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.
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
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 P5CA2019092300190Structure · crackedCRACK ON LOWER CHORD OF HORIZONTAL STABILIZER, RT TIP, AT STAB BL 421.5. REPAIRED DAMAGED AREA IAW EI NR T2019A55M-3713 REV 2. JOB COMPLETED AND CONDITION CHECKS NORMAL.SDR P5CA2019092300189Web · crackedCRACKS ON LOWER CHORD, UPPER CHORD, AND WEB OF LT SIDE HORIZONTAL STABILIZER; TRAILING EDGE AT STAB BL 421.5. REPAIRED DAMAGED AREAS IAW EI NO T2019A55M-3727 REV 3. JOB COMPLETED AND CONDITION CHECKS NORMAL. CRACK LENGTH 0.5", 3", 5"SDR P5CA2019092300188Rib · wornWORN - FASTENER HOLES ON THE RT WING, L/E RIB AT IFSS 443.67. ACCOMPLISHED EI NO T2019A57M-3618 REV 1. JOB COMPLETED AND CONDITION CHECKS NORMAL.SDR P5CA2019081200168Wire · damagedFOUND THE NR 1 APU GENERATOR PIN N HAD SPARK MARK. DISCONNECTED APU GENERATOR 1 WIRE IAW JC ATTACHING SHEET 0192683. REPLACED THE GENERATOR WITH NEW PARTS IAW AMM 24-21-03-004-001, REV 30, AND AMM 24-21-03-404-023, REV 30. PERFORMED APU GENERATION INSTALLATSDR P5CA2019081200167Ram Air Turb · inoperativeFOUND RAT RPM SHOWING ZERO WHEN PERFORMING FUNCTIONAL CHECK OF THE RAT SYSTEM. REMOVED AND REPLACED RAT PUMP IAW AMM 29-21-02-000-801, REV 30, AND AMM 29-21-02-400-801, REV 30, STEP 2A - 2F. REMOVED AND REPLACED RAT GCM IAW AMM 29-21-20-000-801 AND 29-21-400-SDR P5CA2019081200166Rib · crackedRIGHT WING, INBD L/E CAVITY UPPER RIB CRACKED AT LOWER SUPPORT ATTACH AREA, IFSS 439.34. REPAIRED THE DAMAGED AREA IAW EI T2019A57M-3413, REV 1, AND DWG 11642014, SH 3, REV A. CHECKED NORMAL.SDR UIEA2019072404834Panel · crackedRT WING T/E I/B TOP FIXED PANEL AT #8 SPOILER, O/B FWD CUTOUT FOUND CRACKED. (<P>RT WING T/E I/B UPPER FIXED PANEL AT #8 SPOILER O/B FWD, COMPOSITE HOT BOND REPAIRED AS PER RI NO: RI-57-51-13650 REV A AND REF PROCESS CARD: UVH502709-01.</P>)SDR UIEA2019072404835Divider · damagedFWD CARGO COMPARTMENT AFT B/H DIVIDER 123L SURROUNDING EDGE SEVERAL LOCATIONS FOUND TORN AND BUTTONS DAMAGED. (<P>FWD CARGO COMPARTMENT AFT B/H DIVIDER 123L CURTAIN PATCH STITCHES REPAIRED AS PER RI NO: RI-25-52-13647 REV A 16JUL2019.</P>)SDR UIEA2019072404836Seat Track · corrodedM/D LBL 98 SEAT TRACK STA 1720-1740 FOUND CORRODED AS MARKED. (<P>M/D LBL 98 SEAT TRACK AT STA 1720-1740 CORRODED AREA BLENDED OUT AREA DEPTH 0.015", WIDTH 0.7", LENGTH 10" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMIT.</P>)SDR UIEA2019072404837Access Panel · chafed#3 PYLON TORQUE BOX ACC PANEL 472GL, FOUND CHAFE MARK AS MARKED. (<P>DAMAGE REMOVED AND NDT INSPECTION CARRIED OUT WITH NO CRACK FOUND RESULT. REPAIR INSTRUCTION PER RI 54-50-13651 REV A.</P>)SDR UIEA2019072404838Seat Track · corrodedM/D LBL 98 SEAT TRACK STA 1820-1840, FOUND CORRODED AS MARKED. (<P>M/D LBL 98 SEAT TRACK AT STA 1820-1840 CORRODED AREA REMOVED AND RE-PROTECTED PER SRM 51-10-02 AND SRM 51-20-01. BLENDED AREA DEPTH 0.025", WIDTH 0.7", LENGTH 3" WITHIN SRM 53-00-52-1A-1 ALLOWASDR P5CA2019072000156Cap · open1 HOUR INTO FLIGHT "ENGINE 2 OIL SYSTEM" STATUS. 