# Service difficulty reports: N812NK, cancelled Jan 27, 2005

A list on [N812NK, cancelled Jan 27, 2005](https://openairdocs.org/deregistered/N812NK-2005-01-27.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 · 92 reports

- [SDR GTIA040661](https://openairdocs.org/sdr/GTIA040661.md): Floorboard · sheared · Jul 2, 2004 · N812NK · Doug DC982 · Fuselage Floor Panel
  > FTW - FOUND G1 FORWARD INBOARD MOUNT NUT PLATE SHEAREDON INSTALLATION. REMOVED FLOORBOARD AT OUTBOARD STATION 160-200. FLOORBOARD HAS EXTENSIVE DELAMINATION. FABRICATED NEW FLOORBOARD. INSTALLED FLOORBOARD. (M)
- [SDR GTIA040643](https://openairdocs.org/sdr/GTIA040643.md): Floor Panel · corroded · Jun 29, 2004 · N812NK · Doug DC982 · Fuselage Floor Panel
  > FTW - FOUND MAIN CABIN STATION 1250 TO STATION 1155 LEFT SIDE INBOARD FLOOR PANEL HAS SEVERAL INSERTS CORROSION SOFT/MUSHEY EDGE FILLER IS MISSING. FABRICATED NEW PANEL. (M)
- [SDR GTIA040666](https://openairdocs.org/sdr/GTIA040666.md): Bracket · cracked · Jun 25, 2004 · N812NK · Doug DC982 · Fuselage Miscellaneous Structure
  > FTW - FOUND FORWARD PIT DOOR AFT LOWER INTERNAL EDGE BRACKET CRACKED. REMOVED CRACKED BRACKET. FABRICATED BRACKET. INSTALLED NEW BRACKET. (M)
- [SDR GTIA040667](https://openairdocs.org/sdr/GTIA040667.md): Skin · worn · Jun 24, 2004 · N812NK · Doug DC982 · Passenger/Crew Doors
  > FTW - FOUND R1 DOOR LOCK TO HAVE EXCESSIVE MATERIAL LOSS ON LOWER SKIN. (M)
- [SDR GTIA040662](https://openairdocs.org/sdr/GTIA040662.md): Skin · damaged · Jun 23, 2004 · N812NK · Doug DC982 · Fuselage Main, Plate/Skin
  > FTW - FOUND EXISTING REPAIR AT FS 427 BETWEEN LONGERONS 18 AND 20R REQUIRES TO BE REPLACED WITH DC9/MD80 SRM 53-05 FIG 105 REPAIR. INSTALLED REPAIR NO LONER MEETS REQUIREMENTS FOR REPAIR AREA. REMOVED EXISTING REPAIR DOUBLER. FABRICATED DOUBLER AND TRIPLER.
- [SDR GTIA040665](https://openairdocs.org/sdr/GTIA040665.md): Skin · damaged · Jun 23, 2004 · N812NK · Doug DC982 · Fuselage Main, Plate/Skin
  > FTW - FOUND 20 INCH CREASE AT FS 617 BETWEEN LONGEORN 22 AND 23R, CREASE IS IN THE CONTROLLED RVSM AREA AND MUST BE REPAIRED. CUT OUT DAMAGED SKIN BETWEEN L22R-L26R STATION 586-636 SIZE, 25 INCH BY 50 INCH. FABRICATED NEW SECTION OF SKIN. DOUBLERS AND FINGE
- [SDR GTIA040652](https://openairdocs.org/sdr/GTIA040652.md): Floorboard · damaged · Jun 22, 2004 · N812NK · Doug DC982 · Fuselage Floor Panel
  > FTW - FOUND MAIN CABIN STATION 1117 TO 1174 CENTER FLOOR PANEL HAVE SOFT/MUSHEY AND DAMAGE ON EDGE. FABRICATED CABIN FLOORBOARD. (M)
- [SDR GTIA040653](https://openairdocs.org/sdr/GTIA040653.md): Floor Panel · cracked · Jun 22, 2004 · N812NK · Doug DC982 · Fuselage Floor Panel
  > FTW - FOUND MAIN CABIN STATION 806 TO STATION 826, FLOOR PANEL ONE INSERT DAMAGE/CRACKS ON EDGES. FABRICATED NEW FLOOR PANEL. (M)
