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 IPXA2026050781934Profile · corrodedAFT CARGO COMP, FR 54.2, FROM Y700 TO Y1959, CEILING SUPPORT STRUCTURE WITH CORROSION ON EACH SCREW RECEPTACLE. REMOVED CORROSION IAW SRM 53-16-18-001. DEEPEST MATERIAL LOSS IS .006 (ON ALL 3 PROFILES) AND FOUND CRACK AT HOLE ON CENTER PROFILE. REMOVE AND REPApr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR HNAA2026052000427Skin · damagedPOSSIBLE LIGHTNING STRIKE ON FUSELAGE EXTERNAL SKIN AT FR 37-38, STRG 6R-7R. PERFORMED DRILL OUT OF LIGHTNING STRIKE AREA AND REPAIRED WITH SOLID BUTTON HEAD RIVET AND WASHER PER EMB 145 SRM 53-00-01,ITEM 2, FIG 201, SHEET 1 AND 2.Apr 7, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR HNAA2026052000426Skin · damagedPOSSIBLE LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FR33-34, STRG 5R-6R. PREPPED PRIMED AND PAINTED FUSELAGE SKIN FR 33-34, STRG 5R-6R IAW EMB 145 CPM 51-21-05 AND 51-21-06 51-21-03 AND PIEDMONT DRAWING AE-ERJ145-IR PIEDMONT BULLETIN CPM 51-02Apr 7, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR HNAA2026052000425Skin · damagedPOSSIBLE LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FR-25-26, STRG 6R-7R. PERFORMED RIVET AND WASHER IN AFFECTED HOLE ON EXTERNAL FUSELAGE SKIN BTW FR 25-26 AND BTW STR 6R-7R IAW ETD 2026-145-0, SRM 53-00-01, ITEM 2, FIG 201, SHEET 1 AND 2 AND EO1-53-26-0239Apr 7, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR HNAA2025052000424Drag Angle · crackedRIGHT VERTICAL STABILIZER DRAG ANGLE HAS POSSIBLE CRACK AT FRAME 78. REMOVED AND REPLACED RT VERTICAL TO FUSELAGE DRAG ANGLE IAW SRM 51-40-02.Apr 7, 2026 · N655AE · Emb EMB145LR · Fuselage, Stabilizer Attach FittingsSDR IPXA2026042780631Support Angle · crackedAFT CARGO COMP, FR 54, Y0, FWD BULKHEAD SUPPORT ANGLE WITH CRACK. DOT 73-024 INSTALLED NEW SUPPORT ANGLE (BRACKET) I.A.W. A300-600 SRM 51-40-21.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042780683Support Angle · crackedAFT CARGO COMP, FR 54, -Y1959, FWD BULKHEAD SUPPORT ANGLE WITH CRACK. DOT 73-030 INSTALLED NEW SUPPORT ANGLE (BRACKET) I.A.W. A300-600 SRM 51-40-21.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042780662Support Angle · crackedFAULT - STR - Z100 - AFT CARGO COMP, FR 54, Y953, L/H FWD BULKHEAD SUPPORT ANGLE WITH CRACK. DOT 73-026 INSTALLED NEW SUPPORT ANGLE (BRACKET) I.A.W. A300-600 SRM 51-40-21.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042780634Support Angle · crackedAFT CARGO COMP, FR 54, Y1959, FWD BULKHEAD SUPPORT ANGLE WITH CRACK. DOT 73-027 INSTALLED NEW SUPPORT ANGLE (BRACKET) I.A.W. A300-600 SRM 51-40-21.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050781897Support · corrodedAFT CARGO COMP, FR 54.2, FROM -Y700 TO -Y1959, CEILING SUPPORT STRUCTURE WITH CORROSION ON EACH SCREW RECEPTACLE. INSTALLED NEW PROFILE (CEILING SUPPORT/ 1EA) AT AFT CARGO COMP, FR 54.2, FROM -Y700 TO -Y1959 IAW SRM 51-40-21.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042780694Support Angle · crackedAFT CARGO COMP, FR 54, -Y953, L/H FWD BULKHEAD SUPPORT ANGLE WITH CRACK. INSTALLED NEW SUPPORT ANGLE (BRACKET) IAW SRM 51-40-21.