# Service difficulty reports: N7881A

A list on [N7881A](https://openairdocs.org/aircraft/N7881A.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 · 185 reports

- [SDR SWAA2026101351251](https://openairdocs.org/sdr/SWAA2026101351251.md): Lock Pin · installed · Oct 12, 2026 · N7881A · Boeing 7377CT · Landing Gear Retraction/Extension System
  > LANDING GEAR DOES NOT RETRACT WHEN LANDING GEAR LEVER MOVED TO UP POSITION. REMOVED LANDING GEAR DOWN LOCK PINS IAW AMM 32-00-01
- [SDR SWAA2025120136615](https://openairdocs.org/sdr/SWAA2025120136615.md): Scuff Plate · cracked · Nov 18, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > FWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT LOWER CORNER. REMOVE AND REPLACED FWD SERVICE DOOR SCUFF PLATE IS CRACKED AT AFT LOWER CORNER IAW AMM 53-11-01-420-801, REJECT; FWD SERVICE DOOR FWD LOWER CORNER CUTOUT LEAK CHECK FAILED. IT HAS A HISSING SOUN
- [SDR SWAA2025120132998](https://openairdocs.org/sdr/SWAA2025120132998.md): Floorbeam · cracked · Nov 7, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Floor Beam
  > DURING OK TO CLOSE, FOUND THE FLOORBEAM CRACKED AT BS 540, RBL 1 - 25. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, AND DWG 143A0060, REV B;
- [SDR SWAA2025120130518](https://openairdocs.org/sdr/SWAA2025120130518.md): Plate · cracked · Oct 31, 2025 · N7881A · Boeing 7377CT · Wing Main, Frame Structure
  > RIGHT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE I/B SIDE IS CRACKED. REMOVED AND REPLACED THE RT WING T/E WIGGLE PLATE COMMON TO PANEL 651EB ON THE INBD SIDE IAW SRM 51-40-02, AND DWG 115A2781, REV B.
- [SDR SWAA2025120130385](https://openairdocs.org/sdr/SWAA2025120130385.md): Bulkhead · cracked · Oct 30, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Bulkhead
  > BS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 45, WL 173. THE COMPOSITE BULKHEAD WAS REPAIRED IAW SRM 51-70-04-2R-10.
- [SDR SWAA2025120129664](https://openairdocs.org/sdr/SWAA2025120129664.md): Rib · cracked · Oct 28, 2025 · N7881A · Boeing 7377CT · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STABILIZER NR 6 INSPAR RIB AT STABILIZER STATION 138.70; 3RD VERTICAL STIFFENER IS CRACKED. PERFORMED REPAIR AT HORIZONTAL STABILIZER NO 6 INSPAR RIB STABILIZER STATION 138.70 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4, REPAIR 4.
- [SDR SWAA2025120129201](https://openairdocs.org/sdr/SWAA2025120129201.md): Frame · cracked · Oct 27, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Frame
  > CRACKED FRAME BS 312 LBL 33 WL 282 ABOVE FWD ENTRY DOOR UPPER SILL WEB. REPAIRED IAW SRM 22-153-01244.
- [SDR SWAA2025120129202](https://openairdocs.org/sdr/SWAA2025120129202.md): Stringer · cracked · Oct 27, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 7L, BS 296, LBL 41, WL 274. THE DAMAGE WAS REPAIRED IAW SRM 53-00-03-2R-1, REPAIR 1, AND EA 25-153-02976 WITH AN INSPECTION PROGRAM DEFINED IN 25-153-02976-INSP. HFEC INSPECTED AREA IAW NDTM PART 6, 51-00-00, PROCEDURE 23. CRACK NOTED. NO
- [SDR SWAA2025120128469](https://openairdocs.org/sdr/SWAA2025120128469.md): Girt Bar · loose · Oct 25, 2025 · N7881A · Boeing 7377CT · Emergency Equipment
  > AFT ENTRY DOOR SLIDE GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED FASTENER AFT ENTRY DOOR SLIDE GIRT BAR BRACKET IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025120128621](https://openairdocs.org/sdr/SWAA2025120128621.md): Skin · cracked · Oct 25, 2025 · N7881A · Boeing 7377CT · Leading Edge Devices
  > RIGHT WING NR 8 SLAT NOSE SKIN AT ACTUATOR RIB HAS POSSIBLE CRACK. CLEANED RIGHT WING NR 8 SLAT NOSE SKIN AT ACTUATOR IAW SOPM 20-30-03. REPAIRED SLAT IAW SRM 57-42-01-2R-8, REPAIR 8, ALTERNATIVE 1, FIG 202.
