# N130NK: 1974 Mcdonnell Douglas DC-9-41, registration cancelled 2004-06-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 7, 2004
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-9-41](https://openairdocs.org/model/mcdonnell-douglas-dc-9-41) (registry code 302207P)
- Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 47604
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 11, 1996
- Certificate issued: December 17, 2003
- Last registry action: December 17, 2003
- Mode S code: A07C67
- Owner when cancelled: [Alameda Corp Trustee](https://openairdocs.org/faa-owner/ALAMEDA%20CORP%20TRUSTEE)
- Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio)
- Owner type: Corporation
- Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N130NK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=130NK
- Page: https://openairdocs.org/deregistered/N130NK-2004-06-07

From the FAA registry file of October 31, 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-9-41: https://openairdocs.org/model/mcdonnell-douglas-dc-9-41.md

## Service difficulty reports (79, newest 50)

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

- [SDR GTIA030274](https://openairdocs.org/sdr/GTIA030274), Apr 22, 2003: SLIDE. DISLODGED. PBI - FLT 330 - LEFT SIDE PACK FELL OFF. REINSTALLED SLIDE/COVER. (M)
- [SDR GTIA030243](https://openairdocs.org/sdr/GTIA030243), Apr 2, 2003: SLIDE. DISLODGED. EMERGENCY SLIDE PACK FELL OFF. REINSTALLED LANYARD SLIDE CHECK OK. (M)
- [SDR GTIA030241](https://openairdocs.org/sdr/GTIA030241), Mar 31, 2003: LINER. CRACKED. FOUND RT ENGINE HAS A SECTION OF ACCOUSTIC LINER MISSING AND CRACKED TAILPIPE 2 O'CLOCK POSITION. REMOVED AND REPLACED THRUST REVERSER SPACER. OPS AND LEAK CHEC
- [SDR GTIA030116](https://openairdocs.org/sdr/GTIA030116), Mar 2, 2003: FLASHLIGHT. INOPERATIVE. FORWARD F/A HANDHELD EMERGENCY LIGHT, INOPERATIVE. REMOVED AND REPLACED FWD HANDHELD EMERGENCY LIGHT. OPS CHECK GOOD.
- [SDR GTIA030115](https://openairdocs.org/sdr/GTIA030115), Mar 2, 2003: SIGN. INOPERATIVE. TAILCONE INTERIOR LUMINESCENT EXIT SIGN INOPERATIVE. REMOVED AND REPLACED TAILCONE INTERION LUMINESCENT EXIT SIGN. OPS CHECK GOOD.
- [SDR GTIA030003](https://openairdocs.org/sdr/GTIA030003), Jan 14, 2003: SKIN. CRACKED. DTW - FOUND CRACK/PUNCTURE IN SKIN AT STATION NR 1012 LONGERON STATION NR 26R JUST AFT OF CARGO PIT DOOR. REPAIRED CRACK/PUNCTURE IN SKIN AT STATION1012 LONGERO
- [SDR GTIA030019](https://openairdocs.org/sdr/GTIA030019), Jan 6, 2003: OIL SYSTEM. FLUCTUATES. ACY - FLT 277 - GATE RETURN, NR 2 OIL PRESSURE FLUCTUATING. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M)
