Boeing 767-34AF

Service difficulty reports · 6,321

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 = '76734AF'
  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.

SDR IPXA10659143Floorbeam · crackedINSPECTION TYPE:C FX STA246 MAIN DECK FLOORBEAM ATT CLIP FOUND CRACK AT RBL10". FX STA 246 MAIN DECK FLOORBEAM ATT CLIP AT RBL10" AREA REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 46.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA10659142Floorbeam · crackedINSPECTION TYPE:C, AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE FOUND CRACK AT STA1581 LBL70". AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE REPLACED AND INSTALLED AT STA1581 LBL70" IAW SRM 51-10-02 AND 51-40-02, REV 46.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA10659139Floorbeam · crackedINSP TYPE:6C, AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE FOUND CRACKED AT STA 1581, RBL70". AFT BULK CARGO COMPT MAIN DECK FLOORBEAM ATT ANGLE REPLACED AND INSTALLED AT STA 1581 RBL 70" IAW SRM 51-10-02 AND 51-40-02 REV46.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA10659115Stiffener · crackedINSPECTION TYPE:C WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA785.9 RBL10.94. WING CTR SECT FRONT SPAR AT STA785.9 RBL10.94 VERT STIFFENER REPAIRED IAW RS R57-00-36677 ORG MATL IS BAC1518-749-2024T3511 CRK LENGTH IS 3" CUT OFF LENGMar 29, 2010 · N326UP · Boeing 76734AF · Wing, Center BoxSDR IPXA10659101Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 1041 TO STN 1114, RBL 33" TO RBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659100Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 540 TO STN 654+22, LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659099Floor Panel · gougedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND DEEP GOUGE MARKS AT STN 540 TO STN 654+22, RBL 33" TO RBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659098Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 1344 TO STN 1425, RBL 55" TO RBL 77". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659097Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND SEVERAL PUNCTURES AT STN 1370 TO STN 1480, RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALL IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659091Floor Panel · puncturedINSP TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 833 TO STN 930, LBL 11" TO RBL 11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659083Floor Panel · puncturedINSPECTION TYPE:6C MCD FLOOR PANEL FOUND PUNTURED AT STN 833 TO STN 930, LBL 33" TO LBL 55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659082Floor Panel · puncturedINSPECTION TYPE:6C, MCD FLOOR PANEL FOUND PUNCTURED AT STN 932 TO STA 985, RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Mar 29, 2010 · N326UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658998Skin · dented6 SKIN DENTS AT STA 450 JUST FWD OF LWR FWD CARGO DOOR CUTOUT. DENTS ARE IN CLOSE PROX TO EACH OTHER. REPAIRED IAW EO B767-5330-36821-B.Mar 29, 2010 · N310UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10659001Floor Panel · damagedFLOOR PANEL AT POS 5/6L HAS NUMEROUS HOLES. FABRICATED NEW FLOOR PANELS IAW STANDARD REPAIR EO B767-5320-9693-G.Mar 28, 2010 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659000Floor Panel · damagedMAIN DECK FLOOR PANEL HAS HOLE. FABRICATED NEW FLOOR PANEL IAW STANDARD REPAIR EO B767-5320-9693-G.Mar 28, 2010 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658991Skin · dented6 SKIN DENTS AT STA 450 JUST FWD OF LWR FWD CARGO DOOR CUTOUT. DENTS ARE IN CLOSE PROX TO ONE ANOTHER. COMPLETED REPAIR IAW EO B767-5330-36821-B.Mar 28, 2010 · N310UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10658912Handle · out of adjustF/O'S SLIDING WINDOW R2 IS DIFFICULT TO OPEN. SEEMS TO BE BINDING WHEN OPENING OR CLOSING. ADJUSTED F/O R2 WINDOW HANDLE. PERFORMED ADJ/TEST IAW MM 56 11 02 5. OPS NORMAL AT THIS TIME.Mar 23, 2010 · N307UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA10658898Floor Panel · damagedMAIN CARGO POS 10 R FWD OB CORNER HAS .7500" DIAMETER HOLE IN UPPER SKIN 5" AFT OF THE 9/10 SPLIT LINE AND 74" RT OF CTR. REPLACED FLOOR PANEL IAW EO B767-5320-9693.Mar 20, 2010 · N303UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658846Floor Panel · damagedFLOOR PANEL AT POS 10R DAMAGED. REPAIRED REF 767, SRM 53-00-50-2R.Mar 15, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658845Floor Panel · damaged3.5 X1.5 CUTOUT IN MAIN DECK FLOOR POS 10L, REPAIRED IAW SRM 53-00-50-2R.Mar 15, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658840Floor Panel · damagedPOS 13R OB FWD FLOOR PANEL HAS A .5 DIA HOLE. REPAIRED IAW SRM 767-300F 53-00-50-2R.Mar 14, 2010 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659035Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK RT WING NR 10 SLAT INBD AREA AT OSS723.9 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201. ORG MATL IS CLAD7075T6-0.063" CRK LENGTH IS 0.14" DAMAGED CUTOUT IS 8.875" X 7.125". THISMar 10, 2010 · N326UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658863Panel · delaminatedINSPECTION TYPE:C, EMP - VERT STAB RT EXTERIOR SURFACE AREA (NEAR NR 321E UPPER) FOUND DELAMINATED, REF UPS EO B767-5530-37028-A.Mar 8, 2010 · N313UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA10658862Panel · damagedINSPECTION TYPE:C, VERTICAL STAB RT SIDE PANEL (175T2001-4) AFTER REMOVAL FOUND PANEL MID SECTION FWD EDGE 1 EA LOCATION DAMAGED. REF SRM 55-30-01-2R REPAIR 1, FIG 201, SHEET 1, REF SRM 51-70-10-2R REPAIR 4 FIG 202, SHEET 3 REV 46.Mar 8, 2010 · N313UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA10658772Seal · deterioratedFL 