# Service difficulty reports: N37077, cancelled Nov 4, 2005

A list on [N37077, cancelled Nov 4, 2005](https://openairdocs.org/deregistered/N37077-2005-11-04.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA0100048](https://openairdocs.org/sdr/CALA0100048.md): Floorbeam · corroded · Jan 19, 2001 · N37077 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED IN PASSENGER CABIN AT STA 495, LT SIDE. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-31-01.
- [SDR CALA0100047](https://openairdocs.org/sdr/CALA0100047.md): Floor Support · corroded · Jan 19, 2001 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TRANSVERSAL SUPPORT UNDER FLOOR PANEL 244AF IN MID PASSENGER CABIN CORRODED AT STA 816. REPLACED SUPPORT IAW SRM 51-31-01.
- [SDR CALA0100036](https://openairdocs.org/sdr/CALA0100036.md): Frame · cracked · Jan 16, 2001 · N37077 · Doug DC1030 · Fuselage Main, Frame
  > INSPECTION FOUND A 0.8 INCH CRACK IN FRAME AT STA 1841 IN CENTER CARGO AREA. REPAIRED IAW SRM 53-00-01, FIGURE 4, SHEET 2.
- [SDR CALA0100035](https://openairdocs.org/sdr/CALA0100035.md): Floor Support · corroded · Jan 16, 2001 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LEFT O/B GALLEY FLOOR SUPPORT CORRODED IN MID PASSENGER CABIN, STA 824 - 840. THE SUPPORT WAS REPLACED IAW SRM 51-31-01.
- [SDR CALA0100034](https://openairdocs.org/sdr/CALA0100034.md): Floor Support · corroded · Jan 16, 2001 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PASSENGER CABIN RT SUPPORT IN CENTER LAV CORRODED. THE SUPPORT WAS REPLACED IAW SRM 51-31-01.
- [SDR CALA0100033](https://openairdocs.org/sdr/CALA0100033.md): Floorbeam · corroded · Jan 16, 2001 · N37077 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT LT MID PASSENGER CABIN, STA 857 - 899. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-31-01.
- [SDR CALA0100028](https://openairdocs.org/sdr/CALA0100028.md): Frame · cracked · Jan 15, 2001 · N37077 · Doug DC1030 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN CENTER CARGO FRAME AT STA 1841. REPAIRED IAW SRM 53-00-01, FIGURE 4, SHEET 2.
- [SDR CALA0100027](https://openairdocs.org/sdr/CALA0100027.md): Bracket · cracked · Jan 15, 2001 · N37077 · Doug DC1030 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN RT WING I/B BRACKET AT I/B SIDE PANEL. A NEW BRACKET WAS INSTALLED IAW ECRA 5730-01741.
- [SDR CALA9900100](https://openairdocs.org/sdr/CALA9900100.md): Elevator · damaged · Feb 1, 1999 · N37077 · Doug DC1030 · Elevator Structure
  > INSPECTION FOUND IMPACT DAMAGE TO RT ELEVATOR TIP CAUSED BY HANGAR DOOR. A NEW ELEVATOR WAS INSTALLED IAW MM 27-30-09, PAGE 401. ELEVATOR OPERATION CHECKED GOOD IAW MM 27-30-03, PAGE 601.
- [SDR CALA9900099](https://openairdocs.org/sdr/CALA9900099.md): Skin · cracked · Jan 31, 1999 · N37077 · Doug DC1030 · Wing, Plate/Skin
  > INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE DROOP PANEL UPPER SKIN. TWO RIBS WERE REMOVED AND REPLACED. THE SKIN WAS REINFORCED WITH DOUBLER AND INSTALLED IAW SRM 57-10-00, FIGURE 55, 51-21-01, AND 51-31-01.
- [SDR CALA9900098](https://openairdocs.org/sdr/CALA9900098.md): Rib · cracked · Jan 30, 1999 · N37077 · Doug DC1030 · Leading Edge Devices
  > INSPECTION FOUND A.25 INCH CRACK IN NR 1 SLAT RIB. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-31-01.
