Boeing 767-3S2F
Service difficulty reports · 2,378
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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 = '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 FDEA202405220716Wedge · wornLH WING, OUTBOARD SLAT 5, TRAILING EDGE WEDGE, LOWER SKIN AT OSS 514.75, PREVIOUS REPAIR WITH WEAR LH WING, OUTBOARD SLAT 5 TRAILING EDGE WEDGE, LOWER SKIN AT OSS 514.75 WAS REPAIRED IAW B767 SRM 57-43-02-2R FIG 201 SHEET 1-2 PAGE 1-2, AND SRM 51-70-10-2RSDR FDEA202405210713Skin · delaminatedRH WING,INBOARD FLAP, MAIN FLAP WITH DELAMINATION AT WBL 289.4 RH WING, INBOARD FLAP, MAIN FLAP AT WBL 289.4 WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG 201 TABLE II AND SRM 51-70-06-0G PAR 5G FIG 3 REV 88 DEC 15/2023SDR FDEA202405210712Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222CFF SECTION 41 AT MDC. MDC, SECTION 41, FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405210711Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222BFF SECTION 41 AT MDC. MDC, SECTION 41, FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405180688Skin · delaminatedRH WING OUTBOARD FLAP LEADING EDGE WITH TWO DELAMINATIONS BETWEEN WS 720.2 AND WS 616.2 RH WING OUTBOARD FLAP LEADING EDGE BETWEEN WS 720.2 AND WS 616.2 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 REV 88 DESDR FDEA202405180687Support Angle · crackedMEC, LT TUNNEL, AFT SIDE OF STA 246 BEAM HAS 1 EACH CRACKED "L" BRACKET. (PN: 141T5146- 16) REMOVED AND REPLACED SUPPORT ANGLE 147T5146-16 AT STA 246 PER DWG 141T5146 AND SRM 51-40-02-0G-0 "MINOR REPAIR"SDR FDEA202405180684Stiffener · crackedMEC, LT TUNNEL, FWD SIDE OF STA 246 BEAM HAS 1 EACH CRACKED "L" BRACKET (PN: 141T5814- 136) REMOVED AND INSTALLED NEW STIFFENER PN: 141T5814-136. REF SRM 51-40-02-0G AND BOEING DWG 141T5104, ALODINE AND PRIMED AS REQUIRED. REF SRM 51-20-01-0G. (MINOR REPAISDR FDEA202405150673Skin · damagedE&E BAY DOOR AND SURROUNDING STRUCTURE DAMAGED. E&E BAY DOOR REPLACE AND SURROUNDING STUCTURES REPAIRED UNDER FED-RE-2403203 REM 97-2.SDR FDEA202405150672Skin · damagedLOWER FUSELAGE SKIN DAMAGED AT APPROX. STATION 157. FUSELAGE SKIN REPAIRED IAW FED-RE-2403203SDR FDEA202405140668Support Angle · gougedDURING INSPECTION FOUND DAMAGE TO FWD. LOWER CARGO DOOR CEILING SUPPORT ANGLE COVER. MARKED WITH TAPE. REPAIRED DAMAGE TO FWD. LOWER CARGO DOOR SEAL REF. EA H-5320-T0379144. FOR REPAIR WORK...SEQ. 161. SEE JPF FOR OTHER WORK PERFORMED. (WRI 53200994)SDR FDEA202405130661Skin · dentedRH WING, INBOARD AFT FLAP, TRAILING EDGE WEDGE, LOWER SURFACE, BETWEEN IFS 160.5 AND IFS 169 APPROX SKIN WITH DENTS. RH WING, INBOARD AFT FLAP, TRAILING EDGE WEDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 AND SRM 51-70-10-2R REP 2 FIG 203SDR FDEA202405130660Skin · gougedRH WING, INBOARD AFT FLAP, TRAILING EDGE WEDGE, LOWER SURFACE, BETWEEN IFS 220.5 AND IFS 206 APPROX SKIN WITH GOUGES. RH WING, INBOARD AFT FLAP, TRAILING EDGE WEDGE, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 (SHEET 6) AND SRM 51-70-06-0G SDR