# Service difficulty reports: N217FE, cancelled Jun 18, 2013

A list on [N217FE, cancelled Jun 18, 2013](https://openairdocs.org/deregistered/N217FE-2013-06-18.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 · 67 reports

- [SDR FDEA201204111362](https://openairdocs.org/sdr/FDEA201204111362.md): Light · dislodged · Apr 11, 2012 · N217FE · Boeing 7272S2F · Emergency Lighting
  > ENTRY WAY EMERGENCY LIGHT FIXTURE FELL OUT ON ROLL OUT. REINSTALLED EMERGENCY LIGHT FIXTURE IAW MM 33-50-001-2-0. OPS CHECKED NORMAL.
- [SDR FDEA201203130907](https://openairdocs.org/sdr/FDEA201203130907.md): Web · cracked · Mar 13, 2012 · N217FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RT LOWER TORQUE BOX INBD WEB HAS IMPROPER REPAIR AT BS 1293. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 51-40-02 FIG 1.
- [SDR FDEA201203130913](https://openairdocs.org/sdr/FDEA201203130913.md): Web · cracked · Mar 13, 2012 · N217FE · Boeing 7272S2F · Cargo/Baggage Doors
  > C2 DOOR INTERIOR WEB IS CRACKED AT UPPER LIGHTNING HOLE BS 970. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3. REF EA 7-5230-143974.
- [SDR FDEA201203120906](https://openairdocs.org/sdr/FDEA201203120906.md): Skin · gouged · Mar 12, 2012 · N217FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > SKIN GOUGED BS 1320, S21L. CUT OUT DAMAGED SKIN DIM 2.750" X 1.600" IAW SRM 53-30-3 FIG 3 REV 103. FABRICATED REPAIR AND INSTALLED IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 3.
- [SDR FDEA201203050908](https://openairdocs.org/sdr/FDEA201203050908.md): Stringer · corroded · Mar 5, 2012 · N217FE · Boeing 7272S2F · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 29L, BETWEEN BS 950E AND 950F. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG1. FABRICATED REPAIR PARTS AND INSTALLED IAW EA 7-5310-143970.
- [SDR FDEA201203020765](https://openairdocs.org/sdr/FDEA201203020765.md): Web · cracked · Mar 2, 2012 · N217FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RIGHT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE BS 1243 PLUS 6 INCHES. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-40-02, FIG 1.
- [SDR FDEA201203020763](https://openairdocs.org/sdr/FDEA201203020763.md): Web · cracked · Mar 2, 2012 · N217FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RIGHT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE BS 1233, PLUS 7 INCHES. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-40-02, FIG 1.
- [SDR FDEA201203020761](https://openairdocs.org/sdr/FDEA201203020761.md): Web · cracked · Mar 2, 2012 · N217FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RIGHT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE BS 1223 PLUS 3 INCHES. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-40-02, FIG 1.
- [SDR FDEA201203020760](https://openairdocs.org/sdr/FDEA201203020760.md): Web · cracked · Mar 2, 2012 · N217FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR LEFT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE BS 1253 PLUS 7 INCHES. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-40-02 FIG 1.
- [SDR FDEA201203020758](https://openairdocs.org/sdr/FDEA201203020758.md): Web · cracked · Mar 2, 2012 · N217FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR LEFT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE BS 1223, PLUS 4 INCHES. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-40-02, FIG 1.
- [SDR FDEA201110154510](https://openairdocs.org/sdr/FDEA201110154510.md): Smoke Detector · malfunctioned · Oct 15, 2011 · N217FE · Boeing 7272S2F · Smoke Detection
  > ON FINAL, TWICE RECEIVED INTERMITTENT (1 SEC) MASTER FIRE WARNING LIGHTS (GLARESHIELD) AND BELL - NO FIRE INDICATIONS. AT ABOUT 600' AGL, FIRE LIGHTS ILLUMINATED, FIRE BELL SOUNDED AND THE NR 4 MAIN CARGO FIRE ILLUMINATED. LANDED AND EVACUATED THE COCKPIT THR
- [SDR FDEA201109073737](https://openairdocs.org/sdr/FDEA201109073737.md): Hook And Loop · failed · Sep 7, 2011 · N217FE · Boeing 7272S2F · Emergency Equipment
  > PBE IN AFT CABIN CAME LOOSE ON INITIAL TAKEOFF. REATTACHED HOOK AND LOOP IN REF TO SMP, GOOD FOR SERVICE.