- [SDR GTIA021037](https://openairdocs.org/sdr/GTIA021037), Oct 1, 2002: ISOLATOR. DEFECTIVE. DTW - FOUND LOWER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE LOWER ISOLATOR, CLOSED 10/10/02. (M)
- [SDR GTIA021036](https://openairdocs.org/sdr/GTIA021036), Oct 1, 2002: ISOLATOR. DEFECTIVE. DTW - FOUND UPPER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE UPPER ISOLATOR, CLOSED 10/10/02. (M)
- [SDR GTIA021071](https://openairdocs.org/sdr/GTIA021071), Oct 1, 2002: COMBUST CHAMBER. WORN. BOROSCOPE RECORD, FOUND IGNITER GUIDE NR 4 COMBUSTION CHAMBER WORN AND OUT OF CHAMBER RESTING IN OUTER COMBUSTION CASE IGNITER PORT NR 4. BURNER CANS HAVE BEEN 
- [SDR GTIA020292](https://openairdocs.org/sdr/GTIA020292), Apr 17, 2002: AUTOPILOT SYS. MALFUNCTIONED. AEX - AUTOPILOT TURNS A/C RIGHT WITH TURN KNOB CENTERED AUTOPILOT OVER TRIMS AIRCRAFT DURING TURNS RESULTING IN LARGE OUT OF TRIM CORRECTIONS. (M)
- [SDR GTIA010226](https://openairdocs.org/sdr/GTIA010226), Apr 23, 2001: CONTROL UNIT. INOPERATIVE. FLL - FLT 41 - AUTOPILOT PITCH CONTROL IS INOPERATIVE. TRANSFERRED TO CMI NR 0019690-3. CAT C MEL 22-10. PLACARD INSTALLED. (M)
- [SDR GTIA010112](https://openairdocs.org/sdr/GTIA010112), Apr 14, 2001: SERVO. MALFUNCTIONED. FLL - FLT 139 - WITH A/P ENGAGED AL PORPOISES ABRUPTLY WITH A/P ELEV SERVO OFF PROBLEM CEASES. DMI NR 1669-1 ASSIGNED PER MEL 22-3-0 CAT C DUE DATE D4-24-01 AME
- [SDR GTIA010113](https://openairdocs.org/sdr/GTIA010113), Apr 12, 2001: AUTOPILOT SYS. FLUTTER. MLB - FLT 72 - WHEN AUTOPILOT IS ENGAGED THERE IS A RAPID OSCILLATION (FLUTTER) IN PITCH, SERVO OFF NO OSCILLATION. TRANFERRED TO MEL 22-16-0 DMI NR 0001663-1 C
- [SDR GTIA010097](https://openairdocs.org/sdr/GTIA010097), Apr 7, 2001: AUTOPILOT SYS. MALFUNCTIONED. FLT 72 - FLL - AUTO PILOT WILL NOT ENGAGE AT ALL. CHECKED THE AUTO PILOT OPERATIONS. FUNCTIONS NORMAL. TALKED TO THE CAPTAIN, HE STATED AUTO PILOT IS NORMAL BOT
- [SDR GTIA010096](https://openairdocs.org/sdr/GTIA010096), Apr 6, 2001: AUTOPILOT SYS. VIBRATION. WITH AUTO PILOT ON, THERE IS A LOW FREQUENCY VIBRATION IN PATCH AXIS, PITCH SERVO OFF, NO VIBRATION. NORMAL OPERATION. OPS CHECK GOOD ON GROUND IAW DC-9 MM 22-1
- [SDR GTIA010047](https://openairdocs.org/sdr/GTIA010047), Feb 24, 2001: TAIL CONE. DISLODGED. MYR - FLT 303 - TAILCONE CAME OFF ON LANDING. TAILCONE RELEASE SYSTEM EVACUATED AND REPAIRED BY BOEING. REPLACED EXTERIOR CABLE FITTING AND RIGHT LOWER LOCKING 
- [SDR GTIA010043](https://openairdocs.org/sdr/GTIA010043), Feb 23, 2001: TAIL CONE. SEPARATED. DCA - FLT 72 - TAILCONE FELL OFF DURING LANDING. REMOVED AND REPLACED TAILCONE IAW MM 53-50-3, OPS CHECK NORMAL. (M)
