# Service difficulty reports: N211FE, cancelled May 12, 2014

A list on [N211FE, cancelled May 12, 2014](https://openairdocs.org/deregistered/N211FE-2014-05-12.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 · 98 reports

- [SDR FDEA201208042837](https://openairdocs.org/sdr/FDEA201208042837.md): Guide · out of adjust · Aug 4, 2012 · N211FE · Boeing 7272S2F · Flight Compartment Windows
  > ON BLOCK-IN, CAPTAIN OPENED SLIDING WINDOW TO TALK TO GROUND CREW. UNABLE TO CLOSE. TROUBLESHOT DOWN TO FWD AND AFT GLIDES. ADJUSTED AND TESTED L2 CAPT'S SLIDING WINDOW IAW MM56-12-011-5. OPS NORMAL.
- [SDR FDEA201207282730](https://openairdocs.org/sdr/FDEA201207282730.md): Pin · out of adjust · Jul 28, 2012 · N211FE · Boeing 7272S2F · Flight Compartment Windows
  > ON PREFLIGHT, CAPTAIN`S SLIDING WINDOW WILL NOT CLOSE. ADJUSTED GUIDE PIN IAW MM 56-12-011-5. OPS CHECKED NORMAL.
- [SDR FDEA201206142233](https://openairdocs.org/sdr/FDEA201206142233.md): Attach Fitting · worn · Jun 14, 2012 · N211FE · Boeing 7272S2F · Emergency Equipment
  > OPEN RT ATTACH FITTING FOR L1 DOOR THAT HOLD ESCAPE SLIDE HAS ONE OF THE FITTINGS WORN. OTHER SIDE SNAPS IN WORN FITTING. HOLDS ROD IN WITH NO RESTRAINT. REMOVED AND STOWED SLIDE IAW MM 25-60-015-2, PART 2A, 2B. REPLACED GIRT BAR RETAINING CLIPS ON COVER
- [SDR FDEA201206142244](https://openairdocs.org/sdr/FDEA201206142244.md): Position Switch · failed · Jun 14, 2012 · N211FE · Boeing 7272S2F · Leading Edge Slat Control System
  > RETRACTING FLAPS FROM 5 TO 2 DEGREES, AMBER L/E FLAPS LIGHT STAYED ON. S/O POSITION TEST SELECTOR SHOWED NR 2 KREGER FLAP OUT. COMPLIED WITH QRH. NO HELP. RETURNED TO DEPARTURE. R & R FLAP POSITION SWITCH IAW AMM 27-82-0001-4. OPS CHECKED GOOD.
- [SDR FDEA201206012042](https://openairdocs.org/sdr/FDEA201206012042.md): Slide · dislodged · Jun 1, 2012 · N211FE · Boeing 7272S2F · Escape Slide
  > EVACUATION SLIDE FELL OUT OF ITS CONTAINER. STOWED L1 DOOR ESCAPE SLIDE IAW AMM 25-60-015-2.
- [SDR FDEA201205312036](https://openairdocs.org/sdr/FDEA201205312036.md): Slide · dislodged · May 31, 2012 · N211FE · Boeing 7272S2F · Escape Slide
  > EVACUATION SLIDE FELL OUT OF ITS CONTAINER. STOWED L1 DOOR ESCAPE SLIDE PER AMM 25-60-015-2.
- [SDR FDEA201201190264](https://openairdocs.org/sdr/FDEA201201190264.md): Slide · dislodged · Jan 19, 2012 · N211FE · Boeing 7272S2F · Escape Slide
  > SLIDE FELL OFF L1 DOOR. REINSTALLED SLIDE L-1 DOOR.
- [SDR FDEA201201170272](https://openairdocs.org/sdr/FDEA201201170272.md): Slide · dislodged · Jan 17, 2012 · N211FE · Boeing 7272S2F · Escape Slide
  > SLIDE FELL OFF L1 DOOR. REINSTALLED SLIDE L-1 DOOR REF AMM 25-60-015-2.
- [SDR FDEA201111275062](https://openairdocs.org/sdr/FDEA201111275062.md): Slide · unsecure · Nov 27, 2011 · N211FE · Boeing 7272S2F · Escape Slide
  > WHEN OPENING L1 DOOR FOR PREFLIGHT CHECK FOUND DOOR SLIDE LAYING ON FLOOR. REINSTALLED SLIDE ON L1 DOOR REF AMM 25-60-015-2. ACFT OK FOR SERVICE.
