# Service difficulty reports: N7730A, cancelled Jun 5, 2026 A list on [N7730A, cancelled Jun 5, 2026](https://openairdocs.org/deregistered/N7730A-2026-06-05.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 5 · 213 reports - [SDR SWAA2025010683034](https://openairdocs.org/sdr/SWAA2025010683034.md): Girt Bar · loose · Jan 4, 2025 · N7730A · Boeing 7377BD · Emergency Equipment > FORWARD SERVICE DOOR RIGHT(REAR) GIRT BAR CLIP LOOSE.<[01] RESECURED FORWARD SERVICE DOOR RIGHT GIRT BAR CLIP PER MM 25-66-01 - [SDR SWAA2024122680881](https://openairdocs.org/sdr/SWAA2024122680881.md): Lens · missing · Dec 25, 2024 · N7730A · Boeing 7377BD · Emergency Lighting > MAIN ENTRY DOOR EXIT SIGN ON THE FORWARD BULKHEAD IS MISSING.<[01] INSTALLED EXIT SIGN LENS IAW AMM 33-51-01. - [SDR SWAA2024100744957](https://openairdocs.org/sdr/SWAA2024100744957.md): Battery Pack · inoperative · Oct 4, 2024 · N7730A · Boeing 7377BD · Emergency Lighting > PASSENGER CABIN; EMERGENCY LIGHT AT 6DEF INOP.<[01] R&R OVERHEAD AREA LIGHT ASSEMBLY (EMERGENCY LIGHT HOUSING) AT SEAT 6DEF REF AMM 33-51-03; R&R BATTERY PACK M1674 & ASSOCIATED POWER SUPPLY CHARGER IAW AMM 33-51-06. - [SDR SWAA2024100745933](https://openairdocs.org/sdr/SWAA2024100745933.md): Charger · inoperative · Oct 4, 2024 · N7730A · Boeing 7377BD · Emergency Lighting > PASSENGER CABIN; EMERGENCY LIGHT AT 6DEF INOP.<[01] R&R OVERHEAD AREA LIGHT ASSEMBLY (EMERGENCY LIGHT HOUSING) AT SEAT 6DEF REF AMM 33-51-03; R&R BATTERY PACK M1674 & ASSOCIATED POWER SUPPLY CHARGER IAW AMM 33-51-06. - [SDR SWAA2024090934839](https://openairdocs.org/sdr/SWAA2024090934839.md): Attach Fitting · loose · Sep 6, 2024 · N7730A · Boeing 7377BD · Emergency Equipment > R1 SLIDE FELL OUT BUSTLE<[01] INPECTED R1 DOOR SLIDE & FOUND GIRT BAR ATTACHMENT TO BE LOOSE. RESECURED AS REQUIRED PER AMM 25-66-01. A/C OK FOR SERVICE. - [SDR SWAA2024090934827](https://openairdocs.org/sdr/SWAA2024090934827.md): Girt Bar · out of adjust · Sep 6, 2024 · N7730A · Boeing 7377BD · Emergency Equipment > DOOR 1R GRIT BAR HOLDER IS LOOSE<[01] ADJUSTED GRIT BAR HOLDER IAW AMM 25-66-00 - [SDR SWAA2024052489513](https://openairdocs.org/sdr/SWAA2024052489513.md): Slide · out of position · May 23, 2024 · N7730A · Boeing 7377BD · Escape Slide > AFT LEFT SERVICE DOOR SLIDE OUT OF POSITION<[01] REPACKED SIDE IAW MT 725-62-01 AC OK FOR SERVICE - [SDR SWAA2024031964415](https://openairdocs.org/sdr/SWAA2024031964415.md): Slide · dislodged · Mar 16, 2024 · N7730A · Boeing 7377BD · Escape Slide > FAULT RAISED TO ADD MX TASK MT 725-61-06 FOR PREVIOUSLY WORKED FAULT' L1 DOOR SLIDE DISLODGED'; REF TTQ8Q00S5R6W (LP 2721617)<[01] CW MT 725-61-06 - [SDR SWAA2024031864410](https://openairdocs.org/sdr/SWAA2024031864410.md): Slide · dislodged · Mar 15, 2024 · N7730A · Boeing 7377BD · Escape Slide > CREW REPORTS L1 SLIDE DISLODGED<[01] RESECURED L1 DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06;[02] UPDATING CORRECTIVE ACTION ONLY AS PER TELECOM REQUEST TO ADD FAULT REF FOR ADDED MT 725-61-06 PERFORMED ON TTG8Q00S5REE BY E90554 - [SDR SWAA2024021552573](https://openairdocs.org/sdr/SWAA2024021552573.md): Handle · loose · Feb 15, 2024 · N7730A · Boeing 7377BD · Service Doors > FWD SVC DOOR HANDLE LOOSE<[01] CHECKED INSTALLATION OF INTERIOR DOOR HANDLE. HANDLE IS SECURED PER AMM 52-41-31-020-010 - [SDR SWAA2024012443963](https://openairdocs.org/sdr/SWAA2024012443963.md): Lamp · burned out · Jan 23, 2024 · N7730A · Boeing 7377BD · Emergency Lighting > R1 DOOR EXTERIOR EMER LIGHT BURNT OUT<[01] RELAMPED IAW AMM 33-51-04 - [SDR SWAA2024010336287](https://openairdocs.org/sdr/SWAA2024010336287.md): Light · inoperative · Dec 30, 2023 · N7730A · Boeing 7377BD · Emergency Lighting > FWD PASSENGER CABIN EMERGENCY LIGHT AT CEILING PANEL INOP<[01] RELAMPED FWD PASSENGER CABIN EMERGENCY LIGHT AT CEILING PANEL AND PERFORMED GOOD TEST PER AMM 33-51-03-960-801.;[02] VERIFIED CORRECTIVE ACTION 1.
VERIFIED MEASUREMENT TABLE.
JOB COMPLETE. - [SDR SWAA2024010331938](https://openairdocs.org/sdr/SWAA2024010331938.md): Scuff Plate · cracked · Dec 14, 2023 · N7730A · Boeing 7377BD · Cargo Compartments > FCB FWD CORNER SCUFF PLATE IS CRACKED<[01] VERIFIED STEPS 1;2 COMPLETE.;[02] REMOVED; REPAIRED; AND REINSTALED CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1.;[03] VERIFIED JOB COMPLETE

VERIFIED MEASUREMENT TABLE - [SDR SWAA2024010331939](https://openairdocs.org/sdr/SWAA2024010331939.md): Scuff Plate · cracked · Dec 14, 2023 · N7730A · Boeing 7377BD · Cargo Compartments > ACB AFT CORNER SCUFF PLATE IS CRACKED<[01] VERIFIED STEPS 1;2; COMPLETE.;[02] REMOVED; REPAIRED; AND REINSTALED CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1.;[03] VERIFIED JOB COMPLETE

VERIFIED MEASUREMENT TABLE - [SDR SWAA2024010330244](https://openairdocs.org/sdr/SWAA2024010330244.md): Strip · corroded · Dec 10, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous Structure > CAPSTRIPS IN AFT CARGO BAY ARE CORRODED-ALL ON THE R/H SIDE AND FROM BS727 TO BS 847 ON THE L/H SIDE<[01] THE STRUCTURAL ITEMS DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES. THEREFORE; MUST BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02-0G-0 PARAGRAPH 9

REPL - [SDR SWAA2024010328981](https://openairdocs.org/sdr/SWAA2024010328981.md): Panel · cracked · Dec 7, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous Structure > PANEL BREAK CRACKED BS 540 LBL 1 WL 208<[01] REMOVED AND REPLACED PANEL BREAK BS540; LBL1; WL208;
IAW SRM 51-40-02 & DWG 143A0060;[02] COMPLETED. - [SDR SWAA2024010328982](https://openairdocs.org/sdr/SWAA2024010328982.md): Closeout Panel · cracked · Dec 7, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous Structure > CLOSEOUT PANEL P/N 232A1432-7 BELOW PANEL 211AC IS CRACKED<[01] REMOVED AND REPLACED PANEL P/N 232A1432-7 BELOW PANEL 211AC IAW SOPM 20-50-01;[02] JOB COMPLETE. - [SDR SWAA2024010326872](https://openairdocs.org/sdr/SWAA2024010326872.md): Frame · cracked · Dec 2, 2023 · N7730A · Boeing 7377BD · Fuselage Main, Frame > CRACKED UPPER FRAME AT FWD ENTRY DOORWAY; BS 312; WL 282; IB RADIUS; MARKED.<[01] NDT HFEC SURFACE INSPECTED AREA IAW 737 NDTM PART 6 51-00-00 PROC 23. CRACK NOTED;.5' LONG; MARKED DIRECTION AND END OF CRACK.
