FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO: 4453C024 REV 4 PART 3 STEP 3. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025052700700](https://openairdocs.org/sdr/UIEA2025052700700.md): Lug · cracked · Jun 11, 2025 · N499MC · Boeing 74747UF · Fuselage Miscellaneous Structure > 1EA CRACK WAS FOUND ON RH STA 1000 RBL 11.33 FRONT SPAR INTERCOSTAL LUG FITTING.(FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO: 4453C024 REV 4 PART 7 STEP 3. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025052900703](https://openairdocs.org/sdr/UIEA2025052900703.md): Panel · cracked · Jun 11, 2025 · N499MC · Boeing 74747UF · Fuselage Main, Structure > COCKPIT CTR CONSOLE LH FWD VERTICAL METAL PNL LWR CORNER NEAR I/B RUDDER PEDAL FOUND CRACK.(PANEL CRACK AREA REPAIRED AS PER RI-25-10-17662 REV A. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025052900704](https://openairdocs.org/sdr/UIEA2025052900704.md): Panel · cracked · Jun 11, 2025 · N499MC · Boeing 74747UF · Fuselage Main, Structure > COCKPIT - CTR CONSOLE RH FWD VERTICAL METAL PANEL LWR CORNER NEAR I/B RUDDER PADAL FOUND CRACK.(PANEL CRACK AREA REPAIRED AS PER RI-25-10-17662 REV A. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060100708](https://openairdocs.org/sdr/UIEA2025060100708.md): Skin · dented · Jun 11, 2025 · N499MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B MID FLAP FAIRING EXTERIOR SURFACE FOUND DENT.(PERFORMED REPAIR AT DENT AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060100709](https://openairdocs.org/sdr/UIEA2025060100709.md): Skin · delaminated · Jun 11, 2025 · N499MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060100710](https://openairdocs.org/sdr/UIEA2025060100710.md): Skin · delaminated · Jun 11, 2025 · N499MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060100711](https://openairdocs.org/sdr/UIEA2025060100711.md): Skin · delaminated · Jun 11, 2025 · N499MC · Boeing 74747UF · Trailing Edge Flaps > LHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060100712](https://openairdocs.org/sdr/UIEA2025060100712.md): Skin · delaminated · Jun 11, 2025 · N499MC · Boeing 74747UF · Trailing Edge Flaps > RHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5A.(1) REV 103. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060200713](https://openairdocs.org/sdr/UIEA2025060200713.md): Structure · damaged · Jun 11, 2025 · N499MC · Boeing 74747UF · Wing Structure > LHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060200714](https://openairdocs.org/sdr/UIEA2025060200714.md): Structure · damaged · Jun 11, 2025 · N499MC · Boeing 74747UF · Trailing Edge Flaps > LHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060200715](https://openairdocs.org/sdr/UIEA2025060200715.md): Structure · damaged · Jun 11, 2025 · N499MC · Boeing 74747UF · Trailing Edge Flaps > RHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060300719](https://openairdocs.org/sdr/UIEA2025060300719.md): Thrust Reverser · delaminated · Jun 11, 2025 · N499MC · Boeing 74747UF · Engine Thrust Reverser > #4 ENG O/B T/REV INNER WALL FOUND DELAMINATED AT FWD 3 O'CLOCK POSITION(DELAMINATE AREA REPAIRED AS PER ATLAS AIR EA-1978A219 REV O FIG 2. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060300720](https://openairdocs.org/sdr/UIEA2025060300720.md): Longeron · cracked · Jun 11, 2025 · N499MC · Boeing 74747UF · Fuselage Main, Longeron/Stringer > 1 EA CRACK WAS FOUND ON RH BS 1480 LONGERON EXTENSION FITTING RADIUS AREA.