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 FDEA202307141216Shear Tie · cracked1EA ATTACH CLIP IS CRACKED AT #2 PYLON AFT BULKHEAD ON INBD SIDE AT APPROX NAC STA 295, JUST BELOW INBD MID-SPAR FITTING REMOVED AND REPLACED #2 PYLON, INBOARD SHEAR TIE AT NAC STA 297 IAW BAC DWG 313T2310, SHEET 95, REVISION -SDR FDEA202307121203Bracket · cracked#1 PYLON/NACELLE, I/B SIDE, ACCESSED BY PANEL 437BR, HYD. RESERVOIR BAY FWD BULKHEAD UPPER CORNER ATTACH BRACKET CRACKED REMOVED AND REPLACED ATTACH BRACKET LOCATED ON #1 PYLON/NACELLE, I/B SIDE, ACCESSED BY PANEL 437BR, HYD. RESERVOIR BAY FWD BULKHEAD UPPSDR FDEA202307121200Slat · damagedRH #8 SLAT LOWER SURFACE T/E FOUND A NICK AT I/B AUXILIARY TRACK POSN. REPAIRED THE NICK ON RH #8 SLAT PER B767 SRM57-43--02-2R & SRM51-70-10-2R REPAIR 4. THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100. TRACKING EA: H-5750-T0375302 P1 WAS ISSUSDR FDEA202307101195Fitting · cracked#1 PYLON AFT FAIRING, INBD SIDE FRAME, NAC STA 380, MID ATTACH CLIP, IS CRACKED. REMOVED AND REPLACED ATTACH CLIP (BRACKET) LOCATED ON #1 PYLON AFT FAIRING, INBD SIDE FRAME, NAC STA 380, PER BOEING DWG 313T2303, REV -SDR FDEA202307101194Fitting · cracked#2 PYLON AFT FAIRING, OTBD SIDE, FRAME ATTACH CLIP, AT APPROX. NAC STA 380, IS CRACKED REMOVED AND REPLACED ATTACH CLIP LOCATED ON #2 PYLON AFT FAIRING, OTBD SIDE, FRAME ATTACH CLIP, AT APPROX. NAC STA 380, PER BOEING DWG 313T2303, REV -SDR IXXA2022071004Cowling · damaged#2 ENGINE I/B CORE COWL HAS A HOLE IN THE UPPER AFT EXTERIOR NAC 220-225SDR FDEA202307081186Former · failedNOSE FORMER ANGLE CRACKED AT RIGHT WING OSS 565. VISUALLY INSPECTED FORMER AT FLE OSS 565 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F & A WITH SRM TR 57-111 AS REFERENCE.SDR FDEA202307081185Former · failedNOSE FORMER ANGLE CRACKED AT THE RIGHT WING OSS 499.6. PER EA H-5720-T0367172 REV A VISUALLY INSPECTED FORMER AT FLE OSS 499.603 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F WITH SRM TR 57-111 AS REFERENCE.SDR FDEA202307071174Floor Panel · dentedDENTS ON FLOOR PANEL 221DFF SECTION 41 OF MDC. FLOOR PANEL 221DFF SEC.41 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15,2022SDR FDEA202307071173Floor Panel · dentedDENTS ON FLOOR PANEL 221CFF SECTION 41 OF MDC. FLOOR PANEL 221CFF SECTION 41 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307071172Floor Panel · dentedDENTS ON FLOOR PANEL 222AFF SECTION 41 OF MDC. FLOOR PANEL 222AFF SECTION 41 OF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R, FIG.201 SHEET 2 REV.85 DEC 15-22SDR FDEA202307071171Floor Panel · dentedDENTS ON FLOOR PANEL 222BFF SECTION 41 OF MDC. FLOOR PANEL 222BFF SECTION 41 OF MDC WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR.4.B FIG 201 REV.85 DEC 15/2022SDR FDEA202307071170Floor Panel · dentedDENTS ON FLOOR PANEL 222CFF SECTION 41 OF MDC. FLOOR PANEL 222CFF SEC.41 OF MDC WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307071169Bracket · crackedRIGHT WING FUELING STATION PANEL HOLD OPEN SUPPORT BRACKET CRACKED REMOVED AND REPLACED SUPPORT BRACKET ON RIGHT WING FUELING STATION PANEL PER BOEING DWG 114T2450, SHT 1, REV JSDR FDEA202307071168Bracket · crackedRIGHT WING FUELING STATION PANEL LIGHT SUPPORT BRACKET CRACKED REMOVED AND REPLACED LIGHT SUPPORT BRACKET ON RIGHT WING FUELING STATION PANEL PER BOEING DWG 284T0562, SHT 1, REV B,SDR FDEA202307061217Skin · gougedLH HORIZONTAL STAB. UPPER SKIN IS DENTED AND GOUGED AT APPROX 75" OB OF STAB. ROOT, JUST AFT OF LE PANEL 332BL. REPAIRED LH HORIZONTAL STABILIZER UPPER SKIN DENT AND GOUGE APPROX 75" OB OF STAB. ROOT, JUST AFT OF LE PANEL 332BL AS REQUIRED IAW FDX B767 SRMSDR IXXA2023070203Stringer · crackedSTRINGER CAP CRACKED @ STA 340,S24RSDR IXXA2023070202Seal Depressor · damagedMCD CUTOUT FORWARD LOWER CORNER DAMAGEDSDR IXXA2023070201Seal Depressor · damagedMCD CUTOUT AFT LOWER CORNER DAMAGEDSDR FDEA202306291126Slat · damagedPERFORM MAJOR REPAIR TO SLAT #11 TRAILING EDGE WEDGE IN ACCORDANCE WITH 51-70-10-2R IN THE AREA OF SLAT #11 OSS 933.729. REF B767 SRM51-70-10-2R REPAIR4 & EA:H-5750-T0369144 P3 REPAIR THE #11 SLAT TRAILING EDGE WEDGE AT OSS 933.729. EA TITLE: WINGS - RHSDR IPXA2023071240405Aileron · unknown*SUPPLEMENTAL SDR* ON WAI RIGHT AILERON SHOWS LIGHTENING STRIKE***SM40/LMX3*** EO-87507-REQ2 ASSIGNED TO THE FAULT. NEW MOMENT OF -113.6125 ADDED AS NOTE TO THE TRACKED AILERON. C/WSDR IPXA2023062940405Unknown · unknown*SDR FILED OPEN* *MAJOR REPAIR* ON WAI RIGHT AILERON SHOWS LIGHTENING STRIKE***SM40/LMX3*** ASSIGNED EO-87507-PRELIM3 TO FAULTSDR FDEA202306271123Former · crackedR/W L/E FORMER CRACKED STA OSS 499 0000237172 : LAFFOND, MARK P - 27-JUN-2023 19:21 REMOVED AND INSTALLED NEW FORMER A R/H L/E OSS 499. REF SR 67-57-002 REV F. (MPN: B67-57-002-12)SDR FDEA202306271122Former · crackedR/W L/E FORMER CRACKED STA OSS 437 CORRECTION, STA OSS 565 INSTEAD OF STA OSS 437 0000358872 : FERGUSON, STEVE M - 27-JUN-2023 19:18 REMOVED AND INSTALLED NEW FORMER ON RIGHT WING FIXED LEADING EDGE AT OSS 565 REF SR67-57-002 REV F (MPN: B67-57-002-06)SDR FDEA202306271121Former · crackedR/W L/E FORMER CRACKED STA OSS 441 0000245521 : EDWARDS, WILLIAM B - 27-JUN-2023 19:14 REMOVED AND REPLACED PANEL 621ANB FOR FORMER ACCESS REF B767 AMM 57-41-57-4. REMOVED AND REPLACED R/W L/E FORMER AT STA 441, REF FEDEX DRAWING SR67-57-002, SHEET 3. (MPN:SDR IXXA2023062703Skin · abnormalHOLE IN SKIN