# Service difficulty reports: N801NK, cancelled Jun 16, 2005

A list on [N801NK, cancelled Jun 16, 2005](https://openairdocs.org/deregistered/N801NK-2005-06-16.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 · 150 reports

- [SDR GTIA040794](https://openairdocs.org/sdr/GTIA040794.md): Slide · unsecure · Oct 2, 2004 · N801NK · Doug DC982 · Escape Slide
  > L1 SLIDE PACK CAME OFF DOOR. RESECURED SLIDE PACK.
- [SDR GTIA040789](https://openairdocs.org/sdr/GTIA040789.md): Strut · damaged · Sep 27, 2004 · N801NK · Doug DC982 · Main Landing Gear Strut/Axle/Truck
  > ACY - FLT 1174 - AFTER TAKEOFF FELT RUMBLE WHICH FELT LIKE NOSE GEAR DOOR NOT CLOSING. RECYCLED NOSE GEAR AND UNSAFE LIGHT ILLUMINATED. PER MNCTL DIRECTION, RECYCLED GEAR AGAIN, LIGHT CAME ON AND THEN WENT OUT. CONTINUED FLIGHT. SERVICED NOSE STRUT. ALL O
- [SDR GTIA040799](https://openairdocs.org/sdr/GTIA040799.md): Turbine Blades · loose · Sep 21, 2004 · N801NK · Doug DC982 · Turbine Section
  > DURING NOTCH CK IW SB A6224, TABLE 3, FOUND MORE THAN ONE - 4TH STAGE BLADES WITH LESS THAN OR EQUAL TO 5 IN LBS (6 BLADES LOOSE). REPLACED WITHIN 20 HOURS OR CYCLES. REMOVED AND REPLACED ENGINE.
- [SDR GTIA040705](https://openairdocs.org/sdr/GTIA040705.md): Warning Light · illuminated · Aug 5, 2004 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > TPA - FLT 642 - RIGHT GEAR LIGHT 'RED' STAYS ON AFTER GEAR IS UP. NO GEAR DOOR OPEN LIGHT RECYCLE GEAR ALL NORMAL. SEE LOG PGS 291781-1N 2, 3 AND 291782-1, 2 AND 3 FOR FINDING AND CORRECTIONS. CYCLED MAIN GEAR SEVERAL TIMES. NO DISCREPANCY NOTED. GEAR PIN
- [SDR GTIA040704](https://openairdocs.org/sdr/GTIA040704.md): Rod · out of adjust · Aug 4, 2004 · N801NK · Doug DC982 · Landing Gear Door Retract Section
  > AFTER GEAR RETRACTION RT MAIN RED INDICATOR LIGHT STAYED ON 15 SECOND LONGER THAN THE OTHER GEAR INDICATOR LIGHTS. RT HYD PRESSURE MOMENTARILY DROPPED TO 1500 PSI. ALL PUMPS ON HI/ON CRUISE ALT, FL 350, WHEN LEVELING OFF THE GEAR DOOR OPEN LIGHT FLICKERED ON
- [SDR GTIA040698](https://openairdocs.org/sdr/GTIA040698.md): Position Switch · malfunctioned · Jul 31, 2004 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > RIGHT RED GEAR UP AND LOCK LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. RECYCLED GEAR PER QRH. LIGHT WENT OUT ABOUT 45 SECONDS AFTER RETRACTION. LUBRICATED RT MAIN GEAR UPLOCK MECH. REMOVED AND REPLACED RT MLG POSITION SWITCH. REMOVED AND REPLACED SENS
- [SDR GTIA040695](https://openairdocs.org/sdr/GTIA040695.md): Uplock Sensor · malfunctioned · Jul 29, 2004 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > THE RIGHT RED GEAR UNSAFE LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE AMBER GEAR DOOR OPEN LIGHT CAME ON WHEN HYDRAULIC PUMPS WERE SELECTED TO LOW PSI. CHECKED HYD PLUMBING, GEAR, DOOR MECH'S. ON RIGHT GEAR NO DEFECTS NOTED. REMOVED AND REPLACED TR
