N2816W, cancelled Jun 11, 2013

Service difficulty reports · 57

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 = 'N2816W' AND deregistration_id = 'N2816W-2013-06-11'
  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 DL72W010827Actuator · failedNOSE GEAR FAILED TO EXTEND, ASSOCIATED HYDRAULIC SYSTEM QTY WENT TO ZERO. FOUND NLG LOCK ACTUATOR BLOWN APART. REPLACED SAME.May 23, 2001 · N2816W · Boeing 727247 · Landing Gear ActuatorSDR DL72W010810Door · obstructedAFT CARGO DOOR LIGHT ILLUM DURING CLIMBOUT. THERE WAS NO REPORTED PRESSURIZATION PROBLEMS. MTC CLEANED DEBRIS FROM THE DOOR JAMB. NO FURTHER PROBLEMS.May 19, 2001 · N2816W · Boeing 727247 · Door Warning SystemSDR DL72W010643Window · wornR-2 WINDOW CAME OPEN ON T/O ROLL. CREW CLOSED WNDOW AND RETURNED TO ABQ. REMOVED AND REPLACED THE R-2 WINDOWApr 18, 2001 · N2816W · Boeing 727247 · Flight Compartment WindowsSDR DL72W010509Gasper Fan · failedPAX REPORTED ELECT SMELL IN CABIN, STRONGEST NEAR ROW 14 OCCURED JUST PRIOR TO LANDING AND DURING TAXI TO GATE.A PAX IN THE VICINITY OF ROW 14 ALSO MENTIONED THE SOUND OF HYD PUMPS GETTING LOUDER JUST PRIOR TO LANDING. FOUND GASPER FAN BAD. REPLACED SAME.Mar 28, 2001 · N2816W · Boeing 727247 · Air Distribution FanSDR DL72W010399Module · failedLOSS OF SYSTEM A FLUID AND PRESSURE SHORTLY AFTER LDG GEAR WAS SELECTED DN. ALL 3 GREEN DN LOCK LGTS ILLUM AND RED DR LGT REMAINED ILLUM. THE L/R GEAR DR AND TAIL SKID AMBER ANNUNCIATORS ON S/O PNL REMAINED ILLUM. FOLLOWED HYD LOSS PRO CEDURES PER POM. UNMar 11, 2001 · N2816W · Boeing 727247 · Hydraulic System, MainSDR DL72W010273Frame · crackedTHE INNER CHORD OF THE FS 1303 RT FRAME WAS FOUND WITH A CRACKED FLANGE AT A HYDRAULIC BRACKET ATTACH POINT JUST ABOVE THE AFT VENTRAL STAIRWAY TORQUE BOX. THE CRACKED PORTION OF FLANGE WAS TRIMMED OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER EFeb 13, 2001 · N2816W · Boeing 727247 · Fuselage Main, FrameSDR DL72W010271Skin · crackedTHE UPPER AFT CORNER OF THE R5 COCKPIT WINDOW WAS FOUND WITHA .25 INCH LONG CRACK IN THE SKIN. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380034-14, REV A.Feb 13, 2001 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W010250Stiffener · crackedWING L/E SPAR STIFFENER CRACKED O/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-21-8.Feb 12, 2001 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W010249Stiffener · crackedWING L/E SPAR STIFFENER CRACKED I/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-021-8.Feb 12, 2001 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W010248Skin · crackedA 1 INCH CRACK NR 2 L/E FLAP OUTER SKIN AT LOWER LIP INBD HINGE CUTOUT. REPAIR PER M/M 57-53-000-8.Feb 12, 2001 · N2816W · Boeing 727247 · Trailing Edge FlapsSDR DL72W010231Frame · damagedTHE FS 720D FUSELAGE FRAME WEB WAS DAMAGED BY TOOLING JUST BELOW STRINGER 25R AND THE EXISTING FRAME SPLICE. THE DAMAGE WAS REMOVED WITH A 2 INCH CUTOUT IN THE WEB. THE DAMAGE WAS REPAIRED BY REMOVING THE EXISTING FRAME SPLICE AND FABRIACTING A LARFeb 8, 2001 · N2816W · Boeing 727247 · Fuselage Main, FrameSDR DL72W002093Engine · leakingOIL QUANTITY ON NB 3 ENGINE DECREASING AT A RATE OF APPROX 1 QUART EVERY 15 MINUTES. ADDED 18 PINTS OF OIL TO NR 3 ENGINE. FOUND OIL LINE LEAKING. REPLACED BOTH O-RINGS, ITEM 75 AND 40 IPC 79-20-00-20 NR 4, 5 AND 6 BREATHER LINE.Oct 23, 2000 · N2816W · Boeing 727247 · Turbine Engine Oil SystemSDR DL72W001390Battery · inoperativeAFT RIGHT SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, NOW CKS NORMAL.Jul 23, 2000 · N2816W · Boeing 727247 · Emergency LightingSDR DL72W001341Valve · malfunctionedNR 1 ENGINE COWL ANTI-ICE VALVE WON''T INDICATE OPEN IN FLT. GOOD EPR DROP WHEN SWITCHED OPEN. REPLACED NR 1 ENGINE COWL ANTI-ICE VALVE. NO HELP. FOUND BAD GROUND TO PIN B OF VALVE CANNON PLUG. INSTALLED NEW TERMINAL TO GROUND. OPERATION CHECKS GOOD WITHJul 16, 2000 · N2816W · Boeing 727247 · Air Intake Anti/De-Ice SystemSDR DL72W992659Skin · delaminatedLTR