# Service difficulty reports: N809MC, cancelled Nov 8, 2010

A list on [N809MC, cancelled Nov 8, 2010](https://openairdocs.org/deregistered/N809MC-2010-11-08.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 · 70 reports

- [SDR UIEA200900002](https://openairdocs.org/sdr/UIEA200900002.md): Blades · missing · Dec 30, 2008 · N809MC · Boeing 747228F · Turbine Section
  > DURING DESCENT CREW REPORTED SIGNIFICANT VIBRATION FROM NR 1 ENGINE. INSPECTION FOUND MISSING BLADES IN THE LPT AREA. ENGINE CHANGE IS IN PROGRESS.
- [SDR UIEA200900003](https://openairdocs.org/sdr/UIEA200900003.md): Inu · failed · Dec 24, 2008 · N809MC · Boeing 747228F · Inertial Guidance System
  > AIR TURN BACK DUE TO NR 1 INS RED WARNING LIGHT ON WITH HDG AND FLIGHT DIRECTOR FLAGS IN VIEW. FOUND NR 1 INU FAILED. REPLACED INU, OPS CHECKED OK.
- [SDR UIEA200800328](https://openairdocs.org/sdr/UIEA200800328.md): Panel · cracked · Oct 12, 2008 · N809MC · Boeing 747228F · Fuselage Miscellaneous Structure
  > NOSE WHEEL WELL LT SIDE AT STA 273.0, WATER LINE 160 HAS A 0.250 INCH CRACK DETECTED WITH HFEC INSPECTION. INTERM REPAIR WAS ACCOMPLISHED IAW SRM 53-10-04, FIG 116, SHEETS 1 THRU 6. INITIAL AND REPEAT INSPECTION TO BE ACCOMPLISHED AT 15,000 FC AND THERE AFTE
- [SDR UIEA200800329](https://openairdocs.org/sdr/UIEA200800329.md): Skin Panel · debonded · Oct 12, 2008 · N809MC · Boeing 747228F · Wing, Plate/Skin
  > RT WING UPPER SURFACE L/E PANEL AT ILES 328.5 HAS A PREVIOUS REPAIR AREA 7.0 BY 6.0 INCHES DISBONDING AND CRACKING. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09, FIG 18, SHEETS 2 AND 5, PREPREG 250 DEGREE F CURE IAW SRM 51-40-12. ALSO, REF EO NR 4757A465.
- [SDR UIEA200800295](https://openairdocs.org/sdr/UIEA200800295.md): Inu · failed · Aug 18, 2008 · N809MC · Boeing 747228F · Inertial Guidance System
  > NR 1 INS DIFFERS FROM NR 2 INS BY 35 NM OR 50 KTS. FAILED ACCURACY TEST. DUMPED FUEL AND DIVERTED TO JFK. REPLACED NR 1 INU AND ALIGNED OPS CHECKED OK PER 34-41-03. (S)
- [SDR UIEA200800192](https://openairdocs.org/sdr/UIEA200800192.md): Door · damaged · May 14, 2008 · N809MC · Boeing 747228F · Landing Gear Doors
  > WHILE TROUBLESHOOTING INBOUND LOG ITEM FOR NR 1 HYD SYSTEM OVERHEAT BODY GEAR DOORS BOTH SIDES CAME IN CONTACT WITH THE TIRES WHEN HYD POWER WAS APPLIED. CAUSING DAMAGE TO BOTH DOORS. REMOVED AND REPLACED RT AND LT INBOARD BODY GEAR DOORS PER AMM 32-14-01.
