GE CF6-6D

Service difficulty reports · 1,051

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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 engine_model_key = 'CF66D'
  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 FDEA201012024537Lamp · inoperativeR1 DOOR PRESSURE, PRESS TO TEST INDICATOR INOP. FOUND P/N 387 HIGH VOLTAGE LAMPS IN DOOR SLIDE PUSH BUTTON SWT. INSTALED P/N 368 LAMPS PER IPC. GRD OPS CHECKS OK.Dec 2, 2010 · N68057 · Doug MD1010F · Emergency EquipmentSDR 2010F00248Structure · corroded(VGQY) RT HORIZ STABILIZER INTEGRAL LOWER CHORD AND STR NR1, STA XE 48.500 TO XE 67.333 FOUND WITH CORROSION.Dec 1, 2010 · N220AU · Doug DC1010 · Horizontal Stabilizer StructureSDR FDEA201011284502Transmitter · failedELT ON 121.5 FOLLOWED US, SUSPECT ACFT ELT IS ALERTING. FACT 28NOV10 19:44 MEM R R & R EMERGENCY LOCATOR TRANSMITTER IAW 23-25-00-4. OPS CHECK GOOD, OK FOR SERVICE. (CLOSED)Nov 28, 2010 · N68052 · Doug MD1010F · Emergency Locator BeaconSDR FDEA201011274498Landing Gear · malfunctionedDURING LANDING GEAR RETRACTION, THE LT MLG PRIMARY AND SECONDARY INDICATIONS, INDICATED UNSAFE. CHECK LIST WAS ACCOMPLISHED. GEAR WAS EXTENDED AND RETRACTED. ALL INDICATORS WERE SAFE. LANDED WITHOUT INCIDENT. INSPECTED GEAR UPLOCK SENSORS AND LUBED GEARNov 27, 2010 · N373FE · Doug MD1010F · Landing Gear Retraction/Extension SystemSDR FDEA201011274501Wire Harness · malfunctionedEMERGENCY EXIT SIGNS INOP. RELEASED FOR SERVICE IAW MEL: 33-50-02, WHEN SHAKING HARNESS BY L1 DOOR LIGHTS COME ON, BUT UNABLE TO FIND EXACT CAUSE AT THIS TIME. REPLACED L1 DOOR "EXIT" LIGHT ASSY. ACCOMPLISHED ADJ AND TEST IAW MM 33-50-00-5.Nov 27, 2010 · N556FE · Doug MD1010F · Light System WiringSDR FDEA201011244485Skin · corrodedSKIN SHOWS BULGING AT STA 1705, STR 50R. REMOVED CORROSION BY REPLACING SKIN SEC REF EA 8-5330-138730.Nov 24, 2010 · N363FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201011234470Seat Track · misrepaired(P2-38) EXISTING SEAT TRACK REPAIR IN THE MAIN CABIN AT STA 1411, X = 27 REQUIRES CONDITION CHECK. VISUALLY INSPECTED REPAIR AND FOUND NOT TO BE IAW FAA APPROVED DATA. REMOVED, FABBED AND REPLACED SPLICE IAW SRM 53-70-00, FIG 1, VOL I.Nov 23, 2010 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011234471Seat Track · misrepaired(P2-39) EXISTING SEAT TRACK REPAIR IN THE MAIN CABIN FROM STA 1371 TO STA 1411, X = 8.5 REQUIRES CONDITION CHECK. VISUALLY INSPECTED REPAIR AND FOUND NOT TO BE IAW FAA APPROVED DATA. R & R SEAT TRACK SPLICES AT STA 1371 AND 1411, X = 8.5 IAW SRM 53-70- 00,Nov 23, 2010 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011234472Seat Track · misrepaired(P2-45) EXISTING SEAT TRACK REPAIR IN THE MAIN CABIN FROM STA 1661 TO STA 1681, X = 47 REQUIRES CONDITION CHECK. VISUALLY INSPECTED REPAIR AND FOUND NOT TO BE IAW FAA APPROVED DATA. REMOVED, FABBED AND REPLACED SPLICE AT STA 1661 - 1681, X = 47 IAW SRM 53-Nov 23, 2010 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011234473Frame · misrepairedFWD PIT EXISTING "J " CHANNEL REPAIR AT STA 824 BETWEEN LONGERON 51L AND LONGERON 51R REQUIRES EVALUATION. VISUALLY INSPECTED REPAIR - FOUND NOT IN COMPLIANCE WITH APPROVED DATA. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR IAW SRM 53-30-00, FIG 5, VOL I. THNov 23, 2010 · N389FE · Doug MD1010F · Fuselage Main, FrameSDR FDEA201011234466Cable · bentSTARTED T/O ROLL NR 2 THROTTLE WAS SLOW TO ACHIEVE TAKEOFF POWER. AFTER ACHIEVING TAKEOFF POWER NR 2, N1 ROLLED BACK TO 10 O'CLOCK ON THE GAUGE AND ENGINE FAIL CAME ON AROUND 90 KTS. REMOVED AND REPLACED NR 2 ENGINE VSV FEEDBACK CABLE PER MM 75-31-01-2. REMNov 23, 2010 · N370FE · Doug MD1010F · Fuel Control/Turbine EnginesSDR FDEA201011214445Filter · contaminatedABOUT 10 MINS AFTER T/O, NR1 ENG OIL QTY DECREASED TO 0. PRESS AND TEMP REMAINED NORMAL FOR ABOUT 10 MINS. THEN PRESS DECREASED AND INCREASED OUT OF NORMAL RANGE. SHUT ENG DOWN BEFORE PRESS REACHED RED LINE AND OR TEMP HIT YELLOW LINE. FOUND TGB SCAV IN FNov 21, 2010 · N359FE · Doug MD1010F · Turbine Engine Oil SystemSDR FDEA201011204433Transmitter · failedOIL QUANTITY DROPPED TO ZERO AFTER TAKEOFF ON ENGINE 1, OIL PRESSURE STARTED FLUCTUATING -10-20 PSI AND OIL TEMP CLIMBED TO 130 (NR2 100, NR3 105. SHUTDOWN ENGINE AND RETURNED. DID NOT NOTICE OIL PRESSURE ON WINDMILLING ENGINE. DURING 20 MIN OF FLIGHT BANov 20, 2010 · N359FE · Doug MD1010F · Engine Oil Indicating SystemSDR FDEA201011204432Mec · failedON TAKEOFF, NR 2 ENGINE DID NOT REACH T/O, N1 WITH THROTTLE ALIGNED WITH NR1 AND NR3. THROTTLE WAS MOVED SLIGHTLY FWD MANUALLY, AND N1 ROLLED BACK. ENGINE FAIL LIGHT ILLUMINATED, TAKEOFF REJECTED AT 85KTS. INSTALLED FUEL PUMP/MEC IAW MM 73-20-01-2. PERFOMENov 20, 2010 · N370FE · Doug MD1010F · Fuel Controlling SystemSDR FDEA201011204434Skin · crackedLT WING REAR SPAR LOWER CAP AT XORS 345, HFEC OPEN HOLE INSP. FOUND 01EA FASTENER HOLE WITH CRACKED INDICATION. LEFT HAND WING REAR SPAR LOWER CAP AT XORS 345, 01 EACH FASTENER HOLE WITH CRACKED INDICATION REPAIRED AS PER E.A. 8-5710-143797 PART 1. REPAIR CNov 20, 2010 · N373FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201011174408Support · crackedLEFT OTBD FLAP INBD HINGE-FWD FITTING ATTACHED TO THE WING HAS A CRACK ON INBD SIDE. REMOVED CRACKED SUPPORT FITTINGS IAW SRM 51-33-01. WORKED HOLES TO FINAL SIZE .325 ON OTBD FLALP SUPPORT FITTINGS COMPLIED WITH EA 8-5710-125587 FOR MISLOCATED HOLE REPAIR. Nov 17, 2010 · N68050 · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201011124323Hinge Fitting · corrodedRT WING OTBD FLAP OTBD HINGE