- [SDR CALA9900090](https://openairdocs.org/sdr/CALA9900090.md): Support · corroded · Jan 27, 1999 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED IN MAIN DECK AT STA 1871 NEAR LAV E. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-70-00, 51-21-01, AND 51-31-01.
- [SDR CALA9800101](https://openairdocs.org/sdr/CALA9800101.md): Hyd Pump · leaking · Jan 24, 1998 · N37077 · Doug DC1030 · Hydraulic Pump (Electric/Engine), Main
  > THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT CAME ON JUST PRIOR TO LANDING AT LGW. THE ELEVATOR FEEL CHANNEL LIGHT CAME ON AFTER LANDING. THE AIRCRAFT HAD LOST FLUID FROM THE NR 3 HYDRAULIC SYSTEM. MAINTENANCE FOUND THE NR 3 ENGINE DRIVEN RIGHT HYDRAULIC PUMP
- [SDR CALA9700336](https://openairdocs.org/sdr/CALA9700336.md): Relay · inoperative · Mar 12, 1997 · N37077 · Doug DC1030 · Battery/Charger System
  > THE GROUND REFUEL POWER, FUEL TANK FILL VALVE, AND BATTERY BUS SENSING CIRCUIT BREAKERS POPPED WHILE EN ROUTE FROM FCO TO EWR. THE BATTERY BUS OFF LIGHT ILLUMINATED AND THE FUEL FILL VALVES CLOSED. FUEL COULD NOT BE TRANSFERRED. THE AIRCRAFT WAS DIVERTED TO L
- [SDR CALA9700105](https://openairdocs.org/sdr/CALA9700105.md): Skin · cracked · Jan 15, 1997 · N37077 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT DOOR ACCESS CUTOUT SKIN CRACKED AT STA 1308.5 AND STA 1255. BOTH CRACKS WERE 1 INCH LONG. DOUBLERS WERE INSTALLED IAW SRM 53-00-01, FIGURE 4 AND SRM 51-35-01.
- [SDR CALA9700104](https://openairdocs.org/sdr/CALA9700104.md): Support · corroded · Jan 9, 1997 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 1986 LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01 FIGURE 1.
- [SDR CALA9700161](https://openairdocs.org/sdr/CALA9700161.md): Support · corroded · Jan 3, 1997 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND T-ANGLE FLOOR SUPPORT CORRODED IN FORWARD CARGO COMPARTMENT AT STA 1099, RBL 20. THE CORRODED AREA WAS CUT OUT, REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, PAGE 8 AND 51-21-01.
- [SDR CALA9700162](https://openairdocs.org/sdr/CALA9700162.md): Hinge Angle · cracked · Dec 18, 1996 · N37077 · Doug DC1030 · Trailing Edge Flaps
  > INSPECTION FOUND A 5.5 INCH CRACK IN UPPER RADIUS OF LOWER AFT FAIRING 535JL INBOARD HINGE AT OUTBOARD LT FLAP INBOARD FACE. THE FAIRING WAS REMOVED AND THE CORRODED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW DRAWING SKB 02
- [SDR CALA9700106](https://openairdocs.org/sdr/CALA9700106.md): Slat · gouged · Dec 18, 1996 · N37077 · Doug DC1030 · Leading Edge Devices
  > INSPECTION FOUND RT NR 6 SLAT CHAFED AND GOUGED AT INBOARD END, 12 INCHES UP FROM L/E TIP. THE SLAT WAS REPAIRED IAW ECRA 5750-02573.
- [SDR CALA9700107](https://openairdocs.org/sdr/CALA9700107.md): Support · corroded · Dec 8, 1996 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 472 LBL 54. A FLOOR SUPPORT REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-21-01, 51-31-01, 51-35-01 AND 53-60-01 FIGURE 1.