EQUIP USED: NORTEC 600 IS0000680 DUE 05/24;[02] - [SDR SWAA2024010326873](https://openairdocs.org/sdr/SWAA2024010326873.md): Stub Frame · cracked · Dec 2, 2023 · N7730A · Boeing 7377BD · Fuselage Main, Frame > CRACKED STUB FRAME AT THE FWD GALLEY DOORWAY; BS 294.5; RBL 54; WL 208.1; IB FLANGE MARKED.<[01] NDT HFEC SURFACE INSPECTED AREA IAW 737 NDTM PART 6 51-00-00 PROC 23. CRACK NOTED;.75' LONG; DIRECTION AND END OF CRACK MARKED.
EQUIP USED: NORTEC 600 IS00006 - [SDR SWAA2024010326870](https://openairdocs.org/sdr/SWAA2024010326870.md): Floorbeam · cracked · Dec 1, 2023 · N7730A · Boeing 7377BD · Fuselage Main, Floor Beam > FLOOR BEAM CRACKED AT FASTENER HOLE BS 312 RBL 31 WL 208<[01] ACCOMPLISHED HFEC SURFACE SCAN OF SUSPECTED AREA IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. NO CRACKS NOTED.

EQUIPMENT USED: NORTEC 600 ID: ATS2353 CAL DUE: 01/2024;[02] VERIFIED COMP - [SDR SWAA2024010326871](https://openairdocs.org/sdr/SWAA2024010326871.md): Floor Support · cracked · Dec 1, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous Structure > INTERCOSTAL CRACKED AT FASTENER HOLE BS 277 - 295 BL0 WL 208<[01] REMOVED AND REPLACED INTERCOSTAL BS 277 - 295 BL0 WL 208 I.A.W SRM 51-10-02-0G-0 PAR 9.C. SRM 51-40-02-0G-0 AND DWG 141A5400.;[02] VERIFIED CORRECTIVE ACTION STEPS AND MEASUREMENT TABLE. - [SDR SWAA2024010326868](https://openairdocs.org/sdr/SWAA2024010326868.md): Floor Support · corroded · Dec 1, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL UPPER FLANGE BS 294-312 LBL 12 WL 208<[01] REMOVED AND REPLACED NEW INTERCOSTAL ON BS 294 - BS 312 LBL 12 IAW SRM 51-40-02 AND DWG 141A5600;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE. - [SDR SWAA2024010326650](https://openairdocs.org/sdr/SWAA2024010326650.md): Door · corroded · Dec 1, 2023 · N7730A · Boeing 7377BD · Service Doors > AFT PASSENGER COMPARTMENT MOPSILL AT THE AFT SERVICE DOOR HAS CORROSION AT BS 967+9; RBL 47; BS 967+9 - +14 RBL 45; 987 RBL 48 WL 208<[01] FAULT RESOLVED ON TTG8Q00PYVBU;[02] VERIFIED CORRECTIVE ACTION AND MEASUREMENT TABLE - [SDR SWAA2024010326154](https://openairdocs.org/sdr/SWAA2024010326154.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > AFT FLOOR PANEL 241AAF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETE. - [SDR SWAA2024010326151](https://openairdocs.org/sdr/SWAA2024010326151.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > AFT FLOOR PANEL 241ACF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 241ACF UPPER SKIN HAD PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED FLOOR PANEL 241ACF IS REPAIRED SRM 53-00-50-2R-1;[03] WORKSCOPE IS COMPLETE. - [SDR SWAA2024010326152](https://openairdocs.org/sdr/SWAA2024010326152.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > AFT FLOOR PANEL 241ADF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETE. - [SDR SWAA2024010326156](https://openairdocs.org/sdr/SWAA2024010326156.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AREAS OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 242VF IAW SRM 53-00-50-2R-1.;[02] VERIFIED REPAIR OF UPPER SKIN OF FLOOR PANEL 242VF PER SRM 53-00-50-2R-1;[03] WORKSCOPE COMPL - [SDR SWAA2024010326157](https://openairdocs.org/sdr/SWAA2024010326157.md): Floor Panel · deformed · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > AFT FLOOR PANEL 242WF FWD I/B CORNER IS SOFT.<[01] REPAIRED FWD I/B CORNER ON AFT FLOOR PANEL 242WF IAW SRM 53-00-50-2R-6.;[02] VERIFIED REPAIR OF FLOOR PANEL 242WF IAW SRM 53-00-50-2R-6.;[03] WORKSCOPE COMPLETE. - [SDR SWAA2024010326168](https://openairdocs.org/sdr/SWAA2024010326168.