# Service difficulty reports: N7866A

A list on [N7866A](https://openairdocs.org/aircraft/N7866A.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 4 · 191 reports

- [SDR SWAA2025110731480](https://openairdocs.org/sdr/SWAA2025110731480.md): Slat · cracked · Nov 4, 2025 · N7866A · Boeing 7377Q8 · Leading Edge Devices
  > RIGHT WING, NR 7 SLAT HAS A CRACK AT ACTUATOR ATTACH POINT. VERIFIED WITH HFEC PART 6 51-00-00, PROCEDURE 23. C/W SLAT INSPECTION NO FOD FOUND. R & R NR 6 L/E SLAT AND TORQUED IAW AMM 27-81-21.
- [SDR SWAA2025082105688](https://openairdocs.org/sdr/SWAA2025082105688.md): Slide · partial deploy · Aug 18, 2025 · N7866A · Boeing 7377Q8 · Escape Slide
  > FORWARD SERVICE ENTRY ESCAPE SLIDE PARTIALLY DEPLOYED. REPOSITIONED FWD SERVICE ENTRY ESCAPE SLIDE PER AMM 25-66-01 AND MT 725-61-06.
- [SDR SWAA2025030401958](https://openairdocs.org/sdr/SWAA2025030401958.md): Handle · broken · Mar 4, 2025 · N7866A · Boeing 7377Q8 · Passenger/Crew Doors
  > L1 DOOR PLASTIC ASSIST HANDLE BROKEN. <[01] SWAPPED FWD LAV DOOR HANDLE WITH L1 DOOR ASSIST HANDLE PER AMM 52-11-31. PLACED FWD LAV ASSIST HANDLE ON MEL. OK TO CONTINUE PER MEL 25-10-01 SP1B AUTH #240150. 3901019;[02] INSTALLED NEW ASSIST HANDLE TO ROBBED FWD
- [SDR SWAA2025020491976](https://openairdocs.org/sdr/SWAA2025020491976.md): Skin · cracked · Feb 1, 2025 · N7866A · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE SKIN HAS 1/2' LONG CRACK ON AFT SIDE OF VACUUM WASTE EXHAUST PORT. FUSELAGE STATION 918 AND 3.5 INCHES ABOVE STRINGER 22L. COMPLIED WITH TASK CARD. COMPLIED WITH EA 25-153-00283.
- [SDR SWAA2025020491670](https://openairdocs.org/sdr/SWAA2025020491670.md): Angle · cracked · Jan 31, 2025 · N7866A · Boeing 7377Q8 · Turbine Section
  > RIGHT ENGINE; LPT COOLING TUBE SUPPORT ANGLE BRACKET CRACKED 4OCLOCK POSITION <[01]. REMOVED AND REPLACED CRACKED LPT COOLING TUBE SUPPORT ANGLE BRACKET AT 4 O?CLOCK POSITION IAW SIP.
- [SDR SWAA2025013191669](https://openairdocs.org/sdr/SWAA2025013191669.md): Battery Pack · failed · Jan 31, 2025 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACK M1670 FAILED CAPACITY TEST.<[01] R&R PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACK M1670 IAW AMM 33-51-06.
- [SDR SWAA2025013191668](https://openairdocs.org/sdr/SWAA2025013191668.md): Battery Pack · failed · Jan 31, 2025 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACK M1675 FAILED CAPACITY TEST.<[01] R&R PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACK M1675 IAW AMM 33-51-06.
- [SDR SWAA2025013191658](https://openairdocs.org/sdr/SWAA2025013191658.md): Handle · loose · Jan 31, 2025 · N7866A · Boeing 7377Q8 · Galley Doors
  > AFT GALLEY SERVICE DOOR R2 DOOR HANDLE CAM LOOSE.<[01] RE-SECURED AFT GALLEY SERVICE DOOR R2 DOOR HANDLE CAM REF AMM 20-50-11.