- [SDR GTIA040699](https://openairdocs.org/sdr/GTIA040699.md): Uplock Sensor · malfunctioned · Jul 29, 2004 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > THE RIGHT RED GEAR UNSAFE LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE AMBER GEAR DOOR OPEN LIGHT CAME ON WHEN HYD PUMPS WERE SELECTED TO LOW PSI. CHECKED HYD PUMPING, GEAR AND DOOR MECH ON RIGHT GEAR. NO DEFECTS NOTED REMOVED AND REPLACED RIGHT GEAR
- [SDR GTIA040659](https://openairdocs.org/sdr/GTIA040659.md): Latch · dirty · Jul 13, 2004 · N801NK · Doug DC982 · Escape Slide
  > R1 GIRT BAR SPRING LOADED LATCHES HAVE TO BE MANUALLY MANIPULATED TO LOCK GIRT BAR IN PLACE. CLEANED AND LUBED R1 DOOR GIRT BAR LATCHES. OPS CHECK GOOD. (M)
- [SDR GTIA040585](https://openairdocs.org/sdr/GTIA040585.md): Slide · dislodged · Jun 19, 2004 · N801NK · Doug DC982 · Escape Slide
  > RSW - FLT 670 - FOUND FORWARD CABIN SLIDE PACK FELL OUT. REINSTLALED L1 SLIDE PACK ASSEMBLY. (M)
- [SDR GTIA040465](https://openairdocs.org/sdr/GTIA040465.md): Proximity Sensor · inoperative · May 17, 2004 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > RT MLG UNSAFE LIGHT ON AFTER GEAR RETRACTION. RECYCLE GEAR. LIGHT OUT. REMOVED AND REPLACED MLG UPLOCK PROXIMITY SENSOR. OPS CHECK NORMAL.
- [SDR GTIA040463](https://openairdocs.org/sdr/GTIA040463.md): Proximity Switch · inoperative · May 14, 2004 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > GEAR DOOR OPEN LIGHT ILLUMINATED. DURING CRUISE. EXT AFTER 30 MIN. ADJ. RT AND LT DOOR PROXIMITY SWITCHES. OPS CHECK GOOD WITH GEAR SWING. MONITIORED DOOR LIGHT WITH NO PRESSURE AND GEAR UP. ALL INDICATIONS NORMAL.
- [SDR GTIA040450](https://openairdocs.org/sdr/GTIA040450.md): Proximity Switch · inoperative · May 11, 2004 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > ON TAKEOFF, GEAR RETRACTION RT MAIN GEAR UNSAFE LIGHT, RECYCLED GEAR LIGHT WENT OUT. ON CLEANED RT MAIN PROXIMITY SWITCH. PERFORMED PROXIMITY BOX CHECK SYSTEM OPS CHECK.
- [SDR GTIA040440](https://openairdocs.org/sdr/GTIA040440.md): Warning Light · illuminated · May 8, 2004 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > AFTER T/O NOSE GEAR UNSAFE LIGHT ON FOLLOWED QRH AND LANDED. PERFORMED NOSE GEAR EXTENSION AND RETRACTION OPERATIONAL CK. OPS CK OK.
- [SDR GTIA040337](https://openairdocs.org/sdr/GTIA040337.md): Support · broken · Apr 23, 2004 · N801NK · Doug DC982 · Fuselage Main, Attach Fittings
  > DTW - FOUND AFT GALLEY SERVICE DOOR, ONE GIRT BAR SUPPORT TAB BROKEN. INSTALLED NEW GIRT BAR SUPPORT TAB ON AFT GALLEY SERVICE DOOR. (M)
- [SDR GTIA040333](https://openairdocs.org/sdr/GTIA040333.md): Connector · loose · Apr 15, 2004 · N801NK · Doug DC982 · Electrical Connectors
  > FOUND TAIL COMPARTMENT EMERGENCY EXIT IDENTIFIER IS NOT LIGHT ON TEST. SECURED CONNECTOR, OPS CHECK. (M)
