Boeing 767-3S2F
Service difficulty reports · 2,378
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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 = '7673S2F' 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 = '7673S2F' 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 FDEA202407151004Floor Panel · dentedZONE 200, UPPER HALF OF FUSELAGE, MAIN DECK CARGO COMPARTMENT, MAIN DECK FLOOR PANEL 221CFF WITH DENTS. MDC, FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV: 88 DEC 15/2023SDR FDEA202407080971Skin · delaminatedLEFT WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION AT 60" FROM OUTBOARD FITTING NO 1. LEFT WING OUTBOARD FLAP LEADING EDGE AT 60" FROM OUTBOARD FITTING NO 1 WAS REPAIRED IAW B767 SRM 57-53-01-2R TABLE I AND SRM 51-70-03-0G PAR 5.A FIG 9 REV 88 DEC 15SDR FDEA202407080970Floor Panel · crackedMAIN DECK CARGO COMPARTMENT, SEC 46, FLOOR PANEL 251FFF WITH HOLE. MAIN DECK CARGO COMPARTMENT, SEC 46 FLOOR PANEL 251FFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202407080969Floor Panel · crackedMAIN DECK CARGO COMPARTMENT, SEC 46, FLOOR PANEL 251EFF WITH PUNCTURE. MDC, SEC 46, FLOOR PANEL 251EFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202407080968Floor Panel · crackedMAIN DECK CARGO COMPARTMENT, SEC 43, FLOOR PANEL 241DFF WITH PUNCTURE. MDC, SEC 43, FLOOR PANEL 241DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202407080966Floor Panel · crackedMAIN DECK CARGO COMPARTMENT, SEC 43, FLOOR PANEL 241AFF BROKEN. MAIN DECK CARGO COMPARTMENT SEC 43 FLOOR PANEL 241AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202407080965Wedge · chafedLH WING #5 SLAT TRAILING EDGE WEDGE HAS A (2.0" X 0.5") GOUGE AT WS OSS 441 ON THE LOWER SURFACE . REPAIRED LH WING L/E # 5 SLAT TRAINLING EDGE WEDGE AT WS OSS 441 IN REF TO 767 SRM 57- 43-02-2R, PG 1-2 DETAIL I & III, FIG.201 SHEETS 1 & 2, AND 767 SRM 51-SDR FDEA202407060952Skin · gougedFOUND RAMP AIRCRAFT STRIKE AFT OF AFT LOWER CARGO DOOR. ACCOMPLISHED A DVI OF THE DAMAGED AREA AND 10 INCHES AROUND TO ENSURE THAT THE DENT IS SMOOTH AND FREE OF CREASES OR CRACKS, NO PULLED LOOSE OR MISSING FASTENERS. SCRATCHS BLENDED PER SRM . DVI WSDR FDEA202407050947Skin · delaminatedRH OUTBOARD FLAP LEADING EDGE LOWER SURFACE AT OTEF STA 47 APPROX SKIN WITH DELAMINATION. RH OUTBOARD FLAP LEADING EDGE LOWER SURFACE AT OTEF STA 47 APPROX SKIN WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 TABLE I PAG 1-5 AND SRM 51-70-03-0G PAR 5.A FIG 5 SDR FDEA202407040935Fairing · damagedRH FAIRING PANEL 196GR PN 113T1740-276 (ALONG WITH ATTACHING PANELS AND DOOR ON FAIRING) DAMAGED FROM FLAP RE-TRACK. TO INCLUDED PN 113T1740-178 FAIRING PANEL, WITH PN 113T2022-32 (WITH SUPPORT ASSY PN 113T2016-2 ATTACHED) & PN 113T2022-36 (WITH SUPPORT ASDR FDEA202407040934Escape Rope · stuckESCAPE ROPE CAUGHT IN DOOR TRACK. ESCAPE ROPE RETAINER DAMAGED. FREED EMERGENCY ESCAPE ROPE AND INSPECTED LOWER PORTION FOR DAMAGE REF AMM 25-61-02-2. NO DEFECTS NOTED. REPLACED ESCAPE ROPE RETAINER.SDR FDEA202407010907Skin · wornRH WING, SLAT #8, TRAILING EDGE, NEAR INNER AUXILIARY TRACK, LOWER SKIN WITH WEAR. RH WING, SLAT #8, TRAILING EDGE, NEAR INNER AUXILIARY TRACK, LOWER SKIN WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 PAG 1-2 AND SRM 51-70-10-2R FIG 201 (SHEET 1) PAG 150,151,1SDR FDEA202407010906Angle · damagedLOWER FORWARD CARGO DOOR CUT OUT, TOP SEAL DEPRESSOR ABOUT STA. 520 TO 565, DAMAGED 453T1654-17 REMOVED AND REINSTALLED NEW PART IAW B767 SRM 51-40-02-0G. 453T1654-18 REPAIRED IAW EA# H-5320-T0379743 FUSELAGE - AUXILIARY STRUCTURE - FWD LOWER CARGO CUTSDR FDEA202407010902Floorboard · damagedMAIN CARGO DECK FLOORBOARD AT STA.936 RBL. 33 PNL# 232QFF (MPN: 145T5876-94) HAS A (1 X 1 IN.) PUNCTURED HOLE IN REF. TO (SEQ# 711). SIGN OFF: REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 960 RBL. 33 PNL# 232QFF (MPN: 145T5876-94) IN REF. TO 767 SRM 53-00-5SDR FDEA202406300893Skin · gougedSKIN GOUGE AT FS 287 9.75 JUST INBOARD OF S-38L SHGN 26JUN24 06:50 IND SRM: 53-00-01-1A DAMAGE MEASURES 0.1 X 0.4 AND 0.075 DEEP. DAMAGE FOUND TO BE OUT OF LIMITS REF ABOVE SRM. INFO 26JUN24 21:35 ** ATTACHED TO WORK ORDER 00088805 ** REPAIRED GSDR FDEA202406280876Angle · damagedNEED TO CREATE ANGLE B67-57-003-01 TO REPLACE 114T2171-4 AT FLE LW OSS 441.569. FABRICATED AND REPLACED FORMER 114T2170-5 & ANGLE 114T2171-4 WITH B67-57-002-01 & B67- 57-003-01SDR FDEA202406270872Floor Panel · crackedPUNCTURE ON FLOOR PANEL 231VFF. SECTION 43 OF MDC. MDC, FLOOR PANEL 231VFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202406260870Skin · crackedLOWER FUSELAGE SKIN CRACKED APPROX 1" LOCATED 10" FWD OF BS 1654.5 AND OTBD OF S36L. COMPLIED WITH E.A. # H-5310-T0379685 PT 11808. TITLE - FUSELAGE - MAINFRAME - REPAIRS DUE TO CONTAINER STRIKE, FUSELAGE SKIN, ST 1629-1702, S-36L TO S-36R AND STA 1678 FRASDR FDEA202406260869Frame · damagedFOUND DAMAGE TO FRAME BS 1678 OTBD OF S36R. COMPLIED WITH E.A. # H-5310-T0379685 PT 2. TITLE - FUSELAGE - MAINFRAME - REPAIRS DUE TO CONTAINER STRIKE, FUSELAGE SKIN, ST 1629-1702, S-36L TO S-36R AND STA 1678 FRAME.SDR FDEA202406240858Skin · dentedLEFT WING, SLAT NO.6 INTERNAL SURFACE WITH DENT AT 6" FROM UPPER EDGE AND 14.5" FROM OUTBOARD EDGE. LH WING, SLAT NO.6 INTERNAL SURFACE WITH DENT AT 6" FROM UPPER EDGE AND 14.5" FROM OUTBOARD EDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 PAG 1-2 AND SRMSDR FDEA202406240857Skin · dentedLEFT WING, SLAT NO.6 INTERNAL SURFACE WITH DENT AT 6" FROM UPPER EDGE AND 14.5" FROM OUTBOARD EDGE. LH WING, SLAT NO.6 INTERNAL SURFACE WITH DENT AT 6" FROM UPPER EDGE AND 14.5" FROM OUTBOARD EDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 PAG 1-2 AND SRMSDR FDEA202406240856Skin · dentedLEFT WING, SLAT NR 6 INTERNAL SURFACE WITH DENT AT 7.5" FROM UPPER EDGE AND 28" FROM OUTBOARD EDGE. LH WING, SLAT NR 6 INTERNAL SURFACE WITH DENT AT 7.5" FROM UPPER EDGE AND 28" FROM OUTBOARD EDGE WAS REPAIRED IAW SRM 57-43-02-2R REP 1 PAG 1-2 AND SRM 51-7SDR FDEA202406230854Skin · damagedLOWER HALF OF FUSELAGE, BTW STA 1417 AND STA 1439, BTW STRG 33L AND 38L, WITH