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"

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SDR FDEA202010082432Seal · crackedRIGHT WING LEADING EDGE NR 8 SLAT LES 505, INTERNAL LEADING EDGE DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER AT RT WING LEADING EDGE LES 505, IAW B767 SRM 51-40-02 AND BAC DWG 114T2800 REV C.Oct 8, 2020 · N144FE · Boeing 7673S2F · Wing Miscellaneous StructureSDR FDEA202010082431Former · crackedRIGHT WING L/E LES 560 WEB SUPPORT BRACKET CRACKED. REMOVED AND REPLACED FORMER ASSEMBLY P/N'S 114T2512-14 AND 114T2512-12.Oct 8, 2020 · N144FE · Boeing 7673S2F · Wing Miscellaneous StructureSDR FDEA202010052418Static Inverter · failedSTATIC INVERTER FAILS DURING EICAS BUS TIE TEST. WILL NOT POWER THE CAPT PFD. INSTALLED ALT STATIC INVERTER, PASSES EICAS BUSS TIE TEST IAW AMM 24-33-03-4.Oct 5, 2020 · N138FE · Boeing 7673S2F · Pitot/Static SystemSDR FDEA202010052417Stiffener · crackedLT NOSE TUNNEL MAIN CABIN FLOOR BEAM STA 246 APPROX LBL 43 1 EA VERTICAL STIFFENER ANGLE CRACKED. REMOVED AND FABRICATED NEW STIFFENER P/N 141T5146-16, IAW BAC DWG 141T5600 REV. INSTALLED STIFFENER, IAW BAC DWG 141T5600 REV- AND B767 SRM 51-40-02.Oct 5, 2020 · N133FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202010022399Angle · crackedE & E BAY LEFT HAND SIDE, MAIN CABIN FLOOR BEAM, VERTICAL STIFFER ANGLE AT STA 246 APPROX LBL 50 IS CRACKED. REMOVED AND REPLACED ANGLE, PER BAC DWG 141T5600 REV AND B767 SRM 51-40-02.Oct 2, 2020 · N144FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202010022398Angle · crackedBEHIND BULK PIT AFT BULKHEAD, AT STA 1578, MAIN CABIN FLOOR SUPPORT CANTILEVER L-ANGLE IS CRACKED. REMOVED AND REPLACED NEW L-ANGLE, PER B767 SRM 51-40-02 AND BAC DWG 146T5650 REV C.Oct 2, 2020 · N144FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202010012389Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241GFF HAS A PUNCTURE IN THE SKIN. REPAIRED MAIN CABIN FLOOR PANEL 241GFF PUNCTURE, IAW B767 SRM: 53-00-50 FIG 201. MAJOR REPAIR.Oct 1, 2020 · N144FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202010012386Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242GFF HAS MULTIPLE PUNCTURES IN THE SKIN. REPAIRED MAIN CABIN FLOOR PANEL 242GFF PUNCTURES, IAW FEDEX SRZ-25-005 REV R. MAJOR REPAIR.Oct 1, 2020 · N144FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202010012390Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242FFF HAS MULTIPLE PUNCTURES IN THE SKIN. REPAIRED MAIN CABIN FLOOR PANEL 242FF MULTIPLE PUNCTURES, IAW FEDEX SRZ-25-005 REV R. MAJOR REPAIR.Oct 1, 2020 · N144FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202010012388Floor Panel · delaminatedFWD PIT FLOOR PANEL 122CF HAS A PUNCTURE IN THE PANEL SKIN. REPAIRED FLOOR PANEL 122CF, IAW B767 SRM: 53-00-50 FIG 201. MAJOR REPAIR.Oct 1, 2020 · N144FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202010012387Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241ZFF HAS A PUNCTURE IN THE