# Service difficulty reports: N6815, cancelled Jun 21, 2006

A list on [N6815, cancelled Jun 21, 2006](https://openairdocs.org/deregistered/N6815-2006-06-21.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 · 67 reports

- [SDR EISA20010134](https://openairdocs.org/sdr/EISA20010134.md): Structure · corroded · Dec 1, 2001 · N6815 · Boeing 727223 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT FWD LT CORNER NLG TUNNEL BOX AT STA 294.5 LBL 14. REMOVED DAMAGED SECTION AND INSTALLED REPAIR IAW EO 01-294 REV A.
- [SDR EISA20010098](https://openairdocs.org/sdr/EISA20010098.md): Light · inoperative · Jun 19, 2001 · N6815 · Boeing 727223 · Emergency Lighting
  > ON POSTFLIGHT INSPECTION FOUND COCKPIT EMERGENCY LIGHT INOP.CORRECTIVE ACTION: REPLACED COCKPIT EMERGENCY EXIT LIGHT PER MM REF 33-50
- [SDR EISA20010084](https://openairdocs.org/sdr/EISA20010084.md): Light · inoperative · May 21, 2001 · N6815 · Boeing 727223 · Emergency Lighting
  > L-1 EMERGENCY EXIT LIGHT WILL NOT CHARGE.
- [SDR EISA20010071](https://openairdocs.org/sdr/EISA20010071.md): Seat Track · cracked · Mar 5, 2001 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE B-CHECK INSPECTION FOUND CRACK IN SEAT TRACK BETWEEN BS 520 AND BS 540 AT LBL 45. FABRICATED AND INSTALLED SEAT TRACK SPLICE, ALODINED AND PRIMED IAW SRM 51-10-2, 53-10-5 FIG 1, AND SOPM 20-50-01.
- [SDR EISA20000153](https://openairdocs.org/sdr/EISA20000153.md): Actuator · inoperative · Sep 26, 2000 · N6815 · Boeing 727223 · Leading Edge Slat Actuator
  > DURING CLIMBOUT AT FL 190, THE AMBER LEADING EDGE FLAP LIGHT ILLUMINATED. CONFIRMED WITH FE LED PANEL. RIGHT NR 6 SLAT INDICATOR SHOWED SLAT NOT RETRACTED. RETURNED TO (AUS) PER COMPANY REQUEST, EMERGENCY CHECKLIST COMPLIED WITH. REMOVED AND REPLACED NR 6
- [SDR EISA20000123](https://openairdocs.org/sdr/EISA20000123.md): Skin · delaminated · Aug 10, 2000 · N6815 · Boeing 727223 · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSPECTION, LEFT WING I/B AFT FLAP HAS NUMEROUS DELAMINATED DINGS ON I/B LOWER SKIN. REMOVED DAMAGE, CLEANED, PRIMED AREA, BONDED FIBERGLASS OVERLAYS, ALODINED AND PRIMED SURROUNDING AREA. WORK DONE IAW B727 SRM 51-40-6 AND B727 MM 51-2
- [SDR EISA20000122](https://openairdocs.org/sdr/EISA20000122.md): Skin · delaminated · Aug 10, 2000 · N6815 · Boeing 727223 · Leading Edge Devices
  > DURING ROUTINE C-CHECK INSPECTION, I/B FORE FLAP DELAMINATED ON I/B LOWER SIDE. REMOVED DELAMINATED COVER, CLEANED, PREPPED AND POTTED CORE. BONDED FIBERGLASS OVERLAY, ALODINED AND PRIMED SURROUNDING AREA. WORK DONE IAW B727 SRM 51-40-6 AND 51-10-2.
- [SDR EISA20000121](https://openairdocs.org/sdr/EISA20000121.md): Skin · delaminated · Aug 10, 2000 · N6815 · Boeing 727223 · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSPECTION, RIGHT I/B FLAP DELAMINATED FWD SIDE, I/B. REMOVED DELAMINATED EXISTING REPAIR, CLEANED, PREPPED AND PITTED CORE, BONDED FIBERGLASS REPAIR, ALODINED AND PRIMED AREA. WORK DONE IAW B727 SRM 51-40-6 AND 51-10-2.
- [SDR EISA20000120](https://openairdocs.org/sdr/EISA20000120.md): Skin · delaminated · Aug 10, 2000 · N6815 · Boeing 727223 · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSPECTION, RIGHT O/B FLAP I/B END DELAMINATED. REMOVED OLD REPAIR, CUT, BONDED, CURED, BLENDED AND PRIMED IAW B727 SRM 51-40-6, 51-10-2. PAINTED IAW B727 MM 51-20-151.