- [SDR CALA9601868](https://openairdocs.org/sdr/CALA9601868.md): Skin · corroded · Nov 29, 1996 · N37077 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED STA 1509-1521, XCW 25 TO XCW -25. SKIN DOUBLERS WERE FABRICATED AND INSTALLED IAW ECRA 5330-02465 AND SRM 51-31-01.
- [SDR CALA9601870](https://openairdocs.org/sdr/CALA9601870.md): Doubler · cracked · Nov 27, 1996 · N37077 · Doug DC1030 · Nacelle/Pylon Structure
  > INSPECTION FOUND BOTH INBOARD AND OUTBOARD FORWARD UPPER ATTACH DOUBLERS OF NR 3 PYLON AFT FAIRING 489AL CRACKED THROUGH. THE CRACKED DOUBLERS WERE REMOVED IAW SRM 51-30-01. NEW DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM'S 51-21-01, 51-31-01, AND 53-00-0
- [SDR CALA9601852](https://openairdocs.org/sdr/CALA9601852.md): Support · corroded · Nov 14, 1996 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THE UPPER HORIZONTAL SURFACE OF FORWARD END FLOOR SUPPORT CORRODED AT STA 1900, RBL 57. THE CORRODED SECTION WAS REMOVED, A NEW SECTION WAS SPLICED IN IAW SRM 53-70-00, FIGURE 13.
- [SDR CALA9601869](https://openairdocs.org/sdr/CALA9601869.md): Skin · cracked · Nov 11, 1996 · N37077 · Doug DC1030 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A.50 INCH CRACK ON LT AND RT CORNERS OF NR 3 ENGINE PYLON FORWARD END. THE CRACKED AREAS WERE CUT OUT. TWO EACH DOUBLERS, FILLERS, AND TRIPLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 2A.
- [SDR CALA9601866](https://openairdocs.org/sdr/CALA9601866.md): Skin · dented · Nov 5, 1996 · N37077 · Doug DC1030 · Leading Edge Devices
  > INSPECTION FOUND THE RT WING NR 4 SLAT DENTED AT XORS 480. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 12.
- [SDR CALA9601865](https://openairdocs.org/sdr/CALA9601865.md): Skin · gouged · Nov 5, 1996 · N37077 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN GOUGED IN TWO PLACES AT STRINGER 48R, B.S. 1581 AND 1585. THE GOUGES WERE REMOVED IAW SRM 53-00-01, FIGURE 1. TWO DOUBLERS, FILLER, AND A FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 6.
- [SDR CALA9601854](https://openairdocs.org/sdr/CALA9601854.md): Support · corroded · Oct 21, 1996 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1986, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1.
- [SDR CALA9601853](https://openairdocs.org/sdr/CALA9601853.md): Support · corroded · Oct 21, 1996 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND FLOOR PANEL ATTACH HOLES FROM BS 1986 TO 2007, RBL 27. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-60-01 FIGURE 1, 51-31-01 AND 51-20-01.
- [SDR CALA9601851](https://openairdocs.org/sdr/CALA9601851.md): Support · corroded · Oct 21, 1996 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1963, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1.
- [SDR CALA9601848](https://openairdocs.org/sdr/CALA9601848.md): Support · corroded · Oct 21, 1996 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1882, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1.
- [SDR CALA9601856](https://openairdocs.org/sdr/CALA9601856.md): Support · corroded · Oct 20, 1996 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 457, RBL 29. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-35-01 AND 53-11-01, FIGURE 1A.
- [SDR CALA9601874](https://openairdocs.org/sdr/CALA9601874.md): Skin · cracked · Oct 19, 1996 · N37077 · Doug DC1030 · Wing, Plate/Skin
  > THE LT WING FIXED LEADING EDGE SKIN HAD A 2.5 INCH CRACK FROM LOWER EDGE RUNNING FORWARD AT APPROXIMATELY XORS 810. THE CRACKED AREA WAS REMOVED. DOUBLER, FILLERS, AND FASTENERS WERE INSTALLED IAW SRM 57-00-01.
