N529FE

Service difficulty reports · 240

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 = 'N529FE' AND registry_match = 'registration'
  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 FDEA201508072497Hinge Bracket · corrodedLEFT WING, WING SIDE, OTBD FLAP INBD HINGE, SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE, FOUND CORRODED. REPAIRED IAW CMM 57-44-08. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072496Hinge · corrodedLEFT WING, WING SIDE, OTBD FLAP INBD HINGE, OTBD ACTUATOR HOLE BORE, FOUND CORROSIONS. CORROSION AT HOLE 8, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 1.219", FINAL HOLE DIAMETER =1.252", MAXIMUM ALLOWABLE HOLE DIAMETER =1.220".Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072495Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE INBD ACTUATOR HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 1.215", FINAL HOLE DIAMETER =1.254", MAXIMUM ALLOWABLE HOLE DIAMETER =1.220". REPAIRED BAug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072494Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER =2.309", FINAL HOLE DIAMETER =2.336", MAXIMUM ALLOWABLE HOLE DIAMETER =2.3135". REPAIRED BUSHING, Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072493Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 0.643", FINAL HOLE DIAMETER =0.721", MAXIMUM ALLOWABLE HOLE DIAMETER =0.709". REPAIREAug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072492Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE LOWER MOUNT INBD HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 0.703", FINAL HOLE DIAMETER =0.723", MAXIMUM ALLOWABLE HOLE DIAMETER =0.709". REPAIREDAug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508052482Mount · corrodedLEFT WING, WING SIDE OTBD FLAP HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER =0.591", FINAL HOLE DIAMETER =0.599", MAXIMUM ALLOWABLE HOLE DIAMETER =0.584". AIR BUSHING FAug 5, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508052481Fitting · corrodedLEFT WING, WING SIDE, OTBD FLAP HINGE SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE FOUND CORRODED. FOUND WITHIN LIMITS. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.Aug 5, 2015 · N529FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201508052479Doubler · crackedLEFT WING LE AT APPROX STATION XOS 425, FOUND INTERIOR BEADED DOUBLER CRACKED. LEFT WING LE REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 5, 2015 · N529FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201508052478Frame · damagedMAIN DECK RT FRAME AT STATION 535, LONGERON 24R FOUND DAMAGED. MAIN DECK DAMAGE REPAIRED IAW SRM 53-20-07-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 5, 2015 · N529FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201508052477Frame · damagedMAIN DECK RT FRAME AT STATION 535, LONGERON 19R FOUND DAMAGED. MAIN DECK DAMAGE REPAIRED IAW SRM 53-20-07-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 5, 2015 · N529FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201508052476Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT BS 750, X= -8, FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 5, 2015 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201508052475Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT BS 5 - 5, X= 8, FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 5, 2015 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201508052474Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT BS 1406, X= 8 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 5, 2015 