N6815, cancelled Jun 21, 2006

Service difficulty reports · 67

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR EISA20010134Structure · corrodedFOUND 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.Dec 1, 2001 · N6815 · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA20010098Light · inoperativeON POSTFLIGHT INSPECTION FOUND COCKPIT EMERGENCY LIGHT INOP.CORRECTIVE ACTION: REPLACED COCKPIT EMERGENCY EXIT LIGHT PER MM REF 33-50Jun 19, 2001 · N6815 · Boeing 727223 · Emergency LightingSDR EISA20010084Light · inoperativeL-1 EMERGENCY EXIT LIGHT WILL NOT CHARGE.May 21, 2001 · N6815 · Boeing 727223 · Emergency LightingSDR EISA20010071Seat Track · crackedDURING 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.Mar 5, 2001 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA20000153Actuator · inoperativeDURING 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 Sep 26, 2000 · N6815 · Boeing 727223 · Leading Edge Slat ActuatorSDR EISA20000123Skin · delaminatedDURING 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 51-2Aug 10, 2000 · N6815 · Boeing 727223 · Trailing Edge FlapsSDR EISA20000122Skin · delaminatedDURING 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.Aug 10, 2000 · N6815 · Boeing 727223 · Leading Edge DevicesSDR EISA20000121Skin · delaminatedDURING 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.Aug 10, 2000 · N6815 · Boeing 727223 · Trailing Edge FlapsSDR EISA20000120Skin · delaminatedDURING 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.Aug 10, 2000 · N6815 · Boeing 727223 · Trailing Edge FlapsSDR EISA20000106Fitting · crackedDURING 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.Aug 10, 2000 · N6815 · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA20000107Frame · crackedDURING 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.Aug 10, 2000 · N6815 · Boeing 727223 · Fuselage Main, FrameSDR EISA20000124Actuator · crackedDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · Entrance StairsSDR EISA20000119Bushing · wornDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · Main Landing GearSDR EISA20000118Airstair · crackedDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · Entrance StairsSDR EISA20000117Web · corrodedDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA20000115Seat Track · crackedDURING 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 B72Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA20000114Seat Track · corrodedDURING 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, INSAug 9, 2000 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA20000113Structure · crackedDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Main, StructureSDR EISA20000112Skin · dentedDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Main, Plate/SkinSDR EISA20000111Strap · crackedDURING 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 65C2906Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Main, StructureSDR EISA20000110Skin · delaminatedDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · Trailing Edge FlapsSDR EISA20000109Bracket · crackedDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · AileronsSDR EISA20000108Angle · crackedDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA20000116Seat Track · corrodedDURING 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.Aug 9, 2000 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR 20000057Control Panel · failedON TAKEOFF FROM ELP, AIRCRAFT WOULD NOT PRESSURIZE. AIR TURNBACK TO ELP.Jul 17, 2000 · N6815 · Boeing 727223 · Cabin Pressure Control SystemSDR EISA20010082Wire · brokenON 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 32-00May 18, 2000 · N6815 · Boeing 727223 · Landing Gear System WiringSDR EISA2000046Regulator · failedDURING 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 RMay 2, 2000 · N6815 · Boeing 727223 · DC RegulatorSDR EISA2000042Landing Gear · malfunctionedNOSE 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)Apr 3, 2000 · N6815 · Boeing 727223 · Nose/Tail Landing GearSDR EISA99109Light · inoperativeEMERGENCY EXIT LIGHT IN COCKPIT INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT IN COCKPIT IAW BMM 3350. NO DEFECTS NOTED. (M)May 9, 1999 · N6815 · Boeing 727223 · Emergency LightingSDR EISA99031Pcu · leakingIMMEDIATELY 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)Feb 24, 1999 · N6815 · Boeing 727223 · Rudder Control SystemSDR EISA98219Nut · looseREJECTED 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)Sep 9, 1998 · N6815 · Boeing 727223 · Alternator-Generator DriveSDR EISA98179Battery · overheatWHEN 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 24-3Jul 17, 1998 · N6815 · Boeing 727223 · Battery/Charger SystemSDR EISA98039Batteries · dischargedEMERGENCY LIGHT BATTERY DEAD. INSTALLED NEW BATTERIES. (M)Feb 8, 1998 · N6815 · Boeing 727223 · Emergency LightingSDR EISA97226Wire · brokenEMERGENCY EXIT 'UNARMED LIGHT' YELLOW LIGHT INOP. REPAIRED BROKEN WIRE, PER STANDARD PRACTICES, OPS CHECK GOOD. (M)Nov 12, 1997 · N6815 · Boeing 727223 · Light System WiringSDR EISA97078Skin · corrodedFORWARD PIT HAS CORROSION AND METAL FLAKING ON SKIN LAP JOINT BS 517, STRINGER 26R. FABRICATED FILLER AND DOUBLER PER SRM 53-30-3. (M)Mar 17, 1997 · N6815 · Boeing 727223 · Fuselage Main, Plate/SkinSDR EISA97070Seat Track · corrodedSEAT TRACK 3 LEFT CORRODED AT FS 348.2. REMOVED AND REPLACED SEAT TRACK FORM FS 340 TO 360 PER SRM 53-10-05. (M)Mar 17, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA97056Fitting · corrodedLEFT OUTBOARD AILERON INBOARD HINGE CORRODED AROUND BUSHING. REMOVED AND REPLACED FITTING PER SRM 51-10-1. (M)Mar 17, 1997 · N6815 · Boeing 727223 · AileronsSDR EISA97044Clip · crackedCRACKED STRINGER TIE CLIP AT FS 990 STRINGER 8L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-04. (M)Mar 15, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA97074Splice · gougedSTRINGER SPLICE CORRODED ON STRINGER 28R APPROXIMATELY FS 1030. FABRICATED AND INSTALLED NEW SPLICE SECTION PER SRM 53-10-3. (M)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA97073Stringer · corrodedSTRINGER 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)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Main, Longeron/StringerSDR EISA97072Frame · gougedFLOOR 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)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Main, FrameSDR EISA97071Seat Track · corrodedRIGHT OUTBOARD SEAT TRACK CORRODED AT STATION 700. INSTALLED NEW TRACK SECTION PER SRM 51-30-2. (M)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA97069Angle · crackedINTERCOSTAL 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)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA97068Angle · cracked.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)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA97067Web · crackedWEB CRACKED BETWEEN FS 580 AND 600 BELOW CENTER FLOOR TRACK. FABRICATED DOUBLER AND SHIM AND INSTALLED PER SRM 51-40-2. (M)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage Miscellaneous StructureSDR EISA97066Seat Track · wornSEAT TRACK WORN MORE THAN 20 PERCENT MATERIAL LOSS AT FS 740. REPLACED SEAT TRACK SECTION PER SRM 51-30-2. (M)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA97065Seat Track · pitted corrosionPITTING CORROSION ON SEAT TRACK BETWEEN FS 443 AND 461 LBL 44. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-10-5. (M)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA97064Seat Track · crackedFOUND 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)Mar 11, 1997 · N6815 · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR EISA97063Angle · crackedWING 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)Mar 11, 1997 · N6815 · Boeing 727223 · Wing Miscellaneous StructureSDR EISA97062Stiffener · crackedWING 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)Mar 11, 1997 · N6815 · Boeing 727223 · Wing Miscellaneous Structure
Back to N6815, cancelled Jun 21, 2006