- [SDR FDEA201110284672](https://openairdocs.org/sdr/FDEA201110284672.md): Slide · dislodged · Oct 28, 2011 · N211FE · Boeing 7272S2F · Escape Slide
  > FOUND ESCAPE SLIDE OUT OF COMPARTMENT AND UNPACKED, LAYING IN COURIER COMPARTMENT. INSTALLED SERVICABLE ESCAPE SLIDE IAW MM 25-60-015-2.
- [SDR FDEA201109113826](https://openairdocs.org/sdr/FDEA201109113826.md): Web · damaged · Sep 11, 2011 · N211FE · Boeing 7272S2F · Passenger/Crew Doors
  > L1 DOOR INTERIOR WEB DAMAGED, INSIDE SECOND LIGHTNING HOLE FROM BOTTOM NEAR CRNTER OF DOOR BS 328. DAMAGE OUT OF LIMITS IAW SRM 52-00-2. REMOVED WEB IAW SRM 51-30-2. FABRICATED NEW WEB IAW SRM 52-10-1 FIG 1, 51-30-5 AND 51-20-1 FIG7. INSTALLED REPAIR PART
- [SDR FDEA201109103823](https://openairdocs.org/sdr/FDEA201109103823.md): Skin · gouged · Sep 10, 2011 · N211FE · Boeing 7272S2F · Leading Edge Devices
  > RT WING, NR 7 SLAT OTBD HOOK AREA HAS GOUGE ON T/E SKIN OTBD SIDE. REMOVED DAMAGED DOUBLER IAW SRM REV 103 51-30-2 FABRICATED DOUBLER AND INSTALLED IAW SRM 57-50-3 FIG 10.
- [SDR FDEA201109093811](https://openairdocs.org/sdr/FDEA201109093811.md): Rib · cracked · Sep 9, 2011 · N211FE · Boeing 7272S2F · Wing, Rib/Bulkhead
  > LEFT WING NR 3 SLAT INBOARD ACTUATOR ATTACH RIB INSIDE SLAT IS CRACKED. REMOVED CRACKED RIB IAW SRM 51-30-2 REV 103. FABRRICATED NEW RIB IAW DRAWING 65-17294 AND SRM 51-20-1 FIG.7 INSTALLED NEW RIB IAW SRM 51-30-2
- [SDR FDEA201109083777](https://openairdocs.org/sdr/FDEA201109083777.md): Rib · cracked · Sep 8, 2011 · N211FE · Boeing 7272S2F · Leading Edge Devices
  > LT WING NR 3 SLAT OTBD ACTUATOR ATTACH RIB INSIDE SLAT IS CRACKED. REMOVED RIB IAW SRM REV 103 51-30-2. FABRICATED NEW RIB IAW DWG 65-17294 AND SRM 51-20-1 FIG 7. INSTALLED NEW RIB IAW SRM 51-30-2 & 51-10-2.
- [SDR FDEA201109083776](https://openairdocs.org/sdr/FDEA201109083776.md): Support · corroded · Sep 8, 2011 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE INTERIOR, MAIN CARGO DOOR UPPER SILL SUPPORT LOWER SURFACE HAS LIGHT SURFACE CORROSION AT BS 661, STRINGER 2L. REMOVED DAMAGED SILL SUPPORT IAW SRM 51-30-2. FABRICATED NEW SILL SUPPORT IAW SRM 53-10-2, FIG 3 AND 51-20-1, FIG 7. INSTALLED NEW
- [SDR FDEA201109083772](https://openairdocs.org/sdr/FDEA201109083772.md): Stringer · corroded · Sep 8, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE INTERIOR, STRINGER 4L HAS CORROSION AT BS 682. REPLACED STRINGER SPLICE.
- [SDR FDEA201109083771](https://openairdocs.org/sdr/FDEA201109083771.md): Stringer Splice · corroded · Sep 8, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE INTERIOR, STRINGER 4L HAS CORROSION AT BS 678 SPLICE. REMOVED SPLICE IAW SRM 51-30-2 REV 103. FORMED NEW SPLICE IAW SRM 53-10-2. INSTALLED NEW SPLICE IAW SRM 51-30-2
- [SDR FDEA201109083770](https://openairdocs.org/sdr/FDEA201109083770.md): Seat Track · corroded · Sep 8, 2011 · N211FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE BS 344 LBL 25. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2 REV 103. FABRICATED & INSTALLED SEAT TRACK SECTION IAW SRM 53-10-2 FIG. 7.
