · N963DN · Doug MD9030 · Horizontal Stabilizer, Spar/RibSDR DALA2018022801259Skin · damagedDAMAGE T, DURING WEIGHT AND BALANCE CHECK ON RUDDER, SKIN CUT OUT OF HINGES WERE DAMAGED. RUDDER OF THE VERTICAL STABILIZER WAS REPAIRED PER SRM VOL I 55-41-01 PARA 22, WEIGHT AND BALANCE CHECK WAS PERFORMED PER SRM VOL II 55-40-01.Feb 27, 2018 · N963DN · Doug MD9030 · Rudder, Plate/SkinSDR DALA2018022801258Tee Fitting · crackedINITIAL INSPECTION. CRACKED AFT "T" JAMB ON LT MLG WHEEL WELL DOOR JAMB OUTBD SIDE. "T" WAS REPLACED (CRACK 2") PER VOL II SRM 51-30-02 AND 51-30-05.Feb 27, 2018 · N963DN · Doug MD9030 · Fuselage Main, StructureSDR DALA2018022801257Floor Support · corrodedINITIAL INSPECTION. CORROSION ON FLOOR STRUCTURE SUPPORT BTW STA 160 TO STA 200, X=56, X=53 (2EA), X=44, X=24, AND X=14. LT SIDE. SUPPORTS WERE REPLACED PER SRM VOL II 51-30-02 AND 51-30-05.Feb 27, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022801256Floor Support · corrodedINITIAL INSPECTION. CORROSION ON FLOOR STRUCTURE SUPPORT BTW STA160 TO STA 200, X=-53 TO X=-44 RT SIDE. SUPPORTS WERE REPLACED PER SRM VOL II 51-30-02.Feb 27, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022701210Tripler · corrodedCORROSION ON REPAIR TRIPLER OF AFT P-DOME OF STA Y-1395 BTW LONGS 29LH-27RH AT AFT CARGO COMPARTMENT. FINGER DOUBLER, FILLER AND TRIPLER WERE REMPLACED PER MD90 VOL I SRM 53-10-03 FIG 1. (LP0441512)Feb 26, 2018 · N963DN · Doug MD9030 · Fuselage Main, BulkheadSDR DALA2018022701208Frame · corrodedCORROSION FOUND ON THE FRAME WEB AFT FACE AT BS 1395 BETWEEN LONGERONS 27R & 27L. THE FRAME WAS REPAIRED IAW SRM 51-11-01, FIG 1, VOL 1.Feb 26, 2018 · N963DN · Doug MD9030 · Fuselage Main, FrameSDR DALA2018022601137Floor Panel · crackedINITIAL INSPECTION : CRACKED CHANNEL ON FLOOR PANEL 222VG, 222QG, 222KG, 222FG, 221XF, 221TF, 222AG, 222AWG, 222ANG, 222YF, 223JF, 222ADF IN PAX CABIN. FLOOR GENERATION PANEL 222VG, 222QG, 222KG, 222FG, 221XF, 221TF, 222AG, 222AWG, 222ANG, 222YF, 223JF, 222ADFeb 25, 2018 · N963DN · Doug MD9030 · Fuselage Floor PanelSDR DALA2018022601146Pan · crackedCRACKED RINGPANS (2EA) ON LT/RT WINDOW UPPER AFT CORNER OF STA 1003. (CRACK LONG 0.400") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601145Pan · crackedCRACK ON RINGPAN LOWER CORNER FWD STA 1156 RT SIDE. (CRACK LONG 0.385") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601144Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1135 AND LOWER CORNER FWD STA 1154 LT SIDE. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601143Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1078 LT SIDE. (CRACK LONG 0.0405") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601142Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1116 LT SIDE. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601141Pan · crackedCRACK ON RING PAN AFT UPPER CORNER STA Y=1155 RT. (CRACK LONG 0.0380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601140Pan · crackedCRACK ON RING PAN FWD UPPER CORNER STA Y= 1002 AND FWD LWR STA Y= 1136 RT. (CRACK LONG 0.400") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601139Floor Support · corrodedCORROSION ON FLOOR STRUCTURE SUPPORT AT STA 200, BTW X=7 TO X=-7LT/RT, X=8 TO X=14 LT AND STA 196, X=14 TO X =44 LT SIDE. CORROSION 2 IN REF NRC 00643 SUPPORTS WERE REPLACED 3 E/A PER SRM 51-30-02 AND 51-30-05.Feb 25, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022601136Pan · crackedCRACK ON RING PAN FWD UPPER CORNER STA Y= 522 AND AFT LWR STA Y=943 RT. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601135Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1097 AND LOWER CORNER FWD STA 1079 LT SIDE. AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601134Pan · crackedCRACK ON RINGPAN UPPER CORNER AFT STA 1154 AND LOWER CORNER FWD STA 1137 LT SIDE. AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.Feb 25, 2018 · N963DN · Doug MD9030 · Passenger Compartment WindowsSDR DALA2018022601138Longeron · crackedCRACK ON LONG 12 LT STA Y=1486 AT AFT ACCESSORY COMPARTMENT. LONG 12 LT STA Y=1486 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER VOL I SRM 53-10-01 FIG 7.Feb 24, 2018 · N963DN · Doug MD9030 · Fuselage Main, Longeron/StringerSDR DALA2018022601133Floor Support · corrodedCORROSION OUT OF LIMITS ON FLOOR SUPPORT STA 200, X-7 TO X-44 AT CPAX W1(RT SIDE). LEVEL CORROSION 2 FLOOR SUPPORT WAS REPLACED PER SRM VOL II 51-30-02 AND 51-30-05.Feb 24, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022601132Intercostal · crackedCRACK FLOOR STRUCTURE INTERCOSTAL BTW STA 1344 TO STA 1364, X=-0 CTR. NEW INTERCOSTAL BTW STA 1344 TO STA 1364, X=-0 WAS REPLACED PER VOL II SRM 51-30-02.Feb 24, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022601131Splice · crackedLATE FINDING CRACK ON AFT LOWER INTERNAL SPLICE AT LT MLG DOOR. (CRACK LENGTH=4") AFT LOWER INTERNAL SPLICE AT LT MLG DOOR WAS REPAIRED PER CMM 32-17-05 REPAIR 2.Feb 24, 2018 · N963DN · Doug MD9030 · Landing Gear DoorsSDR DALA2018022601130Web · crackedCRACKED WEB STA Y=218, X= -26 AT E&E COMPARTMENT CEILING AREA. DIMENSIONS CRACKS, 1.125", .750" WEB WAS REPAIRED PER VOL I SRM 53-00-01 FIG 6 AND VOL II SRM 51-30-02.Feb 23, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022401121Seat Track · corrodedCORROSION ON SEAT TRACK X=-22, BTW STA 200 TO STA 237 RT SIDE. LEVEL CORROSION 2 SEAT TRACK WAS REPLACED X=-22 STA Y=200 TO Y=266 PER SRM 51-30-01 AND 51-30-05 VOLUME II.Feb 23, 2018 · N963DN · Doug MD9030 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018022401120Seat Track · corrodedINITIAL INSPECTION. CORROSION ON SEAT TRACK X=-44, BTW STA 200 TO STA 256 RT SIDE. SEAT TRACK WAS REPLACED PER SRM 51-30-01 AND 51-10-05 VOLUME II.Feb 23, 2018 · N963DN · Doug MD9030 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018022301082Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PLATES NR 520AT, 520JB, 520DT ON LT WING. (CORROSION LEVEL 2) FUEL ACCESS PLATES NR 520DT, 520JB AND 520AT WAS REPLACED PER SRM VOL I 57-00-04 PAR 4 CONDITION II.Feb 22, 2018 · N963DN · Doug MD9030 · Wing, Plate/SkinSDR DALA2018022301081Web · corrodedINITIAL INSPECTION. CORROSION ON WEB STA Y=195, X=-55 AT E/E. (CORROSION LEVEL 2 ) MEMBRANE WAS REPAIRED PER VOL I SRM 51-11-01.Feb 22, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022201056Beam · crackedINITIAL INSPECTION: CRACK ON BEAM 1 BTW STA Y195/200 AT FWD ENTRY DOOR L1. BEAM NR 1 BTW STA Y: 195-200 WAS REPAIRED PER SRM VOL I 52-10-02 PARAGRAPH 6, FIG 5.Feb 21, 2018 · N963DN · Doug MD9030 · Passenger/Crew DoorsSDR DALA2018022201055Support · corrodedCORROSION ON FLOOR STRUCTURE SUPPORT BTW STA160 TO STA 200, X=7 TO X=-7 LT/RT SIDE. FLOOR SUPPORT WERE REPLACED PER SRM 51-30-01 VOL II.Feb 21, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022201054Seat Track · corrodedOUT OF LIMITS CORROSION ON LT SEAT TRACK X=44 BTW STA Y 1277-1279 AT PASSENGER CABIN. AREA WAS REPAIRED PER VOL I SRM 53-40-01 FIG 2.Feb 21, 2018 · N963DN · Doug MD9030 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018022101053Shim · corrodedINITIAL INSPECTION: CORROSION ON SHIMS BELOW LOWER FITTING STA Y=1231 AT AFT CARGO DOOR. SHIMS BELOW LOWER FITTING STA Y=1231 AT AFT CARGO DOOR WERE REPLACED PER SRM 51-30-02, 51-30-05, 51-30-01 VOL II.Feb 20, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022101050Skin · crackedCRACK ON RAM AIR SCOPE AT VERTICAL STABILIZER LEADING EDGE. CRACKS ON RAM AIR SCOPE AT VERTICAL STABILIZER LEADING EDGE, WERE