- [SDR SWAA2024010432086](https://openairdocs.org/sdr/SWAA2024010432086.md): Floor Panel · debonded · Dec 15, 2023 · N7866A · Boeing 7377Q8 · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKIN HAS AN AREA OF DISBOND NEAR CENTER OF PANEL. (MARKED)<[01] FLOOR PANEL 242AF WITH DISBOND IN UPPER SKIN WAS REPLACED BY FABRICATING NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG NO. 144A5810 ID:0037;[02] VERIFIED CORRECTIVE ACTION ITEM 1
- [SDR SWAA2024010431565](https://openairdocs.org/sdr/SWAA2024010431565.md): Web · corroded · Dec 14, 2023 · N7866A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY THRESHOLD WEB AT BS 447 TO BS 467; STR 25R TO 26R<[01] REMOVED AND INSTALLED NEW FCB SUB-THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 143A8330;[02] VERIFIED CORRECTIVE ACTON ENTRY 1. AND MEASUREMENT TABLE
- [SDR SWAA2024010431567](https://openairdocs.org/sdr/SWAA2024010431567.md): Sidewall Support · corroded · Dec 14, 2023 · N7866A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CARGO BAY RH FLOOR-TO-SIDEWALL SUPPORT AT BS 498; STR 25R TO STR 26R THE DESCRIPTION OF ITEM SUPPOSED TO BE IS SHIELD AND NOT THE FLOOR TO SIDEWALL SUPPORT<[01] COMPLETED BAR CODE TTG8Q00Q9P7G;[02] VERIFIED CORRECTIVE ACTION COMPLETE THROUGH S
- [SDR SWAA2024010431568](https://openairdocs.org/sdr/SWAA2024010431568.md): Web · corroded · Dec 14, 2023 · N7866A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY THRESHOLD WEB AT BS 792 TO BS 847; STR 24R TO STR 26R<[01] REPLACED THRESHOLD WEB AT BS 792 TO BS 847 IAW SRM 51-40-02; DWG 146A8340.;[02] VERIFIED CORRECTIVE ACTION COMPLETE THROUGH STEPS 1-5; MEASUREMENT TABLE VERIFIED.
- [SDR SWAA2024010431566](https://openairdocs.org/sdr/SWAA2024010431566.md): Sidewall Support · corroded · Dec 14, 2023 · N7866A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY RH FLOOR-TO-SIDEWALL SUPPORT AT BS 865; STR 25R THE DESCRIPTION OF ITEM IS SUPPOSE TO BE SHIELD AND NOT FLOOR TO SIDEWALL<[01] BARCODE: TTG8Q00Q9NBW COMPLETED;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. AND STEPS COMPLETED.
- [SDR SWAA2024010430628](https://openairdocs.org/sdr/SWAA2024010430628.md): Scuff Plate · cracked · Dec 12, 2023 · N7866A · Boeing 7377Q8 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] REPAIR FWD CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
- [SDR SWAA2024010430618](https://openairdocs.org/sdr/SWAA2024010430618.md): Panel · debonded · Dec 12, 2023 · N7866A · Boeing 7377Q8 · Fuselage Main, Plate/Skin
  > PANEL 194CR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194CR OUTER SKIN DISBONDED WAS REPAIRED IAW SRM 51-70-05-2R-2;[02] VERIFIED REPAIR OF PANEL 194CR PER SRM 51-70-05-2R-2
- [SDR SWAA2024010431140](https://openairdocs.org/sdr/SWAA2024010431140.md): Stringer · cracked · Dec 12, 2023 · N7866A · Boeing 7377Q8 · Fuselage Main, Longeron/Stringer
