# Service difficulty reports: N8554X

A list on [N8554X](https://openairdocs.org/aircraft/N8554X.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 2 · 57 reports

- [SDR SWAA2026092179944](https://openairdocs.org/sdr/SWAA2026092179944.md): Bolt · loose · Sep 17, 2026 · N8554X · Boeing 7378H4 · Fuel Storage
  > FUEL LEAK REPORTED FROM REFUELING PANEL. RETORQUED MOUNTING BOLTS ON THE CENTER TANK FUELING SHUTOFF VALVE IAW AMM 28-21-51. NO LEAKS NOTED.
- [SDR SWAA2026062515351](https://openairdocs.org/sdr/SWAA2026062515351.md): Light · cracked · Jun 24, 2026 · N8554X · Boeing 7378H4 · Emergency Lighting
  > 2ABC FLOOR PHOTOLUMINESCENCE STRIP IS CRACKED; DAMAGED AND HAS MOISTURE BUILD UP. REMOVED AND REPLACED FLOOR PHOTOLUMINESCENCE STRIP AT 2ABC IAW AMM 35-51-015.
- [SDR SWAA2026062515350](https://openairdocs.org/sdr/SWAA2026062515350.md): Light · cracked · Jun 24, 2026 · N8554X · Boeing 7378H4 · Emergency Lighting
  > 3DEF FLOOR PHOTOLUMINESCENCE STRIP IS CRACKED, DAMAGED AND HAS MOISTURE BUILD UP. REMOVED AND REPLACED FLOOR PHOTOLUMINESCENCE STRIP AT 3DEF IAW AMM 33-51-15.
- [SDR SWAA2026042793295](https://openairdocs.org/sdr/SWAA2026042793295.md): Hmu · leaking · Apr 26, 2026 · N8554X · Boeing 7378H4 · Fuel Controlling System
  > NUMBER 2 ENG FAILED ON TAKEOFF; REJECT AT APPROX 100 KIAS BRK ENERGY 21.1M FT-LB. INSPECTION REQUIRED ABOVE 30.0M FT-LM. DURING INITIAL EVALUTATION FAULT CODE 73-31552 IS PRESENT IN EEC IAW FIM 73-31, TASK 803. PERFORMED GVI OF NR 2 ENGINE AND DISCOVERED H
- [SDR SWAA2026042793346](https://openairdocs.org/sdr/SWAA2026042793346.md): Pump · failed · Apr 26, 2026 · N8554X · Boeing 7378H4 · Engine Fuel Pump
  > NUMBER 2 ENGINE FAILED ON TAKEOFF, REJECT AT APPROX 100 KIAS BRK ENERGY 21.1M FT-LB; INSPECTION REQUIRED ABOVE 30.0M FT-LM. DURING INITIAL EVALUTATION FAULT CODE 73-31552 IS PRESENT IN EEC REF FIM 73-31 TASK 803. PERFORMED GVI OF NR 2 ENGINE AND DISCOVERED
- [SDR SWAA2026042792200](https://openairdocs.org/sdr/SWAA2026042792200.md): Cover · loose · Apr 23, 2026 · N8554X · Boeing 7378H4 · Escape Slide
  > L1 DOOR SLIDE COVER 2EA CLIPS ARE LOOSE. RESECURED L1 DOOR SLIDE COVER 2EA CLIPS IAW SRM 51-40-02.
- [SDR SWAA2026040785437](https://openairdocs.org/sdr/SWAA2026040785437.md): Flashlight · failed · Apr 1, 2026 · N8554X · Boeing 7378H4 · Emergency Equipment
  > LEFT OTBD AFT FLASHLIGHT HAS RED LIGHT. R & R FLASHLIGHT ASSY IAW AMM 25-64-00 IN L/H AFT OTBD POSITION.
- [SDR SWAA2025103029303](https://openairdocs.org/sdr/SWAA2025103029303.md): Megaphone · inoperative · Oct 28, 2025 · N8554X · Boeing 7378H4 · Emergency Equipment
  > AFT MEGAPHONE INOPERATIVE. REMOVED AND REPLACED IAW AMM 25-64-00-SWA-804-NG-01.
- [SDR SWAA2025021496140](https://openairdocs.org/sdr/SWAA2025021496140.md): Flashlight · no test · Feb 14, 2025 · N8554X · Boeing 7378H4 · Emergency Equipment
  > AFT R/H F/A FLASHLIGHT NOT TESTING<[01] REPLACED AFT F/A FLASHLIGHT PER AMM 25-64-00.
