N2815W, cancelled Aug 27, 2012

Service difficulty reports · 55

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 = 'N2815W' AND deregistration_id = 'N2815W-2012-08-27'
  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 DL72W010853Controller · faultyA/C WILL NOT HOLD PRESSURIZATION AT FL240 WITH 1 PACK. DESCENDED TO FL150 TO MAINTAIN CABIN. REPLACED PRESSURE CONTROLLER AND E/E OVERBOARD VALVE.May 27, 2001 · N2815W · Boeing 727247 · Cabin Pressure ControllerSDR DL72W010637Skin · crackedFUSELAGE SKIN, FS 360-480 AT STR 4R SKIN LAP SPLICE CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED 5 CRACKS ALONG THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. AN Apr 17, 2001 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W010572Controller · malfunctionedCLIMBING THROUGH 17,000 FT.IN AUTO MODE AIRCRAFT CABIN ALT. PRESSURE CLIMBED THROUGH 10,000FT RAPIDLY. FOLLOWED LOSS OF PRESSURIZATION, CHECKLISTS AND WAS ABLE TO REGAIN CABIN CONTROL AFTER CYCLING LEFT PACK. STBY.MODE WORKED FINE AFTER THAT.Apr 7, 2001 · N2815W · Boeing 727247 · Air Conditioning SystemSDR DL72W001521Battery · dischargedEMERGENCY FLASHLIGHT AT AFT F/A SEAT LIGHT NOT BLINKING. REPLACED BATTERY, OPS NORMAL.Aug 10, 2000 · N2815W · Boeing 727247 · Emergency EquipmentSDR DL72W001141Skin · crackedWHILE ACCOMPLISHING LFEC INSP PER 4-74176-12AD ON S4L LAP JOINT, CRACK INDICATION WAS NOTED BETWEEN BS 440 AND 460. INTERNAL HFEC INSPECTION OF ENTIRE PANEL PER SI A SINGLE CRACK WAS VERIFIED BETWEEN BS 440 AND 460 (FASTENER NR 10). DAMAGE WAS REPAIRED PER EJun 13, 2000 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W000983Actuator · inoperativeRT MAIN GEAR FAILED TO EXTEND DURING NORMAL EXTENSION. CHECK LIST PROCEDURES WERE USED AND RT GEAR WAS EXTENDED AND LEFT IN THE EXTENDED POSITION FOR THE REMAINDER OF THE FLT. REPLACED RT GEAR SEQUENCE VLV PER MM 32-32-21, NO HELP. STILL NEEDS MANUAL EXTENSMay 19, 2000 · N2815W · Boeing 727247 · Landing Gear ActuatorSDR DL72W000199Skin · crackedTHE UPPER FUSELAGE SKIN WAS FOUND WITH CRACK INDICATIONS AT THE UPPER ROW OF FASTENERS IN THE STRINGER 26R SKIN LAP SPLICE AT FS 662. ALL CRACK DAMAGE WAS REMOVED WITH A 4.25 X 2.75 CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER B727 Jan 26, 2000 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W992594Skin · dentedINBOARD L/E DENTED AND WORN. REPAIRED ON SHOP ORDER 927514 PER M/M 57-52-0 FIG 803 {FLAP SHOP}.Oct 8, 1999 · N2815W · Boeing 727247 · Trailing Edge FlapsSDR DL72W991428Stiffener · crackedTPA LTR CHK B-1, O/B SPAR STIFFENER CRACKED AT NR 3 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21 .Jun 24, 1999 · N2815W · Boeing 727247 · Wing SparSDR DL72W991427Frame · crackedFOUND AT B-1 LTR CK, AFT CABIN ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER SRM 53-10-9.Jun 24, 1999 · N2815W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990923Skin · crackedFUSELAGE SKIN FS 360-380 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETApr 27, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990922Skin · crackedFUSELAGE SKIN FS 481-681, STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 