- [SDR FDEA201109063726](https://openairdocs.org/sdr/FDEA201109063726.md): Skin · corroded · Sep 6, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > CORROSION ON INNER SKIN AT DRAIN VALVE, FWD. PIT BS 682 - 686, RBL 3.0. CUT OUT DAMAGED AREA IAW SRM REV.103, 53-30-3 FIG 3A. FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-30-3 FIG 3A.
- [SDR FDEA201109063725](https://openairdocs.org/sdr/FDEA201109063725.md): Skin · gouged · Sep 6, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > EXTERIOR SURFACE GOUGE AT BS 520 AT S27L. CUT OUT DAMAGED AREA IAW SRM 53-30-3 REV 103 FIGURE 14. FABERICATED REPAIR DOUBLER, STRUCTURAL FILLER, AND FILLER IAW SRM 53-30-3 FIG 14. INSTALLED REPAIR PARTS IAW SRM 51-30-2.
- [SDR FDEA201109063724](https://openairdocs.org/sdr/FDEA201109063724.md): Stringer · corroded · Sep 6, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE INTERIOR, STRINGER 4 LT HAS CORROSION AT BS 720. CUT OUT DAMAGED AREA IAW SRM 53-10-3 REV 103 FIG 3. FABERICATED REPAIR PARTS IAW SRM 53-10-3 FIG 3. INSTALLED REPAIR PARTS IAW SRM 51-30-02.
- [SDR FDEA201109063723](https://openairdocs.org/sdr/FDEA201109063723.md): Stringer · corroded · Sep 6, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE INTERIOR, STRINGER 5 LEFT HAS CORROSION AT BS 720A 3 INCHES. CUT OUT DAMAGED AREA IAW SRM REV.103 53-10-3 FIG3 FABRICATED REPAIR STARS AND FILLER IAW SRM 53-10-3 FIG 3 INSTALLED REPAIR PARTS IAW SRM 51-30-02 AND 53-10-3 FIG 3
- [SDR FDEA201109043662](https://openairdocs.org/sdr/FDEA201109043662.md): Stringer · corroded · Sep 4, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > UPPER FUSELAGE INTERIOR STRINGER 5 LT HAS CORROSION AT BS 702. CUT OUT DAMAGED AREA IAW SRM 53-10-3 REV 103 FIG 3. FABRICATED STRAPS AND FILLER IAW SRM 53-10-3 FIG 3 INSTALLED REPAIR PARTS IAW SRM 51-30-02 AND 53-10-3 FIG 3.
- [SDR FDEA201109013603](https://openairdocs.org/sdr/FDEA201109013603.md): Skin · gouged · Sep 1, 2011 · N211FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE, 2 LONG GOUGES UNDER L-1 DOOR. CUTOUT DAMAGE AREA IAW SRM 53-30-3 REV 103 FIG 1. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 1. INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51-30-2 AND 53-30-3 FIG 1.
- [SDR FDEA201108313717](https://openairdocs.org/sdr/FDEA201108313717.md): Attach Angle · cracked · Aug 31, 2011 · N211FE · Boeing 7272S2F · Wing, Attach Fittings
  > RIGHT WING, NR 8 SPOILER ACTUATOR SUPPORT FITTING, HAS LOWER LT SIDE ATTACH ANGLE CRACKED AT WBL 120. REMOVED SECTION OF ATTACH ANGLE AND FABRICATED REPAIR PARTS IAW DWG SR27-57-038 REV C. INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2 AND DWG SR27-57-038 R
- [SDR FDEA201108313641](https://openairdocs.org/sdr/FDEA201108313641.md): Structure · cracked · Aug 31, 2011 · N211FE · Boeing 7272S2F · Trailing Edge Flaps
  > RT WING, INBD FLAP, MID FLAP AFT CHORD IS CRACKED AT 2 EA AREAS, NEAR THE MOST INBD HINGE AND ACTUATING ROD FOR AFT FLAP. CUT OUT DAMAGED AREA IAW SRM 51-40-4 FIG 1. FABRICATED REPAIR FILLER AND SPLICE ANGLE IAW SRM 41-40-4 FIG 1 AND 57-50-2 FIG 5. TREATED
- [SDR FDEA201108303573](https://openairdocs.org/sdr/FDEA201108303573.md): Web · cracked · Aug 30, 2011 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > CRACK IN SIDE WEB AT LIGHTING HOLE RT SIDE AFT VENTRAL STAIRS BS 1239. CUT OUT DAMAGE AREA TORQUE BOX WEB IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1.