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042780648Support Angle · crackedAFT CARGO COMP, FR 54, Y953, RT FWD BULKHEAD SUPPORT ANGLE WITH CRACK. INSTALLED NEW SUPPORT ANGLE (BRACKET) IAW SRM 51-40-21.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042780689Support Bracket · crackedAFT CARGO COMP, FR 54, -Y953, R/H FWD BULKHEAD SUPPORT ANGLE WITH CRACK. INSTALLED NEW SUPPORT ON CARGO COMPARTMENT, FR 54, -Y953 IAW A300 SRM 51-40-21 PAR. 6 AND IDENTIFIED WITH INDELIBLE MARKER IAW GMM 09-08-01-04.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR FDEA202604070574Fitting · not reportedDOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24 COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OApr 7, 2026 · N669FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR SWAA2026051187259Attach Angle · crackedH.F.E.C. VERIFIED BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED APPROX. LBL 9.<[01] REMOVED ALL FASTENERS ON L/H VAPOR BARRIER ATTACH ANGLE IN FUEL TANK PER SRM 57-10-10-2R-5. REMOVED ALL FASTENERS ON VERTICAL FLANGE OF THE VAPOR BARRIER ATTACH ANGLE FROM APPROXApr 7, 2026 · N8534Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026051187260Attach Angle · crackedHFEC VERIFIED BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED APPROX. LBL 34. REMOVED AND REPLACED VAPOR BARRIER ATTACH ANGLE AT STA. 663 FROM LBL 5 TO LBL 65 PER SRM 51-40-02; EA-M-24-157-02340 AND DRAWING 111A1000.Apr 7, 2026 · N8534Z · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026051187258Attach Angle · crackedHFEC VERIFIED BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED APPROX. RBL 9. REMOVED ALL FASTENERS ON R/H VERTICAL FLANGE IN REPAIR AREA STA 663 RBL 5 TO RBL 16 IAW SRM 57-10-10-2R-5. CUT AND REMOVED DAMAGED SECTION OF RH VAPOR BARRIER ATTACH ANGLE FROM RBL 5 TOApr 7, 2026 · N8534Z · Boeing 7378H4 · Wing, Attach FittingsSDR SWAA2026051187309Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT BS540 AND LBL6 AT AIR CONDITIONING BAY. REMOVED AND REPLACED NEW SUPPORT BRACKET LOCATED ON PNEUMATIC DUCT BS540 AND LBL6 AT AIR CONDITIONING BAY IAW SOPM 20-50-01 REV 40.Apr 7, 2026 · N8637A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026051187310Angle · crackedCRACK ON ANGLE LOCATED BS663 UPPER POSITION RBL37. REPLACED ANGLE UPPER CHORD LOCATED INTERNAL AREA RT SIDE BODY STA 663.75 AND RBL 6 TO RBL 63 AT AIR CONDITIONING BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 111A1000 SHEET 349 REV-.Apr 7, 2026 · N8637A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026043084286Support · corrodedAFT CARGO COMP, FR 58, FROM -Y700 TO Y700, CEILING SUPPORT STRUCTURE WITH 3 SPOTS WITH CORROSION. CORROSION REMOVED AT AFT CARGO COMP, FR 58, FROM -Y700 TO Y700, CEILING SUPPORT STRUCTURE (3 SPOTS): THEREPERFORE IS WHITIN LIMITS IAW A300-600 SRM 51-73-11-001Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050883072Skin · crackedRH WING BETWEEN SLAT# 8 AND #9 ON FIXED LEADING EDGE SKIN IN CRACKED. COMPLIED WITH STEP FOR EO-97223-REQ1 AND VT-MAE EA 757-5741-27-A4443, REV-, PRIOR TO FURTHER FLIGHT IS DOCUMENTED ON T3F18E008PRFYApr 7, 2026 · N421UP · Boeing 75724APF · Wing, Plate/SkinSDR IPXA2026050781905Profile · corrodedAFT CARGO