20 CRACKS. THE EApr 26, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990754Skin · corrodedON HUSH-KIT MOD OPN 57118, LOWER SKIN LAP JOINT INSPECTION FOUND CORROSION ON FUSELAGE SKIN BETWEEN BONDED METAL SKIN LAYERS AT STATION 259.5R TO 360R. REPLACED SKIN SECTION WITH A/C SKIN SECTION FROM MANUFACTURER.Apr 7, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990752Skin · corrodedTHE FUSELAGE SKIN PANEL BETWEEN FS 259.5 AND 360 AND BETWEEN STRINGER 19R AND 24R WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE PANEL WAS REMOVED AND A NEW BOEING SKIN PANEL INSTALLED PER ER/A 366991-14.Apr 6, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990498Angle · corrodedON HUSH-KIT MOD FOUND RT NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG LIMITS. REPLACED CHORD ANGLE WITH PART OF NEW MFG.Mar 10, 1999 · N2815W · Boeing 727247 · Engine Mount SectionSDR DL72W990496Angle · corrodedON HUSH-KIT MOD FOUND LT NR 2 ENGINE AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG LIMITS. REMOVED CHORD ANGLE AND REPLACED WITH NEW MFG PART.Mar 9, 1999 · N2815W · Boeing 727247 · Engine Mount SectionSDR DL72W990585Insulation · crackedDURING HUSH-KIT MOD FOUND INSULATION CRACKED ON GEN FEEDER CABLES IN PYLON ON NR 3 ENGINE. SPLICED IN NEW CABLE (P/N 0122107330) FROM SPLICES IN 48 SECTION TO FIREWALL DISCONNECT.Mar 4, 1999 · N2815W · Boeing 727247 · Electrical Power System WiringSDR DL72W990321Light · inopF/O MAP LIGHT SMOKED AND FUMED. REPLACED LIGHT ASSY.Feb 17, 1999 · N2815W · Boeing 727247 · Flight Compartment LightingSDR DL72W990307Clacker · failedATB - ELECT SMELL FROM RT SIDE OF COCKPIT. REPLACED OVERSPEED CLACKER.Feb 16, 1999 · N2815W · Boeing 727247 · Central WarningSDR DL72W982652Bolt · missingON APPROACH, LEADING EDGE FLAP NR 3 UNSAFE HAD AMBER LIGHT, ON GO-AROUND FLAPS WENT GREEN. SAFE INDICATION ON LANDING. AFTER LANDING FLAPS TO 25 DEGREES, FLAP INDICATION WENT TO AMBER. FOUND ACTUATOR DISCONNECTED FROM FLAP, BOLT MISSING. DAMAGE TO FLAP CODec 29, 1998 · N2815W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W982347Angle · crackedDURING SHOP INSP, THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED 33 AND 36.5 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Oct 22, 1998 · N2815W · Boeing 727247 · Trailing Edge FlapsSDR DL72W981761Shim · migratedTHE I/B TRACK OF THE LT WING I/B FLAP WAS FOUND WITH THE LAMINATED SHIM MIGRATED .25 AS TYPICAL OF S/B 727-57-0178 AND AD 90-07-05. THE SHIM WAS REPLACED PER THE REQUIREMENTS OF THE S/B AND DOCUMENTED PER ER/A 365509-14AD.Aug 22, 1998 · N2815W · Boeing 727247 · Trailing Edge FlapsSDR DL72W981738Battery · dischargedOVERWING EMERGENCY EXIT LIGHTS FLASHING. REPLACED RACK AND BATTERY, OPS CHECK GOOD.Aug 19, 1998 · N2815W · Boeing 727247 · Emergency LightingSDR DL72W981663Battery Pack · dischargedR-1 DOOR EMERG LIGHT INOP. REPLACED BATT PACK, OPS NOW OK.Aug 12, 1998 · N2815W · Boeing 727247 · Emergency LightingSDR DL72W980584Strap · crackedTHE R1 DOOR CUTOUT REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK IN UPPER HINGE CUTOUT. THE SKIN WAS CUT TO ACCESS THE CRACK AND THE