2 HOURS IN FLT FLT COMPACT ENG INDICATIONS DISPLAYED ON LOWER EICAS. ENGINE 2 READING NORMAL, OIL PRESSURE 27-30 PSI, APPROXIMATELY 7 HOURS INTO FLT ENG 2 OIL DISPLAYED OIL FILTER STATUS MESSAGE. ALL ENG 2 INDICSDR UIEA2019070504678Skin · not reportedREPAIR - DISCREPANT CONDITION ON FUSELAGE SKIN NEAR STA 636, S-40R. (<P>ACCOMPLISHED THE JOB IAW EI NO. T2019A53M-3049 REV. 2. JOB COMPLETED AND CONDITION CHECK SATISFIED. </P>)SDR UIEA2019070504679Aileron · delaminatedFOUND LT WING OTBD AILERON DELAMINATION. (<P>CUT OUT THE DELAMINATION MATERIAL AND CLEANED. MEASURED THE DAMAGED AREA (L = 2", W = 0.7", D = 4 PLIES 0), (FROM AFT EDGE .69 FROM INBD EDGE, WBL 918), BOND PLIES (L = 8", W = 5"). USED WET LAYUP WITH RESIN, CUREDSDR UIEA2019070504680Motor · failedFOUND INBD FLAP ELEC MOTOR FAIL. (<P>PERFORMED WIRING CHECK, THE RESULT WAS SATISFACTORY IAW WDM 27-51-21 REV. 21. INSTALLED NEW INBD ELECTRICAL MOTOR IAW AMM 27-51-17-000-801 REV. 29 AND 27-51-17-400-801 REV. 29, STEP 3, A TO D (3). PERFORMED INSTALLATION TESSDR UIEA2019070504681Bracket · wornL INBD ELEVATOR IDLE CRANK BRACKET ASSY AND ATTACH BOLT WORN, AND BEARING MIGRATION AT CRANK ASSY. (<P>REMOVED AND REPLACED LT INBD ELEVATOR IDLE CRANK BRACKET ASSY IAW AMM 20-51-01-912-008 REV. 29. CONDITION CHECK SATISFACTORY. </P>)SDR P5CA2019070200139Fairing · dentedLT HORIZONTAL STAB L/E FAIRING #331CL FOUND DENT. (<P>LT HORIZONTAL STAB L/E FAIRING #331CL DENT AREAS REPAIRED IAW SRM 55-10-01-2R-2 REPAIR 2.</P>)SDR P5CA2019062900137Warning System · false activationREJECTED TAKEOFF DUE TO EICAS MSG "CONFIG GEAR CTR". SECOND TAKEOFF ATTEMPT OKAY. PLEASE NOTE PREVIOUS WRITE-UPS.(<P>NO EICAS MSG AND CMC PLF/EF MSG NOTED, BUT FOUND CMC MSG 32063 FROM FAULT HISTORY. ITEM DEFERRED PER MEL 32-53-01, CAT 'C', MDDR #113933. T/I: SDR P5CA2019062190128Warning Message · illuminatedWHEN SETTING T/O THRUST, ''CONFIG GEAR CTR'' WARNING. 2 ATTEMPTS TO DEPART, SAME RESULT. CHECKED AND FOUND CMC MSG 32066.SDR UIEA2019060744384Engine · malfunctionedAT FL 320, AFTER 1 HR 25 MIN OF FLIGHT, WE HEARD A LOUD BANG. #2 ENGINE ROLLED BACK AND SHUT DOWN. AUTO START TRIED SEVERAL TIMES TO RE-LIGHT BUT IT DID NOT START. N1 21%, N2 22%, OIL PRES 9. HIGHEST EGT DURING RESTART WAS 825. DESCENDED TO FL 300 AND ACCOMPLISDR P5CA2019041600054Support · damagedLHW L/E CAVITY SUPPORT STRUT UPPER MOUNTING HOLE FOUND ELONGATE AT ILES 398, UPPER BEAM.(<P>LHW L/E CAVITY SUPPORT STRUT AT ILES 398 - 404.55 RIB FASTENER HOLES ELONGATION AREAS REPAIRED IAW RI-53-82-13469 REV. A. </P>)SDR P5CA2019041600055Support · damagedLHW L/E CAVITY SUPPORT STRUT UPPER MOUNTING HOLE FOUND ELONGATE AT ILES 440, UPPER BEAM. (<P>LHW L/E CAVITY SUPPORT STRUT AT ILES 440 - 442.84 RIB FASTENER HOLES ELONGATION AREA REPAIRED IAW RI-53-82-13469 REV. A. </P>)SDR P5CA2019041600056Spar · crackedNO.2 PYLON CAVITY REAR SPAR BOTTOM AREA WING FIXED LEADING EDGE VAPOR BARRIER CRACK AT I/B NACELLE AREA. (<P>NO.2 PYLON CAVITY REAR SPAR BOTTOM AREA WING FIXED LEADING EDGE VAPOR BARRIER CRACK AT I/B NACELLE AREA REPAIRED IAW SRM 57-41-01-2R-6 REPAIR 6, TEMPORSDR P5CA2019041600057Support Bracket · crackedAPU COMPARTMENT R/H STA 2696 CONDUIT SUPPORT BRACKET MOUNTED FRAME CRACKED.