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201508052473Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT BS 1199, X= -27.5 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 5, 2015 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201508052472Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT BS 1199, LBL 8 FOUND CORRODED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 5, 2015 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201507222299Gcu · malfunctionedAFTER TAKEOFF AS GEAR WAS RETRACTING CAPTAIN`S 1, 2 & 3 DU'S WENT DARK. MULTIPLE LEVEL 1 & 2 ALERTS, SOME WERE TRANSITORY. THOSE WE WORKED WERE GEN 1 OFF, AC BUS TIE 1, EMER POWER & BATTERY DISCHARGE. CLEANED UP CAC IAW MM 05-50-02. INSPECTED & FOUND NR 1 Jul 22, 2015 · N529FE · Doug MD11F · AC RegulatorSDR FDEA201505151520Proximity Sensor · failedAFTER TAKEOFF & GEAR RETRACTION, HAD NOSE GEAR UNSAFE LIGHT ON PRIMARY. NOTED VERY UNUSUAL AIR NOISE FROM BELOW FUSELAGE, NOSE GEAR AREA. CHECK OF CONFIG PAGE SHOWED NOSE GEAR WAS UP. RED TABS REVIEWED FOR UNSAFE INDICATIONS. MOCC CONSULTED & DUE TO LOUDEMay 15, 2015 · N529FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA201504011137Indicator · inoperativeON LAYOVER, CHECK EVACUATION SLIDE REMOTE PRESSURE, PRESS TO TEST, INDICATING SYS INOPERATIVE. PRESS TO TEST SWITCH INOPERATIVE. FOUND INCORRECT LAMPS INSTALLED IN INDICATOR ASSEMBLY. INSTALLED CORRECT LAMPS AND OPERATIONAL CHECK GOOD.Apr 1, 2015 · N529FE · Doug MD11F · Escape SlideSDR FDEA201409232714Wire · brokenL1 DOOR EVAC SLIDE WILL NOT TEST. RELEASED FOR SERVICE IAW MEL 25-61-02. L1 EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-02. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQUATE ONCE EACH FLIGHT DAY. RESECURED BROKEN WIRE AT BATTERY TESep 23, 2014 · N529FE · Doug MD11F · Equipment/Furnishings WiringSDR FDEA201406111407Fmu · inoperativeREJECTED TAKEOFF FOR AN ENGINE FAIL LIGHT. NR 3 ENGINE WOULD NOT FULLY SPOOL UP. PERFORMED GVI FOR BOTH ENGINE INTAKE & EXHAUST AREA, FOUND NO DEFECTS. NO FAULTS STORED ON ALL EEC. PERFORMED FADEC INTERFACE TEST ON BOTH FCC-1 & FCC-2. ALL TEST PASSED IAW Jun 11, 2014 · N529FE · Doug MD11F · Power Indicating SystemSDR FDEA201405120985Engine · malfunctionedNR 3 ENG WOULD NOT ADVANCE TO MAX POWER, EPR OF 1.61, AUTO THROTTLES ADVANCED ENGINES 1 & 2 TO 1.61 EPR, NR 3 STOPPED AT 5% - 6% BELOW 1 & 2. THROTTLE NR 3 STOPPED 1/2 KNOB BEHIND NR 1 & 2. MANUALLY ADVANCED NR 3 THROTTLE UP, EPR & N1 SETTINGS WOULD NOT ADMay 12, 2014 · N529FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201403130501Battery Pack · misinstalledL1 SLIDE INDICATOR LIGHT INOPERATIVE. FOUND BATTERIES INSTALLED INCORRECTLY, REPOSITIONED BATTERIES & OPS CHECKED GOOD.Mar 13, 2014 · N529FE · Doug MD11F · Emergency EquipmentSDR FDEA201402270417Contact · dirtyL1 DOOR EVACUATION SLIDE REMOTE PRESSURE, PRESS TO TEST LIGHT INOPERATIVE. FOUND LAMP CONTACTS DIRTY, CLEANED IAW SMP. OPS TESTED GOOD. ACFT OK FOR SERVICE.Feb 27, 2014 · N529FE · Doug MD11F · Equipment/Furnishings WiringSDR FDEA201402040259Pressure Switch · failedWITH ANTI-ICE ON, RECEIVED WING ANTI-ICE LT DISAGREE. LT ANTI-ICE VLV SHOWED DISAGREE ON SYNOPTIC & BLEED PRESS ON SYS 1 WENT TO ZERO. SECURED ANTI-ICE IAW QRH & BLEED PRESS RETURNED TO NORMAL. DIVERTED AND LANDED MSP WITHOUT INCIDENT. REMOVED AND REPLACFeb 4, 2014 · N529FE · Doug MD11F · Airfoil Anti/De-ice SystemSDR FDEA201401300223Wire · pulledEMERGENCY EXIT LIGHT OVER L1 DOOR INOPERATIVE WITH EMERGENCY LIGHT SWITCH AT ON POSITION. FOUND POWER WIRE TO LIGHT ASSY. PULLED OUT OF SPLICE, RESPLICED WIRE PER MM 20-30-03-2, LIGHT