# Service difficulty reports: N130NK, cancelled Jun 7, 2004

A list on [N130NK, cancelled Jun 7, 2004](https://openairdocs.org/deregistered/N130NK-2004-06-07.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 · 79 reports

- [SDR GTIA030274](https://openairdocs.org/sdr/GTIA030274.md): Slide · dislodged · Apr 22, 2003 · N130NK · Doug DC941 · Escape Slide
  > PBI - FLT 330 - LEFT SIDE PACK FELL OFF. REINSTALLED SLIDE/COVER. (M)
- [SDR GTIA030243](https://openairdocs.org/sdr/GTIA030243.md): Slide · dislodged · Apr 2, 2003 · N130NK · Doug DC941 · Escape Slide
  > EMERGENCY SLIDE PACK FELL OFF. REINSTALLED LANYARD SLIDE CHECK OK. (M)
- [SDR GTIA030241](https://openairdocs.org/sdr/GTIA030241.md): Liner · cracked · Mar 31, 2003 · N130NK · Doug DC941 · Engine Exhaust System
  > 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 CHECK GOOD. (M)
- [SDR GTIA030116](https://openairdocs.org/sdr/GTIA030116.md): Flashlight · inoperative · Mar 2, 2003 · N130NK · Doug DC941 · Emergency Equipment
  > FORWARD F/A HANDHELD EMERGENCY LIGHT, INOPERATIVE. REMOVED AND REPLACED FWD HANDHELD EMERGENCY LIGHT. OPS CHECK GOOD.
- [SDR GTIA030115](https://openairdocs.org/sdr/GTIA030115.md): Sign · inoperative · Mar 2, 2003 · N130NK · Doug DC941 · Emergency Lighting
  > TAILCONE INTERIOR LUMINESCENT EXIT SIGN INOPERATIVE. REMOVED AND REPLACED TAILCONE INTERION LUMINESCENT EXIT SIGN. OPS CHECK GOOD.
- [SDR GTIA030003](https://openairdocs.org/sdr/GTIA030003.md): Skin · cracked · Jan 14, 2003 · N130NK · Doug DC941 · Fuselage Main, Plate/Skin
  > 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 LONGERON NR 26R JUST AFT OF CARGO PIT DOOR. (M)
- [SDR GTIA030019](https://openairdocs.org/sdr/GTIA030019.md): Oil System · fluctuates · Jan 6, 2003 · N130NK · Doug DC941 · Engine Oil System (Airframe Furnished)
  > 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.md): Isolator · defective · Oct 1, 2002 · N130NK · Doug DC941 · Engine Mount Section
  > 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.md): Isolator · defective · Oct 1, 2002 · N130NK · Doug DC941 · Engine Mount Section
  > 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.md): Combust Chamber · worn · Oct 1, 2002 · N130NK · Doug DC941 · Turbine Engine Combustion Section
  > 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 REPACED DURING SHOP VISIT.
- [SDR GTIA020292](https://openairdocs.org/sdr/GTIA020292.md): Autopilot Sys · malfunctioned · Apr 17, 2002 · N130NK · Doug DC9 · Autopilot System
  > 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.md): Control Unit · inoperative · Apr 23, 2001 · N130NK · Doug DC941 · Autopilot System
  > 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.md): Servo · malfunctioned · Apr 14, 2001 · N130NK · Doug DC941 · Autopilot Main Servo
  > 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 AMEND NR 1 1730Z HR PLACARDED ELEV SERVO SWITCH. (M)
- [SDR GTIA010113](https://openairdocs.org/sdr/GTIA010113.md): Autopilot Sys · flutter · Apr 12, 2001 · N130NK · Doug DC941 · Autopilot System
  > 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 CAT C DUE 4-22-01 AMEND NR 1 1115Z HK. (M)
- [SDR GTIA010097](https://openairdocs.org/sdr/GTIA010097.md): Autopilot Sys · malfunctioned · Apr 7, 2001 · N130NK · Doug DC941 · Autopilot System
  > 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 BOTH ON GROUND AND IN FLIGHT. NO FAULT FOUND. THIS CLEARS DMI NR 0001619-1. PLACARDS REMOVED IAW
- [SDR GTIA010096](https://openairdocs.org/sdr/GTIA010096.md): Autopilot Sys · vibration · Apr 6, 2001 · N130NK · Doug DC941 · Autopilot System
  > 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 22-10-00. THIS CLEARS DMI NR 000165-1. PLACARDS REMOVED. (M)
