Service difficulty reports

1,771,154 reports of malfunctions and defects, newest first. Air carriers must report; 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'
  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 R61A2026080200214Skin · damagedLIGHTNING STRIKE FWD FUSELAGE BETWEEN FRAMES 3-4 STRINGERS 22R-24R.MECHANIC CUT OUT LIGHTNING STRIKE DAMAGE,FABRICATED, DRILLED AND INSTALLED PERMANENT REINFORCING REPAIR AT FWD FUSELAGE BETWEEN FRAMES 3-4 AND STRINGERS 22R-24R IAW ETD2026-170-012124Jul 9, 2026 · N865RW · Emb ERJ170100SE · Fuselage Main, Plate/SkinSDR IPXA2026073173712Hinge · brokenFOUND RT WING NR 24 V.C FLAP INBD SIDE FOLDING NOSE HINGE BROKEN. OK TO INSTALL, CONDITION CHECK SATISFIED. IAW AMM 27-81-02-404-010 REV.117 ASSEMBLY RT WING NR 24 V.C FLAP INBD SIDE FOLDING NOSE & INBD SIDE HINGE. CONDITION CHECK NORMAL.Jul 9, 2026 · N583UP · Boeing 7474R7F · Leading Edge DevicesSDR AALA202607310825Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: RIGHT AFT WET AREA FLOOR SUPPORT AT STATION 947+1", RBL 50-RBL 53 HAS GALVANIC CORROSION (AFT SIDE OF OUTBOARD AFT LAV MOUNT). MAINTENANCE INSTALLED AT STATION 947+1", RBL 50-RBL 53 REPLACEMENT INERCOSTAL PER SRM 53-70-51-2R-5.Jul 9, 2026 · N957NN · Boeing 737823 · Fuselage Main, Floor BeamSDR SCNA20260730333Beam · crackedDURING THE HFEC FASTENER HOLE PERFORMED AT RT WING SLAT NR 7 PER NRI 6-6, FOUND CRACK IN THE NOSE BEAM AT OPEN HOLE ADJACENT TO THE ACTUACTOR RIB. PERFORMED REPAIR RT WING SLAT NR 7 NOSE BEAM SECTION FROM SS290.250" TO SS343.750" DUE TO CRACK IAW BCF SRM 57-Jul 9, 2026 · N5237A · Boeing 737800* · Leading Edge DevicesSDR IPXA2026072885432Angle · crackedMAIN DECK CARGO, BRACKET HAS A CRACK AT FRAME 79 AND Y1580.5 (DOT 64-086). INSTALLED NEW ANGLE AT MAIN DECK CARGO, FRAME 79 AND Y1580.5 IAW A300-600 SRM 51-40-21-001. REVIEWEDJul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR AALA202607290797Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CREASE ANGLE HAS EXFOLIATION CORROSION AT STA 986.5 TO STA 996, LBL 46. MAINTENANCE REPLACED CREASE ANGLE AT STA 986.5 TO STA 996, LBL 46. PER AARD 51-00-05-1 AND BOEING DRAWING 147A8510Jul 9, 2026 · N957NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR IPXA2026072986100Floor Panel · brokenMAJOR REPAIR, MAIN CABIN FLOOR STRUCTURE, FLOOR PANEL 262JM CORNER IS BROKEN. VERIFIED FABRICATION OF FLOOR PANEL 262JM IAW SREO-16407-REQ001 (APPX B) . MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATIONJul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026072986403Floor Panel · brokenMAJOR REPAIR, MDC, FLOOR PANEL 251XJ BROKEN. FLOOR PANEL 251XJ FABRICATION IS COMPLETED IAW SREO-16407-REQ001 ((APPX B). MAIN DECK CARGO FLOOR PANEL FABRICATION.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Floor PanelSDR AALA202607285545Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: LEFT AFT WET AREA. FLOORBEAM BS 947 LBL49-LBL23-LBL27 HAS EXFOLIATION CORROSION AT AND UNDER IB AFT LAV MOUNT. MAINTENANCE COMPLETED INSTALLATION OF NEW T CHORD AT STA.947, RBL 8 TO LBL 59 IAW SRM 53-70-51-2R-5.Jul 9, 2026 · N957NN · Boeing 737823 · Fuselage Main, Floor BeamSDR IPXA2026072486375Seat Track · corrodedMDC, FR 62, Y953, SEAT TRACK CORRODED. VERIFIED AS RII ITEM IAW GMM 04-02, MAJOR REPAIR, A NEW SEAT TRACK SECTION AT MDC, FR 62, Y953 WAS INSTALLED IAW SRM 53-10-16-201, PARAGRAPH 4 FIGURE 201. SURFACE PROTECTION RESTORED AFTER INSTALLATION.