# Service difficulty reports: N808MC, cancelled Feb 1, 2013

A list on [N808MC, cancelled Feb 1, 2013](https://openairdocs.org/deregistered/N808MC-2013-02-01.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR UIEA200500004](https://openairdocs.org/sdr/UIEA200500004.md): Slide · failed · Jan 26, 2005 · N808MC · Boeing 747212B · Escape Slide
  > UPPER DECK EMERGENCY ESCAPE SLIDE DID NOT PROPERLY DEPLOY WHEN ACTIVATED. (EA15200503933)
- [SDR UIEA200400179](https://openairdocs.org/sdr/UIEA200400179.md): Inu · failed · Oct 1, 2004 · N808MC · Boeing 747212B · Flight Environment Data
  > ON CLIMB OUT, NR 1 INS WARNING LIGHT CAME ON. ON CLIMB OUT NR 1 INS WARNING LIGHT CAME ON. NR 1 ADI AND HEADING FAILED. SELECTED NR 3 ATTITUDE AND COMPASS. APPROX 3 MINUTES LATER NR 3 INS WARNING LIGHT CAME ON. BOTH SCREENS WENT BLANK AND SHUT DOWN. REMO
- [SDR UIEA200400120](https://openairdocs.org/sdr/UIEA200400120.md): Controller · failed · Jul 7, 2004 · N808MC · Boeing 747212B · Cabin Pressure Controller
  > GT 8237/03 RMS/DOV AUTO FAIL LIGHT CAME ON DURING FLIGHT: AUTO FAIL LIGHT CAME ON DURING CLIMB ABOUT 8000 FT A/C ALTITUDE OUTFLOW VALVES.2500 CLOSED USED MANUAL IAW ABNORMAL CHECK LIST TO CONTROL DIFFERENTIAL PRESSURE AT 4 PSID CONTINUED FLIGHT. GOING THROU
- [SDR UIEA200400101](https://openairdocs.org/sdr/UIEA200400101.md): Bearing · migrated · Jun 4, 2004 · N808MC · Boeing 747212B · Trailing Edge Flaps
  > D-CHECK, DURING MAINTENANCE INSPECTION, ELONGATION DAMAGE WAS FOUND AT OB TRAILING EDGE FLAP TRACK NR 8 MOVABLE FAIRING ASSEMBLY HINGE FITTING LUGS. OVERSIZED THE BORES. DYE PENETRANT THE BORES TO ENSURE DEFECT FREE CONDITION. REFINISHED, INSTALLED ONE PIEC
- [SDR UIEA200400103](https://openairdocs.org/sdr/UIEA200400103.md): Bulkhead · cracked · Jun 4, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Bulkhead/Firewall
  > D-CHECK, DURING MAINTENANCE INSPECTION. NR 4 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND WL 146.5. THE AFT END OF THE STRAP CRACK WAS STOPPED DRILLED AND HFEC INSPECTED TO ENSURE CRACK CONTAINMENT. THE SKIN ACCESS CUT OUT EDGE CHA
- [SDR UIEA200400102](https://openairdocs.org/sdr/UIEA200400102.md): Bulkhead · cracked · Jun 4, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Bulkhead/Firewall
  > D-CHECK, DURING MAINTENANCE INSPECTION. NR 1 PYLON LT SIDE, BULKHEAD STRAPS WERE FOUND CRACKED AT NAC STA 286.0 AND W.L. 146.5, ALSO THE STRUT SKIN ASSEMBLY AT THE AFT LOWER ACCESS CUT OUT EDGE ADJACENT TO THE STRAP CRACK LOCATION WAS FOUND WITH CHAFING DAMAG
- [SDR UIEA200400104](https://openairdocs.org/sdr/UIEA200400104.md): Frame · damaged · Jun 2, 2004 · N808MC · Boeing 747212B · Fuselage Main, Frame
