N567FE, cancelled Jan 29, 2024

Service difficulty reports · 232

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 = 'N567FE' AND deregistration_id = 'N567FE-2024-01-29'
  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 FDEA201708112177Light · missingPOST-FLT CK, LT FUSELAGE LANDING LIGHT MISSING FROM THE A/C WITH ASSOCIATED C/B TRIPPED.Aug 11, 2017 · N567FE · Doug MD1010F · Exterior LightingSDR FDEA201708112180Light · missingDURING A POST FLIGHT CHECK, THE LT FUSELAGE LANDING LIGHT MISSING FROM THE ACFT. WITH AN ASSOCIATED CIRCUIT BREAKER TRIPPED.Aug 11, 2017 · N567FE · Doug MD1010F · Exterior LightingSDR FDEA201608082842Wire · chafedNR 1 ENGINE FIRE AGENT LOW DURING CRUISE AND DECENT. CLEARED AFTER BLOCK IN TO GATE FOUND SHEILD ON WIRE TO P1-1261 WORN TO CENTER CONTACT IAW WDM 23-33-01. REPAIRED THE WIRE IAW SWP 20-10-01. OPS CHECKED IAW AMM 23-21-06-5. OK FOR SERVICE.Aug 8, 2016 · N567FE · Doug MD1010F · Fire Protection System WiringSDR FDEA201607232607Seat Track · wornMAIN DECK LT SEAT TRACK AT LBL 47.5 BETWEEN BS 1256 AND 1561, HAD SEVERAL AREAS OF WEAR. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-00 FIG 2, DRAWING AFA 7433, SRM 51-31-01, SRM 51-31-01, 53-42-01 FIG 5 VJul 23, 2016 · N567FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607232606Floor Panel · dentedFLOOR PANEL AT BS 791 BETWEEN LBL 27.5 - 45 DENTED IN 3 AREAS. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 51-40-02 AND SRM 51-31-01 VOL II. MAJOR REPAIR.Jul 23, 2016 · N567FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201607232605Floor Panel · dentedFLOOR PANEL AT BS 791 BETWEEN LBL 27.5 - 45 DENTED IN 3 AREAS. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 51-40-02, AND SRM 51-31-01 VOL II. MAJOR REPAIR.Jul 23, 2016 · N567FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201607232604Floor Panel · chafedFLOOR PANEL AT BS 791 BETWEEN LBL 8.5 AND RBL 8.5 IS CHAFED AND WORN. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 51-40-02, AND SRM 51-31-01 VOL II. MAJOR REPAIR.Jul 23, 2016 · N567FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201510143211Engine · faultyDURING CLIMB OUT PASSING FL 260, NR 3 N1 WENT TOWARD ZERO WHILE ACFT EXPERIENCED MODERATE VIBRATION. MOVED THROTTLE TO IDLE EGT & N2 APPEARED NORMAL & WERE SIMILAR TO 1 & 2 ENG, WHEN NR 3 THROTTLE WAS ADVANCED FROM IDLE, MODERATE VIBRATIONS WERE FELT. RAN Oct 14, 2015 · N567FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201507302438Indicator · inoperativeR1 REMOTE SLIDE PACK PRESSURE INDICATOR INOPERATIVE. REPLACED SLIDE REMOTE PRESSURE INDICATOR IAW MM 25-61-03-2. OPERATIONS CHECKED NORMAL.Jul 30, 2015 · N567FE · Doug MD1010F · Emergency EquipmentSDR FDEA201502060463Warning System · false activationAFTER PREFLIGHT SET UP, RECEIVED LEVEL 1 ALERT, EMER PWR ON, RETRIED EMER POWER CHECK WITH NO RESULTS. TROUBLESHOOT CHECKED IAW FIM 24-24-00. PULLED POWER FROM ACFT, DISCONNECTED BATTERY, RECONNECTED BATTERY IAW MM 24-34-01-4. RECONNECTED GND POWER & CYCLEDFeb 6, 2015 · N567FE · Doug MD1010F · Central WarningSDR FDEA201409062500Support · crackedDURING OK TO CLOSE LT WING PANEL 531AT FOUND CRACKED AT BOTTOM FASTENER, APPROX 1 1/2 INCHES PROTRUDING ON THE FASTENER AT 2ND WEB RIB FROM STATION 118.200. REPAIRED SUPPORT PN ARB0647-1 IAW EA 8-5710-T0310822. THIS IS A STACK ANGLE REPAIR. MAJOR REPAIR.Sep 6, 2014 · N567FE · Doug MD1010F · Wing Miscellaneous StructureSDR FDEA201409032437Skin Panel · delaminatedPANEL 635DR, OUTER SKIN HAS DELAMINATION ON OUTER SURFACE, APPROX AREA IS 4 INCHES X 6 INCHES. REPAIRED DELAMINATION TO OUTER SKIN & DOUBLER IAW SRM 51-71-00 PARA 17 B & IAW EA NR 8-5750-T0311007 P1 PANEL 635DR. MINOR REPAIR.Sep 3, 2014 · N567FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201408302375Floorbeam · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT HAS SEVERAL PLACES OF CORROSION BETWEEN STATION X=-56 & X=56 STATION Y-1964. REMOVED FLOOR SUPPORT IN AFT CARGO COMPARTMENT IAW SRM 51-31-01. FABRICATED NEW SUPPORT ON T14 1086876. INSTALLED NEW SUPPORT IAW SRM 51-31-01. Aug 30, 2014 · N567FE · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201408302374Support · crackedNUMBER 1 ENG OTBD CORE COWL, AFT HINGE FITTING, AFT FACE HAS GOUGES. REMOVED & INSTALLED GUSSET IAW SRM 51-31-01. REMOVED & INSTALLED HINGE FITTING IAW CMM 71-31-01. DURING REMOVAL FOUND SUPPORT CRACKED, WELDED CRACK IN UPPER SUPPORT RADIUS IAW EA 8-7110-T0Aug 30, 2014 · N567FE · Doug MD1010F · Engine Cowling SystemSDR FDEA201408292359Skin · chafedRIGHT INBD AILERON LE SKIN LOWER SURFACE, ENTIRE LENGTH HAS CHAFED. R & R SKIN PN ARC1286-6 IAW SRM 51-31-01. FABRICATED SKIN ON STAM TRAVELER T14 1086055. TRACKED ON EA 8-5730-T0310879, RSC TRACKING ONLY. MAJOR REPAIR.Aug 29, 2014 · N567FE · Doug MD1010F · AileronsSDR FDEA201408282344Skin · chafedRIGHT INBD AILERON INBD LOWER LE SKIN HAS CHAFED. FOUND SKIN TO BE OUT OF LIMITS, ORIGINAL MATERIAL .040 INCHES, MATERIAL REMAINING .027 INCHES, MATERIAL LOSS .013 INCHES IAW SRM 57-00-01 FIG 1A SHEET 3. REMOVED INBD AILERON INBD LOWER LE IAW SRM 51-31-01. Aug 28, 2014 · N567FE · Doug MD1010F · AileronsSDR FDEA201408282342Skin · corrodedUPPER AFT RUDDER, LT SIDE, EXTERNAL SURFACE AT UPPER STATIC BASE HAS CORROSION. R & R UPPER AFT RUDDER IAW AMM 27-20-02-4 & IAW WC E8-1110-7-4304 01. OPERATIONS CHECK IS GOOD IAW AMM 27-20-02-4. CLEARANCES WITHIN LIMITS IAW AMM 27-20-02-6. MINOR REPAIR.Aug 28, 2014 · N567FE · Doug MD1010F · Rudder, Plate/SkinSDR FDEA201408272328Cargo Track · corrodedAFT CARGO COMPARTMENT TRACK HAS MULTIPLE SCRATCHES & SEVERAL SPOTS OF CORROSION AT STATION X=20, BETWEEN STATION Y 1781 - 1964. REMOVED CORROSION FROM AFT CARGO COMPARTMENT TRACK STA 1781-1964. FOUND TO BE OUT OF LIMITS AT 1841 WITH 100% MATERIAL LOSS IAW SRAug 27, 2014 · N567FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201408242302Seat Track · wornUPPER CARGO SEAT TRACK RBL 8, FS 1260 HAS 2 WORN LOBES. REMOVED DAMAGED & WORN SEAT TRACK & REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 AT FS 1260 RBL 8. FABRICATED SEAT TRACK REPAIR PARTS. SEAT TRACK PN S4929150, BAT 000287519, SPLICE HAT PN FX-SRM 53-70-00Aug 24, 2014 · N567FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201408212283Floor Support · corrodedAFT CARGO COMPARTMENT RT FLOOR SUPPORT HAS SEVERAL SPOTS OF CORROSION AT STATION X- -64 BETWEEN STATION Y 1781 - 1841. FLOOR SUPPORT FOUND OUT OF LIMITS, 100% MATERIAL LOSS, IAW SRM 53-00-01, FIG 1A, SH 3. R & R RT FLOOR SUPPORT IN AFT CARGO COMPARTMENT AT SAug 21, 2014 · N567FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201408142162Skin · bulgedLEFT INBD FLAP HAS SKIN BULGE AT UPPER CTR TE. REPAIRED LT INBD FLAP IAW SRM 57-20-00 FIG 13. CURRENTLY BEING TRACKED ON EA 8-5710-T0310431. FABRICATED FILLER 2024-T3 BATCH 2550453 & DOUBLER 2024-T3 BATCH 264264. INSTALLED AT UPPER SKIN 177.300 TO 189.300.Aug 14, 2014 · N567FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201408122152Seat Track · wornUPPER CARGO SEAT TRACK LBL 45 FS 755 HAS WORN LOBE. FOUND TO BE OUT OF LIMIT IAW SRM 53-70-00 FIG 5 SHEET1. REMOVED AND REINSTALLED FLOOR PANELS (FOM) IAW SRM 51-31-01. REMOVED WORN SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 53-70-00 FIG 1. FABRICATED Aug 12, 2014 · N567FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201408122150Seat Track · wornUPPER CARGO SEAT TRACK LBL 8 FS 1401 HAS WORN LOBE. REMOVED SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-70-00, FIG 1. ORG MAT .260, LOSS .015, REMAINING MAT.245. FABRICATED