- [SDR GTIA010047](https://openairdocs.org/sdr/GTIA010047.md): Tail Cone · dislodged · Feb 24, 2001 · N130NK · Doug DC941 · Aerodynamic Fairings
  > MYR - FLT 303 - TAILCONE CAME OFF ON LANDING. TAILCONE RELEASE SYSTEM EVACUATED AND REPAIRED BY BOEING. REPLACED EXTERIOR CABLE FITTING AND RIGHT LOWER LOCKING PIN. TAILCONE WAS FIT FOR CLEARANCES AND DROP CHECK PERFORMED AS PER DC-9 MM 53-50-3. (M)
- [SDR GTIA010043](https://openairdocs.org/sdr/GTIA010043.md): Tail Cone · separated · Feb 23, 2001 · N130NK · Doug DC941 · Aerodynamic Fairings
  > 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.md): Wire · broken · Jun 20, 2000 · N130NK · Doug DC941 · Light System Wiring
  > 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.md): Lens · missing · Mar 13, 2000 · N130NK · Doug DC941 · Emergency Lighting
  > 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. OPS CHECKS GOOD. (X)
- [SDR GTIA9901242](https://openairdocs.org/sdr/GTIA9901242.md): Power Supply · failed · Dec 23, 1999 · N130NK · Doug DC941 · Emergency Lighting
  > 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.md): Light · inoperative · Dec 23, 1999 · N130NK · Doug DC941 · Emergency Lighting
  > 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.md): Battery Pack · discharged · Nov 21, 1999 · N130NK · Doug DC941 · Emergency Lighting
  > CLE - FLT 541 - LEFT EXTENSION EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY PACK. OPS CK GOOD. (X)
- [SDR GTIA9901198](https://openairdocs.org/sdr/GTIA9901198.md): Battery Pack · discharged · Nov 6, 1999 · N130NK · Doug DC941 · Emergency Lighting
  > 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.md): Connector · disconnected · Nov 3, 1999 · N130NK · Doug DC941 · Fire Protection System
  > MYR - FLT 257 - LEFT NACELLE EMERGENCY LIGHT WILL NOT ILLUMINATE. FOUND CANNON PLUG UNATTACHED FROM BATTERY PACK. LOCKED CANNON PLUG ON BATTERY. OPS CHECKED GOOD. (M)
- [SDR GTIA9901160](https://openairdocs.org/sdr/GTIA9901160.md): Light · loose · Oct 13, 1999 · N130NK · Doug DC941 · Emergency Lighting
  > DTW - FLOOR TRACK LIGHTING INOPERATIVE, RED STRIP NEAR FORWARD GALLEY. RECONNECTED FLOOR TRACK LIGHTING NEAR FORWARD GALLEY. SYSTEM OPERATION CHECKS GOOD IAW MM 33-53-00. (M)
- [SDR GTIA9901057](https://openairdocs.org/sdr/GTIA9901057.md): Jamb · cracked · Jun 16, 1999 · N130NK · Doug DC941 · Fuselage Miscellaneous Structure
  > 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-99-0001RR AND SPLICED IN NEW CARGO DOOR PAN PER DC9 -40 SRM 53-05 FIG 44. (M)
- [SDR GTIA9901042](https://openairdocs.org/sdr/GTIA9901042.md): Longeron · cracked · Jun 16, 1999 · N130NK · Doug DC941 · Fuselage Main, Longeron/Stringer
  > 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 STATION 237-277 STRINGER 17L FROM 237-323 IAW DC940 SRM 53-02 FIG 18. (M)
- [SDR GTIA9901053](https://openairdocs.org/sdr/GTIA9901053.md): Skin · misrepaired · Jun 15, 1999 · N130NK · Doug DC941 · Vertical Stabilizer, Plate/Skin
  > 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. CUT OFF BONDED FINGER DOUBLER FABRICATED TITANIUM REPAIR DOUBLER PER ENG G INSTRUCTION (DRAWING)
- [SDR GTIA9901056](https://openairdocs.org/sdr/GTIA9901056.md): Skin · scraped · Jun 13, 1999 · N130NK · Doug DC941 · Fuselage Main, Plate/Skin
  > 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 SRM 53-04 FIG 38 SHT 2 FUSELAGE SKIN ALODINE AND PRIME IAW DC9 SRM 51-10-3. (M)
- [SDR GTIA9901045](https://openairdocs.org/sdr/GTIA9901045.md): Skin · gouged · Jun 13, 1999 · N130NK · Doug DC941 · Fuselage Main, Plate/Skin
  > 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 STATION 229 TO STATION 305 APPROX BETWEEN STRINGER 16L AND 17L AND REPAIRED PER DRAWING NR 53-99294-1.