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > FWD FLOOR PANEL 221FF UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] REPAIRED DAMAGED UPPER SKIN ON FWD FLOOR PANEL 221FF IAW SRM 53-00-50-2R-1.;[02] VERIFIED UPPER SKIN OF FLOOR PANEL 221FF REPAIRED PER SRM 53-00-50-2R-1;[03] WORKSCOPE COMPLETE. - [SDR SWAA2024010326161](https://openairdocs.org/sdr/SWAA2024010326161.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > FWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221GF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB - [SDR SWAA2024010326169](https://openairdocs.org/sdr/SWAA2024010326169.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > FWD FLOOR PANEL 222A UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222A UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB CO - [SDR SWAA2024010326170](https://openairdocs.org/sdr/SWAA2024010326170.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > FWD FLOOR PANEL 222B UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222B UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB CO - [SDR SWAA2024010326163](https://openairdocs.org/sdr/SWAA2024010326163.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB - [SDR SWAA2024010326173](https://openairdocs.org/sdr/SWAA2024010326173.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > FWD FLOOR PANEL 231CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB - [SDR SWAA2024010326164](https://openairdocs.org/sdr/SWAA2024010326164.md): Floor Panel · pulled · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Floor Panel > FWD FLOOR PANEL 232AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 232AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB - [SDR SWAA2024010326491](https://openairdocs.org/sdr/SWAA2024010326491.md): Channel · corroded · Nov 30, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous Structure > AFT SERVICE DOOR MOPSILL HAS CORROSION ON UPPER FLANGE; BS 978; RBL 50; WL 209<[01] ASD MOPSILL WILL BE REMOVED AND REPLACED ON FAULT#TTG8Q00PYVBU;[02] VERIFIED ITEM 1.;[03] CARD COMPLETE - [SDR SWAA2024010326492](https://openairdocs.org/sdr/SWAA2024010326492.md): Skin · cracked · Nov 30, 2023 · N7730A · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin > DURING INSPECTION ON TTG8Q00AGQLW; FOUND 1EA CRACK ON L/H HORIZONTAL STABILIZER LOWER SKIN AT STATION 193.90; 18' FROM FWD EDGE L: 1' MARKED<[01] REMOVED THE DAMAGED PART ON LH HORIZONTAL STABILIZER LOWER SKIN STA 193.90 18' FROM FWD EDGE; CUT OUT DIMENSIONS - [SDR SWAA2024010325975](https://openairdocs.org/sdr/SWAA2024010325975.md): Pressure Deck · cracked · Nov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Main, Structure > .5' CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 LBL 41. CORRECTION ==.5' CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 RBL 41<[01] CORRECTION TO TITLE:
INCORRECTLY PUT 'LBL 41'
CORRECT LOCATION IS RBL 41.;[02] REPAIRED HORIZONTAL PRESSURE D - [SDR SWAA2024010325978](https://openairdocs.org/sdr/SWAA2024010325978.md): Frame · corroded · Nov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Main, Frame > AFT PASSENGER COMPARTMENT FLOOR FRAME HAS CORROSION AT FASTENER; BS 986.5; RBL 44; WL 208<[01] ACCOMPLISHED CORROSION REPAIR PER SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE. - [SDR SWAA2024010325977](https://openairdocs.org/sdr/SWAA2024010325977.md): Web · corroded · Nov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous Structure > AFT PASSENGER COMPARTMENT 1016 WEB FLOOR STRUCTURE HAS CORROSION AT BS 