Boeing 767-34AF

Service difficulty reports · 6,321

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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 = '76734AF'
  ORDER BY difficulty_date DESC"

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SDR IPXA1664037Control Cable · damagedCREW REPORTED STAB FAULT INBOUND. MX INSP FOUND LARGE AMOUNT OF ICE WITH PULLEY AND CABLE DAMAGE IN TAIL OF ACFT. FOUND ICE IN STAB AND THE CABLE DRUMS FOR THE STAB INDICATION WERE BROKEN. (OPEN)Jan 6, 2011 · N315UP · Boeing 76734AF · Stabilizer Control SystemSDR IPXA1664029Seal · damagedMAIN CABIN DOOR VERY STIFF DURING OPERATION. EXCESSIVE FORCE REQUIRED TO OPEN AND CLOSE. FOUND FWD DOOR TRIM SEAL BUNCHING UP AT 30-35 IN FROM FLOOR REF IPC 52-11-02, FIG 10A ITEM 15. ACCOMPLISHED CREW ENTRY DOOR ADJUSTMENT/TEST WITH NO ADJUSTMENTS MADE FOUJan 5, 2011 · N337UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA10663910Altimeter · inoperativeSTBY ALTIMETER INOP, DIVERTED. T/S C/O IAW FIM 34-13-06, FIG 104, STEP 1,2,3, AND 23. CYCLED CB'S 11B7 11P2, 11A8. STBY ALTIMETER OPERATES OK. NO FURTHER PROBLEMS AND MALFUNCTIONS FOUND.Dec 21, 2010 · N309UP · Boeing 76734AF · Altimeter, Barometric/EncoderSDR IPXA0663696Panel · damagedREF D439829, POSITION 4, DAMAGE 5" FROM RT SIDE PANEL AND 5' FROM A FT EDGE. FABRICATED AND REPLACED PANEL IAW EO B767-5320-9693-G.Nov 28, 2010 · N327UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA0663704Floor Panel · damagedMAIN CARGO FLOOR PANEL REQUIRES FABRICATION IAW EO B767-5320-9693E. THIS IS A MAJOR REPAIR. ACCOMPLISHED FABRICATION OF MAIN CARGO FLOOR PANEL ON NRC 355114 IAW EO B767-5320-9693E.Nov 25, 2010 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA0663686Floor Panel · damagedMAIN DECK FLOOR PANEL, PN 145T5876-68 IS DAMAGED. FABRICATED NEW FLOOR PANEL ON NRC 355114 IAW EO B767-5320-9693-G.Nov 25, 2010 · N310UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA0663603Skin · dentedNR5 SLAT (LT WING) HAS L/E DENTS. SKIN CUTOUT MEASURES 8.3 X 7.2 REF D -437285. REPAIRED IAW EO B767-5750-40211-B.Nov 15, 2010 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10663562Floor Panel · damagedREF D 434408, POSITION 2L HAS 1 X 1 HOLE IN FLOOR PANEL. REMOVED FLOOR PANEL AND MFG NEW PANEL IAW EO B767-5320-9693G AND INSTALLED IAW AMM 51-01-01.Nov 6, 2010 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10663560Floor Panel · damagedREF D-4344202 POSITION 2L HAS 1 X 1 HOLE IN FLOORBOARD. REMOVED FLOOR PANEL AND MFG NEW PANEL IAW EO B767-5320-9693 AND INSTALLED IAW AMM 51-01-01.Nov 6, 2010 · N324UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10663448Floor Panel · damagedMAIN CARGO DECK POSITON 10L FLOOR PANEL HAS SMALL HOLE 2" X 1". FABRICATIED NEW FLOOR PANEL PN 146T5869-107 IAW EO B767-5320-9693G.Oct 29, 2010 · N336UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10663424Connector · brokenINSPECTION TYPE:ETOP DIVERSION - "CARGO DET AIR" EICAS MESSAGE. M438137. R & R SMOKE DETECTOR VACUUM SWITCH IAW AMM 26-16- 04-4. FOUND CONNECTOR BROKEN ON SWITCH.Oct 29, 2010 · N302UP · Boeing 76734AF · Fire Protection System WiringSDR IPXA10663367Computer · inoperativeR EICAS COMPUTER SCROLLING. ALL WARNING CAUTION STATUS MESSAGES CONTINUALLY CAUSING CONTINUAL ACTIVATION OF THE MATER