Boeing 747-87UF

Service difficulty reports · 1,102

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 = '74787UF'
  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 UIEA2024041900280Skin · worn#9 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2024041900281Skin · worn#7 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2024041900282Skin · worn#8 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2024041900283Skin · worn#18 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPIAR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2024041900284Skin · worn#20 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2024041900285Skin · worn#19 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2024041900286Nut · unknownREFER JOB CARD SEQ 1.725 #1 CANOE AFT FRAME MOD FIG 6 INSTALLATION AFTER ROW HAS 5EA FASTENER HOLE LOCATION CAN NOT USE BACC30AC6 DUE HOLES TOO CLOSE TO ART INTERFERENCE COLLAR(<P>NUTS REPLACED AS PER RI-57-50-16856 REV A. NO FURTHER DEFECTS NOTED</P>)Apr 24, 2024 · N851GT · Boeing 74787UF · Wing Main, Frame StructureSDR UIEA2024042000302Skin · eroded#10 V/C FLAP UPR EDGE FOUND EROSION(<P>PERFORMED REPAIR AT EROSION AREA IAW SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED</P>)Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2024042200303Beam · crackedRHW L/E ILES 560 D BEAM WEB CRACKED(<P>RHW L/E ILES 560 D BEAM WEB REPAIRED AS PER RI-57-41-16827 REV A. NO FURTHER DEFECTS NOTED</P>)Apr 24, 2024 · N851GT · Boeing 74787UF · Wing Main, Frame StructureSDR UIEA2024042200304Intercostal · deformedFUSELAGE - SECT 46 - WTB FAIRING INTERCOSTAL, P/N: 65B07241-1 BETWEEN STA 1480 +60 TO STA 1520 LBL 45. DEFORMATION DAMAGE - TEMPORARY REPAIR REFER EA-4853A0088(<P>FUSELAGE - SECT 46 - WTB FAIRING INTERCOSTAL REPLACED AS PER SRM 51-10-02, SRM 51-40-02 AND RI-53Apr 24, 2024 · N851GT · Boeing 74787UF · Aerodynamic FairingsSDR UIEA2024031900158Battery Pack · no testU/D EMER LIGHT BATT PACK CAP TEST FAILED. REPLACE BATTERY PACK AND OPERATION TEST NORMAL IAW AMM 33-51-04 REV 44. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Emergency LightingSDR UIEA2024031900159Battery Pack · no testU/D EMER LIGHT BATT PACK CAP TEST FAILED. REPLACE BATTERY PACK AND OPERATION TEST NORMAL IAW AMM 33-51-04 REV 44. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Emergency LightingSDR UIEA2024031900160Battery · no testU/D EMER LIGHT BATT PACK CAP TEST FAILED. REPLACED BATTERY POWER SUPPLY AND OPERATION TEST NORMAL IAW AMM 33-51-04 REV 44. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Emergency LightingSDR UIEA2024032100166Skin · torn#8 V/C FLAP LSA FOUDN TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2024032100170Skin · torn#9 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA AS PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2024032100172Skin · torn#6 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2024032100178Skin · torn#7 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2024032100180Skin · torn#21 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2024032100181Skin · torn#20 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2024032100182Skin · torn#19 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2024032100183Skin · torn#18 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER SMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2024032200184Floor Panel · damagedM/D - STA 460 - 480 LBL 30-90 FLOOR PANEL FOUND DEPRESSION. FABRICATED FLOOR PANEL IAW RI-53-00-16779 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Floor PanelSDR UIEA2024032200188Skin · dented2EA DENTS IN LH NLG DOOR AT O/B EDGE CENTERED LENGTHWISE STA 292.82 FWD DENT 3.0W X 0.5 DEEP AFT DENT 3.0W X .05 AFT DENT 2.5W X 0.3 DEEP DEEP. LH NLG DOOR AT O/B EDGE CENTERED LENGTH WISE STA 292.82 FWD WITHIN SRM 52-80-01-1A-1 LIMITS REV 42 ( W=3" Y=0.06Mar 29, 2024 · N850GT · Boeing 74787UF · Landing Gear DoorsSDR UIEA2024032200189Repair · torn#10 V/C FLAP EXISTING PATCH FOUND TORN. PERFORMED REPAIR AT EXISTING PATCH TORN AREA PER SRM 51-70-04 REPAIR 7. