N37078, cancelled Jan 14, 2010

Service difficulty reports · 43

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 = 'N37078' AND deregistration_id = 'N37078-2010-01-14'
  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 CALA0000687Battery · dischargedTHE L-3 DOOR AND R-1 DOOR ESCAPE SLIDE LIGHTS TESTED DIM. THE SLIDE LIGHT BATTERY WAS REPLACED AT EACH DOOR AND OPERATION CHECKED GOOD IAW MM 25-61-01.May 16, 2000 · N37078 · Doug DC1030 · Escape SlideSDR CALA0000492Galley Track · corrodedINSPECTION FOUND GALLEY SUPPORTS CORRODED AT STA 1887 - 1900, BL 0 AND RBL 55 AND AT STA 1871 - 1887, RBL 33. THE SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-31-01.Apr 15, 2000 · N37078 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000491Galley Track · corrodedINSPECTION FOUND GALLEY SUPPORT CORRODED AT STA 1887 - 2007, RBL 27 AND LBL 27. THE SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-31-01.Apr 15, 2000 · N37078 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000490Galley Track · corrodedINSPECTION FOUND GALLEY SUPPORT CORRODED AT STA 1020, LBL 27. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01.Apr 15, 2000 · N37078 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000489Galley Track · corrodedINSPECTION FOUND GALLEY SUPPORT CORRODED AT STA 1910, LBL 55. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01.Apr 15, 2000 · N37078 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000463Floorbeam · corrodedINSPECTION FOUND FLOORBEAMS CORRODED AT STA 1887, BETWEEN RBL 25 - 30, RBL 35 -55, AND RBL 65 - 100. THE FLOORBEAMS WERE REMOVED AND NEW FLOORBEAMS WERE INSTALLED IAW SRM 51-31-01.Apr 13, 2000 · N37078 · Doug DC1030 · Fuselage Main, Floor BeamSDR CALA9901559Gear Handle · bindingWHEN THE LANDING GEAR WAS EXTENDED ON APPROACH TO EWR, NO GREEN GEAR SAFE LIGHTS ILLUMINATED. THE GEAR WAS CYCLED THREE TIMES BEFORE RECEIVING GREEN DOWN AND LOCKED INDICATIONS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED BITE ON PROX BOX ANDec 6, 1999 · N37078 · Doug DC1030 · Landing Gear SelectorSDR CALA9900490Frame · corrodedCENTER CARGO BAY DOOR FRAME LOWER SECTION CORRODED. REPAIRED PER SRM 53-50-00.May 6, 1999 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900473Skin · crackedNR 1 LEFT SLAT OUTER SKIN CRACKED. REPAIRED PER SRM 57-10-00, NR 6 LEADING EDGE RIB FOUND CRACKED. NEW RIBS FABRICATED PER DWG NRB6223 OP 3 AND ARB1583-405 OP 1.May 5, 1999 · N37078 · Doug DC1030 · Leading Edge DevicesSDR CALA9900457Angle · crackedMAN - SUSPECT CRACK LT DRAG ANGLE AT LOWER END OF THIRD BANJO FITTING. AFTER NDT INSPECTION, CRACK CONFIRMED (1 INCH). CRACK STOP-DRILLED PER SRM 55-20-00. REPAIR PLATE MANUFACTURED, HEAT TREATED, AND FITTED PER SRM 55-20-00, FIG 3. (X)May 3, 1999 · N37078 · Doug DC1030 · Nacelle/Pylon StructureSDR CALA9900456Angle · crackedMAN - RIGHT HAND DRAG ANGLE AT LOWER END OF THIRD BANJO FITTING. SUBMITTER SUSPECTED CRACK. AFTER NDT, CRACK CONFIRMED (1 INCH). STOP-DRILLED CRACK PER SRM 55-20-00. REPAIR ANGLE MANUFACTURED, HEAT TREATED, AND FITTED PER SRM 55-20-00 FIG 3. (X)May 3, 1999 · N37078 · Doug DC1030 · Nacelle/Pylon StructureSDR CALA9900455Angle · crackedMAN - SUSPECT CRACK RIGHT DRAG ANGLE REPAIR PLATE AT LOWER END OF FIRST BANJO FITTING. AFTER NDT INSPECTION, CRACK CONFIRMED (1 INCH). CRACK STOP-DRILLED PER SRM 55-20-00, FIG 3. REPAIR PLATE REMOVED AND REPLACED PER SRM 55-20-00 FIG 3. (X)May 3, 1999 · N37078 · Doug DC1030 · Nacelle/Pylon StructureSDR CALA9801328Battery Pack · dischargedTHE EMERGENCY TRACK LIGHTING FAILED TEST. THE MID GALLEY BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.Jul 22, 1998 · N37078 · Doug DC1030 · Emergency LightingSDR CALA9701799Actuator · damagedA LOUD CLUNK WAS HEARD IN COCKPIT AREA ON GEAR RETRACTION, FOLLOWED BY UNSAFE NOSE GEAR INDICATION. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR RETRACT ACTUATOR ROD END, GROUND SENSE Dec 26, 1997 · N37078 · Doug DC1030 · Landing Gear ActuatorSDR CALA9700822Fuel Filter · contaminatedNR 3 ENG FLAMED OUT WHILE DESCENDING THRU FL 220 EN ROUTE. ENG FAILURE WAS ACCOMPANIED BY ILLUMINATION OF BOTH NR 3 GEN OFF LIGHT AND THE NR 3 ENG LOW OIL PRESS LIGHT. ENG WAS RESTARTED, A/C LANDED W/O INCIDENT. INSPECT FOUND THE NR 3 ENG FUEL FILTER AND NRJun 4, 1997 · N37078 · Doug DC1030 · Engine Fuel DistributionSDR CALA9700401Splice · corrodedINSPECTION FOUND STRINGER SPLICE CORRODED AT STA 1135 TO 1137. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 51-31-01.Jan 21, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700403Splice · corrodedINSPECTION FOUND STRINGER 27R SPLICE CORRODED AT STA 1120. THE SPLICE WAS REMOVED AND REPLACED IAW SRM 51-33-01 AND 51-10-00.Jan 19, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700100Splice · crackedINSPECTION FOUND A .5 INCH CRACK IN STRINGER SPLICE BETWEEN STA 1521 AND 1541, STRINGER 1L. THE SPLICE WAS REMOVED AND REPLACED IAW SRM 51-31-01.Jan 16, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700101Angle · corrodedINSPECTION FOUND T-ANGLE CORRODED AT STA 464, X= -4 INSIDE OF NLG WHEEL WELL FORWARD BULKHEAD. THE T-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-40-00, 51-11-01, 51-31-01 AND 51-21-01.Jan 11, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700402Mount · crackedINSPECTION FOUND A 3 INCH CRACK IN FILLET FAIRING MOUNT AT STA 1099, LONGERON 36. THE MOUNT WAS REMOVED AND REPLACED IAW SRM 51-31-01.Jan 8, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700400Support · crackedINSPECTION FOUND FLOORBOARD SUPPORT CRACKED IN SIX PLACES AT STA 1887, X = 38-57. THE CRACKS WERE 1 OR LESS IN LENGTH. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 51-21-01.Dec 28, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700392Support · corrodedINSPECTION FOUND CORROSION ON FLOOR SUPPORT AROUND GALLEY FLOOR SPACER AT STA 497, X+22. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. TWO EACH BOSSES WERE REMOVED AND REPLACED IAW SRM 51-31Dec 28, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700395Panel · gougedINSPECTION FOUND A GOUGE AT CORNER EDGE OF VERTICAL STABILIZER ACCESS PANEL NR 373EL. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-00-01, FIGURE 3 AND 51-21-01.Dec 21, 1996 · N37078 · Doug DC1030 · Vertical Stabilizer, Plate/SkinSDR CALA9700387Panel · crackedINSPECTION FOUND A 1 INCH CRACK AT CUTOUT OF NR 1 ENGINE PYLON PANEL NR 437DR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 1 AND 2.Dec 17, 1996 · N37078 · Doug DC1030 · Nacelle/Pylon, Plate/SkinSDR CALA9700390Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK ON SUPPORT ANGLE UNDER BODY FILLET JUST ABOVE WING AT FS 1341R. THE CRACKED AREA WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01 AND 53-53-01.Dec 11, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700385Longeron · corrodedINSPECTION FOUND LONGERON 4L CORRODED BETWEEN BS 1119 TO 1139. THE CORRODED SPLICE WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 53-10-00 FIGURE 3, 53-13-01 FIGURE 33 AND 51-21-01.Dec 11, 1996 · N37078 · Doug DC1030 · Fuselage Main, Longeron/StringerSDR CALA9700408Support · crackedINSPECTION FOUND TWO CRACKS UP TO .35 LONG IN FLOORBOARD SUPPORT AT STA 1965, X -1 TO 16. ALSO, TWO CRACKS UP TO .20 INCH LONG WERE FOUND IN FLOORBOARD SUPPORT AT STA 1965, X + 1 TO 16. NEW FLOOR SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700407Support · crackedINSPECTION FOUND A .20 INCH CRACK IN FLOORBOARD SUPPORT AT STA 1921, X + 1 TO 16. TWO CRACKS UP TO .30 INCH LONG WERE FOUND IN FLOORBOARD SUPPORT AT STA 1921, X - 1 TO 16. NEW FLOOR SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01.Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700406Support · crackedINSPECTION FOUND THREE CRACKS UP TO .30 INCH LONG IN FLOORBOARD SUPPORT AT STA 1943, X - 11 TO 16. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01.Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700405Support · crackedINSPECTION FOUND A .35 INCH CRACK IN FLOORBOARD SUPPORT AT STA 1943, X-1 TO 16. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01.Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700404Support · crackedINSPECTION FOUND TWO CRACKS APPROXIMATELY .5 INCH LONG IN FLOORBOARD SUPPORT AT STA 1986, X + 1 TO 16. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01.Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700394Support · corrodedINSPECTION FOUND LAV TIE DOWN FLOOR SUPPORT CORRODED AT STA 1915 AND 2004, LBL X+55. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-70-00.Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700391Support · corrodedINSPECTION FOUND CORROSION ON LAV TIE DOWN FLOOR SUPPORT AT STA 2004, X-55. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-70-01, FIGURE 13.Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700386Casting · corrodedINSPECTION FOUND STRINGER 24R CASTING CORRODED BETWEEN STA 1321 AND 1341. THE CASTING WAS REMOVED AND REPLACED IAW SRM 51-33-01.Dec 9, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700389Support · crackedINSPECTION FOUND FLOORBOARD SUPPORT CRACKED IN THREE PLACES AT STA 420, X-13 TO X-22. THE CRACKS WERE .125 INCH LONG. THE FLOOR SUPPORT WAS REMOVED, A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01 AND 51-35-01.Dec 7, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700388Bulkhead Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT L-ANGLE AT CENTER CARGO FORWARD BULKHEAD FS 1521, RBL 19. THE CRACK WAS STOP DRILLED, AN L-ANGLE AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 2 AND 51-31-01.Dec 6, 1996 · N37078 · Doug DC1030 · Fuselage Main, BulkheadSDR CALA9700398Skin · rippledINSPECTION FOUND RIPPLING ONE FOOT IN DIAMETER IN RT WING NR 1 SLAT AT INBOARD END. THE RIPPLED AREA WAS CUT OUT, A SKIN INSERT, SPLICE STRAPS, DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-00, FIGURE 43 AND 51-31-01.Dec 5, 1996 · N37078 · Doug DC1030 · Leading Edge DevicesSDR CALA9700102Skin · dentedINSPECTION FOUND A 5 INCH DIAMETER BY 0.060 DEEP DENT IN OUTBOARD RT WING NR 3 SLAT. A SKIN AND DOUBLER REPAIR WAS INSTALLED IAW SRM 57-10-00, FIGURE 11.Dec 4, 1996 · N37078 · Doug DC1030 · Leading Edge DevicesSDR CALA9700103Wing Tip · creasedINSPECTION FOUND A 3L BY .5W BY 0.080D CREASE IN RT WING TIP AT XW 988, BETWEEN TIP LEADING EDGE AND TRAILING EDGE. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-00-01, FIGURE 4 AND SRM 57-31-01 FIGURE 3.Dec 3, 1996 · N37078 · Doug DC1030 · Wing Miscellaneous StructureSDR CALA9700397Panel · dentedINSPECTION FOUND FOUR DENTS ON UPPER SURFACE OF RT WING TRAILING EDGE PANEL 641HB. A DOUBLER AND FOUR FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-71-00, FIGURE 33.Nov 30, 1996 · N37078 · Doug DC1030 · Wing, Plate/SkinSDR CALA9700399Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 879 AND 899, Y= -44. CHANNEL FLOOR SUPPORT ANGLES AND BOSSES WERE FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01 AND 53-70-00.Nov 27, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700396Angle · corrodedINSPECTION FOUND L-ANGLE CORRODED AT FORWARD ADF LOOP ANTENNA. AN L-ANGLE WAS FABRICATED AND INSTALLED WITH NUT PLATES IAW SRM 53-00-01, FIGURE 2, SHEET 2, 51-11-01, 51-31-01, 51-21-01 AND 51-30-00.Nov 27, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9700393Frame · corrodedINSPECTION FOUND FORWARD SIDE OF FRAME CORRODED IN AFT CARGO BILGE AREA AT STA 1781 FROM LONGERON 50L TO 50R. THE CORRODED SECTION WAS CUT OUT, AN L-ANGLE DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-00, FIGURE 8, 51-21-01 AND 53-30-01 FIGURNov 6, 1996 · N37078 · Doug DC1030 · Fuselage Main, Frame
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