  > D CHECK, DURING MAINT INSP FOUND COCKPIT EMERGENCY EXIT DOOR CUTOUT FRAME AND CHORDS DAMAGED BETWEEN STA 360 AND 380 WITH MISDRILLED HOLES BETWEEN STRINGER 2L AND 2AL. SEVERAL MISDRILLED HOLES AND DRILL STARTS WERE REPAIRED AS FOLLOWS. FOR BS 360, WEB DAMAGE
- [SDR UIEA200400105](https://openairdocs.org/sdr/UIEA200400105.md): Skin · cracked · Jun 2, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/Skin
  > D-CHECK, DAMAGE WAS FOUND ON RT SIDE OF NR 1 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE,
- [SDR UIEA200400107](https://openairdocs.org/sdr/UIEA200400107.md): Skin · cracked · Jun 2, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/Skin
  > (D) CHECK, DURING MAINT INSP DAMAGE WAS FOUND ON RT SIDE OF NR 2 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DO
- [SDR UIEA200400109](https://openairdocs.org/sdr/UIEA200400109.md): Skin · cracked · Jun 2, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/Skin
  > D-CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 4 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER T
- [SDR UIEA200400108](https://openairdocs.org/sdr/UIEA200400108.md): Precooler · cracked · Jun 2, 2004 · N808MC · Boeing 747212B · Pneumatic Distribution System
  > (D) CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 3 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN
- [SDR UIEA200400097](https://openairdocs.org/sdr/UIEA200400097.md): Skin · wrinkled · May 25, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/Skin
  > D CHECK AT SIN. DURING MAINTENANCE INSPECTION, FOUND NR 2 PYLON RT SIDE SKIN WRINKLED. DAMAGE WAS FOUND IN FOUR BAYS OF THE RT SUBJECT SKIN ASSEMBLY AFT OF NAC STA 286. THE DAMAGES ARE JUS AFT OF THE STRUT LARGE TITANIUM DOUBLER. SUBJECT SKIN ASSEMBLY WAS
- [SDR UIEA200400096](https://openairdocs.org/sdr/UIEA200400096.md): Fitting · cracked · May 25, 2004 · N808MC · Boeing 747212B · Nacelle/Pylon, Main Frame
  > D-CHECK. REWORK OF STRUT NR 1 DIAGONAL BRACE LOWER SPAR FITTING, SP 747-54A2196 REV 1. DURING ACCOMPLISHMENT OF THE TERMINATING ACTION, DAMAGE WAS FOUND AT THE UPPER MOST FASTENER HOLE ON THE RIGHT SIDE OF THE FITTING AFT VERTICAL FLANGE. THE DEFECT WAS COM
- [SDR UIEA200400046](https://openairdocs.org/sdr/UIEA200400046.md): Slide · malfunctioned · Apr 8, 2004 · N808MC · Boeing 747212B · Escape Slide
  > UPPER RT EMERGENCY DOOR SLIDE PARTIAL DEPLOYMENT; DURING UPPER RT EMERGENCY DOOR SLIDE RAFT ASSEMBLY DEPLOYMENT TEST, SLIDE/RAFT FAILED TO FULLY INFLATE. SEQUENCING MECHANISM RELEASED TO FACILITATE SLIDE RAFT REMOVAL AND DISPATCH TO STOP. NOTE: ACTUAL OR AP
- [SDR UIEA200300053](https://openairdocs.org/sdr/UIEA200300053.md): Relief Valve · failed · Aug 28, 2003 · N808MC · Boeing 747212B · Pneumatic Distribution System
