# Service difficulty reports: N220FE, cancelled Mar 19, 2013

A list on [N220FE, cancelled Mar 19, 2013](https://openairdocs.org/deregistered/N220FE-2013-03-19.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 3 · 124 reports

- [SDR FDEA201006232116](https://openairdocs.org/sdr/FDEA201006232116.md): Engine · stalled · Jun 23, 2010 · N220FE · Boeing 727233 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE COMPRESSOR STALL/SURGE AT LEVEL OFF - FL340 EPR WAS OBSERVED TO GO DOWN TO 1.6 EPR WITH ENGINE VIBRATION NOISE ASSOCIATED WITH COMPRESSOR STALL. AIRTURN BACK. R & R NR 2 ENGINE AS PER WORK CARD 70T0002 AND TESTED PER WORK CARD 70T0301-02. ALL
- [SDR FDEA201003050653](https://openairdocs.org/sdr/FDEA201003050653.md): Seat Track · corroded · Mar 5, 2010 · N220FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > UPON REMOVAL OF FLOORBOARD TO ACCESS MLG SIDE STRUT AFT BRG, FOUND SEAT TRACK CORRODED AT STA 950, 12 REMOVED DAMAGED SEAT TRACK SECTION FROM BS 950+ 10 TO BS 950B+10 LBL 24, FABRICATED NEW SEAT TRACK SECTION AND SPLICES, INSTALLED NEW SEAT TRACK SECTION AND
- [SDR FDEA200810294619](https://openairdocs.org/sdr/FDEA200810294619.md): Fan · failed · Oct 29, 2008 · N220FE · Boeing 727233 · Air Distribution Fan
  > SLIGHT ELECTRICAL ODOR WAS DETECTED APPROACHING DESTINATION. TURNED OFF GASPER FAN. ODOR WAS STILL DETECTED AND BECOMING STRONGER. DONNED OXYGEN MASKS RAN QRH SMOKE, FUMES, ODORS CHECKLIST. DECLARED ATC EMERGENCY LANDED AT RWY 9 WITH FIRE TRUCKS IN TOW.
- [SDR 08FDEA04619](https://openairdocs.org/sdr/08FDEA04619.md): Gasper Fan · malfunctioned · Oct 29, 2008 · N220FE · Boeing 727233 · Air Distribution Fan
  > AT FL 350 A SLIGHT ELECTRICAL ODOR WAS DETECTED APPROACHING MEMPHIS. TURNED OFF GASPER FAN. ODOR WAS STILL DETECTED AND BECOMING STRONGER. DONNED OXYGEN MASKS RAN QRH SMOKE, FUMES, ODORS CHECKLIST. DECLARED ATC EMERGENCY AND LANDED. AT GATE SHUTDOWN ACFT
- [SDR 08FDEA02133](https://openairdocs.org/sdr/08FDEA02133.md): Beam · corroded · Jun 3, 2008 · N220FE · Boeing 727233 · Fuselage Main, Structure
  > KEEL BEAM END TOP ATTACH ANGLE ON BACK OF BULKHEAD AT FS 740 HAS CORROSION ON TOP SIDE OF ANGLE AT RBL 4, ABOVE CONTROL CABLE PULLEY WHEELS. REMOVED AND REPLACED ANGLE REF SRM 51-30-02. FABRICATED REPLACEMENT ANGLE ON N/R N00726. FLAP PEENED, ALODINED, PRI
- [SDR 08FDEA02132](https://openairdocs.org/sdr/08FDEA02132.md): Beam · corroded · Jun 3, 2008 · N220FE · Boeing 727233 · Fuselage Main, Structure
  > DELTA BEAM INTERIOR RT LOWER CHORD AT BS 747 - 749, RBL 5, IS CORRODED ON INNER SURFACE AT AND AROUND SPLICE. BLENDED CORROSION AT LOWER, FWD CHORD. FOUND TO BE OUT OF LIMITS, REF DWG 69-47111. REPLACED CHORD REF DWG 65-47111. THIS IS CLASSIFIED AS A MAJOR
- [SDR 08FDEA02129](https://openairdocs.org/sdr/08FDEA02129.md): Beam · corroded · Jun 3, 2008 · N220FE · Boeing 727233 · Fuselage Main, Structure
