# Service difficulty reports: N814PH, cancelled May 23, 2001

A list on [N814PH, cancelled May 23, 2001](https://openairdocs.org/deregistered/N814PH-2001-05-23.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 · 55 reports

- [SDR QXEA0100106](https://openairdocs.org/sdr/QXEA0100106.md): Seat Track · corroded · Feb 6, 2001 · N814PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX- FRETTING CORROSION ON INBOARD FLANGE OF LEFT INBOARD SEAT TRACK AT STATION X252.700 IN LINE WITH AFT EDGE OF MAIN CABIN DOOR. REPAIRED IAW PSM 1-GEN-5 CHAPTER 4 PAGE 4-16.
- [SDR QXEA0100109](https://openairdocs.org/sdr/QXEA0100109.md): Skin · dented · Feb 5, 2001 · N814PH · Dhav DHC8102 · Fuselage Main, Plate/Skin
  > PDX- DENT IN AFT FUSELAGE SKIN 6 INCHES LONG,.020 INCH DEEP AFT OF FRAME X600.0 BETWEEN STRINGERS 22R AND 23R. REPAIRED IAW DHC-8 RD 8-53-436.
- [SDR QXEA0100108](https://openairdocs.org/sdr/QXEA0100108.md): Seat Track · corroded · Feb 5, 2001 · N814PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX- FRETTING CORROSION ON INBOARD FLANGE OF LEFT HAND INBOARD SEAT TRACK AT STATION X252.700 IN LINE WITH AFT EDGE OF MAIN CABIN DOOR. REPAIRED IAW DHC-8 SRM 51-40-00 AND RD 8-53-1102.
- [SDR QXEA0100100](https://openairdocs.org/sdr/QXEA0100100.md): Seat Track · misdrilled · Feb 4, 2001 · N814PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX- LEFT HAND INBOARD NR 4 SEAT TRACK SUPPORT ANGLE AT STATION 355.950 AND 354.250 HAS A 10:32 FASTENER HOLE THAT HAS BEEN MISDRILLED. REPAIRED IAW HORIZON AIR EA 9-53-596.
- [SDR QXEA0100113](https://openairdocs.org/sdr/QXEA0100113.md): Elevator · incorrect · Feb 2, 2001 · N814PH · Dhav DHC8102 · Elevator Structure
  > PDX- RIGHT HAND ELEVATOR INBOARD TRAILING EDGE DOES NOT FARE WITH ELEVATOR SKIN. REPAIRED IAW DHC-8 SRM 51-40-00.
- [SDR QXEA0100114](https://openairdocs.org/sdr/QXEA0100114.md): Attach Fitting · corroded · Feb 1, 2001 · N814PH · Dhav DHC8102 · Landing Gear Actuator
  > PDX- LEFT HAND MAIN LANDING GEAR RETRACTION ACTUATOR ATTACH FITTING ATTACH POINT ON H-MEMBER HAS FRETTING CORROSION AT LEFT HAND SIDE OF UPPER MOUNT HOLES. REPAIRED IAW HORIZON AIR EA 9-54-267.
- [SDR QXEA0100116](https://openairdocs.org/sdr/QXEA0100116.md): Stiffener · cracked · Jan 31, 2001 · N814PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > PDX- LOWER FINGERNAIL DECK OUTBOARD FORE/AFT STIFFENER IS CRACKED AT GEARWELL WALL VERTICAL STIFFENER OF LEFT HAND NACELLE. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-20-16.
- [SDR QXEA0100115](https://openairdocs.org/sdr/QXEA0100115.md): Stiffener · chafed · Jan 31, 2001 · N814PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > PDX- FINGERNAIL DECK STIFFENER CHAFED THIN AT XN232.0 TOP SIDE. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-20-16.
- [SDR QXEA0100110](https://openairdocs.org/sdr/QXEA0100110.md): Splice · cracked · Jan 31, 2001 · N814PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX- FRAME JOINT SPLICE ANGLE AT STATION X136.80 AT STRINGER 15A RIGHT HAND IS CRACKED. REPAIRED IAW DHC-8 RD 8-53-576.
