# Service difficulty reports: N7750A

A list on [N7750A](https://openairdocs.org/aircraft/N7750A.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 6 · 257 reports

- [SDR SWAA2026100247358](https://openairdocs.org/sdr/SWAA2026100247358.md): Igniter · failed · Sep 28, 2026 · N7750A · Boeing 7377BD · Ignition System
  > NR 1 ENGINE FUEL FLOW, LI LIGHT OFF, LEFT IGNITION SELECTED NR 1 ENGINE FUEL FLOW LI LIGHT OFF LEFT IGNITION SELECTED 05 - OK TO CONTINUE PER MEL 74-1-02 XA. PERFORMED IGNITION SYSTEM AUDIBLE TEST PER AMM 74-00-00 NO AUDIBLE IGNITION ON L IGNITER ON CH A & CH
- [SDR SWAA2026091175486](https://openairdocs.org/sdr/SWAA2026091175486.md): Panel · cracked · Sep 7, 2026 · N7750A · Boeing 7377BD · Turbine Engine Combustion Section
  > NR 2 ENG AT APPROX 9 O'CLOCK POSITION HAS A AXIAL CRACK IN THE OUTER LINE THAT GOES ACROSS 4 PANELS WITH A CIRCUMFERENTIAL CRACK THAT CONNECTS.THE CIRCUMFERENTIAL CRACK IS LONGER THAN 2 DILUTION LANDS. OK TO CONTINUE PER TLD 72-00-00-200-805-F00-NG-03. 25 CYC
- [SDR SWAA2026072022338](https://openairdocs.org/sdr/SWAA2026072022338.md): Web · cracked · Jul 14, 2026 · N7750A · Boeing 7377BD · Engine Thrust Reverser
  > NUMBER 2 ENGINE INBD THRUST REVERSER HAD A CRACK AT FWD TORQUE WEB, STOW SENSOR ROD CUT OUT LOWER RADIUS. R & R NR 2 ENGINE INBD THRUST REVERSER IAW AMM 78-31-01.
- [SDR SWAA2026032682363](https://openairdocs.org/sdr/SWAA2026032682363.md): Light · inoperative · Mar 23, 2026 · N7750A · Boeing 7377BD · Emergency Lighting
  > RIGHT OVERWING DOOR WINDOW LIGHT IS INOP RIGHT OVERWING DOOR WINDOW IS INOP<[01] RE-LAMPED RT OVERWING EXIT LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.;[02] 02 - INSPECTED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]
- [SDR SWAA2025122253383](https://openairdocs.org/sdr/SWAA2025122253383.md): Hook And Loop · missing · Dec 17, 2025 · N7750A · Boeing 7377BD · Escape Slide
  > PAX CABIN LT AFT DOOR SLIDE LOWER COVER IS CHAFING AGAINST WITH THE DOOR SCUFF PLATE WHEN THE DOOR MOVED TO CLOSE POSITION. PERFORMED VISUAL INSPECTION AND FOUND MISSING HOOK AND LOOP STRIP. INSTALLED THE HOOK AND LOOP ON PAX DOOR SLIDE LOWER COVER IAW SOPM
- [SDR SWAA2025121942006](https://openairdocs.org/sdr/SWAA2025121942006.md): Web · cracked · Dec 2, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BTW BS 927 - 947, S25R IN THE AFT CARGO BAY. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q018WZ23.
- [SDR SWAA2025122238619](https://openairdocs.org/sdr/SWAA2025122238619.md): Stringer · corroded · Nov 21, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27R BTW BS 360 TO BS 380 WL 156.1 IN E/E BAY. PERFORMED PERMANENT REPAIR(CATEGORY A) ON STRINGER 27R LOCATED BTW BS 360 TO BS 400 WL 156.1 AT ELECTRICAL AND ELECTRONIC COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 PARAGRAPH 4.
- [SDR SWAA2025122238192](https://openairdocs.org/sdr/SWAA2025122238192.md): Floor Panel · damaged · Nov 20, 2025 · N7750A · Boeing 7377BD · Fuselage Floor Panel
  > ELONGATED HOLES ON FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT.
- [SDR SWAA2025122238199](https://openairdocs.org/sdr/SWAA2025122238199.md): Shear Web · elongated · Nov 20, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > MAIN CABIN; AFT WET AREA; FLOOR SHEAR WEB DAMAGED AND ELONGATED FASTENER HOLES BTW BS 1006 - 1016, LBL 39. REPLACED THE SHEAR WEB BTW BS 986.5 - 1016, LBL 39, WL 208.1 IAW SRM 51-40-02-0G-0 AND DWG 147A0004, SHEET 64, REV-, DWG 147A5600, SHEET 45, REV C.