- [SDR SWAA20250131001](https://openairdocs.org/sdr/SWAA20250131001.md): Lens · missing · Jan 30, 2025 · N8554X · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS MISSING<[01] REPLACED MISSING CENTER AISLE CEILING EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01. OSD: 1/31/2025
- [SDR SWAA2024092742731](https://openairdocs.org/sdr/SWAA2024092742731.md): Girt Bar · out of adjust · Sep 26, 2024 · N8554X · Boeing 7378H4 · Emergency Equipment
  > PLASTIC PIECE FELL OFF DOOR R1 GIRT BAR.<[01] REPLACED R1 DOOR GIRT BAR EVAC RELEASE STOP PER AMM 25-66-00.
- [SDR SWAA2024080722163](https://openairdocs.org/sdr/SWAA2024080722163.md): Light · inoperative · Aug 3, 2024 · N8554X · Boeing 7378H4 · Emergency Lighting
  > LEFT SIDE ROW 15CB OVER WING EXIT DOOR LIGHT INOPERATIVE<[01] OK TO CONT. PER MEL 33-2-04 SP#1 AUTH.#207613;[02] R&RD WINDOW LIGHT ASSEMBLY AT ROW 15CB IAW AMM 33-21-00; LOADED SOFTWARE AS REQUIRED AND OPS CHECK GOOD
- [SDR SWAA2024072516170](https://openairdocs.org/sdr/SWAA2024072516170.md): Flashlight · inoperative · Jul 23, 2024 · N8554X · Boeing 7378H4 · Emergency Equipment
  > 1 AFT EMERGENCY FLASHLIGHT INOP<[01] REPLACED AFT EMERGENCY FLASHLIGHT AND BATTERY. OPS NORMAL. REF AMM 25-64-00
- [SDR SWAA2024072516811](https://openairdocs.org/sdr/SWAA2024072516811.md): Battery · inoperative · Jul 23, 2024 · N8554X · Boeing 7378H4 · Emergency Equipment
  > 1 AFT EMERGENCY FLASHLIGHT INOP<[01] REPLACED AFT EMERGENCY FLASHLIGHT AND BATTERY. OPS NORMAL. REF AMM 25-64-00
- [SDR SWAA2024050281409](https://openairdocs.org/sdr/SWAA2024050281409.md): Light · inoperative · May 2, 2024 · N8554X · Boeing 7378H4 · Emergency Lighting
  > RH SIDE SERVICE DOOR EMERGENCY LIGHT INOP<[01] R/R RH SLIDE SERVICE DOOR EMERGENCY LIGHT PER AMM 33-51-04
- [SDR SWAA2024010437127](https://openairdocs.org/sdr/SWAA2024010437127.md): Flashlight · inoperative · Jan 3, 2024 · N8554X · Boeing 7378H4 · Emergency Equipment
  > AFT CABIN F/OS SIDE FLASHLIGHT DOES NOT TEST<[01] SECURED AFT F/O FLASHLIGHT TO MOUNT PER SIP. NO DEFECTS NOTED.
- [SDR SWAA2023122735337](https://openairdocs.org/sdr/SWAA2023122735337.md): Cover · loose · Dec 26, 2023 · N8554X · Boeing 7378H4 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT SIGN MID CABIN CAME LOOSE<[01] RE-ATTACHED OVERHEAD EMERGENCY EXIT SIGN PLASTIC COVER REF 33-51-03
- [SDR SWAA2023121331100](https://openairdocs.org/sdr/SWAA2023121331100.md): Battery · inoperative · Dec 9, 2023 · N8554X · Boeing 7378H4 · Emergency Equipment
  > AFT CABIN FLASHLIGHT INOP<[01] R/R AFT CABIN FLASHLIGHT ASSY AND BATTERY IAW AMM 25-64-00 OPS CHECK GOOD
- [SDR SWAA2023121329560](https://openairdocs.org/sdr/SWAA2023121329560.md): Flashlight · inoperative · Dec 9, 2023 · N8554X · Boeing 7378H4 · Emergency Equipment
  > AFT CABIN FLASHLIGHT INOP<[01] R/R AFT CABIN FLASHLIGHT ASSY AND BATTERY IAW AMM 25-64-00 OPS CHECK GOOD
- [SDR SWAA2023120526716](https://openairdocs.org/sdr/SWAA2023120526716.md): Skirt · out of adjust · Dec 3, 2023 · N8554X · Boeing 7378H4 · Escape Slide
  > FWD ENTRY DOOR ESCAPE SLIDE; LOWER SKIRT MAKES HARD CONTACT WITH THE SCUFF PLATE WHEN OPENING AND CLOSING DOOR.<[01] ADJUSTED ESCAPE SLIDE ON FWD ENTRY DOOR PER AMM INTRODUCTION 2. STANDARD INDUSTRY PRACTICES STEP B AND AMM 25-66-01-400-801.;[02] VERIFIED CORR
- [SDR SWAA2023120526713](https://openairdocs.org/sdr/SWAA2023120526713.md): Lens · damaged · Dec 1, 2023 · N8554X · Boeing 7378H4 · Emergency Lighting
  > FWD LAV EMERGENCY EXIT LIGHT LENS DAMAGED<[01] REMOVED AND REPLACED FWD LAV EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01-960-802. OPS CHECK WAS GOOD.;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.
