N221FE, cancelled Aug 10, 2015

Service difficulty reports · 127

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201304090747Battery Pack · failedON 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.Apr 9, 2013 · N221FE · Boeing 727233 · Emergency LightingSDR FDEA201303010484Wire · failedREPEAT 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.Mar 1, 2013 · N221FE · Boeing 727233 · Auto Flight System WiringSDR FDEA201302280478Actuator · inoperativeACFT 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 22-11-14Feb 28, 2013 · N221FE · Boeing 727233 · Auto Flight SystemSDR FDEA201302090315Damper · malfunctionedUNCOMMANDED 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 PASSFeb 9, 2013 · N221FE · Boeing 727233 · Rudder Control SystemSDR FDEA201301120089Unknown · malfunctionedUNCOMMANDED 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, TRANDUCEJan 12, 2013 · N221FE · Boeing 727233 · Rudder Control SystemSDR FDEA201206282384Switch · malfunctionedEQUIPMENT 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.Jun 28, 2012 · N221FE · Boeing 727233 · Door Warning SystemSDR FDEA201109284195Trim System · malfunctionedMAIN 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 27-40-000-5Sep 28, 2011 · N221FE · Boeing 727233 · Stabilizer Control SystemSDR FDEA201108203391Actuator · failedNR 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.Aug 20, 2011 · N221FE · Boeing 727233 · Leading Edge Slat ActuatorSDR FDEA201107313043Connector · dirtyON 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 Jul 31, 2011 · N221FE · Boeing 727233 · Leading Edge Slat ActuatorSDR FDEA201105251983Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 620 STR 15 - 16L ACCOMPLISHED REPAIR AT MCD INNER SURROUND SKIN IAW EA 7-5310-123597.May 25, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201105241973Skin · damagedINNER SKIN STA 540 STR 3L DOUBLE DRILLED HOLES. ACCOMPLISHED REPAIR AT BS 540 STR 3L INNER SKIN IAW EA 7-5310-123595.May 24, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201105241972Support Fitting · damagedMAIN 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.May 24, 2011 · N221FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201105241971Frame · damagedMAIN CARGO DOOR CUT-OUT BS 620 FRAME WEB HAS DOUBLE DRILLED FASTENERS REMOVED AND REPLACED BS 620 FRAME WEB IAW EA 7-5310-123595.May 24, 2011 · N221FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201105191922Frame · damagedAFTER 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 TRMay 19, 2011 · N221FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201105191921Frame · damagedDOUBLE DRILLED HOLES FOUND UPON REMOVAL OF INNER SKIN GOING THROUGH SHIM AND FRAME STA 620, STR 9L AT 2 EACH LOCATIONS.May 19, 2011 · N221FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201105161871Web · damagedBS 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.May 16, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201105111799Skin · damagedSKIN STA. 590 STR 3L HAS DOUBLE DRILLED HOLES. ACCOMPLISHED REPAIR AT BS 590 STR 3L IAW EA 7-5310-123595.May 11, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201105081795Frame · damagedBS 620 FRAME DOUBLER HAS FASTENER HOLES WITH NO ED. REMOVED AND REPLACED BS620 FRAME DOUBLER IAW EA 7-5310-123595.May 8, 2011 · N221FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201105081794Frame · damagedAFTER 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.May 8, 2011 · N221FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201105061764Floorbeam · damagedDOUBLE 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 BSMay 6, 2011 · N221FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201105061762Door Frame · corrodedUPON 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 ANDMay 6, 2011 · N221FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201105061763Rib · chafedNR 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 May 6, 2011 · N221FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201105051761Skin · crackedC-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 SRMMay 5, 2011 · N221FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA201105021750Floorbeam · damagedDOUBLE 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, 51May 2, 2011 · N221FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201104301695Skin · damagedUPON 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.Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201104301694Skin · damagedBS 520 STR, 3L FOUND MISDRILLED HOLES IN THE OEM SKIN. ACCOMPLISHED REPAIR AT BS 520 STR 3L INNER SKIN IAW EA 7-5310-123595.Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201104301693Skin · damagedUPON 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.Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201104301692Skin · damagedBS 560 STR 3L FOUND MISDRILLED HOLES IN THE EOM SKIN. ACCOMPLISHED REPAIR AT BS 560 STR 3L INNER SKIN IAW EA 7-5310-1235.Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201104301691Skin · damagedUPON 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.Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201104301690Skin · damagedBS 610 - 600 STR 3L FOUND MISDRILLED HOLES IN THE OEM SKIN. ACCOMPLISHED REPAIR AT BS 610 - 600 STR 3L IAW EA 7-5130-123595.Apr 30, 2011 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201104291670Attach Angle · crackedATTACH 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.Apr 29, 2011 · N221FE · Boeing 727233 · Fuselage, Landing Gear Attach FittingsSDR FDEA201104271679Seat Track · corrodedAFT 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 TRAApr 27, 2011 · N221FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201104261647Rib · crackedNR 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 HEApr 26, 2011 · N221FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201104201536Window Frame · corrodedCORROSION 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.Apr 20, 2011 · N221FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201104191520Sill · damagedINBD 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.Apr 19, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201104191519Sill · damagedMCD 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.Apr 19, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201104181515Stringer · crackedCRACK 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.Apr 18, 2011 · N221FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201104151805Skin · damagedREMOVED 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.Apr 15, 2011 · N221FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA201104151491Skin · damagedLT 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, Apr 15, 2011 · N221FE · Boeing 727233 · Elevator, Plate/SkinSDR FDEA201104131466Web · crackedAFT 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.Apr 13, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201104131465Web · crackedAFT 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 SRMApr 13, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201104131463Stringer · corrodedFWD 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 SRApr 13, 2011 · N221FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201104121461Sill · damagedMCD 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.Apr 12, 2011 · N221FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201104081462Bulkhead · misinstalledLOCK 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.Apr 8, 2011 · N221FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA200909223367Switch · inoperativeON 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/ISep 22, 2009 · N221FE · Boeing 727233 · Leading Edge Slat Control SystemSDR 08FDEA04554Skin · misrepairedREPAIR 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 DOOct 26, 2008 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA04380Skin · damagedCABIN 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 53Oct 16, 2008 · N221FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA04340Structure · crackedCRACK 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.Oct 14, 2008 · N221FE · Boeing 727233 · Trailing Edge FlapsSDR 08FDEA04309Stringer · corrodedCORROSION 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 SUOct 11, 2008 · N221FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 08FDEA04308Lever · gougedLEFT 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. ALLOct 11, 2008 · N221FE · Boeing 727233 · Landing Gear Doors
Back to N221FE, cancelled Aug 10, 2015