# Service difficulty reports: N493MC A list on [N493MC](https://openairdocs.org/aircraft/N493MC.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 7 · 301 reports - [SDR UIEA2026022200065](https://openairdocs.org/sdr/UIEA2026022200065.md): Adc · faulted · Feb 22, 2026 · N493MC · Boeing 74747UF · Air Data Computer > ALT DISAGREE EICAS MSG LEVEL FLIGHT AT FL280 GREATER THAN 200' L 27760 R/R CAPT LH AIR DATA COMPUTER IAW AMM 34-12-01/401 AND IPC 25-71-31-01A. OPS CHECK GOOD

) - [SDR UIEA2026021300050](https://openairdocs.org/sdr/UIEA2026021300050.md): Engine · failed · Feb 13, 2026 · N493MC · Boeing 74747UF · Engine (Turbine/Turboprop) > 16 SECONDS AFTER T/O OUT OF XHM, SOMETHING WAS INGESTED INFLIGHT INTO ENG NR 1, CREW HEARD A LOUD BANG. ENG NR 1 PARAMETERS STARTED TO DECLINE. VIB STARTED AND THRUST DROPPED, ENG WAS SHUT DOWN, AND FLIGHT DECLARED PAN PAN AND DIVERTED TO PVG. ENGINE 1 REMOV - [SDR UIEA2025121901352](https://openairdocs.org/sdr/UIEA2025121901352.md): Skin · cracked · Dec 20, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > LEFT WING OTBD AFT FLAP BOTTOM SKIN AT INBD AREA FOUND CRACKED. LT WING O/B AFT FLAP BOTTOM SKIN AT I/B AREA PERFORMED TIME-LIMITED REPAIR IAW EA 1957A259 PART 1 REV.0. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025031400335](https://openairdocs.org/sdr/UIEA2025031400335.md): Fairing · dented · Apr 18, 2025 · N493MC · Boeing 74747UF · Horizontal Stabilizer Structure > R/H H.STAB L/E FAIRING 341CR O/B REPAIR PATCH FND DENT(

DENT AREA REPAIRED AS PER SRM 55-10-01-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025031800354](https://openairdocs.org/sdr/UIEA2025031800354.md): Channel · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Miscellaneous Structure > STA 720 RH UPPER DECK TENSION TIE FWD CHANNEL FOUND CRACK APPROX 3/8" IN LENGTH(

TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 (REPAIR IS CAT B). NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032100363](https://openairdocs.org/sdr/UIEA2025032100363.md): Structure · corroded · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Main, Structure > M/D STA 1175 RBL 11.33 CHORD LWR SURFACE CORRODED(

CHORD REPLACED AS PER SRM 51-10-02. NEW CHORD HOLES TRANSFERRED AS PER SRM 51-40-05. NEW CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032100364](https://openairdocs.org/sdr/UIEA2025032100364.md): Lug · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Main, Attach Fittings > INTERCOSTAL LUG FITTING AT STA 1000 RBL 11.33 FOUND CRACK(

INTERCOSTAL LUG FITTING REPLACEMENT AS PER ATLAS AIR EO 4453C024 REV 4 PART 7 STEP 3 CONDITION 11. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032200374](https://openairdocs.org/sdr/UIEA2025032200374.md): Shear Tie · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Internal Mounting Structure > SHEAR TIE AT STA 1000 RBL 33.99 FOUND CRACK(

SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO 4453C024 REV 4 PART 8 STEP 2 CONDITION 13 AND RI-53-14-17485 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032300380](https://openairdocs.org/sdr/UIEA2025032300380.md): Rib · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Horizontal Stabilizer, Spar/Rib > R/H H/STAB TIP CLOSURE RIB FOUND LOWER CHORD CRACKED(

CRACK LOWER CHORD REPLACED AS PER SRM 51-10-02. NEW LOWER CHORD HOLES TRANSFERED AS PER SRM 51-40-05. NEW LOWER CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032300381](https://openairdocs.org/sdr/UIEA2025032300381.md): Rib · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Horizontal Stabilizer, Spar/Rib > R/H H/STAB TIP CLOSURE RIB FOUND WEB CRACKED(