- [SDR UIEA200800185](https://openairdocs.org/sdr/UIEA200800185.md): Pump · failed · May 11, 2008 · N809MC · Boeing 747228F · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTED HYD SYSTEM NR 1 OVERHEAT. ADP AND EDP TURNED OFF. ALL PUMPS ON NR 1 OFF OCCASIONAL OVERHEAT INDICATION CONTINUED. AFTER 1 HOUR NO OVERHEAT INDICATION. THEN THE PROBLEM RETURNED. REMOVED AND REPLACED NR 1 ENGINE EDP PER AMM 29-11-05, OPS AND
- [SDR UIEA200800181](https://openairdocs.org/sdr/UIEA200800181.md): Skin Panel · delaminated · May 9, 2008 · N809MC · Boeing 747228F · Wing, Plate/Skin
  > RT WING UPPER FIXED T/E PANEL HAS LOOSE AND WORKING FASTENERS, PANEL IS DELAMINATED. PANEL LOCATED INBOARD OF INBOARD AILERON, AT WBL STA 445.0, DELAMINATION AFT EDGE OF PANEL. AREA OF DELAMINATION IS 9.0 INCH LONG BY 1.5 INCH WIDE. PERMANENT REPAIR ACCOMPL
- [SDR UIEA200800180](https://openairdocs.org/sdr/UIEA200800180.md): Skin Panel · delaminated · May 9, 2008 · N809MC · Boeing 747228F · Wing, Plate/Skin
  > RT WING UPPER FIXED L/E PANEL DELAMINATED, 6.0 FEET OUTBOARD OF NR 3 ENGINE, 12 INCHES FROM AFT EDGE OF PANEL AT ILES STA 772.5. AREA OF DELAMINATION IS 14.0 INCH LONG BY 3.0 INCH WIDE. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 18, SHEE
- [SDR UIEA200800179](https://openairdocs.org/sdr/UIEA200800179.md): Skin Panel · cracked · May 9, 2008 · N809MC · Boeing 747228F · Wing, Plate/Skin
  > RT WING UPPER FIXED TRAILING EDGE PANEL HAS COMPOSITE CRACK, 3.5 INCHES FROM FORWARD EDGE OF PANEL AT WBL STA 515. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 2, SHEET 1, 2 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-12. REF: ATLAS AIR E
- [SDR UIEA200800178](https://openairdocs.org/sdr/UIEA200800178.md): Skin Panel · delaminated · May 9, 2008 · N809MC · Boeing 747228F · Wing, Plate/Skin
  > LT WING UPPER FIXED L/E PANEL DELAMINATED, INBOARD OF NR 2 ENGINE, 8.0 INCHES FROM AFT EDGE OF PANEL AT ILES STA 545.56. AREA OF DELAMINATION IS 2.0 BY 2.0 INCHES. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 18, SHEETS 3 AND 5 PREPREG 250
- [SDR UIEA200800177](https://openairdocs.org/sdr/UIEA200800177.md): Skin Panel · cracked · May 9, 2008 · N809MC · Boeing 747228F · Wing, Plate/Skin
  > LT WING UPPER FIXED LEADING EDGE PANEL CRACKED AND DELAMINATED, ILES 833.00, 20 INCHES FROM AFT EDGE OF PANEL. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 18, SHEETS 3 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-12. REF: ATLAS AIR EO NR
- [SDR UIEA200800006](https://openairdocs.org/sdr/UIEA200800006.md): O-Ring · leaking · Jan 6, 2008 · N809MC · Boeing 747228F · Hydraulic System, Main
  > APPROX 1 HOUR 15 MIN AFTER T/O NR 1 ENGINE OIL QTY IND ZERO, TEMP AND PRESS NORMAL ABOUT 2 HOURS 30 MIN AFTER T/O PRESSURE BEGAN VERY SLOW DROP WITH SLOW FLUX 5 PSI DURING DESCENT WITH ENGINE AT IDLE OIL PRESSURE LIGHT ILLUMINATED OCCASIONALLY BUT PRESS NEVER
- [SDR UIEA200700481](https://openairdocs.org/sdr/UIEA200700481.md): Skin · delaminated · Nov 30, 2007 · N809MC · Boeing 747228F · Spoilers
  > RIGHT WING SPOILER NR 7 HAS DELAMINATION. DISBONDED UPPER AND LOWER SURFACE 35" BY 25". REMOVED AND REPLACED THE NR 7 SPOILER IAW AMM 27-62-01 OPS CHECKED TRANS TO RUN UP AND LEAK CHECK SHEET 01-AA-74A ITEM NR 3.
- [SDR UIEA200700451](https://openairdocs.org/sdr/UIEA200700451.md): Access Panel · delaminated · Oct 3, 2007 · N809MC · Boeing 747228F · Air Conditioning Doors
  > AIR CONDITION ACCESS PANEL 192ER EXTERNAL SURFACE IS DELAMINATED. REPAIRED AS PER SRM 51-40-17 AND BOEING MESSAGE 1-638498164-2.
- [SDR UIEA200700446](https://openairdocs.org/sdr/UIEA200700446.md): Fitting · corroded · Oct 1, 2007 · N809MC · Boeing 747228F · Fuselage Main, Attach Fittings
  > BS 230 RBL 1 BILGE AREA BEAM WEB SUPPORT FITTING CORRODED. REPLACED FITTING AS PER SRM 51-10-01 AND BOEING MESSAGE 1-637033946-3.