REPAIRED (WELDED) PER ER/A 382101-14MA REV H.Feb 20, 2018 · N963DN · Doug MD9030 · Vertical Stabilizer, Plate/SkinSDR DALA2018022101022Cusp Web · crackedINITIAL INSPECTION, CRACK LT CUSP MEMBRANE ON STA Y=883 AT PASSENGER CABIN. REPAIRED PER VOL I SRM 53-20-02 FIG 6.Feb 20, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022101021Cusp Web · puncturedINITIAL INSPECTION, PUNCTURE ON LT CUSP MEMBRANE STA Y=928 AT PASSENGER CABIN. DOUBLER WAS REMOVED ON STA Y=928 LT PER VOL II S-R-M 51-30-02 AND 51-30-01. PREVIOUS REPAIR DOUBLER WAS FABRICATED PER VOL II SRM 53-10-03, NEW DOUBLER WAS INSTALLED PER VOL II SRM Feb 20, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018022101020Seat Track · corrodedOUT OF LIMITS CORROSION ON SEAT TRACK BTW STA Y=1260-1263 AND X=22 AT PASSENGER CABIN. CORROSION 2 AREA WAS REPAIRED PER VOL I SRM 53-40-01 FIG 2.Feb 20, 2018 · N963DN · Doug MD9030 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018022101019Seat Track · corrodedOUT OF LIMITS CORROSION ON LT SEAT TRACK X=44 BTW STA Y 1262-1264 AT PASSENGER CABIN. AREA WAS REPAIRED PER VOL I SRM 53-40-01 FIG 2.Feb 20, 2018 · N963DN · Doug MD9030 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018021901000Web · crackedINITIAL INSPECTION. CRACKED WEB STA Y=133, X=7 AT COCKPIT FLOOR STRUCTURE. CRACK .750" AREA WAS REPAIRED PER SRM 53-00-01 PAR 8 FIG 6 VOL I.Feb 18, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018021800970Cusp Web · puncturedPUNCTURE ON THE RT CUSP WEB BETWEEN BS 1136 AND 1140, RBL 54 AND 60. REPAIRED IAW SRM 53-00-01, PARAGRAPH 5C, (2), (B), FIG 2.Feb 17, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018021800969Web · crackedCRACKED WEB, BS 1231. THE WEB WAS REPLACED IAW DWG 9957994, REV N, SRM 51-30-02, AND 51-30-05, VOL II.Feb 17, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018021800968Angle · crackedA CRACK ON THE ANGLE BETWEEN BEAM 5 AND INTERNAL PAN, BS 1231 AT AFT CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-02, 52-30-05, AND DRAWING 9957884, REV N.Feb 17, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018021700962Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PLATES NBR 520CT AND 620CT ON LH/RH WINGS. FUEL ACCES PLATES 520CT AND 620CT WERE REPLACED DUE TO BLEND OUT REPAIR IS NOT PERMITED PER MD-90 SRM VOL I 57-00-04 PAR 4 CONDITION III . (LP0428283)Feb 16, 2018 · N963DN · Doug MD9030 · Wing, Plate/SkinSDR DALA2018020100711Hydraulic Line · leakingRIGHT HYDRAULIC QUANTITY LOW, RAN QRH SHOWED NORMAL QUANTITY AFTER CONFIGURING, GOT DOWN TO 5 QUARTS ON LANDING. MAINTENANCE FOUND MAJOR LEAK IN RIGHT ENGINE PYLON, SMALL LEAK ON PTU RIGHT SYSTEM FEED LINE, RETORQUED SAME. FOUND STEADY LEAK DURING DRY MOTOR Jan 31, 2018 · N963DN · Doug MD9030 · Hydraulic System, MainSDR DALA2018010500108Brake · contaminatedPOST FLIGHT INSPECTION FOUND HYDRAULIC FLUID AROUND NR 1 TIRE. SMOKE VISIBLE IN BRAKE AREA. BRAKE TEMPERATURE ONLY 200 DEGREES. HYDRAULIC FLUID SMOKING. REMOVED AND REPLACED THE NR 1 BRAKE IAW MM. OPERATION AND LEAKS CHECK GOOD.Dec 28, 2017 · N963DN · Doug MD9030 · Landing Gear Brake SystemSDR DALA2017122008778Electronic Unit · odorDESCENDING THROUGH 600FT ON APPROACH LEFT GEN OFF AND LEFT AC PWR FAULT. MESSAGES ILLUMINATED ON OAP AFTER ABOUT 1 MINUTE WE LOST ALL AC PWR. SWITCHED EMERGENCY POWER SWITCH TO "ON" BUT GOT NO POWER RESTORED UNTIL THE APU CAME ONLINE. PER ASAP, EMERGENCY DECDec 18, 2017 · N963DN · Doug MD9030 · AC Generator-AlternatorSDR DALA2017111708201Angle · crackedDOUBLER ANGLE CRACKED AT BS 1486 BETWEEN LONGERONS 2 AND 3R. REMOVED, FABRICATED AND INSTALLED A REPAIR IAW DWG 9953016.Nov 16, 2017 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
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