- [SDR FDEA201105101796](https://openairdocs.org/sdr/FDEA201105101796.md): Line · disconnected · May 10, 2011 · N217FE · Boeing 7272S2F · Power Indicating System
  > ON RUNUP FOR TAKEOFF SET EPR'S AT COMPUTED VALUE. NOMINAL N1'S FOR 2 & 3 ALONG WITH CORRESPONDING EGT & FUEL FLOWS NORMAL. NR 1 ENGINE, WHEN SET TO COMPUTED EPR SETTING FOR T/O HAD ABNORMALLY LOW N1 & FUEL FLOW COMPARED TO ENGINES 2 & 3. NR 1 ALSO VERY S
- [SDR FDEA201009023245](https://openairdocs.org/sdr/FDEA201009023245.md): A/C Pack · failed · Sep 2, 2010 · N217FE · Boeing 7272S2F · Cabin Cooling System
  > ON TAKEOFF FROM DSM,THE LT PACK TRIPPED AND THE LT DUCT OVERHEAT LIGHT ILLUMINATED. THIS WAS ACCOMPAINED BY THE USUAL ODOR OF A PACK OVERHEATING AND SMOKE IN THE COCKPIT. QRH PROCEDURES ELIMINATED THE SMOKE & REESTABLISHED THE LT PACK. GIVEN THE OUTSIDE A
- [SDR FDEA201009013243](https://openairdocs.org/sdr/FDEA201009013243.md): Fan · failed · Sep 1, 2010 · N217FE · Boeing 7272S2F · Air Distribution Fan
  > ON TAKEOFF FROM DSM, THE LT PACK TRIPPED AND THE LT DUCT OVERHEAT LIGHT ILLUMINATED. THIS WAS ACCOMPAINED BY THE USUAL ODOR OF A PACK OVERHEATING AND SMOKE IN THE COCKPIT. QRH PROCEDURES ELIMINATED THE SMOKE & REESTABLISHED THE LT PACK. GIVEN THE OUTSIDE A
- [SDR FDEA201008263157](https://openairdocs.org/sdr/FDEA201008263157.md): Unknown · smoke · Aug 26, 2010 · N217FE · Boeing 7272S2F · Air Distribution System
  > AIR TURN BACK, SMOKE IN COCKPIT SMOKE APPEARED TO ORIGINATE FROM THE THROTTLE QUADRANT.
- [SDR FDEA201008263156](https://openairdocs.org/sdr/FDEA201008263156.md): Unknown · odor · Aug 26, 2010 · N217FE · Boeing 7272S2F · Air Distribution System
  > AIR TURNBACK, SMOKE IN COCKPIT, SMOKE APPEARED TO ORIGINATE FROM THE THROTTLE QUADRANT. VISIBLY CHECKED FWD NOSE COMPARTMENT WIRING, LIGHT BALLAST AND UNDER QUADRANT AREA, FOUND NO EVIDENCE OF FAULT. CHECKED AVIONICS BAY, WIRING, BOXES, FOUND LIGHTS ON EPG
- [SDR FDEA200907092560](https://openairdocs.org/sdr/FDEA200907092560.md): Angle · cracked · Jul 9, 2009 · N217FE · Boeing 7272S2F · Leading Edge Devices
  > NR 4 SLAT AFT LOWER ANGLE IS CRACKED BELOW T-DUCT. REMOVED NR 4 SLAT INNER PANELS IAW SRM 51-30-2. REMOVED LOWER ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 57-50- 2. TREATED AND PRIMED. REPAIR PARTS IAW SRM 51-10-2 INSTALLED ANGLE IAW SRM 51-
- [SDR FDEA200907072520](https://openairdocs.org/sdr/FDEA200907072520.md): Spar · cracked · Jul 7, 2009 · N217FE · Boeing 7272S2F · Wing Spar
  > LT WING T/E FALSE SPAR, INBD END REPAIR DOUBLER IS CRACKED. WBL 118 REMOVED NR 7 SPOILER FITTING AND SUPPORT IAW SRM 51-30-2. REMOVED PREVIOUS DOUBLER, TRIMMED OUT WEB AND REMOVED PREVIOUS CHORD REPAIR IAW DWG SR 27-57-038 REV C. FABRICATED NEW WEB FROM 7
- [SDR FDEA200907022466](https://openairdocs.org/sdr/FDEA200907022466.md): Angle · cracked · Jul 2, 2009 · N217FE · Boeing 7272S2F · Leading Edge Devices
  > NR 2 SLAT LOWER AFT ANGLE IS CRACKED BELOW TEE DUCT REMOVED INNER PANELS IAW SRM 51-30-2. CUT OUT DAMAGED AREA OF ANGLE IAW SRM 51-40-4 FIG 1 FABRICATED ANGLE SECTION IAW SRM 57-50-2 AND 51-40-4, ALODINED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR P
- [SDR FDEA200906262444](https://openairdocs.org/sdr/FDEA200906262444.md): Skin · cracked · Jun 26, 2009 · N217FE · Boeing 7272S2F · Leading Edge Devices
  > NR 3 SLAT CRACKED T/E AT OTBD HOOK AFT ATTACH FASTENERS. HFEC VERIFIED THAT CRACK ENDS AT FASTENER HOLE IAW NDTM 51-00-00. FABRICATED DOUBLER AND INSTALLED IAW SRM 57-50-3 AND 51-30-8.