  > POSSIBLE CRACK STR 23L BS 540 NEAR FASTENER HOLE<[01] ACCOMPLISHED STRINGER REPAIR 23L/H BETWEEN BS 500D+6' TO BS 539 AT FCB IAW SRM 53-00-03-2R-1;PAR 4. FIG 205;DWG: 143A1215 AND DWG:143A3210.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2024010431143](https://openairdocs.org/sdr/SWAA2024010431143.md): Support Angle · cracked · Dec 12, 2023 · N7866A · Boeing 7377Q8 · Wing Miscellaneous Structure
  > UPPER T/E PANEL LOWER SURFACE SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT ABOVE #1 PYLON AFT TIP<[01] TASK COMPLETE:<BR>REMOVED SUPPORT ANGLE IAW SRM 51-40-02-0G-0. RECEIVED NEW SUPPORT ANGLE (PN: 115A2982-9 LOT: 1522119-1) AND INSTALLED IAW SRM
- [SDR SWAA2024010331128](https://openairdocs.org/sdr/SWAA2024010331128.md): Seat Track · corroded · Dec 12, 2023 · N7866A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LH HAS CORROSION ON CROWN AT LBL 45.5; STA 500B WL 208<[01] SEAT TRACK WILL BE REPLACED ON CARD#TTG8Q00Q8J4J.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024010331117](https://openairdocs.org/sdr/SWAA2024010331117.md): Seat Track · corroded · Dec 12, 2023 · N7866A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LH HAS CORROSION ON CROWN AT LBL 45.5; STA 380B+3' WL 208<[01] COMPLETED STEP 1.;[02] UPON FURTHER INVESTIGATION; CORROSSION IS AT BS 380+3'; LBL 45.5; WL 208.;[03] COMPLETED STEP 2.;[04] PARTIAL STEP 3.;[05] PARTIAL STEP 3.;[06] COMPLETED STEP 3.;[
- [SDR SWAA2024010331118](https://openairdocs.org/sdr/SWAA2024010331118.md): Seat Track · corroded · Dec 12, 2023 · N7866A · Boeing 7377Q8 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LH HAS CORROSION ON CROWN AT LBL 45.5; STA 520 WL 208<[01] VERIFIED APPLICABILITY FOR SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1.;[02] VERIFIED APPLICABILITY FOR SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1.;[03] COMPLETED STEP 4.;[04] REMOVED AND REPLACED CABIN
- [SDR SWAA2024010430451](https://openairdocs.org/sdr/SWAA2024010430451.md): Angle · cracked · Dec 11, 2023 · N7866A · Boeing 7377Q8 · Wing Miscellaneous Structure
  > CRACKED L-CLIP ON L/W T/E PANEL 551FB AT FWD UPPER EDGE 27' FROM O/B END<[01] TASK COMPLETE:<BR>CRACKED L-CLIP WAS REMOVED IAW SRM 51-40-02-0G-0. NEW L-CLIP WAS RECEIVED AND INSTALLED IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TAB
- [SDR SWAA2023092704939](https://openairdocs.org/sdr/SWAA2023092704939.md): Light · inoperative · Sep 27, 2023 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > FWD CABIN ROW 1 ABC EMERGENCY LIGHT OUT<[01] RELAMPED 1ABC EMERGENCY LIGHT PER AMM 33-51-03
- [SDR SWAA2023091400300](https://openairdocs.org/sdr/SWAA2023091400300.md): Battery Pack · failed · Sep 14, 2023 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > R/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED R/H FWD EMERGENCY LIGHTING BATTERY PACK PER AMM 33-51-06.
