# Service difficulty reports: N728PL, cancelled Jan 7, 2014

A list on [N728PL, cancelled Jan 7, 2014](https://openairdocs.org/deregistered/N728PL-2014-01-07.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 3 · 107 reports

- [SDR IXXA0300086O](https://openairdocs.org/sdr/IXXA0300086O.md): Downlock Switch · broken · Dec 24, 2003 · N728PL · Doug DC862 · Landing Gear Position and Warning
  > WHEN GEAR WAS EXTENED THE LT GEAR LIGHT DID NOT ILLUMINATE. AFTER CYCLING GEAR ALL THREE GEAR LIGHTS WERE NORMAL. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR DOWN LOCK INDICATION SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR IXXA0300070O](https://openairdocs.org/sdr/IXXA0300070O.md): Bearing · lack of lube · Oct 29, 2003 · N728PL · Doug DC862 · Pressure Regulator/Outflow Valve
  > DURING CLIMB FROM FJDG CREW LOST CABIN PRESSURIZATION. CREW RETURNED TO FJDG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED OUTFLOW VALVE. THEY LUBED MECHANICAL ARMS AND BEARINGS. OPERATIONAL CHECK GOOD BOTH IN AUTO AND MANUAL PER ALL APPLICABLE MANUALS. T
- [SDR IXXA0300061O](https://openairdocs.org/sdr/IXXA0300061O.md): Uplock Sensor · contaminated · Oct 12, 2003 · N728PL · Doug DC862 · Landing Gear Position and Warning
  > ON APPROACH, WITH ALL 3 MLG'S DOWN AND LOCKED, BOTH (DOOR NOT LATCHED, GEAR NOT LATCHED) LIGHTS WERE ILLUMIN, ALSO AUDIBLE WARNING HORN. GEAR WAS RECYCLED TWICE, THIS CORRECTED PROBLEM. MAINT INSPECTED LANDING GEAR, GEAR DOOR WARNING SYS. NO DEFECTS WERE NOTED
- [SDR IXXA0300059O](https://openairdocs.org/sdr/IXXA0300059O.md): Valve · malfunctioned · Sep 17, 2003 · N728PL · Doug DC862 · Turbine Engine Oil System
  > DURING CLIMB NR 4 ENG QTY DROPPED & OIL PRESS ROSE TO 60 PSI, TEMP INCREASED. POWER WAS REDUCED PARAMETERS REDUCED OIL PRESS, OIL TEMP REDUCED 20 DEGREES & OIL QTY INCREASED. OIL PRESS LIGHT NEVER ILLUM & OIL PRESS NEVER DROPPED BELOW 40 PSI. MX REMOVED & I
- [SDR IXXA0300037O](https://openairdocs.org/sdr/IXXA0300037O.md): Outflow Valve · contaminated · May 25, 2003 · N728PL · Doug DC862 · Pressure Regulator/Outflow Valve
  > DURING CRUISE AT FLIGHT LEVEL 28K CABIN ALTITUDE BEGAN TO CLIMB. CREW ELECTED TO DEPLOY PASSENGER O2 MASKS. FLIGHT CONTINUED TO WSAP AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION MAINTENANCE CLEANED OUTFLOW VALVE, INSPECTED DUCTING AND OPERATIONALLY CHECKED
- [SDR IXXA0300029O](https://openairdocs.org/sdr/IXXA0300029O.md): Landing Gear · false indication · Mar 21, 2003 · N728PL · Doug DC862 · Landing Gear Position and Warning
  > DURING FLIGHT FROM KWAK TO RJTY LANDING GEAR WAS PUT IN DOWN POSITION. THERE WAS NO LEFT GEAR INDICATION. THE GEAR WAS RECYCLED AND IT INDICATED GEAR DOWN. MAINTENANCE JACKED AIRCRAFT AND SWUNG GEAR A TOTAL OF FIVE TIMES. OPERATIONAL CHECK GOOD IN ACCORDAN
- [SDR IXXA0300012O](https://openairdocs.org/sdr/IXXA0300012O.md): O-Ring · leaking · Feb 4, 2003 · N728PL · Doug DC862 · Hydraulic Pump (Electric/Engine), Main
  > DURING CRUISE CREW NOTED HYD QTY DROPPING ABNORMALLY. CREW COMPLETED ABNORMAL CHECKLIST AND PROCEEDED TOWARDS QPG. WHILE ON FINAL APPROACH, AFTER ADVISING QPG ATC OF ABNORMAL CHECKLIST COMPLETION. QPG ATC DENIED LANDING CLEARANCE. CREW ELECTED TO PROCEED T
