# Service difficulty reports: N308AS, cancelled Feb 13, 2018

A list on [N308AS, cancelled Feb 13, 2018](https://openairdocs.org/deregistered/N308AS-2018-02-13.md).

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

- [SDR C8GA2011000002](https://openairdocs.org/sdr/C8GA2011000002.md): Roller · missing · Apr 22, 2011 · N308AS · Boeing 727227 · Flight Compartment Windows
  > FLT 1112-DURING CLIMB OPERATION OUT OF CLT WHEN PASSING THROUGH 12,000 MSL, A WHITE OPAQUE SUBSTANCE BEGAN TO APPEAR ON THE FIRST OFFICERS WINDOW FOLLOWED BY A HIGH PITCH SOUND. THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPE
- [SDR C8GA2010000080](https://openairdocs.org/sdr/C8GA2010000080.md): Duct · cracked · Dec 22, 2010 · N308AS · Boeing 727227 · Airfoil Anti/De-ice System
  > SHORTLY AFTER TAKEOFF FROM WHEN THE WING ANTI-ICE WAS TURNED ON, A LOUD POP WAS HEARD FOLLOWED BY A SPIKE IN THE ACFT PRESSURIZATION AND THE LOWER AFTER BODY HEAT LIGHT ILLUMINATED. ACFT DIVERTED AND MADE AN UNSCHEDULED LANDING WITHOUT INCIDENT. MX FOUND THE
- [SDR C8GA2010000079](https://openairdocs.org/sdr/C8GA2010000079.md): Warning Light · illuminated · Dec 15, 2010 · N308AS · Boeing 727227 · Landing Gear Position and Warning
  > ON TAKEOFF, THE RED "GEAR DOOR" LIGHT ON THE FWD PANEL REMAINED ILLUMINATED. SYS FOUND TO BE PERVIOUSLY DEFERRED IAW MEL 32-1, ACFT RETURNED TO SERVICE.
- [SDR C8GA2010000078](https://openairdocs.org/sdr/C8GA2010000078.md): Circuit Breaker · popped · Dec 15, 2010 · N308AS · Boeing 727227 · Engine Indicating System
  > ON TAKE-OFF, WHILE DOING A ROLLING POWER CHECK, ENGINE NR 1 AND NR 3 EPR GAUGES FAILED TO COME UP. ABORTED TAKE-OFF AT LOW SPEED AND TAXIED BACK TO THE RAMP. MX FOUND CIRCUIT BREAKERS POPPED, RESET BREAKERS, RAN ENGINES. OPS CHECK GOOD IAW MM 77-11-00, ACFT R
- [SDR C8GA2010000076](https://openairdocs.org/sdr/C8GA2010000076.md): Connector · damaged · Nov 23, 2010 · N308AS · Boeing 727227 · Landing Gear System Wiring
  > ON APPROACH, THE NLG DID NOT INDICATE GREEN. LIGHT REMAINED RED, ALL 3 LANDING GEAR WERE MANUALLY EXTENDED. ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. R & R THE NLG POSITION SWITCH, R & R NLG LOCK SWITCH CONNECTOR PLUG, REPLACED 2 EACH WIR
- [SDR C8GA2010000055](https://openairdocs.org/sdr/C8GA2010000055.md): Switch · inoperative · Oct 5, 2010 · N308AS · Boeing 727227 · Door Warning System
