N101DA

Service difficulty reports not matched to an aircraft · 42

They name N101DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N101DA' AND registry_match IS NULL
  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 DL767050678Line · failedON TOUCHDOWN LOST CTR HYD SYSTEM. FOUND DISCONNECT ON ADP PRESSURE LINE FAILED. REPLACED SAME.Nov 3, 2005 · N101DA · Boeing 767232 · Hydraulic System, MainSDR DL767050669Fan · seizedFUMES REPORTED IN MID CABIN OVERHEAD AREA, DIVERSION RDU. FOUND GASPER FAN AT FAULT. REPLACED SAME.Oct 28, 2005 · N101DA · Boeing 767232 · Air Distribution FanSDR DL767050481Power Supply · inoperativeEMERGENCY LIGHTS INOP THROUGHOUT CABIN. REPLACED M9008 POWER SUPPLY, CHECKS OK.Aug 23, 2005 · N101DA · Boeing 767232 · Emergency LightingSDR DL767050317Skin · corrodedREPAIR OF CORROSION WAS FOUND AT SEVERAL LOCATIONS ALONG STRINGER 38R AND 39R AF FS 434. THE DAMAGE TO THE BUTT SPLICE STRIP WAS BLENDED AND HFEC INSPECTED. SKIN DAMAGE WAS REPAIRED PER THE SRM 53-00-01 FIG 201. INFORMATION WAS PROVIDED TO BOEING AND BOEINGJun 3, 2005 · N101DA · Boeing 767232 · Fuselage Main, Plate/SkinSDR DL767041075Bolt · misinstalledFOUND BY FAA INSPECTOR, RIGHT MLG WING DOOR LOWER AFT MOUNT BOLT INSTALLED INCORRECTLY. BOLT IS DAMAGED AND CENTER SHIMS ARE MISSING. INSTALLED NEW BOLT AND HARDWARE PER AMM 32-12-06 AND IPC32-12-01-05 RIGHT MLG WING DOOR LOWER AFT MOUNT INSTALLATIONS NOW CODec 1, 2004 · N101DA · Boeing 767232 · FastenersSDR DL767031124Panel · gougedTHE GORE PANEL ON THE AFT P-DOME WAS FOUND WITH A GOUGE NEAR STIFFENER 11R. THE GOUGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 087997-14AD.Dec 19, 2003 · N101DA · Boeing 767232 · Fuselage Main, BulkheadSDR DL767031122Panel · crackedINSPECTION OF THE AFT P-DOME GORE PANELS PER AD 88-19-03 REVEALED A CRACK AT A FASTENER LOCATION COMMON TO THE STIFFENER 13R LAP JOINT. THE CRACK WAS REMOVED WITH A CUTOUT TO THE GORE PANEL AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088005-14AD.Dec 19, 2003 · N101DA · Boeing 767232 · Fuselage Main, BulkheadSDR DL767031121Lap Joint · crackedDURING INSPECTION OF THE AFT P-DOME AT FS 1582 A CRACK WAS FOUND AT A FASTENER COMMON TO THE STIFFENER 5L WEB LAP JOINT. THE CRACK WAS REMOVED BY TRIMMING OUT THE LAP JOINT. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088021-14AD.Dec 19, 2003 · N101DA · Boeing 767232 · Fuselage Main, BulkheadSDR DL767030640Wire Harness · chafedFOUND LEFT AFT CHILLER WIRE HARNESS BURNT THROUGH DUE CHAFFING ON CHILLER RACK FRAME. SECURED HARNESS ASSY AND PULLED C/B'S. VERIFIED NO POWER TO HARNESS ASSY. WILL NEED WIRE HARNESS W284 REF IPC 25-33-02-01. ALSO WILL NEED DISCONNECT D2650DPN 014206555. Jul 13, 2003 · N101DA · Boeing 767232 · Equipment/Furnishings WiringSDR DL767030598Skin · dentedSKIN DENT REPAIR THE FUSELAGE SKIN WAS DENTED AT FS 1263 NEAR STRINGER 37L, DUE TO CONTACT WITH GROUND EQUIPMENT. THE DENT WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER IAW ER/A 385345-14 REV B.Jun 29, 2003 · N101DA · Boeing 767232 · Fuselage Main, Plate/SkinSDR DL767030281Wedge · debondedSLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.Mar 27, 2003 · N101DA · Boeing 767232 · Leading Edge DevicesSDR DL767021220Wire Harness · damagedEMERGENCY PATH LIGHT AT SEAT 31AB INOP. REPLACED UNDERSEAT HARNESS. LIGHT OPERATES NORMALLY.Oct 22, 2002 · N101DA · Boeing 767232 · Light System WiringSDR DL767021090Light · inoperativeTHE 1R EXTERIOR EMERGENCY LIGHT INOP. REPLAMPED SAME.Sep 16, 2002 · N101DA · Boeing 767232 · Emergency LightingSDR DL767020785Line · splitON CLIMBOUT, 'C' SYS HYD QTY MSG ACTIVATED. 'C' SYS QTY CK'D AT 0.31 FOUND BROKEN LINE IN RT UPPER OUTBD W/W. RPLD SAMEJul 10, 2002 · N101DA · Boeing 767232 · Hydraulic System, MainSDR DL767021295Connector · shortedNR 2 ENG INFLT SHUTDOWN RT OIL FILTER LIGHT CAME ON. FOUND SHORT BETWEEN D4254P AND D4258J. REPLACED PLUG D4258J. SYSTEM CHECKS NORMAL.May 10, 2002 · N101DA · Boeing 767232 · Engine Oil Indicating SystemSDR DL767011700Rib · damagedINBOARD AFT RT FLAP WAS FOUND WITH ELONGATED FASTENER HOLES IN THE LEADING EDGE RIBS. REPAIR PER ER/A 410559-14 AND NORDAM EWO E0034025, REV A.Oct 22, 2001 · N101DA · Boeing 767232 · Trailing Edge FlapsSDR DL767010926Frame · crackedACCOMPLISHMENT OF PERMANENT REPAIR FOR CRACKED CHORD PER SB 767-53-0078.Jun 5, 2001 · N101DA · Boeing 767232 · Fuselage Main, FrameSDR DL767010237Fan · odorAFTER ENG START ELECTRICAL ODOR IN COCKPIT AND BY L1 DOOR. FOUND EICAS MSG, FWD SUP FAN 1. SECURED C/B H18. RAN ENGS, PACKS, CKD E/E COMPARTMENT, FWD GALLEY. UNABLE TO DUPLICATE WITH FAN DEACTIVATED. FWD FAN TO MCO/PLAC 21-58-03A.Feb 10, 2001 · N101DA · Boeing 767232 · Air Distribution FanSDR DL767010196Battery Pack · dischargedCOACH CLASS SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP ON BOTH LEFT AND RIGHT SIDE. REPLACED BOTH LEFT AND RIGHT BATTERY PACKS.Feb 4, 2001 · N101DA · Boeing 767232 · Emergency LightingSDR DL767001427Slide · misinstalledR1 CABIN DOOR SLIDE NOT PROPERLY ATTACHED TO DOOR. REPLACED R1 DOOR SLIDE PER M/M, OPS CHECKS NORMAL.Jul 29, 2000 · N101DA · Boeing 767232 · Escape SlideSDR DL767000859Brace · mismanufacturedNR 1 ENGINE DIAGIONAL BRACE REPLACED WITH NEW THREE PIECE DIAGONAL BRACE ASSY TO MEET AD 200-07-05 REQUIREMENTS. NEW DIAG BRACE ASSY 0.033 INCH TOO SHORT WITH MAXIMUM SHIMMING ALLOWANCES. FABRICATED THICKER SHIMS WITH FAA APPROVAL. CORRECTIVE ACTION: 33432Apr 28, 2000 · N101DA · Boeing 767232 · Nacelle/Pylon, Plate/SkinSDR DL767000812Bulkhead · corrodedCORROSION DAMAGE FOUND