- [SDR GTIA000230](https://openairdocs.org/sdr/GTIA000230), Jun 20, 2000: WIRE. BROKEN. DTW - EMERGENCY FLOOR TRACK LIGHTING FORWARD SECTION INOPERATIVE. REPAIRED BROKEN WIRE OPS CHECKS GOOD IAW DC9 MM 33-53-00. (M)
- [SDR GTIA000129](https://openairdocs.org/sdr/GTIA000129), Mar 13, 2000: LENS. MISSING. DTW - EMERGENCY RACK LIGHTING DOES NOT HAVE RED LENSES IN AFT OF FUSELAGE. (STRIP LIGHTING) (FAA). INSTALLED RED STRIP IN AFT TRACK LIGHTING IAW DC-9 MM 33-50-0
- [SDR GTIA9901242](https://openairdocs.org/sdr/GTIA9901242), Dec 23, 1999: POWER SUPPLY. FAILED. DTW - FLT 570 - LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT EXTERIOR EMERGENCY LIGHT POWER SUPPLY IAW 24-21-00. OPS CHECKED NORMAL. (M)
- [SDR GTIA9901241](https://openairdocs.org/sdr/GTIA9901241), Dec 23, 1999: LIGHT. INOPERATIVE. CLE - FLT 541 - LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. PLACED EMERGENCY LIGHT ON DMI 539. REF MEL 33-20 CAT 'B'. (M)
- [SDR GTIA9901210](https://openairdocs.org/sdr/GTIA9901210), Nov 21, 1999: BATTERY PACK. DISCHARGED. CLE - FLT 541 - LEFT EXTENSION EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY PACK. OPS CK GOOD. (X)
- [SDR GTIA9901198](https://openairdocs.org/sdr/GTIA9901198), Nov 6, 1999: BATTERY PACK. DISCHARGED. MYR - FLT 257 - OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 2 AND 4. REMOVED AND REPLACED BATTERY PACK AT B5-24 IAW MM 33-53-0, OPS CHECK GOOD. (M)
- [SDR GTIA9900119](https://openairdocs.org/sdr/GTIA9900119), Nov 3, 1999: CONNECTOR. DISCONNECTED. MYR - FLT 257 - LEFT NACELLE EMERGENCY LIGHT WILL NOT ILLUMINATE. FOUND CANNON PLUG UNATTACHED FROM BATTERY PACK. LOCKED CANNON PLUG ON BATTERY. OPS CHECKED GOO
- [SDR GTIA9901160](https://openairdocs.org/sdr/GTIA9901160), Oct 13, 1999: LIGHT. LOOSE. DTW - FLOOR TRACK LIGHTING INOPERATIVE, RED STRIP NEAR FORWARD GALLEY. RECONNECTED FLOOR TRACK LIGHTING NEAR FORWARD GALLEY. SYSTEM OPERATION CHECKS GOOD IAW MM
- [SDR GTIA9901057](https://openairdocs.org/sdr/GTIA9901057), Jun 16, 1999: JAMB. CRACKED. MHV - LOWER AFT CORNER OF FORWARD CARGO PIT DOOR JAMB HAS A CRACK APPROX 2 INCH LONGERON IN THE TORQUE BOX. REMOVED DAMAGED AREA PER ENGINEERING AVQ-XXX-99-0001
- [SDR GTIA9901042](https://openairdocs.org/sdr/GTIA9901042), Jun 16, 1999: LONGERON. CRACKED. MHV - FOUND STATION 237-277 STRINGER 16L AND STATION 237-323 STRINGER 17L LONGERONS CRACKED AT FRAME ATTACH POINTS. REMOVED AND REPLACED STRINGER 16L FROM STATI
- [SDR GTIA9901053](https://openairdocs.org/sdr/GTIA9901053), Jun 15, 1999: SKIN. MISREPAIRED. MHV - VERTICAL STABILIZER L/E ASSY AT STATION 2 FS 52.300 THERE IS AN EXISTING REPAIR THAT IS BLENDED AND FILLED WITH EPOXY 4 COUNTER SINKS BONDO HAS FALLEN OUT
