# Service difficulty reports: N14062, cancelled Jun 11, 2003

A list on [N14062, cancelled Jun 11, 2003](https://openairdocs.org/deregistered/N14062-2003-06-11.md).

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

Page 1 of 2 · 53 reports

- [SDR CALA0100244](https://openairdocs.org/sdr/CALA0100244.md): Support · cracked · Mar 22, 2001 · N14062 · Doug DC1030 · Horizontal Stabilizer Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. THE PIVOT SUPPORT WAS REPLACED IAW EA 5310-03417 AND ECRA 5310-04118.
- [SDR CALA0100238](https://openairdocs.org/sdr/CALA0100238.md): Skin · corroded · Mar 19, 2001 · N14062 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE BELLY SKIN CORRODED AT STA 1364. THE CORRODED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-40-00, FIGURE 20.
- [SDR CALA0100237](https://openairdocs.org/sdr/CALA0100237.md): Bolt · sheared · Mar 19, 2001 · N14062 · Doug DC1030 · Fuselage, Wing Attach Fittings
  > INSPECTION FOUND BOLT SHEARED IN RT WING FORWARD SPAR TO FUSELAGE ATTACH ANGLE. THE BOLT WAS REPLACED IAW SRM 51-38-01.
- [SDR CALA0100236](https://openairdocs.org/sdr/CALA0100236.md): Beam · corroded · Mar 19, 2001 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND GALLEY G1A-G5 RT SUPPORT BEAM CORRODED. A NEW SUPPORT BEAM WAS INSTALLED IAW SRM 51-35-00.
- [SDR CALA0100235](https://openairdocs.org/sdr/CALA0100235.md): Frame · corroded · Mar 18, 2001 · N14062 · Doug DC1030 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME CORRODED AT STA 1139, LONGERON 51L. THE CORRODED SECTION OF FRAME WAS REMOVED AND A NEW SECTION WAS INSTALLED.
- [SDR CALA0100217](https://openairdocs.org/sdr/CALA0100217.md): Floorbeam · cracked · Mar 11, 2001 · N14062 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT STA 1298, RT, APPROXIMATELY TEN INCHES FROM EXTERNAL SKIN JOINT. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 7.
- [SDR CALA0100210](https://openairdocs.org/sdr/CALA0100210.md): Floor Support · corroded · Mar 6, 2001 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND GALLEY G6 O/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1902-2007, X = 48R. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-900-01, SRM 53-16-01, AND ECRA 5100-01844.
- [SDR CALA0100209](https://openairdocs.org/sdr/CALA0100209.md): Floor Support · corroded · Mar 6, 2001 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND GALLEY G7 I/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1887-2007, X = 24L. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-900-01, SRM 53-16-01, AND ECRA 5100-01844.
- [SDR CALA0100208](https://openairdocs.org/sdr/CALA0100208.md): Floor Support · corroded · Mar 6, 2001 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND GALLEY G7 O/B FLOOR SUPPORT BEAM CORRODED AT STA Y = 1902-2007, X = 48L. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW GMM 10-900-01, SRM 53-16-01, AND ECRA 5100-01844.
- [SDR CALA0000083](https://openairdocs.org/sdr/CALA0000083.md): Skin · corroded · Jan 26, 2000 · N14062 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LOWER FUSELAGE SKIN CORRODED WITH A PULLED RIVET AT STA 1761 BETWEEN STRINGER 45R AND 47R. REPAIRED IAW SRM 51-71-00.
- [SDR CALA0000079](https://openairdocs.org/sdr/CALA0000079.md): Door Sill · corroded · Jan 25, 2000 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD CARGO DOOR JAMB LOWER AFT CORNER DOOR SILL CORRODED. THE DOOR SILL WAS REPAIRED IAW SRM 53-70-00.