- [SDR IXXA0200116O](https://openairdocs.org/sdr/IXXA0200116O.md): O-Ring · leaking · Dec 2, 2002 · N728PL · Doug DC862 · Hydraulic System, Main
  > EN ROUTE FROM NKW TO BAH. FLIGHT CREW NOTED MAIN HYDRAULIC SYSTEM FLUID QUANITY DECLINING. CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED WITHOUT INCIDENT TO BAH. MAINTENANCE DISCOVERED O-RING LEAKING AT MAIN HYDRAULIC SYSTEM SELECTOR VALVE. REPLACED O-RING AN
- [SDR IXXA0200114O](https://openairdocs.org/sdr/IXXA0200114O.md): Striker · loose · Nov 19, 2002 · N728PL · Doug DC862 · Landing Gear Position and Warning
  > ENROUTE KWA TO HIK, THE GEAR DOOR NOT LATCH LIGHT ILLUMINATED. THE FLIGHT CREW CYCLED THE GEAR, PERFORMED AN GEAR UPLOCK CHECK AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEA
- [SDR IXXA0200073S](https://openairdocs.org/sdr/IXXA0200073S.md): Structure · corroded · Jun 9, 2002 · N728PL · Doug DC862 · Horizontal Stabilizer, Tab Structure
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE STATION XFS 178 TO XFS 285. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND REPAIR DOUBLER IN ACCOURD
- [SDR IXXA0200072S](https://openairdocs.org/sdr/IXXA0200072S.md): Skin · corroded · Jun 1, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATION 857 TO 902 BETWEEN LONGERONS 10L TO 21L. REPAIR ACCOMPLISHED CORROSION REMOVAL AND FOUND TO BE WITHIN LIMITATIONS. CORROSION REMOVAL AT FUSELAGE
- [SDR IXXA0200071S](https://openairdocs.org/sdr/IXXA0200071S.md): Wing · cracked · May 31, 2002 · N728PL · Doug DC862 · Wing Spar
  > DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING UPPER LEADING EDGE OUTBOARD OF NUMBER FOUR PYLON. REPAIR ACCOMPLISHED REOMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERMAL DOUBLER IN ACCORDANCE WI
- [SDR IXXA0200070S](https://openairdocs.org/sdr/IXXA0200070S.md): Skin · corroded · May 30, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 902, LONGERONS 14,17 AND 18 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL AND DETERMINED TO BE WITH LIMITATION IN ACCORDANCE WITH THE DOUGLAS STRUCTUR
- [SDR IXXA0200069S](https://openairdocs.org/sdr/IXXA0200069S.md): Door · corroded · May 21, 2002 · N728PL · Doug DC862 · Passenger/Crew Doors
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT FUSELAGE STATION 15OO, AFT PASSENGER DOOR FRAME AT THE LOWER AFT CORNER. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGE AREA, FABRICATION AND INSTALLATION OF A NEW INTERNAL REPAIR ANGLE AND FRAME IN ACCO
- [SDR IXXA0200067S](https://openairdocs.org/sdr/IXXA0200067S.md): Door · cracked · May 17, 2002 · N728PL · Doug DC862 · Doors
  > DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD ENTRANCE DOOR CUT OUT FORWARD UPPER CORNER. REPAIR ACCOMPLISHED, REMOVAL OF THE TEMPORARY REPAIR AND DAMAGED AREA, FABRICATION AND INSTALLATIN OF A REPAIR FILLER,
- [SDR IXXA0200066S](https://openairdocs.org/sdr/IXXA0200066S.md): Skin · corroded · May 16, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT HAND SIDE FUSELAGE SKIN BELOW THE AFT PASSENGER DOOR SKIN CUT OUT AT STATION 1480 TO 1510. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED SKIN, FABRICATION AND INSTALLATION OF FILLER REPAIR DOULBE