- [SDR SWAA2023120523637](https://openairdocs.org/sdr/SWAA2023120523637.md): Shield · cracked · Nov 21, 2023 · N8554X · Boeing 7378H4 · Nacelle/Pylon Miscellaneous Structure
  > #2 ENGINE O/B FAN COWL OIL ACCESS DOOR SHEILD IS CRACKED<[01] REMOVED AND REPLACED #2 ENGINE O/B FAN COWL OIL ACCESS DOOR SHEILD PER SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2023120518665](https://openairdocs.org/sdr/SWAA2023120518665.md): Attach Angle · cracked · Nov 6, 2023 · N8554X · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] R/H BS663 UPPER ATTACH ANGLE IS ON VAPOR BARRIER RBL8 WL167.68 REPAIRED BY REMOVED DAMAGE AREA; FABRICATED; LOCATED; DRILLED AND INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 PAR 4 A-P.
- [SDR SWAA2023120518045](https://openairdocs.org/sdr/SWAA2023120518045.md): Floor Panel · pulled · Nov 5, 2023 · N8554X · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 221AF UPPER SURFACE HAS PULLED STRANDS OF FIBERGLASS<[01] UPPER SURFACE REPAIR ON PANEL 221AF COMPLETED IAW SRM 53-00-50-2R-1;[02] VERIFIED RII INSPECTION REQUIREMENTS ARE MET.;[03] VERIFIED UPPER SURFACE REPAIR ON PANEL 221AF COMPLETED IAW SRM 53-00-50-
- [SDR SWAA2023120518782](https://openairdocs.org/sdr/SWAA2023120518782.md): Floor Panel · delaminated · Nov 4, 2023 · N8554X · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 221BF UPPER PLY IS DALAMINATED<[01] PANEL 221BF UPPER PLY DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS.
- [SDR SWAA2023120518039](https://openairdocs.org/sdr/SWAA2023120518039.md): Floor Support · cracked · Nov 4, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED AT BS 380-400 LBL13 WL208.<[01] ALL STEPS COMPLETE REMOVED CRACKED FLOOR SUPPORT AT BS 380-400 LBL13 WL208 PER SRM 51-40-02 COMPLETED MEASUREMENT TABLE.<BR>LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 380-400 LBL13 WL208 PER SRM 51-40-04 B
- [SDR SWAA2023120518040](https://openairdocs.org/sdr/SWAA2023120518040.md): Floor Support · cracked · Nov 4, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED AT BS 390 LBL51 WL208.<[01] REMOVED FLOOR SUPPORT ON BS 390 LBL 51 WL208 PER SRM 51-40-02 AND ENGINEER DWG: 143A5400 ID: 0183 (AND 0182).;[02] COMPLETED ALL STEPS REMOVED CRACKED FLOOR SUPPORT AT BS 390 LBL51 WL208 PER SRM 51-40-02 COMPLE
- [SDR SWAA2023120518037](https://openairdocs.org/sdr/SWAA2023120518037.md): Channel · cracked · Nov 4, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > FWD ENTRY DOOR MOPSILL CRACKED AT BS 303.9 LBL60 WL208<[01] INSTALLED FWD ENTRY DOOR MOPSILL IAW SRM 51-40-02-0G-0; BOEING DWG 140A9810 ID:71 REV:-; BOEING DWG 141A8110 ID:0022 REV:A AND BOEING DWG 141A8110 ID:0023 REV:-.;[02] CARD COMPLETE
- [SDR SWAA2023120518783](https://openairdocs.org/sdr/SWAA2023120518783.md): Floor Panel · exposed · Nov 4, 2023 · N8554X · Boeing 7378H4 · Fuselage Floor Panel
  > PANEL 241AF FORWARD RIGHT CORNER HAS EXPOSED CORE<[01] DUE TO EXTENT OF DAMAGE ON UPPER SURFACE OF PANEL FABRICATED NEW 241AF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1534398-1. INSTALLED INSERTS USING BMS5-107 LOT#AK3BA2380A/A; INSERTS CURED USING HEAT LAMP AND TH
- [SDR SWAA2023120517643](https://openairdocs.org/sdr/SWAA2023120517643.md): Floor Support · cracked · Nov 3, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > WING CENTER SECTION - CRACKED SUPPORT FLOOR AT BS 540 RBL 2 WL 208 (MARKED)<[01] REMOVED AND REPLACED FLOOR SUPPORT @ BS540 BL0-RBL25 WL208 PER SRM 51-40-02 AND DWG:143A0060 REV:A
- [SDR SWAA2023120517645](https://openairdocs.org/sdr/SWAA2023120517645.md): Floor Support · cracked · Nov 3, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > WING CENTER SECTION - CRACKED SUPPORT FLOOR AT BS 540 LBL 2 WL 208 (MARKED)<[01] REMOVED AND REPLACED CRACKED FLOOR SUPPORT AT BS 540 BL0-LBL25 WL 208 PER SRM 51-40-02; DWG#143A0060.;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.