  > DURING CLIMB OPS THE AFT AIR-STAIR GREEN LIGHT ILLUMINATED. ACFT RETURNED, WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, THE TREAD LIGHT SWITCH WAS DETERMINED TO BE AT FAULT. ITEM WAS DEFERRED AND ACFT WAS RETURNED TO SERVICE. NO OTHER
- [SDR C8GA201000054](https://openairdocs.org/sdr/C8GA201000054.md): Strap · corroded · Sep 10, 2010 · N308AS · Boeing 727227 · Wing, Control Surfaces
  > DURING HEAVY MX INSP THE INTERNAL STRAP IS CRACKED AT AFT EDGE OF RT WING INBD MID-FLAP UPPER FLAP CARRIAGE ACCESS PANEL NR 8543 W BL 124.2. REMOVED DAMAGED STRAP FABRICATED NEW STRAP FROM 2024 T3.063". INSTALLED NEW STRAP. NO OTHER DEFECTS NOTED, ACFT WAS R
- [SDR C8GA201000053](https://openairdocs.org/sdr/C8GA201000053.md): Access Panel · corroded · Sep 10, 2010 · N308AS · Boeing 727227 · Wing, Plate/Skin
  > DURING HEAVY MX INSP THE LT FUEL TANK ACCESS PLATE (7340) WAS CORRODED. REMOVED AND REPLACED ACCESS PLATE. NO OTHER DEFECTS NOTED, ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA201000052](https://openairdocs.org/sdr/C8GA201000052.md): Intercostal · corroded · Sep 10, 2010 · N308AS · Boeing 727227 · Fuselage Miscellaneous Structure
  > "SUPPLEMENTAL INFORMATION" DURING HEAVY MX INSP THE FWD CARGO BILGE INTERCOSTAL OUTER CHORD IS CORRODED AT STA 684 LBL13. FABRICATED NEW WEB FROM 7075-0.050" HEAT TREATED TO T6. INSTALLED REPAIR PART, NO OTHER DEFECTS NOTED, ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA201000051](https://openairdocs.org/sdr/C8GA201000051.md): Shear Tie · cracked · Sep 10, 2010 · N308AS · Boeing 727227 · Fuselage Internal Mounting Structure
  > "SUPPLEMENTAL INFORMATION" DURING HEAVY MX INSP THE FWD CARGO FRAME SHEAR TIE WAS FOUND TO BE CRACKED AT STA 520 BETWEEN STRINGER 25-26R. FABRICATED NEW SHEAR TIE FROM BAC1505-100471 7075 T6 DIM 6.25" X 2". INSTALLED SHEAR TIE, NO OTHER DEFECTS NOTED, ACFT WA
- [SDR C8GA201000050](https://openairdocs.org/sdr/C8GA201000050.md): Rib · cracked · Sep 10, 2010 · N308AS · Boeing 727227 · Ailerons
  > "SUPPLEMENTAL INFORMATION" DURING HEAVY MX INSP THE LT OTBD AILERON, L/E INBD END NOSE RIB CRACKED. REMOVED FABRICATED AND INSTALLED END NOSE RIB. NO OTHER DEFECTS NOTED, ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA201000049](https://openairdocs.org/sdr/C8GA201000049.md): Skin · dented · Sep 10, 2010 · N308AS · Boeing 727227 · Fuselage Main, Plate/Skin
  > DURING HEAVY MX INSP, A DENT WAS FOUND AT BS 420 STRINGER 4L. REMOVED DAMAGED AREA 3" 1.1250", FABRICATED DOUBLER FROM 7075-0.063" DIM 12" X 3" HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFECTS NOTED, ACFT WAS RETURNED TO SERVICE.