- [SDR IXXA0200065S](https://openairdocs.org/sdr/IXXA0200065S.md): Skin · cracked · May 15, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK, A CRACK WAS DETECTED IN THE AFT PASSENGER DOOR FORWARD LOWER SKIN CORNER AT SKIN CUTOUT. REPAIR ACCOMPLISHED, REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER, DOUBLER AND TRIPLER IN ACCORDANCE WITH THE DOUG
- [SDR IXXA0200064S](https://openairdocs.org/sdr/IXXA0200064S.md): Spar · corroded · May 15, 2002 · N728PL · Doug DC862 · Wing Spar
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON TOP OF THE LEFT WING INTERSPAR SKIN BETWEEN XRS 190 INBOARD TO WING WALK AREA TO INCLUDE THE MAIN SKIN EXTENSION OVER GEAR TRUNNION AREA. REPAIR ACCOMPLISHED CORROSION REMOVAL. FABRICATION AND INSTA
- [SDR IXXA0200063S](https://openairdocs.org/sdr/IXXA0200063S.md): Spar · corroded · May 15, 2002 · N728PL · Doug DC862 · Wing Spar
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE UPPER WING EXTERNAL PLATING BETWEEN WING STATION XFS 172 AND XFS 255. REPAIR ACCOMPLISHED, CORROSION REMOVAL OF THE DAMAGE ARE, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH
- [SDR IXXA0200062S](https://openairdocs.org/sdr/IXXA0200062S.md): Skin · corroded · May 15, 2002 · N728PL · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, LIGHT CORROSION WAS DETECTED ON THE TOP OF THE LEFT WING INTERSPAR SKIN BETWEEN STATION XW 408 XRS 590 TO STATION XRS 590. REPAIR ACCOMPLISHED CORROSION REMOVAL OF THE AFFECTED AREA IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL R
- [SDR IXXA0200061S](https://openairdocs.org/sdr/IXXA0200061S.md): Skin · cracked · May 14, 2002 · N728PL · Doug DC862 · Leading Edge Devices
  > DURING ROUTINE C-CHECK INSPECTION, A CRACKED WAS DETECTED ON THE RIGHT WING OUTBOARD LEADING EDGE PANEL AT THE INBOARD AREA AT STATION XRS 634. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A FILLER AND REPAIR DOUBLER IN ACC
- [SDR IXXA0200060S](https://openairdocs.org/sdr/IXXA0200060S.md): Skin · cracked · May 14, 2002 · N728PL · Doug DC862 · Leading Edge Devices
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE AT WING STATION XES710, UPPER CHORD MOUNTS. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUB
- [SDR IXXA0200059S](https://openairdocs.org/sdr/IXXA0200059S.md): Skin · cracked · May 11, 2002 · N728PL · Doug DC862 · Leading Edge Devices
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE LEFT WING OUTBOARD LOWER LEADING EDGE AT STATION XFS 566. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBLER IN ACCO
- [SDR IXXA0200058S](https://openairdocs.org/sdr/IXXA0200058S.md): Structure · corroded · May 11, 2002 · N728PL · Doug DC862 · Leading Edge Devices
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LT WING OUTBOARD UPPER LEADING EDGE AT STATION XFS 705. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH THE DOUGLAS S
- [SDR IXXA0200057S](https://openairdocs.org/sdr/IXXA0200057S.md): Structure · corroded · May 11, 2002 · N728PL · Doug DC862 · Leading Edge Devices
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RT WING OUTBOARD LEADING EDGE AT STATION XFS 705. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER AND INTERNAL FILLER IN ACCORDANCE WITH
