N367FE

Service difficulty reports · 138

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 = 'N367FE' AND registry_match = 'registration'
  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 08FDEA01732Frame · gougedRIGHT WING T/E FLAP OUTBD ACTUATOR FAIRING, OUTBD L/E UNDER FAIRING MOUNT FRAME HAS 2 GOUGES. BLENDED GOUGES AND FOUND 1 EACH 0.030 DEEP TO BE OUT OF LIMITS IAW CMM 57-44-01. FABRICATION OF ANGLES WAS ACCOMPLISHED ON N/R N01025. REMOVED CLIPS FABBED IAW SRMay 2, 2008 · N367FE · Doug MD1010F · Trailing Edge FlapsSDR 08FDEA01718Support Angle · crackedUPPER INTERMEDIATE AFT FUSELAGE (ZONE 312); AFT PRESSURE BULKHEAD (STA 2007), AFT FACE UPPER CENTER SECTION. THE FUSELAGE SKIN SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-31-01 & 51-35-01; VOL II; PG 1. ALODINED & PRIMED May 1, 2008 · N367FE · Doug MD1010F · Fuselage Main, BulkheadSDR 08FDEA01671Shear Tie · corrodedSURFACE CORROSION FOUND AT BS 1997, BETWEEN LONGERON 50R AND LONGERON 49R IN THE AFT FUSELAGE COMPT. REMOVED THE CORROSION IAW SRM 51-21-01. ORIGINAL METAL THICKNESS WAS 0.071 IAW DWG AJC 7363. AFTER CORROSION REMOVAL THERE WAS 100% MATERIAL LOSS WHICH IS OApr 29, 2008 · N367FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR 08FDEA01670Web · corrodedCENTER PIT DOORWAY AT STA 1770 THE WEB BELOW THE AFT PDU HAS SIGNS OF CORROSION. WEB AREA IS OUT OF LIMITS IN REF TO SRM 53-00-01 VOL I FIG 1-B. CHANNEL AREA IS OUT OF LIMITS IAW SRM 53-00-01 VOL I FIG 1B. FABRICATED NEW CHANNEL IAW DWG AFA0154, REV AD. FAApr 29, 2008 · N367FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR 08FDEA01647Plate · corrodedFWD CARGO COMP BILGE AT BS 753, THE DOUBLER BETWEEN STRINGER 48R TO STRINGER 49R IS CORRODED. REMOVED THE SPLICE IN REF TO SRM 51-33-01. FOUND TO BE CRACKED & CORRODED OUT OF LIMITS IN REF TO SRM 53-00-01. FABRICATED A NEW ARC3155-7 SPLICE IN REF TO DWG ACA 3Apr 28, 2008 · N367FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR 08FDEA01634Seat Track · damagedMAIN CABIN SEAT TRACK IN BALLMAT AREA SCALLOPS BROKEN AND SEVERAL GOUGES STA 753 TO STA 763 RBL 9. THE DAMAGED SCALLOPS ON THE SEAT TRACK AT RBL 9 & BS 753-763 FOUND TO BE OUT OF LIMITS IN REF TO SRM 53-70-00 VOL I FIG 5 SHEET 1. REMOVED DAMAGED SECTION AT Apr 25, 2008 · N367FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01632Seat Track · damagedMAIN CABIN SEAT TRACK IN BALLMAT AREA SCALLOPS BROKEN AND SEVERAL GOUGES AT STA 755 TO STA 763 LBL 28. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 VOL I FIG 5. REMOVED FLOOR PANELS AT BS 625-890 LBL 28-48 TO GAIN ACCESS. REMOVED TRACK FROM BS 725Apr 25, 2008 · N367FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01630Seat Track · damagedMAIN CABIN SEAT TRACK IN BALLMAT AREA SCALLOPS BROKEN AND SEVERAL GOUGES AT STA 755 TO STA 763 LBL 9. DAMAGED SCALLOPS ON THE SEAT TRACK AT LBL 9 BS 755-763, FOUND TO BE OUT OF LIMITS REF SRM 53-70-00. REMOVED FLOOR PANELS TO GAIN ACCESS AT BS 615-890 LBL 9-2Apr 25, 2008 · N367FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01579Seat Track · gougedMAIN CABIN FLOOR SEAT TRACK SCALLOPS GOUGED AT STA 635 RBL 28. BLENDED GOUGES. GAP BETWEEN SCALLOPS IS 0.500 MAX ALLOWED. REMAINING 0.515. OUT OF LIMITS IAW SRM 53-70-00; VOL I; PG 21. REMOVED & REINSTALLED (2) FLOOR PANELS IAW SRM 51-31-01; VOL II; PApr 25, 2008 · N367FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01475Floorbeam · crackedCABIN OVERWING FLOOR SUPPORT BEAM IS CRACKED AT STA 1276 RBL 107; AT R-3 DOOR THRESHOLD. REPAIRED CRACKED BEAM AT STA 1276 BY SPLICING IN A NEW SECTION IN REF TO E.A. 8-5310-118481.Apr 22, 2008 · N367FE · Doug MD1010F · Fuselage Main, Floor BeamSDR 08FDEA01474Floorbeam · crackedCABIN OVERWING FLOORBEAM IS CRACKED AT STA 1295 RBL 107 AT THE R-3 DOOR THRESHOLD. REPAIRED CRACKED BEAM AT STA 1295 BY SPLICING IN A NEW SECTION IN REF TO EA 8-5310-118482.Apr 22, 2008 · N367FE · Doug MD1010F · Fuselage Main, Floor BeamSDR 07FDEA05043Door · separatedPOST FLIGHT WALK AROUND, DISCOVERED RT WING FUEL DOOR MISSING FROM A/C. INSTALLED RT WING REFUELING ACCESS PANEL DOOR IAW SMP. OPS CHECKS NORMAL. OK FOR SERVICE.Dec 12, 2007 · N367FE · Doug MD1010F · Fluid Service DoorsSDR 06FDEA03815Rib · crackedRT WING, L/E CRACK LONG 0.75" ON INTERNAL RIB AT STA XOS 498. REPAIRED RIB IAW SRM 57-20-00 FIG 1 SHT 1 AND 6 VOL 1.Oct 30, 2006 · N367FE · Doug MD1010F · Wing, Rib/BulkheadSDR 06FDEA03738Pressure Blkhd · crackedCLG W/W FOUND 1 CRACK 1" LONG ON VERTICAL BLKHD BTWN STA 1401 STA 1381 X = 32. DISASSEMBLED PNEU DUCTS ASSY ON BLKHD IAW MM 36-14-02-04. REMOVED SENSING ELEMENT IAW MM 36-23-00-00. REMOVED RIVETS ON STIFFENERS AND ON REINFORCE DOUBLER IAW SRM 51-35-01 VOL 2.Oct 20, 2006 · N367FE · Doug DC1010 · Fuselage Main, BulkheadSDR 06FDEA03737Shear Tie · corrodedDURING INSPECTION FWD CARGO BILGE FOUND SEVERE CORROSION WITH EXFOLIATION ON SHEAR CLIP AT STA 939 FROM STR NR 47 RT TO STR NR 48 RT. REMOVED CLIP IAW SRM 51-35-01 PAR 1-5 VOL 2. TRIMMED OUT SECTIONS OF SHEAR CLIP IAW SRM 53-00-00 FIG 10 VOL 1. INSTALLED NEOct 20, 2006 · N367FE · Doug DC1010 · Fuselage Internal Mounting StructureSDR 06FDEA03735Skin · crackedDURING INSPECTION, FOUND LOWER INTERIOR AND EXTERIOR SKIN PANEL ON HORIZONTAL STABILIZER, WITH CRACKS, SEE ATTACHED SHEET FOR BEST DETAIL. PANEL ALC7205-1 REMOVED AND REPLACED IAW SB 53-16 GROUP 1 AND FIG 7 SHT 1 STEPS 1-3, PANEL ALC7438-2 REPAIRED IAW SB 55-Oct 20, 2006 · N367FE · Doug DC1010 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA03734Frame · crackedLWR FUSELAGE CAC AT STA 1159 BTW LONG NR 29 AND