COMP, FR 54.2, FROM -Y700 TO Y700, CEILING SUPPORT STRUCTURE WITH CORROSION ON EACH SCREW RECEPTACLE. REMOVED CORROSION IAW A300 SRM 53-16-18-001. DEEPEST MATERIAL LOSS IS .006. ACTION OR REPAIR IS TO REMOVE AND REPLACE (FIGURE 6 ITEM 1) P/N A2557660Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR SWIA2026040776004Skin · damagedLIGHTING STRIKES (3) AT FWD FUSELAGE BETWEEN FR 1-2 STGR 26L-28L. REMOVED LIGHTNING STRIKE DAMAGE FROM LOWER FWD FUSELAGE SKIN FR 01-02 STGR 26L-28L BY PERFORMING PERMANENT DOUBLER REPAIR REF. ETD2026-170-006439. CHANGE IN WEIGHT MEASURES 85.51 GRAMS. THIS REApr 7, 2026 · N275SY · Emb ERJ170200LL · Fuselage Main, Plate/SkinSDR REXA2026050700514Channel · corrodedCORROSION ON INTERNAL CHANNEL AT AREA OF AFT DRAIN MAST (FS1031.00 TO FS 1051.30 BTW STGR 27 TO 26RH) INTERNAL CHANNEL AT AREA OF AFT DRAIN MAST (FS1031.00 TO FS 1051.30 BTW STGR 27 TO 26RH) WAS REPAIRED PER EA NO: CRJ953-21943 REV. AApr 7, 2026 · N138EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWAA2026050686915Angle · corrodedFWD CARGO RT TRANSITION ANGLE HAS MULTIPLE AREAS OF CORROSION AROUND FASTENER HOLES FROM BS 500C TO 500I. INSPECTED RT TRANSITION ANGLE OUT-OF LIMIT IAW SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE STA 500A-500I IAW 51-40-02.Apr 7, 2026 · N8531Q · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026050687182Attach Angle · crackedBS 663 VAPOR BARRIER ATTACH ANGLE HAS CRACK AT RBL 9. REMOVED VAPOR BARRIER ATTACH ANGLE AT BS633, RBL 9 IAW SRM 51-40-02. LOCATED AND MATCH DRILLED NEW RT BS 663 VAPOR BARRIER ATTACH ANGLE IAW SRM 51-40-06. PERFORMED NDT PER PART 6; 51-00-00 PROCEDURE Apr 7, 2026 · N8531Q · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026050687183Attach Angle · crackedBS 663 VAPOR BARRIER ATTACH ANGLE HAS CRACK AT RBL 34. REPLACED ATTACH ANGLE PER SRM 51-10-02 & SRM 51-40-02.Apr 7, 2026 · N8531Q · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026050687184Attach Angle · crackedBS 663 VAPOR BARRIER ATTACH ANGLE HAS CRACK AT LBL 9. REMOVED FASTENERS AND DAMAGED SECTION OF CHORD PER SRM 57-10-10-2R-5. PERFORMED AN HFEC OPEN HOLE INSPECTION OF ALL FASTENER HOLES IN INSPECTION AREA PER NDT MANUAL PART 6 51-00-00 PROC. 16. NO DEFECTS Apr 7, 2026 · N8531Q · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026050686906Plate · crackedLEFT WING WAFFLE PLATE IS CRACKED UNDER DEFLECTION RIB FIXED TRAILING EDGE PANEL; I/B SIDE OF ENGINE PYLON. ACCOMPLISHED INSPECTION PER NDT PART 6 CH51-00-00 PROCEDURE 23 WITH NO DEFECTS NOTED. REMOVED WAFFLE PLATE FOR NDT PER SRM 51-40-02.. INSTALLED WAFFApr 7, 2026 · N8531Q · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026050686916Rib · crackedRIGHT WING TRAILING EDGE STRUCTURE SUPPORT ANGLE I/B OF DEFLECTION RIB IS CRACKED. REMOVED STRUCTURE SUPPORT ANGLE PER SRM 51-40-02. INSTALLED NEW STRUCTURE SUPPORT ANGLE INBD OF DEFLECTION RIB IAW SRM 51-40-02. INSTALLED NEW STRUCTURE SUPPORT ANGLE I/B OF Apr 7, 2026 · N8531Q · Boeing 7378H4 · Wing, Rib/BulkheadSDR IPXA2026041984059Angle · corrodedRIGHT WTB PANEL LANDING, 2ND FROM FWD, AT UPPER WING ROOT HAS SURFACE CORROSION. 