- [SDR FDEA200906252332](https://openairdocs.org/sdr/FDEA200906252332.md): Floorbeam · corroded · Jun 25, 2009 · N217FE · Boeing 7272S2F · Fuselage Main, Floor Beam
  > FORWARD ENTRY WAY - FLOORBEAM CORRODED AT BS 344 RBL 10 TO LBL 45. REMOVED FLOORBEAM, FABRICATED NEW FLOORBEAM AND INSTALLED IAW DWG SR27-53-007 AND SRM 53-10-2, 51-30-5 AND 51-30-2.
- [SDR FDEA200906222462](https://openairdocs.org/sdr/FDEA200906222462.md): Skin · bulged · Jun 22, 2009 · N217FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > SKIN BULGE FUSELAGE STATION 219 STRINGER 24L. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2.
- [SDR FDEA200906222334](https://openairdocs.org/sdr/FDEA200906222334.md): Skin · cracked · Jun 22, 2009 · N217FE · Boeing 7272S2F · Landing Gear Doors
  > LT MLG WING DOOR IS CRACKED AT AFT HINGE POINT. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW DRAWING 65C27128 AND SRM 51-30-2.
- [SDR FDEA200906222330](https://openairdocs.org/sdr/FDEA200906222330.md): Unknown · misrepaired · Jun 22, 2009 · N217FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > PREVIOUS REPAIR STA 380 STR 29L HAS FASTENERS WITH IMPROPER EDGE MARGIN. REMOVED PREVIOUS REPAIR, HFEC INSPECTED HOLES WITH NO DEFECTS NOTED, FABRICATED NEW DOUBLER AND INSTALLED IAW EA 7-5330-126836.
- [SDR FDEA200906222203](https://openairdocs.org/sdr/FDEA200906222203.md): Skin · dented · Jun 22, 2009 · N217FE · Boeing 7272S2F · Fuselage Miscellaneous Structure
  > OIL CANNING SKIN AT STA 180 STR 26L. CUT OUT DAMAGED AREAS, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-30-3, 53-30-2, 51-10-2 AND 51-30-2.
- [SDR FDEA200906202333](https://openairdocs.org/sdr/FDEA200906202333.md): Rib · cracked · Jun 20, 2009 · N217FE · Boeing 7272S2F · Leading Edge Devices
  > NR 4 SLAT HAS 2 CRACKED RIBS ON EITHER SIDE OF THE ACTUATOR FWD MOUNT. REMOVED L/E SLAT ACCESS PANEL IAW SRM 51-30-2. REMOVED DAMAGED RIBS AT NR4 SLAT 2 EACH IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIBS IAW SRM 51-30-5 RIB PN 65-17276-9 AND 65-17276-11.
- [SDR FDEA200906202331](https://openairdocs.org/sdr/FDEA200906202331.md): Window Frame · corroded · Jun 20, 2009 · N217FE · Boeing 7272S2F · Fuselage Main, Structure
  > CORROSION ON WINDOW FRAME RT FUSELAGE STA 650. REMOVED CORROSION FROM WINDOW FRAME AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 51-10-6, 56-20-1, 56-20-3 AND 51-30-2.