- [SDR EISA20000106](https://openairdocs.org/sdr/EISA20000106.md): Fitting · cracked · Aug 10, 2000 · N6815 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, FITTING CRACKED AT STA 920 RT JUST ABOVE STR 18-A. REMOVED FITTING, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW FITTING IAW B727 SRM 51-30-5 AND 51-30-2.
- [SDR EISA20000107](https://openairdocs.org/sdr/EISA20000107.md): Frame · cracked · Aug 10, 2000 · N6815 · Boeing 727223 · Fuselage Main, Frame
  > DURING ROUTINE C-CHECK INSP, FRAME CRACKED AT STATION 560 STRINGER 17. FABRICATED DOUBLER AND FILLER, ALODINED PRIMED AND INSTALLED IAW 727 SRM 53-10-2, 51-10-2.
- [SDR EISA20000124](https://openairdocs.org/sdr/EISA20000124.md): Actuator · cracked · Aug 9, 2000 · N6815 · Boeing 727223 · Entrance Stairs
  > DURING ROUTINE C-CHECK INSPECTION, ACTUATOR FOR AFT AIRSTAIRS HAS A TWO INCH CRACK. REMOVED AND REPLACED ACTUATOR FOR AFT AIRSTAIRS IAW B727 MM 53-62-71.
- [SDR EISA20000119](https://openairdocs.org/sdr/EISA20000119.md): Bushing · worn · Aug 9, 2000 · N6815 · Boeing 727223 · Main Landing Gear
  > DURING ROUTINE C-CHECK INSPECTION, HOLES IN BRAKE MOUNTING FLANGES ARE TOO LARGE TO ACCEPT BRAKE ASSY. FABRICATED BUSHINGS, CAD PLATED AND INSTALLED BUSHINGS, ON I/B AND O/B IAW BOEING SERVICE BULLETIN 727-32-241.
- [SDR EISA20000118](https://openairdocs.org/sdr/EISA20000118.md): Airstair · cracked · Aug 9, 2000 · N6815 · Boeing 727223 · Entrance Stairs
  > DURING ROUTINE C-CHECK INSPECTION, CHORD CRACKED RT SIDE OF VENTRAL STAIRS AT FWD AIRSTAIR SUPPORT FITTING STA 1263. REMOVED DAMAGED SECTION OF VENTRICAL WEB, HORIZONTAL WEB, CHORD REPLACED WITH NEW FROM MOD KIT 65C27136-12 PER BAC 65C27136.
- [SDR EISA20000117](https://openairdocs.org/sdr/EISA20000117.md): Web · corroded · Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, EXFOLIATED CORROSION LOWER 4H CORNER ON CUSP LINE AT 1183 BULKHEAD. FABRICATED NEW CUSP WEB, RECEIVED NEW FITTING, LOCATED, DRILLED AND INSTALLED IAW B727 SRM 51-20-1, 51-10-2 AND 51-30-2.
- [SDR EISA20000115](https://openairdocs.org/sdr/EISA20000115.md): Seat Track · cracked · Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSPECTION, LEFT O/B SEAT TRACK CRACKED STA 420. REMOVED SECTION OF DAMAGED SEAT TRACK IAW B727 SRM 53-10-5. FABRICATED NEW SEAT TRACK IAW B727 SRM 53-10-5. TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK SPLICE IAW B72
- [SDR EISA20000114](https://openairdocs.org/sdr/EISA20000114.md): Seat Track · corroded · Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSPECTION, SEAT TRACK SPLICE FROM BS 500 - 680 RBL 45 HAS EXFOLIATED CORROSION THROUGHOUT TRACK ON LOBES AND INSIDE CENTER OF TRACKS AS MARKED. FABRICATED SEAT TRACK SPLICE IAW B727 SRM 53-10-5, ALODINED AND PRIMED IAW SRM 51-10-6, INS
- [SDR EISA20000113](https://openairdocs.org/sdr/EISA20000113.md): Structure · cracked · Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Main, Structure
  > DURING ROUTINE C-CHECK INSPECTION, CRACK INDICATIONS NOTED AT RT SIDE 760.95 HOLES, TOTAL OF 4 HOLES AS MARKED. INSTALLED BOEING PREVENTATIVE MOD KIT 65C36279-36 PER BOEING SERVICE BULLETIN 727-53-0197, INSTALLED 2 DOUBLERS AND 1 STRAP.
