Boeing 767-300
Service difficulty reports · 2,148
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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 NACA202308030001Unknown · unknownRIGHT PACK INOP LIGHT ILLUMINATED. WENT OUT IN STBY NORMAL POSITION FOR FLIGHT. DEFERRED PER MEL 21-51-01-01/SDR FDEA202308031356Floor Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS MDC FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201. REV APR 15 2023SDR FDEA202308031355Floor Panel · dentedMDC FLOOR PANEL 221DFF WITH DENTS MDC FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4B FIG 101 SHEET 2 REV 86 APR 15 2023SDR FDEA202308031349Display · burnedLOUD POP FOLLOWED BY BURNT ELECTRICAL SMELL WHEN F/O S MCDU FAILED. CIRCUIT BREAKER ALSO POPPED. R&R FO'S FMC CDU IAW ABOVE REFERENCE, ALL CKS GOOD. AC OK TO CONTINUE.SDR FDEA202308031353Floor Panel · dentedMDC FLOOR PANEL 222BFF WITH DENTS MDC FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 101 SHEET 2. REV 86 APR 15 2023SDR FDEA202308031352Floor Panel · dentedMDC FLOOR PANEL 222AFF WITH DENTS MDC FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR FIG 201 SHEET 2. REV 86 APR 15 2023SDR FDEA202308031351Floor Panel · dentedMDC FLOOR PANEL 222CFF WITH DENTS MDC FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 SHEET 2. REV 86 APR 15 2023SDR FDEA202308031350Slat · wornLH WING SLAT #4 TRAILING EDGE, INTERNAL SURFACE WITH WEAR. LH WING SLAT #4 TRAILING EDGE, INTERNAL SURFACE WAS REPAIRED IAW B767 SRM 57-43-02-2R, REP. 1 FIG 201 SHEET 1-2 AND SRM 51-70-10-2R REP. 4 FIG 202 SHEET 8-9. REV 86 APR 15 2023SDR NACA2023080200001Unknown · unknown#1 ENGINE BLADE #16 HAS NICK. REPAIRED LEFT ENGINE #16 BLADE LEADING EDGE. FOUND WITHIN LIMITS PER B767 AMM 72-31-02SDR FDEA202308021344Unknown · unknownESCAPE ROPE FOR CREW ENTRY DOOR IS PARTIALLY OUT OF ITS POCKET JAMMING THE DOOR. REINSTALLED EMERGENCY ECSAPE ROPE AS REQUIRED IAW MM 25-61-04-2-1. OK FOR SERVICESDR IXXA2023080103Acoustic Panel · delaminated#2 PYLON O/B STRUT FAIRING SKIN ( ARROWHEAD PANEL ) DELAMINATEDSDR IXXA2023080102Skin Panel · bulged#1 PYLON I/B STRUT FAIRING SKIN/ ARROWHEAD PANEL BULGEDSDR IXXA2023080101Acoustic Panel · delaminated#1 PYLON PANEL 436CR SEPARATED BETWEEN THE METAL BACKING AND OUTER SKINSDR FDEA202307291333Beam · worn#1 ENGINE INBD PYLON ACCESS PANEL (437BR) CENTER 2 HINGE FITTINGS WORN. C/W EA H-5451-T0375481 P1SDR FDEA202307291332Beam · worn#1 ENGINE OTBD PYLON ACCESS PANEL (437BL) AFT HINGE ARM WORN. BOLT IS PULLED ALMOST COMPLETELY THROUGH HINGE FITTING. REPAIRED #1 ENGINE OTBD PYLON ACCESS PANEL (437BL) AFT HINGE ARM REF. EA H-5451-T0375479 P1SDR FDEA202307271320Slat · gougedRW #8 SLAT LOWER T/E SURFACE AFT OF I/B AUX TRACK GUIDE ARM IS GOUGED REPAIRED RW #8 SLAT LOWER T/E SURFACE AFT OF I/B AUX TRACK GUIDE ARM IAW B767 SRM 57- 43-02-2R AND 51-70-10-2RSDR FDEA202307271319Aileron · damagedLEFT WING I/B AILERON I/B L/E ATTACH FAIRING HAS EXPOSED COMPOSITE MATERIAL COMPLETED PERMANENT REPAIR TO L/H WING AILERON I/B L/E ATTACH FAIRING IAW B767 SRM 51-70-05-0G AND 57-60-01.SDR FDEA202307271318Bracket · crackedLW INBD L/E AT LES 289 SLAT TORQUE TUBE GUIDE BRACKET IS CRACKED IN SEVERAL PLACES REMOVED AND REPLACED GUIDE BRACKET IAW BOEING DRAWING 114T1240, SHEET 6, REV -SDR