CRACK WEB REPLACED AS PER SRM 51-10-02. NEW WEB HOLES TRANSFERED AS PER SRM 51-40-05. NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032300382](https://openairdocs.org/sdr/UIEA2025032300382.md): Rib · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Horizontal Stabilizer, Spar/Rib > RH H.STAB TIP CLOSURE RIB FOUND UPPER CHORD CRACKED(

CRACK UPPER CHORD REPLACED AS PER SRM 51-10-02. NEW UPPER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05. NEW UPPER CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032500385](https://openairdocs.org/sdr/UIEA2025032500385.md): Bulkhead · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Main, Bulkhead > LH BS 1480 B/HEAD VERTICAL WEB I/B AREA FOUND CRACK(

VERTICAL WEB CRACK AREA REPAIRED A PER SRM 53-40-08-2R-1 REPAIR FIG 201 AND RI-53-40-17541 REV B. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032500386](https://openairdocs.org/sdr/UIEA2025032500386.md): Bulkhead · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Rotorcraft Tail Boom > RH BS 1480 B/HEAD VERTICAL WB I/B AREA FOUND CRACK(

VERTICAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-08-2R-1 REPAIR 1 FIG 201 AND RI-53-40-17541 REV B. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032500387](https://openairdocs.org/sdr/UIEA2025032500387.md): Skin · worn · Apr 18, 2025 · N493MC · Boeing 74747UF · Nacelle/Pylon, Plate/Skin > #3 RH CORE COWL UPPER AFT AREA FND WORN OUT(

WORN OUT AREA REPAIRED AS PER SRM 54-41-01-2R-5 REPAIR 5 FIG 202 DETAIL III. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032700391](https://openairdocs.org/sdr/UIEA2025032700391.md): Skin · damaged · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Main, Plate/Skin > FUS SECTION 48 APPROX STA 2658 - STA 2701, WL 280-WL 340 AREA FOUND FUS SKIN SEVERAL RIVETS LOOSE(

SKIN REPLACED AS PER RI-53-80-17492 REV B. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032700394](https://openairdocs.org/sdr/UIEA2025032700394.md): Skin · debonded · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > LHW O/B FORE FLAP LOWER T/E O/B AREA FOUND DEBOND(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800395](https://openairdocs.org/sdr/UIEA2025032800395.md): Skin · damaged · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > RHW I/B MID FLAP O/B T/E SCREW HOLE FOUND ELONGATED(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. K. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800396](https://openairdocs.org/sdr/UIEA2025032800396.md): Skin · delaminated · Apr 18, 2025 · N493MC · Boeing 74747UF · Elevator, Plate/Skin > LH ELEVATOR UPPER I/B AREA FOUND DELAMINATION(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800397](https://openairdocs.org/sdr/UIEA2025032800397.md): Skin · chafed · Apr 18, 2025 · N493MC · Boeing 74747UF · Ailerons > RHW I/B AILERON LOWER O/B AREA FOUND CHAFING(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-06 PAR 5. G. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800398](https://openairdocs.org/sdr/UIEA2025032800398.md): Skin · punctured · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > LHW O/B FORE FLAP LOWER T/E MID AREA FOUND PUNCH(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800399](https://openairdocs.org/sdr/UIEA2025032800399.md): Skin · delaminated · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > LHW O/B MID FLAP MOST O/B L/E FAIRING FOUND DELAMINATION(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800400](https://openairdocs.org/sdr/UIEA2025032800400.md): Access Door · worn · Apr 18, 2025 · N493MC · Boeing 74747UF · Nacelle/Pylon, Main Frame > #2 PYLON I/B ACCESS DOOR #462ER FOUND 2EA SCREW HOLES WORN(

PANEL FABRICATED AS PER RI-54-50-17522 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800401](https://openairdocs.org/sdr/UIEA2025032800401.md): Skin · bulged · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B FORE FLAP LOWER SURFACE O/B PANEL FOUND BULGE UP(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800402](https://openairdocs.org/sdr/UIEA2025032800402.md): Skin · bulged · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B FORE FLAP LOWER SURFACE O/B PANEL FOUND BULGE UP(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800403](https://openairdocs.org/sdr/UIEA2025032800403.md): Skin · bulged · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > RHW I/B FORE FLAP LOWER SURFACE I/B PANEL FOUND BULGE UP(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800404](https://openairdocs.org/sdr/UIEA2025032800404.md): Skin · bulged · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > RHW I/B FORE FLAP LOWER SURFACE O/B PANEL FOUND BULGE UP(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.202. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025032800405](https://openairdocs.org/sdr/UIEA2025032800405.md): Skin · chafed · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > RHW I/B AFT FLAP UPPER SURFACE MOST I/B PANEL FOUND CHAFING(

PERFORMED PERMANENT REPAIR AS PER RI-57-53-17513 REV. A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800406](https://openairdocs.org/sdr/UIEA2025032800406.md): Skin · chafed · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > RHW I/B AFT FLAP UPPER SURFACE MOST O/B PANEL FOUND CHAFING(

PERFORMED PERMANENT REPAIR AS PER RI-57-53-17526 REV. A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800407](https://openairdocs.org/sdr/UIEA2025032800407.md): Skin · scratched · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > LHW O/B AFT FLAP UPPER SURFACE I/B PANEL FOUND PUNCH(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG.201. NO FURTHER DEFECTS NOTED

/

) - [SDR UIEA2025032800408](https://openairdocs.org/sdr/UIEA2025032800408.md): Skin · scratched · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > LHW O/B AFT FLAP UPPER SURFACE O/B PANEL FOUND SCRATCH(

PERFORMED PERMANENT REPAIR AS PER RI-57-58-17523 REV. A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800409](https://openairdocs.org/sdr/UIEA2025032800409.md): Skin · scratched · Apr 18, 2025 · N493MC · Boeing 74747UF · Trailing Edge Flaps > LHW O/B AFT FLAP UPPER SURFACE MID PANEL FOUND SCRATCH(

PERFORMED PERMANENT REPAIR AS PER RI-57-58-17523 REV. A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800410](https://openairdocs.org/sdr/UIEA2025032800410.md): Frame · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Main, Frame > LH BS 2231 FRAME STR 16 ONE EACH FASTENER HOLE FOUND 2EA CRACK.(

STR 16 AND STR 17L CRACK AREA REPAIRED AS PER RI-53-60-17501 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800411](https://openairdocs.org/sdr/UIEA2025032800411.md): Frame · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Main, Frame > LH BS 2231 FRAME STR 17 ONE EACH FASTENER HOLE FOUND CRACK(

STR 16L AND STR 17L CRACK AREA REPAIRED AS PER RI-53-60-17501 REV A. (WORK DETAIL REFER WO.4545643 (5.738)). NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800412](https://openairdocs.org/sdr/UIEA2025032800412.md): Spar · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Wing Spar > RHW I/B MID FLAP REAR SPAR WEB O/B EDGE FWD CRACK(

REAR SPAR WEB CRACK AREA REPAIRED AS PER RI-57-53-17514 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800413](https://openairdocs.org/sdr/UIEA2025032800413.md): Floorbeam · punctured · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Main, Floor Beam > AFT CARGO COMPT RH STA 1880 RBL 36 FLOOR BEAM SUPPORT WEB FOUND PUNCH(

WEB REPAIRED AS PER RI-53-65-17515 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800414](https://openairdocs.org/sdr/UIEA2025032800414.md): Web · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Wing Miscellaneous Structure > 1EA CRACK WAS FOUND ON WEB AROUND 2EA FASTENERS ON LHW MID SPAR WEB UPPER FROM WS 382 TO WS 441(