- [SDR EISA20000112](https://openairdocs.org/sdr/EISA20000112.md): Skin · dented · Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Main, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, DENT IN FUSELAGE AT STA 720B STR L10. CUT DAMAGED SKIN AREA, FABRICATED REPAIR PLATE AND FILLER IAW B727 SRM 53-30-3, ALODINED AND PRIMED IAW B727 SRM 51-10-2 AND 51-20-4. INSTALLED IAW B727 SRM 53-30-0.
- [SDR EISA20000111](https://openairdocs.org/sdr/EISA20000111.md): Strap · cracked · Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Main, Structure
  > DURING ROUTINE C-CHECK INSPECTION, FUSELAGE EXTERIOR SUPPORT STRAP HAS CRACKED FLANGE STR 18-A STA 940. REMOVED DAMGED SUPPORT, RECEIVED NEW SECTION OF SUPPORT, RECEIVED MOD KIT, LOCATED, DRILLED AND INSTALLED IAW B727 SRM 51-30-2, 51-30-5 AND BAC DWG 65C2906
- [SDR EISA20000110](https://openairdocs.org/sdr/EISA20000110.md): Skin · delaminated · Aug 9, 2000 · N6815 · Boeing 727223 · Trailing Edge Flaps
  > DURING ROUTINE C-CHECK INSPECTION, RIGHT I/B FLAP DELAMINATED AT SIDE. REMOVED AND REPLACED RIGHT I/B AFT FLAP, ADJUSTMENT, TEST AND OPS CHECK GOOD IAW B727 MM 27-51-2.
- [SDR EISA20000109](https://openairdocs.org/sdr/EISA20000109.md): Bracket · cracked · Aug 9, 2000 · N6815 · Boeing 727223 · Ailerons
  > DURING ROUTINE C-CHECK INSPECTION, RIGHT O/B AILERON LOCKOUT MECHANISM ATTACHING BRACKET IS CRACKED. REMOVED AND REPLACED AILERON LOCKOUT BRACKET. RIGGED RT AILERON LOCKOUT IAW B727 SRM 51-30-2, MM 27-10-121 AND 27-10-131.
- [SDR EISA20000108](https://openairdocs.org/sdr/EISA20000108.md): Angle · cracked · Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, STA 1342 4H ABOVE ATTACH FITTING, ANGLE IS CRACKED. REMOVED CRACKED ANGLE, FABRICATED REPAIR ANGLE AND SPLICE ANGLE, TREATED, PRIMED AND INSTALLED IAW B727 SRM 51-40-3, 51-10-2 AND 51-30-2.
- [SDR EISA20000116](https://openairdocs.org/sdr/EISA20000116.md): Seat Track · corroded · Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE C-CHECK INSPECTION, LT CENTER SEAT TRACK HAS CORROSION STA 837 - 845. RECEIVED NEW SEAT TRACK SPLICE, LOCATED HOLES, COUNTER SUNK AND INSTALLED IAW B727 SRM 51-30-2.
- [SDR 20000057](https://openairdocs.org/sdr/20000057.md): Control Panel · failed · Jul 17, 2000 · N6815 · Boeing 727223 · Cabin Pressure Control System
  > ON TAKEOFF FROM ELP, AIRCRAFT WOULD NOT PRESSURIZE. AIR TURNBACK TO ELP.