- [SDR GTIA040651](https://openairdocs.org/sdr/GTIA040651.md): Floor Panel · cracked · Jun 22, 2004 · N812NK · Doug DC982 · Fuselage Floor Panel
  > FTW - FOUND MAIN CABIN RIGHT INBOARD FLOOR PANEL STATION 1250-1309 HAVE CRACKS, DAMAGE ON EDGES/SEVERAL INSERTS HAVE PULLED THROUGH. FABRICATED NEW FLOOR PANEL. (M)
- [SDR GTIA040644](https://openairdocs.org/sdr/GTIA040644.md): Intercostal · cracked · Jun 22, 2004 · N812NK · Doug DC982 · Fuselage Miscellaneous Structure
  > FOUND CABIN FLOOR STATION 769-788 BL 0 INTERCOSTAL UPPER FLANGE IS CRACKED AROUND FASTENER HOLES WITH MATERIAL MISSING AT 2 LOCATIONS. REMOVED INTERCOSTAL. FABRICATED REPLACEMENT INTERCOSTAL. INSTALLED INTERCOSTAL. (M)
- [SDR GTIA040655](https://openairdocs.org/sdr/GTIA040655.md): Floorboard · broken · Jun 21, 2004 · N812NK · Doug DC982 · Fuselage Floor Panel
  > FOUND FLOORBOARD BROKEN STATION 200-260 LBL 24-31. FABRICATED FLOORBOARD. (M)
- [SDR GTIA040654](https://openairdocs.org/sdr/GTIA040654.md): Floorboard · broken · Jun 21, 2004 · N812NK · Doug DC982 · Fuselage Floor Panel
  > FTW - FOUND FLOORBOARD FASTENER INSERTS MISSING, TWO EACH STATION 200-260 LBL 24-25. UPON FURTHER INVESTIGATION FLOORBOARD PANEL FOUND TO BE BROKEN. FABRICATED FLOORBOARD. (M)
- [SDR GTIA040660](https://openairdocs.org/sdr/GTIA040660.md): Frame · cracked · Jun 21, 2004 · N812NK · Doug DC982 · Wing Spar
  > FTW - FOUND LT WING FIXED LEADING EDGE COMPARTMENT XFS 267 TWO EACH, FRAME CRACKED. STOP DRILLED CRACKS. FABRICATED TWO REPAIR DOUBLER. INSTALLED TWO FORMER REPAIR DOUBLER AND L-ANGLE. (M)
- [SDR GTIA040664](https://openairdocs.org/sdr/GTIA040664.md): Frame · cracked · Jun 20, 2004 · N812NK · Doug DC982 · Wing Spar
  > FTW - FOUND LOWER FIXED LEADING EDGE COMPARTMENT XFS 330 LEADING EDGE FRAME CRACK. STOP DRILL CRACK AT FORMER. FABRICATED 3 AND DRILLED REPAIR FORMER. INSTALLED REPAIR PARTS. (M)
- [SDR GTIA040650](https://openairdocs.org/sdr/GTIA040650.md): Seat Track · corroded · Jun 19, 2004 · N812NK · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 200-1309 IS CORRODED AND GOUGED ALONG ENTIRE LENGTH, FS 494 IS OUT OF LIMITS. REMOVED DAMAGED SECTION OF SEAT TRACK FROM STATION 494 TO 532. LOCATED AND DRILLED NEW SEAT TRACK SECTION AND TWO NEW SPLICES. INSTAL
- [SDR GTIA040663](https://openairdocs.org/sdr/GTIA040663.md): Seat Track · corroded · Jun 19, 2004 · N812NK · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND LEFT INBOARD SEAT TRACK STATION 200-1309 IS CORRODED AND GOUGED ALONG ENTIRE LENGTH. REMOVED CORROSION STATION 200-236 IS OUT OF LIMITS. MATERIAL LOSS AT STATION 948-1231 IS OUT OF LIMITS. REMOVED SEAT TRACKS FROM STATION 200-250. REMOVED LEFT INBOAR
- [SDR GTIA040439](https://openairdocs.org/sdr/GTIA040439.md): Strap · misinstalled · Apr 25, 2004 · N812NK · Doug DC982 · Emergency Equipment
  > TAIL SLIDE COVER HOLD DOWN STRAPS NOT INSTALLED CORRECTLY. INSTALLED TAIL CONE EMERGENCY SLIDE COVER STRAPS CORRECTLY.