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge FlapsSDR UIEA2024032200190Skin · dented2EA DENTS IN LH NLG DOOR AT O/B EDGE CENTERED LENGTHWISE STA 292.82 FWD DENT 3.0W X 0.5 DEEP AFT DENT 2.5W X .03 DEEP. LH NLG DOOR AT O/B EDGE CENTERED LENGTHWISE STA 292.82 AFT WITHIN SRM 52-80-01-1A-1 LIMITS REV 42 DATE 20 FEB 2024 ( W=1" Y=0.030" W/Y = 33Mar 29, 2024 · N850GT · Boeing 74787UF · Landing Gear DoorsSDR UIEA2024032200191Skin · dentedDENT AFT CARGO DOOR BS 1850 LENGTH 1.063 X 0.118 X 0.01 WIDTH WITHIN LIMITS PER SRM 53-00-01-14-2 FIG . REF SRM 52-30-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL V111 REV 42 AND NTM PART 6, 51-00-00 PROC 23 REV 176. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Cargo/Baggage DoorsSDR UIEA2024032200192Door Frame · dentedDENT AT FWD EDGE AFT CARGO DOOR FRAME DENT. SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 REV 42. MEASURED LENGTH 1.25" DEPTH 0.100" WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL I LIMIT REV 42. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, StructureSDR UIEA2024032200193Rib · crackedRH HORI STAB CLOSURE RIB UPPER CHORD FOUND CRACKED. UPPER CHORD REPLACED IAW SRM 51-10-02, SRM 51-40-05 AND SRM 51-40-02 ALL IN REV 42. HORI STAB CLOSURE RIB UPPER CHORD AREA. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer, Spar/RibSDR UIEA2024032200194Web · crackedRH HORI STAB TIP FAIRING I/B SUPPORT WEB LOWER CHORD CRACKED. LOWER CHORD REPLACED PER SRM 51-10-02, SRM 51-40-05 AND SRM 51-40-02 ALL IN REV 42 DATE 20 FEB 2024 AT EMP - RH HORI STAB TIP FAIRING I/B SUPPORT WEB LOWER CHORD AREA. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous StructureSDR UIEA2024032200195Skin · crackedEMP - RH HORI STAB REAR SPAR STIFFENER FOUND CRACK AT STAB STAB. 560-4. FABRICATE THE STIFFENER P/N 65B03779-66 PER 65B03779 DWG 1, 2 AND PL AS PER FORM 02373R02, SRM 51-10-02, 51-40-05 AND SRM 51-40-02 REV 42. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer, Plate/SkinSDR UIEA2024032200196Skin · damagedVERT FIN TIP FAIRING UPPER T/E CORNER BURN MARK. BLEND OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND MEASURED. ALLOWABLE DAMAGE PER SRM 55-30-30-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL XIV ALL IN REV 42.Mar 29, 2024 · N850GT · Boeing 74787UF · Vertical Stabilizer, Plate/SkinSDR UIEA2024032400212Stringer · crackedM/D - STA 920-940 S-7R STRINGER SUSPECT SCRATCH / CRACK AND STA 962 STR 7R 1 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 920-940 AND STA 962 S-7R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16783 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032400213Channel · crackedL/H HORI. STAB. TIP FAIIRNG U CHANNEL FOUND CRACK. BONDED NEW U CHANNEL PER RI-55-10-16799 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous StructureSDR UIEA2024032400214Channel · crackedR/H HORI. STAB. TIP FAIIRNG U CHANNEL FOUND CRACK. BONDED NEW U CHANNEL PER RI-55-10-16798 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous StructureSDR UIEA2024032400215Stringer · crackedM/D - STA 940-960 S-8R STRINGER SUSPECT SCRATCH / CRACK AND STA 982 STR 8R 1 LOC CRACK FROM RIVET TO STRINGER. M/D STA 940-960 AND STA 982 S-8R STRINGER REPAIR AS PER SRM 53-20-03 & RI-53-20-16784 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032400216Stringer · crackedM/D - STA 880-900 S-8R STRINGER SUSPECT SCRATCH / CRACKED. M/D - STA 880-900 S-8R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16784 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032400217Stringer · crackedM/D STA 880-900 S-7R STRINGER SUSPECT SCRATCH / CRACK. M/D STA 880-900 S-7R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16783 REV A. NO FURTHER DEFECTS NOTED. P/N 142U7741-14.