OPS CHECKED GOOD.Jan 30, 2014 · N529FE · Doug MD11F · Light System WiringSDR FDEA201312112956Deu · failedMASTER CAUTION & MASTER WARNING, WITH ASSOCIATED AUDIBLE WARNING, CONTINUOUSLY WENT ON FOR ENTIRE FLIGHT TILL APPROXIMATELY 2000' ON FINAL. DEU 1 FAILED ON CLIMB OUT. REPLACED NR 1 DEU IAW MD11 AMM 34-61-02-4, CHECKED GOOD.Dec 11, 2013 · N529FE · Doug MD11F · Flight Management Computing Hardware SystemSDR FDEA201312032909Handle · brokenDOOR L1 EMERGENCY HANDLE BROKEN ON AFT BRACKET FOUND L1 DOOR EMERGENCY HANDLE, MANUAL LIFT BAR UNCLIPPED. CLIPPED & STOWED HANDLE. ACFT OK FOR CONTINUED SERVICE.Dec 3, 2013 · N529FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201310262619Structure · corrodedBS 1321, XCW= 106 CENTER WING FUEL TANK SURFACE FOUND WITH CORRODED. REPAIRED IAW EA 1-5730-T0303574 PART 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 118.Oct 26, 2013 · N529FE · Doug MD11F · Fuel StorageSDR FDEA201310262618Structure · corrodedBS 1301, XCW= 107, CENTER WING FUEL TANK FOUND CORRODED. REPAIRED IAW EA 1-5730-T0303436 PART 1, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 118.Oct 26, 2013 · N529FE · Doug MD11F · Fuel StorageSDR FDEA201310242602Support Fitting · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON MAIN DECK CARGO DOOR FUSELAGE LOWER FRAME SUPPORT FITTING, NR 6 HOLE B AND D FOUND WITH CRACK INDICATION AND HOLE DIAMETER REACHED 0.560". SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01 ROct 24, 2013 · N529FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201310242601Support Fitting · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON MAIN DECK CARGO DOOR FUSELAGE LOWER FRAME SUPPORT FITTING, NR 1 HOLE NR A, B AND C FOUND CRACKED AND HOLE DIAMETER REACHED 0.560". SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01 REVISION Oct 24, 2013 · N529FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201310242600Support Fitting · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON MAIN DECK CARGO DOOR LOWER FRAME SUPPORT FITTING, NR 7 HOLE A AND B FOUND CRACKED AND HOLE DIAMETER REACHED 0.560". SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 53. REPAIR CLASSIFIED AS Oct 24, 2013 · N529FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201310182545Door Frame · crackedBS 1259, LONGERON 26R, R3 DOOR FORWARD FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Oct 18, 2013 · N529FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201310182544Seat Track · crackedMAIN DECK BS 635 RBL 8.5 SEAT TRACK FOUND CRACKED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Oct 18, 2013 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201310172525Doubler · crackedLEFT WING FIXED L/E BEAD DOUBLER AT LWS 666 FOUND CRACKED. REPAIRED IAW SRM 57-40-02, REPAIR 15 FIGURE 203 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Oct 17, 2013 · N529FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201310172524Strap · crackedRIGHT WING OTBD FLAP, INBD HINGE TENSION STRAP AT WS 486.603, FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-33-01 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.Oct 17, 2013 · N529FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201310142504Skin · chafedFORWARD CARGO DOOR CUT OUT AFT SIDE FOUND EXISTING BLEND OUT AT BS 1009, LONGERON 40 - 41R. REPAIRED IAW SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 53. EA 1-5330-T0303487 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.Oct 14, 2013 · N529FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201310142503Skin · chafedFORWARD CARGO DOOR CUT OUT FORWARD