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026072585472Support Angle · crackedRIGHT PYLON, SUPPORT ANGLE HAD A CRACK AT INBD SIDE, LOWER FWD CORNER OF RIB 18. INSTALLED SUPPORT ANGLE AT INBD SIDE, LOWER FWD CORNER OF RIB 18 IAW SRM 51-40-21-001.Jul 9, 2026 · N136UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR SWAA2026072402698Skin · delaminatedRIGHT OTBD AFT FLAP WAS DELAMINATED AT INBD END LWR SURFACE. REPLACED THE RT OTBD AFT FLAP WITH NEW.Jul 9, 2026 · N8559Q · Boeing 7378H4 · Trailing Edge FlapsSDR IPXA2026072386482Adapter · corrodedFR 34, BTW Y1959 AND Y2462, CLS ADAPTER BASE WITH CORROSION. DOT 73-121 VERIFIED STEP 11 INSTALLED NEW CLS ADAPTER ON MDC AT FR34 BTW Y1959 AND Y2462 IAW SRM 51-40-21 AND REMOVED PROTECTION ELECTRICAL (EWIS) IAW ESPM 20-54-50-02Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR AALA202607227383Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: FILFORM CORROSION ON INTERCOSTAL AT STA 947, LBL 52. MAINTENANCE REPLACED INTERCOSTAL AT STA 947, LBL 562 IAW AARD 51-00-01-5 AND SRM 51-40-02.Jul 9, 2026 · N902AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR IPXA2026072185558Profile · crackedMAIN DECK CARGO, Z PROFILE HAS A CRACK BETWEEN FR74 & 75 UNDERNEATH RH AIR GRILL (DOT 64-091) Z PROFILE INSTALLED ON MAIN CABIN FR74 AND FR75 R/H SIDE. IAW A300-600 SRM 51-40-21-001.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR CALA2026072117936Skin · crackedAFTER EVALUATION REQUIRE ACCESS TO FOM REPAIR ON LH HORIZONTAL STAB STA 101.9 IN-SPAR RIB 1, STIFFENER AND NR 2 STIFFENER. PERFORMED PERMANENT REPAIR AT LT HORIZONTAL STAB LOWER SKIN AT STA 101.9 IN SPAR RIB 1, STIFFENER, AND NR 2 STIFFENER. THIS REPAIR IS A Jul 9, 2026 · N38257 · Boeing 737824 · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026071885468Profile · crackedMAIN DECK CARGO, Z PROFILE HAS A CRACK AT Y2127.5, BETWEEN FR73 & 74. VERIFIED REMOVAL OF EWIS PROTECTION AT MAIN DECK CABIN FR73 AND FR74. IAW ESPM UPS D4-UPS-A300 20-54-50-02. Z PROFILE INSTALLED AT FR73 AND FR74. IAW SRM 51-40-21-001.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026071685417Profile · crackedMAIN DECK CARGO, ZEE PROFILE HAS A CRACK AT FR 80 - 82 BETWEEN Y1221.2 & Y1580.5. MAIN DECK CARGO, FR 80 - 82 BETWEEN Y1221.2 & Y1580.5. INSTALLED ZEE PROFILE, USING SOLID RIVETS IAW SRM 51-40-21-001.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026071685562Shear Web · crackedMAIN DECK CARGO, WEB HAS A CRACK BETWEEN FR76 & 77 BEHIND RT AIR GRILL (DADO PANEL). INSTALLED SHEAR WEB IAW A300-600 SRM 51-40-21-001Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026071685692Profile · crackedMAIN DECK CARGO, Z PROFILE HAS A CRACK AT FR80/82 BETWEEN -Y1580.5 & -Y 1221.2. MAIN DECK CARGO, FR80/82 BETWEEN -Y1580.5 & -Y 1221.2 INSTALLED Z PROFILE, USING SOLID RIVETS IAW SRM 51-40-21-001.Jul 9, 2026 · N144UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR ASAA2026070967332Skin · crackedCRACK INDICATION FOUND: R/H HORZ. STAB. LOWER SKIN SURFACE, STA. 147.90 I/B OF I/B ROW OF FASTENERS, MARKED 1"L, 8" FWD OF AFT SPAR. GROUNDED - YES. REPAIRED THE R/H HORIZ STAB LOWER SKIN AT STA 147.90 USING MAT .100 2024T3 AND .063 2024T3 PER B737-800 SRM 55-Jul 9, 2026 · N579AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR DALA2026071604179Switch · no discrepancyL1 DOOR ARMED LIGHT FA PANEL INOPERATIVE. ADJUSTED PUSH BUTTON LIGHT CARRIER SATIS SYS WORKS PROPERLY. (LP 9127916 - AIRCRAFT WAS GROUNDED)Jul 9, 2026 · N178DZ · Boeing 767332 · Door Warning SystemSDR YENA2026071500578Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION EXTERNAL SKIN ON CUTOUT OF ACCESS PANEL 351AL LOWER FUSELAGE. (RESOLVED ON W/O: 1494820 TASKCARD: NR-00001 ) REF AEM WO 2026 303/1 NR 2026-348233. ACCP REPAIR CORROSION AND CRACKS ON TAIL CONE EXTERNAL SKIN BETWEEN FR81-8Jul 9, 2026 · N809JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2026071500577Tail Cone · crackedDURING HEAVY MAINTENANCE, FUSELAGE TAIL CONE, FR 81-84 & STR 15 CORRODED & CRACKED. PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Jul 9, 2026 · N809JB · Airbus A320232 · Aerodynamic FairingsSDR YENA2026071500576Door Frame · crackedDURING HEAVY MAINTENACE, AFT FUSELAGE, FR 68 R1 DOOR STOP FITTING, LOWER INBD HOLE CRACKED, PERMANENT REPAIR EC A26-496-01 (CONSIDERED A MAJOR REPAIR)Jul 9, 2026 · N809JB · Airbus A320232 · Fuselage Main, StructureSDR CALA2026071517792Bulb · inoperativeLEVEL B, CHRONIC FOR EMERGENCY LIGHTS/ EXIT ROW LIGHTS ABOVE 21DEF NOT WORKING. R & R TWO BULBS IN FLOOR PROXIMITY LIGHT AT SEAT 20ABC. PREFORMED OPS TEST OF EMERGENCY LIGHTS AND OPS CHECK OK IAW AMM 33-51-00.Jul 9, 2026 · N87512 · Boeing 737824 · Emergency LightingSDR CALA2026071517790Fan · faultedSTRONG ELEC BURNING ODOR, FOLLOWED BY LT RECIRC FAN CAS MESSAGE ODOR, ODOR DISAPATED WITH FAN OFF. DEBRIEF WITH CREW, NO SMOKE JUST ODOR WHEN EICAS MESSAGE CAME ON AND LT RECIRC FAN OFF ,ODOR THEN DISSIPATED NO EVIDENCE OR SMOKE OR ODOR DURING THE REST OF TJul 9, 2026 · N671UA · Boeing 767322 · Air Distribution FanSDR DALA2026071504155Brake · draggingAFTER LANDING WITH MINOR BRAKING, NR 1 BRAKE HEATED TO 520 WHILE ALL OTHER BRAKES REMAINED NORMAL (GREEN). 200 DEGREES DIFFERENCE NR 1 & NR 2. FOUND NR 1 BRAKE DRAGGING. REPLACED NR 1 BRAKE IAW AMM 32 -42. (LP: 9205971, AIRCRAFT WAS GROUNDED).Jul 9, 2026 · N373NW · Airbus A320212 · Landing Gear Brake SystemSDR SWIA2026071476649Backboard · crackedFORWARD PAX DOOR EVACUATION SLIDE COMPOSITE BACK BOARD CRACKED AROUND UPPER MOUNTING FASTENER (C-CHECK RO 07/13/2026)REMOVED AND REPLACED FWD PAX DOOR EMERGENCY EVACUATION SLIDE REF EMB 175 AMM 25-65-01 TORQUE WRENCH 693 CAL 6-15-27Jul 9, 2026 · N405SY · Emb ERJ170200LR · Escape SlideSDR AALA202607140367Intercostal · corrodedAIRCRAFT IN BASE MAINTENANCE: GALVANIC CORROSION ON LT INBOARD INTERCOSTAL BS 947 TO 967, LBL 24. MAINTENANCE REPLACED LT INBOARD INTERCOSTAL BS 947 TO 967, LBL 24 IAW SRM 53-70-51-2R-5 AND IPC 53-42-51-23 AND SRM 51-40-02.Jul 9, 2026 · N902AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR CALA2026071317729Light · no