  > LIM-MIA - DURING CLIMB AT FL250, NR 4 NACELLE TEMP WENT OT 8.0 WITH A FIRE BELL AND LIGHT IN NR 4 FIRE SWITCH. WHEN NR 4 THRUST LEVER WAS RETARDED TO IDLE, THE FIRE LIGHT WENT OUT AND THE NACELLE TEMP RETURNED TO NORMAL 2.0. CLOSED NR 4 BLEED VALVE AND ADVAN
- [SDR UIEA200300045](https://openairdocs.org/sdr/UIEA200300045.md): Relief Valve · defective · Aug 19, 2003 · N808MC · Boeing 747212B · Pneumatic Distribution System
  > MIP/POS-AIR TURNBACK, AFTER T/O AND DURING CLIMB, NR 4 ENGINE FIRE WARNING CAME ON. WHEN NR 4 THROTTLE WAS CLOSED THE TEMP WENT BACK TO NORMAL. THROTTLE WAS ADVANCED AGAIN THE TEMP STARTED TO GO UP. NOTICED HIGH STAGE BLEED VALVE LIGHT, ON AND OFF. CLOSED NR 4
- [SDR UIEA200300027](https://openairdocs.org/sdr/UIEA200300027.md): Warning Light · false indication · Jun 27, 2003 · N808MC · Boeing 747212B · Fire Protection System
  > TURN BACK, AFTER TAKEOFF THE LOWER CARGO FIRE PROTECTION AFT LIGHT CAME ON AND WENT OUT 2-4 SECONDS AFTER SILENCING THE BELL. ACCOMPLISHED CHECKLIST AND DUMPED FUEL. RETURNED TO GYE AIRPORT. FUEL DUMPED 43,000 KGS. LOWER CARGO FIRE PROTECTION CHECKED PER M
- [SDR UIEA200300017](https://openairdocs.org/sdr/UIEA200300017.md): Warning Light · illuminated · Apr 11, 2003 · N808MC · Boeing 747212B · Turbine Engine Oil System
  > INFLIGHT ENGINE SHUTDOWN, DURING CRUISE, NR 4 ENGINE SHUTDOWN IN FIGHT DUE TO 'OIL FILTER BYPASS LIGHT. OIL TEMPEARTURE AND PRESSURE NORMAL AT 49 PSI/120 DEGREES AND N2 AT 94 PERCENT. WITH THRUST AT IDEL (75 PERCENT N2) PRESSURE WAS 30 PSI AND TEMPERATURE RO
- [SDR UIEA200200059](https://openairdocs.org/sdr/UIEA200200059.md): Skin · corroded · Oct 25, 2002 · N808MC · Boeing 747212B · Fuselage Main, Plate/Skin
  > DURING CURRENT "C" CHECK, FOUND CORROSION BETWEEN OUTER SKIN, DOUBLER AND TRIPLER AT BS 1960 STR 42 RT, LOCATED AT THE AFT LOWER CORNER CUTOUT OF THE AFT LOWER LOBE COMPARTMENT DOOR. NO LEVEL DECLARED BUT CORROSION CONSIDERED LOCAL. OUTER SKIN, DOUBLER AND T
- [SDR UIEA200200060](https://openairdocs.org/sdr/UIEA200200060.md): Panel · cracked · Oct 25, 2002 · N808MC · Boeing 747212B · Fuselage Miscellaneous Structure
  > DURING CURRENT C-CHECK, AT HKG FOUND REVEAL PANEL CRACKED AT NR 2 MED STATION 800 BETWEEN STRINGER 17L AND 18L. CRACK LENGTH IS APPROX.5 INCH LONG TERMINATING IN A COMMON FASTENER HOLE. PERFORMED E/C INSPECTION TO ENSURE NO CRACK PROPAGATION FROM HOLE. OVE
- [SDR 2002F00031](https://openairdocs.org/sdr/2002F00031.md): Smoke Detector · malfunctioned · Dec 5, 2001 · N808MC · Boeing 747212B · Smoke Detection
  > DURING CLIMB-OUT FROM MIA AT APPROXIMATELY 21,000 FEET, THE CARGO LOWER AFT FIRE LIGHT ILLUMINATED. CHECKLIST SECTION III WAS COMPLETED. THE CARGO FLOOR FELT WARM AT SL, BOTH FORWARD AND AFT CARGO HEAT TURNED OFF. WHILE DESCENDING AT 1800 FT THE FIRE LIGHTS