FITTING, LOCATION NR 3 FWD MOUNTING SURFACE CORRODED. ACCOMPLISHED REPAIR OF THE NR 3 MOUNT SURFACE OF THE OUTBD FLAP OUTBD HINGE FITTING IAW EA 8-5750-123566.Nov 12, 2010 · N389FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201011104302Skin · crackedLT WING ANTI ICE TELESCOPIC DUCT CUTOUT FOUND CRACKED. LT WING ANTI ICE TELESCOPIC DUCT CUTOUT CARRIED OUT REPAIR IAW EA NR 8-5710-143470, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Nov 10, 2010 · N373FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201011104303Skin · crackedRT WING ANTI ICE TELESCOPIC DUCT CUTOUT FOUND CRACKED. RT WING ANTI ICE TELESCOPIC DUCT CUTOUT CARRIED OUT REPAIR IAW NR 8-5710-143471, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Nov 10, 2010 · N373FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201011064267Switch · failedPRIOR TO DESCENT FROM CRUISE, 3 LEVEL 1 ALERTS APPEARED. TANK 3 TIP TRAPPED, TANK 3 PUMP OFF, TANK 3 TRANSFER PUMP OFF. SEVERAL MINUTES AFTER INITIAL DESCENT BEGAN THE ALERTS WENT AWAY AND PUMPS BEGAN OPERATING . EMERGENCY WAS DECLARED. R & R 3 & 4K FLOANov 6, 2010 · N560FE · Doug MD1010F · Fuel Indicating SystemSDR FDEA201011054256Connector · damagedAIR MANF 3 FAIL WHEN WING ANTI ICE PLACED ON FOR DESCENT. MAX TEMP INDICATE 190 C. BLEED AUTO SHUTDOWN. ONLY MANIFOLD LIGHT ON, NO TEMP HI LIGHT. FOUND RT WING PRESSURE SWITCH TRIPPED. RESET PRESSURE SWITCH. ACCESSED PSC-3 CURRENT FAULT SHOWS PRSOV LOW FAULNov 5, 2010 · N384FE · Doug MD1010F · Ice/Rain Protection System WiringSDR FDEA201011044248Pseu · malfunctionedGEAR RETRACTION UNSAFE INDICATION ON RT MAIN GEAR, BOTH PRIMARY AND SECONDARY INDICATIONS SHOWED UNSAFE. COMPLIED WITH QRH -CYCLED GEAR STILL UNSAFE INDICATION ON RETRACTION. RETURNED TO DEPARTURE, DECLARED EMERGENCY, LANDING UNEVENTFUL. NO CURRENT FAULTS. Nov 4, 2010 · N384FE · Doug MD1010F · Landing Gear Position and WarningSDR FDEA201011044254Connector · failedAIR MANF 3 FAIL WHEN WING ANTI ICE PLACED ON FOR DESCENT. MAX TEMP INDICATE 190 C. BLEED AUTO SHUTDOWN. ONLY MANIFOLD LIGHT ON, NO TEMP HI LIGHT. FOUND RT WING PRESSURE SWITCH TRIPPED. RESET PRESSURE SWITCH. ACCESSED PSC-3 CURRENT FAULT SHOWS PRSOV LOW FAUNov 4, 2010 · N384FE · Doug MD1010F · Ice/Rain Protection System WiringSDR FDEA201011034235Skin · chafedLT WING SLAT NR 4 UPPER SURFACE FOUND CHAFED. REMOVED AND CLEANED AS PER SRM 57-00-01 FIGURE 1A, VOLUME I, REVISION 96. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.Nov 3, 2010 · N373FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201011024229Fitting · crackedLWR VERTICAL STABILIZER FOUND RT SIDE BANJO FITTING FWD CRACK. REPAIR CARRIED OUT AS PER SRM 55-30-02 REPAIR 3 REVISION 44 AND EA 1-5530-143476: REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Nov 2, 2010 · N618FE · Doug MD1010F · Vertical Stabilizer, Attach FittingsSDR FDEA201011024224Skin · delaminatedLT WING SPOILER NR 2 UPPER SURFACE FOUND DELAMINATION. LEFT HAND WING SPOILER NO.2 REMOVED AND REPLACED AS PER AMM 27-60-01 REVISION 10.1. OPERATIONAL CHECK CARRIED OUT AS PER AMM 27-60-00-2 REVISION 10.1 FOUND SATISFACTORY. CLEARANCE CHECK CARRIED OUT ASNov 2, 2010 · N373FE · Doug MD1010F · SpoilersSDR FDEA201011024225Skin · chafedLOWER CTR CARGO - AFT DOOR CUTOUT STA Y=1780 STR 40 TO 42R FOUND CHAFING. REPAIRED AS PER SRM 53-50-00 FIGURE 26, VOLUME I, REVISION 97. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.Nov 2, 2010 · N373FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201011024226Skin · chafedFWD CARGO DOOR - AFT DOOR CUTOUT STA Y=959 STR 40 TO 41R EXISTING REPAIR DOUBLER FOUND CHAFING. REPAIRED AS PER SRM 53-50-00 FIGURE 26, VOLUME I, REVISION 97. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.Nov 2, 2010 · N373FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201011024227Skin · crackedWHILE CARRYING OUT WALK AROUND CHECK FOUND RT WING FUEL DUMP ISLAND UPPER SURFACE OTBD AREA EDGE WITH CRACK APPROX .5". REPAIRED AS PER EA 8-5750-143479, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.Nov 2, 2010 · N373FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201011024228Skin · crackedLT WING FIXED L/E FWD INBD SIDE OF PRESSURE REFUEL PANEL CUTOUT FOUND REPAIR DOUBLER CRACKED. CARRIED OUT RECTIFICATION AS PER E.A. 8-5730-143796, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.Nov 2, 2010 · N373FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201010314199Battery · inoperativeDURING THE EMERGENCY LIGHT TEST RECEIVED EMERG BAT 1 LOW ALERT. R & R NR1 EMERGENCY LIGHT BATTERY REF33-51-01-4-0. OPS CHECKED GOOD ACFT OK TO CONTINUE.Oct 31, 2010 · N366FE · Doug MD1010F · Emergency LightingSDR FDEA201010284183Bungee Cylinder · damagedAFTER T/O, LT MAIN REMAINED UNSAFE FOLLOWED QRH CYCLED NO CHANGE. GEAR APPEARED TO BE DOWN ENTIRE TIME. UNEVENTFUL LANDING. REMOVED & REPLACED L/H MLG BUNGEE CYCLINDER ASSY ACFT OK FOR SERVICE.Oct 28, 2010 · N68054 · Doug MD1010F · Landing Gear Retraction/Extension SystemSDR FDEA201010214127Battery Pack · dischargedEMERGENCY LIGHT TEST BATTERY 1 LOW MESSAGE APPEARED. RELEASED FOR SERVICE IAW MEL: 33-50-01 CATEGORY: C EXPIRATION: 31OCT10 "MEL 33-50-01: EMERGENCY LIGHT TEST FUNCTION - INOP." PART(S) IDENTIFIED ARE THE MOST PROBABLE CAUSE. TROUBLESHOOTING IS REQUIRED PROct 21, 2010 · N559FE · Doug MD1010F · Emergency LightingSDR FDEA201010214164Skin · delaminatedRT WING NR5 SPOILER UPPER SURFACE OTBD FWD REPAIR AND FOUND IT DELAMINATED. REMOVED EXISTING REPAIR AND INSTALLED A METAL BOND REPAIR, SEALED ALODINED PRIMED AND PAINTED IAW SRM 57-10-00, VOL I AND SRM 51-71-00, VOL II.Oct 21, 2010 · N389FE · Doug MD1010F · SpoilersSDR FDEA201010214165Channel · corrodedCTR CARGO COMPARTMENT AT BS 1521, LBL 56, CHANNEL IS CORRODED. FABRICATED REPAIR ANGLES IAW SRM 53-00-01, FIG 9, VOL I. FABRICATED "J" CHANNEL IAW DAC DWG 2929469. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-21-01, VOL II. INSTALLED REPAIR PARTS IAW SRM Oct 21, 2010 · N370FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201010194104Unknown · multiple failSIGNIFICANT STATIC DISCHARGE EXPERIENCED WHICH RESULTED IN MOMENTARY WX RADAR FAILURE AND LVL ONE "ENG FIRE AGNT LO". AGT 1 LO & AGT 2 LOW ILLUMINATED FOR ENGS 1 & 3 AND AGT 2 LO ILLUMINATED FOR ENG 2. COMPLIED WITH LIGHTENING INSPECTION REF MM 05-53-00-6Oct 19, 2010 · N567FE · Doug MD1010F · Standard Practices/StructuresSDR FDEA201010164086Seat Track · corrodedCABIN LT STA 1721 TO 1731 X=27.5 SEAT TRACK FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1711 TO STA 1751 X=27.5 AS PER SRM 53-70-00 FIG 1 VOL I REV 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 111.Oct 16, 2010 · N385FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010164088Longeron · corrodedLOWER FUSELAGE STA 1370, STR31L LONGERON SEVERAL AREAS FOUND CORRODED. CORROSION REPAIRED AS PER SRM 53-10-00 FIG 2A VOL I REVISION 96. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Oct 16, 2010 · N385FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201010164090Spar Cap · crackedDURING HFEC OPEN HOLE FOUND 3 EA CRACK INDICATIONS ON RT WING, XORS 345.750. REAR SPAR LOWER CAP. REF TO EO 8-5710-7-5007A, PART 2. CRACKED INDICATION FASTENER HOLES (HOLES 'A', 'B', 'C') REPAIRED AS PER EA 8-5710-143772. REPAIR CLASSIFIED AS MAJOR AS PER GMOct 16, 2010 · N385FE · Doug MD1010F · Wing SparSDR FDEA201010164091Spar Cap · crackedDURING HFEC OPEN HOLE FOUND 1 EACH CRACK INDICATION ON LT WING, XORS 345.750 REAR SPAR LOWER CAP. REF TO EO 8-5710-7-5007A PART 1. EACH CRACK INDICATION ON HOLE 'C' LT WING XORS 345.750 REAR SPAR LOWER CAP. REPAIRED PER EA 8-5710-143775 REPAIR CLASSIFIED Oct 16, 2010 · N385FE · Doug MD1010F · Wing SparSDR FDEA201010144078Slat System · malfunctionedDURING TEST FLIGHT AT 15,500' & 180 KTS, SLAT HANDLE MOVED TO EXTEND POSITION, SLATS WOULD NOT EXTEND. HANDLE MOVED BACK TO RETRACT AND EXTEND AGAIN, SLATS FINALLY EXTENDED NORMALLY. HYD PAGE INDICATED NO QUANTITY,"HYD 3 FAIL" THEN DISPLAYED. COMPLIED W/REOct 14, 2010 · N359FE · Doug MD1010F · Leading Edge Slat Control SystemSDR FDEA201010144074Slat System · malfunctionedDURING TEST FLIGHT AT 15,500' AND 180 KTS, SLAT HANDLE MOVED TO EXTEND POSITION, SLATS WOULD NOT EXTEND. HANDLE MOVED BACK TO RETRACT & EXTEND AGAIN, SLATS FINALLY EXTENDED NORMALLY. HYD PAGE INDICATED NO QUANTITY,"HYD 3 FAIL" THEN DISPLAYED. COMPLIED W/REOct 