- [SDR EISA20010082](https://openairdocs.org/sdr/EISA20010082.md): Wire · broken · May 18, 2000 · N6815 · Boeing 727223 · Landing Gear System Wiring
  > ON APPROACH TO (AUS) GEAR HADLE SELECTED, DOWN NOSE GEAR RED LIGHT DID NOT EXTINGUISH - RECYCLED GEAR OK. CORRECTIVE ACTION: FOUND BROKEN WIRE TO NOSE GEAR DOWN LOCK SWITCH. REPAIRED WIRE AND INDICATION OPS CHECK NORMAL PER M/M 32-00
- [SDR EISA2000046](https://openairdocs.org/sdr/EISA2000046.md): Regulator · failed · May 2, 2000 · N6815 · Boeing 727223 · DC Regulator
  > DURING TAKEOFF, NR 3 BUS TIE LIGHT ILLUMINATED. AFTER TAKEOFF PANEL LIGHT BEGAN TO FLICKER. THEN NR 1 FIELD RELAY AND GENERATOR BREAKER TRIPPED OFF. SMOKE SMELL IN COCKPIT. AIRCRAFT HAD AN OVERWEIGHT LANDING. AIR TURN BACK. REMOVED AND REPLACED VOLTAGE R
- [SDR EISA2000042](https://openairdocs.org/sdr/EISA2000042.md): Landing Gear · malfunctioned · Apr 3, 2000 · N6815 · Boeing 727223 · Nose/Tail Landing Gear
  > NOSE LANDING GEAR TOOK EXCESSIVE AMOUNT OF TIME TO EXTEND AND LOCK. ACCOMPANIED BY A LOUD WHINING NOISE. LUBED NOSE LANDING GEAR. RETRACTION OPERATION CHECK GOOD. (M)
- [SDR EISA99109](https://openairdocs.org/sdr/EISA99109.md): Light · inoperative · May 9, 1999 · N6815 · Boeing 727223 · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN COCKPIT INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT IN COCKPIT IAW BMM 3350. NO DEFECTS NOTED. (M)
- [SDR EISA99031](https://openairdocs.org/sdr/EISA99031.md): Pcu · leaking · Feb 24, 1999 · N6815 · Boeing 727223 · Rudder Control System
  > IMMEDIATELY AFTER TAKEOFF UNCOMMANDED RUDDER INPUT LEFT AND RIGHT. SYSTEM 'A' AND 'B' RUDDER POWER OFF RUDDER INPUT STOPS. REMOVED AND REPLACED UPPER RUDDER PCU IAW MM 27-20-141. (M)
- [SDR EISA98219](https://openairdocs.org/sdr/EISA98219.md): Nut · loose · Sep 9, 1998 · N6815 · Boeing 727223 · Alternator-Generator Drive
  > REJECTED TAKEOFF AT TMP NR 3 GENERATOR TRIPPED OFF LINE ON POWER UP FOR TAKEOFF, CSD LOW OIL LIGHT CAME ON. GENERATED FROM PILOT REPORT. FOUND B-NUT LOOSE ON COOLER, RETORQUED AND SERVICED CSD. LEAK CHECKED OK. (M)
- [SDR EISA98179](https://openairdocs.org/sdr/EISA98179.md): Battery · overheat · Jul 17, 1998 · N6815 · Boeing 727223 · Battery/Charger System
  > WHEN PARKING AIRCRAFT AT EDI, FLIGHT DECK FILLED WITH SMOKE. IT WAS DETERMINED BATTERY WAS OVERHEATING. FIRE DEPARTMENT REMOVED BATTERY FROM AIRCRAFT. GENERATED FROM PILOT REPORT. MAIN BATTERY AND BATTERY CHARGER REPLACED. CHECKED SATISFACTORY IAW MM 24-3
- [SDR EISA98039](https://openairdocs.org/sdr/EISA98039.md): Batteries · discharged · Feb 8, 1998 · N6815 · Boeing 727223 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY DEAD. INSTALLED NEW BATTERIES. (M)
- [SDR EISA97226](https://openairdocs.org/sdr/EISA97226.md): Wire · broken · Nov 12, 1997 · N6815 · Boeing 727223 · Light System Wiring
  > EMERGENCY EXIT 'UNARMED LIGHT' YELLOW LIGHT INOP. REPAIRED BROKEN WIRE, PER STANDARD PRACTICES, OPS CHECK GOOD. (M)
- [SDR EISA97078](https://openairdocs.org/sdr/EISA97078.md): Skin · corroded · Mar 17, 1997 · N6815 · Boeing 727223 · Fuselage Main, Plate/Skin
  > FORWARD PIT HAS CORROSION AND METAL FLAKING ON SKIN LAP JOINT BS 517, STRINGER 26R. FABRICATED FILLER AND DOUBLER PER SRM 53-30-3. (M)
- [SDR EISA97070](https://openairdocs.org/sdr/EISA97070.md): Seat Track · corroded · Mar 17, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 3 LEFT CORRODED AT FS 348.2. REMOVED AND REPLACED SEAT TRACK FORM FS 340 TO 360 PER SRM 53-10-05. (M)
- [SDR EISA97056](https://openairdocs.org/sdr/EISA97056.md): Fitting · corroded · Mar 17, 1997 · N6815 · Boeing 727223 · Ailerons
  > LEFT OUTBOARD AILERON INBOARD HINGE CORRODED AROUND BUSHING. REMOVED AND REPLACED FITTING PER SRM 51-10-1. (M)
- [SDR EISA97044](https://openairdocs.org/sdr/EISA97044.md): Clip · cracked · Mar 15, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous Structure