- [SDR CALA9900120](https://openairdocs.org/sdr/CALA9900120.md): Support · corroded · Feb 8, 1999 · N14062 · Doug DC1030 · Wing, Landing Gear Attach Fittings
  > INSPECTION FOUND THE RT MLG CYLINDER SUPPORT FRAME CORRODED IN ATTACHMENT BOLT HOLES. REPAIRED IAW ECRA 5743-01013.
- [SDR CALA9800218](https://openairdocs.org/sdr/CALA9800218.md): Actuator · leaking · Feb 12, 1998 · N14062 · Doug DC1030 · Landing Gear Retraction/Extension System
  > THE NLG WAS VERY SLOW TO EXTEND AND INDICATE DOWN WHEN GEAR WAS LOWERED DURING TEST FLIGHT WHILE AIRCRAFT WAS IN D-CHECK AT MAN. MAINTENANCE FOUND THE NLG DOWNLOCK ACTUATOR LEAKING INTERNALLY. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-35-00.
- [SDR CALA9800193](https://openairdocs.org/sdr/CALA9800193.md): Frame · corroded · Feb 5, 1998 · N14062 · Doug DC1030 · Fuselage Main, Frame
  > INSPECTION FOUND CORROSION IN FRAME AND INTERCOSTALS IN AVIONICS BAY AT STA 450 BETWEEN STRINGER 44 AND 64L. THE AREA WAS REPAIRED IAW SRM 53-30-00.
- [SDR CALA9800192](https://openairdocs.org/sdr/CALA9800192.md): Stiffener · corroded · Feb 5, 1998 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION AT LOWER LT CORNER OF DOOR IN AVIONICS COMPT AT REAR PRESSURE BULKHEAD STA 475, LT HORIZONTAL AND VERTICAL BEHIND GUSSET PLATE. THE AREA WAS REPAIRED IAW SRM 53-12-01.
- [SDR CALA9800184](https://openairdocs.org/sdr/CALA9800184.md): Longeron · cracked · Feb 4, 1998 · N14062 · Doug DC1030 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36R. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-10-00.
- [SDR CALA9800176](https://openairdocs.org/sdr/CALA9800176.md): Longeron · cracked · Feb 3, 1998 · N14062 · Doug DC1030 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36L. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-00-00.
- [SDR CALA9800131](https://openairdocs.org/sdr/CALA9800131.md): Bulkhead · fretted · Jan 28, 1998 · N14062 · Doug DC1030 · Fuselage Main, Bulkhead
  > INSPECTION FOUND, FRETTING ON CLG AFT PRESSURE BULKHEAD AT STA 1521. A REPAIR WAS ACCOMPLISHED IAW DOUGLAS DRAWING 90-53-1022.
- [SDR CALA9800107](https://openairdocs.org/sdr/CALA9800107.md): Angle · cracked · Jan 26, 1998 · N14062 · Doug DC1030 · Vertical Stabilizer
  > INSPECTION FOUND A 1.2 INCH CRACK IN RT LOWER VERTICAL STABILIZER DRAG ANGLE AT FORWARD CENTER SPAR POSITION. THE ANGLE WAS REPAIRED IAW SRM 53-20-00, FIGURE 3.
- [SDR CALA9701708](https://openairdocs.org/sdr/CALA9701708.md): Frame · cracked · Dec 1, 1997 · N14062 · Doug DC1030 · Wing Spar
  > THE A/C LOST NR 3 HYDRAULIC SYSTEM AND GEAR UNSAFE LIGHT ILLUMINATED WHILE INBOUND TO EWR. THE A/C WAS TAKEN OUT OF SERVICE FOR T/S. INITIAL FINDINGS REVEALED THE LT MLG RETRACT ACTUATOR SUPPORT FRAME ASSEMBLY WAS CRACKED. THE SUPPORT FRAME WAS REMOVED AND
- [SDR CALA9701278](https://openairdocs.org/sdr/CALA9701278.md): Blade · failed · Aug 28, 1997 · N14062 · Doug DC1030 · Turbine Section
  > NR 3 ENG MADE A LOUD BANG WITH EGT RISING TO 800 DEGREES AND N1 DROPPING TO 80 PERCENT WHILE EN ROUTE. THE ENGINE POWER WAS REDUCED TO IDLE AND OIL QUANTITY BEGAN TO DROP. THE ENG WAS SHUTDOWN AND THE ACFT WAS DIVERTED TO BSB WHERE IT LANDED WITHOUT INCIDENT
- [SDR CALA9700731](https://openairdocs.org/sdr/CALA9700731.md): Skin · damaged · May 7, 1997 · N14062 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND IMPACT DAMAGE TO SKIN AT STA 1901 TO 1921, STRINGER 7R AND SHEAR TIE HAD A 1.5 AND 1 INCH CRACK AT STA 1921 BETWEEN STRINGER 7R AND 8R. THE SKIN AND SHEAR TIE WERE REPAIRED IAW SRM 53-20-00, FIGURE 6.
