Service difficulty reports

1,771,708 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 REXA2026070301032Support · corrodedCORROSION ON SUPPORTS (7EAS) OF WHEEL BIN 173BZ AND 174BZ AT FS797.00 TO FS830.40 AND LBL 45.00 TO RBL 45.00 MLG WHEEL WELL AREA. CORROSION ON SUPPORTS (6EAS) OF WHEEL BIN 173BZ AND 174BZ AT FS797.00 TO FS830.40 AND LBL 45.00 TO RBL 45.00 MLG WHEEL WELL AREA WMay 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026070301023Fitting · corrodedCORROSION FLOOR FITTING IN AFT AND FWD ACCESS 107 (2EAS) ON GALLEY 1. FLOOR FITTING IN AFT AND FWD ACCESS 107 (2EAS) ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-67 REV NO.10May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026070301022Fitting · corrodedCORROSION FLOOR FITTING FWD ACCESS 306 (1EA) AND AFT ACCESS 305 (1EA) ON GALLEY 3 FLOOR FITTING FWD ACCESS 306 (1EA) AND AFT ACCESS 305 (1EA) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV NO.5May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026070301020Fitting · corrodedCORROSION FLOOR FITTING FWD ACCESS 306 (1EA) AND AFT ACCESS 305 (1EA) ON GALLEY 3 FLOOR FITTING FWD ACCESS 306 (1EA) AND AFT ACCESS 305 (1EA) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV NO.5May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026070301016Stringer · corrodedCORROSION ON STGR 20R BTW FS 295 TO FS 310. STGR 20R BTW FS 295 TO FS 310 WAS EVALUATED OUT OFF LIMITS PER CRJ-900 SRM 53-21-03-101-002-A04 AND STGR 20R BTW FS 280 TO FS 319 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026070301011Frame · corrodedCORROSION ON FRAME BTW FS=969/ STGR 25L TO 26L,FS=847+16/STGR 27 AND FS=847+32/STGR 26L TO 26R AT FUSELAGE INTERNAL STRUCTURE DUE TO EXCESSIVE CORROSION ON FRAME FS=847+32/STGR 26L TO 26R WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026070301002Frame · corrodedCORROSION ON FRAME BTW FS 319.00 AND STGR 26R TO 26L AT FUSELAGE INTERNAL STRUCTURE. CORROSION ON FRAME BTW FS 319.00 AND STGR 26R TO 26L AT FUSELAGE INTERNAL STRUCTURE WAS REMOVED CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2026050576407Floorbeam · corrodedLT CROSSBEAM AT FS 280 HAS CORROSION. REMOVED AND REPLACED CORRODED LT CROSSBEAM AT FS280.00 WITH NEW LT CROSSBEAM AT FS 280 USING ALL NEW FASTENERS IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01 AND DWG CC670-34010 REV -K. May 5, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR IPXA2026060932327Strap · corrodedAFT CARGO RH OTBD CEILING SUPPORT FRAME EXFOLIATED STA 1400-1420. INSTALLED 1 E/A STABILIZER STRAP SECTION AND 1 E/A SPLICE DOUBLER ON AFT CARGO RH OTBD STA 1400-1420 IAW SRM 51-70-11-0G-0May 5, 2026 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR VNAA202606120019Seat Track · corrodedCORROSION SIDE SEAT RAIL 15RH (5EAS) BTW FS669.40 TO FS977. SIDE SEAT RAIL 15RH (5EAS) BTW FS669.40 TO FS977.00 AREA IS OUT LIMITS PER CRJ-900 SRM 53-31-43-101-001-A01 AND SEAT RAIL 15RH (5EAS) BTW FS669.40 TO FS977.00 WERE REPLACED PER CRJ-900 AMM 53-00-4May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202606120018Seat Track · corrodedCORROSION SIDE SEAT RAIL 15LH (7EAS) BTW FS669.40 TO FS977. SIDE SEAT RAIL 15LH (4EAS) BTW FS847+8 TO FS977.00 WERE EVALUATED EXCESSIVE DAMAGE PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ-900 SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49-400-May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202606120017Seat Track · corrodedSEVERAL DAMAGES FOUND ON ALL THREE VISIBLE SEAT RAILS ABOVE FLOOR FS477.40 TO FS693.00 AT 9LBL/9RBL (WEAR, NICKS, SCRATCHES, CORROSION, SECTIONS AT FS 477 TO 661+32 ON 9RBL WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND NO DAMAGE FOUND, CORROSION ON SEMay 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202606120016Seat Track · corrodedSEVERAL DAMAGES FOUND (WEAR,SCRATCHES, NICKS, CORROSION, GOUGES) ON ALL LH/RH THREE SEAT RAILS ABOVE FLOOR FS280.00 TO FS477.4. DUE EXCESIVE DAMAGE ON ALL LH/RH THREE SEAT RAILS ABOVE FLOOR FS280.00 TO FS477.40 WERE REPLACED PER CRJ-900 SRM 53-21-49-101-001-May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202606120015Seat Track · corrodedSEVERAL DAMAGES ( NICKS, GOUGES, WEAR, CORROSION, SCRATCHES) ON SIDE SEAT RAILS BOTH L/H AND R/H FS379.00 TO FS669.40 STRG15. SEVERAL DAMAGES (NICKS, GOUGES, WEAR, CORROSION, SCRATCHES) ON SIDE SEAT RAILS BOTH L/H AND R/H FS379.00 TO FS669.40 STRG15 WERE EVAMay 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202606120014Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FS=1015 TO FS=1031 LBL27 AT AFT BAGAGGE BAY. FLOOR SUPPORT BETWEEN FS=1015 TO FS=1031 LBL27 AT AFT BAGAGGE BAY. WAS REPAIRED PER SRM 53-00-41-201-001-A03.May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202606120013Floor Support · corrodedCORROSION ON FLOOR SUPPORT FS=280.00 BTW RBL 9 AND LBL 9 AT FWD PASSENGER CABIN STRUCTURE. CORROSION ON FLOOR SUPPORT FS=280.00 BTW RBL 9 AND LBL 9 AT FWD PASSENGER CABIN STRUCTURE WAS EVALUATED OUT LIMITS PER SRM 53-00-00-101-001-A01 AND REPLACED PER SRM 51May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202606120012Fitting · corrodedCORROSION ON FITTINGS SUPPORT (2 EAS) OF GALLEY ATTACHMENT FITTING FS=285.00 RBL 17 AND FS=288.00 LBL 20 AT FWD CPAX CABIN STRUCTURE. CORROSION ON FITTINGS SUPPORT (2 EAS) OF GALLEY ATTACHMENT FITTING FS=285.00 RBL 17 AND FS=288.00 LBL 20 AT FWD CPAX CABIN STMay 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA202606120011Bracket · corrodedCORROSION ON MACHINED BRACKETS (5 EAS) STA FS=661, FS=565 AND FS=517 AT INTERNAL STRUCTURE FWD/CTR BAGGAGE BAY. PAINT ON MACHINED BRACKETS STA FS=661 (2EAS), AND FS=517 (1EAS) AT INTERNAL STRUCTURE FWD/CTR BAGGAGE BAY WERE REMOVED PER CRJ-900 SRM 51-26-01-00May 5, 2026 · N563NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR IPXA2026052633701Rib · crackedLEFT PYLON, RIB 3 A, PANEL FRAME WITH CRACK APPROX 1 INCHE LONG. INSTALLED RIB 3A PANEL FRAME ON LH PYLON I.A.W. A300 AMM 54-52-61/401.May 5, 2026 · N156UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/RibSDR CALA2026061016960Stiffener · crackedRIGHT HORIZONTAL STAB, CRACKED STIFFENER NR 3 ON THE RIB AT STAB STA 129.50 (ON THE