83-021. ATA 53-030 INSTALLED (3EA) NUTPLATES ON FWD SUPPORT ANGLE AND (3EA) NUTPLATES ON AFT SUPPORT ANGLE AT RT WTB UPPER WING ROOT STA-925, WL-208.1. I.A.W. SRM 51-40-02-0G-0 PAApr 7, 2026 · N454UP · Boeing 75724APF · Aerodynamic FairingsSDR SWAA2026050587386Floor Support · crackedFLOOR SUPPORT IS CRACKED AT BS 320, LBL 44, WL 208. R & R THE FLOOR SUPPORT BS 312 - 328, LBL 44, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV -. NO LIMITS GIVEN ON SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1, PAR 4.B FOR SPECIFIC CRACK LOCATION, SRM 51-10-Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587208Cargo Track · crackedAFT CARGO BAY CARGO TRACK CRACKED BS 767, 747, & 727E, RBL 13, WL 156. REPLACED THE CARGO TRACK, BS 727+4 - 887, RBL 13, WL156 IAW SRM 51-40-02 AS SHOWN IN DWG 146A0061 AND DWG 146A7500. SPLICED AT BS 755 PER SRM 53-00-53-2R-3, REPAIR 3, & EA 26-153-01000.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026050587384Floor Support · corrodedCORRODED FLOOR SUPPORT AROUND FLOORBOARD HOLE AT BS 273, LBL 12, WL 208. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G-0, DWG 141A5600, SHEET 2, REV N, & DWG 141A5600, SHEET 1, REV N.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587388Floorbeam · corrodedCORRODED FLOORBEAM, BS 328, RBL 25, WL 208. REMOVED DAMAGE PART OF THE UPPER TEE FITTING ON THE FLOORBEAM, REPAIRED IAW SRM 53-10-51-2R-7, REPAIR 7.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2026050587390Skin · crackedCRACK FOUND ON THE RT HORIZONTAL STAB LOWER SKIN AT HSS 193.90, 24 5/8 FROM L/E; L: 0.200. REMOVED AND REPAIRED THE CRACKED RT HORIZONTAL STAB LOWER SKIN IAW SRM 55-10-01-2R-11, REPAIR 11.Apr 7, 2026 · N928WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026050587387Strap · corrodedCORROSION ON STRAP AT BS 1023 AND 1030, LBL 3, WL 208. REMOVED AND REPLACED REINFORCEMENT STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5600, SHEET 32, REV B.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026050587710Crease Beam · corrodedCORRROSION WAS FOUND ON CREASE BEAM WEBS AT BS 807-827, WL 208, L69. REMOVED AND REPLACED CREASE BEAM AT BS 807-827, WL 208 IAW SRM 51-40-02-0G-0 AND DWG 146A5900, REV-.Apr 7, 2026 · N928WN · Boeing 7377H4 · Fuselage Main, StructureSDR HNAA2026050500372Seat Track · corrodedPASSENGER CABIN UPPER SEAT TRACK SUPPORT SHOWS SURFACE CORROSION. FR. 53 THRU FR. 59.LH SIDE. REMOVED SURFACE CORROSION BY BLENDING ON LH PASSENGER CABIN UPPER SEAT TRACK AT FFR53 THRU FR59 AND IS FOUND TO BE WITHIN MAXIMUM ALLOWABLE LIMITS PER SRM 53-00-11-AApr 7, 2026 · N654AE · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR HNAA2026050500371Skin · corrodedSIGNS OF CORROSION ON RIVET HEADS AT BELLY FR36-37 AND STR 21L. PERFORMED CORROSION REMOVAL OF RIVET HEADS AT BELLY FR36-37 AND STR 21L, NO ADDITIONAL CORROSION FOUND, PER EMB 145 CPM 51-14-00 AND EMB 145 CPM 51-14-02 PARAGRAPH 8, SECTION 4Apr 7, 2026 · N654AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SWAA2026050487312Support Angle · crackedCRACK EDSUPPORT ANGLE LOCATED BS 360 AND BTW STR 27R TO STR 28R AT EQUIPMENT ELECTRONIC COMP. REPLACED SUPPORT ANGLE LOCATED BS 360 AND BTW STR 27R TO STR 28R AT EQUIPMENT ELECTRONIC COMP IAW