- [SDR GTIA040276](https://openairdocs.org/sdr/GTIA040276.md): Light · loose · Apr 10, 2004 · N812NK · Doug DC982 · Emergency Lighting
  > ORD - FLT 1504 - AFT GALLEY AISLE EXIT LIGHTING TRACK CAME UP. RE-ATTACHED AFT GALLEY LUMINESCENT EXIT STRIP. (M)
- [SDR GTIA040272](https://openairdocs.org/sdr/GTIA040272.md): Sign · dislodged · Apr 8, 2004 · N812NK · Doug DC982 · Emergency Lighting
  > EXIT SIGN AT AFT GALLEY FELL OFF ON TAKEOFF. RE-ATTACHED LUMINESCENT EXIT STRIP AT AFT GALLEY FLOOR AREA. (M)
- [SDR GTIA040042](https://openairdocs.org/sdr/GTIA040042.md): Landing Gear · malfunctioned · Jan 30, 2004 · N812NK · Doug DC982 · Nose/Tail Landing Gear
  > PBI - FLT 833 - AFTER TAKEOFF, THE NOSE GEAR FAILED TO RETRACT. CYCLED GEAR DOWN, NOSE GEAR GREEN LIGHT ON INSTANTLY. RECYCLED GEAR UP. NOSE GEAR FAILED TO RETRACT. ABOUT 3 TO 4 MINUTES LATER THERE WAS A POP AND THE NOSE GEAR RETRACTED. AIRSPEED WAS MAINT
- [SDR GTIA040040](https://openairdocs.org/sdr/GTIA040040.md): Glowstrip · loose · Jan 28, 2004 · N812NK · Doug DC982 · Emergency Equipment
  > DTW - FLT 834 - AFT GALLEY FLOOR GLOW STRIP OFF. REINSTALLED GALLEY FLOOR AFT GLOWSTRIP. NO OTHER DEFECTS NOTED. (M)
- [SDR GTIA040033](https://openairdocs.org/sdr/GTIA040033.md): Proximity Sensor · malfunctioned · Jan 26, 2004 · N812NK · Doug DC982 · Landing Gear Position and Warning
  > FLL - FLT 1123 - NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH UPON RETRACTION. RECYCLED PER QRH, WHICH DID NOT REMEDY SITUATION. LIGHT FINALLY WENT OUT APPROXIMATELY 2 MINUTES AFTER LAST RETRACTION. REMOVED AND REPLACED NOSE GEAR UPLOCK PROXIMITY SENSOR (D1-
- [SDR GTIA040029](https://openairdocs.org/sdr/GTIA040029.md): Glowstrip · missing · Jan 20, 2004 · N812NK · Doug DC982 · Emergency Equipment
  > MCO - FLT 1863 - FLOOR GLOW PATH STRIP MISSING BY L2 DOOR. REPLACED MISSING SAFTGLO SUPPORT FLOOR PATH STRIP. (M)
- [SDR GTIA040011](https://openairdocs.org/sdr/GTIA040011.md): Engine · flamed out · Jan 15, 2004 · N812NK · Doug DC982 · Engine (Turbine/Turboprop)
  > RT ENG FLAMED-OUT, AIR RETURN AT 800 TO 1000 MLS RT ENG EPR DROPPED BELOW 1.2 EPR, ARTS FIRED BASES X-TERED TO LT GENERATORS ACCOMPLISHED QRH ITEMS PULLED CVR C/B. PERFORMED ENG HI-POWER TRIM CHECKRUN ENG OPS CK NORM. R & R NR 2 ENG FUEL CONT, OPS CK GOOD.