BOTTON AREA.) NSTALLED RT HORIZONTAL STAB RIB BS 129.50 IAW SRM 51-40-02-0G. REPAIRED RT HORIZONTAL STAB STIFFENER NR 3 ON RIB AT BS 129.50 BOTTOM AREA IAW SRM 55-10-09-2R-4.May 5, 2026 · N14249 · Boeing 737824 · Horizontal Stabilizer Miscellaneous StructureSDR SCNA20260609244Vapor Barrier · crackedCRACK ON VAPOR BARRIER (LOWER WEB) BETWEEN BSTA 663 & LBL 31.83 TO LBL 45.64, ALSO BETWEEN BSTA 663 & RBL 25.00 TO RBL 40. VAPOR BARRIER (LOWER WEB) BETWEEN BSTA 663 & LBL 31.83 TO LBL 45.64, ALSO BETWEEN BS 663 & RBL 25 TO RBL 40 WAS REPAIRED IAW SRM 51-70-May 5, 2026 · N845SY · Boeing 737800* · Fuselage Main, BulkheadSDR SIMA20260505003Seat Track · corrodedCORROSION ON RH SEAT TRACK AT FR84-85, Y= 10.748". (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON R/H SEAT TRACK ABOVE FR 84 REF EMB 175 SRM 51-10-03 L = 1.200" W = .800" H = .058" REMAINING THICK NESS IS .013" ORIGINAL THICKNESS WAS .071" FOUND TO BEMay 5, 2026 · N299JJ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260505005Seat Track · corrodedCORROSION ON LH SEAT TRACK AT FR 84-85, Y= -10.748". (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED CORROSION ON L/H SEAT TR ACK AT FR 84 - 85 -Y10.748 REF SRM 51-10-03. AFTER BLENDING CORROSION FOUND AT END OF TRACK NO ALLOWABLE DAMAGE THIS LOCATION REF SRM 53-23May 5, 2026 · N299JJ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260505004Crossbeam · corrodedCORROSION FOUND ON CROSSBEAM AT FR 87 (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORRODED AREA PER SRM 51-10-03 AND ETN-EJ-51-009. AREA MEASURES L= 2.500" X W=.600" X D=.034" & IS FOUND TO BE OUT OF LIMITS PER SRM 51-75-16 AND ET N-EJ-51-009. FABRICATED FILLERMay 5, 2026 · N299JJ · Emb ERJ170200LR · Fuselage Main, StructureSDR REXA2026060400925Support Angle · corrodedCORROSION ON SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR. SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01.May 5, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400907Support Angle · corrodedCORROSION ON SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR. SUPPORT ANGLES (2EA) ON FUEL PANEL ON ACCESS PANEL 192AR WERE REPLACED PER SRM 51-42-10-001-001-A01.May 5, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR FDEA202605050546Nacelle · not reportedNACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAGE COMPLY WITH EA 1-5450-T0386263 REV NR POS. P2 COMPLY WITH E..A. 1-5450-T0386263 REV NR PS P2 EA: 1-5450-T0386263 PT 2 COMPLLIED WITH EA 1-5450-T0386263 PT 2 REMOVING AND May 5, 2026 · N521FE · Doug MD11F · Nacelle/Pylon StructureSDR SWAA2026060195684Floor Panel · delaminatedDELAMINATED FLOOR PANEL 242AF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.May 5, 2026 · N7875A · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2026060195686Floor Panel · delaminatedDELAMINATED FLOOR PANEL 231XF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 231XF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL. SMay 5, 2026 · N7875A · Boeing 7377Q8 · Fuselage Floor PanelSDR SWAA2026060195805Window Post · crackedCRACK WINDOW 1 POST INTERNAL