SRM 51-10-02 ITEM 9.Apr 7, 2026 · N255WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026043078576Angle · crackedAFT CARGO R/H AFT. WALL ANGLE SUPPORT ZONE 164 FOUND CRACK. ES-009. REMOVED CRACKED AFT CARGO RT AFT. WALL ANGLE SUPPORT AT STA 1640 RBL 24.8 IAW SRM 51-40-02-0G-0. INSTALLED FABRICATED SUPPORT ANGLE P/N 453N1809-36SAAU AND REINSTALLED VERTICAL BULKHEAD PANEL Apr 7, 2026 · N454UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026042382776Tie Down · corrodedFWD CARGO RH OTBD TRANSITION HAS CORROSION BS 770 - 800. REMOVED CORROSION AT R/H STA. 780 ON TIE DOWN FITTING RBL 20R IAW 51-10-02-0G-0. INSTALLED NEW TIE DOWN FITTING AT FWD CARGO BS 780 RBL 20R IAW SRM 51-40-02-0G-0.Apr 7, 2026 · N454UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026042382902Sidewall Support · corrodedFWD CARGO LH LOWER SIDEWALL SUPPORT FRAME CORRODED STA 740 STR. REMOVED CORROSION ON L/H LOWER SIDEWALL SUPPORT AT BS 740 BTW STR 22R-26R IAW B757-200PF SRM 51-10-02-0G-0. CORROSION REMOVAL IS 100% MAT'L LOSS, PART WILL BE REMOVED AND REPLACED. INSTALLED SIDApr 7, 2026 · N454UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026042783844Support Channel · corrodedAFT WTB LOWER FAIRING PANEL LANDING CHORD AT APPROX. BS 1217 HAS EXFOLIATED CORROSION. 83-015. REMOVED 1EA EXFOLIATED CHORD (CHANNEL) AT AFT WTB LOWER FAIRING AREA BTW BS 1180 AND 1220 RBL 7 IAW SRM 51-40-02-0G-0. INSTALLED 1 E/A NEW PART CHANNEL SUPPORT AND RApr 7, 2026 · N454UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026043083949Support Angle · crackedSTR- RH AFT WTB LOWER FAIRING PNL LANDING SUPPORT BRACKET HAS EVIDENCE OF A CRACK. 83-018. REMOVED SUPPORT BRACKET AT RH AFT WTB LOWER FAIRING PNL IAW B757-200PF SRM 51-40-02-0G-0 REV 124- 20 SEP 2025. INSTALLED SUPPORT BRAKET AND ATTACHED BEAM AT STR - RH AFTApr 7, 2026 · N454UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026042884007Angle · corrodedRIGHT WTB FWD PANEL LANDING AT UPPER WING ROOT HAS SURFACE CORROSION. 83-020. REMOVED (1EA) FWD SUPPORT ANGLE AND (1EA) AFT SUPPORT ANGLE FROM RH WTB UPPER WING ROOT STA-900, WL-208.1 I.A.W. B757-200PF SRM 51-40-02-0G-0 PARAG.7. INSTALLED FWD AND AFT SUPPORT AApr 7, 2026 · N454UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026042982498Strap · corrodedAFT CARGO RT OTBD CEILING PROFILE CORRODED BS 1420 - 1440, REMOVED CORROSION ON CEILING PROFILE STABILIZATION STRAP AT BS1420, RBL 24.75 ON BOTH UPPER AND LOWER SURFACES IAW SRM 53-00-51-1A-1. INSTALLED NEW STABILIZATION STRAP RBL 24.75 BETWEEN BS 1440-1360 Apr 7, 2026 · N454UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR BAGA2026043000007Battery Pack · failedEMERGENCY BATT FAULT ON EICAS, FWD RH ELPU FAILED. R/R FWD RH ELPU PER AMM. OPS CHECK GOOD. - LATE SUBMISSIONApr 7, 2026 · N126BZ · Emb ERJ190100IGW · Emergency LightingSDR IPXA2026042683067Channel · corrodedFWD CARGO CEILING CHANNEL AT BEAM C26 FROM -Y953 TO Y1456 HAS CORROSION. REMOVED CORROSION AT FWD CARGO CEILING CHANNEL AT BEAM C26 FROM -Y953 TO Y1456: FOUND A NEGLIGIBLE DAMAGE I.A.W. A300-600 SRM 51-73-11-001. RESTORED SURFACE PROTECTION AT FWD CARGO CEILIApr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure