N367FE

Service difficulty reports · 138

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 = 'N367FE' 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 FDEA201306021348Web · crackedTHREE CRACKS LT MLG WW INBD BULKHEAD 25 INCHES AND 27 INCHES AFT OF FWD BULKHEAD AND BOTH 4 INCHES DOWN FROM UPPER BULKHEAD. LAST CRACK IS 23 INCHES AFT OF FWD BULKHEAD AND 3 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED BULKHEAD IAW EA 8-5310-T0300629.Jun 2, 2013 · N367FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201306021347Bulkhead · crackedTWO CRACKS CENTER MLG WW LT BULKHEAD 25 INCHES AFT OF FWD BULKHEAD AND 4 INCHES AND 5.5 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED IAW EA 8-5310-T0300629.Jun 2, 2013 · N367FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201301270199Line · cloggedENGINE FAIL WARNING ILLUMINATED ON GLARESHIELD ON TAKEOFF, NR 1 ENG N1 DID NOT ACCELERATE PAST 87 PERCENT. ENG DID NOT FAIL. DISCONNECTED NR 1 ENG CDP LINE. BLEW LINE CLEAR, FOUND MINOR DEBRIS IN LINE. CAPPED LINE AND PRESSURE CHECKED FOR LEAKS, NONE FOUJan 27, 2013 · N367FE · Doug MD1010F · Engine (Turbine/Turboprop)SDR FDEA201202230648Bolt · corrodedFOUND TRUNNION BOLT CORRODED. REMOVED AND INSTALLED NEW FWD TRUNNION BOLT ON RT MLG. IAW E.O 8-3210-7-5004 PT 2.Feb 23, 2012 · N367FE · Doug MD1010F · Fuselage, Landing Gear Attach FittingsSDR FDEA201202190620Shear Tie · corrodedAFT CARGO COMPARTMENT WASTE TANK AREA HAS 2 EA CORRODED SHEAR TIES AT STA. 1997 BETWEEN LONGERON L51-52 AND R50-51. REMOVED AND REPLACED SHEAR TIES AT STA 1997 BETWEEN LONGERONS 50-51R AND 50-52L, REF SRM 51-33-01, VOL II.Feb 19, 2012 · N367FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR FDEA201202100544Angle · corrodedAFT CARGO BAY ANGLE COMMON TO FRAME AND SKIN AT BS 1964 BETWEEN R51L AND L51L IS SHOWING EVIDENCE OF EXFOLIATION. REMOVE AND REPLACE WITH NEW ANGLE. LOCATED, DRILLED, AND INSTALLED PER SRM 51-30-01 VOL.II AND INSTALLED IAW SRM 51-30-01.Feb 10, 2012 · N367FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR FDEA201202100545Shear Tie · corrodedAFT CARGO BAY ANGLE COMMON TO FRAME AND SKIN AT STA.1975 BETWEEN R51L AND L51L HAS EVIDENCE OF CORROSION. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-00, VOL II.Feb 10, 2012 · N367FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR FDEA201202090539Beam · crackedR3 DOOR BEAM IS CRACKED. R & R CRACKED DOOR BEAM, REF SRM 51-35-01, VOL II.Feb 9, 2012 · N367FE · Doug MD1010F · Passenger/Crew DoorsSDR FDEA201202090536Structure · gougedLT WING NR 3 SLAT TRACK IS RIDING/CUTTING INTO L/E SUPPORT STRUCTURE. FWD UPPER TRACK CORNERS. CLEARANCE CHECKED GOOD.Feb 9, 2012 · N367FE · Doug MD1010F · Wing Main, Frame StructureSDR FDEA201202090535Structure · gougedLEFT WING NR 1 SLAT TRACK IS RIDING AND CUTTING INTO L/E SUPPORT STRUCTURE. FWD UPPER TRACK CORNERS. BURNISHED THE SLAT TRACK IAW CMM 57-55-04. ALODINE AND PAINT AND PRIMERED IAW SRM 51-21-01 AND 51-21-02. R & R NR 1 LT SLAT AND CLEARANCE AND OPS CHECK C/WFeb 9, 2012 · N367FE · Doug MD1010F · Wing Main, Frame StructureSDR FDEA201202090533Slat Track · gougedLEFT WING NR 16 SLAT TRACK INBD SIDE IS