CAUTION AURAL LIGHT. REMOVED AND REPLACED RT EICAS COMPUTER PER AMM 31-41-02-4.Oct 26, 2010 · N301UP · Boeing 76734AF · Central WarningSDR IPXA10663317Floorboard · dentedREF DMI D429161, MAIN CARGO DECK POS NR 2 RT FLOORBOARD - 2ND BOARD IN FROM OTBD HAS A 1-INCH BY 1-INCH DENT. REPLACED FLOORBOARD WORKING WITH EO B767-5320-9693 AND M/M 53-01-06.Oct 24, 2010 · N337UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10663210Skin · damagedRT OTBD FLAP T/E WEDGE SKIN DAMAGED. REPAIRED IAW EO B767-5750-39284-B.Oct 18, 2010 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10663178Eec · inoperativeINSPECTION TYPE:ETOP, LT ENGINE SHUTDOWN DUE TO AN ENGINE VALVE LIGHT AT 300 FT, WHILE ON FINAL APPROACH. R & R EEC DUE TO STORED PIMU MESSAGE.Oct 15, 2010 · N340UP · Boeing 76734AF · Fuel Controlling SystemSDR IPXA10663155Compressor · stalledINSPECTION TYPE:ETOP, RT ENGINE HAD 4 COMPRESSOR STALLS AT 200 FT, NO HIGH EGT OR ENGINE EXCEEDENCE. CHECKLIST WAS ACCOMPLISHED, TRIED ONE MORE RECOVERY, HOWEVER ENGINE STALLED AGAIN. ENGINE WAS SHUTDOWN, LANDING WEIGHT WAS 320.00. R & R ENGINE.Oct 14, 2010 · N314UP · Boeing 76734AF · Turbine Engine Compressor SectionSDR IPXA10663056Floorboard · damagedHOLE IN MCD FLOORBOARD POSITION 4 CTR FS.635, LBL3. REPAIRED IAW SRM 53-00-50-2R PARA 6.Oct 11, 2010 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662910Floor Panel · damagedPOS 4 RT MAIN CARGO DECK FLOOR PANEL 3 RD FROM RT HAS DAMAGE. REMOVED AND MANFACTURED NEW PANEL IAW EO B767-5310-9693-G.Oct 2, 2010 · N328UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662886Pressure Switch · inoperativeE-TOP DIVERSION LT ENGINE ANTI-ICE DISPLAYED AND ENGINE ANTI ICE VALVE REMAINED ILLUMINATED WITH SWITCH ON. REPLACED LT ENG ANTI ICE VALVE IAW MM 30-21-03-4 AND THERM A/I PRESS SWITCH IAW MM 30-21-04-4. OPS CHECK NORMAL.Oct 1, 2010 · N314UP · Boeing 76734AF · Air Intake Anti/De-Ice SystemSDR IPXA10663051Skin · damagedINSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD SIDE FITTING FAILSAFE STRAP SKIN ATTACH AREA DAMAGE FOUND AFT FAILSAFE STRAP CUTOFF. DAMAGE SMOOTHED OUT & REPROTECTED IAW R53-50-36849 & EO B767-5330-40064. BLEND OUT AREA A 0.75" X 2.75" X 0.025", AREA B 2" X 2.Sep 27, 2010 · N305UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10663042Attach Fitting · crackedINSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD ATTACH FITTING FOUND 1EA FASTENER HOLE CRACKED APPROX 0.020" RUNNING DOWN. AND FOUND 2 EA FASTENER HOLES SHORT EDGE MARGIN ARE 1.33" AND 1.664". ATTACH FITTING REPLACED IAW EO B767-5350-17922G APP C & REPAIRED IAWSep 27, 2010 · N305UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10662847Floorboard · dentedPREVIOUS REPAIR FAILED ON MCD CNTR FLOORBOARD POS 9/10. REQUIRES NEW REPAIR PANEL. REPAIR IS A MAJOR REPAIR TRANSFERRED TO NRC 355064. SEE LOG PAGE 450344 FOR REMOVAL ITEM NR1.Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662846Floor Panel · dentedCTR FLOORBOARD PANEL AT POS 10/11 HAS 3 HOLES ALONG WITH SEVERAL OTHER HOLES ON DEFERRAL REF D413492, D426407. REMOVED PANEL IAW AMM 53-01-05-4. REF L/P 450341/3 FOR PANEL INSTALLATION. THIS IS AS MAJOR REPAIR TRANSFERRED TO NRC 355067. ALL WORK COMPLETED ONSep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662845Floor Panel · dented2ND FROM AFT PANEL AT POSITION 5 CTR IN MCD HAS DENT RUNNING APPROX 2 FT LONG AT AFT EDGE GOING FWD AND THROUGH 2 PREVIOUS REPAIRS. (MARKED) REMOVED PANEL IAW AMM 53-01-05-4. SEE LP 450338/1 REF D413473 AND REF L/P 450342/1 FOR REMOVAL AND REINSTALL. ITEM IS Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662844Floor Panel · dentedAFT PANEL AT POSITION 5 CTR HAS A DENT, FULL LENGTH OF THE PANEL AND THROUGH A PREVIOUS REPAIR. MARKED. REMOVED FLOOR PANEL 14315876-58 IAW AMM 53-01-05-4. REFERENCE L/P 450341 ITEM 2 FOR PNL INSTALL. ITEM IS A MAJOR REPAIR TRANSFERRED TO NRC 355068. COMPLETSep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662817Floor Panel · damagedFLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662816Floor Panel · damagedFLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662815Floor Panel · damagedFLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662814Floor Panel · damagedFLOOR PANEL DAMGED, REPAIRED IAW EO B767-5320-9693-G.Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662813Floor Panel · damagedFLOOR PANEL DAMAGED. REPAIRED IAW EO B767-5320-9693-G.Sep 27, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662795Floor Panel · puncturedFLOOR PANEL .5" HOLE ON UPPER SKIN AT POS 14 AT LBL85 THIS IS A MAJOR REPAIR. REPAIR IAW SRM 53-00-50-2R, PAR 4.Sep 26, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662794Floor Panel · puncturedFLOOR PANEL AT POS 9L HAS SMALL PUNCTURE. REPAIRED IAW SRM 53-00-50-2R.Sep 26, 2010 · N304UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662865Floor Panel · dentedINSPECTION TYPE:8C, M/D STA 540 TO 654+22, RBL 11" TO LBL 11" FLR PNL FND 8 DENTS & 4 DAMAGE. FLOOR PANLE FABRICATE IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53 53-01-01.Sep 25, 2010 · N305UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2675473Floor Panel · damagedHOLE IN MAIN CARGO DECK FLOOR PANEL POS 7R THIRD FLOOR PANEL FROM OTBD. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Sep 23, 2010 · N306UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662864Floor Panel · dentedINSPECTION TYPE:8C, M/D STA 933 TO 970, LBL 11 TO RBL 11 FLR PNL FND 12 DENT MARKS & UPPER SURFACE FIBERGLASS DELAMINATED (1" WIDTH & 37" LONG). FLR PNL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.Sep 23, 2010 · N305UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662787Skin · damagedON ARRIVAL FOUND DAMAGE TO OTBD FLAP L/E SKIN PANEL 666FT, 3.5"X0.75" LOCATED 1.5" FROM L/E OF PANEL AND 1.5" FROM OTBD EDGE OF PANEL. REPAIRED IAW SRM 57-53-01-2R FIG 201 AND SRM 51-70-03.Sep 23, 2010 · N324UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10663043Fitting · crackedINSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 7 O/C POSITION AT TEE FITTING APPROX .2500" IN LENGTH AND FOUND 1 EA FASTENER HOLE SHORT EDGE MARGIN IS 0.66". TEE FITTING REPLACED IAW EO B767-5350-17922G APP. D & REPAIRED IAW HXSep 22, 2010 · N305UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA10663041Stiffener · crackedINSPECTION TYPE:C, LT MLG W/W CANTED PRESSURE DECK AT BS 977 LATERAL "Z" STIFFENER FOUND CRACKED AT FASTENER HOLE AREA BETWEEN LBL 20 AND LBL 55. CRACK LENGTH ARE 1.625" AT LBL 32.94 AND 1.6" AT LBL 54.69. STIFFENER REPAIRED IAW HX RS NR R53-58-36842 REV A &Sep 22, 2010 · N305UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10663010Wedge · puncturedINSPECTION TYPE:C, RT WING OTBD FLAP UPPER SURFACE T/E WEDGE PUNCH HOLE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 9, REV 48.Sep 22, 2010 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10662992Fitting · crackedINSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 4 O/C AND 10 O/C POSITION AT FAIL SAFE STRAP THROUGH THICKNESS & APPROX .12" IN LENGTH. FUSELAGE BS955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-179Sep 22, 2010 · N305UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA10662991Failsafe · crackedINSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 2 O/C POSITION AT FAIL SAFE STRAP APPROX .1250" IN LENGTH. FUSELAGE BS955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-G, APPENDIX C AT LT SIDE.Sep 22, 2010 · N305UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA10662988Skin · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP LWR SURFACE INBD AFT PANEL INBD AREA FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 3, REV 48.Sep 22, 2010 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10662964Wedge · puncturedINSPECTION TYPE:C, RT WING OTBD FLAP T/E WEDGE UPPER SURFACE PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 9, REV 48.Sep 22, 2010 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10663050Intercostal · crackedINSPECTION TYPE:C, M/DECK STA 1043 LBL 11 TO RBL 11 INTERCOSTAL FOUND CRACKED. MAIN DECK STA 1043 LBL 11 TO RBL 11 FLOOR INTERCOSTAL REPLACED AFTER FABRICATED IAW HX RS R53-00-36841 AND EO B767-5320-40037, ORG MATL BAC1518-790-7075T6511. FABRICATE NEW INTERCOSep 21, 2010 · N305UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10662989Skin · chafedINSPECTION TYPE:C, RT WING NR9 SLAT UPPER WEDGE OTBD OF 30" FOUND DEEP CHAFING ON LWR SURFACE. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R. REPAIR 4, FIG 202, SHEET 8, REV 48.Sep 21, 2010 · N305UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10662963Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-71-05, PAR 5A(1) FIG 5, REV 48.Sep 21, 2010 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10662962Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 48.Sep 21, 2010 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10662961Stiffener · crackedINSPECTION TYPE:C, FWD CARGO COMPT WING CTR TANK FRONT SPAR ATT VERT STIFFNER FOUND CRACK AT STA785.9 LBL54.69 THIS REPAIR IS DAMAGE WITHIN 22" OF ANOTHER REPAIR AT LBL32.94, NRC EUW500284. FWD CGO COMPT WING CTR TANK FRONT SPAR AT STA785.9, LBL54.69 VERT STISep 20, 2010 · N305UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10662938Stiffener · crackedINSPECTION TYPE:C, FWD CARGO COMPT WING CTR TANK FRONT SPAR ATT VERT STIFFENER FOUND CRACK AT STA785.9, LBL32.94. THIS REPAIR WITHIN 22" OF ANOTHER REPAIR AT LBL54.69" NRC EUW500292. FWD CGO COMPT WING CTR TANK FRONT SPAR STA785.9, LBL32.94 VERT STIFFENER RESep 20, 2010 · N305UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10662654Floor Panel · damagedD424528 MAIN CARGO POS 4 L FLOOR PANEL 2ND FR PM OTBD HAS .5" HOLE. REMOVED AND MFG NEW FLOOR PANEL IAW B767-5320-9693G.Sep 18, 2010 · N314UP · Boeing 76734AF · Fuselage Floor Panel
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