# Service difficulty reports: N917HA, cancelled Jul 3, 2013

A list on [N917HA, cancelled Jul 3, 2013](https://openairdocs.org/deregistered/N917HA-2013-07-03.md).

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

- [SDR HNAA0200088](https://openairdocs.org/sdr/HNAA0200088.md): Packing · leaking · Dec 9, 2002 · N917HA · Dhav DHC8102 · Aircraft Fuel System
  > 9 DEC. 2002FUEL DRIPPING OUT OF GEAR WELL ABOVE CONTACTOR BOX #2 NACELLE. WIGGINS FITTING FWD OF NACELLE FIRE SEAL WAS FOUND LEAKING. REPLACED O-RINGS PN AS3209-218 LEAK CHECK GOOD.10 DEC. 2002FUEL COMING OUT OF DRAIN ON INBD SIDE OF #2 NACELLE. FOUND LEAK
- [SDR HNAA0200069](https://openairdocs.org/sdr/HNAA0200069.md): Battery · discharged · Oct 4, 2002 · N917HA · Dhav DHC8102 · Emergency Lighting
  > CENTER ISLE EXIT SIGN WHITE DOWN LIGHT AND RIGHT HAND AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY.
- [SDR HNAA020054](https://openairdocs.org/sdr/HNAA020054.md): Battery · discharged · Aug 13, 2002 · N917HA · Dhav DHC8102 · Emergency Lighting
  > TWO OF THE FOUR RED EMERGENCY FLOOR LIGHT FORWARD END ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY 3352 PS1.
- [SDR HNAA0200042](https://openairdocs.org/sdr/HNAA0200042.md): Hydraulic System · malfunctioned · May 30, 2002 · N917HA · Dhav DHC8102 · Hydraulic System, Main
  > DURING SINGLE ENGINE TAXI, CREW REPORTED LOST NR 1 STANDBY HYDRAULIC SYSTEM PRESSURE AND THE USE OF THE NORMAL BRAKE SYSTEM. CREW USED THE PARKING BRAKE TO STOP THE A/C. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY.
- [SDR HNAA0100075](https://openairdocs.org/sdr/HNAA0100075.md): Pump · malfunctioned · Nov 19, 2001 · N917HA · Dhav DHC8102 · Hydraulic Pump, Auxiliary
  > DURING SINGLE ENGINE TAXI, NR 2 AC GENERATOR ON LINE, NR 1 STANDBY HYDRAULIC PUMP FAILED CAUSING LOSS OF NR 1 HYDRAULIC PRESSURE. RECYCLED NR 2 AC GENERATOR, NR 1 STANDBY HYDRAULIC PUMP RETURNED TO NORMAL. INSPECTED BRAKES AND HYDRAULIC SYSTEM, NO LEAKS NOTE
- [SDR HNAA0100027](https://openairdocs.org/sdr/HNAA0100027.md): Computer · failed · Apr 21, 2001 · N917HA · Dhav DHC8102 · Integrated Flight System
  > IN FLIGHT, NR 2 AHRS FLAGGED AND GOR ELECTRICAL SMELL IN COCKPIT AND CABIN. REPLACED 2 AHRS UNIT.
- [SDR HNAA9900109](https://openairdocs.org/sdr/HNAA9900109.md): Light · inop · Aug 6, 1999 · N917HA · Dhav DHC8102 · Emergency Lighting
  > FLOOR EMERGENCY LIGHT 5TH LIGHT AFT IS INOP. REMOVED AND REPLACEDD LIGHT ASSY.
- [SDR HNAA9891772](https://openairdocs.org/sdr/HNAA9891772.md): Power Supply · inoperative · Nov 4, 1998 · N917HA · Dhav DHC8102 · Emergency Lighting
  > SBY - FLT 3200 - PASSENGER EXIT SIGN AT BOARDING DOOR INOP. REMOVED AND REPLACED POWER SUPPLY 3351 PS1. OPS CHECK GOOD. (M)
- [SDR HNAA9891746](https://openairdocs.org/sdr/HNAA9891746.md): Valve · leaking · Sep 8, 1998 · N917HA · Dhav DHC8102 · Brake Anti-Skid Section
  > CRW/CLT - FLT 3342 - DURING DESCENT, NR 1 HYDRAULIC ISOLATE AND ROLL SPOILER INBD HYDRAULIC CAUTION LIGHTS ILLUMINATED WITH REDUCED NR 1 HYDRAULIC SYSTEM QUANTITY. PERFORMED ZERO FLAP LANDING WITH NO NORMAL WHEEL BRAKES. REMOVED AND REPLACED NR 1 ANTI-SKID C
- [SDR HNAA9891731](https://openairdocs.org/sdr/HNAA9891731.md): Door · out of adjust · Jul 5, 1998 · N917HA · Dhav DHC8102 · Landing Gear Door Retract Section
  > CLT/EWN - FLT 3284 - AFTER GEAR UP SELECTION, NOSE GEAR DOORS OPENED. CYCLED GEAR, NOSE GEAR DOORS OPENED AGAIN. AIR TURNBACK TO CLT. ADJUSTED NOSE GEAR DOORS, ACTUATOR END ONE TURN OUT. CYCLED GEAR, OPS CHECK GOOD. (X)