  > CORROSION INSIDE DELTA BEAM STA740, LBL 3, WL 148 CUT AWAY LWR WEB SECTION OF DELTA BOX TO FOM. REMOVED CORROSION FROM DELTA BEAM STA 740, LBL 3, WL 148. VERIFIED MATERIAL LOSS BY NDT, AND FOUND TO BE OUT OF LIMITS REF DWG 65-23555. REPLACED INTERCOSTAL REF
- [SDR 08FDEA02127](https://openairdocs.org/sdr/08FDEA02127.md): Frame · corroded · Jun 3, 2008 · N220FE · Boeing 727233 · Aerodynamic Fairings
  > CORROSION ON TOP OF WING TO BODY FAIRING FRAME WORK AT TWO FWD ADF ANTENNA LEAD POSITION CLAMP ATTACH AT FS 730F, RBL 10, INBOARD OF RT RAM AIR DUCT REMOVED PANELS REF SRM 51-30-2, REMOVED CORROSION REF SRM 53-10-01. FOUND TO BE OUT OF LIMITS REF SRM 51-20-01
- [SDR 08FDEA02074](https://openairdocs.org/sdr/08FDEA02074.md): Bulkhead · corroded · Jun 1, 2008 · N220FE · Boeing 727233 · Fuselage Main, Bulkhead
  > FWD PANEL RACK: BULKHEAD BS 720 FWD PIT FRAME CORROSION AROUND NUT PLATES (MKD) FABRICATED NEW FRAME ANGLE REF DAD DWG 65-82623. TREATED PRIMED RES AMM 51-20-021-7 PG 1-7 51-20-031-7 PG 1-7. MARKED PART REF FEDEX GMM 7-0-1001. THIS IS CLASSIFIED AS AMINOR R
- [SDR 08FDEA02073](https://openairdocs.org/sdr/08FDEA02073.md): Beam · corroded · May 31, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > RT A/C EQUIP BAY PANEL 3455 HAS CORROSION UNDER FWD HINGE PLATE ON FRAME REMOVED PNL NR 3453, 3358, 3465. SPLICED IN NEW BEAM ASSY P/N NR 65-58502-90. FABRICATED 4. REPAIR ANGLES, TREATED AND PRIMED AND INSTALLED. RE-INSTALLED A/C PANELS. REF SRM 51-30-0
- [SDR 08FDEA02072](https://openairdocs.org/sdr/08FDEA02072.md): Mount · corroded · May 31, 2008 · N220FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > CORROSION ON CARGO TIE DOWN MOUNT ON BOTTOM INBOARD FWD CORNER AT FS 720, LBL 22, WL 156. REMOVED AND REPLACED DAMAGED FITTING, REF SRM 51-30-02 PG 1-3. FITTING FOUND TO BE OUT F LIMITS, REF BOEING DWG 65-57848 ITEM NR 1, ORIG THK IS.110 INCH, MAT LOSS IS
- [SDR 08FDEA02071](https://openairdocs.org/sdr/08FDEA02071.md): Panel · delaminated · May 31, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > RT A/C BAY PANEL 3456 R DELAMINATED REMOVED AND REPLACED PANEL 3456R WITH SERVICEABLE PANEL REF SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA02020](https://openairdocs.org/sdr/08FDEA02020.md): Door Frame · cracked · May 29, 2008 · N220FE · Boeing 727233 · Fuselage Main, Structure
  > REF SNRM N00174 JPF ITEM NR 1. MAIN DECK, 1L DOOR FRAME IS CRACKED UNDER REMOVED STOP FITTING, AT BOTTOM CROSS BEAM AFT END. REMOVED DAMAGED MATERIAL REF SRM 51-40-02. VERIFIED CRACK REMOVED REF. 727 NDT MAN. PT. 6 51.00-00 FIG 23. NO DEFECTS FOUND. INS
- [SDR 08FDEA02015](https://openairdocs.org/sdr/08FDEA02015.md): Skin · cracked · May 28, 2008 · N220FE · Boeing 727233 · Landing Gear Doors