testEMERGENCY AISLE LIGHTS AT POSITIONS 3A AND 40A FAIL TO ILLUMINATE WHEN TESTED. REMOVED AND REPLACED EMERGENCY AISLE LIGHTS AT POSITIONS 3A AND 40A. IAW AMM 33-51-05-002-039. OPS CHECK GOOD.Jul 9, 2026 · N59053 · Boeing 767424ER · Emergency LightingSDR CALA2026071217722Flap System · faultedON APPCH GEAR DOWN F15 SLCTD. IND WAS 5 ON THE GAUGE. AFTER GO ARNDWORKED NRML ON RETURN PERFORMED FSEU INBD FAULT AND EXISTING FAULTS TEST, TASK 27-51-00-740-801. NO FAULTS INBD AND ON GND. NO PREVIOUS HISTORY. RAN FLAPS COUPLE OF TIMES AND INSPECTED THEM, Jul 9, 2026 · N28478 · Boeing 737924ER · Trailing Edge Flap Control SystemSDR CALA2026071217687Battery Pack · no testEMERGENCY BATTERY PACK M1674 FAIL. REMOVED AND REPLACED NEW BATTERY PACK M1674. IAW AMM 33-51-06-960-805. TEST GOOD FOR SERVICE.Jul 9, 2026 · N26210 · Boeing 737824 · Emergency LightingSDR CALA2026071217685Channel · corrodedCORROSION RH CHANNEL ZEE AFT CARGO FLOOR FROM BS 747 TO 787. REMOVED AND REPLACED NEW SHIELD ON RH CHANNEL ZEE AFT CARGO FLOOR, APPLIED ALODINE PRIMER IAW SRM 51-40-02-0G-0 STEP 4 SRM 51-40-05-0G-0 STEP 4.C AMM 51-21-41-370-802 AMM 51-21-72-370-804 SRM 51-40Jul 9, 2026 · N38257 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2026071217683Channel · corrodedCORROSION RT CHANNEL ZEE FWD CARGO FLOOR AT STA 500H AND STA500F. COMPLETED REMOVE AND INSTALLED RH ZEE CHANNEL FWD CARGO AT STA 500H AND STA 500F IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G, SRM 51-40-08-0G-0.Jul 9, 2026 · N38257 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2026071217681Channel · corrodedCORROSION LT CHANNEL ZEE FWD CARGO FLOOR FROM BS 500 TO 500H. COMPLETED REMOVED AND INSTALLED LT ZEE CHANNEL FWD CARGO AT BS 500 AND 500H IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G, SRM 51-40-08-0G-0.Jul 9, 2026 · N38257 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2026071217679Channel · corrodedAFT CARGO BAY, RT. SIDE "Z" CHANNEL, MULTIPLE: CORROSION SPOTS AND LOOSE RIVETS ON FRAMES COMPLETED REMOVAL AND INSTALLED Z" CHANNEL R/H SIDE AFT CARGO BTW STA 727 TO 767. IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0, SRM 51-40-08-0G-0 AND SRM 53-00-53-2R-5.Jul 9, 2026 · N38257 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2026071217677Floor Panel · corrodedAFTER EVALUATION AT FWD CARGO FLOOR PANEL 120DF REQUIRE FABRICATION. FABRICATED NEW FWD CARGO FLOOR PANEL 120 DF IAW EC/RA 5320-02744 AND SRM 53-30-53-0I-0, SRM 51-40-05-0G-0,SRM 51-40-08-0G-0, SRM 51-20-01-0G-0, AMM 25-52-10-400-801,AMM 51-21-72-370-804.Jul 9, 2026 · N38257 · Boeing 737824 · Fuselage Floor PanelSDR CALA2026071217675Channel · corrodedLEFT AFT CARGO COMPARMENT ZEE CHANNEL BS 727 TO 847. REMOVED AND REPLACED AFT CARGO LT SIDE ZEE CHANNEL SIDE PLATE FROM BS 727 TO 847 IAW SRM 51-40-02-0G-0, SRM 53-00-53-2R-5, PAR. 4,D., SRM 51-40-05-0G-0, SRM 51-40-08-0G-0.Jul 9, 2026 · N38257 · Boeing 737824 · Passenger Compartment LightingSDR IXXA20260709058Life Vest · tornRIGHT SUPERNUMERARY SEAT LIFE VEST BAG TORN OPEN. PLACED ON DEFERRAL 74891 MINIMUM EQUIPMENT LIST CATEGORY D IAW ATI-25-25-03-01. REMOVED AND REPLACED RIGHT SUPERNUMERARY SEAT LEFE VEST IAW B767 IAI 