- [SDR HNAA9891729](https://openairdocs.org/sdr/HNAA9891729.md): Valve · failed · Jul 5, 1998 · N917HA · Dhav DHC8102 · Landing Gear Door Retract Section
  > CLT/HHH - FLT 3172 - AFTER GEAR RETRACTION, NOSE GEAR DOOR AMBER LIGHT CAME ON. CREW CYCLED GEAR AND LIGHT ON AGAIN. AIR TURNBACK TO CLT. REMOVED AND REPLACED SOLENOID SEQUENCE VALVE, OPS CHECKED GOOD. (X)
- [SDR HNAA9791798](https://openairdocs.org/sdr/HNAA9791798.md): Bushings · failed · Dec 1, 1997 · N917HA · Dhav DHC8102 · Aileron Control System
  > FLT EN69 - BWI-ORF - EXPERIENCED A ROLL CONTROL DISCONNECT ON LANDING, AFTER TOUCHDOWN AT ORF. REMOVED AND REPLACED THE ROLL CONTROL DISCONNECT CLUTCH BUSHINGS PER FCD8-27-291. ALSO, REMOVED AND REPLACED THE CLUTCH SPRING. (M)
- [SDR 98ZZZM178](https://openairdocs.org/sdr/98ZZZM178.md): Clutch Spring · failed · Dec 1, 1997 · N917HA · Dhav DHC8102 · Aileron Control System
  > FLT EN69 - BWI-ORF - EXPERIENCED A ROLL CONTROL DISCONNECT ON LANDING, AFTER TOUCHDOWN AT ORF. REMOVED AND REPLACED THE ROLL CONTROL DISCONNECT CLUTCH BUSHINGS PER FCD8-27-291. ALSO, REMOVED AND REPLACED THE CLUTCH SPRING. (M)
- [SDR HNAA9791702](https://openairdocs.org/sdr/HNAA9791702.md): Bushing · missing · Jan 6, 1997 · N917HA · Dhav DHC8102 · Landing Gear Door Retract Section
  > FLT 3393 - YYZ-BWI - THE LEFT GEAR DOOR WAS OPEN IN FLIGHT WITH NO ADVISORY LIGHT ON, DID NOT CLOSE UPON GEAR UP SELECTION. THE AIRCRAFT CONTINUED TO BWI AND LANDED WITHOUT INCIDENT. INSTALLED HARDWARE ON FORWARD DOOR AFT CONNECTING ROD ASSEMBLY. (M)
- [SDR 97ZZZM212](https://openairdocs.org/sdr/97ZZZM212.md): Bushing · missing · Jan 6, 1997 · N917HA · Dhav DHC8102 · Landing Gear Door Retract Section
  > FLT 3393 - YYZ-BWI - THE LEFT GEAR DOOR WAS OPEN IN FLIGHT WITH NO ADVISORY LIGHT ON, DID NOT CLOSE UPON GEAR UP SELECTION. THE AIRCRAFT CONTINUED TO BWI AND LANDED WITHOUT INCIDENT. INSTALLED HARDWARE ON FORWARD DOOR AFT CONNECTING ROD ASSEMBLY. REF HNAA97
- [SDR 97ZZZM211](https://openairdocs.org/sdr/97ZZZM211.md): Bolt · missing · Jan 6, 1997 · N917HA · Dhav DHC8102 · Landing Gear Door Retract Section
  > FLT 3393 - YYZ-BWI - THE LEFT GEAR DOOR WAS OPEN IN FLIGHT WITH NO ADVISORY LIGHT ON, DID NOT CLOSE UPON GEAR UP SELECTION. THE AIRCRAFT CONTINUED TO BWI AND LANDED WITHOUT INCIDENT. INSTALLED HARDWARE ON FORWARD DOOR AFT CONNECTING ROD ASSEMBLY. REF HNAA97
- [SDR HNAA9691729](https://openairdocs.org/sdr/HNAA9691729.md): Engine · failed · May 15, 1996 · N917HA · Dhav DHC8102 · Engine (Turbine/Turboprop)
  > FLT NR 3461 - MIA-MCO - ON CLIMB-OUT, THE NR 1 ENGINE LOW OIL PRESSURE WARNING LIGHT CAME ON, PRESSURE DECREASED, AND THE CREW SHUT THE ENGINE DOWN. THE AIRCRAFT TURNED BACK TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 ENGINE. (M)
- [SDR HNAA9591715](https://openairdocs.org/sdr/HNAA9591715.md): Spring · broken · Nov 20, 1995 · N917HA · Dhav DHC8102 · Landing Gear Retraction/Extension System
  > FLT NR 3162 - DCA-ISP - AFTER GEAR DOWN SELECTION, DURING APPROACH, THE LEFT GEAR UNSAFE LIGHT ILLUMINATED AND STAYED ON. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED IN ISP WITHOUT INCIDENT. REMOVED AND REPLACED THE STAY STRUT OUTBOARD SPRING. (M)

## 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 = 'N917HA' AND deregistration_id = 'N917HA-2013-07-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N917HA-2013-07-03/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.