- [SDR SWAA2023042831246](https://openairdocs.org/sdr/SWAA2023042831246.md): Slide · loose · Apr 25, 2023 · N7866A · Boeing 7377Q8 · Escape Slide
  > R1 DOOR EVACUATION SLIDE COVER LOOSE<[01] REPACKED R2 SLIDE OER 725-61-06
- [SDR SWAA2022112875399](https://openairdocs.org/sdr/SWAA2022112875399.md): Battery · inoperative · Nov 25, 2022 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > AFT RH OVERHEAD EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED AFT RH OVERHEAD EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD
- [SDR SWAA2022101760445](https://openairdocs.org/sdr/SWAA2022101760445.md): Battery Pack · inoperative · Oct 16, 2022 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > EMERGENCY LIGHTS FOUND LAST 2 CABIN EMERGENY LIGHT AFT CEILING AND BOTH AFT OVER DOOR EMERGENCY LIGHTS TO BE INOP / [01] R&R AFT LH EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06
- [SDR SWAA2022072835358](https://openairdocs.org/sdr/SWAA2022072835358.md): Light · inoperative · Jul 27, 2022 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > EMERGENCY LIGHT@ 9ABC INOP / [01] RELAMPED EMERGENCY LIGHT @ 9ABC IAW AMM 33-51-03. OPS CK GOOD
- [SDR SWAA2022042596278](https://openairdocs.org/sdr/SWAA2022042596278.md): Cover · out of position · Apr 20, 2022 · N7866A · Boeing 7377H4 · Escape Slide
  > FWD SERVICE DOOR EMERG. SLIDE PARTIAL FELL OUT / [01] REPOSITIONED R1 SLIDE IN SLIDE COVER PER AMM25-66-01
- [SDR SWAA2022022376321](https://openairdocs.org/sdr/SWAA2022022376321.md): Lens · missing · Feb 22, 2022 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > FWD ENTRY DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REMOVE AND REPLACED FWD ENTRY LOWER E LIGHT LENS IAW AMM-33-51-01;[02] INSPECTED
- [SDR SWAA2022022376322](https://openairdocs.org/sdr/SWAA2022022376322.md): Lens · missing · Feb 22, 2022 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > FWD SERVICE DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW FWD SERVICE DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REMOVED AND REPLACED FWD SERVICE DOOR E LIGHT LENS IAW AMM-33-51-01;[02] INSPECTED
- [SDR SWAA2022022376324](https://openairdocs.org/sdr/SWAA2022022376324.md): Lens · loose · Feb 22, 2022 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > RIGHT EMERGENCY EXIT DOOR INTERIOR LOWER EMERGENCY LIGHT LENS IS LOOSE / [01] RE SECURED RH EMERGENCY EXIT DOOR LOWER LIGHT LENS REF M/M 33-51-01;[02] INSPECTED
- [SDR SWAA2022022376326](https://openairdocs.org/sdr/SWAA2022022376326.md): Light · missing · Feb 22, 2022 · N7866A · Boeing 7377Q8 · Emergency Lighting
  > R2 AND L2 LOWER EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROWS. / [01] REMOVED AND REPLACED R2 AND L2 EMERGANCY EXIT SIGN COVERS REF AMM 33-51-01;[02] INSPECTED
- [SDR SWAA2022021463393](https://openairdocs.org/sdr/SWAA2022021463393.md): Skin · cracked · Jan 5, 2022 · N7866A · Boeing 737* · Nacelle/Pylon Miscellaneous Structure
  > CRACK INTERNAL SKIN INBOARD FAN COWL LOC. 8 OCLOCK APROX. ON ENGINE 2; 2021-576398 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; CAL DUE DATE: 24-FEB-22; [02] PERFORMED PERMANENT REPAIR SKIN INBOARD FAN COWL ON ENGINE 2 IAW B737-700 SRM 54-
- [SDR SWAA2022021158655](https://openairdocs.org/sdr/SWAA2022021158655.md): Bracket · cracked · Jan 5, 2022 · N7866A · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK BRACKET LOCATED VERTICAL BEAM BETWEEN BL0.0 TO LBL10.0 AND BS727 AT AFT CARGO COMPARTMENT; 2021-576389 / [01] REPLACED BRACKET LOCATED VERTICAL BEAM BETWEEN BL0.0 TO LBL10.0 AND BS727 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; B737-700 SRM 51-4
- [SDR SWAA2022021158654](https://openairdocs.org/sdr/SWAA2022021158654.md): Battery Pack · inoperative · Jan 5, 2022 · N7866A · Boeing 737* · Emergency Lighting
  > INOP EMERGENCY DOOR BATTERY PACK LOCATED BTW BS597-BS616 RH SIDE AT PASSENGER CABIN (1 EA); 2021-576383 / [01] REPLACED EMERGENCY DOOR BATTERY PACK LOCATED BTW BS597-BS616 RH SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-06-960-805 TEST IS GOOD; [02]
- [SDR SWAA2022010658653](https://openairdocs.org/sdr/SWAA2022010658653.md): Fitting · corroded · Jan 5, 2022 · N7866A · Boeing 7377Q8 · Vertical Stabilizer, Attach Fittings
  > CORROSION FITTING ON DRAG BRACE OUTBOARD FWD LOCATED AFT REAR SPAR RT SIDE AT VERTICAL STABILIZER. REPLACED THE FITTING AND FASTENERS ON DRAG BRACE IAW SRM 51-40-02 & DWG 148A8200 REV A.