REPAIR PARS: SEAT TRACK PN: 668105. SPLICE HATS ON T14/1085125, AND 2 EACH SPLICE PLATAug 12, 2014 · N567FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201408122151Seat Track · wornUPPER CARGO SEAT TRACK LBL 08, FS 1810 HAS WORN LOBE. REPAIRED SEAT TRACK AT STA 1810-1890, LBL 8 IAW ARM 53-70-00 FIG 1. SEAT TRACK P/N 60-10964. HAT T14/1085424, 1 EA SPLICE PLATE T14/1085430 PART MARK'S IAW GMM 7-0-1001-1. MAJOR REPAIRAug 12, 2014 · N567FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201408062095Floorbeam · corrodedAFT CARGO COMPARTMENT AFT INTERMEDIATE FLOOR SUPPORT BEAM HAS CORROSION AT STATION X=58, LT LONGERON 43 STATION Y 1781. REMOVED CORROSION FROM STA 1781 FLOORBEAM AT LONGERON 43, FOUND TO BE OUT OF LIMITS, 100% MATERIAL LOSS, IAW SRM 53-00-01, FIG 1A. REPAIREAug 6, 2014 · N567FE · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201211284194Bulkhead Web · crackedCENTER LANDING GEAR WHEEL WELL SPACE, LT WALL, UPPER AFT CORNER HAS THREE CRACKS. TWO RUNNING THROUGH RIVETS AND ONE COMING FROM A HOLE DOUBLER. VERIFIED USING HFEC AND REPAIRED IN REF TO JPF'S AND SRM 53 -00-01, VOL I.Nov 28, 2012 · N567FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201207222636Skin · misrepairedCARGO DOOR SKIN MISREPAIRED. REPAIRED AS PER EA 8-5230-159867.Jul 22, 2012 · N567FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA201207192613Frame · misrepairedFRAME FOUND MISREPAIRED AT BS 1975 BETWEEN L46L-49R. REPAIRED AS PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 19, 2012 · N567FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA201207192612Frame · misrepairedFRAME FOUND MISREPAIRED AT BS 1986 BETWEEN L46 L/R. REPAIRED AS PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 19, 2012 · N567FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA201207172593Floorbeam · misrepairedFORWARD CARGO BAY FLOORBEAM BS 808, "X"= -22 TO "X" = -35 MISREPAIRED. REPAIRED AS PER EA 8-5310-159866. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 17, 2012 · N567FE · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201207172592Skin · misrepairedCENTER CARGO DOOR FRAME FWD CUT OUT SKIN MISREPAIRED AT BS 1701 BETWEEN LONGERON 39 AND LONGERON 42 RT. REPAIR CARRIED OUT PER SRM 53-50-00 FIGURE 26 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Jul 17, 2012 · N567FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201207122552Skin · misrepairedSKIN APPROX STATION 1220 TO STATION 1234 BETWEEN LONGERON 51 LT AND LONGERON 51 RT MISREPAIRED. REPAIRED IAW EA 8-5330-160977Jul 12, 2012 · N567FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201207102528Longeron · misrepairedLONGERON 52 LEFT MISREPAIRED BETWEEN BS 826 AND 840. REPAIRED IAW SRM 51-31-01 VOLUME II REVISION 99. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.Jul 10, 2012 · N567FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201207102527Longeron · misrepairedLONGERON 50 LEFT MISREPAIRED BETWEEN BS 808 AND 825. REPAIRED AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 10, 2012 · N567FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201207102526Longeron · misrepairedLONGERON 51 RT MISREPAIRED BETWEEN BS 780 AND 825. REPAIRED IAW SRM 51-31-01 VOLUME II REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 10, 2012 · N567FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201207102525Longeron · misrepairedLONGERON 51 LT MISREPAIRED, BETWEEN STA 780 AND STA 825. REPAIRED IAW SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.Jul 10, 2012 · N567FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201207102529Longeron · crackedON REMOVAL OF FUSELAGE SKIN, FOUND LONGERON 49 LT CRACKED AT BS 808. CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115Jul 10, 2012 · N567FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201207042480Rib · misrepairedLT WING AILERON LOWER SKIN RIB MISREPAIRED, REPAIRED IAW EA 8-5750-160989, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.Jul 4, 2012 · N567FE · Doug MD1010F · AileronsSDR FDEA201207042479Skin · misrepairedLT WING NR 3 SLAT AFT SKIN INBD OF NR 7 TRACK MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 3, VOL I, REV 98. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.Jul 4, 2012 · N567FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201207042481Skin · crackedLEFT WING INBD FLAP ASSY UPPER SURFACE MID SEGMENT STA XIFH 165, FOUND CRACKED. FOUND CRACKED. CRACKED SKIN AT LEFT HAND WING INBOARD FLAP ASSEMBLY UPPER SURFACE MID SEGMENT TRIMMED AND CARRIED OUT REPAIR AS PER SRM 57-10-00 FIGURE 85 VOLUME I REVISION 98. Jul 4, 2012 · N567FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201207022440Skin · misrepairedRT WING NR 1 SLAT AFT SKIN MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 31, VOL I, REV 99. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Jul 2, 2012 · N567FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201207022436Skin · misrepairedRT WING NR 5 SLAT AFT SKIN MISREPAIRED. REPAIRED IAW EA 8-5100-162351. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.Jul 2, 2012 · N567FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201207022435Skin · misrepairedLT WING NR 8 SLAT INBD LOWER SKIN MISREPAIRED. LT WING NR 8 SLAT R & R AMM 27-80-01-04, REV 14.3. OPS AND GAP CHECK CARRIED OUT IAW AMM 27-80-01-04, REV 14.3 FOUND SATISFACTORY. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.Jul 2, 2012 · N567FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201207022443Fuel Cell · corrodedCENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, RBL 1. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II REVISION 99. FOUND ACCEPTABLE AS PER EA 8-5730-159860. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.Jul 2, 2012 · N567FE · Doug MD1010F · Fuel StorageSDR FDEA201207022442Fuel Cell · corrodedCENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, RBL 40. AFTER CORROSION REMOVAL, FOUND ACCEPTABLE AS PER EA 8-5730-159860. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.Jul 2, 2012 · N567FE · Doug MD1010F · Fuel StorageSDR FDEA201207022441Fuel Cell · corrodedCENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, LBL 102. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II REVISION 99. ORIGINAL MATERIAL THICKNESS = 0.220 INCH, REMAINING MATERIAL THICKNESS = 0.185 INCH, MATERIAL REMOVED = 0.035 INCH Jul 2, 2012 · N567FE · Doug MD1010F · Fuel StorageSDR FDEA201207022438Skin · damagedBULK CARGO DOOR EXTERIOR SKIN LOWER FORWARD CORNER DAMAGED. CARRIED OUT REPAIR AS PER EA 8-5230-162350 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Jul 2, 2012 · N567FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA201207022437Skin · misrepairedLT INBD ELEVATOR UPPER SKIN XE 111.75 MISREPAIRED. REPAIR ACCOMPLISHED PER SRM 55-10-00 FIGURE 8 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Jul 2, 2012 · N567FE · Doug MD1010F · Elevator, Plate/SkinSDR FDEA201207022434Skin · misrepairedHORIZONTAL STABILIZER INBD ELEVATOR UPPER SKIN FROM XE 148 TO XE 153 MISREPAIRED. REPAIR ACCOMPLISHED PER SRM 55-10-00 FIGURE 8 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Jul 2, 2012 · N567FE · Doug MD1010F · Elevator, Plate/SkinSDR FDEA201207022446Skin · corrodedCORROSION BETWEEN FUSELAGE SKIN AND BARE STRAP AT BS 1139, BETWEEN LT STRINGER 46 AND 45. REPAIRED IAW SRM 53-20-00, FIG 18 AND FIG 6, VOLUME I, REV 99. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Jul 2, 2012 · N567FE · Doug MD1010F · Fuselage Main, Plate/Skin
Back to N567FE, cancelled Jan 29, 2024