- [SDR GTIA9901056](https://openairdocs.org/sdr/GTIA9901056), Jun 13, 1999: SKIN. SCRAPED. MHV - REF SPIRIT CARRY OVER NR 0097 SKIN SCRAPES APPROX 1 FT AFT OF FORWARD BAGGAGE DOOR. NDT PERFORMED, NO CRACKS NOTED. LIGHTLY BLENDED AREA AS REQUIRED PER S
- [SDR GTIA9901045](https://openairdocs.org/sdr/GTIA9901045), Jun 13, 1999: SKIN. GOUGED. MHV - W/O'S A096-503-F032, F034, F029 SKIN DENTS AND GOUGE STATION 229 TO STATION 305 APPROX TO BE WORKED ON THIS NON-ROUTINE. REMOVED DENTS AND GOUGES AT STATI
- [SDR GTIA9901055](https://openairdocs.org/sdr/GTIA9901055), Jun 12, 1999: FLOORBEAM. DAMAGED. MHV - FLOORBEAM REPAIR AT STATION 237.5. MACHINED FLOORBEAM REPAIR PER DWG NR 53-9803-1. (M)
- [SDR GTIA9901048](https://openairdocs.org/sdr/GTIA9901048), Jun 12, 1999: CLIP. CRACKED. MHV - FOUND STATION 1219-1244 RT RBL 24 UPPERMOST CLIP UNDER VENT BOX CRACKED COMPLETELY THROUGH AFT ACCESSORY AREA. INSTALLED NEW CLIP AS PER SRM 51-10-1. (M)
- [SDR GTIA9901043](https://openairdocs.org/sdr/GTIA9901043), Jun 12, 1999: SKIN. CRACKED. MHV - REF CARRY OVER ITEM NR 0154 AT FS 1123 NON PRESSURIZED SKIN AT LONGERON 10R, THERE IS A 3 INCH CRACK WITH A CLASS III TEMP REPAIR INSTALLED. CUTOUT DAMAGE
- [SDR GTIA9901054](https://openairdocs.org/sdr/GTIA9901054), Jun 11, 1999: JAMB. DAMAGED. MHV - LOWER CARGO DOOR JAMB PAN REQ 2 EACH -19 AND -21 SPLICE ANGLE REPAIR. FABRICATED ANGLES -19 AND -21 PER DC9 IAW SRM 53-05 PAGE 107 AND 114 FIG 44 SHT 5 SE
- [SDR GTIA9901040](https://openairdocs.org/sdr/GTIA9901040), Jun 11, 1999: FLOORBEAM. CRACKED. MHV - E/E BAY STATION 180 UPPER FLOORBEAM AT BL 0 AFT ANGLE CRACKED AND WEB BOW. REMOVED DAMAGED ANGLE FABRICATED NEW ANGLE FROM 7075T6.032 PO NR 84365 ALODINED
- [SDR GTIA9901052](https://openairdocs.org/sdr/GTIA9901052), Jun 10, 1999: BULKHEAD ANGLE. CORRODED. MHV - T-ANGLE ON BULKHEAD AT FS 1127 RUNNING FROM LONG L6 AND R6 HAS 3 GROUND OUT AREAS AND CORROSION IN EACH AREA. REMOVED AND REPLACED T-ANGLE PER SRM 51-10-1
- [SDR GTIA9901051](https://openairdocs.org/sdr/GTIA9901051), Jun 10, 1999: BULKHEAD T. CORRODED. MHV - T-EXTRUSION AT FS 1127 BULKHEAD IS CORRODED BEYOND USE. MACHINED T-EXTRUSION PER DC9 SRM 51-10 AND EXAMPLE ISSUED TO FLOOR IN BLANK CONDITION LOCATED AND 
- [SDR GTIA9901047](https://openairdocs.org/sdr/GTIA9901047), Jun 10, 1999: BULKHEAD DOUBLER. CRACKED. MHV - STATION 1219-1244 FORWARD OF CANTED BULKHEAD DOUBLER WHERE HARNESS GOES THROUGH IS EXFOLIATING AND CRACKED AFT ACCESSORY AREA. FABRICATED NEW DOUBLER AND 
- [SDR GTIA9901046](https://openairdocs.org/sdr/GTIA9901046), Jun 10, 1999: DOUBLER. CRACKED. MHV - AS MARKED EDDY CURRENT INSPECTION REVEALS A CRACK ON THE FWD PART OF DOUBLER FROM THE FASTENER HOLE TO THE END ON UPPER ANTI-COLLOSION LIGHT. RADIUS OUT C