NACA2023073150002Unknown · unknownL ENG EEC1 ON STATUS PAGE. ACCOMPLISHED PIMU BITE PROCEDURE FIM 7101 FT 803 MESSAGE CLEARED.SDR FDEA202307251293Skin · gougedGOUGE ON LH FUSELAGE SKIN AT STA 1848.35 AND LBL 9.25 LH UPPER FUSELAGE SKIN AT STA 1848.35 AND LBL 9.25 WAS REPAIRED IAW E-A,#: H-5330- T0375329SDR FDEA202307251291Beam · cracked#2 PYLON, O/B WING DOOR ATTACH ANGLE IS CRACKED REPARED #2 PYLON, OUTBOARD LATCHBEAM IAW EA# H-5450-T0375415-P1, RELEASED AUG 01, 2023,SDR FDEA202307241331Unknown · unknownRUDDER TIP HAS WEAR ON UPPER LEADING EDGE. PERFORMED PERMANENT REPAIR OF RUDDER TIP UPPER LEADING EDGE IAW FDX B767-300 SRM 55-40-30-2R, FDX B767-300 SRM 55-40-30-2R, FDX B767 SRM 51-70-17-0G, AND FDX B767 SRM 51-70-14-0G. NO FURTHER ACTION REQUIRED.SDR FDEA202307241283Unknown · unknownRUDDER TRAILING EDGE UPPER TIP WITH LIGHTNING STRIKE. RUDDER TRAILING EDGE UPPER TIP DAMAGE WAS REMOVED IAW B767 SRM 55-40-30-1A FIG.101 NOTE B DETAIL V,X PAG 1-5 REV.86 APR/15/2023.SDR CNMA2023FA0000380Drive Unit · failedBOTH WX RADARS FAILED IN FLIGHT - REMOVED AND REPLACED WX RADAR ANTENNA AND R WX (?) IAW B763 AMM CHP 34-43 OPS CHECKS GOODSDR FDEA202307211272Former · damagedFOUND THE NOSE FORMER ANGLE AT OSS 441, RIGHT SIDE WING FIXED LEADING EDGE, TO BE CRACKED. 0000392280 : BILLMAN, CRAIG B - 22-JUL-2023 05:08 REPLACED FORMER AT OSS 441 AS REQUIRED PER BOEING DRAWING SR67-57-002 REV A.SDR FDEA202307211271Former · crackedFOUND THE NOSE FORMER ANGLE AT OSS 441, RIGHT SIDE WING FIXED LEADING EDGE, TO BE CRACKED. 0000392280 : BILLMAN, CRAIG B - 22-JUL-2023 05:08 REPLACED FORMER AT OSS 441 AS REQUIRED PER BOEING DRAWING SR67-57-002 REV A.SDR FDEA202307211270Former · crackedTHE NOSE FORMER ANGLE AT OSS 499 ON THE RIGHT WING FIXED LEADING EDGE IS CRACKED. REPLACED CRACKED FORMER ON RIGHT WING AT OSS 499 REF. FEDEX DWG SR67-57-002SDR FDEA202307201256Floor Panel · dentedDENTS ON UPPER LAYER OF FLOOR PANEL 221CFF, SEC. 41 MAIN DECK CARGO FLOOR PANEL 221 CFF SEC 41 MDC WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 86 APR/15/2023SDR FDEA202307201261Flap · damagedRIGHT WING INBOARD TRAILING AFT FLAP, LOWER SURFACE WITH NICK AT 19.75" FROM INBOARD EDGE AND 9.5" FROM LOWER EDGE RH WING AFT FLAP INBOARD TRAILING EDGE FLAP, WEDGE LOWER SURFACE AT POSITION IFS 122.4-124.9, SKIN WAS REPAIRED IAW SRM B767 57-53-01-2R REP SDR FDEA202307201260Floor Panel · dentedDENTS ON UPPER LAYER OF FLOOR PANEL 221DFF, SEC 41 MAIN DECK CARGO FLOOR PANEL 221DFF SEC. 41 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4B FIG. 201 SHEET 2. REV 86 APR 15/ 2023SDR FDEA202307201259Floor Panel · dentedDENTS ON UPPER LAYER OF FLOOR PANEL 222AFF, SEC 41 MAIN DECK CARGO FLOOR PANEL 222AFF SEC. 41 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4B FIF 201 SHEET 2 REV 86 APR 15/2023SDR FDEA202307201258Floor Panel · dentedDENTS ON UPPER LAYER OF FLOOR PANEL 222BFF SEC 41 MAIN DECK CARGO FLOOR PANEL 222BFF SEC 41 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4B FIG 201 SHEET 2. REV 86 APR 15/ 2023SDR FDEA202307201257Floor Panel · dentedDENTS ON UPPER LAYER OF FLOOR PANEL 222CFF, SEC. 41 MAIN CARGO COMPARTMENT FLOOR PANEL 222CFF, SEC. 41 MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR, 4.B. FIG 201 SHEET 2. REV 86 APR 15/2023SDR FDEA202307201255Bracket · crackedR/H WING I/B FIXED L/E SLAT TORQUES TUBE GUIDE BRACKET CRACKED AT THE FASTENER HOLES APPROX LES 285. REMOVED AND REPLACED TORQUE TUBE GUIDE BRACKET IAW BAC DWG 114T1240, SHEET 6, REV -.SDR FDEA202307191251Flap · dentedLH WING, OUTBOARD FLAP, LOWER SURFACE, NEAR OF OUTBOARD TRACK WITH DENT. LH WING, OUTBOARD FLAP, LOWER SURFACE, WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG.201 SHEET 3 REPAIR 1 AND SRM 51-70-10-2R REPAIR 4 FIG.201 SHEET 2 REV.86 APR 15/23SDR FDEA202307191250Floor Panel · dentedMDC FLOOR PANEL 221DFF WITH DENTS. MDC FLOOR PANEL 221 DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191249Floor Panel · dentedMDC FLOOR PANEL 222CFF WITH DENTS. MDC FLOOR PANEL 222 CFF WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191248Floor Panel · dentedMDC FLOOR PANEL 222AFF WITH DENTS. MDC FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191247Floor Panel · dentedMDC FLOOR PANEL 222BFF WITH DENTS. MDC FLOOR PANEL 222 BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191246Floor Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS. MDC FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307191245Floor Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS. MDC FLOOR PANEL 221 CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.85 DEC 15/2022SDR FDEA202307181253Floor Panel · damagedFABRICATE FLOORBOARD PN# 145T5876-99 REF SRZ-25-005 R STA. 680-834 LBL 20. FABRICATED FLOOR BOARD REF DRAWING # 145T5876, SHEET 99 AND SRZ-25-005 REV. R.SDR FDEA202307181252Floor Panel · damagedFABRICATE FLOOR PNL PN# 145T5876-38 REF SRZ-25-005 R. PRIMARY STRUCTURE AND MAJOR REPAIR. FABRICATED FLOOR PANEL REF E.A. H-5300-T0375343.SDR FDEA202307181239Rudder · damagedVERT STAB, RUDDER, L/H SIDE, TRAILING EDGE HAS EDGE DAMAGE AT APPROX RUDDER STA 305 REPAIRED RUDDER TRAILING EDGE IAW FEDEX EA# H-5540-T0375223-P1, RELEASED JUL 15, 2023, TITLED "STABILIZERS - RUDDER - LH SIDE, UPPER PANEL ASSY, RUDDER STA 320, TRAILING EDGESDR FDEA202307181238Skin · damagedL/H HOR. STAB, UPPER SKIN IS DENTED AND GOUGED AT APPROX 75" O/B OF STAB ROOT JUST AFT OF L/E PANEL 332BL REPAIRED L/H HOR STAB, UPPER SKIN DENT AND GOUGE APPROX 75" O/B OF THE STAB ROOT, JUST AFT OF L/E PANEL 332BL AS REQUIRED IAW FDX B767 SRM 51-70-10-2RSDR FDEA202307181237Angle · crackedMAIN CABIN FLOOR SUPPORT IS CRACKED AT APPROX STA 1575, LBL 68 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV CSDR FDEA202307181236Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX STA 1575, LBL 65 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV CSDR FDEA202307181235Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT APPROX STA 1575, RBL 68 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV C.SDR FDEA202307181234Angle · crackedMAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX STA 1575, RBL 65 REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW BAC DWG 146T5650, SHEET 5, REV CSDR CALA2023072102286Slide · departed*THIS IS A SUPPLEMENTAL REPORT TO THE ORIGINAL REPORT, WITH THE SAME CONTROL NUMBER, CIRCULATED ON 07/21/2023* PDA 1 THE AIRCRAFT ARRIVED AT T5 GATE M21 WITH RH OVERWING SLIDE DOOR AND SLIDE PACK MISSING. RH OVERWING SLIDE DOOR IS DIFFICULT TO CLOSE(LP 5217256
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