  > NOSE LANDING GEAR RIGHT FWD DOOR, CRACK AT AFT END EDGE SKIN AT O/B STOP ANGLE SUPPORT REPAIRED, R NLG DOOR REF 51-40-3, 51-30-5, 51-10-02, AND MM 32-22-001-4. PERFORMED ADJUSTMENT AND TEST OF DOOR REF MM 32-22-001-5. OPS CHECK GOOD. THIS IS CLASSIFIED AS
- [SDR 08FDEA02014](https://openairdocs.org/sdr/08FDEA02014.md): Floorbeam · corroded · May 28, 2008 · N220FE · Boeing 727233 · Fuselage Main, Floor Beam
  > AFT CABIN, AT BS 1130 FLOORBEAM LOWER FLANGE, UPPER SURFACE CORRODED, BETWEEN LBL 22 AND LBL 35. REMOVED LOWER LT EXISTING T-CAP REPAIR, REF SRM 51-30-2. FABRICATED NEW T-CAP AND SPLICE ANGLES AND STRAP, REF SRM 53-10-8 FIG 10. INSTALLED REPAIR PARTS, REF S
- [SDR 08FDEA01999](https://openairdocs.org/sdr/08FDEA01999.md): Frame · corroded · May 27, 2008 · N220FE · Boeing 727233 · Fuselage Main, Frame
  > AFT PIT BILGE BODY FRAME UPPER FLG IS BUCKLED/CORRODED BS 1050, STR 26L-28L, WL 148 (MKD). REMOVED CORROSION ON AFT PIT BILGE BODY FRAME UPPER FLG STA 1050 STR 26L 28L WL148. ORIGINAL THICKNESS IS.063 REMAINING MATERIAL IS.061,.002 REMOVED FOUND TO BE IN
- [SDR 08FDEA01998](https://openairdocs.org/sdr/08FDEA01998.md): Seat Track · corroded · May 27, 2008 · N220FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR, SEAT TRACK EXTRUSION IS CORRODED, BS 850 - 870, LBL 45, WL 208. REMOVED AND REPLACED TRACK WITH NEW TRACK. FABRICATED FROM BAC 1520-1466 EXTRUSION REF SRM 51-30-2 PG 2, SRM 51-10-2 PG -3, GMM7-0-1001, AMM 51-20-014. THIS IS CLASSIFIED AS A
- [SDR 08FDEA01996](https://openairdocs.org/sdr/08FDEA01996.md): Cover · cracked · May 27, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > C-2 PIT RT THRESHOLD COVER AT STA 950E IS CRACKED AT BOLT HOLE WITH LIGHT CORROSION ON BOTTOM SIDE OF PANEL TRANSFERRED HOLES, INSTALLED NUTPLATES, TREATED, PRIMED AND PAINTED NEW PANEL. REF; SRM 51-30-2 PG 1 - 3, FX 727 200 MM 51-20-151-7, AND FX727-200 M
- [SDR 08FDEA01995](https://openairdocs.org/sdr/08FDEA01995.md): Seat Track · corroded · May 27, 2008 · N220FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK CORRODED STA 1148 - 1170, RBL 45 WL 208 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, ORIGINAL THICKNESS.070 INCH, MATERIAL LOSS OF.030", REMAINING MATERIAL.040". REMOVED SEAT TRACK, REF SRM 53-10-1 PAGE 16 DET 5. SEAT TRACK FABRIC
- [SDR 08FDEA01994](https://openairdocs.org/sdr/08FDEA01994.md): Shear Tie · chafed · May 27, 2008 · N220FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > AFT PIT BILGE BODY FRAME SHEAR TIE ASSY HAS DISBONDED LEVELING COMPOUND/CORROSION BS 1130 AFT, STR 29R - 30, WL 148. BLENDED CORROSION ON SHEAR TIE, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW PIECE. REF SRM 51-30-02 AND DWG NR 69-20813. THIS I
- [SDR 08FDEA01993](https://openairdocs.org/sdr/08FDEA01993.md): Seal · dirty · May 27, 2008 · N220FE · Boeing 727233 · Cargo/Baggage Doors
