N608UP

Service difficulty reports · 54

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N608UP' AND registry_match = 'registration'
  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 IPXA2025092490974Elevator · not reportedELEVATOR EO-85445-JIC1 STEP 137.Sep 23, 2025 · N608UP · Boeing 7478F · Elevator StructureSDR IPXA2025091911559Floor Panel · dentedMAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DENTED, PANEL 252XF. REPAIRED MAIN DECK FLOOR PANEL NEAR BS 1700, BETWEEN RBL 11.33 & 33.99 IAW EGAT EI F2025A53M-2137, REV1 AND EO-95356-REQ 1, REV1. CONDITION CHECK IS SATISFACTORY.Sep 18, 2025 · N608UP · Boeing 7478F · Fuselage Floor PanelSDR IPXA2025091882471Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2360 S-7R ( LEVEL 2 ) (REPAIR). PERFORM REPAIR PER 747-8F SRM 53-60-03-2R-8 REPAIR 8, TR 53-157. PERFORM EO-95136-REQ1 REV.1 AND EI NO.F2025A53M-2068 REV.0 AND EGAT WORK SHEET 50701.Sep 9, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025091882477Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2360 S-10L. (REPAIR). REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS. PERFORM EO-95258-REQ1 REV.1 AND EI NO. F2025A53M-2155 REV.0 AND EGAT WORK SHEET NO.50702.Sep 9, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092367607Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-18L ACCOMPLISHED REPAIR I.A.W UPS EO-95209-REQ1 REV.1 AND EGAT EI NO NO.F2025A53M-2185 REV.0 AND SRM 53-60-03-2R-3 REV.46/TR:53-154 AND EGAT WORK SHEET NO.50700.Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092267597Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-17L PERFORM EO-95208-REQ1 REV.1 AND EI NO.F2025A53M-2194 AND EGAT WORK SHEET NO. 50699. VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS.Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Structure (General)SDR IPXA2025091867493Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 1960 S-11R (LEVEL1) (REPAIR).PERFORMED SRM 53-60-03-2R-4 REV.46/TR:53-155 AND EGAT WORK SHEET NO.50697 STEPS 1-43.PERFORMED EO-95137-REQ1 REV.1 AND EI NO.F2025A53M-2072 REV.0 AND EGAT WORK SHEET NO.50697Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092567592Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-16L. ACCOMPLISHED REPAIR I.A.W UPS EO-95206-REQ1 REV.1 AND EGAT EI NO NO.F2025A53M-2015 REV.2. VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15.Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092567578Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-15L. PERFORM EO-95204-REQ1 REV.1 AND EI NO.F2025A53M-2012 REV.2. VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS.Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092467530Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2180 S-13R. PERFORM EO-95204-REQ1 REV.1 AND EI NO.F2025A53M-2025 REV.1. VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092367676Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2360 S-11L REPAIRED I.A.W SWPM 20-10-11 , 20-10-12 REV.89 INSTALLED WIRE BUNDLE SUPPORT CLAMPS AT MAIN DECK STA 2350 BETWEEN S-9L TO S-13L AND CONDITION CHECK NORMAL. PERFORM EO-95193-REQ1 REV.1 AND EI NO.F2025A53M-2048 REV.1.Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092167607Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 2180 S-18L (LEVEL1) (REPAIR) INSPECTION COMPLETED FOR EGAT WORK SHEET NO.50700 STEP 30 - RESPECTIVELY PART MARK THE REPAIR PARTS. RII COMPLETED FOR EGAT WORK SHEET NO.50700 STEP 31.Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092267448Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-21L (LEVEL1) (REPAIR). FABRICATED REPAIR SPLICE I.A.W. EGAT WORK SHEET NO. 50694 STEP 14 (SRM 53-60-03-2R-12 REV.46/TR:53-160)PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION I.A.W. EGAT WORK SHEET NO.:50Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092267623Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-20L (LEVEL1) (REPAIR).FABRICATED REPAIR SPLICE I.A.W. EGAT WORK SHEET NO. 50695 STEP 14 (SRM 53-60-03-2R-12 REV.46/TR:53-160).PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION I.A.W. EGAT WORK SHEET NO.:50Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092267652Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 2180 S-22L (LEVEL1) (REPAIR)FABRICATED REPAIR SPLICE I.A.W. EGAT WORK SHEET NO. 50696 STEP 14 (SRM 53-60-03-2R-12 REV.46/TR:53-160).PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION I.A.W. EGAT WORK SHEET NO.:506Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092267421Stringer · crackedSTRINGER CRACK, FWD AND AFT SIDE OF STA 1960 S-10R (LEVEL1) (REPAIR). PERFORMED SRM 53-60-03-2R-4 REV.46/TR:53-155 AND EGAT WORK SHEET NO.50698 STEPS 1-43. PERFORMED EO-95172-REQ1 REV.1 & EI NO.F2025A53M-2097 REV.0 AND EGAT WORK SHEET NO.50698.Sep 8, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092254119Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 1960 S-40L (LEVEL1) (REPAIR). IAW EGAT WORK SHEET 50688 STEP:11-21, SRM 53-60-03-2R-9, REV 46, TR 53-150. PERFORMED EO-95191-REQ 1 REV.1 AND EI F2025A53M-2128 REV.0 AND EGAT WORK SHEET 50688.Sep 7, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092254156Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 1960 S-42L (LEVEL1) (REPAIR) RII COMPLETED FOR EGAT WORK SHEET NO.50693 STEP 20. PERFORMED EO-95192-REQ1 REV.1 AND EI NO.F2025A53M-2143 REV.0 AND EGAT WORK SHEET NO.50693Sep 7, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092254125Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 1960 S-38L (LEVEL1) (REPAIR) RII COMPLETED FOR EGAT WORK SHEET NO.50692 STEP 20. PERFORMED EO-95188-REQ1 REV.1 AND EI NO.F2025A53M-2140 REV.0 AND EGAT WORK SHEET NO.50692Sep 7, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092254168Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 1960 S-38L (LEVEL1) (REPAIR). PERFORMED SRM 53-60-03-2R-9 REV.46 / TR: 53-150 AND EGAT WORK SHEET NO.50691 STEPS 1-20.PERFORMED EO-95188-REQ1 REV.1 AND EI NO. F2025A53M-2140 REV.0 AND EGAT WORK SHEET NR 50691.Sep 7, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092254147Stringer · crackedSTRINGER CRACKED, AFT SIDE OF BS 1960 S39L (LEVEL1) (REPAIR). IAW EGAT WORK SHEET 50689, STEPS 11-21, SRM:53-60-03-2R-9, REV 46, TR 53-150. PERFORM EO-95190-REQ 1, REV 1, & EI F2025A53M-2127, REV 0, & EGAT WORK SHEET 50689.Sep 7, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092255048Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 1960 S-42L (LEVEL1) (REPAIR).PERFORMED SRM 53-60-03-2R-9 REV.46 / TR: 53-150 AND EGAT WORK SHEET NO.50690 STEPS 1-20.PERFORMED EO-95192-REQ1 REV.1 AND EI NO.F2025A53M-2143 REV.0 AND EGAT WORK SHEET NR 50690.Sep 7, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092541438Stringer · crackedMAJOR REPAIR, STRINGER CRACKED, AFT SIDE OF BS 740, S42L. PERFORM EO-95167-REQ1, REV 1 AND EI F2025A53M-2129 REV 0, AND EGAT WORK SHEET 50687.Sep 6, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092241519Stringer · crackedMAJOR REPAIR - STRINGER CRACKED, FWD SIDE OF BS 740, S39L. PERFORMED EO-95267-REQ 1, REV 1 & EI F2025A53M-2009, REV 2.Sep 6, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092141490Stringer · crackedSTRINGER CRACKED, FWD & AFT SIDE OF BS 740, S47L. PERFORMED SRM 53-20-03-2R-5 REV.46, TR 53-161, & EGAT WORK SHEET 50685, STEPS 1-21. PERFORMED