  > CRACKED STRINGER TIE CLIP AT FS 990 STRINGER 8L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-04. (M)
- [SDR EISA97074](https://openairdocs.org/sdr/EISA97074.md): Splice · gouged · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous Structure
  > STRINGER SPLICE CORRODED ON STRINGER 28R APPROXIMATELY FS 1030. FABRICATED AND INSTALLED NEW SPLICE SECTION PER SRM 53-10-3. (M)
- [SDR EISA97073](https://openairdocs.org/sdr/EISA97073.md): Stringer · corroded · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > STRINGER 28R CORRODED FROM FS 480 AND FORWARD TO E/E BAY DOOR. REPLACED STRINGER SECTION FROM FS 450 TO 480 PER SRM 53-10-3. (M)
- [SDR EISA97072](https://openairdocs.org/sdr/EISA97072.md): Frame · gouged · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Main, Frame
  > FLOOR FRAME UPPER FLANGE GOUGED AT FS 1030 LEFT SIDE OF CENTER SEAT TRACK. FABRICATED AND INSTALLED REPAIR ON FLOOR FRAME AT STATION 1030 IAW SRM 53-10-8. (M)
- [SDR EISA97071](https://openairdocs.org/sdr/EISA97071.md): Seat Track · corroded · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OUTBOARD SEAT TRACK CORRODED AT STATION 700. INSTALLED NEW TRACK SECTION PER SRM 51-30-2. (M)
- [SDR EISA97069](https://openairdocs.org/sdr/EISA97069.md): Angle · cracked · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 1110-1130 BELOW CENTER SEAT TRACK, LOWER ATTACH ANGLE CRACKED IN SEVERAL PLACES. FABRICATED AND INSTALLED NEW PART AND INTERCOSTAL PER SRM 51-30-2. (M)
- [SDR EISA97068](https://openairdocs.org/sdr/EISA97068.md): Angle · cracked · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous Structure
  > .75 INCH CRACK, AFT SIDE OF FS 1183 BULKHEAD ON 'L' ANGLE, LEFT SIDE, 10 INCH ABOVE FLOOR LEVEL. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-1. (M)
- [SDR EISA97067](https://openairdocs.org/sdr/EISA97067.md): Web · cracked · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous Structure
  > WEB CRACKED BETWEEN FS 580 AND 600 BELOW CENTER FLOOR TRACK. FABRICATED DOUBLER AND SHIM AND INSTALLED PER SRM 51-40-2. (M)
- [SDR EISA97066](https://openairdocs.org/sdr/EISA97066.md): Seat Track · worn · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WORN MORE THAN 20 PERCENT MATERIAL LOSS AT FS 740. REPLACED SEAT TRACK SECTION PER SRM 51-30-2. (M)
- [SDR EISA97065](https://openairdocs.org/sdr/EISA97065.md): Seat Track · pitted corrosion · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > PITTING CORROSION ON SEAT TRACK BETWEEN FS 443 AND 461 LBL 44. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-10-5. (M)
- [SDR EISA97064](https://openairdocs.org/sdr/EISA97064.md): Seat Track · cracked · Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CRACKED SEAT TRACK FS 520-540 LBL 45.5. REPLACED SEAT TRACK SECTION FS 520-540 PER SRM 51-10-5 AND 51-30-2. (M)
- [SDR EISA97063](https://openairdocs.org/sdr/EISA97063.md): Angle · cracked · Mar 11, 1997 · N6815 · Boeing 727223 · Wing Miscellaneous Structure
  > WING CENTER SECTION INTERIOR STATION 740, 'L' ANGLE AT TOP OF VERTICAL BEAM CRACKED IN RADIUS, RBL 12. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-1. (M)
- [SDR EISA97062](https://openairdocs.org/sdr/EISA97062.md): Stiffener · cracked · Mar 11, 1997 · N6815 · Boeing 727223 · Wing Miscellaneous Structure
  > WING CENTER SECTION INTERIOR STATIO 740, VERTICAL BEAM CRACKED IN RADIUS, RBL 8. FABRICATED AND INSTALLED NEW VERTICAL BEAM PER SRM 51-10-1 AND 51-30-2. (M)

Next page: https://openairdocs.org/deregistered/N6815-2006-06-21/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 = 'N6815' AND deregistration_id = 'N6815-2006-06-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N6815-2006-06-21/reports

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