  > LOWER FWD CARGO COMPARTMENT DOOR, UPPER AFT CORNER CRACKED FABRICATED PER BOEING DWG 65-57146 CARGO DOOR AFT UPPER CORNER REF SRM 51-30-2. INSTALLED NEW SEAL DEPRESSOR CORNER REF 51-30-2, RESTORED LEVELING COMPOUND TO AREA. REF AMM 51-40-000-0. THIS IS CLAS
- [SDR 08FDEA01992](https://openairdocs.org/sdr/08FDEA01992.md): Channel · damaged · May 27, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD PIT STA 620 ABOVE STR 27L " U " CHANNEL SUPPORT ON FWD SIDE OF FRAME HAS 2 MISDRILLED HOLES AT LBL 26. REMOVED DAMAGE, FABRICATED 2 REPAIR ANGLES, HEAT TREATED TO T-6 CONDITION. FABRICATED FILLER. ALODINED AND PRIMED ALL REPAIR PARTS, INSTALLED REPAIR P
- [SDR 08FDEA01991](https://openairdocs.org/sdr/08FDEA01991.md): Angle · corroded · May 27, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > C-2 PIT Z - ANGLE FROM STA 960 TO 1036, RT SIDE, HAS SEVERAL LOOSE/MISSING NUT PLATES WITH AREAS OF LIGHT CORROSION ON PANEL REMOVED CORROSION, ORIGINAL THICKNESS,.062 INCH, REMOVED.037 INCH, REMAINING THICKNESS.025 INCH. OUT OF LIMITS. VERIFIED NEW PART
- [SDR 08FDEA01990](https://openairdocs.org/sdr/08FDEA01990.md): Seal · damaged · May 27, 2008 · N220FE · Boeing 727233 · Cargo/Baggage Doors
  > LOWER NR 2 CARGO DOOR S/N BNW 506, AFT LWR CORNER, OF SEAL DEPRESSOR HAS NICKS. NR 2 CARGO DOOR SEAL DEPRESSOR, AFT CORNER FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT CORNER SEAL DEPRESSOR PN NR 65-59948-502, REF 51-40-02 AND DWG 65-60234 THIS IS CLA
- [SDR 08FDEA01989](https://openairdocs.org/sdr/08FDEA01989.md): Stringer Clip · corroded · May 27, 2008 · N220FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > AFT PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 950F FWD, STR 29 R, O/B WL 139. REMOVED AND REPLACED STRINGER CLIP/CHANNEL REF SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA01988](https://openairdocs.org/sdr/08FDEA01988.md): Frame · damaged · May 27, 2008 · N220FE · Boeing 727233 · Fuselage Main, Frame
  > AFT PIT BILGE BODY FRAME UPPER FLG IS BUCKLED, BS 1070, STR 25R - 27R DAMAGE ON FRAME FLANGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 PG 1-3 DETAIL 4 NOTE 5. REMOVED DAMAGE, NDT VERIFIED DAMAGE REMOVAL. VERIFIED MATERIAL FOR REPAIR DOUBLER, 7075 - O -.06
- [SDR 08FDEA01987](https://openairdocs.org/sdr/08FDEA01987.md): Angle · corroded · May 27, 2008 · N220FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN ATTACH ANGLE IN C-1 PIT, FS 700, BL 0, WL 148 REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPLACEMENT ANGLE FROM 7075- T6,.040' REF BOEING DWG 69-14871 AND PRINT NR 65-15938. REMOVED OLD ANGLE REF SRM 51-10-2 AND MM 51-30
- [SDR 08FDEA01986](https://openairdocs.org/sdr/08FDEA01986.md): Stringer Clip · damaged · May 27, 2008 · N220FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > FWD PIT BILGE BODY FRAME STRINGER CLIP IS MISDRILLED BS 720, STR 26L. INSTALLED STRINGER CLIP AT STA STA 720, STR 26L REF SRM 51-30-02.