- [SDR SWAA2022021457987](https://openairdocs.org/sdr/SWAA2022021457987.md): Spar Web · corroded · Jan 3, 2022 · N7866A · Boeing 737* · Wing Spar
  > CUSTOMER REQUEST - CORROSION FRONT SPAR WEB LOCATED OFSS 261 AT LT WING; 2021-576311 / [01] TOOL USED. ULTRASONIC THICKNESS GAGE. P/N: 45MG. S/N: 130066701. DUE DATE: 22-APR-22.; [02] TOOL USED. EDDY CURRENT EQUIPMENT. P/N: NORTEC 500D. S/N: N500X12101V022233
- [SDR SWAA2022021157989](https://openairdocs.org/sdr/SWAA2022021157989.md): Access Panel · elongated · Jan 3, 2022 · N7866A · Boeing 737* · Aerodynamic Fairings
  > ELONGATED HOLE ACCESS PANEL 194BR AT LOWER FUSELAGE; 2021-576315 / [01] HOT BONDER P/N:HCS9000B; S/N: 18175469; DUE DATE: 05-AUG-22.; [02] TOOL USED MULTIMETER P/N: FLUKE 1587; S/N: 31980129; DUE DATE: 11-DEC-22; [03] TOOL USED CALIPER PN:500-464; SN: 15331
- [SDR SWAA2022021157995](https://openairdocs.org/sdr/SWAA2022021157995.md): Intercostal · cracked · Jan 3, 2022 · N7866A · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS927 TO BS947.5 AND STR25R AT AFT CARGO COMPARTMENT; 2021-576321 / [01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS927 TO BS947.5 AND STR25R AT AFT CARGO COMPARTMENT IAW B737-51-10-02 ITEM 9 AND DWG 147A7500; SHEET
- [SDR SWAA2022021157994](https://openairdocs.org/sdr/SWAA2022021157994.md): Angle · cracked · Jan 3, 2022 · N7866A · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BETWEEN STR25R TO STR27R AND BS907 PLUS 7 INCH AT AFT CARGO COMPARTMENT; 2021-576319 / [01] REPLACED FASTENERS AND ANGLE LOCATED BETWEEN STR25R TO STR27R AND BS907 PLUS 7 INCH AT AFT CARGO COMPARTMENT IAW B737-700 SMR 51-10-02 ITEM 9; SRM
- [SDR SWAA2022021157993](https://openairdocs.org/sdr/SWAA2022021157993.md): Angle · cracked · Jan 3, 2022 · N7866A · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BETWEEN STR25R TO STR27R AND BS907 PLUS 11 INCH AT AFT CARGO COMPARTMENT; 2021-576320 / [01] INSTALLED NEW ANGLE LOCATED BETWEEN STR25R TO STR27R AND BS907 PLUS 11 INCH AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 S
- [SDR SWAA2022021157990](https://openairdocs.org/sdr/SWAA2022021157990.md): Track · cracked · Jan 3, 2022 · N7866A · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK CARGO TRACK LOCATED BS727E; RBL13.84 AND WL156 AT AFT CARGO COMPARTMENT; 2021-576318 / [01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101U102020; DUE DATE: 01-JUN-22.; [02] TOOL USED: ELECTRONIC CALIPER; P/N: 500-196-30; S/N: A21033416; DUE DA
- [SDR SWAA2022021157556](https://openairdocs.org/sdr/SWAA2022021157556.md): Bracket · deteriorated · Jan 3, 2022 · N7866A · Boeing 737* · Escape Slide
  > DETERIORATED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA; 2021-576294 / [01] REPLACED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA IAW AMM 25-66-02-400-801.; [02] REPLACED ENTRY DOOR GIRT BAR FLOOR BR