(<P>APU COMPARTMENT R/H STA 2696 WL 292, LOWER SUPPORT FRAME CRACK AREA REPAIRED IAW RI-53-82-13469 REV. A. </P>)SDR P5CA2019040500048Line · leakingGEAR TILT CAUTION MESSAGE DURING CLIMB. FOUND HYDRAULIC LINE TO LEFT BODY GEAR TILT ACTUATOR LEAKING. REMOVED AND REPLACED LINE. LEAK CHECK NORMAL I.A.W. AMM 32-13-14.<BR /></P>)SDR P5CA2019021900024Engine · making metalAFTER LEVELING OFF AT FL 320, # 2 ENGINE OIL PRESSURE WENT TO ZERO. SHUT DOWN ENGINE. NO N1 AFTER FIVE MINUTES.(<P>REMOVED # 2 ENGINE DMS AND FOUND MULTIPLE METAL CHIPS (LP: 719032, ITEM: 1). CARRIED OUT INSPECTIONS OF #2 ENGINE DMS OIL FILTER, A, B, C SUMP, SDR UIEA2019012202994Fitting · chafedRT WING I/B FLAP O/B ROLLER GUIDE FITTING FOUND CHAFFING MARK.(<P>RHW FIXED T/E WBL 448.7 DEFLECTION TRACK CHAFING AREAS REPAIRED IAW RI-57-20-13351 REV.B</P>)SDR UIEA2019012202995Fitting · chafedLT WING I/B FLAP O/B ROLLER GUIDE FITTING FOUND CHAFING MARK.(<P>LHW FIXED T/E WBL 448.7 DEFLECTION TRACK CHAFING AREAS REPAIRED IAW RI-57-20-13351 REV.B.</P>)SDR UIEA2019011602965Rib · not reportedLT HORIZONTAL STABILIZER RIB TIME LIMITED REPAIR CONVERSION REPAIR(<P>LT HORIZONTAL STABILIZER CLOSURE RIB REPAIRED IAW RI-55-10-13346 REV.A<BR /></P>)SDR UIEA2019011502961Lug · crackedNR 3 PYLON I/B NACELLE COVER VAPOR BARRIER O/B LUG FOUND CRACKED(<P>NR 3 PYLON I/B NACELLE COVER VAPOR BARRIER O/B LUG REPAIRED IAW RI-57-41-13342 REV.A</P>)SDR UIEA2019011602963Channel · crackedLT HORIZONTAL STABILIZER T/E BOND ASSY CHANNEL CRACK.(<P>LT HORIZONTAL STABILIZER T/E BOND ASSY. CHANNEL REPAIRED IAW RI-55-10-13343 REV.A<BR /></P>)SDR UIEA2018121982872Control Unit · malfunctionedNUMEROUS ELECTRICAL MALFUNCTIONS REQUIRING AIR TURN BACK.(<P>REMOVED AND REPLACED #1 BCU IAW AMM 24-*23-01. OPS CHECK NORMAL IAW AMM 24-23-01</P>)SDR UIEA201811302739Door · damagedON ARRIVAL FOUND LEFT HAND BODY GEAR DOOR DAMAGED AT TWO AREAS 3.5 X 3.5 AND 3.5 X 4.5 (<P>PERFORMED TEMP REPAIR REF EO 4852A050. </P>)SDR P5CA2018091400256Relay · faultyREJECTED T/O AT LOW SPEED DUE TO "CONFIG PARK BRAKE" T/O WARNING. SHOWED CMC NO REPORTED FOUND AND CHECKED PARKING BRAKE STS THEN FOUND PARKING BRAKE VLV NOT MOVE AND R&R PARKING BRAKE VLV CLOSE RELAY ( R7514) PER FIM 32-04-00-810-802 AND SYS TEST NORMAL PER ASDR P5CA2018091100261Support Fitting · crackedLT WING T/E FLAP NR 2 AFT FAIRING AFT SUPPORT FRAME FOUND CRACKED. SUPPORT FRAME CRACKED AREA REPAIRED AS PER RI-57-50-12969.SDR P5CA2018091100262Retainer · crackedFX LT BS 1241 CANED PRESSURE BULKHEAD MOST O/B FIXED FAIRING SEAL RETAINER FOUND