# N834NK: 1989 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2006-06-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 14, 2006
- Exported to: Spain
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 49847
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 20, 2004
- Certificate issued: February 3, 2005
- Last registry action: February 3, 2005
- Mode S code: AB686C
- Owner when cancelled: [Finova Capital Corp](https://openairdocs.org/faa-owner/FINOVA%20CAPITAL%20CORP)
- Location: [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale)
- Owner type: Corporation
- Owner's area on the map: 33.4945° N, 111.9207° W: Placed by OpenAirDocs at the center of ZIP code 85251, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N834NK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=834NK
- Page: https://openairdocs.org/deregistered/N834NK-2006-06-14

From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas DC-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md

## Service difficulty reports (54, newest 50)

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

- [SDR GTIA200600052](https://openairdocs.org/sdr/GTIA200600052), May 19, 2006: LONGERON. CORRODED. IN FWD PIT, LONGERON 29L STA 235 HAS CORROSION. REMOVED CORROSION. INSTALLED SPLICE REPAIR.
- [SDR GTIA200600051](https://openairdocs.org/sdr/GTIA200600051), May 17, 2006: SUPPORT. CRACKED. FWD CARGO PIT LINING SUPPORT CRACKED AT STA 522, CENTERLINE. INSTALLED STIFFENER.
- [SDR GTIA050286](https://openairdocs.org/sdr/GTIA050286), Dec 10, 2005: BLEED VALVE. MALFUNCTIONED. LT ENGINE N2 DROPS BELOW 45 PERCENT WHEN LOAD APPLIED. REPLACED A/C WITH 832NK ON LINE. REMOVED NR1 ENGINE FUEL CONTROL. OPS AND LEAK CHECK GOOD. REMOVED AND RE
- [SDR GTIA050248](https://openairdocs.org/sdr/GTIA050248), Aug 31, 2005: SKIN. DENTED. LT WING NR 1 SLAT DENTED STATION XTS 128.000, DENT DIAMETER = 2.0 DEPTH = .048. LEFT WING, NR 1 SLAT DENT FOUND OUT OF LIMIT. REPAIRED DENT AREA. (M)
- [SDR GTIA050250](https://openairdocs.org/sdr/GTIA050250), Aug 29, 2005: RIB. CRACKED. FOUND RIGHT HORIZONTAL STABILIZER L/E, OUTBOARD L/E RIB CRACKED AT UPPER EDGE. STOPPED DRILLED CRACKED AREA. FABRICATED REPAIR PART. TREATED, PRIMED AND INSTALL
- [SDR GTIA050244](https://openairdocs.org/sdr/GTIA050244), Aug 27, 2005: DOOR FRAME. CRACKED. FOUND LT MLG, AFT DOOR JAMB IS CRACKED AT CORNER T-CAP. STOPPED DRILLED CRACK AT AFT DOOR JAMB. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER
- [SDR GTIA050239](https://openairdocs.org/sdr/GTIA050239), Aug 26, 2005: CUSP WEB. CORRODED. FOUND CORROSION INSIDE CABIN AT CUSP LINE, WEB STATION 598, L18L. REMOVED CORROSION AT WEB STATION 598. FOUND ITS OUT OF LIMITS. CUT OUT DEFECTIVE AREA. FABRICA
- [SDR GTIA050241](https://openairdocs.org/sdr/GTIA050241), Aug 26, 2005: CUSP WEB. CORRODED. FTW - FOUND CORROSION INSIDE CABIN AT CUSP LINE, WEB STATION 622, L18L. REMOVED CORROSION INSIDE CABIN AT WEB STATION 622, L18L. FABRICATED REPAIR DOUBLER AND F
- [SDR GTIA050242](https://openairdocs.org/sdr/GTIA050242), Aug 26, 2005: SPAR. DAMAGED. LEFT HORIZ STAB AFT SPAR CHANNEL DAMAGED STATION XHS 85. REMOVED CHANNEL ON LEFT HORIZONTAL STAB ON AFT SPAR. FABRICATED CHANNEL. TREATED, PRIMED AND INSTALLED 
- [SDR GTIA050243](https://openairdocs.org/sdr/GTIA050243), Aug 26, 2005: SKIN. CRACKED. FTW - FOUND RIGHT WING REFUELING STATION DOOR CUTOUT INBOARD CORNER DOUBLER CRACKED. REMOVED CRACKED SECTION AND FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND 
- [SDR T48R20050013](https://openairdocs.org/sdr/T48R20050013), Jun 21, 2005: BLADE. FRACTURED. ENGINE WAS REMOVED FROM N834NK NR 2 POSITION FOR IN FLIGHT SHUTDOWN. VISUAL INSPECTION REVEALED THE T-4 BLADES FRACTURED/MISSING AT THE BASE OF THE BLADE ROOT W
- [SDR GTIA050162](https://openairdocs.org/sdr/GTIA050162), Jun 1, 2005: ENGINE. FAILED. RT ENGINE FAILURE DURING CLIMB THROUGH 22,000 FT, COMPRESSOR STALLED, EGT 710 FEET ENGINE ROLLED BACK AND SHUTDOWN. FOUND TURBINE SECTION FAILED. REMOVED AND RE
- [SDR GTIA050040](https://openairdocs.org/sdr/GTIA050040), Feb 25, 2005: ENGINE. MALFUNCTIONED. NR 1 ENGINE SLOW TO SPOOL, TAIL SWAP WITH AIRCRAFT 810. REMOVED AND REPLACED NR 1 ENGINE. (K)
- [SDR GTIA050015](https://openairdocs.org/sdr/GTIA050015), Jan 23, 2005: RELAY. INOPERATIVE. DTW - FLT 706 - AIRCRAFT CROSS TIE WILL NOT RESET, AIRCRAFT TAIL SWAP. REMOVED AND REPLACED AC CROSS TIE RELAY. (M)
- [SDR GTIA040831](https://openairdocs.org/sdr/GTIA040831), Nov 7, 2004: SHAFT. SHEARED. AIR RETURN DUE TO LOSS OF LT SYSTEM HYDRAULIC PRESSURE. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP, NOTED SHEARED SHAFT. LEAK AND OPS CHECK GOOD.