- [SDR SWAA2025120128055](https://openairdocs.org/sdr/SWAA2025120128055.md): Floor Panel · delaminated · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor Panel
  > FWD FLOOR PANEL 221EF UPPER SURFACE DELAMINATED. THE FWD FLOOR PANEL 221EF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 9.A.1,
- [SDR SWAA2025120127810](https://openairdocs.org/sdr/SWAA2025120127810.md): Floor Panel · pulled · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor Panel
  > AFT FLOOR PANEL 242RF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.
- [SDR SWAA2025120128041](https://openairdocs.org/sdr/SWAA2025120128041.md): Floor Support · corroded · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SUPPORT, BS 304, LBL 11, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 141A5600, REV N.
- [SDR SWAA2025120128224](https://openairdocs.org/sdr/SWAA2025120128224.md): Floorbeam · corroded · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM, BS 986, LBL 38-45, WL 208. REMOVED AND REPLACED THE FILLER IAW EXISTING REPAIR SRM 53-70-51-2R-6, ALT 4.
- [SDR SWAA2025120128225](https://openairdocs.org/sdr/SWAA2025120128225.md): Floorbeam · corroded · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM, BS 986, RBL 38-45, WL 208. INSTALLED A REPAIR IAW SRM 53-70-51-2R-6, ALTERNATIVE 3, FIG 204, SHEET 1.
- [SDR SWAA2025120128049](https://openairdocs.org/sdr/SWAA2025120128049.md): Floor Support · cracked · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL, BS 315, RBL 30, WL 208. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV -.
- [SDR SWAA2025120127802](https://openairdocs.org/sdr/SWAA2025120127802.md): Floor Panel · pulled · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor Panel
  > AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241UF WITH UPPER SKIN AREAS OF PULLED STRANDS, REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2025120127808](https://openairdocs.org/sdr/SWAA2025120127808.md): Floor Panel · pulled · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor Panel
  > AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ADF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025120127809](https://openairdocs.org/sdr/SWAA2025120127809.md): Floor Panel · pulled · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor Panel
  > AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241AEF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.
- [SDR SWAA2025120127814](https://openairdocs.org/sdr/SWAA2025120127814.md): Floor Panel · pulled · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor Panel
  > AFT FLOOR PANEL 242UF FWD O/B CORNER IS CRACKED. AFT FLOOR PANEL 242UF WITH FWD O/B CORNER CRACKED WAS REPAIRED PER SRM 53-00-50-2R-1.
- [SDR SWAA2025120127815](https://openairdocs.org/sdr/SWAA2025120127815.md): Floor Panel · pulled · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor Panel
  > AFT FLOOR PANEL 242WF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF DAMAGE. REPLACED AFT FLOOR PANEL 242WF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 195.
- [SDR SWAA2025120127816](https://openairdocs.org/sdr/SWAA2025120127816.md): Floor Panel · damaged · Oct 24, 2025 · N7881A · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 242XF IS SOFT IN THE MIDDLE OF PANEL.<[01] FLOOR PANEL 242XF WITH SOFT AREA IN THE MIDDLE OF PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF DAMAGE.;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025120127302](https://openairdocs.org/sdr/SWAA2025120127302.md): Former · cracked · Oct 23, 2025 · N7881A · Boeing 7377CT · Aerodynamic Fairings
  > WING TO BODY FAIRING FORMER CRACKED, BS 500D BETWEEN S19 & 20L. REMOVED AND REPLACED THE WING TO BODY FAIRING SUPPORT IAW SRM 51-40-02, AND DWG 116A3010, REV-.
- [SDR SWAA2025120127305](https://openairdocs.org/sdr/SWAA2025120127305.md): Strap · corroded · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS 727D+6, RBL 11.5, WL 156. EVALUATED CORROSION OF FLOOR STRAP. FOUND TO BE OUT OF LIMITS, RECEIVED NEW STRAP AND APPLIED WHITE ENAMEL ALL IAW SRM 51-10-02, AMM 51-21-73-370-804, AND ACO 5360
- [SDR SWAA2025120127295](https://openairdocs.org/sdr/SWAA2025120127295.md): Shield · corroded · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS 767+3 - 794, RBL 22, WL 156. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN THE SRM. REMOVED, REPLACED, AND INSTALLED A NEW SHIELD IAW SRM 51-10-02, SRM 51-40-05-0G-0, S
- [SDR SWAA2025120127291](https://openairdocs.org/sdr/SWAA2025120127291.md): Support Plate · corroded · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, LBL 22, WL 156. CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED, AND INSTALLED A N
- [SDR SWAA2025120127290](https://openairdocs.org/sdr/SWAA2025120127290.md): Sidewall Support · corroded · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES, BS 727B - 767, RBL 22, WL 156. CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED, REPLACED, AND INSTALLED
- [SDR SWAA2025120126957](https://openairdocs.org/sdr/SWAA2025120126957.md): Attach Angle · cracked · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Attach Fittings
  > BS 663, LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT LBL 45, WL 165. REMOVED, REPLACED, AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0, AND DWG 111A1000, REV A.