- [SDR SWAA2022021171374](https://openairdocs.org/sdr/SWAA2022021171374.md): Plate · deteriorated · Jan 3, 2022 · N7866A · Boeing 737* · Escape Slide
  > DETERIORATED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA; 2021-576294 / [01] REPLACED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA IAW AMM 25-66-02-400-801.; [02] REPLACED ENTRY DOOR GIRT BAR FLOOR BR
- [SDR SWAA2022021157557](https://openairdocs.org/sdr/SWAA2022021157557.md): Bracket · deteriorated · Jan 3, 2022 · N7866A · Boeing 737* · Escape Slide
  > DETERIORATED AFT SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA; 2021-576295 / [01] REPLACED AFT SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA IAW AMM 25-66-02-400-801.; [02] REPLACED AFT SERVICE DOOR
- [SDR SWAA2022021171375](https://openairdocs.org/sdr/SWAA2022021171375.md): Plate · deteriorated · Jan 3, 2022 · N7866A · Boeing 737* · Escape Slide
  > DETERIORATED AFT SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA; 2021-576295 / [01] REPLACED AFT SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATES AT AFT GALLEY AREA IAW AMM 25-66-02-400-801.; [02] REPLACED AFT SERVICE DOOR
- [SDR SWAA2022021157541](https://openairdocs.org/sdr/SWAA2022021157541.md): Structure · cracked · Jan 2, 2022 · N7866A · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 BL0 FWD GALLEY AND LAV; 2021-576259 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400; SHEET 20;
- [SDR SWAA2022021157542](https://openairdocs.org/sdr/SWAA2022021157542.md): Structure · cracked · Jan 2, 2022 · N7866A · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BS380 TO BS400 BL0 AT FWD GALLEY AREA; 2021-576260 / [01] REPLACED ANGLE - SUPPORT LOCATED BS380 TO BS400 BL0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A5400; SHEET 66; REV -.; [02] REPLACED ANGLE - SUPPORT L
- [SDR SWAA2022021457098](https://openairdocs.org/sdr/SWAA2022021457098.md): None · cracked · Dec 29, 2021 · N7866A · Boeing 737* · Fuselage Main, Plate/Skin
  > CRACK CLIP LOCATED ON AFT FACE BS 500C AT LEVEL STR 26R AT FWD CARGO COMPARTMENT; 2021-576210 / [01] REPLACED CLIP LOCATED ON AFT FACE BS 500C AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 143A7505 SHEET 10 REV A. SEE
- [SDR SWAA2022021457094](https://openairdocs.org/sdr/SWAA2022021457094.md): None · cracked · Dec 29, 2021 · N7866A · Boeing 737* · Fuselage Main, Plate/Skin
  > CRACK CLIP LOCATED ON FWD FACE BS 500B AT LEVEL STR 26R AT FWD CARGO COMPARTMENT; 2021-576209 / [01] REPLACED CLIP LOCATED ON FWD FACE BS 500B AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02 AND DRAWING 143A7505 R

Next page: https://openairdocs.org/aircraft/N7866A/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 = 'N7866A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7866A/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.