# Service difficulty reports: N345PH, cancelled Nov 25, 2008

A list on [N345PH, cancelled Nov 25, 2008](https://openairdocs.org/deregistered/N345PH-2008-11-25.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 5 · 217 reports

- [SDR QXEA2008112401195](https://openairdocs.org/sdr/QXEA2008112401195.md): Bleed Valve · malfunctioned · Nov 20, 2008 · N345PH · Dhav DHC8202 · Compressor Bleed Valve
  > PDX - NR 2 TORQUE INCREASED EXCESSIVELY. TAKEOFF ABORTED AT LOW SPEED (BELOW 60KTS) AIRCRAFT YAWED ACCORDING TO DIFFERENTIAL POWER. RETURNED TO THE GATE. REPLACED NR 2 ENG IBV IAW MTC 9720024, OPS TEST GOOD. ALSO REPLACED THE NR 1 ENG TSCU IAW MM 72-01-1
- [SDR QXEA200800917](https://openairdocs.org/sdr/QXEA200800917.md): Unknown · unknown · Aug 17, 2008 · N345PH · Dhav DHC8202 · Air Distribution System
  > PDX - FLIGHT 2129. FLIGHT ATTENDANT REPORTS A "FOG" COMING FROM THE LAST 3 ROWS FROM ENG START THROUGH 10,000, THEN DISAPPEARED. MAINTENANCE PERFORMED A GROUND RUN OF THE ENGS WITH INDEPENDENT USE OF THE BLEED AIR. NO FOG, OR OTHER DEFECTS NOTED. RETURNED
- [SDR QXEA200800698](https://openairdocs.org/sdr/QXEA200800698.md): Spring · broken · Jun 29, 2008 · N345PH · Dhav DHC8202 · Landing Gear Door Retract Section
  > SEA - FLIGHT 2100. AFTER DEPARTURE, NOISE NOTED AFTER GEAR RETRACTION. TOWER REPORTED NOSE GEAR DOORS OPEN. RETURNED TO FIELD. UNEVENTFUL LANDING. FOUND RT FWD NLG DOOR SPRING AND CONTROL ROD BROKE. REPLACED. OPERATIONAL CHECKS GOOD. RETURNED TO SERVIC
- [SDR QXEA200800651](https://openairdocs.org/sdr/QXEA200800651.md): Lamp · inoperative · Jun 16, 2008 · N345PH · Dhav DHC8202 · Emergency Lighting
  > PDX - AUX BATTERY AND EMERGENCY DISARM LIGHTS DIM. REPLACED LAMPS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A)
- [SDR QXEA200800454](https://openairdocs.org/sdr/QXEA200800454.md): Potentiometer · out of adjust · May 7, 2008 · N345PH · Dhav DHC8202 · Propeller Feathering/Reversing
  > SEA - AUTOFEATHER SLOW TO ARM. ARMS ABOUT 90 PERCENT TORQUE. MAINTENANCE PLACED ON MEL 61-2. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED BY RIGGING THE ARMING POTS IAW 76-10-15-820-802. NOW ARMS AT 78-80 PERCENT. AIRCRAFT RETURNED TO SERVICE. NO PARTS REP
- [SDR QXEA200800450](https://openairdocs.org/sdr/QXEA200800450.md): Switch · loose · May 5, 2008 · N345PH · Dhav DHC8202 · Propeller Feathering/Reversing
  > SEA - AUTOFEATHER SWITCH APPEARS LOOSE AND TAKES LONGER THEN NORMAL TO ARM. MAINTENANCE SECURED THE SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA200800453](https://openairdocs.org/sdr/QXEA200800453.md): Control Unit · malfunctioned · May 5, 2008 · N345PH · Dhav DHC8202 · Propeller Feathering/Reversing
  > SEA - ON TAKEOFF, ABORTED AT 70 KNOTS, DUE TO AUTOFEATHER FAILED TO ARM. RETURNED TO THE GATE. MAINTENANCE REPLACED THE TSCU AND THE AUTOFEATHER SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR QXEA200800429](https://openairdocs.org/sdr/QXEA200800429.md): Relay · malfunctioned · Apr 26, 2008 · N345PH · Dhav DHC8202 · Propeller Feathering/Reversing
  > EUG - FLIGHT 2040 - ON TAKEOFF APPROACHING 70 KNOTS, THE AUTOFEATHER ARM LIGHT DID NOT ILLUMINATE. ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE AUTOFEATHER CONTROL RELAY 6121-K5. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVI
- [SDR QXEA200800001](https://openairdocs.org/sdr/QXEA200800001.md): Poppet Valve · leaking · Jan 2, 2008 · N345PH · Dhav DHC8202 · Fuel Storage
  > PDX - FUEL DRIPPING FROM THE AREA AROUND THE REFUELING DOOR. MAINTENANCE FOUND THE FUEL DRIPPING FROM THE SPR POPPET. RESEATED THE POPPET VALVE. CHECKS GOOD, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.
