N608FE

Service difficulty reports · 370

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 = 'N608FE' 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 FDEA201702020319Hinge · corrodedLEFT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. TWO SHOULDER BUSHINGS AND REPAIR SHIMS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP Feb 2, 2017 · N608FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201702020318Hinge Bracket · corrodedLEFT WING INBD FLAP OUTBOARD AFT HINGE (FLAP SIDE) PIVOT INBD HOLE BORE FOUND WITH CORROSION. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-132705 C, PART 4, STEP 2A & 2C. CLASSIFIEFeb 2, 2017 · N608FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201702020317Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OUTBD HOLE BORE FOUND WITH CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW CMM 57-52-03. OVERSIZE BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-132705 C, PART 4, STEP 2A & 2C. REPAIR CLASSFeb 2, 2017 · N608FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201702020316Frame · chafedMAIN DECK CARGO BAY FRAME CHAFED AT LT BS 535, LONGERON 19L. REPAIRED IAW SRM 53-20-07-2R, FIG 202, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Feb 2, 2017 · N608FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201701270266Seat Track · corrodedMAIN DECK CARGO SEAT TRACK FLANGE CORRODED AT BS 5-73 - 5-113, LBL 107.25. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 27, 2017 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201701270265Seat Track · corrodedMAIN DECK CARGO SEAT TRACK FLANGE CORRODED AT BS 1540 - 1561, LBL 75.25. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 27, 2017 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201701270264Seat Track · corrodedMAIN DECK CARGO BAY SEAT TRACK CORRODED AT BS 1540 - 1561, LBL 107.25. REPAIRED IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 27, 2017 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201701270260Skin · crackedLEFT WING FIXED LEADING EDGE SLAT AT CORNER FOUND CRACKED XOS 490. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 17. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 27, 2017 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701270267Seat Track · corrodedMAIN DECK CARGO SEAT TRACK FLANGE CORRODED AT BS 5-73 - 5-113, LBL 75.25. REPAIRED IAW SRM 53-00-52-2R FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 27, 2017 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201701270268Skin · crackedHFEC INSPECTION ON RT WING FIXED LEADING EDGE CORNER NR 5 SLAT ACTUATOR ACCESS DOOR. FOUND CRACKED AT XOS 490. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 17. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 27, 2017 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701260258Doubler · crackedRT WING LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 669. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 26, 2017 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701260257Doubler · crackedRT WING LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 696. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 26, 2017 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701260256Doubler · crackedRT WING LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 655. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. MAJOR REPAIR IAW GMM 6-2-100.Jan 26, 2017 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701260255Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 626. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.Jan 26, 2017 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201701260252Longeron Splice · crackedCENTER CARGO LONGERON SPLICE FITTING CRACKED AT BS 5-113 TO 1541, LONGERON 33R. REMOVED AND INSTALLED WITH NEW FABRICATED SPLICE FITTING IAW SRM 51-33-01-0G. SPLICE FITTING FABRICATED AS PER DRAWING A5A7112 REVISION D. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-10Jan 26, 2017 · N608FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201612194494Brake Disc · failedNR 7 BRAKE INBD DISC DISINTERGRATING. REMOVED AND REPLACED THE BRAKE ASSY AND LEAK AND BLEED CHECKED OK IAW AMM 32-43-20-4-0.Dec 19, 2016 · N608FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA201612124394Controller · failedCAPT'S WINDSHIELD COMPLETELY COLD SOAKED AND APPEARS W/S HEAT INOP AND FOGGED OVER DURING DESCENT AND APPROACH. SEVERE FOGGING TO POINT OF CAPTS VISIBILITY SERIOUSLY REDUCED AND UNSAFE. REPLACED LT WINDSHIELD HEAT CONTROLLER PER AMM 30-41-01-4. OP CHK OK.Dec 12, 2016 · N608FE · Doug MD11 · Windshield/Door Rain/Ice RemovalSDR FDEA201612034319Wire · looseTHE TWO AGT LOW LIGHTS DOES NOT ILLUMINATE IN THE COCKPIT. PERFORMED ENGINE FIRE TEST IAW AMM 26-11-02-5.TEST OK.DISCONECTED THE CONNECTORS FOR THE CARTRIDGES IAW AMM 26-21-05-4. INSPECTED THE DISCHARGE CATRIDGES, STILL GOOD, INSPECTED THE DISCHAGE LINDec 3, 2016 · N608FE · Doug MD11F · Fire Protection System WiringSDR FDEA201612014301Engine · failedNR 1 ENGINE FAILURE AFTER TAKEOFF. MULTIPLE COMPRESSOR STALLS AND LOSS OF POWER. RETURNED TO DEPARTURE. NO INDICATIONS OF FIRE OR EXTERNAL DAMAGE. PERFORMED STALL INSPECTION IAW AMM 72-00-05-6-1, REMOVED MASTER CHIP DETECTOR MAGNETIC PROBE NO METAL PARTICDec 1, 2016 · N608FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201605111534Pump · faultedINFO NR 3 HYD RES TEMP WAS RUNNING 40 - 5 DEGREES HOTTER THAN HYD SYS 1 & 2. TEMP NORMAL AFTER LANDING HSC HAS FAULTED NR 3 LT HYD PUMP THE LAST FOUR LEGS CREW INFO NOTED IN EAML. SEE MTSI 29-10-3801 & 29-10-3802. MEL 29-11-01-A IS APPLIED TO THE NR 3 ENGMay 11, 2016 · N608FE · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR FDEA201605061492Connector · dirtyHYD SYSTEM NR 3 OFF. QTY 10.1 CONFIGURED HYD SYS 3 PRESSURIZED OK WITH NO LEAKS DETECTED. HOWVEVER RECEIVED RMP 2-3 DISAGREE ALERT. HYD 3 QUANTITY WAS AT PROPER SERVICE OF 7.5 WHEN ACFT BLOCKED IN. ON THE HYDRALUIC SYNOPTIC PAGE THE CYAN PREDEPARTURE May 6, 2016 · N608FE · Doug MD11F · Hydraulic Power System WiringSDR FDEA201512073941Control Panel · faultedFSS PANEL CONTINUOUSLY FAULTS, ARGON PRESSURE, THEN BLINKS BLANK & BACK TO NORMAL EVERY 5 SECONDS. THEN STOPS FOR A FEW MINUTES & FAULTS AGAIN. SERVICED TO 2900 PSI IAW MM 26-00-120. NO LEAKS NOTED IAW 26-00-111. COMPLIED WITH POST MX RTS IAW 26-00-450. Dec 7, 2015 · N608FE · Doug MD11F · Extinguishing SystemSDR FDEA201506302127Line · leakingLEVEL 1, HYD 1 OFF, ALERT DISPLAYED 2.9 GALLONS HYD FLUID REMAINING. AFTER LANDING, HYD 1 FAIL, ALERT DISPLAYED 0.5 GALLONS REMAINING. FOUND NR 1 HYD SYS LEAKING FROM LT SLAT ACTUATOR. REPAIRED THE PIPE IAW AMM 20-10-01-2. SERVICED HYD SYS 1 IAW AMM 12-13Jun 30, 2015 · N608FE · Doug MD11F · Hydraulic System, MainSDR FDEA201503201037Indicator · inoperativeCREW REPORTED L1 DOOR REMOTE PRESS INDICATOR LIGHT INOPERATIVE. R & R REMOTE PRESS INDICATOR ASSEMBLY. PERFORMED OPERATIONAL TEST OF THE REMOTE PRESS INDICATOR, NO ABNORMALITY FOUND IAW AMM 25-61-04-4 & 25-61-04-5. ACFT OK FOR SERVICE.Mar 20, 2015 · N608FE · Doug MD11F · Emergency EquipmentSDR FDEA201503191009Battery · dischargedWALK AROUND CHECK, FOUND L1 DOOR REMOTE PRESS INDICATOR LIGHT INOPERATIVE AMM 25-61-15-5. R & R BOTH BATTERIES & OPERATION CHECKED NORMAL IAW AMM 25-61-15-5.Mar 19, 2015 · N608FE · Doug MD11F · Emergency EquipmentSDR FDEA201503190991Light · inoperativeWALK AROUND CHECK, FOUND L1 DOOR REMOTE PRESS INDICATOR LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-02 CATEGORY C EXPIRATION 29 MAR 15. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQUATE ONCE EACH FLIGHT DAY.Mar 19, 2015 · N608FE · Doug MD11F · Emergency EquipmentSDR FDEA201503050679Web · crackedAFT CARGO WEB PANEL CRACKED AT BS 1841, X= 52. REMOVED IAW SRM 51-31-01-0G AND A NEW WEB FABRICATED IAW DRAWING AGA7170 REVISION R. INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Mar 5, 2015 · N608FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201503040645Slat · wornDUE TO SLAT REMOVED FOR WORK ACCESS, RT HAND WING NR 7 SLAT OTBD RIB FWD HOLE BORE FOUND WORN. RT HAND WING NR 7 SLAT OUTBOARD RIB FORWARD HOLE SPOTFACE REWORKED AND FOUND WITHIN LIMIT AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 10 AND EA 1-5750-T0316077 PART 1Mar 4, 2015 · N608FE · Doug MD11F · Leading Edge DevicesSDR FDEA201503040644Slat · wornDUE TO SLAT REMOVED FOR WORK ACCESS. RT WING NR 7 SLAT OTBD RIB FWD HOLE SPOT FACE FOUND WORN. BUSHING AT RIGHT HAND WING NR 7 SLAT OUTBOARD RIB FORWARD HOLE BORE REMOVED AS PER MD11 CMM 20-10-7 HOLE MEASURED DIA.: 0.875 INCH, AND FOUND WITHIN LIMIT AS PER Mar 4, 2015 · N608FE · Doug MD11F · Leading Edge DevicesSDR FDEA201503040649Skin · crackedRIGHT WING FIXED LE SKIN NR 15 SLAT TRACK INBD CUT OUT SUSPECT CRACK AT XOS 944.556. REPAIRED IAW SRM 57-40-02-2R FIGURE 201 REPAIR 7 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Mar 4, 2015 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201503020628Rib · damagedRIGHT WING NR 8 SLAT INBD RIB FOUND AFT HOLE WORN ON SIDE OF RIB AT HOLE STATION XOS 1005.124. REMOVED AND REPLACED WITH NEW RIB AS PER SRM 51-31-01-0G AND DRAWING NRB6737 REVISION N REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Mar 2, 2015 · N608FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201503010620Skin · damagedEXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT CENTER CARGO CUTOUT AFT SIDE STA 1781 BETWEEN LONGERON 40R - LONGERON 41R EXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT CENTER CARGO CUTOUT AFT SIDE STA 1781 BETWEEN LONGERON 40R - LONGERON 41R EVALUATED AND FOUNDMar 1, 2015 · N608FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201503010619Skin · damagedEXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT FORWARD CARGO CUTOUT AFT SIDE STA 1002.3 BETWEEN LONGERON 40R - LONGERON 41R EXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT FORWARD CARGO CUTOUT AFT SIDE STA 1002.3 BETWEEN LONGERON 40R - LONGERON 41R EVALUATED ANDMar 1, 2015 · N608FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201503010618Skin · damagedEXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT FORWARD CARGO CUTOUT FORWARD SIDE STA 895.7 BETWEEN LONGERON 40R - LONGERON 41R EXISTING DOUBLER REPAIR ON FUSELAGE SKIN AT FORWARD CARGO CUTOUT FORWARD SIDE STA 895.7 BETWEEN LONGERON 40R - LONGERON 41R EVALUATMar 1, 2015 · N608FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201503010624Former · crackedRT WING LEADING EDGE CAVITY FORMER FOUND CRACKED AT STA XOS 584. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2931 REVISION H INSTALLED NEW FORMER AT RT WING LEADING EDGE AT STA XOS 584 AS PER SRM 51-33-01-0G REPAIMar 1, 2015 · N608FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201502270605Beam · crackedCABIN MAIN DECK CARGO COMPARTMENT L3 DOOR PLUG NR 5 DOOR BEAM FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01-0G REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Feb 27, 2015 · N608FE · Doug MD11F · Service DoorsSDR FDEA201502270606Doubler · crackedRIGHT WING LE BEADED DOUBLER AT STATION XOS 636 - 643 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 27, 2015 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201502260601Skin · crackedLEFT WING, LE LOWER ACCESS PANEL 519CB INBD EDGE CUT OUT CORNER. FOUND CRACK AT STATION XOS 611. REPAIR CARRIED OUT PER SRM 57-40-01-2R FIGURE 201 REPAIR 18. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 INITIAL INSPECTION TO BE CARRIED OUT AT NEXT 'C' CHECFeb 26, 2015 · N608FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201401030017Fan · failedDURING COCKPIT SETUP SMELLED STRONG SMOKE & ELEC HOT SMELL. CALLED FIRE DEPT & MX. LAVATORY VENT FAN ON CONVENIENCE PANEL ASSEMBLY FAILED. REMOVED CONVENIENCE PANEL ASSEMBLY TO FACILITATE FAN MOTOR REPLACEMENT. ROUTED CONVENIENCE PANEL TO AVIONICS FOR REPAJan 3, 2014 · N608FE · Doug MD11F · LavatoriesSDR FDEA201306121266Control Panel · failedDURING TRANSIT CHECK, FOUND RT EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM NOT TESTING. R & R PRESSURE ASSY OPS CHECKED NORMAL IAW MM 25-61-04-4.Jun 12, 2013 · N608FE · Doug MD11F · Escape SlideSDR FDEA201305030905Indicator · inoperativeLEFT SLIDE SYS PRESS-TO-TEST INDICATING SYS INOPERATIVE. R & R L1 SLIDE REMOTE PRESSURE INDICATOR IAW MM 25-61-04-4. OPS CHECK NORMAL IAW MM 25-61-04-5.May 3, 2013 · N608FE · Doug MD11F · Escape SlideSDR FDEA201304290881Floor Support · crackedFLOOR SUPPORT CRACKED AT BS 2000-2007 X=20. R & R WITH NEW FLOOR SUPPORT IAW AMM 20-50-02 REV 75.2 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 116.Apr 29, 2013 · N608FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201304230832Door Frame · corrodedCARGO DOOR CUTOUT LOWER FRAME UPPER SURFACE BS 660 FOUND CORRODED. REMOVED AND REPLACED IAW SRM 51-31-01 REVISION 52 AND DRAWING ACA7224 REVISION G. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Apr 23, 2013 · N608FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201304220825Seat Track · corrodedBS 5-49 X= -8.5 SEAT TRACK LOBE FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 5 SHEET 2 OF 3 REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.Apr 22, 2013 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201304200821Seat Track · corrodedBS 1219 -1259 X= -75.25. SEAT TRACK FOUND CORRODED. REPAIRED IAW 53-00-52 FIGURE 201 REPAIR 1REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116Apr 20, 2013 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201304200819Seat Track · corrodedBS 5-65 X= 8.5 SEAT TRACK FOUND CORRODED. REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 52 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116Apr 20, 2013 · N608FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201304200818Bulkhead Web · crackedCENTER CARGO AFT BULKHEAD PANEL FOUND CRACKED AT BS 1841 X= - 52. BULKHEAD WEB REMOVED AND REPLACED WITH NEW FABRICATED WEB AS PER SRM 51-31-01 REVISION 52 NEW WEB FABRICATED AS PER DRAWING AGA7170 REVISION T. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-10Apr 20, 2013 · N608FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201304200817Bulkhead Web · crackedCENTER CARGO AFT BULKHEAD PANEL CRACKED AT BS 1841 X= -20. BULKHEAD WEB REMOVED AND REPLACED WITH NEW FABRICATED WEB AS PER SRM 51-31-01 REVISION 52 NEW WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REVISION T. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVIApr 20, 2013 · N608FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201304200820Frame · dentedBS 1721 L12L FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52, REPETITIVE INSPECTION REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE INSP AT 9,500 CYCLES TO BE CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIApr 20, 2013 · N608FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201304180805Structure · corrodedLT WING T/E LOWER CAP AT 541JB CUT OUT ACCESS FOUND SURFACE CORROSION AT XW326. REMOVED AND REPLACED WITH NEW CAP AS PER SRM 51-33-01 REVISION 52. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.Apr 18, 2013 · N608FE · Doug MD11F · Wing Main, Frame Structure
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