# Service difficulty reports: N242WN A list on [N242WN](https://openairdocs.org/aircraft/N242WN.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 7 · 327 reports - [SDR SWAA2026101559257](https://openairdocs.org/sdr/SWAA2026101559257.md): Flashlight · no test · Oct 11, 2026 · N242WN · Boeing 7377H4 · Emergency Equipment > AFT INBD CABIN EMERGENCY FLASHLIGHT WILL NOT TEST. R & R THE AFT INBD FLASHLIGHT AND BATTERY IAW AMM 25-64-00. OP CHKD GOOD. - [SDR SWAA2026092148915](https://openairdocs.org/sdr/SWAA2026092148915.md): Engine · failed · Sep 18, 2026 · N242WN · Boeing 7377H4 · Engine (Turbine/Turboprop) > ATO FOR LOUD BANG & EGT RED BOX NR1 ENGINE. ENGINE FAILED MESSAGE. R & R NR 1 ENGINE IAW MT 771-00-01 & AMM 05-51-59 - [SDR SWAA2026082786998](https://openairdocs.org/sdr/SWAA2026082786998.md): Flashlight · no test · Aug 23, 2026 · N242WN · Boeing 7377H4 · Emergency Equipment > FWD FA FLASH LIGHT INOP 05 - OK TO CONTINUE PER [MEL 25-12-01PORTABLE FLASHLIGHT HOLDERS/FLASHLIGHTSCABIN]. WITH SP ____1B_____ AND AUTHORIZATION NUMBER __336175_____ REMOVED AND REPLACED FWD LOWER FA FLASHLIGHT BATT IN REFERENCE WITH AMM 25-64-00. EXP SEP29 - [SDR SWAA2026082449316](https://openairdocs.org/sdr/SWAA2026082449316.md): Battery Pack · inoperative · Aug 17, 2026 · N242WN · Boeing 7377H4 · Emergency Lighting > MAIN CABIN MULTIPLE EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK M1673 & PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-06. - [SDR SWAA2026072784169](https://openairdocs.org/sdr/SWAA2026072784169.md): Charger · inoperative · Jul 21, 2026 · N242WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT ON ROW 19 DEF DOES NOT ILLUMINATE. REMOVED AND REPLACED AFT RT BATTERY PACK AND CHARGER IAW AMM 33-51-06. - [SDR SWAA2026072719833](https://openairdocs.org/sdr/SWAA2026072719833.md): Charger · inoperative · Jul 21, 2026 · N242WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY AREA LIGHT ON ROW 22 DEF DOES NOT ILLUMINATE. REMOVED AND REPLACED AFT RT BATTERY PACK AND CHARGER IAW AMM 33-51-06 - [SDR SWAA2026072780289](https://openairdocs.org/sdr/SWAA2026072780289.md): Battery Pack · inoperative · Jul 21, 2026 · N242WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT ON ROW 19 DEF DOES NOT ILLUMINATE. REMOVED AND REPLACED AFT RT BATTERY PACK AND CHARGER IAW AMM 33-51-06. - [SDR SWAA2026072736260](https://openairdocs.org/sdr/SWAA2026072736260.md): Battery Pack · inoperative · Jul 21, 2026 · N242WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT ON ROW 22 DEF DOES NOT ILLUMINATE. REMOVED AND REPLACED AFT RT BATTERY PACK AND CHARGER IAW AMM 33-51-06. - [SDR SWAA2026022071403](https://openairdocs.org/sdr/SWAA2026022071403.md): Angle · cracked · Feb 17, 2026 · N242WN · Boeing 7377H4 · Trailing Edge Flaps > T/E UPPER FIXED PANEL OTBD OF NR 7 SPOILER HAS A CRACKED ANGLE ON INBD SIDE. MATCH DRILLED SERVICEABLE REPLACEMENT FITTING AND INSTALLED TO WEB IAW SRM 51-40-02. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02. - [SDR SWAA2026021364707](https://openairdocs.org/sdr/SWAA2026021364707.md): Access Panel · damaged · Jan 26, 2026 · N242WN · Boeing 7377H4 · Wing, Plate/Skin > ELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026021364708](https://openairdocs.org/sdr/SWAA2026021364708.md): Access Panel · elongated · Jan 26, 2026 · N242WN · Boeing 7377H4 · Wing, Plate/Skin > ELONGATED HOLES ON ACCESS PANEL 661BB, RT WING. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-9, REPAIR 9. - [SDR SWAA2026021362500](https://openairdocs.org/sdr/SWAA2026021362500.md): Support Angle · cracked · Jan 18, 2026 · N242WN · Boeing 7377H4 · Fuselage Main, Structure > CRACKED SUPPORT ANGLE LOCATED BS360 BTW STR27R TO STR28R AT EQUIPMENT ELECTRONIC COMP. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02. MEASUREMENT OF CRACK 0.210 INCH. - [SDR SWAA2026021362674](https://openairdocs.org/sdr/SWAA2026021362674.md): Rib · cracked · Jan 18, 2026 · N242WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACK LEADING EDGE RIB LOCATED LE HSS 105.26, RT HORIZONTAL STAB. REPLACED THE LEADING EDGE RIB AND FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 186A1001, SHEET 10, REV A. - [SDR SWAA2026021362382](https://openairdocs.org/sdr/SWAA2026021362382.md): Angle · cracked · Jan 17, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE BRACKET, BTW BS 540 - 560, LBL 7. REPLACED THE ANGLE BRACKET IAW SRM 51-10-02-0G, ITEM 9, AND DWG 212A1116, SHEET 1, REV -. MEASUREMENT OF CRACK: L: 0.782 INCH. - [SDR SWAA2026021362388](https://openairdocs.org/sdr/SWAA2026021362388.md): Nut Plate · cracked · Jan 17, 2026 · N242WN · Boeing 7377H4 · Wing, Attach Fittings > CRACKED RAIL NUT PLATES, INTERNAL CAVITY LEADING EDGE LOCATED OFSS 577, LT WING. REPLACED RAIL NUT PLATES AND FASTENERS IAW SRM 51-40-02, AND DWG 112A4402, SHEET 14, REV -. MEASUREMENT OF CRACK: 0.438 INCH. - [SDR SWAA2026021362387](https://openairdocs.org/sdr/SWAA2026021362387.md): Nut Plate · cracked · Jan 17, 2026 · N242WN · Boeing 7377H4 · Wing, Attach Fittings > CRACK RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS 734, RT WING. REPLACED THE RAIL NUT PLATES AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 112A4402, SHEET 14, REV-. - [SDR SWAA2026021262182](https://openairdocs.org/sdr/SWAA2026021262182.md): Rib · cracked · Jan 17, 2026 · N242WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACK ON THE INBD SIDE, LOWER CHORD INSPAR RIB HSS 120.30 IN THE RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON THE RIB IAW SRM 55-10-09-2R-5, REPAIR 5, FIGURE 205. - [SDR SWAA2026021262386](https://openairdocs.org/sdr/SWAA2026021262386.md): Nut Plate · cracked · Jan 17, 2026 · N242WN · Boeing 7377H4 · Wing, Attach Fittings > CRACKED RAIL NUT PLATES, INTERNAL CAVITY OF THE LEADING EDGE, OFSS449, LT WING. REPLACED THE NUT PLATES & FASTENERS IAW SRM 51-40-02, & DWG 112A4402, SHEET 40, REV A. - [SDR SWAA2026021262383](https://openairdocs.org/sdr/SWAA2026021262383.md): Bracket · cracked · Jan 17, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED BRACKET, BTWN BS 540 - 560, RBL 7. REPLACED THE BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 212A1116, SHEET 1, REV -. - [SDR SWAA2026021262385](https://openairdocs.org/sdr/SWAA2026021262385.md): Angle · cracked · Jan 17, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 663, RBL 8 IN THE AIR CONDITIONING BAY. REPLACED THE REPAIR ANGLE, BS 663, RBL 5 - RBL 30 IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, SRM 