RIDING INTO L/E STRUCTURE. L/E STRUCTURE HAS DAMAGE DUE TO THIS RIDING CONDITION. BLENDED DAMAGE AREA IAW SRM 57-00-01, VOL 1 AND EA 8-5710-156743.Feb 9, 2012 · N367FE · Doug MD1010F · Leading Edge DevicesSDR FDEA201201100064Lens · missingRT DOOR DISARMED LIGHT LENS IS MISSING. FOUND LENS ON FLOOR. REINSTALLED LENS. LIGHTS WORK OK.Jan 10, 2012 · N367FE · Doug MD1010F · Emergency LightingSDR FDEA201105282016Battery · inoperativeR1 DOOR CIRCUITRY TEST LIGHT INOPERATIVE. REMOVED AND REPLACED THE R1 DOOR REMOTE SLIDE PRESSURE INDICATOR AND REPLACED BATTERIES. OPS CK GOOD.May 28, 2011 · N367FE · Doug MD1010F · Escape SlideSDR FDEA201012044578Controller · failedAT CRUISE FL330, AIR MANF 2 FAIL. COMPLIED WITH QRH AND DIVERTED. RELEASED FOR SERVICE IAW MEL: 36-23-01-02, CATEGORY: C EXPIRATION: 13DEC10 "MEL 36-23-01-02: NR 2 MANIFOLD FAIL DETECTION LOOP NR2 INOP. NO HISTORY 99 DAYS ON SYS 2 MAN FAIL. NO CURRENT FADec 4, 2010 · N367FE · Doug MD1010F · Fire DetectionSDR FDEA201004281382Skin · dentedRT WING INBD FLAP UPPER SURFACE AT APPROX XIFH 215 FOUND 1 EACH DENT WITH DEEP NICK DURING BLEND OUT. DENT WITH DEEP NICK AT RT WING INBD FLAP UPPER SURFACE AT APPROX XIFH 215 REPAIRED IAW SRM 57-10-00 FIG 85 VOL I REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM Apr 28, 2010 · N367FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004261365Seat Track · corrodedAFT CABIN AT STA 1963, X= -107.25 RT CURVE SEAT TRACK FOUND CORROSION. FT CABIN AT STA 1963, X= -107.25 RT CURVE SEAT TRACK R & R IAW SRM 51-31-01, VOL II REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.Apr 26, 2010 · N367FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004261360Skin · deformedLT WING INBD FLAP LOWER L/E INBD OF OTBD HINGE, FOUND SKIN DEFORMED. LT WING INBD FLAP LOWER L/E INBD OF OTBD HINGE DEFORMED SKIN EVALUATED AND FOUND WITHIN LIMIT IAW SRM 57-00-01 FIG 1B VOLUME I REVISION 96. DEPTH OF DENT = 0.013", DIAMETER OF DENT = 3.0"Apr 26, 2010 · N367FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004251359Skin · dentedEMPENNAGE- RT HORIZONTAL STABILIZER NR3 L/E (FROM INBD) FOUND DENTED. DENT AREA TRIMMED OUT AND FABRICATED REPAIR DOUBLER, REPAIR SKIN AND REPAIR CARRRIED OUT IAW SRM 55-10-00 VOL I REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.Apr 25, 2010 · N367FE · Doug MD1010F · Horizontal Stabilizer, Plate/SkinSDR FDEA201004241347Skin · dentedDENT - RT WING INBD FLAP LOWER SURFACE. REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 3, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Apr 24, 2010 · N367FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004231316Structure · crackedLT WING - NR 1 SLAT LOWER SIDE BETWEEN NR 1 AND NR 2 TRACK FOUND EXTRUSION WITH CRACK. REPAIR CARRIED OUT IAW EA 8-5750-137977: REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.Apr 23, 2010 · N367FE · Doug MD1010F · Wing Main, Frame StructureSDR FDEA201004231315Panel · bulgedLT WING T/E UPPER PANEL AT REAR SPAR APPROX XORS 860 FOUND WITH BULGING. CORROSION FOUND AT BULGING AREA REMOVED AND REPROTECTED IAW SRM 51-21-01 VOL II, REV 96, FOUND WITHIN LIMIT IAW SRM 57-20-00 FIG 37, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW Apr 23, 2010 · N367FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201004231314Door Frame · damagedFWD CARGO DOOR JAMB-UPON REMOVAL OF AFT LOWER DOOR JAMB SEAL RETAINER, RIVET HOLES ON WEB STRUCTURE FOUND ELONGATED. REPAIR CARRIED OUT IAW EA NR 8-5310-137983, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.Apr 23, 2010 · N367FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201004231313Angle · crackedFWD CARGO BILGE AREA - APPROX STA 899 FRAME 'L' CLIP FOUND CRACKED. FWD CARGO BILGE AREA STA 899 FRAME 'L' CLIP REPAIR CARRIED OUT IAW SRM 53-30-00, FIG.10, VOL. I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Apr 23, 2010 · N367FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201004231312Beam · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLES B AND D. REPAIR CARRIED OUT IAW EA 8-5310-137972: REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.Apr 23, 2010 · N367FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201004231311Beam · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLE B. REPAIR CARRIED OUT IAW EA NR 8-5310-137972, TITLE: FUSELAGE - MAIN FRAME LOWER JAMB REPAIR TO BORE HOLApr 23, 2010 · N367FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201004231310Beam · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 6 LOWER JAMB FITTING AT HOLE C. REPAIR CARRIED OUT IAW EA 8-5310-137972. REPAIR CLASSIFIED MAJOR GMM 6-2-100, REV 110.Apr 23, 2010 · N367FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201004231309Beam · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 6 LOWER JAMB FITTING AT HOLES C. REPAIR CARRIED OUT IAW EA 8-5310-137972: FUSELAGE - MAINFRAME - MCD LOWER JAMB REPAIR TO BORE HOLES COMMON TOApr 23, 2010 · N367FE · Doug MD1010F · Fuselage Main, StructureSDR FDEA201004231308Beam · crackedCRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 1 LOWER JAMB FITTING AT HOLES A, B AND D. REPAIR CARRIED OUT IAW EA 8-5310-137972. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.Apr 23, 2010 · N367FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201004231307Rib · crackedRT WING FIXED L/E LOWER FOUND CRACKED ON SLAT TRACK NR 16 INBD FWD RIB. CRACKED AT RT WING FIXED L/E LOWER ON SLAT TRACK NR 16 INBD FWD RIB REPLACED IAW SRM 51-31-01, VOLUME II REVISION 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.Apr 23, 2010 · N367FE · Doug MD1010F · Wing, Rib/BulkheadSDR FDEA201004231306Beam · crackedCRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 1, LOWER JAMB FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT IAW EA 8-5310-137972: REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.Apr 23, 2010 · N367FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201004231305Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D IAW SRM 53-50-00 FIG 17Apr 23, 2010 · N367FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201004231304Support Fitting · crackedCRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT AT MAIN CARGO DOOR LOWER JAMB NR2 SUPPORT FITTING AT HOLES A, B, C AND D IAW SRM 53-50-00 FIG 17,Apr 23, 2010 · N367FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201004231303Skin · damagedFUSELAGE - FWD CARGO DOOR CUT-OUT LOWER AFT EXISTING DOUBLER FOUND DAMAGED. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 26 VOL. I REV. 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.Apr 23, 2010 · N367FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201004231302Skin · dentedFUSELAGE - AFT OF NOSE RADOME AT STA 305 LOWER CTR AREA WITH EXISTING BLEND OUT. EXISTING BLEND OUT AT FUSELAGE AFT OF NOSE RADOME AT STA 305, LOWER CTR AREA EVALUATED AND FOUND OUT OF LIMIT IAW SRM 53-10-00 VOL I, REV 96. ORIGINAL THICKNESS = 0.063", MATERIAApr 23, 2010 · N367FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201004231301Skin · damagedWHILE ACCOMPLISHING EA 8-5230-137737 PART 3 -TO REPAIR SKIN OF AFT LOWER CARGO DOOR OUTER SKIN, FOUND REPAIR AREA CLOSE TO COVER CUT-OUT AND PLACARD INSTALLATION. COMPLIED WITH EA 8-5230-132409: DOORS - LOWER CTR CARGO DOOR SKIN - REPAIR. REPAIR CLASSIFIED Apr 23, 2010 · N367FE · Doug MD1010F · Cargo/Baggage DoorsSDR FDEA200912104402Valve · leakingAT FL 280 GOT LEVEL-1 "HYD 3 ELEV OFF" FLUID IN NR 3 3.5 GAL. SECURED HYD SYS NR 3 FOR LANDING. AFTER DIRTY UP LOST REMAINING FLUID FOLLOWED BY "HYD 3 FAIL" TOWED TO GATE. FOUND HORIZONTAL STABILIZER PRIMARY CONTROL VALVE LEAKING. R & R HORIZONTAL STABILDec 10, 2009 · N367FE · Doug MD1010F · Hydraulic System, MainSDR FDEA200810224488Lead · failedWHEN DESCENDING OUT OF FL240 FOR LANDING, GOT "ENG 3 EGT HI" AND ENG 3 EXCEEDANCE ALERTS, EGT 3 INDICATIONS SEQUENCED BETWEEN HIGH INDICATIONS (1053) AND AMBER "X", NO SECONDARY INDICATIONS. SHUT DOWN ENGINE IAW QRH, EGT WAS HIGH APPROX 30 SEC ON LANDING CRASOct 22, 2008 · N367FE · Doug MD1010F · Engine Indicating System WiringSDR 08FDEA04488Lead · malfunctionedWHEN DESCENDING OUT OF FL240 FOR LANDING, GOT "ENG 3 EGT HI" AND ENG 3 EXCEEDANCE ALERTS EGT 3 INDICATION. SEQUENCED BETWEEN HIGH INDICATIONS (1053) AND AMBER "X", NO SECONDARY INDICATIONS. SHUT DOWN ENGINE IAW QRH, EGT WAS HIGH APPROX 30 SEC ON LANDING CRASOct 22, 2008 · N367FE · Doug MD1010F · Engine Indicating System WiringSDR 08FDEA03717Pressure Switch · failedDURING CLIMB-OUT, ABOVE 10,000 FT, RECEIVED LEVEL 1 HYD 2 OFF ALERT WITH SUBSEQUENT SHUTDOWN OF LT AND RT NR 2 ENGINE DRIVEN PUMPS. DURING APPROACH AND LANDING RMP'S REPRESSURIZED SYSTEM AND ACCOMPLISHED NORMAL FLAPS 35 LANDING. GVI DP INDICATORS ON NR 2 ESep 3, 2008 · N367FE · Doug MD1010F · Hydraulic System, MainSDR 08FDEA01954Panel · delaminatedRIGHT WING PANEL 635 BL HAS DELAMINATION AND A PUNCTURE. REPAIRED PANEL BY FABRICATING A NEW INNER SKIN IAW E.A. 8-5720-118490 & TPS 1001, REV E. DURING POST CURE CLEAN UP FOUND 4 CRACKS IN THE PANEL. HEAT TREATED IAW TPS 1003, REV A. FABBED REPAIR DOUBLEMay 22, 2008 · N367FE · Doug MD1010F · Wing, Plate/SkinSDR 08FDEA01852Fitting · corrodedTHE CENTER CARGO COMPARTMENT, LEFT TRANSITION PANEL SUPPORT HAS CORROSION AT STATION 1601, STRINGER 43L. REMOVED CORROSION IAW SRM 51-21-01; VOL II. FOUND TO TO BE EXFOILEATED. REMOVED AND REPLACED ADJ 7003-1 FITTING, IAW SRM 51-33-01; VOL II.May 15, 2008 · N367FE · Doug MD1010F · Fuselage Main, Attach FittingsSDR 08FDEA01847Skin · corrodedRIGHT WING INBD FLAP; INBD UPPER AFT SKIN IS CORRODED. REMOVED AND REPLACED THE SKIN IAW DC/MD-10 SRM 51-35-01; VOL II. FABRICATED NEW PANEL IAW DAC DWG NR ARC 2746, REV Z. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-08. PART MARKED P/N FX-ARC 2746-24 IAW May 14, 2008 · N367FE · Doug MD1010F · Trailing Edge FlapsSDR 08FDEA01841Bracket · gougedRIGHT WING INBD FLAP, INBD HINGE POINT IS GOUGED. BLENDED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 AND DWG ARC 2518. REMOVED DAMAGED FAIL SAFE STRAP AND RECEIVED A NEW STRAP. LOCATED, DRILLED AND INSTALLED THE NEW STRAP IAW SRM 51-35-01, SRM 1-31-01,May 13, 2008 · N367FE · Doug MD1010F · Trailing Edge FlapsSDR 08FDEA01827Fitting · corrodedCENTER CARGO COMPARTMENT LT TRANSITION PANEL SUPPORT FITTING HAS CORROSION; MOUNTED ON THE FRAME AT FS 1661 LBL 43. REMOVED CORROSION IAW 51-21-01; VOL II. FOUND TO BE EXFOLIATED. REMOVED & REPLACED ADJ7003-1 FITTING. IAW SRM 51-33-01; VOL II.May 12, 2008 · N367FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR 08FDEA01832Hinge · corrodedRIGHT WING OUTBD FLAP, OUTBD HINGE LOCATION NR 3 OUTBD BORE IS CORRODED. REMOVED CORROSION FROM THE OUTBD BORE OF THEN 3 LUG IAW CMM 57-44-01. MACHINED BUSHING FOR THE OUTBD BORE IAW 57-44-01. CAD PLATED BUSHING IAW QQP-416-TY2-CL2 7. INSTALLED THE BUSHINGMay 12, 2008 · N367FE · Doug MD1010F · Trailing Edge FlapsSDR 08FDEA01831Hinge · corrodedRIGHT WING OUTBD FLAP, OUTBD HINGE LOCATION NR 3 INBD BORE IS CORRODED. REMOVED THE CORROSION FROM THE INBD BORE IAW CMM 57-44-01. MACHINED NEW BUSHINGS FOR THE INBD BORE IAW CMM 57-44-09. CAD PLATED BUSHING IAW QQP-416-7Y2- CL2. INSTALLED THE NEW BUSHIMay 12, 2008 · N367FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR 08FDEA01830Hinge · corrodedRIGHT WING OUTBD FLAP, INBD HINGE LOCATION NR 3 OUTBD LUG FACE OUTER SURFACE IS CORRODED. LUG THICKNESS VERIFIED TO BE .421 IAW BAC CMM 57-44-01. CORROSION FOUND AND REMOVED FROM THE LUG FACE TO .405. LUG FOUND TO BE OUT OF LIMITS IAW BAC CMM 57-44-01. ETCMay 12, 2008 · N367FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR 08FDEA01829Hinge · corrodedRIGHT WING OUTBD FLAP, INBD HINGE, LOCATION NR 3 INBD LUG FACE OUTER SURFACE IS CORRODED. LUG THICKNESS VERIFIED TO BE .421 IAW BAC CMM 57-44-01. CORROSION FOUND AND REMOVED FROM LUG FACE NR 3 INBD TO .405. LUG FOUND TO BE OUT OF LIMITS IAW BAC CMM 57-44-0May 12, 2008 · N367FE · Doug MD1010F · Trailing Edge FlapsSDR 08FDEA01828Hinge · corrodedRIGHT WING OUTBD FLAP, INBD HINGE LOCATION NR 3 MOUNTING SURFACE IS CORRODED. REMOVED THE CORROSION FROM THE NR 3 LUG FACE IAW CMM 57-44-08. FABRICATED SHIMS IAW CMM 57-44-08. CAD PLATED SHIMS IAW QQP 416 TY2 CL2 AND INSTALLED SHIMS ON THE NR 3 LUG IAW CMM May 12, 2008 · N367FE · Doug MD1010F · Trailing Edge FlapsSDR 08FDEA01795Skin · dentedRIGHT WING FIXED LEADING EDGE SKIN IS DENTED IN 4 PLACES AT STA XFS 627 TO XFS 653. DEPTH OF THE DENTS ARE0.045 TO 0.120. DENTS ARE OUT OF LIMITS IAW SRM 57-00-01 VOL I FIG 1B. FABRICATED REPAIR IAW SRM 52-00-01 VOL I FIG 4. ALODINED IAW SRM 51-21-01 May 8, 2008 · N367FE · Doug MD1010F · Wing, Plate/Skin
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