SCRATCH. LOWER FUSELAGE SKIN BTWN STA 1417/1439 AND STGR 33L/37R WAS REPAIRED IAW E.A. #:H- 5330-T0379538 (P1).SDR FDEA202406210833Skin · wornRH WING, INBOARD AILERON, LEADING EDGE, RH SIDE, WITH WEAR. RH WING, INBOARD AILERON, LEADING EDGE, ACCESS PANEL 656AB WAS REPAIRED IAW B767 SRM 57-60-01-2R REP 1 TABLE VII AND SRM 51-70-17-0G PAR 4.G FIG 15 REV 88 DEC 15/2023SDR FDEA202406210832Skin · damagedLEFT WING, INBOARD AILERON LEADING EDGE INBOARD LOWER SECTION WITH WEAR. LEFT WING, INBOARD AILERON LEADING EDGE, ACCESS PANEL 556AB WAS REPAIRED IAW B767 SRM 57-60-01-2R TABLE VII AND SRM 51-70-17-0G PAR 4.G FIG 15 REV 88 DEC 15/2023SDR FDEA202406210831Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 231AFF, SKIN WITH DENTS. MDC, FLOOR PANEL 231AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202406210830Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 221CFF, SKIN WITH SEVERAL DENTS. MDC, FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202406170810Bulb · failedON APPROACH, AT GEAR EXTENSION, THE RT MLG DID NOT INDICATE SAFE (NO GREEN LIGHTS). THERE WAS NO EICAS OR GEAR DISAGREE LIGHT. BULBS TESTED GOOD. AFTER RETRACTING MLG ON GO AROUND & EXTENDING IT FOR SUBSEQUENT APPROACH, MLG EXTENDED NORMALLY. IAW CREW REPORT,SDR FDEA202406150808Pivot · damagedNR 29 RH (INBD) HORIZONTAL STABILIZER PIVOT PIN FITTING ASSY REQUIRES REMOVAL TO F.O.M. TO PERFORM EA H-5550-T0379419 P1. DURING THE ACCOMPLISHMENT OF THE WIC 5549400-00-01 MAINTENANCE CHECK AT HMV-1 THE BEARING RETAINER LOCKWIRE ON THE HORIZONTAL STABILSDR FDEA202406130804Wedge · wornRH WING, SLAT NO. 8, FROM OSS 441 TO 514, WEAR ON WEDGE (3 EAS) . RH WING, SLAT NO. 8, FROM OSS 441 TO 514 WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 PAG 1-2 AND SRM 51-70-10-2R REP 4 FIG 202 (SHEET 8) REV 88 DEC 15/2023SDR FDEA202406130803Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SEC 41 FLOOR PANEL 221DFF WITH SEVERAL DENTS. MDC, SECTION 41 FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202406110793Skin · dentedDENT WITH GOUGE ON FUSELAGE SKIN AT STA 390 BTW STR 4/5 RH. FUSELAGE SKIN AT STA 390 BTW STR 4/5 RH WAS REPAIRED IAW SRM 53-00-01-2R REPAIR 14 REV 88 DEC 15, 2023.SDR FDEA202406100788Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 241KFF SECTION 45 OF MDC. MDC, SECTION 45, FLOOR PANEL 241KFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202406100787Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR ACCESS PANEL 221DFF. SEC 41 OF MDC. MDC, SEC 41, FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023.SDR FDEA202406060775Floorbeam · cracked[MEC, LT TUNNEL, STA 246 (LBL 26.06) FLOOR BEAM, FWD SIDE, "L" BRACKET CRACKED. (PN 141T5814-136) INSTALLED NEW FABRICARTED SUPPORT (PN 141T5814-136) USING DRW 141T5814, NA: 141T5104 ALONG WITH 767 SRM 51-40-02-0G. MINOR REPAIRSDR FDEA202406050772Tee Angle · crackedMEC, LT TUNNEL, STA 246, APROX BL 20 LT, "T" BRACKET CRACKED. INSTALLED NEW FABERCATED T-CLIP 141T5603-6 IAW DRAWING #141T5601 & 141T5600, SRM 51-40-02-0G.SDR FDEA202406050771Tee Angle · damagedT CLIP