CHK C-1 12/6/99, NR 3 SPOILER DELAMINATED UPPER O/B SIDE. REPAIRED PER SRM 57-50-6.Dec 6, 1999 · N2816W · Boeing 727247 · SpoilersSDR DL72W991030Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED BELOW I/B STOP PAD NR 8 SLAT. REPAIRED PER MM 57-54-0 FIG 812.May 10, 1999 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W991029Angle · crackedA 1.5 INCH CRACK IN SUPPORT ANGLE FWD OF NR 8 SPOILER. REPAIRED PER MM 57-20-22 FIG 806.May 10, 1999 · N2816W · Boeing 727247 · SpoilersSDR DL72W990859Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PAApr 19, 1999 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990858Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PAApr 19, 1999 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990857Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 24 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND Apr 19, 1999 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990156Sign · missingRT FWD OVERWING EXIT SIGN MISSING. REPLACED RT FWD OVERWING EXIT SIGN, OP CKS OK.Jan 22, 1999 · N2816W · Boeing 727247 · Emergency LightingSDR DL72W982373Battery Pack · dischargedRT WING FWD EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK.Nov 16, 1998 · N2816W · Boeing 727247 · Emergency LightingSDR DL72W982165Web · corrodedCORROSION WAS FOUND ON THE UPPER HORIZ PRESSURE WEB DOUBLER OF THE NLG W/W FWD OF BS 315. THE DAMAGE NECESSITATED A NEW SECTION BE SPLICED IN. REPAIRED PER ERA 332271-14.Oct 19, 1998 · N2816W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W982138Frame · crackedCRACK WAS FOUND IN THE AFT ENTRY DOORWAY LT FRAME AT WL 276.6. THE CRACK WAS 4.5 INCH LENGTH AND TYPICAL OF THAT FOUND IN SB 727-53-0055 REV 9. REPAIRED PER ERA 332362-14AD.Oct 14, 1998 · N2816W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W982119Skin · crackedA FAILED FASTENER WAS FOUND IN THE UPPER ROW OF THE S26R SKIN LAP JOINT AT BS 684. CRACKS WERE FOUND EMANATING FROM THIS FASTENER HOLE IN THE OUTER SKIN ONLY. THE CRACKS WERE .125 AND .0937 LONG. REPAIRED PER ERA 332342-14.Oct 12, 1998 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W982118Stringer · corrodedCORROSION WAS FOUND ON THE I/B FLANGE OF S3R AT FS 371 REQUIRING A SECTION OF STRINGER TO BE CUT OUT. REPAIRED PER ERA 332244-14.Oct 12, 1998 · N2816W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W982105Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 33 FROM THE IB END OF FLAP. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0,FIG. 802 BY INSTALLING A DOUBLER AND STOP DRILLING THE CRACK.Oct 6, 1998 · N2816W · Boeing 727247 · Trailing Edge FlapsSDR DL72W982064Stringer · corrodedCORROSION DAMAGE FOUND THAT EXCEEDED ALLOWABLE LIMITS, ON THE S1L, AT BS 375. REPAIRED PER ERA 332246-14.Oct 6, 1998 · N2816W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W981971Spar · crackedSPAR CRACKED AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.Sep 24, 1998 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W982217S-Duct · crackedAT HMV FOUND SKIN - BENT/CRACKED INSIDE S-DUCT APPROX 4FT FROM L/E OF INLET AT 12 O-CLOCK POSITION. CORR: MANUFACTURED REPAIR DBLR AND FILLER PER SRM 54-10-3 P.63 INSTLD PER SAME.Sep 14, 1998 · N2816W · Boeing 727247 · Nacelle/Pylon StructureSDR DL72W982216Stringer · crackedAT HMV, FOUND RT WING OUTER W/UPR STRINGER 2 RIB AT WS 656.5 STRINGER 13 IS CRACKED AT FASTENER HOLE. REPAIR INFO IS REF ON OPN 8602AD ITEM 5. CUT OUT VENT STRINGER, DRILLED UP REPAIR ANGLES RADIUS FILLER COVER ASSY PER M/M 57-13-00. INSTALLED PER SAME.Sep 11, 1998 · N2816W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W982213Stringer · crackedON HMV, RT WING OUTER UPPER STRINGER 2 RIB AT WS 656.5 STR 12 IS CRACKD AT FASTENER HOLE. CUT OUT VENT STRINGER, DRILLED UP REPAIR ANGLES RADUIS FILLERS CVR ASSY PER MM 57-13-00. INSTALLED REPAIR ANGLES.Sep 11, 1998 · N2816W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W982210Guide · wornAT HMV, FOUND GUIDE ON NR 5 SLAT TRAILING EDGE O/B OF