(LONGERON EXTENSION FITTING MOD CARRIED OUT AS PER ATLAS AIR EO NO: 4453A818 REV 20 PART 8. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060300721](https://openairdocs.org/sdr/UIEA2025060300721.md): Frame · cracked · Jun 11, 2025 · N499MC · Boeing 74747UF · Fuselage Main, Frame > 1 EA CRACK WAS FOUND AT FASTENER HOLE 6 O'CLOCK POSITION AT RH BS 1480 B/HEAD FRAME WEB I/B UPPER AREA. FRAME WEB REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 8. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025060600730](https://openairdocs.org/sdr/UIEA2025060600730.md): Skin · damaged · Jun 11, 2025 · N499MC · Boeing 74747UF · Cargo/Baggage Doors > NOSE CARGO DOOR (P/N: 65B13016-10, S/N: 000123) BIRD STRIKE DAMAGE STA 140 AND STA 200, BETWEEN S31R AND S42AR NOSE CARGO DOOR SKIN, FRAMES AND STRINGERS - CAT B PERMANENT REPAIRS.(NOSE CARGO DOOR SKIN DENT #1 AND DENT #2 REPAIRED AS PER RI-52-30-17671 REV - [SDR UIEA2025060600731](https://openairdocs.org/sdr/UIEA2025060600731.md): Stringer · damaged · Jun 11, 2025 · N499MC · Boeing 74747UF · Cargo/Baggage Doors > NOSE CARGO DOOR BIRD STRIKE DAMAGE REPETITION INSPECTION FINDING STA 160 STR 36R, FOUND DENT. STRINGER REPAIRED AS PER RI-52-30-17671 REV A. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025060600732](https://openairdocs.org/sdr/UIEA2025060600732.md): Door · damaged · Jun 11, 2025 · N499MC · Boeing 74747UF · Cargo/Baggage Doors > NOSE CARGO DOOR BIRD STRIKE DAMAGE REPETITION INSPECTION FINDING STA 180 BTN STR 31AR AND STA 34R. DOUBLER FOUND TOOL MARK. FRAME TOOL MARK AREA REPAIRED AS PER RI-52-30-17671 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025060800737](https://openairdocs.org/sdr/UIEA2025060800737.md): Plate · cracked · Jun 11, 2025 · N499MC · Boeing 74747UF · Fuselage Main, Structure > LH BLG I/B W/W DOOR CHAFE PLATE FOUND CRACK.(LH BLG I/B W/W DOOR CHAFE PLATE REPLACE AS PER HX RI-32-14-17675 REV A. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025021300134](https://openairdocs.org/sdr/UIEA2025021300134.md): Seat Track · corroded · Mar 2, 2025 · N499MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings > CORROSION AT SEAT TRACK/FLOOR BEAM AT LBL 11.33 AND STA 1635 AFT CARGO COMPARTMENT.REPAIRED SEAT TRACK/FLOOR BEAM FROM STA 1590 TO STA. 1650 PER B747 SRM 53-00-52-2R-12 REPAIR 12 AFT CARGO COM
- [SDR UIEA2025021300135](https://openairdocs.org/sdr/UIEA2025021300135.md): Seat Track · corroded · Mar 2, 2025 · N499MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
> CORROSION ON SEAT TRACK/FLOOR BEAM AT RBL 11.33 AMD STA 1710 AFT CARGO COMPARTMENT.( REPLACED 2 SECTIONS OF SEAT TRACKS FROM PREVIOUS REPAIR STA. 1610 TO 1766.5 TO FACTORY SPLICE AND SECOND SECTION FROM 17
- [SDR UIEA2025021300136](https://openairdocs.org/sdr/UIEA2025021300136.md): Seat Track · corroded · Mar 2, 2025 · N499MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
> CORROSION ON SEAT TRACK/FLOOR AT RBL 11.33 AND STA. 1675 AFT CARGO COMPARTMENT.( REPLACED TWO EACH SECTIONS OF SEAT TRACKS FROM PREVIOUSLY REPAIR STA 1610 TO 1766.5 TO FACTORY SPLICE AND 2ND SECTION FROM S
- [SDR UIEA2025021300137](https://openairdocs.org/sdr/UIEA2025021300137.md): Seat Track · corroded · Mar 2, 2025 · N499MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
