# Service difficulty reports: N7734H A list on [N7734H](https://openairdocs.org/aircraft/N7734H.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 SWAA2026091617558](https://openairdocs.org/sdr/SWAA2026091617558.md): Battery Pack · inoperative · Sep 12, 2026 · N7734H · Boeing 7377BD · Emergency Lighting > AFT RIGHT EMERGENCY EXIT LIGHT INOP R&R AFT LEFT EMERGENCY BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD. - [SDR SWAA2026060207582](https://openairdocs.org/sdr/SWAA2026060207582.md): Lamp · inoperative · May 29, 2026 · N7734H · Boeing 7377BD · Passenger Compartment Lighting > RH SIDEWALL LT ABOVE EMERGENCY EXIT INOP. REPLACED THE RH EMER EXIT WINDOW LIGHT LAMP IAW AMM 33-21-00. OPS CHECKED GOOD. - [SDR SWAA2026020364600](https://openairdocs.org/sdr/SWAA2026020364600.md): Access Panel · delaminated · Jan 25, 2026 · N7734H · Boeing 7377BD · Aerodynamic Fairings > DELAMINATED INTERNAL AREA ON ACCESS PANEL 193CR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-1, REPAIR 1. - [SDR SWAA2026020362164](https://openairdocs.org/sdr/SWAA2026020362164.md): Access Panel · delaminated · Jan 16, 2026 · N7734H · Boeing 7377BD · Nacelle/Pylon, Plate/Skin > DELAMINATED ACCESS PANEL 431DR ON THE LT PYLON. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026020359998](https://openairdocs.org/sdr/SWAA2026020359998.md): Tie Clip · cracked · Jan 9, 2026 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CRACK ON TIE CLIP LOCATED BS 380 AND STRINGER 8L ON FWD PASS CABIN. REPLACED TIE CLIP AND FASTENERS LOCATED BS 380 AND STRINGER 8L ON FWD PASS CABIN IAW SRM 51-40-02; SRM 51-10-02, ITEM 9 AND DWG 143A1110 SHEET 32, REV -. - [SDR SWAA2026020358926](https://openairdocs.org/sdr/SWAA2026020358926.md): Access Panel · elongated · Jan 6, 2026 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON THE ACCESS PANEL 192E OF BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9. - [SDR SWAA2026020358555](https://openairdocs.org/sdr/SWAA2026020358555.md): Vapor Barrier · no discrepancy · Jan 5, 2026 · N7734H · Boeing 7377BD · Fuselage Main, Bulkhead > CRACKED VAPOR BARRIER, BS 663, LBL 36. PERFORMED A DETAIL VISUAL INSPECTION OF THE AREA AND FOUND NOT A CRACK, ONLY THE REMAINS OF SEALANT IAW SRM 51-10-02-0G. CLEANED AND REMOVED THE REMAINS OF SEALANT IAW SOPM 20-30-03, REV 57. - [SDR SWAA2026020358554](https://openairdocs.org/sdr/SWAA2026020358554.md): Support Bracket · cracked · Jan 5, 2026 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CRACKED SUPPORT BRACKET, BS 540, LBL 6 IN THE AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET IAW SRM 51-10-02-0G-0, ITEM 9, MEASUREMENT OF CRACK: L=0.9360. - [SDR SWAA2026020358007](https://openairdocs.org/sdr/SWAA2026020358007.md): Angle · cracked · Jan 4, 2026 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 500C FWD OF STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 82, REV -. - [SDR SWAA2026020358003](https://openairdocs.org/sdr/SWAA2026020358003.md): Nut Plate · corroded · Jan 4, 2026 · N7734H · Boeing 7377BD · Fuselage Main, Attach Fittings > CORROSION ON THE INTERNAL CAVITY, FRONT SPAR OTBD RAIL NUT PLATE OFSS 460, LT WING. REPLACED RAIL NUT-PLATE IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 112A4402, SHEET 13, REV -. - [SDR SWAA2026020360964](https://openairdocs.org/sdr/SWAA2026020360964.md): Isolation Mount · debonded · Jan 4, 2026 · N7734H · Boeing 7377BD · Fuselage Main, Structure > DEBONDED ISOLATOR MOUNT, BS 540, S10 - 11R. THE ISOLATOR MOUNT WAS BONDED IAW DWG 144A2201, SHEET 7, REV B. - [SDR SWAA2026020358004](https://openairdocs.org/sdr/SWAA2026020358004.md): Nut Plate · cracked · Jan 4, 2026 · N7734H · Boeing 7377BD · Wing, Attach Fittings > CRACKED INTERNAL CAVITY FRONT SPAR OTBD RAIL NUT PLATE LT WING OFSS 332. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 13, REV -. - [SDR SWAA2026020358006](https://openairdocs.org/sdr/SWAA2026020358006.md): Nut Plate · cracked · Jan 4, 2026 · N7734H · Boeing 7377BD · Wing, Attach Fittings > CRACKED INTERNAL CAVITY, FRONT SPAR OTBD RAIL NUT PLATE, RT WING OFSS 594. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 14, REV-.. - [SDR SWAA2026020357892](https://openairdocs.org/sdr/SWAA2026020357892.md): Strap · corroded · Jan 3, 2026 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CORROED STRAP, BTWN BS 847 - 853, RBL 20, WL 155.8. REPLACED THE STRAP AND FASTENERS IAW SRM 51-10-02, ITEM 9, 51-40-02-0G-0, AND DWG 146A0081, SHEET 31, REV -. - [SDR SWAA2026020358000](https://openairdocs.org/sdr/SWAA2026020358000.md): Frame · cracked · Jan 3, 2026 · N7734H · Boeing 7377BD · Fuselage Main, Frame > CRACKED FRAME, BS 440, BTW S8 - 9R. PERFORMED A PERMANENT REPAIR ON THE FRAME IAW EA 26-153-00093-WIP1, EA 26-153-00093-WIP2, AND SUMMARY 26-153-00093. - [SDR SWAA2026020358001](https://openairdocs.org/sdr/SWAA2026020358001.md): Shield · corroded · Jan 3, 2026 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CORRODED SHIELD WEB, BTW BS 492.4 - 500A, RBL 22, WL 152.7, IN THE FWD CARGO BAY, REPLACED THE SHIELD WEB AND FASTENERS IAW SRM 51-40-02, AND DWG 143A0080, SHEET 23, REV-. - [SDR SWAA2026012957894](https://openairdocs.org/sdr/SWAA2026012957894.md): Frame · cracked · Jan 3, 2026 · N7734H · Boeing 7377BD · Fuselage Main, Frame > CRACKED FRAME, BS 440, S8 - 9L. REPAIRED THE FRAME IAW EA 26-153-00085-WIP1, 26-153-00085-WIP2, & SUMMARY 26-153-00085. - [SDR SWAA2026012957999](https://openairdocs.org/sdr/SWAA2026012957999.md): Frame · cracked · Jan 3, 2026 · N7734H · Boeing 7377BD · Fuselage Main, Frame > CRACKED FRAME, BS 400, S8 - 9R. REPAIRED THE FRAME IAW 26-153-00066-WIP1, 26-153-00066-WIP2, & SUMMARY 26-153-00066. - [SDR SWAA2026012957893](https://openairdocs.org/sdr/SWAA2026012957893.md): Frame · cracked · Jan 3, 2026 · N7734H · Boeing 7377BD · Fuselage Main, Frame > CRACKED FRAME, BS 400 S8 - 9L. REPAIRED THE FRAME, BS 400 S7 - 9L IAW EA 26-153-00091-WIP1, 26-153-00091-WIP2, & SUMMARY 26-153-00091. - [SDR SWAA2026012957886](https://openairdocs.org/sdr/SWAA2026012957886.md): Strap · corroded · Jan 3, 2026 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CORROSION STRAP LOCATED BETWEEN BS 842 - 847, RBL 20, WL 155.8 IN THE AFT CARGO BAY. REPLACED THE STRAP & FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 146A8340, SHEET 24, REV A. - [SDR SWAA2026012957884](https://openairdocs.org/sdr/SWAA2026012957884.md): Support Angle · corroded · Jan 3, 2026 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CORROSION ON SUPPORT ANGLE LOCATED BTW BS 767 - 787, RBL 21, WL 156.1 IN THE AFT CARGO COMPARTMENT. REPLACED SUPPORT ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 146A8123, SHEET 16, REV-. - [SDR SWAA2026012957889](https://openairdocs.org/sdr/SWAA2026012957889.md): Shield · corroded · Jan 3, 2026 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CORROSION SHIELD WEB LOCATED BS 767 - 794, RBL 21 AND WL156 AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DWG 146A0081, SHEET 31, REV -. - [SDR SWAA2026020357622](https://openairdocs.org/sdr/SWAA2026020357622.md): Support Angle · cracked · Jan 2, 2026 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, BS 291.5 - 294.5, STR 17R IN THE FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 141A8310, SHEET 25, REV -. - [SDR SWAA2026020357620](https://openairdocs.org/sdr/SWAA2026020357620.md): Angle · cracked · Jan 2, 2026 · N7734H · Boeing 7377BD · Aerodynamic Fairings > CRACKED ANGLE ON BODY FAIRING SUPPORT STRUCTURE BS 500D, STRINGER 19L, LOWER FUSELAGE. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 116A3010, SHEET 23, REV D. - [SDR SWAA2026012957750](https://openairdocs.org/sdr/SWAA2026012957750.md): Frame · cracked · Jan 2, 2026 · N7734H · Boeing 7377BD · Fuselage Main, Frame > CRACKED FRAME, BS 380 S8 - 9L. REPAIRED THE FRAME IAW EA 26-153-00092-WIP1, 26-153-00092-WIP2, & SUMMARY 26-153-00092. - [SDR SWAA2026012957626](https://openairdocs.org/sdr/SWAA2026012957626.md): Frame · cracked · Jan 2, 2026 · N7734H · Boeing 7377BD · Fuselage Main, Frame > CRACKED FRAME, BS 360 BTW S8 - 9R. REPAIRED THE FRAME IAW EA 26-153-00109-WIP1, 26-153-00109-WIP2, & SUMMARY 26-153-00109. - [SDR SWAA2026020358541](https://openairdocs.org/sdr/SWAA2026020358541.md): Access Panel · damaged · Dec 31, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON ACCESS PANEL 194CL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9. - [SDR SWAA2026020358542](https://openairdocs.org/sdr/SWAA2026020358542.md): Access Panel · damaged · Dec 31, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON ACCESS PANEL 194CR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8. - [SDR SWAA2026020358543](https://openairdocs.org/sdr/SWAA2026020358543.md): Access Panel · damaged · Dec 31, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON ACCESS PANEL 195AL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCES PANEL IAW SRM 51-70-05-2R-9, REPAIR 9. - [SDR SWAA2026020358544](https://openairdocs.org/sdr/SWAA2026020358544.md): Access Panel · damaged · Dec 31, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON ACCESS PANEL 195AR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9. - [SDR SWAA2026020358545](https://openairdocs.org/sdr/SWAA2026020358545.md): Access Panel · damaged · Dec 31, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON ACCESS PANEL 194HL BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8. - [SDR SWAA2026020358548](https://openairdocs.org/sdr/SWAA2026020358548.md): Access Panel · damaged · Dec 31, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES OF ACCESS PANEL 194DL WING TO BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8. - [SDR SWAA2026020358546](https://openairdocs.org/sdr/SWAA2026020358546.md): Access Panel · damaged · Dec 31, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON ACCESS PANEL 195BL OF THE BODY FAIRING FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9. - [SDR SWAA2026020358547](https://openairdocs.org/sdr/SWAA2026020358547.md): Access Panel · damaged · Dec 31, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON ACCESS PANEL 195BR, BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-9, REPAIR 9. - [SDR SWAA2026020357122](https://openairdocs.org/sdr/SWAA2026020357122.md): Access Panel · damaged · Dec 31, 2025 · N7734H · Boeing 7377BD · Wing, Plate/Skin > ELONGATED HOLES ON THE ACCESS PANEL 661BB AT TRAILING EDGE, RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING T/E IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026020356928](https://openairdocs.org/sdr/SWAA2026020356928.md): Access Panel · damaged · Dec 30, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-9, REPAIR 9. - [SDR SWAA2026020356929](https://openairdocs.org/sdr/SWAA2026020356929.md): Access Panel · damaged · Dec 30, 2025 · N7734H · Boeing 7377BD · Aerodynamic Fairings > ELONGATED HOLES ON ACCESS PANEL 193CR BODY FAIRING, FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-8, REPAIR 8. - [SDR SWAA2026020356927](https://openairdocs.org/sdr/SWAA2026020356927.md): Access Panel · damaged · Dec 30, 2025 · N7734H · Boeing 7377BD · Wing, Plate/Skin > ELONGATED HOLES ON ACCESS PANEL 561BB AT THE RT WING T/E. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10. - [SDR SWAA2026012956608](https://openairdocs.org/sdr/SWAA2026012956608.md): Skin Panel · cracked · Dec 30, 2025 · N7734H · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin > CRACK INDICATION FOUND ON THE LT HORIZONTAL STAB LOWER SKIN PANEL HSS 193.9 RIB & 16 INCHES FROM FRONT SPAR, INBD SIDE OF RIB. CRACK LENGTH: 0.900 INCH. REPAIRED HORIZONTAL STAB LOWER SKIN IAW SRM 51-40-02, SRM 55-10-01-2R-11, REPAIR 11. - [SDR SWAA2026020356605](https://openairdocs.org/sdr/SWAA2026020356605.md): Wire · deteriorated · Dec 29, 2025 · N7734H · Boeing 7377BD · Light System Wiring > DETERIORATED ELECTRICAL WIRING OF EMERGENCY EXIT LIGHT ON CEILING PANEL 231YDC. REPLACED EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-802, PERFORMED AN OPS TEST. TESTED OK. - [SDR SWAA2026020356601](https://openairdocs.org/sdr/SWAA2026020356601.md): Stub Frame · cracked · Dec 29, 2025 · N7734H · Boeing 7377BD · Fuselage Main, Frame > CRACK INDICATION ON STUB FRAME, BETWEEN BS 294.5 - 296.5, S8 - 9R IN THE FWD GALLEY DOOR AREA. CRACK LENGTH: 0.875 IN. REPLACED THE STUB FRAME IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, & DWG 141A8370, SHEET 10, REV D. - [SDR SWAA2026012956593](https://openairdocs.org/sdr/SWAA2026012956593.md): Scuff Plate · cracked · Dec 29, 2025 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CRACK ON THE FWD CORNER OF THE SCUFF PLATE IN FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2026012956602](https://openairdocs.org/sdr/SWAA2026012956602.md): Scuff Plate · cracked · Dec 29, 2025 · N7734H · Boeing 7377BD · Fuselage Miscellaneous Structure > CRACK ON THE FWD CORNER OF THE SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975. - [SDR SWAA2025091013319](https://openairdocs.org/sdr/SWAA2025091013319.md): Sensor · faulty · Sep 10, 2025 · N7734H · Boeing 7377BD · Trailing Edge Flap Control System > WITH FLAP 1 SELECTED FLAPS REMAINED AT 0 AND WOULD NOT EXTEND. FOLLOWED QRH. ALTERNATE FLAPS WERE USED AND PERFORMED 0 FLAP LANDING<[01] TS AND FOUND FC 27-53251 #2 SKEW IN FSEU; AHM RECORDED A 50 UNIT DIFFERENCE FOR PAIR 2/7. ACMS SHOWED ERRATIC MOTION ON #2 - [SDR SWAA2025090209832](https://openairdocs.org/sdr/SWAA2025090209832.md): Seat · out of adjust · Aug 29, 2025 · N7734H · Boeing 7377BD · Passenger Compartment Equipment > SEAT 11 D RECLINES TOO FAR INTO EXIT ROW, SEAT 11D ADJUSTED RECLINE LOCK PER AMM 25-22-00. - [SDR SWAA2025061281103](https://openairdocs.org/sdr/SWAA2025061281103.md): Lens · missing · Jun 12, 2025 · N7734H · Boeing 7377BD · Emergency Lighting > R/H OVERWING EMER EXIT LIGHT LENS MISSING.<[01] REPLACED MISSING LIGHT COVER ON R/H SIDE OVERWING EMER EXIT PER AMM 33-51-01. - [SDR SWAA2025041523718](https://openairdocs.org/sdr/SWAA2025041523718.md): Bracket · cracked · Apr 11, 2025 · N7734H · Boeing 7377BD · Powerplant System > #2 ENG. HIGH STAGE REGULATOR BRACKET HAS A CRACK. - [SDR SWAA2024120574335](https://openairdocs.org/sdr/SWAA2024120574335.md): Power Supply · depleted · Dec 5, 2024 · N7734H · Boeing 7377BD · Emergency Lighting > AIRCRAFT ON GROUND POWER EMER EXIT LIGHTS IN ARMED POSITION HALF THE EMERGENCY EXIT LIGHTS ARE ON.<[01] RECHARGED & RESET FWD POWER SUPPLY L&R PER AMM 33-51-06. OPS CHK OK. - [SDR SWAA2024110856880](https://openairdocs.org/sdr/SWAA2024110856880.md): Overheat Sensor · faulted · Nov 4, 2024 · N7734H · Boeing 7377BD · Overheat Detection > LEFT WING BODY OVERHEAT LIGHT ILLUMINATED IN CLIMB THEN EXTINGUISHED WHEN ENGINE 1 BLEED SWITCH TURNED OFF<[01] REPLACED M1761 OVHT DETECTOR ON #1 ENGINE FWD STRUT CAVITY IAW AMM 26-18-02; OPS CHECKS GOOD; FAULT CLEARED - [SDR SWAA2024091236274](https://openairdocs.org/sdr/SWAA2024091236274.md): Bracket · cracked · Sep 11, 2024 · N7734H · Boeing 7377BD · Passenger/Crew Doors > DOOR PANEL 834 DZ AFT MOUNTING BRACKET CRACKED. REPLACED AFT SVC DOOR PANEL 834 DZ AFT MOUNTING BRACKET PER AMM 20-50-11. REPLACED AFT ENTRY DOOR PANEL 834 DZ PER AMM 52-13-31. Next page: https://openairdocs.org/aircraft/N7734H/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 = 'N7734H' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N7734H/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.