14, 2010 · N359FE · Doug MD1010F · Leading Edge Slat Control SystemSDR FDEA201010144075Drive System · crackedDURING TEST FLIGHT AT 15,500'& 180 KTS, SLAT HANDLE MOVED TO EXTEND POSITION, SLATS WOULD NOT EXTEND. HANDLE MOVED BACK TO RETRACT & EXTEND AGAIN, SLATS FINALLY EXTENDED NORMALLY. HYD PAGE INDICATED NO QUANTITY,"HYD 3 FAIL" THEN DISPLAYED. COMPLIED W/RED TAOct 14, 2010 · N359FE · Doug MD1010F · Leading Edge Slat Control SystemSDR FDEA201010134047Skin · damagedFWD CARGO DOOR JAMB-AFT EDGE FOUND WITH SLIGHT DAMAGE. FORWARD CARGO DOOR JAMB - AFT EDGE FOUND WITH SLIGHT DAMAGE. REPAIRED AS PER SRM 53-50-00 FIG 26 SHEET 1 REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.Oct 13, 2010 · N385FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201010134049Floorbeam · corrodedAFT CARGO RT FLOOR PANEL SUPPORT AT APPROX STA 1841 SUPPORTING FWD EDGE OF FLOOR PANEL NR 187HF FOUND CORRODED. AFT CARGO RIGHT HAND FLOOR PANEL NUMBER 187HF STA 1841 X=-34 TO X=-90 SUPPORT REPAIRED AND INSTALLED AS PER SRM 53-00-01 FIG 8 VOL I REV 96. REPAIOct 13, 2010 · N385FE · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201010124016Skin · dentedRT EXTERIOR FUSELAGE SKIN PRIMARY STATIC PORT CONTROLLED AREA HAS 5 EA DENTS. REPAIRED RT PRIMARY STATIC PORT CONTROLLED AREA DENTS, 5 EACH IAW EA 8-5330-123564, REV "IR" 10-1-10, ALL DENTS FOUND TO BE WITHIN LIMITS EA 8-5330-123564, REV "IR" 10-1- 10, ANDOct 12, 2010 · N370FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201010124026Longeron · corrodedLOWER FUSELAGE STA 1410 TO STA 1440, STR30L, LONGERON FOUND EVIDENCE OF CORROSION (04 EACH). LONGERON REPAIRED AS PER EA 8-5310-143459. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 111.Oct 12, 2010 · N385FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201010124027Longeron · corrodedLOWER FUSELAGE STA 1361, STR 30L, LONGERON FOUND CORROSION. LONGERON TRIMMED IAW SRM 53-10-00, FIG 5, VOL I, REV 96. NEW LONGERON SEGMENT FROM STA 1302 TO STA 1411.5 FABRICATED IAW DWG AEA 0702 REV NC AND INSTALLED IAW SRM 53-10-00, FIG 5, VOL I, REV 96. REPOct 12, 2010 · N385FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201010114003Skin · crackedRT WING NR3 LEADING SLAT ANTI-ICE DUCT UPPER INBD CUTOUT CRACKED APPROX .5 INCH. CRACKED AREA REPAIRED AS PER EA 8-5710-143448. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 111.Oct 11, 2010 · N385FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201010114004Skin · crackedLT WING NR 3 LEADING SLAT ANTI-ICE DUCT UPPER OTBD CUTOUT CRACKED APPROX .5 INCH. CRACKED AREA TRIMMED AND REPAIR CARRIED OUT AS PER EA 8-5710-143447. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 111.Oct 11, 2010 · N385FE · Doug MD1010F · Wing, Plate/Skin
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