- [SDR C8GA201000048](https://openairdocs.org/sdr/C8GA201000048.md): Skin · gouged · Sep 10, 2010 · N308AS · Boeing 727227 · Nacelle/Pylon, Plate/Skin
  > "SUPPLEMENTAL INFORMATION" DURING HEAVY MX INSPECTION THE RIGHT ENGINE PYLON AFT ENGINE MOUNT SIDE SKIN STRUCTURE WAS FOUND TO BE DAMAGED. FABRICATED NEW SKIN FROM 2024 T3.040" DIM. 8" X 3" AND INSTALLED REPAIR. NO OTHER DEFECTS NOTED, ACFT WAS RETURNED TO SE
- [SDR ABXR201002010001](https://openairdocs.org/sdr/ABXR201002010001.md): Skin · torn · Feb 1, 2010 · N308AS · Boeing 727227 · Wing, Plate/Skin
  > WHILE ACCOMPLISHING ROUTINE SCHEDULED MX, THE LT WING-TIP WAS FOUND TO HAVE A TEAR OUT IN THE AREA OF THE AFT LOWER MOUNTING FASTENER HOLE. CUT DAMAGED AREA OUT AND PERFORMED HFEC TO ENSURE DAMAGE WAS REMOVED IAW NDT MANUAL PART 6 51-00-00 FIG. 23. REPAIR IN
- [SDR C8GA2009133](https://openairdocs.org/sdr/C8GA2009133.md): Rod · broken · Jul 22, 2009 · N308AS · Boeing 727227 · Landing Gear Steering System
  > FLT 712. LANDING IN SAN ACFT DEVELOPED A VIOLENT UNCONTROLLABLE NOSE WHEEL SHIMMY. ACFT SLOWED TO DISCOVER A LOSS OF NLG STEERING. POST FLT INSPECTION PERFORMED, NOTED THE TORSION LINK PIN WAS NOT INSTALLED IN THE LINKS & THE NLG LIGHT CONDUIT WRAPPED AROUND
- [SDR C8G2008F00016](https://openairdocs.org/sdr/C8G2008F00016.md): Line · leaking · Aug 26, 2008 · N308AS · Boeing 727227 · Engine Fuel Distribution
  > ON ROTATION THE NR 3 ENGINE FAILED. THE CREW PERFORMED APPROPRIATE CHECKLIST. AN EMERGENCY WAS DECLARED AND THE AC RETURNED WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, IT WAS NOTED THAT THE FUEL FEED LINE TO THE P & D VALVE WAS LEAKING. T
- [SDR C8G2008F00009](https://openairdocs.org/sdr/C8G2008F00009.md): Connector · dirty · Aug 5, 2008 · N308AS · Boeing 727227 · Flight Control System Wiring
  > AFTER TAKEOFF, DURING CLIMB, OPERATION, THE NR 8 SLAT WOULD NOT RETRACT. POST FLIGHT INSP WAS PERFORMED AND THE NR 8 SLAT ACTUATOR CONNECTOR WAS CLEANED AND SYSTEM WAS OPERATIONAL CHECKED WITH NO DEFECTS. NO OTHER DEFECTS WERE NOTED. AC WAS RETURNED TO SERVI
- [SDR G8GA20080006](https://openairdocs.org/sdr/G8GA20080006.md): Actuator · malfunctioned · Feb 15, 2008 · N308AS · Boeing 727227 · Leading Edge Slat Actuator
  > FLT 715 FROM HRL TO MEM. DURING CLIMB OPERATION ON FLAP RETRACTION THE NR 2 LEADING EDGE SLAT WOULD NOT RETRACT. CREW PERFORM REQUIRED PROCEDURES AND RETURNED TO HRL WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 SLAT ACTUATOR WAS REMOVED AND REPLACED, OPS AND L
- [SDR C8GA20080005](https://openairdocs.org/sdr/C8GA20080005.md): Actuator · leaking · Feb 8, 2008 · N308AS · Boeing 727227 · Leading Edge Slat Actuator
  > FLT 707 FROM PHX TO MCI - AFTER LANDING AND DURING TAXI, A NOTICEABLE STIFFENING IN THE NOSE STEERING, FOLLOWED BY THE ILLUMINATION OF THE "A" SYSTEM HYDRAULIC LIGHT AND LOW HYDRAULIC FLUID QUANTITY OCCURRED. POST FLIGHT INSPECTION REVEALED THAT THE NR 2 SLAT