- [SDR SWAA2025120127299](https://openairdocs.org/sdr/SWAA2025120127299.md): Web · corroded · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS 794 - 847, RBL 26, WL 156. REMOVED AND REPLACED THE THRESHOLD WEB IAW SRM 51-40-02, AND DWG:146A8340 REV-.
- [SDR SWAA2025120127296](https://openairdocs.org/sdr/SWAA2025120127296.md): Scuff Plate · cracked · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > FORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, STEP 4.B.(4).
- [SDR SWAA2025120127297](https://openairdocs.org/sdr/SWAA2025120127297.md): Scuff Plate · cracked · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, STEP 4.B.(4).
- [SDR SWAA2025120126946](https://openairdocs.org/sdr/SWAA2025120126946.md): Doubler · cracked · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Plate/Skin
  > EGPR SURROUND DOUBLER CRACKED BS 233, WL 175+8, ABOVE S24R. TRIMMED DAMAGED AREA; FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-15-2R-4, REPAIR 4, PARG 4 (B-M).
- [SDR SWAA2025120127298](https://openairdocs.org/sdr/SWAA2025120127298.md): Attach Angle · corroded · Oct 22, 2025 · N7881A · Boeing 7377CT · Fuselage Main, Attach Fittings
  > CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS MULTIPLE AREAS UNDER NUT PLATES BS 767 TO 787, RBL 21, WL 156. CORROSION ON AFT CARGO BAY ATTACH ANGLE UNDER SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED, REPLACED, AND
- [SDR SWAA2025120126776](https://openairdocs.org/sdr/SWAA2025120126776.md): Switch · broken · Oct 21, 2025 · N7881A · Boeing 7377CT · Emergency Lighting
  > AFT ATTENDANCE PANEL EMERGENCY LIGHT SWITCH IS BROKEN. REMOVED AND REPLACED AFT ATTENDANT PANEL EMERGENCY LIGHT SWITCH COVER IAW SWPM 20-84-14..
- [SDR SWAA2025120126766](https://openairdocs.org/sdr/SWAA2025120126766.md): Panel · delaminated · Oct 21, 2025 · N7881A · Boeing 7377CT · Aerodynamic Fairings
  > PANEL 194CL DELAMINATED ON OUTER SURFACE. PANEL 194CL REPAIRED IAW SRM 51-70-05-2R-2.
- [SDR SWAA2024120273056](https://openairdocs.org/sdr/SWAA2024120273056.md): Bustle · out of adjust · Dec 1, 2024 · N7881A · Boeing 7377CT · Escape Slide
  > FWD SERVICE DOOR SLIDE BUSTLE TRIM HAS SHARP EDGE ON LOWER RIGHT CORNER.<[01] ADJ DOOR BUSTLE CORRECTED SHARP EDGE PER AMM 52-41-31. AC OK FOR SERVICE.
- [SDR SWAA2024111859384](https://openairdocs.org/sdr/SWAA2024111859384.md): Wheel · separated · Nov 13, 2024 · N7881A · Boeing 7377CT · Tire Tube
  > NOSE TIRE SEPARATION ON ROTATION AT ROTATION NOSEWHEEL VIBRATION INCREASED AND MATERIAL DEPARTED TO THE LEFT FROM THE NOSE WHEEL WELL AREA AND THE VIBRATION INCREASED. WE ELECTED TO LEAVE THE LANDING GEAR EXTENDED DUE TO THE UNKNOWN CONDITION OF THE NOSE GEAR.