- [SDR SWAA2023120517549](https://openairdocs.org/sdr/SWAA2023120517549.md): Floorbeam · corroded · Nov 3, 2023 · N8554X · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT PASSENGER COMPARTMENT FLOOR STRUCTURE - WET AREAS - CORROSION ON FLOOR BEAM BS 947 LBL 23.5 WL 208 (MARKED)<[01] VERIFIED MEASUREMENT TABLE.;[02] REMOVED AND REPAIRED DAMAGES FLANGE OF THE FLOOR BEAM BS947 LBL9-LBL36 WL208 I.A.W SRM 53-70-51-2R-5 REPAIR 5
- [SDR SWAA2023120517555](https://openairdocs.org/sdr/SWAA2023120517555.md): Floorbeam · corroded · Nov 3, 2023 · N8554X · Boeing 7378H4 · Fuselage Main, Floor Beam
  > AFT PASSENGER COMPARTMENT FLOOR STRUCTURE - WET AREAS - CORROSION ON FLOOR BEAM BS 947 LBL 15.75 WL 208 (MARKED)<[01] FAULT RESOLVED ON OTHER FAULT<BR>DAMAGE TO BE REPAIRED ON FAULT TTG8Q00PEN6P DUE TO EXCEED LIMITS GIVEN PER SRM 53-70-51-1A-1 AND REQUIRED A R
- [SDR SWAA2023120517171](https://openairdocs.org/sdr/SWAA2023120517171.md): Web · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS440+10' TO BS490' RBL 26.5 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] REMOVED AND REPLACED FWD CARGO BAY SUB THRESHOLD WEB BS 440-492 RBL 26.5 WL 156 PER
- [SDR SWAA2023120517172](https://openairdocs.org/sdr/SWAA2023120517172.md): Shield · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY AFT SHIELD BS500+3 TO BS500+17 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] VERIFIED STEP 1;2 COMPLETE.;[02] DAMAGED SHIELD REPLACED DUE NO DATA FOUND ON SRM NEW SHIELD LOCATED; DRILLED AND INSTALLED IAW SRM 51-40-02-0G-0
- [SDR SWAA2023120517173](https://openairdocs.org/sdr/SWAA2023120517173.md): Support · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT HAS MULTIPLE AREAS AROUND FASTENER HOLES BS500I LBL21 TO RBL21<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] CORROSION ON LOWER BULKHEAD SUPPORT WAS FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED
- [SDR SWAA2023120517174](https://openairdocs.org/sdr/SWAA2023120517174.md): Support Plate · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500I RBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] CUSTOMER CARD COMPLETE AND VERIFIED MEASUREMENT TABLE.;[03] CORROSION ON
- [SDR SWAA2023120517178](https://openairdocs.org/sdr/SWAA2023120517178.md): Shield · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE.;[02] CORROSION ON SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED
- [SDR SWAA2023120517175](https://openairdocs.org/sdr/SWAA2023120517175.md): Web · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS787+18' TO BS827+10' RBL 26 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB WAS FOUND TO BE OUT OF LIMITS. REMOVED
- [SDR SWAA2023120517176](https://openairdocs.org/sdr/SWAA2023120517176.md): Support Plate · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727E+19' TO BS767 RBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] VERIFIED STEPS 1-6;[03] MADE CORRECTIONS AND CHANGED STEP STATUS
- [SDR SWAA2023120517177](https://openairdocs.org/sdr/SWAA2023120517177.md): Support Plate · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727G+19' TO BS787+1' LBL22 WL156<[01] VERIFIED STEPS 1;2 COMPLETE AND MEASUREMENT TABLE.;[02] VERIFIED STEPS 1-6;[03] MADE CORRECTIONS AND CHANGED STEP STATUS T