- [SDR C8GA20070006](https://openairdocs.org/sdr/C8GA20070006.md): Connector · loose · Jun 8, 2007 · N308AS · Boeing 727227 · Engine Oil System Wiring
  > FLT 716 FROM TOL TO MEM, AFTER TAKEOFF, NR 2 ENGINE OIL TEMPERATURE PEGGED HIGH. CREW PERFORMED PRECAUTIONARY ENGINE SHUT DOWN, DECLARED EMERGENCY, AND RETURNED TO TOL. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND OIL TEMP BULB CONNECTOR BACK
- [SDR C8GA20060005](https://openairdocs.org/sdr/C8GA20060005.md): Quick Disconnect · disconnected · Mar 15, 2006 · N308AS · Boeing 727227 · Outside Air Temperature Indicator/Sensor
  > FLT 716 FROM TOL TO MEM. DURING TAKEOFF, CAPTAINS AIR SPEED INDICATOR FROZE AT 70 KNOTS. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. FOUND CAPTAINS MACH AIRSPEED INDICATOR QUICK DISCONNECT NOT FULLY ENGAGED. RESECURED QUICK DISCONNE
- [SDR C8GA20050014](https://openairdocs.org/sdr/C8GA20050014.md): Fcu · contaminated · Jun 2, 2005 · N308AS · Boeing 727227 · Fuel Control/Turbine Engines
  > FLT 722 FROM TOL TO RDU. IN CRUISE AT FL310, CREW NOTED POWER LOSS OF NR 2 ENGINE ACCOMPANIED BY EPR FLUXUATION, COMPRESSOR STALL, AND VIBRATION. CREW REDUCED POWER SETTING TO IDLE AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO TOL A
- [SDR C8GA20050010](https://openairdocs.org/sdr/C8GA20050010.md): Motor · leaking · Apr 15, 2005 · N308AS · Boeing 727227 · Trailing Edge Flap Actuator
  > FLT 712 FROM TOL TO DEN. 10 MINUTES AFTER TAKE OFF AT FL190, CREW NOTICED LOSS OF SYSTEM A-HYDRAULIC FLUID FOLLOWED BY ILLUMINATION OF HYDRAULIC LOW PRESSURE LIGHTS. CREW DUMPED 600 LBS OF FUEL, RETURNED TO TOL, AND LANDED WITHOUT INCIDENT. FOUND RT OUTBOARD
- [SDR C8GA20050003](https://openairdocs.org/sdr/C8GA20050003.md): Isolation Valve · malfunctioned · Jan 19, 2005 · N308AS · Boeing 727227 · Cabin Pressure Control System
  > FLT 712 FROM TOL TO DEN, IN CRUISE AT 31000 FEET, AIRCRAFT RAPIDLY DEPRESSURIZED. CREW EMERGENCY DESCENDED TO 14000 FEET AND STABILIZED PRESSURE AT 5 PSID. AIRCRAFT CONTINUED TO DEN AND LANDED WITHOUT INCIDENT. SWAPPED ENGINE BLEED VALVES WITH NR 2 ISOLATIO
- [SDR C8GA20030011](https://openairdocs.org/sdr/C8GA20030011.md): Warning Light · illuminated · Apr 30, 2003 · N308AS · Boeing 727227 · Engine Oil Indicating System
  > FLIGHT 201 FROM MIA TO PTY. ABORTED TAKE OFF ROLL DUE TO NR 2 AND 3 ENGINE OIL BYPASS LIGHT CAME ON AT 90 KNOTS. AIRCRAFT RETURNED TO BLOCKS WITHOUT INCIDENT. REMOVED AND INSPECTED NR 2 AND 3 ENGINE OIL FILTERS, BOTH FILTERS WERE FOUND TO BE CLEAN. INSTALLED N
- [SDR C8GA20020009](https://openairdocs.org/sdr/C8GA20020009.md): Duct · blown · Jul 23, 2002 · N308AS · Boeing 727227 · Cabin Pressure Control System
  > Flt CCI723 from KBOS to KROS. After take off, in climb, @ FL250 and 280 knots, aircraft started to vibrate. reduced speed to 250 knots then heard 2 bangs from behind the Flight Engineer station. After second bang, aircraft would not maintain pressurization.