- [SDR GTIA040669](https://openairdocs.org/sdr/GTIA040669), Jul 14, 2004: FIRE LOOP. MALFUNCTIONED. RT ENGINE B-LOOP ILLUMINATED. REMOVED AND REPLACED RIGHT ENGINE FIRE LOOP. (M)
- [SDR GTIA040239](https://openairdocs.org/sdr/GTIA040239), Mar 27, 2004: CABLE. OUT OF POSITION. FLL - FLT 679 - FOUND L2 DOOR EMERGENCY SLIDE GIRT BAR CABLE MISPOSITIONED. INST CABLE ON GIRT BAR. (M)
- [SDR GTIA040220](https://openairdocs.org/sdr/GTIA040220), Mar 19, 2004: LANYARD. MISROUTED. FLL - FOUND L2 DOOR SLIDE LANYARD ROUTED INCORRECTLY. RE-ROUTED L2 DOOR SLIDE LANYARD CORRECTLY. (M)
- [SDR GTIA040247](https://openairdocs.org/sdr/GTIA040247), Feb 25, 2004: LIGHT. BROKEN. FTW - FOUND AFT AIRSTAIRS EMERGENCY LIGHTS SEVERAL LIGHTS NOT WORKING. REMOVED BROKEN AFT AIRSTAIR EMERGENCY LIGHT. INSTALLED NEW LIGHT ASSEMBLY. (M)
- [SDR GTIA040159](https://openairdocs.org/sdr/GTIA040159), Feb 22, 2004: TERMINAL. DEFECTIVE. NUMEROUS EMERGENCY LIGHTS OUT IN CABIN. FOUND DEFECTIVE GROUND TERMINAL AT EMERGENCY LIGHT ASSY. REPAIRED TERMINAL LUG.
- [SDR GTIA040229](https://openairdocs.org/sdr/GTIA040229), Jan 30, 2004: ANGLE. CRACKED. FTW - FOUND LEFT MLG W/W FORWARD OUTBOARD EDGE OF DOOR CUTOUT HAS 1 CRACKED ANGLE. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED ANGLE. (M)
- [SDR GTIA040106](https://openairdocs.org/sdr/GTIA040106), Jan 29, 2004: NOSE COWL. WORN. FTW - NR 1 ENGINE NOSE COWL HAS EXPOSED FIBERGLASS AFT OF INLET RING ENTIRE CIRCUMFERENCE. ON FURTHER INVESTIGATION FOUND NOSE COWL SKIN DELAMINATED. REPAIRED C
- [SDR GTIA040119](https://openairdocs.org/sdr/GTIA040119), Jan 27, 2004: FLOOR PANEL. DELAMINATED. FTW - FOUND LEFT FLOOR PANEL STATION 200-256 DELAMINATED AND TWO INSERTS MISSING. FABRICATED NEW PANEL. (M)
- [SDR GTIA040145](https://openairdocs.org/sdr/GTIA040145), Jan 22, 2004: CHANNEL. DAMAGED. FTW - FOUND PASSENGER CABIN METALLIC PANEL LEFT SIDE STATION 1174 TO 1260 HAS TWO HATS SECTION DISBONDED AND DAMAGE FORWARD END SECTION HAT. REPAIRED PANEL. (M)
- [SDR GTIA040122](https://openairdocs.org/sdr/GTIA040122), Jan 18, 2004: FLOOR PANEL. DEBONDED. FTW - FOUND COCKPIT FLOOR PANEL FOR CONSOLE SKIN IS DEBONDED AND MISSING. REBONDED SKIN. (M)
- [SDR GTIA040118](https://openairdocs.org/sdr/GTIA040118), Jan 18, 2004: SKIN. GOUGED. FTW - FOUND RIGHT ELEVATOR BOTTOM SIDE IS DENTED AND GOUGED NEAR OUTBOARD EDGE. REMOVED DAMAGED SECTION OF RIGHT ELEVATOR BOTTOM SIDE SKIN. FABRICATED TWO FINGE
- [SDR GTIA040236](https://openairdocs.org/sdr/GTIA040236), Jan 15, 2004: FLOOR PANEL. DELAMINATED. FTW - FOUND LEFT FLOOR PANEL STATION 200-256 DELAMINATED AND TWO EACH INSERTS MISSING. FABRICATED NEW PANEL. (M)