- [SDR GTIA9901055](https://openairdocs.org/sdr/GTIA9901055.md): Floorbeam · damaged · Jun 12, 1999 · N130NK · Doug DC941 · Fuselage Main, Floor Beam
  > MHV - FLOORBEAM REPAIR AT STATION 237.5. MACHINED FLOORBEAM REPAIR PER DWG NR 53-9803-1. (M)
- [SDR GTIA9901048](https://openairdocs.org/sdr/GTIA9901048.md): Clip · cracked · Jun 12, 1999 · N130NK · Doug DC941 · Fuselage Miscellaneous Structure
  > 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.md): Skin · cracked · Jun 12, 1999 · N130NK · Doug DC941 · Fuselage Main, Plate/Skin
  > 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 AREA IAW DC9 SRM 53-01 FIG 4 SHT 2. FABRICATED DOUBLER AND PLATE IAW DC9 SRM 53-01 FIG 4 SHT 3.
- [SDR GTIA9901054](https://openairdocs.org/sdr/GTIA9901054.md): Jamb · damaged · Jun 11, 1999 · N130NK · Doug DC941 · Fuselage Miscellaneous Structure
  > 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 SECTION G-G. (M)
- [SDR GTIA9901040](https://openairdocs.org/sdr/GTIA9901040.md): Floorbeam · cracked · Jun 11, 1999 · N130NK · Doug DC941 · Fuselage Main, Floor Beam
  > 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 AND PRIMED ANGLE IAW SRM 51-10-3 AND INSTALLED ANGLE IAW DC9 SRM 51-30-2. (M)
- [SDR GTIA9901052](https://openairdocs.org/sdr/GTIA9901052.md): Bulkhead Angle · corroded · Jun 10, 1999 · N130NK · Doug DC941 · Fuselage Main, Bulkhead
  > 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 AND 51-30-5 AND 51-30-2. (M)
- [SDR GTIA9901051](https://openairdocs.org/sdr/GTIA9901051.md): Bulkhead T · corroded · Jun 10, 1999 · N130NK · Doug DC941 · Fuselage Main, Bulkhead
  > 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 DRILL REF A096S03L053. (M)
- [SDR GTIA9901047](https://openairdocs.org/sdr/GTIA9901047.md): Bulkhead Doubler · cracked · Jun 10, 1999 · N130NK · Doug DC941 · Fuselage Main, Bulkhead
  > MHV - STATION 1219-1244 FORWARD OF CANTED BULKHEAD DOUBLER WHERE HARNESS GOES THROUGH IS EXFOLIATING AND CRACKED AFT ACCESSORY AREA. FABRICATED NEW DOUBLER AND INSTALLED IAW DC9 SRM 53-01 FIG 4 SHT 3. (M)
- [SDR GTIA9901046](https://openairdocs.org/sdr/GTIA9901046.md): Doubler · cracked · Jun 10, 1999 · N130NK · Doug DC941 · Fuselage Miscellaneous Structure
  > 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 CRACK, CRACK REMOVAL BOUGHT OFF BY NDT TRIMMED -17 SHIM AND LAYOUT OF -11 DOUBLER PER SB 53-186 PAGE
- [SDR GTIA9901044](https://openairdocs.org/sdr/GTIA9901044.md): Longeron · cracked · Jun 10, 1999 · N130NK · Doug DC941 · Fuselage Main, Keel
  > MHV - FORWARD FUSELAGE STATION NR 200 AT LONGERON 24 LONGERON CRACKED. REMOVED CRACKED LONGERON FROM STATION 190 TO STATION 228. FABRICATED LOCATED AND DRILLED LONGERON 24 AND SPLICE PER DC9 SRM 53-2. ALODINED AND PRIMED PER DC9 SRM 51-10-3. INSTALLED PART
- [SDR GTIA9901041](https://openairdocs.org/sdr/GTIA9901041.md): Floorbeam · cracked · Jun 10, 1999 · N130NK · Doug DC941 · Fuselage Main, Floor Beam
  > 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 PO NR 84365 ALODINED AND PRIMED PARTS PER SRM 51-10-3 AND INSTALLED DOUBLER IAW DC9 SRM 51-30-2.