- [SDR 08FDEA01985](https://openairdocs.org/sdr/08FDEA01985.md): Seat Track · corroded · May 27, 2008 · N220FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN, LBL 25, SEAT TRACK IB AND OB UPPER FLANGES CORRODED ON LOWER SURFACE AT 1130. REMOVED AND REPLACED SEAT TRACK AT STA 1130, LBL 25, FOUND OLD SEAT TRACK OUT OF LIMITS. FABRICATED NEW AND INSTALLED REF BOEING DWG. 65-19606.
- [SDR 08FDEA01951](https://openairdocs.org/sdr/08FDEA01951.md): Pan · cracked · May 22, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM COMPOSITE REPAIR BS 1176 - 1183, RBL 18-27, WL 208 REMOVED OLD DITCHING PAN. FABRICATED NEW DITCHING PAN OUT OF 6061-O, HEAT TREATED TO T-6, DRILLED TRIMMED, TREATED PRIMED AND INSTALLED. REF BAC D
- [SDR 08FDEA01950](https://openairdocs.org/sdr/08FDEA01950.md): Door · cracked · May 22, 2008 · N220FE · Boeing 727233 · Landing Gear Doors
  > NOSE LANDING GEAR LEFT DOOR, CRACK AT AFT END EDGE SKIN AT B-STOP ANGLE SUPPORT REMOVED DAMAGE, NDT FOR CRACKS REMOVAL, FABRICATED FILLER AND DOUBLER REPAIR PARTS. INSTALLED FILLER AND DOUBLER REF SRM 51-30-2 PG 1, SRM 51-40-3 PG 1-3, SRM 52-80-1 ITEM 3, SRM
- [SDR 08FDEA01946](https://openairdocs.org/sdr/08FDEA01946.md): Fairing · cracked · May 21, 2008 · N220FE · Boeing 727233 · Trailing Edge Flaps
  > NR 4 T/E FLAP TRACK FWD FAIRING, HAS CRACK AT FWD END CUTOUT REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, NDT CHECKED FAIRING AND FOUND CRACK TO BE TERMINATED. MADE ADDITIONAL CUT FINALE CUT. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AND PRIMED. INSTALLED
- [SDR 08FDEA01945](https://openairdocs.org/sdr/08FDEA01945.md): Pan · cracked · May 21, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > DITCHING PAN FWD ATTACH ANGLE BS 1166, RBL 38 - 47, IS CRACKED AT RBL 45 - 4. REMOVED DAMAGED PART (ANGLE) FABRICATED NEW, TREATED AND PRIMED AND INSTALLED IAW SRM 51-10-02 PG 1, 51-30-02, PG 1 AND DWG 65-29548. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01944](https://openairdocs.org/sdr/08FDEA01944.md): Pan · cracked · May 21, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED BS 1176 - 1183, LBL 27 - 37, WL 208 REPLACED DITCHING PAN AT STA 1176 - 1183, LBL 27 - 37, WL 208 REF BOEING DWG 65-29548 AND SRM 51-30-2 AND 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01943](https://openairdocs.org/sdr/08FDEA01943.md): Pan · cracked · May 21, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED BS 1176 - 1183, LBL 27 - 37, WL 208. REPLACED DITCHING PAN AT STA 1176 - 1183, LBL 27 - 37, WL 208 REF BOEING DWG 65-29548 AND SRM 51-30-2 AND 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01941](https://openairdocs.org/sdr/08FDEA01941.md): Doubler · cracked · May 21, 2008 · N220FE · Boeing 727200 · Engine Cowling System