- [SDR C8GA20020008](https://openairdocs.org/sdr/C8GA20020008.md): Warning System · malfunctioned · Jul 9, 2002 · N308AS · Boeing 727227 · Landing Gear Position and Warning
  > FLT 713 FROM SAN TO DEN. ON APPROACH TO DEN, LEFT MAIN GEAR INDICATE UNSAFE BOTH INSTRUMENT PANEL AND SECONDARY. CYCLED GEAR, NO LUCK. EXECUTED GO-AROUND THEN CYCLED GEAR AND GOT GOOD INDICATIONS AND LANDED WITHOUT INCIDENT. INSPECT THE MAIN GEAR ASSEMBLY
- [SDR C8GA20010006](https://openairdocs.org/sdr/C8GA20010006.md): Bearing · loose · Apr 12, 2001 · N308AS · Boeing 727227 · Flight Compartment Windows
  > FLT EB941 FROM MSY TO MCI. AFTER TAKEOFF, CREW HEARD A LOUD SQUEAL FROM THE R2 WINDOW. AIRCRAFT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. FOUND THE R2 WINDOW AFT TRACK LOWER ROLLER BEARING LOOSE. RESECURED BEARING. OPS AND LEAK CHECK GOOD. AIRCRAFT RE
- [SDR C8GA20010003](https://openairdocs.org/sdr/C8GA20010003.md): Sliding Window · cracked · Feb 18, 2001 · N308AS · Boeing 727227 · Flight Compartment Windows
  > FLIGHT 399 FROM KBWI TO KDAY AT FL 330 CO-PILOTS SLIDING WINDOW OUTER PANE EXPERIENCED MULTIPLE CRACKS EMANATING FROM FWD LWR CORNER. AIRCRAFT DESCENDED TO FL 010 AND DEPRESSURIZED CABIN. AIR TURNBACK TO KBWI WITH NO FURTHER INCIDENTS.
- [SDR C8GA20000016](https://openairdocs.org/sdr/C8GA20000016.md): Lead · chafed · Dec 20, 2000 · N308AS · Boeing 727227 · Fire Detection
  > ENGINE NUMBER 3 FIRE WARNING INDICATION OCCURRED DURING LANDING ROLLOUT AT CLT. NUMBER 3 FIRE HANDLE PULLED, LEFT FIRE BOTTLE DISCHARGED AND APPROXIMATELY 15 SECONDS LATER THE FIRE HANDLE LIGHT WENT AND THE BELL SILENCED. *S/D* REPLACED GENERATOR FEEDER CAB
- [SDR 8GA200000002](https://openairdocs.org/sdr/8GA200000002.md): Hydraulic System · leaking · Apr 27, 2000 · N308AS · Boeing 727227 · Hydraulic System, Main
  > FLT 033 FROM KELP TO KDAY, AFTER TAKEOFF DURING CLIMB TO CRUISE ALTITUDE, FLIGHT CREW OBSERVED STEADY AND CONTINUAL LOSS OF SYSTEM A HYDRAULIC FLUID TO BELOW 2.4 GALLONS FLUID QUANTITY. RETURNED TO KELP AND LANDED WITHOUT FURTHER INCIDENT. CHECKED AIRCRAFT H
- [SDR 99ZZZM802](https://openairdocs.org/sdr/99ZZZM802.md): Module · defective · Oct 19, 1999 · N308AS · Boeing 727227 · Landing Gear Position and Warning
  > FLT 127 KOKC-KDAY - AFTER TAKEOFF AND UPON PLACING GEAR HANDLE IN UP POSITION LEFT MLG SHOWED GREEN AND RED LIGHTS ON CENTER PANEL. SECONDARY LIGHTS EXTINGUISHED. CYCLED GEAR HANDLE TO OFF, LIGHTS REMAINED GREEN AND RED. CYCLED GEAR HANDLE TO DOWN SAFE IND
- [SDR 99ZZZM119](https://openairdocs.org/sdr/99ZZZM119.md): Retract Mech · jammed · Dec 31, 1998 · N308AS · Boeing 727227 · Trailing Edge Flap Control System
  > FLT 504 - DDAY-KSAN - AFTER TAKEOFF, OUTBOARD FLAP WOULD NOT RETRACT BEYOND 5 DEGREES. SEVERAL ATTEMPTS TO RETRACT TO 0 DEGREES FAILED. AIRCRAFT RETURNED TO KDAY AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED AND PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM.