- [SDR CALA9700730](https://openairdocs.org/sdr/CALA9700730.md): Skin · damaged · May 7, 1997 · N14062 · Doug DC1030 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND IMPACT DAMAGE TO FUSELAGE SKIN AT STA 1900 TO 1921 BETWEEN STRINGERS 7L AND 8L. THE SKIN WAS REPAIRED IAW SRM 53-20-00, FIGURE 6.
- [SDR CALA9700743](https://openairdocs.org/sdr/CALA9700743.md): Tee Section · corroded · May 6, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND T-SECTION CORRODED AT STA 1986, LONGERONS 50R AND 51R. THE T-SECTION WAS REPLACED IAW SRM 53-10-00.
- [SDR CALA9700742](https://openairdocs.org/sdr/CALA9700742.md): Intercostal · corroded · May 6, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED AT STA 1975, LONGERON 47R AND 48R. THE INTERCOSTAL WAS REPLACED IAW SRM 53-10-00.
- [SDR CALA9700752](https://openairdocs.org/sdr/CALA9700752.md): Beam · corroded · May 3, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUPPORT BEAM CORRODED AT STA 1834 TO 1879, LAV F, X= -33. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00.
- [SDR CALA9700751](https://openairdocs.org/sdr/CALA9700751.md): Beam · corroded · May 3, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LATERAL SUPPORT BEAMS CORRODED AT STA 1879, X= +38 TO +53 AND X= -38 TO -53. THE SUPPORT BEAMS WERE REPLACED IAW SRM 53-22-00.
- [SDR CALA9700750](https://openairdocs.org/sdr/CALA9700750.md): Beam · corroded · May 3, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUPPORT BEAM CORRODED AT STA 1834 TO 1879, LAV E. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00.
- [SDR CALA9700749](https://openairdocs.org/sdr/CALA9700749.md): Beam · corroded · May 3, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INBOARD SUPPORT BEAM AND LATERAL SUPPORT BEAM CORRODED AT STA 1841 TO 1887, LAV F. THE SUPPORT BEAMS WERE REMOVED AND REPLACED IAW SRM 53-22-00.
- [SDR CALA9700748](https://openairdocs.org/sdr/CALA9700748.md): Beam · corroded · May 3, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUPPORT BEAMS CORRODED AT STA 1879, X = 4 TO 33 AND X = -4 TO -33. THE SUPPORT BEAMS WERE REPLACED IAW SRM 53-22-00.
- [SDR CALA9700747](https://openairdocs.org/sdr/CALA9700747.md): Beam · corroded · May 3, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOORBOARD SUPPORT BEAM CORRODED AT STA 1899, X = 0 TO +20. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00.
- [SDR CALA9700745](https://openairdocs.org/sdr/CALA9700745.md): Beam · corroded · May 3, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT GALLEY SUPPORT BEAM CORRODED AT STA 1879 TO 2007, X = 24. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-00.
- [SDR CALA9700746](https://openairdocs.org/sdr/CALA9700746.md): Floorbeam · corroded · May 1, 1997 · N14062 · Doug DC1030 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT L-1 DOOR, STA 395 TO 433. THE FLOORBEAM WAS REPLACED IAW SRM 53-27-00.