- [SDR GTIA040273](https://openairdocs.org/sdr/GTIA040273.md): Cover · loose · Apr 9, 2004 · N801NK · Doug DC982 · Escape Slide
  > FLT 223 - ORD - FOUND L1 SLIDE PACK AND COVER CAME LOOSE FROM ENTRY DOOR. NO DAMAGE NOTED, REINSTALLED L1 SLIDE PACK AND COVER. (M)
- [SDR GTIA040259](https://openairdocs.org/sdr/GTIA040259.md): Lanyard · misrouted · Apr 1, 2004 · N801NK · Doug DC982 · Emergency Equipment
  > FLL - FOUND L1 DOOR ESCAPE SLIDE LANYARD IS ROUTED INCORRECTLY. REROUTED L1 DOOR ESCAPE SLIDE LANYARD. (M)
- [SDR GTIA040242](https://openairdocs.org/sdr/GTIA040242.md): Control Valve · defective · Mar 27, 2004 · N801NK · Doug DC982 · Landing Gear Selector
  > AFTER TAKEOFF RIGHT RED GEAR LIGHT STAYED ON. AMBER DOOR LIGHT WAS OUT, A/C PRESS NORMAL QRH PROCEDURE AFTER APPROX 10 MINUTES GEAR DOOR OPEN LIGHT CAME ON REF QRH. CABIN PRESS STILL NORMAL AFTER 20 MINUTES DOOR LIGHT OUT AT 1200 FT AND 260 KNOTS RED GEAR LI
- [SDR GTIA040243](https://openairdocs.org/sdr/GTIA040243.md): Slide · out of position · Mar 26, 2004 · N801NK · Doug DC982 · Escape Slide
  > LGA - FLT 1174 - L1 DOOR SLIDE PACK FELL OFF OF DOOR WHEN DOOR WAS CLOSED. REINSTALLED FORWARD CABIN DOOR SLIDE ASSEMBLY AND COVER. (M)
- [SDR GTIA040219](https://openairdocs.org/sdr/GTIA040219.md): Proximity Switch · faulty · Mar 23, 2004 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > FTW - FOUND DOOR MLG LIGHT CAME ON DURING CLIMB FOR APPROX 2 MINUTES STAYED OFF THE REST OF FLIGHT. FOUND LEFT MAIN GEAR DOOR PROX SWITCH D1-30. REMOVED AND REPLACED LEFT MAIN GEAR OPEN PROX SWITCH, OPS CHECK GOOD. (M)
- [SDR GTIA040252](https://openairdocs.org/sdr/GTIA040252.md): Clip · corroded · Feb 24, 2004 · N801NK · Doug DC982 · Fuselage Miscellaneous Structure
  > FTW - FOUND MID PIT JAM BEAM FORWARD END CLIP CORRODED AT FS 598 AROUND FASTENER. FABRICATED MID PIT JAM BEAM FORWARD END CLIP. (M)
- [SDR GTIA040212](https://openairdocs.org/sdr/GTIA040212.md): Longeron · corroded · Feb 24, 2004 · N801NK · Doug DC982 · Fuselage Main, Longeron/Stringer
  > FTW - FOUND MIDPIT LONGERON 30 CORRODED AT FS 664 AROUND FASTENER HOLE. REMOVED LONGERON SECTION L30 FROM STATION 585-665. FABRICATED LONGERON. LONGERON REPAIR PER SPIRIT EA 5310-0403. INSTALLED LONGERON, INSTALLED SPLICE AT STATION 665. (M)
- [SDR GTIA040231](https://openairdocs.org/sdr/GTIA040231.md): Longeron · corroded · Feb 24, 2004 · N801NK · Doug DC982 · Fuselage Main, Longeron/Stringer
  > FTW - FOUND MIDPIT LONGERON 28R CORRODED AT FS 617 AROUND FASTENER HOLE. REMOVED LONGERON 28R STATION 588 TO 628. FABRICATED LONGERON. INSTALLED LONGERON. (M)
- [SDR GTIA040172](https://openairdocs.org/sdr/GTIA040172.md): Floorboard · damaged · Feb 21, 2004 · N801NK · Doug DC982 · Fuselage Floor Panel
  > FTW - FOUND MAIN CABIN FLOORBOARD FS 200-256 LEFT INBOARD CENTER HAS MISSING AND DAMAGED INSERTS AND DAMAGED ON END. FABRICATED NEW CABIN FLOORBOARD STATION 200-256. (M)