EO-95169-REQ 1, REV 1, & EU F2025A53M-2105, REV 0 & EGAT WORK SHEET 50685.Sep 6, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025091541450Stringer · crackedMAJOR REPAIR - STRINGER CRACKED, FWD AND AFT SIDE OF BS 740, S43L. PERFORMED EO-95168-REQ 1, REV 1, & EI F2025A53M-2184, REV 1, & EGAT WORK SHEET 50686.Sep 6, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025091541511Stringer · crackedMAJOR REPAIR - STRINGER CRACKED, FWD AND AFT SIDE OF BS 740, S47R. PERFORMED EO-95170-REQ 1, REV 1, EI F2025A53M-2217, REV 0 & EGAT WORK SHEET 50684.Sep 6, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092725310Stringer · crackedSTRINGER CRACK, AFT SIDE OF STA 2360, STA 2377 AT S-6L (LEVEL 2) (REPAIR).REMOVED UPPER CORNER BRACKET FROM LOWER FUSELAGE, WING/BODY FAIRING 194CR IAW B757-200PF SRM 51-40-02-0G-0.FABRICATED UPPER CORNER BRACKET R/H FROM P/N: SHT-7075T6-0.063/12 BATCH: 000323Sep 5, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092625040Stringer · crackedSTRINGER CRACKED, FWD SIDE OF BS 2598 S5L LEVEL 2. PERFORM EO-95354-REQ1 REV.1 AND EI F2025A53M-2043 REV 1.Sep 5, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025091824996Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2598 S-7R LEVEL 2. ACCOMPLISHED REPAIR IAW EO-95138-REQ1 REV.1 AND EGAT EI F2025A53M-2075 REV.0 AND SRM 53-80-03-2R-2 REV.46 / TR53-152 AND EGAT WORK SHEET NR.50683.Sep 5, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092525306Stringer · crackedSTRINGER CRACKED, AFT SIDE OF BS 2360, BS 2377 AT S5R (LEVEL 2) PERFORM EO-95265-REQ1 REV.1 AND EI F2025A53M-2037 REV 2.Sep 5, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025092525301Stringer · crackedSTRINGER CRACK, AFT SIDE OF BS 2360, BS 2377 TO BS 2380 AT S-5L (LEVEL 2). PERFORM EO-95266-REQ1 REV 1 AND EI F2025A53M-2035 REV 2.Sep 5, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025091824925Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2598 S-8L LEVEL 2. (REPAIR). VERIFY REPAIR IS ACCOMPLISHED PER GMM 04.02.01.15 REQUIREMENTS. PAPER FINAL COMPLETED. ACCOMPLISHED REPAIR I.A.W UPS EO-95140-REQ1 REV.1 AND EGAT EI NO.F2025A53M-2076 REV.0 AND SRM 53-80-03-2R-2 REV.Sep 5, 2025 · N608UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2025050105177Skin · damagedDURING OK TO INSTALL OF RH INBD ELEVATOR, FOUND THAT THE RH OTBD ELEVATOR HAS MULTIPLE CRACKS, SMOKING RIVETS, AND MISSING RIVETS. REF; GMM 04-02 ATA 27. VERIFIED AL REQUIREMENTS FOR THE PROPER INSTALLATION OF THE RIGHT OUTBOARD ELEVATOR. MAINTENANCE PART NUMApr 29, 2025 · N608UP · Boeing 7478F · Elevator, Plate/SkinSDR IPXA2025012863945Warning Horn · inoperativeUPON CREW PERFORMING FIRE TEST FOR PRE-DEPARTURE CHECK, APU FIRE WARNING HORN CIRCUIT BREAKER POP OUT. FIRE WAS SHOWING PASS. ALL COCKPIT AURAL WARNING AND INDICATION NORMAL DURING TEST. REMOVED AND REPLACED APU FIRE SHUTDOWN MODULE M869, TESTS ARE GOOD, REF AJan 24, 2025 · N608UP · Boeing 7478F · Fire DetectionSDR IPXA2025012463945Warning Horn · false activationUPON CREW PERFORMING FIRE TEST FOR PRE-DEPARTURE CHECK, APU FIRE WARNING HORN CIRCUIT BREAKER POP OUT. FIRE WAS SHOWING PASS. ALL COCKPIT AURAL WARNING AND INDICATION NORMAL DURING TEST. IAW GMM 03.05.01.03 DEFERRED FAULTS-ADDITIONAL ACTION WDM 49-61-21-1 CB CJan 24, 2025 · N608UP · Boeing 7478F · Fire DetectionSDR IPXA2024060369180Light · handler errorAIRCRAFT EMERGENCY LIGHTS WERE DISCOVERED ON FROM REAR PANEL WHEN CREW BOARDED THE BATTERY CHARGING CONTROL CIRCUIT FOR THE EMERGENCY LIGHTS PROVIDES A TRICKLE CHARGE TO THE BATTERIES AS LONG AS POWER IS AVAILABLE TO THE AIRCRAFT PER SDS AMM PART I 33-51-00-02Jun 3, 2024 · N608UP · Boeing 7478F · Standard