- [SDR QXEA200701784](https://openairdocs.org/sdr/QXEA200701784.md): Warning Light · multiple ind · Dec 1, 2007 · N345PH · Dhav DHC8202 · Central Warning
  > PDX - AFTER STARTING THE NR 1 ENGINE THE START LIGHT REMAINED ILLUMINATED. AFTER MOVING THE START SELECTOR SWITCH MANUALLY BACK TO CENTER THE LIGHT WENT OUT. THE NR 1 DC GENERATOR CAUTION WAS ILLUMINATED. AFTER FOLLOWING THE CHECKLIST, ALL INDICATIONS WENT
- [SDR QXEA200701647](https://openairdocs.org/sdr/QXEA200701647.md): Shutoff Valve · malfunctioned · Nov 3, 2007 · N345PH · Dhav DHC8202 · Engine Bleed Air System
  > SEA FLIGHT NR 2152 DURING CLIMB THROUGH 17,000, NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED. CYCLING ON AND OFF. CAUTION LIGHT EXTINGUISHED AFTER SELECTING FLOW SELECTOR KNOB. PERFORMED BLEED AIR FUNCTION TEST. FOUND NR 1 ENGINE SLOW TO SWITCH FROM LP AIR TO
- [SDR QXEA200701646](https://openairdocs.org/sdr/QXEA200701646.md): Warning System · false activation · Nov 2, 2007 · N345PH · Dhav DHC8202 · Pneumatic System
  > PDX FLIGHT NR 2058 - DURING CLIMB-OUT, NR 1 BLEED HOT CAUTION MESSAGE. PER CHECKLIST TURNED BLEED SELECTOR TO MIN LIGHT STOPPED CYCLING. PERFORMED BLEED AIR FUNCTIONAL TEST COULD NOT DU0PLICATE PROBLEM REPLACED NR 1 BLEED AIR OVERTEMP SWITCH AS A PRECAUTIONA
- [SDR QXEA200701475](https://openairdocs.org/sdr/QXEA200701475.md): Skin · cracked · Sep 26, 2007 · N345PH · Dhav DHC8202 · Nacelle/Pylon, Plate/Skin
  > C5 PDX - ON NR 1 NACELLE SKIN AT THE FORWARD INBOARD CUTOUT RADIUS FOR THE FORWARD GEAR DOOR. THE NACELLE SKIN IS CRACKED 1/4" LONG. REPAIRED IAW RD8-54-873.
- [SDR QXEA200701482](https://openairdocs.org/sdr/QXEA200701482.md): Drag Strut · chafed · Sep 23, 2007 · N345PH · Dhav DHC8202 · Main Landing Gear
  > C5 PDX - RIGHT DRAG STRUT INBOARD ATTACH POINT IS CHAFED. REPAIRED IAW SRM 51-20-26.
- [SDR QXEA200701478](https://openairdocs.org/sdr/QXEA200701478.md): Seat Track · damaged · Sep 23, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - LEFT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X445 - X435/ Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701477](https://openairdocs.org/sdr/QXEA200701477.md): Seat Track · damaged · Sep 23, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - RIGHT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X445 - X435/Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701476](https://openairdocs.org/sdr/QXEA200701476.md): Seat Track · damaged · Sep 23, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - RIGHT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X507 - X516 Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701458](https://openairdocs.org/sdr/QXEA200701458.md): Seat Track · corroded · Sep 23, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Bulkhead Fuselage wiring
  > C5 PDX - CORROSION ON NR 9 SEAT TRACK AT STATION X597.5. REPAIRED IAW RD8-53-784.
