# Service difficulty reports: N221FE, cancelled Aug 10, 2015

A list on [N221FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N221FE-2015-08-10.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 · 127 reports

- [SDR FDEA201304090747](https://openairdocs.org/sdr/FDEA201304090747.md): Battery Pack · failed · Apr 9, 2013 · N221FE · Boeing 727233 · Emergency Lighting
  > ON WALKAROUND, FOUND THE FUSELAGE SLIDE LIGHT IS INOPERATIVE. INSPECTED LIGHT ASSY. FOUND VERY CORRODED. REMOVED OLD BATTERY PACK FROM E&E BAY. R & R EMERGENCY SLIDE LIGHT BATTERY PACK IN REF WITH AMM 33-50-041-2. OPS NORMAL. ACFT IS OK FOR SVC.
- [SDR FDEA201303010484](https://openairdocs.org/sdr/FDEA201303010484.md): Wire · failed · Mar 1, 2013 · N221FE · Boeing 727233 · Auto Flight System Wiring
  > REPEAT WRITE UP: UNCOMMANDED YAW DURING LOW SPEED AND HIGH SPEED FLIGHT. DIRECTED BY GOC TO RETURN TO DEPARTURE. R & R YAW DAMPER LOWER RUDDER WIRE BUNDLE W325 IAW SWPM 20-10-11 20-10-11.
- [SDR FDEA201302280478](https://openairdocs.org/sdr/FDEA201302280478.md): Actuator · inoperative · Feb 28, 2013 · N221FE · Boeing 727233 · Auto Flight System
  > ACFT ENCOUNTERED UNCOMMANDED YAW. GOC/MX DIRECTED RETURN TO DEPARTURE. REMOVED AND REPLACED STANDBY ACTUATOR IAW AMM 27-20-151-2. CHECKED STANDBY ACTUATOR MOVEMENT, NOTHING OUT OF NORMAL FOUND DURING CHECKS. TESTED SYS IAW AMM 27-00-051-6 AND AMM 22-11-14
- [SDR FDEA201302090315](https://openairdocs.org/sdr/FDEA201302090315.md): Damper · malfunctioned · Feb 9, 2013 · N221FE · Boeing 727233 · Rudder Control System
  > UNCOMMANDED RUDDER INPUTS WITH OR WITHOUT AUTOPILOT ENGAGED. PERFORMED YAW DAMPER ADJUSTMENT TEST STEP 1 THRU 10 IAW AMM 22-11-005-5 AND UPPER YAW DAMPER TEST DID NOT PASSED, R & R UPPER YAW DAMPER IAW AMM 22-11-131-4, TESTED IAW AMM 22-11-005-5 AND TEST PASS
- [SDR FDEA201301120089](https://openairdocs.org/sdr/FDEA201301120089.md): Unknown · malfunctioned · Jan 12, 2013 · N221FE · Boeing 727233 · Rudder Control System
  > UNCOMMANDED YAW AT FL300, MACH.835, SMOOTH AIR F/O FELT RUDDER PEDALS MOVE WE WERE IN CRUISE FLIGHT AUTOPILOT ENGAGED. TROUBLESHOT IAW AMM 22-11-005-1 AND R & R LOWER YAW DAMPER RUDDER POWER UNIT COMPONENTS, HYD TRANSFER VALVE, HYD SOLENOIDE VALVE, TRANDUCE
- [SDR FDEA201206282384](https://openairdocs.org/sdr/FDEA201206282384.md): Switch · malfunctioned · Jun 28, 2012 · N221FE · Boeing 727233 · Door Warning System
  > EQUIPMENT BAY ACCESS DOOR LIGHT ILLUMINATED DURING PUSH BACK. R & R ELECTRIC ACCESS LIMIT SWITCH (S114) IAW SWPM 20-30-00. PERFORMED DOOR WARNING TEST IAW AMM 52-70-001-5-1. ALL CHECKED GOOD, ACFT OK FOR SERVICE.