M/D SPAR WEB REPAIRED AS PER RI-57-20-17528 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025032800415](https://openairdocs.org/sdr/UIEA2025032800415.md): Web · cracked · Apr 18, 2025 · N493MC · Boeing 74747UF · Wing Miscellaneous Structure > 5EA CRACK WERE FOUND ON WEB AROUND 2EA FASTENERS ON RHW MID SPAR WEB UPPER FROM WS 382 TO WS 411(

MID SPAR WEB REPAIRED AS PER RI-57-20-17527 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025040100420](https://openairdocs.org/sdr/UIEA2025040100420.md): Keelbeam · corroded · Apr 18, 2025 · N493MC · Boeing 74747UF · Fuselage Main, Keel > KEEL BEAM PNL 191KK AFT SUPPORT BEAM FOUND CORROSION(

KEEL BEAM PNL 191KK APT CORROSION SUPPORT BEAM REPLACED AS PER SRM 51-10-02. NEW SUPPORT BEAM HOLES TRANSFER AS PER SRM 51-40-05. NEW SUPPORT BEAM INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.< - [SDR UIEA2024081500832](https://openairdocs.org/sdr/UIEA2024081500832.md): Oxygen Mask · leaking · Aug 15, 2024 · N493MC · Boeing 74747UF · Crew Oxygen System > CREW REPORTED O2 LEAK, INSUFFICIENT QTY FOR CONTINUING TO ANC, DIVERTED TO YYC. CAPT O2 MASK HAD JUST BEEN REPLACED IN JFK PRIOR TO DEPARTURE.(

FOUND LOOSE FITTING ON 1ST OBSERVER O2 MASK BOX AND RETORQUED IAW AMM 35-11-18. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024061400519](https://openairdocs.org/sdr/UIEA2024061400519.md): Fmc · failed · Jun 14, 2024 · N493MC · Boeing 74747UF · Flight Management Computing Hardware System > LEFT FMC FAILURE(

R/R LEFT FMC IAW AMM 34-61-01 AND IPC 34-61-01-01B. OPS CHECK GOOD. TEST PASSED.

) - [SDR UIEA2024061100513](https://openairdocs.org/sdr/UIEA2024061100513.md): Detector · faulted · Apr 11, 2024 · N493MC · Boeing 74747UF · Air Distribution System > EQUIPMENT COOLING EICAS MESSAGE ON DEPARTURE FROM HKG. NON NORMAL CHECKLIST COMPLETED. EICAS CLEARED. AFTER LANDING EICAS MESSAGE RETURNED. REF CMC MESSAGE 21519. DURING WIRING CHECKS IAW WDM 21-58-01 WIRE BETWEEN F/D LOW FLOW DETECTOR (M7933) PIN 2 AND EQUIP - [SDR UIEA2024020500071](https://openairdocs.org/sdr/UIEA2024020500071.md): Door · missing · Feb 5, 2024 · N493MC · Boeing 74747UF · Landing Gear Doors > DURING WALK AROUND, FOUND LH BODY GEAR STRUT OUTBOARD DOOR MISSING.(

INSTALLED LH BODY LANDING GEAR STRUT OUTBOARD DOOR AND CK OK PER AMM 32-14-06.

) - [SDR UIEA2023040100300](https://openairdocs.org/sdr/UIEA2023040100300.md): Unknown · unknown · Apr 1, 2023 · N493MC · Boeing 74747UF · Oxygen System > RIGHT SUPERNUMERARY SEAT OXYGEN MASKS DEPLOYED (UNCOMMANDED) IN FLIGHT(

TRANSFER TO DMI 183092 PER MEL 35-21-01-02-01 CAT C, DUE DATE 11APR2023. 2 RIGHT SUPERNUMARY SEAT BLOCKED FOR PSU INOP (DOOR NOT SECURABLE). DOOR CLOSED AND SECURED BY TAPE. REPOSITIONE - [SDR UIEA2023031000243](https://openairdocs.org/sdr/UIEA2023031000243.md): Transceiver · unknown · Mar 9, 2023 · N493MC · Boeing 74747UF · UHF Communications System > ATB-RH HF RADIO NOT TRANSMITTING.(