- [SDR 07FDEA03799](https://openairdocs.org/sdr/07FDEA03799.md): Circuit Breaker · failed · Sep 15, 2007 · N217FE · Boeing 7272S2F · Fire Protection System Wiring
  > IN CRUISE SMELL OF SMOKE AND THE SIGHT OF SMOKE COMING FROM BACK OF S/O PANEL. SMOKE MOVED TOWARD F/O SEAT. THE SMELL WAS LIKE CAR EXHAUST. RAN ALL FUMES AND ODORS CHECK LIST. ALSO SHUT OFF GASPER FAN. THE SMOKE ONLY LASTED FOR AROUND 15 SEC. NO OTHER I
- [SDR 06FDEA04330](https://openairdocs.org/sdr/06FDEA04330.md): Skin · damaged · Dec 28, 2006 · N217FE · Boeing 7272S2F · Trailing Edge Flaps
  > LT WING FOREFLAP IS DAMAGED APPROX 79" FROM IB END. DAMAGE IS ON NOSE LE APPROX 3" LONG (DENT) REMOVED DAMAGE FROM L/E OF FLAP, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 57-50-2, AND SRM 57-50-4 PG 2A & 2B.
- [SDR 06FDEA03058](https://openairdocs.org/sdr/06FDEA03058.md): Feeder Cable · chafed · Aug 23, 2006 · N217FE · Boeing 7272S2F · Electrical Power System Wiring
  > DURING C-1 CHECK, FOUND GENERATOR FEEDER CABLE CHAFED AND SHORTED TO LOOP SUPPORT CLAMP, LOCATED AT STA 720E WATERLINE, 153" AND LBL 10" IN THE AIR DISTRIBUTION BAY. WO NR 33554, SNRM NR N00628. REPLACED APU FEEDER WIRE NR 300-011-2. REF SWPM 20-30-13 AND W
- [SDR 06FDEA03056](https://openairdocs.org/sdr/06FDEA03056.md): Skin · misrepaired · Aug 23, 2006 · N217FE · Boeing 7272S2F · Standard Practices/Structures
  > DURING C-1 CHECK, AGING AIRCRAFT INSPECTION IDENTIFIED EXTERNAL FUSELAGE SKIN REPAIR INSTALLED WITHOUT FAA APPROVED DATA. REPAIR IS LOCATED AT STA 294 AT STR 21R. REMOVED AND REPLACED REPAIR REF: SRM 53-30-3 WO NR 33554, SNRM NR N00420. REMOVED EXT REPAIR A
- [SDR 06FDEA3056](https://openairdocs.org/sdr/06FDEA3056.md): Skin · misrepaired · Aug 23, 2006 · N217FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > DURING C-1 CHECK, AGING AIRCRAFT INSPECTION IDENTIFIED EXTERNAL FUSELAGE SKIN REPAIR INSTALLED WITHOUT FAA APPROVED DATA. REPAIR IS LOCATED AT STA 294 AT STR 21R. REMOVED AND REPLACED REPAIR REF: SRM 53-30-3.
- [SDR 06FDEA3058](https://openairdocs.org/sdr/06FDEA3058.md): Feeder Cable · chafed · Aug 23, 2006 · N217FE · Boeing 7272S2F · Electrical Power System Wiring
  > DURING C-1 CHECK, FOUND GENERATOR FEEDER CABLE CHAFED AND SHORTED TO LOOP SUPPORT CLAMP. LOCATED AT STA 720E WATERLINE, 153 INCH AND LBL 10 INCH IN THE AIR DISTRIBUTION BAY.
- [SDR 06FDEA03004](https://openairdocs.org/sdr/06FDEA03004.md): Skin · misrepaired · Aug 18, 2006 · N217FE · Boeing 7272S2F · Standard Practices/Structures
  > DURING C-1 CHECK AGING AIRCRAFT INSPECTION, IDENTIFIED EXTERNAL FUSELAGE SKIN REPAIR INSTALLED WITHOUT FAA APPROVED DATA. REPAIR IS LOCATED AT STA.640 BETWEEN STRINGERS 24L AND STR 28L. REMOVED AND REPLACED REPAIR PER B727 SRM 53-30-3 FIG 5 PG 22. INSTALLED
- [SDR 06FDEA03003](https://openairdocs.org/sdr/06FDEA03003.md): Skin · misrepaired · Aug 18, 2006 · N217FE · Boeing 7272S2F · Standard Practices/Structures
  > DURING C-1 CHECK, AGING AIRCRAFT INSPECTION IDENTIFIED EXTERNAL FUSELAGE SKIN REPAIR INSTALLED WITHOUT FAA APPROVED DATA. REPAIR IS LOCATED AT STA 950 AT STR 28L. REMOVED AND REPLACED REPAIR REF: B727 SRM 53-30-3 FIG 1 PG 8 WO NR 33554, SNRM NR N00556. INST
- [SDR 06FDEA3003](https://openairdocs.org/sdr/06FDEA3003.md): Skin · misrepaired · Aug 18, 2006 · N217FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > DURING C-1 CHECK, AGING AIRCRAFT INSPECTION IDENTIFIED EXTERNAL FUSELAGE SKIN REPAIR INSTALLED WITHOUT FAA APPROVED DATA. REPAIR IS LOCATED AT STA 950 AT STR 28L. REMOVED AND REPLACED REPAIR REF: B727 SRM 53-30-3 FIG 1 PG 8.