- [SDR UIEA200700444](https://openairdocs.org/sdr/UIEA200700444.md): Bulkhead · cracked · Oct 1, 2007 · N809MC · Boeing 747228F · Fuselage Main, Bulkhead
  > RIGHT SIDE NOSE WHEEL WELL BULKHEAD WEB CRACKED AT STATION 260, WL 182 RBL 38. WEB REPAIRED AS PER BOEING MESSAGE 1-636527780-4.
- [SDR UIEA200700447](https://openairdocs.org/sdr/UIEA200700447.md): Skin · corroded · Sep 30, 2007 · N809MC · Boeing 747228F · Spoilers
  > NR 8 SPOILER AREA OF UPPER SKIN AND REAR SPAR HAS AREA OF CORROSION. REPAIRED AS PER BOEING MESSAGE 1--638467931-2.
- [SDR UIEA200700450](https://openairdocs.org/sdr/UIEA200700450.md): Brace · loose · Sep 29, 2007 · N809MC · Boeing 747228F · Nacelle/Pylon, Attach Fittings
  > NR 1 PYLON DIAGONAL BRACE UNDERWING FITTING TENSION FASTENER HEAD SHEARED. REMOVED AND INSTALLED FASTENER AS PER 51-30-02.
- [SDR UIEA200700449](https://openairdocs.org/sdr/UIEA200700449.md): Spar Cap · corroded · Sep 29, 2007 · N809MC · Boeing 747228F · Wing Spar
  > RIGHT WING FRONT SPAR LOWER CHORD AREA BETWEEN FSSO 1322 AND 1340 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND BOEING MESSAGE 1-638497220-2.
- [SDR UIEA200700448](https://openairdocs.org/sdr/UIEA200700448.md): Spar Cap · corroded · Sep 29, 2007 · N809MC · Boeing 747228F · Wing, Rib/Bulkhead
  > RIGHT WING FRONT SPAR LOWER CHORD AREA FSSO 1356 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND BOEING MESSAGE 1-638497220-2.
- [SDR UIEA200700443](https://openairdocs.org/sdr/UIEA200700443.md): Brace · chafed · Sep 29, 2007 · N809MC · Boeing 747228F · Nacelle/Pylon, Attach Fittings
  > NR 4 STRUT DIAGONAL BRACE FORWARD END CHAFED. CHAFING AREA DAMAGE BLENDED AS PER BOEING MESSAGE 1-636565614-4.
- [SDR UIEA200700445](https://openairdocs.org/sdr/UIEA200700445.md): Fairing · delaminated · Sep 26, 2007 · N809MC · Boeing 747228F · Aerodynamic Fairings
  > FUSELAGE FAIRING 193C AREA OF DELAMINATION. DELAMINATED AREA REPAIRED AS PER SRM 51-40-12
- [SDR UIEA200700324](https://openairdocs.org/sdr/UIEA200700324.md): Skin · delaminated · Aug 24, 2007 · N809MC · Boeing 747228F · Wing, Plate/Skin
  > LT WING UPPER SURFACE TRAILING EDGE FIXED PANEL AT STATION 1224 HAS AN AREA OF 2.0 INCH LONG BY 15.0 INCH WIDE AREA OF DELAMINATION. PERMANENT REPAIR OF AREA WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 4 & 5.
- [SDR UIEA200700248](https://openairdocs.org/sdr/UIEA200700248.md): Skin · dented · Jun 16, 2007 · N809MC · Boeing 747228F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE, RT SIDE AT STA 660 HAS A DENT BETWEEN S43 AND S44 RT CAUSED BY ACCIDENT DURING STORM. ACCOMPLISHED PERMANENT REPAIR OF EXTERIOR SKIN AS PER 747-200 SRM 53-30-03 FIG 17, ALSO, PERMANENT REPAIR OF BROKEN SHEAR TIE AT BS 660 S43R-S44R WAS REPAIRE
- [SDR UIEA200700247](https://openairdocs.org/sdr/UIEA200700247.md): Skin · unknown · Jun 16, 2007 · N809MC · Boeing 747228F · Fuselage Main, Plate/Skin
  > RADOME SKIN HAS A 2.0 INCH BY 4.0 INCH PREVIOUS REPAIR FILLER ERODED AT 11 O'CLOCK POSITION. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 53-50-03 PAGE 23, PAR 15. ALSO REFERENCE ATLAS AIR XEO 53-061507-1.