1016+13; LBL 5; WL 208<[01] AFT PASSENGER COMPARTMENT 1016 WEB FLOOR STRUCTURE HAS CORROSION AT BS 1016+13; LBL 5; WL 208 WAS REPAIRED IAW EA 23-153-03550;[02] VERIFIED CORRECTIVE ACTION EN - [SDR SWAA2024010325979](https://openairdocs.org/sdr/SWAA2024010325979.md): Channel · corroded · Nov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous Structure > AFT PASSENGER COMPARTMENT MOPSILL AT THE AFT SERVICE DOOR HAS CORROSION AT BS 967+14; RBL 47; WL 208<[01] REMOVED AND REPLACED MOPSILL AT BS 907 - 1006 RBL 47; WL 208;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE. - [SDR SWAA2024010325976](https://openairdocs.org/sdr/SWAA2024010325976.md): Strap · corroded · Nov 29, 2023 · N7730A · Boeing 7377BD · Fuselage Miscellaneous Structure > AFT PASSENGER COMPARTMENT 1016 TENSION STRAP HAS CORROSION AT BS 1016+11; LBL 3; WL 208<[01] VERIFIED MEASUREMENTS TABLE.;[02] VERIFIED FAULT IS COMPLETED - [SDR SWAA2023020297730](https://openairdocs.org/sdr/SWAA2023020297730.md): Sign · out of adjust · Feb 2, 2023 · N7730A · Boeing 7377BD · Emergency Lighting > 11 CB LOWER EXIT SIGN MISSING DIRECTIONAL ARROW.<[01] REPLACED EXIT SIGN REF AMM 33-51-01;[02] INSPECTED - [SDR SWAA2023020297723](https://openairdocs.org/sdr/SWAA2023020297723.md): Handle · loose · Feb 2, 2023 · N7730A · Boeing 7377BD · Passenger/Crew Doors > AFT ENTRY DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED AFT ENTRY DOOR ASSIST HANDLE NUTS REF AMM 52-41-31;[02] COMPLIED WITH - [SDR SWAA2023010587314](https://openairdocs.org/sdr/SWAA2023010587314.md): Handle · detached · Jan 3, 2023 · N7730A · Boeing 7377BD · Passenger/Crew Doors > FWD ENTRY DOOR ASSIST HANDLE CAME OFF. REPLACED FWD ENTRY DOOR ASSIST HANDLE IN APPLICABLE STEPS OF AMM 52-11-31. OPS CHECK GOOD - [SDR SWAA2022090750280](https://openairdocs.org/sdr/SWAA2022090750280.md): None · inoperative · Sep 5, 2022 · N7730A · Boeing 7377BD · Emergency Lighting > FWD LH MULTIPLE EMERGENCY LIGHT NEAR MAIN ENTRY DOOR FWD EXTERIOR ENTRY LIGHT INOP FWD ENTRY LIGHT INTERIOR LOWER ENTRY LIGHT INOP FWD LH OVERHEAD BIN LIGHT INOP / [01] REMOVED AND REPLACED LH FWD BATTERY PACK IAW AMM 33-51-06. ALL LIGHTS OPS CHECK GOOD. - [SDR SWAA2022080237518](https://openairdocs.org/sdr/SWAA2022080237518.md): Lens · missing · Aug 2, 2022 · N7730A · Boeing 7377BD · Emergency Lighting > EMER EXIT LENS MISSING / [01] REPLACED EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-03 - [SDR SWAA2022052309689](https://openairdocs.org/sdr/SWAA2022052309689.md): Holder · loose · May 19, 2022 · N7730A · Boeing 7377BD · Galley Doors > GALLEY DOOR GIRT BAR FORWARD HOLDER LOOSE / [01] RESECURED PER SIP - [SDR SWAA2022052310326](https://openairdocs.org/sdr/SWAA2022052310326.md): Holder · loose · May 19, 2022 · N7730A · Boeing 7377BD · Galley Doors > GALLEY DOOR GIRT BAR FORWARD HOLDER LOOSE / [01] RESECURED PER SIP - [SDR SWAA2022021670864](https://openairdocs.org/sdr/SWAA2022021670864.md): Light · failed · Feb 10, 2022 · N7730A · Boeing 7377BD · Emergency Lighting > FLIGHT DECK EMERGENCY DOME LIGHT DOES NOT ILLUMINATE DURING EMERGENCY LIGHT OPERATIONAL TEST. / [01] RE-LAMPED FLIGHT DECK EMERGENCY DOME LIGHT PER AMM 33-14-00-00-801 AND AMM 33-14-00-400-801. OPS CHECK GOOD.;[02] VERIFIED CORRECTIVE ACTION 1; OPS CHECK GOOD. Next page: https://openairdocs.org/deregistered/N7730A-2026-06-05/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 = 'N7730A' AND deregistration_id = 'N7730A-2026-06-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N7730A-2026-06-05/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.