- [SDR GTIA040126](https://openairdocs.org/sdr/GTIA040126), Jan 15, 2004: FLOOR PANEL. DELAMINATED. FTW - FOUND CENTER FLOOR PANEL STATION 927 DELAMINATED AND DAMAGED EDGE FILLER. FABRICATED NEW FLOOR PANEL. (M)
- [SDR GTIA040109](https://openairdocs.org/sdr/GTIA040109), Jan 15, 2004: FLOOR PANEL. CRACKED. FOUND CENTER FLOOR PANEL STATION 800 BOTTOM LEFT AND RIGHT SUPPORT STIFFENERS CRACKED IN SEVERAL AREAS. REMVOED AND REPLACED SUPPORT STIFFENERS. (M)
- [SDR GTIA040108](https://openairdocs.org/sdr/GTIA040108), Jan 15, 2004: FLOOR PANEL. DAMAGED. FTW - FOUND LEFT CAPTAIN FLOOR PANEL BRACKET MISSING AND BOTTOM STIFFENERS DETACHED. REATTACHED BOTTOM STIFFENERS. INSTALLED NEW BRACKET. (M)
- [SDR GTIA040111](https://openairdocs.org/sdr/GTIA040111), Jan 15, 2004: FLOOR PANEL. CRACKED. FTW - FOUND CENTER FLOOR PANEL STATION 860 UPPER DOUBLER CRACKED AND BOTTOM LEFT AND RIGHT STIFFENERS CRACKED IN SEVERAL AREAS. REPLACED UPPER DOUBLER BOTTOM LE
- [SDR GTIA040121](https://openairdocs.org/sdr/GTIA040121), Jan 15, 2004: FLOOR PANEL. DELAMINATED. FTW - FOUND RIGHT OUTBOARD FLOOR PANEL STATION 120 DELAMINATED AND THREE DAMAGED INSERTS. FABRICATED NEW FLOOR PANEL. (M)
- [SDR GTIA040123](https://openairdocs.org/sdr/GTIA040123), Jan 13, 2004: DOUBLER. MISSING. FTW - FOUND FLOOR PANEL OUTBOARD STATION 927 DOUBLER MISSING ON PANEL EDGE. FABRICATED NEW DOUBLER. INSTALLED DOUBLER. (M)
- [SDR GTIA040107](https://openairdocs.org/sdr/GTIA040107), Jan 13, 2004: FLOOR PANEL. DAMAGED. FTW - FOUND FLOOR PANEL RIGHT OUTBOARD STATION 927 STIFFENER DETACHED AND CENTER STIFFENER 3 AREAS OF INCORRECT REPAIRS. REMOVED DAMAGED STIFFENER. FABRICATED N
- [SDR GTIA040113](https://openairdocs.org/sdr/GTIA040113), Jan 13, 2004: CLIP. CORRODED. FTW - FOUND AFT PIT FS 1117 INTERCOSTAL CLIP RBL 13 CORRODED. REMOVED CLIP. FABRICATED CLIP. INSTALLED CLIP. (M)
- [SDR GTIA040112](https://openairdocs.org/sdr/GTIA040112), Jan 13, 2004: FLOOR PANEL. DAMAGED. FTW - FOUND FLOOR PANEL OUTBOARD STATION 800 STIFFENER DEATTACHED IN 2 AREAS. REBONDED STIFFENER. (M)
- [SDR GTIA040244](https://openairdocs.org/sdr/GTIA040244), Jan 11, 2004: SEAT TRACK. DAMAGED. TW - FOUND MAIN CABIN STATION 875 TO 1309 LBL 44 INCHES SEAT TRACK HAS SEVERAL NICKS, GOUGED, LIGHT CORROSION, BARE METAL. SEAT TRACK AT STATION 1031 TO 937 WAS
- [SDR GTIA040246](https://openairdocs.org/sdr/GTIA040246), Jan 11, 2004: SKIN. DENTED. FTW - FOUND RIGHT ELEVATOR ANTI-FLOAT TAB DENTED ON BOTH SIDES NUMEROUS PLACES. REMOVED RIGHT ELEVATOR ANTI-FLOAT TAB. INSTALLED RIGHT ELEVATOR ANTI-FLOAT TAB. 