- [SDR SWAA2025122238200](https://openairdocs.org/sdr/SWAA2025122238200.md): Floorbeam · cracked · Nov 20, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM CRACKED AT BS 540; BL0 - RBL 24.75. FAULT RESOLVED ON OTHER FAULT, SEE TTG8Q018V1LJ.
- [SDR SWAA2025121947497](https://openairdocs.org/sdr/SWAA2025121947497.md): Floor Panel · damaged · Nov 20, 2025 · N7750A · Boeing 7377BD · Fuselage Floor Panel
  > ELONGATED HOLES ON FLOOR PANEL 140DF IN THE AFT CARGO BAY. REPLACED THE FLOOR PANEL 140DF IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 453A2610, SHEET 13, REV B.
- [SDR SWAA2025121938198](https://openairdocs.org/sdr/SWAA2025121938198.md): Floorbeam · cracked · Nov 20, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM HAS A CRACK AT BS 540, BL 0 - LBL 24.75. REPLACED MAIN CABIN FLOORBEAM IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 143A0060, SHEET 51, REV-, AND DWG 143A5240 SHEET 32 REV-; MEASUREMENT OF CRACK IS: 0.915 INCH.
- [SDR SWAA2025121936995](https://openairdocs.org/sdr/SWAA2025121936995.md): Floor Panel · delaminated · Nov 19, 2025 · N7750A · Boeing 7377BD · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 242UF IN THE AFT GALLEY AREA. REPAIRED THE FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1, REPAIR 1.
- [SDR SWAA2025122236200](https://openairdocs.org/sdr/SWAA2025122236200.md): Shield · corroded · Nov 17, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB LOCATED BTW STA 767 TO STA 794.3 AND WL 156 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BTW STA 767 TO STA 794.3 AND WL 156 IAW SRM 51-10-02-0G-0 PARAGRAPH 9,SRM 51-40-02-0G-0 AND DWG 146A0081, SHEET:37, REV:-.
- [SDR SWAA2025122236192](https://openairdocs.org/sdr/SWAA2025122236192.md): Fitting · cracked · Nov 17, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK FITTING LOCATED STA 947.5 AND STR 26L AT AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL FITTING BS 927 TO BS 947 AT LEVEL STR25R IAW SRM 51-40-02, SRM 51-10-02 ITEM 9 AND DWG 147A7500 SHEET 29 REV-.
- [SDR SWAA2025122236191](https://openairdocs.org/sdr/SWAA2025122236191.md): Fitting · cracked · Nov 17, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Attach Fittings
  > CRACK FITTING LOCATED STA 947.5 AND STR 26L AT AFT CARGO COMPARTMENT. REPLACED FITTING AND FASTENERS LOCATED STA 947.5 AND STR 26L AT AFT CARGO COMPARTMENT IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 149A8103 SHEET 7 REV: A.
- [SDR SWAA2025122347480](https://openairdocs.org/sdr/SWAA2025122347480.md): Intercostal · cracked · Nov 17, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK WEB-INTERCOSTAL LOCATED BTW STA 927 TO STA 947 STR 25R AT AFT CARGO COMPARTMENT. INTERCOSTAL REPLACED IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A7500, SHEET 29, REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED WEB - INTERCOSTAL LOCATED BS 9
- [SDR SWAA2025122236199](https://openairdocs.org/sdr/SWAA2025122236199.md): Support · corroded · Nov 17, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW STA 727 TO STA 767 AT LEVEL STR 25L AND WL 156 AT AFT CARGO COMPARTMENT (14 EA) 2025-696383<
- [SDR SWAA2025121947486](https://openairdocs.org/sdr/SWAA2025121947486.md): Support · corroded · Nov 17, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727 - 767, S25L, WL 156 IN THE AFT CARGO BAY (14 EA). FAULT RESOLVED ON ANOTHER FAULT TTG8Q018X19T.
- [SDR SWAA2025121947487](https://openairdocs.org/sdr/SWAA2025121947487.md): Web · corroded · Nov 17, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB, BETWEEN BS 767 - 794.3, WL 156 IN THE AFT CARGO BAY (4 EA). REPLACED THE SHIELD WEB IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 146A0081, SHEET 37, REV-.
- [SDR SWAA2025121936201](https://openairdocs.org/sdr/SWAA2025121936201.md): Support · corroded · Nov 17, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORRODED SUPPORT ZEE, BETWEEN BS 727 - 807, S25L, WL 156 IN THE AFT CARGO BAY, (12 EA). REPAIRED SUPPORT ZEE IAW SRM 53-00-53-2R-6, REPAIR 6, AND DWG 146A7500, SHEET 113, REV -.