SKIN. REPAIRED CABIN FLOOR PANEL 241ZFF, IAW B767 SRM 53-00-50 FIG 201.Oct 1, 2020 · N144FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202010012385Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241FFF HAS A PUNCTURE IN THE SKIN. REPAIRED CABIN FLOOR PANEL 241FFF, IAW B767 SRM 53-00-50 FIG 201.Oct 1, 2020 · N144FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202010012391Support Angle · crackedAFT CARGO COMPARTMENT ZONE 152 ANGLE JUST BELOW THE FLOOR LEVEL IS CRACKED IN THE RADIUS APPROX RBL 25 AT STA 1087. REMOVED AND REPLACED ANGLE P/N 146T8250-6, IAW B767 SRM 51-40-02 AND BAC DWG 146T8250 REV.Oct 1, 2020 · N133FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202009302364Floor Panel · damagedMAIN CARGO COMPARTMENT FLOOR PANEL 241ZFF IS PUNCTURED. REPAIRED MAIN CARGO COMPARTMENT FLOOR PANEL 241ZFF PUNCTURES, IAW B767-SRM 53-00-50-2R PARA 4C.Sep 30, 2020 · N133FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202009302363Floor Panel · damagedMAIN DECK FLOOR PANEL 241BFF REQUIRES REPAIR. FABRICATED REPLACEMENT FLOOR PANEL TO REPLACE INCOMING DAMAGE ON MAIN DECK FLOOR PANEL 241BFF, IAW SRZ-25-005 REV R.Sep 30, 2020 · N133FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202009292355Skin · dentedLT WING TRAILING EDGE INBOARD AFT FLAP, LOWER SURFACE DENTED. REPAIRED LT WING TRAILING EDGE INBOARD AFT FLAP LOWER SURFACE, IAW B767 SM 57-53-01-2R REPAIR 1 FIG 201 AND 51-70-03-0G PARA 5A FIG 5.Sep 29, 2020 · N133FE · Boeing 7673S2F · Trailing Edge FlapsSDR FDEA202009292354Skin · dentedLT WING TRAILING EDGE INBOARD AFT LAP, UPPER SURFACE DENTED INBOARD. REPAIRED DENT ON UPPER SURFACE L/W T/E INBOARD AFT FLAP WITH BONDED DOUBLER REPAIR, IAW B767 SRM 57-53-01-0I DETAIL 2, 57-53-01-2R TABLE 1, 57-70-10-2R FIG 201, AMM 51-21-01/701.Sep 29, 2020 · N133FE · Boeing 7673S2F · Trailing Edge FlapsSDR FDEA202009292353Bracket · crackedRIGHT WING SLAT DRIVE TORQUE TUBE BRACKET HAS CRACK AT CRACKED AT UPPER FASTENER HOLE. UNDER NR 7 SLAT STREAMER ATTACHED. REMOVED AND REPLACED RT WING SLAT DRIVE TORQUE TUBE BRACKET UNDER NR 7 SLAT, IAW BAC DWG 114T1240 REV E.Sep 29, 2020 · N167FE · Boeing 7673S2F · Leading Edge Slat Control SystemSDR FDEA202009292352Bracket · crackedLEFT WING SLAT DRIVE TORQUE TUBE BRACKET HAS CRACK AT CRACKED AT UPPER FASTENER HOLE. UNDER NR 6 SLAT STREAMER ATTACHED. REMOVED AND REPLACED BRACKET, PER BOEING DWG 114T1240 REV E.Sep 29, 2020 · N167FE · Boeing 7673S2F · Wing, Attach FittingsSDR FDEA202009272336Floorboard · damagedMAIN CABIN FLOORBOARD 242FFF HAS EDGE DAMAGE. REPAIRED MAIN CABIN FLOORBOARD 242FFF HAS EDGE DAMAGE, IAW FED EX B767-300 SRM 53-00-50-0I, 53-00-50-1A, AND 53-00-50-2R PARA 4B.Sep 27, 2020 · N167FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202009272335Floorboard · damagedMAIN CABIN FLOORBOARD 241LFF HAS EDGE DAMAGE. REPAIRED MAIN CABIN FLOORBOARD 241LFF HAS EDGE DAMAGE, IAW FED EX B767-300 SRM 53-00-50-1A AND 53-00-50-2R PARA 4B.Sep 27, 2020 · N167FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202009262331Slide · unwanted deployFUELING REPORTED TROUBLE WITH MAIN ENTRY DOOR. ARRIVED AT AIRCRAFT AND FOUND ESCAPE DEPLOYED. ESCAPE ROPE COVER BOTTOM FORWARD SNAP RIPPED THROUGH. FACT 26SEP20 06:54 MEM U. RE-INSTALLED ESCAPE ROPE. REMOVED AND REPLACED L1 DOOR EMERGENCY ESCAPE ROPE CHASep 26, 2020 · N114FE · Boeing 7673S2F · Escape SlideSDR FDEA202009222339Skin · dentedRT WING, OUTBOARD FLAP, INBOARD LEADING EDGE DENTED. REPAIRED RIGHT WING OUTBOARD FLAP INBOARD LEADING EDGE PANEL 666AT BY BONDING REPAIR PLIES, IAW B767 SRM 57-53-01-01 AND 57-53-01-2R FIG 201 AND 51-70-05. REPAIR GENERAL AND PARAGRAPH 5A AND 5L FIG 5.Sep 22, 2020 · N167FE · Boeing 7673S2F · Trailing Edge FlapsSDR FDEA202009212393Channel · gougedAFT CARGO DOOR CEILING SUPPORT CHANNEL IS GOUGED AND HAS BARE METAL. ACCOMPLISHED REPAIR OF AFT CARGO DOOR CEILING SUPPORT CHANNEL, IAW FEDEX EA H-5320-T0356964, P1.Sep 21, 2020 · N167FE · Boeing 7673S2F · Fuselage Miscellaneous StructureSDR FDEA202009212357Fitting · crackedNR 2 PYLON CENTER SUPPORT STRUCTURE FITTING (BATH TUB) INBOARD SIDE IS CRACKED. ACCOMPLISHED BATH TUB FITTING REPAIR, IAW B767 SRM 54-52-71-2R.Sep 21, 2020 · N167FE · Boeing 7673S2F · Nacelle/Pylon, Attach FittingsSDR FDEA202009182252Skin · chafedLT WING NR 5 SLAT LOWER SURFACE L/E AREA DAMAGE 2 (EA), PLACE AS MARK STREAMER ATTACH. REPAIRED NR 5 SLAT LOWER SURFACE 1EA AREA 89.5" FROM O/B, IAW B767 SRM 57-43-02-2R REPAIR 1 AND 51-70-10-2R REPAIR 4 FIG. 202; 1EA AREA 47.5" FROM O/B FOUND MISSING PAINT NSep 18, 2020 · N166FE · Boeing 7673S2F · Leading Edge DevicesSDR FDEA202009162253Floor Panel · delaminatedMAIN CARGO FLOOR PANEL 242TFA DELAMINATED AND HAS EDGE DAMAGE AT CORNER. REPAIRED AREAS OF DELAMINATION AND EDGE DAMAGE TO CARGO FLOOR PANEL 242TFA, IAW B767 SRM 53-00-50-2R.Sep 16, 2020 · N127FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202009162228Ground Stud · meltedWHILE COMPLYING WITH EA H-4910-F0356148 REVISION A PART 1 DATED SEP 11, 2020 STEP 3, FOUND APU GROUND GD1300-DC ARCHED AND PARTIALY MELTED. REPLACED BRACKET AND CHECKED GROUNDS GD01298-AC AND GD-1300-DC. REPAIRED LEADS AND OPS CHECKED APU. ALL WORK DONE IAWSep 16, 2020 · N169FE · Boeing 7673S2F · APU System WiringSDR FDEA202009162226Angle · crackedNR 2 PYLON AFT BULKHEAD TO AFT FAIRING INBOARD ATTACH ANGLE CRACKED AT NAC STA 295 LT. REMOVED AND REPLACED ANGLE, PER B767 SRM 551-40-02 AND BOEING DWG 313T3310 REV B.Sep 16, 2020 · N127FE · Boeing 7673S2F · Nacelle/Pylon Miscellaneous StructureSDR FDEA202009152221Housing · crackedAFT CARGO DOOR UPPER AFT CARGO LIGHT GOUGED AND CRACKED. REPAIRED AFT CARGO DOOR UPPER AFT CARGO LIGHT, IAW B767-AMM 25-00-00-8.Sep 15, 2020 · N127FE · Boeing 7673S2F · Cargo Compartment LightingSDR FDEA202009152220Housing · crackedAFT CARGO DOOR UPPER FWD CARGO LIGHT GOUGED AND CRACKED. REPAIRED AFT CARGO DOOR UPPER FWD CARGO LIGHT, IAW B767-AMM 25-00-00-8.Sep 15, 2020 · N127FE · Boeing 7673S2F · Cargo Compartment