- [SDR QXEA200701455](https://openairdocs.org/sdr/QXEA200701455.md): Seat Track · damaged · Sep 23, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - LEFT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME AT STATION X507 - X516/Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701454](https://openairdocs.org/sdr/QXEA200701454.md): Seat Track · damaged · Sep 23, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - RIGHT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X473 - 484. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701474](https://openairdocs.org/sdr/QXEA200701474.md): Web · corroded · Sep 22, 2007 · N345PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > C5 PDX - MTX REQUEST - CORROSION ON WEB MATING SURFACE TO STRINGER 24L FROM STATION X487 TO X501. REPAIRED IAW SRM 51-20-11, 51-40-11.
- [SDR QXEA200701472](https://openairdocs.org/sdr/QXEA200701472.md): Skin · corroded · Sep 21, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > C5 PDX - X487 AND STRINGER 23L FORWARD OF FRAME AND UNDERSIDE THERE IS CORROSION IN 3 SPOTS. REPAIRED IAW SRM 51-20-11, 51-20-36.
- [SDR QXEA200701471](https://openairdocs.org/sdr/QXEA200701471.md): Skin · corroded · Sep 21, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > C5 PDX - X487 STRINGER 23L THERE IS CORROSION FORWARD OF FRAME AT ATTACH CLIP. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-26.
- [SDR QXEA200701468](https://openairdocs.org/sdr/QXEA200701468.md): Skin · corroded · Sep 21, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > C5 PDX - SKIN CORROSION AT NR 1 DME ANTENNA MOUNT LOCATED JUST AFT OF NOSE GEAR AT STATION 110 LT SIDE OF CENTER. REPAIRED IAW RD8-53-5384 AND RD8-53-9800, AND SRM 51-20-16.
- [SDR QXEA200701457](https://openairdocs.org/sdr/QXEA200701457.md): Seat Track · corroded · Sep 21, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - CORROSION ON NR 1 SEAT TRACK AT STATION X342. REPAIRED IAW RD8-53-1342, SRM 51-40-00.
- [SDR QXEA200701469](https://openairdocs.org/sdr/QXEA200701469.md): Skin · corroded · Sep 20, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Plate/Skin
  > C5 PDX - AT STRINGER 23L X511 THERE IS CORROSION SHOWING AROUND A RIVET HEAD. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-26.
- [SDR QXEA200701466](https://openairdocs.org/sdr/QXEA200701466.md): Stringer Clip · corroded · Sep 20, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Attach Fittings
  > C5 PDX - STRINGER 23L CLEAT IS CORRODED FORWARD SIDE OF FRAME 424.124 AT STATION X419-X422. REPAIRED IAW SRM 51-20-11, 51-40-11.
- [SDR QXEA200701473](https://openairdocs.org/sdr/QXEA200701473.md): Frame · damaged · Sep 20, 2007 · N345PH · Dhav DHC8202 · Nacelle/Pylon, Frame/Spar/Rib
  > C5 PDX - NR 2 NACELLE, FRAME FITTING FOR FORWARD MAIN LANDING GEAR DOOR, AFT HINGE ARM SUPPORT RIB HAS ONE FASTENER HOLE BLOWN OUT. REPAIRED IAW SRM 51-40-11.
- [SDR QXEA200701470](https://openairdocs.org/sdr/QXEA200701470.md): Stringer · corroded · Sep 20, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Longeron/Stringer
  > C5 PDX - AT STRINGER 23L X492 THERE IS CORROSION AT A RIVET HEAD. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-26.
- [SDR QXEA200701465](https://openairdocs.org/sdr/QXEA200701465.md): Stringer · corroded · Sep 20, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Longeron/Stringer
  > C5 PDX - STRINGER 24L CLEAT IS CORRODED AFT SIDE OF FRAME 424.124 AT STATION X426-X429. REPAIRED IAW SRM 51-20-11, 51-40-11.
- [SDR QXEA200701464](https://openairdocs.org/sdr/QXEA200701464.md): Arm · damaged · Sep 20, 2007 · N345PH · Dhav DHC8202 · Landing Gear Doors
  > C5 PDX - RIGHT NACELLE CUTOUT FOR FORWARD MAIN LANDING GEAR DOOR AFT HINGE ARM HAS DENT AND GOUGE IN SUPPORT RIB, AFT SIDE OF OPENING. REPAIRED IAW SRM 51-20-11, 51-40-11.