- [SDR IXXA0200056S](https://openairdocs.org/sdr/IXXA0200056S.md): Structure · corroded · May 11, 2002 · N728PL · Doug DC862 · Wing Main, Frame Structure
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED IN THE LEFT WING LEADING EDGE TOP SIDE AT STATION XFS 825. REMOVAL ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR
- [SDR IXXA0200055S](https://openairdocs.org/sdr/IXXA0200055S.md): Skin · corroded · May 11, 2002 · N728PL · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AROUND THE SCREW HEADS ON THE TOP LEFT WING LEADING EDGE XFS 885. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS
- [SDR IXXA0200054S](https://openairdocs.org/sdr/IXXA0200054S.md): Structure · corroded · May 10, 2002 · N728PL · Doug DC862 · Fuselage Main, Structure
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE AT STATION 1440 AT LONGERON 22RT. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER AND INTERNAL FILLER IN ACCORDANCE WITH THE DOUGLAS ST
- [SDR IXXA0200053S](https://openairdocs.org/sdr/IXXA0200053S.md): Skin · corroded · May 10, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE AFT LOWER FUSELAGE FORWARD OF ACCESS PANEL NUMBER 60, STATION 1557 TO 1574, LONGERON 35 RT. REPAIR ACCOMPLISHED, REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A INTERNAL FILLER AN
- [SDR IXXA0200052S](https://openairdocs.org/sdr/IXXA0200052S.md): Skin · corroded · May 10, 2002 · N728PL · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE AFT LOWER FUSELAGE STATION 1520 BETWEEN LONGERONS 30LT TO 30RT. REPAIR ACCOMPLISHED, DAMAGED AREA CUT OUT, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLA
- [SDR IXXA0100074O](https://openairdocs.org/sdr/IXXA0100074O.md): Fan · defective · Nov 22, 2001 · N728PL · Doug DC862 · Air Distribution Fan
  > ENROUTE FROM KWA TO HIK, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT AND THE AFT PASSENGER COMPARTMENT WHEN THE RIGHT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDIN
- [SDR IXXA0100038](https://openairdocs.org/sdr/IXXA0100038.md): Uplock · lack of lube · Jul 5, 2001 · N728PL · Doug DC862 · Landing Gear Retraction/Extension System
  > EN ROUTE FROM HIK TO SUU, THE LANDING GEAR NOT LATCH LIGHT ILLUMINATED DURING THE LANDING GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO SUU FOR AN UNEVENTFUL LANDING. MAINTE
- [SDR IXXA0100005](https://openairdocs.org/sdr/IXXA0100005.md): Door · missing · Feb 12, 2001 · N728PL · Doug DC862 · Landing Gear Doors
  > AFTER AN UNEVENTFUL LANDING AND DURING POST FLIGHT INSPECTION AT WRI. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR LOWER FLYING DOOR MISSING FROM THE GEAR. NO OTHER DAMAGE TO THE AIRCRAFT WAS NOTED. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY FOR RE
- [SDR IXXA01000052](https://openairdocs.org/sdr/IXXA01000052.md): Door · missing · Feb 12, 2001 · N728PL · Doug DC862 · Landing Gear Doors
  > AFTER AN UNEVENTFUL LANDING AND DURING POST FLIGHT INSPECTION AT WRI. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR LOWER FLYING DOOR MISSING FROM THE GEAR. NO OTHER DAMAGE TO THE AIRCRAFT WAS NOTED.