- [SDR GTIA040211](https://openairdocs.org/sdr/GTIA040211.md): Hook · cracked · Feb 19, 2004 · N801NK · Doug DC982 · Emergency Equipment
  > FTW - FOUND L2 DOOR HAS SEVERAL CRACKS AT SLIDE COVER AND LINER/GIRT BAR HOOK IS BROKEN. INSTALLED NEW GIRT BAR HOOK. (M)
- [SDR GTIA040227](https://openairdocs.org/sdr/GTIA040227.md): Doubler · corroded · Feb 19, 2004 · N801NK · Doug DC982 · Fuselage Main, Plate/Skin
  > FTW - FOUND LEFT ALTERNATE STATIC PORT INTERNAL DOUBLER CORRODED. REMOVED INTERNAL DOUBLER. LOCATED AND DRILLED NEW DOUBLER. INSTALLED INTERNAL DOUBLER. (M)
- [SDR GTIA040186](https://openairdocs.org/sdr/GTIA040186.md): Panel · cracked · Feb 19, 2004 · N801NK · Doug DC982 · Vertical Stabilizer, Plate/Skin
  > FTW - FOUND DORSAL FIN PANEL FORWARD 9 EACH FASTENER HOLES CRACKED, CHAFED, AND BROKEN OUT. FABRICATED DOUBLER. BLENDED OUT CRACKED AREAS. INSTALLED DOUBLER. (M)
- [SDR GTIA040185](https://openairdocs.org/sdr/GTIA040185.md): Door · cracked · Feb 17, 2004 · N801NK · Doug DC982 · Engine Thrust Reverser
  > FTW - FOUND RIGHT THRUST REVERSER UPPER DOOR INBOARD SIDE CRACKED AND BENT. REMOVED DOUBLER. STOP DRILLED END OF CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)
- [SDR GTIA040184](https://openairdocs.org/sdr/GTIA040184.md): Thrust Reverser · corroded · Feb 17, 2004 · N801NK · Doug DC982 · Engine Thrust Reverser
  > FTW - FOUND RIGHT THRUST REVERSER UPPER SIDE PITTED HEAVILY. FOUND CRACK IN THE TOP SIDE UPPER DOOR. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)
- [SDR GTIA040226](https://openairdocs.org/sdr/GTIA040226.md): Beam · corroded · Feb 16, 2004 · N801NK · Doug DC982 · Fuselage Main, Structure
  > FTW - FOUND MID PIT DOOR JAMB IS CORRODED STATION 636 TO 623 ON EDGE AND AROUND FASTENERS. REMOVED JAMB BEAM. DRILLED AND LOCATED NEW JAMB BEAM. INSTALLED JAMB BEAM. (M)
- [SDR GTIA040170](https://openairdocs.org/sdr/GTIA040170.md): Panel · corroded · Feb 16, 2004 · N801NK · Doug DC982 · Wing, Plate/Skin
  > FTW - FOUND LEFT WING PANEL 1163C SCRATCHED LIGHT SURFACE CORRODED. REMOVED CORROSION FROM LEFT PANEL 1163C. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M)
- [SDR GTIA040183](https://openairdocs.org/sdr/GTIA040183.md): Attach Angle · cracked · Feb 16, 2004 · N801NK · Doug DC982 · Vertical Stabilizer, Attach Fittings
  > FTW - FOUND RIGHT SIDE DORSAL FIN ATTACH ANGLE CRACKED THROUGH VERTICAL LEG AND INTO 1ST ROW OF FAST ON HORIZONTAL LEG AND GOUGED AND BROKEN FAST. DYE PEN INSPECTION SHOWS NO CRACKS. REMOVED RIGHT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHER INSPECTION FOUND R
- [SDR GTIA040182](https://openairdocs.org/sdr/GTIA040182.md): Attach Angle · cracked · Feb 16, 2004 · N801NK · Doug DC982 · Vertical Stabilizer, Attach Fittings