Practices/StructuresSDR IPXA2024042998391Seat · odorCAPTAIN SEAT WHEN ADJUSTING THE SEAT FWD VIA THE FWD/AFT SWITCH FLIGHTCREW HEARD A POP AND SAW AN ELECTRICAL FLASH. CREW THEN SMELLED AN ELECTRICAL ODOR SEAT TRACK OF CAPTAIN SEAT CLEANED AND OPS TEST OF SEAT CARRIED OUT I.A.W. AMM 25-11-00-710-801 REV. 44 SEVApr 26, 2024 · N608UP · Boeing 7478F · Flight Compartment EquipmentSDR IPXA2025022646527Skin · dentedDURING WALK AROUND FOUND LARGE DENT ON RIGHT LEADING EDGE HORIZONTAL STAB. ACCOMPLISHED PERMANENT REPAIR PER EO 89543 REQ 3. RE-INSTALLED ORIGINAL HORIZONTAL STABILIZER LEADING EDGE WITH REF TO AMM 55-10-01-404-007 UP TO AND INCLUDING STEPS F(9) AS REQUIRED. CFeb 19, 2024 · N608UP · Boeing 7478F · Horizontal Stabilizer, Plate/SkinSDR IPXA2024021946527Skin · dentedDURING WALK AROUND FOUND LARGE DENT ON RIGHT LEADING EDGE HORIZONTAL STAB. C/W EO -89543-REQ1. OPENFeb 19, 2024 · N608UP · Boeing 7478F · Horizontal Stabilizer, Plate/SkinSDR IPXA2023100427867Wedge · crackedTRAILING EDGE WEDGE PANEL, SUPPORT CHANNEL CRACK REMOVED TRAILING EDGE WEDGE PANEL AND ROUTED TO S/M SHOP FOR REPAIR. REF SRM 51-40-02. ALL WORK WAS ACCOMPLISHED ON EO-88328-PRELIM1. WITH NO CHANGESSep 30, 2023 · N608UP · Boeing 7478F · Wing StructureSDR IPXA2023100427592Rib · crackedEND RIB UPPER CHORD CRACK ON T/E TO FIRST FASTENER HOLE FWD INSTALLED NEW T-CHORD AS PER SRM 51-40-02.Sep 30, 2023 · N608UP · Boeing 7478F · Standard Practices/StructuresSDR IPXA2023032284575Fuel · out of balance€ŒFUEL IMBAL 2-3€? MSG NO EICAS MSG AFTER ARRIVAL. CHKED CMC EXISTING & PRESENT FAULTS, FOUND MX MSG # 28798 (INTERMITTENT), NO ANY CORRELATED MSGS NOTED. FOLLOW FIM 28-22-00-810-851 & FIM 28-20-00-810-864, ACCOMPLISHED SYS TEST ON THE P42 & FUEL QTY TEST PEMar 19, 2023 · N608UP · Boeing 7478F · Fuel Boost PumpSDR IPXA2023041177371Unknown · crackedL/H HORIZ STAB UPPER CHORD CRACKED AT AFT END ACCOMPLISHED R/R OF CHORD AS PER SRM 51-40-02Jan 1, 2023 · N608UP · Boeing 7478F · Standard Practices/StructuresSDR IPXA2022030479711None · indicationINSPECTION TYPE:NAL1 ENTRY DOOR INDICATED NOT CLOSED WHEN ATTEMPTING TO CLOSE ITREPLACED ENTRY DOOR LOWER CONTROL ROD PER CMM 52-11-21. OPS TEST GOOD OF L1 ENTRY DOOR INDICATION. OK FOR SERVICE. SEE ITEM #3 FOR DETAILSMar 4, 2022 · N608UP · Boeing 7478F · Passenger/Crew DoorsSDR IPXA2022010477508None · noneINSPECTION TYPE:N/ASAFETY WIRE ON EMERG LIGHTS SW IS BENTRE ALLIGNED RETAINER SPRING OPS CHECK PER AMM 33-51-00-715.Jan 4, 2022 · N608UP · Boeing 7478F · Emergency LightingSDR IPXA2021120176533None · noneINSPECTION TYPE:N/A"SMOKE/OVRD VLV" STATUS MSG. ILLUMINATED APPROX FL210 DURING DESCENT.MX MSG 21405 EQUIMENT COOLING CMC TEST C/W - PASS PER FIM 21-50-00-810-824Nov 29, 2021 · N608UP · Boeing 7478F · Air Distribution SystemSDR IPXA2021110975815None · noneINSPECTION TYPE:N/ADURING CRUISE FLIGHT AT FL320 THE STATUS MESSAGE "CARGO DET AFT 22" ILLUMINATEDACCOMPLISHED 747-8 FIM TASK 31-98-00-810-801 FOR FAULT CODE 261 263 22. NO ACTIVE FAULTS OR IND. A/C OK FOR SERVICE.Nov 9, 2021 · N608UP · Boeing 7478F · Smoke DetectionSDR IPXA2021110475591Panel · noneINSPECTION TYPE:C2CRACK AND DISBOND DAMAGE(DAMAGE AREA SIZE:APPROX. 6.0" X 1.2") WAS FOUND ON OUTBD EDGE OF BONDED ASSY (P/N:113U4300-11) OF NO.5 SPOILER.REPAIR I.A.W. 747-8F SRM 57-70-01 REPAIR 1 REV 35.00, 747-8F SRM 51-70-04 REPAIR 5 REV.35.00, AND 747-8F SOct 25, 2021 · N608UP · Boeing 7478F · Wing StructureSDR IPXA2020032353435Floor Panel · puncturedINSPECTION TYPE:N/AMAIN DECK FLOOR PANEL PUNCTURE REPAIR STA 560 LBL 16REPAIRED PER SRM 53-00-50-2R-2 REPAIR 2Mar 22, 2020 · N608UP · Boeing 7478F · Fuselage Floor Panel
Back to N608UP