FDEA202405130657Actuator · failedNLG FAILED TO EXTEND, UPON LANDING ACFT REMAINED ON CENTERLINE OF RUNWAY SURFACE. REF E.A H-5310-T0380090 P1 WORKED IN CONJUSCTION WITH 53-10/0463 COMPLETED INSTALLATION OF NOSE LANDING GEAR RETRACT ACUATOR REF B767 AMM 32-34-01-4 OPS AND LEAK CHECK GOOD.SDR FDEA202405130656Altimeter · faultedIN CRUISE AT ALTITUDE FL340, WITH RIGHT AUTOPILOT ENGAGED. FO ALTIMETER DROPPED ABOUT 330 FT. WITH EICAS ALT DISAGREE, AUTOPILOT ATTEMPTED TO CLIMB BACK TO RECAPTURE FL340 WITH CAPT ALTIMETER SUBSEQUENTLY CLIMBING TO FL342. DISENGAGED AUTOPILOT AND RETURNSDR FDEA202405120647Nut · looseHORIZONTAL STABILIZER PIVOT FITTINGS AFT RH SIDE . LOCKING SAFETY WIRE LOOSE. LOCKWIRE ON THE HORIZONTAL STABILIZER PIVOT FITTINGS AFT RH SIDE WAS REPLACED I.A.W. AMM 55-17-51-4 REV. 141 DEC 22 2023. THIS TASK CARD WAS PERFORMED DUE TO THE LOCKWIRE AT RH PSDR FDEA202405120645Skin · wornRH WING, OUTBOARD SLAT 8, TRAILING EDGE WEDGE, LOWER SURFACE AT OSS 433.71 APPROX, PREVIOUS REWORK DETERIORATED. RH WING OUTBOARD SLAT #8 TRAILING EDGE WEDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R REPAIR 1 NOTE B AND SRM 51-70-10-2R REPAIR 4 REV 88 DEC 15/SDR FDEA202405120644Skin · crackedRH WING SPOILER #7, LOWER SURFACE, AT WBL 167.54 APPROX, SKIN WITH PUNCTURE. RH WING SPOILER #7, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-70-01-2R REP 1 PAG 1-4 AND SRM 51-70-17-0G PAR C FIG 11 REV 88 DEC 15/2023SDR FDEA202405110643Skin · dentedRH WING INBOARD AILERON LWR SKIN TO 21 IN OF TE WITH TWO DENTS. RH WING INBOARD AILERON LWR SKIN WAS REPAIRED IAW B767 SRM 57-60-01-2R REPAIR 1 TABLE III (SHEET 6) AND SRM 51-70-03-0G PAR 5.L REV 88 DEC 15/2023SDR FDEA202405100642Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 222CFF WITH SEVERAL DENTS. MDC, SECTION 41, FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405100641Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 222AFF WITH SEVERAL DENTS. MDC, SECTION 41, FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405100640Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 222BFF WITH SEVERAL DENTS. MDC, SECTION 41, FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405100639Bracket · bentL FWD ENTRY DOOR EICAS MESSAGE WITH DOOR CLOSED AND SECURE. WOULD GO OUT WHEN CLOSING THE DOOR THEN APPEAR AGAIN. CREW ENTRY DOOR INDICATION SYSTEM - INOP. VERIFY THAT CREW ENTRY DOOR IS CLOSED, LATCHED, AND LOCKED BEFORE EACH DEPARTURE. USE HAND SIGNSDR FDEA202405080614Tee Fitting · crackedCABIN FLOOR BOARD SUPPORT LOWER SUPPORT "T" SEVERED, STA 246-20, 6" RIGHT OF CENTER. MARKED WITH DOT. REPLACED "T" FITTING FABRICATED AND PROCESSED CABIN FLOORBOARD CLIP (141T5603-7 AT RBL 5.805, STA 272.70, WL 199.60 REF B767 DWG 141T5603) NSTALLED CLIP (SDR FDEA202405060603Floorboard · damagedMAIN DECK FLOORBOARD MPN: 145T55876-114( PNL 252DFF) AT RBL 77.50 STA.1000 PUNCHURED DAMAGE. REPAIRED MAIN DECK FLOORBOARD MPN: 145T5876-114 (PNL:252DFF) AT STA. 1000 RBL 77.50 IN REF. TO 767 SRM 53-00-50 FIG 201. SHEET 6. THIS IS MAJOR REPAIR.SDR FDEA202405030568Floor