- [SDR CALA9700744](https://openairdocs.org/sdr/CALA9700744.md): Beam · corroded · May 1, 1997 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LONGITUDINAL SUPPORT BEAM CORRODED AT LAV G, STA 1913 TO 2007. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22-0.
- [SDR CALA9700297](https://openairdocs.org/sdr/CALA9700297.md): Prox Switch · inoperative · Mar 2, 1997 · N14062 · Doug DC1030 · Landing Gear Position and Warning
  > WHEN GEAR WAS EXTENDED FOR LANDING, THERE WERE NO GREEN LIGHTS INDICATED ON FORWARD PANEL OR SECOND OFFICER'S PANEL. THE GEAR WAS CYCLED AND INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY CONTRO
- [SDR CALA9700287](https://openairdocs.org/sdr/CALA9700287.md): Hyd Line · chafed · Feb 27, 1997 · N14062 · Doug DC1030 · Hydraulic System, Main
  > THE NR 1 HYDRAULIC SYSTEM FLUID QUANTITY AND PRESSURE DROPPED TO ZERO WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE TO LT ENGINE DRIVEN HYDRAULIC PUMP CHAFED THROUGH. THE HYDRAULIC LI
- [SDR CALA9601793](https://openairdocs.org/sdr/CALA9601793.md): Hyd Line · ruptured · Dec 15, 1996 · N14062 · Doug DC1030 · Hydraulic System, Main
  > THE AIRCRAFT LOST NR 1 HYDRAULIC SYSTEM FLUID AFTER FLAP RETRACTION DEPARTING MAD. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO MAD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE LT ENGINE DRIVEN PUMP PRESSURE LINE TO MANIFOLD RUPTUR
- [SDR CALA9601489](https://openairdocs.org/sdr/CALA9601489.md): Wat Sep Bags · dirty · Oct 19, 1996 · N14062 · Doug DC1030 · Humidity Control System
  > THE FLIGHT ATTENDANTS REPORTED AN ODOR OF ELECTRICAL SMOKE WHILE ON APPROACH. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT FOR AN ELECTRICAL FAILURE AND FOUND NO FAULTS. ALL THREE WATER SEPARATOR BAGS WERE FOUND EXTREMELY
- [SDR CAL960407](https://openairdocs.org/sdr/CAL960407.md): Skin · damaged · Mar 8, 1996 · N14062 · Doug DC1030 · Fuselage Main, Plate/Skin
  > KUL - INSPECTION FOUND IMPACT DAMAGE AT LOWER AFT SECTION OF FORWARD CARGO DOOR CUT-OUT. THE AREA WAS REPAIRED IAW ECRA 5330-02370. (X)
- [SDR CAL960405](https://openairdocs.org/sdr/CAL960405.md): Angle · cracked · Mar 4, 1996 · N14062 · Doug DC1030 · Fuselage Miscellaneous Structure
  > KUL - INSPECTION FOUND TWO 1 INCH CRACKS IN ANGLE AT STA XCW 14 LT AND XCW 14 RT, BS 2123. A REPAIR WAS CARRIED OUT PER SRM 53-00-01, PAGE 7. (X)
- [SDR CAL960404](https://openairdocs.org/sdr/CAL960404.md): Skin · cracked · Mar 4, 1996 · N14062 · Doug DC1030 · Horizontal Stabilizer, Plate/Skin
  > KUL - INSPECTION FOUND A DENT AND 1.25 INCH CRACK IN THE TOP SKIN OF THE LT HORIZONTAL STABILIZER INBOARD PANEL. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-71-00 AND A FIBERGLASS REPAIR WAS INSTALLED IAW SRM 57-71-00, PAGE 65. (X)
- [SDR CAL960406](https://openairdocs.org/sdr/CAL960406.md): Frame · damaged · Feb 29, 1996 · N14062 · Doug DC1030 · Fuselage Main, Frame
  > KUL - INSPECTION FOUND A.50 INCH DIAMETER HOLE IN FRAME, STA 1841, ABOVE CENTER CARGO FLOOR AREA ON LT SIDE. THE FRAME WAS REPAIRED IAW ECRA 5310-03243. (X)
- [SDR CAL960408](https://openairdocs.org/sdr/CAL960408.md): Spar Cap · cracked · Feb 25, 1996 · N14062 · Doug DC1030 · Wing Spar
  > KUL - INSPECTION FOUND A 6 INCH CRACK JUST ABOVE RADIUS ON FORWARD SIDE OF RT WING AFT LOWER SPAR CAP AT STA 1043. THE SPAR CAP WAS REPAIRED IAW ECRA 5710-01720. (X)
- [SDR CAL960158](https://openairdocs.org/sdr/CAL960158.md): Valve · leaking · Feb 18, 1996 · N14062 · Doug DC1030 · Stabilizer Control System
  > FLT NR 10 - EWR - THE NR 1 HYDRAULIC SYSTEM BEGAN TO LOSE FLUID WHILE EN ROUTE FROM IAH TO ORY. THE QUANTITY DROPPED STEADILY. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LOWER PRIMARY TRIM CONTROL VALVE LEAKING.