  > FTW - FOUND LEFT SIDE DORSAL FIN ATTACH ANGLE CRACKED AND GOUGED THROUGH VERTICAL LEG INTO 1ST ROW OF HORIZONTAL. REMOVAL LEFT SIDE DORSAL FIN ATTACH ANGLE. PER FURTHER INSPECTION FOUND INNER ATTACH ANGLE LEFT SIDE CRACKED SEVERAL PLACES. REMOVED LEFT INNER
- [SDR GTIA040187](https://openairdocs.org/sdr/GTIA040187.md): Nose Cowl · damaged · Feb 13, 2004 · N801NK · Doug DC982 · Turbine Engine Compressor Section
  > FTW - NR 2 NOSE COWL LIP RING HAS OVERHEAT INDICATIONS. MEASUREMENTS OBTAINED EXCEEDED UPPER LIMIT FOR 2024-T42 MATERIAL. NR 2 ENGINE NOSE COWL S/N 099-362. REMOVED AND REPLACED SAS WO B00127-11N-00001. (M)
- [SDR GTIA040032](https://openairdocs.org/sdr/GTIA040032.md): Slide · loose · Jan 26, 2004 · N801NK · Doug DC982 · Escape Slide
  > FLL - FLT 679 - L1 DOOR SLIDE NOT ATTACHED AT BOTTOM SIDE. REINSTALLED L1 DOOR SLIDE. (M)
- [SDR GTIA031039](https://openairdocs.org/sdr/GTIA031039.md): Controller · failed · Dec 11, 2003 · N801NK · Doug DC982 · Cabin Temperature Controller
  > AIRCRAFT WOULDN'T HOLD CABIN PRESSURE. CABIN WARNING VOICE FLOW LIGHT ON. LEFT VALVE TEMP FULL HOT (AUTO) REDUCED TEMP BOTH PACKS LEFT PACK ON 30 SEC FLOW LIGHT ON MASK DROPPED. MANUAL MODE ON OUTFLOW VALVE. PERFORMED TEST ON TEMP CONTROLLER SYSTEM WITH TES
- [SDR GTIA030864](https://openairdocs.org/sdr/GTIA030864.md): Slide · dislodged · Oct 24, 2003 · N801NK · Doug DC982 · Escape Slide
  > DTW - FOUND L1 DOOR SLIDE PACK FELL OFF. INSTALLED L1 DOOR EVACUATION SLIDE. NO DISCERPANCIES NOTED. (M)
- [SDR GTIA030713](https://openairdocs.org/sdr/GTIA030713.md): Slide · out of position · Sep 24, 2003 · N801NK · Doug DC982 · Escape Slide
  > LGA - FLT 705 - SLIDE PACK FELL OFF L-1. FORWARD ENTRY DOOR SLIDE PACK FELL OFF WHEN OPENING DOOR AT ARRIVAL GATE. GIRT BAR LATCH ON THE FLOOR IS VERY DIRTY AND STICKY. REINSTALLED L1 DOOR SLIDE AND CHECKED GIRT BAR LATCHES FOR OPERATION, OPS NORMAL. (M)
- [SDR GTIA030623](https://openairdocs.org/sdr/GTIA030623.md): Blade · damaged · Aug 9, 2003 · N801NK · Doug DC982 · Turbine Engine Compressor Section
  > ON PREFLIGHT INSPECTION, FOUND FOD DAMAGE TO THE NR 2 ENGINE C-1 BLADES. REMOVED AND REPLACED NR 2 ENGINE. (M)
- [SDR GTIA030486](https://openairdocs.org/sdr/GTIA030486.md): Line · leaking · Jun 27, 2003 · N801NK · Doug DC982 · Engine Oil Distribution (Airframe Furnished)
  > RT ENGINE WAS LOSING OIL PRESSURE AND QUANTITY. FOLLOWED QRH PROCEDURES SHUT DOWN ENGINE. OIL PRESSURE AT SHUTDOWN 30 PSI OIL TEMP AT SHUTDOWN 135 DEGREES, OIL QTY AT SHUTDOWN 5 QUARTS, OIL PRESSURE WINDMILLING 2 PSI, OIL QUANTITY WINDMILLING 4 QUARTS. FOUN
- [SDR GTIA030279](https://openairdocs.org/sdr/GTIA030279.md): Liner · damaged · Apr 28, 2003 · N801NK · Doug DC982 · Engine Air Intake System
  > NR 2 ENGINE INLET HAS TWO CUTS ON ACCOUSTIC LINING AT 4 AND 6 O`CLOCK POSITION. REPAIRED NR 2 ENGINE INLET ACCOUSTIC LINING. NO OTHER DEFECTS NOTED AT THIS TIME.