- [SDR SWAA2023120517180](https://openairdocs.org/sdr/SWAA2023120517180.md): Strap · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS767+6 RBL11 WL156<[01] UPDATED MEASUREMENT TABLE. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFI
- [SDR SWAA2023120517181](https://openairdocs.org/sdr/SWAA2023120517181.md): Strap · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6 RBL6 WL156<[01] UPDATE MEASUREMENT TABLE. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFIE
- [SDR SWAA2023120517182](https://openairdocs.org/sdr/SWAA2023120517182.md): Strap · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727I+6 RBL10 WL156<[01] UPDATE MEASUREMENT TABLE. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFI
- [SDR SWAA2023120517183](https://openairdocs.org/sdr/SWAA2023120517183.md): Strap · corroded · Nov 2, 2023 · N8554X · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS887 RBL11.5 WL168<[01] UPDATE MEASUREMENT TABLE. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. PART REPLACEMENT REQUIRED PER SRM 51-10-02.;[02] VERIFIE
- [SDR SWAA2023120517302](https://openairdocs.org/sdr/SWAA2023120517302.md): Web · cracked · Nov 2, 2023 · N8554X · Boeing 7378H4 · Wing Miscellaneous Structure
  > RIGHT WING DEFLECTION CONTROL RIB WEB IS CRACKED AT THE O/B UPPER FASTENER CORNER (MARKED)<[01] UPDATED MEASUREMENTS; AND STEPS 1 & 2.;[02] REMOVED; REPLACED; AND INSTALLED A NEW R/W; T/E DEFLECTION CONTROL RIB WEB IAW SRM 51-40-02 AND BOEING DWG 115A2512. ALS
- [SDR SWAA2023120516251](https://openairdocs.org/sdr/SWAA2023120516251.md): Skin · debonded · Oct 31, 2023 · N8554X · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > PANEL 194CL OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 194CL WITH OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL WAS REPAIRED IAW SRM 51-70-05-2R-2.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE. JOB COMPLETE.
- [SDR SWAA2023100909080](https://openairdocs.org/sdr/SWAA2023100909080.md): Fseu · faulty · Oct 7, 2023 · N8554X · Boeing 7378H4 · Trailing Flap Position Indicating System
  > FLAP MALFUNCTION AT FLAPS 5. NO ASYMMETRY NOTED. T/EDGE FLAPS DISAGREE QRH RUN. C/W ALTN FLAPS DUTY CYCLE<[01] REMOVED AND REPLACED T/E FLAP POSITION INDICATOR PER M/M OPS CHECKED GOOD PER M/M 27-58-02; ALSO R AND R FSEU BOX PER M/M 27-58-02 OPS CHECKED GOOD-
- [SDR SWAA2023100908968](https://openairdocs.org/sdr/SWAA2023100908968.md): Indicator · faulty · Oct 7, 2023 · N8554X · Boeing 7378H4 · Trailing Flap Position Indicating System
  > FLAP MALFUNCTION AT FLAPS 5. NO ASYMMETRY NOTED. T/EDGE FLAPS DISAGREE QRH RUN. C/W ALTN FLAPS DUTY CYCLE<[01] REMOVED AND REPLACED T/E FLAP POSITION INDICATOR PER M/M OPS CHECKED GOOD PER M/M 27-58-02; ALSO R AND R FSEU BOX PER M/M 27-58-02 OPS CHECKED GOOD-
- [SDR SWAA2023072481288](https://openairdocs.org/sdr/SWAA2023072481288.md): Slide · out of position · Jul 21, 2023 · N8554X · Boeing 7378H4 · Escape Slide
  > FWD SVC DOOR SLIDE GIRYT BAR HARD TO INSTALL/REMOVE<[01] REPOSITION FWD SVC DOOR ESCAPE SLIDE IN CONTAINER PER AMM 25-66-01

Next page: https://openairdocs.org/aircraft/N8554X/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 = 'N8554X' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8554X/reports

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