25-63-00. DEFERRAL 74891 CLEARED.Jul 9, 2026 · N619AZ · Boeing 767332 · Life JacketSDR DXTA2026071308773Shutoff Valve · failedINTERMITTENT AMBER FUEL FW S/O FAIL R CAS MESSAGE. THE RT ENGINE DID NOT SHUT DOWN. REMOVED RIGHT FUEL SHUTOFF VALVE AND INSTALLED RIGHT FUEL SHUTOFF VALVE, OPS CHECK SAT.Jul 9, 2026 · N834QS · Textrn TEXTRON700 · Aircraft Fuel Distribution SystemSDR YENA2026071400569Trigger · over extendedFLT 2115, BOS-BUF. L2 DOOR WILL NOT ARM; FOUND EOAM TRIGGER MECHANISM FOUND OVER CENTER POSITION INTO PROPER CONFIG IAW AMP 52-12-08 ARM SYS OPERATES NORMALLY.Jul 9, 2026 · N3102J · Airbus BD5001A11 · Passenger/Crew DoorsSDR YENA2026071300566Horn · activatedFLT #1236, DTW-BOS. UNCOMMANDED "EVAC CMD" HORN AT ALTITUDE AFT GALLEY SW ILLUMINATED EVAC HORN; RESET AIRCRAFT POWER OPS CHK EVAC HORN SUCESSFUL REF AMP J-44-11-17-02AAA-320AJul 9, 2026 · N3138J · Airbus BD5001A11 · Emergency EquipmentSDR YENA2026071300565Oil Tube · tornFLT#373, BOS-AUA (DIVERTED TO PLS). AT 31000 FT OIL QTY DROPPED TO 5 QTS SPOKE WITH MCC OIL DROPPED TO 3.5 QTS DIVERTED TO MBPV OIL CONT TO DROP AND SHOWED 0.0 QTS ON APPROACH AFTER SHUTDOWN OIL ROSE TO 6.5QTS; NO LOAD 15 REPORT GENERATED PER AMM 05-51-11 DOESJul 9, 2026 · N997JL · Airbus A321231 · Turbine Engine Oil SystemSDR YENA2026071300564Bulb · burned outFLT#257, BOS-BZN. 2 BULB BURN OUT AFT GALLEY EMG EXIT SIGN ( EXIT MARKING SIGNS WALL MOUNTED EXIT (MARKING) SIGNS ); RELAMPEDL2 DOOR EXIT SIGN REF AMM 33-51-17. OPS CK GOOD. THIS CLEARS MDDR # 623289. MX-4 UPDATED, PLACARD REMOVEDJul 9, 2026 · N516JB · Airbus A320232 · Emergency LightingSDR YENA2026071300563Lamp · inoperativeFLT#257, BOS-BZN. RH EMG. EXIT SIGN HAS NUMEOUS OF BURN OUT BULB ( VERY DIM) ( EXIT MARKING SIGNS WALL MOUNTED EXIT (MARKING) SIGNS ); RELAMPED R1 DOOR EXIT SIGN REF AMM 33-51-17. OPS CK GOOD. THIS CLEARS MDDR # 623288. MX-4 UPDATED, PLACARD REMOVED.Jul 9, 2026 · N516JB · Airbus A320232 · Emergency LightingSDR SWAA2026071319907Lamp · inoperativeAFT LEFT PASSENGER ENTRY DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT LEFT PASSENGER ENTRY DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-51-04. OPS CHKD GOOD.Jul 9, 2026 · N8894Q · Boeing 7378 · Emergency LightingSDR SWAA2026071319694Seal · crackedRIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED ALONG SEAL TRACK EDGE. REMOVED AND REPLACED RT HORIZONTAL STAB UPPER SLIDING SEAL IAW AMM 53-31-31.Jul 9, 2026 · N1809U · Boeing 7378 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026071319864Spring · out of positionFWD ENTRY DOOR HANDLE IN VERTICAL POSITION ON THE OUTSIDE WITH FWD ENTRY DOOR HANDLE ON THE INTERIOR; IN THE CLOSED & LOCKED POSITION. R & R FWD ENTRY DOOR HANDLE SHAFT SPRING IN REF. TO AMM 52-11-11. OPS CHECKED GOOD.Jul 9, 2026 · N8317M · Boeing 7378H4 · Passenger/Crew DoorsSDR SWAA2026071320137Fmu · fluctuatesNR 1 ENGINE THRUST ALERT APX 3 SECONDS FOLLOWED BY W/ENGINE INDICATIONS FLUCTUATING FLUCTUATING N1, EGT, N2, FF MINOR FLUCTUATIONS. IN DESCENT WITH PARTIAL THRUST APX 75% N1. INDICATIONS STABLE DURING APPROACH. ACCOMPLISHED IFIM 73-00-00-810-C05. REMOVED ANJul 9, 2026 · N8789Q · Boeing 7378 · Fuel Controlling System