FOUND @ STA 344, S21RSDR IXXA2023062702Support · crackedLW, T/E, I/B FLAP ANGLE GEARBOX SUPPORT PLATE CRACKEDSDR IXXA2023062701Seat Track · crackedFIRST OFFICERS FWD SEAT TRACK CRACKEDSDR FDEA202306251103Web · crackedAFT CARGO COMPARTMENT BETWEEN STA 1329 AND BL 0 FLOOR SUPPORT STIFFER WITH CRACK. THE PANEL THE FLOOR SUPPORT STIFFER WAS REPLACED AT AFT CARGO COMPARTMENT BETWEEN STA 1329 AND BL 0 IAW SRM 51-10-02-0G PARAGRAPH (9) REV. 85 DEC 15,2022 DRAWING 451T2612 SSDR FDEA202306251102Panel · dentedMDC FLOOR PANEL 222CFF WITH DENTS. FLOOR PANEL 222 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG.201 SHEET 2 REV.85 DEC 15/22SDR FDEA202306251101Panel · dentedMDC FLOOR PANEL 222BFF WITH DENTS. FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R. FIG.201 SHEET 2 REV.85 DEC15/22SDR FDEA202306251100Panel · dentedMDC FLOOR PANEL 222AFF WITH DENTS. FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG. 201 SHEET 2 REV. 85 DEC15/22SDR FDEA202306251099Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS. MDC FLOOR PANEL 221CFF WAS REPAIRED WITH B767 SRM 53-00-50-2R FIG. 201 SHEET 2 REV. 85 DEC15/22SDR FDEA202306251098Panel · dentedMDC FLOOR PANEL 221DFF WITH DENTS. MDC FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG. 201 SHEET 2 REV. 85 DEC15/22SDR FDEA202306241091Bracket · crackedRH WING OUTBD LEADING EDGE, FUELING STATION DOOR HOLD-OPEN BRACKET AT INBD EDGE OF DOOR IS CRACKED REMOVED AND REPLACED BRACKET IAW BAC DWG 114T2450, SHEET 1, REVISION JSDR FDEA202306241090Panel · dentedRH WING LOWER O/B ACCESS PANEL 643BB IS DENTED ON LOWER SURFACE REPAIRED RH WING LOWER O/B ACCESS PANEL 643BB REMOVING DAMAGE ON LWR SURFACE, CLEANING, POTTING HOLE REPAIR, LAYING UP REPAIR DOUBLER AND CURED IAW B767 SRM 57- 20-01-2R FIG. 201 REP 7 AND SRM SDR FDEA202306231081Bracket · crackedR/W, I/B LEADING EDGE, LES 283, TORQUE TUBE SUPPORT BRACKET IS CRACKED REMOVED CRACKED TORQUE TUBE BRACKET ON RIGHT WING I/B LEADING EDGE LES 283 IAW FEDEX B767 SRM 51-40-02-0G AND REPLACED WITH NEW TORQUE TUBE BRACKET PN 256T2425-5, P.O 1060626.1 PER BOEISDR FDEA202306231080Spoiler · crackedRH WING, SPOILER 7, UPPER SURFACE WITH PUNCTURE. RH WING, SPOILER #7, UPPER SURFACE WAS REPAIRED IAW B767 SRM 57-70-01-2R, FIG. 201 SHEET 4, PAGE 1-4 AND SRM 51-70-04-0G, PARA. 5.A., FIG. 5, PAGE 30, 48, 61 REV. 85 DEC15-22SDR FDEA202306211066Flap · dentedLEFT WING, OUTBOARD FLAP LOWER SKIN WITH DENT AT 6" FROM LOWER EDGE AND 21" FROM INBOARD EDGE D= 0.023" L= 2.250" W= 1.220" LEFT WING, OUTBOARD FLAP LOWER SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R, FIG 201 SHEET 1, 3-6 AND SRM 51-70-06-0G, FIG 9 SHEET SDR FDEA202306201269Former · crackedFOUND NOSE FORMER ANGLE AT