- [SDR CALA9601873](https://openairdocs.org/sdr/CALA9601873.md): Skin · dented · Oct 19, 1996 · N37077 · Doug DC1030 · Leading Edge Devices
  > INSPECTION FOUND LT WING NR 1 LEADING EDGE SLAT DENTED ON LEADING EDGE NOSE STARTING 30 INCHES OUTBOARD OF XFS 145. THE DENTED AREA WAS CUT OUT AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 43.
- [SDR CALA9601864](https://openairdocs.org/sdr/CALA9601864.md): Skin · cracked · Oct 19, 1996 · N37077 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1308.5, AT CABIN FLOOR. THE SKIN WAS REPAIRED BY FABRICATING AND INSTALLING A DOUBLER IAW SRM'S 51-21-01 AND 53-00-01, FIGURE 4.
- [SDR CALA9601863](https://openairdocs.org/sdr/CALA9601863.md): Skin · cracked · Oct 19, 1996 · N37077 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1255, AT CABIN FLOOR. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 4, SRM 51-21-01, AND 51-35-01.
- [SDR CALA9700163](https://openairdocs.org/sdr/CALA9700163.md): Clip · corroded · Oct 18, 1996 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CLIP FROM RT WHEEL WELL PRESSURE PANEL TO FRAME CORRODED ON UPPER FORWARD FACE OF FLANGE AT STA 1501, SIX INCHES BELOW CABIN FLOOR. A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-31-01, 53-00-01, FIGURE 1 AND 53-14-01, FIGURE 11
- [SDR CALA9601855](https://openairdocs.org/sdr/CALA9601855.md): Support · corroded · Oct 15, 1996 · N37077 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 472, LBL 54. TWO ANGLES, FILLER AND A FLOOR SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01, 51-35-01 AND 53-60-01 FIGURE 1.
- [SDR CALA9601871](https://openairdocs.org/sdr/CALA9601871.md): Hinged Panel · cracked · Oct 13, 1996 · N37077 · Doug DC1030 · Horizontal Stabilizer, Plate/Skin
  > INSPECTION FOUND A.50 INCH CRACK AROUND FASTENER OF LT HORIZONTAL STABILIZER LOWER TRAILING EDGE HINGED PANEL AT STA XE 158. THE AREA WAS REPAIRED IAW SRM 51-70-00.
- [SDR CALA9601872](https://openairdocs.org/sdr/CALA9601872.md): Blkhd Stiffener · corroded · Oct 12, 1996 · N37077 · Doug DC1030 · Fuselage Main, Bulkhead
  > INSPECTION FOUND CORROSION AROUND LOWER BOLT HOLE OF T-SHAPED VERTICAL STIFFENER AT CENTER WHEELWELL AFT FACE OF FORWARD BULKHEAD, XCW -15.0. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM'S 51-10-00, 51-21-01, AND 51-31-01.
- [SDR CALA9601867](https://openairdocs.org/sdr/CALA9601867.md): Frame · corroded · Oct 10, 1996 · N37077 · Doug DC1030 · Landing Gear Doors
  > THE RT CENTER MLG DOOR AFT FRAME WAS FOUND CORRODED. THE AFT FRAME WAS REMOVED AND REPLACED IAW SRM'S 51-35-01 AND 51-35-02.
- [SDR CALA9601850](https://openairdocs.org/sdr/CALA9601850.md): Skin · corroded · Oct 10, 1996 · N37077 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 1009 TO 1029, STRINGER 52. THE CORRODED AREA WAS CUT OUT. REPAIR DOUBLERS, FINGER DOUBLERS AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.
- [SDR CALA9601849](https://openairdocs.org/sdr/CALA9601849.md): Skin · corroded · Oct 10, 1996 · N37077 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CORROSION ON FUSELAGE SKIN AT BS 1049 TO 1069, STRINGER 52. THE CORRODED AREA WAS REMOVED. REPAIR DOUBLERS, FINGER DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.

## 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 = 'N37077' AND deregistration_id = 'N37077-2005-11-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N37077-2005-11-04/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, except the copies of manufacturers’ service documents, which belong to their rights holders.