Boeing 767-300
Service difficulty reports · 2,148
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '767300' 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.
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 aircraft_model_key = '767300' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202306141036Beam · crackedL/H WING T/E SUPPORT STRUCTURE IS CRACKED AT APPROX WS 1030 REMOVED & REPLACED LEFT WING TRAILING EDGE PANEL SUPPORT BEAM IAW BAC DWG 113T1913, REVISION ASDR FDEA202306131030Angle · crackedMAIN CABIN FLOORBEAM AT STA 1575 RBL 65-68, ATTACH ANGLE IS CRACKED FABRICATED AND REPLACED CRACKED ATTACH ANGLE AT STA 1575, RBL 65-68, PER BOEING DWG 146T5650, SHT 5, REV C. FABRICATION OF ATTACH ANGLE, 146T5651-6 AND 146T5651-8, COMPLETED ON WORK CARD, SDR FDEA202306131029Angle · crackedMAIN CABIN FLOORBEAM AT STA 1575 LBL 65, ATTACH ANGLE IS CRACKED FABRICATED AND REPLACED CRACKED ATTACH ANGLE AT STA 1575, LBL 65, PER BOEING DWG 146T5650, SHT 5, REV C. FABRICATION OF ATTACH ANGLE, 146T5651-5, COMPLETED ON WORK CARD, WO#83419, NR#N00131.SDR FDEA202306131028Slat · gougedLW #5 SLAT LWR TE HAS 2 GOUGES . CLEANED SANDED REMOVED DAMAGE AND REPAIRED LW #5 SLAT LWR TE 2 GOUGES WITH PERMANENT REPAIR IAW B767 SRM 57-43-02 AND 51-70-10-2R REPAIR 4SDR FDEA202306121025Flap · dentedRH WING, OUTBOARD FLAP, LOWER SURFACE WITH DENT AT 52" FROM OUTER EDGE AND 10.75" FROM LOWER EDGE. RH WING, OUTBOARD FLAP, LOWER SURFACE, DENT WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG. 201 SHEET 6 REPAIR 1 AND SRM 51-70-06-0G PAR. 5.A. FIG. 9 REV. 85 DECSDR FDEA202306111023Slat · dented#8 SLAT LOCATED JUST OB OF OB TRACK, SLAT TE HAS A DENT . CLEANED SANDED AND REMOVED DAMAGE ON RIGHT WING #8 SLAT AND REPAIRED IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REPAIR 4, REPAIR WAS A PERMANENT REPAIR ON #8 SLAT JUST O/B OF O/B TRACK / SLAT T/E.SDR FDEA202306091015Support Beam · crackedA DETAILED INSPECTION OF THE 113T1913-26 SUPPORT BEAM AT THE WS 1098 UPPER CHORD ATTACHMENT SHOWED A CRACK INDICATION. REF IN STEP 5.E COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098SDR FDEA202306091014Support Beam · crackedA DETAILED INSPECTION OF THE 113T1913-24 SUPPORT BEAM AT THE WS 1054 UPPER CHORD ATTACHMENT IN STEP 5.C SHOWED CRACK INDICATIONS. COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SBSDR FDEA202306091013Support Beam · crackedDURING DETAILED INSPECTION OF THE 113T1913-25 SUPPORT BEAM AT THE WS 1098 UPPER CHORD ATTACHMENT CRACKS WERE NOTED. COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-0136.SDR FDEA202306091012Support Beam · crackedDURING DETAILED INSPECTION OF THE 113T1913-23 SUPPORT BEAM AT THE WS 1054 UPPER CHORD ATTACHMENT CRACKS WERE NOTED. COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5): LS WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-01SDR FDEA202306081009Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202306081008Panel · dentedMDC FLOOR PANEL 222CFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202306081007Panel · dentedMDC FLOOR PANEL 222BFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/22SDR FDEA202306081006Panel · dentedMDC FLOOR PANEL 222AFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202306081005Panel · dentedMDC FLOOR PANEL 221DFF WITH DENTS ALONG SURFACE. MDC FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/22SDR FDEA202306071018Support · crackedL/W LWR T/E PANEL 113T1657-21 AFT UPPER SUPPORT CHORD CRACKED AT ATTACH POINTS WS 1072-1127. COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5) & PART 6 (P6): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-0136; WHICH CALLSDR FDEA202306071017Support · crackedL/W LWR. T/E PANEL 113T165-29 UPPER SUPPORT CHORD CRACKED AT ATTACH POINTS WS 1032-1070 COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5) & PART 6 (P6): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-0136; WHICH CALL FOR SDR FDEA202306071016Panel · damagedLH WING-OUTBOARD TOP PANEL HAS SEVERAL MISSING RIVETS COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5) & PART 6 (P6): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-0136; WHICH CALL FOR BOTH SIDES TO HAVE PARTS REPLACESDR FDEA202306070998Roller · out of alignmentL1 ENTRY DOOR MISALIGNED AND WILL NOT CLOSE. FOUND MOVABLE CEILING PANEL ROLLER OUT OF TRACK, REPOSITIONED ROLLER, OPS CHK GOOD. A/C OK FOR SERVICE.SDR CNMA2023F00205Relay · inoperativeRAT DID NOT DEPLOY DURING AUTO DEPLOYMENT TEST ~ RAT DEPLOY RELAY K235 REPLACED RAT AUTO DEPLOY TESTED SERVICEABLE IAW B767-300 AMM 29-21-00-735-048 REV 139.SDR FDEA202306050995Bracket · crackedRW INBD L/E AT STA LES 285 TORQUE TUBE GUIDE BRACKET IS CRACKED REMOVED AND REPLACED RIGHT WING, INBOARD LEADING EDGE, TORQUE TUBE GUIDE BRACKET IAW B767 SRM 51-40-02-0G AND BAC DWG 114T1240, SHEET 6, REVISION -SDR FDEA202305300973Door · gouged#1 ENGINE I/B T/R LOWER FWD PANEL INNER SURFACE HAS 2EA GOUGES AS MARKED REPAIRED #1 ENGINE, INBOARD TR, FWD BLOWOUT DOOR IAW FEDEX EA# H-7830-T0374581-P1, TITLED " EXHAUST SYSTEM - THRUST REVERSER GEN - #1 INBD TR, BLOWOUT DOOR, GOUGE"SDR FDEA202305280968Display · unknownAFTER FO MCDU FAILURE, SMELL OF ACRID SMOKE ON FLIGHT DECK. EMERGENCY DECLARED ON ARRIVAL INTO KGEG. EMERGENCY DECLARED. SMELL CONFIRMED TO BE ORIGINATING FROM F/O'S MCDU. NO OTHER DAMAGE NOTED AFTER INPECTION REF WRI 34-61/2194 FOR CORRECTIVE ACTION. C/SDR FDEA202305260966Elt · unknownELT HAS BEEN DETECTED EMITTING DURING FLIGHT. FOR INFO: IST STATION LOCAL TOWER WARNED US FOR ELT SIGNAL. RELEASED FOR SERVICE PER MEL : 25-63-10-02-A ON ARRIVAL ELT SWITCH (GUARDED) THAT IN THE OVERHEAD PANEL FOUND ARM POSITION. YESTERDAY HAPPENED ONE SDR FDEA202305260959Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221CFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR.4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260958Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260957Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222BFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260956Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260955Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260954Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222AFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260951Frame · cracked#1 PYLON, HYDRAULIC BAY, OUTBOARD MID SPAR FITTING IS CRACKED REPAIRED #1 PYLON, AFT FAIRING ASSY, NAC STA 329 MID SPAR FRAME IAW B767 SRM 54-52-71- 2R, REPAIR 4.SDR FDEA202305260950Slat · wornLH WING, SLAT# 5, TRAILING EDGE, LOWER SURFACE (INTERIOR) WITH WEAR ON TWO POINTS. LH WING, SLAT #5, TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-43-02-2R REP.1 FIG. 