Panel · damagedFLOOR PANEL DAMAGED STA.1197 13, BL-O HAS A 3.5 X 4.5 DENT IN UPPER SKIN NEAR EDGE OF PANEL. FABRICATED AND REPLACED FLOOR PANEL. FEDEX DRAWING SRZ-25-005 REV.R. , FLOOR PANEL INSTALLATION B767 AMM 53-01-06-4. THIS IS A MAJOR REPAIR.SDR FDEA202405030567Skin · dentedREWORK NR N00056 LH WING OUTBOARD FLAP LOWER SURFACE WITH DENT AT 10" FROM LOWER EDGE AND 61" FROM INBOARD FAIRING FLAP REWORK WAS PERFORMED NR N00056 ON LH WING OUTBOARD FLAP LOWER SURFACE AT 10" FROM LOWER EDGE AND 61" FROM INBOARD FAIRING FLAP IAW B767 SDR FDEA202405020553Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 221CFF WITH SEVERAL DENTS. MDC, SECTION 41, FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202405020552Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 222BFF WITH SEVERAL DENTS. MDC, SECTION 41, FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202404300524Engine · failedCLIMBING THRU FL330, LEFT ENGINE OIL PRESSURE DROPPED TO 1 PSI. EICAS RED BOX, L ENG OIL PRESS, AND A BUMP FELT. RAN QRH, EVENTUALLY SHUT DOWN ENGINE, DECLARED EMERGENCY, RETURNED TO INDY. OIL TEMP DROPPED FROM ~115 TO 85. EMERGENCY DECLARED. PER THE DFSDR FDEA202404270517Warning Message · false activationREJECTED TAKEOFF AT ~35KTS. FOR CONFIG WARNING WITH SPOILERS EICAS. TO CONFIG TESTED NORMALLY PER BEFORE TAKEOFF CHECKLIST. TOGW 282.9. RETURNED TO RAMP. NO FURTHER DEFECTS NOTED. CAN AMM: 05-51-14-2 AMM: 32-41-08-216-001-003 PER AMM 32-41-08-216-001-00SDR FDEA202404260297Switch · failedAIRPLANE HAD A STRONG ACRID SMOKE SMELL WHEN RUNWAY TURNOFF LIGHT WERE TURNED ON. FOUND RIGHT RUNWAY TURNOFF SWITCH BAD. WHEN SWITCH ACTIVATED SMOKE EMITS FROM RT RUNWAY TURNOFF SWITCH. REMOVED AND REPLACED OVERHEAD PANEL P5 PER SMP, OPS CHECK LIGHT FUNSDR FDEA202404240294Washer · missingMDIS 145 32-41 5927 24APR24 13:26 MTY FACT ON WALKAROUND RH NOSE TIRE FOUND AXLE NUT NEAR TO FLUSH WITH THE END OF THE AXLE. MXALERT 20-0126. AFTER THE REMOVAL OF THE RH WHEEL TANG WASHER IS MISSING. PART 24APR24 13:26 MTY IDENTIFIED PARTSSDR FDEA202404240286Nut · looseSECTION 48, LH HORIZONTAL PIVOT FITTING, INBOARD FACE, LOCKWIRE BROKEN. SECTION 48, LH HORIZONTAL PIVOT FITTING, INBOARD FACE NUT OF BEARING WAS TIGHTENED AND APPLIED TORQUE, AND INSTALLED LOCKWIRE IAW AMM 55-17-51-4 REV. 141. THE STABILIZER WAS OPERATED SSDR FDEA202404240285Washer · missingON WALKAROUND RH NOSE TIRE FOUND AXLE NUT NEAR TO FLUSH WITH THE END OF THE AXLE. MXALERT 20-0126. AFTER THE REMOVAL OF THE RH WHEEL TANG WASHER IS MISSING. TANG WASHER INSTALLED ON RH NLG WHEEL IAW AMM.A/C OK FOR SVC.SDR FDEA202404240283Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 222BFF WITH SEVERAL DENTS. FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202404240282Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 222CFF WITH SEVERAL DENTS. FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202404240281Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 222AFF WITH SEVERAL DENTS. FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202404240280Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 