- [SDR SWAA2025121847479](https://openairdocs.org/sdr/SWAA2025121847479.md): Access Panel · elongated · Nov 17, 2025 · N7750A · Boeing 7377BD · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED THE ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025121835981](https://openairdocs.org/sdr/SWAA2025121835981.md): Access Panel · damaged · Nov 17, 2025 · N7750A · Boeing 7377BD · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025121835677](https://openairdocs.org/sdr/SWAA2025121835677.md): Skin · delaminated · Nov 16, 2025 · N7750A · Boeing 7377BD · Trailing Edge Flaps
  > DELAMINATION ON UPPER & LOWER SKIN INBD EDGE OF LT WING OTBD AFT FLAP. REPAIRED UPPER AND LOWER SKIN INBD EDGE OF LT WING OTBD AFT FLAP IAW EA 25-157-03324.
- [SDR SWAA2025121935673](https://openairdocs.org/sdr/SWAA2025121935673.md): Web · cracked · Nov 15, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED WEB LOCATED AT THE CEILING AREA BTW BS 847 - 867, LBL 20 IN THE AFT CARGO BAY. REPLACED THE WEB IAW SRM 51-40-02-0G, AND DWG 149A8100, SHEET 1, REV-.
- [SDR SWAA2025122235284](https://openairdocs.org/sdr/SWAA2025122235284.md): Floorbeam · corroded · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LOCATED BS 986.5 RBL 44 WL 208.1. REPAIRED THE FLOORBEAM IAW EA 25-153-03179-WIP1, EA 25-153-03179-WIP2, EA 25-153-03179-WIP3 AND EA 25-153-03179.
- [SDR SWAA2025122235267](https://openairdocs.org/sdr/SWAA2025122235267.md): Web · corroded · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB LOCATED BTW STA 492.4 TO STA 500A STR 26R AND WL 156 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BTW STA 492.4 TO STA 500A STR 26R AND WL 156 AT FWD CARGO COMPARTMENT IAW SRM 51-40-02; SRM 51-10-02 AND DWG 143A0080
- [SDR SWAA2025122247460](https://openairdocs.org/sdr/SWAA2025122247460.md): Intercostal · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA. REPAIRED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA IAW EA 25-153-03173-WIP1 AND EA 25-153-03173.
- [SDR SWAA2025122247462](https://openairdocs.org/sdr/SWAA2025122247462.md): Frame · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Frame
  > CRACK FRAME ON BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. PERFORMED REPAIR ON FRAME ON BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA M-22-153-01244.
- [SDR SWAA2025122235372](https://openairdocs.org/sdr/SWAA2025122235372.md): Frame · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Frame
  > CRACK FRAME ON BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. PERFORMED REPAIR ON FRAME ON BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA M-22-153-01244.
- [SDR SWAA2025122235341](https://openairdocs.org/sdr/SWAA2025122235341.md): Intercostal · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA. REPAIRED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA IAW EA 25-153-03173-WIP1 AND EA 25-153-03173.
- [SDR SWAA2025122235374](https://openairdocs.org/sdr/SWAA2025122235374.md): Access Panel · damaged · Nov 14, 2025 · N7750A · Boeing 7377BD · Aerodynamic Fairings
  > ELONGATED HOLES ON ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10 REPAIR 10. S
- [SDR SWAA2025122235365](https://openairdocs.org/sdr/SWAA2025122235365.md): Support Angle · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE BTW BS 291.5 - 294.5, S17R IN THE FWD GALLEY AREA. REPLACED THE ANGLE SUPPORT AND FASTENERS IAW SRM 51-40-02, SRM 51-20-01, ITEM 9, AND DWG 141A8310, SHEET 25, REV -.
- [SDR SWAA2025122235362](https://openairdocs.org/sdr/SWAA2025122235362.md): Support Angle · corroded · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ANGLE BTW BS 294.5 - 328, RBL 55, WL 208.1 IN THE FWD GALLEY AREA. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02 ITEM 9, AND DWG 141A8310, SHEET 23, REV-.
- [SDR SWAA2025122235275](https://openairdocs.org/sdr/SWAA2025122235275.md): Web · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED WEB, BTW BS 312 - 328, RBL 31, WL 208.1 IN FWD GALLEY AREA. REPLACED THE WEB IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 141A5400, SHEET 39, REV-. S
- [SDR SWAA2025121935276](https://openairdocs.org/sdr/SWAA2025121935276.md): Intercostal · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ON WEB INTERCOSTAL, BTW BS 344 - 360, RBL 33, WL 208.1. REPLACED WEB INTERCOSTAL BTW BS 344 - 360, RBL 33, WL 208.1 IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 141A5400, SHEET 33, REV-.