ON THE AFT FACE AND FLANGES OF THE REAR SPAR BULKHEAD FITTINGS. THE CORROSION IS LOCATED JUST FWD OF THE FWD EDGE OF THE MLH W/W UPPER PRESSURE WEB, AND PROCEEDS INTO THE VERTICAL RAD II OF THE MACHINED FITTINGS ON BOTH THE LT AND RT SIApr 25, 2000 · N101DA · Boeing 767232 · Fuselage Main, BulkheadSDR DL767992553Module · crackedON TOUCHDOWN, LOST CTR HYD SYS AND INTERMITTENT BRAKE VLV LIGHT WITH ALT SELECTED. RES BRAKE VLV EICAS MSG. CTR HYD SYS SHOWS .09 RF. NO RES BRAKE OR OR STEERING. BRAKE SOURCE LIGHT ON. C/ MTC IN PROG. RAT MODULE REPLACED.Nov 20, 1999 · N101DA · Boeing 767232 · Hydraulic System, MainSDR DL767991014Relay · failedRELAY K459 SHORTED OUT IN P-33 PANEL, CAUSING ELECTRICAL SHORT. REMOVED P33 PANEL. REPLACED K459 RELAY. FOUND HEAT DAMAGE ON TB090. REPLACED ALL HIGH DENSITY BLOCKS AND RE-TERMINATED WIRING. REPLACED NUMEROUS RELAYS FOR POSSIBLE HEAT DAMAGE. PERFORMED CAMay 8, 1999 · N101DA · Boeing 767232 · Entertainment SystemSDR DL767990986Engine · failedIN DESCENT RT ENGINE FAILED, OIL PRESS WENT TO ZERO. REPLACED ENGINE.May 6, 1999 · N101DA · Boeing 767232 · Engine (Turbine/Turboprop)SDR DL767980499Wedge · delaminatedTHE LT WING NR 4 SLAT WAS FOUND WITH A 3 INCH DIAMETER AREA OF SKIN DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364149-14AD.Mar 2, 1998 · N101DA · Boeing 767232 · Leading Edge DevicesSDR DL767972547Stringer · corrodedCORROSION DAMAGE BEYOND LIMITS FOUND ON STR 34R FROM STA 550 TO STA 654. REPAIRED PER ERA 331055-14.Dec 5, 1997 · N101DA · Boeing 767232 · Fuselage Main, Longeron/StringerSDR DL767972546Stringer · corrodedSTR 30R CORRODED BEYOND LIMITS BETWEEN STA 1439 AND 1461. ALSO, STR 32R CORRODED BEYOND LIMITS BETWEEN STA 1417 AND 1439. REPAIRED PER ERA 331054-14.Dec 5, 1997 · N101DA · Boeing 767232 · Fuselage Main, Longeron/StringerSDR DL767972545Floorbeam · corrodedCORROSION FOUND ON STA 287 FLOORBEAM UPPER CHORD FROM LBL 10 TO THE RT EOP. REPAIRED PER ERA 331029-14.Dec 5, 1997 · N101DA · Boeing 767232 · Fuselage Main, Floor BeamSDR DL767972544Floorbeam · crackedFS 246 FLOORBEAM UPPER WEB FOUND WITH TYP CRACK AT RBL 20 UNDERNEATH THE RBL 20 STIFFENER. ALSO, STIFFENER CRACKED. ADDITIONALLY, CORROSION FOUND ON WEB AND MID CHORD AT APPROX RBL 30 AND RBL 40. REPAIRED ERA 331015-14.Dec 5, 1997 · N101DA · Boeing 767232 · Fuselage Main, Floor BeamSDR DL767972543Skin · corrodedADDITIONAL CORROSION DAMAGE FOUND NEAR EXISTING REPAIRED CORROSION DAMAGE (REF ERA208585-14). REPAIR IS REMOVED AND A LARGER REPAIR INSTALLED. REPAIR PER ERA 208585-14, REV B.Dec 5, 1997 · N101DA · Boeing 767232 · Fuselage Main, Plate/SkinSDR DL767972513Skin · corrodedTHE FUSELAGE SKIN AT BS 1202, STR 39R WAS FOUND CORRODED. THE CUTOUT IS APPROX 5.5 X 1.75 IN THE SKIN. REPAIRED PER ERA 331052-14.Dec 1, 