320 LOUD THUD FOLLOWED BY DEAFENING LOUD HOWL. INCREASING & DECREASING PSI, CHANGED ALTITUDE, NOISE DID NOT CHANGE. DIFFICULT TO COMMUNICATE WITH EACH OTHER AND AR DUE TO NOISE. NOISE STOPPED AS DESCENDING THRU FL220. CHECKED FLT COMPT FOR AIR LEAK, FOUNDMar 6, 2010 · N327UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA10658726Seal · deformedATB - STATUS MESSAGE LANDING GEAR MONITOR APPEARED DURING CLIMB-OUT. RETURNED TO MIA. C/W FIM 32-61-00 FIG 104. FOUND PSEU FAULT CODE 234 AND 235. FOUND LONGITUDINAL SEALS ON BOTH DOORS DEFORMED AND INTERFERING WITH DOOR CLOSING. ACCOMPLISHED BLOCK 1 OF FMar 5, 2010 · N311UP · Boeing 76734AF · Landing Gear DoorsSDR IPXA10658705Unknown · odorINSPECTION TYPE:ETOP WHEN LANDING GEAR EXTENDED APPROACH A STRONG ODOR OF BURNING RUBBER ENTERED THE COCKPIT. ODOR DISSIPATED BY LANDING. PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST ON LEFT AND RIGHT PACK. RAN BOTH PACKS AT FULL HOT NO DISCREPANCIES NOMar 3, 2010 · N324UP · Boeing 76734AF · Air Distribution SystemSDR IPXA10658814Stiffener · crackedINSPECTION TYPE:C, RT WING - L/E OFSS821 FRONT SPAR STIFFENER FOUND CRACKED. RT WING L/E OFSS821 FRONT SPAR STIFFENER REPLACED AND INSTALLED IAW RS R57-00-36628. ORG MAT'L IS BAC1503-100631-7075T6511 EXTRUSION CRACK LENGTH IS .3750". THIS REPAIR IS CLASSIFMar 1, 2010 · N313UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA10658748Fairing · delaminatedINSP TYPE:C- LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 46.Mar 1, 2010 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658747Fairing · delaminatedINSP TYPE:C - RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 46.Mar 1, 2010 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658734Fairing · delaminatedINSPECTION TYPE:C LT WING OTBD T/E FLAP INBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 46.Mar 1, 2010 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658878Support · crackedINSP TYPE:C, LT WING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACKED, CRACK .2500" IN LENGTH. LT WING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP, REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.Feb 26, 2010 · N313UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA10658764Floor Panel · puncturedINSP TYPE:C- MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA1480 TO 1598 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658762Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 412 TO 540 L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658761Floor Panel · puncturedINSPECTION TYPE:C- MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 833 TO 930 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658760Floor Panel · puncturedINSPECTION TYPE:C - MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 731 TO 833 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658759Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 879 TO 933 L77 TO L88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658758Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 1207 TO 1344 L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658757Floor Panel · puncturedINSPECTION TYPE:C- MCD FLOOR PANEL, FOUND SEVERAL PUNCTURED HOLES AT STA 654+22 TO 690 R11 TO R33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658756Floor Panel · puncturedINSP TYPE:C - MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 1197+22 TO 1207 R11 TO R33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658755Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 1344 TO 1480 L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658754Floor Panel · puncturedINSPECTION TYPE:C- MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA 654+22 TO 690 R33 TO R55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658753Floor Panel · puncturedINSPECTION TYPE:C -MCD FLOOR PANEL FOUND SEVERAL PUCNTURED HOLES AT STA 690 TO 764 L77 TO L88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658752Floor Panel · puncturedINSPECTION TYPE:C MCD FLOOR PANEL FOUND SEVERAL PUNCTURED HOLES AT STA731-833 R33 TO R55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658751Floor Panel · puncturedINSPECTION TYPE:C- MCD FLOOR PANEL, FOUND SEVERAL PUNCTURED HOLES AT STA 580 TO 654+22 R77 TO R88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658750Floor Panel · puncturedINSP TYPE:C- MCD FLOOR PANEL, FOUND SEVERAL PUNCTURED HOLES AT STA 654+22 TO 696 R77 TO R88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658749Floor Panel · puncturedINSP TYPE:C -MCD FLOOR PANEL, FOUND SEVERAL PUNCTURED HOLES AT STA 412 TO 540 L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658746Structure · crackedINSPECTION TYPE:C E AND E COMPT STA 246 RBL 10 INCH CLIP FOUND CRACKED CRACK LENGTH 1.25 INCH. E AND E COMPT STA 246 RBL 10 CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 46.Feb 26, 2010 · N313UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658716Skin · crackedINSPECTION TYPE:C LT WING NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR 3 SLAT INBD AREA AT OSS723.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV46 ORG MAT'L IS CLAD7075T6-0.063" CRACK LENGTH IS 0.12 INCH DAMAGED CUTOUT IS 8 7/8 INFeb 26, 2010 · N313UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658715Skin · crackedINSPECTION TYPE:C LT WING NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING NR 3 SLAT OTBD AREA AT OSS792.5 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV46 ORG MAT'L IS CLAD7075T6-0.063" CRACK LENGTH IS 0.11 INCH DAMAGED CUTOUT IS 8 13/16 Feb 26, 2010 · N313UP · Boeing 76734AF · Leading Edge Devices
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