CRACK. FX LT BS 1241 FIXED FAIRING SEAL RETAINER PN 149U7255-31 REPAIRED IAW RI NO RI-57-00-13013 REV A. THIS REPAIR IS A PERMANENT REPAIR.SDR P5CA2018091100263Vapor Barrier · crackedRT WING L/E I/B NACELLE COVER (NR 3 PYLON) VAPOUR BARRIER FOUND CRACK ON O/B TAG. RT WING L/E I/B NACELLE COVER (NR 3 PYLON) VAPOUR BARRIER O/B TAG CRACK AREA REPAIRED AS PER RI-57-00-12982.SDR P5CA2018091100267Vapor Barrier · crackedLT WING L/E I/B NACELLE COVER (NR 2 PYLON) VAPOR BARRIER FOUND CRACK ON O/B TAG. LT WING L/E I/B NACELLE COVER (NR 2 PYLON) VAPOR BARRIER ON O/B TAG CRACKED AREA REPAIRED AS PER RI-57-00-12982.SDR P5CA2018091100278Support Frame · crackedLT WING T/E FLAP NR 3 AFT FAIRING FWD SUPPORT FRAME FOUND CRACKED. LT WING T/E FLAP NR 3 AFT FAIRING FWD SUPPORT FRAME CRACKED AREA REPAIRED AS PER RI 57-50-12970.SDR P5CA2018091100279Floor Panel · damagedM/D BS 1560-1680 LBL 98-115 FLOOR PANEL FOUND SPONGY. FLOOR PANEL WAS REPAIRED AS PER RI 53-00-12965 REV A.SDR P5CA2018082700214Vapor Barrier · crackedRIGHT WING LE, INBD NR 3 NACELLE COVER, VAPOR BARRIER WAS FOUND CRACKED ON THE OTBD TAG. THE VAPOR BARRIER OTBD TAG WAS REPAIRED IAW RI-57-00-12982.SDR UIEA2018070601356Actuator · faultyDURING INITIAL CRUISE AT FL37.0 GOT DOOR NOSE CARGO CAUTION MSG. FOLLOWED ELECTRONIC CHECKLIST, DESCENDED TO 8000', DURING DESCENT EICAS MSG WENT AWAY. DIVERT TO MIA. INITIAL EVALUATION FOUND INTERMITTENT CMC MSG 52044 AND 52052. FOLLOWED IFIM 52-31-00, REMOVESDR P5CA2018061500091Warning Message · false activationCABIN ALTITUDE EICAS DURING CRUISE, NO EICAS MESSAGE FOUND. STS MESSAGE, & CMC MESSAGE AFT ARR SPOT. BOTH OUTFLOW VALVE TESTED OKAY. ALL DOOR & OUTLETS OK, BOTH CPCS GND TEST PASSED AIW AMM 21-31-00/501. DOOR & SEAL INSPECTED OF ALL REVR AND OUTFLOW IAW SDR P5CA201806050084Support Beam · crackedRIGHT WING FIXED LEADING EDGE AT ILES 434.51, THE LOWER SUPPORT BEAM WAS CRACKED. REPAIRED IAW RI-57-41-12740, REV A.SDR P5CA201806050083Rib · crackedRIGHT WING, ILES 440, LEADING EDGE RIB WAS FOUND CRACKED. REPAIRED IAW RI-57-41-12740, REV A. INTERIM REPAIR.SDR P5CA201806050085Support · crackedNR 3 PYLON CAVITY VAPOUR BARRIER, OTBD FWD SUPPORT CRACKED. REPAIRED IAW RI-57-41-12749, REV A. INTERIM REPAIR.SDR P5CA201805060086Structure · damagedWHILE ACCOMPLISHED EO 4853A024 PART 1, STEP 4 FOUND A FASTENER HOLE OVERSIZED BS 2484 - 2486, REPAIRED IAW RI-53-00-12745, REV A.SDR P5CA2018060510087Brace · brokenRIGHT WING ILES 440, LEADING EDGE BRACE WAS BROKEN. FABRICATED AND REPLACED IAW RI-57-41-12740, REV A. INTERIM REPAIR.SDR UIEA2018050100818Door · crackedLEFT BODY LANDING GEAR INBD STRUT DOOR, AFT EDGE FOUND CRACKED. REPAIRED IAW RI-52-80-12655, REV A.SDR UIEA2018050100819Frame · crackedRIGHT WING INBD T/E FLAP NR 6 AFT FAIRING, FWD FRAME ASSY WAS FOUND CRACKED THROUGH THE THICKNESS OF FWD FRAME ALONG THE OTBD BEARING FITTING AREAS. REPAIRED IAW RI-57-50-12656, REV A.
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