- [SDR UIEA01104](https://openairdocs.org/sdr/UIEA01104.md): Fire Warning · false indication · Oct 30, 2001 · N808MC · Boeing 747212B · Fire Detection
  > DURING TAKEOFF ROLL FROM SUU AT ABOUT 80 KTS, HAD A CARGO FIRE WARNING LIGHT. REJECTED TAKEOFF PERFORMED. PERFORMED VISUAL INSPECTION OF FORWARD AND AFT CARGO COMPARTMENTS. BOTH COOL, NO EVIDENCE OF HEAT OR OVERHEAT CONDITION EXISTS. INSPECTED AFT CARGO HE
- [SDR UIEA01099](https://openairdocs.org/sdr/UIEA01099.md): Light · faulty · Sep 30, 2001 · N808MC · Boeing 747212B · Smoke Detection
  > AIRCRAFT ATB DUE TO LOWER AFT CARGO AND BULK CARGO COMPARTMENT FIRE WARNING INDICATION. PERFORMED TROUBLE SHOOTING PER MM 26-16-00 AND FOUND NR 4, NR 5 AND NR 6 SMOKE DETECTOR LAMPS AT FAULT. REMOVED AND REPLACED LAMPS AND PERFORMED SYSTEM TEST. ALL OPS OK.
- [SDR UIEA00045](https://openairdocs.org/sdr/UIEA00045.md): Duct · leaking · Oct 6, 2000 · N808MC · Boeing 747212B · Fire Detection
  > MIA/BOG -ATB - FLT GT063/06 - ENGINE A-LOOP FIRE WARNING FLUCTUATED, B-LOOP READ 4-5 STEADY. ENGINE SHUT DOWN AND FLIGHT RETURNED TO MIA. MIA MAINTENANCE FOUND PRESSURE REGULATOR VALVE AND DUCT LEAKING. REPLACED BOTH PRV, DUCT AND CLAMPS. OPERATIONAL CHECK
- [SDR UIEA01026](https://openairdocs.org/sdr/UIEA01026.md): Floorbeam · damaged · Mar 19, 2000 · N808MC · Boeing 747212B · Fuselage Main, Floor Beam
  > AFTER REMOVAL OF SEAT TRACK, FOUND FLOORBEAM 1840-1860 UPPER CHORD FASTENER HOLES AT LBL 98.5 ELONGATED. REAMED HOLES, PERFORMED E/C CHECK. NO CRACKS FOUND. FABRICATED REPAIR ANGLES. SPLICED IN REPLACEMENT WEB AND STIFFENERS PER SRM 51-30-02. INSTALLED RE
- [SDR UIEA01027](https://openairdocs.org/sdr/UIEA01027.md): Bulkhead · corroded · Mar 19, 2000 · N808MC · Boeing 747212B · Fuselage Main, Bulkhead
  > DURING INSPECTION, FOUND THE LOWER END OF THE CANTED BULKHEAD PRESSURE WEB AT STATION 1241 CORRODED FROM LBL 11.33 TO 65. REMOVED CORROSION IN AREA PER SRM 51-10-01. FABRICATED REPAIR WEB, DOUBLERS, REINFORCING ANGLES AND FILLERS. INSTALLED IAW KLM 747-2001-
- [SDR 20010423SG001](https://openairdocs.org/sdr/20010423SG001.md): Floorbeam · damaged · Mar 19, 2000 · N808MC · Boeing 747212B · Fuselage Main, Floor Beam
  > AFTER REMOVAL OF SEAT TRACK, FOUND FLOORBEAM 1840-1860 UPPER CHORD FASTENER HOLES AT LBL 98.5 ELONGATED. REAMED HOLES, PERFORMED E/C CHECK. NO CRACKS FOUND. FABRICATED REPAIR ANGLES. SPLICED IN REPLACEMENT WEB AND STIFFENERS PER SRM 51-30-02. INSTALLED RE
- [SDR UIEA01025](https://openairdocs.org/sdr/UIEA01025.md): Skin · corroded · Mar 9, 2000 · N808MC · Boeing 747212B · Wing, Plate/Skin
  > DURING ROUTINE INSPECTION, FOUND UPPER SURFACE OF LOWER LEFT WING SKIN CORRODED AFT REAR SPAR WS 235. REMOVED FASTENERS FROM THE TRAILING EDGE ATTACH FITTING. AREA BLENDED, TREATED AND PAINTED IAW 57-30-01. A REPLACEMENT FILLER BLOCK AS FABRICATED AND INSTA