- [SDR EISA98243](https://openairdocs.org/sdr/EISA98243.md): Igniter Box · failed · Sep 30, 1998 · N308AS · Boeing 727227 · Exciter
  > NR 1 ENGINE FLAMED OUT IN FLIGHT. UNABLE TO RESTART. AIR TURN BACK TO BGY. REMOVED AND REPLACED IGNITOR BOX, FUEL CONTROL. FUEL PUMP, RAN ENGINE AND TRIMMED. CHECKS NORMAL. (M)
- [SDR 98ZZZM824](https://openairdocs.org/sdr/98ZZZM824.md): Igniter Box · failed · Sep 30, 1998 · N308AS · Boeing 727227 · Fuel Boost Pump
  > NR 1 ENGINE FLAMED OUT IN FLIGHT. UNABLE TO RESTART. AIR TURN BACK TO BGY. REMOVED AND REPLACED IGNITOR BOX, FUEL CONTROL. FUEL PUMP, RAN ENGINE AND TRIMMED. CHECKS NORMAL. (M)
- [SDR 98ZZZM823](https://openairdocs.org/sdr/98ZZZM823.md): Fuel Control · failed · Sep 30, 1998 · N308AS · Boeing 727227 · APU Engine Fuel and Control
  > NR 1 ENGINE FLAMED OUT IN FLIGHT. UNABLE TO RESTART. AIR TURN BACK TO BGY. REMOVED AND REPLACED IGNITOR BOX, FUEL CONTROL. FUEL PUMP, RAN ENGINE AND TRIMMED. CHECKS NORMAL. (M)
- [SDR EISA98142](https://openairdocs.org/sdr/EISA98142.md): Stick Shaker · malfunctioned · Jun 18, 1998 · N308AS · Boeing 727227 · Stall Warning System
  > DURING TAKEOFF ROLL, STICK SHAKER ACTIVATED. DISCONTINUED TAKEOFF AT 70 KNOTS. GENERATED FROM PILOT REPORT. OPS CHECKED STALL WARNING IAW BMM CHAPTER 34-18-01, PAGES 502 THROUGH 504. NO DEFECTS NOTED. (X)
- [SDR EISA98069](https://openairdocs.org/sdr/EISA98069.md): Compass Rack · inop · Apr 5, 1998 · N308AS · Boeing 727227 · Integrated Flight System
  > DEPARTING BRUSSELS CAPTAINS HSI HAS COMPASS FLAG IN VIEW AND CO-PILOT RMI OFF FLAG IN VIEW. AIR TURNBACK TO BRUSSELS. GENERATED FROM PILORT REPORT. REMOVED AND REPLACED NR 1 COMPASS RACK IAW MM 34-00. OPS CHECK NORMAL. (M)
- [SDR 98ZZZX1474](https://openairdocs.org/sdr/98ZZZX1474.md): Compass · failed · Apr 5, 1998 · N308AS · Boeing 727227 · Integrated Flight System
  > CAPTAIN'S HSI HAS COMPASS FLAG. COPILOT'S RMI OFF FLAG IN VIEW. REMOVED AND REPLACED NR 1 COMPASS.
- [SDR EISA97109](https://openairdocs.org/sdr/EISA97109.md): Epr Indicator · failed · May 16, 1997 · N308AS · Boeing 727227 · Engine Pressure Ratio (EPR)
  > ON TAKEOFF, EPR NR 3 ROSE TO 2.9 WITH NORMAL N1. NR 1 AND NR 2 NORMAL INDICATION. REMOVED AND REPLACED INDICATOR. OPS CHECK GOOD. (M)
- [SDR EISA97003](https://openairdocs.org/sdr/EISA97003.md): Switch · inoperative · Jan 13, 1997 · N308AS · Boeing 727227 · Landing Gear Position and Warning
  > NOSE GEAR POSITION LIGHT ILLUMINATES WITH GEAR UP. REPLACED NOSE GEAR POSITION SWITCH PERFORMED LANDING GEAR, OPS CHECK OPS GOOD. (M)
- [SDR EISA97002](https://openairdocs.org/sdr/EISA97002.md): Switch · loose · Jan 12, 1997 · N308AS · Boeing 727227 · Landing Gear Position and Warning
  > AFTER RETRACTING GEAR, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CLEANED AND RESEALED CONNECTORS ON BOTH NOSE GEAR LOCK SWITCH AND NOSE GEAR POSITION SWITCH, OPERATIONAL TESTED PER MM 32-62-71 PAGE 501. (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 = 'N308AS' AND deregistration_id = 'N308AS-2018-02-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N308AS-2018-02-13/reports

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