- [SDR GTIA030716](https://openairdocs.org/sdr/GTIA030716.md): Conduit · out of position · Sep 28, 2003 · N812NK · Doug DC982 · Landing Gear System Wiring
  > LEFT MAIN RED GEAR LIGHT ON WITH LANDING GEAR HANDLE UP. QRH PROCEDURE FOLLOWED, NO CHANGE. REPOSITIONED LT MAIN GEAR UPLOCK SENSOR CONDUIT AND OPS CHECKED. NO DEFECTS NOTED. OK FOR SERVICE. (M)
- [SDR GTIA030680](https://openairdocs.org/sdr/GTIA030680.md): Control Unit · malfunctioned · Sep 14, 2003 · N812NK · Doug DC982 · Fire Detection
  > LT ENGINE LOOP 'A' LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURE. REMOVED AND REPLACED CONTROL UNIT. OPS CHECK NORMAL. (M)
- [SDR GTIA030657](https://openairdocs.org/sdr/GTIA030657.md): Inlet Guide Vane · cracked · Aug 26, 2003 · N812NK · Doug DC982 · Engine Air Intake System
  > ENGINE 2-217A ESN 708450 INLET GUIDE VANE HAS ROOT AND INNER SHROUD WELD TO SHROUD CRACKED. REMOVED AND REPLACED IGV CASE. (M)
- [SDR GTIA030656](https://openairdocs.org/sdr/GTIA030656.md): Blade · damaged · Aug 26, 2003 · N812NK · Doug DC982 · Turbine Engine Compressor Section
  > NR 2 ENGINE 1ST STAGE FAN BLADE IS MANGLED BEYOND BLENDABLE LIMITS. REMOVED AND REPLACED TWO C-1 BLADES IAW MD-80 A/C MM REV 76 REV 76 SECTION 72-33-21. COMPLIED WITH TEST 6 AND 1 PER SECTION 72-00-00 PER TIMCO ENGINE CENTER CERT T48R384Y. (M)
- [SDR GTIA030414](https://openairdocs.org/sdr/GTIA030414.md): Bracket · damaged · Jun 1, 2003 · N812NK · Doug DC982 · Escape Slide
  > SLIDE PACK BRACKET ON R-1 DOOR WILL NOT HOLD SLIDE PACK GIRT BAR. REPOSITIONED AFT GIRT BAR HOOK ON R-1 SLIDE PACK. GIRT BAR OPERATION NORMAL. (M)
- [SDR GTIA030275](https://openairdocs.org/sdr/GTIA030275.md): Engine · smoke · Apr 24, 2003 · N812NK · Doug DC982 · Engine (Turbine/Turboprop)
  > AIR RETURN, ON TAKEOFF AFT CABIN FILLED WITH SMOKE. AFT LAV SMOKE ALARMS WENT OFF. RETURNED TO DTW. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECK AND LEAK GOOD, NO DEFECTS NOTED.
- [SDR GTIA030244](https://openairdocs.org/sdr/GTIA030244.md): Smoke Detector · malfunctioned · Apr 2, 2003 · N812NK · Doug DC982 · Smoke Detection
  > CARGO FIRE DETECTION FORWARD 'B' FAIL LIGHT AND ANNUNCIATOR PANEL SMOKE DETECTOR LOOP LIGHT ILLUMINATED. REMOVED AND REPLACED CARGO COMPARTMENT SMOKE DETECTOR. (M)
- [SDR GTIA030162](https://openairdocs.org/sdr/GTIA030162.md): Screw · missing · Mar 10, 2003 · N812NK · Doug DC982 · Fuselage Miscellaneous Structure
  > LEFT FORWARD OVERWING EMERGENCY EXIT WINDOW IS STUCK CLOSED. FORWARD SCREW ON EXIT COVER MISSING THUS JAMMING DOOR CLOSED. INSTALLED SCREW ON COVER, DOOR NOW FUNCTIONS PROPERLY.