- [SDR CAL951068](https://openairdocs.org/sdr/CAL951068.md): Hyd Pump · case cracked · Nov 27, 1995 · N14062 · Doug DC1030 · Hydraulic Pump (Electric/Engine), Main
  > FLT NR 0005 - IAH - THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED AND THE NR 3 HYDRAULIC QUANTITY AND PRESSURE DECREASED TO ZERO IN FLIGHT. THE EMERGENCY CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3
- [SDR CAL950941](https://openairdocs.org/sdr/CAL950941.md): Eel Pin · loose · Oct 19, 1995 · N14062 · Doug DC1030 · Emergency Lighting
  > LAX - FLT NR 0063 - ROWS 19-33, INCLUDING OVERWING EMERGENCY LIGHTS COME ON WHEN POWER IS SHUTOFF. FOUND PIN 'V' DISARMED, PUSHED PIN BACK IN AT CONNECTOR. (M)
- [SDR CAL950919](https://openairdocs.org/sdr/CAL950919.md): Trailing Edge · missing · Oct 13, 1995 · N14062 · Doug DC1030 · Elevator Structure
  > FLT NR 0011 - ORY - A WALK AROUND INSPECTION, FOUND RIGHT INBOARD ELEVATOR TRAILING EDGE STRIP MISSING (APPROXIMATELY 24 INCHES). A PERMANENT REPAIR WAS PERFORMED PER SRM 55-30-00, FIGURE 2. (M)
- [SDR CAL950600](https://openairdocs.org/sdr/CAL950600.md): Eel Battery · discharged · Jul 15, 1995 · N14062 · Doug DC1030 · Emergency Lighting
  > FLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. THE FORWARD CENTER BATTERY CHARGER WAS ALSO FOUND INOPERATIVE. BOTH OF THE BATTERY PACKS AND THE BA
- [SDR CAL950599](https://openairdocs.org/sdr/CAL950599.md): Eel Battery · discharged · Jul 15, 1995 · N14062 · Doug DC1030 · Emergency Lighting
  > FLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. THE FORWARD CENTER BATTERY CHARGER WAS ALSO FOUND INOPERATIVE. BOTH OF THE BATTERY PACKS AND THE BA
- [SDR CAL950598](https://openairdocs.org/sdr/CAL950598.md): Eel Batt Charger · inoperative · Jul 15, 1995 · N14062 · Doug DC1030 · Emergency Lighting
  > FLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. THE FORWARD CENTER BATTERY CHARGER WAS ALSO FOUND INOPERATIVE. BOTH OF THE BATTERY PACKS AND THE BA

Next page: https://openairdocs.org/deregistered/N14062-2003-06-11/reports.md?page=2

## 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 = 'N14062' AND deregistration_id = 'N14062-2003-06-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14062-2003-06-11/reports

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