REMOVED AND REPLACED RH HF TRANSCEIVER PER AMM 23-11-00. OPS CHECK GOOD

) - [SDR UIEA2023020500091](https://openairdocs.org/sdr/UIEA2023020500091.md): None · none · Mar 1, 2023 · N493MC · Boeing 74747UF · Fuselage Structure (General) > STA 900 LBL68" U/D TENSION TIE AFT CHANNEL 1EA HOLE FOUND CRACKED.(

STA 900 LBL68" U/D TENSION TIE AFT CHANNEL 1EA HOLE CRACK AREA OVERSIZE REPAIRED IAW EO 4453A301 PART 5 AND SB 747-53A2502 FIG 11.

) - [SDR UIEA2023021400112](https://openairdocs.org/sdr/UIEA2023021400112.md): None · none · Mar 1, 2023 · N493MC · Boeing 74747UF · Fuselage Structure (General) > RH 920 UPPER DECK TENSION TIE AT AFT CHANNEL FOUND 1 EA FASTENER HOLE CRACK AT 1 O/C POSITION(

STA 920 RBL 67" TENSION TIE CHANNEL 1 EA FASTENER HOLE CRACK AREA OVERSIZED DIA 0.278 REPAIRED IAW EO 4453A301 PART 6 AND SB 747-53A2502 REV A FIG 11

) - [SDR UIEA2023021400113](https://openairdocs.org/sdr/UIEA2023021400113.md): None · none · Mar 1, 2023 · N493MC · Boeing 74747UF · Fuselage Structure (General) > RH 880 UPPER DECK TENSION TIE AFT CHANNEL FOUND 1EA FASTENER HOLE CRACK AT 10 O/C POSITION(

STA 880 RBL 70.25 TENSION TIE CHANNEL 1 EA FASTENER HOLE CRACK AREA OVERSIZED DIA 0.309 REPAIRED IAW EO 4453A301 PART 6 AND SB 747-53A2502 REV.A FIG 11

) - [SDR UIEA2023021400114](https://openairdocs.org/sdr/UIEA2023021400114.md): None · none · Mar 1, 2023 · N493MC · Boeing 74747UF · Fuselage Structure (General) > RH 840 UPPER DECK TENSION TIE AFT CHANNEL FOUND 1 EA FASTENER HOLE CRACK AT 10 O/C POSITION(

STA 840 RBL 74.5" TENSION TIE CHANNEL 1 EA FASTENER HOLE CRACK AREA OVERSIZED DIA 0.309 REPAIRED IAW EO 4453A301 PART 6 AND SB 747-53A2502 REV.A FIG 11

) - [SDR UIEA2023021500118](https://openairdocs.org/sdr/UIEA2023021500118.md): None · none · Mar 1, 2023 · N493MC · Boeing 74747UF · Wing Structure > RHW L/E OLES 1520 LWR FIXED PNL SUPPORT CHANNEL FOUND CORROSION.(

RHW L/E OLES 1520 TO OLES 15835 LWR FIXED PNL SUPPORT CHANNEL P/N: 65B11862-30 CORROSION DAMAGE AREA REPAIRED IAW RI-57-00-16071 REV.A

) - [SDR UIEA2023021500120](https://openairdocs.org/sdr/UIEA2023021500120.md): None · none · Mar 1, 2023 · N493MC · Boeing 74747UF · Fuselage Structure (General) > F/D COCKPIT CENTER CONSOLE ADJACENT OF PEDDLE LHS PANEL FOUND CRACK(

F/D - COCKPIT LH PILOTS FORWARD PANEL SUPPORT WEB CRACK AREA REPAIRED IAW RI-53-00-16058 REV.A

) Next page: https://openairdocs.org/aircraft/N493MC/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 = 'N493MC' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N493MC/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.