- [SDR IXXA0000025](https://openairdocs.org/sdr/IXXA0000025.md): Fan · defective · Jul 12, 2000 · N728PL · Doug DC862 · Air Distribution Fan
  > EN ROUTE FROM ASI TO ANU, THE FLIGHT CREW DETECTED SMOKE IN THE COCKPIT ACCOMPANIED BY THE LEFT RECIRCULATION FAN SHUTING DOWN, SMOKE SUBSIDED. THE FLIGHT CONTINUED TO ANU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECT THE LEFT RECIRCULATION FAN AND FOUND IT
- [SDR IXXA0000017](https://openairdocs.org/sdr/IXXA0000017.md): Fan · defective · Apr 25, 2000 · N728PL · Doug DC862 · Air Distribution Fan
  > EN ROUTE FROM FJR TO NKW, THE FLIGHT CREW NOTICED SMOKE INTO THE COCKPIT WHEN THE LEFT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE SMOKE SUBSIDED. THE FLIGHT CONTINUED TO NKW FOR AN UNEVENFUL LANDING. MAINTENANCE INSPECTED THE F
- [SDR IXXA9900032](https://openairdocs.org/sdr/IXXA9900032.md): Fan · failed · Nov 23, 1999 · N728PL · Doug DC862 · Air Distribution System
  > EN ROUTE FROM QPG TO NKW, AN ELECTRICAL ODOR WAS SENSED IN THE COCKPIT WHEN THE RIGHT RECIRCULATING FAN WAS TURNED ON. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED AND THE FLIGHT CONTINUED TO NKW. MAINTENANCE INSPECTED THE FAN AND WAS FOUND DEFECTIVE
- [SDR IXXA9900007](https://openairdocs.org/sdr/IXXA9900007.md): Turbine · failed · Apr 20, 1999 · N728PL · Doug DC862 · Turbine Section
  > EN ROUTE FROM PKWA TO PHIK DURING CLIMB, A LOUD NOISE WAS HEARD FROM THE NUMBER TWO ENGINE, ACCOMPANIED BY INCREASING ENGINE GAS TEMPERATURE AND A DECLINE IN OIL PRESSURE. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND CONTINUED TO PHIK F
- [SDR IXXA9800080](https://openairdocs.org/sdr/IXXA9800080.md): Tires · worn · Oct 12, 1998 · N728PL · Doug DC862 · Tire
  > AFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW HEARD AND FELT A VIBRATION THROUGH THE COCKPIT FLOOR. THE AIRCRAFT RETURNED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE NOSE TIRES OUT OF ROUND.
- [SDR IXXA9800079](https://openairdocs.org/sdr/IXXA9800079.md): Retract Mech · lack of lube · Oct 12, 1998 · N728PL · Doug DC862 · Landing Gear Door Retract Section
  > AFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A NOSE GEAR DOOR HAD FALLEN OPEN CAUSING A LOUD NOISE AND SLIGHT VIBRATION FROM THE NOSE WHEEL WELL AREA. THE CREW CYCLED THE GEAR, THE VIBRATION CONDITION WAS STILL PRESENT. THE AIR
- [SDR IXXA9800068](https://openairdocs.org/sdr/IXXA9800068.md): Switch · defective · Aug 28, 1998 · N728PL · Doug DC862 · Landing Gear Position and Warning
  > EN ROUTE FROM BWI TO WRI, WHEN THE LANDING GEAR WAS RETRACTED, THE LANDING GEAR UNSAFE LIGHT REMAINED ON. THE CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO WRI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE
- [SDR IXXA9800060](https://openairdocs.org/sdr/IXXA9800060.md): Ballast · failed · Jul 7, 1998 · N728PL · Doug DC862 · Flight Compartment Lighting
  > EN ROUTE FROM KWA TO HIK, SMOKE EMANATED FROM THE FIRST OFFICERS RIGHT PEDESTAL CONSOLE. THE CREW EXTINGUISHED THE MAIN INSTRUMENT GLARESHIELD WHITE LIGHTING, THE SMOKE STOPPED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND THAT T
- [SDR IXXA9800057](https://openairdocs.org/sdr/IXXA9800057.md): Actuator · misrigged · Jun 18, 1998 · N728PL · Doug DC862 · Landing Gear Actuator
  > EN ROUTE, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCH WARNING LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR WITH THE INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO SUU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR AND IND
- [SDR IXXA9800034](https://openairdocs.org/sdr/IXXA9800034.md): Fan · failed · Apr 5, 1998 · N728PL · Doug DC862 · Air Distribution Fan
  > ENROUTE, A BURNT ELECTRICAL ODOR WAS SENSED IN THE COCKPIT WITH THE RIGHT RECIRCULATION FAN OPERATING. THE FAN WAS SHUT OFF FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED AND FOUND THE FAN DEFECTIVE. MAINTENANCE DEFERRED THE RIGHT RECIRCULATION FAN.