- [SDR GTIA040245](https://openairdocs.org/sdr/GTIA040245), Jan 11, 2004: SKIN. DENTED. FTW - FOUND LEFT ELEVATOR ANTI-FLOAT TAB DENTED ON BOTH SIDES NUMEROUS PLACES. REMOVED LEFT ELEVATOR ANTI-FLOAT TAB. INSTALLED LEFT ELEVATOR ANTI-FLOAT TAB. (M)
- [SDR GTIA040124](https://openairdocs.org/sdr/GTIA040124), Jan 11, 2004: WEB. CRACKED. FTW - FOUND MAIN CABIN FS 1200 WEB CRACKED L18L. STOP DRILLED CRACK. FABRICATED, LOCATED AND DRILLED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)
- [SDR GTIA040125](https://openairdocs.org/sdr/GTIA040125), Jan 11, 2004: CUSP WEB. CORRODED. FTW - FOUND MAIN CABIN FS 237-256 CORRODED ON CUSP AND WEB L18L. REMOVED CORROSION. FABRICATED NEW DOUBLER. INSTALLED REPAIR DOUBLER. (M)
- [SDR GTIA040114](https://openairdocs.org/sdr/GTIA040114), Jan 11, 2004: CUSP WEB. CORRODED. FTW - FOUND MAIN CABIN, RIGHT CUSP WEB AT FS 276-296 IS CORRODED. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER. (M)
- [SDR GTIA040110](https://openairdocs.org/sdr/GTIA040110), Jan 11, 2004: SEAT TRACK. GOUGED. FTW - FOUND MAIN CABIN STATION 875 TO STATION 1309 LBL 22 INCHES INBOARD SEAT TRACK HAS SEVERAL NICKS, GOUGED, LIGHT CORRODED BARE METAL. SEAT TRACK OUT OF LIMI
- [SDR GTIA040120](https://openairdocs.org/sdr/GTIA040120), Jan 11, 2004: STANCHION. CRACKED. FTW - FOUND MID PIT BULKHEAD FRAME STANTION IS CRACKED LEFT. STOP DRILLED CRACK. FABRICATED REPAIR ANGLES. INSTALLED REPAIR ANGLES. (M)
- [SDR GTIA040248](https://openairdocs.org/sdr/GTIA040248), Jan 10, 2004: SEAT TRACK. CRACKED. FTW - FOUND MAIN CABIN STATION 256 TO 875 RBL 22 INCHES INBOARD SEAT TRACK HAS SEVERAL NICKS, GOUGED, LIGHT CORROSION, BARE METAL. AFTER FURTHER INSPECTION DISC
- [SDR GTIA040158](https://openairdocs.org/sdr/GTIA040158), Jan 10, 2004: NOSE COWL. MISSING. RT ENGINE NOSE COWL SN 49123 ACOUSTIC LINING MISSING ON LOWER HALF OF PERFORATED INTERIOR. REMOVED NOSE COWL. INSTALLED RT NOSE COWL.
- [SDR GTIA040116](https://openairdocs.org/sdr/GTIA040116), Jan 10, 2004: ESCAPE ROPE. DETERIORATED. FTW - FOUND CAPTAINS AND F/O'S ESCAPE LINES DETERIORATED. REMOVED AND REPLACED CAPTAINS AND F/O'S ESCAPE LINES. (M)
- [SDR GTIA040117](https://openairdocs.org/sdr/GTIA040117), Jan 9, 2004: FLOOR SUPPORT. CORRODED. FTW - FOUND CORROSION ON CABIN FLOOR SUPPORT FS 200 55 INCHES LBL. REMOVED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT. (M)
- [SDR GTIA040115](https://openairdocs.org/sdr/GTIA040115), Jan 7, 2004: SKIN. CRACKED. FTW - FOUND LEFT ELEVATOR INBOARD FORWARD EDGE SKIN CRACKED. FABRICATED LEFT ELEVATOR INBOARD FORWARD SKIN. INSTALLED FABRICATED SKIN. (M)
- [SDR GTIA040039](https://openairdocs.org/sdr/GTIA040039), Jan 7, 2004: INTERCOSTAL. CRACKED. FTW = FOND MID PIT CRACKED INTERCOSTAL IN OVERHEAD AT PAX CABIN FLOORBOARD NUT CLIP HOLES, FS 769-788 0 BL. REMOVED INTERCOSTAL. CUT OFF DAMAGED LIP. FABRICATED

All 54: https://openairdocs.org/deregistered/N834NK-2006-06-14/reports.md

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