N575FE

Service difficulty reports · 416

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 = 'N575FE' 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 FDEA201205271974Longeron · crackedCRACK INDICATION FOUND DURING X-RAY INSPECTION AT STA 5-0, LONGERON -11L. REPAIRED IAW EA 1-5310-160957. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.May 27, 2012 · N575FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201205251963Skin · misrepairedSKIN BS 313, LONGERON 52 MISREPAIRED. REPAIRED CARRIED OUT IAW SRM 53-00-01, FIG 201. REPAIR 1, REV 49 EO E1-5100-7- 5001B-PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.May 25, 2012 · N575FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201205241954Skin · crackedFOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND 700. REPAIRED IAW EA 1-5710-157200 PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.May 24, 2012 · N575FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201205241953Skin · crackedFOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT THE RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 690 AND 700. REPAIRED IAW EA 1-5710-160951 PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 114.May 24, 2012 · N575FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201205241952Skin · damagedIMPACT DAMAGE TO LOWER CARGO DOOR AT THE FORWARD EDGE, REPAIRED IAW EA 1-5230-160323. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.May 24, 2012 · N575FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA201205231939Panel · crackedLOWER VERTICAL STAB RT REAR CENTER SPAR LOWER PANEL FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2, REV 49 AND DWG AJC7582 REV H. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.May 23, 2012 · N575FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA201205231938Tee Fitting · crackedCENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT TEE FITTING FOUND CRACKED. TEE FITTING REMOVED IAW SRM 51-31-01, REV 49. NEW TEE FITTING FABRICATED IAW DWG APB7158 REV C AND INSTALLED IAW SRM 51-33-01, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV May 23, 2012 · N575FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201205211898Support · crackedL3 DOOR NR 7 BEAM FORWARD STOP SUPPORT FOUND CRACKED. REMOVED IAW SRM 51-31-01, REV 49 AND REPLACED IAW SRM 51-33-01 AND 51-35-01, REV 49 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 49.May 21, 2012 · N575FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201204301672Wire · brokenEMERGENCY POWER TEST FAIL. TROUBLESHOT IAW FIM 24-30-03-00 FOUND PIN K AT P1-1957 BATTERY CHARGER R7-10 BROKEN. RETERMINATED PIN K IAW SWPM 20 & WDM 24-33-01. OPS NORMAL IAW AMM SECURE PLANE BATTERY CHARGER MAINT PRAC 24-30-00-2.Apr 30, 2012 · N575FE · Doug MD11F · Electrical Power System WiringSDR FDEA201010294193Battery Pack · out of positionTEST LIGHT ON L1 DOOR DOES NOT ILLUMINATE DURING TEST. REPOSITIONED BATTERIES IAW AMM 25-61-04-4-0. OPS WAS NORMAL. ACFT OK FOR CONTINUED SERVICE.Oct 23, 2010 · N575FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201007282692Computer · malfunctionedLIGHTING STRIKE ON DEPT OUT OF VHHH. LOST CADC 2 ACCOMPANIED BY NUMEROUS ALERTS. DUMPED 140,000 LBS OF FUEL AND RETURNED TO AN UNEVENTFVL LANDING. PERFORMED LIGHTENING STRIKE INSPECTION CHECK PER MM 05-53-01-6, NO DEFECT NOTED. REMOVED AND REPLACED NR 2 CADC Jul 28, 2010 · N575FE · Doug MD11F · Altimeter, Barometric/EncoderSDR FDEA201006021761Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STA. 1341 X= 8.5 FOUND WITH CORROSION. REPAIR CARRIED OUT FROM STA. 1331 TO 1371 X= 8.5 AS PER SRM 53-00-52 FIG. 201 REPAIR I REV. 43. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.Jun 2, 2010 · N575FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006021760Longeron Splice · crackedCABIN - 1 OFF LONGERON SPLICE AT STA 1511-1531 LONGERON 15R CRACK AT TOP CORNER AREA. REMOVED AND REPLACED AS PER SRM 51-31-01 REV. 43. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV.110Jun 2, 2010 · N575FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200905031493Engine · making metalFROM CAN AT FL331, RECEIVED LVL2 "ENG 2 OIL FILTER" ALERT RAN QRH PROCEDURE, NO HELP. SHUT DOWN ENG NR 2. ALERT REMAINED FOR DURATION OF ELT. PERFORMED NR 2 ENG INSPECTION FOUND MASTER CHIP DETECTOR HEAVILY COVER BY METALLIC SILVER FLAKES, REMOVED OIL FILMay 3, 2009 · N575FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA200812165182Doubler · chafedRIGHT WING LEADING EDGE WING ANTI-ICE TELESCOPIC DUCT CUT OUT REPAIR DOUBLER FOUND CHAFED. DOUBLER REMOVED AS PER SRM 51-31-01 VOLUME II AND INSTALLED WITH A NEW REPAIR DOUBLER AS PER EA 1-5740-122639 PART 1. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-Dec 16, 2008 · N575FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200812065101Skin · corrodedMAIN DECK, UNDER FLOOR CENTER WING UPPER PANEL UPPER SURFACE FOUND CORROSION AT STATION 1229, -X97, RIGHT. REPAIR CARRIED OUT AS PER EA 1-5710-122662. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Dec 6, 2008 · N575FE · Doug MD11F · Wing, Center BoxSDR FDEA200812055088Longeron Splice · crackedAFT CARGO COMPARTMENT RIGHT TUNNEL, LONGERON SPLICE FITTING CRACKED AT STATION 1861 L-38. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II WITH NEW FABRICATED LONGERON SPLICE AS PER DRAWING AFA7105. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Dec 5, 2008 · N575FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200812055087Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL FOUND LEFT TRUNNION AFT HOLE INTERIOR SURFACE CORRODED. CORROSION REPAIRED AS PER EA NR 1-5310-122650. REPAIR BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2Dec 5, 2008 · N575FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA200812045073Beam · crackedCABIN LEFT DOOR NR 3 FORWARD STOP, 5TH FROM TOP, FOUND CRACK APPROXIMATELY 2 INCHES. CABIN LEFT DOOR NR 3 FORWARD CRACKED STOP (BEAM) (5TH FROM TOP) REMOVED AS PER SRM 51-31-01 VOLUME II. NEW BEAM HOLES PICKED UP AND INSTALLED AS PER SRM 51-31-01 VOLUME II. Dec 4, 2008 · N575FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200812035055Skin · cracked07 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. REAMED AND REPAIR CARRIED OUT AS PER EA NR 1-5710-122655. REPAIR CDec 3, 2008 · N575FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200812035054Skin · cracked08 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. EACH CRACKED FASTENER HOLES REAMED AND REPAIR CARRIED OUT AS PER EA Dec 3, 2008 · N575FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200812035053Seat Track · corrodedCABIN RIGHT SEAT TRACK STATION 1289 TO 1321 FOUND WITH CORROSION AS MARKED AT X = -75.5. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM EXISTING SPLICE AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Dec 3, 2008 · N575FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200812035052Frame · chafedCABIN LEFT FRAME STATION 535 BETWEEN LONGERON 23 AND 24 FOUND WITH CHAFING MARKS. REPAIR CARRIED OUT AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Dec 3, 2008 · N575FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200812035051Frame · chafedCABIN LEFT FRAME STATION 535 BETWEEN LONGERON 19 AND 20 FOUND WITH CHAFING MARKS. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Dec 3, 2008 · N575FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200812035050Longeron · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT RIGHT SIDE NOSE LANDING GEAR TRUNNION FITTING TRIM OUT, FOUND LONGERON CRACKED. CRACKED LONGERON AT RIGHT SIDE NOSE LANDING GEAR TRUNNION FITTING REMOVED AS PER SRM 51-31-01 VOLUME II. NEW LONGERODec 3, 2008 · N575FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200812015020Stiffener · crackedAFT FUSELAGE COMPARTMENT AFT PRESSURE BULKHEAD STATION 2007 AFT SURFACE QUANTITY 01 STIFFENER AT X = -15.250 FOUND CRACKED APPROXIMATELY 0.5 INCH. EMPENNAGE, AFT FUSELAGE COMPARTMENT AFT PRESSURE BULKHEAD STATION 2007 AFT SURFACE STIFFENER AT X = -15.250 REDec 1, 2008 · N575FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200812015019Support Fitting · crackedDURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7, FOR CRACKED BOLDec 1, 2008 · N575FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200812015021Skin · corrodedEMPENNAGE, RIGHT AFT FUSELAGE EXTERNAL SKIN COMMON TO BODY FAIRING NR 347DF MATING SURFACE FOUND WITH CORROSION. CORRODED SKIN AT EMPENNAGE RIGHT AFT FUSELAGE EXTERNAL SKIN COMMON TO BODY FAIRING NR 347DF. REPAIRED AS PER SRM 53-20-00 FIGURE 13 VOLUME I. REDec 1, 2008 · N575FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200812015018Support Fitting · crackedDURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOR CRACKEDec 1, 2008 · N575FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA200812015017Fitting · crackedDURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES NR B AND NR C. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOR CRACKED BOLT HOLESDec 1, 2008 · N575FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200812015016Fitting · crackedDURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATION AT HOLE NR A. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 2 SUPPORT FITTING REMOVED AND REPLACED AS PDec 1, 2008 · N575FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200812015015Fitting · crackedDURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATION AT HOLE NR C. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOR CRACKED BOLT HOLE NR C, BUSHINDec 1, 2008 · N575FE · Doug MD11F · Fuselage Main, StructureSDR FDEA200811295008Fitting · crackedLEFT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING FOUND CRACKED, CRACK LENGTH APPROXIMATELY: 3/4 INCH. LEFT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. Nov 29, 2008 · N575FE · Doug MD11F · Fuselage Main, Attach FittingsSDR FDEA200811295007Fitting · crackedRIGHT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING FOUND CRACKED, CRACK LENGTH APPROXIMATELY : 1 INCH. RT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 (SHEET 1 OF 6). REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100Nov 29, 2008 · N575FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA200811295006Seat Track · corrodedCABIN SEAT TRACK STATION 959 RIGHT X =-8.5 FOUND CORRODED. CABIN: CORRODED SEAT TRACK AT STATION 959, X =-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 949 TO STATION 969, X = -8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS Nov 29, 2008 · N575FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200811284994Skin · chafedRIGHT WING LEADING EDGE SURFACE FOUND CHAFED AT BOTH SIDE OF WING ANTI-ICE TELESCOPIC DUCT CUT OUT AREA. RT WING LEADING EDGE CHAFED SURFACE AT BOTH SIDE OF WING ANTI-ICE TELESCOPIC DUCT CUT OUT AREA REPAIR CARRIED OUT AS PER EA NO 1-5740-122639 PART 1. REPANov 28, 2008 · N575FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA02274Structure · corrodedCENTER CARGO BETWEEN STA 1559 AND STA 1565 LONGERON 48R FOUND CORROSION. [07-09-07] CENTER CARGO BETWEEN STA 1559 AND STA 1565 LONGERON 48R CARRIED OUT REPAIR AS PER SRM 53- 10-00 VOLUME I FIGURE 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 26, 2007 · N575FE · Doug MD11F · Fuselage Main, StructureSDR 07FDEA02273Bushing · wornLEFT WING INBOARD FLAP VANE OUTBOARD TEE FITTING BUSHING FOUND WORN. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5750-112340, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jun 26, 2007 · N575FE · Doug MD11F · Trailing Edge FlapsSDR 07FDEA02272Longeron · crackedCENTER CARGO AT STA 5-123 LONGERON 47R FOUND 1EA LOCK FASTENER HOLE CRACKED. [07-09-07] REMOVED SPLICE AT STA 5-123 STR 47R AS PER SRM 51-33-01 VOLUME II AND HFEC INSPECTION CARRIED OUT PER NDT SPM 06-10-01.001 REV 13 FOUND NO CRACK EVIDENT. INSTALLED EJun 25, 2007 · N575FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR 07FDEA02271Structure · wornRIGHT WING, AFTER REMOVING NR 3 SLAT FOUND OUTBOARD MOUNTING HOLE WORN. [07-06-07] WORN OUTBOARD MOUNTING HOLE AT RIGHT HAND WING NR 3 SLAT REWORKED AND INSTALLED WITH NEW FABRICATED BUSHING AS PER FEDEX E.A. 1-5740-112339, REPAIR CLASSIFIED AS MINOR PEJun 25, 2007 · N575FE · Doug MD11F · Leading Edge DevicesSDR 07FDEA02231Spar Cap · corrodedRT WING REAR SPAR UPPER CAP FOUND WITH CORROSION AT XORS 1043 - 1045. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5710-111132. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.Jun 20, 2007 · N575FE · Doug MD11F · Wing SparSDR 07FDEA02230Stiffener · crackedLT WING FIXED LEADING EDGE CAVITY AT XOS = 665, STIFFENER FOUND WITH CRACK. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5710-111130. CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.Jun 20, 2007 · N575FE · Doug MD11F · Wing Miscellaneous StructureSDR 07FDEA02229Rib · crackedLT WING FIXED LEADING EDGE CAVITY AT XORS = 492 RIB STIFFENER FOUND CRACKED. [07-09-07] REMOVED CRACKED RIB STIFFENER AND FABRICATED NEW RIB STIFFENER AS PER DOUGLAS DRAWING ARB2931. INSTALLED NEW RIB STIFFENER AT LT WING FIXED LEADING EDGE CAVITY AT XORS 4Jun 20, 2007 · N575FE · Doug MD11F · Wing, Rib/BulkheadSDR 07FDEA02220Stiffener · crackedLEFT WING FIXED LEADING EDGE CAVITY, AT XOS = 570, STIFFENER FOUND CRACKED. [07-06-07] REPAIRED AS PER FEDEX EA 1-5710-111129, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jun 20, 2007 · N575FE · Doug MD11F · Wing Miscellaneous StructureSDR 07FDEA02219Rib · crackedRIGHT WING FIXED LEADING EDGE RIB FOUND CRACKED AT XOS 911. [07-06-07] CRACKED RIB REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEW RIB FABRICATED PER DOUGLAS DRAWING ARB2921. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jun 20, 2007 · N575FE · Doug MD11F · Wing, Rib/BulkheadSDR 07FDEA02218Skin · crackedLEFT WING FIXED LEADING EDGE, AT 3 SLAT ANTI-ICE TELESCOPE DUCT CUT-OUT, FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND FEDEX E.A. 1-5710-112343, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jun 20, 2007 · N575FE · Doug MD11F · Wing, Plate/SkinSDR 07FDEA02217Skin · crackedRIGHT WING FIXED LEADING EDGE TELESCOPE DUCT CUTOUT FOUND CRACKED. [07-06-07] CRACK AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND FEDEX E.A. #1-5710-112342, REPAIR CLASSIFIED AS MINOR PER GMJun 20, 2007 · N575FE · Doug MD11F · Wing, Plate/SkinSDR 06FDEA1818Adc · malfunctionedON TAKEOFF, ALL AIRSPEED INDICATIONS LOST, RECEIVED SELECT FADEC OFF; AIRSPEED INDICATIONS CAME BACK BUT ERRONEOUS; LOST ALTITUDE INDICATION, LSAS ALL FAIL ALERT; YAW DAMP ALL FAIL. INFO NOTE: PER CREW DEBRIEF INDICATION LOSS ONLY ON CAPTAINS SIDE. FAULT RMay 10, 2006 · N575FE · Doug MD11 · Air Data ComputerSDR 06FDEA0496Stiffener · brokenDURING MODIFICATION FROM P TO F FOUND STIFFENER AT STA 525 TO STA 595, S28L TO STRINGER 36 LT BROKEN. REPLACE STIFFENER FOR DWG SP10530071 AND SRM 51-33-01 PAG 34/47.Feb 2, 2006 · N575FE · Doug MD11 · Fuselage Miscellaneous StructureSDR 05FDEA04350Frame · crackedDURING AIRPLANE'S CONVERSION FROM P TO F: A CRACK 2.2" LONG HAS BEEN FOUND ON FRAME AT THE STA Y=1305 LT BETWEEN L=11 AND L=12. PERFORMED REPAIR IN ACCORDANCE WITH FEDEX EA N 1-5310-93785.Dec 16, 2005 · N575FE · Doug MD11 · Fuselage Main, Frame
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