- [SDR FDEA201109284195](https://openairdocs.org/sdr/FDEA201109284195.md): Trim System · malfunctioned · Sep 28, 2011 · N221FE · Boeing 727233 · Stabilizer Control System
  > MAIN STAB TRIM (ON FINAL) DID NOT WORK, TRIED CAPT AND F/O TRIM BUTTONS ON YOKE LIGHT ON CENTER CONSOLE DID COME ON. DID NOT WORK TAXIING IN. AFTER SHUTDOWN OF ENGINES WORKED NORMALLY BOTH SIDES. ACCOMPLISHED THE STABILIZER TRIM SYS TEST IAW AMM 27-40-000-5
- [SDR FDEA201108203391](https://openairdocs.org/sdr/FDEA201108203391.md): Actuator · failed · Aug 20, 2011 · N221FE · Boeing 727233 · Leading Edge Slat Actuator
  > NR 1 SLAT FAILED TO RETRACT AFTER TAKEOFF. QRH COMPLIED WITH NO HELP. REPLACED L/E SLAT NR 1 ACTUATOR IAW TO AMM 27-81-000-2. TEST SEVERAL TIMES NO DISCREPANCIES FOUND.
- [SDR FDEA201107313043](https://openairdocs.org/sdr/FDEA201107313043.md): Connector · dirty · Jul 31, 2011 · N221FE · Boeing 727233 · Leading Edge Slat Actuator
  > ON CLIMB OUT, FLAPS 15 ALL IS WELL. WHEN FLAP HANDLE RAISED FROM FLAPS 15 GOT AN ASSYMETRYCAL WARNING LIGHT. RUN QRH RETURNED TO DEPARTURE. FAULT CONTINUES ON GROUND OPERATION. VERIFIED SLAT ACTUATOR NR 1 DIDN`T RETRACT AT HANDLE AT 2 DEG POS. INSPECTED
- [SDR FDEA201105251983](https://openairdocs.org/sdr/FDEA201105251983.md): Skin · gouged · May 25, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MCD INNER SURROUND SKIN GOUGED STA 620 STR 15 - 16L ACCOMPLISHED REPAIR AT MCD INNER SURROUND SKIN IAW EA 7-5310-123597.
- [SDR FDEA201105241973](https://openairdocs.org/sdr/FDEA201105241973.md): Skin · damaged · May 24, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > INNER SKIN STA 540 STR 3L DOUBLE DRILLED HOLES. ACCOMPLISHED REPAIR AT BS 540 STR 3L INNER SKIN IAW EA 7-5310-123595.
- [SDR FDEA201105241972](https://openairdocs.org/sdr/FDEA201105241972.md): Support Fitting · damaged · May 24, 2011 · N221FE · Boeing 727233 · Fuselage Main, Structure
  > MAIN CARGO DOOR BS 620 AFT O/B SUPPORT FITTING HAS ELONGATED FASTENER HOLES REMOVED DAMAGED BS 620 TENSION ANGLE (SUPPORT FITTING), FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-2, 51-10-2, AND DRAWING 53FX1286.
- [SDR FDEA201105241971](https://openairdocs.org/sdr/FDEA201105241971.md): Frame · damaged · May 24, 2011 · N221FE · Boeing 727233 · Fuselage Main, Frame
  > MAIN CARGO DOOR CUT-OUT BS 620 FRAME WEB HAS DOUBLE DRILLED FASTENERS REMOVED AND REPLACED BS 620 FRAME WEB IAW EA 7-5310-123595.
- [SDR FDEA201105191922](https://openairdocs.org/sdr/FDEA201105191922.md): Frame · damaged · May 19, 2011 · N221FE · Boeing 727233 · Fuselage Main, Frame
  > AFTER FRAME REMOVAL AND CLEAN UP FOUND DOUBLE DRILL HOLES STA 620 BETWEEN STR 10L TO STR 13L. CUTOUT DAMAGED AREAS (3) AT BS 620 STR 10L, STR 11L, AND STR 13L AND FABRICATED FILLERS (3). INSTALLED FILLERS (3) AND FABRICATED REPAIR DOUBLER AND REPAIR TR
- [SDR FDEA201105191921](https://openairdocs.org/sdr/FDEA201105191921.md): Frame · damaged · May 19, 2011 · N221FE · Boeing 727233 · Fuselage Main, Frame
  > DOUBLE DRILLED HOLES FOUND UPON REMOVAL OF INNER SKIN GOING THROUGH SHIM AND FRAME STA 620, STR 9L AT 2 EACH LOCATIONS.
- [SDR FDEA201105161871](https://openairdocs.org/sdr/FDEA201105161871.md): Web · damaged · May 16, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > BS 1183 HORIZONTAL CHORD & WEB WL 190 HAS FASTENERS WITH NO SPACING & DAMAGED FASTENER HOLES. ACCOMPLISHED REPAIR AT BS 1183 HORIZONTAL CHORD & WEB IAW EA 7-5310-123591.
- [SDR FDEA201105111799](https://openairdocs.org/sdr/FDEA201105111799.md): Skin · damaged · May 11, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > SKIN STA. 590 STR 3L HAS DOUBLE DRILLED HOLES. ACCOMPLISHED REPAIR AT BS 590 STR 3L IAW EA 7-5310-123595.
- [SDR FDEA201105081795](https://openairdocs.org/sdr/FDEA201105081795.md): Frame · damaged · May 8, 2011 · N221FE · Boeing 727233 · Fuselage Main, Frame
  > BS 620 FRAME DOUBLER HAS FASTENER HOLES WITH NO ED. REMOVED AND REPLACED BS620 FRAME DOUBLER IAW EA 7-5310-123595.
- [SDR FDEA201105081794](https://openairdocs.org/sdr/FDEA201105081794.md): Frame · damaged · May 8, 2011 · N221FE · Boeing 727233 · Fuselage Main, Frame
  > AFTER REMOVAL OF FRAME AND CLEANUP FOUND DOUBLE DRILL HOLES STA. 620 BETWEEN STR 3L - 4L. REPAIRED BS 620 STRINGER 3-4L SKIN AND FRAME IAW EA 7-5310-123595.
- [SDR FDEA201105061764](https://openairdocs.org/sdr/FDEA201105061764.md): Floorbeam · damaged · May 6, 2011 · N221FE · Boeing 727233 · Fuselage Main, Floor Beam
  > DOUBLE DRILLED FLOORBEAM WEB MAIN CABIN STA 783, RBL 55. REMOVED SEAT TRACK, REMOVED DAMAGED WEB AT BS 783 RBL 55, CUTOUT DAMAGE AREA OF WEB, FABRICATED WEB REPAIR, INSTALLED WEB REPAIR AT BS 783 RBL 55, REINSTALLED SEAT TRACK SECTION AT RBL 65 BETWEEN BS
- [SDR FDEA201105061762](https://openairdocs.org/sdr/FDEA201105061762.md): Door Frame · corroded · May 6, 2011 · N221FE · Boeing 727233 · Fuselage Main, Structure
  > UPON REMOVAL OF AFT LOWER RADIUS SEAL DEPRESSOR, FOUND C-2 DOOR SFT FRAME CORRODED AT LOWER STUB. CUTOUT DAMAGE ON C-2 DOOR LOWER AFT FRAME IAW FED EX B727 SRM REV 103, 51-10-1. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW FED EX EA# 7-5230-136757 AND
- [SDR FDEA201105061763](https://openairdocs.org/sdr/FDEA201105061763.md): Rib · chafed · May 6, 2011 · N221FE · Boeing 727233 · Leading Edge Devices
  > NR 5 SLAT OTBD END WEB IS CHAFED. REMOVED RIB WEB, FORMED RIB WEB FROM 20240.032 DIM 17.3" X 6.8", HEAT TREATED TO T4 CONDITION IAW FAS ENG REP. 2-37153-801 REV A & DWG. 65-17286, INSTALLED RIB WEB IAW SRM 51-30-2, 51-30-5, 51-10-2 AT NR 5 SLAT OUTBOARD END
- [SDR FDEA201105051761](https://openairdocs.org/sdr/FDEA201105051761.md): Skin · cracked · May 5, 2011 · N221FE · Boeing 727233 · Cargo/Baggage Doors
  > C-2 DOOR INNER SKIN IS CRACKED AT RIVNUT, UPPER SECTION BTWN BS 950F - 970. CUT OUT DAMAGE ON C-2 DOOR INNER SKIN UPPER SECTION IAW SRM, REV 103, 52-30-2, FIG 3. FABRICATED DOUBLER AND SHIMS IAW SRM 52-30-2, FIG 3. INSTALLED FITTING, DOUBLER AND SHIMS IAW SRM
- [SDR FDEA201105021750](https://openairdocs.org/sdr/FDEA201105021750.md): Floorbeam · damaged · May 2, 2011 · N221FE · Boeing 727233 · Fuselage Main, Floor Beam
  > DOUBLE DRILLED FLOORBEAM WEB MAIN CABIN STA 783, RBL 55. REMOVED SEAT TRACK REMOVED DAMAGED WEB AT BS 783 RBL 55, CUTOUT DAMAGE AREA OF WEB, FABRICATED WEB, INSTALLED WEB REPAIR AT BS 783 RBL 55, AND REINSTALLED SEAT TRACK SECTION IAW SRM 51-30-2, 51-10-1, 51
- [SDR FDEA201104301695](https://openairdocs.org/sdr/FDEA201104301695.md): Skin · damaged · Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF MCD HEADER BEAM NOTED FASTENER HOLES WITH SHORT OFF CTR SPACING AT FS 490 BETWEEN STRINGERS 3 & 4 LT. ACCOMPLISHED REPAIR AT BS 490 STR 3L INNER SKIN IAW EA 7-5310-123595.