- [SDR GTIA9901044](https://openairdocs.org/sdr/GTIA9901044), Jun 10, 1999: LONGERON. CRACKED. MHV - FORWARD FUSELAGE STATION NR 200 AT LONGERON 24 LONGERON CRACKED. REMOVED CRACKED LONGERON FROM STATION 190 TO STATION 228. FABRICATED LOCATED AND DRILLED 
- [SDR GTIA9901041](https://openairdocs.org/sdr/GTIA9901041), Jun 10, 1999: FLOORBEAM. CRACKED. MHV - E/E BAY STATION 180 LBL 20 FLOORBEAM CRACKED 3 PLACES FORWARD SIDE OF WEB. FABRICATED REPAIR DOUBLER PER SRM 53-05 PAGE 227 AND 247 FIG 17 FROM 7075T6.032
- [SDR GTIA9901039](https://openairdocs.org/sdr/GTIA9901039), Jun 10, 1999: FLOORBEAM. CRACKED. MHV - E/E BAY STATION 180 LBL 22 FLOORBEAM WEB CRACKED FORWARD SIDE AND ANGLE ON AFT SIDE CRACKED. FABRICATED DOUBLER IW DC9 SRM 53-05 PAGE 227. TREATED AND PRI
- [SDR GTIA9901036](https://openairdocs.org/sdr/GTIA9901036), Jun 9, 1999: ANGLE. CRACKED. MHV - FOUND STATION 1041 LEFT SIDE A/C AFT SIDE OF FRAME ANGLE (FRAME TO LONGERON) AT LONGERON NR 17 CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-01 PAGE 1 AP
- [SDR GTIA9901058](https://openairdocs.org/sdr/GTIA9901058), Jun 8, 1999: FLOORBEAM. CRACKED. MHV - FORWARD CARGO CABIN FLOORBEAM STATION 237 LEFT 10 INCH CRACK IN FLOORBEAM AT SERVO FULLY BRACKET EXISTING REPAIR NEEDS FURTHER EVALUATION. COMPLETED REPAI
- [SDR GTIA9901050](https://openairdocs.org/sdr/GTIA9901050), Jun 8, 1999: ANGLE. CRACKED. MHV - RIGHT WING ROOT AREA .5 INCH CRACK INDICATION ON ANGLE 5910465-340 TO CENTER WING BOX APPROX BODY STATION 710. NDT VERIFY CRACK IN ANGLE. REMOVED AND REPL
- [SDR GTIA9901035](https://openairdocs.org/sdr/GTIA9901035), Jun 8, 1999: LONGERON. CRACKED. MHV - FOUND STATION 1041, STATION 1051 LONGERON NR 17 CRACKED BOTH MARKED IN RED. REMOVED AND REPLACED LONGERON NR 17 STATION 1041 AND 1051 AND SHOVEL CUPS PER 
- [SDR GTIA9901038](https://openairdocs.org/sdr/GTIA9901038), Jun 2, 1999: SKIN. DENTED. MHV - FORWARD FUSELAGE SKIN AT STATION 313 NEAR BOTTOM OF FUSELAGE HAS A 1.5 INCH BY 1 INCH DENT. CUT OUT DAMAGE IAW DC9 SRM 53-04 FIG 38 VIEW 1. FABRICATED DOU
- [SDR GTIA9900944](https://openairdocs.org/sdr/GTIA9900944), Jun 2, 1999: BATTERY PACK. DISCHARGED. MHV - FLT 951A - COCKPIT OVERHEAD EMERGENCY LIGHT OUT. TROUBLESHOT SYSTEM, FOUND EMERGENCY BATTERY PACK WITH DEAD BATTERIES. REPLACED BATTERIES ON JOB CARD. LIG
- [SDR GTIA9901037](https://openairdocs.org/sdr/GTIA9901037), May 28, 1999: CLIP. CRACKED. MHV - STATION 1041 LEFT SIDE A/C FORWARD SIDE OF FRAME SHEER CLIP BETWEEN LONGERON 16 AND 17 CRACKED. REMOVED AND REPLACED SHEAR CLIP IAW SRM 51-01 PAGE 1 APPLI

All 79: https://openairdocs.org/deregistered/N130NK-2004-06-07/reports.md

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