LONG NR 30 LT SIDE ON FRAME FOUND CRACK 1" LONG AREA CLEANED IAW SRM 51-31-01 VOL 2 PAR 22. NDI INSP CARRIED OUT (SEE JPF). CRACK REMOVED IAW SRM 53-30-00 VOL 1 FIG 7 P/N'S I015877-3; -5; -13; -15. INSTALLED IOct 20, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA03733Rib · crackedLT WING L/E AT STA XOS 632 ON RIB FOUND CRACK .75"LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1SHT 1 AND 6 VOL 1.Oct 20, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA03564Skin · damagedINTERNAL FUSELAGE FWD CARGO COMPARTMENT FROM STA 1019 TO STA 1029 AT LONGERON 40 RT INTERNAL DOUBLER ON SKIN. REMOVED AND REPLACED FASTENERS IAW SRM 53-20-00 FIG 13 VOL 1.Oct 3, 2006 · N367FE · Doug DC1010 · Fuselage Main, Plate/SkinSDR 06FDEA03563Seat Track · damagedINTERNAL FUSELAGE MAIN CABIN FROM STA 515 TO STA 535 X= -47 RT SIDE SEAT TRACK REPAIR. REMOVED AND REINSTALLED NEW SEAT TRACK IAW DWG SP10580218.Oct 3, 2006 · N367FE · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03562Skin · bulgedUPPER FUSELAGE EXT SKIN FOUND SKIN BULGE ON R1 DOOR AT STA 445 LONG NR 26 RT. REPAIRED SKIN WITH FILLER AND DOUBLER IAW SRM 52-10-00 FIG 12A VOL 1 AND PROTECTED AREA IAW SRM 51-21-01 PAG 16 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I015181/N00181 ANDOct 3, 2006 · N367FE · Doug DC1010 · Fuselage Main, Plate/SkinSDR 06FDEA03561Rib · crackedRT WING TANK NR 3 STATION XORS 345 FWD OF STRINGER 43 CRACK ON RIB LOWER FRAME CHORD APPROX 0.45" LONG WING RIB XORS 346. CRACK STARTING FROM RADIUS AND RUNNING FORWARD. DAMAGED FLANGE TRIMMED. NEW PART P/N N01167-3. FABRICATED AND INSTALLED IAW SRM 57-20-Oct 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA03560Rib · crackedLT WING L/E AT STA XOS 454 ON RIB FOUND CRACK 1" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 3 VOL 1.Oct 3, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA03559Frame · crackedRT MLG W/W FOUND 1 CRACK 2" LONG ON FRAME AT STA 1505 X= -98. DISCONNECTED PIPES IAW MM 20-10-01-2. REMOVED PARTS IAW SRM 51-35-01 VOL 2 PAR 1-5. REPAIRED FRAME IAW SRM 53-00-01 VOL 1 FIG 8 SHEET 2-4. REINSTALLED PARTS IAW SRM 51- 35-01 VOL 2 PAR 1-5. RECOct 3, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA03262Skin · wornCTR CARGO DOOR FOUND DEEP WEAR ON EXT SKIN LOWER SIDE. TRIMMED OUT DAMAGED PORTION OF SKIN, AND INSTALLED 1EA FILLER AND 1EA EXTERNAL. REPAIR DOUBLER IAW SRM 52-10-00 VOL 1 FIG 17. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N/R N00621 AND IAW SRM 52-10-00 VSep 13, 2006 · N367FE · Doug DC1010 · Cargo/Baggage DoorsSDR 06FDEA03261Pressure Panel · unknownHORIZONTAL PRESSURE PANEL BETWEEN STA 535 AND 555 X= 86 LT SIDE WEB FOUND EXISTING DOUBLER. ACCOMPLISHED EA NR 8-5330-99720. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I016410/N01410 AND IAW EA NR 8-5330-99720.Sep 13, 2006 · N367FE · Doug DC1010 · Standard Practices/StructuresSDR 06FDEA03260Bulkhead · crackedNLG W/W FOUND 4 CRACKS ON VERTICAL BULKHEAD BTWN STA 583 AND STA 588 Z=-37 X=-24. ACCOMPLISHED NR 8-5330-100639. FABRICATED PARTS IAW DETAIL PARTS TRAVELER NR I015840/N00840 AND IAW EA NR 8-5330-100639, TOUCH UP WITH WHITE TOPCOAT IAW SRM 51-21-02 VOL 2.Sep 13, 2006 · N367FE · Doug DC1010 · Fuselage Main, BulkheadSDR 06FDEA03259Bulkhead · crackedAIR CONDITION COMPT LT FOUND 2 CRACKS 2" LONG ON VERTICAL BULKHEAD FROM STA 480 TO STA 493 Z=-58 X= 24. REPAIRED WEB IAW SRM 53-30-00 VOL 1 FIG 6 SHT 4,5,10. THIS NRC COVER FEDEX NRC N00845. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I016370/N01370 AND IAW Sep 13, 2006 · N367FE · Doug DC1010 · Fuselage Main, BulkheadSDR 06FDEA03248Bulkhead · corrodedAFT WASTE TANK COMPT FOUND SEVERE CORROSION ON "T" CAP VERTICAL BULKHEAD AT STA 2007 Z= -19 X= -55. REMOVED FLOOR PANELS TO ACCESS REPAIR IAW MM 20-50-02-2. REMOVED DAMAGED SECTION OF "T", FABRICATED AND INSTALLED "T" AND ANGLES IAW SRM 53-40-00 VOL 1 FIG 16Sep 12, 2006 · N367FE · Doug MD1010F · Fuselage Main, BulkheadSDR 06FDEA03247Rib · crackedLT WING L/E AT STA XOS 856 ON RIB FOUND CRACK 0.50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1/6 VOL 1.Sep 12, 2006 · N367FE · Doug MD1010F · Wing, Rib/BulkheadSDR 06FDEA03246Rib · crackedLEFT WING L/E AT STA XOS 1026 ON RIB FOUND CRACK 1" LONG. REPAIRED RIB IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PART TRAVELER I015458/N00458 AND IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1.Sep 12, 2006 · N367FE · Doug MD1010F · Wing, Rib/BulkheadSDR 06FDEA03213Bulkhead · crackedLT MLG WW AT STA 1490 X=32 Z=-65 ON SKIN BULKHEAD FOUND 4 CRACK 1" LONG TRIM DAMAGED AREA AND REPAIR IAW SRM 53-00-01 FIG 10 SHEET 4.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, BulkheadSDR 06FDEA03212Skin · damagedAFT CARGO DOOR EXT SKIN LWR CORNER EX REPAIR REMOVED AND REPAIRED IAW SRM 52-10-00 FIG 17 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Cargo/Baggage DoorsSDR 06FDEA03211Rib · crackedLT WING L/E CRACK LONG 0.5" ON RIB STA XORS 873 REPAIRED IAW SRM 57-00-01 FIG 3 SHEET 2 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA03210Rib · crackedLT WING L/E CRACK LONG 1" ON RIB STA XORS 824 REPAIRED IAW SRM 57-20-00 FIG 1 SHEET 3.Sep 6, 2006 · N367FE · Doug DC1010 · Wing, Rib/BulkheadSDR 06FDEA03209Intercostal · crackedRT WING L/E CRACK LONG 1" ON INTERNAL INTERCOSTA AT STA XORS 540 REPAIRED IAW SRM 57-00-01 FIG 10 SHEET 1.Sep 6, 2006 · N367FE · Doug DC1010 · Wing Miscellaneous StructureSDR 06FDEA03208Bulkhead · crackedRT MLG W\W FOUND 1 CRACK 0.25 LONG AND 3 RIVETS LOOSE ON VERTICAL BLKD AT STA 1395 X=-32. REPAIRED IAW SRM 53-00-01 VOL1 FIG 4.