- [SDR FDEA201104301694](https://openairdocs.org/sdr/FDEA201104301694.md): Skin · damaged · Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > BS 520 STR, 3L FOUND MISDRILLED HOLES IN THE OEM SKIN. ACCOMPLISHED REPAIR AT BS 520 STR 3L INNER SKIN IAW EA 7-5310-123595.
- [SDR FDEA201104301693](https://openairdocs.org/sdr/FDEA201104301693.md): Skin · damaged · Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF MCD, FOUND FASTNER HOLE WITH ZERO EDGE MARGIN. FUSELAGE SKIN STA 545 BENEATH STR 3L. CUTOUT DAMAGED AREA, FABRICATED FILLER AND INSTALLED REPAIR PARTS IAW EA 7-5310-123595.
- [SDR FDEA201104301692](https://openairdocs.org/sdr/FDEA201104301692.md): Skin · damaged · Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > BS 560 STR 3L FOUND MISDRILLED HOLES IN THE EOM SKIN. ACCOMPLISHED REPAIR AT BS 560 STR 3L INNER SKIN IAW EA 7-5310-1235.
- [SDR FDEA201104301691](https://openairdocs.org/sdr/FDEA201104301691.md): Skin · damaged · Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF MCD, FOUND FASTENER HOLE WITH ZERO EDGE MARGIN - FUSELAGE SKIN, STA 590 BENEATH STR 3L. REPAIRED FUSELAGE SKIN AT BS 500 STR 3L IAW EA 7-5310-123595.
- [SDR FDEA201104301690](https://openairdocs.org/sdr/FDEA201104301690.md): Skin · damaged · Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > BS 610 - 600 STR 3L FOUND MISDRILLED HOLES IN THE OEM SKIN. ACCOMPLISHED REPAIR AT BS 610 - 600 STR 3L IAW EA 7-5130-123595.
- [SDR FDEA201104291670](https://openairdocs.org/sdr/FDEA201104291670.md): Attach Angle · cracked · Apr 29, 2011 · N221FE · Boeing 727233 · Fuselage, Landing Gear Attach Fittings
  > ATTACH ANGLE CRACKED, APPROX 3" LONG CRACK, AT NLG RT TRUNNION FITTING. (NDT VERIFIED). REMOVED RT NLG TRUNNION FITTING SUPPORT IAW SRM REV 103, 51-30-2. DRILLED, DEBURRED SUPPORT ANGLE IAW SRM 51-30-5 AND 51-30-2. INSTALLED SUPPORT IAW SRM 51-30-2.
- [SDR FDEA201104271679](https://openairdocs.org/sdr/FDEA201104271679.md): Seat Track · corroded · Apr 27, 2011 · N221FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > AFT MAIN CABIN CARGO DECK AT BS 1140 - BS 1150 RBL 25 INBD SEAT TRACK ATTACHMENT FLANGE HAS 2 EA LOCALIZED AREAS OF CORROSION. REMOVED DAMAGED SEAT TRACK SECTION AT RBL 25 FROM BS 1130 - BS 1175. FABRICATED NEW SEAT TRACK SECTION. INSTALLED NEW SEAT TRA
- [SDR FDEA201104261647](https://openairdocs.org/sdr/FDEA201104261647.md): Rib · cracked · Apr 26, 2011 · N221FE · Boeing 727233 · Leading Edge Devices
  > NR 3 SLAT OTBD END RIB IS CRACKED. REMOVED RIB ANGLE AT NR 3 SLAT OUTBD END, IAW SRM 51-30-2 FABRICATED NEW RIB ANGLE IAW SRM 51-20-4 FIG 2 AND DWG 65-17304, TREATED AND PRIMED NEW RIB ANGLE IAW SRM 51-10-2, INSTALLED NEW RIB ANGLE SECTION IAW SRM 51-30-2 HE
- [SDR FDEA201104201536](https://openairdocs.org/sdr/FDEA201104201536.md): Window Frame · corroded · Apr 20, 2011 · N221FE · Boeing 727233 · Fuselage Main, Structure
  > CORROSION WINDOW FRAME RT SIDE STA. 950 REMOVED CORROSION IAW SRM 51-10-6. MEASURED BLEND TO BE OUT OF LIMITS IAW SRM 56-20-1 FIG 1. FABRICATED DOUBLER REPAIR AND INSTALLED DOUBLE REPAIR IAW SRM 56-20-3 FIG 1.