> CORROSION ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 770 TO 785 AT MAIN CARGO DECK.( CLEANED AREA ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 770-785 AT MAIN DECK CARGO DECK. NO CORROSION NOTED. PER BSOPM 20-30-80 PAR. 1.A. REV 153. NO FURTHER DEFECTS NOTED. CLEANED AREA ON SEAT TRACK AT LBL 11.33 BETWEEN STA. 760-770 AT MAIN CARGO DECK, NO CORROSION NOTED PAR. 1.A REV 153 SOPM 30-20-80. NO FURTHER DEFECTS NOTED. REMOVED AND REPLACED BUSHING PER B747 SRM 53-40-90-2R-1 REPAIR 1 AND B747 AMM 32-13-01-004-001 AND 32-13-01-404-022. NO FURTHER DEFECTS NOTED. REMOVED AND REPLACED LH BODY GEAR BEARING CAP PER B747 SRM 53-40-90-2R-1 REPAIR 1 FIG. 201. NO FURTHER DEFECTS NOTED. REPLACED 2 SECTIONS OF SEAT TRACKS FROM PREVIOUS REPAIR STA 1610 TO STA 1766.5 TO FACTORY SPLICE AND 2ND SECTION FROM STA 1766-.5 TO STA. 1910 TO PREVIOUS REPAIR SPLICE RBL 11.33 PER B747-400F SRM
- [SDR UIEA2025021300142](https://openairdocs.org/sdr/UIEA2025021300142.md): Seat Track · corroded · Mar 2, 2025 · N499MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
> CORROSION ON SEAT TRACK/FLOOR BEAM AT RBL 11.33 STA. 1820.( REPLACED 2 EACH SECTIONS OF SEAT TRACKS FROM PREVIOUS REPAIR STA. 1610-1766.5 TO FACTORY SPLICE AND 2ND SECTON FROM STA. 1766.5 TO STA. 1910 TO PREVIOUS REPAIR SPLICE RBL 11.33 PER B747-400F SRM 53-
- [SDR UIEA2025021300143](https://openairdocs.org/sdr/UIEA2025021300143.md): Seat Track · corroded · Mar 2, 2025 · N499MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
> CORROSION ON SEAT TRACK/FLOOR BEAM AT LBL 11.33 AT STA. 1740.( CLEANED AREA ON SEAT TRACK/FLOOR BEAM AT LBL 11.33 AT STA. 1740 AT MAIN CARGO DECK. NO CORROSION NOTED PER SOPM 20-30-03 PAR. 1.A. REV 153 & SRM 53-60-52-001-1 FIG. 001 REV 102. NO FURTHER DEFECT
- [SDR UIEA2025021300144](https://openairdocs.org/sdr/UIEA2025021300144.md): Seat Track · corroded · Mar 2, 2025 · N499MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach Fittings
> CORROSION ON SEAT TRACK/FLOOR BEAM AT LBL 11.33 AT STA. 1620, REPAIRED SEAT TRACK FROM STA 1590-1650 LBL PER B747-400 SRM 53-00-52-2R-12 REPAIR 12. NO FURTHER DEFECTS NOTED REMOVED AND REPLACED RH SIDE BODY LANDING GEAR BEARING FITTING CAP PER B747 AMM 32-13-01-004-001 AND 32-13-01-404-022. SRM 53-40-90-2R-1
- [SDR UIEA2024110901083](https://openairdocs.org/sdr/UIEA2024110901083.md): Clamp · failed · Nov 9, 2024 · N499MC · Boeing 74747UF · Humidity Control System
> FL320 EICAS MESSAGE EQUIP COOLING. RETURNED TO MIA. REPEAT WRITE UP. AFTER LANDING, EICAS MESSAGE RETURNED( INSTALLED CLAMP ON WATER SEPERATOR IAW AMM 21-51-05-402-025. REACTIVATED PACK 2. OPS CHECK GOOD. DMI 220071 CLOSED. UPON LANDING, COMPLETED LIGHTING STRIKE INSP IAW AMM 05-51-13, OVERW
- [SDR UIEA2023093000861](https://openairdocs.org/sdr/UIEA2023093000861.md): Unknown · unknown · Sep 28, 2023 · N499MC · Boeing 74747UF · Standard Practices/Structures
> LIGHTNING STRIKE DURING CLIMB, AIR TURN BACK. OVERWEIGHT LANDING AND HIGH ENERGY STOP RESULTED IN 9 MELTED MAIN LANDING GEAR TIRE FUSE PLUGS AND DEFLATION OF TIRES.( AXLES NEED REPLACEMENT. MX CURRENTLY IN WORK PER AMM 05-51-10. 1) REMOVE THE DAMAGE AREA IAW SRM 51-40-02-0G-0 & 53-20-30-2R-2 REV 97. 2) REPAIR THE TENSION TIE AFTER CHANNEL IAW SRM 53-20-30-2R-2 REV 97. 3) CONDITION CHECK NORMAL & JOB COMPLETED 1) PFM EI T2023A53M-875 SEQUENCE A REV 0. 2) ACCOMPLISHED EI T2023A53M-875 REV 1 AND CONDITION CHECK NORMAL 1) REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORMED EI T2023A53M-834 SEQUENCE A REV 0. 3) ACCOMPLISHED EI T2023A53M-834 REV 1 & CONDITION CHECK NORMAL. 4) RECORD TH