- [SDR UIEA200700144](https://openairdocs.org/sdr/UIEA200700144.md): Skin · cracked · Mar 24, 2007 · N809MC · Boeing 747228F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS A CRACK APPROX 400", AT BS 789 S46R AND RIVET PULLING THROUGH. REPAIRED ACCOMPLISHED AS PER XEO NR 53-032207.
- [SDR UIEA200700132](https://openairdocs.org/sdr/UIEA200700132.md): Oil Filter · unserviceable · Mar 2, 2007 · N809MC · Boeing 747228F · Turbine Engine Oil System
  > NR 2 OIL FILTER BY PASS LIGHT ILLUMINATED DURING DESCENT, LIGHT REMAINED AT IDLE THRUST, SHUT DOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE OIL FILTER AS PER MM 79-21-04. PERFORMED ENGINE RUN NO LEAK NOTED.
- [SDR UIEA200700002](https://openairdocs.org/sdr/UIEA200700002.md): Seat Track · broken · Jan 8, 2007 · N809MC · Boeing 747228F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPARTMENT SEAT TRACK AT STATION 1960 RT, RBL 11 HAS 1 EACH BROKEN CROWN LUG. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STATION 1946 TO 1969 RT AS PER 747 SRM 53-10-05 FIG 14.
- [SDR UIEA200600291](https://openairdocs.org/sdr/UIEA200600291.md): Circuit Card · failed · Nov 12, 2006 · N809MC · Boeing 747228F · Landing Gear Retraction/Extension System
  > RED GEAR LIGHT CAME ON AFTER RETRACTION WITH AURAL WARNING ON IN UP POSITION, GEAR UNSAFE CHECK ACCOMPLISHED PER FHB PROCEDURES AND RETURNED FOR LANDING. T/S FOUND A-9 CARD IN ALT CONTROL BOX FAILED. REMOVED AND REPLACED CARD PER AMM 32-61-00.
- [SDR UIEA200600282](https://openairdocs.org/sdr/UIEA200600282.md): Skin · cracked · Nov 1, 2006 · N809MC · Boeing 747228F · Passenger/Crew Doors
  > MAIN ENTRY DOOR L-1, LOWER, FORWARD HINGE CUT-OUT HAS A CRACK AT PREVIOUS REPAIR DOUBLER. PERMANENT EXTERNAL DOUBLER REPAIR WAS ACCOMPLISHED IAW SB 747-52-2144 REV 2 AND REFERENCE EO NR 4752A111.
- [SDR UIEA200600197](https://openairdocs.org/sdr/UIEA200600197.md): Skin · delaminated · Aug 4, 2006 · N809MC · Boeing 747228F · Trailing Edge Flaps
  > RT AFT IB FLAP UPPER AND LOWER SIDES OF SKIN HAVE AN AREA OF DELAMINATION. UPPER SIDE IS AT WBL 278.750 AND DAMAGE AREA IS 1.5 INCHES. LOWER SIDE IS AT WBL 272.00 AND DAMAGE IS 2.0 INCHES. ACCOMPLISHED PREPREG 250 DEGREES F. PERMANENT REPAIR OF BOTH AREAS IAW
- [SDR UIEA200600156](https://openairdocs.org/sdr/UIEA200600156.md): Flap · activated · Jul 2, 2006 · N809MC · Boeing 747228F · Trailing Edge Flap Control System
  > AFTER CLIMB-OUT AND FLAP RETRACTION FROM 5*-1*, FLAPS STAYED IN FLAPS 5* POSITION, ACCOMPLISHED ALT FLAP OPERATION SECT III FLAPS MOVED TO APPROX 3*, THEN STOPPED NO OTHER MOVEMENT WAS POSSIBLE INITIAL CK FOR OPEN C/B'S AND FURTHER INVESTIGATED PROBLEM. NO SP
- [SDR UIEA200600142](https://openairdocs.org/sdr/UIEA200600142.md): Steering Sys · malfunctioned · Jun 22, 2006 · N809MC · Boeing 747228F · Landing Gear Steering System
  > RTO AT 30 KTS AIRCRAFT DRIFTED LEFT WITH NO EFFECTIVE CONTROL, W/NOSE WHEEL STEERING. NOSE WHEEL STEERING APPEARS TO BE INOP. TRANSF TO DMI M06-076 PER MEL 32-18 CAT 'C'.PLACARD. VERIFIED OPS RUDDER PEDAL NORMAL. VERIFIED OPS TILLER STEERING NORMAL.