- [SDR GTIA9901039](https://openairdocs.org/sdr/GTIA9901039.md): Floorbeam · cracked · Jun 10, 1999 · N130NK · Doug DC941 · Fuselage Main, Floor Beam
  > 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 PRIMED DOUBLER IAW DC9 SRM 51-10-3. INSTALLED DOUBLER IAW DC9 SRM 53-05 PAGE 227. (M)
- [SDR GTIA9901036](https://openairdocs.org/sdr/GTIA9901036.md): Angle · cracked · Jun 9, 1999 · N130NK · Doug DC941 · Fuselage Miscellaneous Structure
  > 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 APPLIED SEALANT IAW SRM 51-20-0 PAGE 1 AND PAGE 13 FIG 3. INSTALLED FASTENERS IAW SRM 51-01 PAGE 1 A
- [SDR GTIA9901058](https://openairdocs.org/sdr/GTIA9901058.md): Floorbeam · cracked · Jun 8, 1999 · N130NK · Doug DC941 · Fuselage Main, Floor Beam
  > MHV - FORWARD CARGO CABIN FLOORBEAM STATION 237 LEFT 10 INCH CRACK IN FLOORBEAM AT SERVO FULLY BRACKET EXISTING REPAIR NEEDS FURTHER EVALUATION. COMPLETED REPAIR IAW DC9 SRM 53-05 AND RESEMBLE CARGO PANELS. (M)
- [SDR GTIA9901050](https://openairdocs.org/sdr/GTIA9901050.md): Angle · cracked · Jun 8, 1999 · N130NK · Doug DC941 · Fuselage Miscellaneous Structure
  > 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 REPLACED ANGLE AIW DC9 SRM 51-10-2, 51-10-4 AND 51-30-5. REINSTALLED FAIRINGS 3 PANELS OPENED FOR ACC
- [SDR GTIA9901035](https://openairdocs.org/sdr/GTIA9901035.md): Longeron · cracked · Jun 8, 1999 · N130NK · Doug DC941 · Fuselage Main, Longeron/Stringer
  > 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 SRM 51-10-1 AND 51-30-2 LONGERON INSTALLED USING EXISTING SPLICES. (M)
- [SDR GTIA9901038](https://openairdocs.org/sdr/GTIA9901038.md): Skin · dented · Jun 2, 1999 · N130NK · Doug DC941 · Fuselage Main, Plate/Skin
  > 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 DOUBLER AND FILLER INSTALLED REPAIR COMPLETE IAW SRM 53-04 FIG 38 AND DC9 SRM 51-30-2. (M)
- [SDR GTIA9900944](https://openairdocs.org/sdr/GTIA9900944.md): Battery Pack · discharged · Jun 2, 1999 · N130NK · Doug DC941 · Emergency Lighting
  > MHV - FLT 951A - COCKPIT OVERHEAD EMERGENCY LIGHT OUT. TROUBLESHOT SYSTEM, FOUND EMERGENCY BATTERY PACK WITH DEAD BATTERIES. REPLACED BATTERIES ON JOB CARD. LIGHTS WORK CARD. (X)
- [SDR GTIA9901037](https://openairdocs.org/sdr/GTIA9901037.md): Clip · cracked · May 28, 1999 · N130NK · Doug DC941 · Fuselage Miscellaneous Structure
  > 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 APPLIED SEALANT IAW DC9 SRM 51-20-0 PAGE 1 AND PAGE 13 FIG 3. INSTALLED FASTENERS IAW SRM DC9 51-30-2 P

Next page: https://openairdocs.org/deregistered/N130NK-2004-06-07/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 = 'N130NK' AND deregistration_id = 'N130NK-2004-06-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N130NK-2004-06-07/reports

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