- [SDR SWAA2025121935277](https://openairdocs.org/sdr/SWAA2025121935277.md): Web · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED WEB LOCATED BTW BS 328 - 344, LBL 47.5, WL 208.1 IN THE FWD GALLEY AREA. REPLACED THE WEB IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 141A5400, SHEET 44, REV-.
- [SDR SWAA2025121935279](https://openairdocs.org/sdr/SWAA2025121935279.md): Angle · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ANGLE, BS 663.75, RBL 13 IN THE AIR CONDITIONING BAY. REPLACED ANGLE LOCATED BS 663.75, BETWEEN RBL 5 & RBL 65 IAW SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02, AND DWG 111A1000, SHEET 259, REV A.
- [SDR SWAA2025121935333](https://openairdocs.org/sdr/SWAA2025121935333.md): Tie Clip · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED THE TIE CLIP IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 141A1110, SHEET 17, REV -, AND DWG 141A8380, SHEET 20, REV -.
- [SDR SWAA2025121935354](https://openairdocs.org/sdr/SWAA2025121935354.md): Access Panel · delaminated · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Plate/Skin
  > DELAMINATED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-2, REPAIR 2.
- [SDR SWAA2025121935047](https://openairdocs.org/sdr/SWAA2025121935047.md): Floorbeam · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Floor Beam
  > AAI INSPECTION: CRACKED FLOORBEAM LOCATED IN FLOOR STRUCTURE BS 540 BETWEEN BL 0 - RBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A0060, SHEET 51, REV-.
- [SDR SWAA2025121935274](https://openairdocs.org/sdr/SWAA2025121935274.md): Web · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS 277 - 294.5, RBL 1, WL 208.1 IN THE FWD GALLEY AREA. REPLACED WEB IAW SRM 51-40-02, DWG 141A5400, SHEET 20, REV -.
- [SDR SWAA2025121947449](https://openairdocs.org/sdr/SWAA2025121947449.md): Web · cracked · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS 312 - 328, RBL 31, WL 208.1 AT FWD GALLEY AREA. REPLACED WEB IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 141A5400, SHEET 39, REV-.
- [SDR SWAA2025121947454](https://openairdocs.org/sdr/SWAA2025121947454.md): Floorbeam · corroded · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM LOCATED BS 986.5, RBL 44, WL 208.1 AT AFT GALLEY AREA (3 POINTS). PERFORMED REPAIR ON THE FLOORBEAM IAW EA 25-153-03179-WIP1, EA 25-153-03179-WIP2, EA 25-153-03179-WIP3, AND EA 25-153-03179.
- [SDR SWAA2025121935266](https://openairdocs.org/sdr/SWAA2025121935266.md): Plate · corroded · Nov 14, 2025 · N7750A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON PLATE LOCATED BS 1016 PLUS 14 INCHES RBL 3 WL 208.1 AT AFT GALLEY AREA. REPLACED PLATE (STRAP) LOCATED BETWEEN BS 1006 TO BS 1030 RBL 3 WL 208.1 AT AFT GALLEY AREA IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND DWG 147A5600 SHEET: 46 RE
- [SDR SWAA2025121847461](https://openairdocs.org/sdr/SWAA2025121847461.md): Access Panel · damaged · Nov 14, 2025 · N7750A · Boeing 7377BD · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661AB AT RT WING. REPAIRED ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025121835360](https://openairdocs.org/sdr/SWAA2025121835360.md): Access Panel · elongated · Nov 14, 2025 · N7750A · Boeing 7377BD · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025121835361](https://openairdocs.org/sdr/SWAA2025121835361.md): Access Panel · elongated · Nov 14, 2025 · N7750A · Boeing 7377BD · Trailing Edge Flaps
  > ELONGATED HOLES ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025121835359](https://openairdocs.org/sdr/SWAA2025121835359.md): Access Panel · elongated · Nov 14, 2025 · N7750A · Boeing 7377BD · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661AB AT RT WING. REPAIRED ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2025122235042](https://openairdocs.org/sdr/SWAA2025122235042.md): Skin · corroded · Nov 13, 2025 · N7750A · Boeing 7377BD · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL SKIN BTW BS 967 AND BS 986.5 AND BTW STR 26L AND STR 27L LOWER FUSELAGE. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q018UWBN.

Next page: https://openairdocs.org/aircraft/N7750A/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 = 'N7750A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7750A/reports

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