  > NR 3 ENG LOWER COWL, I/B SIDE EDGE, 3RD LATCH CUTOUT FROM FWD END, LOWER CUTOUT AREA, DOUBLER CRACKED OUT. REMOVED AND REPLACED DOUBLER, REF SRM 51-30-2 PG 2, THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01940](https://openairdocs.org/sdr/08FDEA01940.md): Pan · cracked · May 21, 2008 · N220FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM / DISBONDED. COMPOSITE REPAIR, BS 1176 - 1183, RBL 27-37, WL 208. REMOVED CRACKED DITCHING PAN. FABRICATED NEW DITCHING PAN, HEAT TREATED TO T-6 CONDITION, TREATED AND PRIMED, AND INSTALLED. REF
- [SDR 08FDEA01939](https://openairdocs.org/sdr/08FDEA01939.md): Pan · cracked · May 21, 2008 · N220FE · Boeing 727200 · Fuselage Miscellaneous Structure
  > AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM COMPOSITE REPAIR BS 1176-1183, RBL 37-47 WL 208 (MKD). FABRICATED NEW DITCHING PAN, HEAT TREATED, ALODINED AND PRIMED, INSTALLED IAW SRM 51-10-2, PG 1, 51-30-2, PG 1, 51-30-5 PG 1. BOEING DWD: 65
- [SDR 08FDEA01933](https://openairdocs.org/sdr/08FDEA01933.md): Angle · corroded · May 21, 2008 · N220FE · Boeing 727233 · Fuselage Main, Bulkhead
  > AFT PIT BS 950E BULKHEAD RIGHT FWD BLOW OUT PANEL FRAME HAS CORROSION AROUND NUTPLATES. REMOVED DAMAGED Z-ANGLE, REPLACED WITH FABRICATED Z-ANGLE. INSTALLED ON BULKHEAD PANEL STA 950E IAW DWG 65-57172 AND SRM 51-40-02. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01930](https://openairdocs.org/sdr/08FDEA01930.md): Floor Panel · corroded · May 21, 2008 · N220FE · Boeing 727233 · Fuselage Floor Panel
  > C-2 PIT FLOOR PANELS NR 3 HAS CORROSION ALONG ONE SIDE EDGE FABRICATED NEW C-2 NR 3 PIT FLOOR PANEL REF DRAWING 65-67245 AND SRM 51-30-05 PG 13-21. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01928](https://openairdocs.org/sdr/08FDEA01928.md): Frame · corroded · May 21, 2008 · N220FE · Boeing 727233 · Fuselage Main, Frame
  > AFT PIT BILGE BODY FRAME UPPER FLG IS CORRODED BS 103, STR 26R - 28R, WL 147 REMOVED.007 INCH FROM ORIGINAL MATERIAL OF.063 INCHES WITH.056 INCH REMAINING AND FOUND FRAME TO BE OUT OF LIMITS. HEAT TREATED, DRILLED TREATED, PRIMED AND PAINTED, REPAIR DOUBLE
- [SDR 08FDEA01917](https://openairdocs.org/sdr/08FDEA01917.md): Pan · cracked · May 20, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT MAIN DECK FLOOR DITCHING PAN ASSY HAS 2 CRACKS AND A MISSING FASTENER COLLER, BS 1176 - 1183,LBL 18 - 27, WL 208. REPLACED DITCHING PAN AT STA 1176 - 1183, LBL 18 - 27 REF BOEING DWG 65-29548 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01910](https://openairdocs.org/sdr/08FDEA01910.md): Skin · corroded · May 20, 2008 · N220FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CORROSION ON AFT SKIN IN C-1 PIT AT FS 683 LBL 11, WL 148 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. ORIINAL "T" IS.045" REMAINING 'T' IS.024. MATERIAL LOSS OF.021 REF SRM 53-30-1 FIG 1. FABRICATED DOUBLER AND FILLER, TREATED AND PRIMED, INSTALLED D