- [SDR FDEA201108303574](https://openairdocs.org/sdr/FDEA201108303574.md): Web · cracked · Aug 30, 2011 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > CRACK IN SIDE WEB AT LIGHTING HOLE LT SIDE AFT VENTRAL STAIR OPENING, BS 1303. CUTOUT DAMAGE AREA TORQUE BOX WEB IAW SRM 51-10-1, FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2, FIG 6 AND 51-40-2, FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2, FIG 1.
- [SDR FDEA201108193383](https://openairdocs.org/sdr/FDEA201108193383.md): Slide · damaged · Aug 19, 2011 · N211FE · Boeing 7272S2F · Escape Slide
  > FWD ENTRY DOOR ESCAPE SLIDE, PART OF THE SLIDE DROOPING OUT OF CONTAINER. TROUBLESHOOTING. REMOVED ESCAPE SLIDE FROM ENCLOSURE. SECURED LOOSE ITEMS WITH EXISTING HOOK AND LOOP ON FLAPS. RE-INSTALLED ESCAPE SLIDE INTO ENCLOSURE IAW MM 25-60-015-2. OPS NORM
- [SDR FDEA201107022556](https://openairdocs.org/sdr/FDEA201107022556.md): Fitting · inoperative · Jul 2, 2011 · N211FE · Boeing 7272S2F · Emergency Equipment
  > SLIDE FALLS OUT TOO EASILY. REPLACED GIRT BAR PLASTIC CLIPS.
- [SDR FDEA201005071486](https://openairdocs.org/sdr/FDEA201005071486.md): Gearbox · leaking · May 7, 2010 · N211FE · Boeing 7272S2F · Accessory Gearboxes
  > DURING CRUISE NR 3 LOW OIL FILTER BYPASS LITE ILLUMINATED. OIL PRESSURE INDICATED 28PSI QTY WAS 3.5 GALLONS AND TEMP WAS 95 DEG, OPERATED 2 MIN AT IDLE SHUTDOWN IAW RED TABS DID NOT LOOSE OIL QTY. ENGINE CONTINUED TO WINDMILL AFTER SHUTDOWN. R & R THE NR 3
- [SDR FDEA200910153577](https://openairdocs.org/sdr/FDEA200910153577.md): Switch · failed · Oct 15, 2009 · N211FE · Boeing 7272S2F · Hydraulic System, Main
  > AILERON SYS A ANNUNCIATOR LIGHT ON F/O PANEL CAME ON 30 AFTER LEVEL OFF, NO LOSS OF A SYS A HYD FLUID. REMOVED AND REPLACED AILERON "A" SYS HYD LOW PRESSURE WARNING SWITCH IAW AMM 27-10-144-4, OPS CHECKED GOOD.
- [SDR FDEA200902270766](https://openairdocs.org/sdr/FDEA200902270766.md): Warning Light · false activation · Feb 27, 2009 · N211FE · Boeing 7272S2F · Landing Gear Position and Warning
  > TAILSKID LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW REPORTED THAT AFTER CYCLING GEAR THE SYSTEM WORKED NORMALLY AND ON APPROACH, SYSTEM FUNCTIONED NORMAL. INSPECTED SWITCH AT TAILSKID. NO DEFECTS FOUND. SUSPECT ICE IN BILLINGS CAUSED SWITCH TO STICK.