ACTUATOR WORN. WEAR LIMITS OK, REPAIRED PER M/M 27-81-11.Sep 10, 1998 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W982209Angle · crackedAT HMV, FOUND NR 5 SLAT ANGLES - ACTUATOR ATTACH POINT BOTH I/B AND O/B ANGLES CRACKED. STOP DRILLED CRACK PER M/M, FABD REPAIR DOUBLERS, INSTALLED PER MM 57-54-00 FIG 809.Sep 10, 1998 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W982197Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 32 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 FIG 802, BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.Sep 10, 1998 · N2816W · Boeing 727247 · Trailing Edge FlapsSDR DL72W981982Rib · crackedI/B AFT RIB IS CRACKED AT AFT LWR CORNER. REPAIRED PER MM 57-52-0 FIG 808.Sep 9, 1998 · N2816W · Boeing 727247 · Trailing Edge FlapsSDR DL72W981509Skin · cracked.25 INCH CRACK DORSAL FIN SKIN LEFT SIDE BELOW PANEL 9523. REPAIRED PER M/M 54-30-0 PG 804.Jul 20, 1998 · N2816W · Boeing 727247 · Aerodynamic FairingsSDR DL72W981485Battery Pack · dischargedWORKING L/O, NR 2 FOUND AIRSTAIR UPPER EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER M/M OP CK GOOD.Jul 16, 1998 · N2816W · Boeing 727247 · Emergency LightingSDR DL72W972589Light Assy · inoperativeRIGHT EMERGENCY OVERWING EXIT LIGHT INOP ON EMERGENCY PWR. OP NORMAL ON AC PWR. REPLACED LIGHT ASSY AT OVERWING EXIT.Dec 9, 1997 · N2816W · Boeing 727247 · Emergency LightingSDR DL72W972560Bracket · crackedNR 1 SLAT ACTUATOR I/B ATTACH BRACKET CRACKED. OPENED PANELS FOR ACCESS, REMOVED RIB WEB, STOP DRILLED CRACK, DRILLED UP DOUBLER. INSTALLED DOUBLER AND CLOSED UP.Dec 6, 1997 · N2816W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W972559Skin · crackedFOUND ON A1 LETTER CK, .1562 AND .125 INCH CRACKS IN FUSELAGE SKIN COMING OUT OF RIVET HOLE JUST AFT OF L3 WINDOW LOWER END. REPAIRED PER SRM 53-30-3.Dec 6, 1997 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W972558Stiffener · crackedA 1.5 INCH CRACK_IN SPAR STIFFENER LOCATED OUTBD SIDE OF NR 6 SLAT INBD TRACK. REPAIRED PER MM 57-20-21.Dec 6, 1997 · N2816W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W972557Bracket · crackedFOUND ON A1 LETTER CK, NR 1 SLAT ACTUATOR I/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.Dec 6, 1997 · N2816W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W971990Bulkhead · crackedA 2 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT RBL 8.0 AND WL 180. THIS ER/A WILL GIVE INSTRUCTIONS TO ACCOMPLISH A REPAIR UNTIL THE FULL MODIFICATION REQUIRED BY AIRWORTHINESS DIRECTIVE 90-06-09 IS ACCOMPLISHED. THE REPAIR WILL BE INSTALLED ON THE FWD SIDOct 3, 1997 · N2816W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W970919Stringer · crackedSTRINGER 8 CRACKED INSIDE VERT STAB RT SIDE FIN STA 133.800. REPAIRED PER M/M 55-30-0.May 13, 1997 · N2816W · Boeing 727247 · Vertical StabilizerSDR DL72W962336Frame · crackedRT AFT SERVICE DOOR FWD FRAME CRACKED .5 INCH AT LOWER I/B CORNER OF UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4.Oct 16, 1996 · N2816W · Boeing 727247 · Service DoorsSDR DL72W962333Frame · crackedRT AFT SERVICE DOOR FWD FRAME CRACKED .5 INCH AT LWR I/B CORNER OF UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4.Oct 16, 1996 · N2816W · Boeing 727247 · Service DoorsSDR DL72W962332Stiffener · crackedA 1 INCH CRACK IN WING L/E VERTICAL STIFFENER AT NR 5 SLAT I/B TRACK O/B POSITION. REPLACED STIFFENER PER M/M.Oct 16, 1996 · N2816W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W960611Skin · crackedFOUND DURING E-2 LETTER CHECK - 2 EA, .25 INCH CRACKS EXTENDING FROM RIVET HOLES, RT VERTICAL STAB SKIN, JUST BELOW SADDLE PLATE 9501. REPAIRED PER M/M 54-30-0.Mar 19, 1996 · N2816W · Boeing 727247 · Vertical Stabilizer, Plate/SkinSDR DL72W960610Web · crackedFOUND DURING E-2 LETTER CHECK - .50 INCH CRACK, LT FWD TORQUE BOX LIGHTENING HOLE. REPAIRED PER M/M 53-11-0.Mar 19, 1996 · N2816W · Boeing 727247 · Fuselage Miscellaneous Structure
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