AREA AFT UPPER CORNER POSITION RH SIDE. PERFORMED REPAIR ON UPPER CORNER WINDOW R1 AT COCKPIT AREA IAW EA 26-153-01227 THRU WIP1 TO WIP2.May 5, 2026 · N7875A · Boeing 7377Q8 · Fuselage Main, StructureSDR SWAA2026060195830Fitting · crackedCRACK LOWER SURFACE OF LEADING EDGE SLAT 8 NOSE SKIN AT ACTUATOR LOC. AROUND FASTENER AT RT WING. SLAT 8 HAS BEEN REPLACED BECAUSE THE ACTUATOR FITTING WAS FOUND TO BE CRACKED IN TWO HOLES DURING THE ROTO TEST INSPECTION FOR SLAT REPLACEMENT.May 5, 2026 · N477WN · Boeing 7377H4 · Wing, Attach FittingsSDR IPXA2026051925440Structure · crackedCRACKED UPPER CHORD, DURING PERFORM SB EO-85445-JIC1 OPEN HOLE INSP AT ELEV STA 231.8, ELEV STA 256.8 (REPLACE). INSTALL NEW CHORD I.A.W SRM 51-40-02-0G REV.48 AND BOEING DWG NO.65B05731 SH8 REV.A AND 65B05731 SH9 REV.A AND 65B05731 SH10 REV.- AND 183U3301 SHMay 5, 2026 · N611UP · Boeing 7478F · Elevator StructureSDR SWAA2026052895682Web · corrodedCORROSION ON SHIELD WEB LOCATED BTW BS 492 - 500A, RBL21, WL156 IN THE FWD CARGO BAY. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A0080, SHEET 37, REV -.May 5, 2026 · N949WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052895681Angle · crackedCRACKED ANGLE, BS 500C, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02 AND DWG 143A7505 SHEET 118 REV -.May 5, 2026 · N949WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR AALA202605289820Skin Panel · wornAIRCRAFT IN BASE MAINTENANCE: UPPER REAR FUSELAGE CROWN SKIN PANEL WORN AT THE VIASAT ANTENNA MOUNTING AREA BETWEEN FR 62 AND FR 63, BETWEEN S1R AND S2R. REPAIRED SKIN PANEL PER EA 375293.May 5, 2026 · N105NN · Airbus A321231 · Fuselage Main, Plate/SkinSDR CALA2026052616546Pressure Web · crackedCENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN WL192.0 AND WL 200.6, 01 CRACK BETWEEN RBL 39.83/RBL 40.00 AND 01 CRACK BETWEEN RBL 40.00/RBL 45.64. (REF AAR NR 1000073212).ACCOMPLISH THE REPAIR OF THE WING CENTER SECTION REAR SPAR VERTICAL PRESSURE WEB IAMay 5, 2026 · N37290 · Boeing 737824 · Fuselage Main, StructureSDR CALA2026052616525Light · faultedRED PATHWAY EMERGENCY LIGHT INOP FWD OF SEAT 20K . REQUESTING DEFERRAL LENS CRACKED BUT WORKING RED PATHWAY EMERGENCY LIGHT FWD OF SEAT 20K HAS A CRACK BUT WORKING. DEFERRED REF NEF 2520TP DEFERRED REMOVED AND REPLACED LIGHT ASSEMBLY. OPS TEST GOOD. REF AMM 33May 5, 2026 · N663UA · Boeing 767322 · Emergency LightingSDR SWIA2026050576096Seat Track · corrodedSEAT TRACK AT FRAME 86 -2 INCH, Y+10.74 INCH, HAS CORROSION (C-CHECK RO 05/22/2026)FABRICATED, LOCATED AND DRILLED NEW FILLER PN: 7475T761 .071" PO: 264372, AND DOUBLER PN: 7475T761 .080" PO: 341952 INSTALLED REPAIR PARTS PER EMB ETD2026-170-008178 REV .: /..May 5, 2026 · N82366 · Emb ERJ170200LL · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026052129174Bracket · brokenFWD CARGO COMPARTMENT FR38.1/S38L-S40L THERE IS 2EA HARNESS STAND OFF BRACKETS BROKEN. INSTALLED 2EA BRACKETS AT FWD CARGO COMPARTMENT FR38.1/S38L-S40LIAW SRM 51-40-21-001 .May 5, 2026 · N156UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR AALA202605220708Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540 AND LBL2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1May 5, 2026 · N800NN · Boeing 737823 · Fuselage Main, StructureSDR AALA202605227559Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540 AND RBL2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.May 5, 2026 · N800NN · Boeing 737823 · Fuselage Main, StructureSDR AALA202605211337Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE ASSEMBLY BETWEEN STA 500 AND STA 500A AT LBL24. REPLACED BAFFLE ASSEMBLY PER AARD 51-00-05-1.May 5, 2026 · N954NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR IPXA2026051023848Actuator · failedNO BACK BRAKE FUNCTION FAIL AT AFT CARGO DOOR ROTARY ACTUATOR. I.A.W AMM 52-37-04-404-009 REV.148 TO DO AFT CARGO DOOR OPERATIONAL TEST. THE RESULT WAS SATISFIED.May 5, 2026 · N301UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2026052020091Stringer · crackedSTRINGER CRACKED, FWD SIDE OF STA 2360 AT S-11L. ACCOMPLISH THE REPAIR I.A.W EGAT EI F2026A53M-1003 REV.2 AND UPS EO-97410-REQ0023 REV.1.May 5, 2026 · N611UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR SWIA2026050576021Skin · chafedFURTHER CHAFED FOUND ON LT WING SLAT 4 AFT EXTERNAL BOTTOM SKIN AT OTBD HARNESS TUBE AT PREVIOUS BLENDED AREA AS MARKED. FOUND ON ETD2024-170-004693 RECURRING DETAILED VISUAL INSPECTION. REMOVED PAINT FROM THE LT WING SLAT 4 AT THE OUTBOARD HARNESS TUBE ON THEMay 5, 2026 · N267SY · Emb ERJ170200LL · Leading Edge DevicesSDR IPXA2026051920076Stringer · crackedSTRINGER CRACKED, FWD SIDE OF BS 2360, S7L. ACCOMPLISH THE REPAIR I.A.W UPS EO-97410-REQ0022 REV.1 AND SRM 53-60-03-2R-8 REV.48 AND EGAT WORK SHEET NO.60355 AND EGAT EI NO.F2026A53M-1043 REV.0.May 5, 2026 · N611UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2026051919736Stringer · crackedSTRINGER CRACK, FWD SIDE OF STA 2360 AT S-7R (LEVEL2)(REPAIR). ACCOMPLISHED REPAIR I.A.W EO-97410-REQ0026 REV.1 AND EGAT EI NO.F2026A53M-1052 REV.0 AND EGAT WORK SHEET NO.60354 AND SRM 53-60-03-2R-8 REV.48. REVIEWED TASK PER GMM-MTX 09.05.01.09.May 5, 2026 · N611UP · Boeing 7478F · Fuselage Main, Longeron/StringerSDR IPXA2026051023870Actuator · noisyNOISE DURING FWD CARGO DOOR OPERATION. (REPLACE) I.A.W AMM 52-33-04-404-028 REV.148 TO DO FWD CARGO DOOR OPERATIONAL TEST. THE RESULT WAS SATISFIED.May 5, 2026 · N301UP · Boeing 76734AF · Cargo/Baggage DoorsSDR FDEA202605050597Autothrottle Sys · failedAUTO THROTTLES UNSATISFACTORY ON DEPARTURE. SPEED HELD AT 24 KNOTS LESS THAN COMMANDED SPEED WITH THROTTLES COMMANDED TO AN INTERMEDIATE POWER SETTING. HAD TO PERFORM MULTIPLE INTERVENES TO MAINTAIN SPEED AND AVOID GETTING BELOW SAFE POWER SETTINGS AND SMay 5, 2026 · N270FE · Boeing 7673S2F · Auto Throttle SystemSDR CALA202602150107Skin · ground damageA}7C HITTED BY LAV TRUCK, NEXT TO LAV SERVICE DOOR. CONDITIONAL INSPECTION FOR HIT WITH GROUND EWUIPPMENT PERFORMED IAW AMM 05-51-59-200-801 BETWEEN BS 867 & 905 AND S-22 LH& S-24 LH // PERMANENT REPAIR PERFORMED IAW ERI-132-2026May 5, 2026 · N188AM · Boeing 7378 · Fuselage Main, Plate/Skin