- [SDR UIEA200700249](https://openairdocs.org/sdr/UIEA200700249.md): Panel · cracked · Jun 16, 2006 · N809MC · Boeing 747228F · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STABILIZER, LOWER T/E ACCESS PANEL 334 GBL HAS 2 EACH CRACKS ON INBOARD SIDE OF PANEL. CRACKS ARE 2.0 INCH IN LENGTH. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-09 FIG 13, 747-200 SRM 51-40-12. ALSO REFERENCE ATLAS AIR XEO 55-06150
- [SDR UIEA200600122](https://openairdocs.org/sdr/UIEA200600122.md): Apu · malfunctioned · Jun 1, 2006 · N809MC · Boeing 747228F · APU Core Engine
  > APU FIRE BOTTLE WAS DISCHARGED DUE TO HEAVY BLACK SMOKE COMING FROM INLET, TAILPIPE, AND COWLING OF APU. APU INOP DUE TO FIRE BOTTLE PREVIOUSLY DISCHARGED. FIRE BOTTLE TRANSFERRED TO DI PG 88002 CAT C, PER MEL 26-8 M06-056. INSPECTED APU PER MM 49-11-00 PG6
- [SDR UIEA200600115](https://openairdocs.org/sdr/UIEA200600115.md): Skin · dented · May 8, 2006 · N809MC · Boeing 747228F · Fuselage Main, Plate/Skin
  > FOUND DENTS AT BS 660 BETWEEN S-46L AND S-45R. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-17408378 AND FAA FORM 8100-9.
- [SDR UIEA200600114](https://openairdocs.org/sdr/UIEA200600114.md): Skin · cracked · May 8, 2006 · N809MC · Boeing 747228F · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON RIGHT SIDE SKIN ASSEMBLY WAS FOUND CRACKED IN THE AREA COVERED BY TITANIUM DOUBLERS. INTERIM REPAIR FOR THE NR 1 PYLON 65B94100 SKIN ASSEMBLY, WAS ACCOMPLISHED AS PER BOEING MESSAGE 1-178658112 AND FAA FORM 8100-9.
- [SDR UIEA200600113](https://openairdocs.org/sdr/UIEA200600113.md): Skin · cracked · May 8, 2006 · N809MC · Boeing 747228F · Nacelle/Pylon, Plate/Skin
  > DURING A C-CHECK, CRACK DAMAGE WAS FOUND IN THE 65B94052 SKIN ASSEMBLY NR 3 STIFFENER AND PRE-COOLER EXHAUST CUT OUT EDGE ADJACENT TO N.S. 248 NR 2 PYLON. INTERIM REPAIR AS AN AMOC TO AD 95-13-07, ON THE RIGHT SIDE OF THE STRUT STRUCTURAL ASSEMBLIES OF THE NR
- [SDR UIEA200600111](https://openairdocs.org/sdr/UIEA200600111.md): Skin · cracked · May 8, 2006 · N809MC · Boeing 747228F · Nacelle/Pylon, Plate/Skin
  > THE CRACKS WERE FOUND IN THE SUBJECT STRUT CAP SKIN ASSEMBLY AND ADJACENT BULKHEAD STRAP AT STA-286 BULKHEAD INSTALLATION CROWN AREA AT B-L. 0-0. THE AFT EDGE OF CAP SKIN ASSEMBLY. THE BULKHEAD STRAP IN AREA COMMON TO CAP SKIN. INTERIM REPAIR OF THE 65B9405
- [SDR UIEA200600110](https://openairdocs.org/sdr/UIEA200600110.md): Skin · cracked · May 8, 2006 · N809MC · Boeing 747228F · Nacelle/Pylon, Plate/Skin
  > CRACK DAMAGE WAS FOUND IN THE 65B94052 SKIN ASSEMBLY NR 3 STIFFENER, AND PRE-COOLER EXHAUST CUT OUT ADJACENT TO THE AFT CORNER AT N.S.248, ON THE RIGHT SIDE OF THE STRUT STRUCTURAL ASSEMBLIES FOR NR 3 AND NR 4 PYLONS. INTERIM REPAIR FOR THE NR 3 AND NR 4 STRU
- [SDR UIEA200600106](https://openairdocs.org/sdr/UIEA200600106.md): Bulkhead · cracked · May 8, 2006 · N809MC · Boeing 747228F · Fuselage Main, Bulkhead
  > BS 2598 BULKHEAD AFT OUTER CHORD ATTACH FASTENER CRACKS AT STR 12L,LBL 50-55, WL 310-315. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-17563784 AND FAA FORM 8100-9.