- [SDR GTIA040339](https://openairdocs.org/sdr/GTIA040339.md): Proximity Switch · inoperative · Apr 22, 2003 · N801NK · Doug DC982 · Landing Gear Position and Warning
  > MYR - FLT 1582 - RIGHT MAIN LANDING GEAR INDICATION ON DEPARTURE. QRH ACCOMPLISHED AND LANDING GEAR RECYCLED GEAR DOOR OPEN LIGHT INTERMITTENTLY ON WITH NO VIBRATION NOTED. RIGHT MLG LIGHT EXTINGUISHED WHEN REACHING 10000 FT ON DESCENT. TROUBLESHOT SYSTEM,
- [SDR GTIA021163](https://openairdocs.org/sdr/GTIA021163.md): Striker · defective · Nov 1, 2002 · N801NK · Doug DC982 · Leading Edge Slat Position Indicating System
  > ACY - FLT 311 - UPON SLAT RETRACT, THE SLAT DISAGREEMENT LIGHT CAME ON AND SLAT OVERSPEED WARNING IN FLIGHT. FOLLOWED QRH PROCEDURES RETURNED TO KACY THERE WAS NO ROLL ASYMMETRY, AIRCRAFT WAS STABLE IN FLIGHT. REMOVED AND REPLACED NR 4 SLAT DRIVE DISAGREE PR
- [SDR GTIA020889](https://openairdocs.org/sdr/GTIA020889.md): Wire · cut · Aug 3, 2002 · N801NK · Doug DC982 · Light System Wiring
  > FTW - FOUND ONE AFT STAIRWAY EMERGENCY LIGHT IS INOPERATIVE. TROUBLESHOT FOUND EMERGENCY LIGHT WIRES CUT AT SPLICE POINTS. RESPLICED WIRES. (M)
- [SDR GTIA020875](https://openairdocs.org/sdr/GTIA020875.md): Contactor · bent · Jul 30, 2002 · N801NK · Doug DC982 · Emergency Lighting
  > FTW - FOUND LEFT AND RIGHT OVERWING EXIT SIGNS INOPERATIVE, UPPER SIGNS ONLY. FOUND BATTERY PACK CONTACT BENT. REALIGNED CONTACT. (M)
- [SDR GTIA020846](https://openairdocs.org/sdr/GTIA020846.md): Blade · nicked · Jul 14, 2002 · N801NK · Doug DC982 · Turbine Engine Compressor Section
  > NR 1 ENGINE C1 FAN BLADES ARE ROUGH AND HAVE NICKS. NR 1, SN 718528, FAILED BORESCOPE INSPECTION, C-7 DISK 10 BLADES WITH NICKS AND MISSING MATERIAL. 2 BLADES DAMAGED NEAR TIP (1) MEASURES.140 INCH LONG (2) MEASURES.165 INCH LONG WITH A CRACK PROPAGATING
- [SDR GTIA020835](https://openairdocs.org/sdr/GTIA020835.md): Longeron · gouged · Jul 13, 2002 · N801NK · Doug DC982 · Fuselage Main, Longeron/Stringer
  > FTW - AFT ACCESSORY COMP GOUGE ON LONGERON 22L FLANGE, STATION 1380. FABRICATED REPAIR DOUBLER, INSTALLED DOUBLER. (M)
- [SDR GTIA020845](https://openairdocs.org/sdr/GTIA020845.md): Skin · damaged · Jul 11, 2002 · N801NK · Doug DC982 · Fuselage Main, Plate/Skin
  > FTW - FOUND STATION 546-552 BETWEEN LONGERON 17R AND 18R, 6 INCHES LONG CREASE IN FUSELAGE SKIN. CUT OUT DAMAGE. FORMED FINGER DOUBLER. FORMED SKIN DOUBLER. INSTALLED FINGER DOUBLER AND FILLER. (M)
- [SDR GTIA020851](https://openairdocs.org/sdr/GTIA020851.md): Skin · punctured · Jul 10, 2002 · N801NK · Doug DC982 · Rudder, Tab Structure
  > FTW - FOUND RUDDER TAB HAS PUNCTURE MARK (HOLE) APPROX.25 INCH DIAMETER 3 INCHES ABOVE FIXED TAB. RUDDER TRIM TAB FIXED TAB DEBONDED. THIS TAB REPLACED. (M)

Next page: https://openairdocs.org/deregistered/N801NK-2005-06-16/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 = 'N801NK' AND deregistration_id = 'N801NK-2005-06-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N801NK-2005-06-16/reports

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