BEAR STRAP WAS CUT TO REMOVE THE CRACK. THE CUTOUTS WERE REPAIRED WITH A DOUBLER AND TRIPLER PER THE GUIDLIMar 11, 1998 · N2815W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W980556Aux Spar · chafedMLG AUX SPAR CHAFED AT INBD FWD END LT SIDE. REPAIRED PER MM 57-43-0 P 801.Mar 11, 1998 · N2815W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W980555Web · crackedFOUND ON A1 LETTER CK .25 IN CRACK AT LIGHTENING HOLE VERTICAL WEB STA 1233R IN 48 SECTION. ROUTED OUT DAMAGED AREA PER MM 53-11-0.Mar 11, 1998 · N2815W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W972475Frame · crackedNR 2 CARGO DOOR FWD FRAME HAS A 1.5 INCH CRACK AT LWR DOOR STOP FITTING. INSTALLED DOUBLER PER SRM 53-10-4.Nov 24, 1997 · N2815W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W970775Battery · dischargedRT OVERWING EXTERIOR EMERG LIGHT INOP. REPLACED BATTERY, CKS NORMAL.Apr 26, 1997 · N2815W · Boeing 727247 · Emergency LightingSDR DL72W970268Power Supply · inoperativeON L/O CK, FOUND RT OVERWING EXIT SIGNS WOULD NOT ILLUMINATE WITH EMER LTS ON. REPLACED POWER SUPPLY AND BATTERY, OPS CKS OK.Feb 12, 1997 · N2815W · Boeing 727247 · Emergency LightingSDR DL72W970265Power Supply · inoperativeON L/O CK, FOUND RT OVERWING EXIT SIGNS WOULD NOT ILLUMINATE WITH EMERGENCY LIGHTS ON. REPLACED POWER SUPPLY AND BATT, OPN CKS OK.Feb 12, 1997 · N2815W · Boeing 727247 · Emergency LightingSDR DL72W970216Skin · corrosionCORROSION WAS FOUND ON THE FUSELAGE LOWER SKIN BETWEEN AT 681 AND 720 JUST I/B OF STR 26R IN THE VICINITY OF AN EXISTING REPAIR. THE EXISTING DOUBLER WAS REMOVED AND A SINGLE REPAIR COVERED BOTH AREAS. THIS REPAIR IS APPROVED BY FAA/DER FORM 8110-3, DER DESIJan 27, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W970190Skin · gougedDURING THE INSTALLATION OF THE UPPER HINGE REPAIR/MODIFICATION PER 727-53-0198, A GOUGE WAS FOUND IN THE LOWER FUSELAGE SKIN JUST AFT OF THE REPAIR AREA. DAMAGE REMOVAL RESULTED IN A 1 INCH BY 2 INCH CUT-OUT IN THE SKIN. DUE TO THE CLOSE PROXIMITY OF THIS DAJan 16, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W970102Skin · crackedAT MIDVISIT, THE SKIN AT GROUND PNEUMATIC DUCT ACCESS DOOR WAS FOUND CRACKED AT THE AFT I/B CUTOUT CORNER. A DOUBLER WAS FABRICATED AND DRILLED AND INSTALLED PER MM 53-30-0 FIG 802.Jan 16, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W970191Skin · crackedTWO CRACKS IN THE SKIN AND DOOR SURROUND STRUCTURE WERE FOUND IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE FIRST CRACK MEASURES APPROXIMATELY 2.25 INCHES AND PENETRATES THE EXTERNAL SKIN AND BONDED DOUBLER. THE SECOND CRACK MEASURES APPROXIMATELY 2.25 Jan 15, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W970180Angle · corrosionCORROSION ON MOUNT ANGLES AROUND PERIPHERY OF LOWER FUSELAGE FAIRING OPENING AFT OF LOWER ROTATING BEACON. BEGAN REMOVING T-ANGLES FROM STA 820-920. FABRICATED NEW REPLACEMENT PARTS FOR RT BEAM PER SRM 53-30-1. COMPLETED INST OF RT ANGLE. FABRICATED LT BEJan 14, 1997 · N2815W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W970130Bulkhead · crackedAT MIDVISIT THE BULKHEAD WEB WAS FOUND CRACKED AT BOTH LOWER