- [SDR FDEA201104191520](https://openairdocs.org/sdr/FDEA201104191520.md): Sill · damaged · Apr 19, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > INBD CTR SILL HAS DOUBLE DRILLED HOLES STA 530-570, STRINGER 3L ACCOMPLISHED REPAIR AT MAIN CARGO DOOR SILL IAW EA 7-5310-123588 AND EA 7-5310-123595.
- [SDR FDEA201104191519](https://openairdocs.org/sdr/FDEA201104191519.md): Sill · damaged · Apr 19, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > MCD CUTOUT INBD AFT UPPER SILL HAS DOUBLE DRILLED HOLE AT STA 620, STR 3L. ACCOMPLISHED REPAIR AT MAIN CARGO DOOR UPPER SILL IAW EA 7-5310-123588 AND EA 7-5310-123595.
- [SDR FDEA201104181515](https://openairdocs.org/sdr/FDEA201104181515.md): Stringer · cracked · Apr 18, 2011 · N221FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CRACK ON STR 5R, STA 340 AT 9G BULKHEAD FWD SIDE. CUTOUT DAMAGED STRINGER, FABRICATED REPAIR PARTS (FILLER AND SPLICE). INSTALLED NEW REPAIR PARTS AT STRINGER 5R, BS 340 IAW SRM 53-10-3, FIG 1.
- [SDR FDEA201104151805](https://openairdocs.org/sdr/FDEA201104151805.md): Skin · damaged · Apr 15, 2011 · N221FE · Boeing 727233 · Cargo/Baggage Doors
  > REMOVED DOUBLER AND FILLER REPAIR AT MCD OUTER SKIN STA 560 STR 7L IAW EA 7-5230-136753. FABRICATED NEW DOUBLER AND FILLER REPAIR IAW E.A. 7-5230-136753. INSTALLED NEW DOUBLER AND FILLER REPAIR IAW E.A. 7-5230-136753.
- [SDR FDEA201104151491](https://openairdocs.org/sdr/FDEA201104151491.md): Skin · damaged · Apr 15, 2011 · N221FE · Boeing 727233 · Elevator, Plate/Skin
  > LT ELEVATOR TOP SIDE AT TRIM TAB CTR BOB WEIGHT HAS 3 LIGHTING STRIKES. REMOVED DAMAGE ON LT ELEVATOR UPPER AFT SKIN IAW SRM REV 103, 51-10-1. FABRICATED FILLER AND DOUBLER IAW SRM 55-20-3, FIG 5, INSTALLED DOUBLER AND FILLER IAW SRM 51-40-20 AND 55-20-3,
- [SDR FDEA201104131466](https://openairdocs.org/sdr/FDEA201104131466.md): Web · cracked · Apr 13, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR LT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTNING HOLE BETWEEN BS 1223 - 1233. CUT OUT DAMAGE 5/8" X 1" IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 & 51-40-2 FIG 1.
- [SDR FDEA201104131465](https://openairdocs.org/sdr/FDEA201104131465.md): Web · cracked · Apr 13, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR RT LOWER TORQUE BOX INBD WEB IS CRACKED AT LIGHTNING HOLE BETWEEN BS 1293- 1303. CUT OUT DAMAGE 1/2" X 1" ON AFT AIRSTAIR RT LOWER TORQUE BOX WEB IAW SRM REV 103 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1. INSTALLED DOUBLER IAW SRM
- [SDR FDEA201104131463](https://openairdocs.org/sdr/FDEA201104131463.md): Stringer · corroded · Apr 13, 2011 · N221FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > FWD PIT STR 26L IS CORRODED WITH EXFOLIATION FROM BS 720D- 720E. CUTOUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1 REV 103. FABRIATED HAT SECTION (2 EACH) AND SPLICE CHANNEL (3 EACH) IAW SRM 53-10-3 FIG 1 REV 103. INSTALLED STRINGER REPAIR PARTS IAW SR
- [SDR FDEA201104121461](https://openairdocs.org/sdr/FDEA201104121461.md): Sill · damaged · Apr 12, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > MCD UPPER SILL BS 502 BETWEEN STR 3L AND 4L UPPER FLANGE HAS DOUBLE DRILLED FASTENER HOLE. ACCOMPLISHED UPPER SILL REPAIR IAW EA 7-5310-123588 AND EA 7-5310-123595.