221CFF WITH SEVERAL DENTS. FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202404240279Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, SECTION 41, FLOOR PANEL 221DFF WITH SEVERAL DENTS. FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202404240276Skin · delaminatedL/H WING INBD FLAP LEADING EDGE OTBD POSITION CAP PANEL #555DB IS DELAMINATED, MPN 113T2201-413G. REPAIRED, INSTALLED, AND SEALED L/H WING INBD FLAP LEADING EDGE OTBD POSITION CAP PANEL #555DB IS DELAMINATED, MPN 113T2201-413G. IAW E.A. # H-5750-T0378910 ASDR FDEA202404230273Skin · crackedTHE R/H WING FIXED LEADING EDGE IS CRACKED O/B OF THE #2 ENG. PYLON. REPAIRED THE R/H WING FIXED LEADING EDGE REF. B767 SRM 57-41-01SDR FDEA202404210485Skin · delaminatedL/H WING INBOARD FLAP ASSY - THE FORE FLAP LEADING EDGE OUTBOARD POSITION CAP PANEL # 555DB IS DELAMINATED, MPN 113T2201-413G. REPAIRED L/H WING INBOARD FLAP ASSY, FORE FLAP LEADING EDGE OUTBOARD POSITION CAP PANEL # 555DB, MPN 113T2201-413G. IAW E.A. # HSDR FDEA202404180471Tire · leakingNLG TIRE RH FOUND WITH RETAINING SEAL LOCK MISSING (EXTERNAL) AND GREASE SPREAD AROUND OF WHEEL. REPLACED NLG WHEEL RH IAW AMM. A/C GOOD FOR SERVICE.SDR FDEA202404180467Valve · failedWHILE WE WERE AWAITING TAKEOFF CLEARANCE WITH THE PARKING BRAKE SET, RECEIVED A MASTER CAUTION WITH A R HYD QTY EICAS MESSAGE FOLLOWED BY A R HYD PRIM PUMP EICAS MESSAGE. ACTIVATED THE STATUS PAGE AND WITNESSED THE RIGHT HYDRAULIC RESERVOIR QUANTITY DROP SDR FDEA202404130462Skin · dentedDENT ON LOWER SKIN OF INBOARD TRAILING EDGE MAIN FLAP AT LH WING. LH WING INB. T/E MAIN FLAP LOWER SKIN WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R REPAIR 1 FIG. 201 SHEET 2 NOTE A AND B767 SRM 51-70-03-0G PARAGRAPH 5.L. FIG. 16 REV. 88.SDR FDEA202404130461Skin · dentedDENT ON LOWER SKIN OF INBOARD TRAILING EDGE AFT FLAP AT LH WING. LH WING, LOWER SKIN OF INBOARD TRAILING EDGE AFT FLAP WAS REPAIRED I.A.W. B767 SRM 57- 53-01-2R REP. 1 AND SRM 51-70-03-0G PAR. 5.L. FIG. 16 PAG. 27-52 REV. 88.SDR FDEA202404130460Skin · dentedSEVERAL DENTS, LOWER SURFACE, INBOARD TRAILING EDGE FLAP, RH WING. RH WING INB. T/E AFT FLAP LOWER SURFACE WAS EVALUATED AND FOUND 3 DENTS WITHIN LIMITS I.A.W. B767 SRM 57-53-01-1A FIG. 101 SHEET 4 NOTE C DET. IV. ONE DENT WAS FOUND OUT OF LIMITS AND WAS RSDR FDEA202404120459Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222CFF . FLOOR PANEL 222CFF WAS REPAIRED IAW SRM 53-00-50-2R PARAG 4B FIG 201 SHEET 2. REV 88.SDR FDEA202404120458Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222BFF ON MDC. FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PARAG 4B FIG 201 SHEET 2. REV 88.SDR FDEA202404110455Warning Message · illuminatedAFTER TOUCHDOWN GOT A R HYD PRIM PUMP EICAS, RAN QRH, CONTINUED TAXI, DURING TAXI GOT A R HYD SYS PRESS EICAS, RAN QRH LOST SOME BRAKING, SO ELECTED TO GET TOW IN GATE. SHGN 10APR24 17:37 MEM AMM: 29_11_00_2_0 VERVIFIED AT RIGHT SYSTEM HYD RESERVOI
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