- [SDR GTIA021264](https://openairdocs.org/sdr/GTIA021264.md): Ring · corroded · Nov 29, 2002 · N812NK · Doug DC982 · Passenger Compartment Windows
  > FTW - FOUND LEFT 346 WINDOW UPPER AFT FRAME CORRODED. REMOVED LEFT NR 46 WINDOW UPPER AFT CRACKED FRAME. LOCATED AND DRILLED NEW ORDERED WINDOW RING. INSTALLED NEW WINDOW RING. (M)
- [SDR GTIA021263](https://openairdocs.org/sdr/GTIA021263.md): Floor Support · corroded · Nov 27, 2002 · N812NK · Doug DC982 · Fuselage Miscellaneous Structure
  > FTW - L2 DOOR OPENING FLOOR PANEL SUPPORT BRACKETS (2) CORRODED. FORWARD FLOOR PANEL SUPPORT BRACKET L2 DOOR FOUND TO BE OUT OF LIMITS. FABRICATED FORWARD FLOOR PANEL SUPPORT. INSTALLED NEW FORWARD FLOOR SUPPORT. (M)
- [SDR GTIA021261](https://openairdocs.org/sdr/GTIA021261.md): Attach Angle · cracked · Nov 24, 2002 · N812NK · Doug DC982 · Fuselage, Stabilizer Attach Fittings
  > FTW - FOUND DORSAL FIN INBOARD LEFT, RIGHT ANGLE ATTACH IS CRACKED. REMOVED LEFT AND RIGHT FIN INBOARD ATTACH ANGLES. LOCATED AND DRILLED LEFT INBOARD FIN ANGLE. LOCATED AND DRILLED LEFT OUTBOARD ATTACH ANGLE. LOCATED AND DRILLED RIGHT INBOARD FIN ANGLE AN
- [SDR GTIA021260](https://openairdocs.org/sdr/GTIA021260.md): Seat Track · corroded · Nov 23, 2002 · N812NK · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > FTW - FOUND RIGHT INBOARD SEAT TRACK CORRODED AT STATION 200 AND 256. MATERIAL LOSS OUT OF LIMITS AT SEAT TRACK STATION 267. REMOVED DAMAGE AREA. FABRICATED NEW SEAT TRACK FS 200-320. INSTALLED SEAT TRACK AND SPLICE. (M)
- [SDR GTIA021257](https://openairdocs.org/sdr/GTIA021257.md): Longeron · corroded · Nov 21, 2002 · N812NK · Doug DC982 · Fuselage Main, Longeron/Stringer
  > E/E BAY STATION 180-218 L30 CORROSION IN LONGERON AROUND FASTENERS. REMOVED DAMAGED SECTION OF LONGERON AND SPLICE. INSTALLED NEW LONGERON AND SPLICE. (M)
- [SDR GTIA021262](https://openairdocs.org/sdr/GTIA021262.md): Web · cracked · Nov 21, 2002 · N812NK · Doug DC982 · Fuselage Miscellaneous Structure
  > FTW - FOUND PAX CABIN STATION 503, STATION 231 WEB MEMBRANE IS CRACKED. STOP DRILLED CRACK. FABRICATED DOUBLER. INSTALLED DOUBLER REPAIR. STOP DRILL CRACK AT WEB MEMBRANE ON STATION 503. FABRICATE DOUBLER REPAIR. INSTALLED REPAIR DOUBLER AT STATION 503.