- [SDR 06FDEA3004](https://openairdocs.org/sdr/06FDEA3004.md): Skin · misrepaired · Aug 18, 2006 · N217FE · Boeing 7272S2F · Fuselage Main, Plate/Skin
  > DURING C-1 CHECK AGING AIRCRAFT INSPECTION, IDENTIFIED EXTERNAL FUSELAGE SKIN REPAIR INSTALLED WITH OUT FAA APPROVED DATA. REPAIR IS LOCATED AT STA 640 BETWEEN STRINGERS 24L AND STR 28L REMOVED AND REPLACED REPAIR PER B727 SRM 53-30-3 FIG 5 PG 22.
- [SDR 06FDEA1960](https://openairdocs.org/sdr/06FDEA1960.md): Duct · leaking · May 17, 2006 · N217FE · Boeing 7272S2F · Engine (Turbine/Turboprop)
  > ON TAKEOFF LEG AT APPROX 500' AGL, NR 2 FIRE LIGHT ILLUMINATED AND FIRE WARNING BELL SOUNDED. ACCOMPLISHED RED TAB PROCEDURES. FIRELIGHT WENT OUT AFTER DISCHARGING ONE FIRE BOTTLE. INSPECTED NR 2 ENG IAW PW MM 72-00-00 FOR WINDMILLING. INSPECTED OIL FILT
- [SDR 05FDEA04115](https://openairdocs.org/sdr/05FDEA04115.md): O-Ring · damaged · Dec 4, 2005 · N217FE · Boeing 7272S2F · Power Indicating System
  > REJECTED FIRST T/O DUE TO ENG FAIL LIGHT ON, NR 3 ENG ADV UP TO RED LINE N1 BUT EPR WAS STILL VERY LOW TO CONTINUE T/O, PILOT SAID ENG RED LINE NI WAS NOT EXCEEDED, REMOVED NR 3 ENG BULLET, PRESS TESTED THAT SECTION OF PT2 LINE, CHKS GOOD. FOUND THE TWO O-RIN
- [SDR 04FDEA00003](https://openairdocs.org/sdr/04FDEA00003.md): Smoke Detector · malfunctioned · Jan 1, 2004 · N217FE · Boeing 727200 · Smoke Detection
  > ON CLIMBOUT, MAIN CARGO SMOKE WARNING ACTIVATED. SHORTLY THERE AFTER LIGHT EXTINGUISHED. APPROXIMATELY 1.5 TO 2 MINS LATER MAIN CARGO SMOKE WARNING RE-ACTIVATED. ALSO MIGRATED FROM ONE ZONE ILLUMINATED TO 2 ZONES (BULBS) ILLUMINATED. REPLACED ZONE 1 AND 2
- [SDR 03FDEA01838](https://openairdocs.org/sdr/03FDEA01838.md): Motor · failed · Oct 30, 2003 · N217FE · Boeing 727200 · Leading Edge Slat Actuator
  > ALT FLAPS EXT SYSTEM DOES NOT EXTEND LED'S. FLAPS APPEAR TO WORK OK BUT DIDN'T GO BEYOND 2. TROUBLESHOT ALT FLAP SYS. REPLACED L/E MOTOR PUMP ASSY. REPLACED L/E FLAP AND SLAT SELECTOR VALVE. REPAIRED L/E STANDBY DRIVE SHUT OFF VALVE GROUND WIRES AT GD846.