- [SDR 08FDEA01907](https://openairdocs.org/sdr/08FDEA01907.md): Rib · cracked · May 20, 2008 · N220FE · Boeing 727233 · Horizontal Stabilizer, Spar/Rib
  > LT HORIZ STAB TRAILING EDGE ELEVATOR HINGE SUPPORT RIB CRACKED 2 AREAS AT ELEVATOR STA 99.79 AFT INBOARD SIDE. REPAIRED LT HORIZONTAL TRAILING EDGE HINGE SUPPORT RIB AT STA 99.79 REF SRM 55-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA01923](https://openairdocs.org/sdr/08FDEA01923.md): Angle · cracked · May 20, 2008 · N220FE · Boeing 727233 · Wing Miscellaneous Structure
  > LEFT WING INBD LE CAVITY NR 2 FLAP ACTUATOR AFT MOUNT, UPPER CORNER ANGLE IS CRACKED REMOVED AND REPLACED WEB REF SRM 51-30-2. OPS CHECKED ACCOMPLISHED ON W/C 70C003-00 THIS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01921](https://openairdocs.org/sdr/08FDEA01921.md): Angle · corroded · May 20, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD PANEL RACK, FWD PIT FRAME BS 720 CORROSION AROUND NUTPLATES REMOVED CORROSION IAW SRM 51-10-6, ORIGINAL "T''.040 INCH, MAT. REMOVED IS.012. MAT REMAINING.028 INCH IS OUT OF LIMITS IAW SRM 53-1031. FABRICATED NEW LINER SUPPORT ANGLE FROM 7075-0.050
- [SDR 08FDEA01915](https://openairdocs.org/sdr/08FDEA01915.md): Pan · cracked · May 20, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT MAIN DECK FLOOR DITCHING PANS PAN ASSY IS CRACKED BS 1176 - 1183, LBL 37-47, WL 208. REMOVED DITCHING PAN, FABRICATED, HEAT TREATED TO T-6 CONDITION, ALODINED AND PRIMED AND INSTALLED NEW PAN, REF SRM 51-30-2 PG 1, CWG 65-29549, MM 51-30-05 PG1, SRM 51-10
- [SDR 08FDEA01906](https://openairdocs.org/sdr/08FDEA01906.md): Structure · cracked · May 20, 2008 · N220FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD LAV SINK CABINET WASTE DISPOSAL FIBERGLASS SHOOT IS CRACKED. REPAIRED LAV SINK CABINET WASTE DISPOSAL CHUTE REF SRM 51-40-9 PAR 7, THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01905](https://openairdocs.org/sdr/08FDEA01905.md): Stringer · corroded · May 20, 2008 · N220FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION ON I/B SIDE OF STR 28L AT FS 661, LBL6, WL 149 REPAIRED STRINGER AT 292 AT FS 661 LBL 6, WL 149. REF SRM 53-10-3, PG 3 -4, FIG 1, DETAIL 1, THIS IS CLASSIFIED AS MAJOR REPAIR.
- [SDR 08FDEA01904](https://openairdocs.org/sdr/08FDEA01904.md): Frame · damaged · May 20, 2008 · N220FE · Boeing 727233 · Fuselage Main, Frame
  > AFT PIT, BILGE BODY FRAME, HAS A DRILL START ON UPPER FLANGE AND CORRODED WEB BS 1143, FWD AND AFT SIDE, STR 26R - 27R, WL 153 - 156 LEVEL 1 CORROSION BLENDED AREA, FLAP PEENED AREA, APPLIED ALODINE AND PRIMER TO AREA APPLIED CORROSION INHIBITOR TO AREA, REF E

Next page: https://openairdocs.org/deregistered/N220FE-2013-03-19/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 = 'N220FE' AND deregistration_id = 'N220FE-2013-03-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N220FE-2013-03-19/reports

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