- [SDR QXEA200701467](https://openairdocs.org/sdr/QXEA200701467.md): Stringer Clip · corroded · Sep 19, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Attach Fittings
  > C5 PDX - STRINGER 24L CLEAT IS CORRODED AFT SIDE OF FRAME 387.350 AT STATION X389-X392. REPAIRED IAW SRM 51-20-11, 51-40-11.
- [SDR QXEA200701459](https://openairdocs.org/sdr/QXEA200701459.md): Firewall · cracked · Sep 19, 2007 · N345PH · Dhav DHC8202 · Nacelle/Pylon, Bulkhead/Firewall
  > C5 PDX - THERE IS A CRACK IN THE RIGHT FIREWALL ABOUT 2" LONG JUST ABOVE AND INBOARD OF THE RIGHT ENGINE FIRE EXTINGUSHING LINE. REPAIRED IAW RD8-54-2396.
- [SDR QXEA200701462](https://openairdocs.org/sdr/QXEA200701462.md): Support Bracket · chafed · Sep 19, 2007 · N345PH · Dhav DHC8202 · Nacelle/Pylon, Main Frame
  > C5 PDX - RIGHT NACELLE INBOARD FRAME SUPPORT BRACKET CHAFED. REPAIRED IAW SRM 51-20-51, RD8-54-2397.
- [SDR QXEA200701460](https://openairdocs.org/sdr/QXEA200701460.md): Door Frame · chafed · Sep 18, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Structure
  > C5 PDX - CHAF ON FRAME AT STATION 222 - 2100, LEFT SIDE, MAIN CABIN DOOR FORWARD SIDE. REPAIRED IAW RD8-53-9791.
- [SDR QXEA200701456](https://openairdocs.org/sdr/QXEA200701456.md): Seat Track · corroded · Sep 18, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - NUMBER 4 SEAT TRACK FLANGE CORRODED AT MAIN CABIN DOOR ENTRY. REPAIRED IAW RD8-53-4473 AND RD8-53-1102.
- [SDR QXEA200701453](https://openairdocs.org/sdr/QXEA200701453.md): Seat Track · corroded · Sep 18, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - NUMBER 7 SEAT TRACK, TOP SURFACE CORRODED FROM STATION 242 THRU 195, GALLEY AND LAV ATTACH AREA. REPAIRED IAW SRM 51-40-11, RD8-53-1102 AND RD8-53-4473.
- [SDR QXEA200701463](https://openairdocs.org/sdr/QXEA200701463.md): Mount · damaged · Sep 17, 2007 · N345PH · Dhav DHC8202 · Horizontal Stabilizer, Attach Fittings
  > C5 PDX - HORIZONTAL STAB FORWARD RIGHT MOUNTING STRUCTURE HAS NICKS AND GOUGES ON OUTBOARD SIDE. REPAIRED IAW RD8-55-847, SRM 51-20-51, 51-20-16.
- [SDR QXEA200701461](https://openairdocs.org/sdr/QXEA200701461.md): Mount · damaged · Sep 17, 2007 · N345PH · Dhav DHC8202 · Horizontal Stabilizer, Attach Fittings
  > C5 PDX - HORIZONTAL STAB FORWARD MOUNT POSTS ARE SCRATCHED ON OUTBOARD SURFACE. REPAIRED IAW RD8-55-847 AND SRM 51-20-51, 51-20-16.
- [SDR QXEA200701479](https://openairdocs.org/sdr/QXEA200701479.md): Seat Track · damaged · Sep 16, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - LEFT INBOARD SEAT TRACK HAS WEAR DAMAGE, BOTTOM OF TRACK FRAME STATION X473 - X484/ Y9.2. REPAIRED IAW RD8-53-1339.
- [SDR QXEA200701481](https://openairdocs.org/sdr/QXEA200701481.md): Angle · cracked · Sep 16, 2007 · N345PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > C5 PDX - SUSPECT CRACK IN FORWARD RIGHT CLOSING ANGLE RADIUS AT STATION X387, STRINGER 5 RIGHT UNDER PANEL 261JT. REPAIRED IAW RD8-53-5192.