1997 · N101DA · Boeing 767232 · Fuselage Main, Plate/SkinSDR DL767971804Power Supply · inoperativeTWO SECTIONS OF EMERGENCY FLOOR TRACK LIGHTS IN REAR SECTION OF AIRCRAFT INOP. REPLACED BATTERY PACKS AND RACKS M9009 AMD M9010. EMERGENCY FLOOR TRACK LIGHTS OPS NORMAL.Sep 15, 1997 · N101DA · Boeing 767232 · Emergency LightingSDR DL767971379Power Supply · inoperativeAFT SECTION OVERHEAD AISLE EMERGENCY LIGHTS AND R-4 DOOR EXIT LIGHT INOP. REPLACED POWER SUPPLY. SYSTEM CHECKS NORMAL.Jul 14, 1997 · N101DA · Boeing 767232 · Emergency LightingSDR DL767971332Slat · delaminatedTHE NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 4 INCH INBOARD/OUTBOARD X 2 FWD/AFT SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCATED INBOARD OF THE END OF THE SLAT WEDGE. THIS AREA WAS REPAIRED PER B767 SRM 57-43-02, FIGURE 201Jul 8, 1997 · N101DA · Boeing 767232 · Leading Edge DevicesSDR DL767970299Skin · crackedDURING A LAYOVER VISIT, SKIN WAS FOUND CRACKED AND CORRODED AT STRINGER 32R AND 34R BETWEEN FS 1461 AND FS 1480. BOTH WERE REPAIRED PER SRM.Jan 18, 1997 · N101DA · Boeing 767232 · Fuselage Main, Plate/SkinSDR DL767962074Switch · malfunctionedALL EXTERIOR EMERGENCY LIGHTS REPORTED ON. RETURNED TO GATE. ASSOCIATED WITH RT AFT ENT DOOR LIGHT CYCLING ON AND OFF. REPLACED PROX SWITCH AT RT AFT DOOR, SYSTEM OPS CHECK GOOD.Sep 7, 1996 · N101DA · Boeing 767232 · Door Warning SystemSDR DL767961965Coffee Maker · faultyTHE F/C NR 2 COFFEE MAKER STARTED SMOKING WHEN BREW BUTTON WAS PRESSED. SMOKE STOPPED AFTER CIRCUIT BREAKER PULLED. REPLACED COFFEE MAKER. SYSTEM CHECK GOOD.Aug 25, 1996 · N101DA · Boeing 767232 · Buffet/GalleysSDR DL767961519Wire · brokenAFT GALLEY EMERGENCY TRACK LIGHTS ARE OUT. REPAIRED BROKEN WIRE ON TRACK, CHECKS GOOD.Jun 24, 1996 · N101DA · Boeing 767232 · Light System WiringSDR DL767960638Coffee Maker · failedSMOKE AND HOT SMELL IN AFT GALLEY. HOT WATER COMING OUT OF COLD WATER FAUCET UNDER LT SIDE COFFEE MAKERS. FOUND NR 3 COFFEE MAKER OVERHEATING. PULLED AND COLLARED C/B. FWD TO MCO AND PLAC. REPLACED COFFEE MAKER, OPERATION NORMAL.Mar 22, 1996 · N101DA · Boeing 767232 · Buffet/GalleysSDR DL767954424Hyd Line · chafedLT HYD SYS PRES MESSAGE, HYD QTY APPEARED TO STOP DECREASING AFTER TURNING OFF LEFT HYD SYSTEM. FOUND LEFT ENG HYD LINE FROM ENG PUMP CHAFING. REPLACED HYD LINE PER M/M CHAPTER 29. RAN ENG AND OPERATED ALL FLT CONTROLS, NO FURTHER LEAKS FOUND. A/C OK FOR SNov 18, 1995 · N101DA · Boeing 767232 · Hydraulic System, MainSDR DL767953201Window · shatteredDURING CRUISE, FIRST OFFICER'S NR 1 WINDSHIELD SHATTERED, LANDED MCO. REPLACED WINDOW AND CONTROLLER, GROUND OPERATION NORMAL.Jul 25, 1995 · N101DA · Boeing 767232 · Flight Compartment Windows
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