57-10-10-2R-5, REPAIR 5, DWG 111A10000, SHEET: 202, REV -, & MPM 52.1.1.1. - [SDR SWAA2026021262340](https://openairdocs.org/sdr/SWAA2026021262340.md): Web · corroded · Jan 17, 2026 · N242WN · Boeing 7377H4 · Wing Main, Frame Structure > CORROSION WEB INTERNAL CAVITY LEADING EDGE LOCATED OFSS276, RT WING. PERFORMED PERMANENT REPAIR ON WEB IN THE INTERNAL CAVITY LEADING EDGE IAW SRM 51-70-11-2R-0, REPAIR GENERAL, PARAGRAPH 4. - [SDR SWAA2026021262079](https://openairdocs.org/sdr/SWAA2026021262079.md): Support · corroded · Jan 16, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION SUPPORT ZEE, BS 727 - 767, RBL 21, WL 156 IN THE AFT CARGO BAY. MANUFACTURED & DRILLED A NEW SUPPORT ZEE IAW SRM 51-40-05, AND DWG 146A7502, SHEET 26, REV-. REPLACED THE SUPPORT ZEE & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, - [SDR SWAA2026021262175](https://openairdocs.org/sdr/SWAA2026021262175.md): Floor Support · corroded · Jan 16, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED FLOOR SUPPORT, BS 706 - 716, LBL 65, WL 202. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, DWG 144A7700, SHEET 144, REV B, & DWG 144A7730, SHEET 7, REV -. - [SDR SWAA2026021262177](https://openairdocs.org/sdr/SWAA2026021262177.md): Floor Support · corroded · Jan 16, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED FLOOR SUPPORT BTWN BS 706 - 716, RBL 65, WL 202. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, DWG 144A7700, SHEET 144, REV B, & DWG 144A7730, SHEET 7, REV -. - [SDR SWAA2026021262078](https://openairdocs.org/sdr/SWAA2026021262078.md): Support · corroded · Jan 16, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED SUPPORT ZEE, BS 727 - 847, LBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE IAW SRM 51-10-02, SRM 51-40-02, DWG 146A7502, SHEET 27, REV -, & DWG 145A7500, SHEET 85, REV A. - [SDR SWAA2026021262178](https://openairdocs.org/sdr/SWAA2026021262178.md): Door · corroded · Jan 16, 2026 · N242WN · Boeing 7377H4 · Fluid Service Doors > CORRODED WASTE SERVICE DOOR 145AL. PERFORMED A PERMANENT REPAIR ON THE WASTE SERVICE DOOR IAW SRM 52-40-01-2R-8, REPAIR 8. - [SDR SWAA2026021262082](https://openairdocs.org/sdr/SWAA2026021262082.md): Strap · corroded · Jan 16, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED STRAP, BS 887, RBL 10, WL 156 IN THE AFT CARGO BAY. REPLACED THE STRAP IAW SRM 51-10-02, SRM 51-40-02, AND DWG 14YA7500, SHEET 85, REV A. - [SDR SWAA2026021361875](https://openairdocs.org/sdr/SWAA2026021361875.md): Angle · cracked · Jan 15, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 294.5, S13L. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 141A1311, SHEET 1, REV C. - [SDR SWAA2026021361876](https://openairdocs.org/sdr/SWAA2026021361876.md): Tie Clip · cracked · Jan 15, 2026 · N242WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK TIE CLIP, BS 277, S10R. REPLACED THE TIE CLIP, MEASUREMENT OF DAMAGE: 1.650 INCH. REPLACED THE TIE CLIP, MEASURE OF DAMAGE: 1.650 INCH, & NO FOUND ALLOWABLE DAMAGE, IAW 51-40-02 AND DWG 141A1110, SHEET 18, REV-. - [SDR SWAA2026021261874](https://openairdocs.org/sdr/SWAA2026021261874.md): Web · cracked · Jan 15, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED INTERCOSTAL WEB, BS 294.5 - 303.9, S16L. PERFORMED A REPAIR CAT B ON THE INTERCOSTAL WEB IAW EA 26-153-00182-WIP1, & EA 26-153-00182. - [SDR SWAA2026021261873](https://openairdocs.org/sdr/SWAA2026021261873.md): Light · deteriorated · Jan 15, 2026 · N242WN · Boeing 7377H4 · Emergency Lighting > DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN (1KT). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING IAW AMM 33-51-15-400-802. - [SDR SWAA2026021261762](https://openairdocs.org/sdr/SWAA2026021261762.md): Shield · corroded · Jan 15, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED SHIELD WEB, BTW BS 492.4 - 500A, RBL 21, WL 156 IN THE FWD CARGO BAY. REPLACED THE SHIELD WEB AND FASTENERS IAW SRM 51-10-02 ITEM 9, AND DWG 143A0080, SHEET 23, REV -. - [SDR SWAA2026021261877](https://openairdocs.org/sdr/SWAA2026021261877.md): Floor Support · cracked · Jan 15, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED FLOOR SUPPORT BETWEEN BS 291.5 TO 294.5, S17R. REPLACED THE FLOOR SUPPORT AND & FASTENERS IAW SRM 51-10-02 ITEM 9, AND 141A8310, SHEET 25, REV-. - [SDR SWAA2026021361129](https://openairdocs.org/sdr/SWAA2026021361129.md): Access Panel · elongated · Jan 13, 2026 · N242WN · Boeing 7377H4 · Wing, Plate/Skin > ELONGATED HOLES ON ACCESS PANEL 561BB, LT WING. REPAIRED ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026021361132](https://openairdocs.org/sdr/SWAA2026021361132.md): Access Panel · elongated · Jan 13, 2026 · N242WN · Boeing 7377H4 · Wing, Plate/Skin > ELONGATED HOLES ON ACCESS PANEL 661BB, RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-9, REPAIR 9. - [SDR SWAA2026021260970](https://openairdocs.org/sdr/SWAA2026021260970.md): Frame · cracked · Jan 13, 2026 · N242WN · Boeing 7377H4 · Fuselage Main, Frame > CRACKED FRAME, BS 259.5, S8 - 9R IN THE FLIGHT DECK. PERFORMED A REPAIR, CAT B ON THE FRAME BS 259.5 BTWN STR 6 - 11R IAW EA 26-153-00146-WIP1. & EA 26-153-00146. - [SDR SWAA2026021260968](https://openairdocs.org/sdr/SWAA2026021260968.md): Rib · cracked · Jan 13, 2026 · N242WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACKED INSPAR RIB, HSS 120.30 AND 10 INCHES FROM REAR SPAR IN THE RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR OF THE RIB IAW SRM 55-10-09-2R-4, REPAIR 4, FIGURE 202. - [SDR SWAA2026021260969](https://openairdocs.org/sdr/SWAA2026021260969.md): Rib · cracked · Jan 13, 2026 · N242WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACKED INSPAR RIB, HSS 111.10 AND 28 INCHES FROM FRONT SPAR IN THE LT HORIZONTAL STAB. REPAIRED THE RIB LOCATED IAW SRM 55-10-09-2R-4, REPAIR 4. - [SDR SWAA2026021360792](https://openairdocs.org/sdr/SWAA2026021360792.md): Access Panel · delaminated · Jan 12, 2026 · N242WN · Boeing 7377H4 · Wing, Plate/Skin > DELAMINATED ACCESS PANEL 644BB AT RT WING. REPAIRED THE ACCESS PANEL 644BB IAW SRM 57-53-70-2R-5, REPAIR 5. - [SDR SWAA2026021260593](https://openairdocs.org/sdr/SWAA2026021260593.md): Stub Frame · cracked · Jan 12, 2026 · N242WN · Boeing 7377H4 · Fuselage Main, Frame > A CRACK INDICATION ON THE STUB FRAME, BTWN BS 294.5 - 296.5, S8R - S9R AT THE FWD GALLEY DOOR AREA. REPLACED THE STUB FRAME IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, & DWG 141A8370, SHEET 9, & SHEET 11, DWG 141A3310, SHEET 43, REV -, & DWG 141A8380, SHEET - [SDR SWAA2026021260791](https://openairdocs.org/sdr/SWAA2026021260791.md): Gusset · cracked · Jan 12, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED GUSSET, BS 500D, S19R IN THE FWD CARGO BAY. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A7902, SHEET 174, REV -. - [SDR SWAA2026021260595](https://openairdocs.org/sdr/SWAA2026021260595.md): Floor Support · cracked · Jan 12, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED FLOOR SUPPORT, BS 695, BL0. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A. - [SDR SWAA2026021260597](https://openairdocs.org/sdr/SWAA2026021260597.md): Crossbeam · cracked · Jan 12, 2026 · N242WN · Boeing 7377H4 · Fuselage Main, Structure > CRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REMOVED PROTECTIVE TREATMENT & PERFORMED GVI AND DID NOT FIND ADDITIONAL DAMAGE ON AREA IAW AMM 51-21-11-150-801, REPLACED THE CROSSBEAM AND FASTENERS IAW SRM 51-10-02, ITEM 9, AND DWG 143A0060, SHEET 46, REV - - [SDR SWAA2026021270218](https://openairdocs.org/sdr/SWAA2026021270218.md): Crossbeam · cracked · Jan 12, 2026 · N242WN · Boeing 7377H4 · Fuselage Main, Structure > CRACKED CROSSBEAM, BS 540, BL0 - LBL 24.75. REMOVED PROTECTIVE TREATMENT AND PERFORMED GVI & DID NOT FIND ADDITIONAL DAMAGE IN AREA IAW AMM 51-21-11-150-801, REPLACED THE CROSSBEAM AND FASTENERS IAW SRM 51-10-02 ITEM 9, & DWG 143A0060, SHEET 46, REV -. - [SDR SWAA2026021260591](https://openairdocs.org/sdr/SWAA2026021260591.md): Angle · cracked · Jan 12, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED FLOOR SUPPORT, BS 695, RBL24.75. REPLACED THE FLOOR SUPPPORT IAW SRM 51-40-02, & DWG 273A9110, SHEET 6, REV A. - [SDR SWAA2026021260594](https://openairdocs.org/sdr/SWAA2026021260594.md): Angle · cracked · Jan 12, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED FLOOR SUPPORT, BS 695, LBL24.75. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A. - [SDR SWAA2026021260598](https://openairdocs.org/sdr/SWAA2026021260598.md): Crossbeam · cracked · Jan 12, 2026 · N242WN · Boeing 7377H4 · Fuselage Main, Structure > CRACKED CROSSBEAM, BS 540, BL0 - RBL 24.75. REPLACED THE CROSSBEAM & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A0060, SHEET 46, REV -. - [SDR SWAA2026021259899](https://openairdocs.org/sdr/SWAA2026021259899.md): Scuff Plate · cracked · Jan 9, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED FWD CORNER OF THE SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1. PARAGRAPH 4.B, & BAC 5975. - [SDR SWAA2026021259900](https://openairdocs.org/sdr/SWAA2026021259900.md): Scuff Plate · cracked · Jan 9, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED AFT CORNER OF THE SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4.B, & BAC 5975. - [SDR SWAA2026021259901](https://openairdocs.org/sdr/SWAA2026021259901.md): Scuff Plate · cracked · Jan 9, 2026 · N242WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED AFT CORNER OF THE SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4.B, AND BAC 5975. Next page: https://openairdocs.org/aircraft/N242WN/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N242WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N242WN/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.