- [SDR QXEA0100102](https://openairdocs.org/sdr/QXEA0100102.md): Flap Track · damaged · Jan 31, 2001 · N814PH · Dhav DHC8102 · Trailing Edge Flaps
  > PDX- RIGHT HAND INBOARD FLAP, NR 2 OUTBOARD FLAP TRACK UPPER TRACK HAS A DIVET 10 INCHES AFT OF FORWARD END. REPAIRED IAW DHC-8 RD 8-57-986.
- [SDR QXEA0100101](https://openairdocs.org/sdr/QXEA0100101.md): Flap Track · damaged · Jan 31, 2001 · N814PH · Dhav DHC8102 · Trailing Edge Flaps
  > PDX- RIGHT HAND INBOARD FLAP, NR 1 INBOARD UPPER TRACK HAS DIVETS IN TOP AND BOTTOM 10 INCHES AFT OF FORWARD END. REPAIRED IAW DHC-8 RD 8-57-985.
- [SDR QXEA0100112](https://openairdocs.org/sdr/QXEA0100112.md): Skin · cracked · Jan 30, 2001 · N814PH · Dhav DHC8102 · Rudder, Plate/Skin
  > PDX- TOP RIGHT HAND SIDE OF TRAILING RUDDER SKIN HAS A CRACK PROGRESSING OUT FROM RIVET HOLE AT PREVIOUS REPAIR SKIN PATCH. REPAIRED IAW DHC-8 SRM 55-40-28 AND 51-40-00.
- [SDR QXEA0100111](https://openairdocs.org/sdr/QXEA0100111.md): Splice · cracked · Jan 30, 2001 · N814PH · Dhav DHC8102 · Fuselage Miscellaneous Structure
  > PDX- CRACK FOUND IN LEFT HAND JOINT SPLICE FRAME AT STATION X136.80 AND STRINGER 15A. REPAIRED IAW DHC-8 RD 8-53-576.
- [SDR QXEA0100117](https://openairdocs.org/sdr/QXEA0100117.md): Door Frame · corroded · Jan 29, 2001 · N814PH · Dhav DHC8102 · Fuselage Main, Structure
  > PDX- MAIN CABIN DOOR SURROUND FORWARD FRAME CORRODED AROUND NUTPLATE THAT IS BETWEEN 2ND AND 3RD STOPS FROM BOTTOM. REPAIRED IAW DHC-8 SRM 51-20-11 AND 53-00-16.
- [SDR QXEA0100107](https://openairdocs.org/sdr/QXEA0100107.md): Seat Track · corroded · Jan 28, 2001 · N814PH · Dhav DHC8102 · Fuselage, Seat/Cargo Attach Fittings
  > PDX- CORROSION ON LEFT INBOARD SEAT TRACK FLANGE LOCATED IN CARGO AREA AT STATION 580.50. REPAIRED IAW DHC-8 SRM 51-20-16.
- [SDR QXEA0003187](https://openairdocs.org/sdr/QXEA0003187.md): Ballast · malfunctioned · Dec 10, 2000 · N814PH · Dhav DHC8102 · Passenger Compartment Lighting
  > PDX- BURNED ELECTRICAL INSULATION SMELL IN CABIN. REMOVED AND REPLACED BALLAST. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0002065](https://openairdocs.org/sdr/QXEA0002065.md): Actuator · malfunctioned · Aug 2, 2000 · N814PH · Dhav DHC8102 · Landing Gear Door Actuator
  > YVR- AFTER DEPARTURE LEFT HAND GEAR DOOR RETRACTED, THEN FELL OPEN. CYCLED GEAR, DOOR REMAINED CLOSED. REMOVED AND REPLACED LEFT HAND AFT AND CENTER GEAR DOOR ACTUATORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0001824](https://openairdocs.org/sdr/QXEA0001824.md): Sequence Valve · malfunctioned · Jul 7, 2000 · N814PH · Dhav DHC8102 · Landing Gear Retraction/Extension System
  > PSC- AFTER SELECTING GEAR UP, MAIN GEAR DOOR AMBER LIGHT ON AND VISUALLY CONFIRMED LIGHT GEAR DOOR FAILED TO CLOSE. PERFORMED ALTERNATE GEAR EXTENSION METHOD. LANDED OK. REMOVED AND REPLACED MAIN GEAR SOLENOID SEQUENCE VALVE. OPERATIONAL CHECKS GOOD. AIRC
- [SDR QXEA0001823](https://openairdocs.org/sdr/QXEA0001823.md): Pseu · malfunctioned · Jul 6, 2000 · N814PH · Dhav DHC8102 · Landing Gear Retraction/Extension System
  > SEA- AFTER SELECTING GEAR UP, MAIN GEAR DOOR AMBER LIGHT ON AND VISUALLY CONFIRMED LIGHT GEAR DOOR FAILED TO CLOSE. PERFORMED ALTERNATE GEAR EXTENSION METHOD. LANDED OK. REMOVED AND REPLACED PSEU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0001343](https://openairdocs.org/sdr/QXEA0001343.md): Stop · malfunctioned · May 20, 2000 · N814PH · Dhav DHC8102 · Passenger/Crew Doors
  > SEA- MAIN CABIN DOOR IS HARD TO OPEN FROM THE OUTSIDE. REPLACED RUBBER STOP FOR EXTERIOR HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA0001127](https://openairdocs.org/sdr/QXEA0001127.md): Fairing · damaged · Apr 17, 2000 · N814PH · Dhav DHC8102 · Landing Gear/Wheel Fairing
  > PDX- ON TAKEOFF AT GEAR RETRACTION, NOTED RUMBLING NOISE. LEFT DOOR, NOSE DOOR, RIGHT UNSAFE (RED) LIGHTS APPEARED. COMPLIED WITH LANDING GEAR NOT RETRACTING CHCEKLIST. GEAR CAME DOWN WELL ON EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLAC
- [SDR QXEA0000751](https://openairdocs.org/sdr/QXEA0000751.md): Inverter · malfunctioned · Mar 14, 2000 · N814PH · Dhav DHC8102 · AC Inverter
  > BOI- STRONG FISH SMELL COMING FROM BEHIND CAPTIN''S SEAT AREA. REMOVED AND REPLACED PRIMARY INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9902592](https://openairdocs.org/sdr/QXEA9902592.md): Light · malfunctioned · Dec 9, 1999 · N814PH · Dhav DHC8102 · Emergency Lighting
  > PDX- COCKPIT EMERGENCY LIGHT ILLUMINATED WHEN EMERGENCY LIGHTS WERE ARMED. REPLACED COCKPIT LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD.
- [SDR QXEA9902444](https://openairdocs.org/sdr/QXEA9902444.md): Switch · failed · Nov 25, 1999 · N814PH · Dhav DHC8102 · Emergency Lighting
  > SEA- EMERGENCY LIGHTS CIRCUIT BREAKER POPS EVEN WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED FLIGHT ATTENDENTS EMERGENCY LIGHTING SWITCH AND EMERGENCY LIGHTING CONTROL BOX, OPERATIONAL CHECKS GOOD.
- [SDR QXEA9901524](https://openairdocs.org/sdr/QXEA9901524.md): Bolt · loose · Jul 29, 1999 · N814PH · Dhav DHC8102 · Passenger/Crew Doors
  > SEA - MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE RESECURED HANDRAIL SUPPORT PIVOT BOLT. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED.
- [SDR QXEA9900510](https://openairdocs.org/sdr/QXEA9900510.md): Engine · flamed out · Mar 22, 1999 · N814PH · Dhav DHC8102 · Engine (Turbine/Turboprop)
  > SEA- ON DESCENT INTO SEA, THE AIRCRAFT EXPERIENCED MODERATE TO SEVERE TURBULENCE WHILE IN INSTRUMENT METROLOGICAL CONDITIONS (IMC). DURING THIS PERIOD, BOTH ENGINES APPARENTLY FLAMED-OUT, AND THEN BOTH IMMEDIATELY RELIT. THERE WAS A LOUD SURGE WITH THE POWER
- [SDR QXEA9801057](https://openairdocs.org/sdr/QXEA9801057.md): Valve · malfunction · Aug 3, 1998 · N814PH · Dhav DHC8102 · Landing Gear Door Retract Section
  > SEA - LEFT GEAR DOOR LIGHT REMAINED ON WHEN THE LANDING GEAR WAS RETRACTED. DOOR VISUALLY INSPECTED AND VERFIED TO BE OPEN. WHEN GEAR CYCLED THE LIGHT WENT OUT. FERRIED AIRCRAFT FROM SEA TO PDX FOR REPAIRS. IN PDX, RIGGED THE ALTERNATE EXTENSION SYSTEM AND
- [SDR QXEA9801052](https://openairdocs.org/sdr/QXEA9801052.md): Valve · malfunction · Aug 2, 1998 · N814PH · Dhav DHC8102 · Landing Gear Door Retract Section
  > LEFT MAIN GEAR DOOR REMAINED OPEN AFTER LANDING GEAR RETRACTION. AFTER CYCLING GEAR, THE DOOR CLOSED NORMALLY. FERRIED AIRCRAFT FROM SEA TO PDX FOR REPAIRS. IN PDX, REPLACED THE NR 1 MAIN GEAR DOOR PROXIMITY SENSOR AND THE SEQUENCE VALVE. OPERATIONAL CHECK
- [SDR QXEA9801044](https://openairdocs.org/sdr/QXEA9801044.md): Actuator · malfunction · Jul 23, 1998 · N814PH · Dhav DHC8102 · Landing Gear Retraction/Extension System
  > DURING LANDING GEAR RETRACTION, THE LEFT GEAR DOOR LIGHT STAYED ON AND THE GEAR DOOR WAS NOTICED TO BE OPEN. CYCLED THE LANDING GEAR AND THE DOOR OPERATED PROPERLY. REPLACED THE FORWARD GEAR DOOR ACTUATOR AND PERFORMED GEAR SWINGS, OPERATIONAL CHECKS GOOD.
- [SDR QXEA9801035](https://openairdocs.org/sdr/QXEA9801035.md): Actuator · out of adjust · Jul 19, 1998 · N814PH · Dhav DHC8102 · Landing Gear Door Actuator
  > AFTER GEAR SELECTED UP THE AMBER DOOR LIGHT REMAINED ON. VISUALLY VERIFIED THAT THE GEAR DOOR WAS OPEN. CYCLED LANDING GEAR AND ALL LIGHTS WENT OUT. ADJUSTED AFT GEAR DOOR ACTUATOR ROD END IAW MM MANUAL 32-10-36. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED
- [SDR QXEA9800949](https://openairdocs.org/sdr/QXEA9800949.md): Stop · missing · Jul 15, 1998 · N814PH · Dhav DHC8102 · Passenger/Crew Doors
  > ALW - MAIN CABIN DOOR MISSING BLACK RUBBER STOPPER FOR THE EXTERNAL HANDLE. AIRCRAFT FERRIED FROM ALW TO SEA FOR REPAIRS. IN SEA, REPLACED THE BLACK RUBBER STOPPER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9800636](https://openairdocs.org/sdr/QXEA9800636.md): Retract Mech · out of adjust · May 5, 1998 · N814PH · Dhav DHC8102 · Landing Gear Door Retract Section
  > SEA - AFTER GEAR RETRACTION, THE LEFT GEAR DOOR REMAINED IN THE OPEN POSITION. CYCLED THE LANDING GEAR AND THE DOOR CLOSED NORMALLY. INSPECTED THE AIRCRAFT AND FOUND IT SAFE FOR A FERRY FLIGHT SEA-PDX. IN PDX ADJUSTED THE JAM NUT ON THE LEFT FORWARD DOOR AC
- [SDR QXEA9800534](https://openairdocs.org/sdr/QXEA9800534.md): Retract Mech · malfunctioned · Apr 17, 1998 · N814PH · Dhav DHC8102 · Landing Gear Door Retract Section
  > LEFT MAIN FORWARD GEAR DOOR REMAINS OPEN AFTER TAKEOFF. GEAR WAS CYCLED, AND THE DOOR CLOSED. INSPECTED FORWARD GEAR DOOR ACTUATION MECHANISM, NO DEFECTS NOTED. CLEANED BOTH RESTRICTORS AT THE FORWARD GEAR DOOR ACTUATOR, OPERATIONAL CHECKS GOOD. NO PARTS R
- [SDR QXEA9800453](https://openairdocs.org/sdr/QXEA9800453.md): Pseu · malfunction · Mar 31, 1998 · N814PH · Dhav DHC8102 · Landing Gear Position and Warning
  > AFTER TAKEOFF, WHEN THE LANDING GEAR WAS SELECTED UP, ALL GEAR INDICATION LIGHTS WENT OUT NORMALLY. AFTER ABOUT 5 SECONDS THE LEFT GEAR DOOR LIGHT ILLUMINATED. VISUAL INSPECTION CONFIRMED THE GEAR DOOR TO BE OPEN. CYCLED LANDING GEAR AND THE GEAR DOOR CLOSE
- [SDR QXEA9800016](https://openairdocs.org/sdr/QXEA9800016.md): Hyd Line · leaking · Jan 8, 1998 · N814PH · Dhav DHC8102 · Hydraulic System, Main
  > AFTER TAKEOFF, NOTICED AN ODORLESS CHEMICAL IRRITANT IN THE COCKPIT. THE IRRITANT WAS NOTICED IN THE COCKPIT FOR A PERIOD OF ABOUT 20 SECONDS. MX PERFORMED AN ENGINE RUN WITH BLEEDS ON AND TEMP HOT FROM IDLE TO TAKEOFF POWER RPM. NO IRRITANT NOTED. PRESSUR
- [SDR QXEA9700673](https://openairdocs.org/sdr/QXEA9700673.md): Seat Mechanism · lack of lube · Oct 17, 1997 · N814PH · Dhav DHC8102 · Flight Compartment Equipment
  > PDX - FIRST OFFICERS SEAT SLIPPED BACK IN ITS TRACK DURING FLIGHT. CLEANED AND LUBED FIRST OFFICERS SEAT TRACK MECHANISM. NO PARTS REPLACED, OPERATIONAL CHECK GOOD.
- [SDR QXEA9700574](https://openairdocs.org/sdr/QXEA9700574.md): Mechanism · out of adjust · Sep 19, 1997 · N814PH · Dhav DHC8102 · Landing Gear Door Retract Section
  > PDX - LEFT HAND GEAR DOOR LIGHT STAYED ON AFTER GEAR WAS RAISED. ADJUSTED MAIN LANDING GEAR DOOR (REAR AND CENTER) ACTUATORS. ADJUSTED MAIN LANDING GEAR FORWARD DOOR CONNECTING LINK. RETRACTION AND EXTENSION TEST GOOD.
- [SDR QXEA9700610](https://openairdocs.org/sdr/QXEA9700610.md): Ball Screw Act · damaged · Aug 28, 1997 · N814PH · Dhav DHC8102 · Trailing Flap Position Indicating System
  > PDX - NR 3 AND NR 4 BALL SCREW ACTUATORS HAVE SLIGHT BRINELLING DAMAGE. REPAIRED IAW EA 9-27-69.
- [SDR QXEA9700609](https://openairdocs.org/sdr/QXEA9700609.md): Ball Screw · damaged · Aug 28, 1997 · N814PH · Dhav DHC8102 · Trailing Flap Position Indicating System
  > PDX - BALL SCREWS WITH SLIGHT BRINELLING DAMAGE. REPAIRED IAW EA 9-27-69.
- [SDR QXEA9700607](https://openairdocs.org/sdr/QXEA9700607.md): Angle · cracked · Aug 27, 1997 · N814PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > PDX - CRACK FLANGE OF THE NACELLE DRAG ANGLE, (P/N 85710323). REPAIRED IAW EA 9-57-291.
- [SDR QXEA9700608](https://openairdocs.org/sdr/QXEA9700608.md): Web · chafed · Aug 25, 1997 · N814PH · Dhav DHC8102 · Nacelle/Pylon Structure
  > PDX - RIGHT HAND NACELLE FINGERNAIL UPPER DECK CHAFE HOLE IN WEB. DAMAGE IS JUST OUTBOARD OF YN=0.00 AND JUST AFT OX XN=245. REPAIRED IAW 9-54-139.
- [SDR QXEA9700606](https://openairdocs.org/sdr/QXEA9700606.md): Hinge Bolt · misinstalled · Aug 25, 1997 · N814PH · Dhav DHC8102 · Landing Gear Doors
  > PDX - RIGHT MAIN LANDING GEAR FORWARD DOOR AFT HINGE AFT FRAME (85410422) AND JOINT STRAP (85410426) THAT WAS DAMAGED BY THE HINGE BOLT BEING INSTALLED BACKWARDS CHAFING THE FRAME AND JOINT STRAP. REAIRED IAW EA 9-54-138.
- [SDR QXEA9700322](https://openairdocs.org/sdr/QXEA9700322.md): Pseu · malfunction · Jul 10, 1997 · N814PH · Dhav DHC8102 · Landing Gear Position and Warning
  > ON APPROACH WHEN LANDING GEAR SELECTED DOWN, HAD 3 RED LANDING GEAR UNSAFE LIGHTS AND A LANDING GEAR HANDLE DISAGREEMENT LIGHT. PERFORMED AND ALTERNATE EXTENSION OF THE LANDING GEAR, AND ACCOMPLISHED A UNEVENTFUL LANDING. REPLACED THE PROXMITY SENSOR ELECTRO
- [SDR QXEA9700148](https://openairdocs.org/sdr/QXEA9700148.md): Diode · defective · Apr 25, 1997 · N814PH · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY EGRESS LIGHTS WILL NOT EXTINGUISH WHEN THE ARM-OFF SWITCH IS PLACED INTO THE OFF POSITION. AIRCRAFT FERRIED FROM SEA-PDX. REPLACED DIODE 3351-CR5, OPERATIONAL CHECKS GOOD.
- [SDR QXEA9700144](https://openairdocs.org/sdr/QXEA9700144.md): Control Box · defective · Apr 24, 1997 · N814PH · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT EXTINGUISH USING THE ARM-OFF SWITCH. REPLACED LIGHT CONTROL UNIT AND PS2, PS1, P1, P2, P4, P5 POWER SUPPLIES AND BATTERIES, OPERATIONAL CHECK GOOD.
- [SDR QXEA9700142](https://openairdocs.org/sdr/QXEA9700142.md): Control Box · defective · Apr 23, 1997 · N814PH · Dhav DHC8102 · Emergency Lighting
  > EMERGENCY EGRESS LIGHTS REMAIN ON EVEN WHEN THE SWITCH IS MOVED FROM ARM TO OFF. REPLACED EMERGENCY LIGHT CONTROLLER, OPERATIONAL CHECK GOOD.
- [SDR QXEA9700135](https://openairdocs.org/sdr/QXEA9700135.md): Detector · defective · Apr 20, 1997 · N814PH · Dhav DHC8102 · Smoke Detection
  > PDX- NR 1 BAGGAGE SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED NR 1 SMOKE DETECTOR. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA9700105](https://openairdocs.org/sdr/QXEA9700105.md): Radar Indicator · failed · Apr 1, 1997 · N814PH · Dhav DHC8102 · Weather Radar System
  > RADAR SCREEN WENT BLANK FOLLOWED BY STRONG ACRID SMELL IN COCKPIT, CREW TURNED RADAR OFF AND SMELL WENT AWAY. FLIGHT LANDED WITHOUT INCIDENT, RADAR DEFERRED PER MEL PROCEDURES. RADAR INDICATOR REPLACED LATER SAME DAY AND MEL CLEARED. AIRCRAFT RELEASED FOR
- [SDR QXEA9700010](https://openairdocs.org/sdr/QXEA9700010.md): Wire · broken · Jan 11, 1997 · N814PH · Dhav DHC8102 · Landing Gear System Wiring
  > PDX - ON APPROACH TO PDX RECEIVED 3 RED INTRANSIT LIGHT INDICATIONS, BUT LANDING GEAR DID NOT EXTEND. ALTERNATE GEAR EXTENSION PERFORMED AND GEAR EXTENDED. AIRCRAFT LANDED IN PDX WITHOUT FURTHER PROBLEM. WIRING FOR GEAR DOWN SELECTOR INHIBIT SWITCH, REPAIRE
- [SDR QXEA9600415](https://openairdocs.org/sdr/QXEA9600415.md): Light · malfunctioned · Sep 29, 1996 · N814PH · Dhav DHC8102 · Emergency Lighting
  > DURING OPS CHECK OF EMERGENCY LIGHTS, LIGHTS WOULD STAGGER OFF AND THEIR OWN WITHIN A COUPLE ON MINUTES. AIRCRAFT FERRIED TO PDX FOR REPAIR. PORTABLE EMERGENCY LIGHT AND RECEPTICAL WERE REPLACED AND LIGHTS OPS CHECKED GOOD.

Next page: https://openairdocs.org/deregistered/N814PH-2001-05-23/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 = 'N814PH' AND deregistration_id = 'N814PH-2001-05-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N814PH-2001-05-23/reports

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