- [SDR FDEA201104081462](https://openairdocs.org/sdr/FDEA201104081462.md): Bulkhead · misinstalled · Apr 8, 2011 · N221FE · Boeing 727233 · Fuselage Main, Bulkhead
  > LOCK FASTENER FOUND WITH NO EDGE DISTANCE STA 1183 FWD SIDE OF BULKHEAD WL 163, LBL 24 VERTICAL BEAM. ACCOMPLISHED REPAIR AT BS 1183 VERTICAL BEAM IAW EA 7-5310-123591.
- [SDR FDEA200909223367](https://openairdocs.org/sdr/FDEA200909223367.md): Switch · inoperative · Sep 22, 2009 · N221FE · Boeing 727233 · Leading Edge Slat Control System
  > ON CLIMBOUT RT INBD LED WOULD NOT RETRACT. RUN QRH, RTB, NO RESTRICTION NR 4 L/E FLAP HAS JUMPER CABLE INSTALLED IAW MM 27-82-000-1. REMOVED AND REPLACED AND CHECKED NR 4 L/E SWITCH IAW AMM 27-82-011-4, ALL SYS CHECKED GOOD AT THIS TIME. PREMATURE REMOVAL/I
- [SDR 08FDEA04554](https://openairdocs.org/sdr/08FDEA04554.md): Skin · misrepaired · Oct 26, 2008 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > REPAIR AT STA 440 STR 10L NOT IAW SRM. REMOVED PREVIOUS REPAIR AND CUTOUT DAMAGED AREA DIMS 12" BY 9" IAW WITH EA 7-5330-126855 HFEC INSPECTED EDGE OF CUTOUT AND.040 INSURANCE CUT AND EXISTING HOLES FREE OF CRACK INDICATIONS IAW NDTM 51-00-00. FABRICATED DO
- [SDR 08FDEA04380](https://openairdocs.org/sdr/08FDEA04380.md): Skin · damaged · Oct 16, 2008 · N221FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CABIN STA 440 STR 10L HAS MIS-DRILLED FASTENER HOLES. CUT OUT DAMAGED AREA DIMS 2 INCH BY 7/8 INCH. FABRICATED DOUBLER USING 2024-T3.090 PO NR 9007561 DIMS 12 5/8 BY 9 1/2 INCH, FILLER USING 2024-T3.190 PO NR 314676 DIMS 2 INCH BY 7/8 INCH, IAW B727 SRM 53
- [SDR 08FDEA04340](https://openairdocs.org/sdr/08FDEA04340.md): Structure · cracked · Oct 14, 2008 · N221FE · Boeing 727233 · Trailing Edge Flaps
  > CRACK ON AFT STRUCTURE OF RT INBD FLAP WBL 114.2 FABRICATED AFT STRUCTURE REPAIR FILLER, ANGLE SPLICE, INSTALLED REPAIR SPLICE AND FILLER ON RT INBD FLAP IAW SRM 57-50-2, SRM 51-40-4, AND SRM 51-30-2.
- [SDR 08FDEA04309](https://openairdocs.org/sdr/08FDEA04309.md): Stringer · corroded · Oct 11, 2008 · N221FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION ON S29R AT BS 970-990. BLENDED OUT S29R FLANGE AS NECESSARY TO REMOVE CORROSION, REMAINING THICKNESS DIMENSIONS MAINTAIN A 20-1 BLENDOUT RATIO WITH A MIN 1.0: RADIUS PER MESSAGE 1-1013418906-2,3,4,5,6, AND ARE WITHIN LIMITS. ACCOMPLISHED HFEC AND SU
- [SDR 08FDEA04308](https://openairdocs.org/sdr/08FDEA04308.md): Lever · gouged · Oct 11, 2008 · N221FE · Boeing 727233 · Landing Gear Doors
  > LEFT AND RIGHT WHEEL WELL MLG DOOR RELEASE HANDLES ARE GOUGED. REWORKED GOUGED AREAS ON LH AND RH WHEEL WELL MLG DOOR REALEASE HANDLES IAW B727 SRM 51-10-1, PERFORMED DYE PENETRANT INSPECTION IAW SOPM 20-20-02 NO DEFECTS NOTED TREATED AND PRIMED AREAS. ALL

Next page: https://openairdocs.org/deregistered/N221FE-2015-08-10/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 = 'N221FE' AND deregistration_id = 'N221FE-2015-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N221FE-2015-08-10/reports

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