- [SDR 03FDEA01828](https://openairdocs.org/sdr/03FDEA01828.md): Clamp · out of position · Oct 29, 2003 · N217FE · Boeing 727200 · Landing Gear Position and Warning
  > FLIGHT TEST: NOSE GEAR INDICATOR LIGHT FLICKERS & IS INTERMITTENTLY OFF WITH GEAR DOWN & LOCKED. FOUND IF PRESSURE IS APPLIED TO INBOARD EDGE OF MASTER DIM AND TEST SWITCH, LIGHTS (NOSE GEAR AND NR 3 OIL PRESSURE LIGHT) WOULD FLICKER, LOOSENED PANEL, AND FO
- [SDR 03FDEA01765](https://openairdocs.org/sdr/03FDEA01765.md): Floorbeam · damaged · Oct 17, 2003 · N217FE · Boeing 727200 · Fuselage Main, Floor Beam
  > STA 950F, WL 208, LBL 30 & 36 FLOORBEAM HAS TOOL MARKS. BLENDED TOOL MARKS FROM 950F FLOORBEAM WL 208, LBL 30-36, REMOVED 1 X1 X.150 & 1 X2 X.045 FROM ORIGINAL OF.225. OUT OF LIMIT PER SRM 51-10-1. CUT OFF DAMAGE SECTION OF FLOOR BEAM, AFT UPPER
- [SDR 03FDEA01738](https://openairdocs.org/sdr/03FDEA01738.md): Lap Joint · chafed · Oct 15, 2003 · N217FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > CHAFING ON LAP JOINT SKIN STR19R, BS720D PLUS 10 INCHES. BLENDED OUT LAP JOINT SKIN STR 19R, BS 720D 10, 2 X 2 X.022 FROM ORIGINAL OF.060. FOUND TO BE OUT OF LIMITS PER SRM 53-30-1 CUT OUT DAMAGE FROM LAP AND REPAIRED PER SRM 53-30-3,
- [SDR 03FDEA01737](https://openairdocs.org/sdr/03FDEA01737.md): Skin · chafed · Oct 14, 2003 · N217FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > CHAFING ON LAP JOINT SKIN STR 19L B/S 720D PLUS 10 INCHS. BLENDED CHAFFE FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA AND REPAIRED. PER SRM 53-30-3 FIG 14.
- [SDR 03FDEA01713](https://openairdocs.org/sdr/03FDEA01713.md): Floorbeam · corroded · Oct 8, 2003 · N217FE · Boeing 727200 · Fuselage Main, Floor Beam
  > CORROSION BS 320-340, RBL 40, WL 208 ON TOP OF FLOORBEAM AND INTERCOSTAL REMOVED AND REPLACED FLOORBEAM.
- [SDR 03FDEA01708](https://openairdocs.org/sdr/03FDEA01708.md): Keelbeam · corroded · Oct 7, 2003 · N217FE · Boeing 727200 · Fuselage Main, Keel
  > CORROSION ON RT KEEL BEAM BS 950F 8 O/B FLANGE. *S/D* BLENDED CORROSION ON RT KEEL BEAM BS 950F 8 O/B FLANGE AND FOUND OUT OF LIMITS. FABRICATED REPAIR STRAP AND INSTALLED REPAIR STRAP. ALL WORK DONE IAW SR 27-53- 023A.
- [SDR 03FDEA01696](https://openairdocs.org/sdr/03FDEA01696.md): Frame · dented · Oct 3, 2003 · N217FE · Boeing 727200 · Fuselage Main, Frame
  > FWD CARGO SIDE FRAME DENTED STA 680, LBL 33, WL 160. OUT OF LIMITS. CUT OUT DAMAGE & REPAIRED FRAME BS 680, LBL 33, WL 160 PER SRM 53-10- 1, 51-40-3 FIG 1 AND FED EX EA 7-5310-55028.
- [SDR 03FDEA01700](https://openairdocs.org/sdr/03FDEA01700.md): Frame · dented · Oct 3, 2003 · N217FE · Boeing 727200 · Fuselage Main, Frame
  > FWD CARGO SIDE FRAME DENTED STA 680 RBL 30 WL 157. FWD CARGO SIDE FRAME DENTED STA 680, RBL 30, WL 157 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIR FRAME PER SRM 51-40-3.

Next page: https://openairdocs.org/deregistered/N217FE-2013-06-18/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 = 'N217FE' AND deregistration_id = 'N217FE-2013-06-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N217FE-2013-06-18/reports

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