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"

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SDR FDEA201005251634Fitting · crackedMAIN DECK CARGO DOOR - HFEC OPEN HOLE INSP ON NR 6 LOWER JAMB FITTING, 0.520 INCH HOLE AT HOLE 'B' FOUND CRACKED INDICATION ON FIRST LAYER WEB FROM TOP. REPAIR CARRIED OUT IAW EA NR8-5310-140322, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.May 25, 2010 · N68049 · Doug MD1010F · Fuselage Main, StructureSDR FDEA201005251654Beam · damagedMAIN DECK CARGO COMPARTMENT RT NR 3 DOOR PLUG MOST UPPER BEAM AFT END FOUND DAMAGED. MAIN DECK CARGO COMPARTMENT RT 3 DOOR AREA REMOVED IAW SRM 51-31- 01 VOL. II REV. 96. REPAIR CLASSIFIED AS MINOR IAWAS PER GMM 6-2-100, REV. 110.May 25, 2010 · N68049 · Doug MD1010F · Service DoorsSDR FDEA201005251643Skin · misrepairedRT NR 1 L/E SLAT HAS A FLUSH DOUBLER REPAIR ON THE INBD L/E EXTERIOR, NR 1 TRACK VICINITY. EXISTING REPAIR AT RT NR1 L/E SLAT FLUSH DOUBLER REPAIR ON THE INBD L/E EXTERIOR, NR 1 TRACK VICINITY EVALUATED AND FOUND NOT IAW SRM REPAIR SCHEME. RT NR 1 SLAT R May 25, 2010 · N68049 · Doug MD1010F · Leading Edge DevicesSDR FDEA201005251651Skin · misrepairedEXISTING REPAIR ON FUSELAGE SKIN AT STA 715, LONGERON 29L EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 53-20-00 FIG 13, VOLUME I, REV 96. HOWEVER, 08 EACH EXISTING BOLTS WERE FOUND PREVIOUSLY INSTALLED NOT IAW SRM. 08 EACH EXISTING BOLTS R & R WITH LOCMay 25, 2010 · N68049 · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201005251652Skin · misrepairedLT DROOP L/E FOUND EXISTING REPAIR AT INBD LOWER CORNER, EXTERIOR. EXISTING REPAIR AT LT DROOP L/E INBD LOWER CORNER EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR DOUBLER REMOVED IAW SRM 51-31-01, VOLUME II REV 96 AMay 25, 2010 · N68049 · Doug MD1010F · Wing, Plate/SkinSDR FDEA201005251653Skin · misrepairedLT OTBD T/E FLAP OTBD LOWER SURFACE FOUND 1 EACH EXISTING REPAIR. EXISTING REPAIR AT LT OTBD T/E FLAP OTBD LOWER SURFACE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-35-01, VOLUME II, REVISION 9May 25, 2010 · N68049 · Doug MD1010F · Trailing Edge FlapsSDR FDEA201005221610Seat Track · crackedSEAT TRACK STA815 X=8.5 IN CABIN. SEAT TRACK FOUND CRACKED. CABIN - LT STA 815 X= 8.5 SEAT TRACK CARRIED OUT REPAIR IAW SRM 53-70-00, FIG I , VOL. I REV. 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 110.May 22, 2010 · N68049 · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201005201584Switch · sparksWHILE TURNING ON LT AND RT LANDING LIGHTS AND NOSE LIGHT NOTICED SPARKS FROM LIGHT SWITCHES. UNABLE TO DETERMINE WHICH SWITCH ACTUALLY SPARKED. WHILE CHECKING PROBLEM, FOUND NOSE GEAR TAXI LIGHT TOGGLE LOOSE FROM SWITCH, BUT FOUND NOTHING ELSE OBVIOUS WRONG WMay 19, 2010 · N68053 · Doug MD1010F · Exterior LightingSDR FDEA201005181566Skin · damagedFUSELAGE, LT SIDE AFT OF AFT PIT DOOR, APPROX AT STA 1853 TO STA 1902, BETWEEN L38 TO L39 HAS 2 EA 10 INCHES CREASED IN SKIN. REPAIRED SKIN WITH DOUBLERS INSTALLATION IAW SRM 51-31-01, AND SRM 53-20-00, MAJOR REPAIR.May 18, 2010 · N394FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201005151540Skin · crackedLOWER FUSELAGE - NR 1 AIR CONDITION COMPARTMENT DOOR CUT OUT AFT UPPER CORNER EXTERIOR SKIN FOUND CRACKED. REPAIRED IAW EA1-5330-140315.May 15, 2010 · N604FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201005151541Pseu · failedAFTER TAKEOFF HAD AN UNSAFE GEAR INDICATION FOR LT MAIN ON BOTH PRIMARY AND SYNOPTIC DISPLAY WHEN GEAR RETRACTED. COMPLETED WITH QRH, RECYCLED GEAR AND GOT A NORMAL UP INDICATION ON BOTH PRIMARY AND SYNOPTIC. LANDED WITHOUT INCIDENT. VISUALLY INSPECTED LT May 15, 2010 · N599FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA201005141538Skin · gougedRT FUSELAGE, AFT OF CTR PIT DOOR APPROX STA 1801, BELOW L36 HAS 2 GOUGLES. CUT OUT DAMAGE IAW SRM 53-20-00, FIG 16-6, FABRICATED REPAIR DOUBLERS IAW SRM 53-20- 00 AND INSTALLED ALL REPAIR PARTS IAW SRM 53-20-00 AND SRM 51-31-01, MAJOR REPAIR.May 14, 2010 · N394FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201005141539Skin · gougedRT FUSELAGE, AFT OF CTR CARGO DOOR , APPROX STA 1781 AT HINGE LEVEL, L-28 HAS CREASE IN SKIN FWD OF PREVIOUS REPAIR. REPAIRED SKIN IAW SRM 53-20-00, FIG 6 WITH DOUBLERS AND FILLERS AS REQUIRED, MAJOR REPAIR.May 14, 2010 · N394FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201005011410Skin · corrodedCTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -RBL 106 TO RBL 73, FS 1332 TO 1365. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1332-1365, RBL 106-73 AND COMPLIED WITH EA 8-5730-139141. REPAIRMay 1, 2010 · N394FE · Doug MD1010F · Fuselage Main, KeelSDR FDEA201005011411Skin · corrodedCTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -RBL 73 TO RBL 38, FS 1300 TO 1332. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1300-1332, RBL 73-RBL38 AND COMPLIED WITH EA 8-5730-139141. REPAMay 1, 2010 · N394FE · Doug MD1010F · Fuselage Main, KeelSDR FDEA201005011412Skin · corrodedCTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -RBL 106 TO RBL 73, FS 1300 TO 1332. REMOVED CORROSION BY BLENDING. REMOVED 11 EA FASTENERS CHECKED LIMITS IAW EA8-5730-139141 AND REINSTALLED FASTMay 1, 2010 · N394FE · Doug MD1010F · Fuselage Main, KeelSDR FDEA201005011413Skin · corrodedCTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -LBL 106 TO LBL 73, FS 1332 TO 1365. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1332-1365, LBL 106-73 AND COMPLIED WITH EA 8-5730-139141. REPAIMay 1, 2010 · N394FE · Doug MD1010F · Fuselage Main, KeelSDR FDEA201005011414Skin · corrodedCTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -LBL 38 TO LBL 0, FS 1300 TO 1332. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1300-1332, LBL 38-0 AND COMPLIED WITH EA 8-5730-139141. REPAIR CMay 1, 2010 · N394FE · Doug MD1010F · Fuselage Main, KeelSDR FDEA201005011415Skin · corrodedCTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -LBL 73 TO LBL 38, FS 1300 TO 1332. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1300-1332, LBL 73-LBL38 AND COMPLIED WITH EA 8-5730-139141. REPAMay 1, 2010 · N394FE · Doug MD1010F · Fuselage Main, KeelSDR FDEA201005011416Skin · corrodedCTR WING BOX UPPER SURFACE EXFOLIATED IN SEVERAL LOCATIONS AND HAS CORROSION AT THE MAJORITY OF FASTENER HOLES -LBL 106 TO LBL 73, FS 1300 TO 1332. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1300-1332, LBL 106-73 AND COMPLIED WITH EA 8-5730-139141. REPAIRMay 1, 2010 · N394FE · Doug MD1010F · Wing, Center BoxSDR FDEA201005011417Skin · corrodedCORROSION AT FASTENER IN UPPER SURFACE OF CTR WING BOX, FS 1289, LBL93. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1289, LBL 93 AND COMPLIED WITH EA 8-5730-139141. REPAIR CLASSIFIED AS MAJOR REPAIR.May 1, 2010 · N394FE · Doug MD1010F · Wing, Center BoxSDR FDEA201005011418Skin · corrodedCORROSION AT FASTENER IN UPPER SURFACE OF CTR WING BOX, FS 1222 LBL75. BLENDED CORROSION IAW EA 8-5730-139141 AT STA 1222 LBL 75 AND COMPLIED WITH EA 8-5730-139141.May 1, 2010 · N394FE · Doug MD1010F · Fuselage Main, KeelSDR FDEA201004301405Hinge Fitting · corrodedRT OTBD FLAP, OTBD HINGE FLAP SIDE PIVOT BORES HAS PITTING CORROSION. REPAIRED IAW EA 8-5750-139132 WITH REPAIR BUSHINGS, MAJOR REPAIR.Apr 30, 2010 · N394FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004291397Skin · delaminatedLT WING NR 2 SPOILER UPPER SURFACE IS DELAMINATED. REPAIRED THE LT WING NR 2 SPOILER PN NRC 6048-503N; SN MTM-368 BY FABRICATING AND BONDING SKINS; DOUBLERS; TRIPPLERS; RIBS; CORE AND FITTING CLOSE OUTS IAW SRM 57-10-00, VOL I.Apr 29, 2010 · N361FE · Doug MD1010F · SpoilersSDR FDEA201004281376Longeron · corrodedFWD PIT, STA 1039 AT RBL 51 HAS CORROSION AT AROUND AND UNDER FASTENERS AT PREVIOUS BLEND OUT AREA. REPAIRED FWD PIT AT STA 1039 AT RBL 51 STRINGER IAW SRM 53-10-00, FIG 2, MAJOR REPAIR.Apr 28, 2010 · N394FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR 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 FDEA201004271368Thrust Reverser · damagedNR 3 THRUST REVERSER UNLOCK WILL NOT EXTINGUISH. CYCLED REVERSER NUMEROUS TIMES ON GROUND, NO JOY. ITEM ENTERED AS MX WRITE UP IN ERROR. ITEM IS A PILOT WRITE UP, BOS U REVERSER HAS HEAVY DAMAGE, IN THE PROCESS OF TAKING PICTURES AND MAKING A PARTS LISTApr 27, 2010 · N40061 · Doug MD1010F · Engine Thrust ReverserSDR 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 FDEA201004201260Rib · chafedRT WING NR 6 SLAT TRACK OTBD CLOSURE RIB IS CHAFED AT 2 LOCATIONS BY THE TRACK FWD OF THE FWD UPPER ROLLER. ACCOMPLISHED EA 8-5720-123350.Apr 20, 2010 · N361FE · Doug MD1010F · Wing, Rib/BulkheadSDR FDEA201004201258Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE AT LOCATION NR 8 INBD LUG FACE IS CORRODED. REMOVED CORROSION IAW CMM 57-44-09. ACCOMPLISHED HFEC IAW NTW 51-00-17. ETCHED, ROTO-PEENED, CLEANED, CALCULATED AMP HRS, CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-02. PRIMED IApr 20, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004201259Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE AT LOCATION NR 8 INBD LUG FACE IS CORRODED. REMOVED CORROSION IAW CMM 57-44-09. ACCOMPLISHED HFEC IAW NTW 51-00-17. ETCHED, ROTO-PEENED, CLEANED, CALCULATED AMP HRS, CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-02. PRIMED IApr 20, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191224Floor Panel · damagedMAIN CABIN FLOOR PANEL AT BS 570; LBL 75 HAS A SOFT SPOT. FABRICATED MAIN CABIN FLOOR PANEL AT BS 570 / LBL 75 IAW DWG SRZ 25-005, REV "H" INSTALLED FABRICATED FLOOR PANEL AT BS 570; LBL 75 IAW SRM 51-31-01, VOL II AND AMM 53-21-08-2.Apr 19, 2010 · N361FE · Doug MD1010F · Fuselage Floor PanelSDR FDEA201004191229Fitting · corrodedLT OTBD FLAP; OTBD HINGE LOCATION NR3 MOUNTING SURFACE IS CORRODED. VERIFIED LUG THICKNESS AND REMOVED CORROSION IAW CMM 57-44-09. ETCHED; FLAP- PEENED; CLEANED; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-01. PRIMED SURFACE; MATERIALApr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191232Fitting · corrodedLT OTBD FLAP; OTBD HINGE LOCATION NR 7 SIDE LOAD FITTING MOUNTING SURFACE IS CORRODED. VERIFIED LUG THICKNESS. REMOVED CORROSION; ETCHED; ROTO-PEENED; CAD PLATED; PRIMED SURFACE. MATERIAL ID FOR REPAIR SHIM; MACHINED REPAIR SHIM; PRIMED REPAIR SHIM AND BOApr 19, 2010 · N361FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201004191233Fitting · corrodedLT OTBD FLAP; INBD HINGE LOCATION NR 4 BORE IS CORRODED. REMOVED BUSHING. VERIFIED BORE DIAMETER. REMOVED CORROSION. ETCHED BORE. FLAP-PEENED BORE. CAD PLATED BORE. PRIMED BORE. MATERIAL ID FOR REPAIR BUSHING. MACHINED REPLACEMENT BUSHING. CAD PLATApr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191235Fitting · corrodedLT OTBD FLAP; INBD HINGE LOCATION NR 3 MOUNTING SURFACE IS CORRODED. REMOVED CORROSION AND SOLD LIMITS IAW CMM 57-44-08. ETCHED; FLAP PEENED; CLEANED; CADMIUM PLATED AND ADHESION TESTED IAW BSOP 20-11-01. AND BSOP 20-10-02. PRIMED SURFACE; MATERIAL ID SHIMS;Apr 19, 2010 · N361FE · Doug MD1010F · Wing, Control Surface Attach FittingsSDR FDEA201004191238Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 2 JUST AFT OF MOUNTING SURFACE IS CORRODED. REMOVED CORROSION AND ETCHED IAW BAC CMM 57-44-09. FLAP-PEENED; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED IAW BSOP 20-10-02. PRIMED IAW CMM 57- 44-09.Apr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191239Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 3 MOUNTING SURFACE IS CORRODED. REPAIRD IAW CMM 57-44-09. VERIFIED LUG THICKNESS. REMOVED CORROSION. ETCHED SURFACE. ROTO-PEENED SURFACE. FLAP PEENED SURFACE. CAD PLATED SURFACE. MATERIAL ID FOR SHIM. MACHINED SHIApr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191240Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 7 SIDE LOAD FITTING MOUNTING SURFACE IS CORRODED. REPAIRED IAW CMM 57-44-09. VERIFIED LUG THICKNESS. REMOVED CORROSION. ETCHED SURFACE. ROTO-PEENED SURFACE. CAD PLATED SURFACE. PRIMED SURFACE. MATERIAL ID FOR SHIMApr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191241Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 3 OTBD LUG FITTING IS CORRODED. REMOVED COROSION AND ACID ETCHED IAW CMM 57-44-09. ROTO-PEENED; CLEANED; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED IAW BSOP 20-10-02. PRIMED SURFACE IAW CMM 57-44-09.Apr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191242Fitting · corrodedRT OTBD FLAP; INBD HINGE FITTINGS AND LUGS HAVE SEVERAL AREAS OF BARE METAL IS CORRODED. PRIMED BARE AREAS IAW SOPM 20-11-02.Apr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191244Fitting · corrodedRT OTBD FLAP; INBD HINGE LOCATION NR 4 OTBD LUG FACE IS CORRODED. VERIFIED THICKNESS AND REMOVED CORROSION IAW CMM 57-44-08. ETCHED; CLEANED; CALCULATED AMP-HRS; PREPPED; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10- 02. PRIMED IAW CMM 57-44-08.Apr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191245Structure · corrodedRT OTBD FLAP; INBD HINGE BARREL NUT HOLE IS CORRODED. REPAIRED BARREL NUT HOLE IAW CMM 57-44-08.Apr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191246Fitting · corrodedRT OTBD FLAP; INBD LOCATION NR 3 MOUNTING SURFACE IS CORRODED. REMOVED CORROSION AND SOLD LIMITS IAW CMM 57-44-08. ETCHED; FLAP-PEENED; CLEANED; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-11-01 AND BSOPM 20-10-02. PRIMED SURFACE; MATERIAL ID FOR SHIMSApr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191247Fitting · corrodedRT OTBD FLAP; INBD LOCATION NR 2 MOUNTING SURFACE IS CORRODED. REMOVED CORROSION AND SOLD LIMITS IAW CMM 57-44-08. ETCHED; FLAP-PEENED; CLEANED; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-11-01 AND BSOPM 20-10-02. PRIMED SURFACE; MATERIAL ID FOR SHIM; FApr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191248Fitting · corrodedRT OTBD FLAP; INBD LOCATION NR 4 INBD LUG FACE IS CORRODED. VERIFIED LUG THICKNESS AND REMOVED CORROSION IAW BAC CMM 57-44-08. ETCHED; ROTO- PEENED; CLEANED; CALCULATED AMP-HRS; PREPPED; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-02. PRIMED IAW CMApr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191250Fitting · crackedRT OTBD FLAP; OTBD HINGE LOCATION NR 2 BORE HAS CRACK INDICATION. REMOVED CRACK INDICATION IAW CMM 57-44-09. ACCOMPLISHED HFEC IAW NTW 51-00-17. ETCHED AND ROTO-PEENED BORE; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED BORE IAW BSOPM 20-10-01. PRIMApr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191251Fitting · corrodedLT WING OTBD FLAP; OTBD HINGE LOCATION NR 7 BORES (2 EA) ARE CORRODED INSIDE. REMOVED CORROSION FROM BORES. BORE FOUND TO BE WITHIN LIMITS. ETCHED BORES. CAD PLATED BORES. PRIMED BORES IAW CMM 57-44-09.Apr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004191249Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 5 OTBD LUG FACE IS CORRODED. REMOVED CORROSION IAW 57-44-09. ACOMPLISHED HFEC IAW NTW 51-00-17. ETCHED; ROTO- PEENED; CLEANED; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-02. PRIMED IAW CMM 57-Apr 19, 2010 · N361FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA201004141186Hinge · corrodedCTR CARGO DOOR HINGE HAS RUST. CHECKED HINGE FOUND ALL 5 SECTIONS TO BE OUT OF LIMITS REF SRM 52-10-00, VOL I. REMOVED HINGE FROM CTR CARGO DOOR REF SRM 51-31-01, VOL II. REMOVED LINER IAW AMM 52-32-02-2. RECEIVED 5 EA DOOR HINGE SECTIONS. INSTALLED 5 EAApr 14, 2010 · N361FE · Doug MD1010F · Fuselage, Door Hinge
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