- [SDR UIEA01024](https://openairdocs.org/sdr/UIEA01024.md): Skin · worn · Mar 9, 2000 · N808MC · Boeing 747212B · Nacelle/Pylon, Plate/Skin
  > DURING ROUTINE INSPECTION, FOUND NR 3 PYLON SKIN WORN AT NAC STATION 290 WL 145 R/S ACCESS PANEL. TRIMMED OUT WORN AREA. FABRICATED FILLER FROM CRES STEEL 301.5 HARD AND ALUMINUM DOUBLER. INSTALLED PER STANDARD PRACTICES. (M)
- [SDR UIEA01023](https://openairdocs.org/sdr/UIEA01023.md): Flap Track · corroded · Mar 9, 2000 · N808MC · Boeing 747212B · Trailing Edge Flaps
  > DURING ROUTINE INSPECTION, FOUND NR 6 INBOARD FLAP TRACK REAR SPAR FORWARD AFT ATTACH HOLES CORRODED. CORROSION REMOVED BY MILLING FLANGE THICKNESS TO.8799 AT THE FORWARD HOLES;.8630 AT THE AFT HOLES. FABRICATED NEW BEARING PLATES. REWORK AREA TREATED, PA
- [SDR UIEA01022](https://openairdocs.org/sdr/UIEA01022.md): Frame · dented · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1860 STRINGER 12 AND 13R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLER, FILLERS AND SHEAR TIE. INSTALLED PER STANDARD PRACTICES. (M)
- [SDR UIEA01021](https://openairdocs.org/sdr/UIEA01021.md): Frame · dented · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1840 STRINGER 12 AND 13R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLERS, FILLERS AND SHEAR TIE. INSTALLED PER STANDARD PRACTICES. (M)
- [SDR UIEA01020](https://openairdocs.org/sdr/UIEA01020.md): Frame · dented · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1820 STRINGER 12R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLERS, FILLERS AND SHEAR TIE. INSTALLED PER STANDARD PRACTICES. (M)
- [SDR UIEA01019](https://openairdocs.org/sdr/UIEA01019.md): Frame · dented · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION, FOUND FRAME DENTED AT STATION 1760 STRINGER 13R. TRIMMED AWAY DAMAGE. FABRICATED REPAIR DOUBLERS, FILLERS AND SHEAR TIE. INSTALLED PER STANDARD PRACTICES. (M)
- [SDR UIEA01018](https://openairdocs.org/sdr/UIEA01018.md): Frame · dented · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION, FOUND OUTER CHORD DAMAGED/DENTED AT BS 1680 STRINGER 15R. TRIMMED AWAY DAMAGE. MANUFACTURED FILLER, REPAIR DOUBLER AND STRAPS. INSTALLED IAW SRM 53-10-04. (M)
- [SDR UIEA01017](https://openairdocs.org/sdr/UIEA01017.md): Seat Track · scratched · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE INSPECTION, FOUND SEAT TRACK GOUGED/SCRATCHED AT LBL 75.92 BETWEEN STATION 1320 AND 1460. ALL AREAS BLENDED PER SRM 51-10-01. HFEC INSPECTION PERFORMED. ALL WITHIN LIMITS PER SRM 53-10-01. AT STATION 1450 SEAT TRACK LUGS AFTER BLENDING WERE