- [SDR IXXA9800035](https://openairdocs.org/sdr/IXXA9800035.md): Switch · defective · Apr 2, 1998 · N728PL · Doug DC862 · Landing Gear Position and Warning
  > ENROUTE, GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCHED WARNING LIGHT ILLUMINATED. THE FLIGHT CREW CYCLED THE GEAR EXTINGUSHING THE WARNING LIGHT. GROUND INSPECTION FOUND THE LEFT MAIN GEAR UPLATCH SWITCH INTERMITTENT AND ELECTRICAL CONNECTOR DAMAGED.
- [SDR IXXA980016](https://openairdocs.org/sdr/IXXA980016.md): Sealing Tape · misinstalled · Mar 3, 1998 · N728PL · Doug DC862 · Cargo Compartments
  > DURING DESCENT INTO HIK, THE NUMBER TWO AND FIVE MAIN CARGO COMPARTMENT SMOKE DETECTOR WARING LIGHTS ILLUMINATED. THE FLIGHT CREW TURNED OFF THE CARGO COMPARTMENT LIGHTING AND THE WARNING LIGHTS EXTINGUISHED. MAINTENANCE INSPECTED THE CARGO COMPARTMENT WITH T
- [SDR IXXA9800027](https://openairdocs.org/sdr/IXXA9800027.md): Plating · corroded · Nov 26, 1997 · N728PL · Doug DC862 · Fuselage Main, Plate/Skin
  > DURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATIONS 1120 TO 1160, LONGERON 31 RIGHT. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERN
- [SDR IXXA9800041](https://openairdocs.org/sdr/IXXA9800041.md): Frame · corroded · Nov 19, 1997 · N728PL · Doug DC862 · Fuselage Main, Frame
  > DURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE FRAME AT FUSELAGE STATION 133 LONGERON 21 RIGHT. REPAIR ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF TWO NESTED ANGLE REPAIR DOUBLERS IN ACCORDANCE WITH FAA PER APPRO
- [SDR IXXA9800024](https://openairdocs.org/sdr/IXXA9800024.md): Bulkhead Panel · cracked · Nov 19, 1997 · N728PL · Doug DC862 · Fuselage Main, Bulkhead
  > DURING ROUTINE D-CHECK INSPECTION, A CRACK WAS FOUND ON THE PRESSURE BULKHEAD PANEL BETWEEN FUSELAGE STATIONS 133 AND 148. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF FILLER, NESTED ANGLE DOUBLERS AND FINGER DOUBLER IN ACCO
- [SDR IXXA980014](https://openairdocs.org/sdr/IXXA980014.md): Access Panel · corroded · Nov 7, 1997 · N728PL · Doug DC862 · Wing, Plate/Skin
  > DURING ROUTINE D CHECK INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING LEADING EDGE ACCESS PANEL LAND AT STATION XFS 361. REPAIR ACCOMPLISHED REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND TWO REPAIR DOUBLERS AND THIPLERS IN

Next page: https://openairdocs.org/deregistered/N728PL-2014-01-07/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 = 'N728PL' AND deregistration_id = 'N728PL-2014-01-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N728PL-2014-01-07/reports

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