SIDE FOUND EXISTING BLEND OUT AT BS 888, LONGERON 40 - 41 RT. REPAIRED IAW SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 53. EA 1-5330-T0303487 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.Oct 14, 2013 · N529FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201310142497Seat Track · corrodedBS 1014, LBL 8.5, SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 969 TO 1029 IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.Oct 14, 2013 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201307191584Pump · failedHYD 1 OFF ALERT, TWO HOURS INTO FLT AT F360, SYS PRESSURE 40 PSI (AFTER ISOLATED), 39 DEGREES AND 8.6 GAL AT RESERVOIR, 30 MINUTES LATER QTY 0.3, HYD 1 FAIL ALERT. PUMPS SHUTOFF TWO HRS INTO FLT AND DIDN'T COME BACK ON. R & R NR 1 ENG DRIVEN HYD PUMP ASSY IJul 19, 2013 · N529FE · Doug MD11F · Hydraulic System, MainSDR FDEA201304020709Warning System · false indicationTIP TANK FUEL TRAPPED LT WING. PERFORMED TESTS IN REF TO FIM 28-14-16-00, ALL TESTS PASS. FQBU TEST RESULTED IN NO FAULTS, AND ALL FLOAT SWITCH TESTS PASS. ACFT OK FOR SERVICE.Apr 2, 2013 · N529FE · Doug MD11F · Fuel Indicating SystemSDR FDEA201209053606Control Unit · malfunctionedBATTERY DISCHARGING LEVEL 1, ALERT. INTERMITTENT AT FIRST, THEN CONTINUOUS. BATTERY VOLTAGE SHOWED 30V-34V. R & R EPCU REF AMM24-08-01-4, OPS CHECKED NORMAL. ALL TROUBLESHOOTING PERFORMED IAW FIM 24-30-03-00. NO FAULTS NOTED, SYSTEM OPS CHECKS NORMAL.Sep 5, 2012 · N529FE · Doug MD11F · Battery/Charger SystemSDR FDEA201209023206Battery · unknownBATTERY DISCHARGE ILLUMINATED SEVERAL TIMES STAYED ON FOR APPROX 2 MIN LAST DURATION THEN EXTINGUISHED. EPCU FAULT REVIEW SHOWED "COOLING VALVE 3/ INTFC", BATTERY CHARGER FAULT DISPLAY SHOWED "CHARGER FAIL, BATT FAIL, BUSS OK". TROUBLE SHOT IAW MM 24-30-0Sep 2, 2012 · N529FE · Doug MD11F · Battery/Charger SystemSDR FDEA201207262721Relay · inoperativeAPPROX 6.5 HRS INTO FLIGHT BATTERY DISCHARGING ALERT ILLUMINATED IAW QRH, DIVERTION INITIATED, AFTER 5-7 MINUTES THE ALERT WENT OUT. ELECTED TO PROCEED TO DESTINATION. VOLTAGE WAS CONSTANT 33 VOLTS DURING AND AFTER THE ALERT. ILLUMINATED AGAIN ON SHORT FJul 26, 2012 · N529FE · Doug MD11F · Battery/Charger SystemSDR FDEA201112115242Indicator · inoperativeDOOR ESCAPE SLIDE LOW PRESSURE INDICATOR LIGHT WILL NOT PRESS TO TEST. R & R LENS, LAMP RETAINER AND BULBS, IAW AMM 25-61-04-4-0. OPS CHECKED NORMAL. RETURNED TO SERVICE.Dec 11, 2011 · N529FE · Doug MD11F · Escape SlideSDR FDEA201111265051Doubler · crackedLT WING BEADED DOUBLER FOUND CRACKED. REPAIRED IAW EA 1-5730-154256. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.Nov 26, 2011 · N529FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201111235013Fitting · looseAFTER REMOVAL OF FIREWALL ACCESS PANEL, VERTICAL STABILIZER BANJO FITTING AFT SIDE CENTER FASTENER FOUND SHEARED OFF. FASTENER R & R IAW SRM 51-31-01, REV 48 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.Nov 23, 2011 · N529FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA201111235004Skin · crackedLEFT WING L/E AT XOS 928 SKIN FOUND CRACKED UPON REMOVAL OF FORMER. REPAIRED IAW EA 1-5730-154256. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.Nov 23, 2011 · N529FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201111235012Fitting · looseVERTICAL STABILIZER LT SIDE BANJO FITTING AFT SIDE HAS A FASTENER LOOSE. FASTENER R & R IAW EA 1-5530-154251 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 23, 2011 · N529FE · Doug MD11F · Vertical Stabilizer, Attach Fittings
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