201 SHEET 1 AND SRM 51-70-10-2R REP. 4 FIG. 202 SHEET 8 REV. 85 DEC15/2022SDR FDEA202305260949Slat · wornLH WING, SLAT# 5, TRAILING EDGE, LOWER SURFACE (INTERIOR) WITH WEAR ON TWO POINTS. LH WING, SLAT #5, TRAILING EDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-43-02-2R REP.1 FIG. 201 SHEET 1 AND SRM 51-70-10-2R REP. 4 FIG. 202 SHEET 8 REV. 85 DEC15/2022SDR FDEA202305260947Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-8, WO# 85583, NR# N00127. PER BOEING DWG 146T5651, SHT 5, REV CSDR FDEA202305260946Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-6, WO# 85583, NR# N00112. PER BOEING DWG 146T5651, SHT 5, REV CSDR FDEA202305260945Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-5, WO# 85583, NR# N00113. PER BOEING DWG 146T5651, SHT 5, REV CSDR FDEA202305260944Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-7, WO# 85583, NR# N00128. PER BOEING DWG 146T5651, SHT 5, REV CSDR FDEA202305250941Unknown · wornNUMBER 1 R/H THRUST REVERSER DEFLECTORS AFT SUPPORT RING CHAFFED AT UPPER BALLSCREW ACTUATOR. M.W.T. T.R. P/N 681L270G13 MSN REPAIRED AREA AS REQUIRED. REF E.A. H-7830-T0374585 AND CFM-80 CMM 78-32-02SDR FDEA202305240935Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-6, WO# 85583, NR# N00112. PER BOEING DWG 146T5651, SHT 5, REV CSDR FDEA202305240934Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-8, WO# 85583, NR# N00127. PER BOEING DWG 146T5651, SHT 5, REV CSDR FDEA202305240933Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-5, WO# 85583, NR# N00113. PER BOEING DWG 146T5651, SHT 5, REV CSDR FDEA202305240932Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-7, WO# 85583, NR# N00128. PER BOEING DWG 146T5651, SHT 5, REV CSDR FDEA202305230927Access Panel · dentedMAIN CARGO COMPARTMENT FLOOR ACCESS PANEL 221DFF WITH DENTS. MAIN CARGO COMPARTMENT FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305230926Access Panel · dentedMAIN CARGO COMPARTMENT FLOOR ACCESS PANEL 221CFF WITH DENTS. MAIN CARGO COMPARTMENT FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305230925Access Panel · dentedMAIN CARGO COMPARTMENT FLOOR ACCESS PANEL 222AFF WITH DENTS. MAIN CARGO COMPARTMENT FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305230924Access Panel · dentedMAIN CARGO COMPARTMENT FLOOR ACCESS PANEL 222BFF WITH DENTS. MAIN CARGO COMPARTMENT FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG. 201 PAR. 4.B. SHEET 2 REV. 85 DEC15/2022SDR FDEA202305230923Access Panel · dentedMAIN CARGO COMPARTMENT FLOOR ACCESS PANEL 222CFF WITH DENTS. MAIN CARGO COMPARTMENT FLOOR PANEL 222 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR IXXA202305250001Power Supply · inoperativeEMERGENCY LIGHTS FWD FUSELAGE BELOW L1 DOOR AND ENTRANCE INOPSDR FDEA202305220914Slat · chafed#5 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OF OBRD MAIN TRACK. REPAIRED #5 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OUTBOARD MAIN TRACK WITH PERMANENT REPAIR IAW B767 SRM 57-43-02-2R FIG 201 SHEET 1 AND 51-70-10-2R REPAIR 4.SDR FDEA202305220913Flap · damagedLW INBOARD MAIN FLAP, UPPER SKIN HAS DAMAGE ON OB EDGE. REPAIRED LW INBOARD MAIN FLAP, UPPER SURFACE SKIN IAW FED EX EA H-5750-T0374477-P1- WING-FLIGHT SURFACES-LH INBD MAIN FLAP, FRANGIBLE STRUCTURE ASSY UPPER SKIN, NICK.
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