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, BulkheadSDR 06FDEA03207Frame · corrodedAIR COND COMPT LT FOUND CORROSION ON FRAME AT STA 542 X=30 CUT FRAME AND REPAIR IAW SRM 53-30-00 VOL 1 FIG 5.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA03206Frame · damagedINTERNAL FUSELAGE AVIONICS COMPT AT STA 322 X=60 EXISTING FRAME REPAIR, REPLACE PARTS IAW DWG ABA 7034 AND ABA 7202.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA03205Bulkhead · damagedINTERNAL FUSELAGE AFT CARGO COMPT AT STA 2007 PRESS BULKD BETWEEN 51 LT TO 51 RT, EXISTING REPAIR REPAIRED IAW SRM 53-40-00 FIG 9 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, BulkheadSDR 06FDEA03204Beam · crackedFWD CARGO STA 1099 STRINGER 43 LT BILGE AREA CRACK 4.5' ON BEAM. REPLACED BEAM IAW DWG AFA0039.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Miscellaneous StructureSDR 06FDEA03203Frame · crackedMAIN CABIN AT STA 1721 L13 RT SIDE ON FRAME FOUND CRACK 5" LONG CUT FRAME IAW SRM 53-30-00 FIG 5 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA03202Frame · crackedMAIN CABIN AT STA 1741 L13 RT SIDE ON FRAME FOUND CRACK 0,5" LONG REPAIRED FRAME IAW SRM 53-30-00 FIG 4 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA03201Frame · crackedMAIN CABIN AT STA 1761 L13 RT SIDE ON FRAME FOUND CRACK 5" LONG CUT FRAME AND REPAIRED IAW SRM 53-30-00 FIG 5 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA03200Frame · crackedMAIN CABIN AT STA 1781 L13 LT SIDE ON FRAME FOUND CRACK 6" LONG CUT FRAME AND REPAIRED IAW SRM 53-30-00 FIG 5 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA03199Frame · crackedMAIN CABIN AT STA 1801 L13 LT SIDE ON FRAME FOUND CRACK 6" LONG CUT FRAME AND REPAIRED IAW SRM 53-30-00 FIG 5 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, FrameSDR 06FDEA03198Skin · damagedEXTERNAL FUSELAGE MAIN CABIN STA 481 X= 70 LT SIDE EXISTING DOUBLER REMOVED AND REPAIRED IAW SRM 53-20-00 FIG 6 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, Plate/SkinSDR 06FDEA03197Door Frame · damagedINTERNAL FUSELAGE MAIN CABIN STA 1305 TO 1315 BETWEEN LONG 26 TO 27 RT R3 DOOR JAMB EXISTING REPAIR REMOVED AND REPAIRED IAW SRM 53-50-00 FIG 19 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, StructureSDR 06FDEA03196Door Frame · damagedINTERNAL FUSELAGE MAIN CABIN STA 1305 TO 1315 BETWEEN LONG 26 TO 27 LT R3 DOOR JAMB EXISTING REPAIR REMOVED AND REPAIRED IAW SRN 53-50-00 FIG 19 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, StructureSDR 06FDEA03195Door Frame · damagedINTERNAL FUSELAGE MAIN CABIN STA 1305 TO 1315 BETWEEN LONG 26 TO 27 RT R3 DOOR JAMB EXISTING REPAIR REVED AND REPAIR IAW SRM 53-50-00 FIG 19 VOL 1.Sep 6, 2006 · N367FE · Doug DC1010 · Fuselage Main, Structure
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