</P>)Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032400218Stringer · crackedM/D - STA 900 STR 10R 1 LOC CRACK FROM RIVET TO STRINGER AND STA 920 STR 10R 5 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 900 AND STA 920 STR 10R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16786 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032400219Stringer · crackedM/D - STA 820 STR 9R 1 LOC CRACK AT STRINGER AND STA 840 STR 9R 1 LOC CRACK AT STRINGER. M/D - STA 820 STR 9R AND STA 840 STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16785 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032500220Stringer · crackedM/D - STA 910 STR 12R 1 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 910 STR 12R STRINGER REPAIR AS PER SRM 53-20-03 REPAIR 2, REFER TO HKA-TLS-24-0130. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032500221Stringer · crackedM/D - STA 918 - 920 STR 9R 8 LOC CRACK FROM RIVET TO STRINGER AND STA 962 STR 9R 1 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 918 - 920 AND STA 962 STR 9R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16785 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032500222Stringer · crackedM/D - STA 778 STR 9L 1 LOC CRACK FROM RIVET TO STRINGER AND STA 781 STR 9L 2 LOC CRACK. M/D - STA 778 AND STA 781 STR 9L STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16782 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032500223Stringer · crackedM/D - STA 934, 938, 942 STR 9L 3 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 934, 938, 942 STR 9L STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16782 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032500224Stringer · crackedBS 943, STR 7L 1 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 943 STR 7L STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16781 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/StringerSDR UIEA2024032500225Flap · eroded#16 K/FLAP BULLNOSE FOUND EROSION. PERFORMED REPAIR AT EROSION AREA PER SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Leading Edge DevicesSDR UIEA2024032500227Seat Track · damagedM/D - STA 1512 AND STA 1552 LBL 11:33 SEAT TRACK HOLES INSPECTION FINDING ARE BUSHING MISSING AS PER EO 4835A085(<P>STA 1512 AND STA 1552 LBL 11:33 SEAT TRACK REPAIRED IAW SRM 53-00-52 REPAIR 9 REV 42 DATE 20 FEB 2024 AND RI-53-00-16801 REV A. NO FURTHER DEFECMar 29, 2024 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2024032600228Skin · dentedRH SIDE SECTION 46 13" AFT MIDWAY UP FROM AFT CARGO DOOR CUTOUT 3" X 3" CIRCULAR BLEND. REPAIR IAW SRM 51-10-02 AND SRM 51-20-01 REV 42 DATE 20 FEB 2024 AND RI-53-60-16802 REV A. NO FURTHER DEFECTS NOTED.Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Plate/SkinSDR P5CA2024032300006Actuator · brokenBODY GEAR STEERING EICAS MESSAGE. RTO AT LOW SPEED(<P>PERFORMED DVI OF R/H BODY GEAR AND FOUND R/H BODY GEAR, R/H ACTUATOR BROKEN. PERFORMED CONDITIONAL INSPECTION PER AMM 05-41-07. NO FURTHER DAMAGE NOTED. </P>)Mar 21, 2024 · N857GT · Boeing 74787UF · Landing Gear Steering SystemSDR UIEA2023121540997Unknown · unknownFLAPS DRIVE ON APPROACH WHEN SELECTING FLAPS 5 (FROM FLAPS 1). T/E FLAPS STATUS MSG AFTER LANDING. EMERGENCY DECLARED.(<P>RAN FCC GROUND TEST. ALL PASSED REF AMM 27-51-00. FLAPS OPERATE NORMAL. </P>)Nov 11, 2023 · N850GT · Boeing 74787UF · Trailing Edge Flap Control SystemSDR P5CA2023091400105Unknown · unknownLWR RUDDER - FX, L/H AFT SEAL TORN(<P>LOCALLY FABRICATE REPAIR IAW RI #RI-53-00-16472 REV A. NO FURTHER DEFECTS NOTED</P>)Sep 22, 2023 · N858GT · Boeing 74787UF · Rudder Structure
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