- [SDR QXEA200701480](https://openairdocs.org/sdr/QXEA200701480.md): Flap Track · corroded · Sep 16, 2007 · N345PH · Dhav DHC8202 · Trailing Edge Flaps
  > C5 PDX - PITTING ON RIGHT INBOARD FLAP, LOWER SIDE OF UPPER NR 2 TRACK AT ZERO DEGREE ROLLER INDICATION. REPAIRED IAW RD8-57-986.
- [SDR QXEA200701483](https://openairdocs.org/sdr/QXEA200701483.md): Angle · cracked · Sep 15, 2007 · N345PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > C5 PDX - SUSPECT CRACK RIGHT AFT CLOSING ANGLE AT STINGER 6 RIGHT UNDER FLAP PCU. REPAIRED IAW RD8-53-5192.
- [SDR QXEA200701439](https://openairdocs.org/sdr/QXEA200701439.md): Skin · corroded · Sep 15, 2007 · N345PH · Dhav DHC8202 · Passenger/Crew Doors
  > C5 PDX - MAIN CABIN DOOR SHELL HAS CORROSION BY FORWARD NR 1 STOP/STEP ASSEMBLY ATTACH POINT. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-26.
- [SDR QXEA200701432](https://openairdocs.org/sdr/QXEA200701432.md): Bracket · corroded · Sep 15, 2007 · N345PH · Dhav DHC8202 · Fuselage Miscellaneous Structure
  > C5 PDX - SUSPECT CORROSION TO HORIZONTAL STRINGER/RISER BRACKET AT STRINGER 31R STATION 201. REPAIRED IAW SRM 51-40-11.
- [SDR QXEA200701436](https://openairdocs.org/sdr/QXEA200701436.md): Floorboard · corroded · Sep 14, 2007 · N345PH · Dhav DHC8202 · Fuselage Floor Panel
  > C5 PDX - FLOORBOARD FLANGE AT STATION 599.00 RIGHT END UPPER SURFACE HAS CORROSION. REPAIRED IAW SRM 51-20-11, 51-40-11, AND 51-20-16.
- [SDR QXEA200701429](https://openairdocs.org/sdr/QXEA200701429.md): Stringer · corroded · Sep 14, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Longeron/Stringer
  > C5 PDX - RIGHT STRINGER 21 HAS CORROSION ON INBOARD LEADING EDGE FLANGE AT STATION 357.70. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-20-36, AND 51-20-26.
- [SDR QXEA200701430](https://openairdocs.org/sdr/QXEA200701430.md): Frame · corroded · Sep 14, 2007 · N345PH · Dhav DHC8202 · Fuselage Main, Structure
  > C5 PDX - FORWARD CENTER UNDERFLOOR VERTICAL FRAME STRUCTURE AT STATION 201, STRINGER 31L. SUSPECT CORROSION UP FRONT SKIN ON AFT INBOARD CORNER OF FLOOR RISER FRAME. REPAIRED IAW SRM 51-20-36, 51-20-11, 51-20-26, AND 51-2016.
- [SDR QXEA200701435](https://openairdocs.org/sdr/QXEA200701435.md): Seat Track · corroded · Sep 13, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - FLOORBOARD FLANGE TO SEAT TRACK GUSSET AT STATION 599.0 INBOARD OF LEFT INBOARD SEAT TRACK HAS CORROSION ON LOWER SURFACE AND ALONG EDGE ON FLANGE. REPAIRED IAW SRM 51-20-11, 51-20-16, 51-40-11.
- [SDR QXEA200701434](https://openairdocs.org/sdr/QXEA200701434.md): Seat Track · corroded · Sep 13, 2007 · N345PH · Dhav DHC8202 · Fuselage, Seat/Cargo Attach Fittings
  > C5 PDX - FLOORBOARD NUT PLATE AND FLANGE ARE CORRODED AT STATION 599.0 INBOARD OF LEFT INBAORD SEAT TRACK. REPAIRED IAW SRM 51-40-11, 51-20-11, 51-20-36.

Next page: https://openairdocs.org/deregistered/N345PH-2008-11-25/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 = 'N345PH' AND deregistration_id = 'N345PH-2008-11-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N345PH-2008-11-25/reports

---
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