- [SDR 08FDEA03520](https://openairdocs.org/sdr/08FDEA03520.md): Fitting · corroded · Aug 20, 2008 · N211FE · Boeing 7272S2F · Horizontal Stabilizer, Attach Fittings
  > GENERATED BY EO 7-5510-7-5000, HORIZONTAL STAB RT HINGE FITTING O/B BUSHING BORE HAS CORROSION OVERSIZED LUG BORE TO 2.2244 INCH CORROSION REMOVED. HFEC INSPECTED BORE NO DEFECTS NOTED. FABRICATED OVERSIZE BUSHING, CAD PLATED BUSHING. INSTALLED OVERSIZE BUS
- [SDR 08FDEA03498](https://openairdocs.org/sdr/08FDEA03498.md): Support Angle · corroded · Aug 19, 2008 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > RT WHEEL WELL, LOWER FUSELAGE FAIRING SUPPORT FRAME HAS CORROSION, RBL 21, STA 950 FABRICATED TEE ANGLE FROM RT WHEEL WELL FUSELAGE FAIRING SUPPORT STA 950 REFB DWR 65-25550 AND CUSTOMER REQUEST, HEAT TREATED TRACKING NUMBER 2008-08-057. TREATED AND PRIMED, R
- [SDR 08FDEA03456](https://openairdocs.org/sdr/08FDEA03456.md): Bracket · cracked · Aug 16, 2008 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AIRSTAIR COMPARTMENT LT BRACKET FOR FIRE LOOP SUPPORT IS CRACKED AT BULKHEAD STA 1183 NEAR FLOOR LEVEL. REMOVED OLD BRACKET REF SRM 51-30-02 P 1-7, IDENTIFIED MATERIALS REF DWR 65-27195 FRAME 1 SHEET 3 REV E ALSO A-TAG NR A03329. FABRICATED NEW BRACKET REF D
- [SDR 08FDEA03455](https://openairdocs.org/sdr/08FDEA03455.md): Beam · corroded · Aug 16, 2008 · N211FE · Boeing 7272S2F · Fuselage Main, Structure
  > LT MLG W/W UPPER BOX BEAM LOWER WEBS AFT OF STA 910 AND 930 HAVE CORROSION REMOVED FASTENERS FOR ACCESS. REMOVED CORROSION, ORIGINAL.080 REMAINING.070. REMOVED.010 OUT OF LIMITS, FABRICATED REPAIR DOUBLER 7075-O-100 HEAT TREAT T6. APPLIED ALODINE AND PRI
- [SDR 08FDEA03451](https://openairdocs.org/sdr/08FDEA03451.md): Fairing · cracked · Aug 16, 2008 · N211FE · Boeing 7272S2F · Trailing Edge Flaps
  > RT WING NR 6 FLAP TRANSMISSION FAIRING IS CRACKED AT CENTER ATTACH HOLE REMOVED FAIRING REF 51-30-2, PG 1-7 STOP DRILLED CRACKS REF 727 SRM 51-10-1 PG 13. NDT VERIFIED CRACK CONTAINMENT. NDT MANUAL PART 6, 51-00-00 FIG 23. ORIGINAL AND REPAIR MATERIAL IDENT
- [SDR 08FDEA03449](https://openairdocs.org/sdr/08FDEA03449.md): Fairing · cracked · Aug 16, 2008 · N211FE · Boeing 7272S2F · Trailing Edge Flaps
  > NR 5 FLAP TRACK MIDDLE FAIRING, AFT SKIN BENT/CRACKED. REMOVED DAMAGED SKIN, REF 51-30-2, PG 1-7. ORIGINAL SKIN AND REPLACEMENT BOTH IDENTIFIED AS 7075-T6,.040 REF 65-21795, REV E, PG 35 AND DWG 65-21795, AND A-TAG NR A27927. FABRICATED NEW SKIN, REF SRM 5
- [SDR 08FDEA03448](https://openairdocs.org/sdr/08FDEA03448.md): Attach Angle · cracked · Aug 16, 2008 · N211FE · Boeing 7272S2F · Wing, Attach Fittings
  > RT WING, LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR I/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51-30-5, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA03447](https://openairdocs.org/sdr/08FDEA03447.md): Attach Angle · cracked · Aug 16, 2008 · N211FE · Boeing 7272S2F · Wing, Attach Fittings
  > RT WING LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR O/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51-30-5, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA03446](https://openairdocs.org/sdr/08FDEA03446.md): Bracket · cracked · Aug 16, 2008 · N211FE · Boeing 7272S2F · Fuselage Main, Attach Fittings