LightingSDR FDEA2020091432191Skin · chafedRIGHT WING SLAT NR 11, T/E LOWER SURFACE CHAFE AT O/B TRACK. REPAIRED RT WING NR 11 SLAT T/E LOWER SURFACE CHAFE AT O/B TRACK WITH 250 DEG METAL BOND, IAW B767 SRM 57-43-01-01 FIG 1 DETAIL NR 1, 57-43-02-01 FIG 1 DETAIL NR 4, 57-43-02-2R REPAIR 1 DETAIL NR Sep 13, 2020 · N127FE · Boeing 7673S2F · Leading Edge DevicesSDR FDEA2020091422186Beam · gougedNR 2 PYLON AFT FAIRING INBOARD LONGITUDINAL BEAM GOUGED AT NUTPLATE LOCATION AT NAC STA 308 LT. REMOVED LATCH BEAM, IAW B767 SRM 51-40-02-0G. REPAIRED LATCH BEAM, IAW B767 SRM 54-52-71-2R AND FED EX EA H5450-T0356442 P1. REINSTALLED LATCH BEAM, IAW B767 SRMSep 12, 2020 · N127FE · Boeing 7673S2F · Nacelle/Pylon, Main FrameSDR FDEA202009142174Floor Panel · delaminatedMAIN CABIN FLOOR PANEL AT BL-0 AND STA 955 TO 1065 DAMAGED. FABRICATED NEW FLOOR PANEL, IAW FED EX EXPRESS SRZ-25-005.Sep 11, 2020 · N143FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202009112171Floor Panel · damagedMAIN CABIN FLOOR PANEL 242GFF IS DAMAGED. REPAIRED MAIN CABIN FLOOR PANEL 242GFF, IAW B767 SRM 53-00-50-2R.Sep 11, 2020 · N127FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202009112170Floor Panel · damagedMAIN CABIN FLOOR PANEL 241ZFF IS DAMAGED. REPAIRED MAIN CABIN FLOOR PANEL 241ZFF, IAW B767 SRM 53-00-50-2R.Sep 11, 2020 · N127FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA202009092157Connector · dirtyPDIS 107, 29-11, 6407, 09SEP20, PEN, FACT, U. WHEN LEVELING AT FL 240 C HYD SYS PRESS LIGHT ILLUMINATED, COMPLIED WITH QRH PROCEDURE. FACT 09SEP20 14:00 PEN U. A/C BLOCKED IN WITH PRESSURE 2970 AT CENTER R HYD SYS WITH SWITCH PUMPS IN OFF POSITION. RECYCLESep 9, 2020 · N107FE · Boeing 7673S2F · Hydraulic Power System WiringSDR FDEA2020090982147Former · crackedRT WING LEADING EDGE INTERNAL FORMER CRACKED ON OUTBOARD SIDE OF SLAT NR 8 OUTBOARD ACTUATOR. REMOVED AND REPLACED RT WING RIB FORMER AT W/S 480, PER FEDEX B767 SRM 51-40-02 & BAC DWG 114T2511. LOCATED AND DRILLED PER FEDEX B767-SRM 51-40-05.Sep 8, 2020 · N127FE · Boeing 7673S2F · Wing Main, Frame StructureSDR FDEA2020090972139Bracket · crackedLT WING, LEADING EDGE CAVITY FWD FORMER BRACKET CRACKED, LEADING EDGE STA 430. REMOVED CRACKED FORMER BRACKET IAW B767 SRM 51-40-02, MATERIAL ID 2024T3 .040" IAW BAC DWG 114T2170. FABRICATED RIB FORMER BRACKET, IAW BOEING DWG 114T2170 REV ALODINED, IAW BOEINSep 7, 2020 · N127FE · Boeing 7673S2F · Wing Main, Frame StructureSDR FDEA2020090972138Splice Plate · crackedRT WING LEADING EDGE INTERNAL SPLICE PLATE CRACKED APPROX 1' OUTBOARD OF SLAT #8 OUTBOARD ACTUATOR. REMOVED AND REPLACED SPLICE P/N 114T2800-165, PER BAC DWG 114T2800 REV G.Sep 7, 2020 · N127FE · Boeing 7673S2F · Wing Main, Frame StructureSDR FDEA2020090972137Bracket · crackedLT WING, LEADING EDGE CAVITY FWD FORMER BRACKET CRACKED. LEADING EDGE STA 480 REMOVED AND REPLACED NOSE FORMER, IAW BOEING DWG 114T2511, REV D, B767 SRM 51-40-02 AND B767 SRN 51-40-03.Sep 7, 2020 · N127FE · Boeing 7673S2F · Wing, Attach FittingsSDR FDEA2020090962134Bracket · crackedLEFT WING PANEL 511KB AREA INBOARD BRACKET CRACKED. REMOVED AND REPLACED BRACKET P/N 256T2425-6, PER BOEING DWG 114T1240 REV D.Sep 6, 2020 · N127FE · Boeing 7673S2F · Wing, Attach FittingsSDR FDEA2020090942107Bracket · crackedRT WING PANEL 611KB AREA IB BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON RT WING PANEL 611KB AREA, PER FEDEX B767 SRM 51-40-02 AND PER BOEING DWG 114T1240 REV D.Sep 4, 2020 · N127FE · Boeing 7673S2F · Wing, Attach FittingsSDR FDEA2020090922082Former · crackedLT WING LEADING EDGE CAVITY FWD FORMER STRAP CRACKED LEADING EDGE STA 505. REMOVED AND REPLACED LT WING LEADING EDGE CAVITY FWD FORMER STRAP LES 505 PN 114T2800-165 SEAL STRIP PO NR 979532.1, IAW BAC DWG 114T2800 REV G, B767 SRM 51-40-02.Sep 2, 2020 · N127FE · Boeing 7673S2F · Wing Main, Frame StructureSDR FDEA202008282050Skin · gougedFUSELAGE, FWD LOWER FUSELAGE SKIN AT STATION 773 STRINGER 36 LT FOUND WITH EXISTING BLEND OUT WITH GOUGE MARK. FWD LOWER FUSELAGE SKIN AT STATION 773 STRINGER 36 LT EXISTING BLEND OUT WITH GOUGE MARK, EVALUATED AND FOUND EXCEED LIMIT PER B767 SRM 53-00-01-1Aug 28, 2020 · N107FE · Boeing 7673S2F · Fuselage Main, Plate/SkinSDR FDEA202008262032Skin · damagedFUSELAGE, FORWARD LOWER FUSELAGE SKIN AT STATION 478, STRINGER 35 LEFT FOUND WITH EXISTING BLEND OUT. FWD LOWER FUSELAGE SKIN AT STATION 478 STRINGER 35 LEFT EXISTING BLEND OUT AREA. REPAIRED AS PER E.A NR: H-5330-T0356108 PART 1 TITLE: FUSELAGE-PLATES & SKIAug 26, 2020 · N107FE · Boeing 7673S2F · Fuselage Main, Plate/SkinSDR FDEA202008262030Skin · damagedFUSELAGE, FWD LOWER FUSELAGE AT STATION 325, STRINGER 34 LT FOUND WITH EXISTING BLENDOUT. FWD LOWER FUSELAGE SKIN AT STATION 325 STRINGER 34 LT EXISTING BLENDOUT EXCEED LIMIT AS PER B767 SRM 53-00-01-1A ALLOWABLE DAMAGE 1 FIGURE 101 DETAIL II. DAMAGED SKINAug 26, 2020 · N107FE · Boeing 7673S2F · Fuselage Main, Plate/SkinSDR FDEA202008262027Skin · damagedFUSELAGE - RIGHT HAND LOWER FUSELAGE AT STATION 390, BETWEEN STRINGER 29 RIGHT TO 30 RIGHT FOUND WITH EXISTING BLEND OUT. RIGHT HAND LOWER FUSELAGE SKIN AT STATION 390 BETWEEN STRINGER 29 RIGHT - STRINGER 30 RIGHT EXISTING BLEND OUT EXCEED LIMIT PER B767 SAug 26, 2020 · N107FE · Boeing 7673S2F · Fuselage Main, Plate/SkinSDR FDEA2020082652033Slat System · out of rigAPPROACHING THE FIELD (IND) WHEN SELECTING FLAPS 1 DEG, RECEIVED "LE SLAT ASYM". RAN CHECKLIST, LANDED FLAPS 20 USING ALT TE FLAPS. IND U FOUND A SPLIT BETWEEN SLAT NR 2 AND NR 3 WITH DAMAGE TO ANTI ICE DUCT. PERFORMED DVI ON DISPLACED NR 2/3 TORQUE TUBE Aug 25, 2020 · N131FE · Boeing 7673S2F · Leading Edge Slat Control SystemSDR FDEA2020082642008Attach Angle · crackedNR 2 PYLON LT FWD SKIRT BEAM ATTACH ANGLE CRACKED. REMOVED AND REPLACED ATTACH ANGLE PER B767 SRM 51-40-02 AND BAC DWG 313T3310 REV.Aug 24, 2020 · N128FE · Boeing 7673S2F · Nacelle/Pylon, Attach Fittings
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