- [SDR GTIA021253](https://openairdocs.org/sdr/GTIA021253.md): Door Frame · corroded · Nov 21, 2002 · N812NK · Doug DC982 · Fuselage Main, Structure
  > FTW - FOUND AFT CARGO JAMB BEAM HAS CORROSION STATION 1112-1249, DOOR JAMB BEAM REPAIR STRAP HAS CORROSION UNDER STRAP ON JAMB BEAM. CORRODED REMOVAL WAS FOUND TO BE OUT OF LIMITS ON DOOR JAMB. REMOVED DOOR JAMB BEAM. CORROSION REMOVAL ON DOOR WEB WAS FOUND
- [SDR GTIA021287](https://openairdocs.org/sdr/GTIA021287.md): Intercostal · cracked · Nov 18, 2002 · N812NK · Doug DC982 · Passenger/Crew Doors
  > FTW - FOUND L1 DOOR UPPER MOST INTERCOSTAL BEAM (TWO) CRACKS IN LOWER RADIUS FORWARD AND AFT SIDES. REMOVED CRACKED DOOR BEAM. FORMED BEAM. INSTALLED DOOR BEAM. (M)
- [SDR GTIA021255F](https://openairdocs.org/sdr/GTIA021255F.md): Frame · corroded · Nov 17, 2002 · N812NK · Doug DC982 · Fuselage Main, Frame
  > FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LBL 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 579 REPAIR. INSTALLE
- [SDR GTIA021255E](https://openairdocs.org/sdr/GTIA021255E.md): Frame · corroded · Nov 17, 2002 · N812NK · Doug DC982 · Fuselage Main, Frame
  > FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LBL 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 579 REPAIR. INSTALLE
- [SDR GTIA021255D](https://openairdocs.org/sdr/GTIA021255D.md): Frame · corroded · Nov 17, 2002 · N812NK · Doug DC982 · Fuselage Main, Frame
  > FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LBL 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 579 REPAIR. INSTALLE
- [SDR GTIA021255C](https://openairdocs.org/sdr/GTIA021255C.md): Frame · corroded · Nov 17, 2002 · N812NK · Doug DC982 · Fuselage Main, Frame
  > FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LBL 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 579 REPAIR. INSTALLE
- [SDR GTIA021255B](https://openairdocs.org/sdr/GTIA021255B.md): Frame · corroded · Nov 17, 2002 · N812NK · Doug DC982 · Fuselage Main, Frame
  > FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LBL 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 579 REPAIR. INSTALLE
- [SDR GTIA021255A](https://openairdocs.org/sdr/GTIA021255A.md): Frame · corroded · Nov 17, 2002 · N812NK · Doug DC982 · Fuselage Main, Frame
  > FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LBL 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 579 REPAIR. INSTALLE
- [SDR GTIA021354](https://openairdocs.org/sdr/GTIA021354.md): Door Frame · corroded · Nov 17, 2002 · N812NK · Doug DC982 · Fuselage Main, Structure
  > FTW - FOUND DOOR JAMB BEAM REPAIR STRAP HAS CORROSION UNDER STRAP AND ON JAMB BEAM. REMOVED DOOR JAMB BEAM TO BE OUT OF LIMITS. HOLES LOCATED AND DRILLED ON NEW JAMB BEAM. REMOVED DOOR JAMB WEB STATION 1150-1220 STRINGER 28-29 RIGHT SIDE. FABRICATED NEW DO
- [SDR GTIA021255](https://openairdocs.org/sdr/GTIA021255.md): Frame · corroded · Nov 17, 2002 · N812NK · Doug DC982 · Fuselage Main, Frame
  > FTW - FOUND FORWARD PIT HAS CORROSION AT THE FRAME STATION 541, STATION 560, 579, 636, 701, 750 AT 788, RBL 16 INCHES LBL 16 INCHES. FOUND THE AREA AT FS 541, 579 IS OUT OF LIMITS. FABRICATED (1 EACH) -3, (1 EACH) -7, (2 EACH)-11 FOR FS 579 REPAIR. INSTALLE
- [SDR GTIA021238](https://openairdocs.org/sdr/GTIA021238.md): Stringer · cracked · Nov 17, 2002 · N812NK · Doug DC982 · Fuselage Main, Longeron/Stringer
  > FTW - AFT ACCESSORY COMPARTMENT 1474 CANT LONGERON 18L, 1 INCH CRACK ON STRINGER. STOP DRILL CRACK. FABRICATED TWO FORMER DOUBLERS. INSTALLED TWO FORMER DOUBLER REPAIR. (M)
- [SDR GTIA021288](https://openairdocs.org/sdr/GTIA021288.md): Floor Panel · damaged · Nov 16, 2002 · N812NK · Doug DC982 · Fuselage Floor Panel
  > FTW - FOUND CAPTAIN FLOOR PANEL NEXT TO CONTROL COLUMN HAS DELAMINATED AND BROKEN WOOD FILLER AS MARKED. LOCATED AND DRILLED NEW PANEL. (M)

Next page: https://openairdocs.org/deregistered/N812NK-2005-01-27/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 = 'N812NK' AND deregistration_id = 'N812NK-2005-01-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N812NK-2005-01-27/reports

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