- [SDR UIEA2023052200466](https://openairdocs.org/sdr/UIEA2023052200466.md): Unknown · unknown · May 17, 2023 · N499MC · Boeing 74747UF · Fuselage Structure (General)
> DEFORM - FOUND MAIN DECK SEAT TRACK FLOOR COVER DEFORM STA 1730 RBL 75( 1) REPAIR DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 97 & BOEING DWG 65B38251 SH 75 REV - & 65B38251 SH 32 REV -. 2) CONDITION CHECK NORMAL AND JOB COMPLETED 1) REPAIR DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 97 & BOEING DWG 144U0882 SH 3 REV B & 65B38251 SH 32 REV -. 2) CONDITION CHECK NORMAL AND JOB COMPLETED 1) REPAIR DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 97 REV 97 AND DWG 65B16004 SH 4 REV A. 2) CONDITION CHECK NORMAL AND JOB COMPLETED 1) REPAIR DAMAGE IAW SRM 53-00-52-2R-13 REV 97 AND DWG 65B16004 SH 4 REV A. 2) CONDITION CHECK NORMAL AND JOB COMPLETED 1) PERFORM REPAIR OF BROKEN SKIN DAMAGE FOUND ON RH WING INBD AILERON T/E OUTBD SIDE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFO. 2) CONDITION CHECK IS GOOD. 1) PERFORM DEVIATION AND PERFORM REPAIR IAW EI T2023A53M-835 REV 1. 2) ACCOMPLISHED EI T2023A53M-835 REV 2. 3) JOB COMPLETED 1) REPAIR DAMAGE AREA IAW EI T2023A53M-900 REV 0 AND SRM 53-00-51-02R-3 REPAIR 3 REV 97. 2) INSTALL REPAIR PARTS IAW EI T2023A53M-900 REV 0 AND SRM 53-00-51-2R-3 REPAIR 3 REV 97 & BOEING DWG
- [SDR UIEA2023052200473](https://openairdocs.org/sdr/UIEA2023052200473.md): Unknown · unknown · May 17, 2023 · N499MC · Boeing 74747UF · Fuselage Structure (General)
> FOUND M/D CGO FLOOR STRUCTURE CORROSION AT STA 2240 RBL 59 TO 80( 1) REPAIR DAMAGE AREA IAW EI T2023A53M-902 REV 0 AND SRM 53-00-51-2R-3 REPAIR 3 REV 97. 2) INSTALL REPAIR PARTS IAW EI T2023A53M-902 REV 0 AND SRM 53-00-51-2R-3 REPAIR 3 REV 97 AND BOEING DWG
- [SDR UIEA2023052200474](https://openairdocs.org/sdr/UIEA2023052200474.md): Shear Tie · unknown · May 17, 2023 · N499MC · Boeing 74747UF · Fuselage Structure (General)
> CRACK ON SHEAR TIE AT STA 1000 RBL 57.50 WL195( 1) REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) REPAIR DAMAGE AREA IAW EI T2023A53M-1018 SEQUENCE A REV 0. 3) INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 97 AND EI T2023A53M-1018 SEQUENCE A REV 0. 4)
- [SDR UIEA2023052200475](https://openairdocs.org/sdr/UIEA2023052200475.md): Shear Tie · unknown · May 17, 2023 · N499MC · Boeing 74747UF · Fuselage Internal Mounting Structure
> CRACK ON SHEAR TIE AT STA 1000 RBL 33.99 WL195( 1) REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) REPAIRED DAMAGE AREA IAW EI T2023A53M-1018 SEQUENCE A REV 0. 3) INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 97 AND EI T2023A53M-1018 SEQUENCE A REV 0.
- [SDR UIEA2023052200476](https://openairdocs.org/sdr/UIEA2023052200476.md): Unknown · unknown · May 17, 2023 · N499MC · Boeing 74747UF · Fuselage Structure (General)
> FND M/D BEAM CORROSION AT STA 2100 RBL 100( 1) REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 97 AND EI T2023A53M-1103 SEQUENCE A REV 0 AND BOEING DWG 65B38105 SH12 REV -, 65B38251 SH 62 REV A, 65B38251 SH 33 REV -, 65B38251 SH 67 REV A, 65B38406 SH 48 REV A.
Next page: https://openairdocs.org/aircraft/N499MC/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 = 'N499MC' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```
This list as a web page: https://openairdocs.org/aircraft/N499MC/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.
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