CRACKED AT APPROX. STA 266 BL 0. INSTALLED NEW FABERCATED T-CLIP 141T5603-7 IAW DRAWING #141T5601, SRM 51-40-02-0G.SDR FDEA202405300753Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 242TFA, SKIN WITH DENT. MDC, FLOOR PANEL 242TFA WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405300751Skin · dentedSLAT #2, UPPER WEDGE, EXTERNAL SURFACE WITH 4 DENTS LOCATED AT 38.5" OF INBOARD FRAME OF SLAT AND 5" OF TE APPROX. SLAT #2, UPPER WEDGE, EXTERNAL SURFACE WAS REPAIRED IAW B767 SRM 57-43-02-2R PAG 1-2 NOTE B AND SRM 51-70-10-2R REP 4 FIG 201 (SHEET 1) PAG 1SDR FDEA202405300746Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 222CFF, SKIN WITH DENTS. MDC, FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405300745Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 221CFF, SKIN WITH DENTS. MDC, FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405300744Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 222BFF, SKIN WITH DENTS. MDC, FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405290743Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 222AFF, SKIN WITH DENTS. MDC, FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405290742Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 221DFF, SKIN WITH DENTS. MDC, FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405240725Former · crackedWING FIXED LEADING EDGE NOSE FORMER ANGLE CRACKED AT OSS 499.6 ON THE LEFT WING. REMOVED THE DAMAGED NOSE FORMER ANGLE FROM THE LEFT WING FIXED LEADING EDGE AT OSS 499.6. INSTALLED A NEW NOSE FORMER ANGLE. FEDEX DRAWING SR67-57-002 REV. A.SDR FDEA202405240724Former · crackedFIXED LEADING EDGE NOSE FORMER ANGLE CRACKED AT OSS 441 ON THE LEFT WING. REMOVED THE DAMAGED NOSE FORMER ANGLE FROM THE LEFT WING FIXED LEADING EDGE. INSTALLED A NEW FORMER ANGLE, B67-57-002-01. FEDEX DRAWING SR67-57-002 REV. A.SDR FDEA202405230723Skin · delaminatedLEFT WING, INBOARD MAIN FLAP, LEADING EDGE WITH DELAMINATION AT 31" FROM OUTBOARD EDGE. LEFT WING, INBOARD MAIN FLAP, LEADING EDGE AT 31" FROM OUTBOARD EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R TABLE I PAG 1,2,5 AND SRM 51-70-17-0G PAR 4.A FIG 10 PAG 24-2SDR FDEA202405230722Skin · dentedRH WING, INBOARD AFT FLAP, LOWER SURFACE, DENT NEAR INBOARD EXTERNAL HINGE. RH WING, INBOARD AFT FLAP, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 (SHEET 4) NOTE A AND SRM 51-70-03-0G PAR 5.L FIG 16 REV 88 DEC 15/2023SDR FDEA202405220718Wedge · dentedLH WING #3 SLAT TRALING EDGE WEDGE TOP SURFACE HAS A (3.5 INCH) DENT AT WING STATION 750. REPAIRED LH WING L/E # 3 SLAT TRAINLING EDGE WEDGE AT WS OSS 750 IN REF TO 767 SRM 57- 43-02-2R, PG 1-2 DETAIL I & III, FIG.201 SHEETS 1 & 2, AND 767 SRM 51-70-10-2R. SDR FDEA202405220717Skin · delaminatedLH WING, OUTBD FLAP, APPROX WBL 355.0 TO 400 LE FLAP WITH TWO DELAMINATIONS LH WING, OUTBD FLAP, APPROX WBL 355.0 TO 400 LE FLAP WAS REPAIRED IAW B767 SRM 57-53- 01-2R REP 1 TABLE I FIG 201 AND SRM 51-70-17-0G PAR 4.A FIG 10 REV 88 DEC 15/2023
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