  > FWD NOSE COMPARTMENT WEATHER RADAR MOUNT BRACKET CRACKED REMOVED WEATHER RADAR R/T. REPLACED MOUNT BRACKET, INSTALLED WEATHER RADAR R/T AND PERFORMED GOOD OPS CHECK REF SRM 51-30-02, AMM 34-41-041-4 AND AMM 34-41-000-5. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA03407](https://openairdocs.org/sdr/08FDEA03407.md): Angle · cracked · Aug 13, 2008 · N211FE · Boeing 7272S2F · Wing Miscellaneous Structure
  > LT WING ROOT TE UPPER PNL IB OF NR 7 SPOILER HAS FRETTED/CRACKED IB SUPPORT ANGLE BS 950A, WBL 70. REPLACED SUPPORT ANGLES REF SRM 51-30-02 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA03406](https://openairdocs.org/sdr/08FDEA03406.md): Angle · cracked · Aug 13, 2008 · N211FE · Boeing 7272S2F · Wing Miscellaneous Structure
  > LEFT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 4 SLAT WELL. REMOVED INTERCOSTAL AND DAMAGED SUPPORT ANGLE, FABRICATED NEW SUPPORT ANGLE, HEAT TREAT "T-3". TREAT AND PRIMED SUPPORT ANGLE, INSTALL
- [SDR 08FDEA03403](https://openairdocs.org/sdr/08FDEA03403.md): Duct · cracked · Aug 13, 2008 · N211FE · Boeing 7272S2F · Pneumatic Distribution System
  > RT EXT FUSE NR 3 ENG FAN AIR EXH PORT ASSY IS FRETTED/CRACKED. REMOVED AND REPLACED FAN AIR EXH POT ASSY REF SRM 51-30-2 PG 1-32, REF MM 51-20-151-7 PG 1-5, REF MM 36-00-001-2 PG 1-4. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA03402](https://openairdocs.org/sdr/08FDEA03402.md): Frame · corroded · Aug 13, 2008 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > LWR EXT FUSE BODY FRAME LWR CHORD IS CORRODED BS 351, LBL 17, WL 148-150. REMOVED CORROSION AT LWR EXT FUSE BODY FRAME LWR CHORD STA 351 LBL 17 - RBL 17, REF SRM 51-10-6 PG 1-5. MATERIAL LOSS 50 PERCENT, FOUND OUT OF LIMITS REF SRM 53-10-1 FIG 1. REMOVED AN
- [SDR 08FDEA03401](https://openairdocs.org/sdr/08FDEA03401.md): Support Angle · cracked · Aug 13, 2008 · N211FE · Boeing 7272S2F · Wing Miscellaneous Structure
  > RIGHT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 5 SLAT WELL. REMOVED INTERCOSTAL AND SUPPORT ANGLE AT SLAT STA 260. FABRICATED NEW SUPPORT ANGLE. VERIFIED MATERIAL 2024 T-3, FAB'D WITH 2024-0,
- [SDR 08FDEA03400](https://openairdocs.org/sdr/08FDEA03400.md): Floorbeam · cracked · Aug 13, 2008 · N211FE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > MAIN DECK FLOORBEAM INTERCOSTAL MID CHORD EXISTING REPAIR DOUBLER IS CRACKED BS 302, WL 207 FABRICATED NEW REPAIR ANGLE REF SRM 51-40-3 PG 1. TREATED AND PRIMED REF SRM 51-10-2 PG 1-9. INSTALLED ANGLE REF SRM 51-30-2 PGS 1-7. THIS IS CLASSIFIED AS A MINOR R
- [SDR 08FDEA03391](https://openairdocs.org/sdr/08FDEA03391.md): Bracket · corroded · Aug 12, 2008 · N211FE · Boeing 7272S2F · Fuselage Main, Attach Fittings
  > CORROSION ON RT A/C BAY FWD COMPARTMENT LIGHT LENS RETAINER AND LIGHT MOUNT BRACKET. REPLACED FWD COMPARTMENT LIGHT, LENS RETAINER AND LIGHT MOUNT BRACKET. REFERENCE SWPM 20-84-10, PG 3-5; SRM 51-30-02 PG 2-3; BOEING DRW NR 66-14827-1/1. OPERATIONAL TEST OF
- [SDR 08FDEA03390](https://openairdocs.org/sdr/08FDEA03390.md): Duct · cracked · Aug 12, 2008 · N211FE · Boeing 7272S2F · Engine Bleed Air System
  > BLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON CRACKED AT AFT EDGE OF OPENING. REMOVED AND REPLACED BLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON. REF IPC 36-10-00-10 FIG 10, SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR REPAIR.

Next page: https://openairdocs.org/deregistered/N211FE-2014-05-12/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 = 'N211FE' AND deregistration_id = 'N211FE-2014-05-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N211FE-2014-05-12/reports

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