- [SDR SWAA2024090433101](https://openairdocs.org/sdr/SWAA2024090433101.md): Rivet · missing · Sep 1, 2024 · N7881A · Boeing 7377CT · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR RETAINING CLIP MISSING RIVET<[01] INSTALLED MISSING RIVET IAW AMM 25-66-01
- [SDR SWAA2024082931055](https://openairdocs.org/sdr/SWAA2024082931055.md): Girt Bar · loose · Aug 26, 2024 · N7881A · Boeing 7377CT · Emergency Equipment
  > GIRT BAR RETAINING HOOK ON FORWARD GALLEY DOOR IS LOOSE<[01] C/W EA M-23-125-01839
- [SDR SWAA2023122133492](https://openairdocs.org/sdr/SWAA2023122133492.md): Skirt · out of adjust · Dec 19, 2023 · N7881A · Boeing 7377CT · Escape Slide
  > L2 DOOR SLIDE SKIRT NEEDS ADJUST. IT HITS SCUFF PLATE WHEN CLOSING DOOR<[01] ADJUSTED L2- DOOR SLIDE SKIRT AS PER AMM 25-66-01-000-801;[02] VERIFIED STEP 1
- [SDR SWAA2023122133488](https://openairdocs.org/sdr/SWAA2023122133488.md): Skirt · out of adjust · Dec 19, 2023 · N7881A · Boeing 7377CT · Escape Slide
  > R2 DOOR SLIDE SKIRT NEEDS ADJUST. IT HITS SCUFF PLATE WHEN CLOSING DOOR<[01] ADJUSTED R2- DOOR SLIDE SKIRT AS PER AMM 25-66-01-000-801;[02] VERIFIED STEP 1
- [SDR SWAA2023122131831](https://openairdocs.org/sdr/SWAA2023122131831.md): Battery Pack · inoperative · Dec 14, 2023 · N7881A · Boeing 7377CT · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY PACK STA 727C LEFT<BR>M1673 BATTERY PACK STA 952 LEFT<BR>I/A/W BOEING AMM 33-51-06-960-805; OPS CHECK
- [SDR SWAA2023122134441](https://openairdocs.org/sdr/SWAA2023122134441.md): Battery Pack · inoperative · Dec 14, 2023 · N7881A · Boeing 7377CT · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY PACK STA 727C LEFT<BR>M1673 BATTERY PACK STA 952 LEFT<BR>I/A/W BOEING AMM 33-51-06-960-805; OPS CHECK
- [SDR SWAA2023122134442](https://openairdocs.org/sdr/SWAA2023122134442.md): Battery Pack · inoperative · Dec 14, 2023 · N7881A · Boeing 7377CT · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INTERIOR/EXTERIOR INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS<BR>M2335 BATTERY PACK STA 500C LEFT<BR>M1670 BATTERY PACK STA 727C LEFT<BR>M1673 BATTERY PACK STA 952 LEFT<BR>I/A/W BOEING AMM 33-51-06-960-805; OPS CHECK
- [SDR SWAA2023122131068](https://openairdocs.org/sdr/SWAA2023122131068.md): Light · damaged · Dec 12, 2023 · N7881A · Boeing 7377CT · Emergency Lighting
  > EMERGENCY LIGHT ASSEMBLY ON G4 DAMAGED<[01] REMOVED AND REPLACED LIGHT ASSEMBLY I/A/W ENCORE CMM 25-31-05; OPS CHECK FOUND NORMAL;[02] VERIFIED STEP 1
- [SDR SWAA2023122125815](https://openairdocs.org/sdr/SWAA2023122125815.md): Beam · corroded · Nov 28, 2023 · N7881A · Boeing 7377CT · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA FLOOR BEAM AT STA 986.5 LBL 44' HAS EXFOLIATING CORROSION THAT IS OUT OF LIMITS<[01] REPAIRED MAIN CABIN AFT WET AREA FLOOR BEAM AT STA 986.5 LBL 44' REF SRM 53-70-51-2R-6;[02] RII VERIFIED STEP 1;[03] COMPLETED SME INSPECTION OF WORKMA
- [SDR SWAA2023122125458](https://openairdocs.org/sdr/SWAA2023122125458.md): Seal · cracked · Nov 28, 2023 · N7881A · Boeing 7377CT · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 343AT BLADE METAL SEAL CRACKED<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB UPPER GAP COVER ACCESS PANEL 343AT BLADE METAL SEAL REF SRM 51-40-02-0G-0;[02] VERIFIED STEP #1
- [SDR SWAA2023122125459](https://openairdocs.org/sdr/SWAA2023122125459.md): Seal · deteriorated · Nov 28, 2023 · N7881A · Boeing 7377CT · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 332AT RUBBER SEAL DETERIORATED AND BROKEN PIECE AT END TIP.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 332AT RUBBER SEAL AS PER SRM 51-40-02-0G-0;[02] VERIFIED STEP
- [SDR SWAA2023122125220](https://openairdocs.org/sdr/SWAA2023122125220.md): Floor Panel · cracked · Nov 27, 2023 · N7881A · Boeing 7377CT · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL #221GF FWD SECTION TIP CRACKED<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL 221GF AS PER B737 SRM 53-00-50-2R-6 PARAG 3-G-M; MATERIAL USED PO#1798939; PO#1690463.;[02] VERIFIED AND INSPECTED STEP #1. P
- [SDR SWAA2023122124947](https://openairdocs.org/sdr/SWAA2023122124947.md): Seal · cracked · Nov 27, 2023 · N7881A · Boeing 7377CT · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER UPPER GAP COVER ACCESS PANEL 333AT BLADE SEAL CRACKED.<[01] REMOVED AND REPLACED BLADE SEAL AT LEFT HORIZONTAL STABILIZER UPPER GAP COVER PANEL REF SRM 51-40-02-0G-0;[02] VERIFIED STEP #1

Next page: https://openairdocs.org/aircraft/N7881A/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 = 'N7881A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7881A/reports

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