OSS 441 RIGHT SIDE WING FIXED LEADING EDGE TO BE CRACKED. REMOVED AND REPLACED FORMER AS REQUIRED PER DWD SR67-57-002.SDR FDEA202306201065Panel · dentedMDC FLOOR PANEL 221DFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 221 DFF UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PARA. 4.B. FIG. 201 SHEET 2, PAGE 1-16 REV. 85 DEC15/22SDR FDEA202306201064Panel · dentedMDC FLOOR PANEL 222CFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 222 CFF ALONG UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PARA. 4.B. FIG. 201 SHEET 2, PAGE 1-16 REV. 85 DEC15/22SDR FDEA202306201063Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 221 CFF, UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PARA. 4.B. FIG. 201 SHHET 2, PAG. 1-16 REV.85 DEC15/22SDR FDEA202306201062Panel · dentedMDC FLOOR PANEL 222AFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 222 AFF, UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PAR. 4.B. FIG. 201 SHEET 2, PAG. 1-16 REV. 85 DEC15/22SDR FDEA202306201061Panel · dentedMDC FLOOR PANEL 222BFF WITH DENTS ALONG UPPER SURFACE. SECTION 41. MDC FLOOR PANEL 222 BFF, UPPER SURFACE WAS REPAIRED IAW B767 SRM 53-00-50-2R, PARA. 4.B. FIG. 201 SHEET 2, PAGE 1-16 REV. 85 DEC15/2022SDR FDEA202306171050Beam · crackedTHIS SDR IS A CORRECTION TO SDR 23-1014 (AS IT CALLED OUT P5 INSTEAD OF P6 OF EO E.O. H- 5720-E0353920 REV A) A DETAILED INSPECTION OF THE 113T1913-24 SUPPORT BEAM AT THE WS 1054 UPPER CHORD ATTACHMENT SHOWED A CRACK INDICATION. REF IN STEP 5.E COMPLIED WSDR FDEA202306171049Beam · crackedTHIS SDR IS A CORRECTION TO SDR 23-1015 (AS IT CALLED OUT P5 INSTEAD OF P6 OF EO E.O. H- 5720-E0353920 REV A) A DETAILED INSPECTION OF THE 113T1913-26 SUPPORT BEAM AT THE WS 1098 UPPER CHORD ATTACHMENT SHOWED A CRACK INDICATION. REF IN STEP 5.E COMPLIEDSDR FDEA202306151044Skin · delaminatedRUDDER , R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE ON THE AFT EDGE. REPAIRED RUDDER , R/H EXTERNAL SURFACE APPROX 8FT UP FROM THE FUSELAGE ON THE AFT EDGE BY REMOVING DAMAGE , CLEANING AREA , LAYING UP REPAIR PLIES AND CURED IAW B76SDR FDEA202306151043Skin · delaminatedRUDDER , R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE APPROX 10" FWD OF THE AFT EDGE REPAIRED R/H EXTERNAL SURFACE OF RUDDER APPROX 8FT UP FROM THE FUSELAGE ,APPROX 10" FWD OF AFT EDGE BY REMOVING DAMAGE , CLEANING AREA , LAYING UP RESDR FDEA202306151042Skin · delaminatedRUDDER , R/H EXTERNAL SURFACE IS DELAMINATED APPROX 8FT UP FROM THE FUSELAGE APPROX 27" FWD OF THE AFT EDGE REPAIRED RUDDER , R/H EXTERNAL SURFACE , APPROX 8FT UP FROM THE FUSELAGE , APPROX. 27" FWD OF THE AFT EDGE BY REMOVING DAMAGE , CLEANING , LAYING UP
Back to Boeing 767-300