- [SDR UIEA01016](https://openairdocs.org/sdr/UIEA01016.md): Seat Track · scratched · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE INSPECTION, FOUND SEAT TRACK GOUGED/SCRATCHED AT LBL 98.58 BETWEEN STATION 1030 AND 1135. ALL AREAS BLENDED PER SRM 51-10-01. HFEC INSPECTION PERFORMED. ALL FOUND WITHIN LIMITS PER SRM 53-10-01. FOUND SEAT TRACK LBL 75.92 GOUGED/SCRATCHED AT
- [SDR UIEA01015](https://openairdocs.org/sdr/UIEA01015.md): Skin · corroded · Mar 9, 2000 · N808MC · Boeing 747212B · Wing, Plate/Skin
  > DURING ROUTINE INSPECTION, FOUND UPPER WING SKIN CORRODED AT BS 1140, FROM RBL 57 TO RBL 98. REMOVED CORROSION PER SRM 51-10-01, FOUND AREAS FROM RBL 57-87 WITHIN LIMITS PER 57-30-01. AREA FROM RBL 88 TO 98 WAS BLENDED PER REPAIR INSTRUCTIONS, FASTENERS REMO
- [SDR UIEA01014](https://openairdocs.org/sdr/UIEA01014.md): Frame · cracked · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION, FOUND FRAME WEB CRACKED AT STATION 360 R/S STRINGER 23R CUT OUT. ROUTED CRACKED AREA OF WEB. MANUFACTURED REPAIR DOUBLER AND FILLERS. INSTALLED IAW 747-53A2265 WITH OVERSIZED RIVETS BACR15BB6D. (M)
- [SDR UIEA01013](https://openairdocs.org/sdr/UIEA01013.md): Frame · cracked · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION, FOUND FRAME WEB CRACKED AT STATION 360 R/S STRINGER 15 AND 16R. TRIMMED DAMAGE AREA OF WEB. MANUFACTURED REPAIR ANGLES, FILLERS, STRAPS. INSTALLED PER STANDARD PRACTICES USING BACB30MY6K FASTENERS AND BACC30M COLLARS. (M)
- [SDR UIEA01012](https://openairdocs.org/sdr/UIEA01012.md): Shear Tie · cracked · Mar 9, 2000 · N808MC · Boeing 747212B · Fuselage Main, Structure
  > DURING ROUTINE INSPECTION, FOUN FRAME SHEAR TIE CRACKED IN RADIUS BETWEEN STATION 340-360 R/S AT MAIN DECK LEVEL (WBL200). TRIMMED DAMAGE AREA. MANUFACTURED REPAIR ANGLES AND FILLER. INSTALLED PER STANDARD PRACTICES WITH RIVETS BACR15BB5AD. (M)
- [SDR UIEA9909](https://openairdocs.org/sdr/UIEA9909.md): Skin · damaged · Feb 25, 1999 · N808MC · Boeing 747212B · Service Doors
  > FLT GT065 - ATB - APPROX 3.5 HOURS INTO THE FLIGHT, AND ADDITIONAL CARGO CHECK WAS MADE AN A HOLE APPROXIMATELY 1 FT SQUARE WAS DISCOVERED AT THE BOTTOM LEFT CORNER OF R4 MED. AIRCRAFT WAS AT FL 33, PRESSURIZATION WAS NORMAL (8.3). AFTER AIRCRAFT RETURNED TO
- [SDR UIEA9706](https://openairdocs.org/sdr/UIEA9706.md): Pdu · defective · Jul 4, 1997 · N808MC · Boeing 747212B · Leading Edge Slat Control System
  > ATB - FLT MIA-BOG - ON FLAP RETRACTION AFTER TAKEOFF, NR 4 LE ON LEFT DID NOT INDICATE UP. USED ALTERNATE SYSTEM, BUT STILL DID NOT INDICATE UP. SCANNED LED'S VISUALLY WITH FLAPS SELECTED TO 0 AND 1 DEGREE POSITIONS. LEFT INBOARD LED SECTION DID NOT APPEAR

## 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 = 'N808MC' AND deregistration_id = 'N808MC-2013-02-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N808MC-2013-02-01/reports

---
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