# Service difficulty reports: N37078, cancelled Jan 14, 2010 A list on [N37078, cancelled Jan 14, 2010](https://openairdocs.org/deregistered/N37078-2010-01-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA0000687](https://openairdocs.org/sdr/CALA0000687.md): Battery · discharged · May 16, 2000 · N37078 · Doug DC1030 · Escape Slide > THE 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. - [SDR CALA0000492](https://openairdocs.org/sdr/CALA0000492.md): Galley Track · corroded · Apr 15, 2000 · N37078 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION 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. - [SDR CALA0000491](https://openairdocs.org/sdr/CALA0000491.md): Galley Track · corroded · Apr 15, 2000 · N37078 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND GALLEY SUPPORT CORRODED AT STA 1887 - 2007, RBL 27 AND LBL 27. THE SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-31-01. - [SDR CALA0000490](https://openairdocs.org/sdr/CALA0000490.md): Galley Track · corroded · Apr 15, 2000 · N37078 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND GALLEY SUPPORT CORRODED AT STA 1020, LBL 27. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA0000489](https://openairdocs.org/sdr/CALA0000489.md): Galley Track · corroded · Apr 15, 2000 · N37078 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND GALLEY SUPPORT CORRODED AT STA 1910, LBL 55. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA0000463](https://openairdocs.org/sdr/CALA0000463.md): Floorbeam · corroded · Apr 13, 2000 · N37078 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION 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. - [SDR CALA9901559](https://openairdocs.org/sdr/CALA9901559.md): Gear Handle · binding · Dec 6, 1999 · N37078 · Doug DC1030 · Landing Gear Selector > WHEN 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 AN - [SDR CALA9900490](https://openairdocs.org/sdr/CALA9900490.md): Frame · corroded · May 6, 1999 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > CENTER CARGO BAY DOOR FRAME LOWER SECTION CORRODED. REPAIRED PER SRM 53-50-00. - [SDR CALA9900473](https://openairdocs.org/sdr/CALA9900473.md): Skin · cracked · May 5, 1999 · N37078 · Doug DC1030 · Leading Edge Devices > NR 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. - [SDR CALA9900457](https://openairdocs.org/sdr/CALA9900457.md): Angle · cracked · May 3, 1999 · N37078 · Doug DC1030 · Nacelle/Pylon Structure > MAN - 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) - [SDR CALA9900456](https://openairdocs.org/sdr/CALA9900456.md): Angle · cracked · May 3, 1999 · N37078 · Doug DC1030 · Nacelle/Pylon Structure > MAN - 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) - [SDR CALA9900455](https://openairdocs.org/sdr/CALA9900455.md): Angle · cracked · May 3, 1999 · N37078 · Doug DC1030 · Nacelle/Pylon Structure > MAN - 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) - [SDR CALA9801328](https://openairdocs.org/sdr/CALA9801328.md): Battery Pack · discharged · Jul 22, 1998 · N37078 · Doug DC1030 · Emergency Lighting > THE EMERGENCY TRACK LIGHTING FAILED TEST. THE MID GALLEY BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA9701799](https://openairdocs.org/sdr/CALA9701799.md): Actuator · damaged · Dec 26, 1997 · N37078 · Doug DC1030 · Landing Gear Actuator > A 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 - [SDR CALA9700822](https://openairdocs.org/sdr/CALA9700822.md): Fuel Filter · contaminated · Jun 4, 1997 · N37078 · Doug DC1030 · Engine Fuel Distribution > NR 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 NR - [SDR CALA9700401](https://openairdocs.org/sdr/CALA9700401.md): Splice · corroded · Jan 21, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND STRINGER SPLICE CORRODED AT STA 1135 TO 1137. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS INSTALLED IAW SRM 51-31-01. - [SDR CALA9700403](https://openairdocs.org/sdr/CALA9700403.md): Splice · corroded · Jan 19, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND STRINGER 27R SPLICE CORRODED AT STA 1120. THE SPLICE WAS REMOVED AND REPLACED IAW SRM 51-33-01 AND 51-10-00. - [SDR CALA9700100](https://openairdocs.org/sdr/CALA9700100.md): Splice · cracked · Jan 16, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700101](https://openairdocs.org/sdr/CALA9700101.md): Angle · corroded · Jan 11, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700402](https://openairdocs.org/sdr/CALA9700402.md): Mount · cracked · Jan 8, 1997 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700400](https://openairdocs.org/sdr/CALA9700400.md): Support · cracked · Dec 28, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700392](https://openairdocs.org/sdr/CALA9700392.md): Support · corroded · Dec 28, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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 51-31 - [SDR CALA9700395](https://openairdocs.org/sdr/CALA9700395.md): Panel · gouged · Dec 21, 1996 · N37078 · Doug DC1030 · Vertical Stabilizer, Plate/Skin > INSPECTION 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. - [SDR CALA9700387](https://openairdocs.org/sdr/CALA9700387.md): Panel · cracked · Dec 17, 1996 · N37078 · Doug DC1030 · Nacelle/Pylon, Plate/Skin > INSPECTION 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. - [SDR CALA9700390](https://openairdocs.org/sdr/CALA9700390.md): Angle · cracked · Dec 11, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700385](https://openairdocs.org/sdr/CALA9700385.md): Longeron · corroded · Dec 11, 1996 · N37078 · Doug DC1030 · Fuselage Main, Longeron/Stringer > INSPECTION 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. - [SDR CALA9700408](https://openairdocs.org/sdr/CALA9700408.md): Support · cracked · Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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 51 - [SDR CALA9700407](https://openairdocs.org/sdr/CALA9700407.md): Support · cracked · Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700406](https://openairdocs.org/sdr/CALA9700406.md): Support · cracked · Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700405](https://openairdocs.org/sdr/CALA9700405.md): Support · cracked · Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700404](https://openairdocs.org/sdr/CALA9700404.md): Support · cracked · Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700394](https://openairdocs.org/sdr/CALA9700394.md): Support · corroded · Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700391](https://openairdocs.org/sdr/CALA9700391.md): Support · corroded · Dec 10, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700386](https://openairdocs.org/sdr/CALA9700386.md): Casting · corroded · Dec 9, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND STRINGER 24R CASTING CORRODED BETWEEN STA 1321 AND 1341. THE CASTING WAS REMOVED AND REPLACED IAW SRM 51-33-01. - [SDR CALA9700389](https://openairdocs.org/sdr/CALA9700389.md): Support · cracked · Dec 7, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700388](https://openairdocs.org/sdr/CALA9700388.md): Bulkhead Angle · cracked · Dec 6, 1996 · N37078 · Doug DC1030 · Fuselage Main, Bulkhead > INSPECTION 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. - [SDR CALA9700398](https://openairdocs.org/sdr/CALA9700398.md): Skin · rippled · Dec 5, 1996 · N37078 · Doug DC1030 · Leading Edge Devices > INSPECTION 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. - [SDR CALA9700102](https://openairdocs.org/sdr/CALA9700102.md): Skin · dented · Dec 4, 1996 · N37078 · Doug DC1030 · Leading Edge Devices > INSPECTION 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. - [SDR CALA9700103](https://openairdocs.org/sdr/CALA9700103.md): Wing Tip · creased · Dec 3, 1996 · N37078 · Doug DC1030 · Wing Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700397](https://openairdocs.org/sdr/CALA9700397.md): Panel · dented · Nov 30, 1996 · N37078 · Doug DC1030 · Wing, Plate/Skin > INSPECTION 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. - [SDR CALA9700399](https://openairdocs.org/sdr/CALA9700399.md): Support · corroded · Nov 27, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700396](https://openairdocs.org/sdr/CALA9700396.md): Angle · corroded · Nov 27, 1996 · N37078 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9700393](https://openairdocs.org/sdr/CALA9700393.md): Frame · corroded · Nov 6, 1996 · N37078 · Doug DC1030 · Fuselage Main, Frame > INSPECTION 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 FIGUR ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N37078-2010-01-14/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.