- [SDR UIEA200600105](https://openairdocs.org/sdr/UIEA200600105.md): Skin · corroded · May 8, 2006 · N809MC · Boeing 747228F · Fuselage Main, Plate/Skin
  > CORROSION IN THE INTERNAL BEAR STRAP AT THE RT AFT CORNER OF THE FORWARD LAVATORY SERVICE DOOR CUT-OUT, BS 560, STR 46R. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE NR 1-177290023 ANF FAA FORM 8100-9.
- [SDR UIEA200600108](https://openairdocs.org/sdr/UIEA200600108.md): Floorbeam · corroded · May 4, 2006 · N809MC · Boeing 747228F · Fuselage Main, Floor Beam
  > REPORTED CORROSION ADJACENT TO AN EXISTING REPAIR ANGLE AT THE MAIN DECK FLOORBEAM UPPER T-CHORD HORIZONTAL FLANGE AT STA 620. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-178210650 AND FAA FORM 8100-9.
- [SDR UIEA200600103](https://openairdocs.org/sdr/UIEA200600103.md): Floorbeam · corroded · May 4, 2006 · N809MC · Boeing 747228F · Fuselage Main, Floor Beam
  > REPORTED CORROSION ON THE MAIN DECK FLOORBEAM UPPER T-CHORD HORIZONTAL FLANGE AT STA 500 BETWEEN APPROXIMATELY LBL 50.0 AND LBL 60.0. THE UPPER CHORD WAS REPLACED WITH SPLICES AT LBL 21.37.5 AND LBL 78.5, SIMILAR TO 747 SRM 53-10-07 FIG 12. REPAIR ACCOMPLISH
- [SDR UIEA200600112](https://openairdocs.org/sdr/UIEA200600112.md): Spar · corroded · May 3, 2006 · N809MC · Boeing 747228F · Trailing Edge Flaps
  > CORROSION DAMAGE FOUND IN SUBJECT SPAR AFT FLANGE AT WBL 770. INTERIM REPAIR TO OUTBOARD TRAILING EDGE MIDFLAP, NR 3 SPAR LOWER CHORD ACCOMPLISHED AS PER BOEING MESSAGE 1-177581561 AND FAA FORM 8100-9. DETAIL VISUAL INSPECTION THE EXPOSED AFFECTED AREA, FOR
- [SDR UIEA200600109](https://openairdocs.org/sdr/UIEA200600109.md): Skin · cracked · May 3, 2006 · N809MC · Boeing 747228F · Elevator, Plate/Skin
  > CRACKED RT OUTBOARD ELEVATOR PANEL AT ELEV STA 244 AND 306, P/N 65B05730-2. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-174409992 AND FAA FORM 8100-9.
- [SDR UIEA200600107](https://openairdocs.org/sdr/UIEA200600107.md): Web · cracked · Apr 25, 2006 · N809MC · Boeing 747228F · Horizontal Stabilizer Structure
  > CRACKED WEB AND LOWER CHORD AT THE RT HORIZONTAL STABILIZER STA BL 421.50. WEB AND LOWER CHORD REPAIR CARRIED OUT AS PER BOEING MESSAGE 1-17410726 AND FAA FORM 8100-9.
- [SDR UIEA200600104](https://openairdocs.org/sdr/UIEA200600104.md): Web · cracked · Apr 25, 2006 · N809MC · Boeing 747228F · Horizontal Stabilizer Structure
  > LT HORIZONTAL STAB, UPPER CHORD AT STAB BL 421.5 FOUND 1/2" CRACK AT AFT END. CHORD REPAIR CARRIED OUT AS PER BOEING MESSAGE 1-176012397 AND FAA FORM 8100-9.
- [SDR UIEA200600085](https://openairdocs.org/sdr/UIEA200600085.md): Frame · cracked · Apr 25, 2006 · N809MC · Boeing 747228F · Fuselage Main, Frame
  > RT STA 360 FRAME WEB AT STR 14E CUT OUT FOUND CRACKED 7.5". CRACKS WERE FOUND ON FRAME WEB. REPAIR DOUBLERS WERE INSTALLED IAW BOEING MESSAGE NR 1-175762603, AND FAA FORM 8100-9.

Next page: https://openairdocs.org/deregistered/N809MC-2010-11-08/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 = 'N809MC' AND deregistration_id = 'N809MC-2010-11-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N809MC-2010-11-08/reports

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