O/B CORNERS AT FS 1303. THIS WAS REPAIRED PER SRM 53-10-4.Jan 14, 1997 · N2815W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W970115Door Frame · crackedFOUND R-2 DOOR FRAME CRACKED AT UPPER HINGE CUTOUT. FABRICATED DOUBLER PER SRM 52-40-2 FIG 4. ROUTED OUT DAMAGE PER SRM 52-40-2 FIG 4, INSTALLED DOUBLER PER SRM 52-40-2 FIG 4.Jan 14, 1997 · N2815W · Boeing 727247 · Passenger/Crew DoorsSDR DL72W970034Stiffener · crackedL/E VERTICAL SPAR STIFFENER CRACKED AT NR 3 SLAT O/B TRACK I/B STIFFENER. REPLACED STIFFENER PER MM 57-20-21.Jan 8, 1997 · N2815W · Boeing 727247 · Leading Edge DevicesSDR DL72W961557Tr Unit · burntVISIBLE SMOKE EXHAUSTING FROM E/E COMP WITH ESS TR C/B POPPED, SMELLS ELECTRICAL. FOUND AND REMOVED ESS T/R AND REPLACED NR 3 TR, OPS OK.Jun 29, 1996 · N2815W · Boeing 727247 · DC Rectifier/ConverterSDR DL72W961352Skin · corrosionMTC REPORTS CORROSION ON THE FUSELAGE SKIN AT STA 540 AT STR 27R. CUT-OUT RESULTED IN 5.5 INCHES FWD/AFT BY 3.3 INCHES CIRCUM. AN EXISTING REPAIR INBD OF NEW DAMAGE REPAIRS A CUTOUT MEASURING .15 INCH FWD/AFT BY 2.5 INCHES CIRCUM. SKIN IS MACHINED FROM .125 May 29, 1996 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961310Frame · crackedL-2 DOOR FRAME UPPER HINGE CUTOUT CRACKED. REPAIRED PER SRM 52-40-2.May 28, 1996 · N2815W · Boeing 727247 · Passenger/Crew DoorsSDR DL72W961309Skin · crackedTWO, .75 INCH CRACKS IN VERTICAL STAB SKIN FWD OF SADDLE PANEL RT SIDE ABOVE PANEL 9516. REPAIRED PER M/M 54-30-0.May 28, 1996 · N2815W · Boeing 727247 · Vertical Stabilizer, Plate/SkinSDR DL72W961308Doubler · crackedREPAIR DOUBLER CRACKED RT ELEV 3RD FROM O/B HINGE RIB. REPAIRED PER M/M 55-10-31.May 28, 1996 · N2815W · Boeing 727247 · Elevator StructureSDR DL72W961270Light · inoperativeON T/S INSP, FOUND COCKPIT OVER DOOR EMERGENCY EXIT/FLASHLIGHT DID NOT OPERATE IN THE ON POSITION DURING TEST. REPLACED ASSEMBLY 334701743.May 23, 1996 · N2815W · Boeing 727247 · Emergency LightingSDR DL72W954737Bulb · failedENGINE FIRE TEST CAUSES NR 1 ENG A/B FIRE DETECTION CIRCUIT BREAKER TO TRIP. REPLACED ENG FIRE TEST PANEL. REPLACED FIRE DET MOD. NO HELP. REPLACED FAULT BULB IN FIRE HANDLE. SYSTEM NOW CKS NORMAL.Dec 19, 1995 · N2815W · Boeing 727247 · Fire DetectionSDR DL72W954576Skin · crackedDURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH FLOATING SKIN CRACKED AT FASTENERS BETWEEN RIBS NR 8 AND 9, 13 AND 14. REPAIRED PER MM 57-54-0.Nov 29, 1995 · N2815W · Boeing 727247 · Leading Edge DevicesSDR DL72W954611Rib · crackedDURING ROUTINE SHOP INSPECTION, RIB NR 13 FROM THE O/B END WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER THE B-727 MM 57-54-0 PG 806 AND 807, FOR NR 1 L/E SLAT.Nov 21, 1995 · N2815W · Boeing 727247 · Leading Edge DevicesSDR DL72W954680Skin · crackedUPON INITIAL INSPECTION, CRACK FOUND IN NR 5 SLAT SKIN UNDER AIR FENCE. REPAIRED PER M/M 57-54-0.Nov 20, 1995 · N2815W · Boeing 727247 · Leading Edge DevicesSDR DL72W954580Rib · crackedNR 1 SLAT RIB MARKED 15 CRACKED. REPAIRED PER MM 57-54-0 PG 819.Nov 20, 1995 · N2815W · Boeing 727247 · Leading Edge Devices
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